Airworthiness Directives 2004 - Revocation and Remaking - Gulfstream (Rockwell) 112 Series Aeroplanes (Cth)

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