{"product_id":"tupolev-tu-204c-technical-documentation-archive","title":"Tupolev Tu-204C — Technical Documentation Archive","description":"\u003ch2\u003eTupolev Tu-204C — Technical Documentation Archive\u003c\/h2\u003e\u003cp\u003eThe most comprehensive primary-source documentation collection for the \u003cstrong\u003eTupolev Tu-204C freighter\u003c\/strong\u003e available in digital format. This archive brings together \u003cstrong\u003e42 original factory documents\u003c\/strong\u003e issued and approved by АНТК им. А.Н. Туполева (OAO Tupolev), Moscow, covering the complete 1997 technical documentation package for the Tu-204C cargo variant — including freighter-specific systems not present in passenger Tu-204 documentation.\u003c\/p\u003e\u003chr\u003e\u003ch3\u003eTechnical Overview\u003c\/h3\u003e\u003ch4\u003eAerodynamic Profile\u003c\/h4\u003e\u003cp\u003eThe Tu-204C utilizes high-aspect-ratio (AR = 7.7) \u003cstrong\u003esupercritical wings\u003c\/strong\u003e with vertically mounted winglets providing a 2.2% aerodynamic efficiency gain, saving 500–600 kg of fuel on maximum-range missions. Advanced wing profile geometry confers natural ice resistance on main lifting surfaces and tail units — eliminating the need for a complex wing anti-icing system, a unique feature among contemporary peers.\u003c\/p\u003e\u003ch4\u003ePowerplant Options\u003c\/h4\u003e\u003ctable\u003e\n\u003cthead\u003e\u003ctr\u003e\n\u003cth\u003eEngine\u003c\/th\u003e\n\u003cth\u003eManufacturer\u003c\/th\u003e\n\u003cth\u003eMax Thrust\u003c\/th\u003e\n\u003cth\u003eNoise Compliance\u003c\/th\u003e\n\u003c\/tr\u003e\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eAviadvigatel PS-90A\u003c\/td\u003e\n\u003ctd\u003eAviadvigatel (Russia)\u003c\/td\u003e\n\u003ctd\u003e160 kN (36,000 lbf)\u003c\/td\u003e\n\u003ctd\u003eICAO Chapter 4\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eRolls-Royce RB211-535E4\u003c\/td\u003e\n\u003ctd\u003eRolls-Royce (UK)\u003c\/td\u003e\n\u003ctd\u003e192 kN (43,100 lbf)\u003c\/td\u003e\n\u003ctd\u003eICAO Chapter 3\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\u003ch4\u003ePerformance Data\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003eMTOW: 103,000 kg (227,076 lbs)\u003c\/li\u003e\n\u003cli\u003eMaximum Payload: 27,000 kg (59,400 lbs)\u003c\/li\u003e\n\u003cli\u003eMaximum Fuel Capacity: 32,800 kg (72,311 lbs)\u003c\/li\u003e\n\u003cli\u003eMaximum Cruise Speed: 850 km\/h (Mach 0.80 \/ 458 KT)\u003c\/li\u003e\n\u003cli\u003eMaximum Operating Altitude: 12,100 m (39,700 ft)\u003c\/li\u003e\n\u003cli\u003eOperational Range: 4,500 km (2,430 NM) at max structural payload\u003c\/li\u003e\n\u003cli\u003eTakeoff Distance (MTOW): 2,050 m\u003c\/li\u003e\n\u003cli\u003eLanding Distance: 1,780 m\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch4\u003eFlight Control System\u003c\/h4\u003e\u003cp\u003eMulti-channel \u003cstrong\u003eFly-By-Wire (FBW)\u003c\/strong\u003e system providing flight envelope protection, automatic gust alleviation, and continuous stability augmentation across the full CG envelope. Spoiler\/speedbrake deployment requires explicit main gear strut compression signals — a critical handling characteristic documented in accident analyses including the Vnukovo runway overrun study.\u003c\/p\u003e\u003chr\u003e\u003ch3\u003eDocument Manifest — 42 Original Documents\u003c\/h3\u003e\u003ch4\u003eРЛЭ — Flight Manual (Руководство по Лётной Эксплуатации) · 7 Documents\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003eBook 1 — Flight Manual, Part 1 (Книга 1) · First Edition, 2000\u003c\/li\u003e\n\u003cli\u003eBook 2 — Flight Manual, Part 2 (Книга 2) · First Edition, 2000\u003c\/li\u003e\n\u003cli\u003eAppendix — Flight Manual Supplement (Приложение) · First Edition\u003c\/li\u003e\n\u003cli\u003eBook 2, Part 1 — АСЦ GosNII GA registered copy, экз. 432 · Approved 2.03.2000\u003c\/li\u003e\n\u003cli\u003eBook 2, Part 2 — АСЦ GosNII GA registered copy, экз. 432 · Approved 19.03.2007\u003c\/li\u003e\n\u003cli\u003eOxygen Equipment Section (Кислородное оборудование)\u003c\/li\u003e\n\u003cli\u003eAmendment No. 1 — RVSM Compliance \u0026amp; Expanded Operational Envelope (Изменение № 1, 2001)\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch4\u003eРТЭ — Maintenance Manual (Руководство по Технической Эксплуатации) · 15 Documents\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003eSection 012 — General\u003c\/li\u003e\n\u003cli\u003eSections 021, 030 — Air Conditioning, Oil\u003c\/li\u003e\n\u003cli\u003eSections 022, 034, 035, 142 — Auto Flight, Fuel, Hydraulic, Avionics\u003c\/li\u003e\n\u003cli\u003eSections 023, 182 — Communications, Special Systems\u003c\/li\u003e\n\u003cli\u003eSection 024 — Electrical Power\u003c\/li\u003e\n\u003cli\u003eSections 025, 038 — Equipment\/Furnishings, Water\/Waste\u003c\/li\u003e\n\u003cli\u003eSection 029 — Hydraulic Power\u003c\/li\u003e\n\u003cli\u003eSection 031 — Instruments\u003c\/li\u003e\n\u003cli\u003eSection 032 — Landing Gear\u003c\/li\u003e\n\u003cli\u003eSection 033 — Lights\u003c\/li\u003e\n\u003cli\u003eSections 051, 052, 053, 054 — Structures: Fuselage, Wings, Stabilizers, Flight Controls\u003c\/li\u003e\n\u003cli\u003eSections 055, 056, 057 — Structures: Empennage, Windows, Doors\u003c\/li\u003e\n\u003cli\u003eSections 071, 076, 077, 079, 080 — Power Plant, Engine Controls, Engine Indicating, Oil, Starting\u003c\/li\u003e\n\u003cli\u003eSection 113 — Cargo Loading Systems (freighter-specific)\u003c\/li\u003e\n\u003cli\u003eSection 144 — Cargo Door \u0026amp; Freight Equipment (freighter-specific)\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch4\u003eРТО — Technical Servicing Manual (Руководство по Техническому Обслуживанию) · 1 Document\u003c\/h4\u003e\u003cul\u003e\u003cli\u003eSingle volume — Approved 11 February 1997\u003c\/li\u003e\u003c\/ul\u003e\u003ch4\u003eРТЭО — Technical Operation Manual (Руководство по Технической Эксплуатации Оборудования) · 19 Documents\u003c\/h4\u003e\u003cul\u003e\u003cli\u003eBooks 1 through 19 — Complete set, approved 11 February 1997\u003c\/li\u003e\u003c\/ul\u003e\u003chr\u003e\u003ch3\u003eProvenance \u0026amp; Certification\u003c\/h3\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003ePublisher:\u003c\/strong\u003e АНТК им. А.Н. Туполева (OAO Tupolev), Moscow\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eApproval Authority:\u003c\/strong\u003e Mintrans Russia (Yu.P. Tarshin), GosNII GA, OAO Tupolev Chief Designer (O.Yu. Alasheev)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePrimary approval date:\u003c\/strong\u003e 11 February 1997 (РТЭ\/РТО\/РТЭО); 2000–2001 (РЛЭ)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eНЕ ЭТАЛОН stamps:\u003c\/strong\u003e Operational working copies bearing НЕ ЭТАЛОН (non-master) stamps — authentic fleet-use documents with traceable registered copy numbers. These are not sanitized reprints.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eEASA Type Certificate:\u003c\/strong\u003e TCDS EASA.IM.A.162 (Tu-204-120CE)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAirworthiness Directive:\u003c\/strong\u003e RU-2014-55-01 — Stabilizer structural inspection mandate\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFreighter-specific sections:\u003c\/strong\u003e Sections 113 and 144 cover cargo loading systems and freight door mechanisms not present in passenger Tu-204 documentation.\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003ch3\u003eIntended Use\u003c\/h3\u003e\u003cp\u003eThis collection is intended for aviation historians, researchers, museum restoration teams, flight simulation developers, and engineering professionals requiring primary-source reference material on the Tu-204C freighter platform.\u003c\/p\u003e\u003chr\u003e\u003cp\u003e\u003cem\u003e⚠️ Airliner Category Notice: Documentation standards for commercial airliner collections are currently under development at Online Aviation Library. Content structure and manifest depth for this category may be updated as our airliner standards are finalized.\u003c\/em\u003e\u003c\/p\u003e\u003cp\u003e\u003cem\u003e⚠️ Regulatory Notice: 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\/em\u003e\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":53460527808859,"sku":null,"price":99.85,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/tu-204c-promotional-square.png?v=1782633930","url":"https:\/\/onlineaviationlibrary.com\/products\/tupolev-tu-204c-technical-documentation-archive","provider":"Online Aviation Library","version":"1.0","type":"link"}