# AD 68-06-04: Static Inverter Panel

- Type: Airworthiness directive
- Status: Current
- Products: Airbus BAC 1-11 200 Series and BAC 1-11 400 Series
- Effective: March 26, 1968
- Superseded by: Nothing supersedes this AD
- Product type: Aircraft, Large airplane
- Amendment: 39-567
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/9982551AA2EE04DC862569A40053A76C.0001
- DRS record last changed: May 30, 2024
- Page: https://openairdocs.org/ad/68-06-04

## 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 data sheets (1) (OpenAirDocs)

The type certificate data sheets whose models the AD names.

- [TCDS A5EU](https://openairdocs.org/tcds/A5EU): Airbus SAS; names 2 of 2 models: BAC 1-11 200 Series, BAC 1-11 400 Series

## Registered aircraft it may apply to (OpenAirDocs)

No registered aircraft matched the models it names.

Its text cites no advisory circulars or STCs.

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.