Mi-8AMT helicopter is an advanced version of world famous Mi-8 helicopter. More than 10000 of Mi-8/Mi-17/Mi/-171 helicopters were produced, around 4000 among them were exported. At present Mi-8/Mi-17 helicopters are operated in more than 80 countries worldwide. Total flying hours for these helicopters exceed 35 million.
Design, useable materials, documentation, manufacturing procedure and performances of the helicopter ensure its safe operation.
The helicopter is ideal in all climate conditions: land, sea, in any microclimatic area including marine, tropical and cold types of climate, under the influence of maritime fog and sea water.
The helicopter can be operated within outside temperature from minus 50°С to plus 50°С and at relative humidity up to 100%.
Mi-171E helicopter in transport configuration is designed for:

1. Carriage:

- cargo carriage inside the cargo cabin and on external sling up to 4 000 kg;
- carriage of passengers (up to 30) on folding troop seats;

1. search-and-rescue operations (SAR);
2. patrolling (if optional equipment is installed);
3. firefighting (if optional equipment is installed);
4. medevac operations (if optional equipment is installed);

Completion of Mi-171E helicopters manufacture (5 set.) in transport configuration, ser Nos.171Е00643157509U/-12U is November 2016.
 Key advantages:

• Mi-171E helicopters are ready to be delivered right now
• At Buyer's option the helicopter can be repainted in accordance with any color schemes as (under a separate agreement);
• The helicopters have built-in attachment points for installation of external sling, troop seats, mooring and medical equipment;
• Upon the Customer request the helicopters can be equipped with Search Light TSL-1600 and large variety of other additional equipment that is desired

 

GENERAL PERFORMANCE

1. Takeoff weight:
maximum	13,000 kg
normal	11,100 kg
2. Cargo cabin dimensions:
length	5.34 m
width	2.34 m
height	1.8 m
usable area	12.5 m2
usable volume	23 m3
3. Ceiling without ground effect (anti-ice system off)
with normal takeoff weight	3,980 m
4. Service ceiling:
with normal takeoff weight	6,000 m
with maximum takeoff weight	4,800 m
5. Range with 30 minutes guarantee fuel supply and maximum takeoff weight:
with main fuel tanks	610 km
6. Maximum speed:
with takeoff weight no less than 11,100 kg	250 km/h
with takeoff weight no more than 11,100 kg	230 km/h
7. Cruise speed:
with takeoff weight no less than 11,100 kg	230 km/h
with takeoff weight no more than 11,100 kg	215 km/h
8. Engine power:
emergency	2 х 2,200 hp
takeoff	2 х 2,000 hp
nominal	2 х 1,700 hp
cruise	2 х 1,500 hp

2.2 Helicopter assigned service life and life time: 18,000 hours or 30 years