# Airworthiness Directives; Bombardier Model CL-215-6B11 (CL215T Variant) and CL-215-6B11 (CL415 Variant) Series Airplanes
> **Rule** · Final rule. · Published 2005-01-05 · Effective 2005-02-09 · 70 FR 684
## Document
- **Document number:** 05-101
- **Category:** airworthiness
- **Manufacturer:** Bombardier Model CL-215-6B11 (CL215T Variant) and CL-215-6B11 (CL415 Variant) Series
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 70 FR 684
- **Publication date:** 2005-01-05
- **Effective date:** 2005-02-09
- **FAA docket:** Docket No. FAA-2004-19496
## Abstract

The FAA is adopting a new airworthiness directive (AD) for certain Bombardier Model CL-215-6B11 (CL215T variant) and CL-215-6B11 (CL415 variant) series airplanes. This AD requires replacing the mounting pad studs of the auxiliary feather pump with new, longer studs, and installing a pressure relief valve. This AD is prompted by a few incidents of external oil leaks from the oil pump of the power control unit due to a malfunction of the pressure regulating valve. We are issuing this AD to prevent fracturing of the pump body, which could result in loss of engine oil, and consequent inability to maintain engine oil pressure and to feather the propeller.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2005/01/05/05-101/airworthiness-directives-bombardier-model-cl-215-6b11-cl215t-variant-and-cl-215-6b11-cl415-variant)
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