Airworthiness Directives 2004 - Revocation and Remaking - Short SD3-30 Series Aeroplanes

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Legislation au F2006B08024 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

 Short SD3-30 Series Aeroplanes

 AD Name AD Number

 Galley Urn Restraint - Modification AD/SD3-30/1

 Fuselage Top Skin Sealing - Inspection AD/SD3-30/2

 Engine Power Levers - Modification AD/SD3-30/3

 Fuselage Frame at Station 340.46 - Modification AD/SD3-30/4

 Aileron, Pilots Handwheel Stop - Modification AD/SD3-30/5

 Passenger Cabin Window - Modification AD/SD3-30/6

 Aft Baggage Compartment - Modification AD/SD3-30/7

 Horizontal Stabilizer/Fuselage Attachment Fittings, Pins and Bushes AD/SD3-30/8 Amdt 3

 Fuel System - Inspection and Modification - CANCELLED AD/SD3-30/9 Amdt 2

 Fuel Fume Seal Installation - Modification AD/SD3-30/10 Amdt 1

 Flexible Brake Hoses/Main Landing Gear Beam - Inspection and Modification AD/SD3-30/11

 Rib/Skin Attachment Cleats at Left Wing Station 160 AD/SD3-30/12 Amdt 1

 Right and Left Drag Links - Inspection and Modification AD/SD3-30/13 Amdt 1

 Electrical Power Line Contactor Bodies AD/SD3-30/14 Amdt 1

 Toilet Waste Bin Flap - Improve Fire Resistance AD/SD3-30/15

 Elevator Torque Shaft Assembly AD/SD3-30/16 Amdt 3

 Fuel Pipe Fumeproof Shrouds AD/SD3-30/17 Amdt 1

 Fuselage Sealing AD/SD3-30/18

 Oxygen Bottle Protection AD/SD3-30/19

 Landing Gear Warning Horn AD/SD3-30/20

 Rudder Lower Bearing AD/SD3-30/21

 Elevator and Rudder Control Guards AD/SD3-30/22

 Propeller Attaching Bolts AD/SD3-30/23 Amdt 1

 Nose Landing Gear Pins AD/SD3-30/24

 Airworthiness Limitations AD/SD3-30/25

 Pitot Static Heaters AD/SD3-30/26 Amdt 1

 Wing Strut Distance Piece and Adjacent Side Plates Corrosion AD/SD3-30/27 Amdt 1

 LP Levers AD/SD3-30/28

 Main Landing Gear - Beam Sub Assembly AD/SD3-30/29


 Fin to Tailplane Attachment Bolts and Upper Shear Angle AD/SD3-30/30

 Flap Hydraulic Unit Brackets AD/SD3-30/31

 Inner Flap Sub-Assembly Lever Bracket AD/SD3-30/32

 Elevator and Rudder Skin Flukes AD/SD3-30/33

 Autofeather System Wiring AD/SD3-30/34

 Emergency Brake Accumulator Mounting Structure AD/SD3-30/35

 Engine Mounting Tubes and Fittings AD/SD3-30/36 Amdt 3

 Elevator Control Torque Tube Bearing Housing AD/SD3-30/37

 Stub Wing Shear Deck and Rib Corrosion AD/SD3-30/38 Amdt 1

 Baggage Bay Fire Extinguisher Adapter Covers - CANCELLED AD/SD3-30/39

 Oxygen System O Ring Replacement - CANCELLED AD/SD3-30/40

 Flight Control Trim Chain Connecting Link AD/SD3-30/41

 Electrical Wiring and Hydraulic Pipelines AD/SD3-30/42

 Elevator Torque Shaft Assembly Bearing Housings AD/SD3-30/43

 Engine Intake Anti-Icing  Vane Annunciator AD/SD3-30/44 Amdt 1

 Baggage Bay Fire Extinguisher  Adapter Covers AD/SD3-30/45

 Main Landing Gear Aft Pintle Pin Bushes AD/SD3-30/46

 Fuel Tank Bonding and Inspection AD/SD3-30/47

 

Overview

The Airworthiness Directives 2004, enacted by David Alan Villiers as a delegate of the Civil Aviation Safety Authority, serve to revoke and remake existing airworthiness directives concerning SD3-30 series aeroplanes. This legislative instrument was introduced to address gaps in the current airworthiness directives that required updating or cancellation. The directives are remade to reflect the latest published editions, ensuring that the safety regulations remain current and effective. The objective of these directives is to maintain the airworthiness of aircraft, thereby ensuring the safety of passengers and crew. The directives cover a wide range of modifications and inspections, from fuel system issues to structural components, highlighting the comprehensive approach taken to aviation safety.

Scope and Application

The Airworthiness Directives 2004, made under the authority of the Civil Aviation Safety Authority (CASA), apply to the specified aviation industry and cover a range of aircraft types and their associated systems. These directives are intended to ensure the airworthiness of aircraft by setting out mandatory requirements and modifications that must be adhered to by aircraft operators and other relevant parties. The scope of the Act encompasses various aspects of aircraft maintenance and operational standards, ensuring that aircraft meet the necessary safety and airworthiness criteria set forth by CASA. The application of these directives extends across the Commonwealth of Australia, enforcing compliance with airworthiness standards on a national level. Notably, the legislation does not explicitly state any exclusions, exemptions, or thresholds, suggesting that the directives apply broadly to all relevant aircraft within the Australian jurisdiction. However, the directives may be further refined or extended through subordinate instruments, allowing for specific operational or regional considerations to be addressed.

Key Provisions

The legislative instrument, F2006B08024, establishes Airworthiness Directives under the Civil Aviation Safety Regulations 1998, with David Alan Villiers as the delegate of the Civil Aviation Safety Authority. The primary focus of this instrument is to revoke certain Airworthiness Directives listed in Schedule 1 and re-make them as separate instruments (sections 1(a) and 1(b)). The revised directives are presented in the exact form as they appear in the latest published edition. The schedule lists the specific Airworthiness Directives that are to be revoked and remade, detailing a range of modifications and inspections required for various parts of the aircraft, such as the galley, fuselage, engine, and landing gear, among others. The Airworthiness Directives impose specific obligations on aircraft owners and operators, requiring them to comply with the detailed modifications and inspections outlined in the directives. For instance, these may include inspecting and modifying the fuselage top skin sealing, ensuring the proper functioning of engine power levers, and making necessary changes to the aileron and pilots handwheel stop. Compliance with these directives is essential for maintaining the airworthiness of the aircraft, ensuring that they meet safety standards set by the Civil Aviation Safety Authority. Failure to comply with the Airworthiness Directives can result in significant legal consequences. The Act does not explicitly state the penalties for non-compliance, but under the Civil Aviation Safety Regulations 1998, there may be civil and criminal penalties for breaches. Civil penalties can include fines, while criminal penalties could involve imprisonment, depending on the severity of the breach and its impact on aviation safety. The exact penalties would be determined in accordance with the Civil Aviation Safety Regulations 1998 and any relevant case law.

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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.