# Airworthiness Directives; Raytheon Aircraft Company Beech Models 45 (YT-34), A45 (T-34A, B-45), and D45 (T-34B) Airplanes
> **Rule** · Final rule; request for comments. · Published 1999-06-14 · Effective 1999-07-09 · 64 FR 31689
## Document
- **Document number:** 99-14932
- **Category:** airworthiness
- **Manufacturer:** Raytheon
- **Type:** Rule
- **Action:** Final rule; request for comments.
- **Citation:** 64 FR 31689
- **Publication date:** 1999-06-14
- **Effective date:** 1999-07-09
- **FAA docket:** Docket No. 99-CE-22-AD
## Abstract

This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 99-12-02, which was sent previously to all known U.S. owners and operators of Raytheon Aircraft Corporation (Raytheon) Beech Models 45 (YT-34), A45 (T-34A, B-45), and D45 (T-34B) airplanes. This AD requires incorporating operating limitations that restrict operation of the airplanes to normal category operation and prohibit them from acrobatic and utility category operations; limit the flight load factor to 0 to 2.5 G; and limit the maximum airspeed to 175 miles per hour (mph) (152 knots). This AD resulted from a report of an in-flight separation of the right wing on a Raytheon Beech Model A45 (T-34A) airplane. The actions specified by this AD are intended to assure the operational safety of the above- referenced airplanes.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1999/06/14/99-14932/airworthiness-directives-raytheon-aircraft-company-beech-models-45-yt-34-a45-t-34a-b-45-and-d45)
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