{"product_id":"sukhoi-su-17-su-22-fitter-technical-description-exploitation-manuals","title":"Sukhoi Su-17 \/ Su-22 Fitter — Technical Description \u0026 Exploitation Manuals","description":"\u003ch3\u003eSukhoi Su-17 \/ Su-22 \"Fitter\" — Technical Description \u0026amp; Exploitation Manuals\u003c\/h3\u003e\n\u003ch3\u003eSoviet Domestic \u0026amp; Export Variants | Variable-Sweep Wing Fighter-Bomber\u003c\/h3\u003e\n\u003cp\u003eThe Sukhoi Su-17 and Su-22 are the same aircraft — one designation, two destinies. The \u003cstrong\u003eSu-17\u003c\/strong\u003e served the Soviet Air Force and its successor states as a frontline fighter-bomber; the \u003cstrong\u003eSu-22\u003c\/strong\u003e is the export designation applied to downgraded and modified variants delivered to allied nations across the Middle East, Africa, Latin America, and Eastern Europe throughout the Cold War. Both share the same variable-sweep wing airframe, the same Lyulka AL-21F-3 powerplant family, and the same fundamental aerodynamic character.\u003c\/p\u003e\n\u003cp\u003eThis archival collection brings together primary-source \u003cstrong\u003eTechnical Description\u003c\/strong\u003e (Техническое описание) and \u003cstrong\u003eTechnical Exploitation Manuals\u003c\/strong\u003e (Руководство по технической эксплуатации) covering the full aircraft system suite across multiple variants.\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eAircraft Technical Profile\u003c\/h3\u003e\n\u003cp\u003e\u003cstrong\u003ePowerplant:\u003c\/strong\u003e Lyulka AL-21F-3 afterburning turbojet (76.5 kN dry \/ 109.8 kN with full afterburner) — or Tumansky R-29BS-300 in specific export variants. 14-stage axial compressor, 3-stage turbine. APU or external pneumatic air start.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eVariable-Sweep Wing Geometry:\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e28° — Minimum sweep (takeoff, landing, loiter)\u003c\/li\u003e\n\u003cli\u003e45° — Intermediate sweep (cruise, manoeuvring)\u003c\/li\u003e\n\u003cli\u003e62° — Maximum sweep (high-speed dash, supersonic flight)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003ePerformance Envelope:\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eMaximum Speed (Sea Level): Mach 1.1 \/ 1,400 km\/h\u003c\/li\u003e\n\u003cli\u003eMaximum Speed (Altitude): Mach 1.7 \/ 1,860 km\/h\u003c\/li\u003e\n\u003cli\u003eService Ceiling: 14,200 m (46,585 ft)\u003c\/li\u003e\n\u003cli\u003eRate of Climb: 230 m\/s (45,275 ft\/min)\u003c\/li\u003e\n\u003cli\u003eMTOW: 19,430 kg (42,835 lbs)\u003c\/li\u003e\n\u003cli\u003eCombat Radius: 1,150 km (Hi-Lo-Hi, 2,000 kg payload)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eDocument Manifest\u003c\/h3\u003e\n\u003cp\u003e\u003cstrong\u003eSu-17M2 — Technical Description (Техническое описание), 1975\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eBook 1, Part 1 — Airframe \u0026amp; General Systems Description\u003c\/li\u003e\n\u003cli\u003eBook 4, Part 1 — Aerodynamics \u0026amp; Flight Characteristics\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eSu-22UM3K \u0026amp; Su-22 (54K) — Technical Exploitation Manuals (Book 8)\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003ePart 1 — Electrical Equipment \u0026amp; Lighting Systems: Description and Operation\u003c\/li\u003e\n\u003cli\u003ePart 3 — Instrument Equipment, UUAP-72M, IKV-1, KN-23 Complex: Description and Operation\u003c\/li\u003e\n\u003cli\u003ePart 7 — Weapons Systems, PWU\/FKA: Description and Service\u003c\/li\u003e\n\u003cli\u003ePart 8 — Tester Systems (ver. 1 \u0026amp; ver. 2): Description and Service\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eAdditional Coverage:\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eSAU-22 Automatic Flight Control System (terrain-following retrofit)\u003c\/li\u003e\n\u003cli\u003eSPS-141 ECM Pod Integration — structural and electrical hardpoint modifications\u003c\/li\u003e\n\u003cli\u003eKDS-23 Chaff\/Flare Countermeasure Dispensers — upper fuselage spine installation\u003c\/li\u003e\n\u003cli\u003eComputational-Sight Instrumentation, Photo-Control \u0026amp; SSPP Systems\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eAerodynamic \u0026amp; Stability Documentation\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003eLongitudinal control via all-moving horizontal stabilator — pitch sensitivity vs. sweep position\u003c\/li\u003e\n\u003cli\u003eLateral\/directional stability — adverse yaw at low speed, full forward sweep\u003c\/li\u003e\n\u003cli\u003eRoll control: differential tailplanes + wing spoilers (swept configuration)\u003c\/li\u003e\n\u003cli\u003eStall characteristics: AOA limits 16°–18° depending on configuration\u003c\/li\u003e\n\u003cli\u003eBoundary layer fence analysis — fixed wing panel, high-AOA separation prevention\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eDelivery Format\u003c\/h3\u003e\n\u003cp\u003eDigital download — instant access upon purchase. Archival document scans in high-resolution format. Language: Russian \/ Русский.\u003c\/p\u003e\n\u003chr\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\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 authorised 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","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53456866378075,"sku":"OAL-SU17-SU22-FITTER-TD-TEM","price":49.85,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/su-17-su-22-fitter-simple-banner.png?v=1782566533","url":"https:\/\/onlineaviationlibrary.com\/products\/sukhoi-su-17-su-22-fitter-technical-description-exploitation-manuals","provider":"Online Aviation Library","version":"1.0","type":"link"}