AD/BAL/23 - Triple and Quad Burner Support

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Legislation au F2006B03562 In force Legislative Instrument

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


AIRWORTHINESS DIRECTIVE

For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (1) of CASR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.


 

Hot Air Balloons

 

AD/BAL/23 Triple and Quad Burner Support 13/2004

DM

 

Applicability: All Cameron Shadow/Shadow Stealth - Triple, Quad, and Stratus Triple, Quad gimballed burner assemblies installed on, but not limited to Cameron Balloons Ltd A, N, O, Z, Thunder S1, S2, and Colt A Series Hot Air Balloons.

 

Requirement: Inspect the burner support plate and mounting tube in accordance with Cameron Balloons Ltd Alert Service Bulletin (ASB) No. 13, dated 29 October 2004, or later EASA approved revision.

 

Replace any cracked or damaged support plates or mounting tubes before further flight with serviceable parts that have been inspected in accordance with ASB No. 13, dated 29 October 2004, or later EASA approved revision.

 

Note: UK CAA AD G-2004-0026 refers.

 

Compliance: Before further flight after 10 November 2004.

 

This Airworthiness Directive becomes effective on 10 November 2004.

 

Background: The manufacturer has identified several occurrences of cracked welds between the burner support plate and the mounting tube following road transportation. Failure to identify a cracked or damaged burner support assembly could result in burner separation, and an uncontrolled flame that presents a hazard to the envelope, the balloon’s occupants, and persons on the ground.


David Villiers

Delegate of the Civil Aviation Safety Authority 4 November 2004

 

 

 

 

 

The above AD is notified in the Commonwealth of Australia Gazette on 10 November 2004.

 


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Overview

The Civil Aviation Safety Regulations 1998 (CASR) were enacted to ensure that civil aviation activities in Australia are conducted in a safe manner. Part 39 of these regulations specifically addresses airworthiness directives, which are legally binding orders issued by the Civil Aviation Safety Authority (CASA) to address identified safety issues with aircraft or aeronautical products. The Airworthiness Directive AD/BAL/23, issued on 13 October 2004, targets the issue of cracked burner support plates and mounting tubes in certain hot air balloons manufactured by Cameron Balloons Ltd, such as the Shadow, Stealth, Stratus, Thunder S1, S2, and Colt A series. The directive was issued in response to occurrences of cracked welds between the burner support plate and mounting tube following road transportation. The problem identified is that failure to detect and rectify such cracks could lead to burner separation and uncontrolled flames, posing a risk to the balloon’s occupants, the balloon envelope, and persons on the ground. The policy objective of this directive is to mandate inspections and necessary replacements of the affected parts to ensure continued airworthiness and safety of the affected hot air balloons.

Scope and Application

The Civil Aviation Safety Regulations 1998, as part of the legislative instrument F2006B03562, apply to all Cameron Shadow/Shadow Stealth - Triple, Quad, and Stratus Triple, Quad gimballed burner assemblies installed on, but not limited to, Cameron Balloons Ltd A, N, O, Z, Thunder S1, S2, and Colt A Series Hot Air Balloons. This Airworthiness Directive (AD) mandates that specific actions be taken to address the identified unsafe conditions concerning the burner support plate and mounting tube. The AD requires these components to be inspected in accordance with Cameron Balloons Ltd Alert Service Bulletin (ASB) No. 13, dated 29 October 2004, or later EASA approved revisions, and any cracked or damaged support plates or mounting tubes must be replaced with serviceable parts that have been inspected in accordance with the same bulletin before further flight. This directive applies to all affected aircraft in the Commonwealth of Australia and becomes effective on 10 November 2004, with compliance required before further flight after this date.

Key Provisions

The Civil Aviation Safety Regulations 1998, particularly under Part 39, establish stringent safety standards for aviation, with the Airworthiness Directive (AD) being a key component of these regulations. Section 39.1 (1) of the CASR 1998 empowers the Civil Aviation Safety Authority (CASA) to issue Airworthiness Directives. This particular AD, identified as AD/BAL/23, pertains to specific hot air balloons and their burner assemblies, mandating detailed inspections and repairs to ensure safety. The AD is applicable to Cameron Shadow/Shadow Stealth, Stratus Triple, Quad, and gimballed burner assemblies installed on Cameron Balloons Ltd A, N, O, Z, Thunder S1, S2, and Colt A Series Hot Air Balloons. The directive requires that the burner support plate and mounting tube be inspected and, if necessary, replaced according to Cameron Balloons Ltd Alert Service Bulletin (ASB) No. 13, dated 29 October 2004, or later revisions approved by the European Aviation Safety Agency (EASA). Compliance with these requirements must be achieved before further flights, with the directive becoming effective on 10 November 2004. The obligations imposed by this AD are significant for the owners and operators of the specified hot air balloons. They must ensure that all inspections and repairs are carried out by qualified personnel, following the guidelines set out in ASB No. 13 or later revisions. This includes verifying the integrity of the burner support plate and mounting tube and replacing any cracked or damaged parts with serviceable ones that have been inspected in accordance with the specified bulletin. Failure to comply with these obligations could compromise the safety of the aircraft and its occupants, as well as pose a risk to persons on the ground. The directive is explicit that these actions must be completed before any further flights after 10 November 2004. Failure to comply with the requirements of this Airworthiness Directive can lead to severe consequences. Non-compliance with safety directives under the CASR 1998 can result in enforcement actions by CASA. While the specific penalties for breach are not detailed in the AD itself, the general provisions of the CASR 1998 and related legislation may include administrative penalties, fines, and potential prosecution. In extreme cases, the operation of a non-compliant aircraft could be prohibited, leading to grounded aircraft and operational disruptions. The safety of passengers, crew, and the public is paramount, and adherence to these directives is mandatory to avoid legal and safety repercussions.

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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.