AD 95-14-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus SAS | BAC 1-11 200 Series | Airworthiness Directives; British Aerospace Model BAC 1-11-200 and -400 Series Airplanes |
| aircraft | Airbus SAS | BAC 1-11 400 Series | Airworthiness Directives; British Aerospace Model BAC 1-11-200 and -400 Series Airplanes |
Unsafe Condition
Failure of the center torque shaft of the spoiler on the left and right wing due to severe corrosion.
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Required Actions
Perform radiographic inspections to detect internal corrosion of the center torque shaft on left and right wing spoilers per Alert Service Bulletin 27-A-PM6007. If corrosion is found, replace the shaft assembly with a used serviceable or new assembly prior to further flight.
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Compliance Time
Within 9 months after the effective date of this AD or within 10 years after the date of installation, whichever occurs later. Repeat inspections at intervals not to exceed 4 years if no corrosion is detected.
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Affected Aircraft
British Aerospace Model BAC 1-11-200 and -400 series airplanes, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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