AD/PA-36/11 - Muffler Clamp - Installation

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Legislation au F2006B05928 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

 


Piper PA-36 (Pawnee Brave) Series Aeroplanes

 

AD/PA-36/11 Muffler Clamp - Installation 5/76

Applicability: Model PA-36-285 with S/Nos. 36-7360001 to 36-7560110. Document:  Piper SB No. 489.

Compliance: Within 100 hours time in service after 31 May 1976.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, amended by the Legislative Instrument F2006B05928, introduce specific directives to enhance the safety standards of civil aviation in Australia. This legislation, enacted by the Australian Parliament, aims to fill gaps in safety protocols by providing detailed directives for aircraft maintenance and operational standards. Specifically, the regulations address issues related to the installation and compliance of muffler clamps on Piper PA-36 (Pawnee Brave) Series aeroplanes, particularly for models PA-36-285 with serial numbers ranging from 36-7360001 to 36-7560110. The policy objective is to ensure that these aircraft meet necessary safety standards, thereby reducing the risk of mechanical failures and enhancing overall aviation safety. This legislative instrument mandates compliance within 100 hours of time in service after 31 May 1976, as referenced in Piper Service Bulletin No. 489. The regulations are part of the broader schedule of airworthiness directives managed by the Civil Aviation Safety Authority, reinforcing the commitment to maintaining high safety standards across the Australian aviation industry.

Scope and Application

The Civil Aviation Safety Authority (CASA) is responsible for the administration and enforcement of the Civil Aviation Regulations 1998, which include specific Airworthiness Directives (AD) for various aircraft models. One such AD, AD/PA-36/11, pertains to the installation of a muffler clamp on Piper PA-36 (Pawnee Brave) Series Aeroplanes. This particular directive applies to aircraft model PA-36-285 with serial numbers ranging from 36-7360001 to 36-7560110, and the compliance deadline is set within 100 hours of time in service after 31 May 1976. The directive is applicable nationwide within the Commonwealth of Australia, and it is enforced by CASA to ensure the airworthiness and safety standards of the specified aircraft are maintained. This AD is a critical component of aviation safety regulations, ensuring that specific modifications are implemented to prevent potential hazards and maintain the operational integrity of the aircraft.

Key Provisions

The main sections of AD/PA-36/11 focus on the specific requirements for the installation of muffler clamps on the Piper PA-36 (Pawnee Brave) series aeroplanes. Section 39.105(1) outlines the applicability of the directive, which applies to aircraft models PA-36-285 with serial numbers ranging from 36-7360001 to 36-7560110. This directive is based on Piper Service Bulletin No. 489 and must be complied with within 100 hours of the aircraft's time in service after 31 May 1976. The directive requires the installation of specified muffler clamps to ensure the safety and airworthiness of the aircraft. The obligations imposed by this directive include ensuring that the specified muffler clamps are correctly installed on the applicable aircraft models within the prescribed timeframe. This involves thorough checks and documentation to confirm compliance. The responsible parties, which could include aircraft owners, operators, and maintenance personnel, must adhere to the specifications provided in Piper Service Bulletin No. 489 to meet regulatory requirements. It is essential that all modifications are carried out by qualified personnel and that records of the installation are maintained and readily available for inspection. Failure to comply with the requirements of AD/PA-36/11 can lead to significant consequences. Under section 39.105(2), non-compliance may result in the aircraft being deemed unairworthy. This could lead to enforcement actions by the Civil Aviation Safety Authority (CASA). The potential penalties for non-compliance include fines and, in severe cases, the suspension or revocation of the aircraft's airworthiness certificate. These penalties are intended to ensure that safety standards are upheld and that the risk of in-flight incidents due to mechanical failure is minimised.

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Area of Law
Aviation Law
Instrument
Regulation
Concepts
Definitions & Interpretation
Compliance Obligations
Regulatory Standards

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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.