AD/L200/4 - Nose Wheel Retract Strut - Inspection

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Legislation au F2006B11054 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/L200/4 Nose Wheel Retract Strut - Inspection 7/68

Applicability: All models L200A and L200D. Document:  Omnipol SB No. L200/113.

Compliance: Within 100 hours time in service after 11 July 1968 and thereafter at intervals not exceeding 100 hours time in service.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Australian Parliament, establish the legal framework for ensuring the safety and efficiency of civil aviation in Australia. This comprehensive legislation includes the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, which addresses specific safety issues for various aircraft models. The legislation seeks to mitigate risks and ensure the continued safe operation of aircraft within Australia’s airspace. A notable directive under this legislation is AD/L200/4, which pertains to Morava L200 Series Aeroplanes. This directive specifically mandates inspections of the nose wheel retract strut for models L200A and L200D, ensuring compliance within 100 hours of time in service after the directive’s issuance date of 11 July 1968, and at regular intervals not exceeding 100 hours thereafter. The policy objective behind this directive is to enhance aircraft safety by identifying and rectifying potential structural issues in a timely manner.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, mandates that the Airworthiness Directives issued by the Civil Aviation Safety Authority (CASA) apply to all Morava L200 Series aeroplanes, including models L200A and L200D. This directive, AD/L200/4, pertains to the inspection of the nose wheel retract strut, as documented in Omnipol Service Bulletin No. L200/113. The legislation is applicable to all persons and entities operating these specific aircraft models within Australia, encompassing both commercial and private aviation sectors. The geographic reach of this regulation is national, applying uniformly across all states and territories in Australia. The requirement for compliance stipulates that inspections must be conducted within 100 hours of time in service after 11 July 1968 and subsequently at intervals not exceeding 100 hours of time in service. This directive does not extend or restrict its application through subordinate instruments and applies without exclusions, exemptions, or specific thresholds as outlined in the Civil Aviation Regulations.

Key Provisions

The Civil Aviation Regulations 1998, specifically under Part 39, Section 105, establish the requirements for the airworthiness of aircraft. Section AD/L200/4 pertains to Morava L200 Series Aeroplanes and mandates that all models L200A and L200D undergo inspections of the nose wheel retract strut. These inspections must occur within 100 hours of time in service after 11 July 1968 and subsequently at intervals not exceeding 100 hours of time in service. This directive is documented in Omnipol SB No. L200/113. The Act imposes specific obligations on the operators and owners of Morava L200A and L200D aeroplanes to ensure compliance with these airworthiness directives. Operators must conduct the specified inspections within the stipulated timeframes to maintain the aircraft's airworthiness certification. Additionally, they are required to document all inspections and ensure that any necessary repairs or replacements are carried out by qualified personnel. Failure to comply with these directives can result in the aircraft being deemed unairworthy, which could lead to grounding and potential legal ramifications. Failure to adhere to the airworthiness directives outlined in the Civil Aviation Regulations can lead to serious consequences. Under Section 88 of the Civil Aviation Act 1988, non-compliance with airworthiness directives can be considered an offence. This includes situations where the aircraft is operated while not meeting the specified maintenance and inspection requirements. The penalties for such offences can be severe, with maximum fines and imprisonment terms applicable. In civil cases, the penalties may include substantial fines, while in criminal cases, the maximum penalty for serious breaches can be up to five years imprisonment. These stringent measures underscore the importance of strict compliance with airworthiness directives to ensure the safety of aviation operations.

Legal classification tags

Area of Law
Aviation Law
Instrument
Regulation
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.