AD/MU-2/18 - Flap Jack Screw - Inspection: Flap Gearbox - Inspection and Re-adjustment

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Legislation au F2006B11346 In force Legislative Instrument

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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-2/18  Flap Jack Screw - Inspection: Flap Gearbox - Inspection and Re-adjustment


3/77

 

Applicability: Model MU-2B-10, -51, -20, -25 and -26 with S/Nos. 005 to 326. Model MU-2B-30, -

35 and -36 with S/Nos. 501 to 672.

 

Document: Mitsubishi SB No. 167C.

 

Compliance: Within 100 hours time in service after 30 April 1977.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Safety Authority (CASA) introduced the Civil Aviation Regulations 1998 as a comprehensive framework to govern civil aviation activities in Australia, ensuring the safety and efficiency of the nation's aviation industry. This legislation was enacted by the Commonwealth of Australia and is overseen by the Civil Aviation Safety Authority, with the overarching policy objective of maintaining the highest standards of safety and operational efficiency within the aviation sector. One specific aspect of this regulatory approach is addressed in Part 39, which includes Airworthiness Directives aimed at ensuring that aircraft meet specific safety standards. For instance, AD/MU-2/18 pertains to the Mitsubishi MU-2 Series Aeroplanes, directing mandatory inspections of the flap jack screw and adjustments of the flap gearbox to ensure continued airworthiness and safe operation of these aircraft models. The enactment of these regulations by the Australian Parliament reflects a commitment to addressing gaps and problems in aviation safety through detailed and specific directives. By mandating thorough inspections and adjustments, such as those outlined in AD/MU-2/18 for certain Mitsubishi MU-2 Series Aeroplanes, the regulations aim to proactively identify and rectify potential safety issues, thereby enhancing the overall safety of Australia's civil aviation operations. This targeted approach under the Civil Aviation Regulations 1998 helps mitigate risks and ensures compliance with international aviation safety standards.

Scope and Application

The Civil Aviation Regulations 1998, as amended, under the jurisdiction of the Civil Aviation Safety Authority, specifically address the maintenance and safety requirements of Mitsubishi MU-2 Series Aeroplanes through the Airworthiness Directive AD/MU-2/18. This directive applies to specific models of the Mitsubishi MU-2B series, including the MU-2B-10, -51, -20, -25, -26, -30, -35, and -36 with serial numbers falling within the specified ranges. The directive mandates that inspections of the flap jack screw and flap gearbox, as detailed in Mitsubishi Service Bulletin No. 167C, be conducted within 100 hours of time in service following the directive's issuance date of 30 April 1977. Compliance with these directives is crucial for maintaining the airworthiness of the affected aircraft, ensuring they meet the necessary safety standards set forth by the Australian aviation regulatory framework.

Key Provisions

The Civil Aviation Regulations 1998, Part 39, Section 105, specifically AD/MU-2/18, outlines critical requirements for the inspection and maintenance of flap jack screws and flap gearboxes for certain Mitsubishi MU-2 series aeroplanes. This directive applies to specific models of the MU-2 series with serial numbers within defined ranges (Section 3). Compliance with these provisions is mandatory for the specified aircraft models, ensuring that they meet safety standards and operational requirements as set by the Civil Aviation Safety Authority (CASA). The directive mandates a thorough inspection of the flap jack screws and the flap gearbox within 100 hours of time in service after 30 April 1977. This inspection is essential to verify the condition and functionality of these critical components, which are vital for the safe operation of the aeroplane (Section 3). Furthermore, the inspection must adhere to Mitsubishi SB No. 167C, which provides detailed procedures and standards for these checks. These requirements are designed to prevent mechanical failures and ensure that the aircraft can be operated safely and efficiently. Entities and individuals governed by these regulations must ensure that all inspections and maintenance are carried out by qualified personnel and documented properly. Failure to comply with these directives can result in severe consequences, as the safety of the aircraft and its occupants is paramount. The regulations impose a clear obligation on operators and maintenance personnel to adhere strictly to the specified timelines and procedures to avoid any safety risks. Non-compliance with AD/MU-2/18 can lead to significant penalties and legal consequences. The Civil Aviation Regulations 1998 outline various penalties for breaches of safety directives, including fines and potential imprisonment for individuals and organisations. The severity of these penalties underscores the importance of adhering to the outlined procedures and maintaining the required standards. By ensuring compliance, operators can avoid legal repercussions and contribute to the overall safety of the aviation industry.

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.