AD 2005-11-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier | Various | Airworthiness Directives; Bombardier Model CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), and CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604) Airplanes Modified by Supplemental Type Certificate (STC) SA4900SW |
Unsafe Condition
A damaged microphone jack assembly may interfere with movement of the control column, which could result in loss of control of the airplane.
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Required Actions
Revise the airplane flight manual (AFM) to require repetitive visual checks of the microphone jack assemblies on both control columns to detect damage. Modify the microphone jack assembly and perform related investigative and corrective actions as specified in the service information. Remove the AFM revision after completing the modifications.
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Compliance Time
Within 15 flight hours or 15 days after the effective date, whichever is earlier.
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Affected Aircraft
Bombardier Model CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), and CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604) airplanes modified by Supplemental Type Certificate (STC) SA4900SW.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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