Commonwealth legislation

AD/PA-28/35 Amdt 1 - Main Landing Gear Torque Links - Inspection

RepealedCTH

This Act has been repealed and is no longer in force. It is retained for historical reference.

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This mandatory Airworthiness Directive requires owners/operators of certain Piper PA-28 fixed‑gear aircraft to inspect main landing‑gear torque links for cracks, corrosion, or wear per Piper Service Letter No. 600. Aircraft already fitted with the upgraded torque link assembly (P/N 78032‑00V or later) are excluded. The inspections prevent landing‑gear collapse and related injury or damage.

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Current sections

Direct links to the current provisions in AD/PA-28/35 Amdt 1 - Main Landing Gear Torque Links - Inspection.

AD/PA-28/35 Amdt 1 - Main Landing Gear Torque Links - 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-28/35

Amdt 1

Main Landing Gear Torque Links - Inspection 8/79

Applicability: All models with fixed landing gear except those with torque link assembly P/N 78032-00V or later P/N.

Document: Piper SL No. 600.

Compliance: As detailed in the requirement document.

Source text

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