AD 94-11-07
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
Worn main landing gear brakes may result in loss of brake effectiveness during a high energy rejected takeoff (RTO).
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Required Actions
Inspect main landing gear brakes for wear and replace any brake exceeding the maximum wear limit (0.75 inch for BAC 1-11-200, 1.0 inch for BAC 1-11-400) prior to further flight. Incorporate the specified maximum brake wear limits into the FAA-approved maintenance inspection program.
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Compliance Time
Within 180 days after the effective date of this AD (July 5, 1994).
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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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