Airworthiness Directives; General Electric Company (GE) CF6-50 Turbofan Engines
airworthiness · Rule · Final rule. · Published 2001-06-21 · Effective 2001-07-26 · 66 FR 33166
Document
Document number
01-15446
Federal Register citation
66 FR 33166
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
General Electric Company (GE) CF6-50 Turbofan
Publication date
2001-06-21
Effective date
2001-07-26
FAA docket
Docket No. 2000-NE-30-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that is applicable to General Electric Company (GE) CF6-50 turbofan engines. This amendment requires removal of old high pressure compressor (HPC) air ducts and mating hardware and replacement with newly designed air ducts and reworked mating hardware. This amendment also requires the repetitive inspection of certain reworked mating hardware. This amendment is prompted by reports of an uncontained low pressure turbine (LPT) disk failure that resulted from an air duct failure that caused a fan mid shaft (FMS) separation. The actions specified by this AD are intended to prevent HPC air duct failures that could result in FMS failures, that in turn could result in rejected takeoffs or uncontained LPT events, and to prevent HPC rear shaft failures that could result in uncontained engine failures.