AD/PL 12/3 Amdt 1 - Longitudinal Trim Augmenter

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Legislation au F2006B06268 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

 


Transavia PL 12 Series Aeroplanes

 

AD/PL 12/3

Amdt 1


Longitudinal Trim Augmenter 2/89

 

Applicability: PL 12, PL 12U, PL 12/T320, PL 12/T300. Requirement:  Action in accordance with Transavia SB No. 16. Compliance:               At intervals not exceeding 100 hours time in service.

Background:  This Amendment deletes “All models” from the “Applicability” to reflect the design and manufacturing improvements in the later model aircraft.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Australian Parliament, serve as a fundamental framework governing civil aviation safety and operations within Australia. A particular focus of these regulations is the oversight and maintenance of aircraft airworthiness, ensuring that all aircraft meet stringent safety standards. Among the various amendments and directives, the Transavia PL 12 Series Aeroplanes AD/PL 12/3 Amendment 1 addresses the specific issue of longitudinal trim augmenter requirements for certain Transavia aircraft models. This legislative instrument was introduced to rectify a gap in the applicability criteria, ensuring that only the relevant models—PL 12, PL 12U, PL 12/T320, and PL 12/T300—are subject to the specified maintenance actions, thereby reflecting improvements in later model designs and manufacturing processes. The primary objective of this amendment is to enhance safety by ensuring that maintenance actions are appropriately targeted to aircraft models that require specific interventions. By updating the applicability criteria to exclude "All models" and instead specifying the exact models that need attention, the regulation aligns with the latest design and manufacturing advancements. This targeted approach not only improves the precision and effectiveness of maintenance procedures but also reinforces the overarching goal of maintaining high safety standards in civil aviation.

Scope and Application

The Civil Aviation Regulations 1998, specifically under PART 39 - 105, apply to the Civil Aviation Safety Authority Schedule of Airworthiness Directives, which include the Transavia PL 12 Series Aeroplanes. This legislation is applicable to the specific models PL 12, PL 12U, PL 12/T320, and PL 12/T300, with a requirement that action be taken in accordance with Transavia Service Bulletin No. 16. The directive mandates that compliance with these actions must be achieved at intervals not exceeding 100 hours of time in service. The regulations are applicable within the Commonwealth of Australia, overseen by the Civil Aviation Safety Authority (CASA). The scope of this Act is narrowly focused on these particular aircraft models, reflecting improvements and modifications in later models. This amendment, AD/PL 12/3 Amendment 1, adjusts the applicability by removing "All models" from the directive, thereby targeting only the specified models, which have undergone design and manufacturing enhancements.

Key Provisions

The Civil Aviation Regulations 1998, under Part 39, specifically in the Schedule of Airworthiness Directives, mandates certain actions regarding the Transavia PL 12 Series Aeroplanes (sections 105, AD/PL 12/3, Amendment 1). This amendment pertains to the longitudinal trim augmenter, dated 2/89, and affects the PL 12, PL 12U, PL 12/T320, and PL 12/T300 models. The primary requirement here is that the action must be taken in accordance with Transavia Service Bulletin No. 16. This bulletin provides detailed instructions on the necessary maintenance or modifications required to ensure the aircraft’s airworthiness. Entities and parties governed by these regulations must adhere to the specified intervals for compliance. According to the directive, compliance must occur at intervals not exceeding 100 hours of time in service. This ensures that the necessary checks and actions are taken regularly, thereby maintaining the aircraft's safety and operational standards. The applicability of this directive has been refined to exclude "All models" due to design and manufacturing improvements in the later model aircraft. In terms of obligations, the responsible parties must ensure that the required actions outlined in Transavia SB No. 16 are performed within the stipulated timeframe. This involves thorough inspections, maintenance, or modifications as necessary to comply with the airworthiness directive. Failure to comply with these regulations can result in serious repercussions, including potential grounding of the aircraft and enforcement actions by the Civil Aviation Safety Authority. The non-compliance not only poses a risk to the safety of the aircraft but also has legal and financial implications for the operators and maintenance providers. In terms of consequences, breaches of these regulations can lead to both civil and criminal penalties. Civil penalties may include fines, while criminal penalties can involve imprisonment, depending on the severity of the breach and its impact on aviation safety. The specific maximum penalties are not detailed in the provided text but generally, under Australian aviation law, the penalties can be significant, reflecting the critical nature of air safety regulations. It is imperative for all stakeholders to adhere strictly to the requirements to avoid these adverse outcomes.

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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.