AD/PA-34/18 - Quick Disconnect Seat Retention Mechanism - Inspection

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Legislation au F2006B05889 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-34 (Seneca) Series Aeroplanes

 

AD/PA-34/18 Quick Disconnect Seat Retention Mechanism - Inspection

Applicability: Model PA-34-200 with S/Nos. 34-7250001 to 34-7450220. Model PA-34-200T with S/Nos. 34-7570001 to 34-7570054.

Document: Piper SL No. 763.

 

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

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


12/75

Overview

The Civil Aviation Regulations 1998 were enacted to provide comprehensive regulations for civil aviation safety, ensuring that all aircraft operating in Australian airspace meet safety standards. One specific aspect addressed by these regulations is the implementation of Airworthiness Directives (ADs), which are legally enforceable safety measures. AD/PA-34/18 is an example of such an AD, specifically concerning the Piper PA-34 (Seneca) Series Aeroplanes. The directive was introduced to address safety concerns regarding the quick disconnect seat retention mechanism on certain models of the Piper PA-34 aircraft, mandating inspections to ensure compliance within specified time frames. This directive was issued by the Civil Aviation Safety Authority, aiming to mitigate risks and maintain high safety standards in civil aviation. The enacting body of the Civil Aviation Regulations 1998 is the Australian Parliament, with the intent to safeguard public safety by establishing stringent aviation safety regulations. The policy objective behind AD/PA-34/18, as with all ADs, is to ensure the continued airworthiness of aircraft through timely and effective safety interventions. By requiring inspections of the seat retention mechanism within 100 hours after the specified date, the directive aims to prevent potential safety hazards and maintain the integrity of the aircraft's operation.

Scope and Application

The Civil Aviation Regulations 1998, specifically PART 39 - 105, applies to the Piper PA-34 (Seneca) Series Aeroplanes, encompassing models PA-34-200 with serial numbers ranging from 34-7250001 to 34-7450220 and PA-34-200T with serial numbers from 34-7570001 to 34-7570054. This regulation is part of the broader framework managed by the Civil Aviation Safety Authority (CASA) and is designed to ensure the safety and airworthiness of these aircraft types. The directive mandates compliance within 100 hours of time in service after 30 January 1976, as outlined in Piper Service Letter No. 763. The regulation is applicable nationally within the Commonwealth of Australia and applies to all aircraft falling within the specified serial number ranges. There are no stated exclusions or exemptions in this directive, but compliance is mandatory for the listed aircraft models within the specified parameters. Subordinate instruments may further detail implementation and enforcement of these safety directives.

Key Provisions

The key provisions of the Civil Aviation Regulations 1998, particularly in relation to the Piper PA-34 (Seneca) Series Aeroplanes, are set out in Part 39 - 105. Specifically, Airworthiness Directive (AD) AD/PA-34/18 pertains to the quick disconnect seat retention mechanism and requires an inspection of this component. The directive applies to Model PA-34-200 with serial numbers (S/Nos.) ranging from 34-7250001 to 34-7450220, and Model PA-34-200T with S/Nos. from 34-7570001 to 34-7570054. Compliance with this directive is mandatory and must be completed within 100 hours of time in service after 30 January 1976. The obligations imposed by AD/PA-34/18 include conducting a thorough inspection of the quick disconnect seat retention mechanism as specified in Piper Service Letter No. 763. Operators of these aircraft are required to ensure that the inspection is carried out by a qualified individual and that any identified issues are rectified in accordance with the manufacturer's guidelines. This is essential to maintain the airworthiness of the aircraft and ensure the safety of all passengers and crew. Failure to comply with AD/PA-34/18 can result in serious consequences. Civil Aviation Safety Authority (CASA) regulations outline that non-compliance with airworthiness directives can lead to enforcement actions. These may include administrative penalties, such as fines, and in severe cases, the grounding of the aircraft until compliance is achieved. Additionally, operators may face criminal charges if their negligence results in an aviation accident or incident. The maximum penalties for these offences can be substantial, reflecting the gravity of ensuring aircraft safety. The enforcement of these regulations is crucial in maintaining the high safety standards expected in the aviation industry. CASA has the authority to conduct audits and inspections to ensure compliance with airworthiness directives. Any identified non-compliance can lead to immediate corrective actions being mandated, including potential suspension of operations if the safety risk is deemed significant. Operators must stay informed and proactive in adhering to these directives to avoid any legal repercussions and ensure the continued safety of their operations.

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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.