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Airworthiness directives › 2009-04-03

AD 2009-04-03 Airworthiness Directives; Rolls-Royce Corporation AE 3007A1E and AE 1107C Turbofan/Turboshaft Engines

2009-03-24
2009-02-17
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Engine
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Applicability*9

This AD applies to Rolls-Royce Corporation (RRC) AE 3007A1E and AE 1107C turbofan/turboshaft engines, with the following parts in Table 1 installed, as applicable: Table 1—Affected Parts and Reduced Life Limits Engine Part name Part No. New reduced published life limit, in flight cycles AE 3007A1E 2nd Stage Compressor Wheel 23050752 15,200   3rd Stage Compressor Wheel 23065303 13,300 AE 1107C 2nd Stage Compressor Wheel 23050752 11,400   2nd Stage Compressor Wheel 23084157 11,400   3rd Stage Compressor Wheel 23065303 6,200   3rd Stage Compressor Wheel (serial numbers L72422, L72475, L72505, L130704, L130829, L130830, L138218, L138226, L138621, L206084, L206163) 23065303 5,000   3rd Stage Compressor Wheel 23084158 6,200   4th Stage Compressor Wheel 23050754 14,900   4th Stage Compressor Wheel 23071259 14,900   4th Stage Compressor Wheel 23084159 14,900   Compressor Cone Shaft Assembly 23050728 2,900   Compressor Cone Shaft Assembly 23070729 2,900   1st to 2nd-Stage Turbine Spacer 23065300 9,500 AE 3007A1E turbofan engines are installed on, but not limited to, EMBRAER EMB-135BJ and EMB-145XR airplanes. AE 1107C turboshaft engines are U.S. type-certificated and are installed on, but not limited to, certain U.S. military aircraft.

Compliance

You are responsible for having the actions required by this AD performed within 5 days after the effective date of this AD, unless the actions have already been done. (f) Remove from service the parts listed in Table 1 of this AD, at the new, reduced, published life limits specified in Table 1 of this AD. Alternative Methods of

Unsafe condition

This AD results from RRC applying an updated lifing methodology to the affected parts. We are issuing this AD to prevent low-cycle-fatigue failure of the parts listed in Table 1 of this AD, which could result in an uncontained engine failure and damage to the aircraft.

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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