COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Casa 212 Series Aeroplanes
AD/CASA/15 Flight Idle Stops 9/92 TX
Applicability: All model C-212- series aircraft.
Requirement: Action in accordance with the technical requirements of FAA Telegraphic AD T92-13-51.
Note: CASA SB 212-76-07 provides service data on the backup blocking system.
Compliance: Within 48 hours from 24 June 1992. Thereafter reinspect at intervals not exceeding 300 hours time in service.
Background: During investigation of a fatal accident a backup power lever flight idle stop was found to be inoperative. This directive introduces a functional test of the system.
Overview
The Civil Aviation Regulations 1998, specifically under Part 39 - 105, establish the Civil Aviation Safety Authority's (CASA) schedule of Airworthiness Directives (AD) designed to maintain the highest standards of airworthiness for all aircraft operating in Australia. This particular legislation, AD/CASA/15, pertains to the CASA 212 series aeroplanes, aiming to address a safety concern identified through the investigation of a fatal accident. The directive mandates that all model C-212 series aircraft must comply with the technical requirements of the Federal Aviation Administration's (FAA) Telegraphic AD T92-13-51, which involves a functional test of the backup power lever flight idle stop system. The urgency of this directive is underscored by the requirement for compliance within 48 hours from 24 June 1992, followed by reinspection at intervals not exceeding 300 hours time in service. This measure was introduced to ensure that such safety issues are promptly and effectively managed, thereby enhancing the overall safety of civil aviation in Australia.
Scope and Application
The Civil Aviation Safety Authority (CASA) Regulations 1998, specifically Part 39 - 105, addresses the airworthiness directives concerning CASA 212 series aeroplanes, establishing regulations that apply to all model C-212-series aircraft. This legislation mandates compliance with the technical requirements outlined in FAA Telegraphic AD T92-13-51, requiring corrective action to be taken within 48 hours from 24 June 1992, and subsequent reinspection at intervals not exceeding 300 hours in service. The directive stems from an investigation into a fatal accident where a backup power lever flight idle stop was found to be inoperative, necessitating a functional test of the system. Additionally, CASA SB 212-76-07 offers pertinent service data on the backup blocking system to aid in compliance. The scope of this regulation is comprehensive, applying to all relevant aircraft, and is enforced under the jurisdiction of the Commonwealth of Australia. There are no specific exclusions or exemptions mentioned in the directive, thereby encompassing all applicable aircraft within its purview.
Key Provisions
The Civil Aviation Regulations 1998, under Part 39, Section 105, specifically address the airworthiness of CASA 212 Series Aeroplanes through the Airworthiness Directive (AD) CASA/15 (AD/CASA/15). This directive applies to all model C-212-series aircraft and mandates actions in line with the technical requirements outlined in FAA Telegraphic AD T92-13-51. To ensure compliance, the directive requires an initial action within 48 hours from 24 June 1992, followed by reinspection at intervals not exceeding 300 hours of time in service. This directive was prompted by the discovery of an inoperative backup power lever flight idle stop during an investigation into a fatal accident, thereby necessitating a functional test of the system.
The obligations imposed by AD/CASA/15 are straightforward yet critical for maintaining the safety standards of CASA 212 Series Aeroplanes. Operators must ensure that the technical requirements set out in FAA Telegraphic AD T92-13-51 are met without delay. Specifically, they must complete the initial compliance action within 48 hours from the specified date and schedule subsequent reinspections to be conducted at intervals of no more than 300 hours of flight time. Additionally, CASA Service Bulletin 212-76-07 provides supplementary service data on the backup blocking system, which operators should consult to aid in compliance and maintenance procedures.
Failure to comply with the requirements of AD/CASA/15 can result in serious consequences. The regulations do not explicitly detail specific penalties in the text provided; however, general provisions within the Civil Aviation Act 1988 and Civil Aviation Regulations 1988 outline penalties for non-compliance with airworthiness directives. Such breaches can result in enforcement actions, including fines and potential grounding of the aircraft, which could affect the operator's licence. The severity of penalties depends on the extent of non-compliance and its impact on flight safety. It is essential for operators to adhere strictly to these requirements to avoid legal repercussions and ensure the continued airworthiness of their aircraft.