COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 90 and 65-90 (King Air) Series Aeroplanes
AD/BEECH 90/67
Amdt 1
Fuel Filler Anti-Siphon Assemblies - Inspection
4/83
Applicability: All model F90 with S/Nos. LA-2 to LA-62. Document: Beechcraft SI No. 1201, Rev. 1.
Compliance: Unless already accomplished, within 100 hours’ time in service after 31 July 1983.
Background: This Directive has been amended to reflect the revision status of Beechcraft SI No. 1201. The Service Instruction has been revised to correct errors, and to introduce a modification kit.
Inspection is required to ensure that the correct anti-siphon assembly is fitted to the auxiliary fuel filler ports.
Overview
The Civil Aviation Regulations 1998, specifically Part 39 - 105, was enacted by the Parliament of the Commonwealth of Australia to regulate and ensure the safety and efficiency of civil aviation within the country. This legislation aims to address various safety concerns and gaps in the aviation industry by setting forth comprehensive regulations governing the operation and maintenance of aircraft. The regulations are administered by the Civil Aviation Safety Authority (CASA), with a policy objective to maintain and enhance the safety of civil aviation. One such regulation is the Airworthiness Directive (AD) concerning Beechcraft 90 and 65-90 (King Air) Series Aeroplanes, which includes AD/BEECH 90/67 Amendment 1 regarding fuel filler anti-siphon assemblies. This directive mandates inspections to ensure the correct anti-siphon assembly is fitted to the auxiliary fuel filler ports, reflecting CASA's commitment to maintaining stringent safety standards within the aviation sector.
Scope and Application
The Civil Aviation Safety Authority Schedule of Airworthiness Directives, as specified in the Civil Aviation Regulations 1998, applies to all model F90 Beechcraft 90 and 65-90 (King Air) series aeroplanes with serial numbers LA-2 to LA-62. This legislation mandates the inspection of fuel filler anti-siphon assemblies to ensure compliance with the directives issued by the Civil Aviation Safety Authority. The inspection is required to be completed within 100 hours’ time in service after 31 July 1983, ensuring adherence to the updated specifications as outlined in Beechcraft Service Instruction No. 1201, Revision 1. This revision was made to correct previous errors and introduce a modification kit to address safety concerns. The scope of this directive is specific to the mentioned aircraft models, and it applies across the Commonwealth of Australia, overseen by the Civil Aviation Safety Authority. There are no stated exclusions or exemptions within the scope of this directive.
Key Provisions
The primary operative section of the Civil Aviation Regulations 1998, specifically Part 39 - 105, pertains to the Schedule of Airworthiness Directives for Beechcraft 90 and 65-90 (King Air) Series Aeroplanes (section 39-105). This section mandates that all model F90 aircraft with serial numbers LA-2 to LA-62 must undergo an inspection of their fuel filler anti-siphon assemblies. This requirement is outlined in AD/BEECH 90/67 Amendment 1, which was issued on 4 August 1983. The directive mandates that the inspection must be completed within 100 hours of the aircraft's time in service following 31 July 1983, unless the inspection has already been performed.
The obligations and requirements imposed by this Act are primarily centred around ensuring the airworthiness of the specified aircraft models. Owners or operators of Beechcraft 90 and 65-90 (King Air) Series Aeroplanes must comply with the inspection requirements stipulated in the AD/BEECH 90/67 Amendment 1. This involves verifying that the correct anti-siphon assembly is correctly fitted to the auxiliary fuel filler ports. This compliance ensures that there are no risks associated with fuel siphoning, which could compromise the safety of the aircraft. Additionally, the directive references Beechcraft Service Instruction No. 1201, Revision 1, which details the specific procedures and modifications required for this inspection.
Failure to comply with the requirements of this directive could result in significant consequences. If an aircraft owner or operator does not adhere to the inspection and modification requirements, they could be in breach of the Civil Aviation Regulations 1998. Such a breach could lead to enforcement actions being taken by the Civil Aviation Safety Authority (CASA). The potential penalties for non-compliance may include fines or other regulatory actions deemed appropriate by CASA. The specific penalties are not detailed within the legislative instrument but could be substantial, reflecting the critical nature of ensuring the airworthiness of these aircraft models.