AD/FA-200/5 - Fuselage Skin - Modification

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

Legislation au F2006B09940 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

 


Fuji FA-200 Series Aeroplanes

 

AD/FA-200/5 Fuselage Skin - Modification 5/70

Applicability: All models with S/Nos. 3, 9, 10 and 11. Document:  Fuji SB No. FAS-017.

Compliance: Within 100 hours time in service after 30 June 1970.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, serve to govern civil aviation safety within the country. One specific legislative instrument, F2006B09940, addresses the maintenance and safety of Fuji FA-200 Series Aeroplanes, particularly focusing on fuselage skin modifications. This instrument, issued under the authority of the Civil Aviation Safety Authority, was introduced to ensure that all affected aircraft meet stringent airworthiness standards. The policy objective is to maintain and enhance the safety of civil aviation by mandating specific compliance measures for certain models of Fuji FA-200 Series Aeroplanes, as detailed in the directive. The regulation requires compliance within 100 hours of time in service after 30 June 1970, with reference to Fuji Service Bulletin No. FAS-017 for applicable models with serial numbers 3, 9, 10, and 11.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105 under the Civil Aviation Safety Authority Schedule of Airworthiness Directives, outlines the requirements for maintaining the airworthiness of the Fuji FA-200 Series Aeroplanes. This directive applies to all models with specific serial numbers, namely 3, 9, 10, and 11, mandating a modification to the fuselage skin. The requirement for compliance must be fulfilled within 100 hours of time in service following 30 June 1970, as referenced in Fuji Service Bulletin No. FAS-017. The scope of this directive is geographically and operationally broad, extending to all civil aviation operators within the Commonwealth of Australia who operate the specified Fuji FA-200 Series Aeroplanes. There are no exclusions, exemptions, or thresholds stated within the directive itself, though the application and enforcement may be further defined or detailed in subordinate instruments or additional regulatory guidance provided by the Civil Aviation Safety Authority.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105, includes a schedule of airworthiness directives (AD) for the Fuji FA-200 Series Aeroplanes, with AD/FA-200/5 focusing on fuselage skin modifications (section 5/70). This directive applies to all models with serial numbers (S/Nos.) 3, 9, 10, and 11. Compliance with these requirements is mandated within 100 hours of time in service after 30 June 1970, as detailed in Fuji Service Bulletin No. FAS-017. The key provisions of AD/FA-200/5 require operators of the specified Fuji FA-200 aeroplanes to perform a modification to the fuselage skin to ensure continued airworthiness. This involves following the instructions and specifications outlined in Fuji SB No. FAS-017. This directive aims to address potential safety issues identified with the fuselage skin, ensuring that these aircraft maintain their airworthiness standards and safety certifications. Operators of the affected Fuji FA-200 aeroplanes have specific obligations under AD/FA-200/5. They must ensure that the fuselage skin modification is completed within the stipulated timeframe of 100 hours of time in service after 30 June 1970. The modifications must be carried out according to the detailed instructions provided in Fuji SB No. FAS-017, which includes precise steps and specifications for the modification work. Additionally, operators must document the completion of these modifications and maintain records to demonstrate compliance with the directive. Failure to comply with AD/FA-200/5 may result in serious consequences, both civil and criminal. Under section 18 of the Civil Aviation Act 1988, non-compliance can lead to enforcement actions, including fines, suspension, or revocation of the aircraft’s certificate of airworthiness. The maximum penalties for such breaches can be substantial, reflecting the critical nature of airworthiness directives. Additionally, non-compliance could potentially result in criminal charges if the breach is deemed to have caused significant safety risks or harm. Therefore, it is imperative for operators to adhere strictly to the requirements of AD/FA-200/5 to avoid these serious repercussions.

Legal classification tags

Area of Law
Aviation Law
Instrument
Legislative Instrument
Concepts
Definitions & Interpretation
Compliance Obligations
Regulatory Standards
Catchwords
Airworthiness Directives

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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.