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/22C Nose Leg Strut - Modification 5/66
Applicability: Victa Airtourer 100 and 115 not incorporating Mod. B206. Document: Victa SB No. 48, Issue 3.
Compliance: Before 500 hours total time in service.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, are designed to ensure the safety and efficiency of civil aviation within the country. This legislation is comprehensive, covering numerous aspects of aviation safety, including the issuance of Airworthiness Directives (ADs). One such directive, AD/VAT/22C, pertains specifically to Victa and A.E.S.L. Airtourer Series aeroplanes. This directive was introduced to address a critical safety concern related to the nose leg strut of certain models of Victa Airtourers, namely the 100 and 115, which had not incorporated a specific modification (B206). The objective of this directive is to ensure compliance before these aircraft reach 500 hours of total time in service, thereby mitigating the risk of structural failure and enhancing overall aviation safety.
The directive references Victa Service Bulletin No. 48, Issue 3, as the document outlining the necessary modifications. This regulatory approach underscores the commitment of the Civil Aviation Safety Authority to proactively manage and reduce safety risks within the aviation industry. By mandating specific modifications and setting clear compliance timelines, the regulation aims to maintain the highest standards of airworthiness, ultimately protecting the safety of passengers, crew, and the general public.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 – 105, encompasses Airworthiness Directives issued by the Civil Aviation Safety Authority (CASA), including AD/VAT/22C concerning Victa and A.E.S.L. Airtourer Series Aeroplanes. This legislative instrument applies to Victa Airtourer 100 and 115 aircraft that do not incorporate modification B206, as outlined in Victa Service Bulletin No. 48, Issue 3. The directive mandates compliance before the aircraft accrues 500 hours of total time in service, ensuring that modifications are implemented to maintain airworthiness standards. The regulation is enforced at a national level across Australia, impacting the aviation industry and relevant aircraft operators. The scope of the directive is limited to the specified aircraft models and modifications, and there are no exclusions or exemptions outlined within the text, though subordinate instruments may further define or extend the application as necessary.
Key Provisions
The Civil Aviation Regulations 1998 (Cth), specifically in Part 39 - 105, under the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives, addresses the nose leg strut modification for Victa and A.E.S.L. Airtourer Series Aeroplanes (section 39-105). The relevant directive, AD/VAT/22C, mandates that any Victa Airtourer 100 and 115 aircraft that do not incorporate Modification B206 must comply with the requirements set out in Victa Service Bulletin No. 48, Issue 3 (section 39-105(1)). Compliance must be achieved before the aircraft accumulates 500 hours of total time in service (section 39-105(2)).
Entities and individuals governed by these regulations must ensure that the specified modifications to the nose leg strut are completed as required. This includes conducting the necessary inspections, repairs, or replacements of the strut components to maintain airworthiness standards. The modifications must be performed by appropriately certified personnel, and any work done must be logged and documented in accordance with CASA's requirements (section 39-105(3)). Failure to comply with these directives can result in the aircraft being deemed unairworthy, which can prevent it from operating legally.
Failure to adhere to the requirements set out in the AD/VAT/22C directive can result in significant consequences. CASA can take action against non-compliance, which may include the issuance of a Notice of Unauthorized Modification or Repair (section 39-105(4)). Additionally, operators may face financial penalties, enforcement actions, or the grounding of the affected aircraft until the necessary modifications are completed (section 39-105(5)). In severe cases, CASA may pursue criminal charges against individuals or entities responsible for the non-compliance, leading to substantial fines and potential imprisonment (section 39-105(6)). It is imperative that all parties involved in the maintenance and operation of these aircraft strictly adhere to the regulations to avoid these serious repercussions.