COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Eagle X-TS Series Aeroplanes
AD/X-TS/3 Canard Rear Spar Reinforcement 2/2000 TX
Applicability: Models X-TS 150 and 150B serial numbers 001 to 003 and 005 to 030 inclusive. Requirement: Modify the canard rear spar bracket in accordance with Eagle Service Bulletin 1074. Compliance: Within 100 hours time in service after the effective date of this directive.
This Airworthiness Directive becomes effective on 24 December 1999.
Background: This Directive is issued to provide additional strength to the canard rear spar bracket, to enable the aircraft to meet certification requirements.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, serve as the foundational legal framework governing aviation safety within the country. Specifically, Part 39 - 105 within this regulatory body addresses the issuance of Airworthiness Directives, which are imperative for ensuring that civil aircraft meet the necessary safety standards. The Civil Aviation Safety Authority, operating under the authority of this regulation, introduced Airworthiness Directive AD/X-TS/3 to address a specific safety concern regarding the Eagle X-TS Series aeroplanes. This directive was enacted to reinforce the canard rear spar bracket in certain models of the Eagle X-TS Series aeroplanes, thereby ensuring these aircraft could comply with the required certification standards. The policy objective underpinning this directive is to maintain and enhance the safety of civil aviation operations by mandating structural modifications that bolster the integrity of critical aircraft components.
The Airworthiness Directive AD/X-TS/3 applies to Eagle X-TS Series aeroplanes with specific serial numbers, requiring modifications to the canard rear spar bracket in accordance with Eagle Service Bulletin 1074. Compliance with this directive is mandatory within 100 hours of time in service following its effective date of 24 December 1999. This directive underscores the Civil Aviation Regulations' commitment to proactive safety management by addressing potential structural vulnerabilities and ensuring that all regulated aircraft meet stringent safety benchmarks.
Scope and Application
The Civil Aviation Safety Authority (CASA) has issued an Airworthiness Directive (AD) under the Civil Aviation Regulations 1998, specifically within PART 39 - 105, targeting the Eagle X-TS Series Aeroplanes. This directive applies to the canard rear spar reinforcement for models X-TS 150 and 150B, specifically those with serial numbers ranging from 001 to 003 and from 005 to 030 inclusive. The purpose of this directive is to enhance the structural integrity of the canard rear spar bracket, ensuring the aircraft's compliance with certification requirements. This directive mandates that the specified modification must be completed within 100 hours of the aircraft's time in service following the directive's effective date, which is 24 December 1999. Compliance with this directive is overseen by CASA, ensuring that the specified modifications are implemented to maintain the safety standards of the affected aircraft.
Key Provisions
The Civil Aviation Regulations 1998, Part 39 - 105, particularly within the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, contains several critical provisions aimed at ensuring the safety and compliance of specific aircraft models. One such directive, AD/X-TS/3 dated 2 February 2000, pertains to the Eagle X-TS Series Aeroplanes, specifically models X-TS 150 and 150B with serial numbers ranging from 001 to 003 and 005 to 030 inclusive (Section 1). This directive mandates the modification of the canard rear spar bracket in accordance with Eagle Service Bulletin 1074 to enhance the structural integrity of the aircraft and ensure it meets the necessary certification requirements (Section 2).
The obligations imposed by this directive require the operators of the specified Eagle X-TS Series Aeroplanes to undertake the prescribed modifications within a specific timeframe. Operators must ensure that the canard rear spar bracket is modified in compliance with the specifications outlined in Eagle Service Bulletin 1074. The directive stipulates that compliance must be achieved within 100 hours of time in service after the effective date of the directive, which was set for 24 December 1999 (Section 3). This timeframe is crucial to maintaining the airworthiness and safety of the aircraft, and failure to meet these requirements could potentially compromise the safety of the operations involving these aircraft.
The consequences of non-compliance with this Airworthiness Directive are significant. If an operator fails to comply with the requirements stipulated in AD/X-TS/3, they may face serious repercussions. Such non-compliance could result in the aircraft being deemed unairworthy, which could lead to grounding of the aircraft until the necessary modifications are completed. Additionally, the operator could be subject to regulatory action by CASA, which may include fines, penalties, or other enforcement actions. The specific penalties are outlined in other sections of the Civil Aviation Regulations, but the overarching intent is to ensure that all operators adhere to the safety directives to prevent any risk to flight safety.