Engineering Division TW-1
|National origin||United States|
|Primary user||United States Army Air Service|
Design and development
Two prototypes of the TW-1 were built powered by a 230 hp (172 kW) Liberty 6. 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.
Data from aerofiles.com
- 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)
- Related lists
|Wikimedia Commons has media related to Engineering Division TW-1.|
- Andrade 1979, p. 171
- "American airplanes: Ea - Ew". www.aerofiles.com. 2 May 2009. Retrieved 13 November 2011.
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