RB211-524H  
Initial Operational Capability (IOC): 1990
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 and RB211-524G/H-T
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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 RB211-524H engine rated at 60,600 pounds was introduced in 1990 powering the Boeing 747-400 and 767-300 commercial aircraft.

RB211-524H Applications


Airliners Boeing 747-400 Boeing 747-400F Boeing 767-300 Boeing 767-300ER Boeing 767-300F

RB211-524H Specifications

Weight
Thrust: 60,600 pound (27.5 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)

RB211-524H News

There is 1 news
on 20 Jan 2011
Thursday, January 20, 2011Rolls-Royce Wins Long Term Trent 700 Maintenance Support Business from Cathay Pacific

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