Commonwealth legislation

AD/PA-34/5 - Stabilator Tip Balance Weight - Inspection

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Commonwealth

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legislative instrument

Plain English Summary

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This AD, issued by CASA, requires owners/operators of specified Piper PA‑34 (Seneca) aircraft (listed serial numbers) to inspect stabilator tip balance weights immediately and, if necessary, replace hardware per Piper Service Bulletin No. 367 before further flight. Compliance is mandatory and may ground affected aircraft until work is done; operators bear parts, labour and downtime costs and must rely on the referenced Service Bulletin for technical procedures.

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AD/PA-34/5 - Stabilator Tip Balance Weight - 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-34/5 Stabilator Tip Balance Weight - Inspection 9/72

Applicability: All models with S/Nos. 34-E4 and 34-7250001 to 34-7250335. Document: Piper SB No. 367.

Compliance: 1. Initial Inspection - prior to further flight after 12 September 1972.

Hardware Replacement - as detailed in requirement document.

Source text

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