COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Mitsubishi MU-2 Series Aeroplanes
AD/MU-2/19 Engine Nacelle Upper Door Rod Assembly - Removal and Modification
Applicability: All models with S/Nos. prior to 697, except S/Nos. 313, 321, 652 and 661. Document: Mitsubishi SB No. 179.
1/78
Compliance: Unless already accomplished, within 100 hours time in service after 28 February 1978.
Overview
The Civil Aviation Regulations 1998, enacted by the Commonwealth of Australia, are a comprehensive set of regulations that govern civil aviation in Australia. Among these regulations, Part 39 specifically addresses airworthiness directives, with the aim of ensuring that aircraft meet the necessary safety standards. One such directive, AD/MU-2/19, pertains to the Mitsubishi MU-2 Series Aeroplanes, specifically focusing on the engine nacelle upper door rod assembly. This directive was introduced to address the identified issue of potential structural integrity failures in the specified models, ensuring continued safety and compliance with civil aviation standards. The Civil Aviation Safety Authority, which is the enacting body, aims to mitigate risks and ensure the safe operation of aircraft within Australia's airspace.
Scope and Application
The Civil Aviation Safety Authority's regulation under the Civil Aviation Regulations 1998, specifically in Part 39 - 105, mandates adherence to Airworthiness Directives (AD) for Mitsubishi MU-2 Series aeroplanes. This regulation applies to all models of these aircraft with serial numbers prior to 697, excluding specific serial numbers 313, 321, 652, and 661. The directive, AD/MU-2/19, pertains to the removal and modification of the engine nacelle upper door rod assembly, necessitating compliance unless such actions have already been completed. The compliance period requires these modifications to be executed within 100 hours of time in service following 28 February 1978. This directive is pivotal in ensuring the ongoing airworthiness and safety of the specified Mitsubishi MU-2 Series aeroplanes, thereby impacting the aviation industry's safety standards and operational procedures.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39, Section 105, outlines the Airworthiness Directives (AD) for various aircraft, including Mitsubishi MU-2 Series Aeroplanes. Section AD/MU-2/19 pertains to the engine nacelle upper door rod assembly, detailing its removal and modification. The directive applies to all models of Mitsubishi MU-2 with serial numbers (S/Nos.) prior to 697, with specific exceptions for S/Nos. 313, 321, 652, and 661. Compliance with these directives is mandated by Mitsubishi Service Bulletin No. 179.1/78 and must be completed within 100 hours of time in service following 28 February 1978.
Under this directive, the primary obligation for operators and owners of the specified Mitsubishi MU-2 Series Aeroplanes is to ensure the engine nacelle upper door rod assembly is removed and modified according to the specifications outlined in Mitsubishi Service Bulletin No. 179.1/78. This involves a thorough inspection and, where necessary, modification of the door rod assembly to comply with safety standards. The directive aims to address potential safety issues that could affect the aircraft's airworthiness, ensuring that these planes continue to meet the regulatory safety requirements set by the Civil Aviation Safety Authority (CASA).
Failure to comply with the provisions outlined in AD/MU-2/19 may result in serious legal consequences. The Civil Aviation Regulations 1998 impose strict penalties for non-compliance, which can include fines and potential grounding of the aircraft until the required modifications are completed. The severity of the penalties may vary depending on the extent of the non-compliance and any resulting safety risks. The maximum penalties for such breaches are substantial, reflecting the critical importance of adhering to these airworthiness directives to maintain safety standards in civil aviation.
In summary, AD/MU-2/19 is a crucial directive that mandates specific modifications to the engine nacelle upper door rod assembly on certain Mitsubishi MU-2 Series Aeroplanes. Operators and owners must ensure timely compliance to avoid severe penalties, including fines and potential aircraft grounding. This directive underscores the importance of adhering to safety regulations to maintain the airworthiness of aircraft and protect public safety.