COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Aerospatiale (Socata) TBM 700 Series Aeroplanes
AD/TBM 700/9 Windshield De-Icing 2/95
Applicability: Model TBM 700 series aeroplanes with serial numbers 1 to 62, 67, 68, 70, 73 to 75,
77, 78 and 80.
Requirement: Action in accordance with Socata TBM 700 Mandatory Service Bulletin SB 70-037- 30 dated October 1994, (installation of Kit OPT70 K043-30 is only mandatory if the right-hand windshield de-icing option is fitted).
Note: DGAC AD 94-267(B) dated 7 December 1994 refers.
Compliance: Either within 100 hours time in service after 2 February 1995 or during the next annual inspection, whichever occurs first.
Background: Compliance with this Directive provides additional protection against Electromagnetic Interference (EMI) being conducted by the windshield de-icing system wiring.
Overview
The Civil Aviation Regulations 1998, as amended, encompass a comprehensive regulatory framework designed to ensure the safety of civil aviation operations within Australia. One specific legislative instrument, AD/TBM 700/9, pertains to Aerospatiale (Socata) TBM 700 Series aeroplanes, addressing a particular safety concern related to windshield de-icing systems. Enacted to mitigate the risk of Electromagnetic Interference (EMI) in these aircraft, the directive ensures compliance with specific service bulletins and installation requirements, thereby enhancing flight safety. This legislative instrument is promulgated by the Civil Aviation Safety Authority, reflecting the overarching policy objective to maintain the highest standards of aviation safety through stringent regulatory measures.
The enactment of this directive fills a critical gap in ensuring the airworthiness of the specified TBM 700 series aeroplanes by mandating timely compliance with established safety protocols. By requiring adherence to Socata TBM 700 Mandatory Service Bulletin SB 70-037-30, the legislation seeks to prevent potential EMI issues that could compromise flight safety. The directive underscores the commitment of the Civil Aviation Safety Authority to proactively address safety issues and ensure that all civil aviation operations adhere to rigorous safety standards.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertain to the Airworthiness Directives for the Aerospatiale (Socata) TBM 700 Series Aeroplanes, with a focus on the windshield de-icing systems. This regulation applies to model TBM 700 series aeroplanes with specific serial numbers identified within the legislative instrument. The directive mandates that the specified aeroplanes comply with Socata TBM 700 Mandatory Service Bulletin SB 70-037-30 dated October 1994, which includes the installation of Kit OPT70 K043-30 if the right-hand windshield de-icing option is fitted. This requirement aims to enhance protection against Electromagnetic Interference (EMI) that may be conducted by the windshield de-icing system wiring. Compliance with this directive must be achieved either within 100 hours of the aeroplanes being in service after 2 February 1995, or during the next annual inspection, whichever occurs first. The regulation underscores the importance of maintaining airworthiness standards to ensure safety and operational reliability of the affected aircraft.
Key Provisions
The Civil Aviation Regulations 1998, under Part 39-105, contains an Airworthiness Directive (AD) specifically concerning Aerospatiale (Socata) TBM 700 Series aeroplanes. This AD, numbered AD/TBM 700/9, mandates the installation of a windshield de-icing kit for certain models of these aeroplanes. Specifically, the directive applies to model TBM 700 series aeroplanes with serial numbers 1 to 62, 67, 68, 70, 73 to 75, 77, 78, and 80. The requirement outlined in this AD is for the aeroplanes to comply with Socata TBM 700 Mandatory Service Bulletin SB 70-037-30 dated October 1994. The installation of Kit OPT70 K043-30 is mandatory only if the right-hand windshield de-icing option is fitted. This directive also references DGAC AD 94-267(B) dated 7 December 1994 for further information.
Operators of the specified TBM 700 series aeroplanes must ensure that the required action is taken either within 100 hours of time in service after 2 February 1995 or during the next annual inspection, whichever comes first. This ensures that the aeroplanes are maintained to a standard that mitigates risks associated with Electromagnetic Interference (EMI) conducted by the windshield de-icing system wiring. Compliance with this directive is crucial to maintaining the airworthiness of the aeroplanes and ensuring safe operations.
The AD imposes specific obligations on the operators of the TBM 700 series aeroplanes. They must follow the instructions in Socata TBM 700 Mandatory Service Bulletin SB 70-037-30 and ensure that the appropriate modifications are made within the specified timeframe. This involves either installing the Kit OPT70 K043-30 if the right-hand windshield de-icing option is fitted, or ensuring the aeroplane undergoes an annual inspection to verify compliance. Failure to comply with this directive can result in significant safety risks and potential regulatory action.
Failure to comply with the requirements of AD/TBM 700/9 can lead to serious consequences. The Civil Aviation Safety Authority (CASA) may take enforcement action against operators who do not adhere to the directive, which can include fines, penalties, or even grounding of the aeroplanes. The exact penalties are not specified in the AD itself, but under the Civil Aviation Act 1988 and associated regulations, severe non-compliance can result in substantial financial penalties and criminal charges for individuals responsible for the oversight of the aeroplanes. It is essential for operators to ensure strict compliance to avoid these adverse outcomes.