ARMSTRONG WHITWORTH ATALANTA Civil Aircraft Model Details

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General Information of ARMSTRONG WHITWORTH ATALANTA

First Flight : 11845

Introduction : 1933

Manufacturer : Sir W.G. Armstrong Whitworth Aircraft Limited

Number Built : 8

Primary Users : Imperial Airways; Royal Air Force; Indian Air Force

Retired : 1942

Role : airliner

General characteristics of ARMSTRONG WHITWORTH ATALANTA

Capacity : 9–17 passengers

Crew : 3

Empty Weight : 14,832lb (6,727 kg)

Height : 14 ft 0 in[nb 1] (4.57 m)

Length : 71 ft 6 in (21.79 m)

Max Takeoff Weight : 21,000 lb (9,525 kg)

Powerplant : 4 × Armstrong Whitworth Serval III 10-cylinder two-row air-cooled radial engine, 340 hp (254 kw) each

Wing Area : 1,285 ft² (119.38 m²)

Wingspan : 90 ft 0 in (27.43 m)

Performance of ARMSTRONG WHITWORTH ATALANTA

Cruise Speed : 118 mph (103 knots, 190 mph) at 9,000 ft (2,740 ft)

Maximum Speed : 156 mph (136 knots, 251 km/h) at 3,000 ft (910 m)

Range : 640 miles (557 knots, 1,030 km)

Rate Of Climb : 700 ft/min[12](3.6 m/s)

Service Ceiling : 14,200 ft (4,330 m)

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