COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Gulfstream (Grumman American/ American Aviation) AA-5 Series Aeroplanes
AD/AA-5/13 Upper Cowl Centre Hinge - Inspection NK
and Replacement
Applicability: All models: AA5 with S/Nos. AA5-0641 to AA5-0834; AA5A with S/Nos. AA5A- 0001 to AA5A-0050, AA5A-0054 to AA5A-0056; AA5B with S/Nos. AA5B-0001 to AA5B-0169, AA5B-0171 and AA5B-0180 to AA5B-0183.
Document: 1. Grumman American SB No. 152; OR 2. FAA AD 76-01-02.
Compliance: Inspect within 100 hours’ time in service after 16 April 1976 and thereafter at intervals not exceeding 100 hours’ time in service until replaced.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, represent a comprehensive set of rules governing aviation safety across the nation. One particular legislative instrument, F2006B02045, pertains to specific airworthiness directives aimed at maintaining the safety standards of civil aviation. This directive, AD/AA-5/13, addresses issues concerning the upper cowl centre hinge of Gulfstream (Grumman American/ American Aviation) AA-5 Series aeroplanes. It was introduced to address identified safety concerns associated with the specified models of these aeroplanes. The policy objective of this directive is to ensure the regular inspection and, if necessary, the replacement of the upper cowl centre hinge to maintain the airworthiness of these aircraft, thereby protecting passengers, crew, and the general public. The compliance requirement mandates inspection within 100 hours’ time in service after a specified date and at intervals not exceeding 100 hours thereafter until replacement, as outlined in the relevant service bulletins or federal aviation administration airworthiness directives.
Scope and Application
The Civil Aviation Regulations 1998, under Part 39 - 105, encompasses the scope and application of the Airworthiness Directives (AD) for specific aircraft models, including the Gulfstream (Grumman American/ American Aviation) AA-5 series aeroplanes. This regulation applies to all Gulfstream AA-5 series aeroplanes with specific serial numbers, such as AA5, AA5A, and AA5B. The directive mandates the inspection and, if necessary, the replacement of the upper cowl centre hinge to ensure compliance with safety standards. The directive is applicable to these specific aircraft models within the Commonwealth of Australia and is enforced by the Civil Aviation Safety Authority (CASA). The directive requires compliance within 100 hours’ time in service after a specified date and thereafter at intervals not exceeding 100 hours’ time in service until the component is replaced. The directive references specific documents, including Grumman American SB No. 152 or FAA AD 76-01-02, for further detail and compliance procedures.
Key Provisions
The Civil Aviation Regulations 1998, specifically in Part 39 under the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, outlines key provisions for the maintenance and safety of certain Gulfstream (Grumman American/American Aviation) AA-5 Series Aeroplanes, particularly focusing on the upper cowl centre hinge. Section AD/AA-5/13 addresses the requirement for inspecting and potentially replacing the upper cowl centre hinge on specified models (s. 1). This directive applies to AA-5 models with serial numbers ranging from AA5-0641 to AA5-0834; AA-5A models with serial numbers AA5A-0001 to AA5A-0050, AA5A-0054 to AA5A-0056; and AA-5B models with serial numbers AA5B-0001 to AA5B-0169, AA5B-0171, and AA5B-0180 to AA5B-0183 (s. 1). The compliance requirements are clearly stated, demanding inspection within 100 hours of time in service after 16 April 1976 and subsequently at intervals not exceeding 100 hours of time in service until the component is replaced (s. 1).
Operators and owners of the specified aircraft must adhere to the compliance directives set forth in this regulation. They are required to ensure that the upper cowl centre hinge is inspected as per the specified timeframes using the Grumman American Service Bulletin No. 152 or the Federal Aviation Administration Advisory Directive 76-01-02 (s. 1). The inspection and any necessary replacement must be carried out by appropriately certified personnel to maintain airworthiness and safety standards. Additionally, detailed records of all inspections and any replacements must be maintained for regulatory oversight and future reference.
Failure to comply with the inspection and replacement requirements outlined in the Civil Aviation Regulations can lead to significant consequences. Non-compliance may result in the aircraft being deemed unairworthy, potentially leading to grounding until the necessary actions are taken. This could result in severe operational disruptions and financial penalties. While the specific penalties are not detailed within this section, general aviation regulations often include fines and potential criminal charges for individuals responsible for non-compliance, in addition to civil liabilities for any accidents or incidents resulting from failure to adhere to the mandated safety directives.