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Airworthiness Directives; General Electric Company Engines

airworthiness · Rule · Final rule. · Published 2025-07-21 · Effective 2025-08-25 · 90 FR 34178

Document

Document number
2025-13644
Federal Register citation
90 FR 34178
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
General Electric Company
Publication date
2025-07-21
Effective date
2025-08-25
FAA docket
Docket No. FAA-2024-1885

Abstract

The FAA is adopting a new airworthiness directive (AD) for certain General Electric Company (GE) Model CF34-10E2A1, CF34-10E6, CF34-10E6A1, CF34-10E7, CF34-10E7-B, CF34-10E5, and CF34-10E5A1 engines. This AD was prompted by a report of cracks found in the high- pressure turbine (HPT) front rotating air seal. This AD requires performing repetitive fluorescent penetrant inspections (FPIs) to detect indications or linear indications (any indication which is four times longer than the width of that same indication) in the HPT front rotating air seal and, if necessary, replacing the HPT front rotating air seal or HPT rotor disk with parts eligible for installation as applicable. This AD also includes an optional terminating action to the repetitive FPIs. The FAA is issuing this AD to address the unsafe condition on these products.

Source

Authoritative
Federal Register document
Machine
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