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Airworthiness Directives; Bombardier, Inc. Airplanes

airworthiness · Rule · Final rule. · Published 2014-08-19 · Effective 2014-09-23 · 79 FR 48954

Document

Document number
2014-18863
Federal Register citation
79 FR 48954
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2014-08-19
Effective date
2014-09-23
FAA docket
Docket No. FAA-2014-0120

Abstract

We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model CL-215-6B11 (CL-215T Variant), and CL-215-6B11 (CL-415 Variant) airplanes. This AD was prompted by several reports indicating that shorter nacelle strut bushings were inadvertently installed on certain airplanes. This AD requires a general visual inspection of the left and right nacelle upper strut bushings; installation of the bolts and preload indicating (PLI) washers, if necessary; and replacement of the bushing or repair of the bushing installation, if necessary. We are issuing this AD to detect and correct inadequate nacelle strut bushings, which provide insufficient engagement in the strut fork end, and could deform under the bearing load and lead to the failure of the joint.

Source

Authoritative
Federal Register document
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