Airworthiness Directives 2004 - Revocation and Remaking - Cessna 207 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

 Cessna 207 Series Aeroplanes

 AD Name AD Number

 Control Systems AD/CESSNA 207/1

 Flap Actuator - CANCELLED AD/CESSNA 207/2

 Auxiliary Fuel Pump Electrical System AD/CESSNA 207/3

 Exhaust Manifold Heat Exchanger AD/CESSNA 207/4

 Front Seat Restraint Installations AD/CESSNA 207/5

 Alternator Earth Lead AD/CESSNA 207/6

 Aft Tailcone Assembly AD/CESSNA 207/7 Amdt 2

 Right Hand Wing Rear Spar AD/CESSNA 207/8

 Nose Landing Gear - CANCELLED AD/CESSNA 207/9

 Fuel Quantity Placard AD/CESSNA 207/10

 Rudder Trim Chain AD/CESSNA 207/11

 Wing Flap Actuator Ball Nut Assemblies AD/CESSNA 207/12

 Turbocharger Thrust Bearing Pin and Centre Housing Assembly AD/CESSNA 207/13 Amdt

 Fuel Selector Valve - CANCELLED AD/CESSNA 207/14

 Fuel Reservoir Fitting AD/CESSNA 207/15

 Goodyear Fuel Cells AD/CESSNA 207/16

 Fuel Vent Tube AD/CESSNA 207/17

 Ammeter Type and Position AD/CESSNA 207/18

 Vented Fuel Caps AD/CESSNA 207/19 Amdt

 Fuel Flow Stabilisation Placard AD/CESSNA 207/20

 Alternator Ground Strap AD/CESSNA 207/21 Amdt

 Flying Control System Turnbuckles AD/CESSNA 207/22

 Turbocharger AD/CESSNA 207/23

 Fuel Cap Alignment Placard AD/CESSNA 207/24

 Wing Tip Navigation/Strobe Lights AD/CESSNA 207/25

 Bladder Type Fuel Cells AD/CESSNA 207/26 Amdt

 Fuel Filler Caps and Adaptors AD/CESSNA 207/27 Amdt

 Fuel Selector Valve Safety Wire AD/CESSNA 207/28

 Rear Wing Spar Doubler AD/CESSNA 207/29


 Fuel System Water Drainage Placard AD/CESSNA 207/30

 Seat Adjustment Mechanism AD/CESSNA 207/31 Amdt

 Forward Door Post Bulkhead AD/CESSNA 207/32 Amdt

 Fuel Strainer AD/CESSNA 207/33

 Horizontal Stabilizer Front Spar AD/CESSNA 207/34 Amdt

 Horizontal Stabiliser Attachment  Brackets AD/CESSNA 207/35

 Brackett Engine Air Filters AD/CESSNA 207/36 Amdt

 Cigar Lighter Wiring AD/CESSNA 207/37

 Upper Shoulder Harness Adjuster Spring AD/CESSNA 207/38

 

Overview

The Airworthiness Directives 2004, enacted under the authority of the Civil Aviation Safety Regulations 1998, were introduced to address the need for updated and consolidated regulatory requirements for the airworthiness of certain aircraft models, particularly the Cessna 207 series aeroplanes. This legislative instrument was enacted by David Alan Villiers, acting as a delegate of the Civil Aviation Safety Authority (CASA) under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998. The primary policy objective of this instrument is to ensure that all airworthiness directives are current, accessible, and enforced uniformly across the aviation industry. This was achieved by revoking previous directives and re-making them as separate instruments to maintain clarity and consistency in regulatory standards. The re-made directives appear in the latest published editions to reflect any necessary updates and amendments, ensuring that all stakeholders have access to the most current regulatory requirements.

Scope and Application

The Airworthiness Directives 2004, issued under the authority of the Civil Aviation Safety Authority, specifically applies to the maintenance and operation of the Cessna 207 Series Aeroplanes, affecting various components and systems of these aircraft. The directives are applicable to the owners, operators, and maintainers of the specified aircraft within the Australian jurisdiction. These directives provide detailed requirements for the continued airworthiness of the aircraft, ensuring that safety standards are met through specific maintenance and operational procedures. The directives are geographically applicable within Australia, governed by the Civil Aviation Safety Regulations 1998. While the primary focus is on the Cessna 207 Series, the directives are part of a broader regulatory framework that ensures the safety of air operations across the country. The Act extends its application through subordinate instruments, which are detailed in the attached Airworthiness Directives, ensuring comprehensive coverage of the required safety standards.

Key Provisions

The legislative instrument, Airworthiness Directives 2004, revokes and re-makes certain Airworthiness Directives as detailed in Schedule 1. The delegate of the Civil Aviation Safety Authority, David Alan Villiers, exercises this authority under subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998. Each Airworthiness Directive mentioned in Schedule 1 is re-made in the same form as it appears in the latest published edition of the Directive. These Airworthiness Directives pertain specifically to the Cessna 207 Series Aeroplanes, covering various components and systems such as control systems, fuel systems, and structural integrity. For example, AD/CESSNA 207/2 addresses the Auxiliary Fuel Pump Electrical System, while AD/CESSNA 207/11 concerns the Wing Flap Actuator Ball Nut Assemblies. The re-making of these directives ensures that the latest safety standards and compliance requirements are uniformly applied. The obligations imposed by these directives require aircraft operators and maintenance personnel to adhere strictly to the specified safety measures and operational procedures. This includes conducting mandatory inspections, repairs, and replacements as outlined in the respective directives. For instance, AD/CESSNA 207/14 requires the replacement of the Fuel Reservoir Fitting, while AD/CESSNA 207/23 mandates the installation of the Fuel Cap Alignment Placard. Compliance with these obligations is crucial to maintaining the airworthiness of the aircraft. Failure to comply with these Airworthiness Directives can result in significant legal consequences. Under the Civil Aviation Safety Regulations 1998, non-compliance may lead to civil penalties. The maximum penalty for each offence can be substantial, reflecting the importance of adhering to safety regulations. Additionally, continued non-compliance may result in criminal charges, which could lead to fines and imprisonment, further emphasizing the seriousness of these obligations.

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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.