{"product_id":"ilyushin-il-114-il-114-300-flight-operations-engine-technical-manual-archive","title":"Ilyushin Il-114 \/ Il-114-300 — Flight Operations \u0026 Engine Technical Manual Archive","description":"\u003ch2\u003eIlyushin Il-114 \/ Il-114-300 — Flight Operations \u0026amp; Engine Technical Manual Archive\u003c\/h2\u003e\u003cp\u003e\u003cem\u003ePrimary-Source Documentation | Ilyushin Design Bureau \u0026amp; Klimov\u003c\/em\u003e\u003c\/p\u003e\u003cp\u003eThis Living Collection brings together the complete primary-source flight operations and engine technical documentation for the \u003cstrong\u003eIlyushin Il-114\u003c\/strong\u003e regional turboprop and its fully modernized, newly certified variant, the \u003cstrong\u003eIl-114-300\u003c\/strong\u003e. Developed by the Ilyushin Aviation Complex (ИАК) and powered by the Klimov TV7-117 turboprop family, the Il-114 represents the definitive Soviet and post-Soviet approach to short-haul regional aviation — engineered for unpaved strips, arctic conditions, and high-frequency domestic routes.\u003c\/p\u003e\u003chr\u003e\u003ch3\u003eAircraft Overview\u003c\/h3\u003e\u003cp\u003eThe Il-114 is a low-wing, twin-turboprop regional transport designed for routes up to 1,500 km with 60–68 passengers. Its high-efficiency wing (aspect ratio 11.0) and fixed dihedral configuration deliver strong lateral stability and low fuel burn. The tricycle landing gear with telescopic shock absorption enables operations from unpaved and arctic ice strips — a defining operational requirement for Russian regional aviation.\u003c\/p\u003e\u003cp\u003eThe \u003cstrong\u003eIl-114-300\u003c\/strong\u003e modernization introduces the TV7-117ST-01 engine (2,900 shp, FADEC-controlled), six-blade Aerosila AV112-114 composite propellers, the TsPNK-114M2 dual-redundant flight-navigation suite (ICAO Cat. II autopilot), and a reduced takeoff run of just 730 m. Russian Federal Air Transport Agency type certification for serial production has been granted.\u003c\/p\u003e\u003chr\u003e\u003ch3\u003eCollection Manifest — 5 Documents\u003c\/h3\u003e\u003ctable\u003e\n\u003cthead\u003e\u003ctr\u003e\n\u003cth\u003e#\u003c\/th\u003e\n\u003cth\u003eDocument\u003c\/th\u003e\n\u003cth\u003eLanguage\u003c\/th\u003e\n\u003cth\u003eReference\u003c\/th\u003e\n\u003c\/tr\u003e\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003e1\u003c\/td\u003e\n\u003ctd\u003eIl-114 — Flight Operations Manual (RLE) — Book 1\u003c\/td\u003e\n\u003ctd\u003eRussian\u003c\/td\u003e\n\u003ctd\u003eIlyushin \/ Aeroflot\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003e2\u003c\/td\u003e\n\u003ctd\u003eIl-114 — Flight Operations Manual (RLE) — Book 2, Part 1\u003c\/td\u003e\n\u003ctd\u003eRussian\u003c\/td\u003e\n\u003ctd\u003eIlyushin \/ Aeroflot\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003e3\u003c\/td\u003e\n\u003ctd\u003eIl-114 — Flight Operations Manual (RLE) — Book 2, Part 2\u003c\/td\u003e\n\u003ctd\u003eRussian\u003c\/td\u003e\n\u003ctd\u003eIlyushin \/ Aeroflot\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003e4\u003c\/td\u003e\n\u003ctd\u003eTV7-117S — Technical Maintenance Manual (RTE) 065.00.0300 РЭ — Book 1\u003c\/td\u003e\n\u003ctd\u003eRussian\u003c\/td\u003e\n\u003ctd\u003eKlimov \/ Dec 2000\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003e5\u003c\/td\u003e\n\u003ctd\u003eTV7-117S — Technical Maintenance Manual (RTE) 065.00.0300 РЭ — Book 2\u003c\/td\u003e\n\u003ctd\u003eRussian\u003c\/td\u003e\n\u003ctd\u003eKlimov \/ Dec 2000\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\u003cp\u003e\u003cem\u003eNote: TV7-117S manuals carry the original «НЕ ЭТАЛОН» (Non-Master Copy) archival stamp — a standard Soviet-era distribution marking.\u003c\/em\u003e\u003c\/p\u003e\u003chr\u003e\u003ch3\u003eKey Technical Data\u003c\/h3\u003e\u003ctable\u003e\n\u003cthead\u003e\u003ctr\u003e\n\u003cth\u003eParameter\u003c\/th\u003e\n\u003cth\u003eIl-114 Baseline\u003c\/th\u003e\n\u003cth\u003eIl-114-300\u003c\/th\u003e\n\u003c\/tr\u003e\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eMTOW\u003c\/td\u003e\n\u003ctd\u003e23,500 kg\u003c\/td\u003e\n\u003ctd\u003e23,500 kg\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax Payload\u003c\/td\u003e\n\u003ctd\u003e6,500 kg\u003c\/td\u003e\n\u003ctd\u003e6,800 kg\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003ePassenger Seating\u003c\/td\u003e\n\u003ctd\u003e60–64\u003c\/td\u003e\n\u003ctd\u003e66–68\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eCruising Speed\u003c\/td\u003e\n\u003ctd\u003e470–500 km\/h\u003c\/td\u003e\n\u003ctd\u003e500 km\/h\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eService Ceiling\u003c\/td\u003e\n\u003ctd\u003e7,600 m\u003c\/td\u003e\n\u003ctd\u003e8,000 m\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eFull Payload Range\u003c\/td\u003e\n\u003ctd\u003e~1,000–1,500 km\u003c\/td\u003e\n\u003ctd\u003e1,400 km\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eTakeoff \/ Landing Run\u003c\/td\u003e\n\u003ctd\u003e1,500 m \/ 1,300 m\u003c\/td\u003e\n\u003ctd\u003e730 m \/ 440 m\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\u003chr\u003e\u003ch3\u003ePropulsion — TV7-117 Family\u003c\/h3\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eTV7-117S\u003c\/strong\u003e (baseline): 2,500 shp — documented in this collection's engine manuals\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTV7-117ST-01\u003c\/strong\u003e (Il-114-300): 3,100 shp takeoff power | FADEC: BARK-65SM digital core (Auto-Thrust, Reverse Thrust, Surge Protection) | Six-blade Aerosila AV112-114 composite propellers — high-chord, low-noise profile | Up to 4,000 kg thrust | Compressor: 5-stage axial + 1-stage centrifugal\u003c\/li\u003e\n\u003cli\u003eFuel flow: 500–550 kg\/h | Efficiency: 20.8 g\/passenger·km\u003c\/li\u003e\n\u003cli\u003eAPU: Aerosila TA-14-114 (tailcone-mounted, unassisted ground start)\u003c\/li\u003e\n\u003cli\u003eThermal operating envelope: −60°C to +45°C (certified)\u003c\/li\u003e\n\u003cli\u003eTest validation: 3,000+ flight hours across 400+ test flights\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003ch3\u003eSystems Engineering Highlights\u003c\/h3\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eHydraulics:\u003c\/strong\u003e Dual independent circuits at 207 bar (3,000 psi) — flaps, landing gear, airbrakes, nosewheel steering\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePressurization:\u003c\/strong\u003e Dual-redundant ECS using engine bleed air, max differential 0.44 bar (6.4 psi)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAnti-Icing:\u003c\/strong\u003e Electrical pulse-wave system (wings\/tail leading edges), electrothermal (propellers\/windscreens), hot air (engine intakes)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eElectrical:\u003c\/strong\u003e 115\/220V 400Hz AC via 40 kW alternators per engine + 24V DC backup\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFlight Navigation:\u003c\/strong\u003e TsPNK-114M2 dual-redundant suite, ICAO Cat. II autopilot; glass cockpit simulator with 60° × 180° direct-projection visual system\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eArctic Certification:\u003c\/strong\u003e Full system performance validated at −45°C (Yakutsk \/ Magan field trials)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eLRU Support:\u003c\/strong\u003e AOG spare parts delivery target: 72 hours\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003ch3\u003ePermitted Uses\u003c\/h3\u003e\u003cp\u003eHistorical research · Flight simulation · Museum and restoration reference · Aviation education · Scale modelling · Engineering study\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\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":53610824270171,"sku":null,"price":35.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/banner-4-il-114-300-prototype-belly-view.png?v=1784265456","url":"https:\/\/onlineaviationlibrary.com\/products\/ilyushin-il-114-il-114-300-flight-operations-engine-technical-manual-archive","provider":"Online Aviation Library","version":"1.0","type":"link"}