Ryan S-C

Summary

The Ryan S-C (Sports-Coupe) (or Sport Cabin[1]) was an American three-seat cabin monoplane designed and built by the Ryan Aeronautical Company. At least one was impressed into service with the United States Army Air Forces as the L-10.

Ryan S-C
Ryan SCW-145 (NC18914) - 1.jpg
Ryan SCW-145
Role Three-seat cabin monoplane
National origin United States
Manufacturer Ryan Aeronautical Company
First flight 1937
Number built 13

DevelopmentEdit

The Ryan S-C was a low-wing cantilever monoplane with a fixed tailwheel landing gear, designed to be an up-market version of the Ryan S-T trainer. The prototype first flew in 1937, and had a nose-mounted 150 hp (112 kW) Menasco inline piston engine. Production aircraft were fitted with a 145 hp (108 kW) Warner Super Scarab radial engine. With the company's involvement in producing trainer aircraft for the United States military, the S-C was not seriously marketed, and only 11 complete SCs (s/n 202 through 212) were built, all delivered in 1938; two more were later assembled from parts (s/n 213 in 1941 and s/n 214 in 1959). At least one example – probably as many as five, s/n 202, 203, 207, 211 and 212[1] – were impressed into service with the Civil Air Patrol, auxiliary of the United States Army Air Forces for anti-submarine patrol and warfare duties on the East coast of the US, and was designated the L-10.[2] At the start of the 21st Century, four examples were still airworthy in the United States.

 
Ryan SCW-145

VariantsEdit

S-C later S-C-M
Prototype powered by a 150hp (112kW) Menasco C4S inline engine, one built later converted to S-C-W.
S-C-W
Production aircraft powered by a 145hp (108kW) Warner Super Scarab radial engine, 12 built.
L-10
United States Army Air Forces designation for one S-C-W impressed into service in 1942, it was disposed of in November 1944.[3]
Later Modifications
Two SC-Ws exist with a horizontally opposed 6-cylinder Continental engine. One was modified from a radial-powered SC-W, and one was built with the 6-cylinder engine after WWII using spare airframe parts from the original pre-WWII production run.

OperatorsEdit

  United States

Specifications (S-C-W)Edit

 
Ryan SCW 3-view drawing from L'Aerophile January 1938

Data from American Planes and Engines for 1940[4]

General characteristics

  • Crew: 1
  • Capacity: 2 passengers
  • Length: 25 ft 4+12 in (7.734 m)
  • Wingspan: 37 ft 6 in (11.43 m)
  • Height: 6 ft 10 in (2.08 m)
  • Wing area: 202.0 sq ft (18.77 m2)
  • Empty weight: 1,345 lb (610 kg)
  • Gross weight: 2,150 lb (975 kg)
  • Powerplant: 1 × Warner Super Scarab radial engine, 145 hp (108 kW)

Performance

  • Maximum speed: 150 mph (240 km/h, 130 kn) at sea level
  • Cruise speed: 135 mph (217 km/h, 117 kn) at 8,500 ft (2,600 m)
  • Stall speed: 45 mph (72 km/h, 39 kn)
  • Range: 525 mi (845 km, 456 nmi)
  • Service ceiling: 17,200 ft (5,200 m)
  • Rate of climb: 900 ft/min (4.6 m/s)

See alsoEdit

Related lists

ReferencesEdit

  1. ^ a b Cassagnere, Ev (1995) The new Ryan : development and history of the Ryan ST and SC, p. 119-144, Flying Books, Eagan, MN. ISBN 0911139206.
  2. ^ Donald, David (ed.) (1997) The Encyclopedia of World Aircraft, p. 792, Prospero Books, Etobicoke, ON. ISBN 185605375X.
  3. ^ Andrade 1979, p. 130
  4. ^ Aviation February 1940, pp. 42, 69–70.
  • "American Planes and Engines for 1940". Aviation. Vol. 39, no. 2. February 1940. pp. 36–54, 67–74.
  • Andrade, John M. U.S. Military Aircraft Designations and Serials since 1909. Leicester, England: Midland Counties Publications. ISBN 0 904597 22 9.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
  • World Aircraft Information Files. London: Bright Star Publishing.
  • Aerofiles

External linksEdit

  Media related to Ryan SCW at Wikimedia Commons