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Airworthiness Directive

AD 2008-03-11 73 FR 6592 Active

Federal Aviation Administration · 14 CFR part 39

FR document
E8-1829
Amendment
39-15361
Published
2008-02-05
Effective
2008-03-11
Models covered
1
Last live check
2026-10-01

Printed from https://aircraftdirectives.com/ad/2008-03-11 · 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

2008-03-11

FR doc E8-1829 · 73 FR 6592

AD 2008-03-11Published 2008-02-05Effective 2008-03-11

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 that are intended to address the unsafe condition described in the MCAI.

Full official abstract

We are superseding an existing airworthiness directive (AD) for the products listed above. 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 distortion of the rudder bars due to rudder control forces during aerobatic operation and nose wheel steering reaction forces. Rudder bar distortion could result in reduced control or loss of control. This AD requires actions that are intended to address the unsafe condition described in the MCAI.

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All Avions Pierre Robin directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab)

Applies to 1 model in our index