COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Cessna 210 Series Aeroplanes
AD/CESSNA 210/31 Fuel Reservoir Fitting - Inspection 5/78
Applicability: Model T210 with S/Nos. 21061040 to 21061963. AND: Model T210 with S/No. below 21061040 which has had a fuel reservoir assembly P/N 1216407-( ) replaced with a fuel reservoir originating from Cessna since 1 July 1975.
Requirement: Inspect fuel reservoir upper fitting for correct inside diameter in accordance with Figure 1 of Cessna SL No. SE77-38.
Note: Attention is also drawn to Cessna SL No. SE78-2.
Compliance: Within 100 hours time in service after 31 May 1978.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, represent a comprehensive framework designed to ensure the safety and efficiency of civil aviation within the country. Among its various parts, Part 39 focuses specifically on airworthiness directives, with Regulation 105 detailing the authority of the Civil Aviation Safety Authority (CASA) to issue such directives. This regulation addresses the need for specific safety measures for certain aircraft models, ensuring that they meet required safety standards. The enactment of this legislation was driven by the necessity to establish clear protocols for maintaining and inspecting aircraft to prevent accidents and ensure the safety of passengers and crew.
The legislative instrument F2006B08080, specifically AD/CESSNA 210/31, is an airworthiness directive issued under the authority of Part 39 of the Civil Aviation Regulations 1998. This directive applies to the Cessna 210 Series Aeroplanes, mandating the inspection of the fuel reservoir upper fitting for specific models within the series. The directive aims to ensure that the inside diameter of the fuel reservoir fitting conforms to the specifications outlined in Figure 1 of Cessna Service Letter SE77-38, with compliance required within 100 hours of time in service after 31 May 1978. The policy objective of this directive is to mitigate potential safety risks associated with incorrect fuel reservoir fittings, thereby enhancing the overall safety of air travel.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, which pertains to the Civil Aviation Safety Authority’s Schedule of Airworthiness Directives, applies to certain Cessna 210 series aeroplanes. This particular directive, AD/CESSNA 210/31, targets aircraft of the Model T210 with serial numbers ranging from 21061040 to 21061963, as well as those with serial numbers below 21061040 that have undergone a replacement of their fuel reservoir assembly part number 1216407-( ) with a fuel reservoir from Cessna since 1 July 1975. The directive mandates an inspection of the fuel reservoir upper fitting to ensure it matches the correct inside diameter as detailed in Figure 1 of Cessna Service Letter SE77-38, with additional considerations noted in Service Letter SE78-2. Compliance with this directive is required within 100 hours of the aircraft’s time in service after 31 May 1978. This regulation is enforceable under Commonwealth jurisdiction and applies to entities operating within Australia’s aviation industry, specifically those maintaining or operating the specified Cessna 210 series aeroplanes.
Key Provisions
The Civil Aviation Regulations 1998, particularly Part 39 - 105, mandate specific airworthiness directives for certain aircraft models, including the Cessna 210 series aeroplanes. Section AD/CESSNA 210/31 focuses on the inspection of fuel reservoir fittings for a subset of these aeroplanes. Specifically, it applies to model T210 with serial numbers (S/Nos.) ranging from 21061040 to 21061963, and also to model T210 with serial numbers below 21061040 that have had their fuel reservoir assembly part number (P/N) 1216407-( ) replaced with a fuel reservoir from Cessna since 1 July 1975.
The directive requires a thorough inspection of the fuel reservoir's upper fitting to ensure it has the correct inside diameter as outlined in Figure 1 of Cessna Service Letter (SL) No. SE77-38. The regulation also references Cessna SL No. SE78-2, indicating that further attention should be given to any additional notes or specifications provided in this document. Compliance with this directive must be achieved within 100 hours of the aeroplane's time in service after 31 May 1978.
The obligations imposed by this regulation are clear: operators of the specified Cessna 210 models must ensure that the required inspections are performed by qualified personnel within the stipulated timeframe. Failure to comply with these directives can result in serious consequences, as the regulations are designed to maintain the airworthiness and safety of the aircraft. This includes ensuring that all components meet the specified standards to prevent any potential failures that could compromise flight safety.
In terms of consequences for non-compliance, the Civil Aviation Regulations 1998 do not explicitly detail the penalties within the legislative instrument provided. However, non-compliance with airworthiness directives generally can lead to severe civil and criminal penalties. Civil penalties may include fines, and criminal penalties may involve imprisonment, depending on the severity of the breach and its impact on safety. It is essential for operators to adhere strictly to these directives to avoid any legal repercussions and to ensure the continued safe operation of their aircraft.