COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
SAAB Safir Series Aeroplanes
AD/SAAB/1
Amdt 1
Retirement Life - Critical Components 5/95
Applicability: All Saab Safir 91B, 91B-2, 91C and 91D.
Requirement: Inspect, check and retire structure and components in accordance with Saab Service Bulletin (SB) 91.1.005 Revision 2.
Note: Swedish LFV SAD 1-058 Revision B refers.
Compliance: Effective 30 May 1995.
Background: This Amendment references the latest issue of the applicable Service Bulletin which has superseded Saab SB’s 91.1.003 and 91.3.001.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, serve to regulate civil aviation safety and include a schedule of airworthiness directives. One such directive, AD/SAAB/1Amdt 1, pertains specifically to the Saab Safir Series aeroplanes, namely the 91B, 91B-2, 91C, and 91D variants. This amendment addresses the problem of ensuring the continued airworthiness of critical components within these aircraft by mandating inspections, checks, and retirements in alignment with the Saab Service Bulletin (SB) 91.1.005 Revision 2, thereby filling a gap in the safety oversight of these aircraft models. The policy objective is to maintain and enhance aviation safety by enforcing stringent checks and adherence to the latest service bulletins.
Scope and Application
The Saab Safir Series Aeroplanes Airworthiness Directives, as specified in the Civil Aviation Regulations 1998, apply to all Saab Safir 91B, 91B-2, 91C, and 91D aircraft. This regulation mandates that operators of these aircraft must inspect, check, and retire specific structural components and elements in accordance with the guidelines set out in Saab Service Bulletin (SB) 91.1.005 Revision 2, with reference to Swedish LFV SAD 1-058 Revision B. This directive is a critical component of ensuring the airworthiness and safety of Saab Safir series aircraft operating within Australian airspace. Compliance with this directive is mandatory and became effective on 30 May 1995, superseding previous Saab Service Bulletins 91.1.003 and 91.3.001. The scope of this directive is limited to the specified Saab Safir aircraft models, and any deviation from the outlined procedures could result in non-compliance with Australian civil aviation safety standards.
The application of this directive is geographically bound to the Australian Commonwealth, governing all aviation activities within its jurisdiction. There are no stated exclusions or exemptions in this directive, and it applies uniformly to all operators of the specified Saab Safir series aeroplanes. The directive extends its reach by referencing subordinate instruments such as the Saab Service Bulletins and Swedish LFV SAD 1-058 Revision B, ensuring that all applicable safety measures and compliance standards are met. Operators must adhere to the specified procedures to maintain the airworthiness of their aircraft, thereby contributing to the overall safety of civil aviation in Australia.
Key Provisions
The key operative sections of the Civil Aviation Regulations 1998, specifically PART 39 - 105, address the requirements for the retirement life of critical components in Saab Safir Series Aeroplanes. According to AD/SAAB/1 Amendment 1, all Saab Safir 91B, 91B-2, 91C, and 91D models are subject to these regulations (Section 39-105). The primary requirement outlined in these sections is the necessity for thorough inspection, checking, and the retirement of specific structural and component parts in compliance with Saab Service Bulletin 91.1.005 Revision 2. This service bulletin provides detailed instructions and procedures that must be followed to ensure the continued airworthiness and safety of these aircraft.
The Act imposes stringent obligations on the operators and maintainers of Saab Safir aircraft. They must adhere to the guidelines set forth in the Saab Service Bulletin 91.1.005 Revision 2, ensuring that the specified components are inspected and checked according to the prescribed schedule. This includes the timely retirement of any parts that no longer meet the required safety standards. Non-compliance with these regulations can result in significant safety risks and potential legal repercussions for the operators. The Swedish LFV SAD 1-058 Revision B also serves as a reference for these directives, further guiding the compliance process.
Failure to comply with the provisions of the Civil Aviation Regulations 1998 can lead to severe consequences. Operators who neglect to adhere to the mandated inspections and retirement procedures risk facing both civil and criminal penalties. The regulations outline that non-compliance with these airworthiness directives can result in penalties that may include substantial fines and potential criminal charges for those responsible. The maximum penalties can vary, but they are designed to ensure that operators take the required safety measures seriously and maintain the highest standards of aircraft safety and reliability.