AD/B747/98 - Auxiliary Power Unit (APU) Pneumatic Ducts

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Legislation au F2006B03276 In force Legislative Instrument

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Boeing 747 Series Aeroplanes

 

AD/B747/98 Auxiliary Power Unit (APU) Pneumatic Ducts 11/91

Applicability: Boeing 747 series aeroplanes as listed in FAA Airworthiness Directive 91-15-24 Amdt 39-7089.

 

Requirement: Action in accordance with the Technical Requirements of FAA AD 91-15-24.

 

Note: Boeing Service Bulletin 747-36-2081 and 747-36-2092 refers.

 

Compliance: Required prior to the accumulation of 7 000 flight cycles or within the next 3 000 flight cycles after the 14 November 1991, which ever occurs later.

 

Background: FAA AD action prompted by reports of cracked or ruptured APU ducts that have caused damage to adjacent structure, pneumatic ducts, and hydraulic lines. This condition, if not corrected, could result in damage to the adjacent structure, pneumatic ducts, hydraulic lines and/or electrical wiring.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, aim to maintain high safety standards in the aviation industry. This legislation is part of a broader framework designed to ensure the safety and reliability of aircraft operations within Australia. Specifically, Part 39 - 105 of the Civil Aviation Regulations addresses Airworthiness Directives, which are mandatory safety instructions issued by the Civil Aviation Safety Authority. These directives are critical in mitigating risks associated with specific aircraft components or systems. For instance, AD/B747/98 concerning Boeing 747 series aeroplanes focuses on the Auxiliary Power Unit (APU) pneumatic ducts, responding to reports of structural damage caused by cracked or ruptured ducts. The directive requires corrective actions in accordance with the Federal Aviation Administration's Technical Requirements, ensuring that any identified issues are promptly addressed to prevent potential hazards that could compromise flight safety.

Scope and Application

The Civil Aviation Regulations 1998, under PART 39 - 105, specifically the Civil Aviation Safety Authority Schedule of Airworthiness Directives, addresses the maintenance and safety standards for Boeing 747 series aeroplanes. This legislation mandates compliance with the FAA Airworthiness Directive 91-15-24, Amendment 39-7089, which pertains to the Auxiliary Power Unit (APU) pneumatic ducts. This directive applies to all Boeing 747 series aeroplanes listed in the referenced FAA Airworthiness Directive and requires action in accordance with the specified technical requirements. The requirement necessitates compliance either before the aeroplane accumulates 7,000 flight cycles or within the next 3,000 flight cycles following 14 November 1991, whichever is later. This action is prompted by reports of cracked or ruptured APU ducts that could result in damage to adjacent structure, pneumatic ducts, hydraulic lines, and electrical wiring, hence the imperative for timely corrective measures. Compliance with Boeing Service Bulletins 747-36-2081 and 747-36-2092 is also referenced for relevant technical guidance.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105, addresses the safety standards for the maintenance and operation of aircraft in Australia. Under this part, the Airworthiness Directives (ADs) set forth mandatory requirements for ensuring the safety of civil aircraft. AD/B747/98 pertains to the Boeing 747 series aeroplanes and focuses on the Auxiliary Power Unit (APU) pneumatic ducts. Section (11/91) of the directive states that it applies to Boeing 747 series aeroplanes as specified in FAA Airworthiness Directive 91-15-24 Amendment 39-7089. The requirement outlined in this directive mandates that operators of Boeing 747 series aeroplanes must take action in accordance with the technical requirements of the Federal Aviation Administration (FAA) Airworthiness Directive 91-15-24. Boeing Service Bulletins 747-36-2081 and 747-36-2092 provide further guidance on implementing these requirements. Compliance with these directives is critical, with the directive stipulating that the necessary actions must be taken either before the aeroplane accumulates 7,000 flight cycles or within the next 3,000 flight cycles after 14 November 1991, whichever occurs later. Operators of Boeing 747 series aeroplanes must adhere to these directives to ensure the safety of the aircraft. Failure to comply with the AD/B747/98 could result in severe consequences, as the directive is prompted by reports of cracked or ruptured APU ducts that have caused significant damage to adjacent structures, pneumatic ducts, hydraulic lines, and electrical wiring. If left unaddressed, this condition could lead to catastrophic failures during flight, posing serious risks to passengers, crew, and the aircraft itself. The implications of non-compliance with the AD/B747/98 are significant. The Civil Aviation Safety Authority (CASA) may impose penalties on operators who fail to adhere to the airworthiness directives. Offences related to non-compliance can lead to both civil and criminal consequences. Civil penalties can include fines, and in severe cases, criminal charges may be brought against individuals responsible for the non-compliance. The specific penalties depend on the severity of the breach and the impact on aviation safety.

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Aviation Law
Instrument
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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.