Airworthiness Directives 2004 - Revocation and Remaking - Robin Aviation Series Aeroplanes

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Legislation au F2006B08001 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

 Robin Aviation Series Aeroplanes

 AD Name AD Number

 Pilot Safety Harness - Change of Straps AD/ROBIN/1

 Flap Control Mechanism Dented Plate - Inspection AD/ROBIN/2

 Engine Mount - Inspection and Replacement AD/ROBIN/3

 Aileron/Flap Support Brackets - Inspection and Reinforcement AD/ROBIN/4

 Engine Mount AD/ROBIN/5 Amdt 1

 Wing Structural Fatigue Life - CANCELLED AD/ROBIN/6

 Nose Landing Gear Bracket AD/ROBIN/7 Amdt 2

 Wing Assembly AD/ROBIN/8 Amdt 2

 Rudder Bar Assembly Welds AD/ROBIN/9

 Control Column Assembly Welds AD/ROBIN/10 Amdt 1

 Carburettor Inlet Fitting AD/ROBIN/11

 Safety Harness Link AD/ROBIN/12 Amdt 1

 Vertical Stabiliser Spar AD/ROBIN/13

 Fuel Tank Selector Valve AD/ROBIN/14

 Lateral Console Panel AD/ROBIN/15

 Ball and Socket Fitting AD/ROBIN/16

 Safety Harness Link AD/ROBIN/17

 Shoulder Harness Installation AD/ROBIN/18

 Throttle Control AD/ROBIN/19

 Main Gear Torque Link Attachment AD/ROBIN/20

 Stabilator Spar and Attachment Brackets AD/ROBIN/21 Amdt 1

 Carburettor Spacer AD/ROBIN/22

 Anti-Tab Control AD/ROBIN/23

 Empennage Attach Bolts AD/ROBIN/24

 Aileron Mass Balance AD/ROBIN/25

 ATL Rudder Bar AD/ROBIN/26

 HR200/R2000 Rudder Bar AD/ROBIN/27

 Wing Attachment Hardware AD/ROBIN/28 Amdt 1

 Hydraulic Lines AD/ROBIN/29


 Engine Air Intake Inspection AD/ROBIN/30 Amdt 1

 Airspeed Indicator AD/ROBIN/31

 Wing Internal Inspection AD/ROBIN/32

 Control Surface Balance AD/ROBIN/33

 Brake Fluid Reservoir Cap AD/ROBIN/34

 Fuel Shut-off Valve Control AD/ROBIN/35

 Air Intake By-pass Flap AD/ROBIN/36

 Fuel Pressure Indication System AD/ROBIN/37

 Oil Hoses AD/ROBIN/38

 

Overview

The Airworthiness Directives 2004, issued under the authority of the Civil Aviation Safety Regulations 1998, were enacted by David Alan Villiers, as the delegate of the Civil Aviation Safety Authority. This legislative instrument was introduced to ensure that specific airworthiness directives concerning the Robin Aviation Series Aeroplanes are revoked and re-made to reflect the most current safety requirements. Each directive in the Schedule has been re-made in the same form as it appears in the latest published edition. The primary objective of this legislative action is to maintain the safety standards of civil aviation by ensuring that all airworthiness directives are up-to-date and accurately reflect the latest safety requirements and recommendations. This systematic approach helps to uphold the integrity and safety of the aviation industry in Australia.

Scope and Application

The Airworthiness Directives 2004, made under the authority of David Alan Villiers as the delegate of the Civil Aviation Safety Authority (CASA) and pursuant to subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998, pertains specifically to Robin Aviation Series Aeroplanes. This legislative instrument revokes and re-makes various airworthiness directives that address specific safety and maintenance requirements for these aircraft. The directives cover a wide range of technical aspects, including the inspection, reinforcement, and replacement of structural components, as well as safety measures for pilot equipment and engine systems. These directives are intended to ensure that the aircraft meet the necessary safety standards to be airworthy. The scope of application of these directives is limited to the aircraft types specified, and they are designed to be enforceable under the Civil Aviation Safety Regulations 1998. The legislative instrument does not explicitly state any exclusions, exemptions, or thresholds, but it is understood that compliance is mandatory for all relevant aircraft operators within Australia's jurisdiction.

Key Provisions

The legislative instrument (F2006B08001) outlines the revocation and remaking of several Airworthiness Directives (ADs) for Robin Aviation series aeroplanes. Specifically, the Airworthiness Directives mentioned in Schedule 1 are revoked, and new versions of these directives are created as separate instruments. The new directives are made in the exact form as they appear in the latest published edition. The operative sections include the revocation of existing directives and the creation of new ones, each identified by an AD name and number, such as AD/ROBIN/1 for Pilot Safety Harness - Change of Straps, and AD/ROBIN/2 for Flap Control Mechanism Dented Plate - Inspection. The obligations and requirements imposed by this legislation primarily pertain to aircraft manufacturers, operators, and maintenance providers. These parties are required to adhere to the newly remade Airworthiness Directives, ensuring that their aeroplanes comply with the specified safety and maintenance standards. For instance, AD/ROBIN/1 requires the change of straps for pilot safety harnesses, while AD/ROBIN/2 mandates inspections for dented plates in flap control mechanisms. Compliance with these directives is essential to maintaining the airworthiness of the aircraft and ensuring the safety of passengers and crew. The Airworthiness Directives themselves outline specific safety and maintenance requirements that must be met. For example, AD/ROBIN/3, which pertains to Engine Mount - Inspection and Replacement, requires that the engine mounts be inspected and replaced if necessary to prevent structural failure. Similarly, AD/ROBIN/4, concerning Aileron/Flap Support Brackets - Inspection and Reinforcement, requires thorough inspections and reinforcement of these components to prevent failure during flight. Failure to comply with these directives can lead to serious safety issues and potential grounding of the aircraft. In terms of consequences for non-compliance, breaches of the Airworthiness Directives can result in both civil and criminal penalties. Civil penalties may include fines and orders to rectify non-compliance, while criminal penalties may include imprisonment for individuals found guilty of willfully violating safety regulations. The exact penalties depend on the severity of the breach and the specific provisions of the Civil Aviation Safety Regulations 1998. Additionally, non-compliance can result in the suspension or revocation of an aircraft's certificate of airworthiness, which can have significant operational and financial implications for operators.

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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.