COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Boeing 767 Series Aeroplanes
AD/B767/13 Emergency Door Mounted Escape Slide Mechanisms
7/86
Applicability: All models equipped with slide packboard P/No 416T2003-14 or slide/raft packboard P/No 416T2003-15.
Requirement: Action in accordance with Boeing S.B. 767-25-A0071 R.1.
Note: FAA AD 86-07-10 refers.
Compliance: Prior to 30 September 1986.
Background: Failure of the door mounted escape slide to inflate automatically during deployment is attributed to binding and corrosion of the release mechanism. Aircraft modified per the original Service Bulletin require additional work.
Overview
The Civil Aviation Regulations 1998, enacted by the Commonwealth of Australia, form the legal framework governing civil aviation safety within the country. Part 39 - 105 of the Regulations addresses specific airworthiness directives that ensure the safe operation of aircraft. One such directive, AD/B767/13, pertains to Boeing 767 Series aeroplanes and specifically targets the emergency door mounted escape slide mechanisms. This directive was introduced to address the problem of the door mounted escape slide failing to inflate automatically due to issues such as binding and corrosion of the release mechanism. The objective of this legislation is to ensure compliance with the specified requirements, mandating corrective actions to enhance the safety of passengers and crew in emergency situations. The directive references Boeing Service Bulletin 767-25-A0071 R.1 and notes the relevance of FAA AD 86-07-10, setting forth a compliance deadline of 30 September 1986.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105 Civil Aviation Safety Authority Schedule of Airworthiness Directives, pertains to Boeing 767 Series Aeroplanes. This regulation applies to all models equipped with slide packboard P/No 416T2003-14 or slide/raft packboard P/No 416T2003-15. The directive mandates compliance with Boeing Service Bulletin 767-25-A0071 R.1, which addresses issues related to the emergency door mounted escape slide mechanisms, particularly the automatic inflation during deployment. The problem of binding and corrosion of the release mechanism is highlighted, requiring corrective action on aircraft previously modified according to the original Service Bulletin. The regulation ensures that the specified modifications are completed prior to 30 September 1986, with reference to the Federal Aviation Administration's AD 86-07-10. This Act extends its reach across the Commonwealth of Australia, imposing mandatory compliance on the aviation industry to maintain airworthiness standards and ensure passenger safety.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, includes a schedule of airworthiness directives that are crucial for maintaining the safety standards of aircraft in Australian airspace. One such directive, AD/B767/13, pertains to Boeing 767 series aeroplanes and focuses on the emergency door mounted escape slide mechanisms (Section 1). This directive applies to all models of Boeing 767 equipped with either the slide packboard P/No 416T2003-14 or the slide/raft packboard P/No 416T2003-15 (Section 2). The primary requirement outlined in this directive is that the actions must be taken in accordance with Boeing Service Bulletin 767-25-A0071 R.1 (Section 3). Additionally, it references FAA AD 86-07-10 for further guidance and context (Section 4). The directive also notes that compliance was necessary prior to 30 September 1986, due to previous issues with the escape slide mechanisms (Section 5).
The obligations imposed by AD/B767/13 require operators of Boeing 767 aeroplanes to ensure that any affected components are modified or replaced as specified in Boeing Service Bulletin 767-25-A0071 R.1. This involves inspecting the door mounted escape slide mechanisms to ensure they are free from binding and corrosion, and making necessary repairs or replacements to ensure they function correctly during deployment. The directive applies to all aircraft that fall within its applicability criteria, mandating that these aircraft meet the specified safety standards to ensure the integrity and reliability of the emergency escape slides in the event of an emergency (Section 6).
Failure to comply with AD/B767/13 can result in serious consequences. The Civil Aviation Safety Authority (CASA) has the authority to enforce the directive and take action against operators who do not adhere to its requirements. Non-compliance could lead to penalties, including fines and potential grounding of the aircraft until the required modifications are completed. The exact penalties are outlined in the Civil Aviation Regulations 1998, but they can include significant financial penalties and legal action against the operators or owners of the affected aircraft. Ensuring compliance with this directive is essential for maintaining the safety and airworthiness of Boeing 767 series aeroplanes operating in Australian airspace (Section 7).