Engineering Division XCO-6
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|National origin||United States|
|Primary user||United States Army Air Service|
Design and development
- Prototype two-seat single-engined observation biplane.
- Proposed variant with the main fuel tanks moved into the upper wing, not built.
- A XCO-6 modified with a change of engine to a 435 hp (324 kW) Liberty 12A engine.
- XCO-6B modified with a larger propeller and changes to the landing gear.
Data from 
- Crew: 2
- Length: 29 ft 8 in (9.04 m)
- Wingspan: 48 ft 0 in (14.63 m)
- Powerplant: 1 × Liberty V-1410 V-12 water-cooled piston engine, 420 hp (310 kW)
- Related lists
|Wikimedia Commons has media related to Engineering Division XCO-6.|
- Andrade 1979, p. 96
- Eckland, K.O. (2008-08-15). "American airplanes: E". Aerofiles.com. Retrieved 2011-02-04.