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GA-21M

Cunningham-Hall Aircraft Corporation · United States · Interwar (1919–1938)

GA-21M — Fixed Wing
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The Cunningham-Hall GA-21 was an American two-seat monoplane design to compete for the Guggenheim Safe Aircraft Competition in 1934. Its distinguishing feature was full span flaps which could be manually or automatically adjusted. The GA-36 was a military version of it with tandem, rather than side-by-side seating.

Specifications

Category
Fixed Wing
Domain
Civil
Era
Interwar (1919–1938)
Country
United States
Manufacturer
Cunningham-Hall Aircraft Corporation
Service Entry
1934
Produced
1
Engine
1× seven cylinder air-cooled radial piston engine
Thrust / Power
145 hp
Length (ft)
20
Wingspan (ft)
30
Empty Weight (lb)
1490
MTOW (lb)
2100
Service Ceiling (ft)
14000
Range (mi)
450
Max Speed (mph)
158