# Airworthiness Directives; Bombardier Model CL-600-2B19 Series Airplanes
> **Rule** · Final rule; correction. · Published 2001-12-14 · Effective 2001-12-04 · 66 FR 64739
## Document
- **Document number:** 01-30863
- **Category:** airworthiness
- **Manufacturer:** Bombardier Model CL-600-2B19 Series
- **Type:** Rule
- **Action:** Final rule; correction.
- **Citation:** 66 FR 64739
- **Publication date:** 2001-12-14
- **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 an error that resulted in the omission of the AD and amendment numbers in the "Product Identification" section of the AD. This correction is necessary to ensure that the correct AD and amendment numbers are specified.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2001/12/14/01-30863/airworthiness-directives-bombardier-model-cl-600-2b19-series-airplanes)
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