AD/AMD 50/18 - Frame 25 Water Drainage

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Legislation au F2006B02384 In force Legislative Instrument

Legislation content

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


AMD Falcon 50 and 900 Series Aeroplanes

 

AD/AMD 50/18 Frame 25 Water Drainage 13/99

Applicability: MF 900 S/n 1 to 177 and F900 EX S/n 1 to 41.

 

Requirement: Modify in accordance with Dassault Aviation SB MF900-232 or F900EX-093 as appropriate.

 

Note: DGAC AD 1999-446-028(B) refers.

 

Compliance: Before 30 June 2000.

 

This Airworthiness Directive becomes effective on 30 December 1999.

 

Background:  Manufacturer flight testing revealed that water does not drain properly through the Frame 25 filter and if it froze could lead to jamming of the flight controls.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Australian Parliament, serve as the primary regulatory framework for civil aviation within Australia, aiming to ensure the safety and efficiency of the nation's airspace. One specific legislative instrument under this Act is F2006B02384, which pertains to Airworthiness Directives for particular aircraft types. The problem this directive addresses is the improper drainage of water in the Frame 25 filter of Falcon 50 and 900 Series aeroplanes, a defect identified by the manufacturer through flight testing. If water accumulates and subsequently freezes, it could potentially lead to jamming of the flight controls, thereby compromising the safety of the aircraft. This directive mandates that modifications be made in accordance with the relevant Dassault Aviation Service Bulletins, and it requires compliance before 30 June 2000, with the directive becoming effective on 30 December 1999. The policy objective underpinning this regulation is to mitigate safety risks associated with the identified defect, ensuring that aircraft maintain the necessary standards of airworthiness and operational safety. The enactment and enforcement of such directives are overseen by the Civil Aviation Safety Authority, which plays a crucial role in overseeing compliance and ensuring the continued safety of civil aviation in Australia.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105 under the Civil Aviation Safety Authority Schedule of Airworthiness Directives, pertains to the maintenance and safety compliance of Falcon 50 and 900 Series aeroplanes. This legislation applies to all aircraft within the specified serial numbers, including those identified as MF 900 with serial numbers 1 to 177 and F900 EX with serial numbers 1 to 41. The directive mandates that modifications be made in accordance with Dassault Aviation Service Bulletins MF900-232 or F900EX-093 as appropriate. This requirement is grounded in the need to address the issue of water drainage, where improper drainage through Frame 25 filter could potentially lead to frozen water, resulting in jammed flight controls. Compliance with these directives is mandatory, with an effective deadline of 30 June 2000, although the Airworthiness Directive itself became effective on 30 December 1999. This directive is part of a broader safety regulation framework overseen by the Civil Aviation Safety Authority, ensuring that all applicable aircraft maintain the highest standards of safety and operational integrity.

Key Provisions

The Civil Aviation Regulations 1998, specifically under Part 39, Section 105, includes an Airworthiness Directive (AD) concerning the maintenance and modifications of Falcon 50 and 900 Series Aeroplanes. This AD, identified as AD/AMD 50/18, pertains to a critical issue related to the water drainage system of these aircraft models. The requirement outlined in this AD (section 1) is that the aircraft must be modified in accordance with Dassault Aviation Service Bulletins MF900-232 for the MF 900 and F900EX-093 for the F900EX series, as appropriate. This modification is intended to rectify a problem where water does not drain properly through the Frame 25 filter, which could potentially freeze and lead to jamming of the flight controls. The directive imposes obligations on aircraft operators and maintenance personnel to ensure that the required modifications are implemented. Specifically, it mandates that the modifications be carried out before a specified compliance deadline, in this case, before 30 June 2000. The AD became effective on 30 December 1999, indicating that operators must have been aware of and initiated the compliance process within this timeframe. The compliance requirement is crucial to maintaining the airworthiness and safety of these aircraft, as it addresses a potential safety hazard that could compromise flight operations. Breach of the requirements outlined in this AD could lead to serious consequences. While the specific penalties are not detailed in the legislative instrument, failure to comply with airworthiness directives in Australia can result in severe penalties under the Civil Aviation Act 1988. This may include fines, imprisonment, or both, depending on the severity of the breach and the impact on aviation safety. Additionally, non-compliance could lead to the grounding of affected aircraft, which would significantly affect operational capabilities and potentially result in civil or criminal liability for the operator. Therefore, it is imperative that all stakeholders adhere strictly to the directives to avoid these adverse outcomes.

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.