COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Gulfstream (Rockwell) 114 Series Aeroplanes
AD/ROCK-114/2A Aileron Hinge Supports - Inspection 7/78
Applicability: All model 114 aeroplanes with S/Nos. 14000 to 14376. Document: Rockwell International SB No. SB-114-14A.
Compliance: 1. Unless already accomplished as per SB No. 114-14, initially inspect before further flight as per Part 1 of SB No. 114-14A and perform external visual inspection before each subsequent flight until modified.
Note: Pilot in command may perform and certify for visual inspection.
2. Unless already accomplished as per SB No. 114-14 modify as per Part 2 of SB No. 114-14A within 100 hours time in service after 15 August 1978.
Overview
The Civil Aviation Regulations 1998, enacted by the Australian Parliament, aim to ensure the safety of civil aviation through comprehensive regulatory frameworks. One particular legislative instrument, F2006B06648, addresses specific safety concerns associated with the Gulfstream (Rockwell) 114 Series aeroplanes. This directive, AD/ROCK-114/2A, was introduced to tackle the problem of potential failure in the aileron hinge supports of the mentioned aircraft series. The policy objective behind this legislation is to maintain the airworthiness of these aeroplanes by mandating regular inspections and necessary modifications to prevent potential structural failures. The responsibility for ensuring compliance with these safety directives falls under the purview of the Civil Aviation Safety Authority, thereby ensuring adherence to the highest safety standards in the industry.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, governs the airworthiness directives for civil aviation in Australia, and under this, AD/ROCK-114/2A pertains to the inspection of aileron hinge supports for the Gulfstream (Rockwell) 114 Series Aeroplanes. This directive applies to all model 114 aeroplanes with serial numbers ranging from 14000 to 14376, and it mandates compliance with Rockwell International Service Bulletin No. SB-114-14A. The inspection requirement includes an initial inspection before further flight if not already performed as per SB No. 114-14, followed by an external visual inspection before each subsequent flight until modifications are made. The pilot in command is authorised to perform and certify this visual inspection. Furthermore, any modifications to the aileron hinge supports must be completed within 100 hours of time in service after 15 August 1978, unless they have already been performed as per SB No. 114-14. The regulations extend to ensuring that these directives are adhered to by relevant aircraft operators and maintainers within Australia's jurisdiction.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, includes a schedule of airworthiness directives for various aircraft types, such as the Gulfstream (Rockwell) 114 Series Aeroplanes. This directive, AD/ROCK-114/2A, concerns the aileron hinge supports, requiring inspections and modifications for model 114 aeroplanes with serial numbers (S/Nos.) 14000 to 14376. The directive references Rockwell International Service Bulletin No. SB-114-14A, which provides detailed guidance on the required actions.
Under this directive, the primary requirement (Section 1) is to inspect the aileron hinge supports before the initial flight if the modification specified in SB No. 114-14 has not already been performed. This inspection must be conducted in accordance with Part 1 of SB No. 114-14A. Additionally, an external visual inspection must be performed before each subsequent flight until the specified modification is made. Notably, the pilot in command is authorised to perform and certify the visual inspection. The second requirement (Section 2) mandates that the modification outlined in Part 2 of SB No. 114-14A must be completed within 100 hours of time in service after 15 August 1978.
The obligations imposed by this directive are primarily on the operators and owners of the affected aircraft. They must ensure that the inspections and modifications are carried out as per the specified guidelines and timeframes. This includes ensuring that the aircraft is inspected and modified before it is allowed to fly, and that these actions are documented appropriately. The directive ensures that the aircraft maintains its airworthiness by addressing potential issues with the aileron hinge supports.
Failure to comply with the requirements of this airworthiness directive can lead to serious consequences. While specific penalties are not detailed in the directive itself, non-compliance with airworthiness directives generally results in potential enforcement actions by the Civil Aviation Safety Authority (CASA). Such actions can include fines, suspension or revocation of the aircraft's certificate of airworthiness, and possible criminal charges for operators who deliberately or negligently fail to comply with the regulations. The severity of the penalties can depend on the nature and extent of the non-compliance, as well as any resultant safety risks or incidents.