AD/BEECH 60/37 - Nose Baggage Locker Door

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B04097 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

 


Beechcraft 60 (Duke) Series Aeroplanes

 

AD/BEECH 60/37 Nose Baggage Locker Door 8/81

Applicability: All models 60, A60 and B60 with S/Nos. P-4 to P-569. Requirement:  Action in accordance with Beechcraft SI No. 1169.

Compliance: Before 1 January 1982.

 

Background: The manufacturer has designed a secondary latch installation for the nose baggage locker door which the factory considers as a mandatory modification.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Australian Parliament, provide a comprehensive framework for regulating aviation safety and operations within Australia. This legislation was introduced to address the need for stringent safety standards and regulatory oversight in the aviation industry, aiming to ensure the safety of passengers and personnel, as well as to maintain the integrity of civil aviation infrastructure. The specific legislative instrument, F2006B04097, pertains to Part 39 - 105 of the Civil Aviation Regulations and focuses on Airworthiness Directives, ensuring aircraft meet necessary safety standards. This directive, AD/BEECH 60/37, targets the Beechcraft 60 (Duke) series aeroplanes, mandating a modification to the nose baggage locker door to comply with Beechcraft Service Instruction No. 1169. The directive underscores the policy objective of enhancing aircraft safety by requiring compliance before 1 January 1982.

Scope and Application

The Civil Aviation Regulations 1998, under Part 39 - 105, specifically address the safety of Beechcraft 60 (Duke) Series Aeroplanes through Airworthiness Directives. This regulation applies to all models 60, A60, and B60 with serial numbers ranging from P-4 to P-569, mandating compliance with Beechcraft Service Instruction No. 1169 for the nose baggage locker door. This requirement ensures that a secondary latch installation is implemented as a mandatory modification, with compliance necessary before 1 January 1982. This regulation is part of the overarching framework managed by the Civil Aviation Safety Authority, ensuring that the specified aircraft meet necessary safety standards. The scope of this legislative instrument is explicitly defined for the mentioned aircraft models and serial numbers, underscoring the importance of adhering to the prescribed modifications. The geographic reach of this regulation is national, applying across the Commonwealth of Australia, ensuring that all aircraft within the specified parameters are uniformly compliant with the set safety standards. There are no stated exclusions, exemptions, or thresholds in this directive, reinforcing the mandatory nature of the compliance requirement. The regulation's application is further extended through subordinate instruments as necessary, ensuring that any updates or additional safety measures are effectively communicated and implemented.

Key Provisions

The Civil Aviation Regulations 1998 (Cth), particularly under Part 39 - 105 and the Civil Aviation Safety Authority Schedule of Airworthiness Directives, includes specific directives for aircraft such as the Beechcraft 60 (Duke) Series Aeroplanes. One such directive is AD/BEECH 60/37, which concerns the nose baggage locker door. This directive applies to all models 60, A60, and B60 with serial numbers P-4 to P-569. The requirement outlined in this directive mandates that the installation of a secondary latch in the nose baggage locker door must be carried out in accordance with Beechcraft Service Instruction No. 1169. To ensure compliance with this directive, any modifications must be completed before 1 January 1982. The regulations impose certain obligations on the owners and operators of the affected aircraft. These obligations include ensuring that the specified modifications are performed by qualified personnel, in accordance with the manufacturer's instructions, to maintain the airworthiness of the aircraft. The directive underscores the importance of adhering to the manufacturer’s guidelines to prevent any potential safety issues related to the nose baggage locker door. Owners and operators must also maintain documentation proving that the required modifications have been completed, as this may be necessary for compliance verification during airworthiness inspections. Failure to comply with the provisions set out in AD/BEECH 60/37 could result in significant consequences. Non-compliance with airworthiness directives is a serious matter under the Civil Aviation Act 1988 (Cth) and the Civil Aviation Regulations 1998. The consequences for breach may include enforcement actions by the Civil Aviation Safety Authority (CASA), which could involve fines or other penalties. The maximum penalties for non-compliance can be severe, reflecting the critical importance of ensuring that aircraft meet required safety standards. Such penalties are intended to enforce adherence to safety regulations and maintain the highest standards of airworthiness in civil aviation.

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Area of Law
Civil Aviation Law
Instrument
Regulation
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Definitions & Interpretation
Compliance Obligations
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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.