GRUMMAN G-21 GOOSE Civil Aircraft Model Details

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General Information of GRUMMAN G-21 GOOSE

First Flight : 1937

Manufacturer : Grumman

Number Built : 345

Primary Users : United States Navy; United States Army Air Forces; Royal Air Force; Royal Canadian Air Force

Role : Transport amphibious aircraft

Unit_Cost : US$62,180.00 for JRF-6B (1942)

General characteristics of GRUMMAN G-21 GOOSE

Airfoil : Root: NACA 23015, Tip: NACA 23009

Capacity : five to seven passengers

Crew : one to three

Empty Weight : 5,425 lb (2,466 kg)

Height : 16 ft 2 in (4.93 m)

Length : 38 ft 6 in (11.74 m)

Loaded_Weight : 8,000 lb (3,636 kg)

Max Takeoff Weight : 8,000 lb (3,636 kg)

Powerplant : 2 × Pratt & Whitney R-985-AN-6 Wasp Junior nine-cylinder air-cooled radials, 450 hp (340 kW) each

Useful Load : 2,575 lb (1,170 kg)

Wing Area : 375 ft² (34.9 m²)

Wingspan : 49 ft 0 in (14.94 m)

Performance of GRUMMAN G-21 GOOSE

Cruise Speed : 191 mph (166 knots, 308 km/h) at 5,000 ft (1,520 m)

Maximum Speed : 201 mph (175 knots, 324 km/h) at 5,000 ft (1,520 m)

Power/Mass : 0.11 hp/lb (0.19 kW/kg)

Range : 640 mi (557nmi, 1,030 km)

Rate Of Climb : 1,100 ft/min (5.6 m/s)

Service Ceiling : 21,300 ft (6,494 m)

Wing Loading : 21.3 lb/ft² (104 kg/m²)

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