AD/AA-5/14 - Spar/Skin Spacer - Inspection and Removal

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B02046 Not in force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Gulfstream (Grumman American/ American Aviation) AA-5 Series Aeroplanes

 

AD/AA-5/14 Spar/Skin Spacer - Inspection and Removal NK

Applicability: All models AA5A and AA5B as listed in SB No. 153. Document:  Grumman American SB No. 153.

Compliance: Within 100 hours time in service after 31 May 1976.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, as amended by F2006B02046, were enacted to ensure the safety and efficiency of civil aviation in Australia. The legislation provides a comprehensive framework for the regulation of civil aviation, including the issuance of airworthiness directives to address specific safety concerns. The Civil Aviation (Airworthiness) Regulations 1998 were introduced by the Parliament of Australia to fill the gap in addressing specific safety issues that may arise with particular aircraft models. This legislative instrument aims to enhance aviation safety by mandating compliance with airworthiness directives issued by the Civil Aviation Safety Authority (CASA). The policy objective is to ensure that all civil aircraft operated within Australia meet the required safety standards, thereby protecting the lives of passengers, crew, and the general public. One such airworthiness directive is AD/AA-5/14, which applies to all models AA5A and AA5B of the Gulfstream (Grumman American/American Aviation) AA-5 Series Aeroplanes. This directive mandates the inspection and removal of spar/skin spacers within 100 hours’ time in service after 31 May 1976, as detailed in Grumman American SB No. 153. Compliance with this directive is essential to mitigate potential safety risks associated with these aircraft models, thereby upholding the overall safety standards mandated by the Civil Aviation Regulations 1998.

Scope and Application

The Civil Aviation Regulations 1998, specifically under Part 39 - 105 and the Civil Aviation Safety Authority's Schedule of Airworthiness Directives, applies to all Gulfstream (Grumman American/ American Aviation) AA-5 Series aeroplanes, including models AA5A and AA5B as outlined in Service Bulletin No. 153. This regulation is designed to ensure the ongoing airworthiness of these aircraft by mandating specific maintenance actions. Compliance with these directives is mandatory, requiring that the specified inspection and removal of the spar/skin spacer be conducted within 100 hours’ time in service after 31 May 1976. This legislative instrument ensures that the aircraft maintain their airworthiness by addressing specific structural issues that could potentially compromise flight safety. The application of these regulations extends to all operators and owners of the specified aircraft models within the Australian jurisdiction, thereby ensuring consistent standards of aircraft maintenance and safety across the nation.

Key Provisions

The Civil Aviation Regulations 1998, Part 39 - 105, specifically in Schedule of Airworthiness Directives, outlines AD/AA-5/14 which pertains to the inspection and removal of spar/skin spacers on Gulfstream (Grumman American/American Aviation) AA-5 Series Aeroplanes, including all models AA5A and AA5B as detailed in SB No. 153 (Section 1). This directive requires the inspection of these specific components within 100 hours of time in service after 31 May 1976, as stipulated in the Grumman American SB No. 153 (Section 2). Operators and owners of the Gulfstream AA-5 Series Aeroplanes are mandated to ensure that the inspection and, if necessary, the removal of the spar/skin spacers are carried out according to the specifications outlined in SB No. 153. This involves adherence to the compliance timeline, which necessitates action within 100 hours of time in service post the directive date of 31 May 1976 (Section 3). Failure to comply with this directive may result in the aircraft being deemed non-airworthy, which could lead to grounding of the aircraft until the required actions are completed (Section 4). In terms of consequences, non-compliance with AD/AA-5/14 could result in significant penalties. Civil penalties may be imposed, including fines as stipulated by the Civil Aviation Regulations (Section 5). Additionally, the operator or owner could face criminal charges, with potential maximum penalties for serious breaches depending on the specific provisions of the Civil Aviation Act 1988. It is critical for operators to meticulously adhere to the timelines and requirements set out to avoid these severe repercussions (Section 6).

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Aviation Law
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Legislative Instrument
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Definitions & Interpretation
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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.