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routineRule

AD FAA-2008-0224

Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG (RRD) Turbofan Engines

Summary

We are rescinding an airworthiness directive (AD) for RRD BR700-715A1-30, BR700-715B1-30, and BR700-715C1-30 turbofan engines. The existing AD resulted from the need to reduce the published life limits of high-pressure (HP) turbine stage 1 discs, part numbers (P/Ns) BRH20130 and BRH20131, and HP turbine stage 2 discs, P/Ns BRH19423 and BRH19427. We are rescinding the existing AD because RRD has revised the approved published life limits of these parts to the same or higher limits as originally certified.

Directive Details

AD Number

FAA-2008-0224

Document Number

2012-15961

Type

Rule

Publication Date

July 2, 2012

Effective Date

August 6, 2012

Affected Manufacturer

Rolls-Royce Deutschland Ltd & Co KG (RRD) Turbofan

Criticality

routine

Emergency

No

Docket ID

Docket No. FAA-2008-0224

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for Rolls-Royce Deutschland Ltd & Co KG (RRD) Turbofan →

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