AD 2000-23-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier | Various | Airworthiness Directives; Bombardier Model CL-600-2B16 (CL-604) Series Airplanes |
Unsafe Condition
Corrosion of the inboard flap actuator beam assembly, part number 600-14250-25, and gaps between the vane brackets, part numbers 600-14306-1 and -2, and adjacent skin, which could compromise the structural integrity of the flap systems and reduce the controllability of the airplane in the event of a failure during flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect for gaps between the vane bracket(s) and adjacent skin; perform corrective actions if necessary, including non-destructive inspection for cracks in vane brackets, replacing cracked brackets, and eliminating gaps by filling with liquid shim or installing a solid shim; replace the six flap vane actuator beams with new beams; return certain parts to the manufacturer and submit a data report.
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Compliance Time
Before further flight
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Affected Aircraft
Bombardier Model CL-600-2B16 (CL-604) series airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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