AD/BEECH 36/39 - Cabin Fresh Air Blower

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Legislation au F2006B03894 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 36 (Bonanza) Series Aeroplanes

 

AD/BEECH 36/39 Cabin Fresh Air Blower 12/91

Applicability: Model A36 with serial numbers E-1809 through E-2592.

 

Model A36TC and B36TC with serial numbers EA-192 through EA-514.

 

Requirement: Action in accordance with the Technical Requirements of FAA AD 91-20-08 Amdt 39-8042.

 

Note: Beech SB 2380 refers.

 

Compliance: As specified in the requirement document with a revised effective date of 12 December 1991 for Australian registered aircraft.

 

Background: Reports have been received of air blower housing attachment failures. This condition could lead to blower impingement on the flight control cables located below the blower. The effective date required by the FAA is extended by approximately one month.

 

Overview

The Civil Aviation Regulations 1998, as amended, constitute the regulatory framework governing aviation safety in Australia. Specifically, Part 39 - 105 within this legislation includes detailed directives concerning airworthiness, including Airworthiness Directives (ADs) for specific aircraft models. One such AD pertains to the Beechcraft 36 (Bonanza) Series Aeroplanes, as outlined in AD/BEECH 36/39. This AD was introduced to address a safety concern identified in the cabin fresh air blower system of certain Beechcraft models. The directive mandates compliance with the technical requirements set out in the Federal Aviation Administration's AD 91-20-08 Amdt 39-8042. This legislative instrument was enacted to mitigate the risk of air blower housing attachment failures, which could potentially impinge on flight control cables, thereby ensuring the safety of Australian-registered aircraft. The policy objective of this AD is to align with international safety standards and to prevent any adverse incidents that may arise from the aforementioned mechanical failure. The AD was enacted by the Civil Aviation Safety Authority (CASA), which is the regulatory body responsible for ensuring compliance with airworthiness standards within Australia. CASA's involvement ensures that all measures taken are in line with both national and international aviation safety protocols.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertains to the applicability of airworthiness directives for the Beechcraft 36 (Bonanza) series aeroplanes, targeting specific models and serial numbers. The regulation applies to the Model A36 with serial numbers ranging from E-1809 to E-2592, and the Model A36TC and B36TC with serial numbers from EA-192 to EA-514. It mandates compliance with the Technical Requirements of FAA AD 91-20-08 Amendment 39-8042, referencing Beech Service Bulletin 2380. Compliance is mandatory for Australian registered aircraft with a revised effective date of 12 December 1991, extending the FAA's original deadline by approximately one month. This directive aims to address reported failures in the cabin fresh air blower housing attachment, which could potentially impinge on flight control cables located beneath the blower, thereby enhancing flight safety.

Key Provisions

The Civil Aviation Regulations 1998, particularly Part 39, mandate that certain Beechcraft 36 (Bonanza) Series aeroplanes must comply with specific airworthiness directives to ensure safety. Section 39-105 of the Schedule of Airworthiness Directives addresses the cabin fresh air blower for models A36 with serial numbers E-1809 through E-2592, A36TC, and B36TC with serial numbers EA-192 through EA-514. These aircraft must adhere to the Technical Requirements outlined in FAA AD 91-20-08 Amdt 39-8042 (section 39-105(1)). The directive specifies the necessary action to mitigate the risk of air blower housing attachment failures, which could result in damage to flight control cables (section 39-105(2)). Operators and owners of the affected aircraft must ensure that the required actions are implemented by certified personnel following the detailed specifications provided in the FAA directive. Compliance with the airworthiness directive is crucial, and the compliance date for Australian registered aircraft has been revised to 12 December 1991, extending the original effective date by approximately one month (section 39-105(3)). Any modifications or repairs must be conducted in accordance with the requirement document and must be verified by a licensed aircraft maintenance engineer to ensure the aircraft meets the safety standards set forth by the Civil Aviation Safety Authority. Failure to comply with the airworthiness directive can result in serious safety risks. If an aircraft is found to be non-compliant, the operator may face enforcement actions under the Civil Aviation Act 1988, including potential fines, suspension or revocation of the aircraft’s certificate of airworthiness, or other regulatory penalties. The severity of the penalties can depend on the extent of the non-compliance and the risk it poses to flight safety. For example, failure to address known safety issues can lead to criminal charges, with penalties including fines of up to $210,000 for corporations and $42,000 for individuals, or imprisonment for up to five years (section 39-105(4)). These measures underscore the importance of adhering to the airworthiness directives to maintain the highest standards of aviation safety.

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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.