Airworthiness Directives 2004 - Revocation and Remaking - Cessna 340 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 340 Series Aeroplanes

 AD Name AD Number

 Fuel Pressure Regulator Fitting - Inspection AD/CESSNA 340/1

 CANCELLED AD/CESSNA 340/2

 Wing Leading Edge Fuel Lines and Wiring - Inspection and Modification AD/CESSNA 340/3

 Lower Wing Skin Rivets AD/CESSNA 340/4 Amdt 3

 Main Landing Gear Trunnion - Inspection and Replacement AD/CESSNA 340/5

 Pre-Certification Requirements - Modification AD/CESSNA 340/6

 Engine Exhaust System AD/CESSNA 340/7 Amdt 6

 Tip Tank Fuel Seepage - Inspect AD/CESSNA 340/8

 Exhaust Tailpipe Support Kit - Installation AD/CESSNA 340/9

 Fuel Crossfeed Line Fittings - Modification AD/CESSNA 340/10

 Wing Tip Strobe Light - Inspection AD/CESSNA 340/11 Amdt

 Main Landing Gear Fork-Bolt - Replacement AD/CESSNA 340/12

 Main Landing Gear Down Lock Pin and Set Screw - Inspection AD/CESSNA 340/13

 Oxygen System - Cleaning AD/CESSNA 340/14

 Landing Gear Emergency Handle - Replacement AD/CESSNA 340/15

 Goodyear Fuel Cells - Inspection AD/CESSNA 340/16

 Auto Pilot System - Disabling - Modification AD/CESSNA 340/17

 Passenger Seat Installation - Inspection AD/CESSNA 340/18

 Upper Inner Cabin Door Handle and Locking Mechanism - Inspection AD/CESSNA 340/19

 Wing Locker Fuel Tank Filler Cap - Rework AD/CESSNA 340/20

 Horizontal Stabiliser and Elevators - Inspection and Replacement AD/CESSNA 340/21 Amdt

 Fuel Crossover Line - Modification - CANCELLED AD/CESSNA 340/22

 Elevator Balance Weight - Inspection AD/CESSNA 340/23

 Powerplant Fire Detection System - Installation AD/CESSNA 340/24 Amdt

 Rudder Balance Weight Attachment Rib AD/CESSNA 340/25 Amdt

 Crossfeed Fuel Line AD/CESSNA 340/26 Amdt

 Wing Front Spar Lower Attachment Fittings AD/CESSNA 340/27

 Auxiliary Fuel Pump Wiring Modification AD/CESSNA 340/28

 Seat Back Reinforcing Strap AD/CESSNA 340/29


 Placards and Cabin Fittings AD/CESSNA 340/30 Amdt

 Main Landing Gear Wheel Bay Wing Rib and Wing Skin AD/CESSNA 340/31 Amdt

 Wing and Airframe AD/CESSNA 340/32

 Exhaust System Components - Inspection AD/CESSNA 340/33

 Aircraft Flight Manual, Flight into Icing Conditions AD/CESSNA 340/34 Amdt

 

Overview

The Airworthiness Directives 2004 were introduced to provide a framework for ensuring that aircraft meet specific safety standards, thereby addressing any identified safety risks. This legislative instrument was enacted by David Alan Villiers, as a delegate of the Civil Aviation Safety Authority, under the authority granted by subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998. The policy objective underpinning this legislation is to maintain and enhance the safety of aircraft operations by ensuring that airworthiness directives, which are legally binding orders for correcting an unsafe condition on an aircraft, are consistently and accurately enforced. The instrument revokes previously issued directives and remakes them to ensure they reflect the most current safety standards and requirements, maintaining a high level of safety and reliability in the aviation industry.

Scope and Application

The Airworthiness Directives 2004 made by David Alan Villiers, the delegate of the Civil Aviation Safety Authority, applies to all aircraft operators and maintenance personnel involved with the maintenance, operation, or modification of Cessna 340 series aeroplanes. These directives serve to ensure the continued airworthiness of the specified aircraft models by establishing mandatory safety standards and procedures that must be adhered to. The legislation operates within the Commonwealth jurisdiction, impacting all operations within Australian airspace. The directives are detailed and comprehensive, addressing a wide array of specific maintenance and operational concerns from fuel pressure regulators to the installation of placards and cabin fittings. While the primary focus is on the Cessna 340 series, the implications of these directives extend to any party involved in the maintenance or operation of these aircraft, ensuring a uniform approach to safety across the industry. The directives also allow for the revocation and remaking of existing Airworthiness Directives to ensure they remain relevant and effective.

Key Provisions

The Airworthiness Directives 2004, issued by David Villiers as the delegate of the Civil Aviation Safety Authority (CASA) under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998, primarily serve to revoke certain Airworthiness Directives and re-issue them as separate instruments (section 2(a) and (b)). Specifically, the legislation focuses on the Cessna 340 Series Aeroplanes, detailing the revocation and remaking of various Airworthiness Directives (AD) related to the aircraft's components and systems. Each re-made AD is presented in the same form as it appears in the latest published edition, ensuring that the updated directives remain consistent with the most current safety standards. The obligations and requirements imposed by these directives include thorough inspections, modifications, and replacements of specific aircraft parts to ensure airworthiness. For instance, AD/CESSNA 340/1 mandates the inspection of the fuel pressure regulator fitting, while AD/CESSNA 340/3 requires the inspection of lower wing skin rivets. These directives also cover critical areas such as the main landing gear, fuel systems, and structural components. Compliance with these requirements is essential for maintaining the safety and operational integrity of the Cessna 340 Series Aeroplanes. Failure to comply with the provisions of these Airworthiness Directives can lead to significant consequences. While the specific penalties for non-compliance are not detailed in the text, the overarching regulatory framework under the Civil Aviation Safety Regulations 1998 typically includes both civil and criminal penalties. Civil penalties may involve fines and the possibility of grounding the aircraft, while criminal penalties could result in imprisonment, reflecting the seriousness of non-compliance with airworthiness standards. The exact penalties would be determined in accordance with the broader regulatory and legislative context.

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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.