COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Piper PA-31 Series Aeroplanes
AD/PA-31/24
Amdt 1
Rudder Control Cables - Inspection 12/74
Applicability: Model PA-31-350 with S/Nos. 31-5001 to 31-7405495. Document: Piper SB No. 379A.
Compliance: Within 25 hours time in service after 15 November 1974.
Overview
The Civil Aviation Regulations 1998, enacted by the Australian Parliament, provide a comprehensive framework for ensuring the safety and regulation of civil aviation within Australia. This legislation is essential for maintaining the highest standards of airworthiness and operational safety across the country. One specific directive under this Act is the Piper PA-31 Series Aeroplanes AD/PA-31/24 Amendment 1, which addresses the critical issue of rudder control cable inspections for certain Piper PA-31 models. This directive was introduced to mitigate potential risks associated with rudder control cable failures, ensuring that the specified aircraft meet stringent safety standards. The policy objective behind this amendment is to enhance the safety and reliability of civil aviation operations by mandating regular inspections and timely maintenance of essential aircraft components. The enforcement of such directives is overseen by the Civil Aviation Safety Authority, which plays a pivotal role in implementing and monitoring compliance with airworthiness directives to safeguard the aviation industry.
Scope and Application
The Civil Aviation Safety Authority Schedule of Airworthiness Directives, as outlined in Part 39 - 105 of the Civil Aviation Regulations 1998, specifically addresses the airworthiness of aircraft models including the Piper PA-31 Series aeroplanes. This particular directive, AD/PA-31/24 Amendment 1, pertains to the inspection of rudder control cables for Model PA-31-350 aeroplanes with serial numbers ranging from 31-5001 to 31-7405495. This applies to all operators of these aircraft within the Commonwealth of Australia, ensuring that the safety standards set forth by the Civil Aviation Safety Authority are met. The directive mandates that the required inspection of the rudder control cables must be completed within 25 hours of time in service after the directive's effective date of 15 November 1974, as referenced in Piper Service Bulletin No. 379A. The directive does not explicitly mention any exclusions, exemptions, or thresholds, indicating that it applies universally to the specified aircraft within the given serial number range.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39, Section 105, includes an Airworthiness Directive (AD) concerning Piper PA-31 Series Aeroplanes, identified as AD/PA-31/24 Amendment 1. This directive addresses the inspection of rudder control cables for certain models of Piper PA-31 aeroplanes. The directive applies to model PA-31-350 with serial numbers ranging from 31-5001 to 31-7405495. The purpose of this AD is to ensure the safety of these aircraft by mandating regular inspections of the rudder control cables to prevent potential failures that could compromise flight safety.
Under this directive, the operator of the specified Piper PA-31 Series aeroplanes must ensure that the rudder control cables are inspected within 25 hours of time in service after 15 November 1974, as referenced in Piper Service Bulletin No. 379A. This inspection is critical for maintaining the airworthiness of the aircraft, ensuring that the cables are free from defects, wear, or any conditions that might lead to operational hazards during flight.
Failure to comply with this AD may result in serious safety implications, as the rudder control system is essential for the aircraft's stability and control. The Civil Aviation Safety Authority (CASA) has the authority to take enforcement actions against non-compliance. The penalties for not adhering to this directive can include fines, suspension of the aircraft's operating certificate, or other regulatory actions as deemed necessary by CASA. The specific penalties and consequences for non-compliance are determined by the severity of the breach and are outlined in the Civil Aviation Regulations.
The AD underscores the importance of adhering to scheduled inspections and maintenance procedures to ensure the safety of all involved in aviation activities. Operators must strictly follow the compliance timeline and ensure that the inspections are conducted by qualified personnel. By doing so, they mitigate the risk of accidents and maintain the high safety standards required in civil aviation.