GRUMMAN AA-1

 

BRAND and MODEL
GRUMMAN AA-1
TYPE
Two-seat light touring monoplane
ORIGIN
United States of America
ENGINE

[AA-1 Yankee] One 81 kw (108 hp) Lycoming O-235-C2C four cylinder horizontally-opposed air-cooled engine

(AA-1B Trainer, AA-1C and T-Cat) One 86 kw (115 hp) Lycoming O-235-L2C four cylinder horizontally-opposed air-cooled engine

SPECIFICATIONS

[AA-1C]

Wingspan: 7.47 m (24 ft 6 in)

Length: 5.86 m (19 ft)

strong>Height: 2.32 m (7 ft 7¼ in)

Wing area: 9.4 m² (100.9 sq ft)

Max speed at sea level: 218 km/h (136 mph)

Cruising speed at 75% power at 1,372 m (4,500 ft): 208 km/h (129 mph)

Initial rate of climb: 228 m/min (750 ft/min)

Service ceiling: 3,627 m (11,900 ft)

Range with 45 mins reserve: 543 km (337 miles)

Empty weight: 455 kg (1,002 lb)

Loaded weight: 726 kg (1,600 lb)

PHOTO
sky4buy.com:Source of phothograph