avia.wikisort.org - Aeroplane

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]

This article may be expanded with text translated from the corresponding article in Russian. (March 2016) Click [show] for important translation instructions. Machine translation like DeepL or Google Translate is a useful starting point for translations, but translators must revise errors as necessary and confirm that the translation is accurate, rather than simply copy-pasting machine-translated text into the English Wikipedia. Do not translate text that appears unreliable or low-quality. If possible, verify the text with references provided in the foreign-language article. You must provide copyright attribution in the edit summary accompanying your translation by providing an interlanguage link to the source of your translation. A model attribution edit summary is Content in this edit is translated from the existing Russian Wikipedia article at [[:ru:М-101Т]]; see its history for attribution. You should also add the template {{Translated|ru|М-101Т}} to the talk page. For more guidance, see Wikipedia:Translation.

This article relies largely or entirely on a single source. (March 2016)

M-101T
An M-101T at 2007 MAKS Airshow
Role	Passenger and cargo aircraft Type of aircraft
National origin	Russia
Manufacturer	Myasishchev
First flight	31 March 1995

Operators

 Russia

• Dexter Air Taxi (3 aircraft).
• 3 more aircraft operated by Buguruslansk Civil Aviation School.[2]
• 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^{[citation needed]}.

Specifications

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

General characteristics

• 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)
• 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 engine, 567 kW (760 hp)

Performance

• Maximum speed: 525 km/h (326 mph, 283 kn)
• Cruise speed: 360–450 km/h (220–280 mph, 190–240 kn) at 7,600 m (24,934 ft)
• Stall speed: 112–125 km/h (70–78 mph, 60–67 kn)
• Range: 1,410 km (880 mi, 760 nmi)
• Time to altitude: 7,600 m (24,934 ft) in 25 minutes

See also

Aircraft of comparable role, configuration, and era

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

References

Further reading

• Taylor, Michael J.H. Brassey's World Aircraft & Systems Directory 1999/2000. London:Brassey's, 1999. ISBN 1-85753-245-7.

External links

• Class Struggle

На других языках

---

[de] Mjassischtschew M-101

Die Mjassischtschew M-101 Gschel (russisch Мясищев М-101 Гжель) ist ein einmotoriges Passagierflugzeug bzw. Frachtflugzeug, das vom russischen Konstruktionsbüro Mjassischtschew entwickelt wurde, um in den Markt der zivilen Reiseflugzeuge einzusteigen.

---

- [en] Myasishchev M-101T

---

[it] Myasishchev M-101T

Il Myasishchev M-101T Gzhel (in cirillico Мясищев М-101Т Гжель) è un monomotore turboelica ad ala bassa destinato al trasporto business progettato dall'OKB 23 Myasishchev e sviluppato in Unione Sovietica negli anni novanta. Realizzato dall'azienda russa SOKOL è attualmente in fase di produzione.

---

[ru] М-101Т

М-101Т «Гжель» — ближнемагистральный пассажирский самолёт, разрабатывавшийся в ОКБ Мясищева с 1989 года по 2002 год. Первый полёт 1995 год. Выпускался на Нижегородском авиастроительном заводе «Сокол». Производство прекращено, выпущено 26 самолётов, из них 4 прототипа и 22 серийных.

---

---