| AD Number | 66-16-02 | Status | Active |
| Effective Date | July 31, 1966 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-254 |
| Product Type | ["Aircraft"] | Product Subtype | ["Large Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Airbus SAS |
| Model(s) | BAC 1-11 200 Series |
66-16-02 BRITISH AIRCRAFT CORPORATION: Amdt. 39-254 Federal Register July 1, 1966. Applies to Model BAC 1-11 200 Series Airplanes.
Compliance required before the accumulation of 3,000 hours' time in service for airplanes with less than 2,900 hours' time in service on the effective date of this AD and within the next 100 hours' time in service after the effective date of this AD for airplanes with 2,900 or more hours' time in service on the effective date of this AD unless already accomplished.
To prevent chafing of the fuselage frame forward flange by the aft end of the headliner, rework the headliner, P/N AB77 A1605, and inspect the flange of fuselage frame, P/N AB29 A501, and rework as necessary in accordance with British Aircraft Corporation (BAC) One- Eleven Alert Service Bulletin 53-A-PM 2107, dated February 1, 1966, or later ARB-approved issue.
This directive effective July 31, 1966.