Summary
We are adopting a new airworthiness directive (AD) for all Rolls-Royce plc (RR) Trent 1000-A, 1000-C, 1000-D, 1000-E, 1000-G, and 1000-H turbofan engines. This AD requires removing engine electronic controller (EEC) software earlier than standard MB6.15 and replacing with a software standard eligible for installation. This AD was prompted by a finding that an intermediate pressure (IP) shaft failure may not be detected by EEC software earlier than standard MB6.15. We are issuing this AD to detect IP shaft failure and prevent IP compressor turbine burst, uncontained engine failure, and damage to the airplane.
Directive Details
AD Number
FAA-2014-0705
Document Number
2014-25739
Type
Rule
Publication Date
October 30, 2014
Effective Date
November 14, 2014
Affected Manufacturer
Rolls-Royce plc Turbofan
Criticality
important
Emergency
No
Docket ID
Docket No. FAA-2014-0705
Topics
Official Documents
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