COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
S.L. Industries Commander 100 Series and Volair 10 Series Aeroplanes
AD/AC-100/18 Nose Landing Gear Steering Rod - Modification 4/73
Applicability: All models with S/Nos. 026 to 360 and 5001 to 5181. Document: Aero Commander SL No. S-1024.
Compliance: For aircraft which have exceeded 200 hours’ time in service as at 30 April 1973 - within 100 hours’ time in service after 30 April 1973. For all other aircraft - prior to achieving 300 hours’ time in service.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, aim to ensure the safety of civil aviation operations within Australia. Specifically, Part 39 - 105 of these regulations establishes a schedule of airworthiness directives designed to maintain the highest safety standards for aircraft. One such directive, AD/AC-100/18, pertains to the nose landing gear steering rod modification for S.L. Industries Commander 100 Series and Volair 10 Series aeroplanes. This directive was introduced to address potential safety issues associated with the nose landing gear steering rods in these specific aircraft models. The policy objective behind AD/AC-100/18 is to mandate modifications to the nose landing gear steering rods to prevent mechanical failures that could compromise the safety of flight operations. Compliance with this directive is critical for ensuring the continued airworthiness of affected aircraft, thereby protecting both passengers and crew.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, mandates the Civil Aviation Safety Authority (CASA) to issue airworthiness directives, including AD/AC-100/18 concerning the nose landing gear steering rod modification for S.L. Industries Commander 100 Series and Volair 10 Series aeroplanes. This directive applies to all models with serial numbers ranging from 026 to 360 and 5001 to 5181. The legislation dictates compliance timelines based on the aircraft's hours in service, requiring modifications for aircraft that have exceeded 200 hours of service by 30 April 1973 to be completed within 100 hours following that date, while all other aircraft must comply before reaching 300 hours of service. This regulation extends to all aeroplanes within the specified serial number range, regardless of their location or the operator's identity, thereby ensuring a national standard of safety and airworthiness across the aviation industry.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39, Section 105, provides detailed safety directives aimed at ensuring the airworthiness of certain aircraft models. The regulation in focus, AD/AC-100/18, pertains to the modification of the nose landing gear steering rod in S.L. Industries Commander 100 Series and Volair 10 Series aeroplanes. This directive applies to all models with specific serial numbers: from 026 to 360 and 5001 to 5181. The compliance requirement is outlined in Aero Commander SL No. S-1024, which mandates that aircraft which have accumulated over 200 hours of service by 30 April 1973 must undergo the modification within 100 hours after that date. For all other aircraft, the modification must be completed before reaching 300 hours of service.
Under this regulation, the primary obligation for the operators and owners of the affected aircraft is to ensure that the specified nose landing gear steering rod modification is carried out within the stipulated timeframes. This involves detailed inspection and potential repair or replacement of the steering rod, as prescribed in the referenced document. The modifications must be performed by authorised personnel or entities to guarantee compliance with safety standards set by the Civil Aviation Safety Authority (CASA). This includes keeping thorough records of all modifications undertaken and ensuring that the aircraft meet the required safety benchmarks before further operation.
Breaches of the requirements set out in the Civil Aviation Regulations 1998 can lead to serious consequences. The legislation does not explicitly detail specific offences or penalties in the referenced section, but generally, non-compliance with CASA directives can result in enforcement actions. These may include fines, the grounding of non-compliant aircraft, and potential prosecution under civil aviation laws. The severity of penalties can vary based on the nature and extent of the breach, but they can be substantial, reflecting the critical importance of maintaining airworthiness standards. Operators found in violation of these regulations may face significant financial penalties, and in severe cases, criminal charges could be pursued.