COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Partenavia P68 Series Aeroplanes
AD/P68/34 Engine Mount 5/91 DM
Applicability: All P68C-TC up to serial number XXX-46TC.
All P68 OBS-TC up to serial number XXX-030 BTC.
Requirement: Action in accordance with the Technical Requirements of R.A.I. AD 91-83.
Note: Partenavia SB 82 refers.
Compliance: Within 25 hours time in service after 27 March 1991 or prior to 30 April 1991; whichever occurs first.
Background: Reports of cracks in the engine mount structure have been received. This Directive requires a detail inspection in the area of the lower attachment.
Overview
The Civil Aviation Regulations 1998, specifically under Part 39, addresses various directives to ensure the safety of civil aviation operations. Among these, Partenavia P68 Series Aeroplanes AD/P68/34 pertains to the engine mount, enacted to address reports of cracks in the engine mount structure. This directive applies to all P68C-TC up to serial number XXX-46TC and all P68 OBS-TC up to serial number XXX-030 BTC. It requires actions in accordance with the Technical Requirements of R.A.I. AD 91-83, with reference to Partenavia SB 82, to ensure compliance within a specified timeframe. This regulation was introduced by the Civil Aviation Safety Authority to mitigate safety risks associated with engine mount failures.
The Civil Aviation Regulations 1998 were enacted by the Parliament of the Commonwealth of Australia to establish comprehensive safety standards for civil aviation. The policy objective of these regulations is to ensure the safety and reliability of aircraft operations, and Part 39, which includes AD/P68/34, specifically targets identified safety issues within particular aircraft models. By mandating detailed inspections and timely corrective actions, the regulations aim to prevent potential hazards and maintain the highest safety standards in the aviation sector.
Scope and Application
The Civil Aviation Regulations 1998, under Part 39 - 105, pertains to airworthiness directives issued by the Civil Aviation Safety Authority and applies to specific aircraft models, including all Partenavia P68C-TC up to serial number XXX-46TC and all P68 OBS-TC up to serial number XXX-030 BTC. This particular airworthiness directive, AD/P68/34, mandates action in accordance with the technical requirements specified in R.A.I. AD 91-83, with reference to Partenavia Service Bulletin 82. The directive was prompted by reports of cracks in the engine mount structure, necessitating a detailed inspection of the lower attachment area. Compliance with this directive must be achieved within 25 hours of time in service after 27 March 1991, or prior to 30 April 1991, whichever is earlier. The directive applies nationally and is enforced to ensure the safety and airworthiness of the specified aircraft models.
Key Provisions
The Civil Aviation Safety Authority (CASA) has issued an Airworthiness Directive (AD) AD/P68/34, specifically addressing the Partenavia P68 Series Aeroplanes. This directive applies to all P68C-TC models up to serial number XXX-46TC and all P68 OBS-TC models up to serial number XXX-030 BTC. The directive requires actions to be taken in accordance with the Technical Requirements outlined in R.A.I. AD 91-83, referencing Partenavia Service Bulletin 82 for additional guidance. The directive mandates a detailed inspection of the lower attachment area of the engine mount to address reports of cracks in the engine mount structure.
Compliance with AD/P68/34 is mandatory for the specified aircraft models, and it must be completed within 25 hours of time in service after 27 March 1991 or before 30 April 1991, whichever comes first. This requirement is designed to ensure that any identified issues are promptly addressed, thereby maintaining the airworthiness of the aircraft and enhancing safety. Operators and owners of the affected aircraft must ensure that the necessary inspections and actions are carried out in strict adherence to the directive’s specifications.
Operators and owners of the Partenavia P68 Series Aeroplanes covered by this directive are required to comply with the inspection and repair procedures as outlined. This involves conducting a thorough examination of the engine mount's lower attachment area to identify any signs of cracks or structural weaknesses. Any deficiencies found must be rectified in accordance with the prescribed technical requirements. CASA mandates that the inspection must be completed within the specified timeframe to ensure that the safety standards are upheld. Failure to comply with this directive could result in the aircraft being deemed unairworthy.
The Civil Aviation Regulations 1998 impose significant obligations on aircraft operators and owners to adhere to all ADs issued by CASA. Non-compliance with AD/P68/34 could lead to serious consequences, including potential grounding of the aircraft and enforcement actions by CASA. In cases of significant non-compliance, individuals or entities may face legal penalties, including fines and potential imprisonment. The exact penalties can vary, but they are determined by the severity of the breach and are subject to the provisions of the Civil Aviation Act 1988 and other relevant legislation.