federal_register: 2016-10286
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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 2016-10286 | Airworthiness Directives; Airbus Helicopters (Type Certificate Previously Held by Eurocopter France) | Rule | We are superseding airworthiness directive (AD) 2013-08-17 for Airbus Helicopters Model SA-365N, SA-365N1, AS-365N2, AS 365 N3, and SA-366G1 helicopters. AD 2013-08-17 required initial and recurring inspections of the 9-degree fuselage frame for a crack and repairing the frame if a crack exists. This new AD modifies the compliance times and expands the inspection area of the 9-inch frame. The actions of this AD are intended to detect a crack in the 9-degree frame to prevent loss of structural integrity and subsequent loss of control of the helicopter. | 2016-05-06 | 2016 | 5 | https://www.federalregister.gov/documents/2016/05/06/2016-10286/airworthiness-directives-airbus-helicopters-type-certificate-previously-held-by-eurocopter-france | https://www.govinfo.gov/content/pkg/FR-2016-05-06/pdf/2016-10286.pdf | Transportation Department; Federal Aviation Administration | 492,159 | We are superseding airworthiness directive (AD) 2013-08-17 for Airbus Helicopters Model SA-365N, SA-365N1, AS-365N2, AS 365 N3, and SA-366G1 helicopters. AD 2013-08-17 required initial and recurring inspections of the 9-degree fuselage frame for a... |