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Airworthiness Directives; General Electric Company Turbofan Engines

airworthiness · Rule · Final rule. · Published 2013-12-03 · Effective 2014-01-07 · 78 FR 72552

Document

Document number
2013-28293
Federal Register citation
78 FR 72552
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
General Electric Company Turbofan
Publication date
2013-12-03
Effective date
2014-01-07
FAA docket
Docket No. FAA-2013-0475

Abstract

We are adopting a new airworthiness directive (AD) for certain General Electric Company model GEnx-2B67 and GEnx-2B67B turbofan engines. This AD was prompted by the original equipment manufacturer's disclosure that certain critical rotating life-limited parts (LLPs) used in Boeing 747-8 flight tests had consumed more cyclic life than they would have in revenue flight cycles. These parts were then installed into engines and introduced into revenue service without adjustment to remaining cyclic life. This AD requires a one-time adjustment to the cycle counts of those LLPs to account for the additional low cycle fatigue (LCF) life consumed during flight tests. We are issuing this AD to prevent the failure of critical rotating LLPs, uncontained engine failure, and damage to the airplane.

Source

Authoritative
Federal Register document
Machine
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