AD/G159/13 Amdt 3 - Trim Tab Actuators
1AD/G159/13 Amdt 3 - Trim Tab Actuators
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COMMONWEALTH OF AUSTRALIA CIVIL AVIATION ORDERS CIVIL AVIATION SAFETY AUTHORITY PART 105 SCHEDULE OF AIRWORTHINESS DIRECTIVES
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GULFSTREAM (GRUMMAN) G.159 SERIES AEROPLANES
AD/G159/13 Amdt 3 Trim Tab Actuators 10/9 7
Applicability: All models not fitted with trim tab actuators Part Number 159SCC100-11.
Requirement: 1. Action in accordance with Gulfstream (Grumman) Customer Bulletin 208A as amended by Amendments 1 and 2.
- Install trim tab actuator 159SCC100-11 in accordance with Gulfstream Aircraft Service Change 191.
Note: FAA AD 97-14-09 refers
Compliance: 1. Within 200 hours time in service after the last inspection carried out in accordance with the previous issue of this Directive, or before 30 September 1997, whichever occurs last; thereafter at intervals not exceeding 200 hours time in service.
- Within 1000 hours time in service after 11 September 1997.
This airworthiness directive becomes effective on 11 September 1997.
Background: This directive was originally issued with subsequent amendment to prevent failure of the of the elevator trim tab mounting lugs due to cracking.
Amendment 3 is issued to provide terminating action for the inspection.