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
Official Documents
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