COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
DH114 (Heron) Series Aeroplanes
AD/DH114/45 Tailplane Upper Pick-Up Eyebolt NK
in Bulkhead 7 - Inspection
Applicability: All models.
Document: British Aerospace TNS Heron (114) No. F.21. Compliance: Before 31 May 1979.
Overview
The Civil Aviation Regulations 1998, which were enacted by the Parliament of Australia, form a comprehensive set of rules governing all aspects of civil aviation within Australia. One particular legislative instrument within this framework is F2006B08957, which pertains to airworthiness directives for specific aircraft models. This legislation was introduced to address safety concerns and ensure that aircraft operating within Australian airspace meet the required safety standards. The policy objective is to maintain and enhance aviation safety by enforcing regular inspections and compliance with specific airworthiness directives, such as AD/DH114/45, which mandates the inspection of the tailplane upper pick-up eyebolt in the NKin bulkhead 7 of Heron series aeroplanes.
This legislative instrument is part of the broader regulatory efforts overseen by the Civil Aviation Safety Authority (CASA) to ensure that aircraft are maintained in a safe and airworthy condition. By implementing specific airworthiness directives, the legislation aims to proactively address potential safety issues, thereby protecting passengers, crew, and the public from aviation-related risks. The inclusion of detailed directives such as the one for Heron series aeroplanes exemplifies the commitment to maintaining high safety standards within the civil aviation sector.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105 Civil Aviation Safety Authority Schedule of Airworthiness Directives DH114 (Heron) Series Aeroplanes, applies to all models of the DH114 (Heron) series aeroplanes. This legislation mandates compliance with the airworthiness directive AD/DH114/45 concerning the inspection of the tailplane upper pick-up eyebolt NK in Bulkhead 7 for aircraft that were in compliance before 31 May 1979. The directive is applicable to the entire Commonwealth of Australia, encompassing federal jurisdiction over civil aviation. This regulation ensures that the specified aircraft maintain their airworthiness through periodic inspections, thereby enhancing safety standards for these aircraft within the Australian airspace. The application of this regulation extends to any entity or individual operating a DH114 (Heron) series aeroplane within the Commonwealth, with no stated exclusions or exemptions within the provided text. The enforcement of this directive may be further detailed or expanded through subordinate instruments, which may provide additional specifications or procedures for compliance.
Key Provisions
The Civil Aviation Regulations 1998 (Cth) Part 39 - 105, specifically AD/DH114/45, pertains to the inspection of the tailplane upper pick-up eyebolt in the Nkin bulkhead 7 of DH114 (Heron) series aeroplanes (section 39-105). This Airworthiness Directive mandates that all models of DH114 (Heron) aeroplanes undergo a thorough inspection of the specified component before 31 May 1979. The directive aims to ensure that this critical component, which plays a significant role in the structural integrity of the aircraft, is free from any defects or degradation that could compromise safety.
Under this directive, the responsible parties, typically the aircraft operators and maintenance providers, must conduct a detailed inspection of the tailplane upper pick-up eyebolt located in the Nkin bulkhead 7. This inspection is to be performed meticulously to identify any signs of wear, corrosion, or other forms of damage. Should any issues be detected during the inspection, appropriate corrective actions must be taken in accordance with the maintenance manual and any other relevant guidelines to rectify the identified deficiencies. The directive underscores the importance of adhering to the specified timeline, ensuring that all inspections are completed well before the deadline to maintain compliance and uphold the safety standards set by the Civil Aviation Safety Authority.
Failure to comply with the requirements outlined in AD/DH114/45 could result in significant legal and operational repercussions. The Civil Aviation Regulations impose strict obligations on the operators and maintainers of DH114 (Heron) aeroplanes to adhere to these airworthiness directives. Non-compliance may lead to enforcement actions by the Civil Aviation Safety Authority, including the potential grounding of the aircraft until the required inspections are satisfactorily completed. Furthermore, operators found in breach of these regulations could face substantial fines and other penalties, as stipulated by the Civil Aviation Act 1988 (Cth). The seriousness of these consequences highlights the imperative for strict adherence to the mandated inspection procedures and timelines.