- Effective
- May 11, 1969
- Models
- BAC 1-11 200 Series, BAC 1-11 400 Series
- Data sheet
- TCDSA5EU
- Product
- Aircraft · Large airplane
- Amendment
- 39-749
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 | 9b3fb169…d9b16d6 | FAA DRS (API key needed) |
On this page
The airworthiness directive
69-08-05 BRITISH AIRCRAFT CORPORATION: Amdt. 39-749. Applies to Model BAC 1-11, 200 and 400 Series airplanes.
Compliance required within the next 1500 hours' time in service after the effective date of this AD, unless already accomplished.
To ensure that the shear pin which is installed within the Elevator Centralizing Spring Pots, Part Numbers AB34-A881, A3003, A3017, A3019, and A3021 remains effective, remove and disassemble the spring pots from the right and left elevators and modify in Accordance with BAC 1-11 Service Bulletin No. 27-A-PM 3536 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.