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Airworthiness Directive

AD 2006-22-10 71 FR 62897 Active

Federal Aviation Administration · 14 CFR part 39

FR document
E6-17870
Amendment
39-14807
Published
2006-10-27
Effective
2006-12-01
Models covered
1
Last live check
2026-10-01

Printed from https://aircraftdirectives.com/ad/2006-22-10 · 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

2006-22-10

FR doc E6-17870 · 71 FR 62897

AD 2006-22-10Published 2006-10-27Effective 2006-12-01

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 correct the unsafe condition on these products.

Full official abstract

We are adopting a new 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 a failure in the flap actuating circuit. An investigation showed that the lever at the torsional drive in the fuselage failed at the weld. We are issuing this AD to require actions to correct the unsafe condition on these products.

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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