Specifications (AH-64A/D)
General characteristics
- Crew: 2: pilot, CPG (co-pilot/gunner)
- Length: 58.17 ft (17.73 m) (with both rotors turning)
- Rotor diameter: 48 ft 0 in (14.63 m)
- Height: 12.7 ft (3.87 m)
- Disc area: 1,809.5 ft² (168.11 m²)
- Empty weight: 11,387 lb (5,165 kg)
- Loaded weight: 17,650 lb (8,000 kg)
- Max takeoff weight: 23,000 lb (10,433 kg)
- Powerplant: 2× General Electric T700-GE-701 and later upgraded to T700-GE-701C (1990-present) & T700-GE-701D (AH-64D block III) turboshafts, -701: 1,690 shp, -701C: 1,890 shp, -701D: 2,000 shp (-701: 1,260 kW, -701C: 1,490 kW, -701D: 1,490 kW) each
- Fuselage length: 49 ft 5 in (15.06 m)
- Rotor systems: 4 blade main rotor, 4 blade tail rotor in non-orthogonal alignment[45]
Performance
- Never exceed speed: 197 knots (227 mph, 365 km/h)
- Maximum speed: 158 knots (182 mph, 293 km/h)
- Cruise speed: 143 knots (165 mph, 265 km/h)
- Combat radius: 260 nmi (300 mi, 480 km)
- Ferry range: 1,024 nmi (1,180 mi, 1,900 km)
- Service ceiling: 21,000 ft (6,400 m)
- Rate of climb: 2,500 ft/min (12.7 m/s)
- Disc loading: 9.80 lb/ft² (47.90 kg/m²)
- Power/mass: 0.18 hp/lb (310 W/kg)
Armament
- Guns: 1× 30x113 mm (1.18x4.45 in) M230 cannon, 1,200 rounds
- Rockets: Hydra 70 FFAR rockets
- Missiles: combination of AGM-114 Hellfire, AIM-92 Stinger, and AIM-9 Sidewinder
