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MIL Mi-38

From SKYbrary Wiki

Name Mi-38
Manufacturer MIL
Wing Rotary
Position Five-blade main rotor
Tail Four-blade tail rotor
WTC Medium
Type code H2T
Engine Turboshaft
Engine count Multi
Position Above cabin
Landing gear Tricycle fixed
Mass group 3

Manufacturered as:

MIL Mi-38

MIL Mi-38

MIL Mi-38 MIL Mi-38 3D


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 21.10 m69.226 ft
Length 19.70 m64.633 ft
Height 5.13 m16.831 ft
Powerplant 2 x Klimov TV7-117V or PW127TS turboshaft, 1,864 kW (2,500 shp) each.
Engine model Klimov TV7-117, Pratt & Whitney Canada PW100

Performance Data

Take-Off Initial Climb
(to 5000 ft)
Initial Climb
(to FL150)
Initial Climb
(to FL240)
MACH Climb Cruise Initial Descent
(to FL240)
(to FL100)
Descent (FL100
& below)
V2 (IAS) kts IAS kts IAS kts IAS kts MACH TAS 135 kts MACH IAS kts IAS kts Vapp (IAS) kts
Distance m ROC ft/min ROC ft/min ROC ft/min ROC ft/min MACH ROD ft/min ROD ft/min MCS kts Distance m
MTOW 1450014,500 kg
14.5 tonnes
Ceiling FL210 ROD ft/min APC
WTC M Range 700700 nm
1,296,400 m
1,296.4 km
4,253,280.843 ft

Accidents & Serious Incidents involving MI38

None on SKYbrary