Let L 410 NG Turbolet

Let Kunovice

ICAOL410IATAL4T
Let L 410 NG 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

The NG is the current Turbolet: a longer fuselage at 15.074 m, GE H85 engines, a wing that carries its fuel instead of the cabin, and 7,000 kg of take-off weight against the UVP-E's 6,400. It is the only L-410 model still being built. 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)

7,020kg
0
25k
50k
68k

MTOW (Maximum Takeoff Weight)

7,000kg
0
25k
50k
68k

MLW (Maximum Landing Weight)

6,800kg
0
25k
50k
56k

MZFW (Maximum Zero Fuel Weight)

6,660kg
0
25k
53k

Capacitycompared to Airbus A318

Passenger Capacity

19passengers
0
100
132

14% of A318 maximum capacity

Crew

Total
2
Cockpit
2

Dimensions

Length

15.1m

Wingspan

20.0m

Height

6.0m

Wing Area

35.2m²

Engine Specifications

Engine Count

2×

Engine Model

Walter/GE H85-200 BC04 turboprop

Production & History

Production Status

In production

Business jets and the API are coming

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