{"product_id":"let-l-410-uvp-e-turbolet-technical-documentation-engineering-dossier","title":"LET L-410 UVP-E Turbolet — Technical Documentation and Engineering Dossier","description":"\u003ch3\u003eLET L-410 UVP-E Turbolet — Technical Documentation and Engineering Dossier\u003c\/h3\u003e\n\u003cp\u003eThis living collection consolidates surviving primary-source technical documentation for the LET L-410 UVP-E Turbolet family — one of the most operationally significant short-haul twin-turboprops of the Soviet and post-Soviet era. From regional commuter routes across Siberia to mountain strips in Central Europe, the L-410 UVP-E earned its reputation through rugged STOL capability, twin-turboprop reliability, and a design envelope that tolerated extremes from −50 °C to +50 °C.\u003c\/p\u003e\n\u003cp\u003eThis dossier documents the UVP-E variant — the stretched, upgraded evolution featuring increased wingspan, dihedral refinements, Walter M601E (and M601E-21) powerplants, and the later GE H80-200 transition in the E20 sub-variant.\u003c\/p\u003e\n\u003chr\u003e\n\u003ch3\u003eUnderstanding What This Documentation Is — and Is Not\u003c\/h3\u003e\n\u003cp\u003eThese are original factory-issued technical publications produced by LET Kunovice (Aircraft Industries), not simplified guides, RC plans, or reconstructed data.\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eThey are written for licensed engineers, maintenance professionals, restoration specialists, and serious researchers — not for casual readers.\u003c\/li\u003e\n\u003cli\u003eNo airworthiness-complete documentation set for any Cold War-era commuter aircraft exists in a single archive. This dossier represents the deepest known surviving layer of primary-source documentation for the L-410 UVP-E family, drawn from multiple source streams.\u003c\/li\u003e\n\u003cli\u003eDocuments are fixed at their original publication dates and carry the signatures, stamps, and authority marks of the issuing bodies — GosNII GA, GosNII AN, UPLG GVS FS VT Russia, and the Civil Aviation Inspection of the Czech Republic.\u003c\/li\u003e\n\u003cli\u003e\u003cstrong\u003eIf you are looking for simplified plans to build a replica or an RC model, this is not the right product for you.\u003c\/strong\u003e\u003c\/li\u003e\n\u003cli\u003e\u003cstrong\u003eIf you are a researcher, restorer, museum professional, MRO engineer, or type club member who needs access to the deepest available layer of surviving primary-source factory documentation — this is it.\u003c\/strong\u003e\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eDocuments Included in This Dossier\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eDo-L410-2011.3\u003c\/strong\u003e — Руководство по Профилактическому Техническому Обслуживанию Самолёта (РПТО) \/ Preventive Maintenance Manual — L 410 UVP-Э (November 25, 1999). Approved by LET Chief Designer M. Pešak; countersigned by GosNII GA and GosNII AN; introduced by UPLG GVS FS VT Russia.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDo-L410-1222.2\u003c\/strong\u003e — Регламент Технического Обслуживания \/ Maintenance Schedule — L 410 UVP-Э без капитального ремонта (Without Overhaul) (November 25, 1999). Multi-authority approval: LET, GosNII GA, GosNII AN, and Russian aviation authority.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDo-L410-1223.2\u003c\/strong\u003e — Maintenance Schedule for the L410 UVP-E20 Aeroplane Without Overhaul. Chapter 9.7 approved by the Civil Aviation Inspection of the Czech Republic in Prague (August 31, 1995).\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDo-L410-1242.2\u003c\/strong\u003e — Wiring Manual for the L410 UVP-E, E9, and E20 Aeroplanes — Book 1. Originally issued April 30, 1987; reissued August 5, 1992 and February 28, 1995. LET Kunovice \/ Aircraft Industries.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDo-L410-1214.2\u003c\/strong\u003e — Airplane Flight Manual for the L 410 UVP-E20 — Book 1 (Sections 0 to 5). Certified to FAR 23 Amendment 34. Approved by the Civil Aviation Inspectorate of the Czech Republic (May 13, 1998). Serial No. 912533 \/ Registration D-CLED \/ Type Certificate 90-03.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ems-r05\u003c\/strong\u003e — Checklist of Emergency, Abnormal and Normal Procedures — L 410 UVP-E20. LET Kunovice.\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eDo-L410-1215.2\u003c\/strong\u003e — Airplane Flight Manual (additional flight manual document, L 410 UVP-E series).\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eAircraft Technical Overview\u003c\/h3\u003e\n\u003cp\u003e\u003cstrong\u003eAirframe \u0026amp; Aerodynamics\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eAll-metal high-wing twin-turboprop STOL commuter\u003c\/li\u003e\n\u003cli\u003eStretched fuselage with increased wingspan and dihedral modifications for spanwise lift optimisation\u003c\/li\u003e\n\u003cli\u003eDouble-slotted trailing edge flaps, automatic flaps, and spoilers for steep STOL approach profiles\u003c\/li\u003e\n\u003cli\u003eFixed wingtip fuel tanks reducing induced drag and extending stage range\u003c\/li\u003e\n\u003cli\u003eEquivalent fuselage diameter (de): approximately 2.04 m (6 ft 8.2 in)\u003c\/li\u003e\n\u003cli\u003eHorizontal tailplane MAC (cht): 1.48 m (4 ft 10.3 in)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003ePowerplant\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eWalter M601E (or M601E-21 for hot-and-high operations) free power turbine turboprops — 750 SHP \/ 559 kW MTOP per engine\u003c\/li\u003e\n\u003cli\u003eAvia V510 five-blade constant-speed, fully feathering, reversible propellers (2.3 m diameter) with autofeather\u003c\/li\u003e\n\u003cli\u003eUVP-E20 sub-variant: General Electric H80-200 engines — 597 kW driving AV-725 propellers\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eHandling \u0026amp; Systems\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eStrict CG discipline required — aft CG shift is a documented terminal stall risk on final approach\u003c\/li\u003e\n\u003cli\u003eClimatic envelope: −50 °C to +50 °C\u003c\/li\u003e\n\u003cli\u003eDual-locking aileron, elevator, and rudder trim tab controls (ref. SB 006b)\u003c\/li\u003e\n\u003cli\u003eCertified for known icing: pneumatic de-icing boots + electro-thermal propeller de-icing\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003ePerformance (EASA TCDS A.026)\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003eMTOW: 6,400–6,600 kg (14,109–14,550 lbs, variant dependent)\u003c\/li\u003e\n\u003cli\u003eMax Payload: 1,650–1,800 kg (3,637–3,968 lbs)\u003c\/li\u003e\n\u003cli\u003eMax Cruise Speed: 380 km\/h (205 KIAS \/ 219 KTAS)\u003c\/li\u003e\n\u003cli\u003eRange: 1,380–1,500 km (745–810 NM)\u003c\/li\u003e\n\u003cli\u003eService Ceiling (two engines): 4,200–6,320 m (14,000–20,735 ft)\u003c\/li\u003e\n\u003cli\u003eSingle Engine Ceiling: 4,755 m (15,600 ft at 95% MTOW)\u003c\/li\u003e\n\u003cli\u003eFuel Consumption: ~280 kg\/hour cruise\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003chr\u003e\n\u003ch3\u003eDocument Reference Index\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003eDo-L410-2011.3 — Preventive Maintenance Manual (РПТО)\u003c\/li\u003e\n\u003cli\u003eDo-L410-1222.2 — Maintenance Schedule (Without Overhaul, Russian approval)\u003c\/li\u003e\n\u003cli\u003eDo-L410-1223.2 — Maintenance Schedule (Without Overhaul, Czech approval, UVP-E20)\u003c\/li\u003e\n\u003cli\u003eDo-L410-1242.2 — Wiring Manual, Book 1 (UVP-E \/ E9 \/ E20)\u003c\/li\u003e\n\u003cli\u003eDo-L410-1214.2 — Airplane Flight Manual, Book 1 (UVP-E20, FAR 23 Am.34)\u003c\/li\u003e\n\u003cli\u003eDo-L410-1215.2 — Airplane Flight Manual (UVP-E series)\u003c\/li\u003e\n\u003cli\u003ems-r05 — Emergency, Abnormal and Normal Procedures Checklist\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 authorised distributor.\u003c\/p\u003e\n\u003cp\u003eLiving Collections with Free Lifetime Updates – Please review our Legal Notice and Export Notice before purchasing.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53931292721499,"sku":null,"price":59.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/let-l-410-uvp-e-single-aircraft-banner.png?v=1788170537","url":"https:\/\/onlineaviationlibrary.com\/products\/let-l-410-uvp-e-turbolet-technical-documentation-engineering-dossier","provider":"Online Aviation Library","version":"1.0","type":"link"}