Mohawk M-2-C Chieftain

From Wikipedia, the free encyclopedia
M-2-C Chieftain
Mohawk M2-C Aero Digest May 1929.jpg
Role Light Twin
National origin United States
Manufacturer
Introduction 1930
Number built 1

The Mohawk M-2-C Chieftain is a prototype light twin aircraft from the Mohawk Aircraft Company.[1]


Design[]

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

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.[3]

Specifications (M-2-C)[]

Mohawk M2-C 3-view drawing from Aero Digest May 1929

Data from Skyways

General characteristics

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

Performance

  • Maximum speed: 91 kn (105 mph, 169 km/h)
  • Cruise speed: 78 kn (90 mph, 140 km/h)

References[]

  1. ^ Journal American Aviation Historical Society. Winter 2008. {{cite journal}}: Missing or empty |title= (help)
  2. ^ Skyways: 56. April 2000. {{cite journal}}: Missing or empty |title= (help)
  3. ^ Skyways: 56. April 2000. {{cite journal}}: Missing or empty |title= (help)
Retrieved from ""