COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 90 and 65-90 (King Air) Series Aeroplanes
AD/BEECH 90/27 Control Wheel Adapter - Inspection 6/72
Applicability: All models.
Document: Beechcraft SI No. 0497-155.
Compliance: Within 25 hours’ time in service after 10 May 1972 and thereafter at intervals not exceeding 500 hours’ time in service until adapter P/No. 99-524036-33 is installed.
Overview
The Civil Aviation Regulations 1998, which were enacted by the Commonwealth of Australia, contain detailed provisions for ensuring the safety of civil aviation operations within Australian airspace. One particular piece of legislation within this framework is the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, specifically addressing the Beechcraft 90 and 65-90 (King Air) Series Aeroplanes. This directive, identified as AD/BEECH 90/27, was introduced to address potential safety issues related to the control wheel adapter of these aircraft models. The policy objective behind this legislation is to ensure that all applicable aircraft are maintained to a standard that safeguards against risks associated with the control wheel adapter, thereby enhancing overall aviation safety. Compliance with this directive is mandatory for all models, requiring inspections within specific time intervals post-manufacture and after certain service hours.
The enactment of these regulations by the Commonwealth of Australia, through CASA, underscores the commitment to maintaining stringent safety standards in civil aviation, aiming to prevent accidents and ensure the reliability and safety of aircraft operations.
Scope and Application
The Civil Aviation Regulations 1998, under the scope of Part 39 - 105, specifically addresses airworthiness directives pertaining to civil aircraft. One such directive is AD/BEECH 90/27, which mandates inspections on the control wheel adapter of Beechcraft 90 and 65-90 (King Air) series aeroplanes. This directive applies universally to all models of the specified aircraft, ensuring the ongoing safety and compliance of the aircraft within the Australian aviation industry. The regulation demands compliance within 25 hours of time in service following the directive’s issuance date of 10 May 1972, and subsequently mandates inspections at intervals not exceeding 500 hours of time in service, until the installation of adapter P/No. 99-524036-33. The directive is applicable across the Commonwealth of Australia, overseen by the Civil Aviation Safety Authority, ensuring adherence to the safety standards set forth by the regulatory body.
Key Provisions
The main operative sections of this Civil Aviation Regulation concern the inspection of the control wheel adapter on Beechcraft 90 and 65-90 (King Air) Series Aeroplanes. Section 39-105 of the Civil Aviation Regulations 1998 mandates that all models of these aircraft must adhere to the inspection requirements outlined in AD/BEECH 90/27. Specifically, this directive applies to the control wheel adapter and necessitates an inspection within 25 hours of time in service after 10 May 1972. Thereafter, the inspection must occur at intervals not exceeding 500 hours’ time in service until the installation of adapter P/No. 99-524036-33. This regulation is documented in Beechcraft SI No. 0497-155, which serves as the reference for compliance.
The obligations imposed by this regulation require aircraft operators and maintenance personnel to conduct regular inspections of the control wheel adapter as specified. The primary responsibility lies with the operator to ensure that these inspections are performed within the prescribed timeframes. This involves adhering to the detailed procedures outlined in the referenced document, Beechcraft SI No. 0497-155, to ensure that the adapter is examined for any signs of wear, damage, or malfunction. Failure to comply with these inspection intervals could compromise the safety and airworthiness of the aircraft.
Failure to comply with the requirements set forth in AD/BEECH 90/27 may result in civil or criminal consequences. The Civil Aviation Safety Authority (CASA) has the authority to enforce these regulations and may take action against non-compliant operators. Potential penalties for non-compliance include fines, suspension or revocation of aircraft certificates, and other administrative actions deemed necessary to ensure compliance. The specific penalties are determined by CASA based on the severity and frequency of the non-compliance. Additionally, any accidents or incidents resulting from failure to adhere to these inspection requirements could lead to further legal repercussions and liabilities for the operators involved.