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PW2000
IOC: 1982
Total Production: 852
F117-PW-100
IOC: 1995
Unitary Cost: USD$8.4 million
Origin
United States of America
Contractor/s
United Technologies
Applications
C-17A Globemaster III
Family Members
PW2000
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Description:
The F117 engine was developed to power the newest USAF's C-17 Globemaster III transport aircraft. The engine's design minimizes fuel consumption while rugged rotating components are designed to tolerate sand, pebbles, ice or other debris found at small and austere airfields anywhere in the world.
Specifications
Dimensions: Diameter 2.2 m, Length 3.7 m
Weights: Max Weight 3,221 kg (7,101 lb)
Engine/s Performance: Thrust 41,700 lb (18,915 kg)
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Notes
(*) lead contractor
IOC: Initial Operating Capability
FOC: Full Operating Capability
CEP: Circular Error Probable
Comm: Commissioning Date
Meters (m) Kilometers (km) Nautic Miles (nm) Inch (in) Yard (yd) Foot (ft) Millimeter (mm)
Pound (lb) Kilogram (kg) kN (KiloNewton) Ton (t)
Meters per Second (mps) Kilometers per Hour (kph) Knot (kt) Miles per Hour (mph)
Liter (l) Galon (gl)
Year (yr) Minutes (min) Second (sec)
Shaft-Horse-Power (shp)
Last Updated: Saturday, November 22, 2008
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Australia / 16 
Canada / 16 
United Kingdom / 20 
United States of America / 800 