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AD/G1159/48 - Roll Axis Hardover Protection System
Gulfstream (Grumman) G1159 and G-IV SeriGulfstream (Grumman) G1159 and G-IV Series Aeroplanes
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Gulfstream (Grumman) G1159 and G-IV Series Aeroplanes
| AD/G1159/48 | Roll Axis Hardover Protection System | 8/2007 |
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<table cellspacing="0" cellpadding="0" style="width:510.3pt; margin-top:0pt; margin-bottom:0pt; border-collapse:collapse"><tbody><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Applicability:</span></p></td><td colspan="3" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Gulfstream Aerospace Corporation model/series aeroplanes as follows:</span></p></td></tr><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span></span></p></td><td colspan="2" style="width:201.9pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-bottom:12pt"><span style="width:36pt; display:inline-block"></span><span style="font-weight:bold">Mode/Series</span></p><p style="margin-top:12pt; margin-left:36pt; text-indent:-36pt"><span style="width:36pt; text-indent:0pt; display:inline-block"></span><span>GV</span><br><span>GV-SP</span></p></td><td style="width:201.95pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-bottom:12pt"><span style="font-weight:bold">Serial Numbers</span></p><p style="margin-top:12pt"><span>674 through 693 inclusive</span><br><span>5001 through 5072 inclusive</span></p></td></tr><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Requirement:</span></p></td><td colspan="3" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-left:21.3pt; text-indent:-21.3pt"><span>1.</span><span style="width:12.3pt; text-indent:0pt; display:inline-block"> </span><span>If not previously accomplished, repair the force link assembly wire harness by doing all actions specified in the Accomplishment Instructions of the applicable service information identified in Table 1 of this Directive.</span></p></td></tr><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span></span></p></td><td colspan="3" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="text-align:center"><span style="font-weight:bold">Table 1</span></p></td></tr><tr style="height:6.45pt"><td rowspan="4" style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span></span></p></td><td style="width:101pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="text-align:center"><span style="font-weight:bold">Model</span></p></td><td colspan="2" style="width:302.85pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="text-align:center"><span style="font-weight:bold">Service Information</span></p></td></tr><tr style="height:6.35pt"><td style="width:101pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>GV-SP series</span></p></td><td colspan="2" style="width:302.85pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Gulfstream G500 Customer Bulletin 14, dated 13 June 2005</span></p></td></tr><tr style="height:6.35pt"><td style="width:101pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>GV-SP series</span></p></td><td colspan="2" style="width:302.85pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Gulfstream G550 Customer Bulletin 14, dated 23 June 2005</span></p></td></tr><tr style="height:6.35pt"><td style="width:101pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>GV series</span></p></td><td colspan="2" style="width:302.85pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Gulfstream GV Customer Bulletin 135, dated 23 June 2005</span></p></td></tr><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p class="Note"><span></span></p></td><td colspan="3" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p class="Note"><span>Note 1: </span><span></span><span>The Gulfstream customer bulletins identified in Table 1 of this Directive include Vought Service Bulletin SB-VAIGV/GVSP-27-PG0098, dated 9 May 2005, as an additional source of service information for the repair.</span></p></td></tr><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span></span></p></td><td colspan="3" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-left:21.3pt; text-indent:-21.3pt"><span>2.</span><span style="width:12.3pt; text-indent:0pt; display:inline-block"> </span><span>If, during the Requirement 1 repair, any nick or other damage is found on or to the environmental seal around the installed wires (see paragraph 2.B.(2)c)7. or 2.C.(2)c)7. of SB-VAIGV/GVSP-27-PG0098), repair using a method approved by the Manager, Atlanta Aircraft Certification Office (ACO), United States Federal Aviation Administration (FAA).</span><span> </span><span>For a repair method to be approved by the Manager, Atlanta ACO, as required by this paragraph, the Manager's approval letter must specifically refer to FAA AD 2006-18-13.</span></p></td></tr><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span></span></p></td><td colspan="3" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p class="Note"><span>Note 2:</span><span> </span><span>For information regarding a repair method approved by the </span><span>Manager, </span><span>Atlanta</span><span> ACO contact your area Gulfstream Field Service Representative.</span></p></td></tr><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span></span></p></td><td colspan="3" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p class="Note"><span>Note 3:</span><span> </span><span>FAA AD 2006-18-13 Amdt 39-14752 refers.</span></p></td></tr><tr style="height:0pt"><td style="width:85.05pt"></td><td style="width:111.7pt"></td><td style="width:100.9pt"></td><td style="width:212.65pt"></td></tr></tbody></table>