Airworthiness Directives 2004 - Revocation and Remaking - Robinson R22 Series Helicopters

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Legislation au F2006B08002 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

 Robinson R22 Series Helicopters

 AD Name AD Number

 Main Rotor Blade AD/R22/1 Amdt 1

 Tailcone Support Structure - Inspection AD/R22/2

 Tail Rotor Transmission - Inspection AD/R22/3 Amdt 1

 Retirement Lives - Fatigue Critical Components AD/R22/4 Amdt 7

 Main Gearbox Flexible Coupling Yokes - Inspection AD/R22/5 Amdt 2

 A628-1 and -2 Seat Harness Assembly Latch Modification AD/R22/6

 Main Rotor Blades S/Nos. 1 to 91 - Replacement - CANCELLED AD/R22/7

 Control Systems Safety Washers - Installation AD/R22/8

 Main Rotor Blades - Inspection and Retirement - CANCELLED AD/R22/9 Amdt 4

 Tail Rotor Drive Shaft Damper Clips - Replacement AD/R22/10

 Clutch Shaft Plug Installation - Inspection AD/R22/11

 Upper Steel Tube Frames AD/R22/12 Amdt 2

 Tail Rotor Drive Shaft - Replacement AD/R22/13

 Main Rotor Low R.P.M. Warning - Modification - CANCELLED AD/R22/14

 Upper Steel Tube Frames - CANCELLED AD/R22/15

 Lower Actuator Bearing AD/R22/16 Amdt 4

 Clutch Lock Switch - Modification AD/R22/17

 Actuator Drive Screw A506-1 - Replacement AD/R22/18

 Vee Belt Guide - Installation AD/R22/19

 Push Pull Tubes and Guides - Inspection and Modification AD/R22/20

 Sprag Clutch Replacement AD/R22/21 Amdt 2

 Gascolator Fuel Filter - Inspection AD/R22/22

 Main Rotor Gearbox Ring Gear Bolts - Inspection and Modification AD/R22/23

 Lower Actuator Bearing Mounting Brackets AD/R22/24 Amdt 1

 Airframe - Overhaul - CANCELLED AD/R22/25 Amdt 2

 Clutch Actuator Overtravel Limit Switch AD/R22/26

 Vertical Fin Attachments AD/R22/27

 AM-Safe Harness Buckle Assemblies AD/R22/28

 Main Rotor Pitch Link AD/R22/29


 Main Rotor Spindle AD/R22/30 Amdt 5

 Main Rotor Blades AD/R22/31 Amdt 11

 Carburettor Air Box Latches AD/R22/32

 Tail Rotor Pedal Retaining Clip AD/R22/33

 Suspect Bolts AD/R22/34

 Rotor Mast Shaft Nuts AD/R22/35 Amdt 1

 Main Rotor Blades - 2 AD/R22/36

 Forward Flexplate AD/R22/37 Amdt 2

 Tail Rotor Gearbox Output Shaft Key AD/R22/38 Amdt 1

 Upper Clutch Actuator Bearing AD/R22/39

 Placard To Prohibit Pushovers AD/R22/40

 Upper Steel Tube Frames - 2 AD/R22/41 Amdt 1

 Main Rotor Blades AD/R22/42

 Tail Rotor Blades AD/R22/43

 V Belt Upper Sheave AD/R22/44

 Throttle Governor and Low RPM Warning AD/R22/45

 MA-4-5 Carburettor AD/R22/46

 Fuel Tank Vent System AD/R22/47

 Sprag Clutch AD/R22/48

 Main Rotor Drive Shaft Yoke Half Assembly AD/R22/49

 Tail Rotor Pitch Control Assembly AD/R22/50

 Main Rotor Clutch Shaft AD/R22/51 Amdt 1

 

Overview

The Airworthiness Directives 2004 is a legislative instrument introduced to ensure the airworthiness of aircraft and address specific safety concerns related to the Robinson R22 Series Helicopters. Enacted by David Alan Villiers, the delegate of the Civil Aviation Safety Authority (CASA), this instrument revokes existing airworthiness directives and remakes them as separate instruments, maintaining the directives in their latest published form. This legislative action aims to provide clear, updated safety regulations and directives for the specified aircraft models, thereby enhancing aviation safety standards and addressing any identified issues with the Robinson R22 Series Helicopters. The directives focus on various components such as rotor blades, gearboxes, and control systems, ensuring they meet the required safety standards. The Airworthiness Directives 2004 was introduced by the Civil Aviation Safety Authority (CASA) under the authority granted by the Civil Aviation Safety Regulations 1998. This legislative instrument addresses the need for updated and comprehensive safety regulations for the Robinson R22 Series Helicopters. By revoking and remaking the existing directives, CASA aims to ensure that all safety measures are current and effectively communicated, thereby reducing risks associated with aircraft operations. The policy objective is to maintain and improve airworthiness standards, ensuring that all aircraft operate within safe parameters, thereby protecting passengers, crew, and the public.

Scope and Application

The Airworthiness Directives 2004, as re-made by David Alan Villiers, delegate of the Civil Aviation Safety Authority, applies to Robinson R22 Series Helicopters, encompassing various specific components and systems within these helicopters. These directives are designed to ensure the ongoing airworthiness of these aircraft by specifying requirements and standards that must be adhered to for their maintenance, inspection, and modification. The scope of these directives includes the main rotor blades, tailcone support structure, tail rotor transmission, main gearbox, control systems, and numerous other components that are critical to the safe operation of the aircraft. The legislation applies across the Commonwealth of Australia, thereby extending its reach nationally, impacting all operators and entities involved in the maintenance and operation of Robinson R22 Series Helicopters within the country. The instrument provides for the revocation and remaking of previous airworthiness directives, ensuring that current safety standards are uniformly applied and that any outdated or superseded directives are removed to avoid confusion or non-compliance.

Key Provisions

The main operative sections of the Airworthiness Directives 2004 (F2006B08002) involve the revocation and remaking of specific airworthiness directives related to the Robinson R22 Series Helicopters, as detailed in Schedule 1. Section (1) of the legislative instrument revokes existing airworthiness directives while simultaneously remaking each of them as separate instruments. These directives cover a range of components and safety measures, such as inspections, replacements, and modifications to various parts of the helicopter, including the main rotor blade, tailcone support structure, tail rotor transmission, and more. The directives are meticulously outlined in Schedule 1, each with its corresponding AD name, AD number, and specific instructions. The obligations imposed by this Act on the parties or entities it governs are primarily centred around compliance with the newly remade airworthiness directives. Operators and owners of Robinson R22 Series Helicopters are required to adhere to the specified inspections, modifications, and replacements as outlined in the individual airworthiness directives. This includes conducting regular inspections, implementing necessary modifications, and replacing parts as mandated. Non-compliance with these directives can result in the aircraft being deemed unairworthy, thereby affecting its ability to operate legally. Ensuring that these directives are strictly followed is crucial for maintaining the safety and airworthiness of the helicopters. Any breach of the provisions set out in the Airworthiness Directives 2004 could lead to significant consequences. While the legislation does not explicitly state penalties, breaches of airworthiness directives generally carry substantial ramifications under the Civil Aviation Safety Regulations 1998. In the context of civil aviation, failure to comply with airworthiness directives can result in penalties, including fines and potential legal action. In more severe cases, where non-compliance leads to accidents or significant safety hazards, criminal charges may be pursued. The specific penalties would be determined by the relevant authorities and could include substantial fines and imprisonment, depending on the severity of the breach and its impact on aviation safety.

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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.