# Proposed AD FAA-2010-1108: Bombardier, Inc. Model CL-215-1A10 (CL- 215), CL-215-6B11 (CL-215T Variant), and CL-215-6B11 (CL-415 Variant) Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2011-03-08
- Products: Bombardier
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: November 9, 2010, 75 FR 68728
- Comments due: December 27, 2010
- Became: [AD 2011-03-08](https://openairdocs.org/ad/2011-03-08)
- Docket: FAA-2010-1108 (https://www.regulations.gov/docket/FAA-2010-1108, where comments are filed)
- Project: 2010-NM-151-AD
- FR document: 2010-28275
- Official PDF: https://openairdocs.org/files/sha256/53/9d/539dd104d11168acb82958e3440a71f83935b5dc3fff93db502937422e6fdd02 (from https://www.govinfo.gov/content/pkg/FR-2010-11-09/pdf/2010-28275.pdf)
- Federal Register: https://www.federalregister.gov/documents/2010/11/09/2010-28275/airworthiness-directives-bombardier-inc-model-cl-215-1a10-cl-215-cl-215-6b11-cl-215t-variant-and
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C2409201A6751301862577D6004A3DF9.0001
- Page: https://openairdocs.org/proposed/FAA-2010-1108

## Summary

We propose to adopt a new airworthiness directive (AD) for the products listed above. This proposed AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

Seven cases of on-ground hydraulic accumulator screw cap or end cap failure have been experienced * * * resulting in loss of the associated hydraulic system and high-energy impact damage to adjacent systems and structure. * * * * * * * *

A detailed analysis of the systems and structure in the potential line of trajectory of a failed screw cap/end cap for each accumulator has been conducted. It has identified that the worst- case scenarios would be impact damage to various components, potentially resulting in fuel spillage, uncommanded flap movement, or loss of aileron control [and consequent reduced controllability of the airplane].* * * * *

The proposed AD would require actions that are intended to address the unsafe condition described in the MCAI.

## Notices in this docket

- Nov 9, 2010: Notice of proposed rulemaking (NPRM). (first notice), FR document 2010-28275, comments due Dec 27, 2010 (https://www.federalregister.gov/documents/2010/11/09/2010-28275/airworthiness-directives-bombardier-inc-model-cl-215-1a10-cl-215-cl-215-6b11-cl-215t-variant-and)

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