COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Cessna 188 (Agwagon) Series Aeroplanes
AD/CESSNA 188/27 Fuel Quantity Placard 4/76
Applicability: As detailed in Requirement Document.
Requirement: Install fuel quantity placards as detailed in Cessna SL SE75-7 and Supplement No. 1.
Compliance: 1. Model A188 with S/Nos. as detailed in Cessna SL SE75-7 within 100 hours time in service after 16 April 1976.
2. Model A188 with S/Nos. prior to 01347:
(a) If currently fitted with one or more replacement fuel cells bearing a manufacturing date of June 1973 or later -within 100 hours time in service after 16 April 1976.
(b) Concurrent with fitting one or more replacement fuel cells bearing a manufacturing date of June 1973 or later.
Overview
The Civil Aviation Regulations 1998, amended through legislative instrument F2006B05162, was enacted to ensure the safe operation of civil aircraft within Australian airspace. This particular update, concerning Cessna 188 (Agwagon) series aeroplanes, was introduced to address potential safety risks associated with the aircraft's fuel system. Specifically, it targets the installation of fuel quantity placards as outlined in Cessna Service Letter SL SE75-7 and its supplement, to ensure pilots have accurate and readily available information about fuel levels. This directive is enforced by the Civil Aviation Safety Authority under the authority of the Australian Parliament, with a clear policy objective of enhancing aviation safety by mitigating risks associated with fuel management.
The compliance requirements set forth in the regulations mandate that certain models of Cessna 188 aeroplanes must install the specified fuel quantity placards within a defined timeframe following the directive's issuance on 16 April 1976. This includes models with specific serial numbers and conditions relating to replacement fuel cells, ensuring that all affected aircraft adhere to these safety standards. The overarching goal of these regulations is to maintain high safety standards within the civil aviation sector, thereby protecting both the aircraft's occupants and the broader flying public.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertains to the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, which applies to ensuring the safety of aircraft within Australia. In this context, the regulation concerns the Cessna 188 (Agwagon) Series Aeroplanes and mandates the installation of fuel quantity placards as per the detailed requirements in Cessna SL SE75-7 and Supplement No. 1. The applicability of these directives is narrowly tailored to certain models and serial numbers of the Cessna 188 aeroplanes. Compliance with these directives is mandatory for aircraft within the specified criteria, with particular attention to installation timelines contingent on the aeroplane’s serial number and the date of manufacture of any replacement fuel cells. These regulations ensure that only certain configurations of the Cessna 188 series are subject to the requirement of installing the fuel quantity placards, which is crucial for maintaining safety standards in civil aviation within Australia.
Key Provisions
The Civil Aviation Regulations 1998, specifically under Part 39 - 105, include an Airworthiness Directive (AD) for Cessna 188 (Agwagon) series aeroplanes, titled AD/CESSNA 188/27. This directive mandates the installation of fuel quantity placards as per the requirements detailed in Cessna Service Letter (SL) SE75-7 and its Supplement No. 1. The directive's applicability and compliance details are outlined to ensure the safety and airworthiness of the aircraft.
According to section 39 - 105, model A188 aircraft with specific serial numbers must install the fuel quantity placards within a specified timeframe. For aircraft with serial numbers as detailed in Cessna SL SE75-7, the installation must be completed within 100 hours of time in service after 16 April 1976. For model A188 aircraft with serial numbers prior to 01347, the compliance requirements are slightly different. If these aircraft are already equipped with replacement fuel cells manufactured on or after June 1973, the placards must be installed within 100 hours of time in service following 16 April 1976. Additionally, if replacement fuel cells manufactured on or after June 1973 are installed, the fuel quantity placards must be fitted concurrently with these cells.
The AD imposes specific obligations on the parties governed by the Civil Aviation Regulations. Operators and owners of the affected Cessna 188 aircraft must ensure that the fuel quantity placards are installed in accordance with the detailed requirements of the directive. This includes verifying the serial numbers of the aircraft and ensuring that any replacement fuel cells meet the specified manufacturing dates. The directive ensures that these placards are visible and correctly installed, contributing to the safe operation of the aircraft.
Failure to comply with the AD/CESSNA 188/27 could result in serious safety risks, potentially leading to operational non-compliance and regulatory penalties. While the Civil Aviation Regulations do not explicitly detail penalties in this specific directive, general provisions within the Civil Aviation Act 1988 could apply. Penalties for non-compliance with airworthiness directives could include fines and potential grounding of the aircraft until compliance is achieved. The seriousness of non-compliance underscores the importance of adhering to the specified requirements to maintain the safety standards mandated by the Civil Aviation Safety Authority.