federal_register: 2014-08071
Data license: Public Domain (U.S. Government data) · Data source: Federal Register API & Regulations.gov API
This data as json
| document_number | title | type | abstract | publication_date | pub_year | pub_month | html_url | pdf_url | agency_names | agency_ids | excerpts | regulation_id_numbers |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 2014-08071 | Airworthiness Directives; Airbus Airplanes | Proposed Rule | We propose to adopt a new airworthiness directive (AD) for certain Airbus Model A318, A319, A320, and A321 series airplanes. This proposed AD was prompted by a report of a crack found in the fuselage during a fatigue test campaign. This proposed AD would require repetitive rototest inspections for cracking; corrective actions if necessary; and modification of the torsion box, which would terminate the repetitive inspections. We are proposing this AD to prevent cracking in the side box beam flange of the fuselage, which could affect the structural integrity of the airplane. | 2014-04-10 | 2014 | 4 | https://www.federalregister.gov/documents/2014/04/10/2014-08071/airworthiness-directives-airbus-airplanes | https://www.govinfo.gov/content/pkg/FR-2014-04-10/pdf/2014-08071.pdf | Transportation Department; Federal Aviation Administration | 492,159 | We propose to adopt a new airworthiness directive (AD) for certain Airbus Model A318, A319, A320, and A321 series airplanes. This proposed AD was prompted by a report of a crack found in the fuselage during a fatigue test campaign. This proposed AD... |