Airworthiness Directives; Airworthiness Directives; CFM International (CFMI) CFM56-2, -2A, -2B, -3, -3B, -3C, -5, -5B, -5C, and -7B Series Turbofan Engines
airworthiness · Rule · Final rule. · Published 2000-06-13 · Effective 2000-12-11 · 65 FR 37031
Document
Document number
00-14788
Federal Register citation
65 FR 37031
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2000-06-13
Effective date
2000-12-11
FAA docket
Docket No. 98-ANE-38-AD
Abstract
This amendment supersedes an existing airworthiness directive (AD), applicable to certain CFM International (CFMI) CFM56 series turbofan engines, that requires revisions to the Airworthiness Limitations Section of applicable Engine Shop Manuals (ESMs). These revisions incorporate required enhanced inspection of selected critical life-limited parts at each piece-part exposure. This amendment requires the addition of CFM56 engine models to the applicability section of the AD, and the introduction of additional inspections. This amendment is prompted by additional focused inspection procedures that have been developed by the manufacturer. The actions specified by this AD are intended to prevent critical life-limited rotating engine part failure, which could result in an uncontained engine failure and damage to the airplane.