COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Cessna 210 Series Aeroplanes
AD/CESSNA 210/27 Rudder Trim Chain - Inspection 5/76
Applicability: All models 210 with S/Nos. 21060540 to 21060820, 60889, 60901, 60902, 60903,
60906, 60907, 60908, and 60909.
Document: Cessna SL SE76-3.
Compliance: Within 100 hours time in service after 31 May 1976.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, are a comprehensive set of rules governing civil aviation safety within Australia. One particular legislative instrument, F2006B08077, pertains to Airworthiness Directives for specific aircraft types, including the Cessna 210 Series Aeroplanes. This particular directive, AD/CESSNA 210/27, was introduced to address a specific safety concern related to the rudder trim chain of certain Cessna 210 models. The directive aims to ensure that the rudder trim chain is inspected within 100 hours of time in service after 31 May 1976 for applicable aircraft serial numbers. The policy objective is to maintain the airworthiness of these aircraft and enhance flight safety by preventing potential issues arising from the rudder trim chain.
This legislative instrument is part of a broader regulatory framework managed by the Civil Aviation Safety Authority, which is responsible for enforcing compliance with airworthiness directives to ensure the highest safety standards in civil aviation. By mandating regular inspections of the rudder trim chain, the regulation seeks to mitigate any risks associated with its failure, thereby contributing to the overall safety and reliability of the specified Cessna 210 aircraft models.
Scope and Application
The Civil Aviation Safety Authority (CASA) Regulations 1998, specifically Part 39 - 105, establish airworthiness directives that are critical for maintaining the safety standards of aircraft operations within Australia. One such directive, AD/CESSNA 210/27, applies to all models of the Cessna 210 series aeroplanes with specific serial numbers, namely 21060540 to 21060820, 60889, 60901, 60902, 60903, 60906, 60907, 60908, and 60909. This directive mandates an inspection of the rudder trim chain within 100 hours of time in service after 31 May 1976. Compliance with this directive is essential for ensuring that the specified Cessna aircraft meet the required safety standards, thus preventing potential hazards and maintaining the integrity of civil aviation safety across Australia. The scope of this legislation is confined to the specified Cessna 210 series aircraft, and the directive is enforced under the overarching framework of the Civil Aviation Regulations 1998.
Key Provisions
The key provisions of the Civil Aviation Regulations 1998, specifically AD/CESSNA 210/27, pertain to the inspection of the rudder trim chain on certain Cessna 210 series aeroplanes. Section 39-105 mandates that aeroplanes with specific serial numbers (21060540 to 21060820, 60889, 60901 to 60909) must undergo an inspection of the rudder trim chain. This inspection is required within 100 hours of time in service after 31 May 1976, as outlined in the document Cessna SL SE76-3. The purpose of this directive is to ensure that the rudder trim chain is in proper working condition, thereby enhancing the safety and airworthiness of the aircraft.
The Act imposes several obligations on the parties and entities it governs. Aircraft operators must ensure that the specified Cessna 210 series aeroplanes are inspected according to the schedule and requirements set out in the Airworthiness Directive. This includes conducting a thorough examination of the rudder trim chain to identify any signs of wear, damage, or malfunction. Additionally, operators must maintain records of these inspections, including the date, the serial number of the aircraft, and the results of the inspection. Failure to comply with these obligations could result in the aircraft being deemed unairworthy.
Breach of the provisions set out in AD/CESSNA 210/27 can lead to various consequences. Civil penalties may be imposed for non-compliance, as outlined in the Civil Aviation Regulations. The maximum penalty for a breach of these regulations can be significant, reflecting the importance of adhering to airworthiness directives to ensure public safety. Furthermore, failure to comply with these requirements could result in the suspension or revocation of the aircraft's certificate of airworthiness, rendering it incapable of legal flight operations. Criminal penalties may also apply if the breach is found to have contributed to an aviation accident or incident.