Airworthiness Directives; CFM International CFM56-5 Series Turbofan Engines
airworthiness · Rule · Final rule. · Published 1999-03-22 · Effective 1999-04-21 · 64 FR 13667
Document
Document number
99-6555
Federal Register citation
64 FR 13667
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
CFM International CFM56-5 Series Turbofan
Publication date
1999-03-22
Effective date
1999-04-21
FAA docket
Docket No. 98-ANE-56-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to CFM International CFM56-5 series turbofan engines, that reduces the low cycle fatigue (LCF) retirement lives for certain high pressure turbine rotor (HPTR) front air seals, and provides a drawdown schedule for those affected parts with reduced LCF retirement lives. This amendment is prompted by results of a refined life analysis performed by the manufacturer that revealed minimum calculated LCF lives significantly lower than the published LCF retirement lives. The actions specified by this AD are intended to prevent a LCF failure of the HPTR front air seal, which could result in an uncontained engine failure and damage to the aircraft.