COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Cessna 185 Series Aeroplanes
AD/CESSNA 185/27 Self Locking Nuts 4/78
Applicability: Model 185 with S/Nos. 18502998 to 18503018. Requirement: Action in accordance with Cessna SL No. SE77-44, Item 1. Compliance: Within 100 hours time in service after 30 April 1978.
Overview
The Civil Aviation Regulations 1998, as amended, are a key component of Australia's aviation safety framework, designed to ensure that all civil aircraft operating within the country adhere to stringent safety standards. Among these regulations is Part 39, which includes a schedule of airworthiness directives specifically targeting various aircraft models, including the Cessna 185 series. One such directive, AD/CESSNA 185/27, pertains to the use of self-locking nuts on Model 185 aircraft with serial numbers ranging from 18502998 to 18503018. This directive was enacted to address specific safety concerns associated with these aircraft models, ensuring that they meet the necessary safety standards set by the Civil Aviation Safety Authority (CASA). The directive requires compliance within 100 hours of time in service after 30 April 1978, aligning with Cessna Service Letter No. SE77-44, Item 1, to rectify identified issues and maintain the airworthiness of the aircraft.
Scope and Application
The Civil Aviation Regulations 1998, under Part 39 - 105, pertains to the safety directives for aircraft, specifically addressing the airworthiness of the Cessna 185 series aeroplanes. The regulation applies to a particular subset of this model series, namely those with serial numbers ranging from 18502998 to 18503018. This regulation mandates that these aircraft must adhere to the action specified in Cessna Service Letter No. SE77-44, Item 1, focusing on the use of self-locking nuts. Compliance with this directive is required within 100 hours of time in service following 30 April 1978. The regulation is a specific mandate issued by the Civil Aviation Safety Authority, ensuring that the specified models of Cessna 185 aeroplanes meet necessary safety standards within the stipulated timeframe. This ensures that the aircraft remain airworthy and compliant with safety regulations across the Commonwealth of Australia.
Key Provisions
The Civil Aviation Regulations 1998, under Part 39 - 105, outlines specific requirements for the maintenance and airworthiness of certain aircraft models, including the Cessna 185 Series Aeroplanes. The focus here is on Airworthiness Directive (AD) concerning self-locking nuts, specifically AD/CESSNA 185/27 issued on 4 July 1978. This directive applies to Model 185 aeroplanes with serial numbers ranging from 18502998 to 18503018. The directive mandates that these aircraft must adhere to the actions specified in Cessna Service Letter No. SE77-44, Item 1. This requirement is critical to ensuring the continued airworthiness and safety of the aircraft.
The AD imposes specific obligations on the owners and operators of the affected aircraft. These obligations include ensuring that the self-locking nuts on the aircraft are inspected and, if necessary, replaced or corrected in accordance with the directives outlined in the referenced Cessna Service Letter. The directive requires that these actions be completed within 100 hours of time in service following 30 April 1978, thereby setting a clear and time-bound requirement for compliance. The directive is aimed at addressing specific safety issues identified with the self-locking nuts on these aircraft models, which could potentially compromise the structural integrity and safety of the aeroplanes if left unaddressed.
Failure to comply with the requirements of AD/CESSNA 185/27 can lead to serious legal consequences. The Civil Aviation Regulations 1998 provide for both civil and criminal penalties for non-compliance with airworthiness directives. In the case of civil penalties, operators who fail to comply with the directive may face fines and other sanctions, which can include the grounding of the affected aircraft until the required actions are taken. From a criminal perspective, individuals responsible for the oversight and maintenance of the aircraft who knowingly allow non-compliance can face prosecution, with potential penalties including fines and imprisonment. The exact penalties are detailed within the broader framework of the Civil Aviation Act 1988 and associated regulations, but the overarching principle is to enforce strict compliance to maintain the highest standards of aviation safety.