AD/DC3/10 - Rear Luggage Compartment Tie Down Fittings - Modification

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Legislation au F2006B08787 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 DC3 Series Aeroplanes

 

AD/DC3/10 Rear Luggage Compartment Tie NK

Down Fittings - Modification

 

Applicability: All models modified in accordance with DCA 1900 series conversion drawings.

 

Requirement: 1. Replace rear luggage compartment tie-down fittings of the type called up in Drawing DCA 2188, Issue 1 by the larger type as detailed in Issue 3; or

 

2. ANOs Part 100 Appendix “A” Notice 7/10; or 3. ANO 105.1.16.1.5.10.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998 (Cth) were enacted to provide comprehensive safety regulations for civil aviation within Australia, ensuring that aircraft and aviation operations meet high safety standards. The regulations were brought into force by the Parliament of Australia, and their primary objective is to maintain and enhance the safety of civil aviation. Among the various sections of these regulations, Part 39 - 105, specifically pertaining to Civil Aviation Safety Authority (CASA) Airworthiness Directives, addresses the modification requirements for certain aircraft models to ensure ongoing compliance with safety standards. For instance, Airworthiness Directive AD/DC3/10 concerns the modification of rear luggage compartment tie-down fittings in Douglas DC3 Series Aeroplanes, necessitating the replacement of specific fittings to meet updated safety requirements. This directive is one of the mechanisms through which CASA enforces the continuous improvement of aviation safety, ensuring that all aircraft operate within safe parameters as defined by the regulations.

Scope and Application

The Civil Aviation Regulations 1998, under Part 39 - 105, specifically addresses the airworthiness directives for the Douglas DC3 Series Aeroplanes, with a focus on the modifications required for the rear luggage compartment tie-down fittings. This legislative instrument applies to all models of the Douglas DC3 Series that have been modified in accordance with the DCA 1900 series conversion drawings. The regulation mandates that these aircraft must either replace the rear luggage compartment tie-down fittings as specified in Drawing DCA 2188, Issue 1, with the larger fittings detailed in Issue 3, or comply with the requirements outlined in ANOs Part 100 Appendix “A” Notice 7/10, or ANO 105.1.16.1.5.10. This ensures that the aircraft maintain the necessary safety standards and remain airworthy for operation. The scope of the legislation encompasses the aircraft industry, specifically targeting operators and maintainers of the Douglas DC3 Series aeroplanes within the Commonwealth of Australia, thereby ensuring adherence to stringent safety regulations.

Key Provisions

The Civil Aviation Regulations 1998, particularly Part 39 - 105, contains specific directives for maintaining the airworthiness of certain aircraft models, including the Douglas DC3 series aeroplanes. Specifically, AD/DC3/10 addresses the modification of rear luggage compartment tie-down fittings. According to section 1 of the directive, the rear luggage compartment tie-down fittings must be replaced with a larger type as specified in Drawing DCA 2188, Issue 3, or in accordance with the ANOs Part 100 Appendix "A" Notice 7/10, or ANO 105.1.16.1.5.10. This requirement ensures that the luggage compartment can securely hold cargo, preventing movement that could compromise the aircraft’s stability and safety during flight. The obligations imposed by these regulations are clear and must be adhered to by all parties involved in the modification and maintenance of Douglas DC3 series aeroplanes. Aircraft owners, operators, and maintenance personnel must ensure that the rear luggage compartment tie-down fittings are either replaced with the specified larger type or comply with the referenced ANOs. This includes verifying that the modifications are carried out according to the approved drawings and notices, ensuring that all work is conducted by qualified personnel and that appropriate records are maintained. Failure to comply with the airworthiness directives outlined in AD/DC3/10 can lead to serious consequences. Civil Aviation Safety Authority (CASA) regulations mandate strict adherence to these standards to maintain the safety and airworthiness of the aircraft. Any breach of these provisions can result in severe penalties. Under section 3 of the Civil Aviation Act 1988, non-compliance may lead to enforcement actions, including fines, suspension or revocation of certificates of airworthiness, and potential criminal charges for individuals responsible for the oversight or execution of the modifications. The maximum penalties for such offences can include substantial fines and imprisonment, reflecting the high importance placed on adherence to these safety directives.

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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.