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Airworthiness Directives; Bombardier Model CL-600-2B19 Series Airplanes

airworthiness · Rule · Final rule; correction. · Published 2001-11-26 · Effective 2001-12-04 · 66 FR 58931

Document

Document number
01-29322
Federal Register citation
66 FR 58931
Type
Rule
Action
Final rule; correction.
Category
airworthiness
Manufacturer
Bombardier Model CL-600-2B19 Series
Publication date
2001-11-26
Effective date
2001-12-04
FAA docket
Docket No. 2000-NM-68-AD

Abstract

This document corrects information in an existing airworthiness directive (AD) that applies to certain Bombardier Model CL-600-2B19 series airplanes. That AD currently requires repetitive eddy current inspections for cracking of the main landing gear (MLG) main fittings, and replacement with a new or serviceable MLG, if necessary. That AD also requires servicing the MLG shock struts; inspecting the MLG shock struts for nitrogen pressure, visible chrome dimension, and oil leakage; and performing corrective actions, if necessary. This document corrects a typographical error existing in the "Applicability" section of the AD. This correction is necessary to ensure that the correct airplane model is specified.

Source

Authoritative
Federal Register document
Machine
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