Document ID: chunk:federal_register_of_legislation:F2006B10034:body:0
Version: federal_register_of_legislation:F2006B10034
Segment Type: other
Provision Reference: 
Character Range: 0–971

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/G1159/31
 Amdt 1

  Elevator Trim Tab Outboard Hinge Fittings - Inspection

 7/82

 Applicability: All model GII and GIIB aircraft.

 Document: Grumman Customer Bulletin No. 325 Amendment 1. (FAA AD 82-11-02 Amdt. 39-
            4384 refers).

             Compliance: 1. Unless already accomplished, before further flight after 31 July 1982 - as detailed in the requirement document.

             2. Repeat inspection as detailed in the requirement document until repair or replacement as detailed in the Aircraft Service Change No. 315.

            Background: Manufacturer reports trim tab hinge fitting cracks have occurred. Amendment 1 raised to cover increases in applicability and revisions to repeat inspection, repair or replacement requirements.