# Airworthiness Directives; McCauley Propeller Systems Propeller Assemblies Models 2D34C53/74E-X; D2A34C58/90AT-X; 3AF32C87/82NC-X; D3AF32C87/82NC-X; D3A32C88/82NC-X; D3A32C90/82NC-X; and 3AF34C92/90LF-X.
> **Rule** · Final rule; request for comments. · Published 2005-11-30 · Effective 2005-12-15 · 70 FR 71753
## Document
- **Document number:** 05-23430
- **Category:** airworthiness
- **Manufacturer:** McCauley
- **Type:** Rule
- **Action:** Final rule; request for comments.
- **Citation:** 70 FR 71753
- **Publication date:** 2005-11-30
- **Effective date:** 2005-12-15
- **FAA docket:** Docket No. FAA-2005-22731
## Abstract

The FAA is adopting a new airworthiness directive (AD) for McCauley Propeller Systems propeller assemblies, models 2D34C53/74E-X; D2A34C58/90AT-X; 3AF32C87/82NC-X; D3AF32C87/82NC-X; D3A32C88/82NC-X; D3A32C90/82NC-X; and 3AF34C92/90LF-X. This AD requires, within 10 flight hours or 10 days after the effective date of this AD, whichever occurs first, removing certain serial number propeller hubs from service. This AD results from a report by the manufacturer that they manufactured and released 40 propeller hubs with improperly machined socket retention threads. We are issuing this AD to prevent cracked propeller hubs, which could cause failure of the propeller hub, blade separation, and loss of control of the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2005/11/30/05-23430/airworthiness-directives-mccauley-propeller-systems-propeller-assemblies-models-2d34c5374e-x)
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