AD/BEECH 95/12 - Flap Bracket

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

Legislation au F2006B04286 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 95 (Travelair) Series Aeroplanes

 

AD/BEECH 95/12 Flap Bracket 8/72

Applicability: All models which have achieved 1000 or more hours time in service.

 

Requirement: Inspect flap actuator bracket and adjacent structure on RH and LH flaps for cracks or signs of distress.

 

Compliance: Within 100 hours time in service after 31 August 1972 and thereafter at intervals not exceeding 300 hours’ time in service.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Commonwealth of Australia, establish a comprehensive framework for ensuring the safety of civil aviation within Australia. Specifically, Part 39 - 105 of these regulations focuses on the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives, which are mandatory instructions issued to ensure the continued airworthiness of aircraft. One such directive, AD/BEECH 95/12, targets Beechcraft 95 (Travelair) series aeroplanes, addressing the critical need for inspecting the flap actuator bracket and adjacent structure on both the right and left flaps for cracks or signs of distress. This directive was introduced to mitigate the risk of structural failure due to fatigue, which could potentially lead to catastrophic in-flight events. The policy objective behind this directive is to maintain the highest safety standards in civil aviation by ensuring regular and rigorous inspections of specified aircraft components.

Scope and Application

The Civil Aviation Regulations 1998, under Part 39, specifically address the airworthiness of aircraft through directives, such as AD/BEECH 95/12 which pertains to the Beechcraft 95 (Travelair) series aeroplanes. This legislation applies to all models of these aeroplanes that have accumulated 1,000 or more hours of time in service. The primary requirement outlined in the directive is the inspection of the flap actuator bracket and the adjacent structure on both the right-hand and left-hand flaps for any cracks or signs of distress. Compliance with this directive must occur within 100 hours of time in service after 31 August 1972 and subsequently at intervals not exceeding 300 hours of time in service. The directive is applicable nationwide within the jurisdiction of the Commonwealth of Australia and is enforced by the Civil Aviation Safety Authority. There are no stated exclusions or exemptions within the text, though the authority may extend or restrict application through subordinate instruments as necessary.

Key Provisions

The Civil Aviation Regulations 1998, particularly Part 39 - 105, addresses airworthiness directives with specific focus on the Beechcraft 95 (Travelair) Series Aeroplanes. Section AD/BEECH 95/12 pertains to the flap bracket, establishing crucial safety measures for these aircraft. According to the regulation (AD/BEECH 95/12), the directive applies to all models of the Beechcraft 95 series that have accumulated 1000 or more hours of time in service (Section 8/72). The primary requirement is that the flap actuator bracket and the adjacent structure on both the right-hand (RH) and left-hand (LH) flaps must be inspected for any cracks or signs of distress. The obligations under this directive are quite specific and critical for maintaining airworthiness. Operators of the Beechcraft 95 series must ensure that the inspections are conducted by qualified personnel. The initial inspection must be carried out within 100 hours of time in service after 31 August 1972. Following this initial inspection, further inspections must be conducted at intervals not exceeding 300 hours of time in service. This periodic inspection requirement ensures that any potential structural issues are identified and addressed promptly, thereby maintaining the safety standards required by the Civil Aviation Safety Authority (CASA). Failure to comply with these airworthiness directives can result in severe consequences. Under the Civil Aviation Regulations, non-compliance with an airworthiness directive can be considered a breach of regulations, leading to enforcement actions. In terms of penalties, the severity of the penalty depends on the nature and extent of the breach. For significant violations, CASA can impose fines, suspend or revoke air operator certificates, and even take legal action against the operators. The exact penalties are determined by the specific circumstances of the breach but can include substantial financial penalties and other administrative actions aimed at ensuring compliance and upholding safety standards in the aviation industry.

Legal classification tags

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

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.