HC-130J Combat King II

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The HC-130J replaces HC-130P/Ns as the only dedicated fixed-wing Personnel Recovery platform in the Air Force inventory. It is an extended-range version of the C-130J Hercules transport. Its mission is to rapidly deploy to execute combatant commander directed recovery operations to austere airfields and denied territory for expeditionary, all weather personnel recovery operations to include airdrop, airland, helicopter air-to-air refueling, and forward area ground refueling missions. When tasked, the aircraft also conducts humanitarian assistance operations, disaster response, security cooperation/aviation advisory, emergency aeromedical evacuation, and noncombatant evacuation operations.

 

General Characteristics

Primary function: Fixed-wing Personnel Recovery platform

Contractor: Lockheed Aircraft Corp.

Power Plant: Four Rolls Royce AE2100D3 turboprop engines

Thrust: 4,591 Propeller Shaft Horsepower, each engine

Wingspan: 132 feet, 7 inches (40.4 meters)

Length: 97 feet, 9 inches (29.57 meters)

Height: 38 feet, 9 inches (11.58 meters)

Operating Weight: 89,000 pounds (40,369 kilograms)

Maximum Takeoff Weight: 164,000 pounds (74,389 kilograms)

Fuel Capacity: 61,360 pounds (9,024 gallons)

Payload: 35,000 pounds (15,875 kilograms)

Speed: 316 knots indicated air speed at sea level

Range: beyond 4,000 miles (3,478 nautical miles)

Ceiling: 33,000 feet (10,000 meters)

Armament: countermeasures/flares, chaff

Basic Crew: Three officers (pilot, co-pilot, combat system officer) and two enlisted loadmasters

Unit Cost: $66 million (fiscal 2010 replacement cost)

Initial operating capability: 2013