# Airworthiness Directives; Israel Aircraft Industries, Ltd., Model 1121, 1121A, 1121B, 1123, 1124, and 1124A Series Airplanes
> **Rule** · Final rule; request for comments. · Published 2000-11-17 · Effective 2000-12-04 · 65 FR 69439
## Document
- **Document number:** 00-29078
- **Category:** airworthiness
- **Manufacturer:** Israel
- **Type:** Rule
- **Action:** Final rule; request for comments.
- **Citation:** 65 FR 69439
- **Publication date:** 2000-11-17
- **Effective date:** 2000-12-04
- **FAA docket:** Docket No. 2000-NM-364-AD
## Abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to all Israel Aircraft Industries, Ltd., Model 1121, 1121A, 1121B, 1123, 1124, and 1124A series airplanes. This action requires a one-time inspection, and corrective action if necessary, to ensure the proper installation of the tie rod through the dust shield and both jackscrew assemblies on the horizontal stabilizer trim actuator. This action is necessary to prevent jamming or disconnection of the horizontal stabilizer trim actuator, which could result in reduced pitch control of the airplane. This action is intended to address the identified unsafe condition.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2000/11/17/00-29078/airworthiness-directives-israel-aircraft-industries-ltd-model-1121-1121a-1121b-1123-1124-and-1124a)
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