COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
DHA-3 (Drover) Series Aeroplanes
AD/DHA-3/1 Electrical Installation - Modification 9/51
Applicability: All models.
Requirement: Modify the electrical installation in accordance with the following:
Circuit | Remove | Install | Fuse Chart Amendment |
Landing Lights | 10 Amp. Type S Fuses | 15 Amp. Type S fuses in circuit and also spares | Delete “10 Amp.” Insert “15 Amp.” |
Generators | 20 Amp. Type S Fuses | Two Type 5AG fuses boxes and Two 25 Amp. Type 5AG fuses. Connect in places of original Type S fuses. Install spare fuses | Delete “Generators 20 Amp.” From original Fuse Box. Identify new fuse box “Generator 25 Amp.” |
or ANO 105.1.14.14.5.1
Compliance: Forthwith.
Overview
The Civil Aviation Regulations 1998, specifically Part 39 - 105, under the Civil Aviation Safety Authority, introduced Airworthiness Directives to address safety concerns within civil aviation. The Act was enacted to ensure that aircraft meet certain safety standards and to prevent accidents by issuing mandatory modifications to existing aircraft. This legislation was designed to fill the gap in safety compliance by providing clear, enforceable directives that mandate specific modifications to aircraft electrical installations, as outlined in the Airworthiness Directives. The policy objective is to maintain and enhance the safety of civil aviation through proactive measures that rectify identified vulnerabilities in aircraft design and operation.
The Civil Aviation Regulations 1998, as amended, is enforced by the Civil Aviation Safety Authority and represents the Commonwealth of Australia's commitment to ensuring the highest safety standards in civil aviation. The specific Airworthiness Directive DHA-3/1, which mandates modifications to the electrical installation of DHA-3 (Drover) Series Aeroplanes, exemplifies the regulatory body's role in addressing safety issues by requiring the substitution of fuses and the installation of new fuse boxes. This directive aims to mitigate risks associated with the original electrical setup by ensuring compliance with updated safety standards.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105 concerning the Civil Aviation Safety Authority's Schedule of Airworthiness Directives, applies to all models of DHA-3 (Drover) Series Aeroplanes. The legislation mandates that modifications to the electrical installation be carried out as per the specified requirements. This includes altering the fuse types and configurations for the landing lights and generators, ensuring compliance with the new standards immediately. The scope of this legislation extends to the entire fleet of DHA-3 (Drover) Series Aeroplanes, necessitating that all aircraft within this category adhere to the outlined modifications. The regulations are applicable across the Commonwealth of Australia, administered by the Civil Aviation Safety Authority (CASA), ensuring uniformity and safety standards in civil aviation. The regulations do not explicitly mention any exclusions or exemptions, implying that all relevant aircraft must comply with the new directives. Subordinate instruments or amendments may further extend or refine the application of these regulations, though the primary directive is clear and must be strictly adhered to by the operators and owners of DHA-3 (Drover) Series Aeroplanes.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105 Civil Aviation Safety Authority Schedule of Airworthiness Directives, contains AD/DHA-3/1, which pertains to the modification of the electrical installation in DHA-3 (Drover) Series Aeroplanes (Section 9/51). This directive applies to all models within this series. The requirement is to modify the electrical installation by making specific changes to the fuse chart. For the landing lights, the directive mandates the replacement of 10 Amp. Type S Fuses with 15 Amp. Type S fuses. This includes not only the fuses in the circuit but also the spares. The text "10 Amp." should be deleted and replaced with "15 Amp." For the generators, the directive specifies replacing 20 Amp. Type S Fuses with two Type 5AG fuse boxes and two 25 Amp. Type 5AG fuses. These new components should replace the original Type S fuses, and the new fuse boxes should be identified as "Generator 25 Amp." Additionally, the text "Generators 20 Amp." should be deleted from the original fuse box.
The Act imposes specific obligations on the parties governed by this directive. Owners or operators of DHA-3 (Drover) Series Aeroplanes must ensure that the modifications to the electrical installation are completed without delay. The compliance requirement, as stated in Section 105.1.14.14.5.1, mandates immediate action to adhere to the specified changes. These changes are intended to enhance the safety and reliability of the aircraft's electrical systems.
Failure to comply with the Airworthiness Directive AD/DHA-3/1 can result in serious consequences. Although the specific civil or criminal penalties are not detailed in the extract, non-compliance with Civil Aviation Regulations can lead to enforcement actions by the Civil Aviation Safety Authority (CASA). This could include fines, suspension, or revocation of airworthiness certificates, and potentially criminal charges for more severe breaches. The exact penalties would depend on the severity of the non-compliance and any subsequent investigations by CASA. The directive's purpose is to ensure that the modifications are carried out to maintain the safety standards required for the operation of DHA-3 (Drover) Series Aeroplanes.