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

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

Legislation au F2006B10034 In force Legislative Instrument

Legislation content

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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Interactions

Authorises

All Versions

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.