Airworthiness Directives 2004 - Revocation and Remaking - Bell Helicopter Textron 205 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 205 Series Helicopters

 AD Name AD Number

 Airworthiness Limitations AD/BELL 205/1 Amdt 32

 Tail Rotor Yoke - Inspection AD/BELL 205/2

 Main Rotor Blade - Modification AD/BELL 205/3

 Superseded by AD/BELL 205/1W - CANCELLED AD/BELL 205/4

 Superseded by AD/BELL 205/1W - CANCELLED AD/BELL 205/5

 Cyclic Control Supports - Inspection AD/BELL 205/6

 Tail Rotor Blade Grip - Inspection AD/BELL 205/7

 Superseded by AD/BELL 205/46 - CANCELLED AD/BELL 205/8

 Servo Cylinder Upper Control Tube Fittings AD/BELL 205/9

 205A/A1 Tail Boom Vertical Fin Forward - Inspection and Modification AD/BELL 205/10

 Superseded by DCA/BELL 205/1 Amdt4 - CANCELLED AD/BELL 205/11 Amdt 1

 Superseded by AD/BELL 205/46 - CANCELLED AD/BELL 205/12 Amdt 2

 Float Installation - Inspection and Modification AD/BELL 205/13 Amdt 1

 Superseded by DCA/BELL 205/25 Amdt1 - CANCELLED AD/BELL 205/14

 Tail Rotor Hub Assembly - Inspection AD/BELL 205/15

 Fire Detection System - Audible Warning AD/BELL 205/16

 Hydraulic Fluid Temperature Indicators - Installation AD/BELL 205/17

 CANCELLED AD/BELL 205/18 Amdt 1

 Transmission Support Case - Inspection AD/BELL 205/19 Amdt 1

 CANCELLED AD/BELL 205/20 Amdt 2

 Swashplate Scissors Lever Bolts - Inspection AD/BELL 205/21

 Transmission Oil System - Inspection AD/BELL 205/22

 Main Rotor Blades AD/BELL 205/23 Amdt 4

 CANCELLED AD/BELL 205/24

 CANCELLED AD/BELL 205/25 Amdt 3

 Fire Extinguisher Cartridges - Inspection AD/BELL 205/26

 CANCELLED AD/BELL 205/27

 Main Rotor Blade - Removal From Service AD/BELL 205/28

 Main Rotor Blade Bolt Washer - Inspection AD/BELL 205/29


 Stabilizer Bar Outer Tube - Inspection - CANCELLED AD/BELL 205/30

 Tail Boom Attachment Fitting and Longerons - Inspection AD/BELL 205/31 Amdt 1

 Main Beam Cap - Inspection and Repair AD/BELL 205/32

 Synchronised Elevator - Inspection, Modification and Retirement AD/BELL 205/33

 Emergency Exits - Modification and Inspection AD/BELL 205/34 Amdt 2

 Swashplate Support Assembly - Retirement Life AD/BELL 205/35 Amdt 1

 Fuel Boost Pumps - Inspection AD/BELL 205/36

 Main Rotor Hub Fitting Assemblies - Inspection AD/BELL 205/37

 CANCELLED AD/BELL 205/38

 CANCELLED AD/BELL 205/39

 Tail Rotor Pitch Horns - Inspection AD/BELL 205/40

 External Cargo Suspension Kit - Load Restriction and Modification AD/BELL 205/41 Amdt 1

 Main Rotor Hub Inboard Fitting - Life Reduction AD/BELL 205/42

 Engine Air Inlet Screen - Inspection AD/BELL 205/43

 Cyclic Control Cylinder Assembly - Inspection of Piston Rods AD/BELL 205/44

 Main Rotor Yoke AD/BELL 205/45 Amdt 4

 Anti-Torque Control System - Modification to Pushrod Status AD/BELL 205/46

 Hydraulic Servo Cylinder Assembly - Spanner Link Assembly Inspection and  AD/BELL 205/47

 Fuselage Main Beams Splice - Modification AD/BELL 205/48

 Elevator to Horn Assembly Attachment - Modification AD/BELL 205/49

 Main Rotor Grip/Blade Bolt - Inspection and Rework AD/BELL 205/50

 Vertical Fin Spar Cap AD/BELL 205/51 Amdt 1

 Tail Rotor Trunnion Bearing Housing AD/BELL 205/52

 Main Rotor Pillow Block AD/BELL 205/53

 Main Transmission Spiral Bevel Gear AD/BELL 205/54

 Pitch Change Link Universal AD/BELL 205/55

 Tail Rotor Hub P/N 204-011-801-121 AD/BELL 205/56

 Bogus Tension Torsion Straps AD/BELL 205/57

 Time Expired Tail Rotor Yoke AD/BELL 205/58

 Swashplate Outer Ring AD/BELL 205/59

 Tail Rotor Driveshaft Hangar Bearings AD/BELL 205/60

 Main Transmission Lower Planetary Spider AD/BELL 205/61

 42 Degree Tail Rotor Drive Gearbox AD/BELL 205/62

 Tail Rotor Yoke AD/BELL 205/63

 This AD yet to be issued AD/BELL 205/64

 Vertical Fin Spar Cap AD/BELL 205/65


 Main Rotor - Pillow Block Attachment Bolts AD/BELL 205/66

 Main Hydraulic Servo Actuator Rod End Lock Washer AD/BELL 205/67

 Tail Rotor Counterweight Bellcrank  Retention Nut AD/BELL 205/68

 Tail Rotor Grip AD/BELL 205/69

 Tail Rotor Blade Fwd Tip Weight Retention Block and Aft Tip Closure AD/BELL 205/70

 Main Rotor Tension-Torsion Strap AD/BELL 205/71

 Main Rotor Grip AD/BELL 205/72

 

Overview

The Airworthiness Directives 2004 were enacted to ensure the safety of air travel by updating and maintaining the airworthiness standards for specific aircraft, in this case, Bell Helicopter Textron 205 Series Helicopters. This legislative instrument was enacted by David Alan Villiers, a delegate of the Civil Aviation Safety Authority, under the authority of subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998. The primary purpose of these directives is to address the need for updated safety standards and operational procedures in response to emerging safety concerns or technological advancements. By revoking the previous directives and remaking them with the latest standards, the Civil Aviation Safety Authority aims to ensure that all relevant parties are aware of and comply with the most current safety requirements, thus enhancing the overall safety of air travel in Australia. The policy objective behind these Airworthiness Directives is to maintain and improve the airworthiness of aircraft, specifically the Bell Helicopter Textron 205 Series Helicopters, by ensuring that all safety-related modifications, inspections, and operational procedures are up-to-date and strictly followed. This approach helps to mitigate potential risks and ensures that the aircraft remain in a safe and operationally sound condition, thereby protecting passengers, crew, and the general public. The re-making of these directives under the Civil Aviation Safety Regulations 1998 ensures that they align with the overarching regulatory framework designed to safeguard the aviation industry.

Scope and Application

The Airworthiness Directives 2004, issued by David Alan Villiers, the delegate of the Civil Aviation Safety Authority under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998, pertain to the revocation and re-making of specific Airworthiness Directives for Bell Helicopter Textron 205 Series Helicopters. These directives apply to the entities and individuals involved in the operation and maintenance of these helicopters, ensuring that they adhere to the latest safety standards and specifications outlined in the Civil Aviation Safety Regulations 1998. The geographic and jurisdictional reach of these directives is national, as they are administered by the Civil Aviation Safety Authority, an agency of the Commonwealth of Australia. The legislative instrument includes detailed schedules that outline the specific Airworthiness Directives being revoked and remade, each tailored to address various aspects of the helicopters’ airworthiness, such as inspections and modifications to critical components like the tail rotor yoke, main rotor blade, and other structural elements. The legislation does not explicitly state any exclusions, exemptions, or thresholds; however, it does note that each Airworthiness Directive is remade in the same form as appears in the latest published edition, suggesting a comprehensive update and application of safety standards. The directives are enforceable across all states and territories within Australia, ensuring uniformity in aviation safety practices.

Key Provisions

The Airworthiness Directives 2004, under the Civil Aviation Safety Regulations 1998, primarily involve the revocation and remaking of certain Airworthiness Directives for Bell Helicopter Textron 205 Series Helicopters (sections 1 and 2). These directives pertain to various aspects of the helicopters' airworthiness, including inspections, modifications, and other specific requirements that ensure the safe operation of these aircraft. Each directive is re-made in exactly the same form as appears in the latest published edition, thereby ensuring consistency and clarity in the operational standards that must be adhered to (section 1(b)). The obligations imposed by these directives on the parties or entities governed include conducting regular inspections, making necessary modifications, and ensuring compliance with the specific requirements set out in each directive. For example, AD/BELL 205/1 requires an inspection of the tail rotor yoke, while AD/BELL 205/2 mandates a modification to the main rotor blade. These obligations are critical for maintaining the airworthiness of the aircraft and ensuring the safety of all persons on board and on the ground (sections 1 and Schedule 1). Failure to comply with the requirements set out in these Airworthiness Directives can result in significant consequences. While the specific penalties are not detailed in the legislative instrument, non-compliance generally falls under the purview of the Civil Aviation Safety Regulations 1998, which include both civil and criminal penalties. Civil penalties can include fines, while criminal penalties can include imprisonment, reflecting the serious nature of non-compliance with aviation safety regulations. The exact penalties would depend on the specific breach and the circumstances surrounding it, but the overarching aim is to ensure strict adherence to the safety standards mandated by these directives (section 3).

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