Airworthiness Directive

AD 2000-11-05 65 FR 35267

Federal Aviation Administration · 14 CFR part 39

FR document
00-13445
Amendment
39-11753
Published
2000-06-02
Models covered
1
Last live check
2026-08-17
AD

2000-11-05

FR doc 00-13445 · 65 FR 35267

AD 2000-11-05Published 2000-06-02Effective 2000-06-23

Requires that you repetitively inspect the vertical fin front spar attachment fittings for fatigue cracks, and rework the vertical fin if any cracks are found.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Air Tractor Incorporated (Air Tractor) Models AT- 301, AT-401, and AT-501 airplanes that are equipped with a \3/16\-inch thick aluminum fin front spar fitting and an all metal rudder. This AD requires that you repetitively inspect the vertical fin front spar attachment fittings for fatigue cracks, and rework the vertical fin if any cracks are found. This AD is the result of reports of a vertical fin front spar fitting failure on a Model AT-401 airplane. The actions specified by this AD are intended to detect and correct cracks in the vertical fin front spar attachment fittings, which could result in failure of the vertical fin. This condition could lead to loss of directional control and eventual loss of airplane control.

Applies to 1 model in our index