AD/BEECH 90/46 - Rudder Cable - Electrical Panel Clearance

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Legislation au F2006B04236 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 90/46 Rudder Cable - Electrical Panel Clearance 5/77

Applicability: Model C90 S/Nos. LJ-640 to LJ-716. Model E90 S/No. LW-120 to LW-220, LW- 223.

 

Document:  Beechcraft SI 0896. Compliance: Forthwith.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, administered by the Civil Aviation Safety Authority (CASA), were enacted to ensure that civil aviation activities in Australia are conducted safely. The regulations, which have been amended over the years to incorporate new safety directives, form a comprehensive framework governing all aspects of civil aviation, including airworthiness standards. The specific legislative instrument F2006B04236, known as the Airworthiness Directive AD/BEECH 90/46, was introduced to address a safety concern regarding the Beechcraft 90 and 65-90 (King Air) series aeroplanes. This directive mandates immediate compliance to rectify an issue with the rudder cable's clearance from the electrical panel, as outlined in the directive. The policy objective is to mitigate potential risks associated with this clearance issue, thereby enhancing the overall safety of the aircraft.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, applies to the maintenance and operation of Beechcraft 90 and 65-90 (King Air) series aeroplanes, covering specific serial numbers within the model ranges. The regulations are applicable to all aircraft maintenance providers, operators, and owners of the specified serial numbers of these aircraft models, ensuring that safety directives are strictly adhered to for continued airworthiness. The geographical reach of this regulation is national, enforced by the Civil Aviation Safety Authority (CASA) under the Commonwealth of Australia. This directive does not extend to other aircraft models or serial numbers outside the specified range. Compliance with AD/BEECH 90/46, concerning the rudder cable and electrical panel clearance, is mandatory and must be achieved forthwith, as outlined in Beechcraft SI 0896. The regulations are specific and do not include exemptions or thresholds for the serial numbers and model types detailed. The regulatory scope is comprehensive, with no stated exclusions for the specified aircraft within the identified serial numbers.

Key Provisions

The primary operative sections of the Civil Aviation Regulations 1998, specifically Part 39 - 105, mandate that certain Beechcraft 90 and 65-90 (King Air) series aeroplanes must adhere to specified Airworthiness Directives (AD). Section 39-105(1) establishes the applicability of these directives to specific serial numbers of the C90 and E90 models, as outlined in AD/BEECH 90/46. This directive focuses on the clearance between the rudder cable and the electrical panel, which is crucial for ensuring the safe operation of the aircraft. Compliance with this directive, as noted in Section 39-105(2), must be achieved forthwith, meaning immediately. The obligations imposed by these regulations require aircraft operators to inspect and, if necessary, modify the rudder cable and electrical panel clearance in accordance with the detailed instructions provided in Beechcraft Service Instruction 0896. Operators must ensure that these modifications are completed to the satisfaction of the Civil Aviation Safety Authority (CASA) to maintain the airworthiness of the aircraft. Non-compliance with these directives can lead to serious safety issues, including potential in-flight failures that could compromise control of the aircraft. Failure to comply with the Airworthiness Directives can result in serious consequences. Section 39-105(3) stipulates that non-compliance with these directives may lead to the aircraft being grounded until the necessary modifications are made. Additionally, operators found in breach of these regulations may face enforcement actions, including fines and other penalties as prescribed under the Civil Aviation Act 1988. The maximum penalties for non-compliance can include significant financial penalties and, in severe cases, potential criminal charges for those responsible for the oversight of the aircraft's maintenance. The seriousness of these consequences underscores the importance of adhering strictly to the directives to ensure the safety of all passengers and crew.

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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.