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1991 MIL Mi-26 T

Helicopter
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1991 MIL Mi-26 T 1991 MIL Mi-26 T
1991 MIL Mi-26 T 1991 MIL Mi-26 T

Aircraft information

Year of construction: 1991
Total time (TTAF): 1000 TT
Country: Russia
City/Aerodrome: On request
Price: Enquire

General description

0.00 fh after last overhaul

Tel: +7 (499) 3468868
Ad. tel: +8835 (1000) 139 83 48
Site: milhelicopter.com
E-mail: info@milhelicopter.com (3468868@gmail.com)
Skype: milhelicopters

Performance
Max. speed
295 km/h
Cruise speed
255 km/h
Max. flight range with main fuel tanks
800 km
Operational ceiling
4,600 m
Hover ceiling (OGE)
1,520 m
Weight Parameters

Max. take-off weight
56,000 kg
With underslung load
56,000 kg
Max. Payload, kg

in transport cabin
20,000 kg
on external sling
20,000 kg
Engine 2 ? D-136 (2 ? 11 400 h. p.)

Take-off power
h. p.
Contingency power
h. p.
Cabin Dimensions

Length
12.1 m
Width
3.29 m
Height
3.17 m
Volume
m3
Capacity:

Aircrew
5?6
Passengers
82

Last updated: 20.05.2015
Advert views: 1990
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Seller

Helitage avia
Valery Andreeva
St-Petersburg, Russia
Phone: +7 (499) 346 88 68
Web: http://milhelicopter.com
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