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.