AD 2011-24-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Aviat | Various | Airworthiness Directives; BAE SYSTEMS (Operations) Limited Airplanes |
Unsafe Condition
Fatigue cracking of certain structural elements which could adversely affect the structural integrity of these airplanes.
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Required Actions
Revise the aircraft maintenance manual (AMM) to introduce new life limits on certain main landing gear (MLG) components and remove outdated tables containing mandatory life limitations on bolts and pins. Implement the revised life limits and associated inspections and corrective measures as specified in Chapter 05 of the AMM at Revision 100.
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Compliance Time
Before further flight
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Affected Aircraft
All BAE SYSTEMS (Operations) Limited Model BAe 146-100A, -200A, and -300A airplanes; and Model Avro 146-RJ70A, 146-RJ85A, and 146-RJ100A airplanes, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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