|Role||Liaison and training monoplane|
|National origin||United States|
|Manufacturer||Stinson Aircraft Company|
|Primary user||United States Army Air Corps|
Design and development
The Reliant is a high-wing, fixed-tailwheel land monoplane powered with a variety of radial engines.
1,327 Reliants of all types were made from 1933 to 1941, in different models, from SR-1 to SR-10. The final commercial model, the Stinson Reliant SR-10, was introduced in 1938. A militarized version was first flown in February 1942 and remained in production through several additional versions (all externally identical) until late 1943 for the US and British armed forces.
Reliant production can be broken into two distinct types – the straight-wing Reliants (all models up to SR-6) and the gull-wing Reliants (all models from SR-7 and after, including the militarized V-77/AT-19), with there being little in common between the two groups of types. The straight-wing Reliant has a wing of constant chord and thickness which is supported by two struts each side with additional bracing struts. In contrast the taper-wing Reliant has the broadest chord and thickness of the wing at mid-span, with the outer wing trailing edge heavily angled forward and a rounded cutout on the leading edge root, all supported by a single strut. The taper wing has a significant step up between the fuselage and the wing, and the changes in wing thickness gave it a distinct gull appearance from the front.
The Reliant was used by the United States Army Air Forces in World War II as a utility aircraft, designated UC-81, and as trainer designated AT-19. The Royal Navy and Royal Air Force also used Reliants, for light transport and communication duties. After the war they were sold on the civilian market as the Vultee V-77.
The V-77 is a spartan version of the SR-10 with the 300 hp Lycoming R680-E3B, a single door on the left side and the traditional "bump" cowl was replaced with a simpler smooth cowl. Internal structure was beefed up significantly over the commercial models, and a distinctive triangle-shaped counterbalance was added to the rudder.
- Ambulance (two stretchers)
- Target Towing
- SR Reliant
- Powered by a 215 hp (160 kW) Lycoming R-680 radial piston engine.
- Powered by a 240 hp (180 kW) Lycoming R-680-2 radial piston engine. Two built.
- Powered by a 240-hp (179-kW) Lycoming R-680-7 radial piston engine.
- Similar to the SR-1, but with minor structural changes.
- Powered by a 250-hp (186-kW) Wright R-760-E radial piston engine.
- Improved version, powered by a 225-hp (168-kW) Lycoming R-680-4 radial piston engine.
- Powered by a 245-hp (183-kW) Lycoming R-680-6 radial piston engine.
- Powered by a 240-hp (179-kW) Lycoming R-680-2 radial piston engine.
- Powered by a 260-hp (194-kW) Lycoming R-680-5 radial piston engine.
- Powered by a 225-hp (168-kW) Lycoming R-680-4 radial piston engine.
- Powered by a 250-hp (186-kW) Wright R-760-E radial piston engine.
- Five-seat cabin aircraft, powered by a Lycoming R-680-6 radial piston engine.
- Four-seat cabin aircraft, powered by a 225-hp (168-kW) Lycoming R-680-4 radial piston engine.
- Four-seat cabin aircraft, powered by a Lycoming R-680-5 radial piston engine.
- First gull wing series.
- Five-seat cabin aircraft, powered by a Lycoming R-680-B6 radial piston engine. 47 built.
- Five-seat cabin aircraft, powered by a Lycoming R-680-B5 radial piston engine. Three built.
- Four-seat cabin aircraft.
- Four-seat cabin aircraft, powered by a Lycoming R-680-B6 radial piston engine.
- Four-seat cabin aircraft, powered by a Lycoming R-680-B5 radial piston engine.
- Four-seat cabin aircraft, powered by a Wright R-760-E2 radial piston engine.
- Utility transport version of the SR-8D.
- Five-seat cabin aircraft, powered by a 320-hp (239-kW) Wright R-760-E23 radial piston engine.
- Utility transport version of the SR-8E.
- 1937 series. Fitted with a curved windshield, unique to this series.
- Proposed version with Lycoming R-680-B4 engine. Unbuilt.
- Powered by a 245 horsepower (183 kW) Lycoming R-680-B6 engine. 35 built.
- Powered by a 260 horsepower (190 kW) Lycoming R-680-B5 engine. 65 built.
- Powered by a 285 horsepower (213 kW) Wright R-760-E1 engine. 22 built.
- Powered by a 320 horsepower (240 kW) Wright R-760-E2 engine. 43 built.
- Powered by a 450 horsepower (340 kW) Pratt & Whitney Wasp Junior radial engine. 34 built.
- Powered by a Lycoming R-680-D6. One built.
- Powered by a Lycoming R-680-D5 engine. 46 built.
- Wright R-760E-1 engine. 3 built.
- Powered by a Wright R-760E-2 radial piston engine. 21 built.
- Powered by a Pratt & Whitney R-985 Wasp Junior SB radial piston engine. 18 built.
- Powered by a Lycoming R-680-E1 radial piston engine. 12 built.
- Lycoming R-680-E3 engine. 11 built.
- Wright R-760E-3. Two built.
- USAAF designation for a training variant of the UC-81 for the Royal Navy under Lend-Lease as the Reliant I, 500 built.
- Original designation of the L-9A which was a Voyager not a Reliant.
- Original designation of the L-9B which was a Voyager not a Reliant.
- Conversions of AT-19s for photo-survey aircraft for the USAAF, 51 conversions.
- Four impressed SR.8Bs.
- Two impressed SR.10Gs.
- One impressed SR.8E.
- Three impressed SR.9Cs.
- One civil SR.10F operated by the military for the development of glider pick-up techniques.
- Four impressed SR.9Fs.
- Seven impressed SR.10Fs.
- Three impressed SR.9Ds.
- One impressed SR.10E.
- Nine impressed SR.9Es.
- Five impressed SR.10Cs.
- Two impressed SR.8Cs.
- One impressed SR.9EM.
- Two impressed SR.9Bs.
- Two SR.5As impressed into service with the USAAF during World War II.
- Two SR.7Bs impressed into service during World War II.
- One SR-5 Reliant was acquired by the US Coast Guard in 1935, later redesignated XR3Q-1 and decommissioned in 1941.
- One SR-5 Reliant was acquired by the US Navy in 1935.
- Reliant I
- 500 Reliants were supplied to the Royal Navy under Lend-Lease. The Reliants were used for light transport and communications, navigation and radio training duties.
- Aeronaves de México – the Reliant was the first aircraft used by Aeronaves, later to become Mexico's largest airline, Aeromexico, on their initial service between Mexico and Acapulco on 14 September 1934
- Líneas Aéreas de Transporte Nacional (LATN)
- Crew: one, pilot
- Capacity: 3 to 4 passengers
- Length: 27 ft 11 in (8.51 m)
- Wingspan: 41 ft 7 in (12.68 m)
- Height: 8 ft 6 in (2.59 m)
- Wing area: 256.5 sq ft (23.84 m²)
- Empty weight: 3,045 lb (1,384 kg)
- 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)
- Pilot's Flight Operating Instructions for Army Model AT-19 Airplanes and British Model Reliant – 15 June 1944
- Stinson SR-10 Specifications – April 1940
- Wegg 1990, pp. 131, 133.
- Wegg 1990, p. 132.
- Wegg 1990, p. 135.
- Wegg 1990, p. 136.
- Aviation February 1937, p. 36.
- Wegg 1990, pp. 136–137.
- Wegg 1990, p. 137.
- Andrade 1979, p.79
- Andrade 1979, p.81
- Andrade 1979, p.130
- Pearcy 1991, p. 317.
- "A38 Stinson Reliant". RAAF Museum. 2009. Retrieved 20 January 2013.
- Halley 1980, p. 306.
- Swanborough and Bowers 1963, p. 532.
- Aeromexico – The Story of a Great Company, last accessed on 2012 November 30
- Andrade, John (1979). U.S.Military Aircraft Designations and Serials since 1909. Midland Counties Publications. ISBN 0-904597-22-9.
- Halley, James J (1980). The Squadrons of the Royal Air Force. Tonbridge, Kent, UK: Air Britain (Historians). ISBN 0 85130 083 9.
- Pearcy, Arthur (1991). U.S. Coast Guard Aircraft Since 1916. Shrewsbury, UK: Airlife Publishing. ISBN 1-85310-118-4.
- "Stinson Restyles". Aviation Week & Space Technology. Vol. 36 no. 2. February 1937. pp. 35–36.
- Swanborough, F. G.; Bowers, Peter M. (1963). United States Military Aircraft since 1909. London: Putnam.
- Swanborough, Gordon; Bowers, Peter M. (1976). United States Navy Aircraft since 1911 (Second ed.). London: Putnam. ISBN 0-370-10054-9.
- Wegg, John (1990). General Dynamics Aircraft and their Predecessors. London: Putnam. ISBN 0-85177-833-X.
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