Specifications

General Characteristics

* Crew: None
* Landing Type: runway
* Launch Type: runway
* Length: 11 m
* Wingspan: (20 m
* Height: 3.6 m
* Empty weight: 2223 kg
* Fuel Capacity: 1,800 kg
* Max takeoff weight: 4760 kg
* Power Plant: Honeywell TPE331-10 turboprop engine, 671 kW, with Digital Electronic Engine Control (DEEC)

Performance

* Maximum speed: 482 km/h, 300 mph
* Cruise speed: 276–313 km/h, 172–195 mph
* Range: (5,926 km, 3,682 mi
* Endurance: 14–28 hours
* Payload: 1,700 kg
* * Internal: 360 kg
* * External: 1,400 kg
* Service ceiling: 15 km
* Operational altitude: 7.5 km

Sensors

* AN/APY-8 Lynx II radar
* AN/DAS-1 MTS-B Multi-Spectral Targeting System

Armament

* 7 Hardpoints
* * Up to 1,500 lb on the two inboard weapons stations
* * Up to 750 lb on the two middle stations
* * Up to 150 lb on the outboard stations
* * Center station not used
* Up to 14 AGM-114 Hellfire air to ground missiles can be carried or four Hellfire missiles and two 500 lb GBU-12 Paveway II laser-guided bombs. The 500 lb (230 kg) GBU-38 Joint Direct Attack Munition (JDAM) can also be carried. Testing is underway to support the operation of the AIM-92 Stinger air-to-air missile.