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Aircraft Manufacturing Depot Kanpur
 
Construction of this little aircraft is orthodox, with fabric-covered steel-tube fuselage and fabric-covered two-spar metal wings. It is fitted with a 250 h.p. Lycoming O-540-A1B5 engine, and the 40 gal of internal fuel can be supplemented by external tanks carried on the wing bracing struts.
 
The Kanpur-1 prototype was tested with spray-bars.
 
The basic version is a four-seat military AOP and liaison aircraft, but the Kanpur-II is suitable for a wide range of other duties, including agricultural work.
 
Kanpur I
Span: 37 ft 0.5 in
Length: 26 ft 6 in
Height: 7 ft 6 in
Wing area: 200 sq.ft
Gross weight: 2,600 lb
Empty weight: l,700 lb
Max speed: 137 mph
Econ cruising speed: 100 mph
Max rate of climb at SL: l,155 ft/min
Service ceiling: 20,500 ft
TO distance to 50ft: 750 ft
Landing distance from 50ft: 720 ft;
Range with max payload: 460 miles
 
 
 
 
 
 


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