COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Partenavia P68 Series Aeroplanes
AD/P68/26 Stabilator Travel Stop - Modification 12/84
Applicability: All model P68 series with S/Nos referred to in requirement document. Requirement: Partenavia P68 S.B. No. 63 Rev. 1.
Note: RAI AD 84-129/P68-31 Refers.
Compliance: Within 100 hours time in service after 31 December 1984 or at the next scheduled inspection for Maintenance Release issue after 31 December 1984 whichever is the later.
Background: The manufacturer has received reports of bending of the stabilator travel stop screws.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, aim to ensure the safety and efficiency of civil aviation within Australia. This legislation addresses gaps and problems in civil aviation practices through various regulatory measures. One specific instrument within these regulations, AD/P68/26, pertains to the Partenavia P68 Series Aeroplanes, specifically addressing the stabilator travel stop modification. This directive was introduced to address a reported issue of bending in the stabilator travel stop screws of certain Partenavia P68 series aircraft. Compliance with this directive is mandatory and requires that the specified modification be completed within 100 hours of time in service after 31 December 1984 or at the next scheduled inspection for maintenance release, whichever is later. The objective is to ensure the continued airworthiness and safety of the affected aircraft.
The Civil Aviation Regulations 1998 are overseen by the Civil Aviation Safety Authority (CASA), which is responsible for enforcing compliance with these regulations. The policy objective behind AD/P68/26 is to mitigate safety risks associated with the identified issue by mandating a specific modification to the stabilator travel stop screws. By addressing this problem proactively, CASA aims to enhance the overall safety and reliability of civil aviation operations within Australia. The directive is a clear demonstration of the regulatory framework's commitment to addressing potential safety hazards through timely and specific interventions.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105 concerning the Civil Aviation Safety Authority’s schedule of airworthiness directives, applies to all model Partenavia P68 series aeroplanes with serial numbers as detailed in the requirement document. This regulation mandates a modification to the stabilator travel stop as outlined in Partenavia P68 Service Bulletin No. 63 Rev. 1. This directive is integral to ensuring the safety and airworthiness of the specified aircraft, addressing specific reports of bending of the stabilator travel stop screws. The requirement necessitates compliance within 100 hours of time in service after 31 December 1984 or at the next scheduled inspection for maintenance release issue after the same date, whichever is later. This regulation is applicable across the Commonwealth of Australia, overseen by the Civil Aviation Safety Authority, and does not specify any exclusions or exemptions in the provided text. The scope of the directive can be further extended or detailed through subordinate instruments, ensuring comprehensive application and enforcement of the safety measures.
Key Provisions
The main operative sections of the Civil Aviation Regulations 1998, specifically Part 39 - 105, mandate the modification of stabilator travel stops for certain Partenavia P68 series aeroplanes. Section (AD/P68/26) requires compliance with Partenavia P68 S.B. No. 63 Rev. 1, which is aimed at addressing reports of bending of the stabilator travel stop screws. This modification must be carried out within 100 hours of time in service after 31 December 1984, or at the next scheduled inspection for Maintenance Release issue after that date, whichever comes later. The directive is applicable to all model P68 series with specific serial numbers detailed in the requirement document.
The Civil Aviation Regulations impose specific obligations on the parties or entities governed by this legislation. Operators of the affected Partenavia P68 series aeroplanes must ensure that the stabilator travel stop modification is performed in accordance with the manufacturer's Service Bulletin No. 63 Rev. 1. This includes conducting the modification within the stipulated timeframe and ensuring that it is recorded appropriately in the aircraft's maintenance records. Failure to comply with these obligations could lead to significant safety risks and potential non-compliance with aviation safety standards.
Breach of the requirements stipulated in the Civil Aviation Regulations can lead to serious consequences. Specifically, failure to implement the stabilator travel stop modification within the prescribed timeframe may result in the aircraft being deemed unairworthy. The Civil Aviation Safety Authority (CASA) has the authority to take enforcement actions against operators who fail to comply with these safety directives. The specific penalties for non-compliance can include fines and potential grounding of the aircraft until the required modifications are completed. In severe cases, operators may face more stringent penalties as determined by CASA.