AD/G1159/8 - Aileron Control System - Inspection

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

Legislation au F2006B10051 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/G1159/8 Aileron Control System - Inspection 8/73

Applicability: All models with S/Nos. 1 to 119 and 775. Document:  Grumman Customer Bulletin No. 163.

Compliance: Within 100 hours time in service after 31 August 1973 unless already accomplished.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Australian Parliament, play a pivotal role in regulating the safety and operational standards of civil aviation within Australia. Among the various parts, Part 39 - 105, specifically focusing on the Civil Aviation Safety Authority's Schedule of Airworthiness Directives, addresses critical safety concerns for particular aircraft models. One such directive is AD/G1159/8, which pertains to the aileron control system inspection for Gulfstream (Grumman) G1159 and G-IV series aeroplanes. This directive was introduced to ensure that specific models, identified by their serial numbers, are inspected within 100 hours of time in service following 31 August 1973 to mitigate potential safety risks. The policy objective is to maintain and enhance the safety of aircraft operations by enforcing timely and specific maintenance actions as recommended by relevant bulletins, such as Grumman Customer Bulletin No. 163.

Scope and Application

The Civil Aviation Safety Authority (CASA) has issued Airworthiness Directive AD/G1159/8, which applies specifically to Gulfstream (Grumman) G1159 and G-IV series aeroplanes with serial numbers (S/Nos.) ranging from 1 to 119 and 775. This directive mandates an inspection of the aileron control system in compliance with the requirements outlined in Grumman Customer Bulletin No. 163. Operators of these specific aircraft models must ensure the inspection is conducted within 100 hours of the aeroplanes’ time in service following 31 August 1973, unless the inspection has already been completed prior to this date. The directive is a regulatory requirement under the Civil Aviation Regulations 1998, which are applicable throughout the Commonwealth of Australia, ensuring consistent safety standards across the national airspace. The directive does not explicitly state any exclusions, exemptions, or thresholds beyond the specified serial numbers and time frame, but it is subject to further interpretation and application through subordinate instruments issued by CASA.

Key Provisions

The Civil Aviation Regulations 1998, under Part 39, section 105, establish the authority and scope of the Civil Aviation Safety Authority (CASA) to issue Airworthiness Directives (ADs). Specifically, AD/G1159/8 pertains to the Gulfstream (Grumman) G1159 and G-IV Series aeroplanes and mandates an inspection of the aileron control system. This directive applies to all models with serial numbers (S/Nos.) ranging from 1 to 119 and from 775. The requirement is clearly outlined in the Grumman Customer Bulletin No. 163, which provides the technical specifications and procedures to be followed for this inspection. The inspection must be carried out within 100 hours of time in service after 31 August 1973, unless it has already been completed. The AD imposes several obligations on the operators and owners of the affected aircraft. They must ensure that the inspection of the aileron control system is conducted by qualified personnel in accordance with the instructions provided in the Grumman Customer Bulletin No. 163. This includes verifying that all components of the aileron control system are in good working order and free from defects or damage that could compromise the aircraft's safety. Operators and owners are also required to maintain records of the inspections performed, including any repairs or replacements made, and ensure these records are available for inspection by CASA upon request. Failure to comply with the requirements of AD/G1159/8 can result in serious consequences. Under the Civil Aviation Act 1988, non-compliance can lead to enforcement actions by CASA, including fines and potential grounding of the aircraft. The maximum penalty for contravening an AD can be substantial, with fines reaching up to $16,500 for individuals and up to $82,500 for corporations, depending on the severity and frequency of the breach. Additionally, CASA has the authority to initiate legal proceedings, which could result in further financial penalties or even imprisonment in cases of gross negligence or willful disregard of the regulations. The regulatory framework surrounding ADs, such as AD/G1159/8, underscores the importance of maintaining high safety standards in civil aviation. Operators and owners must be diligent in adhering to the specified inspection requirements to ensure the continued airworthiness of their aircraft and to protect the safety of all passengers and crew. Any deviation from the stipulated guidelines not only risks regulatory penalties but also poses significant safety hazards that could lead to catastrophic outcomes. Therefore, understanding and complying with these provisions is crucial for all stakeholders involved in the operation of the affected aircraft.

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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.