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Contact
**Data for each of these
characteristics can be
obtained by contacting
the EICO Aviation Specialist
at the NAVFAC Criteria
Office.

KC-135 Stratotanker
Picture of KC-135 StratotankerThe KC-135 Stratotanker's principal mission is air refueling. This asset greatly enhances the U. S. Air Force's capability to accomplish its mission of Global Engagement. It also provides aerial refueling support to U.S. Navy, U.S. Marine Corps and allied aircraft. Four turbofans, mounted under 35-degree swept wings, power the KC-135 to takeoffs at gross weights up to 322,500 pounds (146,285 kilograms). Nearly all internal fuel can be pumped through the tanker's flying boom, the KC-135's primary fuel transfer method. A special shuttlecock-shaped drogue, attached to and trailed behind the flying boom, may be used to refuel aircraft fitted with probes. An operator stationed in the rear of the plane controls the boom. A cargo deck above the refueling system can hold a mixed load of passengers and cargo. Depending on fuel storage configuration, the KC-135 can carry up to 83,000 pounds (37,648 kilograms) of cargo.

General Information

 Aircraft Type

 Support

 Aircraft Manufacturer

 Boeing

 Engine Manufacturer

 CFM

 Engine Number

 F108-CF-100

 Type of Landing Gear

 Dual Tandem Tricycle

 Design Gear Load

 142,000 psi

 Design Tire Pressure

 155 psi

 Pass/Cov Ratio Channelized

 3.37

 Pass/Cov Ratio Unchannelized

 5.97


Geometry

 Wingspan

130.80 ft

 Length (Overall)

136 ft 3 in"

 Height (Overall)

38 ft 4 in"

 Wheelbase

59 ft

 Nose to centerline of main gear

708.00 ft

 Wheel track (tread)

22.08 ft


Parking Apron Design Information

 Minimum turning radius

**

 Engine operating danger areas

**

 Ground clearance

**

 Electrical Service

 • Maximum kVa by aircraft for 400Hz distribution

**

 Mechanical Service

 • Air starting system

**

 • Preconditioned air

**

 • Environmental control air

**


Weights & Takeoff Distances

 Min takeoff weight

240 klbs

 Min takeoff distance with min takeoff weight

**

 Min takeoff distance with min takeoff weight with abort distance

**

 Max takeoff weight at peace-time

301.6 klbs

 Max takeoff weight at war-time

322.5 klbs

 min takeoff distance with max takeoff weight

**

 Min landing weight

**

 Max landing weight

322.5 klbs

 Min landing distance at min landing weight

**

 Min landing distance at max landing weight

**

 Peace-time weight used for pavement evaluation

**


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