Mi-8P Civil version

Mi-8P Civil version. First flight: 1962 © Konstantinos Panitsidis
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Civil version of the Mi-8 with two TV2-117A engines with a maximum power of 1.267 kW/1.700 h.p. each one, and has a capacity of 28 seats. 

 


Technical specifications

DESIGNER OKB Mil
COUNTRY Russia
TYPE
Civil version
CREW 2 - 3
POWER-PLANT Two turboshaft engines Klimov TV3-117A
Power, h.p. 2x1.700
DIMENSIONS  
Length, m 18,17
Main rotor diameter, m 21,29
Tail rotor diameter, m 3,91
Height, m 5,65
WEIGHT  
Maximum take-off, kg 12.000
Normal take-off, kg 11.100
Empty, kg 6.800
Internal fuel, l -
Weight of transported fuel with external tanks, l -
Warload, kg -
Payload, kg -
- passengers  up to 28
- stretcher 12
- freight in cabin 4.000
- with on hook 3.000
PERFORMANCE  
Maximum speed, km/h 250
Cruising speed, km/h 225
Range, km 420
Ferry range, km -
Combat range, km -
Service ceiling, m 4.500
Static ceiling, m 1.900
Rate of climb, m/s -
Maximum overload, g -
ARMAMENT Doesn't have (defensive).