Airworthiness Directives 2004 - Revocation and Remaking - Fokker F100 (F28 Mk 100) Series Aeroplanes

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

Legislation au F2006B07869 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

 Fokker F100 (F28 Mk 100) Series Aeroplanes

 AD Name AD Number

 Flight Controls - Horizontal Stabiliser Dual Actuator - Periodic Inspection AD/F100/1

 Main Landing Gear Downlock - Inspection/Replacement AD/F100/2

 Engine Cowling - Inspection/Modification/Repair AD/F100/3

 Thrust Reverser Door Bumper Fittings AD/F100/4

 Powerplant - Lower Cowl Door Engagement AD/F100/5

 Rib/Auxiliary Spar Attachment Rivets AD/F100/6

 Vertical Stabiliser AD/F100/7

 RH Wing Skin at Fuel Adaptor Position AD/F100/8

 Forward Partial Pressure Bulkhead AD/F100/9

 Engine Mount Shear Shelf Web AD/F100/10

 Rear Spar & MLG Bottom Joint Fittings AD/F100/11

 Main Wheel Assembly AD/F100/12

 Rear Spar-to-Fuselage Attachment AD/F100/13

 Small Cargo Door Hinge Assembly AD/F100/14

 Centre Section Frame Strips AD/F100/15

 Elevator BCU Backlash Remover Mechanism AD/F100/16

 Vertical Stabiliser Torsion Box AD/F100/17

 MLG Sliding Member Wheel Axle AD/F100/18

 Horizontal Stabiliser Structure AD/F100/19 Amdt 1

 Cleats at Wing Rib STA.8200 AD/F100/20

 Reverse Thrust Control Maximum Detent AD/F100/21

 Passenger Service Units AD/F100/22

 Cargo Door Frame AD/F100/23

 Stubwing Upper Skin AD/F100/24

 Small Cargo Door Hinge Assembly - 2 AD/F100/25

 MLG Main Fitting Sub-Assembly AD/F100/26

 MLG Torque Link Connections AD/F100/27

 MLG Apex Joint and Shimmy Damper Attachment AD/F100/28

 Cabin Decompression Panels AD/F100/29


 Flight Warning Computer Replacement AD/F100/30

 Flight Augmentation Computer Replacement AD/F100/31

 Thrust Reverser Electrical Control Modification AD/F100/32

 Wheel-Speed Sensor Wiring AD/F100/33

 Nose Landing Gear Main Fitting AD/F100/34 Amdt 2

 Elevator Tension Regulator Assembly AD/F100/35

 Fire Extinguisher Electrical Connectors AD/F100/36

 Stabiliser Electrical Bonding AD/F100/37

 Anti-Skid System Control Box - CANCELLED AD/F100/38

 Flight Crew Seat Shoulder Harness AD/F100/39

 Aircraft Flight Manual - Liftdumper Limitations AD/F100/40

 Main Landing Gear Torque Link Dampers AD/F100/41

 Landing Gear Locking Mechanism AD/F100/42

 Anti Skid Control Box AD/F100/43

 No. 1 Pitot Tube AC Sensing Circuit AD/F100/44

 Cargo Compartment Marking AD/F100/45

 Replaceable Frame Strut Attachment Bolts AD/F100/46

 Thrust Reverser Operating Lever AD/F100/47

 Main Landing Gear Main Fitting AD/F100/48 Amdt 4

 Elevator Tension Regulator AD/F100/49

 Engine - Reverse Thrust Operations Limitations AD/F100/50 Amdt 2

 Vertical Stabiliser Torsion Box - 2 AD/F100/51

 Passenger Door Status Lights AD/F100/52 Amdt 2

 Main Landing Gear Sliding Member AD/F100/53 Amdt 1

 Time Limits/Maintenance Checks - Maintenance Requirements AD/F100/54

 Main Landing Gear Main Fitting - 2 AD/F100/55

 Pedestal Side Cover Attachment AD/F100/56

 Low Pressure Fuel Line - Inspection - CANCELLED AD/F100/57

 Engine- Operating Limits and Warnings AD/F100/58

 Flight Manual Amendment - Operation in Icing Conditions AD/F100/59 Amdt 2

 Grimes Aerospace Passenger Service Unit AD/F100/60

 Aileron Tab Drive Rod Assembly AD/F100/61

 Cargo Restraint Strap Assemblies AD/F100/62

 

Overview

The Airworthiness Directives 2004 was enacted to streamline and update the existing airworthiness directives for specific aircraft types. This legislative instrument was issued by David Alan Villiers, 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 legislative instrument was to revoke the existing airworthiness directives listed in Schedule 1 and re-make them as separate instruments. This was done to ensure that the latest published editions of these directives are in effect, thereby enhancing the safety and airworthiness of the Fokker F100 (F28 Mk 100) series aeroplanes. The enactment of this instrument by the Civil Aviation Safety Authority aimed to address any discrepancies or outdated information within the previous directives, thereby maintaining high safety standards in the aviation industry. Each airworthiness directive mentioned in Schedule 1 and attached to the legislative instrument has been re-made in exactly the same form as it appears in the latest published edition. This ensures that all stakeholders, including aircraft operators and maintenance personnel, have access to the most current and accurate information regarding the airworthiness of the Fokker F100 (F28 Mk 100) series aeroplanes. By revoking and re-making these directives, the Civil Aviation Safety Authority aimed to uphold stringent safety measures and regulatory compliance within the aviation sector.

Scope and Application

The Airworthiness Directives 2004, issued under the authority of the Civil Aviation Safety Authority (CASA) and pursuant to subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998, applies to Fokker F100 (F28 Mk 100) series aeroplanes. The legislation mandates the revocation and remaking of specific Airworthiness Directives outlined in Schedule 1, ensuring that each directive is re-made in exactly the same form as appears in the latest published edition of the Directive. These directives encompass a range of safety-related issues, including periodic inspections, modifications, and repairs of various aircraft components such as the horizontal stabiliser, main landing gear, engine cowlings, thrust reverser door bumper fittings, and other structural and operational elements. The directives apply nationally across Australia and are critical for maintaining the airworthiness of Fokker F100 series aeroplanes. The scope of the legislation extends to mandating specific maintenance and operational procedures, ensuring compliance with safety standards, and addressing any identified safety deficiencies in the aircraft models specified. The directives are enforced through CASA's regulatory framework, which includes the ability to extend or restrict their application through subordinate instruments as necessary.

Key Provisions

The Airworthiness Directives 2004, as enacted by David Alan Villiers, delegate of the Civil Aviation Safety Authority, primarily involves the revocation and remaking of specific airworthiness directives concerning Fokker F100 (F28 Mk 100) series aeroplanes (s.1). The primary sections of this legislative instrument focus on the revocation of existing directives listed in Schedule 1 and the remaking of these directives as separate instruments, ensuring they are consistent with the latest published editions (s.1(a) and (b)). These directives impose detailed obligations on the operators and maintainers of Fokker F100 aircraft. They mandate regular inspections and modifications of various aircraft components, including the horizontal stabiliser, main landing gear, engine cowlings, thrust reverser door bumper fittings, and numerous other parts (Schedule 1). Compliance with these directives is crucial to ensure that the aircraft maintain their airworthiness and meet safety standards set by the Civil Aviation Safety Authority. Failure to comply with these airworthiness directives can result in severe consequences. While the specific penalties are not detailed within this legislative instrument, non-compliance generally attracts civil or criminal penalties under the Civil Aviation Safety Regulations 1998. The potential penalties can include substantial fines and, in more severe cases, imprisonment. These measures are in place to enforce adherence to safety standards and to protect the public from potential aviation hazards.

Legal classification tags

Area of Law
Administrative Law
Instrument
Legislative Instrument
Concepts
Definitions & Interpretation
Regulatory Standards
Enforcement Powers

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.