Euromil Mi-38

__NOTOC__infobox Aircraft
name = Euromil Mi-38
type = medium transport helicopter
manufacturer =Mil Moscow Helicopter Plant
caption = Mi-38 in MAKS Airshow 2005 The Euromil Mi-38 is a cargo helicopter designed by Mil but being developed and marketed by an international consortium. It was originally intended as a replacement for the Mi-8 and the Mi-6. It is being marketed in both military and civil versions. It flew for the first time on the 22 December 2003.

pecifications (Mi-38)

aircraft specification

plane or copter?=copter
jet or prop?=prop
crew=Threendash two pilots and one engineer
capacity=32 passengers or 6,000 kg (13,200 lb) on internal/external hardpoints.
length main= 19.70 m
length alt= 64 ft 8 in
span main= 21.10 m
span alt= 69 ft 3 in
height main= 5.13 m
height alt= 16 ft 10 in
area main= 349.5 m²
area alt= 3,762 ft²
empty weight main= 8,300 kg
empty weight alt= 18,300 lb
loaded weight main= 14,200 kg
loaded weight alt= 31,300 lb
max takeoff weight main= 15,600 kg
max takeoff weight alt= 34,400 lb
more general=
engine (prop)= Pratt & Whitney Canada PW127
type of prop=turboshafts
number of props= 2
power main= 2,052 kW
power alt= 2,750 shp
max speed main= 275 km/h
max speed alt= 171 mph
range main= 1,300 km
range alt= 811 miles
ceiling main= 6,500 m
ceiling alt= 21,320 ft
climb rate main= ? m/s
climb rate alt=? ft/min
loading main= 41 kg/m²
loading alt= 8.3 lb/ft²
power/mass main= 260 W/kg
power/mass alt= 0.16 hp/lb
more performance=
armament=

ee also

Related development:

Comparable aircraft:
EH Industries EH101 -
Sikorsky S-92

External links

* [http://www.aviation.ru/Mi/#38 Euromil Mi-38]
*http://www.aviastar.org/helicopters_eng/mi-38.php