AD 68-06-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus SAS | BAC 1-11 200 Series | Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11 200 and 400 Series Airplanes |
| aircraft | Airbus SAS | BAC 1-11 400 Series | Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11 200 and 400 Series Airplanes |
Unsafe Condition
Failure of the static inverter panel could result in loss of electrical power to essential systems.
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Required Actions
Install 'P' clips, part number VGS 6750-2, to the static inverter panel following British Aircraft Corporation Service Bulletin No. 34-PM 2709, Revision 1, or later ARB-approved issue, or an FAA-approved equivalent.
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Compliance Time
Within the next 300 hours' time in service after the effective date of this AD
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Affected Aircraft
BRITISH AIRCRAFT Model BAC 1-11 200 and 400 Series airplanes
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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