johnbr

XA21-bia

Stearman XA-21 (1938) XA-21 Chaser Stearman (U.S.) _______________________________________________________ . Crew: 03 Length: 16.18 m Wingspan: 19.81 m Height: 4.32 m Unladen weight: 5789 kg Maximum takeoff: 8,269 kg Engine: 02 turboprop Pratt & Whitney R-2180-7 1400 horse thrust each. Speed: 414 km / h Altitude: 6100 m Range: 2,400 km Fire: age 04 to 30 (7.62 mm) Browning M1919 nose wing + 01 + 04 in the rear, 1,200 kg bombs. First flight: 1938 Number produced: 01 prototypes. National use: the United States. Compare flight: Douglas A-20 Havoc , Martin

XA21-bia
johnbr, Apr 25, 2011
    • elzombie
      {ppcode}

      The engines are not turbo-prop; that implies a prop driven by a jet-turbine.These are Air-Cooled Radial engines. See http://en.wikipedia.org/wiki/Stearman_XA-21
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