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MC-130J Commando II


Mission
The Commando II flies clandestine, or low visibility, single or multiship, low-level air refueling missions for special operations helicopters and tiltrotor aircraft, and infiltration, exfiltration, and resupply of special operations forces (SOF) by airdrop or airland intruding politically sensitive or hostile territories. The MC-130J primarily flies missions at night to reduce probability of visual acquisition and intercept by airborne threats. Its secondary mission includes the airdrop of leaflets.

Features
The MC-130J includes: advanced two-pilot flight station with fully integrated digital avionics; fully populated Combat Systems Operator (CSO) and auxiliary flight deck stations; 13 color multifunctional liquid crystal displays; head-up displays; fully integrated navigation systems with dual inertial navigation system and global positioning system; integrated defensive systems; low-power color radar; digital moving map display; new turboprop engines with six-bladed, all-composite propellers; digital auto pilot; improved fuel, environmental and ice-protection systems; enhanced cargo-handling system; Universal Air Refueling Receptacle Slipway Installation (UARRSI), air refueling pods, Electro Optical/Infrared (EO/IR) System; dual SATCOM for voice/data; 60/90 KVA generators; increased DC electrical output, loadmaster/scanner restraint system; and LAIRCM provisions.

Background
The MC-130J is replacing the aging SOF fleet of 37 MC-130E and P tankers. The first aircraft was delivered in September 2011 to Cannon Air Force Base, N.M., with final delivery expected in fiscal year 2017.

General Characteristics
Primary Function: Air refueling of SOF helicopter/tilt rotor aircraft, infiltration, exfiltration and resupply of SOF by airdrop or airland
Builder: Lockheed Martin
Power Plant: Four Rolls-Royce AE 2100D3 Turboprops
Thrust: 4,591 shaft horsepower
Wingspan: 132 feet, 7 inches (39.7 meters)
Length: 97 feet 9 inches (29.3 meters)
Height: 38 feet 10 inches (11.9 meters)
Speed: 362 knots at 22,000 feet
Ceiling: 28,000 feet with 42,000 lb payload
Maximum Takeoff Weight: 164,000 lbs
Range: 3,000 miles
Crew: Two pilots, one Combat Systems Officer (officers), and two Loadmasters (enlisted)
Date Deployed: 2011
Unit Cost: $67 million (fiscal 2010 dollars)
Inventory: Active duty, 37 by fiscal 2017

(Current as of December 2013)