{"title":"French Aviation Collection","description":"\u003ch2\u003eFrench Aviation Collection\u003c\/h2\u003e\u003cp\u003eFrance produced some of the most innovative and historically significant aircraft of the twentieth century — from the pioneering designs of the interwar period through the jet age triumphs of Dassault, the regional workhorses of Nord and Aérospatiale, and the enduring training aircraft of Morane-Saulnier and Socata. This collection assembles primary-source technical documentation from the full breadth of French aviation manufacturing — factory manuals, maintenance references, and engineering documents from the manufacturers who defined French aerospace identity.\u003c\/p\u003e\u003cp\u003eFrench aviation history is marked by discontinuity: the 1936 nationalisation, post-war reconstruction, successive mergers into Aérospatiale, and ultimately the formation of EADS and Airbus. Dassault alone survived as a fully independent French manufacturer. This archival collection preserves the documentation of manufacturers that no longer exist as independent entities — making these primary-source documents irreplaceable records of French aerospace heritage.\u003c\/p\u003e\u003ch3\u003eManufacturers Represented\u003c\/h3\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eDassault Aviation\u003c\/strong\u003e — Mirage III, Mirage F-1, Mirage 5, MD.450 Ouragan, MD-315 Flamant\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMorane-Saulnier\u003c\/strong\u003e — MS.760 Paris, MS.733 Alcyon\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSocata\u003c\/strong\u003e — Rallye Family\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eHispano-Suiza\u003c\/strong\u003e — 8 \u0026amp; 12 Series Aero Engines\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNord \/ SNCAN\u003c\/strong\u003e — Coming soon\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAérospatiale \/ Sud Aviation\u003c\/strong\u003e — Coming soon\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eBreguet\u003c\/strong\u003e — Coming soon\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDewoitine\u003c\/strong\u003e — Coming soon\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePotez\u003c\/strong\u003e — Coming soon\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAmiot · Farman · Liore et Olivier · SIPA · SNCASO\u003c\/strong\u003e — Coming soon\u003c\/li\u003e\n\u003c\/ul\u003e\u003cp\u003eThis is a living collection — new manufacturers and documents are added continuously as the archive expands.\u003c\/p\u003e\u003chr\u003e\u003cp\u003e\u003cem\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorised distributor.\u003c\/em\u003e\u003c\/p\u003e\u003cp\u003e\u003cstrong\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/strong\u003e\u003c\/p\u003e","products":[{"product_id":"aerospatiale-as-350-ecureuil-b-version-helicopter-bundle-manuals-to-download","title":"Aerospatiale AS 350 Écureuil Helicopter Manual Collection - Digital Download","description":"\u003ch2\u003eComprehensive AS 350 Écureuil Helicopter Manual Collection\u003c\/h2\u003e\u003cp\u003eThis comprehensive digital collection provides complete technical documentation for the Aerospatiale AS 350 Écureuil helicopter (B versions: B, B1, B2, B3, BA, BB, D, L1). Essential for aviation historians, researchers, restorers, and enthusiasts seeking authentic primary-source documentation from this legendary helicopter's operational history.\u003c\/p\u003e\u003ch3\u003eWhat's Included\u003c\/h3\u003e\u003cp\u003eThis bundle contains the complete technical library for AS 350 operations, maintenance, and repair:\u003c\/p\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eFlight Manuals\u003c\/strong\u003e - AS 350 B1, B2, B3, BA, D versions with DOT\/DGAC approvals\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMaintenance Manual\u003c\/strong\u003e - Complete maintenance procedures (Volumes 1-5)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eRepair Manual\u003c\/strong\u003e - Comprehensive repair procedures (Volumes 1-5)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDescription and Operation Manual\u003c\/strong\u003e - System descriptions and operational procedures\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eIllustrated Parts Catalog (Civil)\u003c\/strong\u003e - Complete parts identification and ordering information\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eWiring Diagrams Manual\u003c\/strong\u003e - Electrical system schematics\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTools Catalog\u003c\/strong\u003e - Specialized tools and equipment specifications\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFault Isolation Manual\u003c\/strong\u003e - Troubleshooting and diagnostic procedures\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eStorage Manual\u003c\/strong\u003e - Long-term storage and preservation procedures\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eIndex of Modifications\u003c\/strong\u003e - Complete modification tracking\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eService Bulletin\u003c\/strong\u003e - Technical service updates\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMaster Servicing Recommendations\u003c\/strong\u003e - Servicing schedules and procedures\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eStandard Practices Manual (All Helicopters)\u003c\/strong\u003e - General helicopter maintenance standards\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch3\u003eHistorical Note\u003c\/h3\u003e\u003cp\u003eThe Aerospatiale AS 350 Écureuil (Squirrel), known as the AStar in North America, represents one of the most successful light utility helicopter designs in aviation history. First flown in 1974, the AS 350 quickly established itself as a versatile workhorse for civilian and governmental operations worldwide.\u003c\/p\u003e\u003cp\u003eThroughout its distinguished service life, the AS 350 has proven invaluable in diverse roles including emergency medical services, law enforcement, news gathering, corporate transport, tourism, and utility operations. Its exceptional high-altitude performance made it legendary in mountainous regions, with AS 350s regularly operating in the Himalayas, Alps, and Andes. The helicopter achieved worldwide recognition when an AS 350 B3 landed on the summit of Mount Everest in 2005, setting an altitude record that demonstrated the aircraft's remarkable capabilities.\u003c\/p\u003e\u003cp\u003eThe B-series variants covered in this manual collection represent the evolution of the design through multiple powerplant and systems improvements. From the original AS 350 B with the Lycoming LTS101 engine to the later Turbomeca Arriel-powered versions (B1, B2, B3), each variant brought enhanced performance and reliability. The BA and BB models introduced specific improvements for different operational requirements, while the D variant featured the Turbomeca Arriel 1D engine. These helicopters saved countless lives in search and rescue operations, supported critical infrastructure projects, and enabled operations in environments where few other aircraft could venture.\u003c\/p\u003e\u003cp\u003eProduction of AS 350 variants exceeded 6,000 units, with the type serving operators in over 120 countries. The helicopter's reliability, maintainability, and versatility made it a favorite among commercial operators, and many examples continue flying today after decades of service. The AS 350's success led to the development of the twin-engine AS 355 Écureuil 2 and influenced subsequent Eurocopter (now Airbus Helicopters) designs.\u003c\/p\u003e\u003cp\u003eThese original technical manuals represent the authentic documentation used throughout the AS 350's operational life by pilots, maintenance technicians, and engineers. They provide comprehensive insight into the helicopter's systems, maintenance requirements, and operational procedures as specified by Aerospatiale and later Eurocopter. For historians studying rotorcraft development, restorers working on preserved examples, or enthusiasts seeking to understand this remarkable helicopter's technical details, these manuals offer invaluable primary-source material from the aircraft's active service period.\u003c\/p\u003e\u003ch3\u003eDisclaimer\u003c\/h3\u003e\u003cp\u003e\u003cstrong\u003eSold for historical and reference purposes only.\u003c\/strong\u003e These original or reproduced manuals and blueprints are transferred to electronic format from active-duty archives. Not intended for current certification or repair work. Ideal for scholars, collectors, modelers, and aviation enthusiasts.\u003c\/p\u003e\u003cp\u003eWe provide civil manuals and blueprints on obsolete aircraft, engines, and helicopters for proprietary reasons. Information is for reference only; completeness and accuracy are not guaranteed.\u003c\/p\u003e\u003cp\u003eAll trade names, trademarks, and manufacturer names are property of their respective owners. Reference to commercial products does not imply endorsement or affiliation.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":51307438834011,"sku":null,"price":300.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/as-350-astar-lb4-banner.png?v=1767722433"},{"product_id":"sud-aviation-aerospatiale-se-313-se-3130-sa-318-alouette-ii-sa-315-lama-helicopter-manuals-bundle-download","title":"Sud Aviation SNCASE SE-3130 \/ SA 313 \/ SA 318 Alouette II \u0026 SE-3131 Gouverneur Helicopter Manuals Collection - Download","description":"\u003ch3\u003eSud Aviation SNCASE SE-3130 \/ SA 313 \/ SA 318 Alouette II \u0026amp; SE-3131 Gouverneur Helicopter Manuals Collection\u003c\/h3\u003e\n\u003cp\u003eThis comprehensive digital collection brings together authentic technical documentation for the legendary Sud Aviation Alouette II helicopter family, including the SE-3130, SA 313, SA 318 variants, and the specialized SE-3131 Gouverneur executive transport version. These original manuals represent the actual documentation used by military and civilian operators worldwide throughout these aircraft's distinguished service history.\u003c\/p\u003e\n\u003ch3\u003eHistorical Note\u003c\/h3\u003e\n\u003cp\u003eThe Sud Aviation Alouette II holds a distinguished place in aviation history as one of the first truly successful turbine-powered helicopters. First flown in 1955, the Alouette II revolutionized rotary-wing aviation by demonstrating the reliability and efficiency of turboshaft engines in helicopter applications. Its compact Turbomeca Artouste engine gave it exceptional performance, including the ability to operate at high altitudes where piston-engine helicopters struggled.\u003c\/p\u003e\n\u003cp\u003eDuring its production run from 1956 to 1975, over 1,300 Alouette II helicopters were manufactured in various configurations. The SE-3130 represented the initial production variant built by SNCASE (Société Nationale de Constructions Aéronautiques du Sud-Est), which later became Sud Aviation. The SA 313 and SA 318 designations reflected later production standards and improvements, incorporating lessons learned from operational experience and featuring enhanced systems and capabilities.\u003c\/p\u003e\n\u003cp\u003eThe helicopter saw extensive military service with armed forces across Europe, Africa, Asia, and South America, performing roles ranging from observation and liaison to medical evacuation and light attack. The French military deployed Alouettes extensively during operations in Algeria and other theaters, where the helicopter's reliability and hot-and-high performance proved invaluable. The Alouette II became the backbone of many nations' light helicopter fleets, serving with distinction in the armies and air forces of over 40 countries.\u003c\/p\u003e\n\u003cp\u003eThe civilian market embraced the Alouette II with equal enthusiasm. Its versatility made it ideal for emergency medical services, mountain rescue operations, agricultural work, and executive transport. In the Swiss Alps and Himalayas, Alouette IIs became synonymous with high-altitude rescue missions, saving countless lives in terrain inaccessible to other aircraft of the era.\u003c\/p\u003e\n\u003cp\u003eThe SE-3131 Gouverneur represented a specialized executive transport variant, offering enhanced comfort, soundproofing, and luxury appointments for VIP operations while retaining the Alouette's legendary reliability and performance. The Gouverneur featured upgraded interior finishes, improved climate control, and executive seating configurations that made it a popular choice for corporate and government transport throughout the 1960s and 1970s.\u003c\/p\u003e\n\u003cp\u003eToday, Alouette II helicopters remain in service worldwide, testament to their robust design and enduring utility. These aircraft are highly valued by collectors, warbird enthusiasts, and operators who appreciate their historical significance and proven capabilities. For restorers working to preserve these important aircraft, for historians documenting rotary-wing aviation development, and for enthusiasts studying the evolution of turbine helicopter technology, these original technical manuals represent authentic primary-source documentation that captures the engineering excellence and operational procedures that made these helicopters legendary.\u003c\/p\u003e\n\u003ch3\u003eManuals Included in This Collection\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eSE-3130 Alouette II Flight Manual\u003c\/strong\u003e - Comprehensive operational procedures, performance data, and flight characteristics for the SNCASE production variant\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSA 313 \/ SA 318 Alouette II Flight Manual\u003c\/strong\u003e - Updated operational documentation for later Sud Aviation production variants with enhanced systems\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSE-3131 Gouverneur Flight Manual\u003c\/strong\u003e - Operational documentation specific to the executive transport variant including VIP configuration procedures\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAlouette II Maintenance Manual\u003c\/strong\u003e - Detailed maintenance procedures, inspection schedules, and technical specifications covering all variants\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eComponent Overhaul Manuals\u003c\/strong\u003e - Detailed overhaul procedures for major components including transmission, rotor systems, and flight controls\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eIllustrated Parts Catalogs\u003c\/strong\u003e - Comprehensive parts identification and ordering information for SE-3130, SA 313, SA 318, and SE-3131 variants\u003cstrong\u003e\u003c\/strong\u003e\n\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eProduct Details\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eFormat:\u003c\/strong\u003e Digital download (PDF)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eLanguage:\u003c\/strong\u003e Primarily English and French (as originally published)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCoverage:\u003c\/strong\u003e SE-3130, SA 313, SA 318 Alouette II variants; SE-3131 Gouverneur\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eContent:\u003c\/strong\u003e Flight operations, maintenance procedures, technical specifications, parts catalogs, wiring diagrams, service bulletins\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDelivery:\u003c\/strong\u003e Immediate download upon purchase\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eDisclaimer\u003c\/h3\u003e\n\u003cp\u003e\u003cstrong\u003eImportant Notice:\u003c\/strong\u003e This documentation is provided for historical, educational, and reference purposes only. These manuals are NOT approved for use in the maintenance, operation, or certification of aircraft. Anyone working on actual aircraft must use only current, manufacturer-approved documentation and comply with all applicable aviation regulations and airworthiness directives. Online Aviation Library makes no warranties regarding the accuracy, completeness, or currentness of this historical documentation. Users assume all responsibility for verifying information against current official sources.\u003c\/p\u003e\n\u003cp\u003eThis collection is intended for historians, researchers, aviation enthusiasts, collectors, and those interested in the technical development of rotary-wing aircraft. It is not intended as a substitute for current maintenance or operational manuals required for airworthiness compliance.\u003c\/p\u003e\n\u003ch3\u003eCopyright \u0026amp; Licensing\u003c\/h3\u003e\n\u003cp\u003eThe documentation in this collection represents historical technical materials for aircraft manufactured by companies no longer producing these specific models under their original corporate structures. Online Aviation Library holds collective copyright for this historical documentation under bilateral licensing agreements that permit the sale and distribution of common technical information for legacy aircraft, engines, and components no longer in active production.\u003c\/p\u003e\n\u003cp\u003eCertain copyrights owned by Online Aviation Library are registered with the Canadian Intellectual Property Office under the company name \"Sicuro Publishing\" and are publicly searchable in the Canadian Copyright Database (https:\/\/www.ic.gc.ca\/app\/opic-cipo\/cpyrghts\/dsplySrch.do?lang=eng). This registration demonstrates our legal ownership and commitment to preserving and legitimately distributing historical aviation documentation.\u003c\/p\u003e\n\u003cp\u003eFor manufacturers still in business, bilateral agreements are in place allowing the sale of common technical information for outdated aircraft models and variants no longer in production. All documentation is distributed in accordance with applicable copyright laws and licensing agreements.\u003c\/p\u003e\n\u003cp\u003e \u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":51307567579483,"sku":null,"price":55.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/alouette-ii-lb4-banner-1.png?v=1767815192"},{"product_id":"aerospatiale-sud-aviation-westland-gazelle-helicopter-manuals-bundle-download","title":"Aérospatiale \/ Westland Gazelle (SA 341\/342) — Maintenance \u0026 Flight Manuals · Digital Download","description":"\u003cp\u003eThe Westland Gazelle represents a distinguished chapter in British military aviation history. Originally developed through Anglo-French collaboration in the late 1960s, the Gazelle entered Royal Air Force service in 1973 as a versatile light helicopter for training, reconnaissance, and liaison roles. The aircraft's exceptional agility, excellent visibility, and reliable turbine engine made it a favorite among military pilots for over four decades.\u003c\/p\u003e\u003cp\u003eThroughout its service life, the Gazelle proved invaluable across multiple variants: the AH Mk.1 for the Army Air Corps in attack and reconnaissance roles, the HT Mk.2 and HT Mk.3 for RAF pilot training, and specialized configurations for the Royal Navy. The helicopter saw active deployment in numerous operations worldwide, earning a reputation for dependability and performance in demanding conditions.\u003c\/p\u003e\u003ch3\u003eThis Comprehensive Collection Includes:\u003c\/h3\u003e\u003ch4\u003ePrimary Manuals:\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003eA.P. 1001C-0901 to 0903-15-16 - Aircrew and Operating Data Manual (1974)\u003c\/li\u003e\n\u003cli\u003eA.P. 1001C-0901 to 0903-3-A - Illustrated Parts Catalog Manual (1984)\u003c\/li\u003e\n\u003cli\u003eA.P. 1001C-0900-5M - Flight Test Schedule Manual, All Marks (1990)\u003c\/li\u003e\n\u003cli\u003eA.P. 1001C-0900-5C - Basic Maintenance Schedule Manual (1990)\u003c\/li\u003e\n\u003cli\u003eA.P. 1001C-0901 thru 0903-5C - Basic Maintenance Schedule Manual (1998)\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch4\u003eAircraft Maintenance Manuals (AMM):\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003eAP101C-0901-1B1 - Basic Maintenance\u003c\/li\u003e\n\u003cli\u003eAP101C-0901-1B2 - Basic Maintenance\u003c\/li\u003e\n\u003cli\u003eAP101C-0901-1C1 - Basic Maintenance\u003c\/li\u003e\n\u003cli\u003eAP101C-0901-1C2 - Basic Maintenance\u003c\/li\u003e\n\u003cli\u003eAP101C-0901-1D1 - Basic Maintenance\u003c\/li\u003e\n\u003cli\u003eAP101C-0901-1D2 - Basic Maintenance\u003c\/li\u003e\n\u003cli\u003eAP101C-0901-1E1 - Basic Maintenance\u003c\/li\u003e\n\u003cli\u003eAP101C-0901-1E2 - Basic Maintenance\u003c\/li\u003e\n\u003cli\u003eAP101C-0901-1F1 - Basic Maintenance\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch4\u003eComponent Manuals - General and Technical Information:\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003eA.P. 105B-1420-136 - Powered Flying Control (Servo Jack)\u003c\/li\u003e\n\u003cli\u003eA.P. 106B-0229-16 - Flexible Tanks (Repair and Reconditioning Instructions)\u003c\/li\u003e\n\u003cli\u003eA.P. 106H-0223-13A - Oil Cooler Engine and Main Gearbox Marston (Illustrated Parts Catalog)\u003c\/li\u003e\n\u003cli\u003eA.P. 107B-1069-13A6 - Cut-Off Valve ABG. SEMCA S.A. (Parts Catalog, Overhaul Instructions)\u003c\/li\u003e\n\u003cli\u003eA.P. 108B-0409-1(R) - Aircrew Equipment Assemblies: Static Seats and Emergency Equipment\u003c\/li\u003e\n\u003cli\u003eA.P. 112G-0610-1 - Engine Oil Temperature Indicator, Brion Lerou\u003c\/li\u003e\n\u003cli\u003eA.P. 112G-0638-1 - Outside Air Temperature Thermometer, Galtier Type\u003c\/li\u003e\n\u003cli\u003eA.P. 112G-0934-1 - Pitot Head, Type 500 Badin\u003c\/li\u003e\n\u003cli\u003eA.P. 112G-1175-1 - Pressure Switch, Jaeger\u003c\/li\u003e\n\u003cli\u003eA.P. 112G-1182-1 - Pressure Switch Low Pressure Type 35111-2 and 35111-3\u003c\/li\u003e\n\u003cli\u003eA.P. 113D-0328-136 - Static Inverter Sfena TSG 420-203 (Parts Catalogue, Overhaul Instructions)\u003c\/li\u003e\n\u003cli\u003eA.P. 113D-07128-13A6 - Voltage Regulator Lucas Aerospace (Parts Catalogue, Repair and Reconditioning Instructions)\u003c\/li\u003e\n\u003cli\u003eA.P. 113D-07199-13A6 - Voltage Regulator and Overvoltage Protection Unit Lucas Aerospace (Parts Catalogue, Repair and Reconditioning Instructions)\u003c\/li\u003e\n\u003cli\u003eA.P. 113E-0495-13A6 - Fuel Pump Intertechnique Part No. 2180F (Parts Catalogue, Overhaul Instructions)\u003c\/li\u003e\n\u003cli\u003eA.P. 113F-0280-13 - Anticollision Lamp Vibration Absorber (Parts Catalogue and Related Information)\u003c\/li\u003e\n\u003c\/ul\u003e\u003cp\u003eThese comprehensive technical manuals—spanning from 1974 through 1998—represent the authentic documentation used throughout the Gazelle's distinguished service career. Prepared by GKN Westland Helicopters Limited and authorized by the Ministry of Defence, these publications were used across the Royal Air Force, Royal Navy, and Army Service for maintenance, operations, and component overhaul procedures.\u003c\/p\u003e\u003cp\u003eFor aviation historians, restorers, researchers, and enthusiasts, this collection offers invaluable primary-source material documenting British military helicopter operations, maintenance procedures, technical specifications, and component-level documentation from an era of significant aviation development.\u003c\/p\u003e\u003chr\u003e\u003ch3\u003eDisclaimer:\u003c\/h3\u003e\u003cp\u003eThis item is sold for historical and reference purposes only. These are either original or copies of manuals and blueprints used when these aircraft were in active duty, now transferred into electronic format.\u003c\/p\u003e\u003cp\u003e\u003cstrong\u003eImportant Notice:\u003c\/strong\u003e These manuals and blueprints are not meant to be used for current update material for certification, maintenance, or repair purposes, but make an excellent reference for scholars, collectors, modelers, and aviation enthusiasts.\u003c\/p\u003e\u003cp\u003eFor proprietary reasons, we generally only provide civil manuals and blueprints on obsolete aircraft, engines, and helicopters. The information is for reference only, and we do not guarantee the completeness, accuracy, or currency of any manuals.\u003c\/p\u003e\u003cp\u003eReference herein to any specific commercial products by trade name, trademark, manufacturer, or otherwise is not meant to imply or suggest any endorsement by, or affiliation with, that manufacturer or supplier. All trade names, trademarks, and manufacturer names are the property of their respective owners.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":51307843584347,"sku":null,"price":180.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/gazelle-military-banner.png?v=1767705899"},{"product_id":"dassault-mirage-iii-aircraft-aeroplane-manuals-bundle-download","title":"Dassault Mirage III Manuals Collection - Delta-Wing Fighter - Comprehensive Digital Archive","description":"\u003ch3\u003eDassault Mirage III Manuals Collection - Comprehensive Digital Archive\u003c\/h3\u003e\n\u003cp\u003eThis extensive collection brings together the most comprehensive archive of Dassault Mirage III technical documentation available, spanning multiple variants and air forces. From the legendary delta-wing interceptor that defined Cold War air superiority to its evolution into multi-role combat aircraft, these authentic manuals represent the complete operational and technical knowledge base used by pilots, maintainers, and engineers across three continents.\u003c\/p\u003e\n\u003ch3\u003eHistorical Note\u003c\/h3\u003e\n\u003cp\u003eThe Dassault Mirage III stands as one of the most successful and influential combat aircraft of the jet age. First flown in 1956, this revolutionary delta-wing fighter became the first Western European aircraft to exceed Mach 2 in level flight, establishing France as a major force in military aviation design. The Mirage III's distinctive tailless delta configuration, combined with its powerful ATAR turbojet engine with afterburner, created an aircraft of exceptional performance and elegant simplicity.\u003c\/p\u003e\n\u003cp\u003eDuring its operational career spanning over five decades, the Mirage III served with distinction in air forces around the world, including France, Australia, Switzerland, South Africa, Argentina, and numerous other nations. The aircraft proved its combat effectiveness in multiple conflicts, most notably during the Six-Day War of 1967 where Israeli Mirage IIIs achieved air superiority, and in the hands of the Royal Australian Air Force (RAAF) where it served as the primary air defense fighter from 1964 to 1988.\u003c\/p\u003e\n\u003cp\u003eThe Mirage III family evolved into numerous variants: the single-seat interceptor Mirage IIIE, the two-seat trainer Mirage IIIB, the reconnaissance Mirage IIIR and IIIRD, the simplified export Mirage IIIO, and the advanced Mirage IIIEE. Each variant adapted the basic design to specific operational requirements while maintaining the aircraft's legendary performance characteristics. Over 1,400 Mirage III aircraft were produced between 1958 and 1990, making it one of the most widely exported fighter aircraft in history.\u003c\/p\u003e\n\u003cp\u003eThese original technical manuals represent authentic documentation used throughout the Mirage III's distinguished service life. Spanning French, English, and Spanish language editions, they reflect the aircraft's truly international operational footprint. The collection includes flight manuals from the Armée de l'Air (French Air Force), RAAF technical publications, and Fuerza Aérea Argentina (Argentine Air Force) operational handbooks, providing unique insights into how different air forces adapted and operated this remarkable aircraft.\u003c\/p\u003e\n\u003cp\u003eFor aviation historians, restorers, researchers, scale modelers, and enthusiasts, this collection offers unparalleled access to the technical heritage of one of aviation's most iconic designs. These manuals document not just an aircraft, but an era when European aviation engineering challenged and often surpassed its American and Soviet counterparts, establishing design principles that influenced fighter development for generations to come.\u003c\/p\u003e\n\u003ch3\u003eWhat's Included: List of Manuals in this Offer\u003c\/h3\u003e\n\u003cp\u003e\u003cstrong\u003eFrench Air Force Mirage III E Manuals:\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eDassault Mirage III E Aircraft Flight Manual - Text UCB103-01-1 - 1965 (French Language)\u003c\/li\u003e\n\u003cli\u003eDassault Mirage III E Aircraft Flight Manual - Planches UCB103-01-2 - 1965 (French Language)\u003c\/li\u003e\n\u003cli\u003eDassault Mirage III E Aircraft Flight Manual - Text (French Language)\u003c\/li\u003e\n\u003cli\u003eDassault Mirage III E Aircraft Flight Manual - Graphic (French Language)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eRAAF (Royal Australian Air Force) Mirage III Manuals:\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eDassault Mirage III D2Z Aircraft Flight Manual - Planches (Illustrations) - AMD-BA-No U-O-M3D2Z - 1973 (English Language)\u003c\/li\u003e\n\u003cli\u003eDassault Mirage III D2Z Aircraft Flight Manual - TEXT - AMD-BA-No U-O-M3D2Z - 1973 (English Language)\u003c\/li\u003e\n\u003cli\u003eDassault Mirage III O and D Aircraft Flight Manual - RAAF - AAP7213.00-1 (English Language)\u003c\/li\u003e\n\u003cli\u003eDassault Mirage III O D Aircraft Flight Manual - Performance Data - RAAF - AAP7213.00-1-1\u003c\/li\u003e\n\u003cli\u003eDassault Mirage III O D Aircraft Weapon Delivery Manual - RAAF - AAP 7213.003-34\u003c\/li\u003e\n\u003cli\u003eDassault RAAF Mirage Aircraft General and Technical Manual - Book 1 of 4 - AAP 7213.003-2-14B1\u003c\/li\u003e\n\u003cli\u003eDassault RAAF Mirage Aircraft General and Technical Manual - Book 2 of 4 - AAP 7213.003-2-14B2\u003c\/li\u003e\n\u003cli\u003eDassault RAAF Mirage Aircraft General and Technical Manual - Book 3 of 4 - AAP 7213.003-2-14B3\u003c\/li\u003e\n\u003cli\u003eDassault RAAF Mirage Aircraft General and Technical Manual - Book 4 of 4 - AAP 7213.003-2-14B4\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eMirage III R\/RD Reconnaissance Variant Manuals:\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eDassault Mirage III RD Aircraft Manual Memento Pilote - Procedures Normales - MCG102-00 - 1972 (French Language)\u003c\/li\u003e\n\u003cli\u003eDassault Mirage III R Aircraft Manual Memento Pilote - Procedures Normales - MCG101-00 - 1968 (French Language)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eMirage III B Trainer Variant Manuals:\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eDassault Mirage III B Aircraft Manual Memento Pilote - Procedures Normales - MCE108-00 - 1969 (French Language)\u003c\/li\u003e\n\u003cli\u003eDassault Mirage III B Aircraft Operating Manual - Manuel Pilot - Text (French Language) - 1964\u003c\/li\u003e\n\u003cli\u003eDassault Mirage III B Aircraft Operating Manual - Manuel Pilot - Planches (French Language) - 1964\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eMirage III O-F Variant Manuals:\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eDassault Mirage III O-F Aircraft Flight Manual - Description and Operation Book 1 - TEXT\u003c\/li\u003e\n\u003cli\u003eDassault Mirage III O-F Aircraft Flight Manual - Description and Operation Book 1 - Plate\u003c\/li\u003e\n\u003cli\u003eDassault Mirage III O-F Aircraft Flight Manual - Weapon and Navigation System - Book 2 - Text\u003c\/li\u003e\n\u003cli\u003eDassault Mirage III O-F Aircraft Flight Manual - Weapon and Navigation System - Book 2 - Plate\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eArgentine Air Force Mirage III E\/EE Manuals (Spanish Language):\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eDassault Mirage III E Aircraft Procedimientos Normales Manual (Spanish Language)\u003c\/li\u003e\n\u003cli\u003eDassault Mirage III E Aircraft Procedimientos De Emergencia Manual (Spanish Language)\u003c\/li\u003e\n\u003cli\u003eDassault Mirage III E Aircraft Procedimientos Operativos Manual - Air to Air (Spanish Language)\u003c\/li\u003e\n\u003cli\u003eDassault Mirage III E Aircraft Procedimientos Operativos Manual - Air to Tierra (Spanish Language)\u003c\/li\u003e\n\u003cli\u003eDassault Mirage III E Aircraft Utilization Manual - Navigation and Weapon System - Graphics Tomo 1 (Spanish Language)\u003c\/li\u003e\n\u003cli\u003eDassault Mirage III E Aircraft Utilization Manual - Navigation and Weapon System - Text - Tomo 1 (Spanish Language)\u003c\/li\u003e\n\u003cli\u003eDassault Mirage III E Aircraft Utilization Manual - Navigation and Weapon System - Graphic - Tomo 2 (Spanish Language)\u003c\/li\u003e\n\u003cli\u003eDassault Mirage III E Aircraft Utilization Manual - Navigation and Weapon System - Text - Tomo 2 (Spanish Language)\u003c\/li\u003e\n\u003cli\u003eDassault Mirage III E Aircraft Manual De Utilizacion del Turborreactor ATAR 09 C5 C6 (Spanish Language)\u003c\/li\u003e\n\u003cli\u003eDassault Mirage III EE Aircraft Description Manual - Manual Del Piloto - Figuras Graphics (Spanish Language)\u003c\/li\u003e\n\u003cli\u003eDassault Mirage III EE Aircraft Description Manual - Manual Del Piloto - Texto Text (Spanish Language)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eTechnical Training Manual:\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eDassault Mirage III Aircraft Airframe Training Manual - A222998 Hunter JW (English Language)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eCollection Highlights\u003c\/h3\u003e\n\u003cp\u003eThis archive contains 35 individual manuals covering flight operations, emergency procedures, normal procedures, weapons systems, navigation systems, engine operations, airframe maintenance, performance data, and technical training across multiple Mirage III variants and air forces.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eCoverage includes:\u003c\/strong\u003e Complete flight manuals for E, B, R, RD, D2Z, O-F, and EE variants; ATAR 09 C5\/C6 turbojet engine documentation; weapons delivery and air-to-air\/air-to-ground operational procedures; navigation and interception systems; RAAF comprehensive technical manuals; multi-language editions reflecting international service.\u003c\/p\u003e\n\u003ch3\u003eDisclaimer\u003c\/h3\u003e\n\u003cp\u003eThis item is sold for historical and reference only. These are either original or copies of manuals and blueprints used when these aircraft were in active duty, now transferred into electronic format. These manuals and blueprints are not meant to be used for current update material for certification\/repair, but make an excellent reference for the scholar, collector, modeler or aircraft enthusiast. For proprietary reasons, we generally only provide civil manuals and blueprints on obsolete aircraft\/engines\/helicopters. The information is for reference only, and we do not guarantee the completeness, accuracy or currency of any manuals.\u003c\/p\u003e\n\u003cp\u003eReference herein to any specific commercial products by trade name, trademark, manufacturer, or otherwise, is not meant to imply or suggest any endorsement by, or affiliation with that manufacturer or supplier. All trade names, trademarks and manufacturer names are the property of their respective owners.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":51456625770843,"sku":null,"price":85.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/mirage-iii-lb4-banner-raaf.png?v=1769503421"},{"product_id":"dassault-mirage-f-1-aircraft-aeroplane-manuals-bundle-download","title":"Dassault Mirage F-1 Manuals Collection - Multi-Role Fighter - Comprehensive Digital Archive","description":"\u003ch3\u003eDassault Mirage F-1 Aircraft Manuals Collection - Comprehensive Digital Archive\u003c\/h3\u003e\n\u003cp\u003eThis extensive collection brings together the most comprehensive archive of Dassault Mirage F-1 technical documentation available, spanning multiple variants and air forces. From the swept-wing multi-role fighter that revolutionized tactical aviation to its evolution into specialized interceptor and ground attack variants, these authentic manuals represent the complete operational and technical knowledge base used by pilots, maintainers, and engineers across multiple continents.\u003c\/p\u003e\n\u003ch3\u003eHistorical Note\u003c\/h3\u003e\n\u003cp\u003eThe Dassault Mirage F-1 represents a bold departure from the delta-wing philosophy that defined the legendary Mirage III series. First flown in December 1966, the F-1 introduced a conventional swept-wing and tailplane configuration that delivered superior low-speed handling, shorter takeoff and landing distances, and enhanced maneuverability compared to its tailless delta predecessors. This design evolution made the F-1 one of the most versatile and successful multi-role fighters of its generation.\u003c\/p\u003e\n\u003cp\u003ePowered by the SNECMA Atar 9K-50 turbojet with afterburner, the Mirage F-1 achieved Mach 2.2 performance while offering exceptional range and payload capacity. The aircraft's advanced navigation and weapons systems, combined with its ability to operate from shorter runways, made it ideal for both air superiority and ground attack missions. The F-1's sophisticated avionics suite included terrain-following radar, inertial navigation, and comprehensive electronic warfare systems, establishing new standards for tactical fighter capabilities in the 1970s and 1980s.\u003c\/p\u003e\n\u003cp\u003eDuring its operational career spanning over four decades, the Mirage F-1 served with distinction in air forces around the world, including France, South Africa, Libya, Spain, Morocco, Iraq, Ecuador, and numerous other nations. The aircraft proved its combat effectiveness in multiple conflicts, including the Iran-Iraq War, the South African Border War, Operation Desert Storm, and various African conflicts. The South African Air Force (SAAF) operated both the F-1AZ ground attack variant and the F-1CZ interceptor variant with particular success, while the French Armée de l'Air deployed the F-1 extensively in overseas operations.\u003c\/p\u003e\n\u003cp\u003eThe Mirage F-1 family evolved into numerous specialized variants: the single-seat interceptor F-1C, the ground attack F-1A, the reconnaissance F-1CR, the two-seat trainer F-1B, and export variants including the F-1AZ, F-1CZ, F-1AD, F-1BD, F-1ED, and others tailored to specific customer requirements. Each variant adapted the basic airframe to specialized operational roles while maintaining the aircraft's legendary performance and reliability. Over 720 Mirage F-1 aircraft were produced between 1966 and 1992, making it one of the most successful Western fighter exports of the Cold War era.\u003c\/p\u003e\n\u003cp\u003eThese original technical manuals represent authentic documentation used throughout the Mirage F-1's distinguished service life. Spanning English and French language editions, they reflect the aircraft's truly international operational footprint. The collection includes flight manuals from the South African Air Force (SAAF) and Libyan Air Force, comprehensive maintenance documentation, weapons systems handbooks, and navigation system guides, providing unique insights into how different air forces adapted and operated this remarkable swept-wing fighter.\u003c\/p\u003e\n\u003cp\u003eFor aviation historians, restorers, researchers, scale modelers, and enthusiasts, this collection offers unparalleled access to the technical heritage of one of aviation's most successful multi-role fighters. These manuals document not just an aircraft, but the evolution of tactical fighter design from pure interceptors to true multi-role combat platforms, establishing design principles that influenced fighter development well into the 21st century.\u003c\/p\u003e\n\u003ch3\u003eWhat's Included: List of Manuals in this Offer\u003c\/h3\u003e\n\u003cp\u003e\u003cstrong\u003eSouth African Air Force (SAAF) Mirage F-1AZ Ground Attack Variant:\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eMirage F1AZ Aircraft Operating Manual – Volume One – Flight Manual (1F-F1K50AZ-1-1) - Contains Aircraft Description, Limitations, Normal and Emergency procedures and Flight Characteristics - Jan 1975, revised to June 1990 (with subsequent Atlas amendments) - Approx 370 pages (English Language)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eSouth African Air Force (SAAF) Mirage F-1CZ Interceptor Variant:\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eMirage F1CZ Aircraft Operating Manual – Volume One – Flight Manual (1F-F1K50CZ-1-1) - Contains Aircraft Description, Limitations, Normal and Emergency procedures, and Flight Characteristics - Jan 1975, revised to June 1990 (with subsequent Atlas amendments) - Approx 365 pages (English Language)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eLibyan Air Force Mirage F-1AD Ground Attack Variant (English Language):\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eMirage F1AD Aircraft Operating Manual – Flight Manual (1F-F1K50AD-1-1) - Contains Aircraft Description, Limitations, Normal and Emergency procedures, and Flight Characteristics - Jan 1978, revised to Change 9 June 1990 - Approx 314 pages (English Language)\u003c\/li\u003e\n\u003cli\u003eMirage F1AD – Flight Manual – Navigation and Weapon System (NWS) Operating Instructions (1F-F1K50AD-1-2) - Contains NWS Description, Normal and Operational procedures and Limitations - Jan 1978, revised to Change 6 dated June 1990 - Approx 224 pages (English Language)\u003c\/li\u003e\n\u003cli\u003eMirage F1AD – In-Flight Guide – Normal and Emergency Procedures (1F-F1K50AD-1-1CL) - Pilot's checklist - Jan 1978, revised to June 1990 - Approx 130 pages (English Language)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eLibyan Air Force Mirage F-1AD Ground Attack Variant (French Language):\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eMirage F1AD Aircraft Operating Manual – Flight Manual (1F-F1K50AD-1-1) - Jan 1978, revised to Change 9 June 1990 - Approx 307 pages (French Language, cover in English)\u003c\/li\u003e\n\u003cli\u003eMirage F1AD – Flight Manual – Navigation and Weapon System (NWS) Operating Instructions (1F-F1K50AD-1-2) - Jan 1978, revised to Change 6 dated June 1990 - Approx 217 pages (French Language, cover in English)\u003c\/li\u003e\n\u003cli\u003eMirage F1AD – In-Flight Guide – Normal and Emergency Procedures (1F-F1K50AD-1-1CL) - Pilot's checklist - Jan 1978, revised to June 1990 - Approx 130 pages (English Language)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eLibyan Air Force Mirage F-1BD Two-Seat Trainer Variant (English Language):\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eMirage F1BD Aircraft Operating Manual – Flight Manual (1F-F1K50BD-1-1) - Contains Aircraft Description, Limitations, Normal and Emergency procedures, and Flight Characteristics - Feb 1978, revised to Change 8 dated Feb 1986 - Approx 332 pages (English Language)\u003c\/li\u003e\n\u003cli\u003eMirage F1BD – Flight Manual – Navigation and Weapon System (NWS) Operating Instructions (1F-F1K50BD-1-2) - Contains NWS Description, Normal and Operational procedures and Limitations - Feb 1978, revised to Change 7 dated June 1990 - Approx 231 pages (English Language)\u003c\/li\u003e\n\u003cli\u003eMirage F1BD – In-Flight Guide – Normal and Emergency Procedures (1F-F1K50BD-1-1CL) - Pilot's checklist - Jan 1978, revised to June 1990 - Approx 129 pages (English Language)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eLibyan Air Force Mirage F-1BD Two-Seat Trainer Variant (French Language):\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eMirage F1BD Aircraft Operating Manual – Flight Manual (1F-F1K50BD-1-1) - Feb 1978, revised to Change 8 dated Feb 1986 - Approx 350 pages (French Language, cover in English)\u003c\/li\u003e\n\u003cli\u003eMirage F1BD – Flight Manual – Navigation and Weapon System (NWS) Operating Instructions (1F-F1K50BD-1-2) - Feb 1978, revised to Change 7 dated June 1990 - Approx 226 pages (French Language, cover in English)\u003c\/li\u003e\n\u003cli\u003eMirage F1BD – In-Flight Guide – Normal and Emergency Procedures (1F-F1K50BD-1-1CL) - Pilot's checklist - Jan 1978, revised to June 1990 - Approx 129 pages (English Language)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eLibyan Air Force Mirage F-1ED Multi-Role Fighter Variant (English Language):\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eMirage F1ED Aircraft Operating Manual – Flight Manual (1F-F1K50ED-1-1) - Contains Aircraft Description, Limitations, Normal and Emergency procedures, and Flight Characteristics - Jan 1978, revised to Change 9 dated June 1990 - Approx 306 pages (English Language)\u003c\/li\u003e\n\u003cli\u003eMirage F1ED – Flight Manual – Navigation and Weapon System (NWS) Operating Instructions (1F-F1K50ED-1-2) - Contains NWS Description, Normal and Operational procedures and Limitations - Jan 1978, revised to Change 7 dated June 1990 - Approx 239 pages (English Language)\u003c\/li\u003e\n\u003cli\u003eMirage F1ED – In-Flight Guide – Normal and Emergency Procedures (1F-F1K50ED-1-1CL) - Pilot's checklist - Dec 1977, revised to June 1990 - Approx 129 pages (English Language)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eLibyan Air Force Mirage F-1ED Multi-Role Fighter Variant (French Language):\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eMirage F1ED Aircraft Operating Manual – Flight Manual (1F-F1K50ED-1-1) - Jan 1978, revised to Change 9 dated June 1990 - Approx 299 pages (French Language, cover in English)\u003c\/li\u003e\n\u003cli\u003eMirage F1ED – Flight Manual – Navigation and Weapon System (NWS) Operating Instructions (1F-F1K50ED-1-2) - Jan 1978, revised to Change 7 dated June 1990 - Approx 234 pages (French Language, cover in English)\u003c\/li\u003e\n\u003cli\u003eMirage F1ED – In-Flight Guide – Normal and Emergency Procedures (1F-F1K50ED-1-1CL) - Pilot's checklist - Jan 1978, revised to June 1990 - Approx 129 pages (English Language)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eMirage F-1AD Maintenance Manual (English Language) - Two Volumes:\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eVolume 1:\u003c\/strong\u003e Contains Manual 01 through Manual 09 (1F-F1K50AD-2-1 through 1F-F1K50AD-2-9) - May 1990 - Approx 3,641 pages (English Language)\n\u003cul\u003e\n\u003cli\u003eManual 01 – General\u003c\/li\u003e\n\u003cli\u003eManual 02 – Servicing Instructions\u003c\/li\u003e\n\u003cli\u003eManual 03 – Structure and Airframe\u003c\/li\u003e\n\u003cli\u003eManual 04 – Flight Controls\u003c\/li\u003e\n\u003cli\u003eManual 05 – Take-off and Landing System\u003c\/li\u003e\n\u003cli\u003eManual 06 – Powerplant\u003c\/li\u003e\n\u003cli\u003eManual 07 – Hydraulic System\u003c\/li\u003e\n\u003cli\u003eManual 08 – Electrical System\u003c\/li\u003e\n\u003cli\u003eManual 09 – Conditioning Installation\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eVolume 2:\u003c\/strong\u003e Contains Manual 10 through Manual 17 (1F-F1K50AD-2-10 through 1F-F1K50AD-2-17) - May 1990 - Approx 1,881 pages (English Language)\n\u003cul\u003e\n\u003cli\u003eManual 10 – NWS General\u003c\/li\u003e\n\u003cli\u003eManual 11 – NWS Radio and Communication System\u003c\/li\u003e\n\u003cli\u003eManual 12 – NWS Control and Navigation\u003c\/li\u003e\n\u003cli\u003eManual 13 – NWS Flight Control Electronics and AP\u003c\/li\u003e\n\u003cli\u003eManual 14 – NWS Operational Systems\u003c\/li\u003e\n\u003cli\u003eManual 15 – NWS Armament\u003c\/li\u003e\n\u003cli\u003eManual 16 – Wiring\u003c\/li\u003e\n\u003cli\u003eManual 17 – Data Recording\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eMirage F-1AD Maintenance Manual (French Language) - Two Volumes:\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eVolume 1:\u003c\/strong\u003e Contains Manual 01 through Manual 09 (1F-F1K50AD-2-1 through 1F-F1K50AD-2-9) - May 1990 - Approx 3,355 pages (French Language, covers in English)\n\u003cul\u003e\n\u003cli\u003eManual 01 – Generalites\u003c\/li\u003e\n\u003cli\u003eManual 02 – Instructions de Piste\u003c\/li\u003e\n\u003cli\u003eManual 03 – Structure et Cellule\u003c\/li\u003e\n\u003cli\u003eManual 04 – Commandes de Vol\u003c\/li\u003e\n\u003cli\u003eManual 05 – Dispositif d'Atterrisage et de Decollage\u003c\/li\u003e\n\u003cli\u003eManual 06 – Installation Propulsive\u003c\/li\u003e\n\u003cli\u003eManual 07 – Installation Hydraulique\u003c\/li\u003e\n\u003cli\u003eManual 08 – Installation Electrique\u003c\/li\u003e\n\u003cli\u003eManual 09 – Installations d'Habitabilite\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eVolume 2:\u003c\/strong\u003e Contains Manual 10 through Manual 17 (1F-F1K50AD-2-10 through 1F-F1K50AD-2-17) - May 1990 - Approx 1,881 pages (French Language, covers in English)\n\u003cul\u003e\n\u003cli\u003eManual 10 – SNA Generalites\u003c\/li\u003e\n\u003cli\u003eManual 11 – SNA Installations Radio Telephonique\u003c\/li\u003e\n\u003cli\u003eManual 12 – SNA Conduite et Navigation\u003c\/li\u003e\n\u003cli\u003eManual 13 – SNA Electronique Cdes de Vol et A.P.\u003c\/li\u003e\n\u003cli\u003eManual 14 – SNA Installations Operationelles\u003c\/li\u003e\n\u003cli\u003eManual 15 – SNA Armament\u003c\/li\u003e\n\u003cli\u003eManual 16 – Cablages\u003c\/li\u003e\n\u003cli\u003eManual 17 – Enregistrement des Parametres\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eCollection Highlights\u003c\/h3\u003e\n\u003cp\u003eThis archive contains over 30 individual manuals covering multiple Mirage F-1 variants (F-1AZ, F-1CZ, F-1AD, F-1BD, F-1ED) across South African and Libyan Air Force operations, with comprehensive flight operations, emergency procedures, navigation and weapons systems, and complete maintenance documentation in both English and French.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eCoverage includes:\u003c\/strong\u003e Complete flight manuals for ground attack, interceptor, trainer, and multi-role variants; comprehensive two-volume maintenance manuals covering all aircraft systems; navigation and weapons system operating instructions; in-flight guides and pilot checklists; SNECMA Atar 9K-50 powerplant documentation; avionics and electronic warfare systems; bilingual editions reflecting international service.\u003c\/p\u003e\n\u003ch3\u003eDisclaimer\u003c\/h3\u003e\n\u003cp\u003eThis item is sold for historical and reference only. These are either original or copies of manuals and blueprints used when these aircraft were in active duty, now transferred into electronic format. These manuals and blueprints are not meant to be used for current update material for certification\/repair, but make an excellent reference for the scholar, collector, modeler or aircraft enthusiast. For proprietary reasons, we generally only provide civil manuals and blueprints on obsolete aircraft\/engines\/helicopters. The information is for reference only, and we do not guarantee the completeness, accuracy or currency of any manuals.\u003c\/p\u003e\n\u003cp\u003eReference herein to any specific commercial products by trade name, trademark, manufacturer, or otherwise, is not meant to imply or suggest any endorsement by, or affiliation with that manufacturer or supplier. All trade names, trademarks and manufacturer names are the property of their respective owners.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":51457432846683,"sku":null,"price":85.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/mirage-f1-lb4-banner-french.png?v=1769504128"},{"product_id":"sud-aviation-sncase-sa-316-319-sa-3160-aluette-iii-helicopter-manuals-collection-download","title":"Sud Aviation Alouette III (SA 316 \/ SA 319 \/ SE 3160) — Maintenance \u0026 Flight Manuals · Digital Download","description":"\u003ch3\u003eSud Aviation Alouette III Helicopter - Comprehensive Technical Manuals Collection\u003c\/h3\u003e\n\u003cp\u003eThis comprehensive digital collection contains authentic technical documentation for the legendary Sud Aviation Alouette III helicopter series, including the SE 3160, SA 316B, SA 316C, and SA 319B variants. These original manuals represent the complete technical library used by military and civilian operators worldwide throughout the aircraft's distinguished service history.\u003c\/p\u003e\n\u003ch3\u003eHistorical Note \u003c\/h3\u003e\n\u003cp\u003eThe Alouette III stands as one of the most successful and versatile helicopters in aviation history. First flown in 1959 as a development of the earlier Alouette II, this remarkable aircraft became the first production helicopter to feature a gas turbine engine (Turbomeca Artouste), revolutionizing rotorcraft performance and reliability. Manufactured by Sud Aviation (later Aérospatiale), the Alouette III quickly proved its exceptional capabilities across an extraordinary range of missions.\u003c\/p\u003e\n\u003cp\u003eDuring its production run from 1961 to 1985, over 2,000 Alouette III helicopters were built, serving with military forces and civilian operators in more than 70 countries across six continents. The aircraft distinguished itself in countless roles: military transport and reconnaissance, search and rescue operations, medical evacuation, mountain rescue in the Alps and Himalayas, offshore oil platform support, police and law enforcement duties, and VIP transport. Its legendary high-altitude performance was demonstrated when an Alouette III became the first helicopter to land on Mount Everest in 1972.\u003c\/p\u003e\n\u003cp\u003eThe Alouette III's versatility stemmed from its robust design, powerful turbine engine, and ability to operate in extreme conditions—from Arctic cold to desert heat, from sea level to altitudes exceeding 20,000 feet. Military operators valued its reliability in combat zones throughout Africa, Southeast Asia, and the Middle East, while civilian operators appreciated its economical operation and exceptional safety record. The aircraft saved countless lives in mountain rescue operations and medical evacuations, earning a reputation as a dependable workhorse that could be counted on when lives were at stake.\u003c\/p\u003e\n\u003cp\u003eToday, the Alouette III remains in active service with numerous operators worldwide, a testament to its enduring design and reliability. These original technical manuals represent the authentic documentation used throughout the aircraft's service life by mechanics, pilots, and engineers who maintained and operated this distinguished helicopter. For restorers working to preserve these historic aircraft, historians documenting aviation heritage, and enthusiasts studying one of rotorcraft's most successful designs, this collection provides invaluable primary-source technical information.\u003c\/p\u003e\n\u003ch3\u003eManuals Included in This Collection\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eSE 3100 Alouette III Structural Repair Manual\u003c\/strong\u003e - Comprehensive structural repair procedures and techniques\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSE 3160 Alouette III Structural Repair Manual (Issue 1: December 31, 1962)\u003c\/strong\u003e - Original issue structural repair documentation\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSA 316C - SA 319 Alouette Illustrated Parts Catalog (Edition N° 1 - 03.1972, Revision N° 5 - 01.1982)\u003c\/strong\u003e - Complete illustrated parts breakdown with part numbers and assembly diagrams\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSA 316B Alouette III Technical Manual Tome 1 (French)\u003c\/strong\u003e - Volume 1 technical manual in French language\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSA 319B Alouette III Technical Manual Tome 1 (French)\u003c\/strong\u003e - Volume 1 technical manual for SA 319B variant in French\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSE 3160 and SA 316B Alouette III Flight Manual (Issue 3a)\u003c\/strong\u003e - Approved flight manual with operating procedures and limitations\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSA 316B Alouette III Flight Manual (Revision 21, 1995)\u003c\/strong\u003e - Updated flight manual with latest revisions\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSA 316B Alouette III Instruction Manual\u003c\/strong\u003e - Operator instruction manual from Aerospatiale Product Support Service\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSA 316B Alouette III Type Specifications\u003c\/strong\u003e - Official type specifications and performance data\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAlouette 3 Promotional Specification Document (1966)\u003c\/strong\u003e - Vintage promotional and technical specification brochure\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eA.F.C.S. SFIM 85A Alouette III Autopilot Manual\u003c\/strong\u003e - Automatic Flight Control System documentation\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAlouette 3 Aerospatiale Helicopter Corporation Marketing Document\u003c\/strong\u003e - Technical marketing and performance standards documentation\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSFIM 146 Auto-Pilot for Navy Alouette III\u003c\/strong\u003e - Naval autopilot system technical manual\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSA 319 B Alouette 3 Technical Data (Données Techniques)\u003c\/strong\u003e - Complete technical data specifications\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eWhat You'll Receive\u003c\/h3\u003e\n\u003cp\u003eUpon purchase, you will receive immediate download access to high-resolution PDF files of all manuals in this collection. These digital reproductions preserve the original documentation in a convenient, searchable format that you can reference on any device. The manuals contain detailed technical diagrams, maintenance procedures, parts illustrations, performance data, operating limitations, and comprehensive system descriptions essential for understanding the Alouette III helicopter.\u003c\/p\u003e\n\u003ch3\u003eIdeal For\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003eAircraft restorers and maintainers working on Alouette III helicopters\u003c\/li\u003e\n\u003cli\u003eAviation historians researching rotorcraft development and operational history\u003c\/li\u003e\n\u003cli\u003eTechnical libraries and educational institutions\u003c\/li\u003e\n\u003cli\u003eCollectors of aviation technical documentation\u003c\/li\u003e\n\u003cli\u003eAerospace engineers studying helicopter design and systems\u003c\/li\u003e\n\u003cli\u003eMilitary history researchers documenting Cold War-era aviation\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eCopyright \u0026amp; Licensing Disclaimer\u003c\/h3\u003e\n\u003cp\u003e\u003cstrong\u003eLegal Ownership and Registration:\u003c\/strong\u003e All copyrights for Sud Aviation, Aérospatiale, and SNCASE documentation offered by Online Aviation Library are legally owned and registered. Certain registrations are publicly verifiable in the Canadian Copyright Database (https:\/\/www.ic.gc.ca\/app\/opic-cipo\/cpyrghts\/dsplySrch.do?lang=eng) under the company name \"Sicuro Publishing,\" demonstrating our legitimate ownership and right to distribute this historical documentation.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eLicensing Framework:\u003c\/strong\u003e For manufacturers no longer in business (such as Sud Aviation and SNCASE), Online Aviation Library owns collective copyright for their technical documentation. For manufacturers still in operation, bilateral licensing agreements are in place allowing the sale of common technical information for outdated aircraft models, engines, helicopters, and components no longer in production. This ensures legal compliance while preserving access to historically significant technical documentation.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eIntended Use:\u003c\/strong\u003e These manuals are provided for historical reference, research, education, and restoration purposes. They represent authentic period documentation and should be used in conjunction with current airworthiness directives and regulatory requirements for any aircraft maintenance or restoration work.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eDigital Download:\u003c\/strong\u003e This is a digital product. No physical items will be shipped. All files are delivered electronically via download link immediately after purchase.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":52002916893019,"sku":null,"price":50.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/sud-aviation-alouette-iii-lb4-banner-2.png?v=1767876620"},{"product_id":"aerospatiale-bac-concorde-aircraft-manuals-collection-download","title":"Aérospatiale-BAC Concorde Aircraft Technical Manuals Collection - 12 Manuals","description":"\u003cp\u003eThis structured digital collection provides comprehensive technical documentation for the Aérospatiale-BAC Concorde, the world's only successful supersonic passenger transport and one of the most technically ambitious aircraft ever built. With 12 manuals covering flight operations, maintenance, structural repair, systems, and the Olympus 593 powerplant, this is the definitive reference library for engineers, restorers, and researchers working with this extraordinary aircraft.\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003eDefinitive Collection with Free Lifetime Updates:\u003c\/strong\u003e This is a living collection that we continuously expand and refine. As we acquire additional Concorde documentation, technical bulletins, or variant-specific materials, we update this collection and provide free lifetime updates to all purchasers. Your one-time purchase guarantees access to all future additions and improvements to this collection.\u003c\/p\u003e\n\n\u003ch3\u003eTechnical Overview and Engineering Challenges\u003c\/h3\u003e\n\n\u003cp\u003eThe Aérospatiale-BAC Concorde represents the pinnacle of supersonic transport engineering, incorporating technologies and design solutions that pushed the boundaries of aeronautical science. Designed for sustained Mach 2+ cruise flight while carrying 100 passengers in comfort, the Concorde faced engineering challenges that required innovative solutions across every aspect of the aircraft's design, from aerodynamics and propulsion to structures and systems.\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003eThermal Expansion and Kinetic Heating:\u003c\/strong\u003e At Mach 2.04 cruise speed, aerodynamic friction heated the Concorde's aluminum alloy skin to temperatures reaching 127°C (260°F) at the nose and 90-100°C along the fuselage. This kinetic heating caused the entire airframe to expand significantly—the fuselage stretched approximately 6-10 inches (15-25 cm) during supersonic cruise. This thermal expansion created numerous engineering challenges: gaps appeared between structural components (a famous gap of about 1 inch opened between the flight engineer's panel and the bulkhead behind it during supersonic flight), fuel tanks had to accommodate dimensional changes without leaking, control cable tensions changed with temperature requiring careful rigging, and windows required special sealing systems to prevent leaks as frames expanded. The aircraft's aluminum alloy structure (primarily RR58 aluminum alloy) was selected for its strength retention at elevated temperatures, but the repeated thermal cycling from subsonic to supersonic flight and back created fatigue concerns that required comprehensive inspection programs throughout the aircraft's service life.\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003eFuel System as Thermal Management System:\u003c\/strong\u003e The Concorde's fuel system was far more than a simple storage and delivery system—it served as the primary heat sink for the aircraft's thermal management. The 13 fuel tanks (holding up to 26,400 gallons \/ 119,500 liters) were strategically located throughout the aircraft, with fuel actively pumped between tanks to serve multiple critical functions: absorbing heat from the air conditioning system (which had to cool the cabin while the outside skin reached 127°C), cooling hydraulic fluid that would otherwise overheat, managing the aircraft's center of gravity during the transonic acceleration and deceleration phases, and maintaining proper trim throughout the flight envelope. The fuel transfer system automatically moved fuel between forward and aft trim tanks to shift the center of gravity rearward as the aircraft accelerated through Mach 1, compensating for the rearward movement of the aerodynamic center of pressure. This system had to operate flawlessly—failure could result in uncontrollable pitch changes or inability to maintain supersonic cruise. The fuel itself heated significantly during flight, with temperatures in some tanks reaching 60°C, requiring careful fuel management to prevent vapor lock and maintain proper engine feed.\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003eOlympus 593 Engine and Intake System Complexity:\u003c\/strong\u003e The Rolls-Royce\/Snecma Olympus 593 Mk 610 turbojet with afterburner represented one of the most sophisticated propulsion systems ever developed for commercial aviation. Each engine produced 38,050 lbf of thrust with afterburner, but this performance came with extraordinary complexity. The variable geometry intake system was critical to engine operation—at supersonic speeds, the intake had to slow incoming air from Mach 2+ to subsonic speeds (around Mach 0.5) before it reached the engine compressor. This was accomplished through a complex system of movable ramps and auxiliary inlet doors that created a series of shock waves to decelerate and compress the air. The intake control system had to position these ramps precisely based on Mach number, altitude, and engine demand—incorrect ramp position could cause intake unstarts (sudden disruption of airflow) that produced violent yawing moments and required immediate pilot action. The engines consumed fuel at prodigious rates, particularly during takeoff and climb with afterburners engaged (approximately 5,600 gallons per hour for all four engines at takeoff power), limiting the aircraft's range and requiring careful fuel planning for every flight.\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003eDelta Wing Aerodynamics and Control Challenges:\u003c\/strong\u003e The Concorde's ogival delta wing (a modified delta with curved leading edges) provided the aerodynamic efficiency needed for supersonic cruise but created significant challenges for low-speed flight. Unlike conventional aircraft, the delta wing generated lift through vortex lift at high angles of attack—during approach and landing, the Concorde flew at angles of attack between 11-14 degrees, with powerful vortices forming over the upper wing surface. This vortex lift was essential for generating sufficient lift at landing speeds, but it made the aircraft's handling characteristics unusual and required specialized pilot training. The wing had no conventional flaps or leading-edge slats—all lift modulation came from angle of attack and speed control. The high approach angle of attack meant the fuselage blocked the pilot's forward view during landing, necessitating the famous drooping nose mechanism. This hydraulically-actuated nose could be lowered 5 degrees for takeoff visibility and 12.5 degrees for landing, with the visor retracting to provide an unobstructed view. The droop nose mechanism added weight and complexity but was essential for safe operations.\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003eStructural Design for Supersonic Flight:\u003c\/strong\u003e The Concorde's structure had to withstand loads and conditions far beyond those encountered by subsonic aircraft. The slender fuselage (maximum diameter only 9 feet 5 inches to minimize drag) required careful structural design to maintain cabin pressurization while handling the bending and torsional loads of flight. The pressure differential of 10.7 psi at cruise altitude (60,000 feet) combined with the thermal stresses from kinetic heating created complex stress distributions that varied throughout each flight. The structure incorporated multiple fail-safe features and redundant load paths to ensure safety even with fatigue cracks present. Fatigue crack growth was carefully monitored through comprehensive inspection programs, with critical areas inspected at regular intervals using advanced non-destructive testing techniques. The wing structure had to handle the unusual load distributions from vortex lift at low speeds and the different load patterns during supersonic cruise, requiring sophisticated structural analysis and testing during development.\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003eCenter of Gravity Management and Trim System:\u003c\/strong\u003e The Concorde's center of gravity (CG) management was critical to efficient supersonic flight. As the aircraft accelerated through the transonic region, the aerodynamic center of pressure moved rearward significantly. To maintain trim without excessive control surface deflection (which would create drag and reduce efficiency), the fuel transfer system automatically pumped fuel from forward tanks to aft trim tanks, shifting the CG rearward to match the rearward movement of the center of pressure. This fuel transfer typically moved about 20 tons of fuel aft during acceleration to Mach 2. During deceleration, the process reversed, moving fuel forward to maintain trim as the center of pressure moved forward. This system had to operate automatically and reliably—manual fuel transfer would have been impractical given the speed of the transonic transition and the precision required. The system included multiple redundancies and safeguards to prevent over-transfer that could make the aircraft uncontrollable.\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003eHydraulic and Flight Control Systems:\u003c\/strong\u003e The Concorde's flight control system used fully powered hydraulic controls with no manual reversion—the control forces at high speed made manual control impossible. Three independent hydraulic systems (Blue, Green, and Yellow) provided redundancy, with each system capable of operating essential flight controls. The hydraulic fluid operated at high temperatures due to heat absorption from the airframe and systems, requiring special high-temperature hydraulic fluid and careful thermal management. The flight control system incorporated artificial feel and stability augmentation to provide acceptable handling characteristics across the wide speed range from approach (around 160 knots) to supersonic cruise (Mach 2.04). The elevons (combined elevator and aileron surfaces on the delta wing trailing edge) provided pitch and roll control, while the rudder provided yaw control. The control system had to handle the dramatically different aerodynamic forces and moments across the flight envelope, from the vortex-dominated low-speed regime to the shock-wave-dominated supersonic regime.\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003eNoise and Environmental Challenges:\u003c\/strong\u003e The Concorde faced significant environmental challenges that ultimately contributed to its commercial limitations. Takeoff noise was extreme—the Olympus 593 engines with afterburners produced noise levels that exceeded regulations at many airports, restricting where the aircraft could operate. The sonic boom produced during supersonic flight (a double boom from the nose and tail shock waves) made overland supersonic flight politically and legally impossible in most countries, restricting the Concorde to oceanic routes where the boom would not disturb populated areas. This limitation severely restricted the aircraft's route network and commercial viability. Engine emissions were also problematic—the engines produced significant nitrogen oxides (NOx) at high altitude, raising environmental concerns about stratospheric ozone depletion. These environmental issues, combined with the aircraft's high fuel consumption and limited passenger capacity, made the Concorde economically marginal despite its technical brilliance.\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003eMaintenance and Inspection Complexity:\u003c\/strong\u003e Maintaining the Concorde required specialized knowledge, tools, and procedures far beyond those needed for subsonic aircraft. The thermal cycling inspection program monitored fatigue crack growth in critical areas subjected to repeated heating and cooling. The intake system required precise rigging and regular inspection to ensure proper operation. The fuel system's complexity demanded careful maintenance to prevent leaks and ensure proper operation of the transfer system. Hydraulic system maintenance had to account for the high operating temperatures and ensure proper fluid condition. The Olympus 593 engines required specialized maintenance procedures and had relatively short time between overhaul intervals compared to modern turbofan engines. As the fleet aged and aircraft were retired, maintaining parts availability and technical expertise became increasingly challenging, contributing to the decision to retire the fleet in 2003.\u003c\/p\u003e\n\n\u003ch3\u003eManuals Included in This Collection\u003c\/h3\u003e\n\n\u003cp\u003e\u003cstrong\u003eFlight Operations Documentation (3 manuals):\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eFlying Manual Volume I - Initial certification and fundamental operations\u003c\/li\u003e\n\u003cli\u003eFlying Manual Volume II(a) - Operating limitations, emergency procedures, abnormal procedures, conditional procedures, and minimum equipment list\u003c\/li\u003e\n\u003cli\u003eFlying Manual Volume II(b) - Normal procedures, checklists, procedures and techniques\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003cp\u003e\u003cstrong\u003eMaintenance and Structural Documentation (4 manuals):\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eMaintenance Manual - Procedures and specifications for aircraft maintenance\u003c\/li\u003e\n\u003cli\u003eStructural Repair Manual - Detailed repair procedures for structural elements and components\u003c\/li\u003e\n\u003cli\u003eNon Destructive Testing Manual - Testing procedures for Air France (Variant 101) and British Airways (Variant 102)\u003c\/li\u003e\n\u003cli\u003eIllustrated Parts Catalogue - Visual reference for aircraft components and parts identification\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003cp\u003e\u003cstrong\u003eSystems and Equipment Documentation (2 manuals):\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eWiring Diagram Manual - Electrical system schematics and diagrams\u003c\/li\u003e\n\u003cli\u003eWiring Diagram Manual (British Airways) - Variant-specific electrical documentation approved by Airbus UK and Airbus France\u003c\/li\u003e\n\u003cli\u003eIllustrated Tool and Equipment Manual - Specialized tools and equipment specifications\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003cp\u003e\u003cstrong\u003ePowerplant Documentation (3 manuals):\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003ePower Plant Build-Up Manual Type 593 MK 610 - Olympus 593 engine assembly and maintenance procedures\u003c\/li\u003e\n\u003cli\u003eBritish Airways Concorde Olympus 593 Maintenance - Heavy maintenance procedures\u003c\/li\u003e\n\u003cli\u003eBritish Airways Concorde Olympus 593 - Maintenance IPC, overhaul manual, and overhaul IPC\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003cp\u003eThis collection provides comprehensive technical coverage of the Concorde supersonic transport. The documentation spans flight operations across all phases of flight, maintenance procedures for airframe and systems, structural repair techniques for the thermally-stressed aluminum structure, non-destructive testing procedures for both Air France and British Airways variants, parts identification and cataloging, electrical system schematics, specialized tooling requirements, and complete Olympus 593 engine build-up, maintenance, and overhaul procedures. These manuals represent the actual documentation used by British Airways and Air France throughout the Concorde's operational service from 1976 to 2003.\u003c\/p\u003e\n\n\u003ch3\u003eEngineering Norms and Standards\u003c\/h3\u003e\n\n\u003cp\u003eThe Concorde was designed and manufactured to unprecedented aviation standards:\u003c\/p\u003e\n\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eAnglo-French Certification Standards:\u003c\/strong\u003e The Concorde was certified under both British Civil Airworthiness Requirements (BCAR) and French certification standards, requiring compliance with two separate regulatory frameworks. This dual certification process was complex and time-consuming but ensured the aircraft met the highest safety standards of both nations.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSupersonic Transport Design Standards:\u003c\/strong\u003e As the first supersonic transport, the Concorde required development of entirely new design standards for sustained supersonic flight, thermal management, structural design for kinetic heating, and systems operation in the supersonic environment. These standards influenced subsequent supersonic aircraft programs worldwide.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eBritish Aircraft Corporation and Aérospatiale Engineering Standards:\u003c\/strong\u003e Production followed the combined engineering standards of BAC and Aérospatiale, requiring coordination between British and French manufacturing facilities and integration of components from both nations. Quality control procedures had to satisfy both organizations' requirements.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eRolls-Royce\/Snecma Engine Standards:\u003c\/strong\u003e The Olympus 593 engine, developed jointly by Rolls-Royce and Snecma, followed rigorous standards for supersonic engine operation, afterburner performance, intake integration, and high-temperature operation. Maintenance procedures reflected the engine's complexity and the demanding operating environment.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFatigue Life and Inspection Standards:\u003c\/strong\u003e Given the severe thermal cycling and structural loads, the Concorde was subject to comprehensive fatigue life tracking and inspection programs. Standards governed inspection intervals, crack detection methods, and structural life extension programs that enabled safe operation throughout the aircraft's service life.\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003cp\u003eThese engineering standards represent the technical framework that enabled the Concorde to operate safely and reliably in the demanding supersonic environment for 27 years. For engineers, restorers, and researchers, understanding these standards provides essential insight into the design philosophy, structural requirements, and maintenance practices that made sustained Mach 2 passenger flight a reality.\u003c\/p\u003e\n\n\u003ch3\u003eFormat and Delivery\u003c\/h3\u003e\n\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eFormat:\u003c\/strong\u003e Digital download (PDF)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eLanguage:\u003c\/strong\u003e English (British Airways and Air France documentation)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTotal Manuals:\u003c\/strong\u003e 12 comprehensive documents\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eOperator Coverage:\u003c\/strong\u003e British Airways (Variant 102) and Air France (Variant 101)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eQuality:\u003c\/strong\u003e High-resolution scans of original operational documentation\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eOrganization:\u003c\/strong\u003e Structured folder hierarchy with flight operations, maintenance, systems, and powerplant documentation clearly separated\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDelivery:\u003c\/strong\u003e Instant digital download upon purchase\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eUpdates:\u003c\/strong\u003e Free lifetime updates as additional documentation is acquired and added to the collection\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003ch3\u003eCopyright \u0026amp; Licensing\u003c\/h3\u003e\n\n\u003cp\u003eThis digital compilation, structure, indexing and presentation are © Sicuro Publishing. All copyrights are registered with the Canadian Copyright Database.\u003c\/p\u003e\n\n\u003cp\u003eThis collection is licensed for research, education, historical preservation, and restoration purposes.\u003c\/p\u003e\n\n\u003ch3\u003eDisclaimer\u003c\/h3\u003e\n\n\u003cp\u003eThis item is sold for historical and reference only. These are either original or copies of manuals and blueprints used when these aircraft were in active duty, now transferred into electronic format. These manuals and blueprints are not meant to be used for current update material for certification\/repair, but make an excellent reference for the scholar, collector, modeller or aircraft buffs. For proprietary reasons, we generally only provide civil manuals and blueprints on obsolete aircraft\/engines\/helicopters. The information is for reference only, and we do not guarantee the completeness, accuracy or currency of any manuals.\u003c\/p\u003e\n\n\u003cp\u003eReference herein to any specific commercial products by trade name, trademark, manufacturer, or otherwise, is not meant to imply or suggest any endorsement by, or affiliation with that manufacturer or supplier. All trade names, trademarks and manufacturer names are the property of their respective owners.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":52074847175003,"sku":null,"price":50.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/concorde-lb4-banner-2-revised.png?v=1768822206"},{"product_id":"aerospatiale-sb-600-601-corvette-aircraft-manuals-collection-download","title":"Aérospatiale SN-600\/601 Corvette Business Jet Manuals - Comprehensive Technical Documentation Collection","description":"\u003ch3\u003eAérospatiale SN-600\/601 Corvette - Comprehensive Technical Documentation Collection\u003c\/h3\u003e\n\u003cp\u003eThis definitive digital archive contains authentic technical documentation for the \u003cstrong\u003eAérospatiale SN-600 and SN-601 Corvette\u003c\/strong\u003e, the elegant French business jet that represented the pinnacle of European corporate aviation during the 1970s. These original flight manuals, maintenance procedures, parts catalogs, wiring diagrams, structural repair documentation, and technical specifications covering both the SN-600 and improved SN-601 variants represent the actual documentation used by pilots, maintenance crews, engineers, and operators throughout the aircraft's distinguished operational service life.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eDefinitive Collection with Free Lifetime Updates:\u003c\/strong\u003e This is a living collection that we continuously expand and refine. As we acquire additional Aérospatiale Corvette documentation, technical bulletins, service information, or operational records, we update this collection and provide free lifetime updates to all purchasers. Your one-time purchase guarantees access to all future additions and improvements to this collection.\u003c\/p\u003e\n\u003ch3\u003eHistorical Note\u003c\/h3\u003e\n\u003cp\u003eThe \u003cstrong\u003eAérospatiale SN-600 Corvette\u003c\/strong\u003e represents a distinguished and elegant chapter in French business aviation history, embodying the sophistication and engineering excellence that characterized European aerospace development during the golden age of business jet innovation. Developed in the late 1960s by Sud Aviation (which merged with Nord Aviation and SEREB to form Aérospatiale in 1970), the Corvette was designed to fill a specific market gap between light twin-engine aircraft and larger corporate jets, offering European businesses an elegant, efficient, and distinctly French solution for executive transport.\u003c\/p\u003e\n\u003cp\u003eThe Corvette project began in 1967 when Sud Aviation identified a market opportunity for a medium-range business jet that could accommodate 6-14 passengers in exceptional comfort while offering performance and operating economics superior to turboprop aircraft. The design team, led by chief engineer Pierre Satre, created an aircraft that combined sleek aesthetics with practical functionality—a hallmark of French aerospace design philosophy.\u003c\/p\u003e\n\u003cp\u003eThe aircraft featured a distinctive and elegant design with a low-wing configuration, graceful fuselage lines, characteristic T-tail arrangement that became a signature of French business jets, and twin Pratt \u0026amp; Whitney JT15D-4 turbofan engines mounted at the rear fuselage in a clean, aerodynamically efficient installation. This rear-engine configuration provided several advantages including reduced cabin noise, improved passenger comfort, cleaner wing aerodynamics, and excellent short-field performance.\u003c\/p\u003e\n\u003cp\u003eThe Corvette first flew on July 16, 1970, from Toulouse-Blagnac Airport, piloted by Sud Aviation test pilot Jean Gonord. The flight test program validated the aircraft's excellent handling characteristics, impressive performance, and refined systems integration. French certification (Certificat de Navigabilité) was awarded by the Direction Générale de l'Aviation Civile (D.G.A.C.) in September 1972, followed by production deliveries beginning in late 1972.\u003c\/p\u003e\n\u003cp\u003eThe baseline SN-600 Corvette could accommodate 6-14 passengers in a pressurized cabin that set new standards for comfort in its class. The cabin featured executive seating configurations with club seating arrangements, refreshment centers, and lavatory facilities—amenities typically found only in larger corporate jets. Maximum cruising speed of approximately 760 km\/h (410 knots), range of 2,780 km (1,500 nautical miles) with maximum fuel, service ceiling of 12,500 meters (41,000 feet), and excellent short-field performance made it ideal for European business travel and short-haul international operations.\u003c\/p\u003e\n\u003cp\u003ePowered by two Pratt \u0026amp; Whitney Canada JT15D-4 turbofan engines, each producing 10.7 kN (2,400 lbf) of thrust, the Corvette offered excellent fuel efficiency and reliability. The JT15D engine family had proven itself in business aviation and provided operators with worldwide support infrastructure—a critical consideration for international operations.\u003c\/p\u003e\n\u003cp\u003eThe improved \u003cstrong\u003eSN-601 Corvette\u003c\/strong\u003e variant, introduced in the mid-1970s, incorporated refinements based on operational experience and customer feedback. Enhancements included upgraded avionics with more sophisticated navigation and communication systems, improved interior appointments and soundproofing, refined systems for enhanced reliability and maintainability, and aerodynamic improvements for better performance and fuel efficiency. The SN-601 became the standard production variant and represented the ultimate development of the Corvette design.\u003c\/p\u003e\n\u003cp\u003eThroughout its production run from 1972 to 1977, approximately 40 Corvettes were manufactured at Aérospatiale's Toulouse facility. While modest by commercial aviation standards, this production reflected the aircraft's position in the specialized business jet market and the economic challenges facing European aerospace during the 1970s oil crisis. Each aircraft was essentially custom-configured to meet individual customer requirements, with bespoke interior layouts, avionics packages, and equipment specifications.\u003c\/p\u003e\n\u003cp\u003eThe Corvette served a diverse range of operators across Europe, Africa, and the Middle East. Corporate clients included major European companies seeking efficient executive transport. Government agencies operated Corvettes for VIP transport, liaison duties, and administrative flights. Charter operators provided on-demand business aviation services. Air ambulance operators utilized the Corvette's pressurized cabin and range for medical evacuation missions. This operational diversity demonstrated the aircraft's remarkable versatility and adaptability to different mission profiles.\u003c\/p\u003e\n\u003cp\u003eOperators consistently praised the Corvette for its reliability, elegant handling characteristics, sophisticated engineering, passenger comfort exceeding expectations for its size class, and distinctly European refinement in design and execution. Pilots appreciated the aircraft's responsive controls, excellent visibility, and forgiving flight characteristics. Passengers enjoyed the quiet, comfortable cabin and smooth ride quality. Maintenance crews valued the aircraft's accessibility and well-thought-out systems design.\u003c\/p\u003e\n\u003cp\u003eThe Corvette competed in a challenging market dominated by American manufacturers like Cessna, Learjet, and Gulfstream. While it never achieved the commercial success of its American competitors, the Corvette earned respect within the aviation community for its engineering excellence and represented French aerospace industry's capability to compete in the sophisticated business jet market. The aircraft demonstrated that European manufacturers could produce world-class business aviation products combining performance, comfort, and operational efficiency.\u003c\/p\u003e\n\u003cp\u003eProduction ended in 1977 as Aérospatiale shifted focus to other programs including the successful Dauphin helicopter and collaborative projects like Airbus. The relatively small production run and specialized nature of the aircraft meant that Corvette operations gradually declined through the 1980s and 1990s as aircraft aged and parts support became more challenging. However, the aircraft's robust construction and quality engineering allowed many examples to remain in service well into the 2000s.\u003c\/p\u003e\n\u003cp\u003eToday, the Aérospatiale Corvette holds a special place among aviation enthusiasts and collectors as a symbol of French aerospace excellence during the golden age of business jet development. The aircraft represents an era when European manufacturers competed vigorously in the business aviation market, producing distinctive designs that offered alternatives to American dominance. Several Corvettes survive in private ownership and museums, preserved as elegant examples of 1970s French aerospace engineering.\u003c\/p\u003e\n\u003cp\u003eThese original technical manuals, maintenance procedures, parts catalogs, and engineering documentation represent authentic primary-source materials used throughout the Corvette's operational service life. They guided pilots through the complexities of operating a sophisticated business jet, provided maintenance crews with procedures for keeping these elegant aircraft airworthy, documented the aircraft's systems and performance characteristics, and recorded the technical evolution from SN-600 to SN-601 variants. For historians, aviation researchers, restorers, and enthusiasts, these documents offer unparalleled insight into the operation, maintenance, and technical details of this distinguished French business jet.\u003c\/p\u003e\n\u003ch3\u003eManuals Included in This Collection\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eAérospatiale SN 601 Corvette - Working Cards Manual - Cartes de Travail\u003c\/strong\u003e - 691 pages in French language (1979) - Comprehensive maintenance task cards and work procedures for scheduled and unscheduled maintenance operations\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAérospatiale SN 601 Corvette - Illustrated Parts Catalog Volume 1\u003c\/strong\u003e - 708 pages in English and French (1979) - Detailed parts identification, part numbers, illustrations, and ordering information essential for maintenance and restoration\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAérospatiale SN 601 Corvette - Airplane Technical Description Brochure\u003c\/strong\u003e - English language (1971) - Comprehensive technical overview with systems descriptions, specifications, and capabilities\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAérospatiale SN 600 Corvette - Airplane Technical Description Brochure\u003c\/strong\u003e - English language (1969) - Technical description for the baseline SN-600 variant documenting original specifications and design\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAérospatiale SN 601 Corvette - Airplane Operation Manual\u003c\/strong\u003e - English language (1980) - Complete operational procedures, normal and emergency operations, and crew guidance\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAérospatiale SN 601 Corvette - Airplane Flight Manual\u003c\/strong\u003e - English language (1974) - Official D.G.A.C.-approved flight manual with performance data, limitations, and operating procedures\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAérospatiale SN 601 Corvette - Maintenance Manual\u003c\/strong\u003e - English and French (1976, revised 1999) - Detailed maintenance protocols, inspection procedures, and service requirements with updates through 1999\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAérospatiale SN 601 Corvette - Wiring Diagram Manual\u003c\/strong\u003e - English and French (1974, revised 1984) - Complete electrical system schematics, circuit diagrams, and wiring documentation\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAérospatiale SN 601 Corvette - Structural Repair Manual\u003c\/strong\u003e - English and French (1975) - Comprehensive structural repair procedures, techniques, and specifications for airframe repairs\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAérospatiale SN 601 Corvette - Specification Manual\u003c\/strong\u003e - (1973) - Detailed aircraft specifications, performance data, and technical characteristics\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003eThis collection provides comprehensive technical coverage of the Aérospatiale Corvette, documenting both the SN-600 baseline variant and the improved SN-601 production standard. The manuals span from 1969 through 1999, capturing the aircraft's development, operational service, and long-term support. The bilingual documentation (English and French) reflects the aircraft's international operations and Aérospatiale's commitment to supporting global customers. The documentation includes detailed specifications for airframe structure, Pratt \u0026amp; Whitney JT15D powerplant operation, fuel and pressurization systems, flight controls, avionics and electrical systems, maintenance procedures, parts information, structural repair techniques, and operational guidance—essential reference material for understanding the complete technical scope of this distinguished French business jet.\u003c\/p\u003e\n\u003ch3\u003eEngineering Norms and Standards\u003c\/h3\u003e\n\u003cp\u003eThe Aérospatiale SN-600\/601 Corvette was designed and constructed in accordance with French civil aviation engineering standards and international airworthiness requirements of the late 1960s and 1970s. The aircraft was certificated by the Direction Générale de l'Aviation Civile (D.G.A.C.), France's civil aviation authority, which governed aircraft certification and operational standards.\u003c\/p\u003e\n\u003cp\u003eKey engineering standards and practices reflected in these manuals include:\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eFrench Civil Aviation Standards:\u003c\/strong\u003e D.G.A.C. certification requirements for transport category aircraft, including structural integrity, systems redundancy, and operational safety standards\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eInternational Airworthiness Standards:\u003c\/strong\u003e Compliance with international standards facilitating operations across European and international airspace\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAérospatiale Engineering Practices:\u003c\/strong\u003e Company-specific design standards, manufacturing procedures, quality control measures, and technical documentation formats developed by Aérospatiale—emphasizing sophisticated systems integration, passenger comfort, and operational reliability\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eBusiness Jet Design Standards:\u003c\/strong\u003e Specialized requirements for executive transport aircraft including pressurization systems, cabin comfort, noise reduction, and operational flexibility\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePratt \u0026amp; Whitney Powerplant Integration:\u003c\/strong\u003e Engine installation practices, fuel system design, and maintenance procedures for JT15D-4 turbofan engines following manufacturer specifications and certification requirements\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eBilingual Documentation Standards:\u003c\/strong\u003e Technical documentation provided in both French and English to support international operations and diverse operator base\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eLong-Term Support Standards:\u003c\/strong\u003e Maintenance manual revisions extending through 1999 demonstrate Aérospatiale's commitment to long-term product support even after production ended\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003eThese technical manuals reflect the engineering rigor and certification standards for business jet aircraft during the 1970s. The D.G.A.C. approval markings and official documentation formats indicate compliance with French and international airworthiness requirements. The manuals provide detailed specifications for materials, construction techniques, system installations, operational parameters, maintenance procedures, and repair techniques—offering valuable insight into French aerospace engineering practices and business jet design standards of the 1970s era.\u003c\/p\u003e\n\u003cp\u003eFor researchers, historians, restorers, and technical enthusiasts, these documents represent authentic primary sources for understanding the design philosophy, construction methods, operational standards, and maintenance practices that characterized French business jet development during this significant period in aviation history.\u003c\/p\u003e\n\u003ch3\u003eFormat and Delivery\u003c\/h3\u003e\n\u003cp\u003e\u003cstrong\u003eFormat:\u003c\/strong\u003e High-resolution PDF digital download\u003cbr\u003e\n\u003cstrong\u003eLanguages:\u003c\/strong\u003e English and French (bilingual documentation where applicable)\u003cbr\u003e\n\u003cstrong\u003eDelivery:\u003c\/strong\u003e Instant download link provided upon purchase\u003cbr\u003e\n\u003cstrong\u003eCompatibility:\u003c\/strong\u003e All devices and PDF readers\u003cbr\u003e\n\u003cstrong\u003eOrganization:\u003c\/strong\u003e Clearly labeled files organized by document type\u003c\/p\u003e\n\u003ch3\u003eDisclaimer\u003c\/h3\u003e\n\u003cp\u003eThis item is sold for historical and reference only. These are either original or copies of manuals and blueprints used when these aircraft were in active duty, now transferred into electronic format. These manuals and blueprints are not meant to be used for current update material for certification\/repair, but make an excellent reference for the scholar, collector, modeler or aircraft enthusiast. For proprietary reasons, we generally only provide civil manuals and blueprints on obsolete aircraft\/engines\/helicopters. The information is for reference only, and we do not guarantee the completeness, accuracy or currency of any manuals.\u003c\/p\u003e\n\u003cp\u003eReference herein to any specific commercial products by trade name, trademark, manufacturer, or otherwise, is not meant to imply or suggest any endorsement by, or affiliation with that manufacturer or supplier. All trade names, trademarks and manufacturer names are the property of their respective owners.\u003c\/p\u003e\n\u003cp\u003eThis digital compilation, structure, indexing and presentation are © Sicuro Publishing.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":52075424973147,"sku":null,"price":55.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/corvette-lb4-banner-landing-approach.png?v=1768832021"},{"product_id":"potez-air-fouga-magister-aircraft-manuals-collection-download","title":"Fouga CM 170 Magister Aircraft Manuals Collection - Digital Download","description":"\u003ch3\u003eFouga CM 170 Magister - Comprehensive Technical Documentation Collection\u003c\/h3\u003e\n\u003cp\u003eThis extensive digital collection brings together the essential technical manuals for the iconic Fouga CM 170 Magister jet trainer. Whether you're a restorer, aviation historian, researcher, or Magister enthusiast, this archive provides authentic documentation that guided pilots, maintenance crews, and technicians throughout the aircraft's distinguished service life.\u003c\/p\u003e\n\u003ch3\u003eWhat's Included:\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003ePilot's Handbooks\u003c\/strong\u003e - Flight operations, procedures, and aircraft systems (multiple editions including English and French versions)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFlight Manuals\u003c\/strong\u003e - Operational procedures for various air forces including German Air Force (GAF) editions\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eManuel de l'Equipage des Avions\u003c\/strong\u003e - Crew manual with text and illustrations (Version TOGO, Edition 1975, Revision 1977)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eManuel de Maintenance\u003c\/strong\u003e - Maintenance manual covering routine servicing (POTEZ, Edition 1982, Updated 1993)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eManuel d'Utilisation\u003c\/strong\u003e - Utilization manual (AEROSPATIALE, Edition 1981, Updated 1992)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTechnical Instructions for Pilots\u003c\/strong\u003e - Detailed technical guidance and procedures\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eIllustrated Parts Breakdown\u003c\/strong\u003e - Section One Introduction (GAF T.O. 1T-CM170 R-4)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eModifications Documentation\u003c\/strong\u003e - Martin-Baker Mk. GZ4 Ejection Seats installation (MB-124)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eHistorical Note:\u003c\/h3\u003e\n\u003cp\u003eThe Fouga CM 170 Magister holds a distinguished place in aviation history as one of the world's most successful and widely-used jet trainers. Designed by French aircraft manufacturer Fouga (later Potez-Air-Fouga, then Aérospatiale), the Magister first flew on 23 July 1952 and entered service with the French Air Force in 1956.\u003c\/p\u003e\n\u003cp\u003eWhat made the Magister revolutionary was its role as the first purpose-built jet trainer to be widely adopted internationally. Its distinctive V-tail configuration, side-by-side seating arrangement, and docile handling characteristics made it an ideal platform for transitioning pilots from piston-engine aircraft to jets. The aircraft's forgiving flight characteristics and relatively low operating costs contributed to its popularity with air forces around the world.\u003c\/p\u003e\n\u003cp\u003eDuring its production run from 1952 to 1962, approximately 929 Magisters were built, serving with over 25 air forces across Europe, the Middle East, Africa, Asia, and South America. The aircraft saw extensive service as an advanced trainer, light attack aircraft, and aerobatic display platform. Notable operators included France, West Germany, Israel, Belgium, Ireland, and many others. The Israeli Air Force famously used armed Magisters in combat during the Six-Day War in 1967.\u003c\/p\u003e\n\u003cp\u003eBeyond military training, the Magister gained international recognition through its use by the renowned Patrouille de France aerobatic team from 1964 to 1980, thrilling millions of spectators with precision formation flying. The aircraft's elegant lines and graceful performance made it a favorite at air shows worldwide.\u003c\/p\u003e\n\u003cp\u003ePost-military service, many Magisters found new life in civilian hands, becoming popular warbirds for collectors and enthusiasts. The aircraft's reliability, relatively simple systems, and availability of parts have made it one of the most accessible vintage jets for private ownership. Today, Magisters continue to delight crowds at air shows and remain active in private collections around the world.\u003c\/p\u003e\n\u003cp\u003eThese original technical manuals represent authentic documentation used throughout the Magister's service life by air forces including France, Germany, and various international operators. The collection spans multiple decades of the aircraft's operational history, from early 1960s editions through updates in the 1990s, reflecting the evolution of maintenance practices, modifications, and operational procedures. For restorers working to return these elegant jets to flight, historians researching Cold War-era training programs, or enthusiasts seeking to understand every system of this iconic aircraft, this documentation provides invaluable primary-source technical information.\u003c\/p\u003e\n\u003ch3\u003ePerfect For:\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003eAircraft restorers and maintainers working on Fouga Magister projects\u003c\/li\u003e\n\u003cli\u003eAviation historians researching jet trainer development and Cold War military aviation\u003c\/li\u003e\n\u003cli\u003eWarbird owners and operators seeking authentic technical reference material\u003c\/li\u003e\n\u003cli\u003eMilitary aviation researchers studying international training programs\u003c\/li\u003e\n\u003cli\u003eScale modelers seeking accurate technical details for authentic builds\u003c\/li\u003e\n\u003cli\u003eFlight simulator enthusiasts developing accurate Magister simulations\u003c\/li\u003e\n\u003cli\u003eAviation collectors building comprehensive technical libraries\u003c\/li\u003e\n\u003cli\u003eAerospace engineering students studying classic jet trainer design\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eFormat \u0026amp; Delivery:\u003c\/h3\u003e\n\u003cp\u003eDigital download in PDF format - Instant access upon purchase. High-quality scans preserving all technical illustrations, diagrams, and specifications from the original documentation.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eDisclaimer:\u003c\/strong\u003e This item is sold for historical and reference only. These are either ORIGINAL or COPIES of manuals and blueprints used when these aircraft were in active duty, now transferred into electronic format. These manuals and blueprints are not meant to be used for current update material for certification \/ repair, but make an excellent reference for the scholar, collector, modeller or aircraft buffs. For proprietary reasons, we generally only provide civil manuals and blueprints on obsolete Aircraft \/ Engines \/ Helicopter. The information is for reference only, and we do not guarantee the completeness, accuracy or currency of any manuals.\u003c\/p\u003e\n\u003cp\u003eReference herein to any specific commercial products by trade name, trademark, manufacturer, or otherwise, is not meant to imply or suggest any endorsement by, or affiliation with that manufacturer or supplier. All trade names, trademarks and manufacturer names are the property of their respective owners.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":52078597538139,"sku":null,"price":45.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/fouga-magister-promotional-banner.png?v=1768847907"},{"product_id":"sud-aviation-se-210-caravelle-aircraft-aeroplane-manuals-collection-download","title":"Sud Aviation SE 210 Caravelle Aircraft Aeroplane Manuals Collection  - Download -","description":"\u003ch3\u003eSud Aviation SE 210 Caravelle Aircraft Manuals Collection\u003c\/h3\u003e\n\u003cp\u003eThis comprehensive digital collection contains authentic technical documentation for the Sud Aviation SE 210 Caravelle, the pioneering French jet airliner that revolutionized commercial aviation in the late 1950s and 1960s. These original manuals provide detailed operational, maintenance, and technical information essential for historians, aviation enthusiasts, restorers, and researchers studying this groundbreaking aircraft.\u003c\/p\u003e\n\u003ch3\u003eCollection Contents\u003c\/h3\u003e\n\u003cp\u003eThis extensive archive includes:\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eFlight Manuals (Multiple Volumes)\u003c\/strong\u003e - Comprehensive operational procedures, performance data, and flight characteristics\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eInstruction Manuals (Volumes 1-3)\u003c\/strong\u003e - Detailed technical instructions covering all aircraft systems and components\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAirline-Specific Editions\u003c\/strong\u003e - SAS and Swissair company editions with operator-specific procedures\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eProduction Documentation\u003c\/strong\u003e - Manufacturing specifications and production standards from Sud Aviation\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTechnical Brochures\u003c\/strong\u003e - Marketing and technical literature including the \"Horizon\" promotional materials\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eHistorical Note: The Caravelle - Europe's Jet Age Pioneer\u003c\/h3\u003e\n\u003cp\u003eThe Sud Aviation SE 210 Caravelle holds a distinguished place in aviation history as the first short\/medium-range jet airliner to achieve widespread commercial success. Developed by France's Société Nationale de Constructions Aéronautiques du Sud-Est (S.N.C.A.S.E., later Sud Aviation), the Caravelle represented a bold European challenge to American dominance in commercial aviation during the early jet age.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eDesign Origins and Innovation:\u003c\/strong\u003e The Caravelle's development began in the early 1950s in response to a French government specification for a medium-range jet airliner. The aircraft featured a revolutionary rear-mounted engine configuration that became its signature design element. This innovative layout, with two Rolls-Royce Avon turbojet engines mounted on either side of the rear fuselage, offered several advantages: a clean wing design for improved aerodynamics, reduced cabin noise, and easier engine maintenance. The distinctive nose section was actually licensed from the de Havilland Comet, Britain's pioneering jet airliner, representing early European aerospace cooperation.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eFirst Flight and Entry into Service:\u003c\/strong\u003e The prototype Caravelle first flew on May 27, 1955, and the aircraft entered commercial service with Air France on May 6, 1959, on the Paris-Rome-Istanbul route. The Caravelle quickly proved its worth, offering jet speed and comfort on routes previously served by piston-engine aircraft, while being more economical to operate than larger long-range jets on shorter sectors.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eCommercial Success and Global Operations:\u003c\/strong\u003e The Caravelle achieved remarkable commercial success for a European aircraft of its era, with 282 units produced between 1958 and 1973. It was operated by over 30 airlines worldwide, including prestigious carriers such as Air France, SAS (Scandinavian Airlines), Swissair, Alitalia, Iberia, Finnair, and even United Air Lines in the United States - making it the first jet airliner of non-American design to be purchased by a U.S. carrier. The aircraft served routes across Europe, the Middle East, Africa, South America, and Asia, proving its versatility and reliability in diverse operating conditions.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eVariants and Evolution:\u003c\/strong\u003e Sud Aviation developed numerous Caravelle variants to meet different market requirements. The series progressed from the initial Caravelle I through to the Caravelle 12, with improvements including more powerful engines (later versions used Pratt \u0026amp; Whitney JT8D turbofans), increased passenger capacity (from 64 to 140 seats depending on variant), extended range, and enhanced performance. The Caravelle VI and VI-R were among the most successful variants, combining proven reliability with improved economics. The \"Super Caravelle\" variants featured mixed-power configurations and represented the pinnacle of the design's evolution.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eTechnical Significance:\u003c\/strong\u003e The Caravelle pioneered several features that became standard in subsequent jet airliner designs. Its rear-engine configuration influenced later aircraft such as the BAC One-Eleven, Douglas DC-9, Boeing 727, and Fokker F28. The aircraft's advanced systems, including comprehensive flight instrumentation, air conditioning and pressurization systems, and sophisticated hydraulic and electrical systems, set new standards for passenger comfort and operational capability in the medium-range jet category.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eOperational Legacy:\u003c\/strong\u003e Throughout its service life, the Caravelle earned a reputation for reliability, passenger comfort, and economic operation. Airlines praised its dispatch reliability and relatively low maintenance requirements. The aircraft's elegant lines and distinctive rear-engine configuration made it instantly recognizable at airports worldwide. Many Caravelles remained in commercial service well into the 1980s, with some continuing in corporate, government, and cargo operations into the 1990s.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eHistorical Impact:\u003c\/strong\u003e The Caravelle represented a crucial milestone in European aerospace achievement, demonstrating that European manufacturers could compete successfully in the global commercial aviation market. Its success paved the way for subsequent European collaborative programs, ultimately leading to the creation of Airbus. The aircraft proved that innovative design, combined with attention to operational economics and passenger comfort, could create a commercially viable product even in a market dominated by American manufacturers.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003ePreservation and Remembrance:\u003c\/strong\u003e Today, several Caravelles are preserved in aviation museums worldwide, including examples at the Musée de l'Air et de l'Espace in Paris, the Imperial War Museum Duxford in England, and various other institutions. These preserved aircraft serve as tangible reminders of an important chapter in aviation history and the beginning of Europe's jet age.\u003c\/p\u003e\n\u003cp\u003eThe technical manuals in this collection represent authentic documentation used throughout the Caravelle's operational life by airlines, maintenance organizations, and flight crews. They provide invaluable insights into the aircraft's systems, operational procedures, and the technical standards of the era. For aviation historians, these documents offer a window into the engineering philosophy and operational practices of the early jet age. For researchers and enthusiasts, they provide comprehensive technical details about one of aviation's most significant and elegant aircraft designs.\u003c\/p\u003e\n\u003ch3\u003eDocument Specifications\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eFormat:\u003c\/strong\u003e High-resolution digital PDF files\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eLanguage:\u003c\/strong\u003e English and French (depending on specific manual)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCoverage:\u003c\/strong\u003e Complete aircraft systems, operations, and maintenance procedures\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eHistorical Period:\u003c\/strong\u003e 1950s-1970s original documentation\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDelivery:\u003c\/strong\u003e Instant digital download upon purchase\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eIdeal For\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003eAviation historians researching early jet airliner development\u003c\/li\u003e\n\u003cli\u003eMuseum curators and restoration specialists working with preserved Caravelles\u003c\/li\u003e\n\u003cli\u003eAerospace engineering students studying classic aircraft design\u003c\/li\u003e\n\u003cli\u003eScale modelers seeking accurate technical details\u003c\/li\u003e\n\u003cli\u003eAviation enthusiasts and collectors of historical documentation\u003c\/li\u003e\n\u003cli\u003eResearchers studying the evolution of commercial aviation technology\u003c\/li\u003e\n\u003cli\u003eFormer Caravelle pilots, crew members, and maintenance personnel\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eDisclaimer:\u003c\/strong\u003e This item is sold for historical and reference only. These are either ORIGINAL or COPIES of manuals and blueprints used when these aircraft were in active duty, now transferred into electronic format. These manuals and blueprints are not meant to be used for current update material for certification \/ repair, but make an excellent reference for the scholar, collector, modeller or aircraft buffs .... For proprietary reasons, we generally only provide civil manuals and blueprints on obsolete Aircraft \/ Engines \/ Helicopter. The information is for reference only, and we do not guarantee the completeness, accuracy or currency of any manuals.\u003c\/p\u003e\n\u003cp\u003eReference herein to any specific commercial products by trade name, trademark, manufacturer, or otherwise, is not meant to imply or suggest any endorsement by, or affiliation with that manufacturer or supplier. All trade names, trademarks and manufacturer names are the property of their respective owners.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":52088793661787,"sku":null,"price":30.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/banner-1-varig-pp-vjd-silver-blue.png?v=1785515058"},{"product_id":"morane-saulnier-ms-760-paris-aircraft-aeroplane-manuals-collection-download","title":"Morane-Saulnier MS.760 Paris Aircraft Manuals Collection - Digital Download","description":"\u003ch3\u003eMorane-Saulnier MS.760 Paris Aircraft Manuals Collection\u003c\/h3\u003e\n\u003cp\u003eThis comprehensive digital collection contains authentic technical documentation for the Morane-Saulnier MS.760 Paris, the elegant French four-seat liaison and training aircraft that served military and civilian operators worldwide from the 1950s through the 1980s.\u003c\/p\u003e\n\u003ch3\u003eCollection Contents\u003c\/h3\u003e\n\u003cp\u003eThis archive includes original French Air Force (Armée de l'Air) technical manuals, flight handbooks, illustrated parts catalogs (Tableau de Composition Illustré), and operational documentation covering:\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eFlight Manuals and Operating Instructions (Manuel d'Utilisation)\u003c\/li\u003e\n\u003cli\u003eDescriptive and Functional Notices (Notice Descriptive et de Fonctionnement)\u003c\/li\u003e\n\u003cli\u003eIllustrated Parts Catalogs - Equipment, Electrical Installations, Turbo-Reactor Installations, and Tooling\u003c\/li\u003e\n\u003cli\u003eTechnical specifications and performance data\u003c\/li\u003e\n\u003cli\u003eMaintenance procedures and servicing instructions\u003c\/li\u003e\n\u003cli\u003eSystem diagrams and technical illustrations\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003eDocumentation includes materials from SOCATA (Société de Construction d'Avions de Tourisme et d'Affaires) and covers various MS.760 variants including the Paris I, Paris IR, and Paris II models, as well as the Beechcraft-marketed versions.\u003c\/p\u003e\n\u003ch3\u003eHistorical Note\u003c\/h3\u003e\n\u003cp\u003eThe Morane-Saulnier MS.760 Paris holds a distinguished place in post-war French aviation history as an innovative four-seat liaison and training aircraft powered by twin Turbomeca Marboré turbojet engines. First flown in 1954, the Paris represented a bold step forward in light jet aircraft design, offering military forces and civilian operators an economical, versatile platform that combined jet performance with practical operating costs.\u003c\/p\u003e\n\u003cp\u003eDuring its production run from 1954 to 1964, approximately 165 MS.760 aircraft were built, serving with the French Air Force, French Navy (Aéronavale), and air forces in Argentina, Brazil, and other nations. The aircraft proved particularly valuable as a liaison transport, communications aircraft, and advanced trainer, introducing countless pilots to jet operations. Its distinctive design featured a low-mounted wing, tricycle landing gear, and side-by-side seating for two crew with two passenger seats behind—an unusual configuration for a jet aircraft of its era.\u003c\/p\u003e\n\u003cp\u003eThe Paris also enjoyed civilian success, with Beechcraft marketing the type in North America and several examples serving corporate and private owners who appreciated its speed, range, and operating economy. The aircraft's reliability and versatility made it a favorite among operators who needed jet performance without the complexity and cost of larger aircraft.\u003c\/p\u003e\n\u003cp\u003ePost-production, many MS.760 aircraft continued flying well into the 1980s and beyond, with some examples still preserved in museums and private collections today. The type's legacy endures among aviation enthusiasts, restorers, and historians who recognize the Paris as a pioneering design that successfully bridged the gap between piston-engine liaison aircraft and modern business jets.\u003c\/p\u003e\n\u003cp\u003eThese original technical manuals represent the authentic documentation used throughout the MS.760's service life by French military maintenance crews, SOCATA technicians, and civilian operators. They provide invaluable reference material for historians researching French aviation development, museum curators preserving MS.760 aircraft, aviation enthusiasts studying jet trainer evolution, and collectors seeking authentic period documentation of this elegant and innovative French jet.\u003c\/p\u003e\n\u003ch3\u003eSpecifications\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eFormat:\u003c\/strong\u003e Digital PDF download\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eLanguage:\u003c\/strong\u003e Primarily French (original military documentation)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDocumentation Source:\u003c\/strong\u003e Direction Centrale du Matériel de l'Armée de l'Air, SOCATA, and manufacturer archives\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCoverage:\u003c\/strong\u003e MS.760 Paris I, Paris IR, Paris II variants\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePages:\u003c\/strong\u003e Comprehensive multi-volume collection\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eQuality:\u003c\/strong\u003e High-resolution scans of original documentation\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eIdeal For\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003eAviation historians researching French military and civilian jet aircraft\u003c\/li\u003e\n\u003cli\u003eMuseum curators and restorers working with MS.760 aircraft\u003c\/li\u003e\n\u003cli\u003eAviation enthusiasts and collectors of French aviation documentation\u003c\/li\u003e\n\u003cli\u003eResearchers studying post-war jet trainer and liaison aircraft development\u003c\/li\u003e\n\u003cli\u003eScale modelers seeking authentic technical references\u003c\/li\u003e\n\u003cli\u003eAcademic institutions with aviation history programs\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003eInstant digital download delivery ensures immediate access to this valuable historical aviation documentation.\u003c\/p\u003e\n\u003ch3\u003eDisclaimer\u003c\/h3\u003e\n\u003cp\u003eThis item is sold for historical and reference only. These are either original or copies of manuals and blueprints used when these aircraft were in active duty, now transferred into electronic format. These manuals and blueprints are not meant to be used for current update material for certification\/repair, but make an excellent reference for the scholar, collector, modeller or aircraft buffs. For proprietary reasons, we generally only provide civil manuals and blueprints on obsolete aircraft\/engines\/helicopters. The information is for reference only, and we do not guarantee the completeness, accuracy or currency of any manuals.\u003c\/p\u003e\n\u003cp\u003eReference herein to any specific commercial products by trade name, trademark, manufacturer, or otherwise, is not meant to imply or suggest any endorsement by, or affiliation with that manufacturer or supplier. All trade names, trademarks and manufacturer names are the property of their respective owners.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":52107621007707,"sku":null,"price":70.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/ms-760-paris-banner-6.png?v=1769352640"},{"product_id":"dassault-md-flamant-aircraft-aeroplane-manuals-collection-download","title":"Dassault MD-315 Flamant Aircraft Manuals Collection - Digital Download","description":"\u003ch3\u003eDassault MD-315 Flamant Aircraft Manuals Collection\u003c\/h3\u003e\n\u003cp\u003eThis digital collection contains authentic French technical documentation for the Dassault MD-315 Flamant family, including Flamant I (MD-315R), Flamant II (MD-312), and Flamant III (MD-311). The source documents were produced for the French Air Force and its technical personnel.\u003c\/p\u003e\n\u003ch3\u003eUpdated Manual Manifest\u003c\/h3\u003e\n\u003cp\u003eBased on the supplied cover pages, the collection currently includes these nine French-language documents:\u003c\/p\u003e\n\u003col\u003e\n\u003cli\u003e\n\u003cstrong\u003eAvion Marcel Dassault 315 “Flamant I” — Recueil de planches à l’usage des mécaniciens de l’Armée de l’Air\u003c\/strong\u003e\u003cbr\u003eSpécialité 51\/120: “Circuit hydraulique et atterrisseur” — 1953.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTableau de composition illustré des avions Flamant I (MD-315R), Flamant II (MD-312), Flamant III (MD-311)\u003c\/strong\u003e\u003cbr\u003eChapitre II, Fascicule 2: “Fuselage” — Partie Planches. Classification ACE-106, édition mai 1959.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTableau de composition illustré des avions Flamant I (MD-315R), Flamant II (MD-312), Flamant III (MD-311)\u003c\/strong\u003e\u003cbr\u003eChapitre II, Fascicule 2: “Fuselage” — Partie Texte. Classification ACE-106, édition mai 1959.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTableau de composition illustré des avions Flamant I (MD-315R), Flamant II (MD-312), Flamant III (MD-311)\u003c\/strong\u003e\u003cbr\u003eChapitre II, Fascicule 7: “Équipements” — Partie Planches. Classification ACE-106, édition mai 1959.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTableau de composition illustré des avions Flamant I (MD-315R), Flamant II (MD-312), Flamant III (MD-311)\u003c\/strong\u003e\u003cbr\u003eChapitre II, Fascicule 7: “Équipements” — Partie Texte. Classification ACE-106, édition mai 1959.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eManuel de maintenance des avions Flamant I, II et III — Service courant\u003c\/strong\u003e\u003cbr\u003ePartie Planches. Classification G.C.E. 106\/2, édition janvier 1958.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eManuel de maintenance des avions Flamant I, II et III — Service courant\u003c\/strong\u003e\u003cbr\u003ePartie Texte. Classification G.C.E. 106\/2, édition janvier 1958.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNotice descriptive et de fonctionnement 12 T 04-06\u003c\/strong\u003e\u003cbr\u003ePartie Planches. Approved by D.M. No. 790-DCMAA\/AT2 dated 26 January 1962, édition mars 1963. Classification NBC-106.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNotice descriptive et de fonctionnement 12 T 04-06\u003c\/strong\u003e\u003cbr\u003ePartie Texte. Approved by D.M. No. 790-DCMAA\/AT2 dated 26 January 1962, édition mars 1963. Classification NBC-106.\u003c\/li\u003e\n\u003c\/ol\u003e\n\u003cp\u003eThe illustrated composition tables cover the Fuselage and Équipements fascicules for the Flamant I, II, and III variants. The maintenance manual is divided into plates and text sections, while the 12 T 04-06 notice is likewise supplied in plates and text sections.\u003c\/p\u003e\n\u003ch3\u003eHistorical Note\u003c\/h3\u003e\n\u003cp\u003eThe Dassault MD-315 Flamant family was a post-war French twin-engine aircraft used in training, liaison, transport, and other military support roles. The family included the MD-315R Flamant I, MD-312 Flamant II, and MD-311 Flamant III. These original technical publications offer valuable reference material for aviation historians, restorers, museums, modelers, and researchers studying French post-war aircraft engineering.\u003c\/p\u003e\n\u003ch3\u003eTechnical Specifications\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eFormat:\u003c\/strong\u003e Digital PDF files\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eLanguage:\u003c\/strong\u003e French, original documentation\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePeriod:\u003c\/strong\u003e 1953–1963 editions\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSource:\u003c\/strong\u003e French Air Force and French military technical publications\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCoverage:\u003c\/strong\u003e Flamant I (MD-315R), Flamant II (MD-312), and Flamant III (MD-311)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eIdeal For\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003eAviation historians researching post-war French military aircraft\u003c\/li\u003e\n\u003cli\u003eAircraft restorers working on Flamant preservation projects\u003c\/li\u003e\n\u003cli\u003eScale modelers seeking authentic technical details\u003c\/li\u003e\n\u003cli\u003eMuseums and educational institutions documenting French aviation heritage\u003c\/li\u003e\n\u003cli\u003eCollectors and researchers of historical aviation technical documentation\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eHistorical reference notice:\u003c\/strong\u003e These historical manuals are provided for research, educational, restoration-reference, collecting, and modeling purposes. They are not current approved airworthiness data and must not be used as a substitute for current manufacturer, regulator, or qualified-maintenance guidance. OAL does not guarantee completeness, accuracy, or currency of the historical material.\u003c\/p\u003e\n\u003cp\u003eReference to any commercial product, trade name, trademark, manufacturer, or supplier does not imply endorsement or affiliation. This digital compilation, structure, indexing and presentation are © Sicuro Publishing.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":52110479786331,"sku":null,"price":50.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/dassault-flamant-lb4-banner-1.png?v=1769424841"},{"product_id":"dassault-md-450-ouragan-aircraft-aeroplane-manuals-collection-download","title":"Dassault MD.450 Ouragan Aircraft Manuals Collection - Digital Download","description":"\u003ch3\u003eDassault MD.450 Ouragan Aircraft Technical Manuals Collection\u003c\/h3\u003e\n\u003cp\u003eThis comprehensive digital collection contains authentic technical documentation for the Dassault MD.450 Ouragan, France's first operational jet fighter. These original manuals represent the actual documentation used by French Air Force personnel, maintenance crews, and pilots throughout the aircraft's distinguished service life.\u003c\/p\u003e\n\u003ch3\u003eCollection Contents\u003c\/h3\u003e\n\u003cp\u003eThis archive includes:\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eNotice Technique Provisoire\u003c\/strong\u003e - Provisional technical manual with detailed aircraft systems information, providing early operational guidance for the Ouragan. (In French.)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNotice Technique (Édition Juin 1955)\u003c\/strong\u003e - Comprehensive maintenance manual for the Ouragan in the standard early 1950s French military format. This updated edition replaced the August 1953 version and was approved by Ministerial Decision N° 38.528\/STA\/A3. Includes detailed aircraft description, maintenance procedures, weight data, dismantling instructions, and complete technical specifications. Document N.C.C. 36 dated June 1955 with approximately 440 pages. (In French.)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTableau de Composition Illustré\u003c\/strong\u003e - Complete illustrated parts catalog for the Ouragan featuring detailed component breakdowns for wing assembly and all aircraft systems, part numbers, and assembly diagrams. Document A.C.C. 2 dated June 1954 with approximately 1,515 pages. (In French.)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCarte de Service 'Pilote'\u003c\/strong\u003e - Pilot service card with essential operational information, quick reference data, and flight procedures for Ouragan pilots. (In French.)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003eAll manuals feature original French text, technical diagrams, detailed maintenance procedures, and specifications for the Hispano-Suiza 'Nene' turbojet engine. Documentation includes ministerial approvals, classification markings, and edition details authenticating their historical provenance.\u003c\/p\u003e\n\u003ch3\u003eHistorical Note\u003c\/h3\u003e\n\u003cp\u003eThe Dassault MD.450 Ouragan (Hurricane) holds a distinguished place in aviation history as France's first domestically-designed jet fighter to enter operational service. Developed in the late 1940s by Marcel Dassault's design bureau, the Ouragan represented France's determination to rebuild its aviation industry after World War II and establish independence in military aircraft production.\u003c\/p\u003e\n\u003cp\u003eFirst flown on February 28, 1949, the Ouragan was powered by the Hispano-Suiza-built version of the British Rolls-Royce Nene turbojet engine, producing 5,000 lbf of thrust. The aircraft featured a distinctive straight-wing design, tricycle landing gear, and four 20mm Hispano-Suiza cannon mounted in the nose. With a maximum speed of 584 mph (940 km\/h) and excellent handling characteristics, the Ouragan proved to be a capable fighter-bomber platform.\u003c\/p\u003e\n\u003cp\u003eThe French Air Force (Armée de l'Air) operated the Ouragan extensively throughout the 1950s, with 350 aircraft produced between 1951 and 1954. The type saw combat action during the Suez Crisis in 1956, where French Ouragans flew ground-attack missions with distinction. Beyond French service, the aircraft was exported to India (where it was known as the 'Toofani') and Israel, where it played a crucial role in the 1956 Sinai Campaign and continued in service through the 1960s.\u003c\/p\u003e\n\u003cp\u003eThe Ouragan's significance extends beyond its operational record. It established Dassault as a premier military aircraft manufacturer and paved the way for the company's legendary Mystère, Mirage, and Rafale fighter families. The aircraft demonstrated that France could design, build, and field world-class jet fighters, marking the renaissance of French military aviation in the jet age.\u003c\/p\u003e\n\u003cp\u003eFor aviation historians, restorers, and enthusiasts, these original technical manuals represent authentic primary-source documentation from the Ouragan's operational era. The detailed maintenance procedures, illustrated parts catalogs, pilot information, and technical specifications provide invaluable insights into the engineering, operation, and support of this pioneering French jet fighter. Each manual bears the official approvals and classifications of the Service des Marchés et de la Production Aéronautique, confirming their authenticity as the actual documentation used throughout the aircraft's service life.\u003c\/p\u003e\n\u003cp\u003eToday, surviving Ouragans are preserved in museums worldwide, celebrated as symbols of French aviation achievement and Cold War military history. This documentation collection preserves the technical legacy of an aircraft that launched one of the world's most successful fighter aircraft dynasties.\u003c\/p\u003e\n\u003ch3\u003eProduct Details\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eFormat:\u003c\/strong\u003e Digital download (PDF)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eLanguage:\u003c\/strong\u003e French (original documentation)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eContent:\u003c\/strong\u003e Original scans of historical technical manuals\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTotal Pages:\u003c\/strong\u003e Approximately 1,955+ pages\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCoverage:\u003c\/strong\u003e Complete maintenance procedures, illustrated parts catalog, and pilot information\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eHistorical Period:\u003c\/strong\u003e 1950s French Air Force documentation\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eDisclaimer:\u003c\/strong\u003e This item is sold for historical and reference only. These are either original or copies of manuals and blueprints used when these aircraft were in active duty, now transferred into electronic format. These manuals and blueprints are not meant to be used for current update material for certification\/repair, but make an excellent reference for the scholar, collector, modeller or aircraft buffs. For proprietary reasons, we generally only provide civil manuals and blueprints on obsolete aircraft\/engines\/helicopters. The information is for reference only, and we do not guarantee the completeness, accuracy or currency of any manuals.\u003c\/p\u003e\n\u003cp\u003eReference herein to any specific commercial products by trade name, trademark, manufacturer, or otherwise, is not meant to imply or suggest any endorsement by, or affiliation with that manufacturer or supplier. All trade names, trademarks and manufacturer names are the property of their respective owners.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":52110940668251,"sku":null,"price":30.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/ouragan-promotional-banner.png?v=1769431012"},{"product_id":"dassault-mirage-5-ba-aircraft-aeroplane-manuals-collection-download","title":"Dassault Mirage 5 BA  Aircraft Aeroplane Manuals Collection - Download -","description":"\u003ch3\u003eDassault Mirage 5 BA Aircraft Manuals Collection\u003c\/h3\u003e\n\u003cp\u003eThis comprehensive digital collection contains authentic technical documentation for the Dassault Mirage 5 BA, the Belgian Air Force variant of France's legendary ground-attack fighter. These original manuals represent the actual documentation used by Belgian military personnel, maintenance crews, and pilots throughout the aircraft's distinguished service life.\u003c\/p\u003e\n\u003ch3\u003eCollection Contents\u003c\/h3\u003e\n\u003cp\u003eThis archive includes detailed technical manuals covering aircraft systems, maintenance procedures, operational guidelines, illustrated parts catalogs, and comprehensive documentation essential for understanding this remarkable aircraft. Each manual has been carefully digitized to preserve the original technical specifications, diagrams, and procedures used during the Mirage 5 BA's operational service.\u003c\/p\u003e\n\u003ch3\u003eHistorical Note\u003c\/h3\u003e\n\u003cp\u003eThe Dassault Mirage 5 BA holds a distinguished place in Belgian military aviation history as the backbone of the Belgian Air Force's ground-attack and tactical strike capabilities from 1970 through the early 1990s. Developed as a simplified, clear-weather ground-attack variant of the Mirage III, the Mirage 5 was specifically designed for export customers seeking a cost-effective yet highly capable tactical fighter.\u003c\/p\u003e\n\u003cp\u003eBelgium ordered 106 Mirage 5 aircraft in multiple variants, with the Mirage 5 BA serving as the primary ground-attack version. First delivered in 1970, these aircraft were stationed at Florennes Air Base and Bierset Air Base, where they formed the core of Belgium's tactical air power during the Cold War era. The \"BA\" designation identified the Belgian ground-attack variant, distinguishing it from the 5 BD reconnaissance and 5 BR trainer versions also operated by the Belgian Air Force.\u003c\/p\u003e\n\u003cp\u003eThe Mirage 5 BA featured reduced avionics compared to the all-weather Mirage III, trading sophisticated radar systems for increased fuel capacity and weapons payload. This made it exceptionally effective for visual ground-attack missions, close air support, and tactical strike operations. Belgian pilots praised the aircraft's excellent handling characteristics, powerful SNECMA Atar 9C turbojet engine, and versatility in carrying a wide range of ordnance including bombs, rockets, and air-to-ground missiles.\u003c\/p\u003e\n\u003cp\u003eThroughout its service life, the Mirage 5 BA participated in numerous NATO exercises and maintained Belgium's commitment to collective defense during the Cold War. The aircraft's reliability and performance made it a valued asset, with Belgian maintenance crews developing exceptional expertise in keeping these fighters mission-ready. The Mirage 5 BA remained in frontline service until the early 1990s, when it was gradually replaced by the F-16 Fighting Falcon.\u003c\/p\u003e\n\u003cp\u003eToday, the Mirage 5 BA is remembered as a symbol of Belgian air power during a critical period in European history. Several examples are preserved in aviation museums, including the Royal Museum of the Armed Forces and Military History in Brussels. For aviation historians, restorers, military researchers, and enthusiasts of Cold War military aviation, these original technical manuals represent authentic primary-source documentation from one of Europe's most capable tactical fighters.\u003c\/p\u003e\n\u003ch3\u003ePerfect For\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003eMilitary aviation historians researching Cold War European air forces\u003c\/li\u003e\n\u003cli\u003eAviation researchers studying French tactical fighter development\u003c\/li\u003e\n\u003cli\u003eMuseum curators and restoration specialists working with Mirage 5 aircraft\u003c\/li\u003e\n\u003cli\u003eScale modelers seeking accurate technical details for Belgian Air Force Mirage 5 BA projects\u003c\/li\u003e\n\u003cli\u003eAviation enthusiasts and collectors of military technical documentation\u003c\/li\u003e\n\u003cli\u003eAcademic researchers studying NATO tactical aviation during the Cold War\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eDigital Download\u003c\/h3\u003e\n\u003cp\u003eAll manuals are provided as high-quality digital files, allowing you to access this valuable technical documentation immediately after purchase. These digitized manuals preserve the original formatting, technical drawings, and specifications exactly as they appeared in the official Belgian Air Force documentation.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eDisclaimer:\u003c\/strong\u003e This item is sold for historical and reference only. These are either original or copies of manuals and blueprints used when these aircraft were in active duty, now transferred into electronic format. These manuals and blueprints are not meant to be used for current update material for certification\/repair, but make an excellent reference for the scholar, collector, modeler or aircraft enthusiast. For proprietary reasons, we generally only provide civil manuals and blueprints on obsolete aircraft\/engines\/helicopters. The information is for reference only, and we do not guarantee the completeness, accuracy or currency of any manuals.\u003c\/p\u003e\n\u003cp\u003eReference herein to any specific commercial products by trade name, trademark, manufacturer, or otherwise, is not meant to imply or suggest any endorsement by, or affiliation with that manufacturer or supplier. All trade names, trademarks and manufacturer names are the property of their respective owners.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":52111549399387,"sku":null,"price":40.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/dassault-mirage-5-ba-lb4-banner-2.png?v=1769493020"},{"product_id":"morane-saulnier-alcyon-aircraft-aeroplane-manuals-collection-download","title":"Morane-Saulnier MS.733 Alcyon Aircraft Technical Manuals Collection - Digital Download","description":"\u003ch3\u003eMorane-Saulnier MS.733 Alcyon - Comprehensive Technical Manuals Collection\u003c\/h3\u003e\n\u003cp\u003eThis comprehensive digital collection contains authentic technical documentation for the Morane-Saulnier MS.733 Alcyon, the French military's primary basic trainer aircraft of the 1950s and 1960s. These original manuals represent the actual documentation used by French Air Force maintenance crews and pilots throughout the aircraft's distinguished service life.\u003c\/p\u003e\n\u003ch3\u003eCollection Contents:\u003c\/h3\u003e\n\u003cp\u003e\u003cstrong\u003eNotice d'Utilisation (Flight Manual)\u003c\/strong\u003e - S.F.A.S.A. Saint-Yan, Edition Provisoire, Juin 1958. Complete operational procedures and flight characteristics for the MS.733.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eNotice Technique (Technical Manual)\u003c\/strong\u003e - Morane-Saulnier 733 with Potez 6D-02-A engine and Ratier 2304 propeller. Approved by Ministerial Decision, February 1958 edition.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eTableau de Composition Illustré (Illustrated Parts Catalog)\u003c\/strong\u003e - Complete parts breakdown with detailed illustrations. Classification A.C.E. 102, February 1958 edition, 413 copies printed.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eManuel de l'Equipage - Partie Texte (Crew Manual - Text Section)\u003c\/strong\u003e - Classification UCD 103, April 1957 edition. Comprehensive crew procedures and operational guidance.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eManuel de l'Equipage - Partie Planches (Crew Manual - Plates Section)\u003c\/strong\u003e - Classification UCD 103, April 1957 edition. Detailed technical illustrations and diagrams.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eNotice Technique de l'Hélice Hydraulique Ratier Type 2304\u003c\/strong\u003e - Complete technical documentation for the Ratier 2304 hydraulic propeller system. Classification N.CH.10 A, April 1957 edition.\u003c\/p\u003e\n\u003ch3\u003eHistorical Note:\u003c\/h3\u003e\n\u003cp\u003eThe Morane-Saulnier MS.733 Alcyon holds a distinguished place in French aviation history as the primary basic trainer that shaped generations of French military pilots during the critical post-war period. First flown in 1949, the Alcyon was developed as a modern replacement for aging wartime trainers, designed specifically to meet the French Air Force's demanding requirements for a robust, reliable, and forgiving training aircraft.\u003c\/p\u003e\n\u003cp\u003eThe MS.733's design origins trace back to Morane-Saulnier's extensive experience with training aircraft, incorporating lessons learned from both pre-war civilian trainers and wartime operational experience. The aircraft featured a conventional low-wing monoplane configuration with tandem seating, powered by the reliable Potez 6D-02-A six-cylinder inline engine producing 240 horsepower, driving a Ratier 2304 hydraulic variable-pitch propeller. This powerplant combination provided excellent performance characteristics ideal for ab-initio training.\u003c\/p\u003e\n\u003cp\u003eThroughout the 1950s and 1960s, the MS.733 Alcyon served as the backbone of French military flight training, operating from bases across France and French territories. The aircraft proved exceptionally well-suited to its training role, offering docile handling characteristics that built student confidence while maintaining sufficient performance to prepare pilots for transition to more advanced aircraft. Its robust construction and reliable Potez engine earned it a reputation for dependability, with many aircraft accumulating thousands of flight hours training successive classes of military aviators.\u003c\/p\u003e\n\u003cp\u003eBeyond its primary military training role, the Alcyon found applications in liaison duties, observation missions, and even limited civilian use. Several examples were operated by French aero clubs and private owners, where the aircraft's economical operation and pleasant flying characteristics made it popular among sport pilots and aviation enthusiasts.\u003c\/p\u003e\n\u003cp\u003eProduction of the MS.733 totaled approximately 180 aircraft, with the type remaining in French military service well into the 1960s before being gradually replaced by more modern jet trainers. The aircraft's contribution to French military aviation cannot be overstated - virtually every French military pilot trained during this era gained their initial flying experience in the Alcyon's cockpit.\u003c\/p\u003e\n\u003cp\u003eToday, the MS.733 Alcyon is remembered fondly by aviation historians and former pilots alike as a capable, honest trainer that served France with distinction during a transformative period in military aviation. Several examples survive in museums and private collections, preserved as testament to this important chapter in French aeronautical heritage.\u003c\/p\u003e\n\u003cp\u003eThese original technical manuals represent authentic primary-source documentation used throughout the MS.733's operational service life. Approved by French military authorities and produced in limited quantities (as noted by the \"Nombre d'exemplaires\" markings), these documents provided maintenance crews, engineers, and pilots with the detailed technical information necessary to operate and maintain the Alcyon fleet. For restorers, historians, researchers, and aviation enthusiasts, this collection offers invaluable insight into the technical specifications, maintenance procedures, and operational characteristics of this significant French trainer aircraft.\u003c\/p\u003e\n\u003ch3\u003eTechnical Specifications:\u003c\/h3\u003e\n\u003cp\u003e\u003cstrong\u003eAircraft:\u003c\/strong\u003e Morane-Saulnier MS.733 Alcyon\u003cbr\u003e\u003cstrong\u003eEngine:\u003c\/strong\u003e Potez 6D-02-A (6-cylinder inline, 240 hp)\u003cbr\u003e\u003cstrong\u003ePropeller:\u003c\/strong\u003e Ratier Type 2304 hydraulic variable-pitch\u003cbr\u003e\u003cstrong\u003eRole:\u003c\/strong\u003e Military basic trainer\u003cbr\u003e\u003cstrong\u003eService Period:\u003c\/strong\u003e 1950s-1960s\u003cbr\u003e\u003cstrong\u003eOperator:\u003c\/strong\u003e French Air Force (Armée de l'Air)\u003c\/p\u003e\n\u003ch3\u003eDocumentation Details:\u003c\/h3\u003e\n\u003cp\u003eAll manuals in this collection are official French military technical publications, bearing original classification markings (N.C.E. 102, A.C.E. 102, UCD 103, N.CH.10 A) and ministerial approval stamps. Edition dates range from 1956-1958, representing the aircraft's peak operational period. Documents include approval references, edition information, and production quantities, confirming their authenticity as limited-distribution military technical publications.\u003c\/p\u003e\n\u003ch3\u003eIdeal For:\u003c\/h3\u003e\n\u003cp\u003eAircraft restorers and maintainers seeking authentic technical specifications, aviation historians researching French military training aircraft development, museum curators documenting MS.733 Alcyon exhibits, scale modelers requiring accurate technical details and dimensions, aviation enthusiasts and collectors of French aeronautical documentation, researchers studying post-war French military aviation programs, and former pilots and crew members seeking documentation of their training aircraft.\u003c\/p\u003e\n\u003ch3\u003eFormat:\u003c\/h3\u003e\n\u003cp\u003eDigital download - high-resolution scans of original documentation preserving all technical illustrations, diagrams, tables, and French text exactly as published by French military authorities.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eDisclaimer:\u003c\/strong\u003e This item is sold for historical and reference only. These are either original or copies of manuals and blueprints used when these aircraft were in active duty, now transferred into electronic format. These manuals and blueprints are not meant to be used for current update material for certification\/repair, but make an excellent reference for the scholar, collector, modeler or aircraft buffs. For proprietary reasons, we generally only provide civil manuals and blueprints on obsolete aircraft\/engines\/helicopters. The information is for reference only, and we do not guarantee the completeness, accuracy or currency of any manuals.\u003c\/p\u003e\n\u003cp\u003eReference herein to any specific commercial products by trade name, trademark, manufacturer, or otherwise, is not meant to imply or suggest any endorsement by, or affiliation with that manufacturer or supplier. All trade names, trademarks and manufacturer names are the property of their respective owners.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":52120087658843,"sku":null,"price":35.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/ms-733-alcyon-promotional-banner.png?v=1769529321"},{"product_id":"max-holste-mh-1521-broussard-aircraft-manuals-collection-download","title":"Max Holste MH. 1521 Broussard  Aircraft  Manuals Collection - Download -","description":"\u003ch3\u003eMax Holste MH.1521 Broussard Aircraft Manuals Collection\u003c\/h3\u003e\n\u003cp\u003eDiscover the comprehensive technical documentation for one of post-war France's most versatile and beloved utility aircraft. This digital collection brings together authentic operational and maintenance manuals for the Max Holste MH.1521 Broussard, the rugged liaison aircraft that served military and civilian operators across five continents from the 1950s through the 1980s.\u003c\/p\u003e\n\u003ch3\u003eWhat's Included in This Collection\u003c\/h3\u003e\n\u003cp\u003eThis extensive manuals package contains original French military documentation covering all aspects of Broussard operation and maintenance:\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eFlight Manuals (Manuel d'Utilisation)\u003c\/strong\u003e - Comprehensive pilot operating handbooks with procedures, performance data, and flight characteristics\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMaintenance Manuals (Manuel de Maintenance)\u003c\/strong\u003e - Detailed service procedures including routine maintenance and major overhaul instructions\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eIllustrated Parts Catalogs (Tableau de Composition Illustré)\u003c\/strong\u003e - Complete parts breakdowns with exploded diagrams and part numbers\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDescriptive and Operational Notices (Notice Descriptive et de Fonctionnement)\u003c\/strong\u003e - Technical descriptions of aircraft systems and their operation\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCrew Equipment Checklists (Memento de l'Equipage)\u003c\/strong\u003e - Standardized checklists for pre-flight, flight, and post-flight operations\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMechanic's Handbooks (Memento Mecanicien)\u003c\/strong\u003e - Quick-reference guides for maintenance personnel\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePratt \u0026amp; Whitney R-985 Engine Documentation\u003c\/strong\u003e - Maintenance manuals, overhaul procedures, and illustrated parts catalogs for the Wasp Junior powerplant\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eHamilton Standard Propeller Manuals\u003c\/strong\u003e - Service and parts documentation for the 2.D 30-237 counterweight propellers\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003eDocumentation spans from original 1950s-1960s editions through updates from the 1970s and 1980s, approved by French military aviation authorities (DCMAA). Manuals are provided in their original French language with some English-language supplements included.\u003c\/p\u003e\n\u003ch3\u003eHistorical Note: The Max Holste MH.1521 Broussard\u003c\/h3\u003e\n\u003cp\u003eThe Max Holste MH.1521 Broussard holds a distinguished place in post-war French aviation history as one of the most successful utility aircraft of its era. Designed by aviation pioneer Max Holste in the early 1950s, the Broussard was created to meet the French military's need for a rugged, versatile liaison and observation aircraft capable of operating from unprepared airstrips in challenging environments.\u003c\/p\u003e\n\u003cp\u003eThe prototype first flew on November 17, 1952, and the aircraft quickly proved its exceptional STOL (Short Takeoff and Landing) capabilities and reliability. Its name \"Broussard\" (meaning \"bush pilot\" in French) perfectly captured its intended role - operating in remote, undeveloped regions where conventional aircraft couldn't venture.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eMilitary Service and Global Operations:\u003c\/strong\u003e The Broussard saw extensive service with the French Air Force (Armée de l'Air) and French Army Light Aviation (ALAT) from the mid-1950s through the 1980s. It proved invaluable during France's operations in Algeria, where its ability to operate from rough desert strips and its excellent visibility made it ideal for liaison, observation, and light transport duties. The aircraft could carry a pilot and up to five passengers, or be configured for casualty evacuation with stretchers.\u003c\/p\u003e\n\u003cp\u003eBeyond French service, the Broussard was exported to numerous countries including Mauritania, Senegal, Ivory Coast, Cameroon, and other former French territories in Africa, where it continued to demonstrate its versatility in challenging tropical and desert conditions. Its robust construction and forgiving flight characteristics made it popular with military and civilian operators alike.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eTechnical Excellence:\u003c\/strong\u003e Powered by the legendary Pratt \u0026amp; Whitney R-985 Wasp Junior nine-cylinder radial engine producing 450 horsepower, the Broussard combined American powerplant reliability with French design ingenuity. The Hamilton Standard constant-speed propeller and the aircraft's high-lift wing design gave it remarkable short-field performance - it could take off in just 180 meters and land in even less distance.\u003c\/p\u003e\n\u003cp\u003eThe aircraft's all-metal construction, fixed tailwheel landing gear with robust shock absorption, and excellent visibility from its greenhouse-style canopy made it both durable and practical for its intended missions. Its maximum speed of 260 km\/h and range of 1,200 kilometers provided excellent operational flexibility.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eProduction and Legacy:\u003c\/strong\u003e Approximately 360 Broussards were produced between 1952 and 1961, making it one of the most successful French aircraft designs of the post-war period. Many examples remained in active service well into the 1980s, a testament to their solid construction and ease of maintenance.\u003c\/p\u003e\n\u003cp\u003eToday, the Broussard is remembered fondly by pilots and aviation enthusiasts for its honest flying qualities, rugged dependability, and its role in opening up remote regions to reliable air service. Several examples have been preserved in museums and private collections, with a handful still flying in civilian hands, keeping alive the legacy of Max Holste's versatile bush plane.\u003c\/p\u003e\n\u003ch3\u003eWhy These Manuals Matter\u003c\/h3\u003e\n\u003cp\u003eThis collection represents authentic technical documentation used throughout the Broussard's operational life by French military maintenance crews and pilots. These manuals contain the detailed technical knowledge required to understand, operate, and maintain this historically significant aircraft.\u003c\/p\u003e\n\u003cp\u003ePerfect for:\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eAviation historians researching post-war French military aviation\u003c\/li\u003e\n\u003cli\u003eRestorers working on Broussard preservation projects\u003c\/li\u003e\n\u003cli\u003eAircraft enthusiasts studying 1950s utility aircraft design\u003c\/li\u003e\n\u003cli\u003eTechnical researchers examining French aviation documentation standards\u003c\/li\u003e\n\u003cli\u003eCollectors of rare aviation technical literature\u003c\/li\u003e\n\u003cli\u003eModelers seeking authentic technical details and specifications\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eDigital Download Details\u003c\/h3\u003e\n\u003cp\u003eAll manuals are provided as high-resolution PDF files, preserving the original document quality including technical drawings, diagrams, and photographs. Files are immediately downloadable upon purchase, giving you instant access to this rare technical library.\u003c\/p\u003e\n\u003ch3\u003eDisclaimer\u003c\/h3\u003e\n\u003cp\u003eThis item is sold for historical and reference only. These are either original or copies of manuals used when these aircraft were in active duty, now transferred into electronic format. These manuals are not meant to be used for current update material for certification or repair, but make an excellent reference for the scholar, collector, modeler, or aviation enthusiast. For proprietary reasons, we generally only provide civil manuals on obsolete aircraft, engines, and helicopters. The information is for reference only, and we do not guarantee the completeness, accuracy, or currency of any manuals.\u003c\/p\u003e\n\u003cp\u003eReference herein to any specific commercial products by trade name, trademark, manufacturer, or otherwise, is not meant to imply or suggest any endorsement by, or affiliation with that manufacturer or supplier. All trade names, trademarks, and manufacturer names are the property of their respective owners.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":52154687029595,"sku":null,"price":35.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/max-holste-broussard-lb4-banner-military.png?v=1770103975"},{"product_id":"sipa-s-10-s-11-s-12-s-121-arado-ar-396-aircraft-manuals-collection-download","title":"SIPA S.12\/S.121 \u0026 Arado Ar 396 Training Aircraft Manuals - Comprehensive Technical Documentation Collection","description":"\u003ciframe title=\"Arado Ar 396, the trainer that the War couldn't stop\" src=\"https:\/\/www.youtube.com\/embed\/AsFkrwbTS14\" height=\"315\" width=\"560\" style=\"display: block; margin: 0 auto 20px;\"\u003e\u003c\/iframe\u003e\n\u003ch3\u003eSIPA S.10\/S.11\/S.12\/S.121 \u0026amp; Arado Ar 396 - Comprehensive Technical Documentation Collection\u003c\/h3\u003e\n\u003cp\u003eThis definitive digital archive contains authentic technical documentation for the \u003cstrong\u003eSIPA S.12\/S.121\u003c\/strong\u003e trainer aircraft and its German predecessor, the \u003cstrong\u003eArado Ar 396\u003c\/strong\u003e—a remarkable aircraft that transcended political boundaries to serve both the German Luftwaffe during World War II and the French Armée de l'Air for years after the war's end. These original German and French manuals, parts catalogs, flight training materials, and crew operating instructions represent the actual documentation used by Luftwaffe training schools during the war and French Air Force training establishments including the prestigious École de l'Air during the postwar period.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eDefinitive Collection with Free Lifetime Updates:\u003c\/strong\u003e This is a living collection that we continuously expand and refine. As we acquire additional Arado Ar 396 or SIPA documentation, technical bulletins, training materials, or variant-specific resources, we update this collection and provide free lifetime updates to all purchasers. Your one-time purchase guarantees access to all future additions and improvements to this collection.\u003c\/p\u003e\n\u003ch3\u003eHistorical Note\u003c\/h3\u003e\n\u003cp\u003eThe \u003cstrong\u003eArado Ar 396\u003c\/strong\u003e and its French-built successor, the \u003cstrong\u003eSIPA S.12\/S.121\u003c\/strong\u003e, represent a fascinating and unique chapter in aviation history—a German trainer aircraft so well-designed and effective that it not only served the Luftwaffe during World War II but continued production in France for years after the war's end, training a new generation of French pilots during the crucial postwar reconstruction period. This remarkable story of continuity across political and military boundaries stands as testament to the fundamental excellence of the aircraft's design.\u003c\/p\u003e\n\u003cp\u003eThe Arado Ar 396 was developed by Arado Flugzeugwerke in Brandenburg during the late 1930s as an advanced trainer for the Luftwaffe, designed to bridge the gap between basic trainers and frontline combat aircraft. The aircraft was conceived to prepare student pilots for the transition to high-performance fighters and bombers, providing training in advanced flying techniques, aerobatics, formation flying, navigation, and instrument procedures in an aircraft with handling characteristics approaching those of operational types.\u003c\/p\u003e\n\u003cp\u003eFirst flown in 1940, the Ar 396 featured robust all-metal construction with a welded steel tube fuselage and metal-covered wings, tandem seating with dual controls for instructor and student, enclosed cockpit providing protection from the elements, retractable tailwheel landing gear, and docile handling characteristics combined with sufficient performance to teach advanced maneuvers. Powered by an Argus As 410 inverted V12 engine producing 465 horsepower—the same reliable powerplant used in the highly successful Ar 96 trainer—the Ar 396 achieved a maximum speed of approximately 340 km\/h (211 mph) and demonstrated excellent handling characteristics that made it ideal for training future fighter pilots.\u003c\/p\u003e\n\u003cp\u003eDuring World War II, the Ar 396 served German flight training schools (Flugzeugführerschulen) across occupied Europe, preparing thousands of Luftwaffe pilots for combat operations. The aircraft's reliability, forgiving flight characteristics, robust construction capable of withstanding the inevitable hard landings and rough handling from student pilots, and straightforward maintenance requirements earned it respect among instructors, students, and ground crews alike. The type proved particularly valuable for advanced aerobatic training and instrument flying instruction.\u003c\/p\u003e\n\u003cp\u003eWhen Germany occupied France in 1940, Arado established production facilities at the former SIPA (Société Industrielle Pour l'Aéronautique) factory near Paris to supplement German production capacity and utilize French industrial resources. This wartime production arrangement would have profound postwar consequences that neither side could have anticipated.\u003c\/p\u003e\n\u003cp\u003eAfter the Liberation of France in 1944 and Germany's surrender in May 1945, the French government and Armée de l'Air faced the challenge of rebuilding French military aviation from the ground up. French aircraft factories had been destroyed or converted to German production, experienced pilots were scarce, and modern training aircraft were desperately needed. In this context, French aviation authorities made a remarkable and pragmatic decision: continue production of the Ar 396 under French designation as the SIPA S.10, S.11, S.12, and S.121 series.\u003c\/p\u003e\n\u003cp\u003eThis decision recognized the Ar 396's exceptional training qualities and the practical reality that the tooling, expertise, and production facilities already existed at the SIPA factory. Rather than delay pilot training for years while developing an entirely new aircraft, France would build upon proven German engineering to meet immediate needs. It was a controversial decision—building an aircraft of German design so soon after the Occupation—but military necessity and the aircraft's undeniable quality prevailed.\u003c\/p\u003e\n\u003cp\u003eThe French-built SIPA variants incorporated minor improvements and modifications while retaining the fundamental design excellence of the original Arado. The SIPA S.10 was the initial postwar production version, closely following the Ar 396 design. The SIPA S.11 featured French-manufactured Renault 12S engines (license-built Argus As 410) and equipment modifications. The SIPA S.12 introduced further refinements based on French operational experience and became the standard production variant. The SIPA S.121 was an improved version with enhanced equipment and systems for advanced training operations.\u003c\/p\u003e\n\u003cp\u003eProduction of the SIPA variants continued from 1945 into the early 1950s, with over 900 aircraft built in total between German Ar 396 production and French SIPA production—an extraordinary production run spanning two nations and two decades. This extended production testified to the soundness of the basic design and its continued relevance even as aviation technology advanced rapidly in the postwar period.\u003c\/p\u003e\n\u003cp\u003eThe French Air Force (Armée de l'Air) adopted the SIPA trainers for their flying schools, including the prestigious École de l'Air at Salon-de-Provence, where they trained a new generation of French military pilots during the crucial postwar reconstruction period and into the early Cold War era. The aircraft served alongside other French trainers, providing advanced instruction that prepared pilots for transition to jet aircraft and modern operational types.\u003c\/p\u003e\n\u003cp\u003eFrench-built SIPA aircraft also found extensive civilian roles with flying clubs (aéro-clubs) and private owners throughout France and French territories. The aircraft's sturdy construction, economical operation with readily available Renault engines, excellent handling characteristics, and suitability for aerobatic training made them popular for recreational flying, aerobatic competition, and civilian pilot training. Many French pilots who learned to fly in the postwar years received their advanced training in SIPA aircraft, continuing the type's training legacy well into the 1960s.\u003c\/p\u003e\n\u003cp\u003eThe manuals in this collection reflect this unique dual heritage. The German Ar 396 parts catalog (Ersatzteil-Liste) from 1944 represents authentic Luftwaffe documentation from the final year of the war, providing detailed component breakdowns and part numbers for the original German trainer. The French SIPA manuals—crew manual (Manuel de l'Équipage), elementary flight training manual (Pilotage Élémentaire), and workshop manual (Manuel d'Atelier)—document the aircraft's postwar French service and training procedures used at French military flight schools.\u003c\/p\u003e\n\u003cp\u003eToday, the Ar 396\/SIPA S.12 story exemplifies how exceptional aircraft design transcends political boundaries and historical circumstances. The aircraft's continued production and service in France—by the very nation Germany had occupied—stands as a remarkable testament to the universal recognition of engineering excellence and the pragmatic realities of postwar reconstruction. Several SIPA aircraft survive in museums and private collections, preserved as tangible links to this unique chapter in aviation history.\u003c\/p\u003e\n\u003cp\u003eThese original technical manuals, parts catalogs, and training materials represent authentic primary-source documentation used throughout the aircraft's service with both the German Luftwaffe and French Armée de l'Air. They provide invaluable insights into the construction, operation, maintenance procedures, and training methodologies associated with this historically significant aircraft that served two air forces across two decades. For historians, aviation researchers, restorers, and enthusiasts, these documents offer unparalleled reference material for understanding this remarkable aircraft and its unique place in aviation history.\u003c\/p\u003e\n\u003ch3\u003eManuals Included in This Collection\u003c\/h3\u003e\n\u003cp\u003e\u003cstrong\u003eGerman Documentation (Arado Ar 396):\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eArado Ar 396 A-1\/A-2 - Illustrated Parts Catalog - Ersatzteil-Liste\u003c\/strong\u003e - 1944 edition in German language featuring detailed component breakdowns, exploded-view diagrams, part numbers, and ordering information for the original German trainer variants—essential reference for understanding the aircraft's construction and for restoration projects\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eFrench Documentation (SIPA S.12\/S.121):\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eSIPA 12 and S.121 - Crew Manual - Manuel de l'Équipage\u003c\/strong\u003e - Comprehensive equipment manual in French language covering all aircraft systems, equipment operation, crew procedures, and operational guidance used by French Air Force training units\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSIPA 12 and S.121 - Elementary Flight Training Manual - Pilotage Élémentaire\u003c\/strong\u003e - French Air Force training manual used at École de l'Air and other flight schools for basic and advanced flight instruction, documenting training procedures, maneuvers, and instructional methods\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSIPA 12-121 - Parts Catalog and Workshop Manual - Manuel d'Atelier Avion\u003c\/strong\u003e - Workshop manual in French language with detailed parts listings, maintenance procedures, repair instructions, and technical specifications for French-built variants\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003eThis collection provides comprehensive technical coverage spanning both the German Ar 396 and French SIPA variants, documenting the aircraft's evolution from Luftwaffe trainer through postwar French production and service. The bilingual documentation (German and French) captures the unique dual heritage of this aircraft, providing essential reference material for understanding both the original German design and its French continuation. The documentation includes detailed specifications for airframe structure, Argus\/Renault powerplant operation, systems descriptions, parts information, maintenance procedures, and flight training methodologies—essential reference material for understanding the complete technical and operational scope of this historically significant training aircraft.\u003c\/p\u003e\n\u003ch3\u003eEngineering Norms and Standards\u003c\/h3\u003e\n\u003cp\u003eThe Arado Ar 396 was designed and constructed in accordance with German military aviation engineering standards and Luftwaffe technical requirements of the early 1940s, while the French SIPA variants were built to French military specifications and Armée de l'Air standards of the late 1940s and early 1950s.\u003c\/p\u003e\n\u003cp\u003eKey engineering standards and practices reflected in these manuals include:\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eGerman Luftwaffe Standards (Ar 396):\u003c\/strong\u003e Military technical documentation standards, training aircraft specifications, and manufacturing practices established by the Reichsluftfahrtministerium (RLM) for advanced trainer aircraft\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFrench Military Aviation Standards (SIPA):\u003c\/strong\u003e Postwar French military specifications, Armée de l'Air technical requirements, and documentation standards established for training aircraft during the reconstruction period\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eArado Engineering Practices:\u003c\/strong\u003e Company-specific design standards, manufacturing procedures, and quality control measures developed by Arado Flugzeugwerke—emphasizing robust construction, excellent handling characteristics, and ease of maintenance\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSIPA Manufacturing Standards:\u003c\/strong\u003e French production practices, quality control procedures, and adaptation of German designs to French manufacturing capabilities and available materials\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eArgus\/Renault Powerplant Integration:\u003c\/strong\u003e Engine installation practices and maintenance procedures for the Argus As 410 engine (German production) and Renault 12S engine (French license-built version)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTraining Aircraft Design Standards:\u003c\/strong\u003e Dual control installation, tandem cockpit layout, visibility requirements, spin recovery characteristics, and structural margins to withstand training operations—standards that remained consistent across both German and French production\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCross-Cultural Documentation:\u003c\/strong\u003e The transition from German technical documentation standards (Ersatzteil-Liste format) to French military documentation standards (Manuel de l'Équipage, Manuel d'Atelier formats)—reflecting different organizational approaches while documenting the same basic aircraft\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003eThese technical manuals reflect the unique dual heritage of this aircraft, documenting both German wartime engineering practices and French postwar adaptation and continuation of the design. The bilingual nature of the collection provides fascinating insight into how different military aviation cultures documented and operated the same basic aircraft design.\u003c\/p\u003e\n\u003cp\u003eFor researchers, historians, and technical enthusiasts, these documents represent authentic primary sources for understanding the design philosophy, construction methods, operational standards, and training practices that characterized both German and French military aviation during this pivotal period in aviation history.\u003c\/p\u003e\n\u003ch3\u003eFormat and Delivery\u003c\/h3\u003e\n\u003cp\u003e\u003cstrong\u003eFormat:\u003c\/strong\u003e High-resolution PDF digital download\u003cbr\u003e\n\u003cstrong\u003eLanguages:\u003c\/strong\u003e German (Ar 396 documentation) and French (SIPA documentation)\u003cbr\u003e\n\u003cstrong\u003eDelivery:\u003c\/strong\u003e Instant download link provided upon purchase\u003cbr\u003e\n\u003cstrong\u003eCompatibility:\u003c\/strong\u003e All devices and PDF readers\u003cbr\u003e\n\u003cstrong\u003eOrganization:\u003c\/strong\u003e Clearly labeled files organized by manufacturer and document type\u003c\/p\u003e\n\u003ch3\u003eDisclaimer\u003c\/h3\u003e\n\u003cp\u003eThis item is sold for historical and reference only. These are either original or copies of manuals and blueprints used when these aircraft were in active duty, now transferred into electronic format. These manuals and blueprints are not meant to be used for current update material for certification\/repair, but make an excellent reference for the scholar, collector, modeler or aircraft enthusiast. For proprietary reasons, we generally only provide civil manuals and blueprints on obsolete aircraft\/engines\/helicopters. The information is for reference only, and we do not guarantee the completeness, accuracy or currency of any manuals.\u003c\/p\u003e\n\u003cp\u003eReference herein to any specific commercial products by trade name, trademark, manufacturer, or otherwise, is not meant to imply or suggest any endorsement by, or affiliation with that manufacturer or supplier. All trade names, trademarks and manufacturer names are the property of their respective owners.\u003c\/p\u003e\n\u003cp\u003eThis digital compilation, structure, indexing and presentation are © Sicuro Publishing.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":52180738834779,"sku":null,"price":45.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/arado-ar-396-sipa-lb4-banner-1.png?v=1770459645"},{"product_id":"socata-rally-family-aircraft-manuals-collection-download","title":"SOCATA Rallye Family Aircraft Manuals Collection - Digital Download","description":"\u003ch3\u003eSOCATA Rallye Family Aircraft Manuals Collection\u003c\/h3\u003e\n\u003cp\u003eThis comprehensive digital collection provides essential technical documentation for the SOCATA Rallye family of aircraft, one of France's most successful and beloved light aircraft designs. Perfect for restorers, maintainers, pilots, historians, and aviation enthusiasts seeking authentic reference material for these iconic French touring aircraft.\u003c\/p\u003e\n\u003ch3\u003eManuals Included in This Collection\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eSOCATA Rallye 235 E Aircraft Flight Manual\u003c\/strong\u003e (English Language)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSOCATA Rallye MS.893 E Aircraft Flight Manual - Manuel de Vol de l'Avion\u003c\/strong\u003e (French Language)\u003c\/li\u003e\n\u003cli\u003e\u003cstrong\u003eSOCATA Rallye Aircraft Repair Manual\u003c\/strong\u003e\u003c\/li\u003e\n\u003cli\u003e\u003cstrong\u003eSOCATA Rallye Aircraft Service Letters, Service Bulletins and Technical Orders Manual\u003c\/strong\u003e\u003c\/li\u003e\n\u003cli\u003e\u003cstrong\u003eSOCATA Rallye Aircraft Illustrated Parts Catalog Manual\u003c\/strong\u003e\u003c\/li\u003e\n\u003cli\u003e\u003cstrong\u003eSOCATA Rallye Aircraft Maintenance Manual\u003c\/strong\u003e\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eHistorical Note: The SOCATA Rallye Legacy\u003c\/h3\u003e\n\u003cp\u003eThe SOCATA Rallye represents one of the most successful chapters in French light aircraft manufacturing. Originally designed by Morane-Saulnier in the late 1950s as the MS.880, the aircraft was conceived as a rugged, versatile touring and training aircraft that could operate from unprepared fields while offering excellent visibility and handling characteristics.\u003c\/p\u003e\n\u003cp\u003eThe design featured distinctive leading-edge slats that provided exceptional slow-flight characteristics and short-field performance, making the Rallye particularly popular for flight training, recreational flying, and glider towing operations. When SOCATA (Société de Construction d'Avions de Tourisme et d'Affaires) was formed in 1966 as part of Groupe Aérospatiale, the Rallye became the cornerstone of their light aircraft production.\u003c\/p\u003e\n\u003cp\u003eThroughout its production run from 1959 to 1983, the Rallye family evolved through numerous variants, including the MS.880, MS.885, MS.890, MS.892, and MS.893 series, with engines ranging from 100 to 235 horsepower. The aircraft proved remarkably versatile, serving as trainers, glider tugs, agricultural aircraft, and personal touring machines across Europe, Africa, and beyond. Over 3,300 Rallye aircraft were produced, making it one of France's most successful light aircraft exports.\u003c\/p\u003e\n\u003cp\u003eThe Rallye earned a distinguished reputation for its forgiving flight characteristics, robust construction, and ability to operate from rough airstrips. Its distinctive appearance, with high wings, generous glazing, and characteristic slats, made it instantly recognizable at airfields throughout the world. The aircraft became particularly popular in France, where it served as the primary trainer for countless pilots and remains a cherished classic among vintage aircraft enthusiasts.\u003c\/p\u003e\n\u003cp\u003eToday, hundreds of SOCATA Rallye aircraft remain in active service worldwide, treasured by owners for their reliability, economy, and delightful flying qualities. These original technical manuals represent the authentic documentation used throughout the aircraft's service life, providing invaluable reference material for current owners, restorers, and anyone maintaining these enduring French classics.\u003c\/p\u003e\n\u003ch3\u003eWhat You Receive\u003c\/h3\u003e\n\u003cp\u003eInstant digital download access to the complete SOCATA Rallye technical documentation collection in PDF format. These manuals preserve the original technical specifications, maintenance procedures, parts information, and operational guidance essential for understanding and maintaining these historic aircraft.\u003c\/p\u003e\n\u003ch3\u003eDisclaimer\u003c\/h3\u003e\n\u003cp\u003eThis item is sold for historical and reference only. These are either original or copies of manuals and blueprints used when these aircraft were in active duty, now transferred into electronic format. These manuals and blueprints are not meant to be used for current update material for certification or repair, but make an excellent reference for the scholar, collector, modeler or aircraft enthusiast. For proprietary reasons, we generally only provide civil manuals and blueprints on obsolete aircraft, engines, and helicopters. The information is for reference only, and we do not guarantee the completeness, accuracy or currency of any manuals.\u003c\/p\u003e\n\u003cp\u003eReference herein to any specific commercial products by trade name, trademark, manufacturer, or otherwise, is not meant to imply or suggest any endorsement by, or affiliation with that manufacturer or supplier. All trade names, trademarks and manufacturer names are the property of their respective owners.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":52182424060251,"sku":null,"price":50.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/socata-rallye-manuals-collection-lb4-banner-clean.png?v=1770473448"},{"product_id":"societe-des-moteurs-salmson-sms-aircraft-engines-manuals-collection-download","title":"Société des Moteurs Salmson Aircraft Engine Manuals Collection - Digital Download","description":"\u003cp\u003eThis collection brings together the essential technical documentation for the legendary Salmson 9-cylinder radial engine family — from the pioneering water-cooled WWI variants to the celebrated air-cooled 9AD that powered the light aircraft movement of the 1920s and 1930s. Produced by the Société des Moteurs Salmson of Billancourt, France, these engines represent a pivotal chapter in aviation engineering history, and this structured collection makes their documentation accessible to historians, restorers, and vintage aviation enthusiasts worldwide.\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003eDefinitive Collection with Free Lifetime Updates:\u003c\/strong\u003e This is a living collection that we continuously expand and refine. As we acquire additional Salmson documentation, technical bulletins, or variant-specific materials, we update this collection and provide free lifetime updates to all purchasers. Your one-time purchase guarantees access to all future additions and improvements to this collection.\u003c\/p\u003e\n\n\u003ch2\u003eHistorical Note\u003c\/h2\u003e\n\u003cp\u003eThe Salmson engine lineage traces its origins to the Canton-Unné patents of 1909, which introduced a uniquely elegant water-cooled radial layout combined with an epicyclic gear system — a design that eliminated the traditional master\/slave rod arrangement and delivered exceptionally smooth power delivery. The company, formally known as the Société des Moteurs Salmson and headquartered in Billancourt, France, began producing aero engines in 1911.\u003c\/p\u003e\n\u003cp\u003eDuring the First World War, the 9Z and 9B variants — producing between 230 and 260 hp — became among the most successful stationary radial engines of the conflict, powering reconnaissance aircraft such as the Salmson 2 A.2 and various Caudron and Farman types. Approximately 3,000 units of the 9Z alone were produced in France, with licensed production also undertaken by British Salmson and Dudbridge Iron Works in the United Kingdom.\u003c\/p\u003e\n\u003cp\u003eAfter the war, Salmson pivoted decisively toward the emerging light aircraft market. The 9AD — a compact, air-cooled 9-cylinder radial producing 40–55 hp — became a defining engine of the interwar light plane movement. It powered aircraft including the Klemm L.25, Caudron C.109, Jodel D.11, and the American Eaglet, and was associated with numerous record-breaking distance and altitude flights throughout the late 1920s. Production continued until the company's liquidation in 1951, with total output across all variants reaching several thousand units.\u003c\/p\u003e\n\u003cp\u003eToday, rare examples of the Salmson 9AD survive in airworthy condition in restored Klemm L.25s and some vintage French homebuilts, while the majority of surviving engines are preserved as static displays in institutions such as the National Air and Space Museum.\u003c\/p\u003e\n\n\u003ch2\u003eManuals Included in This Collection\u003c\/h2\u003e\n\u003cul\u003e\n\u003cli\u003eSalmson AD 9 40 PS — Aircraft Aero Operation and Maintenance Manual — Betrieb und Unterhaltung (German Language)\u003c\/li\u003e\n\u003cli\u003eSalmson M 9 — Aircraft Aero Engine Technical Manual (Italian Language)\u003c\/li\u003e\n\u003cli\u003eSalmson M 7 \/ M 9 — Aircraft Aero Engine Technical Manual (French Language)\u003c\/li\u003e\n\u003cli\u003eSalmson A9 \/ R9 — Aircraft Aero Engine Technical Manual (French Language)\u003c\/li\u003e\n\u003cli\u003eSalmson 9 Zm — Aircraft Aero Engine Description Manual (French Language)\u003c\/li\u003e\n\u003cli\u003eSalmson 9 Zm — Aircraft Aero Engine Technical Manual (French Language)\u003c\/li\u003e\n\u003cli\u003eSalmson 9 AD — Aircraft Aero Engine Technical Manual (French Language)\u003c\/li\u003e\n\u003cli\u003eSalmson 9 AB — Aircraft Engine Technical Manual (French Language)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003eThis collection spans the full Salmson 9-cylinder family, covering water-cooled WWI variants (9Z, 9B, M7, M9) through to the iconic air-cooled interwar types (9AD, 9AB, 9Zm, A9, R9). Documentation is presented in the original languages of publication — French, German, and Italian — reflecting the broad international reach of Salmson engines across European aviation.\u003c\/p\u003e\n\n\u003ch2\u003eEngineering Norms and Standards\u003c\/h2\u003e\n\u003cp\u003eSalmson engines were designed and manufactured to French military aviation standards of the WWI and interwar periods, including specifications issued by the Service Technique de l'Aéronautique (STAé). The Canton-Unné epicyclic gear system was a proprietary engineering solution that distinguished Salmson designs from contemporary rotary and inline engines, and the manuals in this collection document the specific tolerances, assembly procedures, and maintenance practices associated with this unique architecture. Licensed variants produced in the UK by British Salmson and Dudbridge Iron Works adhered to equivalent British Air Ministry standards of the period.\u003c\/p\u003e\n\n\u003ch2\u003eTechnical Specifications — Salmson 9AD (Representative Example)\u003c\/h2\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eEngine type:\u003c\/strong\u003e Air-cooled radial (early models water-cooled)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eConfiguration:\u003c\/strong\u003e 9 cylinders, single-row radial\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDisplacement:\u003c\/strong\u003e 182 cu in (3.0 L) — 9AD; 1,112 cu in (18.2 L) — 9Z\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eHorsepower range:\u003c\/strong\u003e 40 hp (9AD) to 260 hp (9Z)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eBore and stroke:\u003c\/strong\u003e 2.75 × 3.375 in (9AD)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCompression ratio:\u003c\/strong\u003e Approximately 5.6:1 to 6:1 depending on variant\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eWeight:\u003c\/strong\u003e 154 lbs (9AD) to 473 lbs (9Z)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFuel type:\u003c\/strong\u003e Aviation gasoline (standard low-octane for the era)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNotable engineering feature:\u003c\/strong\u003e Canton-Unné epicyclic gear system for exceptionally smooth power delivery\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003ch2\u003eWhere to Find Additional Documentation\u003c\/h2\u003e\n\u003cp\u003e\u003cstrong\u003eHistorical Archives:\u003c\/strong\u003e The Musée de l'Air et de l'Espace (Le Bourget, France) holds archival materials related to Salmson aircraft and engines. The Vintage Aero Flying Museum and the National Air and Space Museum (Washington D.C.) preserve static examples. Type-specific communities such as the Klemm Flugzeugbau enthusiast networks and French homebuilt aviation forums (notably those associated with Jodel and Caudron types) are valuable sources for operational knowledge and surviving documentation.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eSpecialty Vendors:\u003c\/strong\u003e Online Aviation Library continues to expand its coverage of early French aero engines. Additional documentation for related manufacturers — including Gnome-Rhône, Lorraine, and Hispano-Suiza — is available in our catalog.\u003c\/p\u003e\n\n\u003ch2\u003eFormat and Delivery\u003c\/h2\u003e\n\u003cp\u003eAll manuals are delivered as high-resolution PDF files, optimized for both screen reading and print. Files are organized by variant and document type for straightforward navigation. Instant download upon purchase — no shipping required.\u003c\/p\u003e\n\n\u003ch2\u003eDisclaimer\u003c\/h2\u003e\n\u003cp\u003eThese documents are provided for historical reference and research purposes only. The Société des Moteurs Salmson was liquidated in 1951; no current Type Certificate holder exists for these engines. For any airworthy Salmson engine, consult qualified vintage aviation authorities and applicable experimental or vintage aircraft regulations in your jurisdiction. Trade names and designations are used for identification purposes only. Copyright © Sicuro Publishing.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":52788449542491,"sku":null,"price":49.99,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/salmson-promotional-banner-engine-logo-square.png?v=1775831899"},{"product_id":"hispano-suiza-8-12-series-aircraft-engine-manuals-collection-digital-download","title":"Hispano-Suiza 8 \u0026 12 Series Aircraft Engine Manuals Collection - Digital Download","description":"\u003cp\u003eThe Hispano-Suiza 8 and 12 series represent two of the most historically significant aircraft engine families ever produced — the V8 that powered Allied air superiority in the First World War, and the V12 descendants that equipped the finest French fighters of the Second. This collection brings together fourteen original technical manuals covering both families, sourced from French, American, and Finnish military archives and presented as high-quality digital downloads.\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003eDefinitive Collection with Free Lifetime Updates:\u003c\/strong\u003e This is a living collection that we continuously expand and refine. As we acquire additional Hispano-Suiza documentation, technical bulletins, or variant-specific materials, we update this collection and provide free lifetime updates to all purchasers. Your one-time purchase guarantees access to all future additions and improvements to this collection.\u003c\/p\u003e\n\n\u003ch2\u003eHistorical Note\u003c\/h2\u003e\n\u003cp\u003eThe Hispano-Suiza 8 was designed by Swiss engineer Marc Birkigt and first flew in February 1915. Drawing on his pre-war experience with automobile V8 engines, Birkigt created what became the most widely used liquid-cooled aero engine of the Entente Powers — often called the \"Rolls-Royce Merlin of World War I.\" Produced under licence in France, Britain, the United States, Italy, and Russia, approximately 49,893 units were built. The engine powered the SPAD VII, SPAD XIII, S.E.5a, Sopwith Dolphin, and Curtiss JN-4H, among others, and was instrumental in restoring Allied air superiority over the Western Front from 1916 onward.\u003c\/p\u003e\n\u003cp\u003eThe 8A produced 140–150 hp; the 8Ab raised this to 180 hp through increased compression; the geared 8B reached 200–235 hp; and the enlarged 8F achieved 300 hp for bomber applications. The 8C introduced the celebrated \u003cem\u003emoteur-canon\u003c\/em\u003e configuration, firing a 37 mm cannon through the propeller shaft — a concept Birkigt would refine further in the 12Y. Post-war, surplus Hispano-Suiza 8 engines powered barnstorming tours, airmail routes, and air racing circuits across Europe and North America.\u003c\/p\u003e\n\u003cp\u003eThe Hispano-Suiza 12 series emerged in the early 1930s as a 60° V12 evolution of the same engineering philosophy. The 12Y, displacing 36 litres and producing 860–1,000+ hp with a supercharger, became the standard high-performance powerplant of the \u003cem\u003eArmée de l'Air\u003c\/em\u003e at the outbreak of WWII, equipping the Morane-Saulnier M.S. 406, Dewoitine D.520, and Arsenal VG-33. The 12X and 12H variants served in earlier inter-war applications, while the 12Ha (450 hp) and 12Hb (500 hp) bridged the gap between the two generations.\u003c\/p\u003e\n\n\u003ch2\u003eManuals Included in This Collection\u003c\/h2\u003e\n\u003cul\u003e\n\u003cli\u003eHispano-Suiza 12 Y-31 Aircraft Engine — \u003cem\u003eNotice Technique Manuel\u003c\/em\u003e (French)\u003c\/li\u003e\n\u003cli\u003eHispano-Suiza 12 Y Aircraft Engine — Instruction Book (French)\u003c\/li\u003e\n\u003cli\u003eHispano-Suiza 300–330 CV Aircraft Engine — Parts Catalog (French)\u003c\/li\u003e\n\u003cli\u003eHispano-Suiza 12 H Aircraft Engine — Maintenance Manual \u0026amp; Instruction Book (French)\u003c\/li\u003e\n\u003cli\u003eHispano-Suiza 12 Ha 450 \/ Hb 500 Aircraft Engine — Technical Manual \u0026amp; Instruction Book (French)\u003c\/li\u003e\n\u003cli\u003eHispano-Suiza 12 X Aircraft Engine — Maintenance Manual \u0026amp; Instruction Book (French)\u003c\/li\u003e\n\u003cli\u003eHispano-Suiza 12 Y Aircraft Engine — Maintenance Manual \u0026amp; Instruction Book (French)\u003c\/li\u003e\n\u003cli\u003eWright-Martin Hispano-Suiza A-I and E Aircraft Engine — Maintenance Manual \u0026amp; Instruction Book (English, 1918)\u003c\/li\u003e\n\u003cli\u003eWright–Hispano-Suiza 8 150 Aircraft Engine — Maintenance Manual \u0026amp; Instruction Book (French)\u003c\/li\u003e\n\u003cli\u003eHispano-Suiza 8 Aircraft Engine — Technical Manual (French)\u003c\/li\u003e\n\u003cli\u003eHispano-Suiza 8 300 CV Aircraft Engine — Maintenance Manual \u0026amp; Instruction Book (French)\u003c\/li\u003e\n\u003cli\u003eHispano-Suiza 8 150\/180\/200 Aircraft Engine — Maintenance Manual \u0026amp; Instruction Book (French)\u003c\/li\u003e\n\u003cli\u003eHispano-Suiza 8 150 Aircraft Engine — Maintenance Manual \u0026amp; Instruction Book (French)\u003c\/li\u003e\n\u003cli\u003eHispano-Suiza 12Y-31 \/ M-103 A \/ M-105 Aircraft Engine — Structural Description, Operating \u0026amp; Maintenance Instructions (\u003cem\u003eRakenneselostus, käyttö- ja huoltoohjeet\u003c\/em\u003e) (Finnish, 1943) — Valtion Lentokonetehdas\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003cp\u003eThis collection spans the full arc of Hispano-Suiza aero engine development from the 8A of 1915 through the supercharged 12Y of the late 1930s, including its Soviet derivatives M-103 A and M-105 as documented by Finnish military aviation in 1943. Twelve of the fourteen manuals are in French — the original language of the manufacturer and the primary operator — with one American manual in English covering the Wright-Martin licensed variant, and one Finnish-language manual compiled by Valtion Lentokonetehdas (State Aircraft Factory) in Tampere in February 1943.\u003c\/p\u003e\n\n\u003ch2\u003eEngineering Norms and Standards\u003c\/h2\u003e\n\u003cp\u003eHispano-Suiza engines were designed and manufactured to French military aviation standards (\u003cem\u003eService Technique de l'Aéronautique\u003c\/em\u003e) and, for licensed variants, to British Air Board and U.S. Army Signal Corps specifications. The 8 series introduced several engineering firsts: cast aluminium cylinder blocks with screwed-in steel liners, single overhead camshaft (SOHC) valve actuation, and propeller reduction gearing (8B). Bore and stroke for the 8A\/8B were 120 mm × 130 mm (displacement 11.76 L); the 8F used 140 mm × 150 mm (18.5 L). Compression ratios ranged from 4.7:1 (8A) to 5.3:1 (8Ab\/8B). The 12Y operated at a 36-litre displacement with a single-stage supercharger and retained the \u003cem\u003emoteur-canon\u003c\/em\u003e capability. All variants used liquid (water\/glycol) cooling and petrol fuel.\u003c\/p\u003e\n\n\u003ch2\u003eFormat and Delivery\u003c\/h2\u003e\n\u003cp\u003eAll manuals are delivered as high-resolution PDF files, optimised for both screen reading and printing. Files are clearly named by document type and variant. Instant download upon purchase — no shipping, no waiting. Compatible with all PDF readers on desktop, tablet, and mobile devices.\u003c\/p\u003e\n\n\u003ch2\u003eDisclaimer\u003c\/h2\u003e\n\u003cp\u003eThese documents are provided for historical reference and research purposes only. They do not constitute airworthiness guidance for any currently certificated aircraft or engine. Always consult current manufacturer documentation and applicable regulatory authorities for any maintenance activity. Trade names and designations are the property of their respective owners. Copyright © Sicuro Publishing.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":52788902101339,"sku":null,"price":69.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/hispano-suiza-sepia-gold-liberty-lb4-1.png?v=1775842527"},{"product_id":"socata-tbm-700a-camsis-2-maintenance-technical-documentation","title":"SOCATA TBM-700A — CAMSIS-2 Maintenance \u0026 Technical Documentation","description":"\u003ch3\u003eSOCATA TBM-700A — Primary-Source Maintenance \u0026amp; Technical Documentation\u003c\/h3\u003e\n\u003cp\u003eThe \u003cstrong\u003eSOCATA TBM-700A\u003c\/strong\u003e is a pressurized single-engine turboprop built to the highest standards of French aerospace engineering — combining PT6A-64 turbine performance with a fully pressurized cabin, retractable gear, and a capable avionics suite. With approximately 800–900 TBM 700-series aircraft delivered worldwide, this platform has one of the strongest owner\/operator communities in business turboprop aviation.=\u003c\/p\u003e\n\u003cp\u003eThis collection delivers the original \u003cstrong\u003eEADS SOCATA\u003c\/strong\u003e factory documentation for the TBM-700A in the native \u003cstrong\u003eSOCATA Interactive Technical Publications\u003c\/strong\u003e format — the structured, ATA-chapter-navigable system developed and issued by SOCATA's own technical publications department. \u003cstrong\u003eIssue 2, April 2001.\u003c\/strong\u003e This is the original interactive HTML archive as distributed by EADS SOCATA on DVD — not a PDF scan, not a reformatted document.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eNot endorsed by, affiliated with, or authorized by SOCATA, DAHER, EADS, or any manufacturer or regulatory authority. These are archival, static-copy documents.\u003c\/strong\u003e\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eDocument Manifest — EADS SOCATA Interactive Technical Publications, Issue 2 · April 2001\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eMaintenance Manual (MM)\u003c\/strong\u003e — ATA chapters 04–57, full airframe systems coverage\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTool \u0026amp; Equipment Manual\u003c\/strong\u003e — specialized tooling and ground support equipment\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eIllustrated Parts Catalog (IPC)\u003c\/strong\u003e — exploded views, part numbers, effectivity codes\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eWiring Manual\u003c\/strong\u003e — electrical schematics, wire routing, connector data\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eService Bulletins\u003c\/strong\u003e — manufacturer-issued SB archive\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eService Letters\u003c\/strong\u003e — SOCATA\/EADS service correspondence archive\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cem\u003eNavigation: Table of Contents · List of Effective Pages · List of Service Bulletins · List of Effective Pages Index · List of Revision Recording · List of Revised Pages · List of Effective Temporary Revisions · Introduction · List of Publications\u003c\/em\u003e\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eTechnical Profile — TBM-700A\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003ePowerplant:\u003c\/strong\u003e Pratt \u0026amp; Whitney Canada PT6A-64, flat-rated to 700 SHP\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMaximum Speed:\u003c\/strong\u003e 330 KTAS at FL280\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eService Ceiling:\u003c\/strong\u003e 31,000 ft (pressurized)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eRange:\u003c\/strong\u003e ~1,730 nm (standard fuel)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCabin Pressurization:\u003c\/strong\u003e 6.0 psi differential\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eLanding Gear:\u003c\/strong\u003e Electrically actuated retractable tricycle\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eOriginal Manufacturer:\u003c\/strong\u003e SOCATA \/ EADS SOCATA, Tarbes, France\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eType Certificate Holder:\u003c\/strong\u003e DAHER (successor to SOCATA\/EADS SOCATA)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePublication:\u003c\/strong\u003e Issue 2, April 2001 — EADS SOCATA Interactive Technical Publications\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003cp\u003e⚠️ \u003cstrong\u003eRegulatory Notice:\u003c\/strong\u003e Under FAA 14 CFR § 43.13 and EASA Part-M, any mechanic performing maintenance on an active aircraft must use current, manufacturer-approved revision-controlled data. This archival document does not satisfy that requirement.\u003c\/p\u003e\n\u003cp\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorized distributor.\u003c\/p\u003e\n\u003cp\u003e\u003cem\u003eLiving Collections with Free Lifetime Updates — Please review our \u003ca href=\"\/pages\/disclaimer\"\u003eDisclaimer\u003c\/a\u003e and \u003ca href=\"\/pages\/export-notice\"\u003eExport Notice\u003c\/a\u003e before purchasing.\u003c\/em\u003e\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53462848602459,"sku":null,"price":79.85,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/hero-banner-socata-tbm-700a.png?v=1782665743"},{"product_id":"gnome-rhone-type-14m-mars-aircraft-engine-manual-collection","title":"Gnome-Rhône Type 14M \"Mars\" Aircraft Engine — Manual Collection","description":"\u003ch3\u003eGnome-Rhône Type 14M \"Mars\" Aircraft Engine — Manual Collection\u003c\/h3\u003e\n\u003cp\u003e\u003cstrong\u003eVariants covered:\u003c\/strong\u003e Series 0 to 35 \u0026amp; Series 48 to 49  |  \u003cstrong\u003eTotal documents:\u003c\/strong\u003e 5  |  \u003cstrong\u003eLanguages:\u003c\/strong\u003e French, German\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003e📋 Document Manifest\u003c\/h3\u003e\n\u003ch4\u003eVariant: Series 0 to 35 — 4 Documents\u003c\/h4\u003e\n\u003cp\u003e\u003cstrong\u003eType 14M (0 to 35) Engine Handbook\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eType 14M series 0 to 35 Aircraft Engine – Technical Manual, 1940 — \u003cem\u003eNotice Technique\u003c\/em\u003e (French)\u003c\/li\u003e\n\u003cli\u003eType 14M series 4 to 11 Aircraft Engines Technical Notice — \u003cem\u003eNotice Technique des Moteurs d'Aviation Gnome-Rhône Type 14M\u003c\/em\u003e (French)\u003c\/li\u003e\n\u003cli\u003eType 14M series 4 to 7 Engine Handbook Extract — \u003cem\u003eAuszug aus dem Motorenhandbuch\u003c\/em\u003e (German)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eType 14M (0 to 35) Operating and Maintenance\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eType 14M series 4 to 11 Aircraft Engine – Operating Manual, 1940 — \u003cem\u003eBetriebshandbuch der Flugmotoren\u003c\/em\u003e (German)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch4\u003eVariant: Series 48 to 49 — 1 Document\u003c\/h4\u003e\n\u003cp\u003e\u003cstrong\u003eType 14M (48 to 49) Technical Reports \u0026amp; Certificates\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eType 14M series 48, 49 Aircraft Engine – Engine Data Card, 1942 — \u003cem\u003eMotoren-Karte\u003c\/em\u003e (German)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003e⚙️ Engine Overview\u003c\/h3\u003e\n\u003cp\u003eThe \u003cstrong\u003eGnome-Rhône 14M \"Mars\"\u003c\/strong\u003e is a 14-cylinder, two-row air-cooled radial engine developed by Société des Moteurs Gnome et Rhône (France), first introduced in 1937. Derived as a compact, reduced-frame variant of the 14K Mistral Major, it was engineered to replace older single-row engines while minimizing frontal area for twin-engine airframes.\u003c\/p\u003e\n\u003ch3\u003e✈️ Primary Aircraft Applications\u003c\/h3\u003e\n\u003cp\u003e\u003cstrong\u003eMilitary:\u003c\/strong\u003e Henschel Hs 129 B, Potez 631\/633, Gotha Go 244 B, Breguet 693, Hanriot H.220, Morane-Saulnier MS.472\u003cbr\u003e\u003cstrong\u003eCivilian:\u003c\/strong\u003e Potez 670 and pre-war French light transport\/postal prototypes\u003c\/p\u003e\n\u003ch3\u003e🔧 Technical Specifications\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eConfiguration:\u003c\/strong\u003e 14-cylinder, two-row radial\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDisplacement:\u003c\/strong\u003e 18.92 litres (1,154.6 cu in)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePower output:\u003c\/strong\u003e 570–710 hp (peak ~820 hp, late military variants)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eBore × Stroke:\u003c\/strong\u003e 122 mm × 116 mm\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCompression ratio:\u003c\/strong\u003e 6.5:1\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDry weight:\u003c\/strong\u003e 419 kg (924 lbs)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFrontal diameter:\u003c\/strong\u003e 950 mm (37.4 in) — notably compact for a 14-cylinder radial\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFuel:\u003c\/strong\u003e 87-octane aviation gasoline\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSupercharger:\u003c\/strong\u003e Single-stage, single-speed centrifugal\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eReduction gear:\u003c\/strong\u003e Planetary system\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003e📅 Production \u0026amp; History\u003c\/h3\u003e\n\u003cp\u003eProduction ran from 1937 to 1944, continuing under German occupation of France. Estimated output: 2,000+ units. Following the 1940 armistice, production was seized by Germany, making the 14M the definitive powerplant for the Luftwaffe's Henschel Hs 129 B tank-buster. Post-war use was limited to trainers such as the MS.472 Vanneau, phased out by the early 1950s.\u003c\/p\u003e\n\u003ch3\u003e🏛️ Current Status\u003c\/h3\u003e\n\u003cp\u003eNo longer in active service. The original Type Certificate holder (Gnome-Rhône) was nationalized in 1945 to form SNECMA, now part of the Safran Group. Surviving examples are held as static museum exhibits at the Smithsonian National Air and Space Museum and the Musée de l'Air et de l'Espace, Paris.\u003c\/p\u003e\n\u003chr\u003e\n\u003cp\u003e⚠️ \u003cstrong\u003eRegulatory Notice:\u003c\/strong\u003e Under FAA 14 CFR § 43.13 and EASA Part-M, any mechanic performing maintenance on an active aircraft must use current, manufacturer-approved revision-controlled data. This archival document does not satisfy that requirement.\u003c\/p\u003e\n\u003cp\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorized distributor.\u003c\/p\u003e\n\u003cp\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53492552532315,"sku":null,"price":49.85,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/promotional-gnome-rh-ne-14m-with-title.png?v=1783008630"},{"product_id":"bristol-gnome-rhone-jupiter-series-v-vi-viii-ix-xi","title":"Bristol \/ Gnome-Rhône Jupiter Series V, VI, VIII, IX, XI — Historical \u0026 Technical Documentation","description":"\u003ch3\u003eBristol Jupiter \/ Gnome-Rhône 9A Jupiter — Series V, VI, VIII, IX \u0026amp; XI\u003c\/h3\u003e\n\u003cp\u003eThe Bristol Jupiter is one of the most consequential aero-engines of the twentieth century — a nine-cylinder, air-cooled radial that defined the interwar era and powered the first generation of European commercial airliners. Designed by Roy Fedden at Cosmos Engineering during the final months of the First World War and brought to production maturity by the Bristol Aeroplane Company from 1921, the Jupiter was the first production aero-engine in the world to feature \u003cstrong\u003efour overhead valves per cylinder\u003c\/strong\u003e — a configuration that became the industry standard.\u003c\/p\u003e\n\u003cp\u003eIn France, the engine was manufactured under licence by \u003cstrong\u003eSociété des Moteurs Gnome-Rhône\u003c\/strong\u003e from 1923, marketed as the \u003cstrong\u003eGnome-Rhône 9A Jupiter\u003c\/strong\u003e. In the Soviet Union, it was licence-built by \u003cstrong\u003eArkady Shvetsov's bureau\u003c\/strong\u003e and designated the \u003cstrong\u003eM-22\u003c\/strong\u003e — a direct copy of the Bristol Jupiter used in aircraft including the Polikarpov I-5 and Tupolev ANT-9. Across seventeen international licensees — including Alfa Romeo (Italy), Nakajima (Japan), and Shvetsov (USSR) — roughly \u003cstrong\u003e10,000 units\u003c\/strong\u003e were produced globally, making the Jupiter one of the most widely manufactured aero-engines of its generation.\u003c\/p\u003e\n\u003cp\u003e\u003cem\u003eNote on this collection: The Gnome-Rhône Jupiter variants (Series V and VI), the Serbian-edition direct-drive catalog, and the Soviet M-22 document are all licence-built or licence-derived versions of the original British Bristol Jupiter engine. They represent different national adaptations of the same base design, all documented within this collection.\u003c\/em\u003e\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eDocument Manifest — 10 Primary-Source Documents\u003c\/h3\u003e\n\u003ch4\u003eAir Ministry Descriptive Handbooks (English)\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eAP 1278\u003c\/strong\u003e — Jupiter Series VI Aero Engine. Descriptive Handbook. Air Ministry. 1st Edition, March 1927. Published September 1927. H.M. Stationery Office, London. Price 2s. 6d. Net.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAP 1871\u003c\/strong\u003e — Bristol Jupiter Series VIII \u0026amp; IX Aero Engines. Descriptive Handbook. Air Ministry. 1st Edition, July 1929. Published December 1929. H.M. Stationery Office, London. Price 3s. 6d. Net. Ref. 22-104.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAP 1417, Volume I\u003c\/strong\u003e — Jupiter VIII F., VIII F.P., XI F. \u0026amp; XI F.P. Aero Engines. Descriptive Handbook. Air Ministry. 2nd Edition, August 1932. Published October 1932. H.M. Stationery Office, London. Price 5s. 0d. Net. Ref. 22-124.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch4\u003eIllustrated Parts Catalogs\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eGnome \u0026amp; Rhône Jupiter Série V\u003c\/strong\u003e — \u003cem\u003eNomenclature Photographique des Pièces Détachées des Moteurs d'Aviation\u003c\/em\u003e [French]. Société des Moteurs “Gnome \u0026amp; Rhône”, 34 Rue de Lisbonne, Paris (8e). R.C. Seine 176.707.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eGnome \u0026amp; Rhône Jupiter Série VI — Copy 1\u003c\/strong\u003e — \u003cem\u003eNomenclature Photographique des Pièces Détachées des Moteurs d'Aviation\u003c\/em\u003e [French]. Prise Directe: 9 Aex 480 cv \/ 9 Ae 480 cv \/ 9 Ady 420 cv \/ 9 Ad 420 cv. Démultiplié Réducteur II: 9 Akx 480 cv. Société des Moteurs “Gnome \u0026amp; Rhône”, Paris. R.C. Seine 178.707.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eGnome \u0026amp; Rhône Jupiter Série VI — Copy 2\u003c\/strong\u003e — \u003cem\u003eNomenclature Photographique des Pièces Détachées des Moteurs d'Aviation\u003c\/em\u003e [French]. Identical specification to Copy 1; separate print run (orange cover). Société des Moteurs “Gnome \u0026amp; Rhône”, Paris. R.C. Seine 178.707.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eГном-Рон Јупитер — Непосредан пренос\u003c\/strong\u003e — \u003cem\u003eНоменклатура појединих делова аеропланских мотора са сликама\u003c\/em\u003e [Serbian]. Gnome-Rhône Jupiter, Direct Drive — Illustrated Parts Catalog. Земун: Штампарија М. Млађана, 1929.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eM-22 (Bristol Jupiter — Soviet Licence Build)\u003c\/strong\u003e — Russian-language technical document [Cyrillic script]. The M-22 is a direct Soviet licence copy of the Bristol Jupiter, produced under Shvetsov's bureau designation. Publisher details as visible on cover.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch4\u003eOperation \u0026amp; Maintenance Manuals\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eGnome \u0026amp; Rhône Jupiter\u003c\/strong\u003e — \u003cem\u003eManuel pour la Conduite et l'Entretien des Moteurs d'Aviation Gnome \u0026amp; Rhône Jupiter\u003c\/em\u003e [French]. Prix: 20 Francs. [Series not specified on cover.]\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eGnome Rhône Jupiter Série VI\u003c\/strong\u003e — \u003cem\u003eNotice Technique pour la Conduite et l'Entretien des Moteurs d'Aviation\u003c\/em\u003e [French]. Prise directe (420 CV et 480 CV) \/ Démultiplié (480 CV). Société des Moteurs Gnome et Rhône, 34 Rue de Lisbonne, Paris (8e). Rég. Com. Seine 176.707.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eTotal documents in this collection: 10\u003c\/strong\u003e\u003cbr\u003e\u003cem\u003eLanguages represented: English, French, Serbian, Russian\u003c\/em\u003e\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eHistorical Information\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eFirst introduction:\u003c\/strong\u003e 1918 (Cosmos design) \/ 1921 (Bristol production) \/ 1923 (Gnome-Rhône licence)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eManufacturers:\u003c\/strong\u003e Cosmos Engineering; Bristol Aeroplane Company (UK); Société des Moteurs Gnome-Rhône (France); Shvetsov bureau (USSR — M-22, direct licence copy)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDesign origin:\u003c\/strong\u003e Evolved from the experimental Cosmos Jupiter by Roy Fedden\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMilitary applications:\u003c\/strong\u003e Bristol Bulldog, Westland Wapiti, Junkers W.34, Dornier Do X, Polikarpov I-5 (M-22)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCivil applications:\u003c\/strong\u003e Handley Page H.P.42, de Havilland Giant Moth, de Havilland Hercules, Tupolev ANT-9 (M-22)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eProduction period:\u003c\/strong\u003e 1921 to early 1930s (superseded by the Bristol Pegasus)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTotal production:\u003c\/strong\u003e ~10,000 units across 17 international licensees\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eOperational significance:\u003c\/strong\u003e Regarded as one of the most reliable aero-engines of the interwar period; powered many of the first European commercial airliners and military bombers\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePost-service fate:\u003c\/strong\u003e Progressively replaced by the Bristol Mercury and Gnome-Rhône 14K Mistral Major; surviving examples relegated to regional mail and light cargo before complete obsolescence\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eTechnical Specifications\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eEngine type:\u003c\/strong\u003e Air-cooled, single-row radial\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCylinders:\u003c\/strong\u003e 9\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDisplacement:\u003c\/strong\u003e 1,747 cu in (28.6 litres)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePower output:\u003c\/strong\u003e 420 hp – 580 hp (variant-dependent)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eBore × Stroke:\u003c\/strong\u003e 5.75 in (146 mm) × 7.48 in (190 mm)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCompression ratio:\u003c\/strong\u003e 5.3:1 – 6.5:1\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eWeight:\u003c\/strong\u003e 730 lb (direct drive) – 836 lb (geared)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFuel:\u003c\/strong\u003e Aviation gasoline (~80 octane)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNotable engineering:\u003c\/strong\u003e 4 overhead valves per cylinder; BTH SC9-1 magnetos; cast-aluminium crankcase\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch4\u003eSeries Covered in This Collection\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eSeries V\u003c\/strong\u003e — early production direct-drive variant\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSeries VI (9AD)\u003c\/strong\u003e — refined direct-drive; primary export and licence baseline. Sub-variants: 9 Aex \/ 9 Ae (480 cv, 2000 t\/m), 9 Ady \/ 9 Ad (420 cv, 1750 t\/m), 9 Akx geared (480 cv, 1000 t\/m)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSeries VIII \/ VIII F. \/ VIII F.P.\u003c\/strong\u003e — uprated output; F = supercharged, F.P. = supercharged geared\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSeries IX\u003c\/strong\u003e — geared variant; improved propeller efficiency at altitude\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSeries XI F. \/ XI F.P.\u003c\/strong\u003e — highest-output Jupiter production variants; supercharged and supercharged-geared\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eM-22\u003c\/strong\u003e — Soviet licence-built direct copy; Shvetsov bureau designation for the Bristol Jupiter\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eCurrent Status\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eStill flying:\u003c\/strong\u003e No\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eType Certificate holder:\u003c\/strong\u003e Obsolete \/ Historical (formerly Cosmos Engineering, Bristol Aeroplane Company, Snecma\/Safran)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eActive Service Bulletins \/ ADs:\u003c\/strong\u003e None\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePrimary use today:\u003c\/strong\u003e Museum display and historical research\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003cp\u003e⚠️ \u003cstrong\u003eRegulatory Notice:\u003c\/strong\u003e Under FAA 14 CFR § 43.13 and EASA Part-M, any mechanic performing maintenance on an active aircraft must use current, manufacturer-approved revision-controlled data. This archival document does not satisfy that requirement.\u003c\/p\u003e\n\u003cp\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorised distributor.\u003cbr\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53559248421211,"sku":null,"price":48.85,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/bristol-jupiter-portrait-banner.png?v=1783659702"},{"product_id":"socata-tb-20-trinidad-master-documentation-collection","title":"SOCATA TB-20 Trinidad — Master Documentation Collection","description":"\u003ch3\u003eSOCATA TB-20 Trinidad — Master Documentation Collection\u003c\/h3\u003e\n\u003cp\u003eThe most comprehensive archival documentation package available for the \u003cstrong\u003eSOCATA TB-20 Trinidad\u003c\/strong\u003e — 15 official EADS\/SOCATA documents in a single Living Collection. From the cockpit to the last structural fastener, from the wiring bus to the parts catalog: this is the definitive factory library for one of France's finest high-performance touring aircraft.\u003c\/p\u003e\n\u003ch3\u003eCollection Manifest — 15 Documents\u003c\/h3\u003e\n\u003ch4\u003ePilot's Information Manual (PIM) — 1 Document\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eTB-20 Pilot's Information Manual\u003c\/strong\u003e — EADS\/SOCATA. Primary flight operations reference: normal and emergency procedures, performance data, systems descriptions, weight \u0026amp; balance. Issued under EADS\/SOCATA authority.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch4\u003eStandard Illustrated Parts Catalog (IPC) — 5 Tomes\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eIPC Tome 1\u003c\/strong\u003e — P\/N Z00.18082020E0R15. Airframe structural components, fuselage assemblies, primary structural hardware. © SOCATA 1993–2001.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eIPC Tome 2\u003c\/strong\u003e — P\/N Z00.18082020E0R15. Flight control surfaces, landing gear assemblies, actuation hardware.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eIPC Tome 3\u003c\/strong\u003e — P\/N Z00.18082020E0R15. Engine installation, cowling, exhaust, firewall-forward components.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eIPC Tome 4\u003c\/strong\u003e — P\/N Z00.18082020E0R15. Fuel system, hydraulic system, environmental control components.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eIPC Tome 5\u003c\/strong\u003e — P\/N Z00.18082020E0R15. Avionics, instruments, interior furnishings, miscellaneous equipment.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch4\u003eMaintenance Manual (MM) — 4 Tomes\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eMM Tome 1\u003c\/strong\u003e — P\/N Z00.18010320E0R13. Airframe structure, fuselage, primary structural maintenance, inspection intervals, corrosion control. © SOCATA 1991–2001.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMM Tome 2\u003c\/strong\u003e — P\/N Z00.18010320E0R13. Flight controls, landing gear, hydraulic actuation, rigging data, overhaul limits.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMM Tome 3\u003c\/strong\u003e — P\/N Z00.18010320E0R13. Powerplant installation, engine mount, cowling, exhaust, firewall-forward systems, troubleshooting.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMM Tome 4\u003c\/strong\u003e — P\/N Z00.18010320E0R13. Fuel system, electrical system, avionics installation, environmental control, wiring references.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch4\u003eElectrical Maintenance Manual — 4 Tomes\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eElectrical MM Tome 1\u003c\/strong\u003e — Réf. Z00.18320E0R5. Power generation, battery, external power, bus distribution, master circuit protection. © SOCATA\/Aerospatiale Matra 1988–2000.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eElectrical MM Tome 2\u003c\/strong\u003e — Réf. Z00.18320E0R5. Engine electrical systems, ignition, starter circuits, fuel system electrical controls.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eElectrical MM Tome 3\u003c\/strong\u003e — Réf. Z00.18320E0R5. Avionics and instrument electrical installations, lighting systems, pitot-static heating, autopilot wiring.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eElectrical MM Tome 4\u003c\/strong\u003e — Réf. Z00.18320E0R5. Landing gear and flap electrical actuation, warning systems, stall warning, gear position indication.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eAircraft Technical Profile\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eAirframe:\u003c\/strong\u003e Low-wing, all-metal semi-monocoque. Advanced airfoil — positive controllability at low speeds, gentle predictable stall.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eWing Loading:\u003c\/strong\u003e 19.4 lb\/ft² (95 kg\/m²) at MTOW — highest in class, exceptional turbulence tracking stability.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eEngine:\u003c\/strong\u003e Avco Lycoming IO-540-C4D5D — naturally aspirated, fuel-injected, six-cylinder horizontally opposed. 250 BHP at 2,575 RPM.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePropeller:\u003c\/strong\u003e Hartzell two-blade constant-speed (hydraulically actuated). Optional three-blade for improved ground clearance and reduced cabin noise.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFuel:\u003c\/strong\u003e 100LL. Total 88.8 USG (336 L); 86.2 USG usable. Unusable: 2.2 USG (7.2 kg).\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eGT Variants:\u003c\/strong\u003e Swept vertical stabilizer, aerodynamically optimized rounded wingtips.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003ePerformance Data (ISA, Sea Level)\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003eMTOW: 3,080 lb (1,400 kg)\u003c\/li\u003e\n\u003cli\u003eMax Cruise Speed (Vc): 163 KIAS\u003c\/li\u003e\n\u003cli\u003eStall Speed (Vso): 59 KIAS — flaps fully extended, gear down\u003c\/li\u003e\n\u003cli\u003eMax Rate of Climb: 1,200 fpm\u003c\/li\u003e\n\u003cli\u003eService Ceiling: 20,000 ft\u003c\/li\u003e\n\u003cli\u003eTakeoff Roll (ISA, SL): 761 ft (232 m)\u003c\/li\u003e\n\u003cli\u003eDemonstrated Crosswind Component: 25 knots\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eKey Service Bulletins Referenced\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eSB 10-148 (Wing Spar Lower Boom):\u003c\/strong\u003e Periodic NDI for fatigue cracks or corrosion; Type 1 or Type 2 metallic repairs if tolerances exceeded.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSB 10-058 (Cabin Door Latches):\u003c\/strong\u003e Replacement of AU4G aluminum catches with steel hardware P\/N TB10 250 72 101.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eHartzell HC-ASB-61-251:\u003c\/strong\u003e Propeller attachment, dynamic balancing, hub torque standardization.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTextron Lycoming SB No. 480:\u003c\/strong\u003e Multi-viscosity mineral or ashless dispersant engine oil compliance.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e⚠️ \u003cstrong\u003eRegulatory Notice:\u003c\/strong\u003e Under FAA 14 CFR § 43.13 and EASA Part-M, any mechanic performing maintenance on an active aircraft must use current, manufacturer-approved revision-controlled data. This archival document does not satisfy that requirement.\u003c\/p\u003e\n\u003cp\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorized distributor.\u003cbr\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53655014736219,"sku":null,"price":89.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/tb-20-banner-golden-sunset.png?v=1784993756"},{"product_id":"socata-tb21-trinidad-tc-maintenance-manual-illustrated-parts-catalog-electrical-manual","title":"SOCATA TB 21 Trinidad TC — Maintenance Manual, Illustrated Parts Catalog \u0026 Electrical Manual","description":"\u003ch3\u003eSOCATA TB 21 Trinidad TC — Primary-Source Technical Library\u003c\/h3\u003e\n\u003cp\u003eThe \u003cstrong\u003eSOCATA TB 21 Trinidad TC\u003c\/strong\u003e is the turbocharged, high-performance variant of the \"Caribbean\" series — a four-to-five-seat low-wing single-engine aircraft engineered at Tarbes for serious cross-country and IFR operations. This collection delivers the complete factory documentation set as issued by EADS\/Socata and Aérospatiale Matra, covering maintenance, parts, and electrical systems across 14 archival volumes.\u003c\/p\u003e\n\u003ch3\u003eAircraft Overview\u003c\/h3\u003e\n\u003cp\u003ePowered by a single \u003cstrong\u003eAvco Lycoming TIO-540-AB1AD\u003c\/strong\u003e six-cylinder turbocharged engine producing \u003cstrong\u003e250 hp (186 kW)\u003c\/strong\u003e at all certified altitudes, the TB 21 was designed for efficiency and structural integrity. Its airframe uses advanced sheet aluminium alloy panel bonding — eliminating spot welding — and rigid push-pull control rods on all three primary flight surfaces. The pressurised cabin cross-section reaches 49–50 inches shoulder width, and the trailing-link main undercarriage absorbs hard landings with precision.\u003c\/p\u003e\n\u003ch3\u003ePerformance Reference Data\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003eMaximum Cruise Speed: 190–200 knots\u003c\/li\u003e\n\u003cli\u003eService Ceiling: 25,000 ft (7,620 m)\u003c\/li\u003e\n\u003cli\u003eMaximum Range: 962–1,200 nautical miles\u003c\/li\u003e\n\u003cli\u003eRate of Climb: 1,125 fpm\u003c\/li\u003e\n\u003cli\u003eStall Speed (Flaps Down): 54 knots\u003c\/li\u003e\n\u003cli\u003eTakeoff Distance (Over 50-ft Obstacle): 1,953 ft (595 m)\u003c\/li\u003e\n\u003cli\u003eMaximum Gross Weight: 3,083 lbs (1,400 kg)\u003c\/li\u003e\n\u003cli\u003eUsable Fuel Capacity: 86.2 US gallons (326 L)\u003c\/li\u003e\n\u003cli\u003eMaximum Demonstrated Crosswind: 25 knots\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cem\u003eStandard-day conditions at maximum gross weight. Refer to current TCDS EASA.A.378 for certified limits.\u003c\/em\u003e\u003c\/p\u003e\n\u003ch3\u003eDocument Manifest — 14 Unique Documents\u003c\/h3\u003e\n\u003cp\u003e\u003cstrong\u003eMaintenance Manual (MM) — 5 Volumes\u003c\/strong\u003e\u003cbr\u003ePublisher: EADS\/Socata · P\/N: Z00.18010321E0R13 · © 1991–2001\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eTome 1 — General Airframe \u0026amp; Structures\u003c\/li\u003e\n\u003cli\u003eTome 2 — Systems \u0026amp; Powerplant\u003c\/li\u003e\n\u003cli\u003eTome 3 — Flight Controls \u0026amp; Landing Gear\u003c\/li\u003e\n\u003cli\u003eTome 4 — Avionics \u0026amp; Instruments\u003c\/li\u003e\n\u003cli\u003eTome 5 — Supplementary Procedures \u0026amp; Appendices\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eStandard Illustrated Parts Catalog (IPC) — 5 Volumes\u003c\/strong\u003e\u003cbr\u003ePublisher: EADS\/Socata · P\/N: Z00.18082021E0R15 · © 1993–2001\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eTome 1 — Airframe Structures \u0026amp; Panels\u003c\/li\u003e\n\u003cli\u003eTome 2 — Flight Controls \u0026amp; Surfaces\u003c\/li\u003e\n\u003cli\u003eTome 3 — Landing Gear \u0026amp; Hydraulics\u003c\/li\u003e\n\u003cli\u003eTome 4 — Powerplant \u0026amp; Fuel System\u003c\/li\u003e\n\u003cli\u003eTome 5 — Avionics, Electrical \u0026amp; Instruments\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eElectrical Maintenance Manual (EMM) — 4 Volumes\u003c\/strong\u003e\u003cbr\u003ePublisher: Socata\/Aérospatiale Matra · P\/N: Z00.18320320E0R5 · © 1988, 1989, 1990, 1994, 2000\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eTome 1 — TB 20 \u0026amp; TB 21 Electrical Systems Manual\u003c\/li\u003e\n\u003cli\u003eTome 2 — TB 20 \u0026amp; TB 21 Electrical Systems Manual\u003c\/li\u003e\n\u003cli\u003eTome 3 — TB 20 \u0026amp; TB 21 Electrical Systems Manual\u003c\/li\u003e\n\u003cli\u003eTome 4 — TB 20 \u0026amp; TB 21 Electrical Systems Manual\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eRegulatory \u0026amp; Airworthiness Context\u003c\/h3\u003e\n\u003cp\u003eThe TB 21 is certificated under \u003cstrong\u003eEASA TCDS No. EASA.A.378\u003c\/strong\u003e (originally French DGAC\/Aérospatiale). Active operators must use current revision-controlled data from the Type Certificate holder. Notable engineering interventions include FAA Advisory Circular AC 98-18-13 and Lycoming crankcase\/crankshaft directives applicable to the TIO-540 series.\u003c\/p\u003e\n\u003cp\u003e⚠️ \u003cstrong\u003eRegulatory Notice:\u003c\/strong\u003e Under FAA 14 CFR § 43.13 and EASA Part-M, any mechanic performing maintenance on an active aircraft must use current, manufacturer-approved revision-controlled data. This archival document does not satisfy that requirement.\u003c\/p\u003e\n\u003cp\u003e\u003cem\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorized distributor.\u003c\/em\u003e\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/strong\u003e\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53655114154331,"sku":null,"price":89.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/tb-21-banner-takeoff.png?v=1784997228"},{"product_id":"socata-tb-9-tampico-primary-source-technical-documentation-collection","title":"Socata TB-9 Tampico — Primary-Source Technical Documentation Collection","description":"\u003ch3\u003eSOCATA TB-9 Tampico — Primary-Source Technical Documentation Collection\u003c\/h3\u003e\n\u003cp\u003eThe SOCATA TB-9 Tampico is a French all-metal, low-wing, four-seat light aircraft developed by Socata (Groupe Aérospatiale \/ EADS) as a primary and instrument flight trainer. Powered by the Lycoming O-320-D2A (160 HP), the TB-9 became a cornerstone of European flight training fleets from the late 1980s through the 2000s, prized for its structural robustness, positive stability characteristics, and high demonstrated crosswind capability (25 knots).\u003c\/p\u003e\n\u003cp\u003eThis Living Collection brings together \u003cstrong\u003e15 original factory documents\u003c\/strong\u003e spanning the complete technical lifecycle of the TB-9 airframe — from airframe maintenance and structural inspection to parts identification, flight operations, and pilot information.\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eDocument Manifest — 15 Original Factory Documents\u003c\/h3\u003e\n\u003cp\u003e\u003cstrong\u003eMaintenance Manual Series (Socata \/ EADS-Socata):\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eMaintenance Manual — Tome 1\u003c\/li\u003e\n\u003cli\u003eMaintenance Manual — Tome 2\u003c\/li\u003e\n\u003cli\u003eMaintenance Manual — Tome 3\u003c\/li\u003e\n\u003cli\u003eMaintenance Manual — Tome 4\u003c\/li\u003e\n\u003cli\u003eMaintenance Manual — Tome 5\u003c\/li\u003e\n\u003cli\u003eElectrical Maintenance Manual (TB 9–10–200) — Tome 1 (Référence: Z00.18320310E0R6)\u003c\/li\u003e\n\u003cli\u003eElectrical Maintenance Manual (TB 9–10–200) — Tome 2 (Référence: Z00.18320310E0R6)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eIllustrated Parts Catalog Series (EADS-Socata, P\/N Z00.18082009E0R15):\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eIllustrated Parts Catalog — Tome 1\u003c\/li\u003e\n\u003cli\u003eIllustrated Parts Catalog — Tome 2\u003c\/li\u003e\n\u003cli\u003eIllustrated Parts Catalog — Tome 3\u003c\/li\u003e\n\u003cli\u003eIllustrated Parts Catalog — Tome 4\u003c\/li\u003e\n\u003cli\u003eIllustrated Parts Catalog — Tome 5\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eFlight Operations \u0026amp; Pilot Documentation:\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eManuel de Vol \/ Flight Manual — TB 9 (French, Socata \/ Groupe Aérospatiale)\u003c\/li\u003e\n\u003cli\u003ePilot's Operating Handbook (POH) — TB-9\u003c\/li\u003e\n\u003cli\u003ePilot's Information Manual — TB-9 (from S\/N 948, Socata \/ Aérospatiale Matra, P\/N T00.DUOPHPYE, September 1989)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eAirframe \u0026amp; Engine Technical Reference\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eAirframe:\u003c\/strong\u003e All-metal, low-wing monoplane — continuous heavy single milled spar construction\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eEngine:\u003c\/strong\u003e Lycoming O-320-D2A — 4-cylinder, horizontally opposed, air-cooled, direct-drive\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePower Output:\u003c\/strong\u003e 160 HP (120 kW) at 2,700 RPM\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFuel System:\u003c\/strong\u003e Carburetor induction — 40-gallon total capacity\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eElectrical System:\u003c\/strong\u003e 28V DC — 70-amp engine-mounted alternator + backup battery\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMTOW:\u003c\/strong\u003e 1,060 kg (2,332 lbs)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMax Cruise Speed:\u003c\/strong\u003e 109–115 KIAS\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eVNE:\u003c\/strong\u003e 144 KIAS\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eRate of Climb (ISA, SL):\u003c\/strong\u003e 665–738 FPM\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eService Ceiling:\u003c\/strong\u003e 11,000 ft\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMax Range:\u003c\/strong\u003e 505–532 NM\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMax Demonstrated Crosswind:\u003c\/strong\u003e 25 knots\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eIntentional Spins:\u003c\/strong\u003e Prohibited\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eAirworthiness \u0026amp; 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This archival document does not satisfy that requirement.\u003c\/p\u003e\n\u003chr\u003e\n\u003cp\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorized distributor.\u003c\/p\u003e\n\u003cp\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53656551326043,"sku":null,"price":59.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/banner-c-white-factory-livery.png?v=1785036867"},{"product_id":"socata-tb-10-tobago-primary-source-technical-documentation-collection","title":"Socata TB-10 Tobago — Primary-Source Technical Documentation Collection","description":"\u003ch2\u003eSOCATA TB-10 Tobago — Primary-Source Technical Documentation Collection\u003c\/h2\u003e\u003cp\u003eThe SOCATA TB-10 Tobago is a French all-metal, low-wing, four-seat light aircraft developed by Socata (Groupe Aérospatiale \/ EADS) as a touring and instrument flight trainer. Powered by the Lycoming O-360-A1AD (180 HP) with a Hartzell constant-speed propeller, the TB-10 offered a significant performance step over its sibling the TB-9 Tampico, with greater range, higher cruise speed, and a wider cabin. It became a staple of European flight training and private touring fleets through the 1980s and 2000s.\u003c\/p\u003e\u003cp\u003eThis Living Collection brings together \u003cstrong\u003e16 original factory documents\u003c\/strong\u003e spanning the complete technical lifecycle of the TB-10 airframe — from airframe maintenance and structural inspection to parts identification, flight operations, and pilot information.\u003c\/p\u003e\u003chr\u003e\u003ch3\u003eDocument Manifest — 16 Original Factory Documents\u003c\/h3\u003e\u003cp\u003e\u003cstrong\u003eMaintenance Manual Series (EADS-Socata, P\/N Z00.18010310E0R13):\u003c\/strong\u003e\u003c\/p\u003e\u003cul\u003e\n\u003cli\u003eMaintenance Manual — Tome 1\u003c\/li\u003e\n\u003cli\u003eMaintenance Manual — Tome 2\u003c\/li\u003e\n\u003cli\u003eMaintenance Manual — Tome 3\u003c\/li\u003e\n\u003cli\u003eMaintenance Manual — Tome 4\u003c\/li\u003e\n\u003cli\u003eMaintenance Manual — Tome 5\u003c\/li\u003e\n\u003c\/ul\u003e\u003cp\u003e\u003cstrong\u003eElectrical Maintenance Manual Series (TB 9–10–200 Family Document, P\/N Z00.18320310E0R6):\u003c\/strong\u003e\u003c\/p\u003e\u003cul\u003e\n\u003cli\u003eElectrical Maintenance Manual (TB 9–10–200) — Tome 1\u003c\/li\u003e\n\u003cli\u003eElectrical Maintenance Manual (TB 9–10–200) — Tome 2\u003c\/li\u003e\n\u003c\/ul\u003e\u003cp\u003e\u003cstrong\u003eIllustrated Parts Catalog Series (EADS-Socata, P\/N Z00.18082010E0R15):\u003c\/strong\u003e\u003c\/p\u003e\u003cul\u003e\n\u003cli\u003eIllustrated Parts Catalog — Tome 1\u003c\/li\u003e\n\u003cli\u003eIllustrated Parts Catalog — Tome 2\u003c\/li\u003e\n\u003cli\u003eIllustrated Parts Catalog — Tome 3\u003c\/li\u003e\n\u003cli\u003eIllustrated Parts Catalog — Tome 4\u003c\/li\u003e\n\u003cli\u003eIllustrated Parts Catalog — Tome 5\u003c\/li\u003e\n\u003c\/ul\u003e\u003cp\u003e\u003cstrong\u003ePilot Documentation:\u003c\/strong\u003e\u003c\/p\u003e\u003cul\u003e\n\u003cli\u003ePilot's Information Manual — TB 10 (EADS-Socata)\u003c\/li\u003e\n\u003cli\u003ePilot's Information Manual — TB 10 (Socata \/ Aérospatiale Matra, from S\/N 848, P\/N T00.DVDPIPYE, September 1989) — 9 sections + 7 supplements including KAP 100 Autopilot, KAP\/KFC 150 Autopilot, Ground Power Receptacle, Auxiliary Air Pump, Low Noise Exhaust, Garmin 150 GPS\u003c\/li\u003e\n\u003cli\u003eSocata TB-10 User Manual — Tome 1\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003ch3\u003eAirframe \u0026amp; Engine Technical Reference\u003c\/h3\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eAirframe:\u003c\/strong\u003e All-metal, low-wing monoplane — semi-tapered wing planform, fixed tricycle gear with fairings\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCabin Width:\u003c\/strong\u003e 4 ft 3 in — widest in class for a four-seat GA trainer\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eEngine:\u003c\/strong\u003e Lycoming O-360-A1AD — 4-cylinder, horizontally opposed, air-cooled, direct-drive\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePower Output:\u003c\/strong\u003e 180 HP (134 kW) at 2,700 RPM\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePropeller:\u003c\/strong\u003e Hartzell constant-speed, two-blade metal (HC-C2YK-1BF\/F7666A-2)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFuel System:\u003c\/strong\u003e Carburetor induction — 54 US gallons total capacity\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMTOW:\u003c\/strong\u003e 1,150 kg (2,530 lbs) · Standard Empty Weight: 1,477 lbs\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMax Cruise Speed:\u003c\/strong\u003e 127–133 KIAS\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eRate of Climb (Vy):\u003c\/strong\u003e 790 FPM\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eService Ceiling:\u003c\/strong\u003e 13,000 ft\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMax Range:\u003c\/strong\u003e 653 NM\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTakeoff Ground Roll (10° Flaps):\u003c\/strong\u003e 286 m (938 ft)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eStall Speed — VS0 (landing config):\u003c\/strong\u003e 53 KIAS\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eStall Speed — VS (clean):\u003c\/strong\u003e 60 KIAS\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMax Demonstrated Crosswind:\u003c\/strong\u003e 25 knots\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eType Certificate:\u003c\/strong\u003e EASA.A.378 \/ FAA A51EU\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003ch3\u003eAirworthiness \u0026amp; Engineering Bulletin Reference\u003c\/h3\u003e\u003cp\u003eKey mandatory actions tracked in this documentation set:\u003c\/p\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eSB 10-085-57\u003c\/strong\u003e — Wing internal rib structural inspections and reinforcement kit installation\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAerospatiale SB 15 \u0026amp; SB 29\u003c\/strong\u003e — Elevator trim tab linkage and control rod end-fitting checks to prevent attachment play\u003c\/li\u003e\n\u003c\/ul\u003e\u003cp\u003eActive fleet documentation is managed via the Veryon Publications Service Catalog or Daher's official MySocata Portal.\u003c\/p\u003e\u003chr\u003e\u003cp\u003e⚠️ \u003cstrong\u003eRegulatory Notice:\u003c\/strong\u003e Under FAA 14 CFR § 43.13 and EASA Part-M, any mechanic performing maintenance on an active aircraft must use current, manufacturer-approved revision-controlled data. This archival document does not satisfy that requirement.\u003c\/p\u003e\u003chr\u003e\u003cp\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorized distributor.\u003c\/p\u003e\u003cp\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53656554635611,"sku":null,"price":59.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/banner-d-over-the-clouds.png?v=1785038456"},{"product_id":"sncaso-so-90-cassiopee-notice-technique-de-lavion-moteurs-bearn-6-d-07-tomes-i-iii-so-93-brochure","title":"SNCASO SO.90 Cassiopée — Notice Technique de l'Avion, Moteurs Béarn 6.D.07 — Tomes I–III + SO.93 Brochure","description":"\u003ch2\u003eSNCASO SO.90 Cassiopée — Notice Technique de l'Avion\u003c\/h2\u003e\u003cp\u003e\u003cem\u003eSociété Nationale de Constructions Aéronautiques du Sud-Ouest (SNCASO), France\u003c\/em\u003e\u003cbr\u003e\u003cem\u003eÉdition: 15 Janvier 1948 — Archival Collection\u003c\/em\u003e\u003c\/p\u003e\u003chr\u003e\u003cp\u003eThe SNCASO SO.90 Cassiopée stands at the intersection of wartime clandestine engineering and post-war French military transport ambition. Designed under Vichy-era restrictions and refined into a family of operational aircraft serving the Aéronavale, the SO.90 and its direct derivatives — the SO.93, SO.94, and SO.95 Corse series — represent a defining chapter in French aviation's reconstruction era.\u003c\/p\u003e\u003cp\u003eThis archival collection assembles the complete \u003cem\u003eNotice Technique de l'Avion SO-90\u003c\/em\u003e, issued by SNCASO on 15 January 1948, covering all three Tomes across six fascicules, plus the original SO.93 \u003cem\u003eBimoteur\u003c\/em\u003e commercial brochure — a rare promotional document from the same production family.\u003c\/p\u003e\u003cp\u003e\u003cstrong\u003ePowerplant:\u003c\/strong\u003e Twin Béarn 6D.07 inverted 6-cylinder in-line engines, each producing approximately 375–410 hp, driving Ratier 3-blade constant-speed propellers. The SO.90 series later evolved to twin Renault 12S-02 V-12 inverted air-cooled engines (580 hp each) in the SO.94\/SO.95 production variants.\u003c\/p\u003e\u003cp\u003e\u003cstrong\u003eConfiguration:\u003c\/strong\u003e Clean cantilever mid-wing monoplane, all-metal semi-monocoque fuselage, wingspan 17.90 m, wing area 37.60 m². Designed by Maurice Hurel for low drag and regional efficiency. The SO.94 introduced tricycle undercarriage; the SO.95M Corse III reverted to heavy-duty tailwheel for rough military fields.\u003c\/p\u003e\u003cp\u003e\u003cstrong\u003eOperational ceiling:\u003c\/strong\u003e 6,500 m. Maximum speed: 355 km\/h. Cruising speed: 285 km\/h. Payload: 10–13 passengers or equivalent freight.\u003c\/p\u003e\u003chr\u003e\u003ch3\u003eDocument Manifest — 7 Unique Documents\u003c\/h3\u003e\u003cp\u003e\u003cstrong\u003eTome I — Fascicule 1 · Spécifications Générales\u003c\/strong\u003e\u003cbr\u003eGeneral specifications, geometric profiles, and official dimensional data for the SO.90 airframe with Béarn 6D.07 engines.\u003c\/p\u003e\u003cp\u003e\u003cstrong\u003eTome I — Fascicule 2 · Description\u003c\/strong\u003e\u003cbr\u003eStructural and systems description: airframe construction, control surfaces, landing gear, fuel and oil systems.\u003c\/p\u003e\u003cp\u003e\u003cstrong\u003eTome I — Fascicule 3 · Chargement (Weight \u0026amp; Balance)\u003c\/strong\u003e\u003cbr\u003eOfficial weight and balance envelopes, loading configurations, and centre-of-gravity limits.\u003c\/p\u003e\u003cp\u003e\u003cstrong\u003eTome I — Fascicule 5 · Matériel d'Équipement\u003c\/strong\u003e\u003cbr\u003eEquipment list: instruments, electrical systems, pneumatic networks, and installed avionics\/accessories.\u003c\/p\u003e\u003cp\u003e\u003cstrong\u003eTome II — Fascicule 7 · Utilisation en Vol\u003c\/strong\u003e\u003cbr\u003eOperational flight manual: normal, abnormal, and emergency procedures; structural limitations; single-engine handling; stall characteristics and VMC data.\u003c\/p\u003e\u003cp\u003e\u003cstrong\u003eTome III — Fascicule 9 · Entretien \u0026amp; Service au Sol\u003c\/strong\u003e\u003cbr\u003eGround maintenance manual: pneumatic systems, electrical networks, scheduled servicing, and ground handling procedures.\u003c\/p\u003e\u003cp\u003e\u003cstrong\u003eTome III — Fascicule 10 · Démontage – Remontage\u003c\/strong\u003e\u003cbr\u003eDisassembly and reassembly procedures for major structural components and systems.\u003c\/p\u003e\u003cp\u003e\u003cstrong\u003eBONUS — SO.93 Bimoteur · Brochure Commerciale SNCASO France\u003c\/strong\u003e\u003cbr\u003eOriginal factory promotional brochure for the SO.93 twin-engine variant — a rare commercial document from the same aircraft family, issued by SNCASO France.\u003c\/p\u003e\u003chr\u003e\u003cp\u003e\u003cem\u003eThis collection contains 7 unique documents — Cette collection contient 7 documents uniques.\u003c\/em\u003e\u003c\/p\u003e\u003chr\u003e\u003cp\u003e⚠️ \u003cstrong\u003eRegulatory Notice:\u003c\/strong\u003e Under FAA 14 CFR § 43.13 and EASA Part-M, any mechanic performing maintenance on an active aircraft must use current, manufacturer-approved revision-controlled data. This archival document does not satisfy that requirement.\u003c\/p\u003e\u003cp\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorized distributor.\u003cbr\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53658024509787,"sku":null,"price":34.85,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/banner-2-cinematic-wide.png?v=1785056173"},{"product_id":"sncaso-so-9000-trident-notice-pilote-note-technique-trident-i-trident-ii","title":"SNCASO SO.9000 Trident — Notice Pilote \u0026 Note Technique — Trident I \u0026 Trident II","description":"\u003ch3\u003eSNCASO SO.9000 Trident — Archival Technical Documentation\u003c\/h3\u003e\n\u003cp\u003e\u003cem\u003eSociété Nationale de Constructions Aéronautiques du Sud-Ouest (SNCASO), France\u003c\/em\u003e\u003cbr\u003e\u003cem\u003eTrident I \u0026amp; Trident II — Archival Collection, Early 1950s\u003c\/em\u003e\u003c\/p\u003e\n\u003chr\u003e\n\u003cp\u003eThe SNCASO SO.9000 Trident was one of the most radical interceptor concepts ever to reach flight testing. Conceived in the early 1950s to counter supersonic strategic threats, it combined wingtip-mounted turbojets with a liquid-fueled rocket motor in the rear fuselage — a mixed-power formula that pushed French experimental aviation to its absolute limits and ultimately cost the life of test pilot Charles Goujon in 1957.\u003c\/p\u003e\n\u003cp\u003eThis archival collection assembles two primary-source technical documents for the Trident I and Trident II programmes, covering aerodynamic configuration, propulsion systems, flight dynamics, cockpit systems, and the engineering solutions devised for one of the most dangerous aircraft ever built in France.\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eAerodynamic Design \u0026amp; Structural Configuration\u003c\/h3\u003e\n\u003cp\u003eThe SO.9000's aerodynamic profile was optimized explicitly for the transonic and supersonic regimes. The highly streamlined, bullet-shaped fuselage minimized cross-sectional wave drag. Wings were short, straight, and needle-thin — a low-aspect-ratio rectangular structure that minimized supersonic wave drag at the cost of poor lift-to-drag ratios at low speed. Conventional multi-part control surfaces were abandoned in favour of three all-moving slab tailplanes, operating collectively for pitch\/yaw and differentially for roll — the only solution to high-speed control lock-up.\u003c\/p\u003e\n\u003ch3\u003ePropulsion Systems\u003c\/h3\u003e\n\u003cp\u003e\u003cstrong\u003eTurbojet (Wingtip-Mounted):\u003c\/strong\u003e Two Dassault MD.30 “Viper” turbojets at wingtips — annular air intake, 7-stage axial compressor, annular combustion chamber (6 igniter + 12 start injectors), single-stage turbine, fixed-area ejection nozzle. Static ground thrust: 725 kg each. Ground start via cart (compressed air + electrical accumulators), two-phase sequence; in-flight re-ignition possible on onboard battery. Kerosene system: 2 forward tanks (660L) + 2 lateral tanks (90L) + collector\/nourrice (85L). HP pump feeds both reactors via FAURE-HERRMANN counter and independent leading-edge solenoid isolation valves.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eRocket Motor — SEPR Group (Rear Fuselage):\u003c\/strong\u003e Propellants: Furaline (fuel) + pure nitric acid (oxidizer) — hypergolic, instantly igniting on contact, extremely toxic, volatile, and highly corrosive to the airframe. Staged fixed thrust: 3 stages of 1,500 kg \/ 3,000 kg \/ 4,500 kg via 3 × 1,500 kg combustion chambers. Gas generator (nitric acid + Furaline combustion, water\/methanol injection cooled) drives turbine powering centrifugal feed pumps. Pilot operations minimized to a master electric switch and a start timer.\u003c\/p\u003e\n\u003ch3\u003eHydraulic Systems\u003c\/h3\u003e\n\u003cp\u003eHydraulic energy used for: landing gear retraction, servo-control jacks and compensators, braking, and cabin jettison push. Two electric pumps in parallel, pressurized reservoir, feeding four independent circuits: landing gear (+ servo-control emergency), servo-control normal, normal braking, emergency braking. Cabin jettison circuit is fully autonomous — fed by a dedicated accumulator pressurized on the ground; two cabin push jacks fitted with special scissors that sever all service lines connecting cabin to airframe at the moment of jettison.\u003c\/p\u003e\n\u003ch3\u003ePneumatic Systems\u003c\/h3\u003e\n\u003cp\u003e\u003cstrong\u003eCabin Pressurisation (normal \u0026amp; emergency):\u003c\/strong\u003e Bleed air from both MD.30 Viper reactors via SRMCA pressure regulator. Schedule: 0–3,000 m = ambient; 3,000–6,250 m = fixed at 3,000 m equivalent; above 6,250 m = differential 0.250 kg\/cm². Emergency supply: 3.3L bottle at 150 HPZ in forward nose, supplies cabin at Δp = 25 ps on reactor bleed failure or during cabin jettison descent. Secondary circuits feed cockpit seal inflation and anti-g valve.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eRocket Propellant Tank Pressurisation:\u003c\/strong\u003e Acid reservoir pressurized by 150 HPZ bottle in forward nose via pre-reducer and reducer. Furaline and water reservoirs pressurized by separate bottle in fuselage above wing. Pilot can dump acid reservoir rapidly (“vide-vite”) or progressively (“vidange lente”) via same forward nose bottle.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eServo-Stabilizer Valve:\u003c\/strong\u003e Dynamic pressure from pitot antenna transmitted to servo-stabilizer valve cylinder — piston linked to pitch command, applying speed-dependent load feel to pilot.\u003c\/p\u003e\n\u003ch3\u003eElectrical Systems\u003c\/h3\u003e\n\u003cp\u003eTwo ANDZAR 40 Ah (19-cell) batteries. \u003cstrong\u003eBattery 1\u003c\/strong\u003e (forward, “servitudes battery”): powers reactors (LP\/HP cocks, LP pump, fuel counter, tachometers, manometers, thermometers), fire detectors, hydraulic electro-pumps\/gauges\/warning lights, landing gear, intrados flaps, airbrakes, servo-control (roll gyro, friction dampers, compensator motors), windscreen de-icing, pitot heating, cabin pressure\/oxygen, warning lights, navigation (gyro-compass, gyro-horizon), radio (VHF I, radio compass), and flight test instrumentation. \u003cstrong\u003eBattery 2\u003c\/strong\u003e (rear fuselage, “emergency battery”): backs up Battery 1 on failure; powers VHF II and all rocket circuit accessories in normal operation.\u003c\/p\u003e\n\u003ch3\u003eHandling, Stability \u0026amp; Flight Dynamics\u003c\/h3\u003e\n\u003cp\u003eWingtip engine positioning created extreme yaw vulnerability — a single-sided flameout at high speed threatened an unrecoverable pinwheel spin. Early test flights without the active rocket required the full length of military runways to unstick from the tarmac. Conventional ailerons were entirely locked out during supersonic transitions, leaving the all-moving tail surfaces as the sole roll authority. Test pilot Jacques Guignard documented these severe anomalies in flight test reports that form part of the programme’s engineering record.\u003c\/p\u003e\n\u003ch3\u003eEngineering Bulletins \u0026amp; Programme History\u003c\/h3\u003e\n\u003cp\u003eThe second Trident I prototype was lost on its maiden flight in 1953. The Trident II suffered a mid-air explosion in 1957, killing test pilot Charles Goujon. Engineering files detail a fully jettisonable nose capsule — the entire cockpit section designed to separate from the airframe at supersonic speeds, with hydraulic push jacks and scissors that sever all service lines on command. Despite setting multiple unofficial altitude and climb rate records, the programme was officially terminated in 1958 when the French Air Force selected the Dassault Mirage III.\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eDocument Manifest — 2 Unique Documents\u003c\/h3\u003e\n\u003cp\u003e\u003cstrong\u003eDocument 1 — S.O. 9050-001 · Notice Pilote — Note Technique n° 2-0355\u003c\/strong\u003e (Trident II)\u003cbr\u003ePilot’s Notes for the SO.9050-001 — 15 pages. Covers: general description (MD.30 Viper + SEPR 2-chamber rocket), hydraulic servitudes (landing gear, servo-controls, braking, airbrakes), pneumatic systems (cabin pressurisation, hydraulic reservoir pressurisation, rocket propellant tank pressurisation, acid dump circuits, servo-stabilizer valve), electrical systems (two ANDZAR batteries, full circuit breakdown), MD.30 Viper reactor description and start sequence, kerosene fuel circuit, SEPR 63 rocket system (Furaline + nitric acid, 2-stage thrust 1,500 + 2,000 kg, turbopump, pilot controls), and flight control system (irreversible hydraulic jacks, mixer unit, all-moving tail surfaces).\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eDocument 2 — S.O. MDa\/LM · Note Technique 5456\u003c\/strong\u003e (Trident I — SO.9000)\u003cbr\u003eComprehensive systems description — 29 pages + 13 technical plates. Covers: general characteristics (3-chamber SEPR group, 2 × MD.30 Viper), hydraulic systems (4-circuit architecture, cabin jettison autonomous circuit), full pneumatic systems breakdown (cabin pressurisation normal\/emergency\/secondary, hydraulic reservoir pressurisation, rocket tank pressurisation, acid dump rapid\/slow, servo-stabilizer valve), electrical systems (two ANDZAR 40 Ah batteries, complete circuit inventory), MD.30 Viper reactor description and two-phase start sequence, kerosene circuit (660L + 90L + 85L collector), SEPR rocket group (3-stage thrust 1,500\/3,000\/4,500 kg, 3 combustion chambers, gas generator turbopump). 13 technical plates covering general arrangement, fuel feed, hydraulic schematics (4 plates), cabin layout, instrument panels (left\/right consoles, central panel), cabin conditioning, and radio installation.\u003c\/p\u003e\n\u003cp\u003e\u003cem\u003eThis collection contains 2 unique documents — Cette collection contient 2 documents uniques.\u003c\/em\u003e\u003c\/p\u003e\n\u003chr\u003e\n\u003cp\u003e⚠️ \u003cstrong\u003eRegulatory Notice:\u003c\/strong\u003e Under FAA 14 CFR § 43.13 and EASA Part-M, any mechanic performing maintenance on an active aircraft must use current, manufacturer-approved revision-controlled data. This archival document does not satisfy that requirement.\u003c\/p\u003e\n\u003cp\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorized distributor.\u003cbr\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53658048627035,"sku":null,"price":25.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/banner-3-square.png?v=1785057599"},{"product_id":"sncaso-s-o-4050-vautour-n-notice-descriptive-et-de-fonctionnement-tome-ii-2-4-installation-hydraulique-1958","title":"SNCASO S.O. 4050 Vautour N — Notice Descriptive et de Fonctionnement, Tome II: §2.4 Installation Hydraulique (1958)","description":"\u003ch4\u003eSNCASO S.O. 4050 Vautour N — Notice Descriptive et de Fonctionnement, Tome II — Chapitre 2: §2.4 Installation Hydraulique\u003c\/h4\u003e\n\u003cp\u003eThe companion volume to the NDF Tome I (1957), this \u003cstrong\u003eTome II Texte\u003c\/strong\u003e covers \u003cstrong\u003eChapitre 2, §2.4 — Installation Hydraulique\u003c\/strong\u003e of the Vautour Version «N» Notice Descriptive et de Fonctionnement. Revised \u003cstrong\u003e15 Janvier 1958\u003c\/strong\u003e, header stamped \u003cem\u003eS.O. — VAUTOUR — Chapitre 2 \/ 2.4 — Hydraulique\u003c\/em\u003e. Pages run from 2401 onward in the original SNCASO pagination.\u003c\/p\u003e\n\u003cp\u003eThis section documents the complete dual-circuit hydraulic installation of the Vautour N — the most mechanically complex system in the airframe — covering generation, regulation, and all utilisation circuits from landing gear to radar antenna orientation. Hydraulic fluid specification: \u003cstrong\u003eFHS 1 (Norme AIR 3520)\u003c\/strong\u003e.\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eDocument Manifest — §2.4 Installation Hydraulique (Pages 2401–2407A+)\u003c\/h3\u003e\n\u003cp\u003e\u003cstrong\u003e§2.4.0 — Généralités\u003c\/strong\u003e (p.2401–2402)\u003cbr\u003eDual-circuit architecture: circuits normaux (doubled by secours for safety) + circuit d’orientation antenne radar indépendant (avions 311–370). Hydraulic lines on port fuselage wall (normal) and starboard (secours). Five accessory panels: panneau central «normal» (cadres 3–3½, compartiment Train Avant), panneau central «secours» (cadres 4–5, compartiment Radio-compas), panneau «aérofreins» (cadres 9–9½, compartiment Train Arrière), panneau «fuseau réacteur gauche» (partie fixe avant, flanc interne C.3–C.G.), panneau «fuseau réacteur droit».\u003cbr\u003e\u003cem\u003eNOTA: Pour les organes à documentation particulière signalés au cours de ce §, se reporter aux feuillets 2 de la présente notice.\u003c\/em\u003e\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003e§2.4.1 — Alimentation et Régulation\u003c\/strong\u003e\u003cbr\u003e\u003cstrong\u003e§2.4.1.0 Généralités\u003c\/strong\u003e — Circuits normaux fed by générations principales «normale et réserve», each with independent regulation. Circuits secours fed by génération «secours», except circuit de freinage secours (fed by génération principale). Triple-cadran pressure indicator 0–300 kg\/cm² on pilot’s pylon, driven by hydro-electric transmitter.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003e§2.4.1.1 — Organisation des Circuits de Génération Principale «Normale» et «Réserve»\u003c\/strong\u003e (p.2403–2405 — Planche 301)\u003cbr\u003eFeed all circuits normaux + circuit de freinage secours. Component table:\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eUne bâche — §2.4.4.0.1 — Pl. 302–303–304 — fuselage central, cadres 4–5 (compartiment bâche)\u003c\/li\u003e\n\u003cli\u003eUne valve de pressurisation — §2.4.4.0.2 — Pl. 305\u003c\/li\u003e\n\u003cli\u003eDeux pompes «SAMM» — §2.4.4.0.3 — (v. feuillet 2\/10) — relais d’accessoires des réacteurs\u003c\/li\u003e\n\u003cli\u003eTrois clapets anti-retour (avec bouchon) — §2.4.4.0.4 — Pl. 306 — 2 sur panneau central normal + 1 sur panneau fuseau réacteur G.\u003c\/li\u003e\n\u003cli\u003eUn clapet anti-retour avec valve de gonflage — §2.4.4.0.5 — Pl. 307 — panneau réacteur D.\u003c\/li\u003e\n\u003cli\u003eDeux régulateurs de pression G \u0026amp; D — 210 kg — §2.4.4.0.6 — Pl. 308 — panneaux fuseaux réacteurs G. et D.\u003c\/li\u003e\n\u003cli\u003eDeux régulateurs de pression G \u0026amp; D — 240 kg — —d°— — panneaux fuseaux réacteurs G. et D.\u003c\/li\u003e\n\u003cli\u003eDeux accumulateurs G \u0026amp; D, V = 1 litre — §2.4.4.0.7 — Pl. 309 — panneaux fuseaux réacteurs G. et D.\u003c\/li\u003e\n\u003cli\u003eUne électro-valve — §2.4.4.0.8 — Pl. 310 — panneau réacteur D.\u003c\/li\u003e\n\u003cli\u003eUn collecteur général — §2.4.4.0.9 — Pl. 311 — panneau central normal\u003c\/li\u003e\n\u003cli\u003eUn transmetteur hydro-électrique — §2.4.4.0.10 — Pl. 312\u003c\/li\u003e\n\u003cli\u003eUn récepteur-indicateur triple — §2.4.4.0.11 — — — pylône du poste pilote\u003c\/li\u003e\n\u003cli\u003eUn filtre décanteur — §2.4.4.0.12 — Pl. 313 — compartiment bâche\u003c\/li\u003e\n\u003cli\u003eUn filtre sur tuyauterie de refoulement — §2.4.4.0.13 — Pl. 314 — paroi interne fuseau-réacteur G.\u003c\/li\u003e\n\u003cli\u003eDeux prises de terrain «Bessier» (1 aspiration + 1 refoulement) — notice séparée — (v. feuillet 2\/9) — paroi interne fuseau-réacteur G.\u003c\/li\u003e\n\u003cli\u003eDeux robinets coupe-feu — Voir §2.3.1 — — — en partie supérieure (côté emplanture) dans les fuseaux-réacteurs G. et D.\u003c\/li\u003e\n\u003cli\u003eDeux robinets de vidange — §2.4.4.0.14 — — — côté interne fuseaux G. à D.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cem\u003eGénération principale se divise en deux circuits «Normal» et «Réserve» indépendants, avec accessoires communs (bâche, filtre décanteur, transmetteur, collecteur général), accessoires identiques par circuit (robinet coupe-feu, pompe SAMM, régulateurs 210 \u0026amp; 240 kg, accumulateur V=1L, clapet anti-retour, robinet de vidange), et accessoires propres à chaque circuit (clapet anti-retour avec valve de gonflage pour circuit réserve; clapet anti-retour simple + filtre tuyauterie prise de terrain pour circuit normal; électro-valve pour circuit réserve).\u003c\/em\u003e\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003e§2.4.1.2 — Organisation des Circuits de Génération Secours\u003c\/strong\u003e (p.2405–2406 — Planche 315)\u003cbr\u003eDoubles normal supply for: descente des trains, orientation des roues du train avant, servo-gouvernes. Component table:\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eUne électro-pompe — §2.4.4.0.15 — Pl. 316 — Compartiment Train AV, C.4, côté gauche\u003c\/li\u003e\n\u003cli\u003eUn filtre sur tuyauterie — §2.4.4.0.16 — Pl. 316 — Compartiment Train AV entre C.4½ et C.4\u003c\/li\u003e\n\u003cli\u003eTrois clapets anti-retour (avec raccords) — §2.4.4.0.17 — Pl. 317 — 1 dans fuselage central sur C.2 face AV de la cuve; 2 sur panneau «secours»\u003c\/li\u003e\n\u003cli\u003eUn accumulateur de V = 1,750 litres — §2.4.4.0.18 — Pl. 318 — entre les cadres 24 \u0026amp; 25\u003c\/li\u003e\n\u003cli\u003eUne bouteille d’air de V = 5 litres — §2.4.4.0.19 — Pl. 319 — —d°—\u003c\/li\u003e\n\u003cli\u003eUn accumulateur de V = 0,250 litre — §2.4.4.0.20 — Pl. 320 — sur un panneau «Secours»\u003c\/li\u003e\n\u003cli\u003eTrois mano-contacteurs — §2.4.4.0.21 — Pl. 321 — —d°—\u003c\/li\u003e\n\u003cli\u003eUn distributeur à commande mécanique — §2.4.4.0.22 — Pl. 322 — sur le cadre 2 face AV de la cuve\u003c\/li\u003e\n\u003cli\u003eUn clapet taré à 230 kg — §2.4.4.0.23 — Pl. 323 — sur le panneau «Secours»\u003c\/li\u003e\n\u003cli\u003eUn transmetteur hydro-électrique — §2.4.4.0.24 — Pl. 312 — —d°—\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003e§2.4.2 — Circuits d’Utilisation\u003c\/strong\u003e (p.2407A+)\u003cbr\u003e\u003cstrong\u003e§2.4.2.0 Généralités\u003c\/strong\u003e — Utilisation circuits divide into two groups:\u003c\/p\u003e\n\u003cp\u003e\u003cem\u003eCircuits Principaux:\u003c\/em\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e§2.4.2.1 — Circuit de relevage et de descente des trains (normal)\u003c\/li\u003e\n\u003cli\u003e§2.4.2.2 — Circuit de descente des trains (secours)\u003c\/li\u003e\n\u003cli\u003e§2.4.2.3 — Circuit d’orientation des roues du train avant (normal)\u003c\/li\u003e\n\u003cli\u003e§2.4.2.4 — Circuit d’orientation des roues du train avant (secours)\u003c\/li\u003e\n\u003cli\u003e§2.4.2.5 — Circuit de freinage (normal)\u003c\/li\u003e\n\u003cli\u003e§2.4.2.6 — Circuit de freinage (secours)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cem\u003eCircuits Annexes:\u003c\/em\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e§2.4.2.7 — Circuits des servo-gouvernes et des sensibilisateurs\u003c\/li\u003e\n\u003cli\u003e§2.4.2.9 — Circuit d’ouverture et fermeture des aérofreins\u003c\/li\u003e\n\u003cli\u003e§2.4.2.10 — Circuit d’orientation d’antenne radar (valable 304 à 310)\u003c\/li\u003e\n\u003cli\u003e§2.4.2.10.1 — Circuit d’orientation d’antenne radar indépendant (valable 311 à 370)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eDocument Identification\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eAircraft:\u003c\/strong\u003e SNCASO S.O. 4050 Vautour N (Version N — header: S.O. VAUTOUR – N)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDocument:\u003c\/strong\u003e Notice Descriptive et de Fonctionnement — Tome II, Chapitre 2: §2.4 Installation Hydraulique\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eRevision:\u003c\/strong\u003e 15 Janvier 1958\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePagination:\u003c\/strong\u003e Pages 2401–2407A+ (SNCASO original pagination)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eHydraulic Fluid Spec:\u003c\/strong\u003e FHS 1 (Norme AIR 3520)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePlanches Referenced:\u003c\/strong\u003e 301–323 (Génération Principale \u0026amp; Secours complete component set)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eVariant Coverage:\u003c\/strong\u003e Avions 304–310 (radar orientation) and 311–370 (independent radar orientation circuit)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eLanguage:\u003c\/strong\u003e French \/ Français\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCompanion Volume:\u003c\/strong\u003e NDF Tome I Texte (Edition Transitoire, 31 Juillet 1957)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003cp\u003e⚠️ \u003cstrong\u003eRegulatory Notice:\u003c\/strong\u003e Under FAA 14 CFR § 43.13 and EASA Part-M, any mechanic performing maintenance on an active aircraft must use current, manufacturer-approved revision-controlled data. This archival document does not satisfy that requirement.\u003c\/p\u003e\n\u003cp\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorised distributor.\u003cbr\u003e\u003cem\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/em\u003e\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53658778141019,"sku":null,"price":45.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/vautour-iin-banner-fr-301-white-scheme.png?v=1785065223"},{"product_id":"nord-3400-norbarbe-primary-source-documentation-collection","title":"Nord 3400 Norbarbe — Primary-Source Documentation Collection","description":"\u003ch3\u003eNord 3400 Norbarbe — Primary-Source Documentation Collection\u003c\/h3\u003e\n\u003cp\u003eThe \u003cstrong\u003eNord 3400 Norbarbe\u003c\/strong\u003e was a braced high-wing observation and liaison monoplane developed by \u003cstrong\u003eNord Aviation\u003c\/strong\u003e (Société Nationale de Constructions Aéronautiques du Nord) for the French Army's \u003cem\u003eAviation Légère de l'Armée de Terre\u003c\/em\u003e (ALAT). Designed for short-field operations, low-speed stability, and direct battlefield observation, the Norbarbe served as a primary platform for French Army aviation in the late 1950s and early 1960s. This collection assembles the original factory and military documentation issued for the type — a rare and cohesive primary-source archive.\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eEngineering \u0026amp; Technical Profile\u003c\/h3\u003e\n\u003ch4\u003e1. Aerodynamic Specifications\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eAirfoil:\u003c\/strong\u003e NACA 23015 — high C\u003csub\u003eLmax\u003c\/sub\u003e, gentle stall behavior\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eWing Area:\u003c\/strong\u003e 20.82 m² (224.1 sq ft) | Aspect Ratio: 8.2 | Dihedral: 2°\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eHigh-Lift Devices:\u003c\/strong\u003e Large trailing-edge flaps for significantly reduced stall speed\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eStructure:\u003c\/strong\u003e All-metal primary structure; fabric-covered control surfaces; wings fold flat for transport\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch4\u003e2. Powerplant\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eEngine:\u003c\/strong\u003e Potez 4D-34 — 4-cylinder, air-cooled, inverted inline piston\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePower Output:\u003c\/strong\u003e 194 kW (260 hp) supercharged\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePropeller:\u003c\/strong\u003e Ratier Type 24-56 adjustable-pitch, 2-bladed, Ø 2.25 m (7 ft 5 in)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFuel Capacity:\u003c\/strong\u003e 220 L (58.1 US gal) — two self-sealing rubber tanks\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch4\u003e3. Handling \u0026amp; Stability\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003eHigh lateral static stability from high-wing architecture and 2° dihedral\u003c\/li\u003e\n\u003cli\u003eTraditional tailwheel configuration with braced horizontal stabilizer\u003c\/li\u003e\n\u003cli\u003eRear observer's seat rotates 360° for full sightline coverage\u003c\/li\u003e\n\u003cli\u003eTandem two-seat crew cabin optimized for observation missions\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch4\u003e4. Performance Data\u003c\/h4\u003e\n\u003ctable\u003e\n\u003cthead\u003e\n\u003ctr\u003e\n\u003cth\u003eMetric\u003c\/th\u003e\n\u003cth\u003eMetric Unit\u003c\/th\u003e\n\u003cth\u003eImperial Unit\u003c\/th\u003e\n\u003c\/tr\u003e\n\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eMTOW\u003c\/td\u003e\n\u003ctd\u003e1,350 kg\u003c\/td\u003e\n\u003ctd\u003e2,976 lb\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eEmpty Weight (Equipped)\u003c\/td\u003e\n\u003ctd\u003e920 kg\u003c\/td\u003e\n\u003ctd\u003e2,028 lb\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Cruise Speed\u003c\/td\u003e\n\u003ctd\u003e235 km\/h\u003c\/td\u003e\n\u003ctd\u003e127 kts\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eStall Speed (Flaps Extended)\u003c\/td\u003e\n\u003ctd\u003e62 km\/h\u003c\/td\u003e\n\u003ctd\u003e34 kts\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eService Ceiling\u003c\/td\u003e\n\u003ctd\u003e3,000 m\u003c\/td\u003e\n\u003ctd\u003e9,842 ft\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Range\u003c\/td\u003e\n\u003ctd\u003e1,000 km\u003c\/td\u003e\n\u003ctd\u003e540 NM\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eTakeoff Run\u003c\/td\u003e\n\u003ctd\u003e\u0026lt; 100 m\u003c\/td\u003e\n\u003ctd\u003e\u0026lt; 328 ft\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\n\u003chr\u003e\n\u003ch3\u003eDocument Manifest\u003c\/h3\u003e\n\u003cp\u003eThis collection contains \u003cstrong\u003e6 unique primary-source documents\u003c\/strong\u003e issued by Nord Aviation and the French Ministère des Armées (Direction Centrale du Matériel):\u003c\/p\u003e\n\u003col\u003e\n\u003cli\u003e\n\u003cstrong\u003eNord Aviation Sales Brochure — Avion Nord 3400\u003c\/strong\u003e | Nord Aviation, Châtillon-sous-Bagneux | Pre-series factory brochure\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eManuel de l'Equipage de l'Avion Nord 3400 — Partie Planches\u003c\/strong\u003e | MAT 8250 | Ministère des Armées — Terre, Direction Centrale du Matériel | Approved: Decision No. 16216\/DCMAA\/ALAT\/SC, 12 April 1962 | Edition 1962 | Print run: 400\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eManuel de l'Equipage de l'Avion Nord 3400 — Partie Texte\u003c\/strong\u003e | MAT 8250 | Ministère des Armées — Terre, Direction Centrale du Matériel | Approved: Decision No. 16216\/DCMAA\/ALAT\/SC, 12 April 1962 | Edition 1962 | Print run: 400\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNotice Descriptive et de Fonctionnement de l'Avion Nord 3400 — Partie Planches\u003c\/strong\u003e | MAT 8252 | Ministère des Armées — Terre, Direction Centrale du Matériel | Approved: Decision No. 42653\/STAé\/A5, 6 December 1962 | Edition 1962 | Print run: 350\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNotice Descriptive et de Fonctionnement de l'Avion Nord 3400 — Partie Texte\u003c\/strong\u003e | MAT 8252 | Ministère des Armées — Terre, Direction Centrale du Matériel | Approved: Decision No. 42653\/STAé\/A5, 6 December 1962 | Edition 1962 | Print run: 350\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eManuel d'Utilisation de l'Avion Nord 3400\u003c\/strong\u003e | École de Spécialisation de l'Aviation Légère de l'Armée de Terre (ALAT) | Edition: May 1961\u003c\/li\u003e\n\u003c\/ol\u003e\n\u003chr\u003e\n\u003cp\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorized distributor.\u003cbr\u003e\u003cem\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/em\u003e\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53658965082459,"sku":null,"price":35.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/banner-1-formation-flight-redo-3.png?v=1785069201"},{"product_id":"nord-2501-noratlas-primary-source-documentation-collection","title":"Nord 2501 Noratlas — Primary-Source Documentation Collection","description":"\u003ch3\u003eNord 2501 Noratlas — Primary-Source Documentation Collection\u003c\/h3\u003e\n\u003cp\u003eThe \u003cstrong\u003eNord 2501 Noratlas\u003c\/strong\u003e was a twin-boom, high-wing tactical transport aircraft developed by the \u003cstrong\u003eSociété Nationale de Constructions Aéronautiques du Nord (SNCAN)\u003c\/strong\u003e and operated by both the \u003cem\u003eArmée de l'Air\u003c\/em\u003e and the \u003cstrong\u003eGerman Luftwaffe\u003c\/strong\u003e as a primary medium tactical airlifter throughout the 1950s and 1960s. Engineered for rear-loading cargo drops, paratroop operations, and austere-field performance, the Noratlas became one of the defining NATO tactical transports of the Cold War era. This collection assembles the original French military and German Luftwaffe documentation issued for the type — a rare bilingual primary-source archive spanning two air forces.\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eEngineering \u0026amp; Technical Profile\u003c\/h3\u003e\n\u003ch4\u003e1. Aerodynamic Configuration\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eWing Profile:\u003c\/strong\u003e NACA 23018 at root tapering to NACA 23010 at tip — prevents tip stall under high-lift conditions\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eWing Area:\u003c\/strong\u003e 101.2 m² (1,089 sq ft) | Aspect ratio optimized for low-altitude, high-lift tactical performance\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTwin-Boom Architecture:\u003c\/strong\u003e Tail booms integrated directly into engine nacelles — straightens boundary layer airflow, reduces rear fuselage buffeting\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAileron System:\u003c\/strong\u003e Differential slotted ailerons maintain roll authority through deep high-angle-of-attack profiles\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch4\u003e2. Powerplant\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eEngines:\u003c\/strong\u003e 2× SNECMA-built Bristol Hercules 738\/739 or 759 — 14-cylinder, sleeve-valve radial\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePower Output:\u003c\/strong\u003e 2,040–2,090 metric hp (1,558 kW) per engine at takeoff\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePropeller:\u003c\/strong\u003e Four-bladed, variable-pitch, fully feathering constant-speed system\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSleeve-Valve Design:\u003c\/strong\u003e Reciprocating rotating sleeve regulates intake\/exhaust timing — eliminates traditional poppet valves\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch4\u003e3. Handling \u0026amp; Stability\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003eDual vertical fins deliver immense directional authority during asymmetric engine-out scenarios at low speed\u003c\/li\u003e\n\u003cli\u003eHigh-mounted horizontal stabilizer positioned clear of wing wake and propeller slipstream wash\u003c\/li\u003e\n\u003cli\u003eCG shift verified minimal during sequential 35-paratrooper jumps or rapid heavy cargo drops\u003c\/li\u003e\n\u003cli\u003eCertified for aggressive 25° glide slopes into hostile or confined sectors\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch4\u003e4. Performance Data\u003c\/h4\u003e\n\u003ctable\u003e\n\u003cthead\u003e\n\u003ctr\u003e\n\u003cth\u003eMetric\u003c\/th\u003e\n\u003cth\u003eImperial Unit\u003c\/th\u003e\n\u003cth\u003eMetric Unit\u003c\/th\u003e\n\u003c\/tr\u003e\n\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eEmpty Weight\u003c\/td\u003e\n\u003ctd\u003e29,327 lb\u003c\/td\u003e\n\u003ctd\u003e13,302 kg\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMTOW\u003c\/td\u003e\n\u003ctd\u003e45,423 lb\u003c\/td\u003e\n\u003ctd\u003e20,603 kg\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Payload\u003c\/td\u003e\n\u003ctd\u003e18,647 lb\u003c\/td\u003e\n\u003ctd\u003e8,458 kg\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Cruise Speed\u003c\/td\u003e\n\u003ctd\u003e270 mph\u003c\/td\u003e\n\u003ctd\u003e440 km\/h\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eService Ceiling\u003c\/td\u003e\n\u003ctd\u003e22,965 ft\u003c\/td\u003e\n\u003ctd\u003e7,000 m\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Range\u003c\/td\u003e\n\u003ctd\u003e1,600 miles\u003c\/td\u003e\n\u003ctd\u003e2,500 km\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\n\u003ch4\u003e5. Variants \u0026amp; Engineering Bulletins\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eNord 2501-D (Luftwaffe Standard):\u003c\/strong\u003e French instrumentation and avionics replaced with German-manufactured equivalents\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNord 2502 (Turbojet Boost):\u003c\/strong\u003e Two wingtip-mounted Turbomeca Marboré IIE auxiliary turbojets (400 kgp each) for hot-and-high performance\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNord 2504 (ASW Testbed):\u003c\/strong\u003e Reinforced underwing hardpoints, retractable surface-search radar, sonic buoy launch tubes\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eStructural Bulletins:\u003c\/strong\u003e Local reinforcement of main landing gear attach points and bays for unpaved runway operations\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eDocument Manifest\u003c\/h3\u003e\n\u003cp\u003eThis collection contains \u003cstrong\u003e5 unique primary-source documents\u003c\/strong\u003e issued by the French Direction Centrale du Matériel, SNCAN, and the German Materialamt\/Luftwaffenamt:\u003c\/p\u003e\n\u003col\u003e\n\u003cli\u003e\n\u003cstrong\u003eManuel d'Utilisation de l'Avion Nord 2501 — Partie Planches\u003c\/strong\u003e | Identification: UCD 101 | Direction Centrale du Matériel | Edition: Mars 1968 — Approuvée par DM N° 1225\/EMAA\/3\/SV du 6 Mars 1968 | Mise à jour: Janvier 1971 — Approuvée par DM N° 101 484\/DCMAA\/MT2 du 26 Janvier 1971 | Print run: 700\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eManuel d'Utilisation de l'Avion Nord 2501 — Partie Texte\u003c\/strong\u003e | Identification: UCD 101 | Direction Centrale du Matériel | Edition: Mars 1968 — Approuvée par DM N° 1225\/EMAA\/3\/SV du 6 Mars 1968 | Mise à jour: Janvier 1971 — Approuvée par DM N° 101 484\/DCMAA\/MT2 du 26 Janvier 1971 | Print run: 700\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNoratlas 2501D — Flughandbuch\u003c\/strong\u003e | Reference: GAF T.O.1C-NOR2501-1 | Materialamt der Luftwaffe | Herausgegeben mit Genehmigung des Bundesministers der Verteidigung — Führungsstab der Luftwaffe (F·L) | Date: 1 November 1969 | HFB 800\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNoratlas — Standing Operating Procedures, Part III\u003c\/strong\u003e | Luftwaffenamt | Date: 1 October 1965 | Sections A–M: Introduction, Ground Operation, Normal Flight Procedures, Instrument Flying (Basic Instruments), Instrument Flying (Radio Navigation), Night Flying, Cross Country Flying, Cruise Control, Voice Procedures, Check Flights, Standardization Check for IPs and Instr.-Check-Pilots, Recurrency Program | Language: English\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNoratlas (N. 2501) — Notice A. 101\u003c\/strong\u003e | SNCAN (Société Nationale de Constructions Aéronautiques du Nord) | Reference: Notice A. 101 | Illustrated technical\/promotional brochure covering origins, military cargo operations (troops, paratroops, cargo, jeeps, light tanks, parachuting duties) and civil cargo operations (passengers, freight, vehicles) | Language: English\u003c\/li\u003e\n\u003c\/ol\u003e\n\u003chr\u003e\n\u003cp\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorized distributor.\u003cbr\u003e\u003cem\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/em\u003e\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53659010236763,"sku":null,"price":25.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/banner-3-luftwaffe-banking.png?v=1785070836"},{"product_id":"nord-1000-1001-1002-pingouin-aerodynamic-engine-stability-documentation","title":"Nord 1000 · 1001 · 1002 Pingouin — Aerodynamic, Engine \u0026 Stability Documentation","description":"\u003ch3\u003eNord 1000 · 1001 · 1002 \u003cem\u003ePingouin\u003c\/em\u003e — Aerodynamic, Engine \u0026amp; Stability Documentation\u003c\/h3\u003e\u003cp\u003eThe technical documentation, aerodynamic reports, engine specifications, and stability profiles for the Nord 1000, 1001, and 1002 \u003cem\u003ePingouin\u003c\/em\u003e series trace directly back to their origins as French-manufactured variants of the German Messerschmitt Bf 108 Taifun. Production was transferred to the \u003cstrong\u003eSNCAN (Société Nationale des Constructions Aéronautiques du Nord)\u003c\/strong\u003e facility at Les Mureaux in occupied France in 1942. Following the liberation, Nord continued compiling engineering data sheets and operational modifications to transition the airframes from German powerplants to indigenous French engines.\u003c\/p\u003e\u003chr\u003e\u003ch3\u003eDocument Manifest — What You Receive\u003c\/h3\u003e\u003cp\u003eThis collection comprises \u003cstrong\u003e3 primary-source archival documents\u003c\/strong\u003e, each reproduced in full as a static-copy digital edition:\u003c\/p\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eDocument 1 — Avions Nord 1000 · 1001 · 1002 · Fascicule 1 · Caractéristiques\u003c\/strong\u003e\u003cbr\u003eReference: N.C.E. 45A · Catégorie AV · Approved by D.M. N° 37.633 STA A2, 14 November 1945\u003cbr\u003ePublisher: Ministère de l'Air — Service du Matériel · Language: French\u003cbr\u003eContent: Official aerodynamic characteristics booklet. Data recorded on Nord 1000 No. 23 and Nord 1001 No. 68 during official flight trials.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDocument 2 — Me 108 B Messerschmitt-Taifun · Betriebs- und Rüstanleitung\u003c\/strong\u003e\u003cbr\u003eReference: Reg. Nr. 147 · Ausgabe August 1939\u003cbr\u003ePublisher: Messerschmitt A.G., Augsburg · Language: German\u003cbr\u003eContent: Original Operations and Equipment Manual for the Bf 108 B — the direct engineering ancestor of the Nord 1000 series. Covers powerplant operation, airframe servicing, and equipment preparation procedures.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDocument 3 — Nomenclature Illustrée de l'Avion Ramier I · Fascicule 1 · Avant-Propos\u003c\/strong\u003e\u003cbr\u003eReference: Classification ACE.15 · Classification Collective N° 50 · Approved by D.M. N° 0120\/SMAA\/Tech.1, 18 January 1951 · Edition: June 1951 · Print run: 470 copies\u003cbr\u003ePublisher: Service des Marchés et de la Production Aéronautique · Language: French\u003cbr\u003eContent: Illustrated Parts Catalog (IPC) for the Nord 1001 Pingouin I. The Ramier I is the French Air Force designation for the Nord 1001 Pingouin I in liaison service. This fascicule covers the introductory nomenclature and parts classification structure for the Renault 6Q-11 powered variant.\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003ch3\u003eAerodynamic Profiles \u0026amp; Design Specifications\u003c\/h3\u003e\u003cp\u003eThe aerodynamic profile across the 1000-series baseline utilises the low-wing, all-metal monoplane configuration inherited directly from the Messerschmitt Bf 108.\u003c\/p\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eWing Geometry:\u003c\/strong\u003e Outfitted with specialised automatic leading-edge Handley Page slots to optimise low-speed lift airflow and minimise stall tendencies during high angle-of-attack approaches.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eControl Surfaces:\u003c\/strong\u003e Employs narrow-chord ailerons coupled with trailing-edge camber-changing flaps, managed via mechanical linkages to maximise lift coefficients during short-field operations.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eRetractable Landing Gear:\u003c\/strong\u003e Narrow-track taildragger configuration — main wheels retract outward into outer wing wells via a pneumatically assisted manual wobble pump system located on the cockpit centre console.\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003ch3\u003eEngine Technical Notes \u0026amp; Powertrain Transitions\u003c\/h3\u003e\u003cp\u003eThe foundational engineering differences between the three distinct variants reside primarily in the specific powerplants utilised and their respective thrust rotation directions.\u003c\/p\u003e\u003ctable\u003e\n\u003cthead\u003e\u003ctr\u003e\n\u003cth\u003eAircraft Variant\u003c\/th\u003e\n\u003cth\u003eEngine Model\u003c\/th\u003e\n\u003cth\u003eHorsepower\u003c\/th\u003e\n\u003cth\u003ePropeller Rotation\u003c\/th\u003e\n\u003cth\u003eTechnical Note\u003c\/th\u003e\n\u003c\/tr\u003e\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eNord 1000\u003c\/td\u003e\n\u003ctd\u003eArgus As 10C\u003c\/td\u003e\n\u003ctd\u003e240 hp\u003c\/td\u003e\n\u003ctd\u003eClockwise\u003c\/td\u003e\n\u003ctd\u003eBuilt from leftover German component stock.\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eNord 1001 Pingouin I\u003c\/td\u003e\n\u003ctd\u003eRenault 6Q-11\u003c\/td\u003e\n\u003ctd\u003e233 hp\u003c\/td\u003e\n\u003ctd\u003eCounter-Clockwise\u003c\/td\u003e\n\u003ctd\u003eInverted inline 6-cylinder configuration.\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eNord 1002 Pingouin II\u003c\/td\u003e\n\u003ctd\u003eRenault 6Q-10\u003c\/td\u003e\n\u003ctd\u003e230 hp\u003c\/td\u003e\n\u003ctd\u003eClockwise\u003c\/td\u003e\n\u003ctd\u003eIdentical to 6Q-11 but with inverted rotation gears.\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\u003chr\u003e\u003ch3\u003eHandling, Stability \u0026amp; Control Studies\u003c\/h3\u003e\u003cp\u003eTransitioning from the Argus V-8 engine to the longer, inverted Renault inline-6 shifted the centre of gravity (CoG) slightly forward, requiring explicit handling considerations for flight crews.\u003c\/p\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eDirectional Trim Dynamics:\u003c\/strong\u003e The counter-clockwise rotation of the Renault 6Q-11 in the Nord 1001 required opposite rudder trim inputs during high-power takeoffs and climbs relative to the standard clockwise configuration of the Nord 1000 and 1002.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eLow-Speed Stability:\u003c\/strong\u003e Longitudinal control remains responsive at lower airspeed envelopes due to the localised wing slot design. Pilots must monitor the narrow landing gear tracking (2.2 m wheelbase), which makes the aircraft susceptible to ground loops during severe crosswind roll-outs.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePneumatic Interlocking:\u003c\/strong\u003e Technical manuals highlight that extending and retracting landing gear changes pitching moments subtly. The pilot must manually modulate pitch attitude while pumping the manual mechanical floor actuator.\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003ch3\u003ePerformance Data Sheets (ISA Conditions)\u003c\/h3\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eMaximum Airspeed (VNE):\u003c\/strong\u003e 305 km\/h (190 mph) at sea level.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCruise Speed (VC):\u003c\/strong\u003e 260 km\/h (162 mph) at optimum pressure altitude.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMaximum Operational Range:\u003c\/strong\u003e Approximately 1,000 km (621 miles) under baseline fuel loads.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMaximum Takeoff Weight (MTOW):\u003c\/strong\u003e 1,350 kg to 1,700 kg depending on cabin configuration and payload modifications.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDimensional Layout:\u003c\/strong\u003e Total airframe length 8.29 m (27 ft 2 in) · Wingspan 10.61 m (34 ft 10 in).\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003ch3\u003eEngineering Bulletins \u0026amp; Historical Archives\u003c\/h3\u003e\u003cp\u003eOriginal structural drawings, airworthiness directives, and engine maintenance guidelines are archived under the structural designation lists of the French Air Force (Armée de l'Air) and Naval Aviation (Aéronavale), where they served in liaison roles until 1962. Historical flight operating handbooks and structural repair prints cover structural inspections, Renault engine timing setups, and skin-stress loading margins.\u003c\/p\u003e\u003chr\u003e\u003cp\u003e\u003cem\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorised distributor.\u003c\/em\u003e\u003c\/p\u003e\u003cp\u003e\u003cstrong\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/strong\u003e\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53659046674779,"sku":null,"price":100.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/banner-4-hero-g-otme-in-flight-color.png?v=1785072979"},{"product_id":"nord-mh260-super-broussard-maintenance-flight-manual-archive","title":"Max Holste \/ Nord MH.260 Super Broussard — Maintenance Manual \u0026 Flight Manual Archive","description":"\u003ch2\u003eMax Holste \/ Nord MH.260 Super Broussard\u003c\/h2\u003e\u003ch3\u003ePrimary-Source Technical Documentation Archive — Nord-Aviation, 1962–1963\u003c\/h3\u003e\u003cp\u003eThe \u003cstrong\u003eMax Holste MH.260 Super Broussard\u003c\/strong\u003e, later produced as the \u003cstrong\u003eNord 260\u003c\/strong\u003e by Société Nationale de Constructions Aéronautiques (Nord-Aviation), was a rugged, high-wing, unpressurized regional turboprop developed in France during the late 1950s and early 1960s. Engineered for short-takeoff-and-landing (STOL) performance on unpaved airstrips, the Nord 260 bridged the gap between the piston-powered MH.250 prototype and the pressurized Aérospatiale\/Nord 262 that followed. Only 10 production units were built, making original factory documentation exceptionally rare.\u003c\/p\u003e\u003cp\u003eThis archival collection brings together three original Nord-Aviation publications issued between September 1962 and February 1963 — the complete primary-source maintenance and instruction manual set for the Nord 260 \/ Super Broussard.\u003c\/p\u003e\u003chr\u003e\u003ch3\u003eDocument Manifest\u003c\/h3\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eManuel d'Entretien — Planches\u003c\/strong\u003e (Maintenance Manual — Plates \/ Diagrams)\u003cbr\u003eRef: N° 26C-10-09-503 · Exemplaire N° 28 · Septembre 1962\u003cbr\u003eNord-Aviation, Société Nationale de Constructions Aéronautiques\u003cbr\u003eLanguage: French\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eManuel d'Entretien — Texte, Tome 1\u003c\/strong\u003e (Maintenance Manual — Text, Volume 1)\u003cbr\u003eRef: N° 260-10-09-603 · Exemplaire N° 5 · Septembre 1962\u003cbr\u003eNord-Aviation, Société Nationale de Constructions Aéronautiques\u003cbr\u003eLanguage: French\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eManuel d'Instruction de l'Avion Nord 260 — Tome II, Partie: Texte\u003c\/strong\u003e (Aircraft Instruction Manual — Volume II, Text Section)\u003cbr\u003eBi-turbopropulseur Bastan IV · Exemplaire N° 22 · Février 1963\u003cbr\u003eLanguage: French\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003ch3\u003eAircraft Technical Profile\u003c\/h3\u003e\u003ch4\u003eAerodynamic \u0026amp; Structural Design\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003eHigh-wing cantilever monoplane — all-metal twin-spar torsion box construction\u003c\/li\u003e\n\u003cli\u003eAspect ratio ≈ 10 — optimized for high lift at low approach and takeoff speeds\u003c\/li\u003e\n\u003cli\u003eAll-aluminum semi-monocoque fuselage with unpressurized square cross-section for maximum freight\/passenger volume\u003c\/li\u003e\n\u003cli\u003eSlot-type ailerons and double-slotted trailing-edge flaps; fabric-covered control surfaces over aluminum frames\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch4\u003ePropulsion\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003eTwo \u003cstrong\u003eTurbomeca Bastan IV\u003c\/strong\u003e single-shaft turboprop engines\u003c\/li\u003e\n\u003cli\u003ePower output: ≈ 986 hp (735 kW) per engine\u003c\/li\u003e\n\u003cli\u003eRatier-Figeac three-blade, variable-pitch, fully feathering metal propellers\u003c\/li\u003e\n\u003cli\u003eDeeply underslung engine nacelles for optimal ground clearance and maintenance access\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch4\u003eHandling \u0026amp; Stability\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003eHigh-wing layout provides strong inherent lateral\/dihedral stability, mitigating Dutch roll\u003c\/li\u003e\n\u003cli\u003eLarge vertical stabilizer and rudder preserve yaw authority at low airspeeds (engine-out Vmc)\u003c\/li\u003e\n\u003cli\u003eRetractable tricycle undercarriage with wide-track main gear retracting into fuselage-mounted fairings — reduced crosswind tipping risk on unpaved fields\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch4\u003ePerformance Data\u003c\/h4\u003e\u003ctable\u003e\n\u003cthead\u003e\u003ctr\u003e\n\u003cth\u003eParameter\u003c\/th\u003e\n\u003cth\u003eValue\u003c\/th\u003e\n\u003c\/tr\u003e\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Takeoff Weight (MTOW)\u003c\/td\u003e\n\u003ctd\u003e9,800 kg (21,605 lb)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eOptimum Cruise Speed\u003c\/td\u003e\n\u003ctd\u003e195 kt (361 km\/h)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Rate of Climb\u003c\/td\u003e\n\u003ctd\u003e2,500 ft\/min (12.7 m\/s)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eOptimum Cruise Ceiling\u003c\/td\u003e\n\u003ctd\u003e18,000 ft\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eAbsolute Service Ceiling\u003c\/td\u003e\n\u003ctd\u003e25,000 ft\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Passenger Capacity\u003c\/td\u003e\n\u003ctd\u003e23–25 passengers\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Structural Payload\u003c\/td\u003e\n\u003ctd\u003e3,885 kg (8,565 lb)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\u003chr\u003e\u003ch3\u003eProgramme History\u003c\/h3\u003e\u003cp\u003eFinancial constraints at \u003cstrong\u003eAvions Max Holste\u003c\/strong\u003e forced a corporate restructuring; \u003cstrong\u003eNord-Aviation\u003c\/strong\u003e assumed production and formally redesignated the aircraft the \u003cstrong\u003eNord 260\u003c\/strong\u003e. Engineering lessons compiled from Nord 260 service bulletins directly informed a complete redesign, culminating in the \u003cstrong\u003eAérospatiale\/Nord 262\u003c\/strong\u003e — a pressurized, circular-fuselage successor better suited to modern airline networks. The Nord 260 thus occupies a pivotal position in French regional aviation history: a rare, short-lived platform whose engineering legacy outlasted its own production run.\u003c\/p\u003e\u003chr\u003e\u003cp\u003e\u003cem\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorized distributor.\u003c\/em\u003e\u003c\/p\u003e\u003cp\u003e\u003cem\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/em\u003e\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53659146191195,"sku":null,"price":24.85,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/banner-1-landscape-hero.png?v=1785076220"},{"product_id":"nord-sncan-1200-norecrin-carte-de-service-brochure-archive","title":"Nord (SNCAN) 1200 Norécrin — Carte de Service \u0026 Sales Brochure Archive","description":"\u003ch2\u003eNord (SNCAN) 1200 Norécrin\u003c\/h2\u003e\u003ch3\u003ePrimary-Source Technical Documentation Archive — Société Nationale de Constructions Aéronautiques du Nord (SNCAN)\u003c\/h3\u003e\u003cp\u003eThe \u003cstrong\u003eNord 1200 Norécrin\u003c\/strong\u003e, designed and produced by the \u003cstrong\u003eSociété Nationale de Constructions Aéronautiques du Nord (SNCAN)\u003c\/strong\u003e, stands as one of the most significant postwar French light aircraft programmes. Conceived in the final years of the Second World War and first flown in December 1945, the Norécrin introduced a modern, low-wing, all-metal cantilever monoplane configuration with a fully retractable tricycle undercarriage — a bold engineering statement for a four-seat touring aircraft of its era. The type evolved through five principal variants (Norécrin I through V), culminating in the armed military \u003cstrong\u003eNord 1203 Norécrin V\u003c\/strong\u003e equipped with machine-gun and rocket mounts.\u003c\/p\u003e\u003cp\u003eThis archival collection brings together original SNCAN factory publications covering the Norécrin II (Type 1203, Régnier 4L00) — the definitive four-seat touring variant — including the official Carte de Service and period sales brochure material.\u003c\/p\u003e\u003chr\u003e\u003ch3\u003eDocument Manifest\u003c\/h3\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eCarte de Service de l'Avion Norécrin II — Quadriplace\u003c\/strong\u003e\u003cbr\u003eType 1203 · à moteur Régnier 4L00\u003cbr\u003eCaractéristiques · Utilisation · Entretien\u003cbr\u003eÉdition revue et corrigée en Septembre 1950 (annule et remplace l'édition d'Août 1948)\u003cbr\u003eNombre d'exemplaires: 200\u003cbr\u003eLanguage: French\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eLe Norécrin — Brochure Commerciale\u003c\/strong\u003e (Sales Brochure, Title Page)\u003cbr\u003eSNCAN — Société Nationale de Constructions Aéronautiques du Nord\u003cbr\u003eLanguage: French\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eLe Norécrin II — Brochure Commerciale\u003c\/strong\u003e\u003cbr\u003eAvion Quadriplace d'Affaires · de Tourisme · de Transport Public\u003cbr\u003e«C'est une production de la Société Nationale de Constructions Aéronautiques du Nord»\u003cbr\u003eLanguage: French\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003ch3\u003eAircraft Technical Profile\u003c\/h3\u003e\u003ch4\u003eAerodynamic \u0026amp; Structural Design\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003eLow-wing cantilever monoplane — all-metal tapered wing with clean wing-to-fuselage fairings\u003c\/li\u003e\n\u003cli\u003eFully retractable tricycle undercarriage — wide-track layout providing excellent ground handling and crosswind control, significantly reducing parasitic drag vs. contemporary tailwheel designs\u003c\/li\u003e\n\u003cli\u003eConventional mechanical flight controls: responsive ailerons, elevators, and rudder\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch4\u003ePropulsion — Variant Evolution\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003ePrototype:\u003c\/strong\u003e Mathis G4-R, 75 kW (100 hp)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNorécrin I\/II early:\u003c\/strong\u003e Renault 4Pei \/ 4P-01, 100 kW (140 hp)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNorécrin II (Type 1203):\u003c\/strong\u003e Régnier 4L-00 inverted inline, 135 hp\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNorécrin IV:\u003c\/strong\u003e Régnier 4L-02 inverted inline, 170 hp\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNorécrin V (military):\u003c\/strong\u003e Armed variant with machine-gun and rocket mounts\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch4\u003ePerformance Data\u003c\/h4\u003e\u003ctable\u003e\n\u003cthead\u003e\u003ctr\u003e\n\u003cth\u003eParameter\u003c\/th\u003e\n\u003cth\u003eValue\u003c\/th\u003e\n\u003c\/tr\u003e\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Speed\u003c\/td\u003e\n\u003ctd\u003e137 mph (119 kt)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Range\u003c\/td\u003e\n\u003ctd\u003e559 miles (485 NM)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Climb Rate\u003c\/td\u003e\n\u003ctd\u003e710 ft\/min\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eAbsolute Ceiling\u003c\/td\u003e\n\u003ctd\u003e17,000 ft\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eEmpty Weight\u003c\/td\u003e\n\u003ctd\u003e650 kg\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Takeoff Weight (MTOW)\u003c\/td\u003e\n\u003ctd\u003e1,050 kg\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eWingspan \/ Length\u003c\/td\u003e\n\u003ctd\u003e10.22 m \/ 7.21 m\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\u003chr\u003e\u003ch3\u003eEngineering Bulletin Highlights\u003c\/h3\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eCabin Reconfigurations:\u003c\/strong\u003e Factory transition from 2-seat prototype to 3-seat (Norécrin I) and 4-seat quadriplace layouts\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eLanding Gear Modifications:\u003c\/strong\u003e Transition to heavy-duty tricycle configuration on the Norécrin III\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMilitary Retrofit Schematics:\u003c\/strong\u003e Loading sheets and armament installation data for the Nord 1203 Norécrin V\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003cp\u003e\u003cem\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorized distributor.\u003c\/em\u003e\u003c\/p\u003e\u003cp\u003e\u003cem\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/em\u003e\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53659169423707,"sku":null,"price":14.85,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/banner-2-wide-leaderboard_45393822-a85e-4502-b357-22ca4abaa7c6.png?v=1785077257"},{"product_id":"nord-aviation-3202-manuel-utilisation-brochure-archive","title":"Nord Aviation 3202 — Manuel d'Utilisation \u0026 Brochure Archive","description":"\u003ch2\u003eNord Aviation 3202\u003c\/h2\u003e\u003ch3\u003ePrimary-Source Technical Documentation Archive — Nord-Aviation \/ École de Spécialisation de l'Aviation Légère de l'Armée de Terre (ALAT)\u003c\/h3\u003e\u003cp\u003eThe \u003cstrong\u003eNord Aviation 3202\u003c\/strong\u003e is a fully aerobatic, tandem-seat basic trainer designed in the early 1950s to replace the \u003cstrong\u003eStampe SV.4\u003c\/strong\u003e biplane for the \u003cstrong\u003eFrench Army Light Aviation (Aviation Légère de l'Armée de Terre — ALAT)\u003c\/strong\u003e. A clean, low-wing cantilever monoplane with a fixed tailwheel undercarriage and an inverted engine system for sustained negative-G flight, the Nord 3202 bridged the gap between elementary piston trainers and the demanding North American T-6 Texan. Its handling qualities were described by instructors as transitional between a de Havilland Chipmunk and a T-6 — a precise, responsive platform that produced a generation of French Army aviators.\u003c\/p\u003e\u003cp\u003eThis archival collection presents two original Nord-Aviation publications: the official French Army \u003cem\u003eManuel d'Utilisation\u003c\/em\u003e (January 1963, \u003cem\u003eDiffusion Restreinte\u003c\/em\u003e) and the Nord-Aviation commercial brochure for the N.3202.\u003c\/p\u003e\u003chr\u003e\u003ch3\u003eDocument Manifest\u003c\/h3\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eManuel d'Utilisation de l'Avion Nord 3202\u003c\/strong\u003e\u003cbr\u003eÉcole de Spécialisation de l'Aviation Légère de l'Armée de Terre\u003cbr\u003eÉdition de Janvier 1963 · 54 pages\u003cbr\u003e\u003cem\u003eDiffusion Restreinte\u003c\/em\u003e — Ce document ne doit être communiqué qu'aux personnes qualifiées pour le connaître.\u003cbr\u003eLanguage: French\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAvion Biplace d'Entraînement N.3202 — Brochure Commerciale\u003c\/strong\u003e\u003cbr\u003eNord-Aviation · 2 à 18, Rue Béranger, Chatillon-ss-Bagneux, Seine\u003cbr\u003eLanguage: French\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003ch3\u003eAircraft Technical Profile\u003c\/h3\u003e\u003ch4\u003eAerodynamic \u0026amp; Airframe Design\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003eLow-wing cantilever monoplane — NACA 23015 profile at root, tapering to NACA 23012 at wingtips\u003c\/li\u003e\n\u003cli\u003eTotal wing surface area: 16.26 m² (175 sq ft)\u003c\/li\u003e\n\u003cli\u003eFixed cantilever tailwheel undercarriage — engineered for high sink rates during military student instruction\u003c\/li\u003e\n\u003cli\u003eModified variants feature enlarged ailerons for enhanced roll rates in competition aerobatics\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch4\u003ePropulsion\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eNord 3202A:\u003c\/strong\u003e Potez 4D-32 inverted inline air-cooled 4-cylinder — 180 kW (240 hp)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNord 3202B:\u003c\/strong\u003e Potez 4D-34 inverted inline air-cooled 4-cylinder — 194 kW (260 hp)\u003c\/li\u003e\n\u003cli\u003eSpecialized inverted fuel and oil supply systems for sustained negative-G maneuvers\u003c\/li\u003e\n\u003cli\u003eRatier Type 23-92 two-blade adjustable-pitch propeller; variable-pitch on late models\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch4\u003eHandling \u0026amp; Stability\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003eHigh vertical stabilizer providing pronounced directional recovery — stable spin characteristics\u003c\/li\u003e\n\u003cli\u003eFlight control harmony described as transitional between de Havilland Chipmunk and North American T-6 Texan\u003c\/li\u003e\n\u003cli\u003eLater \u003cstrong\u003eNord 3212\u003c\/strong\u003e variant introduced radio compass and advanced blind-flying instruments\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch4\u003ePerformance Data\u003c\/h4\u003e\u003ctable\u003e\n\u003cthead\u003e\u003ctr\u003e\n\u003cth\u003eParameter\u003c\/th\u003e\n\u003cth\u003eValue\u003c\/th\u003e\n\u003c\/tr\u003e\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Speed\u003c\/td\u003e\n\u003ctd\u003e260 km\/h (140 kt) at sea level\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eCruising Speed\u003c\/td\u003e\n\u003ctd\u003e235 km\/h (127 kt) at 2,300 m\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eStall Speed (flaps down)\u003c\/td\u003e\n\u003ctd\u003e102 km\/h (55 kt)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eRate of Climb\u003c\/td\u003e\n\u003ctd\u003e360 m\/min (1,181 ft\/min)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eEmpty Weight\u003c\/td\u003e\n\u003ctd\u003e824 kg (1,817 lb)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Takeoff Weight (MTOW)\u003c\/td\u003e\n\u003ctd\u003e1,220 kg (2,690 lb)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\u003chr\u003e\u003ch3\u003eEngineering \u0026amp; Operations Bulletin Highlights\u003c\/h3\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eManuel d'Utilisation (1963):\u003c\/strong\u003e Primary flight and systems operating instructions issued by the ALAT specialisation school — 54 pages, restricted distribution\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMaintenance Access:\u003c\/strong\u003e Full-length fuselage access panels for rapid component repair turnaround\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNord 3212 Avionics Update:\u003c\/strong\u003e Modified electrical infrastructure accommodating radio compass and blind-flying instrument suite\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003cp\u003e\u003cem\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorized distributor.\u003c\/em\u003e\u003c\/p\u003e\u003cp\u003e\u003cem\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/em\u003e\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53659294728539,"sku":null,"price":14.85,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/banner-2-wide-leaderboard_52152d6f-a8aa-496d-b988-54275f39d44a.png?v=1785078494"},{"product_id":"nord-262-fregate-detailed-model-specification-performance-manual-archive","title":"Nord 262 Frégate — Detailed Model Specification \u0026 Performance Manual Archive","description":"\u003ch2\u003eNord 262 Frégate\u003c\/h2\u003e\u003ch3\u003ePrimary-Source Technical Documentation Archive — Aérospatiale \/ Nord-Aviation, 1970\u003c\/h3\u003e\u003cp\u003eThe \u003cstrong\u003eNord 262 Frégate\u003c\/strong\u003e is a high-wing, twin-turboprop pressurized regional airliner developed by \u003cstrong\u003eNord-Aviation\u003c\/strong\u003e and subsequently produced and marketed by \u003cstrong\u003eAérospatiale\u003c\/strong\u003e. A direct engineering descendant of the unpressurized Nord 260 Super Broussard, the Nord 262 introduced a circular, pressurized fuselage capable of sustained cruise at up to 20,000 ft — transforming the rugged STOL feederliner concept into a credible short-haul airliner. The \u003cstrong\u003eSeries C (Frégate)\u003c\/strong\u003e represented the definitive civil variant, with upgraded Turbomeca Bastan VIIC engines and refined aerodynamics. The type also served with the French Navy and was later converted under the \u003cstrong\u003eMohawk 298\u003c\/strong\u003e programme with Pratt \u0026amp; Whitney Canada PT6A-45 engines for FAA FAR Part 298 certification.\u003c\/p\u003e\u003cp\u003eThis archival collection presents two original Aérospatiale factory publications: the \u003cem\u003eDetailed Model Specification\u003c\/em\u003e (DVE\/N 701, November 1970) and the \u003cem\u003eFrégate Performance Manual\u003c\/em\u003e — the core engineering and operational reference set for the Nord 262 Series C.\u003c\/p\u003e\u003chr\u003e\u003ch3\u003eDocument Manifest\u003c\/h3\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eNord 262 Series C — Frégate Detailed Model Specification\u003c\/strong\u003e\u003cbr\u003eRef: DVE\/N 701 · Issued November 1970\u003cbr\u003eAérospatiale · 37, Boulevard de Montmorency, Paris 16e, France\u003cbr\u003eTurboprop Transport — Detailed Model Specification\u003cbr\u003eLanguage: English\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFrégate Performance Manual\u003c\/strong\u003e\u003cbr\u003eAérospatiale · Nord 262 Series C\u003cbr\u003eGold compass rose cover — Aérospatiale house edition\u003cbr\u003eLanguage: English\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003ch3\u003eAircraft Technical Profile\u003c\/h3\u003e\u003ch4\u003eAerodynamic \u0026amp; Flight Design\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003eHigh-wing configuration — optimizes lift and propeller ground clearance for short-field and unimproved surface operations\u003c\/li\u003e\n\u003cli\u003ePressurized circular fuselage — structural reinforcement over the legacy MH.260 for continuous cruise up to 20,000 ft\u003c\/li\u003e\n\u003cli\u003eIncreased aspect ratio on Series C\/D wing extensions — maximizes lateral glide ratio and lift generation\u003c\/li\u003e\n\u003cli\u003eAerodynamic profile tailored for short-field takeoffs and high-induction regional runways\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch4\u003ePropulsion\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003eTwo \u003cstrong\u003eTurbomeca Bastan VIIC\u003c\/strong\u003e turboprop engines — 1,145 shp (843 kW) per engine at maximum continuous takeoff rating\u003c\/li\u003e\n\u003cli\u003eRatier Figeac FH.146 three-blade or upgraded four-blade variable-pitch propellers\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMohawk 298 conversion:\u003c\/strong\u003e Pratt \u0026amp; Whitney Canada PT6A-45 engines with five-blade assemblies, FAA FAR Part 298 certification\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch4\u003eHandling \u0026amp; Stability\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003eRobust vertical stabilizer providing positive yaw dampening across asymmetric power envelopes\u003c\/li\u003e\n\u003cli\u003eLongitudinal pitch control managed by CG positioning ahead of the wing aerodynamic center\u003c\/li\u003e\n\u003cli\u003eNacelle\/fuselage interference analysis — counters pitch-up tendencies at high lift coefficients\u003c\/li\u003e\n\u003cli\u003eSlight longitudinal handling variations under sudden high-power settings — documented in engineering bulletins\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch4\u003ePerformance Data\u003c\/h4\u003e\u003ctable\u003e\n\u003cthead\u003e\u003ctr\u003e\n\u003cth\u003eParameter\u003c\/th\u003e\n\u003cth\u003eValue\u003c\/th\u003e\n\u003c\/tr\u003e\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Level Speed\u003c\/td\u003e\n\u003ctd\u003e418 km\/h (225 kt) at 20,000 ft\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eEconomical Cruise Speed\u003c\/td\u003e\n\u003ctd\u003e408 km\/h (220 kt)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Range (full fuel)\u003c\/td\u003e\n\u003ctd\u003e2,400 km (1,295 NM)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003ePayload Range (26 pax)\u003c\/td\u003e\n\u003ctd\u003e1,020 km (550 NM) with reserves\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eBasic Empty Weight\u003c\/td\u003e\n\u003ctd\u003e6,200 kg (13,668 lb)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Takeoff Weight (MTOW)\u003c\/td\u003e\n\u003ctd\u003e10,800 kg (23,810 lb)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003ePassenger Capacity\u003c\/td\u003e\n\u003ctd\u003e2 crew + up to 29 passengers\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\u003chr\u003e\u003ch3\u003eEngineering Bulletin Highlights\u003c\/h3\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eStructural Fleet Monitoring:\u003c\/strong\u003e Two-tier strategy using instrumented airframes for ongoing fatigue assessment\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMohawk 298 Conversion:\u003c\/strong\u003e PT6A powerplant retrofit, modern avionics, upgraded APU — full modification instructions\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eExport Compliance:\u003c\/strong\u003e Mandatory system modifications for FAA FAR Part 298 airworthiness alignment\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003cp\u003e\u003cem\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorized distributor.\u003c\/em\u003e\u003c\/p\u003e\u003cp\u003e\u003cem\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/em\u003e\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53659313242459,"sku":null,"price":24.85,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/banner-1-landscape-hero_fbd6f52c-3e80-48b2-8943-6fbb4713734c.png?v=1785079352"},{"product_id":"nord-nc-701-martinet-sncac-aircraft-technical-descriptive-manual","title":"Nord NC-701 Martinet — S.N.C.A.C. Aircraft Technical Descriptive Manual","description":"\u003ch3\u003eNord NC-701 Martinet — S.N.C.A.C. Aircraft Technical Descriptive Manual\u003c\/h3\u003e\n\u003cp\u003eThe \u003cstrong\u003eNord NC-701 Martinet\u003c\/strong\u003e is a French post-WWII twin-engine light transport, aerial photogrammetry, and advanced trainer aircraft developed by \u003cstrong\u003eSNCAC (Société Nationale de Constructions Aéronautiques du Centre)\u003c\/strong\u003e. A direct engineering evolution of the German Siebel Si 204D, the Martinet was adopted across multiple French military and civil roles and exported to allied operators including LOT Polish Airlines and the Swedish government.\u003c\/p\u003e\n\u003cp\u003eThis archival edition reproduces the original factory documentation compiled under reference \u003cstrong\u003eS.N.C.A.C. Notice Technique No. 701.01 — Notice Descriptive\u003c\/strong\u003e, covering the Type de Base No. 701 and its operational variants (Types II through V: Marine, D.T.A., État-Major, École de Navigation, and Mission Photographique).\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003e1. Airframe \u0026amp; Aerodynamic Configuration\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eConfiguration:\u003c\/strong\u003e Low-wing cantilever monoplane — all-metal duralumin semi-monocoque fuselage\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eWing Structure:\u003c\/strong\u003e Single-spar wing with trailing-edge split (crocodile) flaps for high-drag steep approaches\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eControl Surfaces:\u003c\/strong\u003e Fabric-covered ailerons and elevators — minimised weight and flutter tendency\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNose Section:\u003c\/strong\u003e Fully glazed, unstepped ogival nose — optimised for student navigator and bomb-aimer visibility\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eEmpennage:\u003c\/strong\u003e Twin vertical stabiliser and rudder layout — positive directional control and asymmetric yaw management on single-engine operations\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eLongitudinal Trim:\u003c\/strong\u003e Adjustable horizontal stabiliser to counteract pitch moments from CG shifts and flap deployment\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003e2. Powerplant — Renault 12S-00\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eEngine Type:\u003c\/strong\u003e Twin Renault 12S-00 — air-cooled, inverted V-12 inline; French derivative of the wartime Argus As 411A1\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTakeoff Power:\u003c\/strong\u003e 580 hp (427 kW) at sea level\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eContinuous Power:\u003c\/strong\u003e 390 hp (287 kW)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSupercharger:\u003c\/strong\u003e Single-stage mechanically driven centrifugal supercharger with elastic drive coupling — rated to critical altitude of 2,400 m\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePropeller:\u003c\/strong\u003e Variable-pitch three-bladed propellers (upgrade over original German two-bladed design)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003e3. Performance Data\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eMaximum Speed:\u003c\/strong\u003e 350 km\/h (220 mph) at 3,000 m\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCruising Speed:\u003c\/strong\u003e 325 km\/h (202 mph) at 3,000 m\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eLanding \/ Stall Speed:\u003c\/strong\u003e 115 km\/h (71 mph) — flaps fully extended\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eRate of Climb:\u003c\/strong\u003e 5.3 m\/s (1,043 ft\/min) at maximum continuous power\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eService Ceiling:\u003c\/strong\u003e 6,400 m (21,000 ft)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eOperational Range:\u003c\/strong\u003e 810 km (500 mi) standard; up to 1,400 km with auxiliary ferry tanks\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eEmpty Weight:\u003c\/strong\u003e 3,860 kg (passenger layout) \/ 3,920 kg (aerial photography configuration)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMTOW:\u003c\/strong\u003e 5,600 kg\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003e4. Handling, Stability \u0026amp; Systems\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eIce Mitigation:\u003c\/strong\u003e Hot-air de-icing ducts integrated into windscreen and flight deck viewing panels\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFlight Controls:\u003c\/strong\u003e Dual control posts with disconnect capability; electro-hydraulic flap command system\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eUndercarriage:\u003c\/strong\u003e Retractable tricycle gear — mechanical, hydraulic, and electrical actuation with manual emergency backup and braking\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003e5. Operational Variants \u0026amp; Engineering Bulletins\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eAérophotogrammétrie Conversion:\u003c\/strong\u003e Heavy KF radio station, dual automated floor cameras, rear darkroom compartment — operated by LOT Polish Airlines and the Swedish government for mapping missions\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSanitary Evacuation Variant:\u003c\/strong\u003e Cabin conversion for medical evacuation litters — seat removal procedure documented in technical bulletins\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMagnetic Mine Sweeping (NC-701 No. 8):\u003c\/strong\u003e Structural retrofit of Airframe No. 8 for French Navy magnetic mine detonation trigger array testing — unique engineering bulletin\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eDocument Manifest — Notice Technique No. 701.01\u003c\/h3\u003e\n\u003cp\u003e\u003cem\u003eNotice Descriptive — S.N.C.A.C., Numéro 701.01\u003c\/em\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003ePlaneur — Voilure (Wing Assembly): Caissons AV\/AR internes et externes, longeron principal, extrémités d'aile, raccord voilure-fuselage\u003c\/li\u003e\n\u003cli\u003eAileron, Volets d'Intrados, Bâti Moteur Intermédiaire et Capotage\u003c\/li\u003e\n\u003cli\u003eFuselage — Partie AV (Cabine Pilote), Partie Médiane, Partie AR, Pointe AR\u003c\/li\u003e\n\u003cli\u003eCommandes de Vol — Gauchissement, Profondeur, Direction, Flettners, Volets d'Intrados\u003c\/li\u003e\n\u003cli\u003eEmpennages Horizontaux et Verticaux (Dérives, Gouvernails)\u003c\/li\u003e\n\u003cli\u003eAtterrisseurs AV et AR — Commande de Train Rentrant (mécanique, hydraulique, électrique), Freinage, Carénage\u003c\/li\u003e\n\u003cli\u003eAccessibilité et Démontabilité\u003c\/li\u003e\n\u003cli\u003eGroupe Moto-Propulseur — Moteurs, Commandes Moteurs, Démarrage, Alimentation (Essence, Amorçage, Transvasement), Graissage, Refroidissement, Hélices\u003c\/li\u003e\n\u003cli\u003eMatériel d'Équipement — Instruments de Pilotage et Navigation, Contrôle Moteurs, Changement de Pas d'Hélice, Escamotage de Train, Volets d'Intrados, Flettners\u003c\/li\u003e\n\u003cli\u003eMatériel Électrique, Radio Électrique, Radio Goniométrie, Photographique, Téléphonique\u003c\/li\u003e\n\u003cli\u003eInstallation d'Oxygène, Matériels Divers\u003c\/li\u003e\n\u003cli\u003eInstallation de l'Équipage et des Passagers\u003c\/li\u003e\n\u003cli\u003eTable des Figures — 23 numbered figures (pp. 14–45) covering wing, fuselage, flight controls, and electro-hydraulic schematics\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003cp\u003e\u003cem\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorised distributor.\u003c\/em\u003e\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/strong\u003e\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53659345453403,"sku":null,"price":20.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/nc-701-martinet-wide-hero-banner.png?v=1785080450"},{"product_id":"sncaso-so30-bretagne-twin-engine-transport-aircraft-documentation-collection","title":"SNCASO SO.30 Bretagne — Twin-Engine Transport Aircraft Documentation Collection","description":"\u003ch3\u003eSNCASO SO.30 Bretagne — Twin-Engine Transport Aircraft Documentation Collection\u003c\/h3\u003e\n\u003cp\u003eThe \u003cstrong\u003eSNCASO SO.30 Bretagne\u003c\/strong\u003e was a French twin-engine passenger and military transport aircraft developed during World War II and refined through the postwar reconstruction era. Produced by \u003cstrong\u003eSociété Nationale de Constructions Aéronautiques du Sud-Ouest (SNCASO)\u003c\/strong\u003e, the Bretagne served as a critical stepping stone for rebuilding the French aerospace industry — bridging wartime engineering with the jet age through a series of ambitious powerplant and structural experiments.\u003c\/p\u003e\n\u003cp\u003eThis archival collection reproduces original factory documentation across the SO.30 family, including the \u003cstrong\u003eManuel d'Utilisation SO.30 P · B 43 (Bretagne No. 12, 1950)\u003c\/strong\u003e, the original SNCASO commercial brochure for the SO.30 Bretagne, the SO.30P pressurised cabin variant brochure, and the SO.30R Bellatrix development brochure.\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003e1. Airframe \u0026amp; Aerodynamic Configuration\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eLayout:\u003c\/strong\u003e Mid-wing cantilever monoplane — all-metal construction throughout\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTail Assembly:\u003c\/strong\u003e Dual vertical fins and rudders for enhanced directional stability\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eLanding Gear:\u003c\/strong\u003e Early prototypes: tailwheel configuration; production variants: tricycle undercarriage\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAuxiliary Thrust:\u003c\/strong\u003e Select airframes fitted with underwing Turbomeca Palas turbojets to augment takeoff lift profiles\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003e2. Powerplant Variants\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eSO.30P-1:\u003c\/strong\u003e Twin Pratt \u0026amp; Whitney R-2800-B43 radial piston engines — 1,800 hp each\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSO.30P-2:\u003c\/strong\u003e Twin Pratt \u0026amp; Whitney R-2800-CA18 — upgraded to 2,400 hp each\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePropeller Assemblies:\u003c\/strong\u003e 4-bladed Curtiss Electric or 3-bladed Hamilton Standard square-tipped paddle blades\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eJet Testbeds:\u003c\/strong\u003e Airframes modified to test early Rolls-Royce Nene and SNECMA Atar 101 turbojets — significant engineering milestone in French jet development\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003e3. Performance Data\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eMaximum Speed:\u003c\/strong\u003e 575 km\/h (310 kt) at optimal altitude\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCruising Speed:\u003c\/strong\u003e 438 km\/h (237 kt) economical cruise\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eService Ceiling:\u003c\/strong\u003e 8,000 m (26,000 ft)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFerry Range:\u003c\/strong\u003e 2,175 km (1,174 nm)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003e4. Handling \u0026amp; Engineering Notes\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eDead-Engine Trim:\u003c\/strong\u003e Control surfaces designed to maintain safe margins during single-engine operations\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eWeight Profile:\u003c\/strong\u003e High empty structural weight noted in engineering assessments relative to American contemporaries (Douglas DC-3 class)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCargo Variant (SO.30C):\u003c\/strong\u003e Narrow rear loading ramp limited vehicle insertion capability — documented in military logistics bulletins\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eDocument Manifest\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eManuel d’Utilisation SO.30 P · B 43\u003c\/strong\u003e — Bretagne No. 12, 1950 · SNCASO · French language · Operator’s flight manual for the pressurised B 43 variant, Airframe No. 12\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSO.30 Bretagne Commercial Brochure\u003c\/strong\u003e — SNCASO original sales brochure · Illustrated profile artwork · Société Nationale de Constructions Aéronautiques du Sud-Ouest, Paris XVIᵉ\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSO.30P “Bretagne” Pressurised Cabin Brochure\u003c\/strong\u003e — English-language SNCASO brochure · Twin-engined commercial aircraft with pressurised cabin · Includes in-flight photograph of F-BAYK\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSO.30R Bellatrix Development Brochure\u003c\/strong\u003e — SNCASO · French language · Covers the SO.30R long-range development variant with revised powerplant and extended fuselage studies\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003cp\u003e\u003cem\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorised distributor.\u003c\/em\u003e\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/strong\u003e\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53659454603611,"sku":null,"price":20.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/so-30-bretagne-wide-hero-banner.png?v=1785082037"},{"product_id":"potez-25-manual-collection","title":"Potez 25 — Manual Collection","description":"\u003ch2\u003ePotez 25 — Archival Manual Collection\u003c\/h2\u003e\u003cp\u003eThe \u003cstrong\u003ePotez 25\u003c\/strong\u003e (Potez XXV) was one of the most successful military aircraft of the interwar era — a highly versatile French sesquiplane designed by Louis Coroller for \u003cem\u003eSociété des Aéroplanes Henry Potez\u003c\/em\u003e, first flown in 1924 and produced in approximately 4,000 units for over 20 nations. Its defining engineering achievement was a \u003cstrong\u003emodular engine bay\u003c\/strong\u003e capable of accepting any powerplant rated between 370 and 600 hp without structural modification, making it the universal platform of its generation.\u003c\/p\u003e\u003cp\u003eThis Living Collection brings together \u003cstrong\u003e3 primary-source French-language documents\u003c\/strong\u003e issued by the Société des Aéroplanes Henry Potez and the Ministère de la Guerre — all fixed at their original publication dates and presented in archival facsimile.\u003c\/p\u003e\u003chr\u003e\u003ch3\u003eCollection Manifest\u003c\/h3\u003e\u003ch4\u003eT.O.E. Variant — 1 Document\u003c\/h4\u003e\u003cul\u003e\u003cli\u003e\n\u003cstrong\u003eHenry Potez 25 Type T.O.E. — Technical Notice\u003c\/strong\u003e\u003cbr\u003e\u003cem\u003eNotice Technique de l'Avion Henry Potez 25 — Type T.O.E.\u003c\/em\u003e\u003cbr\u003eMoteur Lorraine 450 cv — Type 12 EB\u003cbr\u003eSociété des Aéroplanes Henry Potez — 75, Avenue des Champs-Élysées, Paris\u003cbr\u003eUsine \u0026amp; Aérodrome: Méaulte (Somme)\u003cbr\u003eLanguage: French\u003c\/li\u003e\u003c\/ul\u003e\u003ch4\u003eMilitary A2 Variant — 1 Document\u003c\/h4\u003e\u003cul\u003e\u003cli\u003e\n\u003cstrong\u003ePotez 25 A2 — Technical Notice\u003c\/strong\u003e\u003cbr\u003e\u003cem\u003eNotice Technique de l'Avion Potez Type 25 A2\u003c\/em\u003e\u003cbr\u003eMinistère de la Guerre — Aéronautique Militaire\u003cbr\u003eMoteurs: Lorraine 450 CV 12 E b · Salmson 520 CV 18 C M b\u003cbr\u003eLanguage: French\u003c\/li\u003e\u003c\/ul\u003e\u003ch4\u003eCommercial Brochure — 1 Document\u003c\/h4\u003e\u003cul\u003e\u003cli\u003e\n\u003cstrong\u003eLe Potez 25 A.2 — Reconnaissance and Bombing Aircraft\u003c\/strong\u003e\u003cbr\u003e\u003cem\u003eLe Potez 25 A.2 — Avion de Reconnaissance et de Bombardement\u003c\/em\u003e\u003cbr\u003eAlbum Général — Feuillet No. 25-1 — Avril 1929\u003cbr\u003eSociété des Aéroplanes Henry Potez — Méaulte (Somme)\u003cbr\u003eLanguage: French\u003c\/li\u003e\u003c\/ul\u003e\u003chr\u003e\u003ch3\u003eAircraft Technical Profile\u003c\/h3\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eConfiguration:\u003c\/strong\u003e Sesquiplane (lower wing ~1.5× smaller than upper wing)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePrimary Engine:\u003c\/strong\u003e Lorraine-Dietrich 12Eb — 12-cylinder W inline, water-cooled, 450 ch\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAlternative Engines:\u003c\/strong\u003e Salmson 18 CMb (520 ch) · Gnome-Rhône Jupiter 9Ac (420 ch) · Hispano-Suiza 12Gb\/12Lb (500–600 ch) · Renault 12Kg (550 ch)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eEmpty Weight:\u003c\/strong\u003e 1,510 kg · \u003cstrong\u003eMax Take-off Weight:\u003c\/strong\u003e 2,500 kg\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMax Speed:\u003c\/strong\u003e 208 km\/h (Lorraine) \/ 230 km\/h (Hispano-Suiza)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eService Ceiling:\u003c\/strong\u003e 5,800 m (Lorraine) \/ 7,300 m (Hispano-Suiza)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eRange:\u003c\/strong\u003e 1,260 km (extendable with auxiliary tanks)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eArmament:\u003c\/strong\u003e 1 × fixed forward Vickers · 2 × flexible Lewis on TO7 ring mount · 1 × ventral Lewis\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eT.O.E. Tropicalization:\u003c\/strong\u003e Heavy-duty belly radiators, onboard water storage, auxiliary fuel cells for desert operations\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003cp\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorized distributor.\u003c\/p\u003e\u003cp\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53694850433371,"sku":null,"price":20.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/potez-25-square-side-profile-banner.png?v=1785481151"},{"product_id":"potez-43-touring-monoplane-manual-collection","title":"Potez 43 Touring Monoplane — Manual Collection","description":"\u003ch2\u003ePotez 43 Touring Monoplane — Archival Manual Collection\u003c\/h2\u003e\u003cp\u003eThe \u003cstrong\u003ePotez 43\u003c\/strong\u003e was one of the most successful French light touring monoplanes of the 1930s — a refined, 3-seat derivative of the popular Potez 36, developed by \u003cem\u003eSociété des Aéroplanes Henry Potez\u003c\/em\u003e and produced in 161 units. Its high-wing, strut-braced parasol configuration with fixed leading-edge slats delivered exceptional low-speed safety and benign stall characteristics, making it a favourite of French civil flying clubs and military liaison units alike. The modular engine bay accepted four different powerplants — from the original Potez 6 AC (100 cv) to the de Havilland Gipsy Major (120 cv) — without structural modification.\u003c\/p\u003e\u003cp\u003eThis Living Collection brings together \u003cstrong\u003e2 primary-source French-language documents\u003c\/strong\u003e issued by the Société des Aéroplanes Henry Potez — fixed at their original publication dates and presented in archival facsimile.\u003c\/p\u003e\u003chr\u003e\u003ch3\u003eCollection Manifest\u003c\/h3\u003e\u003ch4\u003eOperating \u0026amp; Maintenance Manual — 1 Document\u003c\/h4\u003e\u003cul\u003e\u003cli\u003e\n\u003cstrong\u003ePotez 43 — Notice d'Utilisation et d'Entretien\u003c\/strong\u003e\u003cbr\u003e\u003cem\u003eNotice d'Utilisation et d'Entretien de l'Avion H. Potez de Tourisme — Type 43\u003c\/em\u003e\u003cbr\u003eMoteurs couverts: Potez 6 AC 100 cv · Potez 6 B 120 cv · Renault “Bengali” 120 cv · Gipsy Major 120 cv\u003cbr\u003e26 pages · 23 technical illustrations\u003cbr\u003eSociété des Aéroplanes Henry Potez\u003cbr\u003eLanguage: French\u003c\/li\u003e\u003c\/ul\u003e\u003ch4\u003eManufacturer Brochure — 1 Document\u003c\/h4\u003e\u003cul\u003e\u003cli\u003e\n\u003cstrong\u003eAvions H. Potez — Potez 43 Triplace Touring Aircraft\u003c\/strong\u003e\u003cbr\u003e\u003cem\u003eAvion de Tourisme Triplace — Potez 43\u003c\/em\u003e\u003cbr\u003eCollection des Bulletins Techniques de la Société des Aéroplanes Henry Potez\u003cbr\u003eNo. 15 Bis — Septembre 1932\u003cbr\u003eLanguage: French\u003c\/li\u003e\u003c\/ul\u003e\u003chr\u003e\u003ch3\u003eAircraft Technical Profile\u003c\/h3\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eConfiguration:\u003c\/strong\u003e High-wing strut-braced parasol monoplane, 3-seat cabin\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eLeading-Edge Slats:\u003c\/strong\u003e Fixed, aileron-span slats for stall delay and low-speed safety\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePrimary Engine:\u003c\/strong\u003e Potez 6 AC — 6-cylinder air-cooled radial, 78 kW (105 hp)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAlternative Engines:\u003c\/strong\u003e Potez 6 B (120 cv) · Renault “Bengali” 4Pei (100–120 cv) · de Havilland Gipsy Major I (120 cv)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMax Speed:\u003c\/strong\u003e 160 km\/h (99 mph) · \u003cstrong\u003eCruise:\u003c\/strong\u003e 140 km\/h (87 mph) · \u003cstrong\u003eStall:\u003c\/strong\u003e 60 km\/h (37 mph)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eService Ceiling:\u003c\/strong\u003e 5,000 m (16,400 ft) · \u003cstrong\u003eRange:\u003c\/strong\u003e 800 km (500 mi)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eGross Weight:\u003c\/strong\u003e 800 kg · \u003cstrong\u003ePayload:\u003c\/strong\u003e 330 kg\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTotal Production:\u003c\/strong\u003e 161 aircraft (variants: Potez 430, 436, 437, 438)\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003cp\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorized distributor.\u003c\/p\u003e\u003cp\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53694911316315,"sku":null,"price":20.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/potez-43-square-f-ambm-overhead-banner.png?v=1785482029"},{"product_id":"potez-630-631-63-11-manual-collection","title":"Potez 630 · 631 · 63-11 — Manual Collection","description":"\u003ch2\u003ePotez 630 · 631 · 63-11 — Archival Manual Collection\u003c\/h2\u003e\u003cp\u003eThe \u003cstrong\u003ePotez 630, 631, and 63-11\u003c\/strong\u003e series formed France’s primary twin-engine multirole aircraft family at the outbreak of World War II — an all-metal, stressed-skin cantilever monoplane with a distinctive twin-fin tail, designed by Avions Henry Potez and produced by SNCAN. The series split into two powerplant families: the \u003cstrong\u003ePotez 630\u003c\/strong\u003e with Hispano-Suiza 14 AB radials, and the \u003cstrong\u003ePotez 631 and 63-11\u003c\/strong\u003e with the more reliable Gnome-Rhône 14 M ultra-compact radials. The 63-11 A3 reconnaissance variant added a heavily glazed stepped nose and carried up to 12 × 7.5 mm MAC 1934 machine guns. Praised by test pilots for docile, predictable handling, the series served as heavy fighter, night fighter, and tactical reconnaissance platform throughout the 1939–1940 campaign.\u003c\/p\u003e\u003cp\u003eThis Living Collection brings together \u003cstrong\u003e5 primary-source French-language documents\u003c\/strong\u003e issued by the Ministère de l’Air — Armée de l’Air, all fixed at their original publication dates and presented in archival facsimile.\u003c\/p\u003e\u003chr\u003e\u003ch3\u003eCollection Manifest\u003c\/h3\u003e\u003ch4\u003ePotez 63-11 A3 — 3 Documents\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eNotice Descriptive et d’Utilisation — Potez 63-11 A3\u003c\/strong\u003e\u003cbr\u003e\u003cem\u003eNotice Descriptive et d’Utilisation de l’Avion Potez 63-11 A 3\u003c\/em\u003e\u003cbr\u003eMoteurs Gnome et Rhône 570 CV — Types 14 M7 – 14 M6\u003cbr\u003eN.C.C. 22 · Catégorie AV · Décembre 1939 · 1,200 exemplaires\u003cbr\u003eApprouvée par Décision Ministérielle n° 7103 2\/MAM 8 du 18 décembre 1939\u003cbr\u003eLanguage: French\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNotice de Caractéristiques et de Performances — Potez 63-11\u003c\/strong\u003e\u003cbr\u003e\u003cem\u003eNotice de Caractéristiques et de Performances de l’Avion Potez 63-11\u003c\/em\u003e\u003cbr\u003eMoteurs Gnôme et Rhône 14 M 04 et 14 M 05\u003cbr\u003eN.C.C. 22 U · Catégorie AV · 1940 — \u003cstrong\u003eOriginal SECRET classification stamp\u003c\/strong\u003e\u003cbr\u003eApprouvée par D.M. n° 111 RS 2\/MAM 8, du 24 février 1940\u003cbr\u003eLanguage: French\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNotice d’Entretien et de Réparation — Potez 63-11 A3\u003c\/strong\u003e\u003cbr\u003e\u003cem\u003eNotice d’Entretien et de Réparation de l’Avion Potez 63-11 A 3\u003c\/em\u003e\u003cbr\u003eMoteurs Gnome et Rhone Type 14 M\u003cbr\u003eN.C.C. 22 R · Catégorie AV · Avril 1940 · 1,200 exemplaires\u003cbr\u003eApprouvée par D.M. n° 1263 2\/M.A.M. 8 du 29 février 1940\u003cbr\u003eLanguage: French\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch4\u003ePotez 630-C3 — 1 Document\u003c\/h4\u003e\u003cul\u003e\u003cli\u003e\n\u003cstrong\u003eNotice Descriptive et d’Utilisation — Potez 630-C3\u003c\/strong\u003e\u003cbr\u003e\u003cem\u003eNotice Descriptive et d’Utilisation de l’Avion Potez 630-C3\u003c\/em\u003e\u003cbr\u003eMoteurs Hispano-Suiza 14 AB (1) — 14 AB-02 et 03 ou 14 AB-10 et 11\u003cbr\u003eN.C.B. 23 · Catégorie AV · Mai 1939 · 1,200 exemplaires\u003cbr\u003eApprouvée par Décision Ministérielle n° 2551 2\/MAM. 8 du 6 mai 1939\u003cbr\u003eLanguage: French\u003c\/li\u003e\u003c\/ul\u003e\u003ch4\u003ePotez 631-C³ — 1 Document\u003c\/h4\u003e\u003cul\u003e\u003cli\u003e\n\u003cstrong\u003eNotice Descriptive, d’Utilisation, d’Entretien et de Réparation — Potez 631-C³\u003c\/strong\u003e\u003cbr\u003e\u003cem\u003eNotice Descriptive d’Utilisation, d’Entretien et de Réparation de l’Avion Potez 631-C³\u003c\/em\u003e\u003cbr\u003eMoteurs Gnome-Rhône 14 M6 et 14 M7\u003cbr\u003eN.C.B. 24 · Catégorie AV · Juin 1939 · 1,200 exemplaires\u003cbr\u003eApprouvée par Dépêche Ministérielle n° 3349 2\/MAM. 8 du 14 juin 1939\u003cbr\u003eLanguage: French\u003c\/li\u003e\u003c\/ul\u003e\u003chr\u003e\u003ch3\u003eAircraft Technical Profile\u003c\/h3\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eConfiguration:\u003c\/strong\u003e All-metal stressed-skin cantilever monoplane, twin-fin twin-rudder tail\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePotez 630 Engine:\u003c\/strong\u003e Hispano-Suiza 14 AB — 14-cylinder air-cooled radial, ~640–725 hp\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePotez 631 \/ 63-11 Engine:\u003c\/strong\u003e Gnome-Rhône 14 M — 14-cylinder ultra-compact radial, ~660–700 hp\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePotez 631 C3 Max Speed:\u003c\/strong\u003e 450 km\/h at 4,000 m · \u003cstrong\u003eRange:\u003c\/strong\u003e 1,200 km\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePotez 63-11 A3 Max Speed:\u003c\/strong\u003e 425 km\/h at 5,500 m · \u003cstrong\u003eCeiling:\u003c\/strong\u003e 8,500 m · \u003cstrong\u003eRange:\u003c\/strong\u003e 1,500 km\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePotez 631 Armament:\u003c\/strong\u003e 2 × 20 mm Hispano-Suiza HS.404 · 6 × 7.5 mm MAC 1934 · 1 × flexible rear gun\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePotez 63-11 Armament:\u003c\/strong\u003e Up to 12 × 7.5 mm MAC 1934 in underwing gondolas and ventral mounts\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eProduction:\u003c\/strong\u003e ~7,500 man-hours per airframe · Served as heavy fighter, night fighter, and tactical reconnaissance platform\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003cp\u003e⚠️ \u003cstrong\u003eRegulatory Notice:\u003c\/strong\u003e Under FAA 14 CFR § 43.13 and EASA Part-M, any mechanic performing maintenance on an active aircraft must use current, manufacturer-approved revision-controlled data. This archival document does not satisfy that requirement.\u003c\/p\u003e\u003cp\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorized distributor.\u003c\/p\u003e\u003cp\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53694924783963,"sku":null,"price":28.85,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/potez-63-series-landscape-overhead-banner.png?v=1785483047"},{"product_id":"potez-heinkel-cm191-twin-jet-executive-aircraft-documentation","title":"Potez-Heinkel CM.191 — Twin-Jet Executive Aircraft | Original Factory Documentation Archive","description":"\u003ch3\u003ePotez-Heinkel CM.191 — Twin-Jet Executive \u0026amp; Liaison Aircraft\u003c\/h3\u003e\n\u003ch3\u003eFranco-German Experimental Programme · 1961–1963\u003c\/h3\u003e\n\u003cp\u003eThe \u003cstrong\u003ePotez-Heinkel CM.191\u003c\/strong\u003e was a four-seat, twin-turbojet executive and liaison aircraft jointly developed in 1961 by \u003cstrong\u003eÉtablissements Henry Potez\u003c\/strong\u003e (Paris, France) and \u003cstrong\u003eErnst Heinkel Flugzeugbau GmbH\u003c\/strong\u003e (Speyer, West Germany). Derived directly from the celebrated \u003cstrong\u003eFouga CM.170 Magister\u003c\/strong\u003e military jet trainer, the CM.191 represented an ambitious attempt to translate the Magister's proven aerodynamic pedigree into a high-performance civil and military liaison platform. Only two prototypes were constructed before the programme was closed.\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eDocument Archive — Manifest\u003c\/h3\u003e\n\u003cp\u003eThis archival edition brings together the surviving primary-source factory documentation for the CM.191 programme:\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eVerkaufsbroschüre (Sales Brochure)\u003c\/strong\u003e — 6 pages · German language · Ernst Heinkel Flugzeugbau GmbH, Speyer · Covers general description, airframe, equipment, avionics, powerplant, and performance data\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFlughandbuch (Flight Manual) — Illustrations Volume\u003c\/strong\u003e · Airframe diagrams and system schematics\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFlughandbuch (Flight Manual) — Text Volume\u003c\/strong\u003e · Operational procedures and systems description\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTechnische Daten \/ Specifications Sheets\u003c\/strong\u003e — 7 pages · Detailed dimensional, structural, aerodynamic, and performance data tables\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAnlage 1 — UHF-Anlage Type AN\/ARC-34\u003c\/strong\u003e · Sender-Empfänger RT-263\/ARC-34 · 225.0–399.9 MHz · 1,750 channels · 10 W output\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAnlage 2 — Funkkompaß-Anlage Type ADF-102\u003c\/strong\u003e · Lear ADF-102 radio compass · Fully transistorised · 5 pre-selectable frequencies · 535–1600 kHz\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAnlage 3 — Bord-Eigenverständigungs-Anlage IV T 3 Serie 01\u003c\/strong\u003e · Intercom system by TEAM, Paris · Licensed manufacture by Bauknecht-GEA, Fellbach · 4.63 kg\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eTotal documents in this archive: 15 unique primary-source pages and plates.\u003c\/strong\u003e\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eAirframe \u0026amp; Design\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eConfiguration:\u003c\/strong\u003e All-metal mid-wing monoplane with twin turbojets mounted aft of the wing roots, side-by-side four-seat cabin\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFuselage:\u003c\/strong\u003e Conventional semi-monocoque shell construction using oval frames and four longerons; pressurised and climate-controlled cabin with full-vision Plexiglas canopy\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eWing:\u003c\/strong\u003e Trapezoidal single-spar structure, aspect ratio 7.67, slight leading-edge sweep (15°), NACA Series 64 profile — 19% thickness at root, 12% at tip; hydraulically actuated Fowler-type flaps, Frise ailerons, retractable spoilers\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eEmpennage:\u003c\/strong\u003e Iconic V-tail (butterfly tail) inherited from the Fouga Magister — combined pitch\/yaw control via differential rudder deflection and servo trim tabs\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eUndercarriage:\u003c\/strong\u003e Tricycle, wide-track main gear (4.41 m), hydraulic retraction — nose gear retracts forward to the nose, main gear folds into the wing roots\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003ePowerplant — Turbomeca Marboré VI\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eType:\u003c\/strong\u003e Single-stage centrifugal compressor \/ single-stage axial turbine \/ annular combustion chamber with centrifugal fuel injection\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eExhaust:\u003c\/strong\u003e Constant-area nozzle\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMax diameter:\u003c\/strong\u003e 0.567 m · \u003cstrong\u003eLength:\u003c\/strong\u003e 1.416 m · \u003cstrong\u003eWeight:\u003c\/strong\u003e 146 kg\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eQuantity:\u003c\/strong\u003e 2 × Marboré VI, mounted on either side of the rear fuselage beneath removable fairings\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eAvionics Suite\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eUHF Transceiver:\u003c\/strong\u003e AN\/ARC-34 (RT-263\/ARC-34) — 225.0–399.9 MHz, 1,750 channels at 1\/10 MHz steps, 20 pre-selectable channels, 10 W output, 27 kg total installation\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eRadio Compass:\u003c\/strong\u003e Lear ADF-102 — fully transistorised, 5 pre-selectable frequencies, 535–1,600 kHz, Gonio antenna and Gonio coupler, indicator ID 91\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eIntercom:\u003c\/strong\u003e Bauknecht-GEA IV T 3 Serie 01 — normal and emergency modes, UHF monitoring capability, pilot priority on transmit\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eKey Performance Data (Factory Specification)\u003c\/h3\u003e\n\u003ctable\u003e\n\u003cthead\u003e\n\u003ctr\u003e\n\u003cth\u003eParameter\u003c\/th\u003e\n\u003cth\u003eValue\u003c\/th\u003e\n\u003c\/tr\u003e\n\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eWingspan\u003c\/td\u003e\n\u003ctd\u003e12.02 m\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eLength\u003c\/td\u003e\n\u003ctd\u003e9.93 m\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eHeight\u003c\/td\u003e\n\u003ctd\u003e3.20 m\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eWing area\u003c\/td\u003e\n\u003ctd\u003e18.83 m²\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eAspect ratio\u003c\/td\u003e\n\u003ctd\u003e7.67\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax take-off weight\u003c\/td\u003e\n\u003ctd\u003e4,437 kg\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax speed (Gm, no tip tanks)\u003c\/td\u003e\n\u003ctd\u003e710 km\/h at 21,500 rpm\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eCruise ceiling (Gm)\u003c\/td\u003e\n\u003ctd\u003e12.1 km\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eClimb rate at sea level (GA, 1 engine)\u003c\/td\u003e\n\u003ctd\u003e3.83 m\/s\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eRange at 9,000 m (no climb\/descent)\u003c\/td\u003e\n\u003ctd\u003e1,270 km\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eRange at 9,000 m (with climb\/descent)\u003c\/td\u003e\n\u003ctd\u003e1,570 km\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eEndurance at 9,000 m\u003c\/td\u003e\n\u003ctd\u003e3.2 h\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax speed (with large tip tanks)\u003c\/td\u003e\n\u003ctd\u003e660 km\/h\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eRange (large tip tanks, no climb\/descent)\u003c\/td\u003e\n\u003ctd\u003e1,800 km\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax endurance (large tip tanks)\u003c\/td\u003e\n\u003ctd\u003e4.42 h\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003e2-seat ferry range (additional tank)\u003c\/td\u003e\n\u003ctd\u003eup to 2,630 km \/ ~5 h\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\n\u003chr\u003e\n\u003ch3\u003eProgramme History\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eOrigin:\u003c\/strong\u003e Developed jointly by Potez-Air Fouga (Paris), Ernst Heinkel Flugzeugbau GmbH (Speyer), and Fouga — derived from the Fouga CM.170 Magister\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFirst flight:\u003c\/strong\u003e 19 March 1962, Toulouse — test pilots Jacques Grangette and Pierre Caneille\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eIntended roles:\u003c\/strong\u003e Civil — business transport, fast feeder, sport aircraft; Military — jet conversion trainer, instrument\/night flying, liaison and courier, reconnaissance\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eProgramme closure:\u003c\/strong\u003e Competition from the Morane-Saulnier MS.760 Paris prevented serial production\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePrototype 1 (N8015Q):\u003c\/strong\u003e Exported to the United States\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePrototype 2:\u003c\/strong\u003e Preserved at Technik Museum Speyer, Germany\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003cp\u003e\u003cem\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorized distributor.\u003c\/em\u003e\u003c\/p\u003e\n\u003cp\u003e\u003cem\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/em\u003e\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53695075516763,"sku":null,"price":20.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/potez-heinkel-cm-191-banner-3.png?v=1785486181"},{"product_id":"potez-840-841-842-turboprop-transport-documentation-archive","title":"Potez 840 \/ 841 \/ 842 — Four-Engine Turboprop Executive \u0026 Regional Transport | Original Factory Documentation Archive","description":"\u003ch3\u003ePotez 840 \/ 841 \/ 842 — Four-Engine Turboprop Executive \u0026amp; Regional Transport\u003c\/h3\u003e\n\u003ch3\u003eSociété des Avions et Moteurs Henry Potez · France · 1962–1967\u003c\/h3\u003e\n\u003cp\u003eThe \u003cstrong\u003ePotez 840, 841, and 842\u003c\/strong\u003e series represents one of the most ambitious and technically distinctive French transport aircraft programmes of the 1960s. Developed by \u003cstrong\u003eSociété des Avions et Moteurs Henry Potez\u003c\/strong\u003e, the series was conceived as a pressurised, four-engine turboprop regional and executive transport capable of challenging the Douglas DC-3 replacement market on short-to-medium-range routes. Fewer than ten total airframes were completed before the company was absorbed into \u003cstrong\u003eSud Aviation\u003c\/strong\u003e in 1967, making surviving primary-source documentation exceptionally rare.\u003c\/p\u003e\n\u003cp\u003eThis archival edition consolidates the known surviving factory documentation across all three variants into a single research collection.\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eDocument Archive — Manifest\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003ePotez 840 — Turbo-Flight Brochure (US English)\u003c\/strong\u003e · 51 pages · General description, airframe overview, powerplant, systems, equipment, and performance data · Ref. A.R.E. 840-1001\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePotez 840 — Luxury Brochure (French)\u003c\/strong\u003e · 34 pages · Executive cabin configuration, interior fittings, and passenger comfort data\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePotez 840 — Preliminary Brochure (1962, English)\u003c\/strong\u003e · 19 pages · Foreword, programme introduction, general aspect, airframe description, and overall dimensions · Ref. A.R.E. 840-1003\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePotez 840 — Specification Sheet (1963)\u003c\/strong\u003e · 17 pages · Dimensional, structural, and performance data tables\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePotez 841 \/ 842 — Sales Brochure\u003c\/strong\u003e · 28 pages · Variant descriptions, engine options, configuration data, and performance comparison\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eTotal documents in this archive: 149 pages across 5 primary-source factory publications.\u003c\/strong\u003e\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eVariant Overview\u003c\/h3\u003e\n\u003ctable\u003e\n\u003cthead\u003e\n\u003ctr\u003e\n\u003cth\u003eVariant\u003c\/th\u003e\n\u003cth\u003eEngine\u003c\/th\u003e\n\u003cth\u003ePower (per engine)\u003c\/th\u003e\n\u003cth\u003ePropeller\u003c\/th\u003e\n\u003cth\u003eTarget Market\u003c\/th\u003e\n\u003c\/tr\u003e\n\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003ePotez 840\u003c\/td\u003e\n\u003ctd\u003eTurbomeca Astazou II\u003c\/td\u003e\n\u003ctd\u003e440 shp (328 kW)\u003c\/td\u003e\n\u003ctd\u003e3-bladed Ratier-Figeac\u003c\/td\u003e\n\u003ctd\u003eInitial production · European market\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003ePotez 841\u003c\/td\u003e\n\u003ctd\u003ePratt \u0026amp; Whitney PT6A-6\u003c\/td\u003e\n\u003ctd\u003e550 shp (417 kW)\u003c\/td\u003e\n\u003ctd\u003e3-bladed, fully feathering\u003c\/td\u003e\n\u003ctd\u003eNorth American corporate sales\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003ePotez 842\u003c\/td\u003e\n\u003ctd\u003eTurbomeca Astazou X \/ XII\u003c\/td\u003e\n\u003ctd\u003e600–640 shp (447–480 kW)\u003c\/td\u003e\n\u003ctd\u003e3-bladed Ratier-Figeac (2.07 m)\u003c\/td\u003e\n\u003ctd\u003eUpgraded payload · hot-and-high operations\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\n\u003chr\u003e\n\u003ch3\u003eAirframe \u0026amp; Design\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eConfiguration:\u003c\/strong\u003e Cantilever low-wing monoplane · four turboprop engines · circular-section pressurised fuselage · single fin and rudder · adjustable stabiliser · retractable tricycle undercarriage\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eWing:\u003c\/strong\u003e Modified NACA 63-series profile · aspect ratio 10.75:1 · wingspan 19.60 m · wing area 35.0 m² (377 sq ft) · optimised for low profile drag at high-speed cruise\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFuselage:\u003c\/strong\u003e Circular cross-section semi-monocoque structure · distinctive triangular cabin windows · pressurised and air-conditioned cabin\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eUndercarriage:\u003c\/strong\u003e Retractable triangular tricycle arrangement · hydraulic actuation\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFlight Controls:\u003c\/strong\u003e Fully mechanical push-pull rod-actuated surfaces · direct feedback · no hydraulic boost\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eCabin Configurations (Potez 840 Standard)\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003e24-seat high-density:\u003c\/strong\u003e For distances up to 600 miles at 310 mph with reserves\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003e16-seat regional:\u003c\/strong\u003e For distances up to 1,200 miles at 310 mph with reserves\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eExecutive layout:\u003c\/strong\u003e For distances up to 2,000 miles at 310 mph with reserves\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003ePerformance Data (Potez 842 — Type Certification Profile)\u003c\/h3\u003e\n\u003ctable\u003e\n\u003cthead\u003e\n\u003ctr\u003e\n\u003cth\u003eParameter\u003c\/th\u003e\n\u003cth\u003eValue\u003c\/th\u003e\n\u003c\/tr\u003e\n\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eSpan\u003c\/td\u003e\n\u003ctd\u003e19.60 m (65 ft 7 in)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eLength\u003c\/td\u003e\n\u003ctd\u003e15.88 m (52 ft 1 in)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eHeight\u003c\/td\u003e\n\u003ctd\u003e5.38 m (17 ft 8 in)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eWing area\u003c\/td\u003e\n\u003ctd\u003e35.0 m²\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eEmpty weight\u003c\/td\u003e\n\u003ctd\u003e5,430 kg (11,971 lbs)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMTOW\u003c\/td\u003e\n\u003ctd\u003e8,900 kg (19,621 lbs)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax speed\u003c\/td\u003e\n\u003ctd\u003e541 km\/h (292 kt \/ 336 mph)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eService ceiling\u003c\/td\u003e\n\u003ctd\u003e11,308 m (37,100 ft)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eStandard fuel capacity\u003c\/td\u003e\n\u003ctd\u003e2,000 L (530 US gal)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax seating\u003c\/td\u003e\n\u003ctd\u003e24 passengers\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\n\u003chr\u003e\n\u003ch3\u003eHandling \u0026amp; Stability Notes\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eAsymmetric thrust:\u003c\/strong\u003e Four small turboprops produce a minimal critical-engine yawing moment — rudder control requirements on engine failure are significantly reduced versus a twin\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFlight controls:\u003c\/strong\u003e Fully mechanical, push-pull rod-actuated — direct, responsive feedback favoured by corporate pilots of the era\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eKnown incident:\u003c\/strong\u003e Airframe F-BMCY sustained a belly-landing in 1981 attributed to undercarriage mechanical complexity\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eStatic test airframe:\u003c\/strong\u003e Airframe No. 04 was designated exclusively for ultimate structural load and wing bending tolerance mapping\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eProgramme \u0026amp; Legacy\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eDeveloper:\u003c\/strong\u003e Société des Avions et Moteurs Henry Potez, France\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eProgramme period:\u003c\/strong\u003e 1962–1967\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTotal airframes built:\u003c\/strong\u003e Fewer than 10\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eProgramme closure:\u003c\/strong\u003e Henry Potez absorbed into Sud Aviation in 1967; type certificate management ceased\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eRegulatory status:\u003c\/strong\u003e No active EASA or FAA Airworthiness Directives — no active TC holder\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSurviving documentation:\u003c\/strong\u003e Original factory brochures, type certificate specifications, and structural blueprints held in French museum archives and specialist repositories\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003cp\u003e\u003cem\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorized distributor.\u003c\/em\u003e\u003c\/p\u003e\n\u003cp\u003e\u003cem\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/em\u003e\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53695332745563,"sku":null,"price":20.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/potez-840-banner-3.png?v=1785487640"},{"product_id":"macchi-nieuport-ni11-ni17-istruzioni-norme-regolaggio-manutenzione","title":"Macchi-Nieuport Ni.11 \u0026 Ni.17 — Istruzioni e Norme per il Regolaggio e la Manutenzione","description":"\u003ch2\u003eMacchi-Nieuport Ni.11 \u0026amp; Ni.17 — \u003cem\u003eIstruzioni e Norme per il Regolaggio e la Manutenzione\u003c\/em\u003e\n\u003c\/h2\u003e\u003cp\u003eSocietà Anonima Nieuport-Macchi, Varese · Arti Grafiche Varesine · 1916–1917\u003c\/p\u003e\u003chr\u003e\u003ch3\u003eCollection Overview\u003c\/h3\u003e\u003cp\u003eThis archival collection brings together the primary-source Italian-language technical manuals issued by \u003cstrong\u003eSocietà Anonima Nieuport-Macchi\u003c\/strong\u003e of Varese for the two most important single-seat sesquiplane fighters operated by the \u003cem\u003eRegia Aeronautica\u003c\/em\u003e and allied air services during the First World War: the \u003cstrong\u003eNi.11 «Bébé»\u003c\/strong\u003e (80 hp Le Rhône 9C) and the \u003cstrong\u003eNi.17\u003c\/strong\u003e (110 hp Le Rhône 9J). Documents span factory maintenance instructions, adjustment norms, and the illustrated parts catalogue covering both airframes.\u003c\/p\u003e\u003chr\u003e\u003ch3\u003eDocument Manifest\u003c\/h3\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eNi.11 «Bébé» — Istruzioni e Norme per il Regolaggio e la Manutenzione del Biplano da Caccia Tipo 11000\u003c\/strong\u003e · Con Motore Rotativo 80 HP · Vol. 8 · Varese, Arti Grafiche Varesine, 1916\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNi.17 — Istruzioni e Norme per il Regolaggio e la Manutenzione del Biplano da Caccia Tipo 17000 (15 mq.)\u003c\/strong\u003e · Con Motore Rotativo 110 HP · Edizione I N.3 · Varese, Arti Grafiche Varesine, 1917\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCatalogo — Apparecchi «Nieuport» Biplani 80 HP 13 mq. – 110 HP 15 mq.\u003c\/strong\u003e · Con Motore Rotativo · Varese, Arti Grafiche Varesine, 1917\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003ch3\u003eAerodynamic Engineering Profile\u003c\/h3\u003e\u003cp\u003eBoth aircraft employed Gustav Delage's \u003cstrong\u003esesquiplane\u003c\/strong\u003e («one-and-a-half plane») configuration: a full-chord upper wing paired with a dramatically narrowed, single-spar lower wing carrying less than half the upper wing's surface area. This layout reduced induced drag and gave the pilot exceptional downward visibility compared to conventional biplanes.\u003c\/p\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eAilerons:\u003c\/strong\u003e Upper wing only. Actuated via torque tubes on the Ni.11; upgraded to streamlined external push-rods and metal control wires on the Ni.17 for cleaner airflow and more immediate response.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCowl:\u003c\/strong\u003e Ni.11 — open «horseshoe» sub-hemispherical cowl for rotary engine venting. Ni.17 — fully circular, closed, tightly faired aluminium cowl, significantly reducing parasitic drag and smoothing fuselage boundary-layer transitions.\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003ch3\u003eEngine Technical Notes\u003c\/h3\u003e\u003ctable\u003e\n\u003cthead\u003e\u003ctr\u003e\n\u003cth\u003eParameter\u003c\/th\u003e\n\u003cth\u003eNi.11\u003c\/th\u003e\n\u003cth\u003eNi.17\u003c\/th\u003e\n\u003c\/tr\u003e\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eEngine\u003c\/td\u003e\n\u003ctd\u003eLe Rhône 9C\u003c\/td\u003e\n\u003ctd\u003eLe Rhône 9J \/ 9Jb\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003ePower\u003c\/td\u003e\n\u003ctd\u003e80 hp\u003c\/td\u003e\n\u003ctd\u003e110–120 hp\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eConfiguration\u003c\/td\u003e\n\u003ctd\u003e9-cyl. air-cooled rotary\u003c\/td\u003e\n\u003ctd\u003e9-cyl. air-cooled rotary\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\u003cp\u003eBecause the entire crankcase and cylinder block rotated around a fixed crankshaft, the engine acted as a massive flywheel, generating severe gyroscopic forces at high RPM. The intermediate Nieuport 16 had fitted the heavier 110 hp motor into the unmodified Ni.11 frame, producing a dangerously nose-heavy aircraft. The Ni.17 resolved this by lengthening the forward fuselage and scaling up overall wing area.\u003c\/p\u003e\u003chr\u003e\u003ch3\u003ePerformance Data\u003c\/h3\u003e\u003ctable\u003e\n\u003cthead\u003e\u003ctr\u003e\n\u003cth\u003eParameter\u003c\/th\u003e\n\u003cth\u003eMacchi-Nieuport Ni.11\u003c\/th\u003e\n\u003cth\u003eMacchi-Nieuport Ni.17\u003c\/th\u003e\n\u003c\/tr\u003e\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eWingspan (upper)\u003c\/td\u003e\n\u003ctd\u003e7.55 m\u003c\/td\u003e\n\u003ctd\u003e8.16 m\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eWing Area\u003c\/td\u003e\n\u003ctd\u003e13.00 m²\u003c\/td\u003e\n\u003ctd\u003e14.75 m²\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eEmpty Weight\u003c\/td\u003e\n\u003ctd\u003e344 kg\u003c\/td\u003e\n\u003ctd\u003e375 kg\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax Takeoff Weight\u003c\/td\u003e\n\u003ctd\u003e480 kg\u003c\/td\u003e\n\u003ctd\u003e560 kg\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Speed\u003c\/td\u003e\n\u003ctd\u003e156 km\/h (sea level)\u003c\/td\u003e\n\u003ctd\u003e170 km\/h (2,000 m)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eService Ceiling\u003c\/td\u003e\n\u003ctd\u003e4,500 m\u003c\/td\u003e\n\u003ctd\u003e5,300 m\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eEndurance\u003c\/td\u003e\n\u003ctd\u003e~2.5 hours\u003c\/td\u003e\n\u003ctd\u003e~2.0 hours\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\u003chr\u003e\u003ch3\u003eHandling \u0026amp; Stability\u003c\/h3\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eGyroscopic Precession:\u003c\/strong\u003e Right-hand turns were aggressively sharp — engine torque and gyroscopic forces pulled the nose naturally into the turn. Left-hand turns forced the nose violently upward, requiring heavy coordinated opposite rudder to prevent high-alpha stalling.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eLongitudinal Trim:\u003c\/strong\u003e No in-flight adjustable stabiliser. Equilibrium managed entirely through pilot stick force against a balanced elevator. Neutral static longitudinal stability — highly responsive but sensitive to atmospheric turbulence.\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003ch3\u003eStructural Advisory — Lower Wing Torsional Weakness\u003c\/h3\u003e\u003cp\u003eThe single most critical structural advisory issued across Allied air services for the Nieuport family concerned \u003cstrong\u003elower wing aeroelastic twisting and structural failure\u003c\/strong\u003e.\u003c\/p\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eV-Strut Torsional Weakness:\u003c\/strong\u003e The sesquiplane layout relied on a single main spar in the narrow lower wing, connected to the upper wing via a single geometric V-strut apex. Lacking a secondary rear spar, the lower wing was prone to catastrophic torsional divergence during extended high-speed dives or high-G pull-outs — ripping fabric and ribs away or shearing the primary spar entirely.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eOperational Directive:\u003c\/strong\u003e Macchi and Nieuport factory advisories ordered strict airspeed management during vertical dives. Field retrofits included reinforcing wire bracing and auxiliary stiffening ribs near the V-strut attachments.\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003cp\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorized distributor.\u003cbr\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53696837058907,"sku":null,"price":34.85,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/banner-2-square.png?v=1785501477"},{"product_id":"salmson-type-2-a2-nomenclature-pieces-detachees-moteur-9zm","title":"Salmson Type 2 A2 — Nomenclature des Pièces détachées \u0026 Moteur Salmson 9ZM","description":"\u003ch3\u003eSalmson Type 2 A2 — \u003cem\u003eNomenclature des Pièces détachées \u0026amp; Moteur Salmson 9ZM\u003c\/em\u003e\n\u003c\/h3\u003e\n\u003cp\u003eSociété des Moteurs Salmson · Paris · 1918–191x\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eCollection Overview\u003c\/h3\u003e\n\u003cp\u003eThis archival collection brings together the primary-source technical publications issued by the \u003cstrong\u003eSociété des Moteurs Salmson\u003c\/strong\u003e for the \u003cstrong\u003eAvion S.A.L. 2 – A2\u003c\/strong\u003e, the premier French two-seat biplane reconnaissance aircraft of the First World War, and its dedicated powerplant, the \u003cstrong\u003eSalmson 9ZM\u003c\/strong\u003e 9-cylinder water-cooled radial engine. Documents are presented in both French and Italian language editions, reflecting the aircraft's widespread Allied service.\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eDocument Manifest\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eNomenclature des Pièces détachées de l'Avion S.A.L. 2 – A2\u003c\/strong\u003e · Société des Moteurs Salmson · Illustrated parts catalogue covering the complete airframe: Cabane, Montants de cellules, Stabilisation Longitudinale, Stabilisation Latérale (Ailerons), Organes de Direction, Atterrissage, Béquille Arrière, Haubannage des Cellules, Haubannage du Train d'Atterrissage, Haubannage du Plan Central, Haubannage du Stabilisateur, Corps de l'Appareil — Fuselage (Menuiserie \u0026amp; Ferrures), Capotage Bois\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNotice d'entretien et Nomenclature — Moteur Salmson 9ZM\u003c\/strong\u003e · 1918 · French language edition\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eManuale Istruzioni e Nomenclatore — Motore Salmson 9ZM\u003c\/strong\u003e · 191x · Italian language edition\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eAirframe Engineering Profile\u003c\/h3\u003e\n\u003cp\u003eThe Salmson 2 A2 was designed as an equal-span, two-bay biplane of high structural rigidity, engineered to replace fragile reconnaissance predecessors on the Western Front.\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eFuselage:\u003c\/strong\u003e Conventional wooden construction (frêne\/spruce longerons, ash\/spruce montants) wrapped in doped fabric. Fuselage frames span plans n°1–11 with full ferrure detailing.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eWing \u0026amp; Aileron System:\u003c\/strong\u003e Coupled dual-wing aileron surfaces on both upper and lower mainplanes. Full aileron IPC coverage: longerons, nervures caisson, nervures pleines, bords de sortie, charnières, guignols, ferrures de conjugaison.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eEmpennage:\u003c\/strong\u003e Empennage horizontal complet entoilé, peint, camouflé et verni — full horizontal stabiliser assembly with ball-bearing roulements, nervures, longerons, and renforts. Gouvernail complet entoilé, peint et verni with full guignol and hauban detailing.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eUndercarriage:\u003c\/strong\u003e V-strut train d'atterrissage with demi-essieux, bobines médianes de sandow, carènes d'essieux aluminium, bagues de butée, roues complètes, chambres à air, sandow amortisseur. Béquille arrière complète with sandow amortisseur and cosses d'attache.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eHaubannage:\u003c\/strong\u003e Comprehensive bracing system — câbles 1 toron, cordes à piano, carènes bois pour haubans de cellules (4\/5, 3\/5, 3, 2\/5 sets), haubannage du plan central and stabilisateur.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eEngine Technical Notes — Salmson 9ZM\u003c\/h3\u003e\n\u003cp\u003eThe Salmson 9ZM was a \u003cstrong\u003e9-cylinder water-cooled radial piston engine\u003c\/strong\u003e generating approximately 230 hp (172 kW) — a technically distinctive powerplant that set the Salmson 2 apart from rotary-engined contemporaries. Its stationary crankcase eliminated the gyroscopic precession penalties of rotary engines, delivering predictable handling and superior high-altitude performance.\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eCooling:\u003c\/strong\u003e Frontal radiator matrix with cockpit-controlled mechanical louvers and shutters.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePropulsion:\u003c\/strong\u003e Fixed-pitch two-bladed laminated wooden propeller keyed directly to the crankshaft.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFuel system:\u003c\/strong\u003e Forward-integrated self-sealing rubber fuel tanks.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003ePerformance Data\u003c\/h3\u003e\n\u003ctable\u003e\n\u003cthead\u003e\n\u003ctr\u003e\n\u003cth\u003eParameter\u003c\/th\u003e\n\u003cth\u003eSpecification\u003c\/th\u003e\n\u003c\/tr\u003e\n\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Speed\u003c\/td\u003e\n\u003ctd\u003e186 km\/h (116 mph) at 2,000 m\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eService Ceiling\u003c\/td\u003e\n\u003ctd\u003e6,250 m (20,500 ft)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eRange\u003c\/td\u003e\n\u003ctd\u003e480 km (300 miles)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eEndurance\u003c\/td\u003e\n\u003ctd\u003e3 hours\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eEmpty Weight\u003c\/td\u003e\n\u003ctd\u003e780 kg\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax Loaded Weight\u003c\/td\u003e\n\u003ctd\u003e1,290 kg\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\n\u003chr\u003e\n\u003ch3\u003eVariants \u0026amp; Service Notes\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eSalmson 2 A2:\u003c\/strong\u003e Standard two-seat reconnaissance variant — the primary subject of this collection.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSalmson 2 B2:\u003c\/strong\u003e Tactical bomber variant with dual under-wing bomb racks.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSalmson 2 E2:\u003c\/strong\u003e Dual-control trainer configuration.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eType Otsu 1:\u003c\/strong\u003e Licensed production by Kawasaki for the Imperial Japanese Army Air Service.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003cp\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorized distributor.\u003cbr\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53696993821019,"sku":null,"price":34.85,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/banner-4-hero-portrait_ea37e21f-e819-4e6d-a934-bac7f7a3fb63.png?v=1785504440"},{"product_id":"dewoitine-d-332-d-333-d-338-notice-technique-aerodynamic-documentation-air-france-trimotor-series","title":"Dewoitine D.332 · D.333 · D.338 — Notice Technique \u0026 Aerodynamic Documentation | Air France Trimotor Series","description":"\u003ch3\u003eDewoitine D.332 · D.333 · D.338 — Notice Technique \u0026amp; Aerodynamic Documentation\u003c\/h3\u003e\n\u003cp\u003e\u003cem\u003eAir France Trimotor Series — Primary-Source Archival Edition\u003c\/em\u003e\u003c\/p\u003e\n\u003cp\u003eThis collection brings together the primary technical documentation for three successive variants of Dewoitine's all-metal low-wing trimotor airliner family, operated by Air France on its prestige South Atlantic and Far East routes during the late 1930s. The centrepiece is the original \u003cstrong\u003eNotice Technique pour Avion Dewoitine Type 338.S\u003c\/strong\u003e, issued by Air France, accompanied by contemporary aerodynamic reports and manufacturer documentation for the D.332 and D.333.\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eDocument Manifest\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eNotice Technique pour Avion Dewoitine Type 338.S\u003c\/strong\u003e — Air France, original issue. Covers: Caractéristiques Générales (Planeur \u0026amp; Moteur), Structure, Ouvertures, Gouvernes, Atterrisseur, Bâtis Moteurs, Commandes Moteurs, Circuits Généraux (Essence, Huile, Air comprimé), Sécurité-Contrôle, Habitabilité, Électricité, T.S.F.–Gonio–ASV, Manœuvre–Entretien, Récapitulation Matières Standards. 69 pages of nomenclature plates.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDewoitine D.332 — NACA Aerodynamic Report AC185\u003c\/strong\u003e — Contemporary U.S. aerodynamic analysis of the D.332 (Émeraude) airframe.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDewoitine D.333 — Manufacturer's Brochure\u003c\/strong\u003e — Original Dewoitine factory documentation for the D.333 variant.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eAerodynamic Profile \u0026amp; Structural Evolution\u003c\/h3\u003e\n\u003cp\u003eThe D.332–D.333–D.338 series represents a disciplined engineering progression driven by aerodynamic refinement, payload growth, and hard lessons from operational losses.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eD.332 \u003cem\u003eÉmeraude\u003c\/em\u003e\u003c\/strong\u003e — Derived directly from the single-engine long-range record-breaker Dewoitine D.33, the D.332 adopted a high-aspect-ratio, all-metal cantilever single-spar wing. Fixed undercarriage drag was mitigated by prominent streamlined \"trousered\" aerodynamic fairings over the main gear legs.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eD.333\u003c\/strong\u003e — Following the 1934 icing loss of the \u003cem\u003eÉmeraude\u003c\/em\u003e over Corbigny, aerodynamicists repositioned the wing-mounted engines closer to the central fuselage to optimise cowling efficiency. To offset a 1,650 kg weight increase, trailing-edge wing flaps were reworked, reducing landing speeds by 20 km\/h. A reinforced spar assembly was mandated following the structural investigation.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eD.338\u003c\/strong\u003e — Wind tunnel research led to a semi-retractable undercarriage: mainwheels tucked upward into extended engine nacelles, eliminating the fixed-gear drag penalty while retaining partial wheel exposure below the nacelles to aerodynamically shield the fuselage skin during emergency gear-up landings. Longitudinal instability discovered during prototype trials (F-AOZA) forced a redesign of the wing leading-edge sweep geometry and empennage.\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eEngine Technical Notes — Hispano-Suiza 9V Series\u003c\/h3\u003e\n\u003cp\u003eAll three variants relied on 9-cylinder air-cooled radial configurations driving two-blade variable-pitch metal propellers.\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eD.332\u003c\/strong\u003e — Three Hispano-Suiza 9V radials (French licence-built Wright R-1820 Cyclone). 575 hp nominal \/ 641 hp take-off. Magnetos: R.B. type P9.BA (6 units). Carburettors: H.S. Solex 70 FFIP. Propellers: Hamilton bipale, ⌀ 3 m 215.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eD.333\u003c\/strong\u003e — Retained the standard Hispano-Suiza 9V powerplant. Fuel management redesigned: fuselage tanks replaced by 4 distinct wing-mounted fuel cells.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eD.338\u003c\/strong\u003e — Upgraded to Hispano-Suiza 9Vd-16et17 variants with specialised supercharging. 650 hp at take-off. Nominal altitude at full admission: 1,450 m. Fuel system: 4 essence + 1 essence éthyl + 3 huile tanks; total capacity 3,420 L essence \/ 300 L huile \/ 170 L essence éthyl.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003ePerformance Data\u003c\/h3\u003e\n\u003ctable\u003e\n\u003cthead\u003e\n\u003ctr\u003e\n\u003cth\u003eParameter\u003c\/th\u003e\n\u003cth\u003eD.332\u003c\/th\u003e\n\u003cth\u003eD.333\u003c\/th\u003e\n\u003cth\u003eD.338\u003c\/th\u003e\n\u003c\/tr\u003e\n\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eCrew \/ Passengers\u003c\/td\u003e\n\u003ctd\u003e4 \/ 8\u003c\/td\u003e\n\u003ctd\u003e3–4 \/ 10\u003c\/td\u003e\n\u003ctd\u003e4 \/ 12–22\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eWingspan\u003c\/td\u003e\n\u003ctd\u003e29.00 m\u003c\/td\u003e\n\u003ctd\u003e29.00 m\u003c\/td\u003e\n\u003ctd\u003e29.40 m\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eLength\u003c\/td\u003e\n\u003ctd\u003e18.95 m\u003c\/td\u003e\n\u003ctd\u003e21.95 m\u003c\/td\u003e\n\u003ctd\u003e22.10 m\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eEmpty Weight\u003c\/td\u003e\n\u003ctd\u003e5,280 kg\u003c\/td\u003e\n\u003ctd\u003e6,375 kg\u003c\/td\u003e\n\u003ctd\u003e7,905 kg\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMTOW\u003c\/td\u003e\n\u003ctd\u003e9,350 kg\u003c\/td\u003e\n\u003ctd\u003e11,000 kg\u003c\/td\u003e\n\u003ctd\u003e11,150 kg\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax Airspeed\u003c\/td\u003e\n\u003ctd\u003e300 km\/h\u003c\/td\u003e\n\u003ctd\u003e290 km\/h\u003c\/td\u003e\n\u003ctd\u003e310 km\/h\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eCruising Speed\u003c\/td\u003e\n\u003ctd\u003e250 km\/h\u003c\/td\u003e\n\u003ctd\u003e240 km\/h\u003c\/td\u003e\n\u003ctd\u003e260 km\/h\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eService Ceiling\u003c\/td\u003e\n\u003ctd\u003e6,500 m\u003c\/td\u003e\n\u003ctd\u003e6,150 m\u003c\/td\u003e\n\u003ctd\u003e4,900 m\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax Range\u003c\/td\u003e\n\u003ctd\u003e2,000 km\u003c\/td\u003e\n\u003ctd\u003e2,000 km\u003c\/td\u003e\n\u003ctd\u003e2,000 km\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\n\u003chr\u003e\n\u003ch3\u003eD.338 Airframe Specifications (from Notice Technique)\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003eWingspan: 29 m 356 | Total height: 5 m 574 | Total length: 22 m 130\u003c\/li\u003e\n\u003cli\u003eWing type: Monoplane trapézoïdale, extrémités elliptiques | Dihedral: 3° | Incidence: 4°\u003c\/li\u003e\n\u003cli\u003eNet wing surface: 87 m² 16 | Total lifting surface: 97 m² 34\u003c\/li\u003e\n\u003cli\u003eFuselage section (maître-couple): 2,400 × 1,776 mm, rectangular, 4 m² 26\u003c\/li\u003e\n\u003cli\u003eHorizontal tail: span 7 m 800, fixed surface 10 m² 50, mobile surface 4 m² 50\u003c\/li\u003e\n\u003cli\u003eVertical tail: height 2 m 811, fixed surface 2 m² 55, mobile surface 2 m² 15\u003c\/li\u003e\n\u003cli\u003eUndercarriage: Escamotable, 2 × Messier independent wheels, 1.630 × 365 tyres, 4 kg\/cm² inflation, Messier shock absorbers, Messier brakes, track 7 m 000\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003cp\u003e\u003cem\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorised distributor.\u003c\/em\u003e\u003c\/p\u003e\n\u003cp\u003e\u003cem\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/em\u003e\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53697453326683,"sku":null,"price":20.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/banner-2-d-338-notice-technique-low-pass.png?v=1785509494"},{"product_id":"dewoitine-d-520-notice-descriptive-et-dutilisation-armee-de-lair-fighter-documentation","title":"Dewoitine D.520 — Notice Descriptive et d'Utilisation | Armée de l'Air Fighter Documentation","description":"\u003ch2\u003eDewoitine D.520 — Notice Descriptive et d'Utilisation\u003c\/h2\u003e\n\u003cp\u003e\u003cem\u003eMinistère de l'Air · Armée de l'Air — Primary-Source Archival Edition\u003c\/em\u003e\u003c\/p\u003e\n\n\u003cp\u003eFrance's most capable fighter at the outbreak of the Second World War, the Dewoitine D.520 represented the pinnacle of SNCAM engineering under Émile Dewoitine — a masterful balance of aerodynamic refinement, liquid-cooled V12 power, and exceptional handling stability. This archival edition presents the original \u003cstrong\u003eNotice Descriptive et d'Utilisation de l'Avion de Chasse D.520 S\u003c\/strong\u003e, issued by the Ministère de l'Air \/ Armée de l'Air, together with the official \u003cstrong\u003eTableau des Caractéristiques\u003c\/strong\u003e data sheet.\u003c\/p\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003eDocument Manifest\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eNotice Descriptive et d'Utilisation — Avion de Chasse D.520 S, Moteur 12-Y45\u003c\/strong\u003e — Ministère de l'Air \/ Armée de l'Air, original issue. Covers airframe description, systems utilisation, and operational procedures.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTableau des Caractéristiques — Avion D.520 S\u003c\/strong\u003e — Official characteristics data sheet. Covers: Forme, Spécifications et Emploi; Encombrement et Assiette de Garage (full dimensional data); undercarriage geometry; propeller ground clearance at all oleo coefficients.\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003eAirframe Geometry — From the Tableau des Caractéristiques\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003eEnvergure maximum: \u003cstrong\u003e10 m 200\u003c\/strong\u003e\n\u003c\/li\u003e\n\u003cli\u003eLongueur totale: \u003cstrong\u003e8 m 760\u003c\/strong\u003e\n\u003c\/li\u003e\n\u003cli\u003eHauteur totale (ligne de vol, train sorti): \u003cstrong\u003e3 m 390\u003c\/strong\u003e\n\u003c\/li\u003e\n\u003cli\u003eHauteur de l'axe hélice au-dessus du sol — Au repos, coefficient 1 (mi-course, ½ aplatiss.): \u003cstrong\u003e2,265 m\u003c\/strong\u003e | tout à plat: \u003cstrong\u003e2,030 m\u003c\/strong\u003e\n\u003c\/li\u003e\n\u003cli\u003eEn ligne de vol, coefficient 1: \u003cstrong\u003e1,845 m\u003c\/strong\u003e | tout à plat: \u003cstrong\u003e1,615 m\u003c\/strong\u003e\n\u003c\/li\u003e\n\u003cli\u003eGarde de l'hélice — Au repos, coefficient 1: \u003cstrong\u003e0,74 m\u003c\/strong\u003e | tout à plat: \u003cstrong\u003e0,465 m\u003c\/strong\u003e\n\u003c\/li\u003e\n\u003cli\u003eEn ligne de vol, coefficient 1: \u003cstrong\u003e0,32 m\u003c\/strong\u003e | tout à plat: \u003cstrong\u003e0,09 m\u003c\/strong\u003e\n\u003c\/li\u003e\n\u003cli\u003eAngle au sol (tangente à la roue \/ extrémité hélice, en ligne de vol, coefficient 1): \u003cstrong\u003e10°\u003c\/strong\u003e\n\u003c\/li\u003e\n\u003cli\u003eType: Avion de chasse monoplace, monomoteur, refroidissement par liquide, monoplan cantilever à aile basse\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003eAerodynamic Design \u0026amp; Airframe Engineering\u003c\/h3\u003e\n\u003cp\u003eThe SNCAM design team prioritised strict drag reduction to extract maximum velocity from a lower-horsepower engine. The wing adopted an all-metal, single-spar duralumin-skinned structure with a NACA 23012 airfoil profile on the vertical stabiliser to enhance tracking stability at high speeds.\u003c\/p\u003e\n\u003cp\u003eThe original prototype (D.520-01) suffered from severe engine overheating via dual underwing radiators. Aerodynamic revisions relocated the cooling apparatus into a single, aerodynamically clean under-fuselage bath, resolving boundary layer separation issues. Under the SNCASE design office in 1942, advanced aerodynamic modelling on D.520 No. 465 eliminated stray airframe drag trails — sealing manufacturing gaps and redesigning engine cowlings shaved 0.65 off the 100 Cx drag coefficient.\u003c\/p\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003eEngine Technical Notes — Hispano-Suiza 12Y-45\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003ePowerplant:\u003c\/strong\u003e Hispano-Suiza 12Y-45, 12-cylinder liquid-cooled V12 — 930 hp (697 kW) at take-off\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSupercharger:\u003c\/strong\u003e Mechanically driven, single-stage, single-speed\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePropeller:\u003c\/strong\u003e Three-blade variable-pitch pneumatic Ratier or Chauvière\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMoteur-canon configuration:\u003c\/strong\u003e Engine blocks cast with a central hollow axis between cylinder banks, allowing a 20 mm Hispano-Suiza HS-404 autocannon to fire through the propeller hub — a defining engineering characteristic of the type\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003eHandling \u0026amp; Stability\u003c\/h3\u003e\n\u003cp\u003eOfficial CEMA (Centre d'Essais du Matériel Aérien) flight testing reported the D.520 as an exceptionally pleasant, stable, and highly manoeuvrable gun platform. Wide-track undercarriage retracted inward into the wing profile — unlike the narrow-track Bf 109 — giving excellent ground handling stability and minimising ground loop risk on unpaved airfields. Aerodynamic reports validated superb stall warning behaviour and predictable spin recovery, making the type significantly safer for low-hour pilots transitioning from biplanes.\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eFlight controls: High-aspect-ratio fabric-covered ailerons; pneumatically actuated split trailing-edge flaps\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003ePerformance Data — CEMA Trials\u003c\/h3\u003e\n\u003ctable\u003e\n\u003cthead\u003e\u003ctr\u003e\n\u003cth\u003eMetric\u003c\/th\u003e\n\u003cth\u003e12Y-45 (Standard)\u003c\/th\u003e\n\u003cth\u003e12Y-49 (Experimental)\u003c\/th\u003e\n\u003c\/tr\u003e\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Speed\u003c\/td\u003e\n\u003ctd\u003e534 km\/h at 5,500 m\u003c\/td\u003e\n\u003ctd\u003e538 km\/h at 7,020 m\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eSea Level Speed\u003c\/td\u003e\n\u003ctd\u003e425 km\/h\u003c\/td\u003e\n\u003ctd\u003e414 km\/h\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eTime to 4,000 m\u003c\/td\u003e\n\u003ctd\u003e5 min 49 sec\u003c\/td\u003e\n\u003ctd\u003e—\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eTime to 8,000 m\u003c\/td\u003e\n\u003ctd\u003e14 min 30 sec\u003c\/td\u003e\n\u003ctd\u003e—\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eCombat Range\u003c\/td\u003e\n\u003ctd\u003e890 km\u003c\/td\u003e\n\u003ctd\u003e1,539 km (aux. tanks)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eService Ceiling\u003c\/td\u003e\n\u003ctd\u003e11,000 m\u003c\/td\u003e\n\u003ctd\u003e—\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003eEngineering Bulletins \u0026amp; Variants\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eBulletin D.520-S \/ No. 465\u003c\/strong\u003e — Higher-pressure supercharger compressor wheel fitted to production lines to boost high-altitude performance under occupational restrictions\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eBulletin D.524\u003c\/strong\u003e — Experimental installation of the 1,200 hp Hispano-Suiza 12Y-89; nose assembly lengthened to accommodate modified cooling plumbing\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eBulletin SE.520Z\u003c\/strong\u003e — Post-war structural conversion framework for the 1,600 hp Hispano-Suiza 12Z engine; all secondary machine guns relocated entirely inside the wing profile for a pure wing-cannon layout\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003chr\u003e\n\n\u003cp\u003e\u003cem\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorised distributor.\u003c\/em\u003e\u003c\/p\u003e\n\u003cp\u003e\u003cem\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/em\u003e\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53697511948635,"sku":null,"price":20.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/banner-1-d-520-wartime-flight-notice-descriptive.png?v=1785510372"},{"product_id":"dewoitine-d-500-d-501-devis-de-poids-notice-technique-armee-de-lair-interceptor-documentation","title":"Dewoitine D.500 · D.501 — Devis de Poids \u0026 Notice Technique | Armée de l'Air Interceptor Documentation","description":"\u003ch2\u003eDewoitine D.500 · D.501 — Devis de Poids \u0026amp; Notice Technique\u003c\/h2\u003e\n\u003cp\u003e\u003cem\u003eAvion de Chasse Type D 500 \/ D 500-510 — Primary-Source Archival Edition\u003c\/em\u003e\u003c\/p\u003e\n\n\u003cp\u003eFrance's first all-metal, low-wing monoplane interceptor, the Dewoitine D.500 and D.501 represented a decisive break from the fabric-covered biplanes of the Great War era. Designed by Émile Dewoitine to meet the 1930 \"C1\" fighter specification, these aircraft served as the Armée de l'Air's primary interceptors through the mid-1930s and directly paved the engineering path to the legendary D.520. This archival edition presents the original factory \u003cstrong\u003eDevis de Poids\u003c\/strong\u003e weight budget sheets, the \u003cstrong\u003eNotice Technique\u003c\/strong\u003e structural description for the Avion Dewoitine Type D 500 \/ D 500-510, and three primary-source engine manuals for the Hispano-Suiza 12Y powerplant family.\u003c\/p\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003eDocument Manifest\u003c\/h3\u003e\n\n\u003ch4\u003eAirframe Documentation\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eDevis de Poids — Article VI: Aménagements Fixes\u003c\/strong\u003e — Supports des instruments de bord (2.600 kg); Supports des armes et munitions: 1° supports des armes 4.940 kg + 2° boîtes à cartouches complètes 8.210 kg = \u003cstrong\u003e13.150 kg\u003c\/strong\u003e; Supports de matériel de sécurité (bouteille d'inhalateur) 0.180 kg; Supports de matériel électrique et canalisations: canalisations 1.600 + prises de courant 0.160 = 1.760 kg; Postes de commandes fixes (commandes des mitrailleuses) 9.035 kg; Sièges fixes — Siège pilote 10.000 kg. \u003cstrong\u003ePoids total aménagements fixes: 36.725 kg\u003c\/strong\u003e\n\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDevis de Poids — Article VII: Combustible\u003c\/strong\u003e — Essence: Réservoir N°1 75.000 + N°2 60.000 + N°3 75.000 = 210.000 kg; Huile: 20.000 kg. \u003cstrong\u003ePoids total du combustible: 230.000 kg\u003c\/strong\u003e\n\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDevis de Poids — Article VIII: Équipement Général\u003c\/strong\u003e — Instruments de bord et navigation: Compas Vion type 31 (1.950 kg); Porte-cartes Aivaz (0.350 kg); Contrôleur de vol Aéra Baclin (3.865 kg); Clinomètre Aéra type 8 (0.540 kg); Altimètre (0.120 kg); Montre (0.120 kg); Rétroplace (0.250 kg). \u003cstrong\u003ePoids total équipement général: 7.195 kg\u003c\/strong\u003e\n\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDevis de Poids — Article IX: Équipement Spécial\u003c\/strong\u003e — Armement: 2× mitrailleuses Vickers 13.400 kg each = 26.800 kg; collimateur OPL clair 2.420 kg; munitions 7.7 mm × 600 cartouches = 19.500 kg. Poids total armement: 48.720 kg. Matériel de sécurité: inhalateur Munerelle 11.140 kg + parachute 12.000 kg = 23.140 kg. Matériel électrique: génératrice MAI 300W 5.500 kg; tableau de contrôle SGE 0.800 kg; accumulateurs 2.500 kg; tableau de chauffage SGE 0.560 kg; rhéostat de collimateur SGE 0.320 kg = 9.680 kg. Radiotélégraphie: poste TSF 30.000 kg. \u003cstrong\u003ePoids total équipement spécial: 111.540 kg\u003c\/strong\u003e\n\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDevis de Poids — Article X: Équipage\u003c\/strong\u003e — Pilote: 1 × 80.000 kg. \u003cstrong\u003ePoids total équipage: 80 kg\u003c\/strong\u003e\n\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNotice Technique — Description Planeur (D 500-510)\u003c\/strong\u003e — Structural description of the trapezoidal low-wing monoplane cellule with elliptical wingtips. Three-section wing joined by two main axes and bolted corner fittings. Central section carries fuel tanks and wing machine guns. Single-spar duralumin caisson construction with profiled ribs and duralumin skin. Spar placed at 1\/3 chord depth, formed of two profiled duralumin flanges and a duralumin sheet web. Includes engineering drawings: Fig. 1 (wing plan section), Fig. 2 (spar profile), Fig. 3 (Attache de Longeron d'Aile — riveted spar attachment plate), Fig. 4 (Détail des Semelles), Fig. 5 (Détail d'un Caisson de Longeron). Bord d'attaque: leading-edge caisson with ribs and skin plates (Fig. 6 onwards).\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003ch4\u003eEngine Documentation — Hispano-Suiza 12Y Series\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eNotice Technique des Moteurs 12 Y\u003c\/strong\u003e — Société Française Hispano-Suiza, factory edition. Primary-source engine technical manual issued directly by the manufacturer covering the 12Y powerplant family as fitted to the D.500, D.501, D.510, and D.520 series.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eInstallation sur Avion du Moteur Hispano-Suiza Type 12 Y\u003c\/strong\u003e — Engine installation guide covering airframe integration requirements: berceau-moteur rigidity, carter table fixation, capotage ventilation, cooling system layout (radiateur under-fuselage bath), oil reservoir positioning, essence circuit siphon avoidance, compresseur air intake placement, and hélice ground clearance calculations. Includes 8 numbered installation directives and aircraft photograph showing engine cowling installation.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNotice Technique des Moteurs Hispano Suiza Type 12 Y-31\u003c\/strong\u003e — Ministère de l'Air \/ Armée de l'Air, Notice N° 110, January 1940. Official military edition of the 12Y-31 engine technical manual, issued under Armée de l'Air authority for operational maintenance reference.\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003eCore Variant Differences\u003c\/h3\u003e\n\u003cp\u003eThe D.500 and D.501 shared an identical airframe but differed in engine and armament configuration:\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eD.500\u003c\/strong\u003e — Hispano-Suiza 12Xbrs, 690 hp. Armament: 2× nose-mounted 7.5 mm MAC machine guns (synchronised through propeller arc) + 2× wing-mounted 7.5 mm machine guns\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eD.501\u003c\/strong\u003e — Hispano-Suiza 12Xcrs. Armament: 1× 20 mm Hispano-Suiza cannon firing through the hollow propeller hub (moteur-canon) + 2× wing-mounted 7.5 mm machine guns\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003eTechnical Specifications (D.501)\u003c\/h3\u003e\n\u003ctable\u003e\n\u003cthead\u003e\u003ctr\u003e\n\u003cth\u003eParameter\u003c\/th\u003e\n\u003cth\u003eData\u003c\/th\u003e\n\u003c\/tr\u003e\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eRole\u003c\/td\u003e\n\u003ctd\u003eSingle-seat interceptor fighter\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eCrew\u003c\/td\u003e\n\u003ctd\u003e1 (Pilote — 80 kg per Devis de Poids)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eWingspan\u003c\/td\u003e\n\u003ctd\u003e12.09 m\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eLength\u003c\/td\u003e\n\u003ctd\u003e7.74 m\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Speed\u003c\/td\u003e\n\u003ctd\u003e361–367 km\/h\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax Take-off Weight\u003c\/td\u003e\n\u003ctd\u003e1,787 kg\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eRange\u003c\/td\u003e\n\u003ctd\u003e870 km\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eFirst Flight\u003c\/td\u003e\n\u003ctd\u003e18 June 1932\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eOperational Deliveries\u003c\/td\u003e\n\u003ctd\u003e1935\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eProduction\u003c\/td\u003e\n\u003ctd\u003e~101 D.500 + ~162 D.501\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003eOperational History \u0026amp; Export\u003c\/h3\u003e\n\u003cp\u003eDesigned to replace the Nieuport 62 biplane, the D.500\/501 entered Armée de l'Air service in 1935 as France's first modern all-metal monoplane fighter. Export customers included the Republic of China (18 aircraft, deployed against Japanese forces), Lithuania (14 aircraft), and Republican Spain. By May 1940, the type was wholly outclassed by the Messerschmitt Bf 109 and relegated to regional defence and advanced pilot training. The D.500\/501 lineage evolved directly through the D.510 (860 hp) into the D.520 — France's premier enclosed-cockpit, retractable-gear fighter of the Battle of France.\u003c\/p\u003e\n\n\u003chr\u003e\n\n\u003cp\u003e\u003cem\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorised distributor.\u003c\/em\u003e\u003c\/p\u003e\n\u003cp\u003e\u003cem\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/em\u003e\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53697561755995,"sku":null,"price":44.85,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/banner-3-cloud-flight-pilot-visible.png?v=1785510963"},{"product_id":"caudron-c-59-notice-technique-parts-catalog-brochure-commerciale-aeroplanes-caudron-trainer-documentation","title":"Caudron C.59 — Notice Technique, Parts Catalog \u0026 Brochure Commerciale | Aéroplanes Caudron Trainer Documentation","description":"\u003ch2\u003eCaudron C.59 — Notice Technique, Parts Catalog \u0026amp; Brochure Commerciale\u003c\/h2\u003e\n\u003cp\u003e\u003cem\u003eAéroplanes Caudron — Primary-Source Archival Edition\u003c\/em\u003e\u003c\/p\u003e\n\n\u003cp\u003eOne of the most successful training aircraft of the 1920s, the Caudron C.59 was produced in greater numbers than almost any other French aircraft of its era — over 1,800 units built between 1922 and 1924, serving the Aéronautique Militaire, French Naval Aviation, and air arms across four continents. Designed by Paul Deville and René Talpin at Société des Avions Caudron, it set the standard for intermediate biplane training through the mid-1920s. This archival edition brings together the original factory \u003cstrong\u003eNotice Technique\u003c\/strong\u003e (two editions), the \u003cstrong\u003eRépertoire des Pièces R.T.2\u003c\/strong\u003e parts catalog, and the complete trilingual \u003cstrong\u003eBrochure Commerciale\u003c\/strong\u003e — a rare survival of Caudron's original sales documentation in French, English, and Spanish.\u003c\/p\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003eDocument Manifest\u003c\/h3\u003e\n\n\u003ch4\u003eTechnical Documentation\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eNotice Technique — Caudron C.59 ET2 (Manufacturer Edition)\u003c\/strong\u003e — Factory-issued technical notice for the C.59, manufacturer’s edition. Covers airframe structure, systems description, and maintenance procedures.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNotice Technique — Caudron C.59 ET2 (Second Edition)\u003c\/strong\u003e — Revised technical notice, second edition. Covers updated structural and systems data.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eRépertoire des Pièces — Caudron C.59 R.T.2 (Parts Catalog)\u003c\/strong\u003e — Original factory parts catalog for the C.59, listing all airframe and engine components with reference numbers.\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003ch4\u003eCommercial Documentation\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eBrochure Commerciale — Aéroplanes Caudron, Type C.59\u003c\/strong\u003e — Complete 8-page trilingual sales brochure (French \/ English \/ Spanish). Includes:\n\u003cul\u003e\n\u003cli\u003eTrilingual specifications sheet — \u003cstrong\u003e140 HP version\u003c\/strong\u003e: Envergure sup. 10 m 240 \/ inf. 9 m 520; Longueur 7 m 800; Hauteur 2 m 700; Poids à vide 590 kg; Poids utile 160 kg; Poids total \u003cstrong\u003e890 kg\u003c\/strong\u003e\n\u003c\/li\u003e\n\u003cli\u003eTrilingual specifications sheet — \u003cstrong\u003e140\/180 HP version\u003c\/strong\u003e: Envergure sup. 10 m 240 \/ inf. 9 m 250; Longueur 7 m 730; Poids à vide 670 kg; Poids utile 160 kg; Poids total \u003cstrong\u003e1,000 kg\u003c\/strong\u003e\n\u003c\/li\u003e\n\u003cli\u003eFactory photograph: \u003cem\u003eVue des Usines Caudron à Issy-les-Moulinaux\u003c\/em\u003e (two editions — orange border and blue border)\u003c\/li\u003e\n\u003cli\u003eAircraft photograph: C.59 registration F-ESAIF on grass airfield\u003c\/li\u003e\n\u003cli\u003eCaudron script logo cover page, Type C.59\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003eDesign \u0026amp; Structure\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eType:\u003c\/strong\u003e Un-staggered two-bay biplane, wood construction, canvas fabric covering\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eWings:\u003c\/strong\u003e Upper wing greater span than lower; ailerons on upper wing only\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCockpit:\u003c\/strong\u003e Open tandem dual-control layout — student forward under upper wing, instructor aft\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eEngine:\u003c\/strong\u003e Hispano-Suiza 8Ab V-8 water-cooled, 130 kW (180 hp), two-blade wooden propeller\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCooling:\u003c\/strong\u003e Lamblin radiator positioned under the fuselage forward of the fixed undercarriage\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003eTechnical Specifications\u003c\/h3\u003e\n\u003ctable\u003e\n\u003cthead\u003e\u003ctr\u003e\n\u003cth\u003eParameter\u003c\/th\u003e\n\u003cth\u003e140 HP Version\u003c\/th\u003e\n\u003cth\u003e140\/180 HP Version\u003c\/th\u003e\n\u003c\/tr\u003e\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eCrew\u003c\/td\u003e\n\u003ctd colspan=\"2\"\u003e2 (Instructor \u0026amp; Student)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eUpper Span\u003c\/td\u003e\n\u003ctd\u003e10 m 240\u003c\/td\u003e\n\u003ctd\u003e10 m 240\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eLower Span\u003c\/td\u003e\n\u003ctd\u003e9 m 520\u003c\/td\u003e\n\u003ctd\u003e9 m 250\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eChord\u003c\/td\u003e\n\u003ctd colspan=\"2\"\u003e1 m 455\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eLifting Area\u003c\/td\u003e\n\u003ctd colspan=\"2\"\u003e26 m²\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eOverall Length\u003c\/td\u003e\n\u003ctd\u003e7 m 800\u003c\/td\u003e\n\u003ctd\u003e7 m 730\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eHeight\u003c\/td\u003e\n\u003ctd colspan=\"2\"\u003e2 m 700\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eEmpty Weight\u003c\/td\u003e\n\u003ctd\u003e590 kg\u003c\/td\u003e\n\u003ctd\u003e670 kg\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eUseful Load\u003c\/td\u003e\n\u003ctd\u003e160 kg\u003c\/td\u003e\n\u003ctd\u003e160 kg\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eInstruments\u003c\/td\u003e\n\u003ctd\u003e10 kg\u003c\/td\u003e\n\u003ctd\u003e10 kg\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eFuel (upper feeder)\u003c\/td\u003e\n\u003ctd\u003e28 l à 20 k\u003c\/td\u003e\n\u003ctd\u003e28 l à 20 k\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eFuel (lower tank)\u003c\/td\u003e\n\u003ctd\u003e120 l à 85 k — 110 kg total\u003c\/td\u003e\n\u003ctd\u003e130 l à 93 k — 113 kg total\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eOil in engine casing\u003c\/td\u003e\n\u003ctd\u003e5 l à 5 k\u003c\/td\u003e\n\u003ctd\u003e18 l — 17 kg\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eWater\u003c\/td\u003e\n\u003ctd\u003e20 kg\u003c\/td\u003e\n\u003ctd\u003e30 kg\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eWhole Load\u003c\/td\u003e\n\u003ctd\u003e300 kg\u003c\/td\u003e\n\u003ctd\u003e300 kg\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003e\u003cstrong\u003eTotal Weight\u003c\/strong\u003e\u003c\/td\u003e\n\u003ctd\u003e\u003cstrong\u003e890 kg\u003c\/strong\u003e\u003c\/td\u003e\n\u003ctd\u003e\u003cstrong\u003e1,000 kg\u003c\/strong\u003e\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003eOperational History \u0026amp; Export\u003c\/h3\u003e\n\u003cp\u003eThe Aéronautique Militaire absorbed approximately 1,000 C.59s as its standard intermediate trainer; French Naval Aviation operated a further batch. Around 800 aircraft were exported to Argentina, Brazil, Bulgaria, China, Finland, Portugal, and Turkey. A modified variant, the \u003cstrong\u003eC.59\/2\u003c\/strong\u003e, used a 230 hp Lorraine 7Ma engine and directly inspired the subsequent \u003cstrong\u003eCaudron C.60\u003c\/strong\u003e. Surviving aircraft saw operational use during the Spanish Civil War.\u003c\/p\u003e\n\n\u003chr\u003e\n\n\u003cp\u003e\u003cem\u003eThis is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorised distributor.\u003c\/em\u003e\u003c\/p\u003e\n\u003cp\u003e\u003cem\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/em\u003e\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53697837629787,"sku":null,"price":30.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/banner-4-french-roundel-tarmac-shot.png?v=1785513113"}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/collections\/french-aviation-collection-banner.png?v=1782659256","url":"https:\/\/onlineaviationlibrary.com\/collections\/french-aviation-collection.oembed?page=2","provider":"Online Aviation Library","version":"1.0","type":"link"}