COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Cessna 205 (210-5) Series Aeroplanes
AD/CESSNA 205/15 Fuel Cap Alignment Placard 9/80
Applicability: Model 205 with S/Nos. 641 and 205-0001 to 205-0577. Requirement: Action in accordance with Cessna SIL No. SE 80-59.
Compliance: Within 100 hours time in service after 30 September 1980.
Background: Correct alignment of flush fitting type fuel caps is essential for efficient operation of the fuel tank secondary vent system.
Overview
The Civil Aviation Regulations 1998, specifically within Part 39, include an Airworthiness Directive (AD) aimed at ensuring the safety and efficiency of certain aircraft models. The AD/CESSNA 205/15, which focuses on the alignment of fuel cap placards for the Cessna 205 (210-5) series aeroplanes, was enacted to address the critical need for proper alignment of flush fitting fuel caps. This directive applies to Model 205 with serial numbers ranging from 641 and 205-0001 to 205-0577, and it requires compliance in accordance with the Cessna Service Information Letter (SIL) No. SE 80-59. The requirement is for action to be taken within 100 hours of time in service after 30 September 1980. The directive was issued by the Civil Aviation Safety Authority (CASA) to ensure the operational efficiency of the fuel tank secondary vent system, thereby enhancing overall aviation safety.
Scope and Application
The Civil Aviation Regulations 1998, under Part 39 - 105, specifically the Schedule of Airworthiness Directives, governs the maintenance and operational standards of aircraft within Australia, including the Cessna 205 (210-5) Series Aeroplanes. The directive AD/CESSNA 205/15 mandates compliance for aircraft models 205 with serial numbers ranging from 641 and 205-0001 to 205-0577. This directive requires action in accordance with Cessna SIL No. SE 80-59 to ensure the correct alignment of flush fitting type fuel caps, which is critical for the efficient operation of the fuel tank secondary vent system. Compliance must be achieved within 100 hours of time in service after 30 September 1980. The scope of this regulation extends to all specified aircraft within the defined serial number range, ensuring that they meet the necessary safety standards for airworthiness. This regulation applies nationwide under the Commonwealth of Australia and the Civil Aviation Safety Authority's oversight, with no exclusions or exemptions mentioned in the directive itself, though further details and extensions might be provided in subordinate instruments.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, detail the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives (AD) for various aircraft, including the Cessna 205 (210-5) Series Aeroplanes. The relevant AD for this model is AD/CESSNA 205/15, which pertains to the fuel cap alignment placard (9/80). This AD applies to Model 205 aircraft with serial numbers ranging from 641 to 205-0577, as well as the specific serial number 205-0001 to 205-0577. The directive requires compliance with the action specified in Cessna Service Information Letter (SIL) No. SE 80-59, which mandates proper alignment of the flush fitting type fuel caps. The alignment is crucial for the effective operation of the fuel tank secondary vent system, ensuring the safety and reliability of the aircraft during flight.
The Cessna 205 (210-5) Series Aeroplanes AD/CESSNA 205/15 imposes specific obligations on the operators and owners of affected aircraft. They must ensure that the fuel cap alignment is corrected according to the requirements outlined in Cessna SIL No. SE 80-59. This involves inspecting and, if necessary, adjusting the fuel caps to achieve proper alignment. The compliance must be achieved within 100 hours of time in service after 30 September 1980. Failure to adhere to these directives could compromise the aircraft's operational safety and lead to potential mechanical failures during flight.
Failure to comply with the AD/CESSNA 205/15 can result in significant legal and operational repercussions. While the Civil Aviation Regulations 1998 do not explicitly state maximum penalties for non-compliance, general provisions under the Civil Aviation Act 1988 and associated regulations may apply. Violations of airworthiness directives can lead to enforcement actions by CASA, including fines, grounding of the aircraft, and potentially, criminal charges for negligence. These consequences underscore the importance of adhering to the specified alignment requirements to ensure the safety and airworthiness of the aircraft.