The Mil – Mi-34

Primarily for pilot training and flight skills perfection, the Mi-34 is used as a sporting rotorcraft for performance of aerobatic maneuvers with load factors up to 3g. A single M-14V26V piston engine powers the helicopter.

Variants:

Mi-34P:
  • A patrol helicopter with additional communication, search and surveillance equipment
Mi-34C:
  • Is a certified version of the Mi-34 for passenger and small loads transportation
Mi-34A:
  • Light utility helicopter with one turbo-shaft engine (Arrius, or Ai-450)
  • FAR-27 (JAR-27) certificated variant of the Mi-34A
Experimental UAV:
  • based on the Mi-34 design
Training:
  • Includes an up-rated M-14V26V1 piston engine

Specifications:

Take-off Weight:
Normal:
---
Maximum:
1450 kg
Empty Weight:
---
Cargo Compartment Dimensions:
0.70 m3
Diameter of Main Rotor:
10.0m
Number of Blades:
Main Rotor:
4
Crew:
1
Passengers:
Seated:
4
Operational Activities:
  • Passenger Transport
  • Patrol
  • Training

Performance:

Load-Carrying Capacity:
In Cargo:
---
On External Sling:
---
Crusing Speed:
200-240 km/h
Ceiling Under ISA Conditions:
Hovering OGE (min):
---
Service (min):
3500-5500m
Powerplant: M14V26V Piston Engine
Fuel Consumption:
---
Service Life:
---
Power:
---
Range:
With Max. Fuel:
525 km
Maximum Flight Duration:
2.1h
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