- Effective
- March 26, 1968
- Models
- BAC 1-11 200 Series, BAC 1-11 400 Series
- Data sheet
- TCDSA5EU
- Product
- Aircraft · Large airplane
- Amendment
- 39-567
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 | 25c327aa…6066c8a | FAA DRS (API key needed) |
On this page
The airworthiness directive
68-06-04 BRITISH AIRCRAFT: Amendment 39-567. Applies to Model BAC 1-11 200 and 400 Series airplanes.
Within the next 300 hours' time in service after the effective date of this AD, unless already accomplished, install "P" clips, P/N VGS 6750-2, to the static inverter panel, in accordance with British Aircraft Corporation BAC 1-11 Service Bulletin No. 34-PM 2709, Revision 1, or later ARB-approved issue, or an FAA-approved equivalent.
This amendment becomes effective March 26, 1968.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.