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RB211-524
IOC: 1972
Total Production: 1,100
RB211-524G
IOC: 1989
Origin United Kingdom
Contractor/s
Rolls-Royce
Applications
Boeing 767-300 Boeing 767-300ER
Family Members
RB211-524D4 RB211-524G/H-T 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.
Specifications
Engine/s Performance: Thrust 58,000 lb (26,309 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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