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Airworthiness Directives; CFM International, S.A. Turbofan Engines

airworthiness · Rule · Final rule. · Published 2022-09-01 · Effective 2022-10-06 · 87 FR 53651

Document

Document number
2022-18923
Federal Register citation
87 FR 53651
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2022-09-01
Effective date
2022-10-06
FAA docket
Docket No. FAA-2022-0160

Abstract

The FAA is adopting a new airworthiness directive (AD) for certain CFM International, S.A. (CFM) LEAP-1A model turbofan engines. This AD was prompted by reports of two in-flight shutdowns (IFSDs) and subsequent investigation by the manufacturer that revealed cracks in the high-pressure turbine (HPT) rotor stage 1 blades. This AD requires initial and repetitive borescope inspections (BSIs) of the HPT rotor stage 1 blades. Depending on the results of the BSIs, this AD requires either additional BSIs at reduced intervals or replacement of the HPT rotor stage 1 blades. This AD also requires sending the inspection results to CFM if any unserviceable finding is found. The FAA is issuing this AD to address the unsafe condition on these products.

Source

Authoritative
Federal Register document
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