Let L-410 UVP-E9 Turbolet

Let Kunovice

ICAOL410IATAL4T
Let L-410 UVP-E9 Turbolet aircraft
Let KunoviceLet L-410 Turbolet

Photograph of the Let L-410 Turbolet family. No photograph on Wikimedia Commons identifies this variant specifically.

Photo: AlfvanBeem · CC0 · Modified

About

A UVP-E cleared to 6,600 kg, 200 kg above the UVP-E, on the same airframe and the same M601E engines. Its section of the certificate gives no zero fuel weight at all. The cruise speed, range, ceiling, climb rate and take-off distance are EUROCONTROL's figures for the L410 type code rather than a certificate's: a type certificate states limits and weights, not cruise performance, and the source does not distinguish sub-variants.

Weightscompared to Airbus A318

MRW (Maximum Ramp Weight)

6,620kg
0
25k
50k
68k

MTOW (Maximum Takeoff Weight)

6,600kg
0
25k
50k
68k

MLW (Maximum Landing Weight)

6,400kg
0
25k
50k
56k

Capacitycompared to Airbus A318

Passenger Capacity

19passengers
0
100
132

14% of A318 maximum capacity

Crew

Total
2
Cockpit
2

Dimensions

Length

14.5m

Wingspan

20.0m

Height

5.8m

Wing Area

35.2m²

Engine Specifications

Engine Count

2×

Engine Model

Walter M601E turboprop

Production & History

Production Status

Out of production

Business jets and the API are coming

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