The M-2-C is a low-wing three place twin engine aircraft with conventional landing gear powered by two Michigan Rover engines.[2]
Operational historyedit
X-590E was registered on March 30, 1929 and sold several times in rapid succession while remaining registered in Minneapolis. The Mohawk Aircraft company was dissolved in 1930.[3]
Specifications (M-2-C)edit
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 × Michigan Rover 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)
Referencesedit
^Journal American Aviation Historical Society. Winter 2008. {{cite journal}}: Missing or empty |title= (help)
^Skyways: 56. April 2000. {{cite journal}}: Missing or empty |title= (help)
^Skyways: 56. April 2000. {{cite journal}}: Missing or empty |title= (help)
January 01, 1970
mohawk, chieftain, prototype, light, twin, aircraft, from, mohawk, aircraft, company, chieftain, role, light, twin, national, origin, united, states, manufacturer, mohawk, aircraft, introduction, 1930, number, built, contents, design, operational, history, spe. The Mohawk M 2 C Chieftain is a prototype light twin aircraft from the Mohawk Aircraft Company 1 M 2 C Chieftain Role Light Twin National origin United States Manufacturer Mohawk Aircraft Introduction 1930 Number built 1 Contents 1 Design 2 Operational history 3 Specifications M 2 C 4 ReferencesDesign editThe M 2 C is a low wing three place twin engine aircraft with conventional landing gear powered by two Michigan Rover engines 2 Operational history editX 590E was registered on March 30 1929 and sold several times in rapid succession while remaining registered in Minneapolis The Mohawk Aircraft company was dissolved in 1930 3 Specifications M 2 C edit nbsp Mohawk M2 C 3 view drawing from Aero Digest May 1929 Data from SkywaysGeneral characteristicsCrew 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 105 mph 169 km h Cruise speed 78 kn 90 mph 140 km h References edit Journal American Aviation Historical Society Winter 2008 a href Template Cite journal html title Template Cite journal cite journal a Missing or empty title help Skyways 56 April 2000 a href Template Cite journal html title Template Cite journal cite journal a Missing or empty title help Skyways 56 April 2000 a href Template Cite journal html title Template Cite journal cite journal a Missing or empty title help Retrieved from https en wikipedia org w index php title Mohawk M 2 C Chieftain amp oldid 1113764286, wikipedia, wiki, book, books, library,
