AD/DC4/11 - Vertical Stabiliser Attachment Fittings, AN Type Bolts - Replacement

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Legislation au F2006B08816 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

 


Douglas DC4 Series Aeroplanes

 

AD/DC4/11 Vertical Stabiliser Attachment Fittings, NK

AN Type Bolts - Replacement

Document: 1. Douglas SB (DC4) No. 11 dated 4 November, 1946; or

 

2. FAA AD 47-2-2; or

 

3. ANO 105.1.16.2.5.10, Issue 2.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Commonwealth of Australia, encompass a broad array of regulations designed to ensure the safety and efficiency of civil aviation within the country. Specifically, Part 39 of these regulations, which pertains to Airworthiness Directives, was introduced to address the need for consistent and enforceable standards in maintaining the airworthiness of aircraft. One such Airworthiness Directive, AD/DC4/11, pertains to the vertical stabiliser attachment fittings of Douglas DC4 series aeroplanes, mandating the replacement of NKAN type bolts. This directive was introduced by the Civil Aviation Safety Authority to mitigate the risk of structural failure in these critical components, thereby ensuring the safety of all air passengers and crew. The overarching policy objective is to maintain the highest possible safety standards in civil aviation, thereby protecting the public and promoting confidence in air travel.

Scope and Application

The Civil Aviation Safety Authority (CASA) under the Civil Aviation Regulations 1998, specifically Part 39 - 105, has issued an Airworthiness Directive (AD) concerning the Douglas DC4 Series Aeroplanes, targeting the vertical stabiliser attachment fittings, NKAN type bolts. This legislation applies to all aircraft operators, maintenance providers, and aviation personnel responsible for the upkeep of Douglas DC4 aircraft within Australia. The directive mandates the replacement of specified bolts to ensure compliance with safety standards, thereby affecting entities involved in the maintenance, operation, and certification of these aircraft. The geographic reach of this legislation is national, applying throughout the Commonwealth of Australia, and it extends to all aircraft registered under the Civil Aviation Regulations, irrespective of their location during operation. There are no stated exclusions or exemptions within the AD itself; however, the application might be subject to modifications or extensions through subordinate instruments issued by CASA, which can further detail the compliance requirements or provide additional clarifications on the implementation of the directive.

Key Provisions

The main operative sections of the Civil Aviation Regulations 1998, specifically under PART 39 - 105, focus on the safety directives for the Douglas DC4 series aeroplanes. The regulation AD/DC4/11 pertains to the replacement of vertical stabiliser attachment fittings and NKAN type bolts. According to section (1), the relevant document for compliance is either the Douglas SB (DC4) No. 11 dated 4 November 1946, the FAA AD 47-2-2, or the ANO 105.1.16.2.5.10, Issue 2. This directive mandates that specific parts of the Douglas DC4 aeroplanes must be replaced to ensure continued airworthiness and safety. The obligations imposed by these regulations are clear and specific. Operators and owners of Douglas DC4 aeroplanes must adhere to the requirements set out in the referenced documents. They must ensure that the vertical stabiliser attachment fittings and NKAN type bolts are replaced as specified. This involves following detailed technical instructions and specifications provided in the documents to maintain compliance with civil aviation safety standards. Failure to comply with these directives could result in the aeroplane being grounded until the necessary repairs and replacements are made. Non-compliance with the AD/DC4/11 directive can lead to serious consequences. Civil Aviation Safety Authority (CASA) may take enforcement actions against operators and owners who fail to adhere to these airworthiness directives. The penalties for non-compliance can include fines, suspension or revocation of the aircraft's certificate of airworthiness, and potential criminal charges. The maximum penalties for these offences are significant, reflecting the importance of adhering to safety directives to prevent accidents and ensure the safety of passengers and crew. It is imperative that all parties involved take these regulations seriously and ensure that all required actions are completed promptly and correctly.

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Aviation Law
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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.