AD/CESSNA 188/37 Amdt 2 - Aileron Cable Pulley

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Legislation au F2006B05173 Not 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

 


Cessna 188 (Agwagon) Series Aeroplanes

 

AD/CESSNA 188/37

Amdt 2


Aileron Cable Pulley 2/83

 

Applicability: All models with S/Nos. listed in Requirement Documents.

 

Requirement: Action in accordance with Cessna SIL Nos. SE81-2 AG81-1, SE82-19 AG82-1, and SE82-42.

 

Compliance: Unless already accomplished, within 100 hours time in service after 28 February 1983.

 

Background: The manufacturer has advised that incorrect pulleys may have been installed in the aileron circuit. Amendment 2 is issued to extend aircraft serial number effectivity.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, as amended by the legislative instrument F2006B05173, addresses the need for the continuous maintenance and safety of aircraft, particularly focusing on the Cessna 188 (Agwagon) series aeroplanes. This regulation was enacted by the Australian Parliament to ensure the safety and airworthiness of aircraft through specific directives and amendments. The problem this legislation targets is the potential installation of incorrect pulleys in the aileron circuit, which could compromise the safety of the aircraft. The policy objective is to mandate compliance with specified Service Information Letters (SIL) to rectify these issues, ensuring that all affected models adhere to the necessary safety standards within a defined timeframe. This regulation, overseen by the Civil Aviation Safety Authority, sets out the requirements for actions to be taken on certain Cessna 188 series aeroplanes, specifically those with serial numbers listed in the requirement documents. It mandates compliance with specific SILs to rectify issues related to aileron cable pulleys, with the goal of enhancing the safety and reliability of these aircraft. The directive is clear that any required actions must be completed within 100 hours of the aircraft being in service after 28 February 1983, ensuring that all necessary safety measures are implemented in a timely manner.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertains to the Civil Aviation Safety Authority's Schedule of Airworthiness Directives for Cessna 188 (Agwagon) Series Aeroplanes. This regulation applies to all models of the Cessna 188 series with serial numbers listed in the requirement documents. The directive mandates that corrective action be taken on the aileron cable pulley to comply with the manufacturer's Service Information Letters (SILs) Nos. SE81-2 AG81-1, SE82-19 AG82-1, and SE82-42. The required action must be completed within 100 hours of time in service following 28 February 1983, unless it has already been addressed. This amendment extends the serial number effectivity to include additional models, ensuring safety across the specified aircraft fleet. The regulation operates under the Commonwealth of Australia and is administered by the Civil Aviation Safety Authority, which has the jurisdictional authority to enforce compliance across the nation.

Key Provisions

The Civil Aviation Regulations 1998, specifically within Part 39, section 105, address the scheduling of airworthiness directives concerning various aircraft, including the Cessna 188 (Agwagon) series aeroplanes. This section mandates the adherence to specific airworthiness directives to ensure safety and compliance with aviation standards. One such directive, AD/CESSNA 188/37 Amendment 2, pertains to the aileron cable pulley, requiring actions according to the Cessna Service Information Letters (SIL) Nos. SE81-2, AG81-1, SE82-19, AG82-1, and SE82-42. The directive applies to all models of the Cessna 188 series with serial numbers listed in the requirement documents, necessitating compliance within 100 hours of time in service after 28 February 1983, unless already addressed. The Civil Aviation Regulations impose specific obligations on operators of Cessna 188 series aeroplanes to ensure that the aileron cable pulley is correctly installed as per the specified service information letters. Operators must conduct a thorough inspection and, if necessary, replace the pulleys to rectify any issues identified by the manufacturer. This requirement ensures that the aircraft remains airworthy and safe for operation, complying with the regulatory standards set forth by the Civil Aviation Safety Authority. Failure to comply with the airworthiness directives can result in significant consequences. Under the Civil Aviation Regulations, non-compliance with airworthiness directives can lead to enforcement actions, including fines and potential grounding of the aircraft. The maximum penalties for non-compliance are not explicitly stated in the directive but may include substantial fines as per the Civil Aviation Act 1988, which governs civil aviation safety in Australia. Additionally, continued operation of an aircraft that does not meet airworthiness standards can result in criminal charges against the operator, leading to imprisonment and further legal repercussions.

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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.