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