- Effective
- May 11, 1969
- Model
- BAC 1-11 200 Series
- Data sheet
- TCDSA5EU
- Product
- Aircraft · Large airplane
- Amendment
- 39-748
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 | 6e8810bd…371beb3 | FAA DRS (API key needed) |
On this page
The airworthiness directive
69-08-04 BRITISH AIRCRAFT CORPORATION: Amdt. 39-748. Applies to Model BAC 1-11, 203/AE and 204/AF airplanes.
Compliance required within the next 2500 hours' time in service after the effective date of this AD, unless already accomplished.
To prevent fuel leakage into the wing center section torque box area, replace the aluminum alloy refuel/defuel valve housing P/N AB 45A101 with modified stainless steel valve housing P/N AB 45A1239 in accordance with BAC 1-11 Service Bulletin No. 28-PM 924 or later ARB-approved issue or FAA-approved equivalent.
This amendment becomes effective May 11,1969.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.