Airworthiness directives › 95-18-14
AD 95-18-14 Airworthiness Directives; General Electric Company CF6 Series Turbofan Engines
Applicability*9
General Electric Company (GE) CF6 series engines. These engines are installed on but not limited to Airbus Industries A300, A310, and A330 series; Boeing 747 and 767 series; and McDonnell Douglas DC10 and MD11 series aircraft. Note: This AD applies to each engine identified in the preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For engines that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must use the authority provided in paragraph (b) to request approval from the FAA. This approval may address either no action, if the current configuration eliminates the unsafe condition, or different actions necessary to address the unsafe condition described in this AD. Such a request should include an assessment of the effect of the changed configuration on the [[Page 46218]] unsafe condition addressed by this AD. In no case does the presence of any modification, alteration, or repair remove any engine from the applicability of this AD.
Compliance
Required as indicated, unless accomplished previously. To prevent an uncontained high pressure compressor rotor (HPCR) engine failure, which can result in damage to the aircraft, accomplish the following: (a) After the effective date of this AD all fluorescent penetrant inspections of HPCR stage 3-9 spools must be accomplished in accordance with the process described in GE All Operators' Wire,
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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