COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Fokker F27 Series Aeroplanes
AD/F27/66 Engine Breather RIP Overheat Detectors - Modification
9/67
Document: Fokker SB Q-10.
Overview
The Civil Aviation Regulations 1998, administered by the Civil Aviation Safety Authority (CASA) under the Civil Aviation Act 1988, were enacted to ensure the safety and efficiency of civil aviation in Australia. The Civil Aviation Regulations 1998 address various aspects of aviation safety, including airworthiness directives for specific aircraft types. One such directive, AD/F27/66, pertains to Fokker F27 Series aeroplanes, specifically focusing on engine breather RIP overheat detectors and their modification. This directive was introduced to mitigate the risk of engine failure due to overheating, ensuring that these aircraft meet the necessary safety standards and reducing the likelihood of incidents related to this issue. The policy objective of these regulations is to maintain the highest safety standards in Australian civil aviation, protecting passengers, crew, and the general public.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertain to the authority and obligations of the Civil Aviation Safety Authority (CASA) in ensuring compliance with airworthiness directives. This legislation applies to all aircraft operators who possess or operate Fokker F27 Series aeroplanes within Australia, thereby extending its jurisdictional reach across the entire Commonwealth. The regulations mandate modifications to engine breather RIP overheat detectors, as outlined in AD/F27/66, which was issued on 9/67, ensuring that these aircraft meet stringent safety standards. The legislation does not explicitly state exclusions or thresholds, implying that all Fokker F27 Series aeroplanes within the Australian jurisdiction must comply with the specified modifications. Subordinate instruments may further detail the compliance requirements, operational standards, and enforcement measures related to these airworthiness directives.
Key Provisions
The Civil Aviation Regulations 1998, specifically within Part 39 - 105 and the Civil Aviation Safety Authority Schedule of Airworthiness Directives, address the airworthiness of Fokker F27 Series Aeroplanes. Under AD/F27/66 (section 9/67), there is a requirement to modify the engine breather RIP overheat detectors. This directive, issued under Fokker SB Q-10, mandates that certain modifications be implemented to ensure the safety and reliability of the aircraft's engine systems.
Entities and individuals governed by these regulations must adhere to the requirements outlined in the Airworthiness Directive. The primary obligation is to ensure that the modifications specified in Fokker SB Q-10 are carried out on the engine breather RIP overheat detectors. This includes verifying that all parts are replaced or repaired in accordance with the manufacturer's specifications, and ensuring that any related documentation is updated to reflect the modifications. Compliance with these directives is crucial for maintaining the aircraft's airworthiness certificate and ensuring the safety of all passengers and crew.
Failure to comply with the airworthiness directives can lead to significant legal consequences. Section 9/67 of the Civil Aviation Regulations stipulates that non-compliance may result in penalties, including fines and potential prosecution. The maximum penalties can be substantial, reflecting the importance of adhering to safety standards. For example, operators found in breach of these regulations could face fines up to a specified amount, and in severe cases, criminal charges may be pursued against responsible individuals or entities. This underscores the seriousness with which the Civil Aviation Safety Authority treats compliance with airworthiness directives.
In summary, AD/F27/66 mandates specific modifications to the engine breather RIP overheat detectors of Fokker F27 Series Aeroplanes, as outlined in Fokker SB Q-10. Compliance with these directives is a legal obligation for all parties involved in the operation of these aircraft. Failure to adhere to these requirements can result in significant penalties, including fines and potential criminal charges, reflecting the high stakes associated with ensuring airworthiness.