Airworthiness Directives 2004 - Revocation and Remaking - Bell Helicopter Textron 412 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

 Bell Helicopter Textron 412 Series Helicopters

 AD Name AD Number

 Engine Mount Fireshield - Installation AD/BELL 412/1

 Retirement Lives - Fatigue Critical Components AD/BELL 412/2 Amdt 1

 Main Rotor Yoke - Inspection - CANCELLED AD/BELL 412/3

 Main Rotor Yoke - Inspection, Retirement and Modification AD/BELL 412/4 Amdt 1

 Engine Fuel Switch - Inspection/Replacement AD/BELL 412/5 Amdt 1

 Main Rotor Pitch Link Assemblies - Replacement AD/BELL 412/6

 Airspeed and Ground Operation Restriction AD/BELL 412/7 Amdt 1

 Installation of Main Rotor Droop Restraint Kit and Cyclic Stick Centring  AD/BELL 412/8

 Main Rotor Blade Pitch Horns - Inspection AD/BELL 412/9 Amdt 1

 Upper Anti-Collision Strobe Light P/No HR, DF-28DRMS Inspection,  AD/BELL 412/10

 Main Rotor Yoke, P/N 412-010-101-123 - Inspection AD/BELL 412/11

 Vertical Fin Forward Spar AD/BELL 412/12 Amdt 5

 Tail Rotor Trunnion Bearing Housing AD/BELL 412/13

 Emergency Flotation System and Squib Valve AD/BELL 412/14 Amdt 1

 Battery Cable Installation AD/BELL 412/15

 Vertical Fin Spar Cap - CANCELLED AD/BELL 412/16

 AM-SAFE Harness Buckle Assemblies AD/BELL 412/17

 Engine Fuel Valve Electrical Connectors P/No MS3456W14S-5S AD/BELL 412/18

 Emergency DC Bus Number One Feeder Circuit AD/BELL 412/19

 Bolts P/N AN4-5A - Pylon Support AD/BELL 412/20

 Fuel Cell Interconnect Tube AD/BELL 412/21

 Main Transmission Spiral Bevel Gear AD/BELL 412/22

 Electrical Wiring Harnesses AD/BELL 412/23

 Main Rotor Pitch Link to Pitch Horn Bolt AD/BELL 412/24

 Main Rotor Flight Control System Bolts AD/BELL 412/25

 Bogus Pressure Gauge Emergency Floats P/N 212-073-905-1 AD/BELL 412/26

 Tailboom Upper Longeron AD/BELL 412/27

 Lower Planetary Spider Gear - CANCELLED AD/BELL 412/28

 Tail Rotor Driveshaft Hangar Bearings AD/BELL 412/29


 Swashplate Support Assembly AD/BELL 412/30

 Fin to Tail Boom Junction AD/BELL 412/31

 Main Driveshaft and Tail Rotor Drive Over-Temperature Indicators AD/BELL 412/32

 Main Transmission Lower Planetary Spider AD/BELL 412/33

 Swashplate Support AD/BELL 412/34

 Tail Boom Doubler and Fin Spar Caps AD/BELL 412/35

 Main Rotor Mast AD/BELL 412/36

 Internal Hoist AD/BELL 412/37

 Hydraulic Servo Actuator Shoulder Bolt AD/BELL 412/38

 Tail Rotor Yoke and Tail Rotor Flapping Stop/Indicator AD/BELL 412/39 Amdt 1

 Main Rotor Yoke AD/BELL 412/40

 Tailboom Attachment Cap Angle AD/BELL 412/41

 Main Hydraulic Servo Actuator Rod End Lock Washer AD/BELL 412/42

 Tail Rotor Counterweight Bellcrank Retention Nut AD/BELL 412/43

 Tail Rotor Blade Fwd Tip Weight Retention Block and Aft Tip Closure AD/BELL 412/44

 

Overview

The Airworthiness Directives 2004 are a legislative instrument enacted to ensure the continued safety and airworthiness of aircraft, specifically Bell Helicopter Textron 412 Series Helicopters, in Australian airspace. This instrument was introduced to address issues related to the maintenance and inspection of various components of these helicopters, ensuring that any identified safety concerns are promptly and effectively managed. Enacted by David Alan Villiers, the delegate of the Civil Aviation Safety Authority under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998, the primary policy objective of this legislative instrument is to safeguard the integrity and safety of air travel by enforcing strict compliance with airworthiness standards. Each Airworthiness Directive is meticulously re-made to match the latest published editions, ensuring that operators are kept abreast of the most current safety requirements.

Scope and Application

The Airworthiness Directives 2004, issued under the authority of the Civil Aviation Safety Regulations 1998, applies to all persons and entities involved in the operation, maintenance, and airworthiness certification of Bell Helicopter Textron 412 Series Helicopters within Australia. This legislative instrument revokes and remakes various Airworthiness Directives concerning specific components and systems of these helicopters, including engine mount fireshields, fatigue critical components, rotor yoke inspections, and electrical system modifications, among others. The directives ensure that these helicopters meet the required safety standards and are airworthy, impacting all aviation operators, maintenance personnel, and aircraft engineers involved with these aircraft. The legislation operates nationally, covering the entire Commonwealth of Australia, and there are no specific exclusions or exemptions mentioned in this particular legislative instrument. The Civil Aviation Safety Authority, through subordinate instruments, may further extend or restrict the application of these directives.

Key Provisions

The Airworthiness Directives 2004, under section 1, revokes several previously issued Airworthiness Directives concerning Bell Helicopter Textron 412 Series Helicopters and re-makes them as separate instruments. Each re-made directive is identical to the latest published edition, as noted in the instrument's note. These directives, detailed in Schedule 1, cover a range of safety concerns, including engine mount fireshield installation, fatigue critical components, and inspections or modifications of various helicopter parts such as the main rotor yoke, pitch link assemblies, and tail rotor trunnion bearing housing. Under the Civil Aviation Safety Regulations 1998, these Airworthiness Directives impose specific obligations on helicopter operators and maintenance providers to ensure that all safety requirements and directives are adhered to. This includes conducting regular inspections, making necessary modifications or retirements, and maintaining proper records of all compliance actions. Operators must ensure that their aircraft meet the specified safety standards before each flight, which involves thorough checks and timely updates to their maintenance schedules. Failure to comply with these Airworthiness Directives can result in severe consequences. Under the Civil Aviation Act 1988, non-compliance may lead to enforcement actions by the Civil Aviation Safety Authority (CASA). Offences can attract penalties including fines and, in serious cases, criminal charges. The exact penalties depend on the nature and severity of the non-compliance but can include substantial fines for corporations and potential imprisonment for individuals responsible for the oversight of the non-compliant operations. It is essential for operators and maintenance personnel to meticulously follow these directives to avoid legal repercussions.

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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.