AD/MCH/7 - Bonding Points - Modification

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Legislation au F2006B11274 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

 


Aero Resources J2 Series Gyroplanes

 

AD/MCH/7 Bonding Points - Modification 12/74

Applicability: All model J2. Requirement:  Install and identify -

(1)     fuelling equipment bonding points at each fuel filling point;

 

(2)     external earthing points for the attachment of ground connections on each main undercarriage assembly or on the nose gear.

 

Compliance: Before issue of a Certificate of Airworthiness.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Australian Parliament, form a crucial part of the regulatory framework governing civil aviation in Australia. Among the various provisions, Part 39 - 105, concerning the Civil Aviation Safety Authority, includes specific airworthiness directives that ensure the safety and compliance of aircraft with established standards. One such directive, AD/MCH/7, pertains to the Aero Resources J2 Series Gyroplanes and mandates modifications to bonding points, specifically requiring the installation and identification of fuelling equipment bonding points at each fuel filling point and external earthing points on the main undercarriage assembly or nose gear. This directive aims to enhance safety by preventing fuel-related accidents and ensuring proper grounding of the aircraft, thus addressing a gap in safety protocols for these gyroplanes. The directive must be complied with before the issuance of a Certificate of Airworthiness, underscoring the importance of these modifications in maintaining airworthiness standards.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, applies to all Aero Resources J2 series gyroplanes operating in Australian airspace. The legislation mandates the installation and identification of specific bonding points to ensure compliance with airworthiness directives. This includes the installation of fuelling equipment bonding points at each fuel filling point and the provision of external earthing points for the attachment of ground connections on each main undercarriage assembly or on the nose gear. These modifications must be completed before the issuance of a Certificate of Airworthiness, ensuring that the aircraft meets the necessary safety standards. The regulations extend to all Aero Resources J2 series gyroplanes within the Commonwealth of Australia, reflecting the national scope of the Civil Aviation Regulations. Any exclusions or exemptions are not specified within this directive, and compliance is mandatory for all affected aircraft.

Key Provisions

The key sections of the Civil Aviation Regulations 1998, specifically Part 39 - 105, address the Airworthiness Directives (AD) related to Aero Resources J2 Series Gyroplanes, with a focus on AD/MCH/7 concerning bonding points. Section 12/74 mandates that all model J2 gyroplanes must have specific modifications to their bonding points. This includes installing and identifying fuelling equipment bonding points at each fuel filling point (subsection (1)), and ensuring external earthing points are available for ground connections on each main undercarriage assembly or on the nose gear (subsection (2)). These modifications must be completed before a Certificate of Airworthiness is issued to the aircraft. The obligations imposed by these regulations are quite clear. Aircraft operators and maintenance personnel must ensure that the specified modifications are carried out correctly and in compliance with the directive. This involves the installation of bonding points as per the requirements outlined, which is a critical safety measure to prevent fuel-related hazards and ensure proper grounding of the aircraft during operations. Compliance with these directives is mandatory, and failure to adhere to the stipulated modifications can result in the aircraft not being granted a Certificate of Airworthiness, thus rendering it unfit for flight. In terms of consequences for non-compliance, the regulations do not explicitly state penalties within the text provided, but non-compliance could lead to serious safety risks. Furthermore, from a regulatory standpoint, an aircraft that does not meet the airworthiness standards set by the Civil Aviation Safety Authority (CASA) cannot legally be operated. This effectively means that any operator found to be in breach of these directives could face legal actions, including fines or other enforcement measures from CASA. While the specific penalties are not detailed in the text, the overarching principle is that adherence to these safety directives is critical to avoid legal repercussions and ensure the safe operation of the aircraft.

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Aviation Law
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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.