COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Cessna 210 Series Aeroplanes
AD/CESSNA 210/41 Fuel Flow Stabilisation Placard - Installation
10/79
Applicability: Model 210 with S/Nos. 21057841 to 58220 (with SK205-5 installed) 58221 to 58351
(with SK206-2 installed), 58352 to 63013, 63015 to 63086, 63088 to 63228, 63230 to
63287, 63289 to 63298, 63300 to 63324, 63326 to 63389, 63391 to 63393, 63396 to
63399, 63401, 63403 to 63407, 63412, 63413, 63419, 63424 and 63426. Model T210
with S/Nos. T210-0001 to T210-0454. Model P210 with S/Nos. P21000001 to 00255, 00257 to 00273, 00275 to 00279, 00281 to 00283, 00287, 00290 and 00292.
Document: 1. Cessna SIL No. SE79-25, Supplement No. 1 or 2. FAA AD 79-15-01, Amendment 39-3517.
Compliance: Within 100 hours time in service after 31 October 1979.
Background: The manufacturer has made placards and instructions available to aid in the recognition and elimination of excessive vapour from the aircraft fuel system. In the event of inflight power interruptions engine restart procedures are also detailed.
Overview
The Civil Aviation Regulations 1998, as amended, represent a comprehensive framework designed to ensure the safety and efficiency of civil aviation within Australia. Part 39, in particular, focuses on airworthiness directives, aiming to maintain and improve the safety standards of aircraft operations. One such directive, AD/CESSNA 210/41, addresses the issue of fuel flow stabilisation and placard installation in specific models of Cessna 210 Series aeroplanes. This directive was introduced to mitigate risks associated with in-flight power interruptions and excessive fuel vapour, ensuring that operators of these aircraft adhere to safety protocols that have been established by both Australian and international regulatory authorities. The policy objective is to safeguard flight operations by mandating compliance with specific maintenance actions within a stipulated timeframe.
The directive was enacted by the Civil Aviation Safety Authority, a body under the Commonwealth of Australia, reflecting the national commitment to harmonising aviation safety standards with international best practices. By requiring the installation of a fuel flow stabilisation placard and adherence to detailed procedures for engine restart in the event of power interruptions, the regulation seeks to enhance the operational safety of the affected aircraft models, thereby protecting both crew and passengers.
Scope and Application
The Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, specifically AD/CESSNA 210/41, pertains to the installation of a fuel flow stabilisation placard in certain Cessna 210 series aeroplanes. This directive applies to specific serial numbers of Model 210, Model T210, and Model P210 aeroplanes, all of which must comply with the installation requirements within 100 hours of time in service following 31 October 1979. The directive aims to address issues of excessive vapour in the aircraft fuel system and provides guidance on engine restart procedures in case of inflight power interruptions. This regulation is part of the Civil Aviation Regulations 1998, administered by CASA and applicable across the Commonwealth of Australia, ensuring compliance with safety standards for civil aviation operations within the nation’s airspace.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, which pertains to the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, includes a directive for the Cessna 210 Series Aeroplanes. The directive in question, AD/CESSNA 210/41, mandates the installation of a fuel flow stabilisation placard (section 1). This directive applies to specific serial numbers of Cessna 210 models, including Model 210 with serial numbers ranging from 21057841 to 63426, Model T210 from T210-0001 to T210-0454, and Model P210 from P21000001 to 00292 (section 1). The directive requires compliance within 100 hours of time in service after 31 October 1979.
The directive imposes specific obligations on the parties governed by it. These include ensuring that the aircraft in question is fitted with the appropriate fuel flow stabilisation placard and that the necessary instructions for recognising and addressing excessive vapour from the aircraft fuel system are readily available. Additionally, the directive requires that engine restart procedures in the event of inflight power interruptions are detailed and implemented as outlined by the manufacturer’s documentation (section 1). The directive references Cessna SIL No. SE79-25, Supplement No. 1, or FAA AD 79-15-01, Amendment 39-3517, as the source for these placards and instructions (section 1).
Failure to comply with the requirements set out in AD/CESSNA 210/41 can lead to significant consequences. The legislation does not explicitly state the penalties or consequences for non-compliance, but non-compliance with CASA directives generally can result in severe repercussions under the Civil Aviation Act 1988 and the Civil Aviation Regulations 1988. These can include fines, suspension or revocation of airworthiness certificates, and potential criminal charges. The specific penalties can vary depending on the nature and severity of the breach but can be significant, reflecting the importance of maintaining airworthiness and safety in aviation operations.