Airworthiness Directives 2004 - Revocation and Remaking - DHC-3 (Otter) Series Aeroplanes

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Legislation au F2006B07838 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

 DHC-3 (Otter) Series Aeroplanes

 AD Name AD Number

 Rudder Quadrant, Rudder Pedal Linkage, Tail Wheel Assembly and Rear  AD/DHC-3/1

 Rear Cargo Door AD/DHC-3/2

 Main Undercarriage Compression Strut AD/DHC-3/3

 Cargo Door Handles AD/DHC-3/4

 Booster Pump, Fuselage Former Cap Strips, Rear Cabin Seats AD/DHC-3/5

 Rudder Control AD/DHC-3/6

 Engine Breather Drain Box AD/DHC-3/7

 With Skin Riveting and Flap Hydraulic System AD/DHC-3/8

 Tailplane Trim Indicator AD/DHC-3/9

 Exhaust System AD/DHC-3/10

 Elevator Quadrant, Inboard Nose Flaps, Empennage, Aileron Centre Hinge  AD/DHC-3/11

 Flap Hydraulic Jack AD/DHC-3/12

 Propeller Counterweight Bearing Shafts AD/DHC-3/13

 Tailplane Fork Attachment Fitting AD/DHC-3/14

 Engine Driven Fuel Pump AD/DHC-3/15

 Flap Control Rod Sub-Assembly AD/DHC-3/16

 Engine Cooling AD/DHC-3/17

 Wing Strut Spar AD/DHC-3/18

 Fuel Line Chafing AD/DHC-3/19

 Mixture Control Lever Quadrant AD/DHC-3/20

 Rudder Pedal Support AD/DHC-3/21

 Elevator Tab Control Arm AD/DHC-3/22

 VNE Placard AD/DHC-3/23

 Main Landing Gear Fuselage Attachment Bolts AD/DHC-3/24

 Wing Strut and Attachments - Retirement Lives AD/DHC-3/25

 Tailplane Hinge Bolts AD/DHC-3/26

 Front Seat Restraint Installation AD/DHC-3/27

 Front Fuselage - Windshield Post AD/DHC-3/28

 Engine Mounting Frame AD/DHC-3/29


 Elevator Connecting Rod AD/DHC-3/30

 Control Column Cracking AD/DHC-3/31

 Utility Seat Forward Leg Positive Lock Installation AD/DHC-3/32 Amdt 1

 Wing Strut to Fuselage Tie Bar AD/DHC-3/33

 Tailplane Main Rib Forward Flange and Forward Lower Flange AD/DHC-3/34 Amdt 1

 Electrical System AD/DHC-3/35

 Fire Detection and Extinguishing System AD/DHC-3/36

 Magneto Cannon Plug AD/DHC-3/37

 Electrically Heated Engine Pneumatic Lines AD/DHC-3/38

 Elevator Servo Tab AD/DHC-3/39

 

Overview

The Airworthiness Directives 2004, enacted by David Alan Villiers as the delegate of the Civil Aviation Safety Authority, focuses on the regulation and maintenance of airworthiness standards for specific aircraft. This legislative instrument aims to revoke existing airworthiness directives and re-issue them in an updated form, ensuring that the latest safety standards and operational requirements are applied to the DHC-3 (Otter) series aeroplanes. The enactment follows the Civil Aviation Safety Regulations 1998 and represents a commitment to maintaining the highest safety standards in civil aviation. The policy objective is to ensure that all airworthiness directives are current and effectively address any identified safety issues, thus protecting the public and enhancing the overall safety of air travel.

Scope and Application

The Airworthiness Directives 2004, made by David Alan Villiers as the delegate of the Civil Aviation Safety Authority, addresses the revocation and remaking of various Airworthiness Directives related to the airworthiness of DHC-3 (Otter) series aeroplanes. These directives apply to the entities and persons responsible for the operation and maintenance of the specified aeroplanes, ensuring compliance with safety standards. The geographic and jurisdictional reach of this legislative instrument is national, as it pertains to airworthiness across Australia under the Civil Aviation Safety Regulations 1998. Each directive has been re-made in the same form as the latest published edition, and they cover specific components and systems of the DHC-3 series aeroplanes, including the rudder quadrant, rudder pedal linkage, tail wheel assembly, and other critical parts. The application of these directives is extended or restricted through subordinate instruments as necessary to maintain airworthiness standards.

Key Provisions

The Airworthiness Directives 2004, as outlined in F2006B07838, primarily focuses on the revocation and remaking of various Airworthiness Directives (ADs) concerning DHC-3 (Otter) Series Aeroplanes (section 1(a) and (b)). This legislative instrument revokes existing ADs listed in Schedule 1 and simultaneously remakes each of them in an identical form as they appear in the latest published edition of the Directive. These directives cover a range of critical safety aspects of the DHC-3 aircraft, such as rudder quadrant, rudder pedal linkage, tail wheel assembly, rear cargo door, main undercarriage compression strut, and numerous other components and systems (Schedule 1). The Airworthiness Directives 2004 impose specific obligations on the parties involved, particularly those responsible for the maintenance, inspection, and operation of DHC-3 (Otter) Series Aeroplanes. These obligations include ensuring that all aircraft comply with the detailed requirements specified in the remade ADs, which are designed to address safety issues and ensure that the aircraft meet airworthiness standards (section 1(b)). Compliance with these ADs is crucial for maintaining the safety and airworthiness of the aircraft, and failure to adhere to these directives can lead to severe consequences. Under the Civil Aviation Safety Regulations 1998, breaches of the remade ADs can result in significant civil and criminal penalties. Operators and individuals failing to comply with the requirements of the ADs may face enforcement actions, which can include fines, the grounding of non-compliant aircraft, and potential criminal charges for serious violations. The maximum penalties for such breaches can vary depending on the nature and severity of the non-compliance, but they are intended to enforce strict adherence to safety regulations within the aviation industry (section 39.001(1)). The legislative instrument underscores the importance of maintaining high safety standards in aviation. By revoking and remaking the ADs, it ensures that the latest safety requirements and best practices are incorporated into the maintenance and operation of DHC-3 (Otter) Series Aeroplanes. This approach helps to mitigate risks and prevent accidents by ensuring that all stakeholders are aware of and comply with the necessary safety protocols. The rigorous enforcement of these directives highlights the Civil Aviation Safety Authority's commitment to ensuring the highest standards of airworthiness and safety in the aviation sector.

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