Grumman
G21
Goose

Photo: Robert Deering 10/23/2006
Smithsonian National Air and Space Museum
Dulles International Airport (IAD)

Chantilly, Virginia
The Grumman G-21 Goose amphibious aircraft was designed as an eight-seat "commuter" aircraft for businessmen in the Long Island area. The Goose was Grumman’s first monoplane to fly, its first twin-engined aircraft, and its first aircraft to enter commercial airline service. During World War II, the Goose became an effective transport for the US military (including the Coast Guard), as well as serving with many other air forces. During hostilities, the Goose took on an increasing number of combat and training roles. The adaptable transport continued in postwar use.

Envisioned as corporate or private "flying yachts" for Manhattan millionaires, initial production models normally carried two to three passengers and had a bar and small toilet installed. As well as being marketed to small air carriers, the G-21 was also promoted as a military transport. In 1938, the U.S. Army Air Force purchased the type as the OA-9 (later, in the war years, examples impressed from civilian ownership were designated the OA-13A). The most numerous of the military versions were the United States Navy variants, designated the JRF.

The amphibian was soon adopted by the Coast Guard and, during World War II, it also served with the RCAF in the transport, reconnaissance, rescue and training roles. The G.21 was used for air-sea rescue duties by the Royal Air Force (RAF). The RAF, in a common naming convention with all of its aircraft, designated the type as "Goose."

On returning to civilian service, after the war, the Goose found continued commercial use in locations from the wilderness of Alaska to the sunny climes of Catalina.

A total of 345 were built, with about 30 still airworthy today (although more like 60 are still on various civil registries, many of them are known to have crashed or been otherwise destroyed), most being in private ownership, some of them operating in modified forms.

SPECIFICATIONS: PERFORMANCE:
Span:  49 ft 0 in (14.94 m) Maximum speed:   201 mph (175 knots, 324 km/h) at 5,000 ft (1,520 m)
Length:  38 ft 6 in (11.74 m) Cruising speed:  191 mph (166 knots, 308 km/h) at 5,000 ft (1,520 m)
Height:  16 ft 2 in (4.93 m) Range:  640 mi (557 nmi, 1,030 km)
Empty Weight:  5,425 lb (2,466 kg) Service ceiling:  21,300 ft (6,494 m)
Gross Weight:  8,000 lb (3,636 kg)  
Crew:  1 - 3 plus up to 7 passengrs.
Engines:  2 × Pratt & Whitney R-985-AN-6 Wasp Junior nine-cylinder air-cooled radials, 450 hp (340 kW) each
   
SOURCE:  Wikipedia