Commonwealth legislation

AD/PC-12/7 - Aileron Tie Rod Assembly

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This AD requires owners/operators of Pilatus PC‑12 and PC‑12/45 aircraft (MSN 101–169) to carry out an inspection and modification, following Pilatus Mandatory Service Bulletin 27‑001, after reports of loose aileron tie‑rod jam‑nuts.

The directive became effective 17 July 1997 and must be complied with by 17 October 1997; costs and work fall to the affected owners/operators.

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Current sections

Direct links to the current provisions in AD/PC-12/7 - Aileron Tie Rod Assembly.

AD/PC-12/7 - Aileron Tie Rod Assembly

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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 PC-12 Series Aeroplanes

AD/PC-12/7 Aileron Tie Rod Assembly 8/97

Applicability: Model PC-12 and PC-12/45 aircraft, with serial numbers MSN 101 through to and including MSN 169.

Requirement: Inspect and modify in accordance with Pilatus Mandatory Service Bulletin 27-001.

Note: FOCA Switzerland AD HB 97-174 refers.

Compliance: Unless already accomplished, before 17 October 1997.

This airworthiness directive becomes effective on 17 July 1997.

Background: A report was received where the aileron tie-rod jam-nuts, on the aileron movement chain of the control wheels, became loose.

Source text

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