COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Boeing 727 Series Aeroplanes
AD/B727/140 Body Station 950 Side Fitting 7/92
Applicability: Model 727 series, listed in Boeing SB 27-53-0126 Revision 6.
Requirement: Action IAW the technical requirements of FAA AD 92-06-14 Amdt 39-8194.
Note: Boeing SB 727-53-0196 and SB 727-53-0126 Revision 6 refer.
Compliance: As specified in the Requirement Document with a revised effective date of 25 June 1992.
Background: The FAA has received reports of cracks and web separations of the BS 950 side fitting. The actions specified in this directive are intended to prevent failure of the fitting and subsequent depressurisation of the aircraft.
Overview
The Civil Aviation Regulations 1998, enacted by the Australian Parliament, are designed to ensure the safety of civil aviation within Australia. Specifically, Part 39 - 105 of these regulations, which pertains to the Civil Aviation Safety Authority’s schedule of airworthiness directives, addresses safety concerns and mandates compliance with international standards, such as those set by the Federal Aviation Administration (FAA). One such directive, AD/B727/140, targets the Boeing 727 series aeroplanes, focusing on the body station 950 side fitting. This directive was introduced to address the problem of cracks and web separations reported in the side fittings, which could lead to aircraft depressurisation. The policy objective is to ensure the airworthiness of these aircraft by requiring compliance with the technical requirements of FAA AD 92-06-14 Amendment 39-8194, with reference to Boeing Service Bulletins SB 727-53-0196 and SB 727-53-0126 Revision 6.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, addresses airworthiness directives for aircraft, including the Boeing 727 series aeroplanes. This legislation applies to aircraft models within the specified series and mandates compliance with the technical requirements outlined in the Federal Aviation Administration's Airworthiness Directive AD 92-06-14 Amendment 39-8194. The directive requires action to address issues such as cracks and web separations of the Body Station 950 side fitting, as referenced in Boeing Service Bulletins 727-53-0196 and 727-53-0126 Revision 6. Compliance with these directives is crucial to prevent potential failure of the fitting and subsequent depressurisation of the aircraft, ensuring the safety of all passengers and crew. The regulations extend to all operators of Boeing 727 series aeroplanes within the Commonwealth of Australia, ensuring adherence to the specified technical requirements and safety standards.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, which pertains to the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, contains AD/B727/140. This directive applies to Boeing 727 series aeroplanes, as detailed in Boeing Service Bulletin (SB) 27-53-0126 Revision 6. The directive mandates actions in accordance with the technical requirements outlined in Federal Aviation Administration (FAA) AD 92-06-14 Amendment 39-8194. Boeing SB 727-53-0196 and SB 727-53-0126 Revision 6 provide further reference. Compliance with the directive is to be achieved as specified in the requirement document, with a revised effective date of 25 June 1992.
The directive imposes specific obligations on the operators of Boeing 727 series aeroplanes. These obligations include the requirement to inspect, repair, or replace the Body Station 950 side fitting as per the detailed technical instructions provided by the FAA. The directive is designed to address reports of cracks and web separations in the specified fitting, which could lead to failure and subsequent depressurisation of the aircraft. Operators must ensure that their maintenance and inspection programs incorporate the actions specified in FAA AD 92-06-14 Amendment 39-8194, ensuring that the fitting is maintained in an airworthy condition.
Failure to comply with the provisions of this directive can result in serious consequences. Non-compliance with airworthiness directives is a breach of the Civil Aviation Regulations 1998. Such breaches can lead to enforcement actions by CASA, which may include fines, suspension, or revocation of the aircraft’s Certificate of Airworthiness. In severe cases, criminal charges may be laid against individuals or corporations responsible for the non-compliance. The maximum penalties for contravening these regulations can be substantial, reflecting the critical nature of maintaining airworthiness standards to ensure the safety of all passengers and crew.
Civil Aviation Regulations 1998 also detail the penalties for non-compliance. The Act provides for both civil and criminal penalties, with the specific consequences depending on the nature and severity of the breach. For civil penalties, CASA can issue infringement notices or impose fines. In more serious cases, the penalties can extend to substantial fines and potential imprisonment for individuals involved in the breach. The criminal penalties are intended to act as a deterrent and to ensure that all parties involved in the operation of aircraft adhere strictly to the safety requirements set out in the regulations. The overarching aim is to maintain the highest standards of safety in civil aviation.
In conclusion, the Civil Aviation Regulations 1998, Part 39 - 105, through AD/B727/140, mandates specific actions for the maintenance of Boeing 727 series aeroplanes to prevent depressurisation due to fitting failure. Operators are obligated to follow the FAA’s technical requirements and ensure compliance by the effective date. Failure to adhere to these provisions can result in severe civil and criminal penalties, reinforcing the importance of strict adherence to airworthiness directives for the safety of all involved in aviation operations.