{"product_id":"sukhoi-su-27sk-flanker-flight-manual-technical-documentation","title":"Sukhoi Su-27SK Flanker — Flight Manual \u0026 Technical Documentation Collection","description":"\u003ch3\u003eSukhoi Su-27SK Flanker — Primary-Source Flight \u0026amp; Technical Documentation\u003c\/h3\u003e\n\u003cp\u003eThe \u003cstrong\u003eSukhoi Su-27SK\u003c\/strong\u003e is one of the most capable air-superiority fighters ever produced — a cornerstone of Soviet and post-Soviet aviation, engineered for extreme agility, long-range intercept, and sustained air dominance. This collection brings together original factory and military-issue documentation covering the Su-27SK across flight operations, technical exploitation, avionics, and electronic warfare systems.\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eDocument Manifest\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eСамолет СУ-27СК — Руководство по летной эксплуатации, Книга 1\u003c\/strong\u003e (Flight Manual, Book 1 — Russian original) · Declassified per KNAAPO letter № 1\/416, 24.02.2004\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSu-27SK Flight Manual — Book 1 \u0026amp; Book 2\u003c\/strong\u003e (English translation)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSu-27SK — Manual de Operaciones de Vuelo, Libro 1\u003c\/strong\u003e (Spanish edition)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eСамолет СУ-27СК — Руководство по технической эксплуатации № 10СК, Книга 6, Часть 2\u003c\/strong\u003e · Radioelectronic Equipment: IFF Systems, Radio Communications, Weapons System Control, Guidance Command Reception\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eСамолет СУ-27СК — Руководство по технической эксплуатации № 10СК, Книга 6, Часть 8\u003c\/strong\u003e · Gardeniya ECM Pod — Airborne Active Jamming Station · Description \u0026amp; Operation\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eEnglish-Russian Dictionary of Civil Aviation\u003c\/strong\u003e (Англо-Русский Словарь по Гражданской Авиации) — essential reference for Russian document interpretation\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eTechnical Profile — Aerodynamic \u0026amp; Systems Overview\u003c\/h3\u003e\n\u003cp\u003eThe Su-27 utilizes a deeply integrated \u003cstrong\u003eblended wing-body (BWB)\u003c\/strong\u003e configuration, where the fuselage semi-monocoque structure transitions seamlessly into low-aspect-ratio trapezoidal wings. The entire fuselage generates additional aerodynamic lift, significantly enhancing effective wing area without scaling wingspan. Long \u003cstrong\u003eLeading-Edge Root Extensions (LERX)\u003c\/strong\u003e generate high-energy vortices at high angles of attack, ensuring continuous airflow attachment and delaying stall behavior.\u003c\/p\u003e\n\u003ch4\u003ePowerplant — Lyulka-Saturn AL-31F\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003eDry thrust: ~16,700 lbs per engine\u003c\/li\u003e\n\u003cli\u003eAfterburner thrust: ~27,560 lbs per engine\u003c\/li\u003e\n\u003cli\u003eVariable-geometry intake ramps with boundary-layer bleeding suppress supersonic shock oscillations\u003c\/li\u003e\n\u003cli\u003eRetractable titanium FOD mesh screens protect compressor faces during ground operations\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch4\u003eFly-By-Wire \u0026amp; Stability\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eSDU-10 quad-channel analog FBW\u003c\/strong\u003e — continuously dampens flight movements, prevents exceedance of structural design envelopes\u003c\/li\u003e\n\u003cli\u003eRelaxed static stability: aerodynamic center forward of CG under subsonic conditions — inherently unstable by design\u003c\/li\u003e\n\u003cli\u003eEnables controlled post-stall maneuvers including \u003cstrong\u003ePugachev's Cobra\u003c\/strong\u003e (dynamic pitch up to 120°)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch4\u003ePerformance Data\u003c\/h4\u003e\n\u003cul\u003e\n\u003cli\u003eMaximum Speed (High Altitude): Mach 2.35 \/ 2,500 km\/h\u003c\/li\u003e\n\u003cli\u003eMaximum Speed (Sea Level): Mach 1.13 \/ 1,400 km\/h\u003c\/li\u003e\n\u003cli\u003eService Ceiling: 19,000 m (62,335 ft)\u003c\/li\u003e\n\u003cli\u003eMaximum Rate of Climb: 300 m\/s (59,000 ft\/min)\u003c\/li\u003e\n\u003cli\u003eFerry Range: 3,530 km (1,910 nmi)\u003c\/li\u003e\n\u003cli\u003eMaximum Instantaneous Turn Rate: 28°\/sec\u003c\/li\u003e\n\u003cli\u003eStructural G-Limits: +9.0g \/ −3.0g\u003c\/li\u003e\n\u003c\/ul\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":53460403880283,"sku":null,"price":34.85,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/su-27sk-promo-banner-landing.png?v=1782628759","url":"https:\/\/onlineaviationlibrary.com\/products\/sukhoi-su-27sk-flanker-flight-manual-technical-documentation","provider":"Online Aviation Library","version":"1.0","type":"link"}