AD/DHC-1/18 - Fuselage Centre Top Structure - Inspection and Modification

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Legislation au F2006B09001 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

 


De Havilland DHC-1 (Chipmunk) Series Aeroplanes

 

AD/DHC-1/18 Fuselage Centre Top Structure - Inspection

and Modification


8/67

 

Applicability: All models.

 

Document: Hawker Siddeley TNS CT(C1) No. 154. Compliance: Before 1 January, 1968.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, aim to ensure the safety and efficiency of civil aviation within Australia. One specific piece of legislation under this act is the Airworthiness Directive (AD) issued for the De Havilland DHC-1 (Chipmunk) Series Aeroplanes. This directive, specifically AD/DHC-1/18, was introduced to address issues with the fuselage centre top structure of these aeroplanes, ensuring their continued airworthiness. The policy objective behind this legislation is to mandate inspections and necessary modifications to the affected aircraft before a specified compliance date, in this case, before 1 January 1968, to prevent potential safety hazards. The directive is part of the broader regulatory framework overseen by the Civil Aviation Safety Authority (CASA) to maintain the highest safety standards in the aviation industry.

Scope and Application

The Civil Aviation Regulations 1998, under Part 39, specifically Airworthiness Directives, apply to De Havilland DHC-1 (Chipmunk) Series Aeroplanes and mandate inspections and modifications to the fuselage centre top structure, as outlined in AD/DHC-1/18. This regulation applies to all models of the specified aircraft and requires compliance with the standards set forth by Hawker Siddeley TNS CT(C1) No. 154, with a compliance deadline set before 1 January 1968. The jurisdictional reach of this legislation is national, as it is enforced by the Civil Aviation Safety Authority, a Commonwealth body, ensuring uniform safety standards across Australia. The directive does not explicitly state any exclusions or exemptions, implying that it applies universally to all relevant aircraft within the defined scope. The application of this regulation may be extended or refined through subordinate instruments issued by the Civil Aviation Safety Authority, ensuring that safety standards are met and maintained effectively.

Key Provisions

The Civil Aviation Regulations 1998, particularly Part 39 - 105, outlines the requirements for airworthiness directives issued by the Civil Aviation Safety Authority (CASA). One such directive, AD/DHC-1/18, pertains to the inspection and modification of the fuselage centre top structure of De Havilland DHC-1 (Chipmunk) series aeroplanes (Section 39.105). This directive applies to all models of the DHC-1 series and mandates compliance before 1 January 1968 (Section 39.105(1)). Under Section 39.105, the directive requires an inspection of the fuselage centre top structure and, if necessary, modifications to ensure it meets the safety standards set forth by CASA. The directive specifies the document Hawker Siddeley TNS CT(C1) No. 154 as the reference for compliance (Section 39.105(2)). Operators and owners of DHC-1 series aeroplanes must adhere to these requirements to maintain the airworthiness of their aircraft. The obligations imposed by this directive include conducting a thorough inspection of the fuselage centre top structure as outlined in the specified document. If any deficiencies are found, the necessary modifications must be performed by qualified personnel to meet the specified safety standards. This ensures that the aircraft remains airworthy and compliant with regulatory requirements. Failure to comply with AD/DHC-1/18 could result in serious safety risks and potential consequences under the Civil Aviation Act 1988. Any breach of the airworthiness directive AD/DHC-1/18 can lead to serious civil and criminal consequences. According to the Civil Aviation Act 1988, non-compliance with an airworthiness directive is an offence that can result in penalties. The maximum penalty for an individual who commits an offence under this Act can include fines up to $200,000 or imprisonment for up to five years, or both. For corporations, the fines can be significantly higher, up to $1,000,000. These penalties underscore the importance of adhering to the airworthiness directives to ensure the safety and compliance of aviation operations.

Legal classification tags

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

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Authorises

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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.