Summary
The FAA is adopting a new airworthiness directive (AD) for certain Bombardier Model CL-215-6B11 (CL-215T variant) and CL-215-6B11 (CL-415 variant) airplanes. This AD requires repetitive inspections for contamination of grease, bearing wear checks, grease applications of the rudder lower torque tube upper bearing, and a rudder upper hinge gap check; and related investigative and corrective actions if necessary. This AD results from a report of corrosion on the rudder lower torque tube upper bearing. We are issuing this AD to detect and correct corroded bearings which could lead to hinge deformation, and could result in a rudder jam and consequent reduced controllability of the airplane.
Directive Details
AD Number
FAA-2009-0159
Document Number
E9-3864
Type
Rule
Publication Date
February 27, 2009
Effective Date
March 16, 2009
Affected Manufacturer
Bombardier Model CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant)
Criticality
important
Emergency
No
Docket ID
Docket No. FAA-2009-0159
Topics
Official Documents
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