BRAND and MODEL
JODEL D-11
TYPE
Two-seat dual-control low-wing touring monoplane
ORIGIN
France
ENGINE
One 67 kw (90 hp) Rolls Royce/Continental O-200-A four-cylinder horizontally-opposed air-cooled engine
SPECIFICATIONS
Wingspan: 8.23 m (27 ft)
Length: 6.46 m (21 ft 2 in)
Wing area: 12.72 m² (137 sq ft)
Never exceed speed: 249 km/h (155 mph)
Max speed: 209 km/h (130 mph)
Cruising speed: 209 km/h (118 mph)
Landing speed: 80 km/h (50 mph)
Stalling speed: 56 km/h (35 mph)
Initial rate of climb: 244 m/min (800 ft/min)
Ceiling: 5,182 m (17,000 ft)
Take-off run: 137 m (450 ft)
Landing run: 137 m (450 ft)
Range: 1,151 km (715 miles)
Fuel capacity: 100 litres (22 Imp gals)
Power loading: 15 lb/hp
Wing loading: 9.9 lb/sq ft
Empty weight: 318 kg (700 lb)
Useful load: 287 kg (632 lb)
Loaded weight: 617 kg (1,360 lb)
PHOTO
Airliners.net:Source of phothograph
