{"product_id":"ilyushin-il-96-300-technical-reference-performance-data-compilation","title":"Ilyushin IL-96-300 — Technical Reference \u0026 Performance Data Compilation","description":"\u003ch3\u003eIlyushin IL-96-300 — Technical Reference \u0026amp; Performance Data Compilation\u003c\/h3\u003e\n\u003cp\u003eThis archival compilation assembles publicly available aeronautical registry data, type certification overviews, and flight-testing performance records for the \u003cstrong\u003eIlyushin IL-96-300\u003c\/strong\u003e — the first Russian widebody airliner designed from inception around highly redundant fly-by-wire flight automation systems. Fully detailed proprietary engineering manuals and internal design data sheets remain restricted to the Ilyushin Design Bureau and United Aircraft Corporation (UAC); this compilation draws exclusively from public aeronautical registries and open technical literature.\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eAerodynamic Configuration \u0026amp; Profile\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eSupercritical Wing Design:\u003c\/strong\u003e High-aspect-ratio supercritical wing profile engineered to delay the onset of wave drag at high transonic speeds.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eWingtip Devices:\u003c\/strong\u003e Integrated vertical winglets reducing induced drag and maximizing lift-to-drag (L\/D) ratios during high-altitude cruise.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eControl Surfaces:\u003c\/strong\u003e Double-slotted trailing-edge flaps, full-span leading-edge slats, and upper-wing spoilers for roll augmentation and lift dumping.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eEngine Technical Notes — Aviadvigatel PS-90A\u003c\/h3\u003e\n\u003ctable\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003cth\u003eParameter\u003c\/th\u003e\n\u003cth\u003eSpecification\u003c\/th\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eEngine Model\u003c\/td\u003e\n\u003ctd\u003eAviadvigatel PS-90A\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eConfiguration\u003c\/td\u003e\n\u003ctd\u003eTwin-spool, high-bypass ratio, direct mixing\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eTakeoff Thrust\u003c\/td\u003e\n\u003ctd\u003e157 kN (35,300 lbf) per engine\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eSpecific Fuel Consumption\u003c\/td\u003e\n\u003ctd\u003e~0.595 kg\/kgf·hour\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eBypass Ratio\u003c\/td\u003e\n\u003ctd\u003e4.4 : 1\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eAcoustic Compliance\u003c\/td\u003e\n\u003ctd\u003e2nd generation sound-absorbing structures (ZPK-2) — ICAO Chapter 4\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eThrust Reversal\u003c\/td\u003e\n\u003ctd\u003eIntegrated into the fan duct system\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\n\u003chr\u003e\n\u003ch3\u003eHandling, Stability \u0026amp; Flight Controls\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eFly-by-Wire (FBW):\u003c\/strong\u003e Analog-backed Electronic Flight Control System (EFCS) managing pilot control laws, automatically limiting structural load factors and preventing stall\/overspeed conditions.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eYaw \u0026amp; Pitch Stability:\u003c\/strong\u003e Expanded vertical stabilizer area providing aerodynamic authority in critical one-engine-inoperative (OEI) scenarios.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFuel Balance System:\u003c\/strong\u003e Automated fuel-management sequence continuously shifting fuel among 9 active tanks to dynamically manage center of gravity (CG) in flight.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003ePerformance Data Sheet\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\u003eMaximum Takeoff Weight (MTOW)\u003c\/td\u003e\n\u003ctd\u003e250,000 kg (551,000 lbs)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eOperating Empty Weight (OEW)\u003c\/td\u003e\n\u003ctd\u003e117,000 kg (257,940 lbs)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Payload Capacity\u003c\/td\u003e\n\u003ctd\u003e40,000 kg (88,185 lbs)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Fuel Capacity\u003c\/td\u003e\n\u003ctd\u003e~150,400 L (~120,300 kg)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eCruising Speed\u003c\/td\u003e\n\u003ctd\u003eMach 0.78 – 0.84 (850–900 km\/h)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eService Ceiling\u003c\/td\u003e\n\u003ctd\u003e13,100 m (43,000 ft)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Range\u003c\/td\u003e\n\u003ctd\u003e11,500 km (reduced payload) \/ 9,000 km (max payload)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eTakeoff Field Length\u003c\/td\u003e\n\u003ctd\u003e2,600 m at standard MTOW\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eLanding Field Length\u003c\/td\u003e\n\u003ctd\u003e~1,980–2,000 m (FAA\/ICAO)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\n\u003chr\u003e\n\u003ch3\u003eEngineering \u0026amp; Fleet Modernization Bulletins\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eAvionics \u0026amp; FMS Overhauls:\u003c\/strong\u003e Transition from initial six-screen EFIS to modern FMS (VSS-95) suites, aligning with PBN and RNAV guidelines.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCategory III Landing Approvals:\u003c\/strong\u003e Upgraded autoland navigation sensors for ICAO Category IIIA and IIIB low-visibility operations.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTwin-Engine Study:\u003c\/strong\u003e Rosstec\/UAC development directives analyzing structural retrofits to transition from four PS-90A engines to two ultra-high-thrust PD-35 turbofans.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eArchive Manifest — 44 Documents\u003c\/h3\u003e\n\u003cp\u003e\u003cstrong\u003eРуководство по Лётной Эксплуатации (РЛЭ) — Flight Operations Manual Set\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eРЛЭ Ил-96-300, Книга 1 — Flight Operations Manual, Book 1 (Dec 1992, amendments to 2001) — Аэрофлот АСЦ copy\u003c\/li\u003e\n\u003cli\u003eДополнение № 5 к РЛЭ — Supplement No. 5 to FOM (1995)\u003c\/li\u003e\n\u003cli\u003eИзменение № 9\/2-2000 (Major) — Amendment to FOM, IAC\/MAK approved (Dec 2000)\u003c\/li\u003e\n\u003cli\u003eИзменение № 11\/12-02 (Major) — Amendment to FOM, avionics modernization, IAC\/MAK approved (Dec 2002)\u003c\/li\u003e\n\u003cli\u003eИзменение № 36 (Minor) к Дополнению № 5 — Minor Amendment to Supplement 5 (Mar 2002)\u003c\/li\u003e\n\u003cli\u003eLetter No. 1036\/150 — Official Ilyushin transmittal letter + Amendment 7 replacement page set (Jul 2006, signed Chief Designer Terentyev)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eРегламент Технического Обслуживания — Maintenance Schedule\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eРегламент ТО Ил-96-300 (оперативные и периодические формы) — Maintenance Schedule, Operational \u0026amp; Periodic Forms (1994) — Шереметьево Technical Library, Инв. № 8239\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eДополнение к РО-96 «ОАО Аэрофлот» — Aeroflot Operations Manual Supplement\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eSupplement to the Aeroflot РО-96 Operations Manual\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eРуководство по Технической Эксплуатации (РТЭ) — Technical Maintenance Manual, Numbered Volumes\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eРТЭ Ил-96-300, Книга 1 through Книга 22 (Books 1–22, including Book 22) — 17 volumes, Контрольный экз., 1st Edition, Шереметьево\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eРТЭ — Section-Specific Volumes (ATA-equivalent)\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eРаздел 005 — Service Life Limits\u003c\/li\u003e\n\u003cli\u003eРаздел 012.10 — Ground Support Equipment (Аэродромное Оборудование)\u003c\/li\u003e\n\u003cli\u003eРаздел 012.50 — Line Maintenance (Оперативное Обслуживание)\u003c\/li\u003e\n\u003cli\u003eРаздел 021, Книга 1 \u0026amp; 2 — Air Conditioning System\u003c\/li\u003e\n\u003cli\u003eРаздел 022 — Automatic Flight Control \/ Autopilot\u003c\/li\u003e\n\u003cli\u003eРаздел 023 — Radio Communications Equipment\u003c\/li\u003e\n\u003cli\u003eРаздел 024 — Electrical Power Supply System\u003c\/li\u003e\n\u003cli\u003eРаздел 025 — Cabin \u0026amp; Emergency Equipment\u003c\/li\u003e\n\u003cli\u003eРаздел 026 — Fire Protection\u003c\/li\u003e\n\u003cli\u003eРаздел 027, Книга 1 \u0026amp; 2 — Flight Controls\u003c\/li\u003e\n\u003cli\u003eРаздел 030 — Ice \u0026amp; Rain Protection\u003c\/li\u003e\n\u003cli\u003eРаздел 031 — Instruments \u0026amp; Indicating Systems\u003c\/li\u003e\n\u003cli\u003eРаздел 049 — Auxiliary Power Unit (APU \/ ВСУ)\u003c\/li\u003e\n\u003cli\u003eРаздел 051 — Airframe Structure (General)\u003c\/li\u003e\n\u003cli\u003eРаздел 053 — Fuselage\u003c\/li\u003e\n\u003cli\u003eРаздел 058 — Non-Destructive Testing (NDT)\u003c\/li\u003e\n\u003cli\u003eРаздел 110 — Radio Navigation Equipment\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cem\u003eAll documents: Контрольный экземпляр (Control\/Reference Copy) — НЕ ЭТАЛОН (Non-Master Copy). Provenance: Техническая Библиотека АЭРМ, ОА Шереметьево, Инв. № 63963. These are genuine working copies from the Sheremetyevo technical library, not reproductions.\u003c\/em\u003e\u003c\/p\u003e\n\u003chr\u003e\n\u003cblockquote\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\u003c\/blockquote\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 Disclaimer and Export Notice before purchasing.\u003c\/em\u003e\u003c\/p\u003e\n\u003cp\u003e\u003cem\u003eArchival edition — for reference, simulation \u0026amp; research only. ⚠️ Not for active airworthiness use. → Disclaimer | Export Notice\u003c\/em\u003e\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53461216493915,"sku":null,"price":249.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/il-96-300-promo-soviet-aeroflot.png?v=1782648262","url":"https:\/\/onlineaviationlibrary.com\/products\/ilyushin-il-96-300-technical-reference-performance-data-compilation","provider":"Online Aviation Library","version":"1.0","type":"link"}