federal_register: 2015-29402
Data license: Public Domain (U.S. Government data) · Data source: Federal Register API & Regulations.gov API
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| document_number | title | type | abstract | publication_date | pub_year | pub_month | html_url | pdf_url | agency_names | agency_ids | excerpts | regulation_id_numbers |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 2015-29402 | Airworthiness Directives; Airbus Helicopters (Formerly Eurocopter France) Helicopters | Proposed Rule | We propose to adopt a new airworthiness directive (AD) for Airbus Helicopters Model SA341G and SA342J helicopters. This proposed AD would require repetitive inspections of a certain part-numbered main rotor hub torsion bar (torsion bar). This proposed AD is prompted by several cases of corrosion in the metal strands of the torsion bar. The proposed actions are intended to detect corrosion and prevent failure of the torsion bar, loss of a main rotor blade, and subsequent loss of control of the helicopter. | 2015-11-19 | 2015 | 11 | https://www.federalregister.gov/documents/2015/11/19/2015-29402/airworthiness-directives-airbus-helicopters-formerly-eurocopter-france-helicopters | https://www.govinfo.gov/content/pkg/FR-2015-11-19/pdf/2015-29402.pdf | Transportation Department; Federal Aviation Administration | 492,159 | We propose to adopt a new airworthiness directive (AD) for Airbus Helicopters Model SA341G and SA342J helicopters. This proposed AD would require repetitive inspections of a certain part-numbered main rotor hub torsion bar (torsion bar). This proposed... | 2120-AA64 |