COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
British Aerospace (Scottish Aviation) Twin Pioneer Series Aeroplanes
AD/SA-TP/10 Main Undercarriage Bracing Strut Shackles NK
Applicability: All models.
Document: Scottish Aviation Mod. No. C598. Compliance: Before 1200 hours component time in service.
Overview
The Civil Aviation Regulations 1998, as amended, are pivotal in regulating aviation safety across Australia. These regulations, enacted by the Australian Parliament, were introduced to address the need for stringent safety standards in civil aviation, ensuring the safety of passengers, crew, and the general public. This particular legislative instrument, F2006B06758, pertains to the airworthiness directives for the British Aerospace (Scottish Aviation) Twin Pioneer Series Aeroplanes. Specifically, it mandates compliance for the main undercarriage bracing strut shackles of all models, with a compliance deadline set before reaching 1200 hours of component time in service. This directive was introduced to mitigate risks associated with the structural integrity of the aircraft's landing gear, thereby enhancing overall flight safety. The policy objective is to maintain high safety standards in line with international best practices, ensuring that all aircraft operating within Australia meet rigorous safety criteria.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertains to Airworthiness Directives issued by the Civil Aviation Safety Authority (CASA) and applies to all aircraft operators within the Commonwealth of Australia. This regulation mandates that all owners and operators of British Aerospace (Scottish Aviation) Twin Pioneer Series aeroplanes must comply with AD/SA-TP/10 concerning the main undercarriage bracing strut shackles, which is documented under Scottish Aviation Modification No. C598. The directive requires compliance before the component reaches 1200 hours of time in service, ensuring that all aircraft maintain the required safety standards and structural integrity. This regulation extends its jurisdictional reach across the entire Commonwealth, applying uniformly to all relevant aircraft and operators. No exclusions or exemptions are specified within the text, indicating that all applicable aircraft must adhere to the directive without exception. The regulation may be further detailed or extended through subordinate instruments issued by CASA.
Key Provisions
The Civil Aviation Regulations 1998, specifically under Part 39 - 105, includes a Schedule of Airworthiness Directives (ADs) that mandates certain safety measures for aircraft, including the British Aerospace (Scottish Aviation) Twin Pioneer Series Aeroplanes. Section AD/SA-TP/10 pertains to the main undercarriage bracing strut shackles, which are critical components of the aircraft’s landing gear. This directive, identified as NK and linked to Scottish Aviation Modification No. C598, requires compliance before the component reaches 1200 hours of time in service.
These airworthiness directives are imperative for ensuring the safety and reliability of the aircraft. Section 39-105(1) necessitates that all relevant aircraft models adhere to the modifications and inspections specified in the ADs. For the Twin Pioneer Series Aeroplanes, this involves ensuring that the main undercarriage bracing strut shackles meet the specified safety criteria before they accumulate 1200 hours of operational time. Failure to comply with these directives can result in the aircraft being grounded until the required modifications are completed.
Entities governed by these regulations, such as aircraft operators and maintenance providers, are obligated to meticulously follow the compliance timelines and requirements set forth in the ADs. This includes conducting regular inspections, performing necessary repairs, and maintaining accurate records of all modifications. Operators must ensure that their aircraft meet the stipulated safety standards to avoid any safety risks and legal repercussions.
Breaching these airworthiness directives can lead to significant consequences, both civil and criminal. Section 39-105(2) stipulates that non-compliance with these directives can result in substantial fines and penalties. The maximum penalties for operating an aircraft that does not meet the required standards can be severe, reflecting the critical nature of air safety. Additionally, the Civil Aviation Safety Authority (CASA) has the authority to impose further administrative actions, including grounding the aircraft, suspension of operational licenses, or even criminal charges against responsible individuals if gross negligence is found.