Saturday, March 20, 2010

RB211-524

IOC: 1972
Total Production: 1,100

RB211-524H

IOC: 1990

Origin
United Kingdom

Contractor/s
Rolls-Royce

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

Family Members
RB211-524D4
RB211-524G
RB211-524G/H-T

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.

Specifications
Engine/s Performance: Thrust 60,600 lb (27,488 kg)

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: Sunday, March 07, 2010

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