federal_register: 2018-14398
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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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 2018-14398 | Airworthiness Directives; The Boeing Company Airplanes | Proposed Rule | We propose to remove AD 93-14-19, which applies to certain The Boeing Company Model 767-200 and -300 series airplanes. AD 93-14-19 requires inspections for disbonding of the trailing edge wedge of the leading edge slat; and repair, if necessary. Since we issued AD 93-14- 19, an updated stability and control analysis showed that the worst- case scenario of a trailing edge wedge disbond in-flight would not adversely affect the controllability of the airplane. Accordingly, we propose to remove AD 93-14-19. | 2018-07-17 | 2018 | 7 | https://www.federalregister.gov/documents/2018/07/17/2018-14398/airworthiness-directives-the-boeing-company-airplanes | https://www.govinfo.gov/content/pkg/FR-2018-07-17/pdf/2018-14398.pdf | Transportation Department; Federal Aviation Administration | 492,159 | We propose to remove AD 93-14-19, which applies to certain The Boeing Company Model 767-200 and -300 series airplanes. AD 93-14-19 requires inspections for disbonding of the trailing edge wedge of the leading edge slat; and repair, if necessary. Since... | 2120-AA64 |