# Proposed AD 2000-NM-03-AD: Raytheon Model Hawker 800A (U-125A) and Hawker 800XP Series Airplanes.

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2000-24-25
- Action: Notice of proposed rulemaking (NPRM).
- Published: August 8, 2000, 65 FR 48402
- Comments due: September 22, 2000
- Became: [AD 2000-24-25](https://openairdocs.org/ad/2000-24-25)
- Docket: 2000-NM-03-AD
- FR document: 00-20001
- Official PDF: https://openairdocs.org/files/sha256/4d/ac/4dacd4541db0a998cc1c1b6ce9504dfec7300c3c84b51de95250bb01da3df01f (from https://www.govinfo.gov/content/pkg/FR-2000-08-08/pdf/00-20001.pdf)
- Federal Register: https://www.federalregister.gov/documents/2000/08/08/00-20001/airworthiness-directives-raytheon-model-hawker-800a-u-125a-and-hawker-800xp-series-airplanes
- Page: https://openairdocs.org/proposed/2000-NM-03-AD

## Summary

This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Raytheon Model Hawker 800A (U-125A) and Hawker 800XP series airplanes. This proposal would require inspecting the roller clearance in the nose landing gear drag stay and making any necessary adjustments. The proposal is prompted by reports indicating multiple findings of roller clearances that are in excess of specifications. The actions specified by the proposed AD are intended to prevent the inability to extend the nose landing gear, which could result in damage to the airplane upon landing.

## Notices in this docket

- Aug 8, 2000: Notice of proposed rulemaking (NPRM). (first notice), FR document 00-20001, comments due Sep 22, 2000 (https://www.federalregister.gov/documents/2000/08/08/00-20001/airworthiness-directives-raytheon-model-hawker-800a-u-125a-and-hawker-800xp-series-airplanes)

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