Commonwealth legislation

AD/PA-28/38 - Stabilator Hinge Attaching Bolts - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This directive requires owners/operators of the Piper PA‑28 models referenced in the cited documents to inspect the stabilator hinge attaching bolts within 100 hours time-in‑service after 31 August 1972, following the procedures in Piper Service Letter No. 614 or FAA AD 72‑14‑7. It shifts inspection and any repair costs to operators and matters because it aims to detect and address potential stabilator hinge bolt problems; technical details and exact affected models are in the referenced documents.

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AD/PA-28/38 - Stabilator Hinge Attaching Bolts - 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-28 Series Aeroplanes

AD/PA-28/38 Stabilator Hinge Attaching Bolts - Inspection 6/78

Applicability: All models referenced in requirement documents. Document: 1. Piper SL No. 614; or

FAA AD 72-14-7.

Compliance: Within 100 hours time in service after 31 August 1972.

Source text

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