AD/VAT/7 - Lower Tailplane Shroud - Modification

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B07581 In force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Victa and A.E.S.L. Airtourer Series Aeroplanes

 

AD/VAT/7 Lower Tailplane Shroud - Modification 5/63

Applicability: Victa Airtourer 100 and 115 with S/Nos. 1 to 13. Document:  Victa SB No. 8.

Compliance: Before 1 September 1971.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, as amended, form a comprehensive legal framework for ensuring the safety of civil aviation in Australia. Specifically, Part 39 - 105 of these regulations pertains to the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives, which includes directives concerning the ongoing airworthiness of various aircraft types. This legislative instrument, F2006B07581, was enacted to address the need for maintaining the structural integrity of the Victa and A.E.S.L. Airtourer Series Aeroplanes by mandating specific modifications to the lower tailplane shroud. The regulations were introduced by the Commonwealth of Australia, with the primary policy objective of enhancing flight safety by ensuring that the specified aircraft meet the necessary airworthiness standards. This directive, AD/VAT/7, applies to Victa Airtourer 100 and 115 with serial numbers ranging from 1 to 13, and compliance is required before 1 September 1971, as referenced in Victa Service Bulletin No. 8.

Scope and Application

The Civil Aviation Regulations 1998, as amended, apply to the Victa and A.E.S.L. Airtourer Series Aeroplanes, specifically those with serial numbers 1 to 13, within the Commonwealth of Australia. This legislation mandates modifications to the lower tailplane shroud, as outlined in the Airworthiness Directive AD/VAT/7, to ensure compliance with civil aviation safety standards. The directive necessitates that the specified modifications be completed prior to 1 September 1971, as detailed in Victa Service Bulletin No. 8. The scope of this legislation is confined to the designated aircraft models and serial numbers, ensuring adherence to stringent safety regulations set forth by the Civil Aviation Safety Authority. This directive does not extend to other aircraft models or entities not specified within the legislation, thereby delineating a clear and targeted application.

Key Provisions

The Civil Aviation Regulations 1998, under Part 39-105, contain Airworthiness Directives (ADs) aimed at ensuring the safety of aircraft operations. Specifically, AD/VAT/7 addresses modifications to the lower tailplane shroud of Victa and A.E.S.L. Airtourer Series Aeroplanes (Section 39-105). This directive applies to Victa Airtourer 100 and 115 models with serial numbers 1 to 13. Compliance with these requirements is expected before 1 September 1971, as detailed in Victa Service Bulletin No. 8. The primary obligation imposed by this directive is the requirement for aircraft owners and operators to modify the lower tailplane shroud according to the specifications outlined in Victa Service Bulletin No. 8. These modifications are essential to maintain the airworthiness of the specified aircraft models. Failure to adhere to these specifications could result in the aircraft being deemed non-compliant with safety standards, thus prohibiting its operation until the required modifications are made. Failure to comply with AD/VAT/7 could lead to serious legal and safety repercussions. The Civil Aviation Safety Authority (CASA) has the authority to take enforcement actions against non-compliant aircraft. Such actions may include grounding the aircraft, imposing fines, and potentially pursuing criminal charges against the aircraft owner or operator. The penalties for non-compliance can be severe, depending on the severity of the breach and any subsequent safety risks posed by the non-compliant aircraft. In extreme cases, non-compliance could result in imprisonment for the responsible parties. Therefore, it is crucial for all stakeholders to ensure strict adherence to the directive to avoid these consequences.

Legal classification tags

Area of Law
Aviation Law
Instrument
Legislative Instrument
Concepts
Regulatory Standards
Compliance Obligations
Definitions & Interpretation

Interactions

Authorises

All Versions

Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.