# Airworthiness Directives; Beech Aircraft Corporation Model 1900D Airplanes
> **Rule** · Final rule; request for comments. · Published 1995-03-30 · Effective 1995-04-17 · 60 FR 16366
## Document
- **Document number:** 95-7784
- **Category:** airworthiness
- **Manufacturer:** Beech
- **Type:** Rule
- **Action:** Final rule; request for comments.
- **Citation:** 60 FR 16366
- **Publication date:** 1995-03-30
- **Effective date:** 1995-04-17
- **FAA docket:** Docket No. 95-CE-15-AD
## Abstract

This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 95-02-17, which was sent previously to known U.S. owners and operators of certain Beech Aircraft Corporation Model 1900D airplanes. This AD requires inspecting (one- time) the elevator trim tab control cables at the top of the vertical stabilizer to ensure that cables (at the left, right, and crossover pulleys) are correctly routed around the pulleys, within the cable guide pins, and are not contacting any structure; and replacing any cable that is incorrectly routed or chafed. The actions specified by this AD are intended to prevent in-flight separation of the elevator trim tab control cable caused by misrouting, which could result in loss of control of the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1995/03/30/95-7784/airworthiness-directives-beech-aircraft-corporation-model-1900d-airplanes)
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