{"product_id":"tupolev-tu-204-300-flight-manual-archive","title":"Tupolev Tu-204-300 — Flight Manual Archive","description":"\u003ch2\u003eTupolev Tu-204-300 — Flight Manual Archive\u003c\/h2\u003e\u003cp\u003eThe \u003cstrong\u003eTupolev Tu-204-300\u003c\/strong\u003e (developed under the designation Tu-234) is a shortened, long-range derivative of the baseline Tu-204-100 — a transcontinental narrowbody twinjet engineered to replace the Tu-154 on demanding long-haul routes. With a fuselage shortened by approximately 6 metres (20 ft) while retaining the same supercritical wing, powerplants, and large fuel capacity, the Tu-204-300 achieves exceptional range efficiency unmatched among its contemporaries.\u003c\/p\u003e\u003cp\u003eThis archive presents the \u003cstrong\u003eprimary-source Flight Manual (Руководство по Лётной Эксплуатации)\u003c\/strong\u003e issued by \u003cstrong\u003eОАО “Туполев” (OAO Tupolev)\u003c\/strong\u003e, Moscow, approved by the Director of the Department of State Policy in Civil Aviation, Ministry of Transport of the Russian Federation, 17 May 2005.\u003c\/p\u003e\u003chr\u003e\u003ch3\u003eTechnical Overview\u003c\/h3\u003e\u003ch4\u003eAerodynamics \u0026amp; Configuration\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eSupercritical Wing:\u003c\/strong\u003e High-aspect-ratio supercritical profile engineered to delay wave drag onset at transonic cruise speeds.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eWingtip Devices:\u003c\/strong\u003e Blended winglets minimizing induced drag by optimizing wingtip vortex distribution.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNatural Anti-Icing:\u003c\/strong\u003e No dedicated wing anti-icing plumbing required on primary lifting surfaces.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFlight Control System:\u003c\/strong\u003e Digital fly-by-wire (FBW) with triple-redundant channels enforcing full flight-envelope protection.\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch4\u003ePowerplant\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eEngine:\u003c\/strong\u003e Aviadvigatel PS-90A \/ PS-90A2 — dual-rotor, high-bypass turbofan\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eThrust:\u003c\/strong\u003e ~157 kN (35,274 lbf) per engine at maximum takeoff rating\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eNoise Compliance:\u003c\/strong\u003e ICAO Annex 16 Chapter 4\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAPU:\u003c\/strong\u003e Aerosila TA18-200M\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch4\u003ePerformance\u003c\/h4\u003e\u003ctable\u003e\n\u003cthead\u003e\u003ctr\u003e\n\u003cth\u003eParameter\u003c\/th\u003e\n\u003cth\u003eHeavy (Long-Range)\u003c\/th\u003e\n\u003cth\u003eLight (Medium-Range)\u003c\/th\u003e\n\u003c\/tr\u003e\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eMTOW\u003c\/td\u003e\n\u003ctd\u003e107,500 kg (237,000 lbs)\u003c\/td\u003e\n\u003ctd\u003e89,000 kg (196,200 lbs)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Payload\u003c\/td\u003e\n\u003ctd\u003e18,000 kg (39,680 lbs)\u003c\/td\u003e\n\u003ctd\u003e18,000 kg\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Passengers\u003c\/td\u003e\n\u003ctd\u003e166 (Single Class)\u003c\/td\u003e\n\u003ctd\u003e166 (Single Class)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eRange (Max Pax)\u003c\/td\u003e\n\u003ctd\u003e9,300 km (5,020 nmi)\u003c\/td\u003e\n\u003ctd\u003e3,500 km (1,890 nmi)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Ferry Range\u003c\/td\u003e\n\u003ctd\u003eUp to 11,000 km\u003c\/td\u003e\n\u003ctd\u003e—\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eCruising Speed\u003c\/td\u003e\n\u003ctd\u003eMach 0.78 – 0.80\u003c\/td\u003e\n\u003ctd\u003eMach 0.78 – 0.80\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eService Ceiling\u003c\/td\u003e\n\u003ctd\u003e12,100 m (39,700 ft)\u003c\/td\u003e\n\u003ctd\u003e12,100 m (39,700 ft)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\u003ch4\u003eSystems\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eCockpit:\u003c\/strong\u003e EFIS with six colour monitors — two-crew operation (no flight engineer)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCG Control:\u003c\/strong\u003e Automated fuel transfer system for long-range CG management\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eETOPS:\u003c\/strong\u003e Certified ETOPS-120 (2015)\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003ch3\u003eDocument Manifest — 4 Original Documents\u003c\/h3\u003e\u003ch4\u003eРЛЭ — Flight Manual (Руководство по Лётной Эксплуатации) · Ref: 74.08.0000000 РЛЭ\u003c\/h4\u003e\u003cul\u003e\n\u003cli\u003eBook 1 — Flight Manual, Part 1 (Книга первая) · First Edition, 2005 · АСЦ ГосНИИ ГА, экз. № 521\u003c\/li\u003e\n\u003cli\u003eBook 2 — Flight Manual, Part 2 (Книга вторая) · First Edition, 2005 · Учтен. экз. № 10\u003c\/li\u003e\n\u003cli\u003eAppendix — Flight Manual Supplement (Приложение) · First Edition, 2005 · Учтен. экз. № 10\u003c\/li\u003e\n\u003cli\u003eLoading \u0026amp; Centre of Gravity Manual (Руководство по Загрузке и Центровке) · Second Edition, approved 5 September 2005 · АСЦ ГосНИИ ГА, экз. № 10\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\u003e\u003ch3\u003eProvenance \u0026amp; Certification\u003c\/h3\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003ePublisher:\u003c\/strong\u003e ОАО “Туполев” (OAO Tupolev), Moscow\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eApproval Authority:\u003c\/strong\u003e Director, Department of State Policy in Civil Aviation, Ministry of Transport of the Russian Federation\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eApproval Date:\u003c\/strong\u003e 17 May 2005\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eRegistered Copies:\u003c\/strong\u003e АСЦ ГосНИИ ГА traceable registered copy numbers — authentic operational fleet documents\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eEASA Type Certificate:\u003c\/strong\u003e TCDS EASA.IM.A.162 (Tu-204-120CE series)\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\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-204-300 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\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":53460590002523,"sku":null,"price":44.85,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/tu-204-300-promo-square.png?v=1782635973","url":"https:\/\/onlineaviationlibrary.com\/products\/tupolev-tu-204-300-flight-manual-archive","provider":"Online Aviation Library","version":"1.0","type":"link"}