STINSON RELIANT Civil Aircraft Model Details

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General Information of STINSON RELIANT

First Flight : 1933

Manufacturer : Stinson Aircraft Company

National Origin : United States

Number Built : 1327

Primary Users : United States Army Air Corps

Role : Liaison and training monoplane

General characteristics of STINSON RELIANT

Capacity : 3 to 4 passengers

Crew : one, pilot

Empty Weight : 3,045 lb (1,384 kg)

Height : 8 ft 6 in (2.59 m)

Length : 27 ft 11 in (8.51 m)

Loaded_Weight : 4,605 lb (2,093 kg)

Powerplant : 1 × Pratt & Whitney Wasp Junior SB nine-cylinder air-cooled radial engine, 400 hp (298 kW)

Wing Area : 256.5 sq ft (23.84 m²)

Wingspan : 41 ft 7 in (12.68 m)

Performance of STINSON RELIANT

Cruise Speed : 154 knots (177 mph, 285 km/h)

Range : 739 nmi (850 mi, 1,369 km)

Rate Of Climb : 1,330 ft/min (6.8 m/s)

Service Ceiling : 21,000 ft (6,400 m)

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