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
Official Documents
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