99-12-02
FR doc 99-14932 · 64 FR 31689AD 99-12-02Published 1999-06-14Effective 1999-07-09
Superseded by 2001-13-18
Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.
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.
Full official 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.