V. M. Myasishchev Experimental Design Bureau
Myasishchev M-101T "Gzhel"
Myasishchev M-101T
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| An M-101T at 2007 MAKS Airshow | |
| Role | Passenger and cargo aircraft |
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| National origin | Russia |
| Manufacturer | Myasishchev |
| First flight | 31 March 1995 |
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History V. M. Myasishchev Experimental Design Bureau
Myasishchev M-101T "Gzhel"
The aircraft is intended to comfortably carry 4-6 passengers at a range of over 1,000 km at an average speed of 500 km/h at an altitude of 6-8 km. The Gzhel’s production was commenced at the Sokol plant (Nizhny Novgorod). The M-101T’s maiden flight was made on 31 March, 1995. As of 2003, two planes had been built for static tests, another two had been manufactured as flying prototypes and yet another six planes make up a pre-production batch.
Design and development
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. Two planes were operationally evaluated by the Phoenix air company, one aircraft in 1999-2000 underwent its opeval with the Central African Airlines company. M-101T was certified under AP-23 standards on 30 December 2002. The Sokol aircraft plant launched production of a 15-ship batch.
Operators
- Dexter Air Taxi (3 aircraft).
- 3 more aircraft operated by Buguruslansk Civil Aviation School.
- 1 aircraft RA15106, was demonstrated in 2004 in South Africa by ROSAVIA and flown at multiple airshows in South Africa. These demonstrations were flown by Yurij Polyakov and South African born Andrew Cross. The project generated a lot of interest but did not sell because the asking price was too high. When the project ended the aircraft was ferried back to Russia by Yurij Polyakov[].
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V. M. Myasishchev Experimental Design Bureau
Myasishchev M-101T "Gzhel"
V. M. Myasishchev Experimental Design Bureau
Myasishchev M-101T "Gzhel"
General Info
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- Crew: 1
- Capacity: 7 passengers / 540 kg (1,190 lb) payload
- Length: 9.975 m (32 ft 9 in)
- Wingspan: 13 m (42 ft 8 in)
- Height: 3.72 m (12 ft 2 in)
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Powerplant
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- Empty weight: 2,016 kg
- Max takeoff weight: 3,000 kg
- Powerplant: 1 × Walter M601F turboprop engine, 567 kW (760 hp)
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Performance
- Maximum speed: 525 km/h
- Cruise speed: 360–450 km/h (220–280 mph, 190–240 kn) at 7,600 m
- Stall speed: 112–125 km/h
- Range: 1,410 km (880 mi, 760 nmi)
- Time to altitude: 7,600 m /25 minutes
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Links to Youtube & Others
The Myasishchev M-101T Gzhel is a single-engine eight-seat touring and utility aircraft developed by the Russian manufacturer JSC Myasishchev Design Bureau, produced by JSC NAZ SOKOL.
V. M. Myasishchev Myasishchev M-101T
The Myasishchev M-101T Gzhel is a single-engine eight-seat touring and utility aircraft developed by the Russian manufacturer JSC Myasishchev Design Bureau, produced by JSC NAZ SOKOL.
Youtube Link
The Myasishchev M-101T Gzhel is a single-engine eight-seat touring and utility aircraft developed by the Russian manufacturer JSC Myasishchev Design Bureau, produced by JSC NAZ SOKOL.
Read more in V. M. Myasishchev Experimental Design Bureau Myasishchev M-101T "Gzhel"
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