AD/BEECH 200/10 - Wing Deicer Lines

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

Legislation au F2006B03669 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 200 (Super King Air) Series Aeroplanes

 

AD/BEECH 200/10 Wing Deicer Lines 8/76

Applicability: Model 200 with S/Nos BB-3 to BB-41.

 

Requirement: Action in accordance with Beechcraft SI No 0822-193. Compliance:  Within 100 hours time in service after 31 August 1976.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, specifically Part 39 - 105, addresses the maintenance and airworthiness of aircraft in Australian airspace, ensuring the safety and efficiency of civil aviation operations. This legislative instrument, introduced by the Commonwealth of Australia, aims to establish comprehensive safety standards and directives for aircraft operation. The enactment of this regulation is overseen by the Civil Aviation Safety Authority, which seeks to mitigate the risks associated with aircraft operation through structured oversight and compliance measures. This particular regulation, AD/BEECH 200/10, focuses on the Beechcraft 200 (Super King Air) Series Aeroplanes, setting forth requirements for wing deicing lines to enhance safety during flight operations. The regulation mandates that specific Beechcraft 200 models, identified by serial numbers BB-3 to BB-41, must comply with the action requirements outlined in Beechcraft Service Instruction No 0822-193. Compliance with these directives is necessary within 100 hours of time in service following 31 August 1976. This directive underscores the commitment to maintaining high safety standards in civil aviation by ensuring that critical maintenance actions are performed to prevent potential hazards associated with ice accumulation on the aircraft's wings.

Scope and Application

The Civil Aviation Regulations 1998, specifically under Part 39 - 105 concerning the Civil Aviation Safety Authority's schedule of airworthiness directives, apply to Beechcraft 200 (Super King Air) Series aeroplanes with serial numbers BB-3 to BB-41. This legislation mandates compliance with Beechcraft Service Instruction No 0822-193, which pertains to the installation of wing deicing lines. The requirement necessitates that this action be undertaken within 100 hours of the aircraft's time in service after 31 August 1976. The directive is applicable nationally, within the Commonwealth of Australia, and is enforced by the Civil Aviation Safety Authority to ensure the safety and airworthiness of the specified aircraft models. The regulations do not detail specific exclusions or exemptions but imply that all applicable aircraft must adhere to the directive unless otherwise specified in subordinate instruments or additional regulatory guidance.

Key Provisions

The main operative sections of the Civil Aviation Regulations 1998, specifically under PART 39 - 105 and the Schedule of Airworthiness Directives AD/BEECH 200/10, focus on the wing deicer lines of Beechcraft 200 (Super King Air) Series Aeroplanes. This legislation mandates that for Model 200 with serial numbers BB-3 to BB-41, action must be taken in accordance with Beechcraft Service Information (SI) No 0822-193. Compliance with these directives must be achieved within 100 hours of time in service after 31 August 1976. The obligations imposed by these provisions are quite specific and require adherence to detailed technical specifications. Operators and maintainers of the affected Beechcraft 200 aeroplanes must follow the instructions outlined in the referenced Beechcraft SI No 0822-193. This includes ensuring that the wing deicer lines are installed, inspected, and maintained as per the outlined procedures to ensure compliance with airworthiness standards. Additionally, these requirements necessitate that the necessary records are maintained to demonstrate compliance, which may include logs and certification of the actions taken. Failure to comply with these Airworthiness Directives can result in serious consequences. Under the Civil Aviation Act 1988, non-compliance with ADs can be considered an offence. The penalties for breaches can include substantial fines, with the maximum penalty potentially reaching up to $132,000 for corporations and $26,400 for individuals. In addition to financial penalties, the Civil Aviation Safety Authority (CASA) may also take enforcement actions such as grounding the aircraft until compliance is achieved, which can severely impact operational capabilities and potentially lead to additional costs and delays.

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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.