AD/G1159/26 - Nose Landing Gear Retract Cylinder Aft Attach Structure - Inspection

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Legislation au F2006B10028 Not 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

 


Gulfstream (Grumman) G1159 and G-IV Series Aeroplanes

 

AD/G1159/26 Nose Landing Gear Retract Cylinder

Aft Attach Structure - Inspection

Applicability: All model G1159 with S/Nos. 001 to 232 and 775. Document:  Gulfstream American Customer Bulletin No. 276. Compliance:               Within 100 hours time in service after 31 March 1979.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

3/79

Overview

The Civil Aviation Regulations 1998, as part of the legislative framework overseen by the Commonwealth of Australia, establish a comprehensive set of rules and guidelines to ensure the safety of civil aviation within Australian airspace. One particular aspect of this regulation is the issuance of Airworthiness Directives (ADs), which are binding requirements imposed on aircraft owners or operators to ensure their aircraft remain airworthy. These ADs address specific safety issues that may arise during the operation of certain types of aircraft. The specific AD/G1159/26, which pertains to Gulfstream (Grumman) G1159 and G-IV series aeroplanes, highlights the need for inspections of the nose landing gear retract cylinder aft attach structure. This directive was introduced to address a critical safety concern identified with these particular aircraft models and was enacted to ensure compliance with safety standards, thus protecting the public and maintaining the integrity of civil aviation operations in Australia. The Civil Aviation Regulations 1998 are administered by the Civil Aviation Safety Authority (CASA) under the authority granted by the Civil Aviation Act 1988. The policy objective behind these regulations, and specifically AD/G1159/26, is to maintain the highest possible safety standards in civil aviation. By mandating inspections and maintenance actions, CASA aims to prevent potential structural failures that could compromise the safety of the aircraft during operation. This legislative instrument underscores the commitment to proactive safety measures and the continuous monitoring of aircraft to mitigate risks associated with identified safety issues.

Scope and Application

The Civil Aviation Regulations 1998, under Part 39 - 105, specifically address the airworthiness of Gulfstream (Grumman) G1159 and G-IV series aeroplanes, with a focus on the nose landing gear retract cylinder aft attach structure inspection. This directive applies to all model G1159 aircraft with serial numbers ranging from 001 to 232 and 775. The directive mandates that the specified inspection must be conducted within 100 hours of time in service after 31 March 1979. The directive is referenced in Gulfstream American Customer Bulletin No. 276. The regulations are applicable within the jurisdiction of the Commonwealth of Australia and are enforced by the Civil Aviation Safety Authority. No exclusions or exemptions are stated within the text provided, and the scope of the directive is narrowly focused on the specified aircraft models and the outlined inspection requirements. The Civil Aviation Regulations 1998 may extend or restrict the application of this directive through subordinate instruments, but such details are not provided in the text.

Key Provisions

The Civil Aviation Regulations 1998, specifically in Part 39 - 105, under the Civil Aviation Safety Authority (CASA) schedule of Airworthiness Directives, addresses the maintenance and safety requirements for the Gulfstream (Grumman) G1159 and G-IV series aeroplanes. This regulation is detailed in AD/G1159/26, which mandates an inspection of the nose landing gear retract cylinder aft attach structure. This directive applies to all model G1159 aeroplanes with serial numbers ranging from 001 to 232 and 775 (Section 3/79). The requirement for compliance is set within 100 hours of time in service after 31 March 1979, as outlined in Gulfstream American Customer Bulletin No. 276. This legislation imposes several obligations on the parties or entities governed by it. Primarily, the operator of the affected Gulfstream G1159 aeroplanes must ensure that the specified inspection is conducted by qualified personnel. This inspection must be carried out within the stipulated timeframe of 100 hours of time in service post the date mentioned, which is 31 March 1979. The operator is also required to maintain accurate records of the inspection and any subsequent actions taken to ensure the aircraft remains airworthy. The Gulfstream G1159 aeroplanes' operators must also ensure that all maintenance and inspections are performed in accordance with the manufacturer's guidelines as detailed in Gulfstream American Customer Bulletin No. 276. Failure to comply with the provisions of AD/G1159/26 can result in significant legal and financial consequences. Under the Civil Aviation Act 1988, non-compliance with Airworthiness Directives can lead to civil penalties, including fines. The specific penalties can vary, but they may include fines of up to $153,000 for corporations and $30,600 for individuals, as stipulated under the Civil Aviation Regulations. Additionally, continued operation of an aircraft that does not meet the airworthiness standards can result in criminal charges, with potential imprisonment for operators or individuals responsible for the oversight of the aircraft. The severity of the penalty reflects the importance of adhering to these safety directives to prevent potential hazards that could compromise flight safety.

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Aviation Law
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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.