COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 50 (Twin Bonanza) Series Aeroplanes
AD/BEECH 50/32 Emergency Exits - Placards and Markings 1/84
Applicability: All models with S/Nos referenced in Beechcraft service instruction No. 1241. Requirement: Action in accordance with Beechcraft S.I. No. 1241.
Compliance: Within 100 hours’ time in service after 31 January 1984 or at the next scheduled inspection for Maintenance Release issue after 31 January 1984, whichever is the later.
Background: To standardise emergency exit placards and modify the openable window latch.
Overview
The Civil Aviation Regulations 1998, specifically Part 39 - 105, address the need for consistent safety standards across the aviation industry. The regulation in question, AD/BEECH 50/32, pertains to the Beechcraft 50 (Twin Bonanza) series aeroplanes and was introduced to address the problem of non-standardised emergency exit placards and inadequate openable window latch modifications. Enacted by the Australian Government under the authority of the Civil Aviation Act 1988, this directive is intended to ensure compliance with safety directives issued by the Civil Aviation Safety Authority, thereby protecting the safety of passengers and crew. The regulation mandates adherence to Beechcraft service instruction No. 1241, requiring compliance within 100 hours of time in service after 31 January 1984, or at the next scheduled inspection, whichever is later, reflecting a policy objective to standardise safety measures and mitigate potential risks associated with emergency exits.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, applies to all Beechcraft 50 (Twin Bonanza) series aeroplanes with serial numbers referenced in Beechcraft Service Instruction No. 1241. This legislation mandates that emergency exits on these aircraft must comply with the requirements outlined in Beechcraft Service Instruction No. 1241, which includes the standardisation of emergency exit placards and modifications to the openable window latch. Compliance with these directives is mandatory and must be achieved within 100 hours of the aircraft's time in service after 31 January 1984, or at the next scheduled inspection for Maintenance Release issue after that date, whichever is later. This regulation applies across the Commonwealth of Australia and is enforced by the Civil Aviation Safety Authority, ensuring the safety and uniformity of emergency procedures in civil aviation.
The regulation extends to the entire nation, encompassing all states and territories within the Commonwealth, and is applicable to any entity operating Beechcraft 50 series aeroplanes within this jurisdiction. There are no specific exclusions or exemptions mentioned in the text, meaning that all aircraft meeting the specified serial numbers must comply with the directives. The application of this regulation is not limited to any particular industry or transaction but focuses solely on the maintenance and safety standards of the specified aircraft models.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105 under the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives, contains a directive concerning Beechcraft 50 (Twin Bonanza) Series Aeroplanes. This directive, AD/BEECH 50/32, pertains to emergency exits and the necessary placards and markings (section 1/84). It applies to all models with serial numbers as referenced in Beechcraft service instruction No. 1241. The requirement outlined in this directive is for action to be taken in accordance with Beechcraft Service Instruction No. 1241, which likely involves updating the emergency exit placards and modifying the openable window latch to meet specified standards (section 1/84).
The directive imposes specific obligations on the parties or entities it governs. Aircraft operators and maintenance personnel must ensure compliance with the requirements within 100 hours’ time in service after 31 January 1984 or at the next scheduled inspection for Maintenance Release issue after 31 January 1984, whichever is later (section 1/84). This means that operators need to adhere to the timeframes set for implementing the necessary changes to the emergency exit placards and window latch modifications.
Failure to comply with the provisions of this directive can result in serious consequences. While the specific offences, penalties, or consequences are not detailed in the provided text, it is clear that non-compliance with CASA directives can lead to significant regulatory actions. Typically, breaches of such directives may result in enforcement actions by CASA, which could include fines, operational restrictions, or other penalties as prescribed by the Civil Aviation Act 1988 or related legislation. The severity of the penalties may depend on the nature and extent of the non-compliance, as well as any resultant safety risks.