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Airworthiness Directives; General Electric Company Engines

airworthiness · Rule · Final rule. · Published 2025-01-08 · Effective 2025-02-12 · 90 FR 1361

Document

Document number
2025-00208
Federal Register citation
90 FR 1361
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
General Electric Company
Publication date
2025-01-08
Effective date
2025-02-12
FAA docket
Docket No. FAA-2024-0755

Abstract

The FAA is adopting a new airworthiness directive (AD) for certain General Electric Company (GE) Model GEnx-1B64, GEnx-1B64/P1, GEnx-1B64/P2, GEnx-1B67, GEnx-1B67/P1, GEnx-1B67/P2, GEnx-1B70, GEnx- 1B70/75/P1, GEnx-1B70/75/P2, GEnx-1B70/P1, GEnx-1B70/P2, GEnx-1B70C/P1, GEnx-1B70C/P2, GEnx-1B74/75/P1, GEnx-1B74/75/P2, GEnx-1B76/P2, GEnx- 1B76A/P2, GEnx-2B67, GEnx-2B67B, and GEnx-2B67/P engines. This AD was prompted by a manufacturer evaluation that determined a lower life limit may be necessary for certain stages 6-10 compressor rotor spools than allowed by the engine shop manual (ESM). This AD requires a one- time inspection of the stages 6-10 spools for previously accomplished blend repairs, a one-time inspection of the blend repairs on the stages 6-10 spools for compliance with the updated allowable limits, and replacement if necessary. The FAA is issuing this AD to address the unsafe condition on these products.

Source

Authoritative
Federal Register document
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