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C-141 STARLIFTER

Click for larger imageMission

The C-141 Starlifter fulfills the vast spectrum of airlift requirements through its ability to airliftcombat forces over long distances, deliver those forces and their equipment either by air, land or airdrop, resupply forces, and transport the sick and wounded from the hostile area to advanced medical facilities.

Features

The C-141B is a "stretched" C-141A with in-flight refueling capability. The stretching of the Starlifter consisted of lengthening the planes 23 feet 4 inches (7.11 meters). The added length increased the C-141 cargo capacity by about one-third, for an extra 2,171 cubic feet (62.03 cubic meters). The lengthening of the aircraft had the same overall effect as increasing the number of aircraft by 30 percent. The C-141A, built between 1963 and 1967, was Air Mobility Command's first jet aircraft designed to meet military standards as a troop and cargo carrier. The development of the B model was the most cost-effective method of increasing AMC's airlift capability. The C-141C includes the addition of advanced avionics.

A universal air refueling receptacle on the C-141, with the ability to transfer 23,592 gallons (89,649.6 liters) in about 26 minutes, means longer non-stop flights and fewer fuel stops at overseas bases during worldwide airlift missions.

With more than 40 years of service and nearly nine million flying hours, the C-141 force has a proven reliability and long-range capability. In addition to training, worldwide airlift and combat support, the C-141 has amassed a laudatory record in response to humanitarian crises.

The C-141, with its changeable cargo compartment, can transition from rollers on the floor for palletized cargo to a smooth floor for wheeled vehicles to aft facing seats or sidewall canvas seats for passengers, quickly and easily, to handle over 30 different missions.

Background

The first C-141A, delivered to Tinker AFB, Okla., in October 1964, began squadron operations in April 1965. The C-141 was the first jet transport from which U.S. Army paratroopers jumped, and the first to land in the Antarctic. The first C-141B was received by the Air Force in December 1979. Conversion from A to B models was completed in 1982. Conversion to the C-models began in 1997 and was completed in 2001.

The last active-duty C-141B retired Sept. 16, 2004, at McGuire AFB, N.J. The last reserve-duty C-141C retired May. 6, 2006, at Wright-Patterson AFB, OH.

General Characteristics

Primary Function: Cargo and troop transport
Contractor: Lockheed-Georgia Co.
Power Plant: Four Pratt & Whitney TF33-P-7 turbofan engines
Thrust: 20,250 pounds, each engine
Wingspan: 160 feet (48.7 meters)
Length: 168 feet, 4 inches (51 meters
Height: 39 feet, 3 inches (11.9 meters)
Cargo Compartment: Height, 9 feet 1 inch (2.77 meters); length, 93 feet 4 inches (28.45 meters); width, 10 feet 3 inches (3.12 meters)
Cargo Door: width, 10.25 feet (3.12 meters); height, 9.08 feet (2.76 meters)
Speed: 500 mph (Mach 0.74) at 25,000 feet
Ceiling: 41,000 feet (12,496 meters) at cruising speed
Range: Unlimited with in-flight refueling
Maximum Takeoff Weight: 323,100 lbs (146,863 kilograms)
Load: Either 200 troops, 155 paratroops, 103 litters and 14 seats, or 68,725 lbs (31,239 kilograms) of cargo
Unit Cost: $47.4 million (fiscal 2002 constant dollars)
Crew: Five or six: two pilots, two flight engineers and one loadmaster and one navigator (added for airdrops). 
Aeromedical Evacuation Crew: Basic crew is five (two flight nurses and three medical technicians). Medical crew may be decreased or increased as required by the needs of the patients. 
Date Deployed: C-141A: October 1964; C-141B: December 1979; C-141C: October 1997.
Inventory: None. Final aircraft retired May 2006


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