Curtiss-Wright CW-12
CW-12 | |
---|---|
Type: | Trainer aircraft |
Design country: | |
Manufacturer: | |
First flight: |
1931 |
Production time: |
1930s |
Number of pieces: |
63 |
The CW-12 Sport Trainer and the CW-16 Light Sport are biplane training aircraft made by the US manufacturer Curtiss-Wright . They were developed in the early 1930s by designers Herbert Rawdon and Ted A. Wells , who previously worked for Travel Air . The aircraft were therefore sometimes referred to as Curtiss-Wright Travel Airs.
construction
The CW-12 and CW-16 are both based on the same construction. They are double-deckers with staggered wings that are connected to each other by means of N-struts. The pilot and the flight instructor sit in tandem in open cockpits . In contrast to the CW-12, whose front cockpit has only one seat, the CW-16 has two seats arranged side by side in the front cockpit. Both machines were available with a number of different engines .
Versions
- CW-12
- CW-12K - powered by a Kinner K-5 , two built copies
- CW-12Q - powered by a Wright- built de Havilland Gipsy , 26 units built
- CW-12W - powered by a Warner Scarab , twelve (plus one replica ) built
- CW-16
- CW-16E - powered by a Wright J-6 Whirlwind 5 , ten copies built
- CW-16K - powered by a Kinner B-5 , eleven built
- CW-16W - powered by a Warner Scarab, a built example
use
In addition to private owners, the following armed forces operated the machines:
- The Argentine Navy Armada Argentina bought fifteen units in 1935 with an option for thirteen more in 1938. The machines were used until 1949.
- The Bolivian Air Force purchased three CW-16s in 1934 and used them until 1943.
- The Brazilian Air Force Força Aérea Brasileira received fifteen CW-16Ws with Warner-Scarab engines with 125 PS (92 kW) in 1935 . The machines were decommissioned in 1940.
- The Colombian Air Force operated six CW-16s from 1933.
- The Ecuadorian Air Force Fuerza Aérea Ecuatoriana purchased six CW-16E in 1935 and three CW-16s in 1936. Three of the machines remained in service until 1944.
Technical specifications
Parameter | CW-12Q data |
---|---|
crew | 2 |
length | 6.52 m |
span | above: 8.78 m below: 8.02 m |
height | 2.69 m |
Wing area | 19.18 m² |
Empty mass | 1,071 lb (486 kg ) |
Max. Takeoff mass | 1,725 lb (782 kg) |
Cruising speed | 141 km / h |
Top speed | 169 km / h |
Service ceiling | 12,000 ft (3,658 m) |
Range | 772 km |
Engines | 1 × air-cooled four-cylinder in- line engine Curtiss-Wright Gipsy with 90 PS (66 kW ) |
See also
literature
- Peter M. Bowers: Curtiss Aircraft 1907-1947 . Putnam, London 1979, ISBN 0-370-10029-8 (English).
- Michael JH Taylor: Jane's Encyclopedia of Aviation . Studio Editions, London 1989, pp. 288 (English).
- World Aircraft Information Files . Bright Star Publishing, London (English).
Web links
Individual evidence
- ^ Dan Hagedorn: Curtiss Types in Latin America . In: Air Enthusiast . March to May 1992. Key Publishing, ISSN 0143-5450 , p. 76 (English).
- ^ A b c Dan Hagedorn: Curtiss Types in Latin America . In: Air Enthusiast . March to May 1992. Key Publishing, ISSN 0143-5450 , p. 75 (English).
- ^ Dan Hagedorn: Curtiss Types in Latin America . In: Air Enthusiast . March to May 1992. Key Publishing, ISSN 0143-5450 , p. 75-76 (English).
- ^ AJ Pelletier: Beech Aircraft and their Predecessors , Putnam Aeronautical, 1995, p. 48