AD 94-09-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | BAE Systems (Operations) Limited | BAe 146-100A | Airworthiness Directives; British Aerospace Model BAe 146 Series Airplanes |
| aircraft | BAE Systems (Operations) Limited | BAe 146-200A | Airworthiness Directives; British Aerospace Model BAe 146 Series Airplanes |
| aircraft | BAE Systems (Operations) Limited | BAe 146-300A | Airworthiness Directives; British Aerospace Model BAe 146 Series Airplanes |
Unsafe Condition
Worn brakes may result in loss of main landing gear braking effectiveness during a high energy rejected takeoff (RTO).
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Required Actions
Incorporate specified maximum brake wear limits into the FAA-approved maintenance inspection program within 180 days after the effective date. Use measurements from the BAe 146 airplane maintenance manual or Dunlop component maintenance manual.
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Compliance Time
Within 180 days after the effective date of this AD
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Affected Aircraft
British Aerospace Model BAe 146 series airplanes equipped with Dunlop brakes, 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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