FACT SHEET

MC-130P Combat Shadow

Mission

The Combat Shadow flies clandestine or low visibility, single or multi-ship low-level missions intruding politically sensitive or hostile territory to provide air refueling for special operations helicopters. The MC-130P primarily flies missions at night to reduce probability of visual acquisition and intercept by airborne threats.

Secondary mission capabilities may include airdrop of small special operations teams, bundles and combat rubber raiding craft, as well as night vision goggles, takeoff and landing procedures and in-flight refueling as a receiver.

 

Features

Special operations forces improvements are being made to the fleet of MC-130P's. When modifications are completed in Fiscal 2000, all MC-130P's will feature improved navigation, communications, threat detection and countermeasures systems. When fully modified, the Combat Shadow fleet will have a fully-integrated inertial navigation and global positioning system, and night vision goggle compatible interior and exterior lighting. It will also have forward looking infrared, radar and missile warning receivers, chaff and flare dispensers, night vision goggle compatible heads-up display, satellite and data-burst communications, as well as in-flight refueling capability as a receiver (on 15 aircraft).

The Combat Shadow can fly in the day against a reduced threat. The crews fly night low-level, air refueling and formation operations using night vision goggles. To enhance the probability of mission success and survivability near populated areas, employment tactics incorporate no external lighting and no communications to avoid radar and weapons detection.

 

History

MC-130P's were previously designated HC-130N/P. However, the "H" designation is a rescue and recovery mission code and not representative of the aircraft's special operations role. In February 1996, AFSOC's tanker fleet was redesignated MC-130P's, aligning the Combat Shadow with other M-series special operations mission aircraft. MC-130P's have been a part of the special operations mission since the mid-80s. They provided critical air refueling to Army and Air Force helicopters during Operation Just Cause in Panama in 1989. In 1990, the aircraft deployed to Saudi Arabia and Turkey for Operation Desert Storm and provided air refueling of special operations helicopters over friendly and hostile territory.

Since Desert Storm, the MC-130P has been involved in operations Northern and Southern Watch, supporting efforts to keep Iraqi aircraft out of the no-fly zones. Although MC-130P's left Southern Watch in 1993, they have returned periodically to relieve Air Combat Command rescue forces. The aircraft also took part in Operation Deny Flight in Yugoslavia in 1993, and Operations Restore Democracy and Uphold Democracy in Haiti in 1994. The MC-130P has been involved in operations Deliberate Force and Joint Endeavor in Bosnia since 1995.

Additionally, the MC-130P took part in Operation Assured Response in 1996, providing air refueling for the MH-53s shuttling evacuees between Liberia and the rear staging area.

In March 1997, the MC-130P was diverted from Italy to provide combat search and rescue during the evacuation of non-combatant Americans from Albania. Also in 1997, the MC-130P provided command and control and refueling support during Operation Guardian Retrieval, the evacuation of Americans from Zaire. In July 1997, the aircraft provided aerial refueling for MH-53J's when U.S. forces prepared for possible evacuations of noncombatants from Cambodia. The aircraft also was part of Operation High Flight, the search to locate an American C-141 involved in a mid-air collision with another aircraft off the coast of Angola in September 1997.

 

General Characteristics

Primary Function: Air refueling for special operation forces helicopters
Builder: Lockheed
Power Plant: Four Allison T56-A-15 turboprop engines
Thrust: 4,910 shaft horsepower each engine
Length: 98 feet, 9 inches (30.09 meters)
Height: 38 feet, 6 inches (11.7 meters)
Wingspan: 132 feet, 7 inches (40.4 meters)
Speed: 289 mph (at sea level)
Ceiling: 33,000 feet (10,000 meters)
Maximum Takeoff Weight: 155,000 pounds (69,750 kilograms)
Range: Beyond 4,000 miles
Crew: Officers - pilot, co-pilot, right navigator and left navigator; enlisted - flight engineer, communications systems operator and two loadmasters
Date Deployed: 1986
Unit Flyaway Cost:(Fiscal Year 98 constant dollars): $18.6 million
Inventory: Active force, 19; Reserve, 0; ANG, 0

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