AD 2014-15-11
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier | Various | Airworthiness Directives; Bombardier, Inc. Airplanes |
Unsafe Condition
Fatigue cracking of the pilot-side rudder pedal tubes, part number 600-90204-3, initiated at the aft taper pin holes where the connecting rod fitting is attached, due to loads induced during parking brake application.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct initial and repetitive inspections for cracking and damage of the pilot-side rudder pedal tubes, part number 600-90204-3. Replace the rudder bar assembly and repair as necessary. Optional terminating action is available for the repetitive inspections.
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Compliance Time
Within 12 months of the effective date of the AD.
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Affected Aircraft
Bombardier, Inc. Model CL-600-2C10 (Regional Jet Series 700, 701, & 702), Model CL-600-2D15 (Regional Jet Series 705), Model CL-600-2D24 (Regional Jet Series 900), and Model CL-600-2E25 (Regional Jet Series 1000) airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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