federal_register: E9-4828
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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| E9-4828 | Airworthiness Directives; Cessna Aircraft Company Models 208 and 208B Airplanes | Rule | We are adopting a new airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) Models 208 and 208B airplanes. This AD requires you to modify the aileron carry-through cable attachment to the aileron upper quadrant with parts of improved design. This AD results from reports of a "catch" in the aileron control system when the control yoke is turned. We are issuing this AD to prevent the cable attach fitting on the aileron upper quadrant assembly from rotating and possibly contacting or interfering with the aileron lower quadrant assembly, which could result in limited roll control and reduced handling capabilities. | 2009-03-11 | 2009 | 3 | https://www.federalregister.gov/documents/2009/03/11/E9-4828/airworthiness-directives-cessna-aircraft-company-models-208-and-208b-airplanes | https://www.govinfo.gov/content/pkg/FR-2009-03-11/pdf/E9-4828.pdf | Transportation Department; Federal Aviation Administration | 492,159 | We are adopting a new airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) Models 208 and 208B airplanes. This AD requires you to modify the aileron carry-through cable attachment to the aileron upper quadrant with parts of... | 2120-AA64 |