Commonwealth legislation

AD/VAT/24 - Rear Fuselage - Sealing of Seams and Rivets - Modification

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This directive, issued in CASA’s Schedule of Airworthiness Directives, mandates sealing seams and rivets on the rear fuselage of Victa Airtourer 100 and 115 aeroplanes (S/Ns 1–110) using Victa Service Bulletin No. 55. Operators must complete the modification within 100 hours TIS after 29 November 1965. The AD names the compliance method but gives no explicit safety rationale, cost estimates, alternative methods, or enforcement/relief procedures.

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AD/VAT/24 - Rear Fuselage - Sealing of Seams and Rivets - Modification

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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/24 Rear Fuselage - Sealing of Seams and

Rivets - Modification Applicability: Victa Airtourer 100 and 115 with S/Nos. 1 to 110. Document: Victa SB No. 55.

Compliance: Within 100 hours time in service after 29 November 1965.

11/65

Source text

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