AD/HS 125/72 - Engine Mounting Cowling Damage

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Legislation au F2006B10513 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

 


British Aerospace BAe 125 Series Aeroplanes

 

AD/HS 125/72 Engine Mounting Cowling Damage 10/85

Applicability: All models fitted with Garrett TFE 731-3R-1H engines.

 

Requirement: Inspect and repair in accordance with British Aerospace 125 S.B. 71-38.

 

Note: If engine mounts are found to be damaged on aircraft fitted with thrust reversers, their fatigue life is limited. Refer AD/HS 125/45 at latest amendment.

 

Compliance: Prior to 30 November 1985.

 

Background: Several cases of damage to the forward engine mounting caused by fouling with the cowling have been reported. This damage could result in reduction of fatigue life.

 

Overview

The Civil Aviation Regulations 1998, under Part 39, includes Airworthiness Directives that aim to address specific safety issues in civil aviation. One such directive, AD/HS 125/72, was enacted to address the problem of engine mounting cowling damage in British Aerospace BAe 125 Series aeroplanes fitted with Garrett TFE 731-3R-1H engines. This legislation was introduced by the Civil Aviation Safety Authority (CASA) to ensure the safety and airworthiness of these aircraft by mandating inspections and necessary repairs as per British Aerospace 125 S.B. 71-38. The directive was prompted by reports of damage to the forward engine mountings due to interference with the cowling, which could compromise the fatigue life of the engine mounts, particularly in aircraft equipped with thrust reversers. Compliance with this directive was required before 30 November 1985, underscoring the urgency and importance of addressing this safety issue.

Scope and Application

The Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, specifically AD/HS 125/72, applies to all models of British Aerospace BAe 125 series aeroplanes that are fitted with Garrett TFE 731-3R-1H engines. This regulation is a part of the broader framework established under the Civil Aviation Regulations 1998, which governs aviation safety across Australia. The directive mandates an inspection and subsequent repair of the engine mounting cowling to ensure airworthiness, as detailed in British Aerospace 125 Service Bulletin 71-38. Notably, if an aircraft of this series is equipped with thrust reversers, the fatigue life of the engine mounts may be compromised if damage is detected, a matter that should be addressed in accordance with AD/HS 125/45. Compliance with these directives must be achieved prior to 30 November 1985, reflecting the urgency and critical nature of the reported damage instances. This regulation applies on a national level, impacting all operators and maintenance personnel involved with the specified aircraft within the Australian jurisdiction.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105, includes the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives (AD) concerning the British Aerospace BAe 125 Series Aeroplanes. One such directive is AD/HS 125/72, which addresses issues of engine mounting cowling damage. This directive applies to all models of the BAe 125 series fitted with Garrett TFE 731-3R-1H engines (Section 39-105). According to the directive, operators must inspect and repair the engine mounting cowling in accordance with British Aerospace Service Bulletin 71-38. This requirement is critical to prevent any potential damage to the engine mounts which could compromise the aircraft's safety and operational integrity. Operators of the BAe 125 Series Aeroplanes are obligated to ensure that inspections and repairs are carried out as specified in the directive. This involves meticulously checking the engine mounting cowling for any signs of damage or wear, and conducting necessary repairs to mitigate any risk of reduced fatigue life in the engine mounts. If the aircraft is equipped with thrust reversers, additional considerations must be made as outlined in AD/HS 125/45. Compliance with these directives is mandatory and must be achieved prior to 30 November 1985, as stipulated in the regulation. Failure to comply with these directives could result in significant safety risks, potentially leading to catastrophic failure of the engine mounts during flight. In terms of consequences, non-compliance with the airworthiness directive could result in serious repercussions. The Civil Aviation Regulations outline various potential penalties and legal consequences for breaches of these requirements. Operators found in violation of the directive could face substantial fines, enforcement actions, or even grounding of the aircraft in question. The seriousness of the potential penalties reflects the importance of adhering to these safety regulations to ensure the safety of passengers, crew, and the general public. The specific maximum penalties are not detailed in the given text but can be found in other sections of the Civil Aviation Regulations, reflecting the stringent approach taken towards enforcing aviation safety standards.

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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.