AD/VAT/13 - Stall Warning Indicator - Installation

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

Legislation au F2006B07545 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/13 Stall Warning Indicator - Installation 4/64

Applicability: Victa Airtourer 100 and 115. Document:  1. Victa Mod. B47; or

2. Victa SB No. 25. Compliance: Before 1 September 1971.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Commonwealth of Australia, form a comprehensive framework designed to ensure the safety and efficiency of civil aviation. This legislation addresses the need to establish and maintain high safety standards within the civil aviation sector, including the regulation of aircraft airworthiness. Specifically, Part 39 - 105 of these regulations pertains to the issuance of airworthiness directives, with AD/VAT/13 being one such directive that mandates the installation of a stall warning indicator for Victa Airtourer 100 and 115 aeroplanes. This directive was introduced to mitigate risks associated with stall conditions, ensuring that pilots are adequately warned and can take corrective action to prevent accidents. The policy objective behind these regulations is to maintain a robust safety standard that protects both the public and aviation personnel by minimising risks inherent in air travel.

Scope and Application

The Civil Aviation Regulations 1998, as amended, apply to all entities involved in the operation, maintenance, and manufacture of civil aircraft within the Commonwealth of Australia. Specifically, Part 39 - 105 Civil Aviation Safety Authority Schedule of Airworthiness Directives, such as AD/VAT/13, mandates that operators of Victa Airtourer 100 and 115 aeroplanes must install a stall warning indicator. This directive applies to aircraft that were manufactured before 1 September 1971 and fall under either the Victa Mod. B47 or Victa SB No. 25 documentation. The application of this regulation is enforced by the Civil Aviation Safety Authority (CASA), which is responsible for ensuring that all civil aviation activities comply with the stipulated safety standards. The directive does not exclude any specific operators or entities within its scope, thus applying uniformly to all relevant aircraft. The regulation extends its reach to ensure that any modifications or operations concerning these aircraft adhere strictly to the specified safety directives.

Key Provisions

The Civil Aviation Regulations 1998, under Part 39 - 105, specifically address the airworthiness directives for the Victa and A.E.S.L. Airtourer Series Aeroplanes in section AD/VAT/13. This section mandates the installation of a stall warning indicator for Victa Airtourer 100 and 115 models. The applicability of this directive is clearly defined, targeting aircraft with documentation either as Victa Mod. B47 or Victa Service Bulletin No. 25, provided these aircraft were compliant before 1 September 1971. This requirement aims to enhance flight safety by ensuring that pilots receive timely stall warnings, thereby preventing accidents associated with unexpected stall situations. Entities governed by these regulations must ensure that their Victa Airtourer 100 and 115 models adhere to the installation specifications outlined in the Civil Aviation Regulations. Specifically, they must equip the aircraft with a stall warning indicator as detailed in the referenced documentation. This involves not only the physical installation of the warning system but also ensuring that the system functions correctly and is regularly maintained in accordance with accepted aviation safety standards. Failure to comply with these requirements can result in serious safety implications, potentially leading to accidents or compromised flight operations. In terms of enforcement, the Civil Aviation Regulations 105 impose stringent obligations on the parties involved. Operators and owners of the affected Victa Airtourer 100 and 115 models must ensure that the stall warning indicator is installed and operational before any flight operations. This includes routine checks and maintenance to confirm that the system remains effective. Non-compliance with these directives can lead to severe consequences, including the grounding of the aircraft until the required modifications are made. Such measures are crucial to maintaining the high safety standards expected in civil aviation. Should a party fail to comply with the airworthiness directive, they may face both civil and criminal penalties. The Civil Aviation Regulations provide for substantial fines and potential imprisonment for serious breaches. For instance, failure to install the required stall warning indicator could result in a fine of up to $275,000 for corporations and $55,000 for individuals, along with imprisonment for up to five years. These stringent penalties underscore the importance of adhering to the regulations and highlight the potential consequences of neglecting safety directives.

Legal classification tags

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

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.