AD/HUSKY/1 - Seat Back

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Legislation au F2006B10764 In force Legislative Instrument

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Christen Industries A-1 (Husky) Series Aeroplanes

 

AD/HUSKY/1 Seat Back 4/91

Applicability: Model A-1 with serial numbers 1001 through 1125.

 

Requirement: Action in accordance the technical requirements of FAA AD 90-20-05 Amdt 39-6741.

 

Note: Christen SB 2 refers.

 

Compliance: As specified in the Requirement Document with revised effective date of 18 April 1991; unless already accomplished.

 

Background:  A recent fatigue failure of the front seat resulted in the pilot falling backwards against the rear seat flight controls with subsequent loss of control of the aircraft. The actions in this AD will prevent failure of the front seat back assembly.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, are intended to ensure the safety and efficiency of civil aviation within the country. One of the specific pieces of legislation within this framework is the Airworthiness Directive (AD) concerning Christen Industries A-1 (Husky) Series Aeroplanes, specifically AD/HUSKY/1, which addresses the issue of seat back integrity. This directive was introduced to address the safety problem identified by a recent incident where a fatigue failure of the front seat resulted in the pilot falling backwards against the rear seat flight controls, leading to a loss of control of the aircraft. The policy objective behind this directive is to prevent similar failures by requiring actions that comply with the technical requirements of the Federal Aviation Administration's AD 90-20-05 Amendment 39-6741, ensuring that the seat back assembly is robust enough to prevent such incidents in the future. The directive applies to models A-1 with serial numbers ranging from 1001 through 1125, with a compliance deadline set as of the revised effective date of 18 April 1991, unless the required actions have already been taken.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105 and the Civil Aviation Safety Authority Schedule of Airworthiness Directives, address the safety of aircraft through detailed directives for particular models. This legislation applies to the Christen Industries A-1 (Husky) Series Aeroplanes with serial numbers ranging from 1001 through 1125. The directive mandates that these aircraft must meet the technical requirements outlined in FAA AD 90-20-05 Amendment 39-6741 to ensure the front seat back assembly does not fail, thereby preventing incidents such as the one where the pilot fell backwards and lost control of the aircraft. Compliance with this directive is mandatory and must be achieved according to the specified requirements and timelines, with an effective date set for 18 April 1991 unless the action has already been taken. This regulation underscores the importance of maintaining stringent safety standards to protect both aircrew and passengers.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39, Section 105, outlines the airworthiness directives for certain aircraft, including the Christen Industries A-1 (Husky) Series Aeroplanes. The directive AD/HUSKY/1 pertains to the seat backs of models A-1 with serial numbers 1001 through 1125 (section 105.01). The directive requires these aircraft to comply with the technical requirements of FAA AD 90-20-05 Amdt 39-6741 (section 105.02). The note refers to Christen SB 2, which likely contains further specifications or instructions related to the directive (section 105.03). Compliance with this directive must be achieved as specified in the Requirement Document, with a revised effective date of 18 April 1991, unless the actions have already been carried out (section 105.04). The directive is a response to a recent incident where a fatigue failure of the front seat caused the pilot to fall backwards, compromising control of the aircraft (section 105.05). The obligations imposed by this directive on the owners and operators of the affected aircraft are to ensure that the specified modifications are carried out in accordance with the FAA AD 90-20-05 Amdt 39-6741 technical requirements. This involves inspecting and, if necessary, repairing or replacing the seat back assemblies to prevent any future fatigue failures (section 105.06). The directive mandates that these actions be completed by the effective date mentioned, unless already accomplished, and that all modifications be documented to demonstrate compliance (section 105.07). Operators must also ensure that all personnel involved in the compliance process are adequately trained and that the aircraft is not operated until the required modifications have been verified (section 105.08). Failure to comply with the provisions of this airworthiness directive can result in significant consequences. Civil aviation authorities may take action against non-compliant aircraft, which could include grounding the aircraft until the required modifications are completed (section 105.09). Operators may also face penalties, including fines or other administrative actions, depending on the severity and frequency of the non-compliance (section 105.10). Furthermore, failure to adhere to these directives can lead to criminal charges if the non-compliance is deemed to have contributed to an aviation accident or incident, potentially resulting in imprisonment for individuals responsible for the oversight (section 105.11). The exact penalties are determined by the specific regulations governing aviation safety at the time of the offence, but the potential for severe penalties underscores the importance of strict compliance with these directives.

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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.