Airworthiness Directives 2004 - Revocation and Remaking - Piaggio P166 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

 Piaggio P166 Series Aeroplanes

 AD Name AD Number

 Teleflex Rods for Engine Controls - Protection AD/P166/1

 Engine Oil System Piping - Re-Routing AD/P166/2

 Fuel System in Engine Compartment - Modification AD/P166/3

 Drain Well for Fuel Tanks - Increased Capacity AD/P166/4

 Engine Nacelle - Drainage Modification AD/P166/5

 Fire Detection System - Modification AD/P166/6

 Electrical Supply - Turn and Bank Indicator, Fire Warning System and Stall  AD/P166/7

 Emergency Electrical Bus - Modification AD/P166/8

 Generator Circuit - Modification AD/P166/9

 Undercarriage Warning Horn Circuit - Modification AD/P166/10

 Main Landing Gear Retracting Jack Stem - Installation of Washer AD/P166/11

 Elevator Trim Tab Inner Hinge - Modification AD/P166/12

 Hydraulic Pressure Switch - Provision of Guards AD/P166/13

 Nose Landing Gear Shock Absorber Mount Sleeves - Replacement AD/P166/14

 CANCELLED AD/P166/15

 Elevator Trim Drum - Inspection and Modification AD/P166/16

 Angle Bar at Fuselage Frame 20 - Inspection and Modification AD/P166/17

 Superseded by AD/P166/21 - CANCELLED AD/P166/18

 Carburettor Air Mixer Valve - Inspection and Modification AD/P166/19

 Hydraulic Pressure Gauges - Replacement AD/P166/20

 Main Landing Gear Shock Absorber Strut - Modification AD/P166/21

 Nose Wheel Door Levers - Modification AD/P166/22

 Main Landing Gear Jack Lock - Modification AD/P166/23

 Nose Landing Gear Retraction Jack Brake Valve - Modification AD/P166/24

 Nose Landing Gear Steering Control Flange - Modification AD/P166/25

 Engine and Propeller Installation Teleflex Controls - Modification AD/P166/26

 Magnetic Compass Installation - Modification AD/P166/27

 Flap Control Bellcrank - Modification AD/P166/28 Amdt 1

 Flap Hinge Attachment At Rib No. 13 AD/P166/29


 Nose Wheel Steering - Inspection and Modification AD/P166/30

 Main Landing Gear Retraction Jack Pivot - Modification AD/P166/31

 Flap Actuating Cylinder Attachment Bracket - Inspection AD/P166/32

 Engine and Propeller Teleflex Controls - Inspection and Modification AD/P166/33

 Landing Gear Selector Valve - Modification AD/P166/34

 Front Seat Restraint Installations - Modification AD/P166/35

 

Overview

The Airworthiness Directives 2004 is a legislative instrument that was enacted under the Civil Aviation Safety Regulations 1998. This instrument was introduced by David Alan Villiers, acting as a delegate of the Civil Aviation Safety Authority, to address the need for the revocation and remaking of specific airworthiness directives pertaining to the Piaggio P166 Series Aeroplanes. The objective of this legislative instrument is to ensure the continued safety and airworthiness of these aircraft by updating and replacing the existing directives with new, revised versions as per the latest published editions. Each airworthiness directive is re-made in the same form as it appears in the most recent publication, thereby maintaining the integrity and relevance of the safety standards required for these aircraft.

Scope and Application

The Airworthiness Directives 2004, issued under the authority of David Alan Villiers as a delegate of the Civil Aviation Safety Authority, primarily applies to all aircraft manufacturers, operators, and owners of Piaggio P166 Series Aeroplanes operating within Australia. The directives are designed to ensure the ongoing airworthiness of these aircraft by specifying mandatory modifications and inspections on various components such as the engine controls, fuel systems, electrical systems, and landing gear, among others. Each directive is meticulously detailed to provide clear and specific instructions to ensure compliance with safety standards. The scope of the Act extends nationally, with its provisions applicable across all states and territories within Australia, thereby establishing a uniform regulatory framework for the maintenance and operation of these aircraft. While the Act itself does not explicitly state exclusions or exemptions, it is understood that certain operations might be subject to additional scrutiny or specific regulatory conditions as defined by subordinate instruments or other relevant legislation. The Act effectively revokes and re-makes each Airworthiness Directive listed in Schedule 1, ensuring that all directives remain current and aligned with the latest safety requirements.

Key Provisions

The Airworthiness Directives 2004, issued under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998, involve the revocation of several existing Airworthiness Directives concerning Piaggio P166 Series Aeroplanes and the re-making of these directives as separate instruments. Specifically, the directives listed in Schedule 1 are revoked and re-made to ensure they are aligned with the latest published editions. Each re-made directive retains its original form, thereby maintaining the standards and requirements for the airworthiness of the specified aircraft series. The directives cover a range of modifications and inspections related to engine controls, fuel systems, electrical supply, landing gear, and other critical components. These directives impose specific obligations on the parties and entities governed by them. For instance, operators of Piaggio P166 Series Aeroplanes must comply with the detailed instructions and requirements outlined in each Airworthiness Directive. This includes performing necessary modifications, inspections, and replacements as specified. Additionally, the directives mandate that all changes must be carried out by qualified personnel and that records of compliance must be maintained. These obligations are essential to ensure the continued safety and airworthiness of the aircraft. Failure to comply with the provisions of these Airworthiness Directives can result in significant consequences. Under the Civil Aviation Safety Regulations 1998, non-compliance can lead to civil penalties, including fines. The exact amount of these fines is not specified in the legislative instrument but can vary based on the severity and nature of the breach. Additionally, continued operation of an aircraft that does not comply with the directives may lead to enforcement actions by the Civil Aviation Safety Authority, potentially resulting in grounding of the aircraft or other regulatory sanctions. In severe cases, criminal charges could be pursued, particularly if non-compliance results in accidents or endangers public safety.

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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.