COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 35 (Bonanza) Series Aeroplanes
AD/BEECH 35/46 Beryl Aviation Filtrator Assembly 4/75
Applicability: Models 35, A35, B35, C35, D35, E35, F35, G35, 35R, H35, J35, K35, M35, N35,
P35, S35, V35, N35A, V35B, which have been modified in accordance with FAA Supplemental Type Certificate No. SA2653WE (Installation of engine crankcase breather and vacuum pump air-oil separator).
Requirement: 1. For Beech Models 35, A35, B35, C35, D35, E35, F35, G35 and 35R, remove the Beryl Aviation filtrator assembly P/N B-1119-1 and install either P/N B-1119-M or P/N B- 1119-RM.
2. For Beech Models S35, V35, V35A and V35B, remove the Beryl Aviation filtrator assembly P/N B-1116-1 and install either P/N B-1116-M or P/N B-1116-RM.
3. For Beech Models H35, J35, K35, M35, N35 and P35, remove the Beryl Aviation filtrator assembly P/N B-1114-1 and install either P/N B-1114-M or P/N
B-1114-RM.
Compliance: Within 100 hours time in service after 28 February 1974.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, address the need for stringent safety standards in civil aviation to ensure the safety and reliability of aircraft operations. Specifically, Part 39 - 105 of these Regulations includes Airworthiness Directives that mandate certain safety measures and modifications for various aircraft models. One such directive, AD/BEECH 35/46, pertains to the Beryl Aviation filtrator assembly in Beechcraft 35 (Bonanza) series aeroplanes. This directive was introduced to address the potential risks associated with the original filtrator assemblies and requires specific modifications to enhance safety. The directive applies to a range of Beechcraft 35 models that have been modified under a particular FAA Supplemental Type Certificate. The objective is to ensure compliance with safety standards by mandating the replacement of specific Beryl Aviation filtrator assemblies with improved versions within a specified timeframe.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, establish the Civil Aviation Safety Authority's Schedule of Airworthiness Directives for the Beechcraft 35 (Bonanza) series aeroplanes, under the legislative instrument F2006B03842. This directive applies to Beechcraft 35 models that have undergone modifications in accordance with FAA Supplemental Type Certificate No. SA2653WE, which pertains to the installation of an engine crankcase breather and vacuum pump air-oil separator. The directive mandates the removal and replacement of specific Beryl Aviation filtrator assemblies with new ones for various Beechcraft 35 models to ensure compliance with safety standards. Compliance must be achieved within 100 hours of time in service after 28 February 1974. The geographic and jurisdictional reach of this regulation is national, applying across all states and territories within Australia, and it is enforced under the regulatory authority of the Civil Aviation Safety Authority. There are no stated exclusions or exemptions in the directive, and any further application or interpretation may be extended or restricted through subordinate instruments as necessary.
Key Provisions
The Civil Aviation Regulations 1998, particularly under Part 39 - 105, address the airworthiness directives (AD) concerning specific models of Beechcraft 35 (Bonanza) series aeroplanes. The relevant AD/BEECH 35/46 pertains to the Beryl Aviation filtrator assembly (sections 1 to 3). These sections specify the requirement to replace certain filtrator assemblies with updated models for different Beechcraft 35 models that have been modified under FAA Supplemental Type Certificate No. SA2653WE. For instance, Beech Models 35, A35, B35, C35, D35, E35, F35, G35 and 35R must replace the Beryl Aviation filtrator assembly P/N B-1119-1 with either P/N B-1119-M or P/N B-1119-RM. Similar replacements are mandated for other Beechcraft models as detailed in sections 2 and 3.
Entities governed by these regulations must ensure compliance within 100 hours of time in service following 28 February 1974. This compliance requirement entails the removal and replacement of specified Beryl Aviation filtrator assemblies. The regulations do not leave much room for interpretation and demand that the specified modifications be carried out as outlined. Failure to adhere to these specifications could potentially compromise the airworthiness of the aircraft, thereby posing significant safety risks.
The legislation imposes clear obligations on the owners and operators of the specified Beechcraft 35 models to perform the required modifications within the stipulated timeframe. This includes ensuring that the correct part numbers are installed as per the AD/BEECH 35/46 directive. Non-compliance with these directives can lead to serious safety issues, and the onus is on the operators to maintain the airworthiness of their aircraft by following the mandated procedures.
Failure to comply with these airworthiness directives can result in significant consequences. While the specific civil or criminal penalties are not detailed in the text, non-compliance can lead to the grounding of the aircraft until the necessary modifications are performed. Furthermore, operating an aircraft that does not meet the specified airworthiness standards can lead to severe safety risks, potentially resulting in accidents. Thus, it is crucial for operators to adhere strictly to these directives to avoid any legal repercussions or safety hazards.