AD/CESSNA 188/11 - Throttle Bellcrank

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Legislation au F2006B05146 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 188/11 Throttle Bellcrank 4/69

Applicability: All models fitted with P/N 0750163-1 throttle control bellcranks. Requirement: Action in accordance with Supplement 1 of Cessna SL No. SE 68-28.

Note: FAA AD 69-4-2 refers.

 

Compliance: Within 100 hours time in service after 15 April 1969.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, serve as the foundational regulatory framework governing civil aviation safety within the country. This comprehensive set of rules aims to address various aviation safety concerns, ensuring that air travel remains as safe as possible for all passengers and personnel involved. One particular aspect of these regulations, detailed in Part 39 - 105 under the Civil Aviation Safety Authority Schedule of Airworthiness Directives, pertains to specific directives for certain aircraft models. For instance, AD/CESSNA 188/11 focuses on the throttle bellcrank for Cessna 188 (Agwagon) series aeroplanes, requiring compliance with specific maintenance actions as outlined in the related supplement to rectify identified safety issues. The overarching policy objective of these regulations is to mandate stringent safety measures and regular compliance checks to mitigate any potential risks associated with civil aviation operations.

Scope and Application

The Civil Aviation Regulations 1998, under the scope of Part 39 - 105, governs the Airworthiness Directives for specific aircraft models, including the Cessna 188 (Agwagon) Series Aeroplanes. This legislation applies to all Cessna 188 models equipped with a P/N 0750163-1 throttle control bellcrank, mandating compliance with the requirements outlined in Supplement 1 of Cessna Service Letter SE 68-28, which is referenced in FAA AD 69-4-2. The directive necessitates corrective action within 100 hours of the aircraft's time in service after 15 April 1969, ensuring that these aircraft meet the necessary safety standards. The regulation's jurisdiction is federally enforced across the Commonwealth of Australia, impacting all operators of the specified aircraft models within Australian airspace.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105, outlines the requirements and obligations for ensuring the airworthiness of certain aircraft models, including the Cessna 188 (Agwagon) series aeroplanes. The relevant Airworthiness Directive (AD) in question is AD/CESSNA 188/11, which pertains to the throttle bellcrank (section 4/69). This directive applies to all models equipped with a P/N 0750163-1 throttle control bellcrank. The directive mandates that action be taken in accordance with Supplement 1 of Cessna Service Letter (SL) No. SE 68-28, and it references FAA AD 69-4-2 for additional information. Compliance with AD/CESSNA 188/11 requires that the specified action be completed within 100 hours of time in service after 15 April 1969. The requirement is clear: operators of Cessna 188 (Agwagon) aeroplanes must follow the instructions provided in the referenced documents to ensure the safety of the aircraft. This involves adhering to specific maintenance procedures and possibly making modifications to the throttle bellcrank to meet the safety standards set by the Civil Aviation Safety Authority (CASA). It is imperative that these steps are taken to maintain the airworthiness of the aircraft and ensure safe operation. The obligations imposed by AD/CESSNA 188/11 are significant for aircraft operators. They must ensure that the specified action is taken within the stipulated timeframe, which is critical for maintaining the safety and airworthiness of the aircraft. Operators must also keep accurate records of any maintenance or modifications performed in compliance with this directive. These records must be readily available for inspection by CASA to verify compliance. Failure to comply with these obligations can result in serious safety implications and potential regulatory action against the operator. In terms of consequences, failure to comply with AD/CESSNA 188/11 can lead to both civil and criminal penalties. Under the Civil Aviation Act 1988, operators who do not comply with airworthiness directives may face fines, with the maximum penalty for contravening the Civil Aviation Regulations being $21,000 for individuals and $105,000 for corporations. Additionally, CASA has the authority to issue enforcement notices, suspend or cancel airworthiness certificates, and take other regulatory actions against non-compliant operators. It is essential for operators to take these requirements seriously to avoid the severe repercussions associated with non-compliance.

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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.