| AD Number | 68-06-04 | Status | Active |
| Effective Date | March 26, 1968 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-567 |
| 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 BAC 1-11 400 Series |
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.