AD 2013-24-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier | Various | Airworthiness Directives; Bombardier, Inc. Airplanes |
Unsafe Condition
Fatigue cracking of the pilot-side rudder pedal tubes, initiated at the aft taper pin holes where the connecting rod fitting is attached, due to loads induced during parking brake application.
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Required Actions
Inspect both pilot-side rudder pedal tubes for cracking and damage using detailed or eddy current inspections. Replace the pilot-side rudder bar assemblies if necessary. Repair any damage found.
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Compliance Time
Before further flight
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Affected Aircraft
Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes, certificated in any category, serial numbers 7003 and subsequent.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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