AD/BEECH 65/3 - Nose Landing Gear Attachment Bolts Replacement

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Legislation au F2006B04127 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 65 and 70 (Queen Air) Series Aeroplanes

 

AD/BEECH 65/3 Nose Landing Gear Attachment

Bolts Replacement Applicability: Model 65-A80 with S/Nos. LD-34, LD-46 & LD-151 to LD-231. Document:               Beechcraft SB 65-15.

Compliance: Within 100 hours time in service after 13 October 1965.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


11/67

Overview

The Civil Aviation Regulations 1998, specifically Part 39 - 105, establish a comprehensive framework for ensuring the airworthiness of aircraft operating in Australia. This part of the regulations includes detailed airworthiness directives, such as AD/BEECH 65/3, which is pertinent to Beechcraft 65 and 70 (Queen Air) Series Aeroplanes. This directive mandates the replacement of nose landing gear attachment bolts on specified models within a defined period after a certain date, in this case, within 100 hours’ time in service after 13 October 1965. The directive was enacted by the Civil Aviation Safety Authority and aims to address specific safety concerns identified in the operation of these aircraft models, ensuring that they maintain a high standard of safety and reliability in Australian airspace. The objective is to mitigate potential risks associated with the failure of these critical components, thereby protecting both passengers and crew.

Scope and Application

The Civil Aviation Safety Authority (CASA) administers the Civil Aviation Regulations 1998, specifically Part 39 - 105, which outlines the Schedule of Airworthiness Directives. This legislation mandates the replacement of nose landing gear attachment bolts for Beechcraft 65 and 70 (Queen Air) series aeroplanes. This directive applies to specific model 65-A80 aircraft with serial numbers ranging from LD-34 to LD-231, excluding LD-46 and LD-151. Compliance is required within 100 hours of time in service after 13 October 1965, as stipulated in Beechcraft Service Bulletin 65-15. The scope of this regulation is limited to the specified aircraft models and serial numbers, and it is enforced across the Commonwealth of Australia, ensuring that all relevant operators and maintenance providers within the national jurisdiction adhere to these safety directives. This regulation extends its application through subordinate instruments, ensuring thorough and consistent enforcement of the airworthiness standards.

Key Provisions

The primary sections of this legislation (AD/BEECH 65/3) require the replacement of specific bolts in the nose landing gear attachments for certain models of the Beechcraft 65 and 70 series aeroplanes. Specifically, it mandates compliance for models 65-A80 with serial numbers LD-34, LD-46, and LD-151 to LD-231. This directive is derived from the Beechcraft Service Bulletin 65-15 and must be implemented within 100 hours of time in service after 13 October 1965, as outlined in section 11/67. The intent is to ensure the continued airworthiness and safety of these aircraft by addressing potential issues with the specified bolts. The obligations under this legislation impose several responsibilities on the operators and maintenance personnel of the affected aircraft. These include conducting a thorough inspection of the nose landing gear attachment bolts, replacing any defective or worn bolts as per the specifications in the Beechcraft Service Bulletin 65-15, and documenting the compliance in the aircraft’s maintenance records. It is critical that these actions are performed by qualified personnel and that all replaced parts are logged appropriately to maintain an accurate history of maintenance activities. The legislation underscores the importance of adhering to the manufacturer's recommendations and ensuring that the aircraft remains in a safe operational condition. Failure to comply with the provisions of this directive can result in significant consequences. Under the Civil Aviation Regulations 1998, non-compliance with airworthiness directives is a serious matter. Violations may lead to penalties for both the aircraft operator and the maintenance personnel involved. Civil penalties can include substantial fines, and in severe cases, criminal charges may be brought against the operator or the certifying authority. Additionally, the aircraft may be grounded until the required maintenance is completed, which can have significant operational and financial repercussions for the operator. The specific penalties and enforcement actions are detailed within the broader framework of the Civil Aviation Regulations.

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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.