AD/BEECH 65/46 - Fire Shield Installation - Inspection

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Legislation au F2006B04143 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 65 and 70 (Queen Air) Series Aeroplanes

 

AD/BEECH 65/46 Fire Shield Installation - Inspection 4/76

Applicability: Model 65-B80 with S/Nos. LD-476 to LD-502 & LD-504. Document:  1. Beechcraft SI No. 0771-065, or

2. FAA AD 75-25-04, Amendment 39-2449.

 

Compliance: Within 50 hours time in service after 16 April 1976.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, serve as a comprehensive regulatory framework governing civil aviation in the country. The regulations are periodically updated to address emerging safety issues and ensure compliance with international standards. One such update is the legislative instrument F2006B04143, which was introduced to address specific safety concerns related to the maintenance and operation of Beechcraft 65 and 70 (Queen Air) Series aeroplanes. The policy objective of this instrument is to mandate the inspection of fire shield installations on these aircraft models to prevent potential fire hazards, thereby enhancing overall aviation safety. This directive applies to Model 65-B80 with specific serial numbers, requiring compliance within 50 hours of time in service following the issuance date of 16 April 1976.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, establish the scope and application of the Civil Aviation Safety Authority’s airworthiness directives, including AD/BEECH 65/46. This particular directive pertains to the Beechcraft 65 and 70 (Queen Air) series aeroplanes, with a focus on the fire shield installation inspection. It applies to Model 65-B80 aircraft with serial numbers ranging from LD-476 to LD-502, and LD-504. Compliance with this directive is mandatory within 50 hours of time in service following 16 April 1976, as outlined in the specified documents: either Beechcraft SI No. 0771-065 or FAA AD 75-25-04, Amendment 39-2449. The directive ensures the aircraft meet necessary safety standards, governing the operations of these specific aircraft within the Commonwealth of Australia, ensuring adherence to federal regulations.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105 under the Civil Aviation Safety Authority, contain detailed provisions for maintaining the airworthiness of certain aircraft models. The regulation in question pertains to Beechcraft 65 and 70 (Queen Air) series aeroplanes, more specifically to the fire shield installation and its inspection, as outlined in AD/BEECH 65/46 (section 4/76). This regulation applies to Model 65-B80 aircraft with serial numbers ranging from LD-476 to LD-502 and LD-504. The primary requirement under this regulation is that the fire shield installation must be inspected in accordance with either Beechcraft Service Instruction No. 0771-065 or FAA AD 75-25-04, Amendment 39-2449. The inspection must be conducted within 50 hours of the aircraft's time in service following 16 April 1976. This ensures that the aircraft's fire shield installation is up to the necessary safety standards, thereby reducing the risk of fire-related incidents. In terms of obligations, the regulation imposes a clear and specific duty on the owners and operators of the affected Beechcraft 65-B80 aircraft. They must ensure that the fire shield installation is inspected within the stipulated timeframe. This requirement applies to any entity or individual who owns or operates these aircraft within the Australian jurisdiction, making compliance a non-negotiable aspect of their operational responsibilities. Failure to comply with this airworthiness directive can lead to serious consequences. While the specific civil or criminal penalties are not detailed within the regulation itself, non-compliance generally results in the aircraft being deemed non-airworthy. This can lead to grounding of the aircraft, preventing it from being operated until the required inspection is performed and any deficiencies are rectified. Additionally, regulatory authorities may impose fines or other sanctions on the operator or owner for failing to adhere to the stipulated safety requirements.

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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.