COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Percival Vega Gull Series Aeroplanes
AD/GULL/1
Amdt 1
Wing Rib to Aileron Spar Joint - Inspection 11/67
Applicability: All models not modified in accordance with Percival Mod. No. 130. Requirement: 1. Inspect the points of attachment of the outer wing ribs to the aileron false spar.
2. If the area shows signs of faulty gluing or failure of joints, strengthen the rib to spar attachment in accordance with Percival Modification No. 130, or
3. ANO 105.1.26.0.2.1.
Compliance: At intervals not exceeding 12 months or 100 hours time in service whichever occurs first.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, were established to ensure safety and operational standards within the civil aviation industry. These regulations, managed by the Civil Aviation Safety Authority, are designed to mitigate risks and protect the public from potential hazards associated with aviation activities. One particular legislative instrument, F2006B10328, pertains to airworthiness directives for the Percival Vega Gull Series aeroplanes, specifically addressing the inspection and maintenance of the wing rib to aileron spar joint. This directive was introduced to address the identified problem of potential faulty gluing or joint failure in the specified area, which could compromise the structural integrity of the aircraft. The policy objective is to mandate regular inspections and corrective actions to ensure ongoing airworthiness and safety compliance, with inspections required at intervals not exceeding 12 months or 100 hours of time in service, whichever comes first.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, applies to all Percival Vega Gull series aeroplanes that have not been modified in accordance with Percival Modification No. 130. This regulation mandates that these aircraft undergo inspections of the points of attachment of the outer wing ribs to the aileron false spar. If any signs of faulty gluing or failure of the joints are detected, the rib to spar attachment must be strengthened as per Percival Modification No. 130 or according to ANO 105.1.26.0.2.1. Compliance with these directives is essential, with inspections required at intervals not exceeding 12 months or 100 hours of time in service, whichever comes first. This regulation falls under the jurisdiction of the Commonwealth of Australia and is administered by the Civil Aviation Safety Authority (CASA). There are no specific exclusions or exemptions stated in this directive, and its application may be extended or restricted through subordinate instruments as determined by CASA.
Key Provisions
The Civil Aviation Regulations 1998, specifically within Part 39, Section 105, addresses airworthiness directives related to various aircraft models, including the Percival Vega Gull Series Aeroplanes. The regulation in focus is AD/GULL/1 Amendment 1, which pertains to the inspection and potential modification of the wing rib to aileron spar joint. According to the directive (AD/GULL/1), all Percival Vega Gull Series aeroplanes that have not been modified in line with Percival Modification No. 130 must undergo an inspection of the points of attachment of the outer wing ribs to the aileron false spar. This inspection is crucial to detect any signs of faulty gluing or failure of the joints (Section 11/67). If any such issues are found, the regulation mandates that the rib to spar attachment be strengthened in accordance with Percival Modification No. 130, or as per ANO 105.1.26.0.2.1.
The obligations under this regulation require aircraft operators to ensure that the specified inspections and any necessary modifications are performed meticulously. This includes maintaining records of the inspections and modifications carried out to comply with the directive. The compliance requirements are stringent, necessitating inspections at intervals not exceeding 12 months or 100 hours of time in service, whichever comes first (Section 11/67). Failure to adhere to these inspection and modification requirements can lead to serious safety issues, potentially compromising the structural integrity of the aircraft.
Violating the provisions of this airworthiness directive can result in significant consequences. The regulations stipulate that non-compliance with the inspection and modification requirements can lead to enforcement actions under civil aviation law. Potential penalties may include fines and the grounding of the aircraft until the necessary modifications are completed and approved. In severe cases, the non-compliance could result in more severe penalties, including potential criminal charges for those responsible for the oversight, leading to imprisonment. The exact penalties are not explicitly stated in the regulation but align with the broader framework of the Civil Aviation Regulations 1998, which can impose substantial financial and criminal penalties for breaches of safety directives.