AD/AA-5/5 - Elevator Trim Tab Hinge - Inspection

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

Legislation au F2006B02063 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

 


Gulfstream (Grumman American/ American Aviation) AA-5 Series Aeroplanes

 

AD/AA-5/5 Elevator Trim Tab Hinge - Inspection NK

Applicability: All models with S/Nos. 0001 to 0284. Document:  American Aviation SB No. 136.

Compliance: Within 100 hours time in service after 31 May 1973.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, establish a comprehensive regulatory framework for civil aviation safety. Within this framework, Part 39 provides for the issuance of Airworthiness Directives to ensure that aircraft meet specific safety standards. One such directive, AD/AA-5/5, targets the Gulfstream (Grumman American/ American Aviation) AA-5 Series aeroplanes, aiming to address the specific issue of elevator trim tab hinge integrity. This directive was introduced to fill a gap identified in the safety of these particular aircraft models, ensuring compliance with safety standards within a specified timeframe to mitigate potential risks associated with hinge failure. The policy objective behind such directives is to enhance the safety of civil aviation operations by mandating regular inspections and maintenance of critical components.

Scope and Application

The Civil Aviation Safety Authority (CASA) regulates the maintenance and airworthiness of aircraft through various instruments, including the Civil Aviation Regulations 1998. Part 39, in particular, contains provisions pertaining to airworthiness directives that apply to specific aircraft types. One such directive, AD/AA-5/5, pertains to Gulfstream (Grumman American/ American Aviation) AA-5 Series Aeroplanes, specifically those with serial numbers ranging from 0001 to 0284. This directive mandates an inspection of the elevator trim tab hinge, as outlined in American Aviation Service Bulletin No. 136, to be completed within 100 hours of the aircraft’s time in service after 31 May 1973. This regulation applies to all owners and operators of the specified aircraft models, ensuring compliance with airworthiness standards and safety protocols set forth by CASA. The directive’s scope is national, extending across all states and territories within Australia, and applies to any entity or individual who holds responsibility for the maintenance and operation of the affected aircraft. No exclusions or exemptions are stated within the directive itself, although further details on compliance and enforcement might be found in subordinate instruments issued by CASA.

Key Provisions

The Civil Aviation Regulations 1998 (Cth), Part 39 – 105, imposes specific airworthiness directives on the maintenance and operation of certain aircraft, including the Gulfstream (Grumman American/ American Aviation) AA-5 Series Aeroplanes. Section AD/AA-5/5 pertains to the elevator trim tab hinge inspection of these aircraft. This directive applies to all models with serial numbers (S/Nos.) ranging from 0001 to 0284. The directive references American Aviation Service Bulletin No. 136 as the document detailing the inspection requirements. The compliance requirement stipulates that this inspection must be conducted within 100 hours of time in service after 31 May 1973. The obligations imposed by this regulation are primarily on the operators and maintenance personnel of the affected Gulfstream AA-5 Series Aeroplanes. Operators must ensure that the specified inspection of the elevator trim tab hinge is performed in accordance with the guidelines outlined in the referenced service bulletin. This entails thorough visual inspection and any necessary repairs or replacements to maintain the structural integrity and safety of the aircraft's elevator system. Maintenance personnel must be adequately trained and authorised to perform these inspections and any subsequent maintenance work. Failure to comply with this airworthiness directive can result in severe consequences. The Civil Aviation Safety Authority (CASA) has the authority to enforce compliance through various measures. Non-compliance may lead to penalties under the Civil Aviation Act 1988 (Cth). The maximum penalty for breaches of the Civil Aviation Regulations can include substantial fines and, in more severe cases, imprisonment. Furthermore, the operation of a non-compliant aircraft can result in immediate grounding, which can have significant financial and operational implications for the operator. The safety of passengers and crew, as well as the overall integrity of the aviation system, is paramount, and CASA takes a stringent approach to enforcing these regulations.

Legal classification tags

Area of Law
Administrative Law
Instrument
Regulation
Concepts
Definitions & Interpretation
Compliance Obligations
Prohibited Conduct

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.