Airworthiness Directive

AD 2009-05-04 74 FR 8860 Active

Federal Aviation Administration · 14 CFR part 39

FR document
E9-3864
Amendment
39-15828
Published
2009-02-27
Effective
2009-03-16
Models covered
1
Last live check
2026-10-02
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AD

2009-05-04

FR doc E9-3864 · 74 FR 8860

AD 2009-05-04Published 2009-02-27Effective 2009-03-16

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

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…

Full official abstract

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.

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All Canadair CL-215 / CL-415 directives

Applies to 1 model in our index