AD/L200/8 - Fin and Stabiliser Front Attachment Hinges - Inspection

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Legislation au F2006B11058 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

 


Morava L200 Series Aeroplanes

 

AD/L200/8 Fin and Stabiliser Front Attachment Hinges - Inspection


11/78

 

Applicability: All models.

 

Document: Omnipol SB No. L200/109.

 

Compliance: Before issue of Certificate of Airworthiness.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, which were enacted by the Australian Parliament, form the backbone of civil aviation regulation in Australia, ensuring that aviation activities are conducted in a safe and orderly manner. Part 39 of these Regulations pertains to airworthiness directives, which are legally enforceable rules that aim to correct an unsafe condition of a product. Specifically, AD/L200/8 addresses the fin and stabiliser front attachment hinges of Morava L200 Series Aeroplanes, requiring an inspection before the issuance of a Certificate of Airworthiness to ensure compliance with safety standards outlined in Omnipol SB No. L200/109. This directive was introduced to mitigate risks associated with potential structural failures in these components, thereby enhancing overall flight safety. The policy objective of AD/L200/8 is to ensure that all Morava L200 Series Aeroplanes meet the necessary safety standards before being deemed airworthy. By mandating inspections and compliance with specific service bulletins, the regulation aims to prevent accidents and incidents related to the structural integrity of the aeroplane's fin and stabiliser attachments. This targeted approach under the Civil Aviation Regulations 1998 helps maintain high safety standards within Australia's civil aviation sector.

Scope and Application

The Civil Aviation Safety Authority (CASA) issued the Airworthiness Directive (AD) AD/L200/8, which applies to all Morava L200 Series aeroplanes. The directive mandates inspections on the fin and stabiliser front attachment hinges, as outlined in Omnipol Service Bulletin No. L200/109, before issuing a Certificate of Airworthiness. This regulation ensures that all models of the specified aircraft undergo these critical inspections, maintaining safety standards across the industry. The directive is part of the Civil Aviation Regulations 1998, which have a nationwide jurisdictional reach within Australia. The application of the AD extends to all operators and owners of the Morava L200 Series aeroplanes, ensuring compliance with safety directives before any aircraft can be certified as airworthy. This legislation does not specify any exclusions, exemptions, or thresholds but operates within the broader framework of civil aviation safety regulations in Australia.

Key Provisions

The Civil Aviation Regulations 1998, Part 39 - 105, specifically addresses the airworthiness directives for aircraft, including the Morava L200 Series Aeroplanes. Within this context, AD/L200/8 pertains to the inspection of fin and stabiliser front attachment hinges (Section 11/78). The directive applies universally to all models of the Morava L200 Series Aeroplanes. Compliance with this directive is mandated, and it must be fulfilled before the issuance of a Certificate of Airworthiness. The directive references the Omnipol Service Bulletin No. L200/109 as the document that provides the necessary guidance and requirements for this inspection. The Civil Aviation Regulations impose specific obligations on aircraft owners and operators to ensure that their aircraft comply with all applicable airworthiness directives. In the case of AD/L200/8, this means that before a Certificate of Airworthiness can be issued, the fin and stabiliser front attachment hinges of the Morava L200 Series Aeroplanes must be inspected in accordance with the guidelines provided in Omnipol Service Bulletin No. L200/109. This requirement is critical to maintaining the safety and airworthiness of the aircraft, ensuring that all components are in good working condition and free from defects that could compromise flight safety. Failure to comply with the provisions of AD/L200/8 could result in significant legal and safety repercussions. Under the Civil Aviation Regulations, non-compliance with airworthiness directives can lead to enforcement actions by the Civil Aviation Safety Authority (CASA). If an aircraft is found to be non-compliant, CASA has the authority to take action, which could include denying the issuance of a Certificate of Airworthiness or imposing fines and other penalties. The seriousness of these consequences underscores the importance of adhering to the directives to ensure the safety and airworthiness of the aircraft. The specific penalties and consequences are outlined in the broader regulatory framework, but they can be substantial, reflecting the high stakes involved in aviation safety.

Legal classification tags

Area of Law
Aviation Law
Instrument
Legislative Instrument
Concepts
Definitions & Interpretation
Compliance Obligations
Enforcement Powers
Catchwords
Airworthiness

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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.