Airworthiness Directives 2004 - Revocation and Remaking - Partenavia P68 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

 Partenavia P68 Series Aeroplanes

 AD Name AD Number

 CANCELLED AD/P68/1

 Pre-Certification Requirements AD/P68/2 Amdt 2

 Engine Mount - Inspection AD/P68/3 Amdt 1

 Auxiliary Fuel Pump Drains - Inspection AD/P68/4

 Circuit Breaker Installation - Inspection AD/P68/5

 Rudder Trim Tab Control Rod P/N 68-506053 - Inspection AD/P68/6

 Ignition Switch Guard - Modification AD/P68/7

 Fuel Filter Bowl - Replacement AD/P68/8

 Superseded by AD/P68/17 - CANCELLED AD/P68/9

 Stabilator Balance Weight Attachment - Inspection and Modification AD/P68/10 Amdt 1

 Rudder Control Pulleys at Fuselage Frame No. 3 - Inspection AD/P68/11 Amdt 1

 Propeller Control Rod End - Inspection and Replacement AD/P68/12

 Longitudinal Trim Indicator - Check and Modification AD/P68/13 Amdt 2

 Fuel Pump Cooling Shroud - Modification AD/P68/14

 Fin, Rudder Upper Hinge Attachment Area - Modification AD/P68/15

 Engine and Engine Mount Attach Bolts AD/P68/16 Amdt 1

 Flap Actuator Switch - Inspection and Replacement AD/P68/17 Amdt 1

 Oil Cooler Elbow Fitting - Replacement AD/P68/18

 Control Wheel Shaft Universal Joint AD/P68/19 Amdt 2

 Flap Bellcrank Attachment Mounting Brackets - Inspection and Modification AD/P68/20 Amdt 1

 Horizontal Stabilator to Fuselage Frame Attachment - Check Torque AD/P68/21

 Wing Lower Front and Rear Spar Assemblies AD/P68/22 Amdt 4

 Aileron Control Cables - CANCELLED AD/P68/23 Amdt 2

 Fuel and Janitrol Lines AD/P68/24 Amdt 3

 Aileron Control Chain Connector - Inspection and Modification AD/P68/25

 Stabilator Travel Stop - Modification AD/P68/26

 Fibre Glass Leading Edges AD/P68/27

 Engine Mount Fittings AD/P68/28 Amdt 3

 Elevator Trim Tab AD/P68/29 Amdt 1


 Rudder Cables - CANCELLED AD/P68/30 Amdt 1

 Fuel Line Fire Sleeving - CANCELLED AD/P68/31

 Longitudinal Trim System AD/P68/32

 Engine and Propeller Control Cables AD/P68/33 Amdt 1

 Engine Mount AD/P68/34

 LH and RH Muffler Assemblies AD/P68/35

 Horizontal Tailplane AD/P68/36

 Frame No. 1 AD/P68/37

 Stabiliser Drive Horn AD/P68/38 Amdt 2

 Fuel Selector Valve AD/P68/39

 Stabilator Torque Tube Attachment Shelves, Flap and Aileron Hinge Shelves AD/P68/40

 IFR Instrument Panel Configuration AD/P68/41 Amdt 1

 Wing Upper Skin Stringers AD/P68/42

 Wing and Airframe - Fatigue Life Limit AD/P68/43 Amdt 4

 Flight Control Cables AD/P68/44

 Wing Spar Inspection AD/P68/45

 Engine Cowl AD/P68/46

 Aircraft Flight Manual, Flight into Icing Conditions AD/P68/47

 Nose Landing Gear Cracking AD/P68/48

 Landing Gear Attach Bolts AD/P68/49

 Flight Control AD/P68/50

 Flight Controls AD/P68/51

 Fuel Selector Control AD/P68/52

 

Overview

The Airworthiness Directives 2004, enacted by David Alan Villiers as the delegate of the Civil Aviation Safety Authority (CASA), addresses the need to revoke and re-make existing airworthiness directives concerning the Partenavia P68 Series Aeroplanes. This legislative instrument was introduced to ensure the continued safety and airworthiness of aircraft by updating and re-promulgating directives in line with the latest safety standards and technological advancements. The directives were revoked and re-made in exactly the same form as they appeared in the latest published edition, aiming to maintain consistency and clarity in regulatory compliance for aircraft operators and maintenance personnel. The enactment of these directives reflects CASA's commitment to maintaining high safety standards within the Australian aviation industry.

Scope and Application

The Airworthiness Directives 2004, issued by the delegate of the Civil Aviation Safety Authority, David Alan Villiers, under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998, pertains to the revocation and re-making of specific airworthiness directives that apply to the Partenavia P68 Series Aeroplanes. This legislative instrument affects all persons and entities involved in the operation and maintenance of these aircraft, including pilots, maintenance personnel, and aviation companies, ensuring compliance with updated safety standards. The directives are applicable nationwide, encompassing the entire Commonwealth of Australia, and are intended to maintain and enhance the airworthiness of the specified aircraft models. The directives cover a wide range of technical requirements, including pre-certification conditions, inspections, modifications, and replacements of various aircraft components. Exclusions or exemptions are not specified in the text; however, the applicability of these directives is subject to any subordinate instruments that may provide further clarification or detail.

Key Provisions

The Airworthiness Directives 2004, made under the authority of the Civil Aviation Safety Authority (CASA) delegate, David Alan Villiers, primarily focus on the revocation and remaking of various Airworthiness Directives related to the Partenavia P68 series aeroplanes. The directive revokes a number of existing Airworthiness Directives, including AD/P68/1, AD/P68/8, AD/P68/22, AD/P68/29, and AD/P68/30, and replaces them with new versions of the same directives. Each new directive is being re-made in exactly the same form as it appears in the latest published edition. This means that the content of these directives has not changed, only their legal status has been updated. The obligations and requirements imposed by these Airworthiness Directives pertain to the maintenance, inspection, and modification of specific components of the Partenavia P68 series aeroplanes. For instance, AD/P68/2 mandates an inspection of the engine mount, while AD/P68/6 requires a modification to the ignition switch guard. Other directives address aspects such as the replacement of fuel filter bowls, modifications to control cables, and inspections of structural components like the rudder trim tab control rod. The directives specify the necessary actions, procedures, and timeframes for compliance, ensuring that the aeroplanes maintain a certain standard of airworthiness. Failure to comply with these Airworthiness Directives can lead to serious consequences. Under the Civil Aviation Safety Regulations 1998, non-compliance may result in enforcement actions, including fines and potential criminal charges. The exact penalties for breach of these directives are not detailed in the legislative instrument itself but are likely to be severe, given the critical nature of airworthiness regulations. The Civil Aviation Safety Regulations 1998 provide a framework for imposing penalties, which could include substantial fines and, in serious cases, imprisonment for individuals found guilty of breaching these safety mandates.

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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.