# Airworthiness Directives; General Electric Company Engines
> **Rule** · Final rule. · Published 2025-01-08 · Effective 2025-02-12 · 90 FR 1361
## Document
- **Document number:** 2025-00208
- **Category:** airworthiness
- **Manufacturer:** General Electric Company
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 90 FR 1361
- **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
- [Federal Register document](https://www.federalregister.gov/documents/2025/01/08/2025-00208/airworthiness-directives-general-electric-company-engines)
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