- Effective
- December 18, 1967
- Model
- BAC 1-11 200 Series
- Data sheet
- TCDSA5EU
- Product
- Aircraft · Large airplane
- Amendment
- 39-512
Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
| File | Size | SHA-256 | Original |
|---|---|---|---|
| FAA DRS HTML | 19 KB | c4216556…3de6bc7 | FAA DRS (API key needed) |
On this page
The airworthiness directive
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.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.