Druine D.62 Condor
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First flow in 1961, the D.62A was a pre-production version of which two were built.
The D.62B was the standard production version.
![]() Rollason D.62B
The D.62C was specially equipped for glider towing with wingtip endplates, larger wheels, raised cockpit canopy, and 130 hp Rolls-Royce Continental O-240 engine.
D.62A
D.62B
Engine: 1 x 75hp Continental A 75
Max take-off weight: 669 kg / 1475 lb
Wingspan: 8.72 m / 28 ft 7 in
Length: 6.95 m / 22 ft 10 in
Height: 1.75 m / 5 ft 9 in
Cruise speed: 160 km/h / 99 mph
Range: 627 km / 390 miles
D.62B
Engine: Continental O-200, 100hp
Wingspan: 27 ft 6 in / 8.38 m
Length: 22 ft 6 in / 6.86 m
Empty weight: 920 lb / 417 kg
MTOW: 1475 lb / 670 kg
Max cruise: 100 kt / 115 mph / 185 kph
ROC SL: 610 fpm / 185 m/min
Service ceiling: 12,000 ft / 3650 m
Range MAUW: 285 nm / 328 mi / 528 km
Seats: 2
D.62C
Engine: Rolls-Royce Continental O-240, 130 hp
![]() D.62B
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