COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Piper PA-32 (Cherokee Six) Series Aeroplanes
AD/PA-32/18 Fuel Selector Valve - Modification 8/70
Applicability: All models with S/Nos. as listed in Piper SB No. 311. Document: Piper SB No. 311.
Compliance: Within 100 hours time in service after 31 August 1970.
Overview
The Civil Aviation Regulations 1998, enacted by the Australian Parliament, govern the safety and operational standards of civil aviation in Australia. Among the various parts of these regulations, Part 39 - 105 addresses the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, which includes specific directives for ensuring the airworthiness of aircraft. One such directive, AD/PA-32/18, pertains to the modification of the fuel selector valve in Piper PA-32 (Cherokee Six) Series aeroplanes. This directive was introduced to address a specific safety issue identified with the fuel selector valves in these aircraft models, aiming to enhance overall aviation safety by mitigating potential risks associated with the fuel system.
The policy objective of AD/PA-32/18, as outlined in the relevant legislative instrument, is to ensure the airworthiness of Piper PA-32 aeroplanes by requiring a modification to the fuel selector valve. This directive applies to all affected models with specific serial numbers as listed in Piper Service Bulletin No. 311. Compliance with this directive is mandatory within 100 hours of time in service after 31 August 1970, underscoring the urgency and importance of addressing the identified safety concern. The directive is a direct response to the need for continuous safety improvements in the aviation industry, as overseen by CASA.
Scope and Application
The Civil Aviation Safety Authority (CASA) has issued an Airworthiness Directive (AD) under the Civil Aviation Regulations 1998, specifically in Part 39 - 105, concerning the modification of the fuel selector valve in Piper PA-32 (Cherokee Six) series aeroplanes. This directive applies to all models with serial numbers as listed in Piper Service Bulletin (SB) No. 311. The directive mandates compliance within 100 hours of time in service after 31 August 1970. The AD is designed to address safety concerns by requiring the modification of the fuel selector valve to ensure that the aeroplanes remain airworthy and meet the required safety standards. This regulation is binding on all entities operating these specific models of Piper PA-32 aeroplanes within the Commonwealth of Australia, ensuring that they adhere to the specified modifications to maintain compliance with safety standards set by CASA.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39, section 105, pertains to the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives. This part addresses modifications and compliance requirements for certain aircraft models, with a particular focus on the Piper PA-32 (Cherokee Six) Series Aeroplanes. The Airworthiness Directive AD/PA-32/18 pertains to a modification of the fuel selector valve, outlined in document Piper SB No. 311. This directive applies to all models within specific serial numbers listed in the referenced Piper Service Bulletin. The compliance requirement is set for within 100 hours of time in service after 31 August 1970.
The obligations imposed by AD/PA-32/18 are clear and directive. Operators of the affected Piper PA-32 aircraft must ensure that the specified fuel selector valve modifications are completed within the stipulated timeframe. This involves adhering to the technical specifications and procedures outlined in Piper SB No. 311. The directive mandates that these modifications be carried out to ensure continued airworthiness and safety of the aircraft in accordance with CASA standards. Failure to comply with these obligations could result in serious safety implications and potential grounding of the aircraft.
Under the Civil Aviation Regulations 1998, violations of the Airworthiness Directive AD/PA-32/18 can lead to significant civil and criminal consequences. The legislation does not specify a maximum penalty within the provided text, but non-compliance can result in enforcement actions by CASA. Such actions might include fines, suspension or revocation of airworthiness certificates, and legal proceedings against the operator. The severity of the penalties will depend on the extent of non-compliance and the impact on aviation safety. It is imperative for operators to take the directive seriously and ensure timely compliance to avoid these adverse outcomes.