Airworthiness Directives 2004 - Revocation and Remaking - Gulfstream (Grumman) G1159 and G-IV Series Aeroplanes

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 Airworthiness Directives 2004

 I, DAVID ALAN VILLIERS, delegate of the Civil Aviation Safety

 Authority, acting under subregulation 39.001 (1) of the Civil

 Aviation Safety Regulations 1998:

 (a) revoke the Airworthiness Directives mentioned in

 Schedule 1; and

 (b) make, as separate instruments, each Airworthiness

 Directive mentioned in Schedule 1 and attached.

 

 

 David Villiers

 Delegate of the Civil Aviation Safety Authority

 

  20 December 2004

 Note:   Each attached Airworthiness Directive is being re-made in exactly the

 same form as appears in the latest published edition of the Directive.

 


 Schedule 1 Revocation and Remaking of

 Airworthiness Directives

 Gulfstream (Grumman) G1159 and G-IV Series Aeroplanes

 AD Name AD Number

 Airspeed Limitation Placard - Rework AD/G1159/1

 Trim Tab Actuators - Inspection AD/G1159/2 Amdt 1

 Fire Extinguishing System - Modification AD/G1159/3

 Life Limited Components - Retirement AD/G1159/4 Amdt 4

 High Pressure Fuel Cock - Modification AD/G1159/5

 Vertical Tail Rear Beam Attaching Bolts - Inspection and Modification AD/G1159/6

 Main Cabin Floorboards - Inspection and Repair AD/G1159/7

 Aileron Control System - Inspection AD/G1159/8

 Fuselage Aft Pressure Dome - Inspection and Modification AD/G1159/9

 Nose Landing Gear Trunnion Assembly - Inspection AD/G1159/10

 Flight Control Trim Systems - Inspection and Modification AD/G1159/11

 Wing Rear Beam Lower Cap Splice Attachment Bolt - Inspection and  AD/G1159/12

 Elevator Mass Balance - Inspection AD/G1159/13

 Hydraulic Power Shut-Off - Modification AD/G1159/14

 Aileron Hydraulic System AD/G1159/15 Amdt 1

 Restricted Authority Electric Trim - Modification AD/G1159/16

 Stall Barrier System In-Line Filters - Replacement AD/G1159/17

 Ground Spoiler System - Deactivation AD/G1159/18

 Landing Gear and Oxygen Systems Gas Cylinders - Inspection and Replacement AD/G1159/19

 Wing Trailing Edge Structure - Inspection AD/G1159/20

 Jumpseat Placard - Installation AD/G1159/21 Amdt 1

 Pitot-Static System Connections - Inspection AD/G1159/22

 Main Landing Gear Side Brace Actuating Cylinders - Inspection AD/G1159/23 Amdt 2

 Cabin Pressure Differential - Restriction AD/G1159/24 Amdt 2

 Windows - Inspection and Modification AD/G1159/25

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

 Baggage Door Frame - Inspection AD/G1159/27

 Control Column Wheel Attaching Shaft - Inspection AD/G1159/28

 Flight Manual - Change to Metric Units AD/G1159/29


 Fuselage, Rudder Actuator Structural Attachment Points - Inspection AD/G1159/30

 Elevator Trim Tab Outboard Hinge Fittings - Inspection AD/G1159/31 Amdt 1

 Flap, Auxiliary and Thrust Reverser Hydraulic Shut-Off Valves - Inspection  AD/G1159/32

 Engine Fire Extinguisher System AD/G1159/33 Amdt 2

 Fluorescent Lighting Installations Incorporating Series '66' Lamps AD/G1159/34 Amdt 1

 Takeoff Warning System AD/G1159/35

 Corrosion and Cracking Fuselage Station 452 AD/G1159/36

 Wing Plank Splice Between BL 135 and BL 156 AD/G1159/37

 Electrical Power - Alternator Feeder Cable AD/G1159/38

 Landing Gear Door Control Valves AD/G1159/39

 Goodyear Flight Eagle Tyres AD/G1159/40

 Engine Fire Extinguisher Bottle Electrical Connections AD/G1159/41

 DC Essential Bus Indication AD/G1159/42

 Damper Shafts AD/G1159/43

 

Overview

The Airworthiness Directives 2004 legislative instrument was enacted by David Alan Villiers, a delegate of the Civil Aviation Safety Authority, under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998. This instrument serves to revoke existing Airworthiness Directives and remake them as separate instruments to ensure the continuing safety and airworthiness of the Gulfstream (Grumman) G1159 and G-IV Series Aeroplanes. The enactment is a response to identified issues requiring specific directives to maintain aircraft safety standards, although the precise nature of these issues is not detailed in the text. The policy objective is implicitly to uphold and enhance aviation safety through the regular updating and enforcement of airworthiness standards.

Scope and Application

The Airworthiness Directives 2004, made by David Alan Villiers, a delegate of the Civil Aviation Safety Authority under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998, apply to the maintenance and operation of Gulfstream (Grumman) G1159 and G-IV series aeroplanes in Australia. These directives cover specific areas of concern such as airspeed limitations, fire extinguishing systems, and inspections of various components, including trim tab actuators, vertical tail rear beam attaching bolts, and hydraulic systems. The geographic scope of these directives is national, as they pertain to all aircraft registered in Australia and operated by Australian entities. The directives are intended to ensure the safety and airworthiness of these specific aircraft models. Notably, the instrument revokes existing directives and remakes them to align with the latest published editions, ensuring that the regulatory framework remains current and effective.

Key Provisions

This legislative instrument, Airworthiness Directives 2004, primarily focuses on the revocation and remaking of certain Airworthiness Directives (ADs) pertaining to the Gulfstream (Grumman) G1159 and G-IV series aeroplanes. The primary sections (1) and (2) of the instrument involve the revocation of existing ADs listed in Schedule 1 and the remaking of these ADs as separate instruments, ensuring that the most current and relevant safety measures are enforced. This action is taken under subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998 by David Alan Villiers, who is acting as a delegate of the Civil Aviation Safety Authority. Each re-made AD is presented in the exact form as it appears in the latest published edition. The obligations and requirements imposed by this instrument are specific to the maintenance, inspection, and modification of various components of the Gulfstream G1159 and G-IV series aeroplanes to ensure their airworthiness. These obligations encompass a wide range of directives, including placard installations, actuator inspections, system modifications, and structural inspections. For example, AD/G1159/1 requires the rework of the airspeed limitation placard, while AD/G1159/3 mandates modifications to the fire extinguishing system. Additionally, AD/G1159/10 involves the inspection and modification of flight control trim systems, and AD/G1159/13 requires modifications to the hydraulic power shut-off. Operators and maintainers of these aircraft must adhere to these detailed requirements to ensure compliance with airworthiness standards. Failure to comply with the provisions outlined in these Airworthiness Directives can lead to significant legal and safety consequences. While the specific penalties for non-compliance are not detailed within this instrument, violations of airworthiness regulations under the Civil Aviation Safety Regulations 1998 can result in both civil and criminal penalties. Civil penalties may include substantial fines, while criminal penalties could include imprisonment. The exact penalties depend on the severity of the breach and the specific regulations violated. It is crucial for operators and maintainers to ensure strict adherence to these directives to avoid such consequences and to maintain the highest standards of aviation safety.

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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.