Airworthiness Directives 2004 - Revocation and Remaking - Cessna 177 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 177 Series Aeroplanes

 AD Name AD Number

 Wing Flap System - CANCELLED AD/CESSNA 177/1

 Flap Extension - CANCELLED AD/CESSNA 177/2 Amdt 1

 Stabilator Slot AD/CESSNA 177/3

 Fuel Tank Vent Line - CANCELLED AD/CESSNA 177/4

 Pneumatic Stall Warning System AD/CESSNA 177/5 Amdt 2

 Oil Pressure Gauge Line - CANCELLED AD/CESSNA 177/6

 Fuel Shut-Off Valve - CANCELLED AD/CESSNA 177/7

 Control Systems AD/CESSNA 177/8

 Fuel Quantity Transmitter AD/CESSNA 177/9

 Flap Actuator - CANCELLED AD/CESSNA 177/10

 Stabilator Attachment Angles AD/CESSNA 177/11 Amdt

 Upper Door Pillar AD/CESSNA 177/12 Amdt

 Front Seat Restraint Installations AD/CESSNA 177/13

 Stabilator Spar - CANCELLED AD/CESSNA 177/14

 Vertical Fin Forward Attachment Bulkhead AD/CESSNA 177/15

 Oil Pressure Gauge Line AD/CESSNA 177/16

 Stabilator AD/CESSNA 177/17

 Throttle Control Support Bracket Attachment AD/CESSNA 177/18

 Air Filter Seal AD/CESSNA 177/19

 Landing Gear Hydraulic Line AD/CESSNA 177/20

 Nose Landing Gear Upper Support Locknut AD/CESSNA 177/21

 Nose Landing Gear Rod End AD/CESSNA 177/22

 Stabilator Trim Actuator Attach Bolt AD/CESSNA 177/23

 Fuel Quantity Transmitter AD/CESSNA 177/24

 Cigar Lighter Wiring AD/CESSNA 177/25

 Vented Fuel Caps AD/CESSNA 177/26 Amdt

 Flying Control System Turnbuckles AD/CESSNA 177/27

 Fuel Cap Alignment Placard AD/CESSNA 177/28

 Seat Adjustment Mechanism AD/CESSNA 177/29 Amdt

 Wing Main Spar Carry-Through Section AD/CESSNA 177/30 Amdt

 Fuel Selector Valve AD/CESSNA 177/31

 Fuel Strainer AD/CESSNA 177/32

 Upper Shoulder Harness Adjuster Spring AD/CESSNA 177/33

 

Overview

The Airworthiness Directives 2004 is a legislative instrument introduced by David Alan Villiers, a delegate of the Civil Aviation Safety Authority (CASA), acting under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998. This legislative instrument addresses the need to revoke certain airworthiness directives and to re-make them in their latest form, ensuring that all safety regulations are up-to-date and accurately reflect current standards. The policy objective is to maintain the highest level of safety within the aviation industry by ensuring that aircraft meet the necessary airworthiness standards. Each of the airworthiness directives listed in Schedule 1 of the legislative instrument is being re-made to exactly match the latest published edition. This ensures that all safety requirements are current and enforceable, directly addressing any identified gaps or issues in the previous directives. By re-making these directives, the Civil Aviation Safety Authority aims to provide clear and updated guidelines for maintaining the airworthiness of aircraft, thereby protecting public safety and enhancing the overall safety of the aviation industry.

Scope and Application

The Airworthiness Directives 2004, issued by David Alan Villiers as the delegate of the Civil Aviation Safety Authority, governs the airworthiness of specific aircraft, namely the Cessna 177 series aeroplanes, by specifying necessary modifications and maintenance requirements to ensure safety and compliance with regulatory standards. This legislative instrument applies to aircraft owners, operators, and maintenance providers who are directly involved with the Cessna 177 series aeroplanes. It pertains to the various systems and components of these aircraft, including the wing flap system, stabilator, fuel tank vent line, control systems, and more, as detailed in the individual Airworthiness Directives attached to the instrument. The legislation operates on a Commonwealth level, applying across Australia in accordance with the Civil Aviation Safety Regulations 1998. While the primary focus is on airworthiness and safety, the specific directives may include exclusions or thresholds relevant to particular aircraft components or situations. This legislative instrument may be extended or further detailed through subordinate instruments, which can provide additional guidance or specific requirements for compliance.

Key Provisions

The Airworthiness Directives 2004, issued under the Civil Aviation Safety Regulations 1998, primarily concerns the revocation and remaking of existing Airworthiness Directives (ADs) related to specific aircraft models. The directive, issued by David Alan Villiers, acting as a delegate of the Civil Aviation Safety Authority, revokes certain ADs related to the Cessna 177 series aeroplanes and re-issues them as separate instruments (subreg. 39.001(1)). The ADs that are revoked and re-made include several concerning the wing flap system, stabilator, fuel tank vent line, pneumatic stall warning system, oil pressure gauge line, control systems, fuel quantity transmitter, and various other components of the aircraft. These directives are being reissued in their latest published form. The obligations imposed by these directives on the relevant parties, such as aircraft manufacturers, operators, and maintenance providers, are primarily concerned with ensuring the safety and airworthiness of the affected aircraft. Specifically, they must comply with the detailed requirements set out in each directive, which may involve conducting inspections, making repairs or modifications, and ensuring that all components meet specified standards. For example, ADs may require regular checks of fuel quantity transmitters, stabilator spars, and other critical systems to ensure they are functioning correctly and safely. Failure to comply with these directives could result in serious safety risks, including potential aircraft accidents or incidents. In terms of penalties and consequences for breaches, the Civil Aviation Safety Regulations 1998 provide for both civil and criminal sanctions. Under the regulations, non-compliance with Airworthiness Directives can result in substantial fines and, in more serious cases, criminal charges. For example, the maximum penalty for an individual found guilty of a civil offence under these regulations can be significant, potentially amounting to hundreds of thousands of dollars. Additionally, in cases where a breach of an AD leads to an accident or incident, the responsible party could face criminal charges, which may include imprisonment. The exact penalties depend on the severity of the breach and the impact on aviation safety. The re-issuance of these directives underscores the importance of maintaining strict adherence to airworthiness standards. The Civil Aviation Safety Authority's role in overseeing these directives is critical to ensuring that all aircraft operate within safe and compliant parameters. Non-compliance not only poses risks to the safety of passengers and crew but also has severe legal ramifications. Therefore, all parties involved in the maintenance and operation of affected aircraft must carefully follow the requirements set out in these directives to avoid any potential legal or safety issues.

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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.