AD/VAT/23 - Fuel Filter Cooling - Modification

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Legislation au F2006B07556 In force Legislative Instrument

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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/23 Fuel Filter Cooling - Modification 4/65

Applicability: Victa Airtourer 100 and 115. Document:  Victa Mod. No. B216.

Compliance: Before 12 April 1965.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, serve as a comprehensive set of rules governing all aspects of civil aviation within Australia. Within this extensive framework, Part 39 - 105, specifically addresses Airworthiness Directives which are instrumental in ensuring the ongoing safety of aircraft. One such directive is AD/VAT/23, which pertains to the Victa and A.E.S.L. Airtourer Series Aeroplanes, focusing on modifications to the fuel filter cooling system. This directive was introduced to mitigate risks associated with fuel system failures, thereby enhancing flight safety. The Civil Aviation Safety Authority is the enacting body responsible for issuing these directives, with the overarching policy objective of maintaining and improving air safety standards in line with international best practices. The specific Airworthiness Directive AD/VAT/23 targets Victa Airtourer 100 and 115 models and mandates modifications to the fuel filter cooling system to be completed before 12 April 1965. This directive is a crucial component of the regulatory framework designed to address the identified gap in aircraft safety protocols. By enforcing this directive, the Civil Aviation Safety Authority aims to ensure that aircraft remain airworthy and compliant with stringent safety standards, thus protecting both passengers and crew from potential hazards associated with fuel system malfunctions.

Scope and Application

The Civil Aviation Safety Authority (CASA) under the Civil Aviation Regulations 1998, specifically within Part 39 - 105, issues Airworthiness Directives to ensure the safe operation of aircraft within Australia. One such directive, AD/VAT/23, applies to Victa Airtourer 100 and 115 aeroplanes, focusing on modifications to the fuel filter cooling system. This directive mandates compliance before 12 April 1965 and is applicable to aeroplanes manufactured by Victa and A.E.S.L., identified by Victa Modification Number B216. The directive applies to all relevant aircraft operators and owners within the Australian jurisdiction, ensuring adherence to safety standards set by CASA. There are no stated exclusions or exemptions in this directive, and it extends its application through subordinate instruments that may provide further details or operational guidance.

Key Provisions

The main operative sections of the Civil Aviation Regulations 1998, particularly in relation to the Airworthiness Directive AD/VAT/23, focus on ensuring the safety and airworthiness of specific models of Victa Airtourer aeroplanes. Section 39.105 specifies that Victa Airtourer 100 and 115 models must comply with modifications regarding fuel filter cooling, as outlined in Victa Modification No. B216. Compliance with this directive is mandatory, and any aircraft must meet these standards before 12 April 1965. This requirement ensures that the aircraft's fuel system is adequately protected against potential overheating, thereby preventing potential hazards during flight. The Civil Aviation Regulations impose specific obligations on the owners and operators of Victa Airtourer 100 and 115 aeroplanes. They must ensure that the aircraft is modified as per Victa Modification No. B216, which typically involves installing or adjusting components related to the fuel filter cooling system. These modifications are designed to maintain the airworthiness of the aircraft, ensuring safety standards are met. Compliance with these directives is a legal requirement, and failure to adhere to the specifications can result in the aircraft being deemed non-airworthy, which would prevent it from flying. In terms of enforcement and consequences for non-compliance, the Civil Aviation Regulations 1998 outline potential penalties for breaching these airworthiness directives. While the specific penalties are not detailed in the text, breaches of airworthiness requirements can lead to enforcement actions by the Civil Aviation Safety Authority (CASA). Such actions might include grounding the aircraft, fines, and other regulatory sanctions. In severe cases, persistent non-compliance could result in more stringent measures, including potential criminal charges if the breach leads to a significant safety incident. The exact penalties and consequences depend on the severity of the non-compliance and the specific circumstances of each case.

Legal classification tags

Area of Law
Aviation Law
Instrument
Regulation
Concepts
Definitions & Interpretation
Compliance Obligations
Enforcement Powers
Catchwords
Airworthiness Directives

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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.