Commonwealth legislation

AD/VAT/20 - Centre Flap Spar - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

Applies to Victa Airtourer 100/115 aeroplanes without Victa Modification B141 and with over 500 hours TIS. Requires repeated inspections of the centre flap spar around flap actuating bracket P/N 16105/1 for cracking (at intervals ≤100 hours from 1 Sep 1971) and repair per an approved scheme before further flight if cracks are found. This directs owners/operators to a recurring maintenance obligation, with associated downtime, repair approval steps and concentrated cost on the specified aircraft.

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AD/VAT/20 - Centre Flap Spar - 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 Victa and A.E.S.L. Airtourer Series Aeroplanes

AD/VAT/20 Centre Flap Spar - Inspection 6/64

Applicability: Victa Airtourer 100 and 115 not incorporating Victa Mod. B141 and which have exceeded 500 hours time in service.

Requirement: Inspect the centre flap spar in the region of the actuating bracket P/N 16105/1 for cracking. If cracking is found repair in accordance with an approved scheme before further flight.

Compliance: At intervals not exceeding 100 hours time in service, after 1 September 1971.

Source text

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