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DOUGLAS B-23 DRAGON


GENERAL INFORMATION
  Type: Medium Bomber
  Origin: Douglas
  Crew/Seats: Four/Five
  Model: B-23 & UC-67
  First Flight: July 27, 1939
  Production: 350

POWERPLANT:
  Model: Wright R-2600-3 Cyclone 14
  Type: Radial piston engine
  Number: Two       Horsepower: 1,600 hp

DIMENSIONS:
  Wing span: 92 ft. 0 in. (28.04m)
  Length: 58 ft. 4¾ in. (17.8m)
  Height: 18 ft. 5½ in. (5.63m)
  Wing Surface Area: 993 Sq. Ft. (92.25m²)

WEIGHTS:
  Empty: 19,089 lb. (8,659 kg)
  Loaded: 32,400 lb. (14,696 kg)
  PERFORMANCE:
  Maximum Speed: 282 mph (454 kph) at 12,000 ft.
  Cruising Speed: 210 mph (338 kph)
  Initial Climb: N/A
  Service Ceiling: 31,600 ft. (9630m)
  Range: 1,400 miles (2253 km)

ARMAMENT:
One .50 machine gun in tail position.
Three .30 machine guns in nose, dorsal, and ventral positions.

PAYLOAD:
4,400 lb. (1996 kg) of bombs carried internally.

AVIONICS: N/A

COMMENTS:
Fifteen aircraft converted to utility transports under designation UC-67.

Sources:
Gunston, Bill - The Encyclodepia of the Worlds Combat aircraft, 1976, Chartwell Books, Inc., New York

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