| AD Number | 67-31-02 | Status | Active |
| Effective Date | December 18, 1967 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-512 |
| 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 |
67-31-02 BRITISH AIRCRAFT: Amdt. 39-512, Part 39, Federal Register November 18, 1967. Applies to Model BAC 1-11 203/AE, 204/AF and 212/AR Airplanes.
Compliance required within the next 3,000 hours' time in service after the effective date of this AD, unless already accomplished. To avoid the possibility of a fuel leak within the pressurized area, relocate the left and right fuel line couplings from Station 630 to a point 3 inches forward, in accordance with British Aircraft Corporation BAC 1-11 Service Bulletin No. 28-PM 2914, dated May 12, 1967, or later ARB-approved issue, or an equivalent approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa, and Middle East Region.
This amendment effective December 18, 1967.