COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Aerospatiale (Socata) TB 200 Series Aeroplanes
AD/TB 200/1 Fuel System - Flowmeter Pipe Integrity 9/99
Applicability: All Socata TB 200 aircraft not equipped with SOCATA Modification No. 150 (Fuel Flowmeter Pipe).
Requirement: 1. Check the tightness of the fuel flowmeter pipe in accordance with SOCATA SB No. 10-108-73 Rev 1, dated March 1999.
2. Replace the fuel flowmeter pipe (SOCATA Mod 150) according to SOCATA SB No. 10-108-73 Rev 1, dated March 1999.
Note: DGAC 1999-061(A)R1 dated 05 May 1999 refers.
Compliance: 1. Within the next 10 flight hours after the effective date of this Directive and thereafter at every scheduled aircraft inspection.
2. Within 150 hours after the effective date of this directive, or 9 December 1999, whichever occurs first.
This Airworthiness Directive becomes effective on 9 September 1999.
Background: The measures outlined in this Directive are deemed necessary to ensure the integrity of the fuel flowmeter pipe and reflect the Country of Origin Airworthiness Authority’s requirements.
Overview
The Civil Aviation Regulations 1998, enacted by the Commonwealth of Australia, serve to ensure safety and compliance within the civil aviation sector. One particular legislative instrument, F2006B07268, introduces specific airworthiness directives to address safety issues pertaining to certain aircraft models. This instrument targets Aerospatiale (Socata) TB 200 Series aeroplanes, specifically addressing the integrity of the fuel system flowmeter pipe. The directive aims to mitigate potential risks associated with loose or compromised fuel flowmeter pipes, ensuring the operational safety of these aircraft. The policy objective, as reflected in the directive, is to comply with the requirements of the Country of Origin Airworthiness Authority, ensuring that all safety measures align with international standards and best practices. Compliance with this directive is mandatory, with checks and replacements required at specific intervals post the directive's effective date.
Scope and Application
The Civil Aviation Regulations 1998, under PART 39 - 105, mandate specific safety requirements for the Socata TB 200 series aeroplanes, specifically focusing on the fuel system flowmeter pipe integrity, as stipulated in the Airworthiness Directive AD/TB 200/1. This legislation applies to all Socata TB 200 aircraft that have not been equipped with SOCATA Modification No. 150 (Fuel Flowmeter Pipe). The regulation requires operators to check the tightness of the fuel flowmeter pipe in accordance with SOCATA Service Bulletin No. 10-108-73 Rev 1, dated March 1999, and replace the fuel flowmeter pipe with SOCATA Mod 150 following the same service bulletin. Compliance with these requirements must occur within the next 10 flight hours after the effective date of the directive and thereafter at every scheduled aircraft inspection, and within 150 hours after the effective date of the directive, or by 9 December 1999, whichever is sooner. This directive, effective from 9 September 1999, aligns with the requirements set by the Country of Origin Airworthiness Authority, reflecting a commitment to maintaining high safety standards in civil aviation.
Key Provisions
The Civil Aviation Regulations 1998, specifically PART 39 - 105, mandates strict compliance with Airworthiness Directives (ADs) to maintain aircraft safety standards. In this case, AD/TB 200/1 concerns the Aerospatiale (Socata) TB 200 Series Aeroplanes, focusing on the fuel system flowmeter pipe integrity (Sections 1-9). It applies to all Socata TB 200 aircraft not equipped with SOCATA Modification No. 150, which pertains to the fuel flowmeter pipe. The directive requires two main actions: first, the tightness of the fuel flowmeter pipe must be checked in accordance with SOCATA SB No. 10-108-73 Rev 1, dated March 1999. Second, the fuel flowmeter pipe must be replaced according to the same service bulletin. These steps are intended to address potential integrity issues with the fuel flowmeter pipe, ensuring it meets the safety standards set by the Country of Origin Airworthiness Authority.
The obligations imposed by this directive are clear and time-bound. Operators of the affected aircraft must ensure that the checks and replacements are conducted within the specified timeframes. Compliance is mandatory, with the first inspection required within the next 10 flight hours after the directive becomes effective, and subsequent inspections must occur at every scheduled aircraft inspection. Additionally, the replacement of the fuel flowmeter pipe must be completed within 150 hours after the directive's effective date or by 9 December 1999, whichever is sooner. Failure to adhere to these timelines and requirements could compromise the aircraft's airworthiness and regulatory compliance.
Failure to comply with the AD/TB 200/1 could result in severe consequences. While the specific penalties are not detailed within this directive, non-compliance with Civil Aviation Regulations can lead to enforcement actions by the Civil Aviation Safety Authority (CASA). Such actions could include fines, suspension or revocation of the aircraft's certificate of airworthiness, or other administrative penalties. Additionally, operators may face civil liabilities if non-compliance results in accidents or incidents. It is crucial for operators to meticulously follow the directive's stipulations to avoid these potential repercussions and maintain the highest safety standards in aviation operations.