{"title":"Dutch Aviation","description":"\u003cp\u003eA primary-source archival collection of technical documentation from the Netherlands' major aircraft manufacturers — Fokker (Royal Dutch Aircraft Factory), Koolhoven (N.V. Koolhoven Vliegtuigen), Pander \u0026amp; Son (H. Pander \u0026amp; Zonen), Maeve Aerospace, and Nationale Vliegtuig Industrie (NVI).\u003c\/p\u003e\u003cp\u003eThis Living Collection spans one of Europe's most distinguished aviation traditions — from the legendary Fokker Triplane and Fokker D.VII of the First World War to the Fokker F27 Friendship and F28 Fellowship of the jet age. Documents are presented as archival, static-copy editions fixed at their original publication dates, intended for historical reference, flight simulation, museum restoration, and educational use only.\u003c\/p\u003e\u003cp\u003eNot approved for active airworthiness maintenance under FAA 14 CFR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","products":[{"product_id":"fokker-f-27-friendship-aircraft-aeroplane-manuals-collection-download","title":"Fokker F-27 Friendship Aircraft Manuals Collection - Digital Download","description":"\u003ch2\u003eFokker F-27 Friendship — Primary-Source Technical Documentation Collection\u003c\/h2\u003e\n\n\u003cp\u003eThe Fokker F-27 Friendship is one of the most thoroughly documented regional transport aircraft of the post-war era. This collection brings together primary-source factory manuals, engineering studies, operator documentation, and aerodynamic research reports issued directly by Fokker, its licensed operators, and the Royal Netherlands Air Force — spanning the aircraft's full production and service life from the 1950s through the late 1990s.\u003c\/p\u003e\n\n\u003cp\u003eType Certificate holder: \u003cstrong\u003eFokker Services B.V., Schiphol, Netherlands\u003c\/strong\u003e — regulatory baseline: \u003cstrong\u003eEASA Type Certificate Data Sheet No. EASA.A.036\u003c\/strong\u003e.\u003c\/p\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003eDocument Manifest — 25 Unique Primary-Source Documents\u003c\/h3\u003e\n\n\u003ch4\u003eFlight Manuals \u0026amp; Pilot Documentation\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eAirplane Flight Manual (AFM) Vol. 1\u003c\/strong\u003e — Fokker B.V., Schiphol, Netherlands. Normal, abnormal, and emergency procedures; performance tables; operating limitations.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAirplane Flight Manual (AFM) Vol. 2\u003c\/strong\u003e — Fokker B.V., Schiphol, Netherlands. Supplementary performance data and systems amplification.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAirplane Flight Manual (AFM) Vol. 3\u003c\/strong\u003e — Fokker B.V., Schiphol, Netherlands. Weight and balance, loading, and configuration data.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFlight Manual — Model F27 Maritime Aircraft\u003c\/strong\u003e — Fokker B.V. \/ Royal Netherlands Air Force. Issued 15 September 1981; last revised 01 September 1998. Maritime patrol variant procedures and systems.\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003ch4\u003eMaintenance Manuals\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eF.27 Maintenance Manual Vol. 1\u003c\/strong\u003e — Fokker B.V. (burgundy binder series). General airframe maintenance practices and structural inspection procedures.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eF.27 Maintenance Manual Vol. 2\u003c\/strong\u003e — Fokker B.V. (burgundy binder series). Powerplant and fuel systems maintenance.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eF.27 Maintenance Manual Vol. 3\u003c\/strong\u003e — Fokker B.V. (burgundy binder series). Hydraulic, pneumatic, and landing gear systems.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eF.27 Maintenance Manual Vol. 4\u003c\/strong\u003e — Fokker B.V. (burgundy binder series). Electrical, avionics, and instrument systems.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eF.27 Maintenance Manual Vol. 5\u003c\/strong\u003e — Fokker B.V. (burgundy binder series). Continued systems coverage and inspection schedules.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eF.27 Maintenance Manual — Chapter 27: Flight Controls\u003c\/strong\u003e — Fokker B.V. Standalone chapter, November 1986. ATA 27 full coverage: ailerons, rudder, elevator, trim tabs, control wheels, torque tubes, crosswheel, differential sector, spring tab balance unit, tension regulators, and all associated maintenance practices.\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003ch4\u003eIllustrated Parts Catalog\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eFokker F-27 Illustrated Parts Catalog (IPC)\u003c\/strong\u003e — Fokker B.V. List of Effective Pages dated 28 October 1981 (previous revision: 02 September 1977). Covers ATA Chapters 11, 21–38, 52–57, 61, 71–83, 91. Full component identification and part number data.\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003ch4\u003eAirframe Engineers Training Manuals\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eF.27 Airframe Engineers Training Manual Vol. 1\u003c\/strong\u003e — Royal Netherlands Aircraft Factories Fokker, Schiphol. Structural systems, metal bonding (Redux), and airframe fundamentals.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eF.27 Airframe Engineers Training Manual Vol. 2\u003c\/strong\u003e — Royal Netherlands Aircraft Factories Fokker, Schiphol-Amsterdam. Advanced structural topics and systems integration.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eF.27 Airframe Engineers Training Manual Vol. 3\u003c\/strong\u003e — Royal Netherlands Aircraft Factories Fokker, Schiphol-Amsterdam. Continued systems and maintenance engineering training.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFokker F27 Friendship Training Manual\u003c\/strong\u003e — Fokker B.V. (brown cover edition). Consolidated systems training reference for ground engineers and technicians.\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003ch4\u003eGround Handling \u0026amp; Servicing\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eGround Handling and Servicing Data\u003c\/strong\u003e — Fokker B.V., Schiphol-Oost. Towing, jacking, fuelling, servicing procedures, and ground support equipment specifications.\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003ch4\u003ePerformance \u0026amp; Description\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eF.27 Friendship Description \u0026amp; Performance\u003c\/strong\u003e — Royal Netherlands Aircraft Factories Fokker, Schiphol-Zuid. Aerodynamic configuration, performance tables, and variant comparison data.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eEngineers Pocket Book — F.27\u003c\/strong\u003e — Fokker B.V., Schiphol. Compact quick-reference data for weights, speeds, systems limits, and servicing parameters.\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003ch4\u003eEngineering Research Reports\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eFlutter and Vibration Analysis of the F.27\u003c\/strong\u003e — Fokker Internal Engineering Report X-27-363. Aeroelastic analysis, flutter margins, and vibration test data.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eF27 Mk 500 RF Pylon Configuration Analysis\u003c\/strong\u003e — Fokker Internal Engineering Report G27-400-I. Structural and aerodynamic analysis of the RF reconnaissance pylon installation.\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003ch4\u003eMilitary Variant Documentation\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eFokker F.27 M Military Transport — Design Summary\u003c\/strong\u003e — Royal Netherlands Aircraft Factories Fokker. Classified original issue; now declassified archival copy. Structural, systems, and performance summary for the military transport variant.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eLe Cargo Militaire F27\u003c\/strong\u003e — Fokker, 1968. French-language military cargo brochure. Cargo loading configurations, military payload data, and operational flexibility documentation.\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003ch4\u003eSpecialist Variant Documentation\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eFokker F27 RFV — Operations on Unsurfaced Runways\u003c\/strong\u003e — Fokker B.V., 1979. Engineering and operational data for the Rough Field Version: minimum bearing strength requirements, tyre pressure data, and unprepared strip performance.\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003ch4\u003eOperator Documentation\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eB.A.C. Express Airlines Operations Manual — Part B2: Aeroplane Operating Matters F27\u003c\/strong\u003e — Record of Amendments current to AL14, April 2004. Airline-specific operating procedures, performance engineering data, and crew operating standards.\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003eEngineering \u0026amp; Aerodynamic Highlights\u003c\/h3\u003e\n\n\u003cp\u003e\u003cstrong\u003eAirframe \u0026amp; Aerodynamics:\u003c\/strong\u003e High-wing configuration with a 29.00 m wingspan and 70 m² total wing area. Fokker pioneered metal-to-metal Redux bonding, replacing traditional rivets — yielding a 15% lighter structure with superior fatigue life. Dual-slotted trailing-edge flaps (inboard and outboard). Wind tunnel research at 1:20 scale confirmed propeller slipstream effects on lift and directional control over the high-wing structure.\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003ePowerplant:\u003c\/strong\u003e Twin Rolls-Royce Dart turboprops (Mk 528, 532-7R, or 536 \/ RDa.7 series), delivering 2,050–2,250 equivalent shaft horsepower (ehp) per engine. Two-stage centrifugal compressor, pressure ratio ~5.62:1. Dowty Rotol four-blade constant-speed fully feathering propellers. Hydraulic Flight Fine Pitch Stop (FFPS) system: minimum in-flight blade pitch 20°; Ground Fine Pitch (GFP) 0°–20° for aerodynamic braking on landing.\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003eHandling:\u003c\/strong\u003e Highly stable lateral and longitudinal platform. Mechanical flight controls with balance tabs — no hydraulic boosting required. Automatic propeller feathering system for single-engine safety within certified V\u003csub\u003eMC\u003c\/sub\u003e limits.\u003c\/p\u003e\n\n\u003ch3\u003ePerformance Reference Data\u003c\/h3\u003e\n\n\u003ctable\u003e\n\u003cthead\u003e\u003ctr\u003e\n\u003cth\u003eParameter\u003c\/th\u003e\n\u003cth\u003eF27-200\u003c\/th\u003e\n\u003cth\u003eF27-400\u003c\/th\u003e\n\u003cth\u003eF27-500\u003c\/th\u003e\n\u003c\/tr\u003e\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eMTOW\u003c\/td\u003e\n\u003ctd\u003e20,410 kg\u003c\/td\u003e\n\u003ctd\u003e19,773 kg\u003c\/td\u003e\n\u003ctd\u003e20,410 kg\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax Passengers\u003c\/td\u003e\n\u003ctd\u003e44\u003c\/td\u003e\n\u003ctd\u003e44–48\u003c\/td\u003e\n\u003ctd\u003e44–52\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eCruise Speed\u003c\/td\u003e\n\u003ctd\u003e509 km\/h (275 kt)\u003c\/td\u003e\n\u003ctd\u003e460–480 km\/h\u003c\/td\u003e\n\u003ctd\u003e460–480 km\/h\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eService Ceiling\u003c\/td\u003e\n\u003ctd\u003e8,992 m (29,500 ft)\u003c\/td\u003e\n\u003ctd\u003e7,620–8,475 m\u003c\/td\u003e\n\u003ctd\u003e8,990 m (29,500 ft)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eFerry Range\u003c\/td\u003e\n\u003ctd\u003e~1,800 km\u003c\/td\u003e\n\u003ctd\u003e~1,500 km\u003c\/td\u003e\n\u003ctd\u003e~991 km\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003eIdeal For\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003eAviation historians and archival researchers\u003c\/li\u003e\n\u003cli\u003eAircraft restorers and museum conservators\u003c\/li\u003e\n\u003cli\u003eFlight simulation developers and enthusiasts\u003c\/li\u003e\n\u003cli\u003eScale modelers requiring primary-source technical references\u003c\/li\u003e\n\u003cli\u003eEngineering students studying post-war European aircraft design\u003c\/li\u003e\n\u003cli\u003eCollectors of primary-source aviation documentation\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003chr\u003e\n\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\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\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":51707129200987,"sku":null,"price":95.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/fokker-f-27-klm-heritage-banner.png?v=1784368761"},{"product_id":"fokker-50-f27-mk50-primary-technical-documentation-collection","title":"Fokker 50 (F-27 Mk 50) — Primary Technical Documentation Collection","description":"\u003ch3\u003eFokker 50 (F-27 Mk 50) — Primary Technical Documentation Collection\u003c\/h3\u003e\n\u003cp\u003eThe Fokker 50 stands as one of the most technically refined regional turboprops ever produced — a direct aerodynamic evolution of the legendary Fokker F27 Friendship, re-engineered from the ground up with composite structures, advanced propulsion, and a hybrid mechanical-electronic flight control suite. This collection brings together the primary-source documentation that defined, certified, and sustained the F-50 throughout its operational life under EASA and FAA oversight.\u003c\/p\u003e\n\u003cp\u003eManaged and issued by \u003cstrong\u003eFokker Services B.V. \/ Fokker Services Group\u003c\/strong\u003e, these documents represent the authoritative engineering and operational record of the aircraft — from its aerodynamic design philosophy to its final structural aging inspections.\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eWhat This Collection Contains\u003c\/h3\u003e\n\u003ch4\u003e✈ Aircraft Operating Manual (AOM) — Fokker 50\u003c\/h4\u003e\n\u003cp\u003eThe definitive operational reference for flight crews. Covers normal and abnormal procedures, performance data, weight and balance, and system descriptions. Includes the full limitations chapter with certified mass data: MTOW 20,820 kg · MLW 19,730 kg · MZFW 18,600 kg · Ramp 20,865 kg. Service ceiling 25,000 ft · Max pax 62 · Crew minimum: 2 pilots.\u003c\/p\u003e\n\u003ch4\u003e✈ Illustrated Parts Catalog (IPC) — Fokker 50\u003c\/h4\u003e\n\u003cp\u003eFactory-issued parts breakdown covering airframe, systems, and powerplant components. Essential reference for maintenance planning, parts sourcing, and restoration work on surviving airframes.\u003c\/p\u003e\n\u003ch4\u003e✈ Fokker 50 Technical Description (1985)\u003c\/h4\u003e\n\u003cp\u003eThe original factory technical description issued at program launch — a landmark primary-source document capturing the design intent, structural philosophy, and systems architecture of the F-50 as conceived by Fokker's engineering teams in Amsterdam.\u003c\/p\u003e\n\u003ch4\u003e✈ Fokker 50 Aircraft Overview (1989 Edition)\u003c\/h4\u003e\n\u003cp\u003eUpdated overview document reflecting the mature production standard, incorporating lessons from early operator experience and design refinements across the airframe and propulsion system.\u003c\/p\u003e\n\u003ch4\u003e✈ airBaltic Operations Manual Part B (OMB) — Fokker 50\u003c\/h4\u003e\n\u003cp\u003eOperator-specific performance and procedures manual from airBaltic, one of the F-50's final European operators. Provides real-world operational context including route performance data, fuel planning, and crew procedures as applied in line service.\u003c\/p\u003e\n\u003ch4\u003e✈ Fokker 50\/60 Non-Destructive Testing (NDT) Manual\u003c\/h4\u003e\n\u003cp\u003eStandardized inspection procedures covering eddy-current and ultrasonic inspection cycles for fuselage frames, skin panels, and structural joints. Defines the continuous airworthiness inspection framework for aging F-50 operators.\u003c\/p\u003e\n\u003ch4\u003e✈ Fokker Services Group (FSG) — Fokker 50 Technical Support Documentation\u003c\/h4\u003e\n\u003cp\u003ePost-production engineering support documentation from Fokker Services Group, covering continued airworthiness management, retrofit compliance, and operator technical support packages.\u003c\/p\u003e\n\u003ch4\u003e✈ APU System Manual\u003c\/h4\u003e\n\u003cp\u003eAuxiliary Power Unit documentation covering ground power generation, pneumatic start capability, and APU fuel system integration with the main fuel circuit.\u003c\/p\u003e\n\u003ch4\u003e✈ Bleed Air System Manual\u003c\/h4\u003e\n\u003cp\u003eEngine bleed-air architecture documentation covering pressurization, air conditioning, wing and engine anti-ice supply, and hydraulic tank pressurization via bleed-air feed.\u003c\/p\u003e\n\u003ch4\u003e✈ Electrical System Manual\u003c\/h4\u003e\n\u003cp\u003ePrimary and secondary electrical power generation, distribution, and protection systems. Covers AC\/DC bus architecture, generator control units, and emergency power configuration.\u003c\/p\u003e\n\u003ch4\u003e✈ Flight Navigation Instruments Manual\u003c\/h4\u003e\n\u003cp\u003eEFIS suite documentation including Symbol Generator Units, Primary Flight Display (PFD), Navigation Display (ND), and integration with the Air Data Computer (ADC) and Inertial Reference System.\u003c\/p\u003e\n\u003ch4\u003e✈ Fuel System Manual\u003c\/h4\u003e\n\u003cp\u003eWing tank architecture, fuel pump configuration, crossfeed system, APU fuel supply, and pressure refueling procedures. Includes bonding and grounding provisions for safe pressure refueling operations.\u003c\/p\u003e\n\u003ch4\u003e✈ Ice and Rain Protection Manual\u003c\/h4\u003e\n\u003cp\u003ePneumatic de-icing boot system for wing leading edges and horizontal stabilizer, engine intake anti-ice, windshield heating, and probe heating systems.\u003c\/p\u003e\n\u003ch4\u003e✈ Integrated Alerting Unit (IAU) Manual\u003c\/h4\u003e\n\u003cp\u003eCentralized crew alerting system documentation covering Level 1 (Warning), Level 2 (Caution), and Level 3 (Advisory) alert logic, master warning\/caution annunciation, and system inhibit logic during critical flight phases.\u003c\/p\u003e\n\u003ch4\u003e✈ Landing Gear System Manual\u003c\/h4\u003e\n\u003cp\u003eHydraulic and alternate (gravity) extension\/retraction procedures, nose gear and main gear door sequencing, selector lock logic, and LOCK OVERRIDE procedures. Includes nose wheel steering and brake system integration.\u003c\/p\u003e\n\u003ch4\u003e✈ Landing Gear \u0026amp; Flaps \/ Flight Controls Manual\u003c\/h4\u003e\n\u003cp\u003eComprehensive flight control documentation: ailerons (spring and balance tabs), rudder (trim and balance tabs), elevator (trim tab, EFCS), flap system, and augmented pitch stability systems — Elevator Feel Control System (EFCS) and Longitudinal Stability Augmentation System (LSAS). Control surface deflection limits: elevator ±25°\/22°, rudder ±20°.\u003c\/p\u003e\n\u003ch4\u003e✈ Hydraulics System Manual\u003c\/h4\u003e\n\u003cp\u003eSingle hydraulic system at 3,000 psi nominal pressure. Two engine-driven pumps (one per engine), electrically driven backup pump for ground maintenance, fire shut-off valves, accumulator, and alternate gravity-extension provisions for landing gear and flaps.\u003c\/p\u003e\n\u003ch4\u003e✈ Limitations Manual\u003c\/h4\u003e\n\u003cp\u003eCertified operational limits: max operating altitude 25,000 ft · max take-off\/landing pressure altitude 8,000 ft · temperature envelope ISA +35°C to −54°C · runway slope ±2% · manoeuvring loads +2.5G\/−1.0G (flaps up), +2.0G\/0.0G (flaps down).\u003c\/p\u003e\n\u003ch4\u003e✈ Service Bulletins — Selected Issued Documents\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eSBF50-28-040 Rev.1\u003c\/strong\u003e (Fuel — General, Nov 2014): Installation of additional bonding provisions and bonding wire on the pressure refueling line inside the RH main tank. EASA-approved Electronic Sign-Off (E.S.O.) procedure.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSBF50-53-063\u003c\/strong\u003e (Fuselage — Forward Fuselage, Mar 2023): One-time inspection of skin lap joints at Stringers 117 and 141 between Station 4550 and 6675. RESTRICTED classification. Critical aging aircraft structural integrity bulletin.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003ePropulsion — Pratt \u0026amp; Whitney Canada PW125B \/ PW127B\u003c\/h3\u003e\n\u003cp\u003eThe F-50 is powered by twin PW125B engines rated at 2,500 shp (1,864 kW) each, or optional PW127B units at 2,750 shp (2,050 kW). Power management is handled by dual Electronic Engine Control (EEC) units operating a unique single-lever system that coordinates propeller pitch and engine power simultaneously via six-bladed Dowty Rotol composite propellers. The flight-idle stop system and mechanical ground-idle locks are documented in the engine technical training papers included in this collection.\u003c\/p\u003e\n\u003ch3\u003eAerodynamic \u0026amp; Structural Design Notes\u003c\/h3\u003e\n\u003cp\u003eThe F-50 incorporates SABCA-designed high-aspect-ratio wings with upturned Fowler flaps and aerodynamic nacelles. Composite materials (aramid and carbon fiber) are used in fairings, trailing edges, and the dorsal fin. The horizontal stabilizer uses a NACA 63A-014 MOD airfoil; the vertical stabilizer a NACA 63A-015 MOD section. Fuji Heavy Industries supplied the rudders and elevators, optimized for steep, low-speed regional approaches.\u003c\/p\u003e\n\u003ch3\u003ePerformance Reference Data\u003c\/h3\u003e\n\u003ctable\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003cth\u003eParameter\u003c\/th\u003e\n\u003cth\u003eValue\u003c\/th\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax Takeoff Weight (MTOW)\u003c\/td\u003e\n\u003ctd\u003e20,820 kg (45,900 lbs)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eCruising Speed\u003c\/td\u003e\n\u003ctd\u003e526 km\/h (284 kt TAS)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eTakeoff Field Length\u003c\/td\u003e\n\u003ctd\u003e1,100 – 1,364 m\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eService Ceiling\u003c\/td\u003e\n\u003ctd\u003e7,620 m (25,000 ft)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Range\u003c\/td\u003e\n\u003ctd\u003e2,632 km (1,421 NM)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eV₂ (Takeoff Safety Speed)\u003c\/td\u003e\n\u003ctd\u003e120 knots\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax Passengers\u003c\/td\u003e\n\u003ctd\u003e62\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\n\u003chr\u003e\n\u003ch3\u003eNature of This Collection\u003c\/h3\u003e\n\u003cp\u003eThis is a \u003cstrong\u003eliving collection\u003c\/strong\u003e — documents are added as new primary-source material is authenticated and processed. Purchasers receive free lifetime updates as the collection expands.\u003c\/p\u003e\n\u003cp\u003eAll documents in this collection are archival, static-copy editions fixed at their original publication dates. 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⚠️ \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 collection does not satisfy that requirement.\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":53616930390363,"sku":null,"price":45.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/fokker-50-banner-klm.png?v=1784364481"},{"product_id":"fokker-f28-fellowship-manuals-collection","title":"Fokker F28 Fellowship — Manuals Collection","description":"\u003ch2\u003eFokker F28 Fellowship — Manuals Collection\u003c\/h2\u003e\n\n\u003cp\u003eThe \u003cstrong\u003eFokker F28 Fellowship\u003c\/strong\u003e was the Netherlands' first purpose-designed jet airliner — a twin rear-fuselage turbofan regional transport that entered service in 1969 and remained in production through 1987, with 241 aircraft delivered across four principal marks. Designed and manufactured by Fokker B.V. at Schiphol-Oost, the F28 established Dutch aerospace engineering on the world stage and served with over 50 operators across six continents.\u003c\/p\u003e\n\n\u003cp\u003eThis living collection assembles the primary-source technical documentation issued by \u003cstrong\u003eFokker B.V.\u003c\/strong\u003e and \u003cstrong\u003eFokker-VFW International B.V.\u003c\/strong\u003e across the operational life of the Fellowship series — from initial certification through the extended Mk 3000 and Mk 4000 variants. Every document is an archival, static-copy edition fixed at its original publication date, presented without alteration or editorial interpolation.\u003c\/p\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003eDocument Manifest\u003c\/h3\u003e\n\n\u003cp\u003e\u003cstrong\u003e1. F28 Engineers Guide\u003c\/strong\u003e\u003cbr\u003e\nPublisher: Fokker-VFW International B.V., Schiphol-Oost, The Netherlands\u003cbr\u003e\nScope: Comprehensive engineering reference covering airframe systems, structural philosophy, powerplant integration, and ground support interface data for maintenance engineers and technical representatives.\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003e2. F28 Flight Handbook — Including R.L.D. Approved Flight Manual\u003c\/strong\u003e\u003cbr\u003e\nPublisher: Fokker B.V., Schiphol, The Netherlands\u003cbr\u003e\nScope: Pilot operating procedures, performance data, systems descriptions, and the R.L.D. (Rijksluchtvaartdienst) approved flight manual supplement. Covers normal, abnormal, and emergency procedures for the Fellowship series.\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003e3. F28 MK 3000 and 4000 — Ground Handling and Servicing Data\u003c\/strong\u003e\u003cbr\u003e\nPublisher: Fokker-VFW International B.V., Schiphol-Oost, The Netherlands\u003cbr\u003e\nScope: Ground servicing procedures, fuelling, towing, jacking, mooring, and ramp handling specifications specific to the stretched Mk 3000 and Mk 4000 variants.\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003e4. Fokker F28 Structural Repair Manual (SRM)\u003c\/strong\u003e\u003cbr\u003e\nDocument Reference: 6670E | ATA Chapter Structure: 51–57\u003cbr\u003e\nRevision: August 1988\u003cbr\u003e\nScope: Full structural repair data organized by ATA chapter — Fuselage (Ch. 53), Doors (Ch. 52), Windows (Ch. 56), Stabilizers (Ch. 55), Nacelle-Stubwing (Ch. 54), Wings (Ch. 57). Includes the F28 Chapter Arrangement index illustration (Fig. 1, Ref. 28-51-4129).\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003e5. Super F28 — Design Features\u003c\/strong\u003e\u003cbr\u003e\nPublisher: Fokker, Schiphol-Oost, Netherlands | Date: January 1979\u003cbr\u003e\nScope: Engineering design features document for the Super F28 development programme — covering aerodynamic refinements, structural upgrades, and performance improvements proposed for the extended-range and higher-capacity variants.\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003e6. Fokker F28 Fellowship Training Manual\u003c\/strong\u003e\u003cbr\u003e\nPublisher: Fokker B.V.\u003cbr\u003e\nScope: Systems training manual for flight crew and technical personnel. Covers aircraft systems in depth for type rating and recurrent training purposes across the Fellowship series.\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003e7. Fokker F28 Brochure (1979)\u003c\/strong\u003e\u003cbr\u003e\nPublisher: Fokker-VFW International B.V., Schiphol-Oost, The Netherlands\u003cbr\u003e\nScope: Original manufacturer's commercial brochure documenting the F28 Fellowship programme as of 1979 — performance summaries, variant overview, and operational characteristics.\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003e8. Fokker F28 Brochure (General Edition)\u003c\/strong\u003e\u003cbr\u003e\nPublisher: Fokker B.V., Schiphol, The Netherlands\u003cbr\u003e\nScope: General commercial and technical overview brochure for the F28 Fellowship series.\u003c\/p\u003e\n\n\u003cp\u003e\u003cstrong\u003e9. Fokker F28 Brochure (1980)\u003c\/strong\u003e\u003cbr\u003e\nPublisher: Fokker-VFW International B.V., Schiphol-Oost, The Netherlands\u003cbr\u003e\nScope: Updated manufacturer's brochure reflecting the 1980 production status, including Mk 3000 and Mk 4000 variant data.\u003c\/p\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003eTechnical Reference Data — Fokker F28 Fellowship Series\u003c\/h3\u003e\n\n\u003ch4\u003eAerodynamic Design \u0026amp; Lift Profile\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eWing Sweep:\u003c\/strong\u003e 16° quarter-chord sweep\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAspect Ratio:\u003c\/strong\u003e 7.3:1\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDesign Cruise Altitude:\u003c\/strong\u003e 25,000 ft (initial variants)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDesign Lift Coefficient:\u003c\/strong\u003e C\u003csub\u003eL\u003c\/sub\u003e = 0.20 at Mach 0.73 (Mk 1000\/2000); C\u003csub\u003eL\u003c\/sub\u003e ≈ 0.45 at Mach 0.73 (Mk 4000 with wing modifications)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMaximum Ceiling:\u003c\/strong\u003e 35,000 ft (Mk 4000)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSpeed Brake System:\u003c\/strong\u003e Split-tail cone speed brake assembly\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003ch4\u003ePowerplant\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eEngine Type:\u003c\/strong\u003e Rolls-Royce RB.183 Spey — twin-shaft bypass turbofan, rear-fuselage mounted\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTakeoff Thrust:\u003c\/strong\u003e 9,850 lbf (43.9 kN) per engine — Spey Mk 555-15\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eUpgraded Configuration:\u003c\/strong\u003e Spey Mk 555-15N per Fokker Service Bulletin No. 71-9\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFuel Compliance:\u003c\/strong\u003e Rolls-Royce Operating Instructions Document No. F-Sp2-F\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003ch4\u003eHandling \u0026amp; Stability\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eTail Configuration:\u003c\/strong\u003e T-tail — single vertical stabilizer with high-mounted horizontal stabilizer\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCruise Pitch Attitude (FL110):\u003c\/strong\u003e 1° – 1.5° nose-up\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNominal Pitch Trim:\u003c\/strong\u003e 0.1°\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFlight Controls:\u003c\/strong\u003e Mechanical push-pull linkages (secondary surfaces); hydraulic boost (primary axes)\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003ch4\u003ePerformance Data by Variant\u003c\/h4\u003e\n\n\u003ctable\u003e\n\u003cthead\u003e\u003ctr\u003e\n\u003cth\u003eParameter\u003c\/th\u003e\n\u003cth\u003eMk 1000\u003c\/th\u003e\n\u003cth\u003eMk 2000\u003c\/th\u003e\n\u003cth\u003eMk 4000\u003c\/th\u003e\n\u003c\/tr\u003e\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax Takeoff Weight (MTOW)\u003c\/td\u003e\n\u003ctd\u003e29,485 kg (65,000 lb)\u003c\/td\u003e\n\u003ctd\u003e29,480 kg (65,000 lb)\u003c\/td\u003e\n\u003ctd\u003e33,110 kg (73,000 lb)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eOperating Empty Weight (OEW)\u003c\/td\u003e\n\u003ctd\u003e16,144 kg (35,517 lb)\u003c\/td\u003e\n\u003ctd\u003e16,707 kg (36,953 lb)\u003c\/td\u003e\n\u003ctd\u003e17,645 kg (38,900 lb)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Cruise Speed\u003c\/td\u003e\n\u003ctd\u003e848 km\/h (458 kn)\u003c\/td\u003e\n\u003ctd\u003e848 km\/h (458 kn)\u003c\/td\u003e\n\u003ctd\u003e844 km\/h (455 kn)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eTakeoff Field Length (ISA, SL)\u003c\/td\u003e\n\u003ctd\u003e1,676 m (5,500 ft)\u003c\/td\u003e\n\u003ctd\u003e1,676 m (5,500 ft)\u003c\/td\u003e\n\u003ctd\u003e1,680 m (5,510 ft)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Passenger Seating\u003c\/td\u003e\n\u003ctd\u003e65\u003c\/td\u003e\n\u003ctd\u003e79\u003c\/td\u003e\n\u003ctd\u003e85\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\n\n\u003ch4\u003eEngineering \u0026amp; Service Bulletin Notes\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eRegulatory Authority:\u003c\/strong\u003e Fokker Services B.V. — EASA Type Certificate Data Sheet A.037\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eStructural Compliance:\u003c\/strong\u003e Fatigue damage tracking per flight via FOQA metrics; validated against full-scale NASA crash modelling data\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDe-icing:\u003c\/strong\u003e C\/FIMS fluid monitoring systems modifying baseline wing leading-edge bleed heating assemblies\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003eNature of the Collection\u003c\/h3\u003e\n\u003cp\u003eAll documents in this collection are archival, static-copy editions fixed at their original publication dates. They are presented as issued by Fokker B.V. and Fokker-VFW International B.V. without editorial modification. This collection is a living archive — additional documents will be added as they are processed and verified, at no additional cost to existing purchasers.\u003c\/p\u003e\n\n\u003ch3\u003eOur Editorial Philosophy\u003c\/h3\u003e\n\u003cp\u003eOnline Aviation Library publishes primary-source aviation documentation for researchers, historians, restorers, flight simulation developers, and serious collectors. We do not simplify, summarize, or repackage. Every document is presented as the manufacturer issued it — with full provenance, original pagination, and unaltered technical content.\u003c\/p\u003e\n\n\u003chr\u003e\n\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\n\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":53617228906843,"sku":null,"price":45.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/fokker-f28-banner-braathens-safe.png?v=1784385293"},{"product_id":"fokker-100-f28-mk-0100-primary-source-documentation-collection","title":"Fokker 100 (F28 Mk 0100) — Primary-Source Documentation Collection","description":"\u003ch3\u003eFokker 100 (F28 Mk 0100) — Primary-Source Documentation Collection\u003c\/h3\u003e\n\u003cp\u003eThis collection assembles the core primary-source documentation for the \u003cstrong\u003eFokker 100 (F28 Mk 0100)\u003c\/strong\u003e, the advanced short-to-medium range twin-turbofan regional jet developed by Fokker Aircraft B.V., Schiphol, The Netherlands. Engineering data, certification details, and operational procedures originate directly from official flight test programs, manufacturer archives, and continuing airworthiness records.\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eDocuments Included in This Collection\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eFokker 100 Aircraft Operating Manual (AOM)\u003c\/strong\u003e — Fokker Aircraft B.V., Schiphol. The definitive operational reference covering normal, abnormal, and emergency procedures for flight crew.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFokker 100 Aircraft Overview (1989)\u003c\/strong\u003e — Fokker Aircraft B.V. Illustrated overview of the aircraft's systems, configuration, and airline service entry, including USAir fleet photography.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFokker 100 Technical Description (1985)\u003c\/strong\u003e — Fokker Aircraft B.V. Pre-certification engineering document covering airframe structure, systems architecture, and powerplant integration.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMDF 100 Detail Type Specification DTS 9200\u003c\/strong\u003e — McDonnell Douglas \/ Fokker joint venture document. Formal type specification for the MDF 100 variant, co-branded McDonnell Douglas and Fokker.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMDF 100 Aircraft Systems\u003c\/strong\u003e — McDonnell Douglas \/ Fokker. Systems-level description of the MDF 100 configuration, covering hydraulics, avionics, environmental control, and propulsion.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMDF 100 Technical Proposal Summary for Delta Air Lines\u003c\/strong\u003e — McDonnell Douglas \/ Fokker. Rare airline-specific technical proposal document prepared for Delta Air Lines fleet evaluation.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAir Europe Fokker 100 Flight Crew Operating Manual — Volume 1\u003c\/strong\u003e — Airline-customized FCOM for Air Europe operations, reflecting operator-specific procedures and limitations.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAir Europe Fokker 100 Flight Crew Operating Manual — Volume 2\u003c\/strong\u003e — Continuation of the Air Europe FCOM, covering systems descriptions and performance data.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eAerodynamic Engineering Notes\u003c\/h3\u003e\n\u003cp\u003eThe Fokker 100 aerodynamic profile derives from an extensively modified evolution of the original F28 Fellowship wing. Key engineering advances include:\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eWing Redesign:\u003c\/strong\u003e Compound chord extension at the root and increased wingspan (28.08 m), dramatically improving aerodynamic efficiency and lift coefficient at high altitudes.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMach Drag Optimization:\u003c\/strong\u003e Root section modifications to delay Mach drag rise during cruise phases.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eWind Tunnel Verification:\u003c\/strong\u003e 25 distinct test campaigns totalling 1,928 test hours, validating stalling characteristics and nacelle-to-pylon airflow interactions.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003ePowerplant — Rolls-Royce Tay\u003c\/h3\u003e\n\u003cp\u003eThe aircraft utilizes rear-mounted, high-bypass twin turbofans designed for high-cycle regional operations:\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eRolls-Royce Tay 620-15:\u003c\/strong\u003e Baseline powerplant — 13,850 lbf static takeoff thrust.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eRolls-Royce Tay 650-15:\u003c\/strong\u003e Upgrade variant — 15,100 lbf takeoff thrust, expanded fan diameter (45 in), enhanced high-pressure turbine blades.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAcoustic Shielding:\u003c\/strong\u003e Rear fuselage installation exploiting wing noise shielding — more than 16 EPNdB below ICAO Stage 3 requirements.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eHandling and Stability\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eControl Surfaces:\u003c\/strong\u003e Dual-acting hydraulic systems controlling elevators, ailerons, and primary\/standby rudder actuators.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eLift Dumpers:\u003c\/strong\u003e Automatic multi-mode ground spoilers with RTO auto-extension above 50 knots on thrust lever retard.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eStability Loading:\u003c\/strong\u003e Longitudinal static stability dictates cargo-first loading, followed by passengers using the window-to-aisle rule, to maintain CG ahead of the aerodynamic center.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003ePerformance Reference 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 Takeoff Weight (MTOW)\u003c\/td\u003e\n\u003ctd\u003e43,000 kg — 45,810 kg (Extended Range)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Operating Speed (V\u003csub\u003eMO\u003c\/sub\u003e \/ M\u003csub\u003eMO\u003c\/sub\u003e)\u003c\/td\u003e\n\u003ctd\u003e320 KIAS \/ Mach 0.77\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eService Ceiling\u003c\/td\u003e\n\u003ctd\u003e37,000 ft\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eTakeoff \/ Landing Field Length\u003c\/td\u003e\n\u003ctd\u003e6,000 ft \/ 4,500 ft\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eOperational Range\u003c\/td\u003e\n\u003ctd\u003e1,320 nm — 1,710 nm (full payload)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\n\u003chr\u003e\n\u003ch3\u003eEngineering Bulletins \u0026amp; Continuing Airworthiness\u003c\/h3\u003e\n\u003cp\u003ePost-production support is managed by Fokker Services Group under \u003cstrong\u003eEASA Type Certificate EASA.A.037\u003c\/strong\u003e:\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eAvionics \u0026amp; RNP:\u003c\/strong\u003e Service Bulletins permit structural and electronic upgrades including RNP 0.3 and ADS-B Out V2 integration.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eStructural Durability:\u003c\/strong\u003e Certified design life of 90,000 landings, supported by fatigue analyses on 2024-T3 aluminum wing\/fuselage joints.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eNature of This Collection\u003c\/h3\u003e\n\u003cp\u003eThese documents represent the primary engineering and operational record of the Fokker 100 program — from pre-certification technical descriptions through airline-customized flight crew manuals and the McDonnell Douglas \/ Fokker MDF 100 joint venture documentation. Together they form an unparalleled archival reference for researchers, historians, restorers, and serious collectors of Dutch aviation heritage.\u003c\/p\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":53617466474843,"sku":null,"price":45.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/fokker-100-promotional-banner-blue-sky.png?v=1784382569"},{"product_id":"fokker-s11-instructor-technical-documentation-collection","title":"Fokker S.11 Instructor — Technical Documentation Collection","description":"\u003ch2\u003eFokker S.11 Instructor — Primary-Source Technical Documentation Collection\u003c\/h2\u003e\n\n\u003cp\u003eThe \u003cstrong\u003eFokker S.11 Instructor\u003c\/strong\u003e completed its maiden flight on \u003cstrong\u003e18 December 1947\u003c\/strong\u003e, entering service as the Royal Netherlands Air Force's foundational post-WWII military pilot trainer. Designed and manufactured by \u003cem\u003eN.V. Koninklijke Nederlandsche Vliegtuigenfabriek Fokker\u003c\/em\u003e, the S.11 became one of the most widely exported Dutch aircraft of the postwar era — adopted as the standard trainer by the Netherlands, Italian, and Israeli Air Forces, with large series orders from Brazil and licence production by Aeronautica Macchi (as the \u003cstrong\u003eMacchi M.416\u003c\/strong\u003e) and Fokker Indústria Aeronautica S.A. The aviation press was unambiguous: \u003cem\u003e“On the whole the Fokker Works have reason to be proud of their new product which should have a useful service life ahead.”\u003c\/em\u003e — Flight \u0026amp; Aeroplane, 1949.\u003c\/p\u003e\n\n\u003cp\u003eThis living archival collection assembles the core technical and operational literature of the S.11 programme, drawn from original factory and RNLAF operator sources. Documents are added as they are processed; purchasers receive all future additions at no extra cost.\u003c\/p\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003e📋 Document Manifest — Current Collection (5 Documents)\u003c\/h3\u003e\n\n\u003col\u003e\n\u003cli\u003e\n\u003cstrong\u003eInstructie Handboek — Fokker S.11\u003c\/strong\u003e (Instructor's Handbook)\u003cbr\u003e\nLanguage: Dutch | Publisher: RNLAF \/ Fokker\u003cbr\u003e\nScope: Instructor methodology and ab initio training philosophy; briefing structure; teaching \u0026amp; learning principles; student psychology; type familiarization exercises; pre- and post-flight procedures. Covers S-11, Piper Super Cub, and T-33 (TVO phase in English). Sections: \u003cem\u003eDe Betekenis van dit Handboek — Onderwijzen en Leren — Oefening 1: Familiarisatie op het Type — Oefening 2: Handeling voor en na de Vlucht.\u003c\/em\u003e\n\u003c\/li\u003e\n\n\u003cli\u003e\n\u003cstrong\u003eReparatie-Handboek — Fokker S.11, Deel II C\u0026amp;D\u003c\/strong\u003e (Repair Manual)\u003cbr\u003e\nLanguage: Dutch | Publisher: N.V. Koninklijke Nederlandsche Vliegtuigenfabriek Fokker\u003cbr\u003e\nScope: Structural repair procedures — damage assessment; structural support during repair; bolt and rivet installation standards; corrosion prevention; sheet metal treatment; marking; riveting; pop-rivets; paint scheme (Schilderschema).\n\u003c\/li\u003e\n\n\u003cli\u003e\n\u003cstrong\u003eBeschrijvend Handboek — Fokker S.11\u003c\/strong\u003e (Systems Description Handbook)\u003cbr\u003e\nLanguage: Dutch | Publisher: N.V. Koninklijke Nederlandsche Vliegtuigenfabriek Fokker\u003cbr\u003e\nScope: Hoofdstuk I — Beschrijving: fuel system (Pliocel wing tanks, 80L each \/ 70L usable, 80 octane, 4-position fuel cock, engine-driven + hand + injection pumps); oil system (wet sump, 11.5L, combined pressure\/temp gauge); vacuum system (artificial horizon + directional gyro); electrical system (600W\/12V generator, 35Ah battery); magneto switch (4 positions); dual controls (stick + 3-position adjustable rudder pedals, left stick folds); trim tabs (elevator adjustable in flight; rudder and aileron ground-adjustable only); flaps (3 positions: in \/ 20° \/ 60°); hydraulic toe-pedal brakes (independent L\/R, parking brake); carburettor heat; cockpit heating; ventilation; night lighting; emergency equipment (fire extinguisher, first aid kit). Hoofdstuk II — Procedures \u0026amp; Vlieggegevens: pre-flight walkaround procedure.\n\u003c\/li\u003e\n\n\u003cli\u003e\n\u003cstrong\u003eHandboek S-11.1, Deel I, Sectie 0\u003c\/strong\u003e (General Description \u0026amp; Specifications Handbook)\u003cbr\u003e\nLanguage: Dutch | Publisher: N.V. Koninklijke Nederlandsche Vliegtuigenfabriek Fokker\u003cbr\u003e\nScope: §0.1 General description — construction overview (steel tube fuselage, all-metal wing, fabric control surfaces, levered suspension gear, dual controls, cable-operated surfaces, 12V electrical, optional radio). §0.2 Dimensions — span 11.0 m; length 8.2 m; height 2.4 m; NACA 2417 (root) \/ NACA 2412 (tip); dihedral 6°30'; wing area 18.5 m²; full control deflection data. §0.3 Component specifications — landing gear (C.G.E.A. Olaer, Good Year 7.00×8, 1.9 Ato); tailwheel (Good Year 10”, 1.75 Ato); engine (Lycoming O-435-A, 80 oct, SAE-40\/50); propeller (Frits Diepen FDV 2015, Ø2.15 m); fuel\/oil system specs; brakes (Aeroshellfluid No. 4); fire extinguisher (Essex No. 3, 2.07 kg); electrical (Delco Remy 25A generator, Exide 6 TAS 9B 34Ah battery); full instrument list (Kollsman ASI, VSI, altimeter, Schwien turn indicator, Sperry gyro compass \u0026amp; artificial horizon, Aero Marine combined gauge, Air Associates fuel gauge, Kollsman vacuum gauge, Stewart-Warner ammeter, Kohler injection pump, Kollsman clock); switch panel (Cutler Hammer, 9 switches); Hughes P-11 compass (s\/n 6190–6214 only).\n\u003c\/li\u003e\n\n\u003cli\u003e\n\u003cstrong\u003eFokker Training Aircraft Brochure 1949\u003c\/strong\u003e (S.11 \/ S.12 \/ S.13 Family)\u003cbr\u003e\nLanguage: French \/ English (bilingual parallel columns) | Publisher: N.V. Koninklijke Nederlandsche Vliegtuigenfabriek Fokker | 11 pp.\u003cbr\u003e\nScope: Manufacturer's official 1949 sales and technical brochure for the complete Fokker trainer family. Covers: S.11 Instructor (tailwheel primary trainer); S.12 (nosewheel variant, identical airframe and performance, maximum spare parts commonality); S.13 (twin-engine crew trainer, 2× P\u0026amp;W Wasp 600 hp, tricycle gear, 4–6 occupants, built to British A.P. 970 spec). Includes: design philosophy; full bilingual technical description; confirmed operator nations; licence production details (Macchi M.416 \/ Fokker Indústria Aeronautica S.A.); factory series production photographs; instrument panel photograph; cutaway structural drawing; and the definitive \u003cstrong\u003ethree-engine variant Specification \u0026amp; Performances comparison table\u003c\/strong\u003e (Lycoming O-435-A \/ Cirrus Bombardier \/ Mathis G.8.R.).\n\u003c\/li\u003e\n\u003c\/ol\u003e\n\n\u003cp\u003e\u003cem\u003e🔄 Forthcoming additions: Illustrated Parts Catalog (IPC), Maintenance Manual (MM) — Italian translation, Overhaul Manual, Engine Manual (Lycoming O-435-A). Price will increase as the collection grows — early purchasers are locked in at the founding price.\u003c\/em\u003e\u003c\/p\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003e📊 Specification \u0026amp; Performances — Three Engine Variants (Factory Brochure Data, 1949)\u003c\/h3\u003e\n\n\u003ctable\u003e\n\u003cthead\u003e\u003ctr\u003e\n\u003cth\u003eParameter\u003c\/th\u003e\n\u003cth\u003eLycoming O-435-A (Aeromatic)\u003c\/th\u003e\n\u003cth\u003eCirrus Bombardier (Rotol)\u003c\/th\u003e\n\u003cth\u003eMathis G.8.R. (Fixed Wood)\u003c\/th\u003e\n\u003c\/tr\u003e\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax Power (SL)\u003c\/td\u003e\n\u003ctd\u003e190 hp\u003c\/td\u003e\n\u003ctd\u003e180 hp\u003c\/td\u003e\n\u003ctd\u003e180 hp\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eCruise Power (1,000 m)\u003c\/td\u003e\n\u003ctd\u003e110 hp\u003c\/td\u003e\n\u003ctd\u003e127 hp\u003c\/td\u003e\n\u003ctd\u003e125 hp\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eEmpty Weight\u003c\/td\u003e\n\u003ctd\u003e795 kg \/ 1,750 lb\u003c\/td\u003e\n\u003ctd\u003e790 kg \/ 1,735 lb\u003c\/td\u003e\n\u003ctd\u003e785 kg \/ 1,730 lb\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMTOW\u003c\/td\u003e\n\u003ctd\u003e1,085 kg \/ 2,395 lb\u003c\/td\u003e\n\u003ctd\u003e1,090 kg \/ 2,400 lb\u003c\/td\u003e\n\u003ctd\u003e1,085 kg \/ 2,395 lb\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax Speed (SL)\u003c\/td\u003e\n\u003ctd\u003e215 km\/h \/ 134 mph\u003c\/td\u003e\n\u003ctd\u003e215 km\/h \/ 134 mph\u003c\/td\u003e\n\u003ctd\u003e210 km\/h \/ 131 mph\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eCruise Speed (1,000 m)\u003c\/td\u003e\n\u003ctd\u003e170 km\/h \/ 106 mph\u003c\/td\u003e\n\u003ctd\u003e190 km\/h \/ 118 mph\u003c\/td\u003e\n\u003ctd\u003e180 km\/h \/ 112 mph\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMin Speed\u003c\/td\u003e\n\u003ctd\u003e98 km\/h \/ 61 mph\u003c\/td\u003e\n\u003ctd\u003e98 km\/h \/ 61 mph\u003c\/td\u003e\n\u003ctd\u003e98 km\/h \/ 61 mph\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eRate of Climb (SL)\u003c\/td\u003e\n\u003ctd\u003e4.6 m\/s \/ 995 ft\/min\u003c\/td\u003e\n\u003ctd\u003e3.7 m\/s \/ 730 ft\/min\u003c\/td\u003e\n\u003ctd\u003e3.6 m\/s \/ 710 ft\/min\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eClimb to 1,000 m\u003c\/td\u003e\n\u003ctd\u003e4.1 min\u003c\/td\u003e\n\u003ctd\u003e5.0 min\u003c\/td\u003e\n\u003ctd\u003e5.0 min\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eClimb to 2,000 m\u003c\/td\u003e\n\u003ctd\u003e9.2 min\u003c\/td\u003e\n\u003ctd\u003e11.2 min\u003c\/td\u003e\n\u003ctd\u003e12.0 min\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eClimb to 3,000 m\u003c\/td\u003e\n\u003ctd\u003e15.7 min\u003c\/td\u003e\n\u003ctd\u003e20.3 min\u003c\/td\u003e\n\u003ctd\u003e24.0 min\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eService Ceiling\u003c\/td\u003e\n\u003ctd\u003e4,400 m \/ 14,500 ft\u003c\/td\u003e\n\u003ctd\u003e4,200 m \/ 13,700 ft\u003c\/td\u003e\n\u003ctd\u003e3,700 m \/ 12,100 ft\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eAbsolute Ceiling\u003c\/td\u003e\n\u003ctd\u003e4,900 m \/ 16,000 ft\u003c\/td\u003e\n\u003ctd\u003e4,800 m \/ 15,700 ft\u003c\/td\u003e\n\u003ctd\u003e4,300 m \/ 14,100 ft\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eEndurance\u003c\/td\u003e\n\u003ctd\u003e3.55 h\u003c\/td\u003e\n\u003ctd\u003e4.5 h\u003c\/td\u003e\n\u003ctd\u003e3.65 h\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eT\/O Run (5.5 mph hw)\u003c\/td\u003e\n\u003ctd\u003e140 m \/ 460 ft\u003c\/td\u003e\n\u003ctd\u003e130 m \/ 420 ft\u003c\/td\u003e\n\u003ctd\u003e200 m \/ 610 ft\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eLanding Run (5.5 mph hw)\u003c\/td\u003e\n\u003ctd\u003e150 m \/ 490 ft\u003c\/td\u003e\n\u003ctd\u003e150 m \/ 490 ft\u003c\/td\u003e\n\u003ctd\u003e150 m \/ 490 ft\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\n\n\u003ch3\u003e✈️ Aerodynamic Development History\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eNLL Wind Tunnel Studies:\u003c\/strong\u003e Scaled-model testing at the National Aviation Laboratory finalized wing and tail architecture prior to serial production clearance.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDihedral Modification:\u003c\/strong\u003e Early flight testing forced an aerodynamic redesign increasing wing dihedral to 6°30' to improve lateral stability.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eEmpennage Redesign:\u003c\/strong\u003e A severe pitch-down flow separation flaw under rudder deflection was corrected by adding a substantially larger vertical fin, extended rudder, and prominent dorsal fin.\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003ch3\u003e🔄 Handling \u0026amp; Stability — RNLAF Service Evaluation\u003c\/h3\u003e\n\u003ctable\u003e\n\u003cthead\u003e\u003ctr\u003e\n\u003cth\u003eFlight Phase \/ Axis\u003c\/th\u003e\n\u003cth\u003eCharacteristics\u003c\/th\u003e\n\u003c\/tr\u003e\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003e\u003cstrong\u003eDirectional Stability\u003c\/strong\u003e\u003c\/td\u003e\n\u003ctd\u003eMarginal in early studies; required constant left-rudder input during landing — factory rudder trim tab not adjustable from cockpit.\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003e\u003cstrong\u003eLateral \u0026amp; Longitudinal\u003c\/strong\u003e\u003c\/td\u003e\n\u003ctd\u003eHighly effective and sufficiently crisp for basic aerobatics once tail modifications were implemented.\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003e\u003cstrong\u003eStall Characteristics\u003c\/strong\u003e\u003c\/td\u003e\n\u003ctd\u003eDocile and highly predictable with prominent pre-stall buffeting — ideal for student pilot training.\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\n\n\u003ch3\u003e🛠️ Engineering \u0026amp; Service Bulletins\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eMain Landing Gear Reinforcement:\u003c\/strong\u003e Mandatory structural reinforcement after cracks developed under high-stress student landings. Some export variants used upgraded assemblies sourced from Nardi.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCockpit Heating Retrofits:\u003c\/strong\u003e Engineering modifications permitting regional operators to integrate custom heating ducts.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAeromatic Propeller Retrofit:\u003c\/strong\u003e RNLAF fleet-wide retrofit of self-regulating Aeromatic propellers to optimize takeoff and climb profiles.\u003c\/li\u003e\n\u003c\/ul\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003e🔗 Related Collection\u003c\/h3\u003e\n\u003cp\u003eThe Fokker S.11 was licence-built in Italy by Aeronautica Macchi as the \u003cstrong\u003eMacchi M.416\u003c\/strong\u003e. The primary-source Italian documentation for that variant — including the Italian-language Maintenance Manual and Illustrated Parts Catalog — is available separately:\u003cbr\u003e\n→ \u003ca href=\"\/products\/macchi-m-416-aircraft-manuals-collection-digital-download\"\u003eMacchi M.416 Aircraft Manuals Collection\u003c\/a\u003e\u003c\/p\u003e\n\n\u003chr\u003e\n\n\u003ch3\u003eNature of the Collection\u003c\/h3\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\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\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":53617945117019,"sku":null,"price":25.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/fokker-s-11-instructor-hero-banner.png?v=1784389843"}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/collections\/dutch-aviation-banner.png?v=1782801661","url":"https:\/\/onlineaviationlibrary.com\/collections\/dutch-aviation-collection.oembed","provider":"Online Aviation Library","version":"1.0","type":"link"}