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Airworthiness Directive

AD 2009-05-12 74 FR 10455 Active

Federal Aviation Administration · 14 CFR part 39

Requires you to modify the aileron carry-through cable attachment to the aileron upper quadrant with parts of improved design.

Federal Register (opens in a new tab)FAA DRS (opens in a new tab)

FR document
E9-4828
Amendment
39-15836
Published
2009-03-11
Effective
2009-04-15
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2009-05-12 · 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

2009-05-12

FR doc E9-4828 · 74 FR 10455

AD 2009-05-12Published 2009-03-11Effective 2009-04-15

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 you to modify the aileron carry-through cable attachment to the aileron upper quadrant with parts of improved design.

Full official abstract

We are adopting a new airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) Models 208 and 208B airplanes. This AD requires you to modify the aileron carry-through cable attachment to the aileron upper quadrant with parts of improved design. This AD results from reports of a "catch" in the aileron control system when the control yoke is turned. We are issuing this AD to prevent the cable attach fitting on the aileron upper quadrant assembly from rotating and possibly contacting or interfering with the aileron lower quadrant assembly, which could result in limited roll control and reduced handling capabilities.

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