Airworthiness Directive

AD 98-12-02 63 FR 30375

Federal Aviation Administration · 14 CFR part 39

FR document
98-14615
Amendment
39-10559
Published
1998-06-04
Models covered
1
Last live check
2026-08-17
AD

98-12-02

FR doc 98-14615 · 63 FR 30375

AD 98-12-02Published 1998-06-04Effective 1998-07-17

Requires inspecting the elevator trim tab fittings for cracks, and replacing any elevator trim tab found to have cracks.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain SOCATA Groupe Aerospatiale (SOCATA) Model TBM 700 airplanes. This AD requires inspecting the elevator trim tab fittings for cracks, and replacing any elevator trim tab found to have cracks. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for France. The actions specified by this AD are intended to prevent cracks in the elevator trim tab fittings, which could result in separation of the elevator trim tab and loss of control of the airplane.

Applies to 1 model in our index