Airworthiness Directives 2004 - Revocation and Remaking - Eurocopter AS 332 (Super Puma) Series Helicopters

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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

 Eurocopter AS 332 (Super Puma) Series Helicopters

 AD Name AD Number

 Main Rotor Shaft AD/S-PUMA/1

 Main Rotor Head - Sleeves AD/S-PUMA/2

 Tail Rotor Head Spindles AD/S-PUMA/3 Amdt 2

 Intermediate Gearbox Aft Attachment Rib - CANCELLED AD/S-PUMA/4 Amdt 2

 Landing Gear Actuator Fairing AD/S-PUMA/5

 Lucas Air Equipment Hoists - Explosive Squib AD/S-PUMA/6 Amdt 1

 Electrical Cabinet Cover Panel AD/S-PUMA/7 Amdt 1

 Engine / Main Gearbox Coupling Shaft - CANCELLED AD/S-PUMA/8

 Electrical Power System AD/S-PUMA/9

 Tail Rotor Pitch Change Bearings AD/S-PUMA/10 Amdt 2

 Main Rotor LE Protective Strip AD/S-PUMA/11 Amdt 2

 Tail Rotor Head - Clevis Sleeves - CANCELLED AD/S-PUMA/12

 Tail Rotor Drive Shaft - CANCELLED AD/S-PUMA/13

 Swashplate Scissors AD/S-PUMA/14

 Sling Installation - 3 Ton Cargo Hook AD/S-PUMA/15 Amdt 1

 Tail Position Lights AD/S-PUMA/16

 Main Gearbox Epicyclic Module Upper Casing Bearing Attachment Bolts AD/S-PUMA/17

 Main Rotor Blade De-Icers AD/S-PUMA/18

 Tail Rotor Electrical Bonding Braids - CANCELLED AD/S-PUMA/19

 Tail Rotor Flange Hinge - CANCELLED AD/S-PUMA/20 Amdt 2

 Tail Rotor Pitch Change Spiders AD/S-PUMA/21 Amdt 1

 Tail Rotor Shaft AD/S-PUMA/22

 Main Rotor Spindles and Flapping Hinge Pins AD/S-PUMA/23

 Intermediate Gearbox Front Stirrup AD/S-PUMA/24 Amdt 1

 Cockpit Doors Hinge Tenons AD/S-PUMA/25 Amdt 1

 Single Pole Circuit Breaker AD/S-PUMA/26

 Main Rotor Head Blade Horn Eye Bolts AD/S-PUMA/27 Amdt 1

 Engine to Main Gearbox Coupling AD/S-PUMA/28 Amdt 4

 Free Turbine Vibration Checks - Makila 1A, 1A1 Turboshaft Engines -  AD/S-PUMA/29


 Tail Rotor Gearbox (TGB) Angular Play Check AD/S-PUMA/30 Amdt 2

 Tail Rotor Blade De-icing Rotating Collector AD/S-PUMA/31 Amdt 1

 Connectral Electrical Connection Modules AD/S-PUMA/32

 Fuel By-pass Valve AD/S-PUMA/33 Amdt 4

 Hoist Arm Lower Fitting Attachment AD/S-PUMA/34 Amdt 1

 Horizontal Stabiliser Spar Tube AD/S-PUMA/35 Amdt 2

 Tail Rotor Blades AD/S-PUMA/36

 Ferry Fuel Tanks AD/S-PUMA/37

 Main Frame 5295 AD/S-PUMA/38 Amdt 3

 Pilot and Co-Pilot Cockpit Pedal Unit AD/S-PUMA/39 Amdt 1

 Engine Indicating - CANCELLED AD/S-PUMA/40

 Main Gearbox Bevel Gear AD/S-PUMA/41 Amdt 2

 Main Rotor and Tail Rotor  Dynamic Components AD/S-PUMA/42 Amdt 1

 Ferry Tank Attachment AD/S-PUMA/43 Amdt 2

 Rescue Hoist AD/S-PUMA/44

 Main Rotor Blades - Vibration Absorbers AD/S-PUMA/45 Amdt 1

 Electric Hoists AD/S-PUMA/46

 Fuel Governor AD/S-PUMA/47

 Hydraulic Reservoir Fittings AD/S-PUMA/48

 Pilot Cyclic Stick Stops AD/S-PUMA/49

 Engine Electronic Control Unit AD/S-PUMA/50

 Tail Rotor Hub Bearing AD/S-PUMA/51

 Hoist Hooks AD/S-PUMA/52

 Hoist Operator's Belt Snap Hook AD/S-PUMA/53

 Plug Doors AD/S-PUMA/54

 BREEZE Hoist Hooks AD/S-PUMA/55

 Hoist Plate Front Attachment AD/S-PUMA/56

 

Overview

The Airworthiness Directives 2004 were enacted under the authority of the Civil Aviation Safety Authority (CASA) to address gaps in the regulation of airworthiness standards for specific aircraft types, particularly the Eurocopter AS 332 (Super Puma) Series Helicopters. This legislative instrument was issued by David Alan Villiers, the delegate of CASA, in accordance with subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998. The primary objective of this legislation was to ensure that the airworthiness directives were up-to-date and aligned with the latest safety standards, thereby enhancing the overall safety of aviation operations in Australia. The directives were revoked and re-made to reflect the most current requirements, as evidenced by their re-issuance in the latest published edition. This systematic approach aimed to maintain a high level of safety by ensuring that all relevant safety concerns were addressed through updated and precise directives.

Scope and Application

The Airworthiness Directives 2004, issued under the authority of the Civil Aviation Safety Authority (CASA) and based on subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998, pertain to the maintenance, operation, and airworthiness standards of the Eurocopter AS 332 (Super Puma) Series Helicopters. This legislative instrument applies to any person or entity involved in the operation or maintenance of the specified aircraft models, ensuring compliance with the directives to maintain airworthiness standards. The geographic reach of these directives is national, as they apply throughout Australia. The directives cover a comprehensive range of components and systems, including the main rotor shaft, tail rotor head spindles, and various other critical parts of the helicopter. The legislative instrument revokes the previously issued Airworthiness Directives and re-makes them in the same form as they appear in the latest published edition. This ensures that the directives are up to date with the most current safety standards and requirements. Subordinate instruments may be used to extend or modify the application of these directives, providing flexibility in response to new safety concerns or technological advancements.

Key Provisions

The primary operative sections of the Airworthiness Directives 2004, as made by David Alan Villiers, delegate of the Civil Aviation Safety Authority, are contained within subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998. This legislative instrument involves two main actions: the revocation of specific Airworthiness Directives listed in Schedule 1 and the remaking of each of these directives as separate instruments. This means that certain existing directives related to Eurocopter AS 332 (Super Puma) series helicopters are being repealed and then immediately re-enacted with identical wording to ensure consistency with the latest published editions. The obligations and requirements imposed by this legislation on the parties or entities it governs primarily concern compliance with the re-made Airworthiness Directives. These directives set out specific maintenance, repair, and operational standards that must be adhered to for the helicopters in question. For instance, these directives may specify certain inspections, replacements, or modifications that need to be performed on helicopter components such as the main rotor shaft, tail rotor gearbox, and electrical systems. Operators and owners of these helicopters must ensure that their maintenance and operational practices align with these detailed directives to maintain airworthiness standards. In terms of consequences for non-compliance, breaches of the Airworthiness Directives can lead to both civil and criminal penalties. Civil penalties may include fines and the possibility of grounding the aircraft until the required actions are taken. Under the Civil Aviation Safety Regulations 1998, the maximum penalties for non-compliance can be substantial, with fines potentially reaching up to $21,000 for individuals and significantly higher for corporations, depending on the severity and frequency of the breach. Criminal penalties could also apply, particularly if non-compliance results in a serious risk to safety, potentially leading to imprisonment for those found guilty of violating the directives. The exact penalties depend on the specific circumstances of each case and the discretion of the court.

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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.