Airworthiness Directives 2004 - Revocation and Remaking - Piper PA-44 (Seminole) Series Aeroplanes

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 Airworthiness Directives 2004

 I, DAVID ALAN VILLIERS, delegate of the Civil Aviation Safety

 Authority, acting under subregulation 39.001 (1) of the Civil

 Aviation Safety Regulations 1998:

 (a) revoke the Airworthiness Directives mentioned in

 Schedule 1; and

 (b) make, as separate instruments, each Airworthiness

 Directive mentioned in Schedule 1 and attached.

 

 

 David Villiers

 Delegate of the Civil Aviation Safety Authority

 

  20 December 2004

 Note:   Each attached Airworthiness Directive is being re-made in exactly the

 same form as appears in the latest published edition of the Directive.

 


 Schedule 1 Revocation and Remaking of

 Airworthiness Directives

 Piper PA-44 (Seminole) Series Aeroplanes

 AD Name AD Number

 Hose Assembly - Inspection and Replacement AD/PA-44/1

 Fuel Line - Inspection and Modification AD/PA-44/2

 CANCELLED AD/PA-44/3

 Throttle Cable Installation - Modification AD/PA-44/4

 Engine Priming System - Modification AD/PA-44/5

 Aileron Push Rod Functional Check AD/PA-44/6 Amdt 1

 Nose Cone Spar - Inspection and Modification AD/PA-44/7

 Aileron Spar Web - Modification AD/PA-44/8

 Aileron Balance Weight Attachment Inspection and Modification AD/PA-44/9

 Engine Mount Frame Cracking AD/PA-44/10 Amdt 1

 Ammeter Installation AD/PA-44/11 Amdt 1

 Engine Mount Frame AD/PA-44/12

 Main Landing Gear - Trunnion Housing AD/PA-44/13

 Nose Gear Drag Link AD/PA-44/14

 Wing and Carry-Through Structure AD/PA-44/15

 Ailerons AD/PA-44/16

 Flap Handle Attach Bolt AD/PA-44/17

 Combustion Heater Fuel Pumps AD/PA-44/18

 Control Wheel Attachment AD/PA-44/19

 

Overview

The Airworthiness Directives 2004, enacted by David Alan Villiers, the delegate of the Civil Aviation Safety Authority, under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998, addresses the need to revoke and re-make certain airworthiness directives concerning Piper PA-44 (Seminole) Series Aeroplanes. This legislative instrument aims to ensure that the directives reflect the latest safety standards and regulatory requirements. Each directive is re-made in exactly the same form as it appears in the most recent published edition, ensuring consistency and compliance with current aviation safety protocols. The objective is to maintain and enhance the safety of air operations by updating and enforcing specific airworthiness directives for identified aircraft models.

Scope and Application

The Airworthiness Directives 2004, made under the Civil Aviation Safety Regulations 1998, apply specifically to the maintenance and operational standards of Piper PA-44 (Seminole) series aeroplanes within the jurisdiction of the Civil Aviation Safety Authority (CASA). This legislation is enacted by David Alan Villiers, a delegate of CASA, and focuses on ensuring the safety and airworthiness of these specific aircraft models by outlining mandatory inspections, modifications, and maintenance procedures. The directives cover a range of components and systems, including fuel lines, throttle cables, engine components, landing gear, and structural elements. The legislation applies to all persons and entities operating these aircraft in Australia, including aircraft owners, operators, and maintenance service providers. The geographic scope of this legislation is limited to Australia, as it is a national regulation enforced by CASA. The legislation does not explicitly mention any exclusions, exemptions, or thresholds, implying that all Piper PA-44 (Seminole) series aeroplanes within Australian jurisdiction must comply with the outlined directives. Additionally, the legislation allows for the creation of subordinate instruments to further detail or modify the application of these directives.

Key Provisions

The Airworthiness Directives 2004, made by David Alan Villiers as a delegate of the Civil Aviation Safety Authority (CASA), primarily serves to revoke existing Airworthiness Directives for specific Piper PA-44 (Seminole) series aeroplanes and to re-make them as separate instruments (sections 1(a) and 1(b)). These directives address various safety concerns related to different components of the aeroplanes, such as hose assemblies, fuel lines, throttle cables, and engine systems, among others (Schedule 1). Each directive is re-made in the exact form as it appears in the latest published edition, ensuring consistency and clarity in the regulatory requirements. These directives impose specific obligations and requirements on the parties and entities they govern, which primarily include aircraft operators, maintenance organisations, and pilots. For example, operators must comply with the inspection, modification, and replacement requirements outlined in the directives to ensure the continued airworthiness of their aircraft (Schedule 1). Maintenance organisations are tasked with performing the necessary modifications and inspections as specified in the directives to ensure compliance with safety standards. Pilots must also be aware of the directives and ensure that their aircraft meet the required standards before flight. Failure to comply with the provisions of the Airworthiness Directives 2004 can lead to various civil and criminal consequences. Under section 39.001(1) of the Civil Aviation Safety Regulations 1998, non-compliance may result in enforcement actions by CASA, including fines, penalties, or other regulatory sanctions. The maximum penalties for breaches of civil aviation safety regulations can be significant, reflecting the importance of maintaining airworthiness standards to ensure public safety. It is essential for all parties governed by these directives to understand and adhere to their requirements to avoid potential legal and safety repercussions.

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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.