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Airworthiness Directive

AD 2013-06-04 78 FR 19088 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2013-06590
Amendment
39-17401
Published
2013-03-29
Effective
2013-05-03
Models covered
1
Last live check
2026-10-02

Printed from https://aircraftdirectives.com/ad/2013-06-04 · 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

2013-06-04

FR doc 2013-06590 · 78 FR 19088

AD 2013-06-04Published 2013-03-29Effective 2013-05-03

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 an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as fretting (wear and/or chafing) found between the elevator pushrod assembly and the horizontal tail structure, which could cause the elevator pushrod to jam and could result in loss of control. We are issuing this AD to require actions to address the unsafe condition on these products.

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All Cessna F406 Caravan II directives

View on Federal Register (opens in a new tab) Search DRS manually for AD 2013-06-04 (opens in a new tab)

Applies to 1 model in our index