The Stinson L-13 (sometimes known as the Grasshopper, like other aircraft of its type) was a US military utility aircraft first flown in 1945. Developed when Stinson was a subsidiary of Consolidated Vultee, rights to it were not included in the 1948 sale of Stinson to Piper. Mass production was therefore undertaken by Convair, which built some 300 of them.
L-13 Grasshopper
Note the windows in the roof giving excellent field of vision
It was a conventional high-wing tailwheel monoplane used for observation, liaison, and air ambulance duties. Following their military service, some were converted for civil bush flying use, fitting a radial engine by Acme Aircraft Company as the Centaur, while others underwent similar conversions by Caribbean Traders Inc, as the Husky.[1]
Variants
XL-13
Prototype aircraft, powered by 245hp (183kW) Franklin O-425-6 engine. Two built.[2]
L-13A
Production aircraft, powered by 250hp (187kW) O-425-9 engine. 300 built.[2]
L-13B
Conversion of L-13A for cold weather operation, capable of operating from wheels, skis or floats. 28 converted.[3][4]
Acme Centaur 101
Conversion of L-13 as six-seat bush aircraft. Powered by 300hp (224kW) Lycoming R-680-E3.[1]
Acme Centaur 102
Similar to Acme Centaur 101, with a 300hp Jacobs R-755-A2 radial.[1]
L-13A converted to Caribbean Traders Husky III standard with a 450 h.p. Wright R-975 engine
Caribbean Traders Husky I
Civil conversion of L-13A. Retained O-425 engine.[1][5]
Caribbean Traders Husky II
Civil conversion of L-13A. Powered by 300hp R-680-13 engine on modified engine mount capable of swinging out for easy maintenance.[1][5]
Caribbean Traders Husky III
Similar to Husky II, but powered by 450hp (338kW) Wright R-975-7 radial engine.[1][5]
Servicair Loadmaster
Reconstruction of L-13A with 450 hp Pratt & Whitney R-985-AN-1 radial engine and rearranged four-seat cabin.[6]
Operators
United States
United States Air Force
United States Army received 43 ex-Air Force L-13As following the outbreak of the Korean War, serving in the Continental United States to free up aircraft for active service overseas.[7]
Specifications (L-13A)
3-view line drawing of the Stinson L-13A
Data from General Dynamics Aircraft and their Predecessors [8]
General characteristics
Crew: 1
Capacity: 2 passengers
Length: 31ft 9in (9.68m)
Wingspan: 40ft 5+1⁄2in (12.332m)
Height: 8ft 5in (2.57m)
Wing area: 270sqft (25m2)
Empty weight: 2,070lb (939kg)
Gross weight: 3,185lb (1,445kg)
Powerplant: 1 × Franklin O-425-9 air-cooled flat-six engine, 250hp (190kW)
Performance
Maximum speed: 115mph (185km/h, 100kn)
Cruise speed: 92mph (148km/h, 80kn)
Range: 368mi (592km, 320nmi)
Service ceiling: 15,000ft (4,600m)
Rate of climb: 830ft/min (4.2m/s)
See also
Aircraft of comparable role, configuration, and era
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