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Airworthiness Directive

AD 2015-16-07 R1 80 FR 72563 Superseded

Federal Aviation Administration · 14 CFR part 39

Requires actions to address the unsafe condition on these products.

Superseded by AD 2021-23-09Federal Register (opens in a new tab)

FR document
2015-29200
Amendment
39-18328
Published
2015-11-20
Effective
2015-12-28
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2015-16-07%20R1 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

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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Superseded by 2021-23-09 Revises 2015-16-07

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 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.

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 Airworthiness Directives; REIMS AVIATION S.A. Airplanes Effective 2015-08-18
  5. AD 2013-06-04 Airworthiness Directives; REIMS AVIATION S.A. Airplanes Effective 2013-05-03

All Cessna F406 Caravan II directives

View on Federal Register (opens in a new tab) Search DRS manually for AD 2015-16-07 R1 (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 1 model in our index