| Crew: | 2: one pilot, one co-pilot/gunner (CPG) |
| Rotor diameter: | 44 ft (13.6 m) |
| Height: | 13 ft 6 in (4.12 m) |
| Empty Weight: | 6,600 lb (2,993 kg) |
| Max. Takeoff Weight: | 10,000 lb (4,500 kg) |
| Powerplant: | 1 × Lycoming T53-L-703 turboshaft, 1,800 shp (1,300 kW) |
| Length: | 53 ft (16.1 m) (with both rotors turning) |
| Rotor System: | 2 blades on main rotor, 2 blades on tail rotor |
| Fuselage length: | 44 ft 7 in (13.6 m) |
| Stub Wing Span: | 10 ft 4 in (3.15 m) |
General Characteristics
Performance
| Never exceed speed: | 170 knots (196 mph, 315 km/h) |
| Maximum speed | 149 knots (172 mph, 277 km/h) |
| Range: | 274 nmi (315 mi, 510 km) |
| Service ceiling: | 12,200 ft (3,720 m) |
| Rate of climb: | 1,620 ft/min (8.2 m/s) |
Armament
| General Dynamics: | 20 mm (0.787 in) M197 3-barreled gatling cannon |
| Hydra | 70 2.75 in (70 mm) rockets - 7 rockets mounted in the M260 launcher or 19 rockets in the M261 launcher[50] |
| TOW Missiles: | 4 or 8 missiles mounted in two-missile launchers on each hardpoint |
