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

airworthiness · Rule · Final rule. · Published 2009-02-17 · Effective 2009-03-24 · 74 FR 7309

Document

Document number
E9-3027
Federal Register citation
74 FR 7309
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Rolls-Royce Corporation AE 3007A1E and AE 1107C Turbofan/Turboshaft
Publication date
2009-02-17
Effective date
2009-03-24
FAA docket
Docket No. FAA-2008-0230

Abstract

The FAA is adopting a new airworthiness directive (AD) for Rolls-Royce Corporation (RRC) AE 3007A1E and AE 1107C turbofan/ turboshaft engines. This AD requires removal from service of certain 2nd stage, 3rd stage, and 4th stage compressor wheels, compressor cone shaft assemblies, and 1st to 2nd-stage turbine spacers at new, reduced, published life limits. 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.

Source

Authoritative
Federal Register document
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