KC-10A Extender - WDRB 41 Louisville News

KC-10A Extender

MISSION
The KC-10A Extender is an Air Mobility Command advanced tanker and cargo aircraft designed to provide increased global mobility for U.S. armed forces. Although the KC-l0A's primary mission is aerial refueling, it can combine the tasks of a tanker and cargo aircraft by refueling fighters and simultaneously carry the fighter support personnel and equipment on overseas deployments. The KC-10A can transport up to 75 people and nearly 170,000 pounds (76,560 kilograms) of cargo a distance of about 4,400 miles (7,040 kilometers) unrefueled.

FEATURES
In addition to the three main DC-10 wing fuel tanks, the KC-10A has three large fuel tanks under the cargo floor, one under the forward lower cargo compartment, one in the center wing area and one under the rear compartment. Combined, the capacity of the six tanks carry more than 356,000 pounds (160,200 kilograms) of fuel -- almost twice as much as the KC-135 Stratotanker.

Using either an advanced aerial refueling boom, or a hose and drogue refueling system, the KC-10A can refuel a wide variety of U.S. and allied military aircraft within the same mission. The aircraft is equipped with special lighting for night operations.

The KC-10A's boom operator controls refueling operations through a digital fly-by-wire system. Sitting in the rear of the aircraft, the operator can see the receiver aircraft through a wide window. During boom refueling operations, fuel is transferred to the receiver at a maximum rate of 1,100 gallons (4,180 liters) per minute; the hose and drogue refueling maximum rate is 470 gallons (1,786 liters) per minute. The Automatic Load Alleviation System and Independent Disconnect System greatly enhances safety and facilitates air refueling. The KC-10A can be air-refueled by a KC-135 or another KC-10A to increase its delivery range.

The large cargo-loading door can accept most tactical air forces' fighter unit support equipment. Powered rollers and winches inside the cargo compartment permit moving heavy loads. The cargo compartment can accommodate loads ranging from 27 pallets to a mix of 17 pallets and 75 passengers.

The KC-10A's crew includes a pilot, copilot, flight engineer and boom operator. The sophisticated avionics of the aircraft are designed to improve crew efficiency and reduce crew workload. On certain missions, additional seats and bunks can be added to accommodate extra crew members.

BACKGROUND
A modified Boeing Company DC-10, the KC-10A entered service in 1981. Although it retains 88 percent systems commonality with the DC-10, it has additional systems and equipment necessary for its Air Force mission. These additions include military avionics; aerial refueling boom, hose and drogue; seated aerial refueling operator station; aerial refueling receptacle and satellite communications. The KC-10A fleet is being modified to add wing-mounted pods to further enhance aerial refueling capabilities.

The KC-10A is operated by the 305th Air Mobility Wing, McGuire Air Force Base, N.J.; and the 60th Air Mobility Wing, Travis AFB, Calif. Air Force Reserve Associate units are assigned to the 349th Air Mobility Wing at Travis, and the 514th Air Mobility Wing at McGuire.

During Operations Desert Shield and Desert Storm in 1991, the KC-10 fleet provided in-flight refueling to aircraft from the U.S. armed forces as well as those of other coalition forces. In the early stages of Operation Desert Shield, in-flight refueling was key to the rapid airlift of materiel and forces. In addition to refueling airlift aircraft, the KC-10, along with the smaller KC-135, moved thousands of tons of cargo and thousands of troops in support of the massive Persian Gulf build-up.

During Operation Desert Storm, in-flight refueling extended the range and capability of all U.S. and other coalition fighter aircraft. Air operations continued without costly and time-consuming ground refueling.

The KC-10A and the KC-135 conducted about 51,700 separate refueling operations and delivered 125 million gallons (475 million liters) of fuel without missing a single scheduled rendezvous.

GENERAL CHARACTERISTICS

  • Primary Function: Aerial tanker and transport
  • Prime Contractor: Douglas Aircraft Co., division of The Boeing Company
  • Power Plant: Three General Electric CF6-50C2 turbofans
  • Thrust: 52,500 pounds (23,625 kilograms), each engine
  • Length: 181 feet, 7 inches (54.4 meters)
  • Height: 58 feet, 1 inch (17.4 meters)
  • Wingspan: 165 feet, 4.5 inches (50 meters)
  • Speed: 619 mph (Mach 0.825)
  • Ceiling: 42,000 feet (12,727 meters)
  • Maximum Takeoff Weight: 590,000 pounds (265,500 kilograms)
  • Range: 4,400 miles (3,800 nautical miles) with cargo; 11,500 miles (10,000 nautical miles) without cargo
  • Maximum Cargo Payload: 170,000 pounds (76,560 kilograms)
  • Pallet Positions: 27
  • Maximum Fuel Load: 356,000 pounds (160,200 kilograms)
  • Crew: Four (aircraft commander, pilot, flight engineer and boom operator)
  • Unit Cost: 86.8 million (FY 96 constant dollars)
  • Date Deployed: March 1981
  • Inventory: Active force, 59; ANG, 0; Reserve, 0

Courtesy U.S. Air Force

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