# AD 69-08-04: Fuel Leakage Into Wing

- Type: Airworthiness directive
- Status: Current
- Products: Airbus BAC 1-11 200 Series
- Effective: May 11, 1969
- Superseded by: Nothing supersedes this AD
- Product type: Aircraft, Large airplane
- Amendment: 39-748
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DD49EF5929690E46862569A40055CB4D.0001
- DRS record last changed: May 30, 2024
- Page: https://openairdocs.org/ad/69-08-04

## The airworthiness directive

69-08-04 BRITISH AIRCRAFT CORPORATION: Amdt. 39-748. Applies to Model BAC 1-11, 203/AE and 204/AF airplanes.

Compliance required within the next 2500 hours' time in service after the effective date of this AD, unless already accomplished.

To prevent fuel leakage into the wing center section torque box area, replace the aluminum alloy refuel/defuel valve housing P/N AB 45A101 with modified stainless steel valve housing P/N AB 45A1239 in accordance with BAC 1-11 Service Bulletin No. 28-PM 924 or later ARB-approved issue or FAA-approved equivalent.

This amendment becomes effective May 11,1969.

## 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 1 of 2 models: BAC 1-11 200 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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