Airworthiness Directives 2004 - Revocation and Remaking - Gulfstream (Rockwell) 112 Series Aeroplanes (Cth)
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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 (Rockwell) 112 Series Aeroplanes
AD Name AD Number
Aileron Hinge Doublers - Inspection and Modification AD/AC-112/1
Wing Structural Life Limitation AD/AC-112/2
Aileron Control System - Modification AD/AC-112/3
Engine Oil Pressure Line - Replacement AD/AC-112/4
Fuel Selector Valve - Inspection and Replacement AD/AC-112/5 Amdt 1
Front Seat and Shoulder Harness AD/AC-112/6 Amdt 4
Lower Vertical Fin Rib - Inspection AD/AC-112/7 Amdt 2
Aileron Hinge Supports - Inspection and Modification AD/AC-112/8 Amdt 1
Wing Structure - Rib - Inspection AD/AC-112/9
Fuel Tank Access Door Sealant - Replacement AD/AC-112/10
Elevator and Rudder Hinge Fittings - Inspection and/or Replacement AD/AC-112/11
Rudder Rib - Inspection AD/AC-112/12
Wing Forward Spar AD/AC-112/13 Amdt 2
Vertical Stabiliser Forward Spar Attachment Structure AD/AC-112/14 Amdt 1
Rudder Spar AD/AC-112/15
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