Airworthiness Directives 2004 - Revocation and Remaking - Cessna 206 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 206 Series Aeroplanes

 AD Name AD Number

 Plastic Control Wheel AD/CESSNA 206/1 Amdt 1

 Throttle/Mixture Control Rods - CANCELLED AD/CESSNA 206/2

 Wing Rear Spar AD/CESSNA 206/3 Amdt 3

 Nose Landing Gear - CANCELLED AD/CESSNA 206/4 Amdt 1

 Auxiliary Fuel Pump Electrical System AD/CESSNA 206/5 Amdt 2

 Fuel System Drain Cock AD/CESSNA 206/6

 Control Systems AD/CESSNA 206/7

 Flap Actuator - CANCELLED AD/CESSNA 206/8

 Aileron Mass Balance Weight Attachment Rivets - CANCELLED AD/CESSNA 206/9 Amdt 1

 Exhaust Manifold Heat Exchanger AD/CESSNA 206/10

 Front Seat Restraint Installations AD/CESSNA 206/11

 Aft Tailcone Assembly AD/CESSNA 206/12 Amdt

 Alternator Earth Lead AD/CESSNA 206/13

 Aileron Control Tube and Automatic Pilot Roll Servo AD/CESSNA 206/14

 Right Hand Wing Rear Spar AD/CESSNA 206/15

 Main Gear Wheel Assemblies AD/CESSNA 206/16

 Pre-Certification Requirements AD/CESSNA 206/17

 Fuel Quantity Placard AD/CESSNA 206/18

 Rudder Trim Chain AD/CESSNA 206/19

 Wing Flap Actuator Ball Nut Assemblies AD/CESSNA 206/20

 Turbocharger Thrust Bearing Pin and Centre Housing Assembly AD/CESSNA 206/21 Amdt

 Fuel Selector Valve - CANCELLED AD/CESSNA 206/22

 Fuel Reservoir Fitting AD/CESSNA 206/23

 Goodyear Fuel Cells AD/CESSNA 206/24

 Fuel Vent Tube AD/CESSNA 206/25

 Ammeter Type and Position AD/CESSNA 206/26

 Vented Fuel Caps AD/CESSNA 206/27 Amdt

 Fuel Tank Filler Neck AD/CESSNA 206/28

 Fuel Flow Stabilisation Placard AD/CESSNA 206/29


 Alternator Ground Strap AD/CESSNA 206/30 Amdt

 Flying Control System Turnbuckles AD/CESSNA 206/31

 Turbocharger AD/CESSNA 206/32

 Fuel Cap Alignment Placard AD/CESSNA 206/33

 Wing Tip Navigation Strobe Lights AD/CESSNA 206/34

 Cylinder Head Temperature Probe AD/CESSNA 206/35

 Bladder Type Fuel Cells AD/CESSNA 206/36 Amdt

 Isolator Mounts P/N 700-2500-1 AD/CESSNA 206/37

 Retirement Lives - Fatigue Critical Components AD/CESSNA 206/38

 Fuel Filler Caps and Adaptors AD/CESSNA 206/39 Amdt

 Fuel Selector Valve Safety Wire AD/CESSNA 206/40

 Rear Wing Spar Doubler AD/CESSNA 206/41

 Fuel System Water Drainage Placard AD/CESSNA 206/42

 Battery Vent System AD/CESSNA 206/43 Amdt

 Electrical Power Distribution and Control AD/CESSNA 206/44

 Passenger Seat Belt Fitting Spacer AD/CESSNA 206/45

 Seat Adjustment Mechanism AD/CESSNA 206/46 Amdt

 Rear Door Emergency Exit AD/CESSNA 206/47 Amdt

 Forward Door Post Bulkhead AD/CESSNA 206/48 Amdt

 Aircraft Repair AD/CESSNA 206/49

 Flight Controls - Inspection AD/CESSNA 206/50

 Oil Pressure Switch AD/CESSNA 206/51

 Fuel Strainer AD/CESSNA 206/52

 Horizontal Stabiliser Attachment Brackets AD/CESSNA 206/53

 Horizontal Stabilizer Front Spar AD/CESSNA 206/54 Amdt

 Horizontal Stabiliser Attachment  Brackets - 2 AD/CESSNA 206/55

 Brackett Engine Air Filters AD/CESSNA 206/56 Amdt

 Cigar Lighter Wiring AD/CESSNA 206/57

 KAP 140 Autopilot System AD/CESSNA 206/58 Amdt

 KAP 140 Autopilot System AD/CESSNA 206/59

 Upper Shoulder Harness Adjuster Spring AD/CESSNA 206/60

 

Overview

The Airworthiness Directives 2004, enacted on 20 December 2004, was introduced to address the need for updated and consolidated safety regulations for aircraft airworthiness, specifically for the Cessna 206 Series Aeroplanes. This legislative instrument was created by David Alan Villiers, a delegate of the Civil Aviation Safety Authority, acting under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998. The primary policy objective of this instrument was to revoke certain outdated airworthiness directives and re-make them to ensure that the latest safety standards and requirements are met, thereby maintaining the highest level of safety in the aviation industry. Each re-made directive is presented in the same form as it appears in the most recent published edition.

Scope and Application

The Airworthiness Directives 2004, made under the Civil Aviation Safety Regulations 1998, apply to the Cessna 206 Series Aeroplanes and are administered by the Civil Aviation Safety Authority (CASA). This legislation concerns the revocation and remaking of specific Airworthiness Directives that pertain to various components and systems of the Cessna 206 aircraft, ensuring they meet safety standards. The directives cover a range of issues including structural integrity, fuel system components, control systems, and other critical areas. The legislation operates within the Commonwealth jurisdiction, impacting all relevant parties including aircraft owners, operators, and maintenance providers within Australia. There are no stated exclusions or exemptions in the text, meaning that all specified aircraft and their components must comply with the directives. The application of this Act can be extended or restricted through subordinate instruments, although none are specified in the text.

Key Provisions

The Airworthiness Directives 2004, promulgated by David Alan Villiers as a delegate of the Civil Aviation Safety Authority (CASA), includes the revocation and remaking of several Airworthiness Directives (ADs) for Cessna 206 series aeroplanes (subreg. 39.001 (1)). Specifically, the Directive revokes and re-issues ADs listed in Schedule 1, ensuring they appear in the latest published edition. The ADs cover a range of aircraft components and systems, including control systems, fuel systems, and structural integrity. For example, AD/CESSNA 206/5 pertains to the Fuel System Drain Cock, while AD/CESSNA 206/14 pertains to the Right Hand Wing Rear Spar. The revocation and remaking process ensures these directives remain current and applicable. Under this legislative instrument, various obligations and requirements are imposed on aircraft operators and owners of the affected Cessna 206 series aeroplanes. These include compliance with the re-made ADs, which may involve inspections, repairs, or modifications to the specified aircraft components and systems. Operators must adhere to the detailed technical requirements outlined in each AD to ensure the airworthiness of their aircraft. This may involve following specific maintenance schedules, conducting inspections, and applying prescribed modifications or replacements to ensure the aircraft meets safety standards. Breaches of the Airworthiness Directives 2004 can lead to significant consequences, including both civil and criminal penalties. While the specific penalties are not detailed in the text, breaches of airworthiness regulations generally result in fines, imprisonment, or both. The severity of the penalty often depends on the nature and extent of the non-compliance, as well as any resulting safety risks. For instance, failure to comply with a critical AD could lead to severe penalties due to the potential risk to flight safety. The Civil Aviation Safety Regulations 1998, under which these directives are issued, provide a framework for enforcing compliance and imposing penalties for non-compliance.

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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.