Mohawk M-2-C Chieftain
{{Short description|Prototype twin aircraft}}
| {{Infobox aircraft begin
| name=M-2-C Chieftain | image=Mohawk M2-C Aero Digest May 1929.jpg | caption= }}{{Infobox aircraft type | type=Light Twin | national origin=United States | manufacturer=Mohawk Aircraft | designer= | first flight= | introduced=1930 | retired= | status= | primary user= | more users= | produced= | number built=1 | program cost= | unit cost= | developed from= | variants with their own articles= }} |
The Mohawk M-2-C Chieftain is a prototype light twin aircraft from the Mohawk Aircraft Company.{{cite journal|journal=Journal American Aviation Historical Society|date=Winter 2008}}
Design
The M-2-C is a low-wing three place twin engine aircraft with conventional landing gear powered by two Michigan Rover engines.{{cite journal|journal=Skyways|date=April 2000|page=56}}
Operational history
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.{{cite journal|journal=Skyways|date=April 2000|page=56}}
Specifications (M-2-C)
File:Mohawk_M2-C_3-view_Aero_Digest_May_1929.png
{{Aircraft specs
|ref=Skyways
|prime units?=kts
|genhide=
|crew=1
|capacity=2
|length m=
|length ft=26
|length in=
|length note=
|span m=
|span ft=44
|span in=
|span note=
|upper span m=
|upper span ft=
|upper span in=
|upper span note=
|mid span m=
|mid span ft=
|mid span in=
|mid span note=
|lower span m=
|lower span ft=
|lower span in=
|lower span note=
|swept m=
|swept ft=
|swept in=
|swept note=
|dia m=
|dia ft=
|dia in=
|dia note=
|width m=
|width ft=
|width in=
|width note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=
|wing area sqft=
|wing area note=
|swept area sqm=
|swept area sqft=
|swept area note=
|volume m3=
|volume ft3=
|volume note=
|aspect ratio=
|airfoil=
|empty weight kg=
|empty weight lb=
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|lift kg=
|lift lb=
|lift note=
|more general=
|eng1 number=2
|eng1 name=Michigan Rover
|eng1 type=Air cooled piston
|eng1 kw=
|eng1 hp=55
|eng1 kn=
|eng1 lbf=
|eng1 note=
|power original=
|thrust original=
|eng1 kn-ab=
|eng1 lbf-ab=
|eng2 number=
|eng2 name=
|eng2 type=
|eng2 kw=
|eng2 hp=
|eng2 kn=
|eng2 lbf=
|eng2 note=
|eng2 kn-ab=
|eng2 lbf-ab=
|eng3 number=
|eng3 name=
|eng3 type=
|eng3 kw=
|eng3 hp=
|eng3 kn=
|eng3 lbf=
|eng3 note=
|eng3 kn-ab=
|eng3 lbf-ab=
|more power=
|prop blade number=2
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=
|rot number=
|rot dia m=
|rot dia ft=
|rot dia in=
|rot area sqm=
|rot area sqft=
|rot area note=
|perfhide=
|max speed kmh=
|max speed mph=105
|max speed kts=
|max speed note=
|max speed mach=
|cruise speed kmh=
|cruise speed mph=90
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|minimum control speed kmh=
|minimum control speed mph=
|minimum control speed kts=
|minimum control speed note=
|range km=
|range miles=
|range nmi=
|range note=
|combat range km=
|combat range miles=
|combat range nmi=
|combat range note=
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|disk loading kg/m2=
|disk loading lb/sqft=
|disk loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}
{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
}}