F.20 Condor

The F.20 Condor was a twin-engined turboprop.

   
F.20 Condor
Powered by Two 420 hp Allison 250-B17C
Propeller Hartzell constant speed
Wing span 10.34m (33' 11")
Length 8.95 m (29' 4")
Wing area 16.02 sq m (172.8 sq ft)
Max takeoff weight 2,400 kg (5,290 lbs)
Max takeoff weight (ext. loads) 2,700 kg (5,952 lbs)
Empty weight 1,435 kg (3,160 lbs)
Accommodation 4 seats
Maximum speed 288 mph
Maximum cruise speed 270 mph
Stall speed 75 mph
Rate of climb 3,000 fpm
Service ceiling 28,000 ft
Maximum range 1,930 sm