# Airworthiness Directives; McCauley Propeller Systems Propeller Models B5JFR36C1101/114GCA-0, C5JFR36C1102/L114GCA-0, B5JFR36C1103/114HCA-0, and C5JFR36C1104/L114HCA-0
> **Rule** · Final rule; request for comments. · Published 2006-07-26 · Effective 2006-08-10 · 71 FR 42258
## Document
- **Document number:** E6-11799
- **Category:** airworthiness
- **Manufacturer:** McCauley
- **Type:** Rule
- **Action:** Final rule; request for comments.
- **Citation:** 71 FR 42258
- **Publication date:** 2006-07-26
- **Effective date:** 2006-08-10
- **FAA docket:** Docket No. FAA-2006-25173
## Abstract

The FAA is adopting a new airworthiness directive (AD) for McCauley Propeller Systems propeller models B5JFR36C1101/114GCA-0, C5JFR36C1102/L114GCA-0, B5JFR36C1103/114HCA-0, and C5JFR36C1104/ L114HCA-0. This AD requires a onetime fluorescent penetrant inspection (FPI) and eddy current inspection (ECI) of propeller blades for cracks, and if any crack indications are found, removing the blade from service. This AD results from a report of two propeller blades on the same propeller assembly, found cracked during propeller overhaul. We are issuing this AD to detect cracks in the propeller blade that could cause failure and separation of the propeller blade and loss of control of the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2006/07/26/E6-11799/airworthiness-directives-mccauley-propeller-systems-propeller-models-b5jfr36c1101114gca-0)
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