Powered by the 1,850 hp Pratt & Whitney R-2800-20 Double Wasp eighteen-cylinder two-row air-cooled radial engine, the aircraft could carry up to 2,000 lb (907 kg) of bombs or one torpedo. Defensive armament consisted of four 0.50 in (12.7 mm) machine guns (one in the engine cowling, two in the wings, one in the dorsal turret), and a single 0.30 cal (7.62 mm) machine gun in the ventral mount.
During an arrested landing test at NAS Anacostia, Washington, D.C. in 1942, the hook caught and tore the whole rear end off the airplane. The airplane was repaired in four weeks, however, while being pushed out, a Navy cadet who was taxiing in the same area lost control of his aircraft and plowed into the tail of the XTBU-1. Rebuilt again, the prototype was finally accepted by the USN, and the aircraft was ordered into production in September 1943.
As Vought was heavily committed to F4U and other contracts, production of 1,100 aircraft (BuNo. 30299 to 31398) was undertaken by Consolidated-Vultee under the designation TBY-2 Sea Wolf and the first aircraft was delivered in November 1944. However, only 180 were completed (BuNo. 30299 to 30367, 30369, 30371 to 30480) before the contract was canceled, while the TBY-2 never became operational.
Span: 56 ft 11in (17.35 m)
Length: 39 ft 2in (11.94 m)
Height: 15 ft 6 in (4.73 m)
Wing area: 440 sq.ft (40.88 sq.m)
Weight empty: 11,366 lb (5,156 kg)
Max T/O weight: 18,940 lb (8,591 kg)
Max speed: 312 mph (502 kmh)
Service ceiling: 29,400 ft (8,961 m)
Range: 1,025 mls (1,650 km)
