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GP7000
IOC: July 2008
Total Production: 396
Total Program's Cost: USD$5.0 billion
GP7268
Unitary Cost: USD$15.0 million
Also Known As
GP7200
Origin
United States of America
Contractor/s
Engine Alliance
Applications
Airbus A380
Family Members
GP7270
GP7277
Derived from:
GE90-94B
PW4062
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Description:
The GP7000 engine family is being developed by a joint venture 50/50 between General Electric Aircraft Engines and Pratt & Whitney to power the Airbus A380 commercial aircraft family. These high-performance, high-reliable, state-of-the-art engines are targeted on a new generation of high-capacity, long-range commercial aircraft.
GP7200 engine is derived from General Electric's GE90 and Pratt & Whitney's PW4000 engine families. They take GE90's core and PW4000's low spool heritage to achieve the requirements for new generation high-capacity, long-range aircraft while delivering lower environmental impact and lower ownership costs.
The GP7200 engines have already been selected along with RR Trent 900 engines to power Airbus A380 high-capacity commercial aircraft. The 70,000-lb class GP7268 engine will power the 548-ton class Airbus A380-800 model.
More than 300 GP7200 engines (60% of engines orders) have already been selected to power 67 aircraft ordered by Emirates (199 engines worth $3 billion to power 45 A380s), Air France, FedEx and International Lease Finance Corporation (ILFC).
The GP7200 engine completed its first flight mounted at the inboard location on the left wing of GE's Boeing 747 testbed during a three hours flight at Victorville, California, on December 3, 2004. The engine performed as expected and highly valuable raw propulsion system data on the nacelle and accessories was gathered during the test. The initial series of seven flights will last until the end of December. The second round of flight-testing will occur in the Spring of 2005.
In mid-November 2005 General Electric announced that GP7200 engine surpassed all required certification tests by US Federal Aviation Administration (FAA). GP7200 engine was awarded FAA airworthiness certification on December 29, 2005. In October 2006 an A380 aircraft powered by GP7200 engines completed high altitude and hot weather testing.
Specifications
Dimensions: Diameter 3.0 m, Length 4.8 m
Engine/s Performance: Thrust 70,000 lb (31,752 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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