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routineRule

AD FAA-2009-0162

Airworthiness Directives; Rolls-Royce plc (RR) RB211-524 Series Turbofan Engines

Summary

We are superseding an existing airworthiness directive (AD) for the products listed above. That AD currently requires initial and repetitive borescope inspections of the head section and meterpanel assembly of the combustion liner, and replacement if necessary. This new AD requires those same inspections, and replacement. This AD also expands the applicability to include part numbers (P/N) of additional combustion liners. This AD was prompted by an inquiry submitted by an operator, which resulted in RR performing a complete review of the affected front combustion liner part numbers. We are issuing this AD to prevent deterioration of the engine combustion liner, which can result in combustion liner breakup, case burn-through, engine fire, and damage to the airplane.

Directive Details

AD Number

FAA-2009-0162

Document Number

2012-134

Type

Rule

Publication Date

January 9, 2012

Effective Date

February 13, 2012

Affected Manufacturer

Rolls-Royce plc (RR) RB211-524 Series Turbofan

Criticality

routine

Emergency

No

Docket ID

Docket No. FAA-2009-0162

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for Rolls-Royce plc (RR) RB211-524 Series Turbofan →

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