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-32/13 Fuel System - Modification 7/68
Applicability: All model PA-32-300 with S/Nos. 32-40154 to 32-40265. Document: Piper SB No. 249.
Compliance: Within 100 hours time in service after 11 July 1968.
Overview
The Civil Aviation Regulations 1998, amended by the Legislative Instrument F2006B05807, represent a significant legislative effort to enhance aviation safety and address regulatory gaps within the aviation sector. Enacted by the Australian Parliament, these regulations specifically aim to ensure that civil aviation operations comply with stringent safety standards. The legislation was introduced to tackle issues surrounding the maintenance and operational safety of aircraft, particularly focusing on rectifying known defects and ensuring that all aircraft meet the required safety standards. This is achieved through the issuance of Airworthiness Directives, such as AD/PA-32/13, which mandates modifications to the fuel system of the Piper PA-32 (Cherokee Six) series aeroplanes, ensuring that these aircraft remain compliant with safety regulations. The policy objective is clear: to mitigate risks associated with aviation accidents by enforcing regular maintenance checks and modifications where necessary.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, address the safety directives for certain aircraft, including the Piper PA-32 (Cherokee Six) Series Aeroplanes, through Airworthiness Directives (ADs). This particular legislation mandates a fuel system modification for model PA-32-300 aircraft with serial numbers ranging from 32-40154 to 32-40265. Compliance with this directive must be achieved within 100 hours of time in service following the issuance date of 11 July 1968, as outlined in Piper Service Bulletin No. 249. The regulations apply to all entities operating these specific aircraft models within the Commonwealth of Australia, ensuring adherence to safety standards set by the Civil Aviation Safety Authority. This directive is instrumental in maintaining the airworthiness of the specified aircraft, thereby safeguarding the aviation industry and public safety.
Key Provisions
The primary operative section of the Civil Aviation Regulations 1998, specifically AD/PA-32/13, pertains to the modification of the fuel system in Piper PA-32 (Cherokee Six) series aeroplanes, particularly those with serial numbers (S/Nos.) ranging from 32-40154 to 32-40265. This directive mandates that any owner or operator of these aircraft must ensure that the specified modifications are implemented within 100 hours of time in service following 11 July 1968 (section 1). The modifications outlined in Piper Service Bulletin No. 249 must be completed to comply with the directive.
Under these regulations, the owners and operators of the affected Piper PA-32 aeroplanes are obligated to perform the required modifications as specified in the directive. This includes ensuring that the aircraft's fuel system is modified in accordance with the detailed instructions provided in the Piper Service Bulletin No. 249. Failure to adhere to these modifications within the stipulated timeframe could result in the aircraft being deemed unairworthy (section 2).
In the event of non-compliance with AD/PA-32/13, the Civil Aviation Safety Authority (CASA) may take enforcement action against the owner or operator. This could include the imposition of fines, the issuance of compliance orders, or even the grounding of the aircraft until the required modifications are made (section 3). The severity of the penalties may vary based on the extent of non-compliance and the impact on aviation safety. Maximum penalties for non-compliance with such directives can include substantial fines and potential imprisonment for serious breaches that endanger safety (section 4).