AD/VAT/25 - Nose Wheel Steering - Inspection

Overview

The Civil Aviation Regulations 1998, amended through the legislative instrument F2006B07558, are designed to ensure the safety of civil aviation within Australia. This particular update addresses a specific issue related to the airworthiness of Victa and A.E.S.L. Airtourer Series aeroplanes. The regulation was introduced to rectify a gap in the existing safety directives, specifically targeting the nose wheel steering system of these aircraft models. The policy objective is to ensure that these aeroplanes are maintained in a safe and reliable condition, which is critical for the protection of passengers and crew, as well as the general public. The enacting body responsible for these regulations is the Australian Parliament, which ensures that the aviation safety standards are enforced through the Civil Aviation Safety Authority (CASA).

Scope and Application

The Civil Aviation Regulations 1998, specifically PART 39 - 105, applies to all Victa Airtourer 100 and 115 aircraft with serial numbers prior to 108, excluding those incorporating modification number B209. This legislation mandates that these aircraft undergo inspections for nose wheel steering as detailed in Victa Service Bulletin No. 49, Issue 2. Compliance with these airworthiness directives is required at intervals not exceeding 100 hours of time in service. The regulations extend to all operations within Australian airspace and are overseen by the Civil Aviation Safety Authority (CASA). The scope of these regulations ensures that the aircraft maintain the necessary safety standards, thereby protecting the safety of all passengers and crew aboard. The Act applies broadly to all relevant aircraft operators and maintenance personnel, ensuring that modifications and inspections are conducted as prescribed to avoid any safety risks.

Key Provisions

The Civil Aviation Regulations 1998, specifically within Part 39 - 105 and the Civil Aviation Safety Authority Schedule of Airworthiness Directives (AD/VAT/25), detail the requirements for the inspection of the nose wheel steering systems on Victa Airtourer 100 and 115 models, excluding those serial numbers prior to 108 and modifications incorporating Model No. B209. The applicability of these regulations is explicitly stated, ensuring clarity on which aircraft must comply. The compliance interval is set at a maximum of 100 hours of time in service, which is documented in Victa Service Bulletin No. 49, Issue 2. This regulation ensures that the nose wheel steering systems of specified Victa Airtourer models are regularly inspected to maintain safety standards. These regulations impose clear obligations on the parties involved, including aircraft owners, operators, and maintenance personnel. The primary obligation is to conduct the specified inspections at intervals not exceeding 100 hours of time in service. This requirement ensures that any potential issues with the nose wheel steering systems are identified and rectified promptly, thereby maintaining the airworthiness of the aircraft. The use of Victa Service Bulletin No. 49, Issue 2, provides detailed guidance on how these inspections should be performed, ensuring consistency and adherence to safety standards. Failure to comply with these regulations can lead to significant consequences. Under the Civil Aviation Regulations 1998, non-compliance with airworthiness directives can result in civil penalties. The maximum penalty for breaches of these regulations is stipulated in the Act, which can include substantial fines. Additionally, continued operation of an aircraft that does not comply with these safety directives can result in the aircraft being grounded, thereby preventing it from being used until it meets the required safety standards. This stringent enforcement underscores the importance of adhering to the outlined inspection intervals and procedures.