Lockheed AH-56 Cheyenne - Specifications (AH-56A)

Specifications (AH-56A)

Data from Jane's Aircraft WarbirdTech AH-56A

General characteristics

  • Crew: Two; one pilot, one copilot/gunner (front seat)
  • Length: 54 ft 8 in (16.66 m)
  • Rotor diameter: 51 ft 3 in (15.62 m)
  • Height: 13 ft 8.5 in (4.18 m)
  • Empty weight: 12,215 lb (5,540 kg)
  • Loaded weight: 18,300 lb (8,300 kg)
  • Max. takeoff weight: 25,880 lb (11,740 kg)
  • Powerplant: 1 × General Electric T64-GE-16 turboshaft, 3,925 shp (2,930 kW)
  • Rotor systems: 4 blades on main rotor, 4 blades on tail rotor, 3 blades on pusher propeller

Performance

  • Maximum speed: 212 knots (244 mph, 393 km/h)
  • Cruise speed: 195 knots (225 mph, 362 km/h)
  • Range: 1,063 nmi (1,225 mi, 1,971 km)
  • Service ceiling: 20,000 ft (6,100 m)
  • Rate of climb: 3,000 ft/min (15.23 m/s)

Armament

  • Guns:
1 × nose turret with either an M129 40 mm (1.57 in) grenade launcher or an XM196 7.62x51 mm machine gun and
1 × belly turret with an XM140 30 mm (1.18 in) cannon
  • Hardpoints: 6
  • Rockets: 2.75 in (70 mm) FFA rockets
  • Missiles: BGM-71 TOW missiles

Read more about this topic:  Lockheed AH-56 Cheyenne