Airworthiness Directive

AD 2015-16-07 R1 80 FR 72563

Federal Aviation Administration · 14 CFR part 39

FR document
2015-29200
Amendment
39-18328
Published
2015-11-20
Models covered
1
Last live check
2026-08-19
AD

2015-16-07 R1

FR doc 2015-29200 · 80 FR 72563

AD 2015-16-07 R1Published 2015-11-20Effective 2015-12-28

Superseded by 2021-23-09

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.

Requires actions to address the unsafe condition on these products.

Full official abstract

We are adopting a new airworthiness directive (AD) for REIMS AVIATION S.A. Model F406 airplanes. This AD revises AD 2015-16-07, which required inspection of the left-hand and right-hand rudder control pedal torque tubes, and, depending on findings, replacement with a serviceable part. This AD retains the actions of AD 2015-16-07 and adds additional acceptable serviceable replacement parts. The AD was prompted by reports of detachment of the pilot's rudder control pedal in flight. We are issuing this AD to require actions to address the unsafe condition on these products.

Applies to 1 model in our index