LET L410 Aircraft

General Information

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The L 410 UVP-E20 is a well proven 19-seat turboprop commuter with outstanding flight characteristics and operational reliability, easy handling and simple maintenance. Its remarkable ~hot and high~ performance, excellent STOL capabilities, durable structure and ability to operate under extreme climatic conditions make it an excellent transportation tool.

The L 410 UVP-E20 is equally "at home" operating in the Sahara desert or the Siberian tundra. The aircraft's consistent and reliable service in an exceptionally wide range of climate conditions from dusty and dry African savannas to rainy areas of Latin America and from sea level to ~hot and high~ mountainous destinations give many operators the competition advantage they are looking for.

With its unique undercarriage, the aircraft can operate virtually anywhere, needing just a few hundred meters of airstrip with a minimum strength of 6 kg/sq cm (85 lb/sq in), being it rain-soaked grass or gravel.

The wide-bodied fuselage and best quality finish provide the highest standard of passenger comfort and allows maximum versatility and utilization of the aircraft including executive, cargo, maritime patrol, surveillance, ambulance and paratroops.

The L 410 UVP-E20 is certified on the basis of FAR 23, Amendment 34 and is accepted by EASA.

Performance

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Maximum Cruise Speed	380 km/hr TAS	208 kTAS
Maximum Range (ISA, reserves for 45 min)	1 318 km	711 NM
Cruise Altitude	4 200 m	13 800 ft
Technical Ceiling	6 100 m	20 000 ft
Take-off Distance to 35 ft
ISA, SL, MTOW	565 m	1 854 ft
ISA+15°C, SL, MTOW	655 m	2 149 ft
Landing Distance from 50 ft
ISA, SL, MLDW	425 m	1 394 ft
ISA+15°C, SL, MLDW	450 m	1 476 ft
Single Engine Service Ceiling (ISA, 95 % MTOW, climb rate 50 fpm)	4 380 m	14 370 ft
Rate of Climb at S/L both Engines	6,6 m/s	1 300 fpm
Rate of Climb at S/L one Engine	1,7 m/s	328 fpm
Power Plant - 2 x Walter M610E Turboprop, 5- blade AVIA Propeller V510
Max. Take-Off Power	560 kW	751 SHP
Max. Continuous Power	490 kW	657 SHP
Crew	2 pilots

Weights and Dimensions

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Dimensions
External
	Wing Span	19,48 m	63,91 ft
	Length	14,42 m	47,30 m
	Height	5,83 m	19,10 ft
Internal
	Max. Cabin Width	1,96 m	6,40 ft
	Max. Cabin Height	1,66 m	5,45 ft
	Passenger Cabin Volume	17,90 m³	632,00 ft³
	Passenger Capacity	17/19 seats
	Passenger Door	0.8x1.46 m	2.6x4.8 ft
	Cargo Door	1.25x1.46 m	4.1x4.8 ft
Weights
	Max. Take-off Weight	6 600 kg	14 550 lb
	Max. Landing Weight	6 400 kg	14 109 lb
	Max. Zero Fuel Weight	6 000 kg	13 228 lb
	Operational Empty Weight	4 150 kg	9 149 lb
	Maximum Payload	1 710 kg	3 770 lb
	Maximum Payload in a Special Cargo Configuration	2 000 kg	4 409 lb

Interior and Exterior

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Interior
	Wide range of colour schemes
	Comfortable seats with seat belts
	Wall-to-wall carpeting
	Curtains
	Newspaper holder
	Pilot map holders
	Toilet
	Front baggage compartment
	Rear baggage compartment
	Oxygen equipment (SCOTT)
	Passenger cabin and cockpit labelling language (-s) according to customer's choice
Optional
	Leather seats
	Variable baggage/cargo compartment
	Stewardess seat
	Seat service tables
	Kitchenette
	Air-condition (ENVIRO)
	Flushable toilet
	Executive conversion kit
	Cargo conversion kit (1700 kg payload)
	Ambulance conversion kit
Exterior
	Wing tip tanks
	Wide choice of external paint schemes
	Labelling language (-s) according to customer's choice
Optional
	Fin lighting / tail surface lighting

Avionics and Instruments

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Standard

Avionics
	Bendix/King SILVER Crown
	NAV/COM/GS	KX 165	2 sets
	MKR	KR 21	1 set
	ADF	KR 87	2 sets
	Gyro compass	KCS 55A	2 sets
	DME	KN 63	1 set
	VHF Transceiver	integrated in NAV/COM/GS
	Interphone and PA system	KMA 24H70	2 sets
	Transponder	KT 70	1 set
	Flight data recorder	BUR 1-2G + SPEEL 59BL	1 set
	Cockpit voice recorder	FA 2100	1 set
	Emergency location transmitter	ARTEX 110-406	1 set
	GPS	Garmin 155 XL	1 set
	EGPWS	MARK VI	1 set
	Radio altimeter	KRA 405 B	1 set
	TCAS II	ACAS 67A full provision only
	HF radio	KHF 950 full provision only
	Weather radar w MFD	RDR 2000 + KMD 550	1 set

Instrument equipment
	Airspeed indicator	LUN 1113.13-8	2 pcs
	Barometric altimeter	5934 PAD-3 (1 pc*)	2 pcs
	Encoding altimeter	KEA 130 A (*)	1 pcs
	Encoding altimeter	SAE 5-35 (1 pc*)	2 pcs
	Rate-of-climb indicator	LUN 1140.03-8	2 pcs
	Artifical horizon LH	LUN 1205.32-8 (or KI 254 *)	1 pc
	Artifical horizon RH	LUN 1205.32-8	1 pc
	Artifical horizon standby	MCI 4300	1 pc
	Turn-and-bank indicator	UI 9551B N.541	2 pcs
	Magnetic compass	LUN 1221.1-8	1 pc
	Torque indicator	LUN 1539.02-8	2 pcs
	Gas generator RPM indicator	LUN 1347.03-8	2 pcs
	Propeller RPM indicator	LUN 1348.03-8	2 pcs
	ITT indicator	LUN 1370.02-8	2 pcs
	Three-pointer indicator	LUN 1538.09-8	2 pcs
	Fuel quantity indicator (main)	LUN 1634.81-8	2 pcs
	Fuel quantity indicator (wing tip)	LUN 1674.81-8	2 pcs
	Flowmeter indicator	PC 900-1	2 pcs
	Outside air thermometer	Rn 45	1 pc
	Double pointer air thermometer	LUN 5610.01-8	1 pc
	Clock	ACS-1MK	1 pc
	( * ) when KFC 275 autopilot is installed

Options

	HF Transceiver	KHF 950
	Transponder 2 + Encoding altimeter 2	KT 70 + KEA 130 (A)
	Radio altimeter 2	KRA 405B
	Autopilot	KFC 275
	TCAS II	B/K CAS 67A + MST 67 + converter

Engines and Propellers

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Engines
	Manufacturer	Walter Engines
	Model	Walter M 601-E
	Maximum take-off power	560 kW - 751 SHP
	Maximum continuous power	490 kW - 657 SHP
	Weight	200 kg (441 lb)
	TBO	3,000 flight hours
Propellers
	Manufacturer	Avia Propeller
	Model	V 510
	Number of blades	5
	TBO	3,000 flight hours

Type Certificates

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EASA.A.026
71-04	Czech Republic
14/90	Sweden
EA-9401	Brazil
72-0341-1 LS/ps	Denmark
AV-9703	Argentina
5VT9800015	Philippines
A-02	Chile
1-99	Cuba
2067	Germany
A204	Australia
A048	Indonesia
Recognition letter 727-2006-MTC/12.04	Peru
Registration letter ZS-OBS	South Africa

The L 410 UVP-E20 is certified on the basis of FAR 23, Amendment 34.

Configurations

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Standard 17/19 Seat Commuter
Executive Version
Cargo Version
Extendable Cargo Module
Flying Ambulance Version
Paratroop Version