{"product_id":"yakovlev-yak-50-technical-dossier-flight-manuals-english","title":"Yakovlev Yak-50 — Technical Dossier \u0026 Flight Manuals (English)","description":"\u003cp\u003eThe Yakovlev Yak-50 is a legendary Soviet-era, single-seat all-metal aerobatic monoplane celebrated for its exceptional power-to-weight ratio and dominant history in world aerobatics.\u003c\/p\u003e\u003cp\u003eThis technical dossier compiles verified data across aerodynamic reports, engine specifications, handling profiles, performance limits, and essential airworthiness engineering bulletins.\u003c\/p\u003e\u003ch2\u003eManuals Included in This Collection\u003c\/h2\u003e\u003cul\u003e\n\u003cli\u003eYak-50 — Flight Manual (A. Yakovlev, original Soviet edition)\u003c\/li\u003e\n\u003cli\u003eYak-50 — Pilots Operating Handbook \u0026amp; Airplane Flight Manual (English)\u003c\/li\u003e\n\u003cli\u003eYak-50 Aircraft with M-14P Engine — Technical Description\u003c\/li\u003e\n\u003cli\u003eYak-50 Aircraft with M-14P Engine — Scheduled Maintenance Manual\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch2\u003eTechnical Specifications \u0026amp; Performance\u003c\/h2\u003e\u003cp\u003eThe core flight profile parameters and performance limitations originate directly from official flight test documentation and civilian validation standards.\u003c\/p\u003e\u003ctable\u003e\n\u003cthead\u003e\u003ctr\u003e\n\u003cth\u003eParameter\u003c\/th\u003e\n\u003cth\u003eMetric Value\u003c\/th\u003e\n\u003cth\u003eImperial Value\u003c\/th\u003e\n\u003c\/tr\u003e\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eNever Exceed Speed (V\u003csub\u003eNE\u003c\/sub\u003e)\u003c\/td\u003e\n\u003ctd\u003e450 km\/h\u003c\/td\u003e\n\u003ctd\u003e243 knots \/ 280 mph\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Maneuvering Speed (V\u003csub\u003eA\u003c\/sub\u003e)\u003c\/td\u003e\n\u003ctd\u003e400 km\/h\u003c\/td\u003e\n\u003ctd\u003e216 knots \/ 249 mph\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eStall Speed (V\u003csub\u003eS\u003c\/sub\u003e)\u003c\/td\u003e\n\u003ctd\u003e100 km\/h\u003c\/td\u003e\n\u003ctd\u003e54 knots \/ 62 mph\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eInitial Climb Rate\u003c\/td\u003e\n\u003ctd\u003e16.0 m\/s\u003c\/td\u003e\n\u003ctd\u003e3,145 ft\/min\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eTakeoff \/ Landing Roll\u003c\/td\u003e\n\u003ctd\u003e100 m \/ 250 m\u003c\/td\u003e\n\u003ctd\u003e328 ft \/ 820 ft\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eEmpty Weight\u003c\/td\u003e\n\u003ctd\u003e750–775 kg\u003c\/td\u003e\n\u003ctd\u003e1,653–1,709 lbs\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Takeoff Weight (MTOW)\u003c\/td\u003e\n\u003ctd\u003e910 kg\u003c\/td\u003e\n\u003ctd\u003e2,006 lbs\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eLoad Factor Limits\u003c\/td\u003e\n\u003ctd\u003e+9.0 G \/ -6.0 G\u003c\/td\u003e\n\u003ctd\u003eDependent on tankage\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\u003ch2\u003eEngine Technical Notes: Vedeneyev M-14P\u003c\/h2\u003e\u003cp\u003eThe Yak-50 is built entirely around its power plant: a 9-cylinder, supercharged, air-cooled radial engine driving a V530TA-D35 two-bladed constant-speed propeller.\u003c\/p\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003ePower Output:\u003c\/strong\u003e 360 horsepower base variant (modifiable with 400 hp M-14PF or 451 hp M-14R).\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAviation Pneumatics:\u003c\/strong\u003e Pneumatic starting and gear retraction system pressurized to 720 psi via a dedicated engine-driven air compressor.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eInverted Flight Capability:\u003c\/strong\u003e Built-in flop-tube mechanism within the main fuel tank, allowing full inverted engine fuel feed for a maximum of 1.5 minutes.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eOperational Limits:\u003c\/strong\u003e Maximum continuous power at 82% RPM, normal intake manifold air pressure of +95 ± 15 mm Hg.\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch2\u003eHandling \u0026amp; Stability Studies\u003c\/h2\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eControl Harmonization:\u003c\/strong\u003e Fabric-covered control surfaces minimize tail weight, producing high control authority. Symmetrical direct and inverted figure radiuses are nearly identical.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eRoll Dynamics:\u003c\/strong\u003e Roll rate varies between 120° and 200° per second depending on entry airspeed. Gyroscopic engine torque causes rolls to snap noticeably faster to the right.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCrosswind Limit:\u003c\/strong\u003e 12 km\/h (7 knots) maximum crosswind component per flight manual.\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch2\u003eEngineering \u0026amp; Service Bulletins\u003c\/h2\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eStructural Fatigue Lifing:\u003c\/strong\u003e Base airframe life 300 hours; mandatory NDT inspections every 100 hours thereafter. Aerobatic figures must be logged for fatigue cycle indexing.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eFuselage Welds:\u003c\/strong\u003e Longeron Cracking Check — mandatory inspection of top fuselage longeron intersection points forward of the instrument panel.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eEngine TBO:\u003c\/strong\u003e 750 hours first lifecycle; subsequent 500-hour intervals; maximum total engineering limit 2,250 hours.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eMaintenance Framework:\u003c\/strong\u003e Bulletins 66BE through 86BE govern torque settings and lubrication schedules.\u003c\/li\u003e\n\u003c\/ul\u003e\u003chr\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.\u003cbr\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":53513832694107,"sku":null,"price":35.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/yak-50-banner-head-on.png?v=1783259956","url":"https:\/\/onlineaviationlibrary.com\/products\/yakovlev-yak-50-technical-dossier-flight-manuals-english","provider":"Online Aviation Library","version":"1.0","type":"link"}