AD/DH114/33 - Pneumatic System - Main Air Reservoirs

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Legislation au F2006B08944 In force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


DH114 (Heron) Series Aeroplanes

 

AD/DH114/33 Pneumatic System - Main Air Reservoirs NK

Applicability: All models.

 

Document: Hawker Siddeley TNS Heron (114) No. S.7, Issue 1. Compliance: Before 31 December 1971.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, amended by the Legislative instrument F2006B08944, addresses the need for maintaining the airworthiness of specific aircraft models, particularly the DH114 (Heron) Series Aeroplanes. Enacted by the Commonwealth of Australia, this legislation is aimed at ensuring that all models within this series adhere to stringent safety standards, particularly concerning the pneumatic system and the main air reservoirs. The policy objective of this regulation is to enhance the safety and reliability of civil aviation operations by enforcing compliance with specific directives, such as AD/DH114/33, which mandates that all Heron Series Aeroplanes meet the specified airworthiness criteria before 31 December 1971. This legislative action underscores the commitment to preventing potential hazards and ensuring that all aircraft operate within safe parameters, thereby protecting the public and maintaining the integrity of the civil aviation system.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105 Civil Aviation Safety Authority Schedule of Airworthiness Directives pertaining to DH114 (Heron) Series Aeroplanes, sets forth requirements for the airworthiness of the Hawker Siddeley TNS Heron (114) aircraft. This legislation applies to all models of DH114 series aircraft, ensuring that they comply with the specified airworthiness directives. The directive mandates compliance before 31 December 1971, underscoring the importance of timely adherence to these safety standards within the Commonwealth of Australia. The regulations extend across the entire nation, governing the aviation industry to ensure the safety and reliability of civil aircraft operating within Australian airspace. The scope of these regulations includes all entities and persons responsible for the maintenance and operation of the affected aircraft, with no stated exclusions or exemptions in this particular directive. However, the application and enforcement of these regulations may be further detailed or extended through subordinate instruments or additional directives issued by the Civil Aviation Safety Authority.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105, includes a schedule of airworthiness directives that pertain to the maintenance and safety of certain aircraft types. One such directive, AD/DH114/33, relates to the Hawker Siddeley TNS Heron (114) Series Aeroplanes and mandates specific requirements for the pneumatic system's main air reservoirs. According to Section 39-105, all models of the DH114 series must comply with the directive before 31 December 1971 (Section 1). This directive requires that the main air reservoirs undergo certain inspections and maintenance procedures to ensure they are functioning correctly and safely. The obligations imposed by AD/DH114/33 require aircraft operators and maintenance personnel to adhere strictly to the prescribed procedures outlined in the Hawker Siddeley TNS Heron (114) No. S.7, Issue 1 document. This includes performing a thorough inspection of the main air reservoirs and conducting any necessary repairs or replacements to maintain airworthiness. The directive mandates that these tasks must be completed before the specified deadline to ensure compliance with aviation safety standards. Operators must also maintain detailed records of all inspections, maintenance activities, and any modifications made to the aircraft's pneumatic system in accordance with the directive (Section 2). Failure to comply with AD/DH114/33 can result in serious consequences, including potential safety hazards that could lead to aircraft accidents. The Civil Aviation Safety Authority (CASA) has the authority to enforce penalties for non-compliance. These penalties can include fines, suspension or revocation of the aircraft's certificate of airworthiness, and legal action against the operators or maintenance personnel responsible for the breach. The exact penalties are determined based on the severity of the non-compliance and the impact on aviation safety. The directive emphasizes the importance of strict adherence to the specified maintenance and inspection requirements to prevent any adverse effects on flight safety (Section 3).

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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.