L410 UVP-E20 AIRPLANE #2
LET L-410 UVP-E · Maintenance Manual
Overview
This document provides maintenance information for the L-410 UVP-E20 aircraft, including technical specifications, maintenance schedules, and operational documentation. It outlines the aircraft's components, their time between overhauls (TBOs), and various performance metrics.
- The L-410 UVP-E20 has a maximum take-off weight of 6,600 kg.
- It features a passenger cabin with seating for up to 19 passengers.
- The aircraft is powered by two GE M601E engines.
- The maximum cruise speed is 386 km/h at 10,000 feet.
- The service ceiling is 4,200 m.
- The aircraft includes oxygen equipment for passengers and pilots.
- Maintenance documentation includes a Maintenance Manual and Inspection Manual.
- The aircraft has a wing span of 19.980 m.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at aircraft24.de. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Maintenance Manual
- Year ·
- 2013
- File size ·
- 402 KB
- Copy found at ·
- aircraft24.de
- Language ·
- en
Specifications & performance
Extracted from this document.
Specifications
- Height m ·
- 5.829
- Length m ·
- 14.424
- Wing span m ·
- 19.980
- Cargo door m ·
- 1.25 x 1.46
- Seat pitch m ·
- 0.76
- Wing surface m2 ·
- 34.86
- Passenger door m ·
- 0.80 x 1.46
- Max cabin height m ·
- 1.66
- Max cabin diameter m ·
- 1.95
- Passenger cabin volume m3 ·
- 17.90
Performance
- Service ceiling m ·
- 4200
- Max cruise speed kmh ·
- 386
Weight & balance
- Mtow kg ·
- 6600
- Max landing weight kg ·
- 6400
- Max fuel weight with tip tanks kg ·
- 1300
- Max fuel weight without tip tanks kg ·
- 1000
What is the L410 UVP-E20 AIRPLANE #2?
The L410 UVP-E20 AIRPLANE #2 is a maintenance manual for the LET L-410 UVP-E, dated 2013.
What year was the L410 UVP-E20 AIRPLANE #2 published?
The L410 UVP-E20 AIRPLANE #2 — the LET L-410 UVP-E maintenance manual on file — is dated 2013.
Common. More common than 87% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the LET L-410 UVP-E.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
LET L-410 UVP-E for sale now
Free — save the L-410 to your watchlist and track it in one place.
More LET L-410 UVP-Emanuals & documents
Related documents
- AEROPRAKT-22LS Airplane Maintenance ManualAEROPRAKT LTD A-22 LS · Maintenance Manual
- AEROPRAKT-22LS Airplane Maintenance ManualAEROPRAKT LTD A-22 LS · Maintenance Manual
- AEROPRAKT-32 Airplane Maintenance ManualAEROPRAKT LTD A-32 · Maintenance Manual
- maintenance manual - dv-1 skylarkDOVA DV-1 Skylark · Maintenance Manual
- AEROPRAKT-A32 Airplane Maintenance Manual A32-060-AMMAEROPRAKT LTD A-32 · Maintenance Manual
If you fly the LET L-410 UVP-E, you may also be researching these.
In this document
Technical Specification
Details the aircraft's year of manufacture, modification type, passenger cabin configuration, and equipment.
Main Parameters
Lists dimensions, weights, and performance metrics including maximum take-off weight and cruise speed.
Power Plant
Describes the engines and propellers, including their specifications and maintenance intervals.
Flight Instrument and Radio Communication
Outlines the electronic systems and instruments used for flight indication and communication.
Airplane Interior for 19 Passengers
Describes the interior layout and accompanying documentation for passenger safety and operational procedures.
Operational Documentation
Lists various manuals and documents required for the operation and maintenance of the aircraft.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Full document text
L410 UVP-E20 AIRPLANE #2 Main components’ TBOs as on 19th of September 2018 Unit TBO Remaining Airframe 20 000 hours/ 20 000 landings 12 017 / 14 739 Main gear strut left 16 000 landings 10 739 Main gear strut right 16 000 landings 10 739 Main gear strut front 10 000 landings 4 739 Unit TBO Remaining Engine GE M601E with water inject 3 000 hours / 6 600 cycles 3 000 / 6 600 Engine GE M601E with water inject 3 000 hours / 6 600 cycles 3 000 / 6 600 Propeller V510 3 500 hours / 72 months 3 500 hours / 72 months Propeller V510 3 500 hours / 72 months 3 500 hours / 72 months TECHNICAL SPECIFICATION L410 UVP-E20 AIRPLANE #2 YOM: 2013 MODIFICATION: L 410 UVP–E20 PASSENGER CABIN: 19/17/15 passenger seats without tables with head cushions, cloth seat covering. Mountable additional rear luggage compartment for 215 or 330 kg. Improved toilet in the rear part of the airplane. LANGUAGE OF DECALS IN COCKPIT: English. LANGUAGE OF OUTER MARKING: For passengers - Russian; For operational information – English/Russian. LANGUAGE OF DECALS IN PASSENGER CABIN: English/Russian. TECHNICAL MAINTENANCE: Being operated without general overhaul. EQUIPMENT \ ACCESSOIRES: Oxygen equipment Avox (4 balloons, 2 balloons for pilots (1 balloon for each) and 2 balloons for passengers. Main accumulator VARTA (HAWKER). Tip tanks MAIN PARAMETERS: DIMENSIONS: Wing span (including fuel tip tanks) 19.980 m 65.55 feet Length 14.424 m 47.32 feet Height 5.829 m 19.12 feet Wing surface 34.86 m2 375.23 feet2 Maximal cabin diameter 1.95 m 6.40 feet Maximal cabin height 1.66 m 5.45 feet Passenger cabin volume 17.90 м3 632 feet3 Seat pitch 0.76 m 29.94 inches Passenger door 0.80 x 1.46 m 2.6 x 4.8 feet Cargo door 1.25 x 1.46 m 4.1 x 4.8 feet WEIGHTS: Max. allowed take-off weight (MTOW) 6.600 kg 14.109 pounds Max. allowed landing weight 6.400 kg 13.668 pounds Maximal fuel weight (without fuel in tip tanks) 1.000 kg 2.205 pounds Maximal fuel weight (with fuel in tip tanks) 1.300 kg 2.866 pounds PERFORMANCE (6.600 kg): Maximal cruise speed (TAS) at altitude 10,000 feet 386 km/h 208 knots Service ceiling 4,200 m 14,000 feet POWER PLANT: Engines GE М601E (3 000 – flight hours or 6 600 cycles between overhauls): Maximal take-off output on shaft (ISA, H=0,v=0) 560 kW 751 SHP Maximal output on shaft in constant working regime (ISA, H=0,v=0) 490 kW 657 SHP Maximal output on shaft in emergency working mode 595 kW 798 SHP Weight of dry engine 198 kg 436.5 pounds Propellers AVIA V510 (3 500 flight hours between overhauls): Number of blades 5 pcs Propeller diameter 2.3 м 7.546 feet Direction of rotation CW Rotation speed (take-off output) 2,080 rpm Weight 94 kg 207 pounds FLIGHT INSTRUMENT AND RADIO COMMUNICATION 1 Electronical sytem for flight indication EFI-890R 2 sets 2 AHRS AHS-1000A 2 sets 3 Indication system for flight parameters AC32.10.21.11.AF 2 sets 4 NAV/ COM/ GPS GNS 430 W 2 sets 5 MKR - marker KMR 675 1 set 6 ADF – Radio compass KR 87 2 sets 7 DME KDM 706A 1 set 8 Communication device and situational awareness system KMA 24H-70 2 sets 9 Radar beacon transponder I MST 67A 1 set 10 Radar beacon transponder II GTX 330 D 1 set 11 Flight data recorder FA 2200 1 set 12 Emergency location transmitter ELT C406-2 1 set 13 Cockpit voice recorder FA 2100 1 set 14 Weather radar RDR 2000 1 set 15 Radioaltimeter KRA 405B 1 set 16 EGPWS MARK VI 1 set 17 Portative emergency locator beacon АRM-406АS1 1 set 18 Autopilot KFC 325 1 set 19 Air traffic awareness system TCAS II Prepared for installation INSTRUMENTATION SYSTEM: 1 Speed indicator - spare 5A16 или LUN 1106.K5Bx 1 set 2 Barometric pressure altimeter - spare 3A62 1 set 3 Aвиагоризонт - запасной 4300-412 or LUN 1241.D8D5R 1 set 4 Магнитный компас 5LUN 1224-8 1 set 5 Указатель крутящего момента LUN 1539.02-8 2 sets 6 Указатель оборотов газогенератора LUN 1347.83-8 2 sets 7 Указатель обор. воздушного винта LUN 1348.03-8 2 sets 8 Указатель температуры между турбинами LUN 1370.08-8 2 sets 9 Three-arrow indicator LUN 1538.01-8 2 sets 10 Fuel level indicator (main) LUN 1634.01-8 2 sets 11 Tip tank fuel fuel level indicator LUN 1674-8 2 sets 12 Fuel level indicator PC 900-1 2 sets 13 Two-arrow indicator of air temperature LUN 5610.01-8 1 set 14 Clock 115EG-7780 2 sets AIRPLANE INTERIOR FOR 19 PASSENGERS: ACCOMPANYING DOCUMENTS (originals in English with translation into Russian): A/ TECHNICAL DOCUMETATION 1. Airplane logbook 1 book 2. Engine logbook 2 books 3. Propeller logbook 2 books 4. Passports and Certificates for aggregates/instruments 5 sets 5. Book of hoses 1 book 6. Protocol of aircraft rigging 1 set 7. Protocol of aircraft weight and balance 1 set 8. Protocols of calibration of recording of flight data 1 set 9. Protocol of system check EFI-890R 1 set 10. Protocol of calibration of spare altimeter 1 set 11. Protocol of final test flight 1 set 12. Instructions for safety of passengers 1 set B/ OPERATIONAL DOCUMENTATION 1. Airplane Flight Manual for the L 410 UVP E-20 1 book Russian translation: Airplane Flight Manual for the L 410 UVP E-20 1 book 2. Checklist of Emergency, Abnormal and Normal procedures L 410 UVP – E20 1 CD Russian translation: Checklist of Emergency, Abnormal and Normal procedures L 410 UVP – E20 1 book 3. Master Minimum Equipment List L 410 UVP-E, E9, E20 1 CD Russian translation: Master Minimum Equipment List L 410 UVP-E E20 1 book 4. Maintenance Manual for for the L 410 UVP-E, E9, E20 aeroplane 1 CD Russian translation: Maintenance Manual for for the L 410 UVP-E20 aeroplane 7 books 5. Maintenance Schedule for the L 410 UVP-E20 Aeroplane without overhaul 1 CD Russian translation: Maintenance Schedule for the L 410 UVP-E20 1 book 6. Inspection Manual for the L 410 UVP-E, E9, E20 1 CD Russian translation: Inspection Manual for the L 410 UVP-E 1 book 7. Wiring Manual for the L 410 UVP-E, E9, E20 aeroplane 1 CD Russian translation: Wiring Manual for the L 410 UVP-E20 2 books 8. V 510 (E-1500) Operation And Installation Manual 1 CD
Show full textShow less
Russian translation: V 510 Operation And Installation Manual 9. Мaintenance Manual Turboprop Engine Model GE M601E (No. 1) 1 СD Russian translation: Мaintenance Manual Turboprop Engine Model GE M601E (No. 2) 10. Ground and flight check procedures for the L 410 UVP-E, E9, E20 1 book Russian translation: Ground and flight check procedures 1 book 11. Illustrated Parts Catalogue for L 410 UVP-E20 Aeroplane 1 CD 12. Repair Manual for the L 410 UVP-E20 1 CD Russian translation: Repair Manual for the L 410 in field conditions 1 book 13. List of performed mandatory bulletins 1 set Russian translation: List of performed mandatory bulletins 1 set 14. Program for decoding of flight data «ROSE» 1 CD