Engineering Division TW-1

TW-1
General information
Type	Training biplane
National origin	United States
Manufacturer	Engineering Division
Primary user	United States Army Air Service
Number built	2
History
First flight	1920

The Engineering Division TW-1 was an American two-seat training biplane designed by the United States Army Engineering Division, only two were built and the type did not enter production. ^{[1] [2]}

Design and development

Two prototypes of the TW-1 were built powered by a 230 hp (172 kW) Liberty 6. ^[1] The second aircraft was tested at McCook Field, (given the McCook designation P-200) and subsequently modified with a 350 hp (261 kW) Packard 1A-1237 engine but no others were built. ^[1]

Specifications

Data from ^[2] aerofiles.com

General characteristics

• Crew: 2
• Length: 28 ft 10 in (8.79 m)
• Wingspan: 41 ft 0 in (12.5 m)
• Powerplant: 1 × Liberty 6 , 230 hp (172 kW)

See also

Related lists

• List of military aircraft of the United States

References

Notes

1. Andrade 1979, p. 171
2. "American airplanes: Ea - Ew". www.aerofiles.com. 2 May 2009. Retrieved 13 November 2011.

Bibliography

• Andrade, John (1979). U.S. Military Aircraft Designations and Serials since 1909. Hinckley, Leicestershire, UK: Midland Counties Publications. ISBN   0-904597-22-9.