JODEL D-11

 

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