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AD FAA-2013-0876

Airworthiness Directives; Rolls-Royce plc Turbofan Engines

Summary

We are adopting a new airworthiness directive (AD) for certain Rolls-Royce plc (RR) RB211 Trent 768-60, 772-60, and 772B-60 turbofan engines. This AD requires modification of the engine by removing an electronic engine control (EEC) incorporating EEC software standard A14 or earlier and installing an EEC eligible for installation. This AD was prompted by an uncontained multiple turbine blade failure on an RR RB211 Trent 772B turbofan engine. We are issuing this AD to prevent failure of the intermediate-pressure (IP) turbine disk drive arm or burst of the high-pressure turbine disk, which could lead to uncontained engine failure and damage to the airplane.

Directive Details

AD Number

FAA-2013-0876

Document Number

2014-16184

Type

Rule

Publication Date

July 11, 2014

Effective Date

August 15, 2014

Affected Manufacturer

Rolls-Royce plc Turbofan

Criticality

important

Emergency

No

Docket ID

Docket No. FAA-2013-0876

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for Rolls-Royce plc Turbofan →

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