RB211-524G  
Initial Operational Capability (IOC): 1989
Total Production: ?
Origin: United Kingdom
Corporations: Rolls-Royce
Parent System: RB211-524
Initial Operational Capability (IOC): 1972
Total Production: 1,100
Family Members: RB211-524D4, RB211-524G/H-T and RB211-524H
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Description: The Rolls-Royce RB211-524, RB211-22B, is a three-shaft layout, shorter and rigid engine designed to power Boeing 747 and 767 commercial aircraft models. Currently, there are more than 1,100 engines of this type in service worldwide, which have logged more than 80 million flying hours. In addition, the engine is fully interchangeable between Boeing 747-400 and 767-300 aircraft that can reduce ownership costs for a 747/767 mixed fleet.

The RB211-524G engine rated at 58,000 pounds was introduced in 1989 powering the Boeing 747-400.

RB211-524G Applications


Airliners Boeing 767-300 Boeing 767-300ER

RB211-524G Specifications

Weight
Thrust: 58,000 pound (26.3 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)

Operators & Related Equipment


 
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