AD/BEECH 36/8 - Engine Mount Bolt Nuts

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B03909 Not in force Legislative Instrument

Legislation content

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Beechcraft 36 (Bonanza) Series Aeroplanes

 

AD/BEECH 36/8 Engine Mount Bolt Nuts 8/70

Applicability: All models with S/Nos. E-42 and subsequent. Requirement:  Action in accordance with Beechcraft SI No. 0396-241. Compliance:               Within 25 hours time in service after 21 August 1970.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Australian Parliament, form a comprehensive set of rules governing civil aviation in Australia, including safety standards and operational requirements. Within this extensive regulatory framework, Part 39 addresses specific airworthiness directives aimed at ensuring the safety of aircraft operations. One such directive, AD/BEECH 36/8 issued on 8 July 1970, pertains to the Beechcraft 36 (Bonanza) series aeroplanes and specifically mandates action concerning engine mount bolt nuts for all models with serial numbers E-42 and subsequent. This directive was introduced to address identified safety issues with the engine mount bolt nuts, ensuring that these components are properly maintained to prevent potential failures that could compromise flight safety. The directive requires compliance within 25 hours of time in service after 21 August 1970, aligning with the specific instructions detailed in Beechcraft Service Instruction No. 0396-241.

Scope and Application

The Civil Aviation Regulations 1998, specifically under Part 39 - 105, applies to all Beechcraft 36 (Bonanza) Series aeroplanes with serial numbers E-42 and subsequent. This regulatory requirement is focused on the maintenance and safety standards of the engine mount bolt nuts for these aircraft models. The directive mandates that operators of these aircraft must adhere to the action specified in Beechcraft Service Instruction No. 0396-241 to ensure compliance with safety standards. This directive is binding within 25 hours of time in service following the date of the directive, which is 21 August 1970. The regulations are applicable nationwide, reflecting the Commonwealth's jurisdiction over civil aviation safety and ensuring uniform safety standards across Australia. There are no stated exclusions or exemptions in this specific directive; however, the broader regulatory framework may allow for variations or waivers under certain circumstances through subordinate instruments.

Key Provisions

The key operative sections of the Civil Aviation Regulations 1998, particularly under PART 39 - 105, pertain to the specific Airworthiness Directives issued for certain aircraft models. For instance, AD/BEECH 36/8 (paragraph 1) pertains to the Beechcraft 36 (Bonanza) Series Aeroplanes, specifically those with serial numbers E-42 and subsequent, and mandates compliance with Beechcraft Service Instruction No. 0396-241. This directive requires corrective action to be taken within 25 hours of time in service after 21 August 1970. The obligations imposed by these regulations are stringent, demanding that all affected aircraft owners or operators adhere to the specified maintenance requirements outlined in the Beechcraft Service Instruction. This involves the inspection and, if necessary, the replacement or repair of engine mount bolt nuts to ensure the continued airworthiness of the aircraft. Failure to comply with these directives can result in serious safety implications and potential non-compliance with the overarching civil aviation safety standards. Additionally, the Act stipulates specific timelines for compliance. Aircraft operators must ensure that the required actions are completed within the stipulated 25 hours of time in service following the issuance date of 21 August 1970. This timeframe underscores the urgency and critical nature of the mandated maintenance actions to prevent potential safety hazards. In terms of consequences for non-compliance, the Civil Aviation Regulations 1998 impose significant penalties. Non-compliance with airworthiness directives can lead to enforcement actions by the Civil Aviation Safety Authority (CASA). The potential penalties can include substantial fines and, in severe cases, the grounding of the aircraft until the required actions are satisfactorily completed. Additionally, continued non-compliance may result in the suspension or revocation of the aircraft’s certificate of airworthiness, which has severe ramifications for the operator’s ability to legally fly the aircraft.

Legal classification tags

Area of Law
Aviation Law
Instrument
Regulation
Concepts
Definitions & Interpretation
Compliance Obligations
Enforcement Powers
Catchwords
Airworthiness Directives

Interactions

Authorises

All Versions

Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.