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Airworthiness directives › 2012-23-01

AD 2012-23-01 Airworthiness Directives; Cessna Aircraft Company Airplanes

2012-12-26
2012-11-21
39-17257
FAA-2010-1084
Airframe
—

Makes named: cessna. Models named: 402C, 414A. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to Cessna Aircraft Company (Cessna) Model 402C airplanes modified by Supplemental Type Certificate (STC) SA927NW and Model 414A airplanes modified by STC SA892NW, all serial numbers, that are certificated in any category.

Compliance

Comply with this AD within the compliance times specified, unless already done.

Required actions

Within 60 days after December 26, 2012 (the effective date of this AD), do a complete inspection of the flap control system following the Inspection Instructions section of Sierra Industries, Ltd. Service Bulletin SI09-82 Series-1, Rev. A, dated June 12, 2012.

Unsafe condition

This AD was prompted by a report of a Cessna Model 414A airplane modified by STC SA892NW that experienced an asymmetrical flap condition causing an uncommanded roll when the pilot set the flaps to the approach position. We are issuing this AD to prevent failure of the flap system, which could result in an asymmetrical flap condition. This condition could result in loss of control.

Affected ADs

None.

Read the original on the Federal Register →

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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1