Summary
We are adopting a new airworthiness directive (AD) for all Rolls-Royce Deutschland Ltd & Co KG (RRD) model Tay 620-15, 650-15, and 651-54 turbofan engines. This AD requires a one-time inspection of the high-pressure (HP) air bleed valve operating mechanism and, depending on findings, corrective action. This AD was prompted by excessive deterioration of the HP air bleed valve operating mechanism, which is influencing the aerodynamic fan flutter margin. This condition, if not corrected, could lead to multiple fan blade failure. We are issuing this AD to prevent multiple fan blade failure, which could result in uncontained engine failure and damage to the airplane.
Directive Details
AD Number
FAA-2013-0397
Document Number
2013-27431
Type
Rule
Publication Date
November 25, 2013
Effective Date
December 30, 2013
Affected Manufacturer
Rolls-Royce Deutschland Ltd & Co KG Turbofan
Criticality
important
Emergency
No
Docket ID
Docket No. FAA-2013-0397
Topics
Official Documents
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