# Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. MU-2B Series Airplanes
> **Rule** · Final rule. · Published 2006-07-20 · Effective 2006-08-24 · 71 FR 41116
## Document
- **Document number:** E6-11419
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 71 FR 41116
- **Publication date:** 2006-07-20
- **Effective date:** 2006-08-24
- **FAA docket:** Docket No. FAA-2006-23645
## Abstract

We are adopting a new airworthiness directive (AD) for certain Mitsubishi Heavy Industries, Ltd. (MHI) MU-2B series airplanes. This AD requires you to incorporate text from the service information into the Limitations Section of the FAA-approved Airplane Flight Manual (AFM). This AD results from a recent safety evaluation that used a data-driven approach to analyze the design, operation, and maintenance of the MU-2B series airplanes in order to determine their safety and define what steps, if any, are necessary for their safe operation. Part of that evaluation was the identification of unsafe conditions that exist or could develop on the affected type design airplanes. Field reports indicate an unsafe condition of improper rigging and/or adjustment of the propeller feathering linkage. Service centers found the unsafe condition during inspections. We are issuing this AD to detect and correct improper rigging of the propeller feathering linkage. The above issue, if uncorrected, could result in degraded performance and poor handling qualities with consequent loss of control of the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2006/07/20/E6-11419/airworthiness-directives-mitsubishi-heavy-industries-ltd-mu-2b-series-airplanes)
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