# AD 67-10-02: Engine Stub Access Panels

- Type: Airworthiness directive
- Status: Current
- Products: Airbus BAC 1-11 200 Series and BAC 1-11 400 Series
- Effective: April 28, 1967
- Superseded by: Nothing supersedes this AD
- Product type: Aircraft, Large airplane
- Amendment: 39-377
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A0F0C9CCE2F12B418625699F006519C1.0001
- DRS record last changed: May 30, 2024
- Page: https://openairdocs.org/ad/67-10-02

## The airworthiness directive

67-10-02 BRITISH AIRCRAFT: Amdt. 39-377 Part 39 Federal Register March 30, 1967. Applies to Model BAC 1-11 Series Airplanes.

Compliance required as indicated.

To prevent the loss of electrical power in the event of a failure in the d.c. essential bus bar, unless already accomplished, within the next 1,000 hours' time in service after the effective date of this AD, install an additional circuit breaker Klixon P/N 7274/11/2 and local internal cables in accordance with British Aircraft Corporation Service Bulletin No. 24-PM 2334, or later ARB-approved issue or FAA-approved equivalent.

This directive effective April 28, 1967.

## 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.

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