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Curtiss Wright CW 12

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Top speed
  
169 km/h

Length
  
6.52 m

Manufacturer
  
Curtiss-Wright

Wingspan
  
8.78 m

First flight
  
1931

Curtiss-Wright CW-12 httpsuploadwikimediaorgwikipediacommonsthu

The Curtiss-Wright CW-12 Sport Trainer and CW-16 Light Sport (also marketed under the Travel Air brand that Curtiss-Wright had recently acquired) were high-performance training aircraft designed by Herbert Rawdon and Ted Wells and built in the United States in the early 1930s.

Contents

Development

The CW-12 and CW-16 shared the same basic design as conventional single-bay biplanes with staggered wings braced with N-struts. The pilot and instructor sat in tandem, open cockpits, the forward cockpit of the CW-12 having a single seat, while the CW-16's forward cockpit could seat two passengers side-by-side. Both versions of the aircraft were available in a variety of engine choices, and some CW-16s were exported as trainers to the air forces of Bolivia and Ecuador.

Variants

CW-12
  • CW-12K - version powered by Kinner K-5 engine (2 built)
  • CW-12Q - version powered by Wright-built de Havilland Gipsy (26 built)
  • CW-12W - version powered by Warner Scarab (12 built + 1 replica)
  • CW-16
  • CW-16E - version powered by Wright J-6 Whirlwind 5 engine (10 built)
  • CW-16K - version powered by Kinner B-5 engine (11 built)
  • CW-16W - version powered by Warner Scarab engine (1 built)
  • Operators

    Civil owners in USA and United Kingdom

     Argentina
  • Argentine Navy purchased 15 CW-16Es in 1935, with 13 more possibly being built from 1938. The type remained in use until 1949.
  •  Bolivia
  • Bolivian Air Force purchased three CW-16s in 1934, with the type in use until 1943.
  •  Brazil
  • Brazilian Air Force received 15 CW-16Ws, with 125 hp (93 kW) Warner Scarab engines in 1935, the type remaining in service until 1940.
  •  Colombia
  • Colombian Air Force received six CW-16s in 1933.
  •  Ecuador
  • Ecuadorian Air Force purchased six CW-16Es in 1935, with three more CW-16s following in 1936. Three remained in use until 1944.
  • Specifications (CW-12Q)

    Data from Curtiss Aircraft 1907–1947

    General characteristics

  • Crew: Two, pilot and instructor
  • Length: 21 ft 5 in (6.52 m)
  • Wingspan: 28 ft 10 in (8.78 m)
  • Height: 8 ft 10 in (2.69 m)
  • Wing area: 206 ft2 (19.1 m2)
  • Empty weight: 1,017 lb (486 kg)
  • Gross weight: 1,725 lb (782 kg)
  • Powerplant: 1 × Curtiss-Wright licence-built de Havilland Gipsy, 90 hp (67 kW) each
  • Performance

  • Maximum speed: 105 mph (169 km/h)
  • Cruise speed: 88 mph (142 km/h)
  • Range: 390 miles (628 km)
  • Service ceiling: 12,000 ft (3,660 m)
  • Rate of climb: 600 ft/min (3.0 m/s)
  • References

    Curtiss-Wright CW-12 Wikipedia


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