{"product_id":"sukhoi-su-24-fencer-flight-manual-technical-documentation","title":"Sukhoi Su-24 Fencer — Flight Manual \u0026 Technical Documentation Collection","description":"\u003ch3\u003eSukhoi Su-24 Fencer — Primary-Source Flight \u0026amp; Technical Documentation\u003c\/h3\u003e\n\u003cp\u003eThe \u003cstrong\u003eSukhoi Su-24 \"Fencer\"\u003c\/strong\u003e is the Soviet Union's definitive variable-sweep tactical strike bomber — engineered to penetrate defended airspace at supersonic speed, just meters above the terrain, in any weather, day or night. This collection brings together original factory, military-issue, and academic documentation covering the Su-24 and Su-24M across aerodynamics, engine exploitation, avionics, crew procedures, and radioelectronic systems.\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eDocument Manifest\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eЗапуск и опробование авиационного двигателя самолёта Су-24М\u003c\/strong\u003e (Engine Start \u0026amp; Run-Up Procedures — Su-24M) · В.С. Мухтаров · Издание ВВИА имени профессора Н.Е. Жуковского, 2007 · Учебное пособие (Academic Training Manual) · Для служебного пользования\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eПрактическая аэродинамика самолёта Су-24\u003c\/strong\u003e (Practical Aerodynamics of the Su-24) · Министерство обороны СССР — Военно-воздушные силы · Primary-source Soviet Air Force aerodynamics reference\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eПамятка по действиям экипажа в особых случаях в полёте — Су-24 (Су-24М)\u003c\/strong\u003e (Crew Emergency Procedures in Special Cases in Flight) · Covers both Su-24 and Su-24M variants\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eТехническое описание № 6М, Книга третья, Часть первая\u003c\/strong\u003e (Technical Description No. 6M — Book 3, Part 1) · Радиоэлектронное оборудование: Аппаратура связи и самолётовождения (Radioelectronic Equipment: Communications \u0026amp; Navigation Systems) · 1985\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eAerodynamic Architecture\u003c\/h3\u003e\n\u003cp\u003eThe Su-24 was engineered with a \u003cstrong\u003evariable-sweep wing\u003c\/strong\u003e to bridge the gap between low-altitude high-speed penetration and STOL field performance.\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eAirfoil Profile:\u003c\/strong\u003e TsAGI SR14S-5.376 at root → TsAGI SR16M-10 at tip\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eWing Sweep Presets:\u003c\/strong\u003e\n\u003cul\u003e\n\u003cli\u003e16° — Maximum span (17.64 m), maximum lift for takeoff\/landing\u003c\/li\u003e\n\u003cli\u003e35° — High-altitude cruise, fuel-efficient\u003c\/li\u003e\n\u003cli\u003e45° — Maneuvering flight and low-level tactical approach\u003c\/li\u003e\n\u003cli\u003e69° — High-speed dash, span reduced to 10.37 m, minimum drag\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eBoundary Layer Management:\u003c\/strong\u003e Fixed splitter plates and diverter channels keep inlet air clean across all sweep angles and Mach regimes\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003ePowerplant — Saturn\/Lyulka AL-21F-3A (×2)\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003eDry thrust: 75.0 kN (17,000 lbf) per engine\u003c\/li\u003e\n\u003cli\u003eAfterburner thrust: 109.8 kN (24,700 lbf) per engine\u003c\/li\u003e\n\u003cli\u003eCompression ratio: 14.5:1 · Air mass flow: 104 kg\/s\u003c\/li\u003e\n\u003cli\u003eCruise SFC (dry): ~0.86 kg\/kgf·h · Full afterburner SFC: 1.86 kg\/kgf·h\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eIntake Engineering:\u003c\/strong\u003e Variable-ramp intakes on early production deleted by engineering bulletin — combat sorties flown at low level; weight saved, maintenance simplified\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eHandling \u0026amp; Stability\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eHigh wing loading\u003c\/strong\u003e — intentional design for gust suppression and stability at high-speed, low-altitude ingress\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAll-moving horizontal stabilator\u003c\/strong\u003e — rapid pitch authority in high dynamic pressure environments\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSAU-6 Autopilot:\u003c\/strong\u003e Communicates directly with wing sweep actuators to auto-trim the stabilizer as CG shifts with sweep angle changes — seamless transition from 16° to 69°\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eAvionics — \"Puma\" Complex\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eOrion-A\u003c\/strong\u003e forward-looking attack radar (nose section)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eRelyef\u003c\/strong\u003e terrain-following radar — integrated into autopilot for hands-free terrain-hugging flight down to 60 m AGL\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSu-24M modernization:\u003c\/strong\u003e Retractable refueling probe + UPAZ-A \"Sakhalin\" buddy pod (1,200 liters\/min transfer rate)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003ePerformance Data\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\u003eEmpty Weight\u003c\/td\u003e\n\u003ctd\u003e22,300 kg (49,163 lb)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Takeoff Weight\u003c\/td\u003e\n\u003ctd\u003e43,755 kg (96,463 lb)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eInternal Fuel Capacity\u003c\/td\u003e\n\u003ctd\u003e11,100 kg (24,471 lb)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Speed (Low Altitude)\u003c\/td\u003e\n\u003ctd\u003eMach 1.35 \/ 1,550 km\/h\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Speed (High Altitude)\u003c\/td\u003e\n\u003ctd\u003eMach 2.18 \/ 2,320 km\/h (early ramp models)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eService Ceiling\u003c\/td\u003e\n\u003ctd\u003e11,000 m (36,000 ft)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Rate of Climb\u003c\/td\u003e\n\u003ctd\u003e9,000 m\/min (29,527 ft\/min)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\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 authorized distributor.\u003c\/p\u003e\n\u003cp\u003e\u003cem\u003eLiving Collections with Free Lifetime Updates — Please review our \u003ca href=\"\/pages\/disclaimer\"\u003eDisclaimer\u003c\/a\u003e and \u003ca href=\"\/pages\/export-notice\"\u003eExport Notice\u003c\/a\u003e before purchasing.\u003c\/em\u003e\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53460409909595,"sku":null,"price":29.85,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/su-24-fencer-promo-banner-banking.png?v=1782629682","url":"https:\/\/onlineaviationlibrary.com\/products\/sukhoi-su-24-fencer-flight-manual-technical-documentation","provider":"Online Aviation Library","version":"1.0","type":"link"}