General characteristics Crew: 6 (one pilot, one co-pilot, navigator/bombardier, turret gunner/engineer, radio operator/waist gunner, tail gunner) Length: 52 ft 11 in (16.13 m) Wingspan: 67 ft 7 in (20.60 m) Height: 16 ft 4 in (4.98 m) Wing area: 610 sq ft (56.7 m²) Empty weight: 19,480 lb (8,855 kg) Max. takeoff weight: 35,000 lb (15,910 kg) Powerplant: 2 × Wright R-2600-92 Twin Cyclone 14-cylinder air-cooled radial engine, 1,700 hp (1,267 kW) each Performance Maximum speed: 272 mph (237 kn, 438 km/h) at 13,000 ft (3,960 m) Cruise speed: 230 mph (200 knots, 370 km/h) Range: 1,350 mi (1,174 nmi, 2,174 km) Service ceiling: 24,200 ft (7,378 m) Armament Guns: 12–18 × .50 in (12.7 mm) machine guns and 75 mm (2.95 in) T13E1 cannon Hardpoints: 2,000 lb (900 kg) ventral shackles to hold one external Mark 13 torpedo[43] Rockets: racks for eight 5 in (127 mm) high velocity aircraft rockets (HVAR) Bombs: 3,000 lb (1,360 kg) bombs From Wiki
VERTICAL LIMIT AVIATION LLC ALBUQUERQUE , NM, US LYCOMING IO-540-AE1A5 (Reciprocating) Horsepower: 260
Crew: 2 Length: 30 ft 10 in - 32 ft 2 in (9.4 m - 9.8 m) Rotor diameter: 27 ft. 4 in (8.33 m) Height: 8 ft 6 in - 11 ft 2 in (2.6 m - 3.4 m) Empty weight: 1,975 lbs (896 kg) Maximum take-off weight: 3,549 lbs (1,610 kg) Powerplant: 1 × One Allison T63-A-5A or T63-A-700 turbo shaft, 317 hp (236 kW) Performance: Maximum speed: 152 knots (175 mph, 282 km/h) Cruise speed: 135 knots (155 mph, 250 km/h) Range: 232 nm (430 km) Service ceiling: 15,994 ft (4,875 m) Rate of climb: 2,067 ft/min (10.5 m/s)
