Airworthiness Directives 2004 - Revocation and Remaking - Agusta A109 Series Helicopters

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Legislation au F2006B07703 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

 Agusta A109 Series Helicopters

 AD Name AD Number

 Main Rotor Blade AD/A109/1 Amdt 3

 Tail Rotor Blade Root Fitting AD/A109/2 Amdt 3

 Passenger and Pilots Door Emergency Release Mechanism AD/A109/3 Amdt 1

 Retirement Lives - Fatigue Critical Components - CANCELLED AD/A109/4 Amdt 3

 MLG Actuator Bracket Assembly Attachment Bolts - CANCELLED AD/A109/5 Amdt 1

 Swashplate Bearing AD/A109/6

 Superflexit Fuel Tanks AD/A109/7

 Tail Rotor Blades AD/A109/8 Amdt 1

 Engine Mount Installation AD/A109/9

 Nose Landing Gear Actuator AD/A109/10

 Emergency Float Assembly P/N 109-0715-01 AD/A109/11

 Main Landing Gear Stiffening Struts AD/A109/12

 Electrical Connectors P/N MS3456W14S-5S AD/A109/13

 Main Landing Gear Wheels AD/A109/14

 Modification of Overhead Console Relay Boards AD/A109/15

 Main Rotor Blades AD/A109/16 Amdt 3

 Main Gearbox Gleason Crown Bolts AD/A109/17 Amdt 1

 Upper Transmission Mount Fitting AD/A109/18 Amdt 3

 Tail Rotor Hub AD/A109/19 Amdt 2

 Main Rotor Hydraulic Actuators AD/A109/20

 Aircruiser Emergency Floats AD/A109/21

 Sliding Doors Emergency Exit Panel AD/A109/22

 Tail Boom and Vertical Fin Modification AD/A109/23

 Main Rotor Blade - Trailing Edge AD/A109/24

 Main Rotor Pitch Change Link Spherical Bearing AD/A109/25 Amdt 1

 Hydraulic System Return Line AD/A109/26

 Tail Rotor Blades P/N 109-8132-01-107 AD/A109/27

 Tail Rotor Blade Grip Assemblies AD/A109/28

 Main Rotor Blades Tip Cap AD/A109/29 Amdt 2


 Gleason Crown Inspection AD/A109/30

 Main Rotor Blade NDI AD/A109/31

 Rescue Hoist AD/A109/32

 Main Rotor Blade Tip Cap - 2 AD/A109/33

 Windshield Wipers AD/A109/34

 Hydraulic Hoses AD/A109/35

 Damper Assembly of Main Rotor Hub AD/A109/36

 Tail Rotor Blades P/N 109-8132-01-111 AD/A109/37

 Tail Rotor Blades AD/A109/38

 Hydraulic Pump AD/A109/39

 Engine Exhaust Ejectors AD/A109/40

 Main rotor rotating scissor assy AD/A109/41

 Passenger Compartment Sliding Door AD/A109/42

 Passenger Compartment Sliding Doors Installation AD/A109/43

 Main Transmission Support Fittings AD/A109/44

 Tail Rotor Hub and Blades Assembly AD/A109/45

 Main Rotor Head Damper Rod-End - CANCELLED AD/A109/46

 Main Rotor Head Damper AD/A109/47

 Rescue Hoist Assembly AD/A109/48

 Battery Bus Circuit Breaker AD/A109/49

 Radio Master Switch Electrical System AD/A109/50

 Transmission Support Fittings Attach Bolts AD/A109/51

 Cargo Hook Installation AD/A109/52

 

Overview

The Airworthiness Directives 2004 is a legislative instrument enacted to address the need for updating and re-making various airworthiness directives concerning the Agusta A109 Series Helicopters. This instrument was introduced to ensure the safety and airworthiness of the specified helicopter models by revoking outdated directives and issuing new ones in their place. The enactment was made by David Alan Villiers, acting as the delegate of the Civil Aviation Safety Authority, under the authority granted by the Civil Aviation Safety Regulations 1998. The policy objective underlying this directive is to maintain and enhance the safety standards for airworthy helicopters, ensuring that all safety-critical components and systems are regularly updated in line with the latest technological and safety advancements. The instrument revokes several existing airworthiness directives and re-makes them to reflect the most current requirements and amendments.

Scope and Application

The Airworthiness Directives 2004, issued under the authority of the Civil Aviation Safety Authority (CASA) and enacted by David Alan Villiers as a delegate, apply specifically to the Agusta A109 series helicopters, impacting both operators and manufacturers within the aviation industry. This legislation is designed to ensure compliance with safety standards, covering a range of technical directives aimed at maintaining the airworthiness of these helicopters. The scope of these directives includes detailed specifications for various components such as the main rotor blades, tail rotor blade root fittings, and emergency release mechanisms, among others. Geographically, these directives apply across the Commonwealth of Australia, ensuring a uniform standard of safety and compliance throughout the nation. The Act also includes provisions for revoking and remaking certain directives as detailed in the attached schedules, ensuring that the latest safety standards are consistently applied. There are no explicit exclusions or exemptions mentioned in the text, implying that all relevant entities and components must comply with the outlined directives.

Key Provisions

The Airworthiness Directives 2004 (F2006B07703) serves to revoke and re-make several airworthiness directives concerning Agusta A109 Series Helicopters. These directives are detailed in Schedule 1, which lists various amendments and specific directives related to components such as the main rotor blades, tail rotor blade root fittings, and emergency release mechanisms. The directives are being re-made to ensure they remain consistent with the latest published editions, thus maintaining updated safety standards for the aircraft in question (Section 1). The Act imposes specific obligations on the entities governed by these directives, primarily those involved in the maintenance, operation, and oversight of Agusta A109 Series Helicopters. Operators and maintenance providers must adhere to the detailed requirements set forth in each directive, ensuring that the aircraft meet the prescribed airworthiness standards. This includes conducting necessary inspections, repairs, and modifications as specified in the directives. Failure to comply with these directives can lead to significant safety risks, thereby impacting the overall airworthiness of the helicopters (Section 2). In terms of consequences for non-compliance, the Act does not explicitly detail offences, penalties, or specific legal consequences within the text. However, the Civil Aviation Safety Regulations 1998, under which this legislative instrument operates, typically include provisions for enforcement actions. Non-compliance with airworthiness directives can result in enforcement actions such as fines, suspension or revocation of airworthiness certificates, and other regulatory measures. The exact penalties would depend on the specific nature and severity of the non-compliance, as outlined in the Civil Aviation Safety Regulations (Section 3).

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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.