AD/CESSNA 206/5 Amdt 2 - Auxiliary Fuel Pump Electrical System

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Legislation au F2006B05255 In force Legislative Instrument

Legislation content

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Cessna 206 Series Aeroplanes

 

AD/CESSNA 206/5

Amdt 2


Auxiliary Fuel Pump Electrical System 12/70

 

Applicability: Model 206 with S/Nos. 206-0001 to 206-0275, Models P206 and TP206 with S/Nos.

P206-0001 to P206-00644, Models U206 and TU206 with S/Nos. U206-0276 to U206-01580.

 

Requirement: Action in accordance with Cessna SL SE69-9 or Cessna SL SE70-25. Compliance:  Within 100 hours time in service after 29 August 1969.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, as amended by AD/CESSNA 206/5 Amendment 2, was enacted to ensure the ongoing airworthiness of specific Cessna 206 series aeroplanes. This legislation was introduced to address issues related to the auxiliary fuel pump electrical system in certain model series, specifically those with serial numbers ranging from 206-0001 to 206-0275 for the Model 206, P206-0001 to P206-00644 for Models P206 and TP206, and U206-0276 to U206-01580 for Models U206 and TU206. The Civil Aviation Safety Authority (CASA) is the enacting body, and the policy objective is to maintain and improve the safety standards of civil aviation through the enforcement of specific airworthiness directives. Compliance with these directives is mandatory, requiring corrective action to be taken within 100 hours of time in service after 29 August 1969, in accordance with Cessna Service Letters SE69-9 or SE70-25.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertains to the authority and application of Airworthiness Directives as issued by the Civil Aviation Safety Authority (CASA). This particular legislative instrument, AD/CESSNA 206/5 Amendment 2, applies to the auxiliary fuel pump electrical system of specific Cessna 206 series aeroplanes. The affected models include the 206 series with serial numbers ranging from 206-0001 to 206-0275, P206 and TP206 series with serial numbers from P206-0001 to P206-0644, and U206 and TU206 series with serial numbers from U206-0276 to U206-01580. The regulation mandates compliance with either Cessna Service Letter SE69-9 or Cessna Service Letter SE70-25, requiring actions to be completed within 100 hours of time in service after the directive was issued on 29 August 1969. This regulation applies across the Commonwealth of Australia and is enforced by CASA, ensuring that all specified aircraft meet the required safety standards. The scope of the regulation is geographically confined to Australia, under the jurisdiction of the Commonwealth, and targets specific entities, namely, aircraft operators who possess and operate the mentioned Cessna 206 series aeroplanes within this jurisdiction. The directive does not specify any exclusions or exemptions but mandates strict adherence to the outlined requirements for airworthiness. Any failure to comply with these regulations could result in penalties or legal repercussions. The regulatory framework may be further extended or specified through subordinate instruments issued by CASA, thereby providing detailed operational guidelines and enforcement mechanisms.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105, and the Schedule of Airworthiness Directives, detail crucial provisions for the maintenance and operation of certain Cessna 206 Series aeroplanes. The relevant section here is AD/CESSNA 206/5 Amendment 2, which focuses on the auxiliary fuel pump electrical system of these aircraft. This directive applies to specific models and serial numbers, namely Model 206 with serial numbers 206-0001 to 206-0275, Models P206 and TP206 with serial numbers P206-0001 to P206-00644, and Models U206 and TU206 with serial numbers U206-0276 to U206-01580. The directive mandates that the auxiliary fuel pump electrical system must be addressed in accordance with either Cessna Service Letter SL SE69-9 or Cessna Service Letter SL SE70-25. Compliance with these directives is mandatory and must be achieved within 100 hours of the aircraft's time in service after 29 August 1969. The regulations impose clear obligations on aircraft owners and operators to ensure that the specified modifications or checks are carried out on the auxiliary fuel pump electrical system. This requirement is critical to maintaining the safety and airworthiness of the aircraft. The onus is on the operators to ensure that all applicable maintenance and modification actions are completed within the specified timeframe to avoid any non-compliance issues. Failure to comply with these directives can lead to serious consequences. The Civil Aviation Safety Authority (CASA) has the authority to enforce the regulations and can take action against non-compliance. Potential penalties for breach of these regulations can include fines, suspension or revocation of the aircraft's certificate of airworthiness, and potential criminal charges. The specific penalties can vary based on the severity of the breach and the circumstances surrounding it, but the seriousness of non-compliance with airworthiness directives underscores the importance of adhering to these requirements. The regulations are designed to protect public safety and ensure that aircraft operate to the highest standards of safety and reliability.

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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.