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Airworthiness directives › 2021-23-09

AD 2021-23-09 Airworthiness Directives; ASI Aviation (Type Certificate Previously Held by Reims Aviation S.A.) Airplanes

2022-01-10
2021-12-06
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Airframe
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Models named: F406. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to ASI Aviation (type certificate previously held by Reims Aviation S.A.) Model F406 airplanes, all serial numbers, certificated in any category.

Compliance

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

Required actions

For the purpose of this AD, a serviceable part is: (1) A rudder control pedal torque tube (left-hand (LH) part number (P/N) 5115260-1 or right-hand (RH) P/N 5115260-2) that has had a magnetic particle inspection by following the instructions of Part B of ASI Aviation Service Bulletin No. F406-104, Revision 1, dated December 14, 2018, and no cracks were found; or (2) A new rudder control pedal torque tube (LH P/N 5115260-1 or RH P/N 5115260-2) that has never been installed on an airplane.

Unsafe condition

This AD was prompted by reports of detachment of the pilot's rudder control pedal in flight. The FAA is issuing this AD to detect and correct cracking of the pilot's rudder control pedal. The unsafe condition, if not addressed, could result in detachment of the pedal with possible loss of airplane directional control.

Affected ADs

This AD replaces AD 2015-16-07 R1, Amendment 39-18328 (80 FR 72563, November 20, 2015) (AD 2015-16-07 R1).

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