AircraftDirectives
MembershipSign inCreate free account
Menu
Airworthiness Directive

AD 99-12-02 64 FR 31689 Superseded

Federal Aviation Administration · 14 CFR part 39

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.

Superseded by AD 2001-13-18Federal Register (opens in a new tab)

FR document
99-14932
Amendment
39-11193
Published
1999-06-14
Effective
1999-07-09
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/99-12-02 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

Opens your browser's print dialog. Choose “Save as PDF” to export a file. Keyboard: Ctrl+P or Cmd+P.

AD

99-12-02

FR doc 99-14932 · 64 FR 31689

AD 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Superseded by 2001-13-18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.

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

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.

More directives for Beechcraft T-34 Mentor

  1. AD 2007-08-08 Airworthiness Directives; Raytheon Aircraft Company (The Beech Aircraft ... Effective 2007-05-25
  2. AD 2007-06-01 Airworthiness Directives; Raytheon Aircraft Company Beech Models 45 (YT-... Effective 2007-04-16
  3. AD 2004-25-51 Airworthiness Directives; Raytheon Aircraft Company Beech Models 45 (YT-... Effective 2004-12-21
  4. AD 2001-13-18 R1 Airworthiness Directives; Raytheon Aircraft Corporation Beech Models 45 ... Effective 2004-03-15
  5. AD 2001-23-10 Airworthiness Directives; Raytheon Aircraft Company 33, T-34, 35, 36, 55... Effective 2001-12-13

All Beechcraft T-34 Mentor directives

View on Federal Register (opens in a new tab) Search DRS manually for AD 99-12-02 (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 1 model in our index