The FAA proposes to adopt a new airworthiness directive (AD) for certain General Electric Company (GE) Model CF6-80E1A2, CF6-80E1A3, CF6-80E1A4, and CF6-80E1A4/B engines. This proposed AD was prompted by a manufacturer investigation that revealed certain high-pressure turbine (HPT) stage 1 and HPT stage 2 disks were manufactured from powder metal material suspected to contain iron inclusion. This proposed AD would require replacement of affected HPT stage 1 and HPT stage 2 disks with parts eligible for installation. The FAA is proposing this AD to address the unsafe condition on these products.
| Document Number | 2025-01728 |
| FR Citation | 90 FR 8505 |
| Type | Proposed Rule |
| Published | Jan 30, 2025 |
| Effective Date | - |
| RIN | 2120-AA64 |
| Docket ID | Docket No. FAA-2024-2721 |
| Pages | 8505–8507 (3 pages) |
| Text Fetched | No |
| Part | Name | Agency |
|---|---|---|
| 14 CFR 39 | Airworthiness Directives... | Federal Aviation Administration |
| Type | Proposed | Final | Method | Conf |
|---|---|---|---|---|
| No paired documents | ||||
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| 2026-01928 | Proposed Rule | Airworthiness Directives; Airbus SAS Air... | Jan 30, 2026 |
| 2026-01878 | Final Rule | Airworthiness Directives; Airbus Helicop... | Jan 30, 2026 |
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