Airworthiness directives › 2006-25-13
AD 2006-25-13 Airworthiness Directives; Rolls-Royce Corporation AE 2100D3 Turboprop Engines
Applicability*9
This AD applies to Rolls-Royce Corporation (RRC) AE 2100D3 turboprop engines with a compressor cone shaft assembly, part number 23050728, 23070729, or 23076017, installed. These engines are installed on, but not limited to, Lockheed Martin C-130J military transport airplanes.
Compliance
You are responsible for having the actions required by this AD performed within the compliance times specified unless the actions have already been done. Removal of Compressor Cone Shaft Assemblies (f) After the effective date of this AD, remove compressor cone shaft assemblies from service at the new reduced life limit of 5,000 engine cycles. Alternative Methods of
Unsafe condition
This AD results from low-cycle-fatigue testing and analysis of the affected compressor cone shaft assemblies, by RRC. We are issuing this AD to prevent uncontained failure of the compressor cone shaft assembly, leading to engine shutdown and damage to the airplane.
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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1