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Engineering Division XCO 6

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Engineering Division XCO-6 httpsuploadwikimediaorgwikipediacommonsthu

The Engineering Division XCO-6 was an American two-seat observation biplane designed by the United States Army Engineering Division, only two were built and the type did not enter production.

Contents

Design and development

Two prototypes of the XCO-6 were built powered by a 420 hp (313 kW) inverted air-cooled V-1410 engine. One was tested at McCook Field and subsequently modified but no others were built.

Variants

XCO-6
Prototype two-seat single-engined observation biplane.
XCO-6A
Proposed variant with the main fuel tanks moved into the upper wing, not built.
XCO-6B
A XCO-6 modified with a change of engine to a 435 hp (324 kW) Liberty 12A engine.
XCO-6C
XCO-6B modified with a larger propeller and changes to the landing gear.

Specifications (XCO-6)

Data from

General characteristics

  • 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)

    • Performance

    References

    Engineering Division XCO-6 Wikipedia
    (Text) CC BY-SA


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