AD/PA-18/8 - Rudder Control Cables - Inspection and Re-Routing

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Legislation au F2006B05398 In force Legislative Instrument

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Piper PA-18 and 19 (Super Cub) Series Aeroplanes

 

AD/PA-18/8 Rudder Control Cables - Inspection and Re-Routing

Applicability: All models with S/Nos. 1807309016 to 18-7609001. Document:  Piper SB No. 485.

Compliance: Within 100 hours time in service after 30 April 1976.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


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Overview

The Civil Aviation Safety Authority (CASA) issued the Civil Aviation Regulations 1998 under the authority of the Australian Parliament, forming the backbone of aviation safety regulation in Australia. These regulations aim to ensure that all aspects of civil aviation in Australia adhere to internationally recognised safety standards. The legislation was enacted to address the need for a comprehensive regulatory framework governing civil aviation operations, safety, and security. By establishing a detailed set of rules and standards, the Civil Aviation Regulations 1998 help mitigate risks associated with civil aviation activities, ensuring the safety and efficiency of the Australian airspace. One specific area of focus within these regulations is addressed by Airworthiness Directives (ADs), which are legally binding requirements issued by CASA to address safety deficiencies in specific aircraft models. The ADs are designed to maintain the airworthiness of aircraft and ensure ongoing compliance with safety standards. For example, AD/PA-18/8 pertains to the Piper PA-18 and 19 (Super Cub) series aeroplanes, specifically focusing on rudder control cables. This directive mandates the inspection and re-routing of rudder control cables for aeroplanes with specific serial numbers, requiring compliance within 100 hours of time in service after April 30, 1976. This directive aims to address potential safety issues related to the rudder control cables, thereby enhancing the overall safety and reliability of the affected aircraft.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105 concerning the Civil Aviation Safety Authority's schedule of airworthiness directives, applies to the Piper PA-18 and 19 (Super Cub) series aeroplanes with serial numbers ranging from 1807309016 to 18-7609001. This regulation mandates a compliance requirement that involves inspecting and re-routing the rudder control cables of these aircraft within 100 hours of time in service after 30 April 1976, as outlined in Piper Service Bulletin No. 485. This directive is integral to ensuring the continued airworthiness and safety of these aircraft, falling under the jurisdiction of the Commonwealth of Australia, and applies to all such aircraft regardless of the location within Australia or the specific operator or pilot involved. No exclusions or exemptions are explicitly stated in the text, implying that all specified aircraft must adhere to these safety directives.

Key Provisions

The key operative sections of the Civil Aviation Regulations 1998, specifically within Part 39 - 105, mandate the maintenance and inspection of rudder control cables for Piper PA-18 and 19 (Super Cub) series aeroplanes. Section 105.485 outlines the applicability, requiring all models with serial numbers ranging from 1807309016 to 18-7609001 to comply with the directive. Compliance must be achieved within 100 hours of time in service after 30 April 1976, as specified in the Piper Service Bulletin No. 485. These provisions impose specific obligations on the operators and owners of the affected aircraft. They must ensure that the rudder control cables are inspected and, if necessary, re-routed in accordance with the directive. This requirement is critical for maintaining the safety and airworthiness of the aircraft, ensuring that the rudder control systems operate effectively and reliably. Owners and operators must document the compliance process, keeping records of inspections and any actions taken, to demonstrate adherence to the regulation. Failure to comply with the Airworthiness Directive AD/PA-18/8 can lead to severe consequences. The Civil Aviation Safety Authority (CASA) has the authority to take enforcement actions against non-compliant aircraft. Potential penalties include fines and potential grounding of the aircraft until the required inspections and repairs are completed. The seriousness of these potential outcomes underscores the importance of adhering to the specified timeframes and procedures outlined in the regulations. In cases of deliberate or reckless non-compliance, the penalties can be significantly more severe, potentially involving criminal charges and substantial fines.

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Area of Law
Aviation Law
Instrument
Legislative Instrument
Concepts
Regulatory Standards
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.