COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Cessna 206 Series Aeroplanes
AD/CESSNA 206/15 Right Hand Wing Rear Spar 10/73
Applicability: All models with S/Nos. P206-0486 and subsequent. Requirement: Action in accordance with Cessna SL SE73-19.
Compliance: Within 100 hours time in service after 31 October 1973.
Overview
The Civil Aviation Regulations 1998, amended through F2006B05220, addresses specific issues related to the airworthiness of the Cessna 206 Series aeroplanes, particularly focusing on the right-hand wing rear spar. This legislative instrument was enacted to ensure the safety and compliance of civil aviation operations by establishing specific directives for maintaining and modifying certain aircraft components. The Australian Government, through the relevant civil aviation authorities, introduced this regulation to mitigate risks associated with the identified structural issues in the specified Cessna models, ensuring that these aircraft meet stringent safety standards. The policy objective is to mandate timely and effective actions for compliance, thereby enhancing the overall safety of civil aviation in Australia.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105 under the Civil Aviation Safety Authority Schedule of Airworthiness Directives, pertains to Cessna 206 Series aeroplanes and mandates compliance with Airworthiness Directive AD/CESSNA 206/15, which addresses the right-hand wing rear spar. This directive applies to all Cessna 206 models with serial numbers P206-0486 and subsequent, necessitating action in accordance with Cessna Service Letter SL SE73-19. Compliance is required within 100 hours of time in service following 31 October 1973. The regulation is a Commonwealth instrument, thus it has a national jurisdictional reach and applies to all relevant aircraft within Australia, irrespective of state or territory boundaries. There are no stated exclusions, exemptions, or thresholds within the primary text of the directive itself; however, the scope and specific details of compliance may be further elaborated upon through subordinate instruments or additional advisories issued by the Civil Aviation Safety Authority.
Key Provisions
The Civil Aviation Regulations 1998, specifically in Part 39 - 105, detail the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives for the Cessna 206 Series Aeroplanes. A critical directive, AD/CESSNA 206/15, pertains to the right-hand wing rear spar of all models with serial numbers P206-0486 and subsequent (Section 10/73). This directive requires action to be taken in accordance with Cessna Service Letter SE73-19 (Section 10/73). Compliance with this directive is mandatory and must be completed within 100 hours of time in service after 31 October 1973 (Section 10/73).
The obligations under this directive are clear and stringent. Operators of the Cessna 206 Series Aeroplanes with the specified serial numbers must adhere to the actions outlined in Cessna Service Letter SE73-19, which likely includes detailed inspection, maintenance, or repair procedures for the right-hand wing rear spar. This ensures that the aircraft meets the necessary safety standards set by CASA. It is imperative that these actions are taken within the prescribed timeframe to maintain airworthiness and comply with regulatory requirements.
Failure to comply with AD/CESSNA 206/15 can result in serious consequences. CASA enforces strict measures for non-compliance with airworthiness directives. Operators found in breach of these directives may face penalties, including fines or other sanctions. The specific penalties are not detailed in the excerpt, but they can include administrative penalties, as well as potential criminal charges if the breach leads to safety incidents. Such consequences underscore the importance of adhering to CASA's directives to ensure the safety and compliance of aircraft operations.