Airworthiness Directives 2004 - Revocation and Remaking - Bell Helicopter Textron Canada (BHTC) 222 Series Helicopters

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B07763 In force Legislative Instrument

Legislation content

 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

 Bell Helicopter Textron Canada (BHTC) 222 Series Helicopters

 AD Name AD Number

 Retirement Lives - Fatigue Critical Components AD/BELL 222/1

 Quick Disconnect Dual Controls AD/BELL 222/2 Amdt 1

 Tail Boom - Inspection and Modification AD/BELL 222/3

 Tail Rotor Servo Control Linkage AD/BELL 222/4

 Ng Operating Speed Restrictions AD/BELL 222/5

 Directional Hydraulic Actuator P/N 222-382-002-101 AD/BELL 222/6 Amdt 1

 Fin Assembly Attachment AD/BELL 222/7

 Emergency Flotation System and Squib Valve AD/BELL 222/8 Amdt 1

 Engine Chip Detector Lights AD/BELL 222/9

 Flapping Bearing AD/BELL 222/10 Amdt 1

 Swashplate Pins AD/BELL 222/11

 Swashplate Drive Link AD/BELL 222/12

 Main Rotor Yoke - CANCELLED AD/BELL 222/13

 Horizontal Stabiliser Assembly AD/BELL 222/14

 Main Rotor Yoke AD/BELL 222/15

 Tail Rotor Boost Cylinder Support Bracket AD/BELL 222/16

 Drive Train Overheat Temperature Indicators AD/BELL 222/17

 Tail Rotor Blades AD/BELL 222/18 Amdt 3

 Retrofit of Engine Overspeed Controller AD/BELL 222/19

 Main Rotor Grip and Flapping Bearing Assembly AD/BELL 222/20

 Vertical Fin Attachment Bolt AD/BELL 222/21

 Flapping Bearing-to-Yoke Attachment Bolts AD/BELL 222/22

 Swashplate Rotating Ring Drive Pins - Torque Test AD/BELL 222/23

 Main Rotor Hydraulic Actuator Support AD/BELL 222/24

 Main Rotor Pendulum Weight Support AD/BELL 222/25

 Main Rotor Grips and Pitch Horns AD/BELL 222/26

 Memcor Truohm Magnetic Brake AD/BELL 222/27

 

Overview

The Airworthiness Directives 2004 is a legislative instrument enacted to address issues related to the airworthiness of Bell Helicopter Textron Canada (BHTC) 222 Series Helicopters. This legislative instrument was introduced by David Alan Villiers, acting as a delegate of the Civil Aviation Safety Authority under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998. The primary objective of this instrument was to revoke certain Airworthiness Directives and simultaneously re-make them to ensure that they remain up-to-date and effective. Each Airworthiness Directive has been remade in exactly the same form as appears in the latest published edition of the Directive. The instrument covers a range of areas including inspection, modification, and operational restrictions to ensure the continued safety of these helicopters.

Scope and Application

The Airworthiness Directives 2004 legislative instrument, promulgated by David Alan Villiers, the delegate of the Civil Aviation Safety Authority, pertains to the revocation and remaking of specific Airworthiness Directives concerning Bell Helicopter Textron Canada (BHTC) 222 Series Helicopters. This instrument operates under the authority granted by subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998, and it applies to all aircraft of the specified series that are registered in Australia and operated within Australian airspace. The instrument specifically addresses various maintenance and operational requirements to ensure the airworthiness of the helicopters, encompassing aspects such as fatigue-critical components, inspection, modification, and operational speed restrictions. The scope of this legislation is national, ensuring compliance with safety standards across all relevant operators within the Commonwealth of Australia. Notably, the instrument does not specify exclusions, exemptions, or thresholds, thereby applying uniformly to all pertinent aircraft and operators. The Airworthiness Directives themselves are remade in their entirety as they appear in the latest published editions, ensuring that the regulations remain current and comprehensive.

Key Provisions

The primary operative sections of this legislative instrument involve the revocation and remaking of several Airworthiness Directives (ADs) concerning Bell Helicopter Textron Canada (BHTC) 222 Series Helicopters (Schedule 1). These ADs, which detail specific safety measures and modifications for various helicopter components, are listed in the Schedule and are re-made as separate instruments attached to the legislation. Each AD is being re-made in exactly the same form as it appears in the latest published edition, ensuring that the latest safety standards and requirements are officially recognised and enforced. The obligations imposed by these ADs on the parties governed by them primarily revolve around ensuring the airworthiness of the helicopters in question. This includes adhering to the specified modifications, inspections, and maintenance schedules for the various components mentioned in the ADs. For instance, AD/BELL 222/3 mandates inspection and modification of the tail boom, while AD/BELL 222/4 sets operating speed restrictions for the engine (Ng). These obligations are essential to maintain the safety and operational integrity of the helicopters. Failure to comply with these Airworthiness Directives can result in serious consequences. While the specific offences and penalties are not detailed in the provided text, it is generally understood that non-compliance with airworthiness directives can lead to significant civil and criminal penalties. Civil penalties may include fines and the potential grounding of non-compliant aircraft. In more severe cases, criminal penalties could be imposed, including imprisonment, particularly if non-compliance results in accidents or endangers public safety. The exact penalties would depend on the specific nature and severity of the breach, as well as applicable aviation laws and regulations.

Legal classification tags

Area of Law
Civil Aviation Law
Instrument
Legislative Instrument
Concepts
Definitions & Interpretation
Repeal & Amendment
Regulatory Standards

Interactions

Authorises

All Versions

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.