AD/MU-2/20 - Engine Nacelle Upper Door Latch Link - Replacement

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Legislation au F2006B11349 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-2/20 Engine Nacelle Upper Door Latch Link - Replacement

Applicability: All models with S/Nos. prior to 697. Document:  Mitsubishi SB No. 180.

Compliance: Before 1 August 1978.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


3/78

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, serve as a comprehensive framework governing various aspects of civil aviation within the country. These regulations are administered by the Civil Aviation Safety Authority (CASA), which is responsible for ensuring the safety of civil aviation. One specific aspect addressed by the regulations is the issuance of airworthiness directives, such as AD/MU-2/20 concerning the Mitsubishi MU-2 Series Aeroplanes. This directive, introduced to address the specific safety issue of the engine nacelle upper door latch link, mandates the replacement of this component in all models with serial numbers prior to 697. The aim of this directive is to enhance the overall airworthiness of these aircraft by rectifying a potential safety concern identified through Mitsubishi SB No. 180, with compliance required before 1 August 1978. This legislative instrument underscores the commitment of CASA to maintaining stringent safety standards in the aviation sector.

Scope and Application

The Civil Aviation Regulations 1998, specifically under Part 39, apply to all aircraft operations within the Commonwealth of Australia, and govern the safety directives issued by the Civil Aviation Safety Authority (CASA). The regulation in focus, AD/MU-2/20, pertains to the Mitsubishi MU-2 Series Aeroplanes and mandates the replacement of the engine nacelle upper door latch link for all models with serial numbers prior to 697. Compliance with this directive must be achieved before 1 August 1978, as stipulated in Mitsubishi Service Bulletin No. 180. This regulation ensures that the specified aircraft models meet the required safety standards, thereby protecting the integrity and safety of civil aviation within Australia. The regulation does not explicitly state exclusions or exemptions, but its application may be further defined through subordinate instruments issued by CASA.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39, Section 105, mandates certain safety directives for Mitsubishi MU-2 series aeroplanes. The key operative section in this instance is AD/MU-2/20, which pertains to the engine nacelle upper door latch link. Section 3/78 of the legislation requires that all Mitsubishi MU-2 aeroplanes with serial numbers prior to 697 must undergo a replacement of the engine nacelle upper door latch link. This requirement is to ensure the continued airworthiness of the aircraft and is based on the Mitsubishi Service Bulletin No. 180. The obligations imposed by this regulation are clear and specific. Owners and operators of Mitsubishi MU-2 aeroplanes with the specified serial numbers must ensure that the engine nacelle upper door latch link is replaced as stipulated. This involves following the guidelines outlined in Mitsubishi Service Bulletin No. 180 and ensuring that the replacement is carried out by certified personnel before the compliance date of 1 August 1978. Failure to comply with these directives can lead to serious consequences, including potential grounding of the aircraft and possible legal ramifications. In terms of penalties and consequences, the Civil Aviation Regulations 1998 do not specify exact penalties for non-compliance with AD/MU-2/20 in this document. However, generally, non-compliance with airworthiness directives can lead to severe civil and criminal penalties under the Civil Aviation Act 1988. The consequences may include fines, imprisonment for individuals responsible for the oversight, or even the revocation of the aircraft’s certificate of airworthiness. The specific penalties can vary based on the severity of the breach and are determined by the Civil Aviation Safety Authority (CASA). For entities, such as airlines or aircraft maintenance organisations, failing to adhere to these directives can result in substantial financial penalties and damage to their reputation. It can also lead to operational disruptions and potential grounding of the affected aircraft, which can have significant financial implications. Ensuring strict compliance with these airworthiness directives is crucial to maintaining safety standards and avoiding these serious consequences.

Legal classification tags

Area of Law
Aviation Law
Instrument
Legislative Instrument
Concepts
Definitions & Interpretation
Compliance Obligations
Enforcement Powers
Catchwords
Airworthiness Directives
Compliance Deadline

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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.