Airworthiness Directives 2004 - Revocation and Remaking - Airparts (NZ) Ltd. FU 24 Series Aeroplanes

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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

 Airparts (NZ) Ltd. FU 24 Series Aeroplanes

 AD Name AD Number

 Elevator Control Cables and Pulleys - Inspection AD/FU24/1 Amdt 2

 Structural Component - Corrosion - Inspection AD/FU24/2 Amdt 1

 CANCELLED AD/FU24/3

 Elevator Balance Horn Attachment - Modification - CANCELLED AD/FU24/4

 Elevator Trim Tab Brackets - Modification AD/FU24/5

 Elevator Lower Pulley Station 337 - 340 - Modification - CANCELLED AD/FU24/6

 Wing Spar - Inspection - CANCELLED AD/FU24/7 Amdt 2

 Aileron Rib Assembly - Modification - CANCELLED AD/FU24/8

 Auxiliary Fuel Pump Switch - Modification - CANCELLED AD/FU24/9

 Fuel Sump Corrosion - Inspection AD/FU24/10

 Fin Rib and Skin Cracking - Inspection AD/FU24/11

 Rudder Lowr Rib - Inspection AD/FU24/12

 Fuel Tank Vent System - Modification - CANCELLED AD/FU24/13

 Hopper and Spray Tank Installation - Modification AD/FU24/14

 Main Landing Gear Axle Socket - Inspection AD/FU24/15

 Rudder Top Hinge Rivnuts - Modification - CANCELLED AD/FU24/16

 Aileron Mass Balance Arms - Modification AD/FU24/17

 Fuselage Skin Panels - Inspection - CANCELLED AD/FU24/18

 Engine Mounts and Firewalls AD/FU24/19

 CANCELLED AD/FU24/20

 CANCELLED AD/FU24/21

 CANCELLED AD/FU24/22

 CANCELLED AD/FU24/23

 CANCELLED AD/FU24/24

 CANCELLED AD/FU24/25

 CANCELLED AD/FU24/26

 CANCELLED AD/FU24/27

 CANCELLED AD/FU24/28

 CANCELLED AD/FU24/29


 CANCELLED AD/FU24/30

 Elevator Hinge and Attachment Fittings AD/FU24/31 Amdt 1

 CANCELLED AD/FU24/32

 CANCELLED AD/FU24/33

 CANCELLED AD/FU24/34

 CANCELLED AD/FU24/35

 Fuselage Structure - Modification AD/FU24/36

 Elevator Horn Assembly - Inspection AD/FU24/37

 Main Landing Gear Lower Torque Link - Modification AD/FU24/38

 Cleveland Wheel and Brake Assembly - Inspection AD/FU24/39

 Cockpit Ventilators - Modification AD/FU24/40

 Pilot Restraint Installation - Modification AD/FU24/41

 Installation of No Step Placard AD/FU24/42

 Installation of Crash Axes AD/FU24/43

 Part 1. Wing Spar Modification, and Part 2. Wing Spar Inspection AD/FU24/44

 Fuel Quantity Indication - Modification AD/FU24/45

 Brake Torque Plates - Inspection and Modification AD/FU24/46

 Cockpit Bulkhead - Modification AD/FU24/47

 Tailplane Mass Balance Weight and Control Horn - Inspection and Modification AD/FU24/48

 Centre Wing, Outboard Rear Fitting - Inspection and Modification AD/FU24/49

 Control Column Grip - Inspection AD/FU24/50

 Fin Forward Attachment Fitting AD/FU24/51 Amdt 2

 Fuel Line - Modification AD/FU24/52

 Flap Control Torque Tube - Inspection AD/FU24/53 Amdt 1

 L.H. Rudder Pedal - Inspection AD/FU24/54

 Oil Pressure Gauge Line - Fitment of Restrictor AD/FU24/55

 Engine Controls - Inspection and Modification AD/FU24/56

 Shoulder Harness Inertia Reel Installation Tension Clip P/N 08-16037-3 -  AD/FU24/57

 Wing Structural Fatigue Limitation AD/FU24/58 Amdt 1

 Rudder Torque Tube to Rudder Attachment - Inspection AD/FU24/59

 Engine Control Cables - Life Limitations - CANCELLED AD/FU24/60 Amdt 2

 Main Landing Gear Torque Link Brackets - Inspection/Replacement AD/FU24/61

 Forward Fin Structure AD/FU24/62

 Main Spar Web AD/FU24/63

 

Overview

The Airworthiness Directives 2004 is a legislative instrument enacted by the Civil Aviation Safety Authority (CASA), under subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998. This instrument was introduced to address the need for updating and ensuring the continued safety and airworthiness of specific aircraft models, particularly the FU 24 Series Aeroplanes manufactured by Airparts (NZ) Ltd. The legislative instrument primarily serves to revoke existing airworthiness directives and re-make them with the most current safety requirements, ensuring compliance with the latest safety standards and practices. The enactment of these directives is pivotal in maintaining the integrity and safety of civil aviation operations in Australia, reflecting CASA's commitment to public safety and the highest standards in aviation maintenance and inspection practices.

Scope and Application

The Airworthiness Directives 2004, issued under the authority of the Civil Aviation Safety Regulations 1998, apply to all aircraft registered in Australia, irrespective of the location of the aircraft or the nationality of the operator. These directives specifically target various components and systems of the FU 24 Series Aeroplanes manufactured by Airparts (NZ) Ltd. The directives include both the revocation of previous directives and the re-making of new ones to ensure compliance with the latest safety standards and to address emerging safety concerns. The scope of these directives encompasses inspections, modifications, and other safety measures for components such as elevator control cables, structural parts, and engine controls. While the primary focus is on ensuring the airworthiness of the specified aircraft, certain components or systems may be exempt if they do not form part of the FU 24 Series Aeroplanes or if they are otherwise exempted under the regulations. The application and enforcement of these directives can be extended or restricted through subordinate instruments issued by the Civil Aviation Safety Authority.

Key Provisions

The Airworthiness Directives 2004 legislative instrument, made by David Alan Villiers as the delegate of the Civil Aviation Safety Authority (CASA), primarily focuses on the revocation and remaking of specific Airworthiness Directives (ADs) for the FU 24 Series Aeroplanes manufactured by Airparts (NZ) Ltd. (sections 1(a) and (b)). This legislative instrument revokes certain ADs listed in Schedule 1 and re-makes them as separate instruments, ensuring they are in the same form as the latest published editions. The primary focus is on maintaining the airworthiness of these aircraft by addressing structural, component, and system-related issues. The obligations and requirements imposed by the Act on the parties or entities it governs include compliance with the specified ADs. Operators of FU 24 Series Aeroplanes must adhere to the inspection, modification, and maintenance requirements outlined in the re-made ADs. This includes conducting regular inspections for corrosion, structural integrity, and other specified issues, and making necessary modifications to ensure the aircraft meet the required safety standards. Non-compliance with these ADs can result in significant safety risks, potentially leading to aircraft accidents or other incidents. Breach of the obligations and requirements outlined in the ADs can lead to various civil and criminal consequences. While the specific penalties are not detailed in the text, the enforcement of ADs generally falls under the Civil Aviation Safety Regulations 1998. Offences under these regulations can result in substantial fines and, in severe cases, imprisonment. The penalties can vary depending on the nature and severity of the breach, with the potential for significant financial and legal repercussions for non-compliance. It is essential for operators to strictly adhere to the ADs to avoid these consequences and ensure the continued safety and airworthiness of their aircraft.

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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.