F110-GE-132  
Initial Operational Capability (IOC): 2003
Total Production: ?
Origin: United States of America
Corporations: General Electric
Parent System: F110
Initial Operational Capability (IOC): 1986
Total Production: 5,859
Family Members: F110-GE-100, F110-GE-129 and F110-GE-400
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Description: The F110 was developed utilizing the same core design of the F101 engine. This engine has different fan and afterburner packages to tailor engine performance compared with the F101 engine.

The F110-GE-132 is the latest and most advanced member of the F110 engine family yielding 32,000 pounds of thrust. Derived from the F110-GE-129, this engine incorporates some advanced technologies related to both the F414 and F120 engines. As a result of that, -132 has an increased combat performance over -129 and lower total ownership costs.

The F110-GE-132 utilizes General Electric Aircraft Engines (GEAE)'s extensive technology base, including: a long-chord blisk fan derived from the F118 engine, a radial afterburner derived from the F414 engine and enhanced for the F136 engine (Joint Strike Fighter), and a composite outer duct based on the F404 and F414 engines. In the future, GEAE plans to infuse a new core developed to extend the service life of the engine thus increasing durability and time on wing.

The F110-GE-132 engine was developed to power the F-16C/D Block 60 or F-16E/F aircraft ordered by the United Arab Emirates (UAE) Air Force. The US Air Force also uses the -132 engine on some Block 50 F-16 since the engine was qualified in September 2003. In addition, General Electric is providing a -132 kit to upgrade current F110 engines.

On 23 May 2005, General Electric was awarded a $57 million contract by the US Air Force (USAF) to upgrade an initial 95 F110 fighter engines to the Service Life Extension Program (SLEP) configuration in support of the F-16C/D aircraft. The SLEP program is expected to conclude in 2012 with approximately 800 F110 engines upgraded and delivered to the USAF at a $280 million estimated cost. SLEP is aimed at reducing maintenance costs by $1 billion.

The SLEP program includes technology upgrades to the combustor, high pressure turbine, compressor and augmentor to reduce unscheduled removals by 50% and reduce the cost-per-flight-hour by 25%. Much of this hot-section hardware is derived from the highly-successful CFM56-7 engine, which powers the Boeing 737 jetliner. SLEP programs are also being developed for both the F101 and F118 engines for the B-1, B-2 and U-2 aircraft.

F110-GE-132 Applications


Combat Aircraft F-16E Desert Falcon F-16F Desert Falcon

F110-GE-132 Specifications

Dimensions
Fan Diameter: 1,170 millimeter (46 inch)
Length: 4.60 meter (181 inch)
Weight
Dry Weight: 1,819 kilogram (4,010 pound)
Thrust: 32,500 pound (14.7 ton)
CEP: Circular Error Probable
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)

F110-GE-132 News

There is 1 news
on 6 Dec 2003
Saturday, December 6, 2003F-16E/F First Flight

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