COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
AMD Fan Jet Falcon (Falcon 20/Mystere-Falcon 200) Series Aeroplanes
AD/AMD 20/15 Passenger Door Locking System 8/78
Applicability: All models with S/Nos. 1 to 370, 372 to 376, 378 to 380, 382, 385, 387, 388. Requirement: 1. Inspect the passenger door locking mechanism in accordance with AMD SB No.
604.
2. Modify the passenger door locking mechanism in accordance with with AMD SB No. 615.
3. Further modify the passenger door locking mechanism in accordance with AMD SB No. 616.
Note: Consigne de Navigabilite (French AD) 78-80-12(B) refers.
Compliance: 1. Within 50 hours time in service after 29 June 1978 and thereafter at intervals not exceeding 50 hours time in service until modified.
2. & 3. Before 1 January 1979.
Overview
The Civil Aviation Regulations 1998, enacted by the Australian Parliament, form a crucial part of the regulatory framework governing aviation safety in Australia. This legislation, administered by the Civil Aviation Safety Authority (CASA), aims to ensure the safety and efficiency of civil aviation within Australia. Specifically, Part 39 - 105, concerning the Schedule of Airworthiness Directives, addresses safety issues through specific amendments and modifications. One such amendment, AD/AMD 20/15, pertains to the passenger door locking system for the Fan Jet Falcon (Falcon 20/Mystere-Falcon 200) series aeroplanes. This directive was introduced to address specific safety concerns identified in the locking mechanisms of these aircraft models, ensuring compliance with stringent safety standards. The policy objective is to mitigate risks associated with the passenger door locking system, thereby enhancing the overall safety of air travel.
The AD/AMD 20/15, applicable to certain serial numbers of the Fan Jet Falcon series, mandates a series of inspections and modifications to the passenger door locking mechanism. This requirement includes inspecting the locking mechanism in accordance with AMD SB No.604, and further modifying it in line with AMD SB No. 615 and 616. The directive stipulates compliance within specific timeframes: inspections must be conducted within 50 hours of time in service after 29 June 1978, and modifications must be completed before 1 January 1979. This directive underscores the importance of timely and thorough safety checks and modifications to ensure the continued airworthiness of the affected aircraft.
Scope and Application
The Civil Aviation Regulations 1998, as amended, specifically within Part 39 - 105, establish the Civil Aviation Safety Authority’s Schedule of Airworthiness Directives for ensuring the safety of aircraft operations within Australia. This particular directive pertains to the Fan Jet Falcon (Falcon 20/Mystere-Falcon 200) series aeroplanes and focuses on the passenger door locking system. It applies to all models of these aeroplanes with specific serial numbers, namely from 1 to 370, 372 to 376, 378 to 380, 382, 385, 387, and 388. The regulations mandate a series of inspections and modifications to the passenger door locking mechanisms, with detailed instructions provided in associated Service Bulletins (SB No. 604, 615, and 616). Compliance with these directives is essential, with inspections required within 50 hours of the aeroplanes' time in service following 29 June 1978, and subsequently at intervals not exceeding 50 hours until modifications are completed. Modifications are mandated before 1 January 1979. This directive is applicable nationally, enforcing safety standards across the Commonwealth of Australia.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, detail a schedule of airworthiness directives for various aircraft, including the Fan Jet Falcon (Falcon 20/Mystere-Falcon 200) series aeroplanes. Section AD/AMD 20/15 pertains to the passenger door locking system and applies to all models with specific serial numbers (1 to 370, 372 to 376, 378 to 380, 382, 385, 388, and 387). The requirement set out in this directive is to inspect the passenger door locking mechanism in accordance with AMD Service Bulletin (SB) No. 604, and subsequently modify it according to SB No. 615, and further modify it in line with SB No. 616. It should be noted that the French airworthiness directive, Consigne de Navigabilite (AD) 78-80-12(B), is also relevant.
Compliance with these directives is crucial. For the inspection, it must be completed within 50 hours of time in service after 29 June 1978 and then at intervals not exceeding 50 hours time in service until the mechanism is modified. The modifications specified in SB No. 615 and SB No. 616 must be completed before 1 January 1979. Failure to comply with these directives can lead to serious safety issues and non-compliance with civil aviation regulations.
The obligations imposed by this directive are specific and time-bound. Aircraft operators must ensure that the passenger door locking system is inspected and modified as required by the service bulletins. This includes adhering to the prescribed timelines for inspections and modifications. Operators must also keep records of all inspections and modifications carried out, as these records may be required for verification by the Civil Aviation Safety Authority (CASA).
Failure to comply with the requirements of these airworthiness directives can result in significant consequences. Under the Civil Aviation Act 1988, non-compliance can be considered an offence. The maximum penalties for such offences can include fines and imprisonment. Specifically, individuals can face fines of up to $165,000 and imprisonment for up to two years. Corporations can face even higher fines, up to $825,000. Additionally, the operation of a non-compliant aircraft can lead to CASA taking enforcement actions, such as grounding the aircraft until compliance is achieved.