COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
McDonnell Douglas (Hughes) and Kawasaki 369 Series Helicopters
AD/HU 369/14 Aft Fuselage Skin - Inspection 4/75
Applicability: All models: 369HE with S/Nos. 0101E to 0215E, 369HS with S/Nos. 0001S to 0661S, 369HM with S/Nos. 0001 to 0004, and 005M to 260M.
Document: Hughes SIN No. HN-82.
Compliance: Within 100 hours time in service after 30 April 1975 and thereafter at intervals not exceeding 100 hours time in service.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, are designed to ensure the safety and efficiency of civil aviation within the country. A specific aspect of these regulations, detailed in Part 39 - 105, pertains to the Civil Aviation Safety Authority’s Schedule of Airworthiness Directives. This legislative framework aims to establish and enforce mandatory safety standards and procedures for aircraft operation. One such directive, AD/HU 369/14, focuses on the inspection of the aft fuselage skin of certain McDonnell Douglas (Hughes) and Kawasaki 369 Series Helicopters to ensure their continued airworthiness. The policy objective of these regulations is to mitigate risks and ensure the safety of all persons on board and on the ground by mandating regular inspections and maintenance procedures for specific aircraft models.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105 Civil Aviation Safety Authority Schedule of Airworthiness Directives, governs the safety and operational standards for aircraft operating within Australia. One such directive, AD/HU 369/14, pertains to the McDonnell Douglas (Hughes) and Kawasaki 369 Series Helicopters, targeting particular models identified by their serial numbers. The directive mandates the inspection of the aft fuselage skin for these specified helicopter models. The directive applies to all models of the 369 Series including 369HE with serial numbers ranging from 0101E to 0215E, 369HS with serial numbers from 0001S to 0661S, 369HM with serial numbers from 0001 to 0004 and 005M to 260M. The inspection must be carried out within 100 hours of time in service after 30 April 1975, and then at intervals not exceeding 100 hours of time in service. The regulation ensures that these helicopters maintain their airworthiness and safety standards, overseen by the Civil Aviation Safety Authority. The application of this directive is comprehensive within its defined parameters, ensuring that the specified helicopters adhere to the safety mandates stipulated by Australian aviation authorities.
Key Provisions
The key provisions of the AD/HU 369/14 Airworthiness Directive mandate specific requirements for the inspection of the aft fuselage skin of certain McDonnell Douglas (Hughes) and Kawasaki 369 Series Helicopters. Under section 39-105, it is stipulated that all models of the 369HE with serial numbers ranging from 0101E to 0215E, the 369HS with serial numbers from 0001S to 0661S, the 369HM with serial numbers from 0001 to 0004, and from 005M to 260M, must adhere to the outlined inspection procedures. The Hughes SIN No. HN-82 document serves as the reference point for compliance, which must be achieved within 100 hours of time in service following the directive's issuance on 30 April 1975, and subsequently at intervals not exceeding 100 hours of time in service.
Operators and owners of the specified helicopter models must ensure that the inspections are performed in accordance with the procedures set out in the Hughes SIN No. HN-82. This includes thorough examination and documentation of the aft fuselage skin condition to verify that there are no structural deficiencies or damage that could compromise the safety of the aircraft. The compliance requirements necessitate that operators maintain detailed records of each inspection, including the date, findings, and any remedial actions taken. These records must be readily available for review by the Civil Aviation Safety Authority (CASA) upon request.
Failure to comply with the AD/HU 369/14 Airworthiness Directive may result in serious consequences. The regulations under section 39-105 impose strict obligations on the parties involved, and non-compliance can lead to enforcement actions. The potential civil and criminal penalties for breaching these regulations include fines and, in severe cases, prosecution. The maximum penalties are determined based on the severity and frequency of the breach, with potential sanctions including substantial financial penalties and, for individuals, imprisonment terms. Ensuring adherence to these directives is critical for maintaining the safety standards set by the Civil Aviation Safety Authority.