Airworthiness Directives; General Electric Company Engines
airworthiness · Rule · Final rule; request for comments. · Published 2024-04-29 · Effective 2024-05-14 · 89 FR 33215
Document
Document number
2024-09109
Federal Register citation
89 FR 33215
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
General Electric Company
Publication date
2024-04-29
Effective date
2024-05-14
FAA docket
Docket No. FAA-2024-0771
Abstract
The FAA is adopting a new airworthiness directive (AD) for certain General Electric Company (GE) Model GE90-110B1 and GE90-115B engines. This AD was prompted by a report of an aborted takeoff due to left engine failure caused by liberation of the interstage high- pressure turbine (HPT) rotor seal rim. This AD requires repetitive ultrasonic inspections (USIs) of the interstage HPT rotor seal for cracks and removal from service if necessary. As a mandatory terminating action to the repetitive USIs of the interstage HPT rotor seal, this AD also requires replacement of the interstage HPT rotor seal. The FAA is issuing this AD to address the unsafe condition on these products.