AD/AC-CLA/2 - Rudder Pedal Torque Tube

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B02195 Not in force Legislative Instrument

Legislation content

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Aircraft Parts and Development (CALL AIR) A-9 Series Aeroplanes

 

AD/AC-CLA/2 Rudder Pedal Torque Tube 11/65

Applicability: All A-9 series.

 

Requirement: Inspect the rudder pedal torque tubes P/N 12016 and 13017 using the dye penetrant method in the vicinity of the pedal and cable bellcrank attachment for cracking in the welds.

 

Compliance: At intervals not exceeding 100 hours time in service after 1 September 1971.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, aim to ensure the safety and efficiency of civil aviation within the country. One specific legislative instrument, F2006B02195, addresses the problem of ensuring that aircraft parts meet safety standards, particularly focusing on the A-9 series aeroplanes. This regulation introduces specific airworthiness directives to enhance safety, with a particular focus on the rudder pedal torque tubes, aiming to prevent potential cracking that could compromise the structural integrity of the aircraft. By setting out requirements for regular inspections using the dye penetrant method, the regulation seeks to maintain high safety standards in civil aviation operations. The Civil Aviation Safety Authority, through the legislative instrument F2006B02195, sets forth directives that mandate the inspection of rudder pedal torque tubes in A-9 series aeroplanes to detect any cracks in welds, thus addressing potential safety hazards. This legislative instrument underscores the authority's commitment to ensuring that aircraft parts comply with stringent safety standards, thereby safeguarding the aviation industry and the public. The policy objective is to enhance aircraft safety and reliability by implementing regular and thorough inspections of critical components.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, which pertains to the Civil Aviation Safety Authority's Schedule of Airworthiness Directives, applies to all A-9 series aircraft. This legislation mandates that these aircraft undergo specific inspections on the rudder pedal torque tubes P/N 12016 and 13017, using the dye penetrant method to check for cracks in the welds near the pedal and cable bellcrank attachment. The requirement necessitates compliance at intervals not exceeding 100 hours of time in service post 1 September 1971. This regulation is applicable across the Commonwealth of Australia, ensuring a uniform standard of aircraft safety and maintenance nationwide. Subordinate instruments may further define or expand upon these requirements, but the primary directive is clearly outlined in the legislation.

Key Provisions

The Civil Aviation Regulations 1998, particularly in Part 39, impose several key requirements on the maintenance and inspection of A-9 series aeroplanes. Specifically, Section 39-105 mandates inspections of the rudder pedal torque tubes (Sections 11/65) for all A-9 series aircraft. These inspections (Section 11/65) are to be conducted using the dye penetrant method to detect any cracking in the welds of the torque tubes, particularly in the vicinity of the pedal and cable bellcrank attachment. The parts in question are identified by the part numbers 12016 and 13017. The inspections must be performed at intervals not exceeding 100 hours of time in service following 1 September 1971. The Act imposes specific obligations on the operators and maintenance personnel of A-9 series aeroplanes to ensure that these inspections are carried out as required. Operators and maintenance personnel must adhere to the specified inspection intervals and use the prescribed dye penetrant method to ensure the integrity of the rudder pedal torque tubes. This includes properly preparing the surface of the torque tubes, applying the dye penetrant, and then examining the area for any indications of cracks or defects. Any detected issues must be appropriately addressed to maintain the airworthiness of the aircraft. Failure to comply with these inspection requirements can result in serious consequences. The Civil Aviation Regulations 1998 outline that non-compliance with airworthiness directives, such as those specified in Section 39-105, can lead to significant penalties. These can include both civil and criminal consequences, depending on the severity of the breach. For instance, operators found to be in breach of these regulations could face substantial fines or even imprisonment. The specific penalties are determined by the seriousness of the violation and the regulatory framework under which the offence is prosecuted.

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Aviation Law
Instrument
Legislative Instrument
Concepts
Definitions & Interpretation
Compliance Obligations
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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.