U.S. NAVAL AVIATION RESOURCE CENTER > BOMBERS > SEAWOLF > PREVIOUS PAGE

CONSOLIDATED TBY SEA WOLF
Specifications

Type: Torpedo bomber
Manufacturer: Consolidated Aircraft
Designed by: Vought
  Crew: 3
Maiden flight: December 22, 1941
Introduced: 1944

Powerplant:
Manufacturer: Pratt & Whitney
Model: R-2800-6 Double Wasp
Type: radial engine
Number: One
Horsepower: 2,000 hp

Dimensions:
Length: 39 ft 2in (11.95 m)
Wingspan: 56 ft 11in (17.35 m)
Height: 15 ft 6in (4.72 m)
Wing area: 440 ft² (40.88 m²)

Weights:
Empty weight: 11,366 lb (5,142 kg)
Max takeoff weight: 18,448 lb (8,386 kg)

  Performance:
Maximum speed: 306 mph (492 km/h)
Range: 1,500 mi (2,414 km)
Service ceiling: 27,200 ft (8,290 m)

Armament
1× .50 cal (12.7 mm) Browning M2
      machine gun in cowling
2× .50 cal in the wings
1× .50 cal in dorsal turret
1× .30 cal (7.62 mm) M1919 Browning
      machine gun in ventral mount
Up to 2,000 lb (907 kg) of bombs
or one torpedo


Sources:
Wikipedia: Consolidated TBY Sea Wolf

U.S. NAVAL AVIATION RESOURCE CENTER > BOMBERS > SEAWOLF > PREVIOUS PAGE