# Proposed AD 2000-CE-42-AD: Raytheon Aircraft Company Beech Model 58 Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2000-22-18
- Action: Notice of proposed rulemaking (NPRM).
- Published: September 7, 2000, 65 FR 54184
- Comments due: October 11, 2000
- Became: [AD 2000-22-18](https://openairdocs.org/ad/2000-22-18)
- Docket: 2000-CE-42-AD
- FR document: 00-22909
- Official PDF: https://openairdocs.org/files/sha256/81/68/816801198bf3c73c4a1a252cf822dd60c5a09f21cbdc05bfbae204876092aaac (from https://www.govinfo.gov/content/pkg/FR-2000-09-07/pdf/00-22909.pdf)
- Federal Register: https://www.federalregister.gov/documents/2000/09/07/00-22909/airworthiness-directives-raytheon-aircraft-company-beech-model-58-airplanes
- Page: https://openairdocs.org/proposed/2000-CE-42-AD

## Summary

This document proposes to adopt a new airworthiness directive (AD) that would apply to certain Raytheon Aircraft Company (Raytheon) Beech Model 58 airplanes. The proposed AD would require you to inspect the rudder bellcrank interconnect tube for damage; replace or refinish the interconnect tube, if necessary; and modify the floorboard. Four reports of damage to the interconnect tube prompted the proposed action. The actions specified by the proposed AD are intended to correct the wrong use of screws and consequent wear in the pilot/ copilot pedal interconnect tube, which could result in loss of rudder control.

## Notices in this docket

- Sep 7, 2000: Notice of proposed rulemaking (NPRM). (first notice), FR document 00-22909, comments due Oct 11, 2000 (https://www.federalregister.gov/documents/2000/09/07/00-22909/airworthiness-directives-raytheon-aircraft-company-beech-model-58-airplanes)

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