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/6 Elevator and Rudder Bellcrank Bearing
Retention - Modification
Applicability: Victa Airtourer 100 and 115 with S/Nos. 1 to 14. Document: Victa SB No. 9.
Compliance: Before 1 September 1971.
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Overview
The Civil Aviation Regulations 1998 (Cth), enacted by the Parliament of Australia, provide a comprehensive framework for ensuring the safety and efficiency of civil aviation within Australian airspace. The regulations address various aspects of aviation safety, including the airworthiness of aircraft, operational standards, and the qualifications of aviation personnel. One particular aspect covered by these regulations is the issuance of Airworthiness Directives (ADs) which are critical in maintaining the safety standards of specific aircraft models. For example, AD/VAT/6 pertains to Victa and A.E.S.L. Airtourer Series Aeroplanes, specifically addressing the elevator and rudder bellcrank bearing retention. This directive was introduced to rectify known safety issues and ensure that these aircraft continue to meet the necessary safety standards. The overarching policy objective is to protect public safety by ensuring that all aircraft in Australian airspace are maintained to a high standard of airworthiness.
The Civil Aviation Safety Authority (CASA) is responsible for issuing these Airworthiness Directives under the authority of the Civil Aviation Regulations 1998. By setting forth specific requirements and compliance deadlines, CASA ensures that aircraft operators take necessary actions to rectify identified issues. This regulatory approach aims to proactively manage and mitigate safety risks associated with particular aircraft models, thereby enhancing the overall safety of civil aviation in Australia. The legislative framework and subsequent directives work in tandem to uphold the highest safety standards, reflecting a commitment to protecting both the flying public and aviation personnel.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 – 105 concerning the Civil Aviation Safety Authority Schedule of Airworthiness Directives, applies to the Victa and A.E.S.L. Airtourer Series Aeroplanes, notably the Victa Airtourer 100 and 115 with serial numbers ranging from 1 to 14. This legislation mandates specific modifications to the elevator and rudder bellcrank bearings as per Victa Service Bulletin No. 9. The regulation necessitates compliance with these modifications before 1 September 1971 to ensure adherence to safety standards and operational airworthiness. The geographic reach of this regulation is national, applying across the Commonwealth of Australia, and it extends to any person or entity involved in the maintenance, operation, or certification of these specified aircraft models. The regulation does not specify any exclusions, exemptions, or thresholds in the provided excerpt but may be further defined or extended through subordinate instruments or additional regulations.
Key Provisions
The Civil Aviation Regulations 1998 (Cth) under PART 39 - 105, particularly AD/VAT/6, specifically address the maintenance and modification requirements for Victa and A.E.S.L. Airtourer Series Aeroplanes. This directive focuses on the elevator and rudder bellcrank bearing retention, requiring modifications to ensure safety. The applicability of this directive is limited to Victa Airtourer 100 and 115 models with serial numbers 1 to 14. The compliance date is set before 1 September 1971, as outlined in Victa Service Bulletin No. 9.
The Act imposes several obligations on the parties involved. Firstly, it mandates that owners and operators of the specified Victa Airtourer models must adhere to the modifications outlined in Victa SB No. 9. This includes ensuring that the elevator and rudder bellcrank bearing retention modifications are completed before the specified compliance date. Failure to comply with these modifications could result in the aircraft being deemed non-airworthy, thus preventing its operation. Operators must also maintain records of compliance with these directives and be prepared to demonstrate adherence during inspections.
Failure to comply with the provisions of AD/VAT/6 can result in several consequences. Civil penalties may be imposed for non-compliance, including fines and potential grounding of the aircraft. The Civil Aviation Safety Authority (CASA) has the authority to take enforcement actions against operators who do not adhere to the requirements. In severe cases, criminal charges could be filed, leading to more significant penalties, including imprisonment. The exact penalties depend on the severity of the breach and are determined on a case-by-case basis by CASA. It is imperative for operators to understand and comply with these directives to avoid legal repercussions and ensure the continued airworthiness of their aircraft.