Commonwealth legislation

AD/PA-30/33 - Wing Main Spar Lower Cap - Inspection

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Commonwealth

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legislative instrument

Plain English Summary

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The Civil Aviation Safety Authority orders a one‑time inspection of the wing main spar lower cap on specified Piper PA‑30 (s/n 30‑2 to 30‑2000) and PA‑39 (s/n 39‑1 to 39‑155) per Piper Service Bulletin No. 751 within 100 flight hours after 30 September 1983, responding to reported chafing where the spar enters the fuselage. Owners/operators must arrange and pay for the inspection and any follow‑on repairs; costs and further action depend on findings and the service bulletin.

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AD/PA-30/33 - Wing Main Spar Lower Cap - 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-30 & 39 (Twin Comanche) Series Aeroplanes

AD/PA-30/33 Wing Main Spar Lower Cap - Inspection 9/83

Applicability: All model PA-30 with S/Nos. 30-2 to 30-2000. All model PA-39 with S/No. 39-1 to 39-155.

Document: Piper Service Bulletin No. 751.

Compliance: Within 100 hours time in service after 30th September 1983.

Background: The Manufacturer reports cases of chafing of the wing main spar lower cap where the spar enters the fuselage.

Source text

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