AD/BEECH 36/42 Amdt 1 - Engine Fuel Metering Unit

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Legislation au F2006B03898 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

 


Beechcraft 36 (Bonanza) Series Aeroplanes

 

AD/BEECH 36/42

Amdt 1


Engine Fuel Metering Unit 9/96

 

Applicability: Bonanza A36TC aircraft serial numbers EA-1 through EA-146.

 

Requirement: To reduce the possibility of a fuel leak which could result in an engine compartment fire, carry out the requirements detailed in Beechcraft Mandatory Service Bulletin (MSB) Number 2420 Revision 1, "Accomplishment Instructions", Parts I or II and III.

 

Note: FAA Airworthiness Directive 92-17-01 refers.

 

Compliance: Effective 15 August 1996:

 

  1. Beechcraft MSB No. 2420 Rev.1, "Accomplishment Instructions" Parts I or II; within 50 hours time in service.

 

2.    Beechcraft MSB No. 2420 Rev.1, "Accomplishment Instructions" Part III; at intervals not to exceed 130 hours time in service.

 

Background: This directive was originally issued in March 1993 to require the inspection and modification of the engine fuel metering unit. The requirement was published to reduce the possibility of a fuel leak which could result in an engine compartment fire. This amendment introduces a requirement to fit a fuel metering unit drain hose with a higher temperature tolerance material, and a requirement to carry out a repetitive inspection of that drain hose.

 

The original issue of this Airworthiness Directive became effective on 4 March 1993.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, specifically Part 39, establish and regulate various safety standards for civil aviation in Australia. One particular legislative instrument, F2006B03898, focuses on issuing Airworthiness Directives (AD) to address safety concerns with specific aircraft models. Enacted by the Civil Aviation Safety Authority (CASA), this directive aims to mitigate risks associated with potential fuel leaks in the Beechcraft 36 (Bonanza) series aeroplanes. The primary objective is to reduce the likelihood of engine compartment fires, which could severely compromise flight safety. This legislative instrument is part of a broader regulatory framework designed to ensure that aircraft maintain the highest standards of safety and reliability throughout their operational life. The Beechcraft 36 (Bonanza) series AD, AD/BEECH 36/42 Amendment 1, addresses specific issues with the engine fuel metering unit by mandating detailed inspections and modifications as outlined in Beechcraft's Mandatory Service Bulletin Number 2420 Revision 1. This directive, effective from 15 August 1996, requires adherence to specific timelines for inspections and modifications to ensure that the aircraft remain airworthy. The legislative instrument was developed in response to identified safety risks and aims to ensure compliance with international safety standards, thus protecting both the aircraft and those on board.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, governs the safety requirements for civil aircraft in Australia, with the aim of ensuring the safety of aircraft operations. This particular legislative instrument pertains to the AD/BEECH 36/42 Amendment 1 concerning the Beechcraft 36 (Bonanza) series aeroplanes, with a focus on the engine fuel metering unit. The regulation applies to Bonanza A36TC aircraft with serial numbers EA-1 through EA-146. It mandates compliance with Beechcraft Mandatory Service Bulletin Number 2420 Revision 1, which includes specific accomplishment instructions designed to mitigate the risk of fuel leaks that could potentially cause an engine compartment fire. The directive outlines a compliance timeline, requiring the completion of certain tasks within 50 hours of time in service and subsequent repetitive inspections at intervals not exceeding 130 hours of time in service. This legislative instrument is a component of the broader Civil Aviation Regulations 1998, which extend to the Commonwealth jurisdiction, ensuring a unified safety standard across Australia.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105, addresses the safety requirements for Beechcraft 36 (Bonanza) Series Aeroplanes through Airworthiness Directive AD/BEECH 36/42 Amendment 1. This directive applies to Bonanza A36TC aircraft with serial numbers EA-1 through EA-146 (section 1). The primary requirement is to mitigate the risk of a fuel leak leading to an engine compartment fire by adhering to the instructions detailed in Beechcraft Mandatory Service Bulletin (MSB) Number 2420 Revision 1. This involves following the "Accomplishment Instructions" in Parts I or II and Part III of the MSB. The directive references the FAA Airworthiness Directive 92-17-01 for additional context. Under this directive, operators of the specified aircraft must ensure that the modifications and inspections outlined in the MSB are carried out within specific timeframes. Specifically, the inspection and modification of the engine fuel metering unit, as described in Parts I or II of the MSB, must be completed within 50 hours of time in service (section 1). Furthermore, repetitive inspections of the fuel metering unit drain hose, as stipulated in Part III of the MSB, must be conducted at intervals not exceeding 130 hours of time in service (section 2). These requirements are intended to maintain the airworthiness of the aircraft and prevent potential safety hazards. Non-compliance with the provisions of AD/BEECH 36/42 Amendment 1 can result in serious safety risks. The regulations impose strict obligations on aircraft operators to adhere to the specified inspection and modification schedules. Failure to comply with these requirements may result in the aircraft being deemed unairworthy, leading to potential grounding and further enforcement actions by the Civil Aviation Safety Authority (CASA). Such non-compliance could also expose operators to civil or criminal liability if a failure to adhere to the directive results in an accident or incident. The Civil Aviation Regulations 1998 do not explicitly outline specific penalties for non-compliance with AD/BEECH 36/42 Amendment 1. However, the broader regulatory framework under which these directives operate does provide for enforcement actions. For instance, CASA can issue fines, impose penalties, or take other regulatory measures against operators who fail to comply with airworthiness directives. The maximum penalties for such breaches can vary depending on the severity of the non-compliance and any resultant incidents. Civil penalties may include substantial fines, while criminal penalties could involve imprisonment, depending on the circumstances of the breach.

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Area of Law
Civil Aviation Law
Instrument
Regulation
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Definitions & Interpretation
Compliance Obligations
Enforcement Powers
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Airworthiness Directives

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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.