AD/CESSNA 208/18 - Emergency Power Lever Shear Wire

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

Legislation au F2005L01360 Not in force Legislative Instrument

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CIVIL AVIATION ACT 1988

CIVIL AVIATION REGULATIONS 1998

ISSUE OF AIRWORTHINESS DIRECTIVE

Under section 98 of the Civil Aviation Act 1988, the Governor-General may make regulations for the purposes of the Act and in the interests of the safety of air navigation.  Under regulation 39.001 of the Civil Aviation Safety Regulations 1998, CASA may issue airworthiness directives (ADs) for kinds of aircraft or aeronautical products.  Subregulation 39.001(5) of the Civil Aviation Safety Regulations 1998 provides that an AD is a disallowable instrument for the purposes of section 46A of the Acts Interpretation Act 1901. Therefore, in accordance with section 6 of the Legislative Instruments Act 2003, an AD is a legislative instrument.

Under Annex 8 to the Convention on International Civil Aviation, the State of Design has overall responsibility for continuing airworthiness of an aircraft type, and must provide any information necessary to ensure the continuing airworthiness of a type to appropriate States of Registry.  ADs (and their equivalents) are the most common form of continuing airworthiness information, and are issued by most ICAO Contracting States.

The State of Registry of an individual aircraft is responsible for its continuing airworthiness.  Under Annex 8, the State of Registry must develop or adopt requirements to ensure the continuing airworthiness of aircraft.  When a State of Design issues an AD against a type of aircraft on the Australian Register, CASA, as Australia’s national airworthiness authority, must assess that information and, if appropriate, issue an Australian AD to mandate the requirements of the State of Design.

CASA has raised AD/CESSNA 208/18 Original issue to correct an unsafe situation on Cessna 208 and 208B aircraft.  Following an incident involving the use of the Emergency Power Lever (EPL), the Australian Transport Safety Bureau (ATSB) recommended the fitment of frangible/ shear wire between the pedestal and the EPL. This will help ensure appropriate maintenance actions when the EPL has been used for any reason.  The AD will become effective on 7 July 2005.

CASA has carried out the required consultation process before the issue of this AD. This Directive is in response to ATSB occurrence report 200400443 and requires compliance with ATSB recommendations. Aircraft modification mandated by this AD is also mandated by the aircraft manufacturer.

The Office of Regulatory Review has determined that ADs do not require a Regulatory Impact Statement.

The AD has been made by the Head of Airworthiness Standards, Airworthiness Standards Branch, Standards Division, on behalf of CASA, in accordance with subsection 84A (2) of the Civil Aviation Act 1988.

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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.