aircraft technical specification - GS Finance
LET L-410 UVP-E20 · Pilot's Operating Handbook
Overview
This document provides the technical specifications and operational data for the L-410 UVP-E20 aircraft. It includes details on dimensions, weights, performance, power plant, and equipment, as well as accompanying documentation for operation and maintenance.
- The aircraft has a maximum take-off weight of 6,600 kg.
- It features a passenger compartment with 19 seats.
- The maximum speed at 10,000 ft is 386 km/hr.
- The aircraft is equipped with two Walter M 601 E engines.
- It has a maximum range of 1,318 km with wing tip tanks.
- The cockpit and passenger cabin are labeled in English and Korean.
- The aircraft includes an emergency toilet located in the rear.
- It has a maintenance schedule based on condition.
Document
Source
Originally published by gsfinance.cz. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Pilot's Operating Handbook
- File size ·
- 73 KB
- Publisher ·
- gsfinance.cz
- 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 area sqm ·
- 34.86
- Entrance door m ·
- 0.80 x 1.46
- Max cabin height m ·
- 1.66
- Max cabin diameter m ·
- 1.95
- Passenger cabin volume cubic m ·
- 17.90
Performance
- Max range km ·
- 1318
- Max speed kmh ·
- 386
- Max operating flight level m ·
- 4200
- Max technical flight level m ·
- 6100
Weight & balance
- Max payload kg ·
- 1710
- Max fuel weight kg ·
- 1000
- Max landing weight kg ·
- 6400
- Max take off weight kg ·
- 6600
- Max fuel weight with tanks kg ·
- 1300
What is the aircraft technical specification - GS Finance?
The aircraft technical specification - GS Finance is a pilot's operating handbook for the LET L-410 UVP-E20.
Where does the aircraft technical specification - GS Finance come from?
This copy of the aircraft technical specification - GS Finance was originally published by gsfinance.cz and is hosted on Sprinkle as a free, searchable reference copy.
Most owners only have the POH. Here's the essential set for the LET L-410 UVP-E20.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More LET L-410 UVP-E20manuals & documents
In this document
Dimensions
The aircraft has a wingspan of 19.980 m, a length of 14.424 m, and a height of 5.829 m.
Weights
The maximum take-off weight is 6,600 kg, and the maximum payload is 1,710 kg.
Performance
At maximum take-off weight, the aircraft can reach a maximum speed of 386 km/hr and a maximum operating flight level of 4,200 m.
Power Plant
The aircraft is powered by two Walter M 601 E engines with a maximum take-off rating of 560 kW.
Radio-Navigation and Communication Equipment
The aircraft is equipped with various navigation and communication systems including VOR, ILS, and GPS.
Accompanying Documentation
Includes technical and operational documentation such as the Airplane Flight Manual and Maintenance Manual.
Full document text
ANNEX A AIRCRAFT TECHNICAL SPECIFICATION BASIC TECHNICAL AND OPERATIONAL DATA YEAR OF PRODUCTION: NEW MODIFICATION: specification complies with the Czech Type Certificate Data Sheet No. 90-03 and Type Certificate EASA.A.026 SERIAL NUMBER: 072621 TTSN: 0 FH TLSN: 0 landings PASSENGER COMPARTMENT: 19 passenger seats with headrests and service tables, leather seat upholstery MAINTENANCE SCHEDULE: on condition PAINTING: client’s paint scheme COCKPIT LABELLING: English PASSENGER CABIN LABELLING: Korean/English TOILET: emergency, located in rear part of the aircraft BAGGAGE COMPARTMENT: standard, accessible from the inside OTHER EQUIPMENT: wing tip tanks, oxygen equipment SCOTT, VARTA batteries, ENVIRO air condition, single point refueling system DIMENSIONS: Wing span (with wing tip tanks) 19.980 m 65.55 ft Length 14.424 m 47.32 ft Height 5.829 m 19.12 ft Wing area 34.86 sq. m 375.23 sq. ft Maximum cabin diameter 1.95 m 6.40 ft Maximum cabin height 1.66 m 5.45 ft Passenger cabin volume 17.90 cu m 632 cu ft Seat pitch 0.76 M 29.94 inch Entrance door 0.80 x 1.46 M 2.6 x 4.8 ft Cargo door 1.25 x 1.46 M 4.1 x 4.8 ft Aircraft Purchase Agreement No. 78/S0400/06, Annex A page 1 of 4 WEIGHTS: Maximum take-off weight 6.600 kg 14.550 lb Maximum landing weight 6.400 kg 14.109 lb Maximum payload 1.710 kg 3.770 lb Maximum fuel weight 1.000 kg 2.205 lb (with wing tip tanks) 1.300 kg 2.866 lb PERFORMANCE (AT ISA CONDITIONS, MTOW = 6,600 KG): Maximum speed (TAS) at 10,000 ft 386 km/hr 208 knots Maximum operating flight level 4,200 m 14,000 ft Maximum technical flight level 6,100 m 20,000 ft Maximum range (45 min holding, wing tip tanks H = 10,000 ft, ISA + 15 °C) 1,318 km 711 NM POWER PLANT : TWO WALTER M 601 E ENGINES – NEW (3000 FH and 3300 cycles TBO): Maximum Take-off rating-shaft output (ISA, H = 0, v = 0, up to + 31oC) 560 kW 751 SHP Maximum continuous rating-shaft output (ISA, H = 0, v = 0) 490 kW 657 SHP Emergency rating-shaft output 595 kW 798 SHP Dry weight 198 kg 436.5 lb TWO AVIA V 510 PROPELLERS – NEW (3000 FH TBO): Number of blades 5 Propeller diameter 2.3 m 7.546 ft Sense of rotation Clockwise Speed (take-off power) 2,080 RPM Weight 94 kg 207 lb Aircraft Purchase Agreement No. 78/S0400/06, Annex A page 2 of 4 RADIO-NAVIGATION AND RADIO-COMMUNICATION EQUIPMENT: VOR / ILS /MKR KX 165 2 set MKR KR 21 2 sets ADF KR 87 1 set Gyro compass KCS 55A 2 sets DME KN 63 1 set Interphone and public address system KMA 24H 2 sets Transponder KT 70 1 set Flight data recorder BUR-1-2G+SPEEL 59 B-L 1 set Emergency location transmitter ELT 110-406 1 set Cockpit voice recorder FA 2100 1 set GPS GARMIN 155XL 1 set HF Transceiver KHF 950 - provisions for installation only TCAS II CAS 67 A – provisions for installation only Weather radar RDR 2000+KMD 550 MFD 1 set Radar Altimeter KRA 405 1 set EGPWS MARK VI 1 set Autopilot KFC 275 1 set INSTRUMENT EQUIPMENT: 1 Airspeed indicator LUN 1113.13-8 2 pcs 2 Barometric altimeter 5934 PAD-3 KEA 130 A 1 pc 1 pc 3 Encoding altimeter SAE535 2 pc 4 Rate-of-climb indicator LUN 1140.03-8 2 pcs 5 Artificial horizon LH KI 254 1 pc 6 Artificial horizon RH LUN 1205.32-8 1 pc 7 Artificial horizon Standby MCI 4300 1 pc 8 Turn-and-bank indicator UI 9551B N.541 2 pcs 9 Magnetic compass LUN 1221.1-8 1 pc 10 Torque indicator LUN 1539.02-8 2 pcs 11 Gas generator RPM indicator LUN 1347.83-8 2 pcs 12 Propeller RPM indicator LUN 1348.03-8 2 pcs 13 ITT indicator LUN 1370.08-8 2 pcs 14 Tree-pointer indicator LUN 1538.01-8 2 pcs 15 Fuel quantity indicator (main) LUN 1634.01-8 2 pcs 16 Fuel quantity indicator (wing tip) LUN 1674-8 2 pcs 17 Flow meter indicator PC 900-1 2 pcs 18 Outside air thermometer Rn 45 1 pc 19 Double pointer air thermometer LUN 5610.01-8 1 pc Aircraft Purchase Agreement No. 78/S0400/06, Annex A page 3 of 4 20 Clock ACS-1M 1 pc ACCOMPANYING DOCUMENTATION A/ TECHNICAL DOCUMENTATION 1. Aeroplane Log Book 1 book 2. Engine Log Book 2 books 3. Propeller Log Book 2 books 4. Leveling and rigging record 1 set 5. Weight and balance record 1 set 6. FDR calibration protocols 1 set 7. Protocol of the altimeters calibration 1 set 8. Flight test Protocol 1 set 9. Book of the hoses 1 book 10. List of the performed bulletins 1 set 11. Safety instructions 1 set B/ OPERATIONAL DOCUMENTATION 1. Airplane Flight manual for L 410 UVP E20 1 book 2. Master Minimum Equipment List L 410 UVP E20 1 book 3. Maintenance Manual for L 410 UVP E20 15 books 4. Maintenance Schedule for L 410 UVP E20 1 book 5. Check Lists of normal procedures L 410 UVP E20 Check Lists of emergency procedures of L 410 UVP E20 1 book 6. Wiring Manual for L 410 UVP E20 1 book 7. V 510 Propeller Operator’s, Installation and Maintenance Manual 1 book or 1 CD 8. Maintenance Manual for M 601 E Engine 1 book 9. Illustrated Spare Parts Catalogue for L 410 UVP E20 5 books 10. Illustrated Spare Parts Catalogue for WALTER M 601 E engine 1 book 11. Illustrated Spare Parts Catalogue for V 510 propeller 1 book or 1 CD 12. Check Flight Methodic 1 book BASIC EQUIPMENT FOR AIRCRAFT OPERATION AND SERVICING Specified in the Enclosure No. 1 to this Annex A. Aircraft Purchase Agreement No. 78/S0400/06, Annex A page 4 of 4