AD 2009-24-18
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier | Various | Airworthiness Directives; Bombardier Model CL-600-2A12 (CL-601) and CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604) Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Bombardier Model CL-600-2A12 (CL-601) and CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604) Airplanes |
Unsafe Condition
Premature wear of the rack and pinion mechanism of part number (P/N) 2100140-005 and -007 Engine Throttle Control Gearbox (ETCG), leading to incidents of throttle jam and engine shutdowns.
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Required Actions
Revise the Airworthiness Limitations section of the Instructions for Continued Airworthiness to incorporate new repetitive functional tests of the ETCG as specified in the applicable Temporary Revisions (TRs).
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Compliance Time
Within 30 days after the effective date of this AD (January 8, 2010).
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Affected Aircraft
Bombardier Model CL-600-2A12 (CL-601) and CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604) 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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