L 410

General description

The L 410 NG is the latest model of the L 410 aircraft. Its development was launched in 2010 under the MOSTA project, serial production began in 2018. This innovative model offers an improved flight envelope, use of advanced technologies and modernized avionics.

The new design of the wing with an integrated fuel tank provides increased fuel capacity, allowing for considerably longer flight range and endurance. Another crucial improvement is the increase of MTOW and payload, resulting in the ability to carry an extra 500 kg of cargo, with increased volume provided by the nose extension. The aircraft is equipped with the more powerful GE H85-200 engine and AV 725 propeller.

Designed for short take-off and landing (STOL)

Low operating and maintenance costs

Excellent performance in hot temperatures and high altitude conditions

Operates in extreme weather conditions (-50 °C to +50 °C)

Varieties of equipment, options to have special interchangeable configurations

Large cargo hold

Safe operation

The most spacious passenger cabin in its category

L 410 NG

Thanks to the implementation of these crucial changes, the customer will receive an aircraft with improved performance, including a higher cruising speed and better performance of the engines in hot temperatures and high altitude conditions. By following the damage tolerance philosophy in the design, we have also considerably increased the lifespan of the aircraft. The cockpit is equipped with a Garmin 3000 touchscreen glass integrated avionics system.

The aircraft has been certified in the transport aircraft category in accordance with regulations of EU (EASA), USA (FAA), Russian Federation (FATA).

SPECIFICATION

Performance

Cruise Speed	417 km/h	225 KTAS
Maximum Range^*	2 570 km	1 387 NM
Endurance^*	10,5 h	630 min
Service Ceiling	6 100 m	20 000 ft
One Engine Inoperative Ceiling	3 900 m	12 800 ft
Absolute Ceiling	8 230 m	27 000 ft

* 45 minutes reserve with tip tanks

Rate Of Climb	8,5 m/s	1 673 fpm
Rate Of Climb One Engine Inoperative	1,7 m/s	335 fpm
Take-off Distance Required	590 m	1 936 ft
Landing Distance Required	600 m	1 969 ft

Dimensions and weights

Cabin Volume	17,9 m³	632 ft³
Passenger Door	0,8 x 1,46 m	2,6 x 4,8 ft
Cargo Door	1,25 x 1,46 m	4,1 x 4,8 ft
Seat Pitch	0,76 m	30 in
Baggage Compartment Capacity	2,98 m³	105,5 ft³

Maximum Take-off Weight	7 000 kg	15 432 lb
Maximum Landing Weight	6 800 kg	14 991 lb
Maximum Zero Fuel Weight	6 600 kg	14 660 lb
Maximum Payload	2 300 kg	5 060 lb
Maximum Usable Fuel	2 254 kg	4 969 lb