{"product_id":"petlyakov-pe-2-soviet-wartime-technical-manual-collection","title":"Petlyakov Pe-2 — Soviet Wartime Technical Manual Collection","description":"\u003ch3\u003ePetlyakov Pe-2 \"Peshka\" — Primary-Source Soviet Wartime Documentation\u003c\/h3\u003e\n\u003cp\u003eThe Petlyakov Pe-2 \"Peshka\" was the primary Soviet twin-engine dive bomber of World War II, praised for its advanced all-metal construction but notoriously demanding to fly. Originally conceived as the high-altitude, pressurized VI-100 interceptor, it was aggressively redesigned into a tactical bomber within a 45-day window — one of the most remarkable engineering pivots of the war.\u003c\/p\u003e\n\u003cp\u003eThis collection brings together original Soviet Air Force (VVS) technical publications, compiled from historical NII VVS (Soviet Air Force Scientific Research Institute) test records and factory-issued manuals spanning 1941–1945.\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eDocument Manifest — 6 Original Soviet Publications\u003c\/h3\u003e\n\u003col\u003e\n\u003cli\u003e\n\u003cstrong\u003eСамолет Пе-2 — Инструкция Авиамеханику\u003c\/strong\u003e\u003cbr\u003ePe-2 Aircraft — Mechanic's Instruction Manual\u003cbr\u003eIssued by: Directorate of the Red Army Air Forces (VVS) — Military Publishing House, NKO — 1943\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eИнструкция по Техническому Обслуживанию Самолета Пе-2\u003c\/strong\u003e\u003cbr\u003eTechnical Servicing Instruction for the Pe-2 Aircraft\u003cbr\u003eIssued by: Directorate of the Red Army Air Forces (VVS) — Military Publishing House, NKO — 1943\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eИнструкция по Технической Эксплоатации Самолета ПЕ-2\u003c\/strong\u003e\u003cbr\u003eTechnical Operation Instruction for the Pe-2 Aircraft\u003cbr\u003eIssued by: Main Directorate of the Red Army Air Forces (RKKA) — Voenizdat NKO USSR — 1941 — Copy No. 878 — For Official Use Only\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eСамолет Пе-2 — Летно-Тактические Данные\u003c\/strong\u003e\u003cbr\u003ePe-2 Aircraft — Flight-Tactical Data\u003cbr\u003e1944\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eСамолет Пе-2 — Описание Конструкции, Издание Шестое\u003c\/strong\u003e\u003cbr\u003ePe-2 Aircraft — Structural Description, 6th Edition (Revised and Expanded)\u003cbr\u003eEdited by Eng. D.P. Soloukhin — Approved by Chief Engineer, 10th Main Directorate NKAP — NKAP-USSR, State Publishing House of the Defence Industry, Moscow — 1945\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eТехническое Описание Самолета Пе-2, Часть II\u003c\/strong\u003e\u003cbr\u003eTechnical Description of the Pe-2 Aircraft, Part II\u003cbr\u003eFactory Edition — Moscow — 1941 — For Official Use Only\u003c\/li\u003e\n\u003c\/ol\u003e\n\u003chr\u003e\n\u003ch3\u003eAerodynamic Configuration\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eConfiguration:\u003c\/strong\u003e Low-wing monoplane with an exceptionally clean aerodynamic profile and twin-tail (dihedral stabilizer) layout, maximizing the rear gunner's field of fire.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDrag Reduction:\u003c\/strong\u003e Main landing gear retracted rearward directly into the engine nacelles. Later batches incorporated low-drag ducting for the oil coolers, smoothly fairing them into the lower engine cowlings to offset speed losses from military equipment additions.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDive Braking:\u003c\/strong\u003e Electrically operated, slatted \"trellis\" dive brakes mounted beneath the outer wing panels. When deployed, they stabilized diving speeds between 400–480 km\/h, permitting steep dive angles up to 70°.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eEngine Technical Notes\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003ePowerplants:\u003c\/strong\u003e Two Klimov M-105 (later VK-105) liquid-cooled V12 engines.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eEvolution:\u003c\/strong\u003e Early production used the M-105R (1,100 hp); mid-to-late variants upgraded to the VK-105PF (1,210 hp), optimized for higher boost pressures at lower and medium tactical altitudes.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eOperational Rules:\u003c\/strong\u003e Mixture controls required strict monitoring — 50% mixture for low-throttle ground operations, 75–80% for full-throttle combat or takeoff to avoid engine detonation.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePropeller Pitch:\u003c\/strong\u003e VISh-61 series constant-speed propellers regulated by viscous hydraulic actuators. Engine failure required manual override pitch adjustment to feather blades and minimize asymmetric windmilling drag.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eHandling \u0026amp; Stability\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eHigh Workload:\u003c\/strong\u003e Heavy, highly responsive aircraft with stiff controls requiring substantial physical effort during high-G dive pull-outs.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDirectional Stability:\u003c\/strong\u003e No tailwheel lock mechanism — the rear assembly rotated freely, making the Pe-2 highly susceptible to ground looping. Pilots required precise, aggressive rudder corrections during takeoffs and high-speed landings.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eStall Characteristics:\u003c\/strong\u003e Thin wing profile caused sharp, unforgiving stalling behavior. Below 200–210 km\/h with flaps up, the aircraft would abruptly drop a wing and frequently enter a spin with minimal warning.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eSingle-Engine Asymmetry:\u003c\/strong\u003e Engine failure below 15 metres required immediate action: maintain heading, jettison all ordnance, and force a wheels-up landing straight ahead to prevent catastrophic asymmetric roll.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003ePerformance Data\u003c\/h3\u003e\n\u003ctable\u003e\n\u003cthead\u003e\n\u003ctr\u003e\n\u003cth\u003eParameter\u003c\/th\u003e\n\u003cth\u003ePe-2 Standard (Early Series)\u003c\/th\u003e\n\u003cth\u003ePe-2 FT (VK-105PF)\u003c\/th\u003e\n\u003c\/tr\u003e\n\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Speed\u003c\/td\u003e\n\u003ctd\u003e540 km\/h at 5,000 m\u003c\/td\u003e\n\u003ctd\u003e555 km\/h at 4,000 m\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eSea Level Speed\u003c\/td\u003e\n\u003ctd\u003e451 km\/h\u003c\/td\u003e\n\u003ctd\u003e460 km\/h\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eService Ceiling\u003c\/td\u003e\n\u003ctd\u003e8,800 m\u003c\/td\u003e\n\u003ctd\u003e8,900 m\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eTime to 5,000 m\u003c\/td\u003e\n\u003ctd\u003e7.0 min\u003c\/td\u003e\n\u003ctd\u003e7.0 min\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eCombat Range\u003c\/td\u003e\n\u003ctd\u003e1,315 km\u003c\/td\u003e\n\u003ctd\u003e1,330 km\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eEmpty Weight\u003c\/td\u003e\n\u003ctd\u003e5,950 kg\u003c\/td\u003e\n\u003ctd\u003e6,000 kg\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax Takeoff Weight\u003c\/td\u003e\n\u003ctd\u003e7,600 kg\u003c\/td\u003e\n\u003ctd\u003e7,800 kg\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\n\u003chr\u003e\n\u003ch3\u003eEngineering Bulletins\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eElectrical Actuation:\u003c\/strong\u003e Unlike contemporary Soviet designs relying on pneumatic systems, the Pe-2 utilized over 50 electric servomotors driving fuel pumps, landing gear, flaps, radiators, and dive brakes — a highly advanced architecture for its era.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eStructural Reinforcement:\u003c\/strong\u003e Transition from the VI-100 interceptor to the dive-bomber variant required dramatic reinforcement of wing spars and skin panels around fuselage joints to absorb intense G-loads during dive recoveries.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eThe M-82 Variant Failure:\u003c\/strong\u003e In 1942–1943, an engineering push attempted to fit Shvetsov M-82 radial engines to bypass inline engine shortages. Bulletins confirmed poor reliability, high vibration, and chronic cold-weather engine stalling at altitude — the project was cancelled after only 32 units.\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\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⚠️ \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\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":53510035669339,"sku":null,"price":30.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/banner-4-pe-2-square-snow.png?v=1783179628","url":"https:\/\/onlineaviationlibrary.com\/products\/petlyakov-pe-2-soviet-wartime-technical-manual-collection","provider":"Online Aviation Library","version":"1.0","type":"link"}