Myasishchev M-101T

The Myasishchev M-101T is a Russian business class aircraft, designed by Myasishchev and built by Sokol. The aircraft was first flown on 31 March 1995.^[1]

Operators

 Russia

• Dexter (3 aircraft). 3 more aircraft operated by Buguruslansk Civil Aviation School.^[2]

Specifications

Data from Brassey's World Aircraft & Systems Directory 1999/2000 ^[1]

General characteristics

• Crew: 1
• Capacity: 7 passengers
• Payload: 540 kg (1,190 lb)
• Length: 9.975 m (32 ft 9 in)
• Wingspan: 13.0 m (42 ft 8 in)
• Height: 3.72 m (12 ft 2½ in)
• Wing area: 17.06 m² (183.6 sq ft)
• Aspect ratio: 9.906
• Empty weight: 2,016 kg (4,445 lb)
• Max takeoff weight: 3,000 kg (6,614 lb)
• Powerplant: 1 × Walter M601F turboprop, 567 kW (760 shp) (take-off power)

Performance

• Maximum speed: 525 km/h (283 knots, 326 mph)
• Cruise speed: 360-450 km/h (194-243 knots, 224-280 mph)
• Stall speed: 112-125 km/h (61-68 knots, 90-93 mph)
• Range: 1,410 km (761 nmi, 876 mi)
• Service ceiling: 7,600 m (24,900 ft) (Cruise altitude)
• Climb to 7,600 m (24,900 ft): 25 minutes

See also

Aircraft of comparable role, configuration and era

• Aero Ae 270 Ibis
• Pilatus PC-12
• Piper Meridian
• Socata TBM
  

References

• Taylor, Michael J.H. Brassey's World Aircraft & Systems Directory 1999/2000. London:Brassey's, 1999. ISBN 1 85723 254 7.

External links

• Class Struggle