Airworthiness Directive

AD 2016-19-15 81 FR 66524

Federal Aviation Administration · 14 CFR part 39

FR document
2016-22830
Amendment
39-18664
Published
2016-09-28
Models covered
1
Last live check
2026-08-17
AD

2016-19-15

FR doc 2016-22830 · 81 FR 66524

AD 2016-19-15Published 2016-09-28Effective 2016-11-02

Unsafe condition: cracks found in the horizontal stabilizer rear attach structure and the vertical fin rear spar attach structure.

Full official abstract

We are adopting a new airworthiness directive (AD) for certain REIMS AVIATION S.A. Model F406 airplanes. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as cracks found in the horizontal stabilizer rear attach structure and the vertical fin rear spar attach structure. We are issuing this AD to prevent structural failure of the horizontal stabilizer and/or the vertical fin rear spar attach structure, which could result in damage to the airplane and loss of control.

Applies to 1 model in our index