# Airworthiness Directives; Bombardier Model CL-600-2B19 Series Airplanes
> **Rule** · Final rule; correction. · Published 2001-11-26 · Effective 2001-12-04 · 66 FR 58931
## Document
- **Document number:** 01-29322
- **Category:** airworthiness
- **Manufacturer:** Bombardier Model CL-600-2B19 Series
- **Type:** Rule
- **Action:** Final rule; correction.
- **Citation:** 66 FR 58931
- **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
- [Federal Register document](https://www.federalregister.gov/documents/2001/11/26/01-29322/airworthiness-directives-bombardier-model-cl-600-2b19-series-airplanes)
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