AD/VAT/36 - Fuel Pump Heat Deflector - Modification

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Legislation au F2006B07570 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/36 Fuel Pump Heat Deflector - Modification 11/70

Applicability: Airtourer 100, 115 and 150.

 

Requirement: Install a deflector plate or similar device to ensure that the exhaust of hot air from the cabin heater distribution box assembly is deflected away from the electric fuel pump when the cabin heater is selected to the OFF position.

 

Note: An acceptable means of compliance is a deflector manufactured to Drawing No. LVAC III which can be obtained from the Latrobe Valley Aero Club, Victoria.

 

Compliance: Before 1 January 1971.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, are a comprehensive set of rules governing civil aviation within Australia. Among these regulations, Part 39 specifically addresses airworthiness directives, ensuring that aircraft meet the necessary safety standards to operate. One such directive, AD/VAT/36, focuses on Victa and A.E.S.L. Airtourer Series Aeroplanes, requiring the installation of a heat deflector to prevent damage to the fuel pump caused by the cabin heater. The objective of this directive is to mitigate the risk of fire or malfunction, thereby enhancing the overall safety of the aircraft. This regulation was introduced to address specific safety concerns identified with the Airtourer series aeroplanes, ensuring they comply with safety standards before a specified date, in this case, before 1 January 1971.

Scope and Application

The Civil Aviation Regulations 1998, under the authority of the Civil Aviation Safety Authority, specifically addresses the airworthiness of certain Victa and A.E.S.L. Airtourer Series aeroplanes in Part 39 - 105, with a particular focus on AD/VAT/36. This regulation mandates the installation of a heat deflector plate or a similar device on Airtourer 100, 115, and 150 models. The directive requires that the deflector ensure the exhaust of hot air from the cabin heater distribution box assembly is directed away from the electric fuel pump when the cabin heater is set to the OFF position. An acceptable means of compliance is a deflector plate manufactured according to Drawing No. LVAC III, which can be sourced from the Latrobe Valley Aero Club in Victoria. This requirement must be met before 1 January 1971, ensuring that the specified modifications are implemented to maintain the aircraft's airworthiness in accordance with Australian civil aviation standards.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105, outlines the Airworthiness Directives (ADs) for Victa and A.E.S.L. Airtourer Series Aeroplanes, particularly focusing on fuel pump heat deflectors (AD/VAT/36). This directive applies to Airtourer models 100, 115, and 150 and mandates the installation of a deflector plate or similar device. The requirement is to ensure that the exhaust of hot air from the cabin heater distribution box assembly is deflected away from the electric fuel pump when the cabin heater is selected to the OFF position (s. 11/70). A recognised method for compliance is the use of a deflector plate manufactured according to Drawing No. LVAC III, available from the Latrobe Valley Aero Club in Victoria. This compliance must be achieved before 1 January 1971. The obligations imposed by the Civil Aviation Regulations are clear and specific. Operators and owners of the affected Airtourer models must ensure that a deflector plate or equivalent device is installed to prevent the hot air from the cabin heater from reaching the electric fuel pump. This installation must be completed in adherence with the specifications provided in Drawing No. LVAC III. The directive leaves some flexibility in the implementation, allowing for devices that meet the functional requirement of deflecting hot air away from the fuel pump, as long as they are equivalent to the specified design. Failure to comply with the Airworthiness Directives can result in significant legal and safety implications. The regulations do not explicitly state penalties in this context, but non-compliance can lead to severe consequences such as aircraft being grounded, potential accidents due to fuel pump overheating, and legal actions under civil aviation law. While the specific penalties are not detailed in the text, non-compliance could result in substantial fines, operational restrictions, or other enforcement actions by the Civil Aviation Safety Authority (CASA). It is crucial for operators to adhere to these directives to maintain airworthiness and ensure the safety of all flights.

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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.