NEW HELICOPTERS SALES
Airline Company "DP" Aero-Kamov sells new Mi-8AMT and MI-171E helicopters with additional equipment to them, as well as KA-32AO helicopters.
Apply for the helicopters price a formal request to the addresses specified in the "Contacts"
Mi-8AMT and Mi-171E helicopters are designed for a wide range of tasks: carrying passengers and cargo, transportation of bulky cargo on the external load, search and rescue operations, injured evacuation.
| MAIN DATA OF MI-8AMT and MI-171E HELICOPTERS |
|---|
| 1. Take-off weight: |
|---|
| • maximum | 13000 kg |
| • normal | 11100 kg |
| 2. Weight of helicopter: |
|---|
| • empty helicopter transport version | 6851 kg |
| 3. Maximum payload: |
|---|
| • inside cargo cabin | 4000 kg |
| • on external sling | 4000 kg |
| 4. Seats: |
|---|
crew
• paratroopers/service passengers (on the landing seats) | 3 persons: 2 pilots and flight mechanic to 37 people |
| • passengers (on the passenger seats) | to 26 people |
| 5. Dimensions of cargo cabin: |
|---|
| • length | 5,34 m. |
| • width | 2,34 m. |
| • height | 1,8 m. |
| • usable area | 12,5 m² |
| • usable volume | 23 m³ |
| Opening the left sliding door | 0,825 × 1,405 m |
| Opening the right sliding door | 1250 × 1405 m |
| Opening in the ramp | 2054 × 1500 m |
| Opening escape hatch | 0,510 × 0,921 m |
| 6. The ceiling outside the influence of land (with the anti-ice system in off-position) |
|---|
| • with a normal takeoff weight of | 3,980 m |
| 7. Service ceiling: |
|---|
| • with a normal takeoff weight of | 6000 m |
| • with a maximum takeoff weight of | 4800 m |
| 8. Practical flight range with a 30-minute reserve of fuel and maximum takeoff weight: |
|---|
| • with the main fuel tanks | 630 km |
| • with one internal extra fuel tank | 835 km |
| • with two internal auxiliary fuel tanks | 1085 km |
| • with three internal auxiliary fuel tanks | 1290 km |
| • with four internal auxiliary fuel tanks | 1490 km |
| 9. Maximum flight speed: |
|---|
| • with a takeoff mass of less than 11100 kg | 250 km/h |
| • with a takeoff mass of more than 11100 kg | 230 km/h |
| 10. Cruising speed: |
|---|
| • with a takeoff mass of less than 11100 kg | 230 km/h |
| • with a takeoff mass of more than 11100 kg | 215 km/h |
| 11. Engine power: |
|---|
| • contingency | 2200 hp |
| • take-off | 2000 hp |
| • rated | 1700 hp |
| • cruising | 1500 hp |
| The power unit — 2 × TV3-117Ð’M Series 2 |
|---|
| • contingency | 4400 hp |
| • take-off | 4000 hp |
| • rated | 3400 hp |
| • cruising | 3000 hp |
