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

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Legislation au F2006B05339 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

 


Partenavia P68 Series Aeroplanes

 

AD/P68/12 Propeller Control Rod End - Inspection

and Replacement Applicability:  All models P68 and P68B with S/Nos. below 160. Document:              Partenavia SB No. 37, Revision 1.


11/78

Compliance: Within 50 hours time in service after 17 October 1978 and thereafter at intervals not exceeding 50 hours time in service until Part 2 of Partenavia SB No. 37, Revision 1 is completed.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, address the need for stringent safety measures in civil aviation to ensure the safety and reliability of aircraft operations. The Civil Aviation Regulations are a critical framework governing various aspects of civil aviation, including airworthiness, licensing, and operational standards. The regulations were introduced to establish a comprehensive set of safety standards and operational requirements for all civil aviation activities within Australia, thereby mitigating risks and ensuring the safety of passengers, crew, and the general public. One specific legislative instrument under these regulations is the "Partenavia P68 Series Aeroplanes AD/P68/12 Propeller Control Rod End - Inspection and Replacement," which was introduced to address issues identified with the propeller control rod end in certain Partenavia P68 models. The policy objective of this directive is to ensure that the propeller control rod end is inspected and replaced as necessary to maintain the airworthiness of the aircraft, thereby enhancing flight safety.

Scope and Application

The Civil Aviation Safety Authority (CASA) under the Civil Aviation Regulations 1998, specifically Part 39 - 105, mandates the application of Airworthiness Directives (AD) for certain aircraft to ensure ongoing safety standards are met. In this context, AD/P68/12 pertains to Partenavia P68 Series Aeroplanes, namely models P68 and P68B, with serial numbers (S/Nos.) below 160. This legislation requires specific actions concerning the propeller control rod end, necessitating inspection and replacement as outlined in Partenavia Service Bulletin No. 37, Revision 1. Compliance with this directive is mandatory within 50 hours of time in service after 17 October 1978, and subsequently at intervals not exceeding 50 hours until the completion of Part 2 of Partenavia SB No. 37, Revision 1. This legislation applies exclusively to the specified aircraft models and serial numbers, ensuring that these aircraft maintain their airworthiness through the prescribed maintenance actions.

Key Provisions

The main operative sections of the Civil Aviation Regulations 1998, particularly Part 39 - 105 which pertains to the Schedule of Airworthiness Directives for the Partenavia P68 Series Aeroplanes, require specific actions concerning the propeller control rod end (AD/P68/12). Section (1) identifies the aircraft models affected by the directive, namely P68 and P68B with serial numbers below 160. Section (2) stipulates that compliance with the directive must occur within 50 hours of time in service after 17 October 1978, and subsequently, at intervals not exceeding 50 hours time in service until the completion of Part 2 of Partenavia SB No. 37, Revision 1. The directive mandates a thorough inspection and, if necessary, the replacement of the propeller control rod end to ensure continued airworthiness. The obligations imposed by this legislation are stringent and specific. Aircraft operators must ensure that the inspection and, if required, the replacement of the propeller control rod end is carried out within the prescribed timeframes. This includes maintaining detailed records of each inspection and any actions taken, as these records must be readily available for review by the Civil Aviation Safety Authority (CASA). The directive requires operators to follow the detailed procedures outlined in Partenavia SB No. 37, Revision 1, ensuring that any deviations from these procedures are documented and justified. Failure to comply with the airworthiness directive can lead to significant consequences. Under the Civil Aviation Act 1988, non-compliance with airworthiness directives can be considered an offence. Operators found in breach of these regulations may face penalties, including substantial fines and potential criminal charges. The severity of the penalties depends on the nature and extent of the non-compliance, but the maximum penalties can be significant, reflecting the critical importance of adhering to these safety directives. The consequences of non-compliance not only affect the operator financially but can also lead to the grounding of the aircraft until the required actions are taken, potentially disrupting operations and passenger schedules.

Legal classification tags

Area of Law
Aviation Law
Instrument
Regulation
Concepts
Definitions & Interpretation
Compliance Obligations
Enforcement Powers
Catchwords
Airworthiness

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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.