AD/BEECH 56/15 - Fuel System - Placards

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

Legislation au F2006B04045 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 56TC (Turbo Baron) Series Aeroplanes

 

AD/BEECH 56/15 Fuel System - Placards 7/74

Applicability:  Models 56TC and A56TC with S/Nos. TG-1 to TG-94. Requirement:  Action in accordance with Beechcraft SI No. 0559-281. Compliance:   Within 100 hours’ time in service after 31 July 1974.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Australian Parliament, serve as the primary regulatory framework governing aviation safety in Australia. Among these regulations, Part 39 specifically addresses Airworthiness Directives, ensuring that aircraft meet the necessary safety standards. The Legislative Instrument F2006B04045, AD/BEECH 56/15, pertains to the Beechcraft 56TC (Turbo Baron) Series Aeroplanes and specifically targets the fuel system placards for models 56TC and A56TC with serial numbers TG-1 to TG-94. This directive was introduced to address a specific safety concern related to fuel system placards, ensuring compliance with Beechcraft Service Instruction No. 0559-281 within 100 hours’ time in service after 31 July 1974. The overarching policy objective is to maintain the highest standards of aviation safety and to mitigate any risks associated with the operation of these aircraft.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertains to airworthiness directives issued by the Civil Aviation Safety Authority (CASA) and applies to certain aircraft types. In this instance, AD/BEECH 56/15 pertains to the Beechcraft 56TC (Turbo Baron) Series Aeroplanes, specifically models 56TC and A56TC with serial numbers ranging from TG-1 to TG-94. The directive mandates that action be taken in accordance with Beechcraft Service Information (SI) No. 0559-281, which pertains to the fuel system placards, to ensure the aircraft's continued airworthiness. This directive must be complied with within 100 hours’ time in service after 31 July 1974, thereby ensuring that the specified aircraft maintain the required safety standards. The geographic and jurisdictional reach of this directive is governed by the Commonwealth of Australia, thus applying nationally across all states and territories. The application of this regulation is limited to the specified models and serial numbers, with no additional exclusions, exemptions, or thresholds outlined within the text. The implementation and enforcement of this airworthiness directive may be further detailed through subordinate instruments issued by CASA.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105, contain the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives (AD) for various aircraft types, including the Beechcraft 56TC (Turbo Baron) series aeroplanes. The relevant AD for this aircraft model is AD/BEECH 56/15, which pertains to the fuel system placards. This directive applies to models 56TC and A56TC with serial numbers ranging from TG-1 to TG-94. The directive requires that the fuel system placards be updated in accordance with Beechcraft Service Instruction (SI) No. 0559-281. Compliance with this directive must be achieved within 100 hours of the aircraft's time in service following 31 July 1974. The AD/BEECH 56/15 imposes certain obligations and requirements on the parties or entities governed by the Civil Aviation Regulations 1998. Primarily, it mandates that the fuel system placards on the specified Beechcraft 56TC models are to be updated according to the guidance provided in Beechcraft SI No. 0559-281. This involves ensuring that the placards accurately reflect the current procedures and safety information related to the aircraft’s fuel system. Owners and operators of these aircraft are required to ensure that the necessary updates are implemented within the stipulated timeframe to maintain the aircraft's airworthiness. Failure to comply with the AD/BEECH 56/15 may result in various consequences. Although specific civil or criminal penalties are not detailed within this directive, non-compliance with CASA airworthiness directives generally can lead to enforcement actions by CASA. Such actions may include grounding of the aircraft until compliance is achieved, fines, and other regulatory penalties. The severity of the consequences depends on the degree of non-compliance and its impact on the safety and airworthiness of the aircraft. It is essential for operators and owners to adhere to these directives to avoid potential safety hazards and regulatory sanctions.

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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.