← FAA Federal Register actions

Airworthiness Directives; Bombardier Model CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant) Airplanes

airworthiness · Rule · Final rule; request for comments. · Published 2009-02-27 · Effective 2009-03-16 · 74 FR 8860

Document

Document number
E9-3864
Federal Register citation
74 FR 8860
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Bombardier Model CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant)
Publication date
2009-02-27
Effective date
2009-03-16
FAA docket
Docket No. FAA-2009-0159

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.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown