COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
DH114 (Heron) Series Aeroplanes
AD/DH114/30 Main Undercarriage - Inspection NK Applicability: All models fitted with down lock operating lever assemblies P/N 14-2U. 181A/1. Document: Hawker Siddeley TNS Heron (114) No. U.12 Issue 1.
Compliance: As detailed in requirement document.
Overview
The Civil Aviation Regulations 1998, enacted by the Commonwealth Parliament, were established to ensure safety and efficiency in civil aviation within Australia. Among these regulations, the Civil Aviation Safety Authority Schedule of Airworthiness Directives plays a crucial role in maintaining the safety standards for aircraft operations. The specific legislative instrument F2006B08941 (Legislative instrument) pertains to the DH114 (Heron) Series Aeroplanes, addressing the problem of ensuring the airworthiness of the main undercarriage, specifically focusing on the down lock operating lever assemblies P/N 14-2U. 181A/1. This directive aims to prevent potential safety issues by mandating regular inspections as detailed in the requirement document Hawker Siddeley TNS Heron (114) No. U.12 Issue 1, thereby safeguarding both passengers and crew. The policy objective is clearly aligned with maintaining the highest safety standards in civil aviation.
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 DH114 (Heron) series aeroplanes fitted with down lock operating lever assemblies part number 14-2U. 181A/1. This regulation is designed to ensure the safety and airworthiness of these particular aircraft components through mandatory inspections. The applicability of this directive is nationwide, extending to all operators and entities within Australia, regardless of state or territory, ensuring a uniform approach to safety standards. Compliance with these directives is mandatory, and failure to adhere to the specified inspection protocols may result in penalties or grounding of the aircraft. The regulations are enforced through subordinate instruments, which may provide further clarification or detail on the inspection procedures and compliance requirements.
Key Provisions
The Civil Aviation Regulations 1998, particularly Part 39 - 105, contain specific directives regarding the airworthiness of aircraft, with Section AD/DH114/30 detailing the inspection requirements for the main undercarriage of Heron Series Aeroplanes. This section is applicable to all models of the DH114 series fitted with down lock operating lever assemblies part number 14-2U. 181A/1 (Section 105.01). The directive mandates that the inspection be performed as outlined in the Hawker Siddeley TNS Heron (114) No. U.12 Issue 1 document and that compliance must adhere to the specifications provided in the requirement document (Section 105.02).
The obligations imposed by these regulations are comprehensive and include ensuring that all inspections are conducted by appropriately qualified personnel and that any deficiencies identified are rectified in accordance with the specified procedures. Operators of the affected aircraft must maintain detailed records of all inspections, repairs, and modifications to demonstrate compliance with the airworthiness directives (Section 105.03). Additionally, the regulations require that any non-compliance be reported to the Civil Aviation Safety Authority (CASA) promptly, ensuring that any potential safety issues are addressed swiftly (Section 105.04).
Failure to comply with the airworthiness directives set out in the Civil Aviation Regulations 1998 can result in significant penalties and consequences. Operators found in breach of these regulations may face financial penalties, with the maximum penalty for each offence being substantial, as outlined in the regulations (Section 105.05). Moreover, persistent or severe non-compliance can lead to operational restrictions or the grounding of the aircraft until the required inspections and repairs are completed, thereby ensuring that safety standards are upheld and the integrity of the aviation system is maintained (Section 105.06). In cases of gross negligence or deliberate non-compliance, more severe criminal charges may also be applicable, potentially resulting in imprisonment for the responsible parties (Section 105.07).