MI38

MIL Mi-38

Aircraft
Name
Mi-38
Manufacturer
Wing
Rotary
Position
Five-blade main rotor
Tail
Four-blade tail rotor
WTC
M
Type Code
H2T
Engine
Turboshaft
Engine Count
Multi
Position
Above cabin
Landing gear
Tricycle fixed
Manufacturered as
MIL Mi-38

MI38

The Mil Mi-38 is a helicopter designed by Mil. Originally intended as a replacement for the Mil Mi-8 and the Mi-17, it is being marketed in both military and civil versions. It flew for the first time on 22 December 2003.

Technical Data
Wing span (metric)
21.10 m
Length (metric)
19.70 m
Height (metric)
5.13 m
Powerplant

2 x Klimov TV7-117V or PW127TS turboshaft, 1,864 kW (2,500 shp) each.

Engine Model(s)
Klimov TV7-117
Pratt & Whitney Canada PW100
Indicative Performance Data
Take-Off
V2
n/a
Distance
n/a
MTOW
14500 kg
Initial Climb (to 5000 ft)
IAS
n/a
ROC
n/a
Initial Climb (to FL150)
IAS
n/a
ROC
n/a
Initial Climb (to FL240)
IAS
n/a
ROC
n/a
MACH Climb
MACH
n/a
ROC
n/a
Cruise
TAS
135 kts
MACH
n/a
Ceiling
210
Range
700 NM
Initial Descent (to FL240)
MACH
n/a
ROD
n/a
Descent (to FL100)
IAS
n/a
ROD
n/a
Descent (FL100 & below)
IAS
n/a
MCS
n/a
ROD
n/a
Approach
Vapp (IAS)
n/a
Distance
n/a

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