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Main Activities / Civil Aircraft Production

M-101T - light passenger turboprop

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M-101T light aircraft is new at the business-class aircraft market.

Long range and high flight speed, pressurized cockpit, comfortable seats, all these create a comfortable environment in the cabin and convert the light aircraft into a business mini-liner that can land on unprepared runways of just 500-600 m long. The complex of onboard equipment provides for all-weather aircraft operation.

The aircraft is designed by FSUE V.M. Myasischev Experimental Machine Building Plant Zhukovsky, Moscow region).

The aircraft is promoted by JSC Sokol.

Performance

Crew

1-2 pilots

Maximum passenger capacity

7 pax.

Maximum take-off weight

3270 kg

Maximum landing weight

3160 kg

Maximum cargo weight in the luggage compartment

540 kg

Maximum fuel weight

450 kg

Engine

Walter M-601F-22(32) turboprop engine

Cruising altitude

7600 m

Cruising speed at 7600 m

300-340 km/h

Flight range at maximum payload and maximum fuel at the altitude of 7600 m and the cruising speed of 340 km/h

 
1100 km

Take off run at hard dry unpaved runway under ISA

590 м

Landing run at unpaved runway under ISA

470 м


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