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FEATURES Mi-8AMT / MI-171E
1. Takeoff weight:
• Maximum 13,000 kg
• Normal 11100 kg
2. Weight of helicopter:
• empty helicopter transport version 6851 kg
3. Maximumpayload:
• in the cargo 4,000 kg
• the external load 4000 kg
4. Seats:
• the number of members of the crew: Marines / service passengers (seats on the landing) 3 persons: 2pilots and flight engineer to 37 people.
• Passengers (in passenger seats) to 26 people.
5. Dimensions of cargo cabin:
• length of 5.34 m.
• width of 2,34 m.
• height of 1.8 m.• the effective area of ​​12.5 m ²
• storage capacity of 23 m ³
Opening the sliding door left 0.825 x 1.405 m
Right opening the sliding door 1250 x 1405 m
Aperture in theramp 2054 x 1500 m
Opening escape hatch 0.510 x 0.921 m
6. Ceiling out of ground effect (with disabled PIC)
• a normal takeoff weight of 3980 m
7. Ceiling:
• a normaltakeoff weight of 6,000 m
• With a maximum takeoff weight of 4800 m
8. Practical flight range with a 30-minute guarantee supply of fuel and maximum takeoff weight:
• the main fueltanks, 630 km
• with one internal extra fuel tank 835 km
• with two internal auxiliary fuel tanks 1085 km
• with three internal extra fuel tanks 1290 km
• With four internalextra fuel tanks 1490 km
9. Maximum speed:
• take-off mass of less than 11100 kg 250 km / h
• take-off mass over 11100 kg 230 km / h
10. Cruising speed:
• take-off mass ofless than 11100 kg 230 km / h
• take-off mass over 11100 kg 215 km / h
11. Engine power:
• 2200 hp emergency
• Take-off 2000 hp
• Rated 1700 hp
• 1500 hp Cruising
Powerplant - 2 × TV3-117VM Series 2
• 4400 hp emergency
• Take-off 4000 hp
• Rated 3400 hp
• 3000 hp Cruising
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