Commonwealth legislation

AD/PA-34/9 - Rudder Servo Trim Tab - Inspection

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Commonwealth

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legislative instrument

Plain English Summary

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This airworthiness directive requires owners/operators of Piper PA‑34 aircraft that have not installed modification kit P/N 760‑800‑V to inspect the rudder servo trim tab per Piper Service Bulletin No. 390A. The first inspection is due within 10 hours TIS after 25 June 1973 and then every 100 hours TIS; operators bear the inspection and repair costs, or may install the kit to be exempt.

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AD/PA-34/9 - Rudder Servo Trim Tab - Inspection

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Piper PA-34 (Seneca) Series Aeroplanes

AD/PA-34/9 Rudder Servo Trim Tab - Inspection 6/73

Applicability: All models not incorporating modification kit P/N 760 800 V. Document: Piper SB No. 390A.

Compliance: Within 10 hours time in service after 25 June 1973 and thereafter at intervals not exceeding 100 hours time in service.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.