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Airworthiness Directives; General Electric Company Turbofan Engines

airworthiness · Rule · Final rule. · Published 2014-10-23 · Effective 2014-11-28 · 79 FR 63307

Document

Document number
2014-24697
Federal Register citation
79 FR 63307
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
General Electric Company Turbofan
Publication date
2014-10-23
Effective date
2014-11-28
FAA docket
Docket No. FAA-2007-28413

Abstract

We are superseding airworthiness directives (ADs) 90-26-01, 91-20-02, and 2009-05-02 for all General Electric Company (GE) CF6-80C2 and CF6-80E1 series turbofan engines. This AD retains the requirements of those ADs and requires removal of additional fuel manifold part numbers (P/Ns), additional repetitive inspections, replacement as required of certain fuel manifold P/Ns and tube (block) clamps, and replacement of loop clamps. This AD was prompted by a report of an under-cowl fire caused by a manifold high-pressure fuel leak, and several additional reports of fuel leaks. We are issuing this AD to prevent failure of the fuel manifold, which could lead to uncontrolled engine fire, engine damage, and damage to the airplane.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown