Proposed rule 2025-08078
Airworthiness Directives; Airbus Helicopters
The FAA proposes to adopt a new airworthiness directive (AD) for all Airbus Helicopters Model EC 130 B4 and EC 130 T2 helicopters. This proposed AD was prompted by a report of heavy damage on the fenestron due to the loss of the tail rotor (TR) blade, which broke at the TR hub tension-torsion bar (tension-torsion bar). This proposed AD would require inspecting the tension-torsion bar and, depending on the inspection results, taking corrective actions. This proposed AD would also prohibit performing maintenance using certain maintenance manuals. These proposed actions are specified in a European Union Aviation Safety Agency (EASA) AD, which is proposed for incorporation by reference. The FAA is proposing this AD to address the unsafe condition on these products.
Source-supplied record
Document details
- Document number
- 2025-08078
- Published
- May 9, 2025
- Effective
- Not supplied
- Comments close
- Jun 23, 2025
- Federal Register citation
- 90 FR 19660
Docket identifiers
- Docket No. FAA-2025-0752
- Project Identifier MCAI-2024-00340-R
CFR references
- Title 14, part 39