Neha Patil (Editor)

Mohawk M 2 C Chieftain

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Manufacturer
  
Mohawk Aircraft

The Mohawk M-2-C Chieftain is a prototype light twin aircraft from the Mohawk Aircraft Company.

Contents

Design

The M-2-C is a low-wing three place twin engine aircraft with conventional landing gear powered by two Michigan Rover engines.

Operational history

X-590E was registered on 30 March 1929, and sold several times in rapid succession remaining registered in Minneapolis. The Mohawk Aircraft company was dissolved in 1930.

Specifications (M-2-C)

Data from Skyways

General characteristics

  • Crew: 1
  • Capacity: 2
  • Length: 26 ft (7.9 m)
  • Wingspan: 44 ft (13 m)
  • Powerplant: 2 × Michigan Rover Air cooled piston, 55 hp (41 kW) each
  • Propellers: 2-bladed

    • Performance

  • Maximum speed: 91 kn; 169 km/h (105 mph)
  • Cruise speed: 78 kn; 145 km/h (90 mph)

    • References

    Mohawk M-2-C Chieftain Wikipedia
    (Text) CC BY-SA