The Grumman Goose reference article from the English Wikipedia on 24-Apr-2004
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Grumman Goose

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Grumman Goose
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Description
Role Reconnaissance, air-sea rescue
Crew 2
First Flight May 29, 1937
Entered Service July 3, 1937
Manufacturer Grumman
Dimensions
Length 38ft 4in 11.7 m
Wingspan 49ft 0in 14.9 m
Height 12ft 0in 3.7 m
Wing Area 375 ft² 34.8 m²
Weights
Empty 5,571 lbs 2,530 kg
Loaded 8,200 lbs 3,720 kg
Maximum takeoff lbs kg
Powerplant
Engine 2 × Pratt & Whitney Wasp Junior SB-2
Power (each) 450 hp 340 kW
Performance
Maximum speed 184mph @ 5,000ft 296km/h @ 1,520m
Combat range 1,050 miles 1,690 km
Ferry range km miles
Service ceiling 21,000 ft 6,400 m
Rate of climb 1,240 ft/min 380 m/min
Wing loading 21.9 lb/ft² 106.9 kg/m²
Power/Mass 0.11 hp/lb 0.183 kW/kg
Armament
Guns 2 machine guns
Bombs 2 × 250lbs (120kg) depth charges

The Grumman G-21 Goose amphibious aircraft was designed as a 6-7 seat 'commuter' plane for businessmen in the Long Island area. It was soon adopted by the US Navy and Coast Guard, and during World War II it served with United States forces and the RCAF in a transport, reconnaissance, rescue and training roles, and was used by the RAF for air-sea rescue duties.

Returning to civilian service after the war, the Goose found use from the wilderness of Alaska to the sunny climes of Catalina.

345 Goose were built, and about 60 are still airworthy today. Various modifications have been made over the years and some are now flying with turboprop powerplants.


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