Airworthiness Directives; CFM International CFM56-2, -3, -3B, and -3C Series Turbofan Engines
airworthiness · Rule · Final rule; request for comments. · Published 1998-03-30 · Effective 1998-03-30 · 63 FR 15073
Document
Document number
98-7560
Federal Register citation
63 FR 15073
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
1998-03-30
Effective date
1998-03-30
FAA docket
Docket No. 98-ANE-16-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that is applicable to CFM International CFM56-2, -3, -3B, and -3C series turbofan engines. This action requires the removal from service of certain No. 3 bearing rear stationary air/oil seals, replacement with serviceable parts, and the installation of retention bushings. This action also requires the removal from service of high pressure compressor rotor (HPCR) stage 1-2 spools that have contacted the outer cone of the seal. This amendment is prompted by several reports of outer cone separation of the No. 3 bearing rear stationary air/oil seal. The actions specified in this AD are intended to prevent rubs between the outer cone of the No. 3 bearing rear stationary air/oil seal and the HPCR stage 1-2 spool, which could result in a potential uncontained failure of the HPCR stage 1-2 spool, and damage to the aircraft.