Commonwealth legislation

AD/VAT/3 - Tailplane and Elevator Bolts - Wirelocking

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

Requires owners/operators of Victa Airtourer 100 and 115 (serials 1–15) to wirelock tailplane and elevator bolts in accordance with Victa Service Bulletin No. 5, to be completed by 1 September 1971.

Maintenance organisations must carry out the work; owners pay parts, labour and downtime. Compliance depends on accessing the external service bulletin; the directive states the required action and deadline but does not specify penalties or alternative compliance routes.

JSON API

Deep dive

Want the full deep dive?

Zoe can write the in-depth analysis on top of the summary above: how it works, who it affects and what each part actually does.

Current sections

Direct links to the current provisions in AD/VAT/3 - Tailplane and Elevator Bolts - Wirelocking.

AD/VAT/3 - Tailplane and Elevator Bolts - Wirelocking

meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-generator: Aspose.Words for .NET 22.10.0

?xml version="1.0" encoding="utf-8" standalone="no"?>

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Victa and A.E.S.L. Airtourer Series Aeroplanes

AD/VAT/3 Tailplane and Elevator Bolts - Wirelocking 2/63

Applicability: Victa Airtourer 100 and 115 with S/Nos. 1 to 15. Document: Victa SB No. 5.

Compliance: Before 1 September 1971.

Source text

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