Airworthiness Directives 2004 - Revocation and Remaking - Douglas DC3 Series Aeroplanes

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Legislation au F2006B07845 In force Legislative Instrument

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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

 Douglas DC3 Series Aeroplanes

 AD Name AD Number

 Wing Tip Root Reinforcement AD/DC3/1

 Rudder Hinge Bracket Rivet - Replacement AD/DC3/2

 Rudder Pedal Slide Tube Support - Modification AD/DC3/3

 Engine Section Throttle Control Rod - Replacement AD/DC3/4 Reissue

 CANCELLED AD/DC3/5

 CANCELLED AD/DC3/6

 CANCELLED AD/DC3/7

 Fire Extinguisher Release Cable Conduit - Replacement AD/DC3/8 Reissue

 Automatic Pilot Control Handle - Modification AD/DC3/9

 Rear Luggage Compartment Tie Down Fittings - Modification AD/DC3/10

 Tailplane Rib - Modification AD/DC3/11

 Oil Dilution Unit - Modification AD/DC3/12 Reissue

 Flap Adjustment AD/DC3/13

 Fuel Tank Filler Cap - Modification AD/DC3/14 Reissue

 Engine Nacelle Fire Protection - Modifications AD/DC3/15 Amdt 2

 Flexible Hose - Replacement AD/DC3/16 Reissue

 Elevator Tab Control Horn - Inspection AD/DC3/17

 Flap Mechanism Attachment Angle - Inspection AD/DC3/18

 Aileron Trim Tab Control Rod - Inspection AD/DC3/19

 Elevator Hinge Bracket - Inspection AD/DC3/20

 Instrument Panel Junction Box - Inspection AD/DC3/21

 CANCELLED AD/DC3/22

 Superseded by AD/DC3/26 - CANCELLED AD/DC3/23

 DME rial Installation - Modification AD/DC3/24

 Outer Aileron Hinge and Associated Structure - Inspection - CANCELLED AD/DC3/25

 Wing Centre Section Structure at Stn 141-142 - Inspection and Modification AD/DC3/26 Amdt 2

 Crew Compartment Acoustic Treatment - Restoration AD/DC3/27

 Hydraulic System - Modification AD/DC3/28 Reissue

 Lower Centre Section Skin and Structure AD/DC3/29 Amdt 4


 Front (Pilots) Seats Restraint Installations - Modification AD/DC3/30

 Undercarriage Y Brace Fitting - Inspection AD/DC3/31 Amdt 2

 Elevator Control System - Inspection AD/DC3/32

 Supplemental Inspection Program AD/DC3/33

 Aircraft Flight Manual, Flight into Icing Conditions AD/DC3/34 Amdt 1

 

Overview

The Airworthiness Directives 2004, enacted by the delegate of the Civil Aviation Safety Authority (CASA), David Alan Villiers, under subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998, address the need to update and manage airworthiness directives for specific aircraft, namely the Douglas DC3 Series Aeroplanes. The objective of these directives is to ensure that the aircraft meet current safety standards and regulatory requirements by revoking outdated directives and re-making them as separate instruments. This legislative instrument aims to maintain and enhance aviation safety by providing clear and updated instructions for aircraft maintenance and operation. CASA, as the regulating body, ensures that the directives reflect the latest safety standards and technological advancements in the aviation industry.

Scope and Application

The Airworthiness Directives 2004, made by the delegate of the Civil Aviation Safety Authority (CASA), concern the revocation and remaking of specific Airworthiness Directives for the Douglas DC3 Series Aeroplanes. These directives are targeted at ensuring the airworthiness of the specified aircraft by addressing various structural, mechanical, and safety issues. The legislation applies to the persons or entities that own, operate, or maintain Douglas DC3 Series Aeroplanes, thereby directly impacting the aviation industry, particularly those involved in the maintenance, operation, and oversight of these aircraft. Geographically, this legislative instrument operates under the Commonwealth jurisdiction, as CASA is a federal authority. The instrument does not specify any exclusions, exemptions, or thresholds, but it does outline the detailed modifications and inspections required for the continued airworthiness of these aircraft. The application of these directives can be further extended or detailed through subordinate instruments, which would provide more specific guidelines or additional requirements as necessary.

Key Provisions

The Airworthiness Directives 2004 (F2006B07845) primarily serves to revoke and reissue certain Airworthiness Directives related to Douglas DC3 Series aeroplanes, ensuring their continued relevance and compliance with safety standards. Specifically, section 3(a) of the legislation revokes the existing Airworthiness Directives listed in Schedule 1, while section 3(b) re-issues each of these directives as separate instruments, maintaining their original content. This ensures that the safety requirements and modifications previously outlined are still in effect but are now legally updated under the new legislative framework. The obligations imposed by this legislation are primarily on aircraft operators and maintenance personnel. They must ensure that all required modifications, inspections, and replacements are carried out as per the reissued Airworthiness Directives. This includes, but is not limited to, reinforcing wing tips, replacing rudder hinge brackets, modifying rudder pedals, and inspecting various structural components such as the elevator tab control horn and aileron trim tab control rod. Each directive specifies the exact actions to be taken, the frequency of inspections, and the methods for compliance, ensuring that the aircraft remain airworthy and safe for operation. Failure to comply with the Airworthiness Directives can result in serious legal consequences. The Civil Aviation Safety Regulations 1998 outline various offences and penalties for non-compliance. For instance, operating an aircraft that does not meet the airworthiness standards can lead to civil penalties, including fines up to a specified maximum amount. Additionally, criminal charges may be brought against individuals or companies responsible for non-compliance, potentially leading to imprisonment. These measures underscore the importance of adhering to the directives to maintain safety and regulatory compliance in 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.