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Airworthiness Directives; CFE Company Model CFE738-1-1B Turbofan Engines

airworthiness · Rule · Final rule. · Published 2002-06-28 · Effective 2002-08-02 · 67 FR 43528

Document

Document number
02-16176
Federal Register citation
67 FR 43528
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
CFE Company Model CFE738-1-1B Turbofan
Publication date
2002-06-28
Effective date
2002-08-02
FAA docket
Docket No. 99-NE-39-AD

Abstract

This amendment revises an existing airworthiness directive (AD), that is applicable to CFE Company Model CFE738-1-1B turbofan engines. That AD currently requires a one-time visual inspection of stage 2 high pressure turbine (HPT) aft cooling plates for nicks, dents, raised metal, and scratches, and if necessary, repair of the cooling plates or replacement with serviceable parts. This amendment reduces the number of stage 2 HPT aft cooling plates affected by AD 99- 27-16, and identifies the applicable engines by engine serial numbers (SN's). This amendment is prompted by an updated alert service bulletin (ASB) that reduces the number of stage 2 HPT aft cooling plates affected by AD 99-27-16 and identifies the applicable engines by engine SN's. The actions specified by this AD are intended to prevent stage 2 HPT aft cooling plate failure, which could result in an uncontained engine failure and damage to the airplane.

Source

Authoritative
Federal Register document
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