COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Casa 212 Series Aeroplanes
AD/CASA/11 Power Quadrant Cover 1/88
Applicability: Model CASA-212 Series aeroplanes as listed in CASA S.B. No 212-76-05 Revision 1A.
Requirement: Action in accordance with CASA S.B. No 212-76-05 Revision 1A. Compliance: Prior to the issue of the next Maintenance Release after 28 February 1988.
Background: The Spanish D.G.A.C. and the FAA have Airworthiness Directives in place requiring modification of the power control quadrant cover, to prevent jamming of the power controls by objects falling into the open slots.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, were designed to establish comprehensive safety standards for civil aviation within the country, aiming to protect the public and ensure the integrity of the aviation industry. Specifically, Part 39 - 105 of these regulations, which governs the issuance of Airworthiness Directives, addresses safety concerns and mandates corrective actions to prevent hazards that could compromise aircraft safety. One such directive, AD/CASA/11, pertains to the power quadrant cover of CASA-212 Series aeroplanes, responding to issues raised by the Spanish D.G.A.C. and the FAA regarding the potential for objects to cause jamming of the power controls. The policy objective is to mitigate risks associated with such hazards, ensuring that aircraft remain airworthy and compliant with international safety standards.
The Civil Aviation Safety Authority (CASA) issued AD/CASA/11 in response to identified risks of power control jamming in CASA-212 Series aeroplanes, which could arise from objects falling into the open slots of the power quadrant cover. This directive requires modifications to be made in accordance with CASA S.B. No 212-76-05 Revision 1A, with compliance necessary before the issuance of the next Maintenance Release following 28 February 1988. The directive aims to maintain the high safety standards required by civil aviation regulations and aligns with international directives from the Spanish D.G.A.C. and the FAA, emphasising a unified approach to addressing safety concerns in aviation.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, which outlines the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, applies to CASA-212 Series aeroplanes as identified in CASA S.B. No 212-76-05 Revision 1A. This legislative instrument mandates that all aeroplanes of the CASA-212 Series must comply with the requirements set forth in CASA S.B. No 212-76-05 Revision 1A, which pertains to the modification of the power quadrant cover. This directive is intended to prevent the jamming of power controls by objects that might fall into the open slots. Compliance with this Airworthiness Directive must be achieved before the next Maintenance Release following 28 February 1988. This legislation extends across the Commonwealth of Australia, ensuring uniform safety standards in the aviation industry, and does not specify any exclusions or exemptions within its scope. The regulatory framework is further enforced and potentially expanded through subordinate instruments which may provide additional details or amendments.
Key Provisions
The Civil Aviation Regulations 1998, particularly in Part 39 - 105, focus on the safety directives for aircraft, including the CASA 212 Series Aeroplanes. Specifically, AD/CASA/11 pertains to the power quadrant cover, which was issued to address potential safety hazards (Reg 39.105). The regulation requires adherence to CASA S.B. No 212-76-05 Revision 1A, which provides detailed instructions for the modification of the power quadrant cover. This directive is crucial to prevent jamming of the power controls by objects that could fall into the open slots, ensuring the safe operation of the aircraft.
For operators and owners of CASA 212 Series aeroplanes, the Civil Aviation Regulations impose specific obligations. They must ensure that any modifications to the power quadrant cover are completed in accordance with CASA S.B. No 212-76-05 Revision 1A before the issuance of the next Maintenance Release after 28 February 1988 (Reg 39.105). This means that the required actions must be undertaken to comply with the specified safety standards, and any maintenance releases issued after the compliance date must reflect these modifications.
Failure to comply with the requirements of the Civil Aviation Regulations regarding the power quadrant cover can lead to serious consequences. The regulations impose both civil and criminal penalties for non-compliance. Civil penalties can include fines, while criminal penalties may involve imprisonment or fines, depending on the severity of the breach. The maximum penalties are not explicitly stated in the provided text, but they are significant enough to enforce adherence to the safety directives. The Spanish D.G.A.C. and the FAA also have similar directives, indicating the international importance of these safety measures.