Commonwealth legislation

AD/PC-6/28 Amdt 1 - Wing Strut Attachment - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This AD requires owners/operators of Pilatus Porter PC‑6 aeroplanes (S/N 338–701) to inspect the wing strut attachment at intervals not exceeding 100 hours TIS, using the procedure in Pilatus Service Bulletin No. 93. It affects aircraft operators and maintenance organisations, shifts maintenance cadence to a 100‑hour inspection cycle, and leaves compliance costs to owners.

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AD/PC-6/28 Amdt 1 - Wing Strut Attachment - 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 Pilatus Porter PC-6 Series Aeroplanes

AD/PC-6/28

Amdt 1

Wing Strut Attachment - Inspection 12/80

Applicability: All models with S/Nos. 338 to 701. Document: Pilatus SB No. 93.

Compliance: At intervals not exceeding 100 hours time in service.

Background: Service experience indicates that the inspection for corrosion in the wing strut attachment can be extended to 100 hourly intervals.

Source text

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