Airworthiness Directive

AD 2015-16-07 80 FR 49127 Superseded

Federal Aviation Administration · 14 CFR part 39

Requires actions to address the unsafe condition on these products.

FR document
2015-19901
Amendment
39-18232
Published
2015-08-17
Effective
2015-08-18
Models covered
1

Last live check: 2026-08-19

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AD

2015-16-07

FR doc 2015-19901 · 80 FR 49127

AD 2015-16-07Published 2015-08-17Effective 2015-08-18

Revised by 2015-16-07 R1

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.

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

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 results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as 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.

More directives for Cessna F406 Caravan II

  1. AD 2021-23-09 Airworthiness Directives; ASI Aviation (Type Certificate Previously Held... Effective 2022-01-10
  2. AD 2021-22-21 Airworthiness Directives; ASI Aviation (Type Certificate Previously Held... Effective 2022-01-03
  3. AD 2016-19-15 Airworthiness Directives; REIMS AVIATION S.A. Airplanes Effective 2016-11-02
  4. AD 2015-16-07 R1 Airworthiness Directives; REIMS AVIATION S.A. Airplanes Effective 2015-12-28
  5. AD 2013-06-04 Airworthiness Directives; REIMS AVIATION S.A. Airplanes Effective 2013-05-03

All Cessna F406 Caravan II directives

Applies to 1 model in our index