Airworthiness Directive 2018-09-17
recurringAirworthiness Directives; Bombardier, Inc., Airplanes
What this AD requires
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model CL-600-1A11 (CL-600), CL-600-2A12 (CL-601 Variant), and CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604 Variants) airplanes. This AD was prompted by reports of fractured rudder pedal tubes on the pilot-side rudder bar assembly. This AD requires repetitive inspections of the rudder pedal tubes for cracking and corrective actions if necessary. Replacement of both pilot-side rudder bar assemblies terminates the inspections. We are issuing this AD to address the unsafe condition on these products.
Which aircraft AD 2018-09-17 applies to
Model CL-600-1A11 (CL-600): S/Ns 1004 through 1085. Model CL-600-2A12 (CL-601 Variant): S/Ns 3001 through 3066. Model CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604 Variants): S/Ns 5001 through 5194, 5301 through 5665, 5701 through 5988, and 6050 through 6099.
Whether AD 2018-09-17 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.
How AD compliance is recorded
A valid compliance record (14 CFR 43.9) states:
Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.
Look up a tail number →Read the full directive (Federal Register)Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.