General characteristics

Crew: Crew: 2 (pilot and 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[46]
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)
Combat Mission: 167 mph
Combat Range: 300 miles
Combat Endurance: 2.5 hours
Length: 49 ft 5 in
Mission Weight: 16,600 lbs
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
Manufacturer:
Airframe - Boeing (Mesa, AZ); Fire Control Radar - Northrup Grummen (Linthicum, MD); Lockheed Martin (Owego, NY); MTADS/PNVS - Lockheed Martin (Orlando, FL); Boeing (Mesa, AZ)