# Proposed AD 2000-NM-398-AD: Bombardier Model CL-215-1A10 and CL- 215-6B11 Series Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2002-12-12
- Products: Bombardier
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: February 8, 2002, 67 FR 5958
- Comments due: March 11, 2002
- Became: [AD 2002-12-12](https://openairdocs.org/ad/2002-12-12)
- Docket: 2000-NM-398-AD
- FR document: 02-3065
- Official PDF: https://openairdocs.org/files/sha256/af/3b/af3bddb805231bcecc8b070dd15867b1300fba8df0be67ca7c8f447741705618 (from https://www.govinfo.gov/content/pkg/FR-2002-02-08/pdf/02-3065.pdf)
- Federal Register: https://www.federalregister.gov/documents/2002/02/08/02-3065/airworthiness-directives-bombardier-model-cl-215-1a10-and-cl-215-6b11-series-airplanes
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/998DFE35FE06F00086256B5A005EBFB6.0001
- Page: https://openairdocs.org/proposed/2000-NM-398-AD

## Summary

This document proposes the supersedure of an existing airworthiness directive (AD), applicable to certain Bombardier Model CL-215-1A10 and CL-215-6B11 series airplanes, that currently requires repetitive inspections to detect cracking on certain wing-to-fuselage frame angles; and repair, if necessary. This action would decrease the compliance time for the initial inspection to detect cracking on certain wing-to-fuselage frame angles and would decrease the interval between repetitive inspections. This proposal is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by the proposed AD are intended to detect and correct cracking in the wing-to-fuselage frame angles, which could result in reduced structural integrity of the airframe.

## Notices in this docket

- Feb 8, 2002: Notice of proposed rulemaking (NPRM). (first notice), FR document 02-3065, comments due Mar 11, 2002 (https://www.federalregister.gov/documents/2002/02/08/02-3065/airworthiness-directives-bombardier-model-cl-215-1a10-and-cl-215-6b11-series-airplanes)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.