AD/BEECH 90/1 - Engine Oil Pressure Gauges - Modification

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Legislation au F2006B04200 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 90 and 65-90 (King Air) Series Aeroplanes

 

AD/BEECH 90/1 Engine Oil Pressure Gauges - Modification 11/67

Applicability: Model 65-90 prior to S/No. LJ-22. Document:  Beechcraft SB 65-6.

Compliance: Forthwith.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998 (Cth), enacted by the Parliament of Australia, form part of a comprehensive regulatory framework overseen by the Civil Aviation Safety Authority (CASA) to ensure the safety and efficiency of aviation in Australia. The regulations address various aspects of aviation safety, including airworthiness, licensing, and operational standards. One such regulation pertains to the Beechcraft 90 and 65-90 (King Air) series aeroplanes, specifically addressing engine oil pressure gauge modifications. This legislative instrument, identified as F2006B04200, was introduced to rectify identified safety concerns related to the accuracy and reliability of engine oil pressure gauges in certain models of the King Air series, specifically those with serial numbers prior to LJ-22. The directive aims to ensure that these aircraft meet the necessary safety standards by mandating timely compliance with the specified modifications as outlined in the Beechcraft Service Bulletin 65-6.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, governs the applicability of the Civil Aviation Safety Authority’s (CASA) Airworthiness Directives, including those for the Beechcraft 90 and 65-90 (King Air) series aeroplanes. This legislation applies to all entities and persons involved in the operation of these aircraft models, particularly focusing on those model 65-90 aeroplanes with serial numbers prior to LJ-22. The directive mandates modifications to the engine oil pressure gauges to ensure compliance with safety standards. The regulations are enforced across the Commonwealth, ensuring a uniform approach to aviation safety throughout Australia. There are no exclusions or exemptions specified in this directive, and the requirement is set forth as a mandatory compliance measure to be fulfilled immediately. This legislative instrument extends its reach by referencing specific documents such as Beechcraft Service Bulletin 65-6, which provides detailed guidance on implementing the required modifications. The regulation's scope is national, applying uniformly across all states and territories within Australia, ensuring that all operators of the specified Beechcraft aeroplanes adhere to the stipulated safety standards. The requirement for immediate compliance is non-negotiable, underscoring the importance of safety in civil aviation operations.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105, contain the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, which is critical for maintaining the safety standards of aircraft. One such directive pertains to the Beechcraft 90 and 65-90 (King Air) Series Aeroplanes, identified as AD/BEECH 90/1, focusing on the modification of engine oil pressure gauges. This directive applies to Model 65-90 aircraft with serial numbers prior to LJ-22 (section 11/67). The directive mandates that compliance with the requirements must be achieved forthwith, as outlined in Beechcraft Service Bulletin 65-6. The obligations under this directive require that modifications to the engine oil pressure gauges must be carried out immediately. Operators of the affected aircraft must ensure that the modifications are made in accordance with the instructions provided in Beechcraft Service Bulletin 65-6. This includes conducting any necessary inspections and ensuring that the modifications are properly documented. Operators must also verify that the modifications have been completed before the aircraft returns to service. Failure to comply with the provisions of this Airworthiness Directive can result in serious consequences. The directive specifies that non-compliance is not just a safety issue but also a regulatory one. If an operator fails to adhere to the requirements, they may face enforcement actions under the Civil Aviation Act 1988. This could include the issuance of a Notice of Proposed Civil Penalty, which may lead to significant fines. The severity of the penalties reflects the importance of ensuring that all modifications are performed correctly to maintain the airworthiness of the aircraft. Therefore, operators must take the directive seriously to avoid any potential legal repercussions.

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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.