AD/DC4/16 - Tailplane Outer Hinge Bracket - Modification

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Legislation au F2006B08821 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/DC4/16 Tailplane Outer Hinge Bracket - Modification NK

Document: 1. Douglas SB (DC4) No. 73, dated 23 September 1947; or

 

2. FAA AD 47-33-1; or

 

3. ANO 105.1.16.2.5.15, Issue 2.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, under Part 39 - 105, address the regulation of airworthiness directives to ensure the safety of aircraft operations within Australia. Specifically, Airworthiness Directive AD/DC4/16 targets the modification of tailplane outer hinge brackets in Douglas DC4 series aeroplanes to rectify known safety issues. Enacted by the Civil Aviation Safety Authority (CASA), this directive aims to mitigate risks associated with structural integrity in older aircraft models, aligning with the overarching policy objective of maintaining high safety standards in civil aviation. By referencing established documents such as the Douglas SB (DC4) No. 73 and FAA AD 47-33-1, CASA ensures that the modifications are consistent with international safety practices and regulatory requirements.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertain to the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives for Douglas DC4 Series Aeroplanes, with a focus on the AD/DC4/16 Tailplane Outer Hinge Bracket - Modification. This regulation applies to all operators of Douglas DC4 aircraft within the Commonwealth of Australia, ensuring that such aircraft meet specific safety standards. The directive mandates modifications to the tailplane outer hinge bracket, referencing documents such as Douglas SB (DC4) No. 73 dated 23 September 1947, FAA AD 47-33-1, and ANO 105.1.16.2.5.15, Issue 2, to ensure continued airworthiness. The application of these regulations is not limited by state or territory boundaries but rather extends across the entire nation, thereby ensuring uniformity in aviation safety standards. There are no stated exclusions or exemptions within this particular directive, meaning that all relevant aircraft must comply with the specified modifications without exception. The application of these regulations may be further detailed or extended through subordinate instruments issued by CASA.

Key Provisions

The Civil Aviation Regulations 1998, particularly under PART 39 - 105, address the safety directives for specific aircraft types, such as the Douglas DC4 series aeroplanes. A notable section is AD/DC4/16, which pertains to the modification of the tailplane outer hinge bracket (subsection 105.1.16.2.5.15). This directive mandates that modifications must be carried out as per the specifications provided in one of three documents: Douglas SB (DC4) No. 73 dated 23 September 1947; FAA AD 47-33-1; or ANO 105.1.16.2.5.15, Issue 2. These documents outline the technical requirements and procedures necessary to ensure the structural integrity of the tailplane outer hinge bracket, which is crucial for the safe operation of the aircraft. Operators and owners of Douglas DC4 aeroplanes are obligated to comply with the requirements set forth in the specified documents. This includes conducting the necessary modifications to the tailplane outer hinge bracket as detailed. The regulations impose a duty on these parties to ensure that the aircraft meets the specified airworthiness standards, thereby maintaining a high level of safety for all passengers and crew on board. Compliance with these directives is critical, as the structural integrity of the tailplane outer hinge bracket directly affects the aircraft's stability and control during flight. Failure to comply with the airworthiness directives stipulated in AD/DC4/16 can lead to significant legal and operational repercussions. For instance, operating a Douglas DC4 aeroplane without the required modifications to the tailplane outer hinge bracket could result in the aircraft being deemed non-airworthy. Consequently, the operator could face enforcement actions, including fines and potential grounding of the aircraft. The severity of the penalties underscores the importance of adhering to these safety regulations to prevent any compromise in flight safety. In cases of non-compliance, the Civil Aviation Safety Authority has the authority to take stringent measures to enforce the directives and uphold safety standards.

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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.