Airworthiness Directive

AD 2003-04-03 68 FR 7900

Federal Aviation Administration · 14 CFR part 39

FR document
03-3614
Amendment
39-13051
Published
2003-02-19
Models covered
1
Last live check
2026-08-17
AD

2003-04-03

FR doc 03-3614 · 68 FR 7900

AD 2003-04-03Published 2003-02-19Effective 2003-04-07

Requires you to repetitively inspect the aileron control gimbal joint for correct alignment and correct operation, and replace any misaligned or defective gimbal joint.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to all SOCATA--Groupe AEROSPATIALE (Socata) Models TB 9, TB 10, TB 20, TB 21, and TB 200 airplanes. This AD requires you to repetitively inspect the aileron control gimbal joint for correct alignment and correct operation, and replace any misaligned or defective gimbal joint. 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 failure of the aileron control gimbal joint. Such failure could lead to loss of control of the airplane.

Applies to 1 model in our index