{"product_id":"ilyushin-il-14-founding-document-set-soviet-lufthansa-mga-1957-1963","title":"Ilyushin Il-14 — Founding Document Set: Aerodynamics (Soviet) · Handbuch IL-14 P (Lufthansa, 1957) · Flight Operations Manual ASh-82T (МГА СССР, 1963)","description":"\u003ch2\u003eIlyushin Il-14 — Founding Document Set\u003c\/h2\u003e\u003cp\u003eThree primary-source documents. Three languages. Two nations. One aircraft that defined Soviet post-war civil and military transport aviation.\u003c\/p\u003e\u003cp\u003eThe \u003cstrong\u003eIlyushin Il-14\u003c\/strong\u003e (NATO: \"Crate\") was the direct successor to the Il-12, engineered to resolve every aerodynamic and handling deficiency of its predecessor. It served Aeroflot, the Soviet Air Forces, East German Interflug, Czechoslovak Airlines (ČSA), and numerous Warsaw Pact operators — and was licensed for production at VEB Flugzeugwerke Dresden (VEB 14) and Avia in Czechoslovakia (Avia 14). This founding set captures the aircraft from three distinct operator perspectives: the Soviet aerodynamic research institute, Lufthansa's engineering division, and the Soviet Ministry of Civil Aviation.\u003c\/p\u003e\u003cp\u003eThis is the opening entry of the \u003cstrong\u003eIl-14 Collection\u003c\/strong\u003e, which will grow as additional primary-source documents are located and processed.\u003c\/p\u003e\u003chr\u003e\u003ch3\u003eDocument 1 — Soviet Aerodynamics Manual\u003c\/h3\u003e\u003cp\u003e\u003cstrong\u003eTitle:\u003c\/strong\u003e Аэродинамика Самолета Ил-14 (Aerodynamics of the Il-14 Aircraft)\u003cbr\u003e\u003cstrong\u003eAuthors:\u003c\/strong\u003e V. Bragin, V. Smolin\u003cbr\u003e\u003cstrong\u003ePublisher:\u003c\/strong\u003e Главное Управление ГВФ при Совете Министров СССР \/ Aeroflot Editorial Division, Moscow\u003cbr\u003e\u003cstrong\u003eLanguage:\u003c\/strong\u003e Russian\u003c\/p\u003e\u003cp\u003eThe foundational Soviet aerodynamic reference for the Il-14, authored by Bragin and Smolin for the Main Directorate of the Civil Air Fleet under the USSR Council of Ministers. Covers the complete aerodynamic redesign from the Il-12: constant-dihedral wing, 3-degree forward sweep on outer panels, upgraded trailing-edge flaps, refined nacelle cowling profiles, and landing gear door engineering to minimize parasitic drag during single-engine climb-out.\u003c\/p\u003e\u003chr\u003e\u003ch3\u003eDocument 2 — Lufthansa Handbuch IL-14 P\u003c\/h3\u003e\u003cp\u003e\u003cstrong\u003eTitle:\u003c\/strong\u003e Handbuch IL-14 P\u003cbr\u003e\u003cstrong\u003ePublisher:\u003c\/strong\u003e Lufthansa\u003cbr\u003e\u003cstrong\u003eEdition:\u003c\/strong\u003e Ausgabe Oktober 1957\u003cbr\u003e\u003cstrong\u003eLanguage:\u003c\/strong\u003e German\u003c\/p\u003e\u003cp\u003eThe complete Lufthansa engineering handbook for the IL-14 P passenger variant, issued October 1957. A rare Western-operator primary-source document for a Soviet aircraft, reflecting Lufthansa's early post-war fleet evaluation and technical documentation standards.\u003c\/p\u003e\u003ch4\u003eContents (Gesamt-Inhaltsverzeichnis)\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003e0 — Technische Daten (Technical Data)\u003c\/li\u003e\n\u003cli\u003e1 — Rumpf (Fuselage)\u003c\/li\u003e\n\u003cli\u003e2 — Tragwerk (Wing Structure)\u003c\/li\u003e\n\u003cli\u003e3 — Leitwerk – Steuerung (Empennage – Flight Controls)\u003c\/li\u003e\n\u003cli\u003e4 — Fahrwerk (Landing Gear)\u003c\/li\u003e\n\u003cli\u003e5 — Triebwerksanlage – Luftschraube (Powerplant – Propeller)\u003c\/li\u003e\n\u003cli\u003e6 — Ausrüstung (Equipment)\u003c\/li\u003e\n\u003cli\u003e7 — Flugbetriebsanleitung (Flight Operations Manual)\u003c\/li\u003e\n\u003cli\u003e8 — Vorschriftsmäßige Prüfungen und Überholungsarbeiten (Mandatory Inspections and Overhaul Procedures)\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003ch3\u003eDocument 3 — Soviet МГА Flight Operations \u0026amp; Piloting Manual\u003c\/h3\u003e\u003cp\u003e\u003cstrong\u003eTitle:\u003c\/strong\u003e Руководство по Летной Эксплуатации и Пилотированию Самолета Ил-14 с Двумя Двигателями АШ-82Т\u003cbr\u003e(Flight Operation and Piloting Manual for the Il-14 Aircraft with Two ASh-82T Engines — 3rd Revised and Supplemented Edition)\u003cbr\u003e\u003cstrong\u003ePublisher:\u003c\/strong\u003e Редакционно-Издательский Отдел МГА СССР, Moscow\u003cbr\u003e\u003cstrong\u003eDate:\u003c\/strong\u003e 1963 (introduced by Order No. 508, 5 August 1963)\u003cbr\u003e\u003cstrong\u003eAuthority:\u003c\/strong\u003e Министерство Гражданской Авиации СССР (Ministry of Civil Aviation, USSR)\u003cbr\u003e\u003cstrong\u003eLanguage:\u003c\/strong\u003e Russian\u003cbr\u003e\u003cstrong\u003eCopy No.:\u003c\/strong\u003e 2,652\u003c\/p\u003e\u003cp\u003eThe definitive Soviet civil aviation authority flight manual for the Il-14 with ASh-82T engines, introduced by \u003cstrong\u003eOrder No. 508\u003c\/strong\u003e of the Head of the Main Directorate of the Civil Air Fleet, signed by Acting Head General-Colonel of Aviation \u003cstrong\u003eG. Schetchikov\u003c\/strong\u003e on 5 August 1963. The order explicitly superseded all previously issued flight operation manuals and individual operational directives for the Il-14. Third edition, revised and supplemented.\u003c\/p\u003e\u003chr\u003e\u003ch3\u003eTechnical Overview — Ilyushin Il-14\u003c\/h3\u003e\u003ch4\u003ePowerplant — Shvetsov ASh-82T\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003eType: 14-cylinder, twin-row, air-cooled radial piston engine\u003c\/li\u003e\n\u003cli\u003eTakeoff output: 1,900 hp (1,417 kW) per engine\u003c\/li\u003e\n\u003cli\u003ePropeller: AV-50 with automatic feathering mechanism (activates on engine failure during climb-out)\u003c\/li\u003e\n\u003cli\u003eFuel storage relocated outboard of nacelles to mitigate fire risk and extend TBO to approx. 500 hours\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\u003eFigure\u003c\/th\u003e\n\u003c\/tr\u003e\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Takeoff Weight\u003c\/td\u003e\n\u003ctd\u003e18,000 kg (39,683 lbs)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eEmpty Weight\u003c\/td\u003e\n\u003ctd\u003e12,600 kg (27,778 lbs)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Speed (at 2,400 m)\u003c\/td\u003e\n\u003ctd\u003e416 km\/h (258 mph)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eCruising Speed\u003c\/td\u003e\n\u003ctd\u003e350 km\/h (217 mph)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eService Ceiling\u003c\/td\u003e\n\u003ctd\u003e7,400 m (24,278 ft)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eOperational Range\u003c\/td\u003e\n\u003ctd\u003e1,306–2,500 km (payload-dependent)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003ePassenger Capacity\u003c\/td\u003e\n\u003ctd\u003e24–32 seats (configuration-dependent)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\u003ch4\u003eAerodynamic \u0026amp; Structural Highlights\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003eCompletely redesigned wing with constant dihedral — replacing the Il-12's problematic geometry\u003c\/li\u003e\n\u003cli\u003e3-degree forward sweep on outer wing panels — preventing premature tip stalls at low speed\u003c\/li\u003e\n\u003cli\u003eUpgraded trailing-edge flaps and gear doors engineered to close flush during gear-extended flight\u003c\/li\u003e\n\u003cli\u003eHighly refined nacelle cowling profile smoothing boundary layer over wing center section\u003c\/li\u003e\n\u003cli\u003eBroader, taller vertical stabilizer and rudder — resolving severe directional instability during single-engine operation\u003c\/li\u003e\n\u003cli\u003eLarger tail area allowing full yaw control even at speeds just above stall with one engine inoperative\u003c\/li\u003e\n\u003cli\u003eHigh-pressure pneumatic landing gear retraction — doubled retraction speed vs. Il-12\u003c\/li\u003e\n\u003cli\u003eCold-weather procedure: manual prop rotation before startup to unseat piston rings and prevent hydraulic lock\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch4\u003eLicensed Production Variants\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eVEB 14\u003c\/strong\u003e — VEB Flugzeugwerke Dresden, East Germany\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAvia 14\u003c\/strong\u003e — Avia, Czechoslovakia\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.\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":53566819238235,"sku":null,"price":29.85,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/il-14-nose-close-up-banner.png?v=1783688204","url":"https:\/\/onlineaviationlibrary.com\/products\/ilyushin-il-14-founding-document-set-soviet-lufthansa-mga-1957-1963","provider":"Online Aviation Library","version":"1.0","type":"link"}