# Proposed AD FAA-2005-22873: Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2006-02-05
- Products: Bombardier
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: November 15, 2005, 70 FR 69291
- Comments due: December 15, 2005
- Became: [AD 2006-02-05](https://openairdocs.org/ad/2006-02-05)
- Docket: FAA-2005-22873 (https://www.regulations.gov/docket/FAA-2005-22873, where comments are filed)
- Project: 2005-NM-197-AD
- FR document: 05-22590
- Official PDF: https://openairdocs.org/files/sha256/10/44/10441a81f120585684cb34051a8cdf4e181599a9c9c246ba70638e1daaa6aa74 (from https://www.govinfo.gov/content/pkg/FR-2005-11-15/pdf/05-22590.pdf)
- Federal Register: https://www.federalregister.gov/documents/2005/11/15/05-22590/airworthiness-directives-bombardier-model-cl-600-2b19-regional-jet-series-100-and-440-airplanes
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/997B42F89D004DDE862570BA00542DE4.0001
- Page: https://openairdocs.org/proposed/FAA-2005-22873

## Summary

The FAA proposes to adopt a new airworthiness directive (AD) for certain Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes. This proposed AD would require replacing the Camloc fasteners on the sidewall of the center pedestal. This proposed AD results from reports of the Camloc fasteners on the sidewall of the center pedestal disengaging and interfering with an inboard rudder pedal. We are proposing this AD to prevent these fasteners from disengaging and interfering with an inboard rudder pedal, which could reduce directional controllability of the airplane.

## Notices in this docket

- Nov 15, 2005: Notice of proposed rulemaking (NPRM). (first notice), FR document 05-22590, comments due Dec 15, 2005 (https://www.federalregister.gov/documents/2005/11/15/05-22590/airworthiness-directives-bombardier-model-cl-600-2b19-regional-jet-series-100-and-440-airplanes)

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