EFTA00620791

(itiiiktrearn Technical Bulletins Report Filters: G-CGUL MYCMP Log Date - 08 Nov 2014 Analyst: Gar Leaver TYPE: ALL CW Status: ALL Current TT 3466.5 Current Lndgs 953 Phone. FA)4 Phone: Current Hr Mtr 3423.6 COMPONENT TIMES Aircraft Make Gulfstream Position Logbook Description Serial Number Total Time Total Cycles TSO CSO Aircraft Model G550 1 Engine Rolls Royce BR700.710C4.11 15455 3466.5 953 (G550) Aircraft Serial No. 5176 2 Engine Rolls Royce BR700.710C4.11 15456 3466.5 953 Airworthiness 26 Nov 2007 (G550) Date 1 APU Honeywell RE220 (G550) P-503 2044.5 0 Regulation ELI-EASA TYP C/W Source Code Description Effectivity IATAI Status Logbook Work Order HRS LDG Date C/I MM REF M HRS aintenance Notes Cert No HYDRAULIC REPLENISHING gs Itn MAN CM 1012.1 326 19 Feb 2010 C 0.00 Airframe 299999 SYSTEM INOPERATIVE Mx. Notes: Hyd replenisher replaced by GS LTN Defect closed 441200 SB GPECSB50001 Cabin System 5365, 5381. 5385 OPT 26 Jan 2013 I Airframe Level E Firmware Update Cabin service bulletin 449002 GCMS SIB 002 Cabin System This Cabin Service OPT 08 Aug 2013 I Airframe Firmware Update 1.9.1 Bulletin is applicable to aircraft with GCMS controller firmware version 1.8.4 installed or later approved version. G-CGUL G550 5176 Technical Bulletins Page 1 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620791 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date C/I MM REF M HRS aintenance Notes Cert No GCMS SB 003 Cabin System This Cabin Service 449003 OPT 13 Sep 2013 I Airframe Firmware Update 4.4.3.3 Bulletin is applicable to aircraft with AC firmware version 4.4.1 installed or later approved version. Serial number effectivity includes 5365, 5381, 5385, 5394, 5395, 5400, 5407 and 5418. Final Phase Production cut- in starts with serial number 5424. CSB 003A • Advanced Cabin Server This Cabin Service 449004 23 OPT 21 Feb 2014 Airframe (ACS) System Firmware Update Bulletin revision 4A.3.3 supersedes CSB 003 Rev. — and Rev A is now re-issued as CSB 003A Rev. B. Aircraft having complied with CSB 003 will only accomplish Preferred Method Steps A.9 through A.17 or Alternate Method Steps B.28 through B.32, Return to Service testing and Service . Serial number effectivity includes 5365, 5381. 5385. 5394, 5395, 5400. 5407, 5418 and sub. with firmware ver. 4.4.1 or later version. G-CGUL G550 5176 Technical Bulletins Page 2 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620792 i T YP CNV Source Code Description Effectivity ATA Status ill oebook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No CSB 002B CPBC Software Installation Effectivity: This Cabin 449202 OPT 11 Dec 2013 I Airframe Instructions Service Bulletin is applicable to aircraft with GCMS controller firmware version 1.8.4 installed or later approved version. Serial number effectivity includes 5365, 5381. 5385. 5394, 5395, 5400. 5407, 5418 and 5424 Final Phase Production cut•in starts with serial number 5426 and Sub. 24 month compliance is for Warranty at Gutfstream G650 Authorized Warranty Facility. ASB BR700.72•A900297 High » Closed by Rev 1. C 880041 CAN CAN 0.0 0 22 May 2014 0.00 Engine 1 Pressure Compressor Fairings - 21 May 2014« Inspection of Upper Left HP Effectivity: Eng SIN Compressor Fairing 15887 • 15899. This SB must be accomplished on the affected eng within 500 flight hours after receipt of this SB. For eng SIN 15887 • 15891 only. it is recommended that this SB is accomplished at the same time as SB 72-A900298. Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link G-CGUL G550 5176 Technical Bulletins Page 3 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620793 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No 880041 ASB BR700.72•A900297 High »Closed by Rev 1. CAN CAN 0.0 0 22 May 2014 C 0.00 Engine 2 (890041) Pressure Compressor Fairings - 21 May 2014 « Inspection of Upper Leh HP Effectivity: Eng S/N Compressor Fairing 15887 • 15899. This SB must be accomplished on the affected eng within 500 flight hours after receipt of this SB. II For eng S/N 15887 15891 only, it is recommended that this SB is accomplished at the same time as SB 72-A900298. Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link ASB BR700.72-A900298 Engine » Closed by Rev 1. C 880042 CAN CAN 0.0 0 22 May 2014 0.00 Engine 1 Combustion Fairings • Replacement 21 May 2014 « of Non.Confonning Upper Left. Upper Effectivity: Eng S/N Right and Lower Right Combustion 15887 • 15891. This Section Fairings SB must be accomplished on the affected eng within 500 flight hours after receipt of this SB. II It is recommended that this SB is accomplished at the same time as SB 72. A900297. Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link 880042 ASB BR700.72-A900298 Engine » Closed by Rev 1. C CAN CAN 0.0 0 22 May 2014 0.00 Engine 2 (890042) Combustion Fairings • Replacement 21 May 2014 « of Non-Conforming Upper Left. Upper Effectivity: Eng S/N Right and Lower Right Combustion 15887 • 15891. This Section Fairings SB must be accomplished on the affected eng within 500 flight hours after receipt of this SB. II It is recommended that this SB is accomplished al the same time as SB 72. A900297. Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link G-CGUL G550 5176 Technical Bulletins Page 4 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620794 L TYP C/W Source Code Description Effectivity ATA Status ii _ogbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No ASB BR700.72-A900497 TLM It is recommended this 880043 REC CM 1007.8 325 14 Feb 2010 C 0.00 Engine 1 Decrease Lives of HP Turbine Discs SIB be accomplished on all engines before 2 -28-10 Mx. Notes: lives amended as per sb 880043 ASB BR700.72-A900497 TLM It is recommended this REC 1007.8 325 14 Feb 2010 C 0.00 Engine 2 (890043) Decrease Lives of HP Turbine Discs SiB be accomplished on all engines before 2 -28-10 Mx. Notes: lives amended as per sb 880044 ASB BR700.72-A900504 Change of It is recommended this INF CM 1114.2 352 06 Apr 2010 C 0.00 Engine 1 Life Counting Method for Touch-and- SiB be accomplished Go and Overshoot on all engines before 7 -31.10 880044 ASB BR700.72-A900504 Change of It is recommended this INF CM 1114.2 352 06 Apr 2010 C 0.00 Engine 2 (890044) Life Counting Method for Touch-and- SIB be accomplished Go and Overshoot on all engines before 7 -31.10 SB BR700.72-900517 LP Compressor 710A1.10 sin 11275 880045 REC 25 Jan 2011 Engine 1 Annulus Fillers DFL and 11276 w/ SB- BR700.72-101699. 710C4.11 s/n 15129. 15179. 15180. 15181. 15413. 15425 wf SB- BR700.72-101699. 880121 SB BR700-77-101875 - N2 Speed Effectivity: BR700- 77 REC 03 Jul 2014 Engine 1 Probes - Introduction of New 710C4.11 Engines Attaching Bolts with Shorter Length prior to Engine Serial Number 16074. which have the Service Bulletin SB-BR700.72- 101588 standard incorporated. Compliance - RECOMMENDED It is recommended that this Service Bulletin be accomplished on engines when the engine or module is disassembled for refurbishment or overhaul. G-CGUL G550 5176 Technical Bulletins Page 5 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620795 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LDG Date CA MM REF M HRS aintenance Notes Cert No 880121 SB BR700.77-101875 • N2 Speed Effectivity: BR700- 77 REC 03 Jul 2014 Engine 2 (890121) Probes • Introduction of New 710G4-11 Engines Attaching Botts with Shorter Length prior to Engine Serial Number 16074. which have the Service Bulletin SB-BR700-72- 101588 standard incorporated. Compliance - RECOMMENDED It Is recommended that this Service Bulletin be accomplished on engines when the engine or module is disassembled for refurbishment or overhaul. Alert SB BR700.72-A900509 BR700.710A1•10 0 880200 CAN CAN 0.0 15 Mar 2012 C 0.00 Engine 1 Replacement of the Fuel Pump Engines.Modules M61. Splined Coupling 148. M61.158. M61- 162. M61.168. M61- 169. M61.176. M61- 179. M61.184. M61- 188, M61.190. M61- 195, M61.196. M61- 197 and M61.203. BR700.710C4.11 Engines. (a) For engines which have hfw config standard 71004.11 engraved on data plate (SB-BR700.72-101466 standard not 'acorn). Modules M61.187 and M61.205 (AccesGearbox Module). (b) For eng which have hfw config 710C4- 11/10 engraved on data plate SB•BR700- 72-101466 incorp. Module M61.202 Ganz see revl 890300 G-CGUL G550 5176 Technical Bulletins Page 6 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620796 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No 880200 Alert SB BR700.72-A900509 BR700.710A1-10 CAN CAN 0.0 0 15 Mar 2012 C 0.00 Engine 2 (890200) Replacement of the Fuel Pump Engines.Modules M61. Splined Coupling 148. M61.I58. M61- 162. M61.168. M61- 169. M61.176. M61- 179. M61.184. M61- 188. M61.190. M61- 195, M61.196. M61- 197 and M61.203. BR700.710C4.l1 Engines. (a) For engines which have h/w config standard 7100441 engraved on data plate (SB-BR700.72-101466 standard not incorp). Modules M61.187 and M61.205 (AccesGearbox Module). (b) For eng which have hive config 710C4- 11/10 engraved on data plate SB.BR700- 72-101466 incorp. Module M61.202 Canx see rev1 890300 SB BR700.72.100981 • LP Impact Effectivity: Prior to 880237 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Adhesive And Filler Engines SN 15133 880237 SB BR700.72.100981 • LP Impact Effectivity: Prior to 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890237) Adhesive And Filler Engines SN 15133 880271 SB BR700-72.101144 • Combustion Effectivity: BR700• 72 INF N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Inner Case And Vanes 710A1.I0 Engines / Prior to Engine Serial Number 11498 // BR700.710C4.// Engines / Prior to Engine Serial Number 15113 and Engine Serial Numbers 15114 and 15115 G-CGUL G55O 5176 Technical Bulletins Page 7 of 164 20 Jan 2015 02015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620797 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No 880271 SB BR700.72.101144 • Combustion Effectivity: BR700- 72 INF NIA 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890271) Inner Case And Vanes 710A1.10 Engines/ Prior to Engine Serial Number 11498 // BR700.710C4.11 Engines / Prior to Engine Serial Number 15113 and Engine Serial Numbers 15114 and 15115 SB BR700.72.101173 • LP / HP NOTE: Prior to Engine 880276 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Turbine Stator Retainer / Seals Serial Number 15189 880276 SB BR700.72.101173 • LP / HP NOTE: Prior to Engine 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890276) Turbine Stator Retainer / Seals Serial Number 15189 SB BR700.72.101195 • Intermediate NOTE: Prior to Engine 72 OPT 14 Dec 2010 I Engine 1 880285 Compressor Case Serial Number 15129, 15130 thru 15141, 15145. 15147 thru 15150. 15154 thru 15159. 15162 thru 15195, 15200 thru 15228 and 15231 onwards 880285 SB BR700-72.101195 • Intermediate NOTE: Prior to Engine I 72 OPT la Dec 2010 Engine 2 (890285) Compressor Case Serial Number 15129, 15130 thru 15141, 15145, 15147 thru 15150, 15154 thru 15159, 15162 thru 15195, 15200 thru 15228 and 15231 onwards SB BR700•72•101203 • HPC Variable NOTE: Prior to Engine 72 OPT 880287 . NA 0.0 0 26 Nov 2007 C 0.00 Engine 1 Guide Vanes Actuating Mechanism Serial Number 15124 880287 SB BR700.72.101203 • HPC Variable NOTE: Prior to Engine 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890287) Guide Vanes Actuating Mechanism Serial Number 15124 SB BR700.72.101246 • New LP NOTE: Prior to Engine 880296 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Compressor Disc Serial Number 15178 G-CGUL G550 5176 Technical Bulletins Page 8 of 164 20 Jan 2015 ®2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620798 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No 880296 SB BR700.72-101246 - New LP NOTE: Prior to Engine (890296) 72 OPT NIA 0.0 0 26 Nov 2007 C 0.00 Engine 2 Compressor Disc Serial Number 15178 880301 Alert SB BR700-72-A900509 Revision I of this Non- CAN CAN 0.0 0 26 Jun 2012 C 0.00 Engine 1 (Revision 1) Replacement of the Fuel Modification Service Pump Splined Coupling Bulletin has been issued to change the Manpower from 4 hours to 10 hours and to include the old standard of fuel pump splined coupling. PIN BRR52639. Superceded see revision 2 - code 880307 880301 Alert SB BR700-72-A900509 Revision 1 of this Non- CAN CAN 0.0 0 26 Jun 2012 C 0.00 Engine 2 (890301) (Revision 1) Replacement of the Fuel Modification Service Pump Splined Coupling Bulletin has been issued to change the Manpower from 4 hours to 10 hours and to include the old standard of fuel pump splined coupling. PIN BRR52639. Superceded see revision 2 - code 880307 880302 SB BR700-73-101376 - Combination 73 REC 16 Jul 2002 Engine 1 Of EEC Hardware Standard 880302 SB BR700.73-101376 - Combination 73 REC 16 Jul 2002 Engine 2 (890302) Of EEC Hardware Standard G-CGUL G550 5176 Technical Bulletins Page 9 of 164 20 Jan 2015 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620799 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No SB BR700.73-101380 - Introduction Effectivity: BR700- 880303 73 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 of an EED with a New Hardware 710C4.11 Engines / Standard For engines which have hardware configuration standard 710C4.11 or 710C4- 11/10 engraved on the engine data plate (Service Bulletin R SB- BR700.72-101466 standard not incorporated). Prior to Engine Serial Number 15105. Orig Issue: 08/09/2002 / Rev 1: 09/11/2002 880303 SB 6R70073-101380 - Introduction Effectivity: BR700- 73 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890303) of an EED with a New Hardware 710O4-11 Engines / Standard For engines which have hardware configuration standard 710C4.11 or 710C4- 11/10 engraved on the engine data plate (Service Bulletin R SB- BR700.72-101466 standard not incorporated). Prior to Engine Serial Number 15105. Orig Issue: 08/09/2002 / Rev 1: 09/11/2002 SB BR700.73-101386 - Fuel Manifold NOTE: Prior to Engine 880304 73 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Damper Wire Serial Number 15181 and from Engine Serial Number 15194 to 15254 880304 SB BR700.73-101386 - Fuel Manifold NOTE: Prior to Engine 73 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890304) Damper Wire Serial Number 15181 and from Engine Serial Number 15194 to 15254 G-CGUL G550 5176 Technical Bulletins Page 10 of 164 20 Jan 2015 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620800 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No SB BR700•73.101400 • EEC with Effectivity: Prior to 1 880305 73 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine S2.1 Software Standard Engine Serial Number 15166 880305 SB BR700•73.101400 • EEC with Effectivity: Prior to 73 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890305) S2.1 Software Standard Engine Serial Number 15166 SB BR700•73.101558 (Rev 1) • Fuel NOTE: For engines 8803 73 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 06 Flow Transmitter prior to Engine Serial Number 15328 which do not have the Service Bulletin SB. BR700.73.101496 standard incorporated 880306 SB BR700.73.101558 (Rev 1) • Fuel NOTE: For engines 73 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890306) Flow Transmitter prior to Engine Serial Number 15328 which do not have the Service Bulletin SB. BR700.73.101496 standard incorporated Alert SB BR700.72.A900509 Revision 2 of this Non. 880307 CAN CAN 0.0 0 26 Jun 2012 C 0.00 Engine 1 (Revision 2) Replacement of the Fuel Modification Service Pump Splined Coupling Bulletin has been issued to revise the Effectivity, to make the NomModification Service Bulletin applicable for all engines. PM BRR52639. See s/b for due time requirement. Cancelled see revision 3 CMP 880309 G-CGUL G550 5176 Technical Bulletins Page 11 of 164 20 Jan 2015 Ce 2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620801 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No 880307 Alert SB BR700.72-A900509 Revision 2 of this Non- CAN CAN 0.0 0 26 Jun 2012 C 0.00 Engine 2 (890307) (Revision 2) Replacement of the Fuel Modification Service Pump Splined Coupling Bulletin has been issued to revise the Effectivity. to make the Non-Modification Service Bulletin applicable for all engines. P/N BRR52639. See s/b for due time requirement. Cancelled see revision 3 CMP 880309 SB BR700-73-101438 External Fuel NOTE: Prior to Engine 73 CAN N/A 880308 0.0 0 26 Nov 2007 C 0.00 Engine 1 System Air TubesiFittings Serial Number 15404 880308 SB BR700.73-101438 External Fuel NOTE: Prior to Engine 73 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890308) System Air TubesiFittings Serial Number 15404 Alert SB BR700.72-A900509 Revision 3 of this Non- GAC LTN 880309 72 CAN CPN 3029.7 875 26 Sep 2013 C Engine 1 (Revision 3) Replacement of the Fuel Modification Service BMX000258 Pump Splined Coupling Bulletin has been issued to delete the requirement to return the removed fuel pump splined coupling to Rolls-Royce Deutschland. Service Enginesting.P/N BRR52639. See s/b for due time requirement. Cancelled See code 880311(890311). UK.145.00883 G-CGUL G550 5176 Technical Bulletins Page 12 of 164 20 Jan 2015 €12015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620802 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No 880309 Alert SB BR700.72•A900509 Revision 3 of this Non- GAC LTN 72 CAN CPAr 3029.7 875 26 Sep 2013 C Engine 2 (890309) (Revision 3) Replacement of the Fuel Modification Service BMX000258 Pump Splined Coupling Bulletin has been issued to delete the requirement to return the removed fuel pump spieled coupling to Rolls-Royce Deutschland, Service Engineering.P/N BRR52639. See sib for due time requirement. Cancelled - See code 880311(890311). UK.145.00883 Alert SB BR700-72-A900509 Revision 4 has been 880311 72 MAN 25 Aug 2014 I Engine 1 (Revision 4) Replacement of the Fuel issued to update the Pump Splined Coupling Effectivity to reflect that engines which have Service Bulletin SB-BR700-73-101833 standard incorporated are no longer affected. See s/b for due time requirement.. 880311 Alert SB BR700.72-A900509 Revision 4 has been 72 MAN 25 Aug 2014 I Engine 2 (890311) (Revision 4) Replacement of the Fuel issued to update the Pump Splined Coupling Effectivity to reflect that engines which have Service Bulletin SB-BR700-73-101833 standard incorporated are no longer affected. See s/b for due time requirement.. 880312 SB BR700.73-101833R2 • Effectivity: See SB. 73 REC 25 Aug 2014 I Engine 1 Introduction of a Revised Drive Shaft Compliance: Connection for the Fuel Pump RECOMMENDED It is recommended that this Service Bulletin be accomplished on engines at the next engine shop visit maintenance opportunity. G-CGUL G550 5176 Technical Bulletins Page 13 of 164 20 Jan 2015 KO 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620803 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No SB BR700-73.101496 - Engine See Revision 1 - CMP 880312 73 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Electronic Controller Code 880313 / 890313 880312 SB BR700.73.101496 • Engine See Revision 1 • CMP 73 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890312) Electronic Controller Code 880313 / 890313 880312 SB BR700-73.101833R2 Effectivity: See SB. 73 REC 25 Aug 2014 I Engine 2 (890312) Introduction of a Revised Drive Shaft Compliance: Connection for the Fuel Pump RECOMMENDED It is recommended that this Service Bulletin be accomplished on engines at the next engine shop visit maintenance opportunity. 880316 SB BR700.73.101558 - Fuel Flow NOTE: For engines 73 OPT 09 Nov 2007 I Engine 1 Transmitter (FFT) prior to Engine Serial Number 15328 which do not have the Service Bulletin SB- BR700.73.101496 standard Incorporated 880316 SB BR700-73.101558 • Fuel Flow NOTE: For engines 73 OPT 09 Nov 2007 I Engine 2 (890316) Transmitter (FFT) prior to Engine Serial Number 15328 which do not have the Service Bulletin SB- BR700.73.101496 standard Incorporated SB BR700-73.101590 - EEC With Also see ASC 058 880317 73 REC 19 Mar 2007 I Engine 1 S3A Software (970580). 880317 SB 8R700-73.101590 - EEC With Also see ASC 058 73 REC 19 Mar 2007 I Engine 2 (890317) S3.4 Software (970580). SB BR700.73.101617 • Fuel Flow NOTE: Prior to Engine 880318 73 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Transmitter Serial Number 15423. Cancelled ref rev 1 880322 G-CGUL G550 5176 Technical Bulletins Page 14 of 164 20 Jan 2015 492015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620804 TYP CNV Source Logbook Code Description Effectivity ATA Status Work Order HRS LOG Date c/I MM REF M HRS aintenance Notes Cert No 880318 SB BR700•73.101617 - Fuel Flow NOTE: Prior to Engine 73 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890318) Transmitter Serial Number 15423. Cancelled ref rev 1 880322 SB BR700.73.900463 • Removal of EFF: For engines 880319 73 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine EEC For C-15 Capacitor Replacement which have an Engine Electronic Controller (EEC) with the part number EECU3000• 02AD and with one of the serial numbers listed the bulletin. 880319 SB BR700-73•900463 • Removal of EFF: For engines 73 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890319) EEC For C-15 Capacitor Replacement which have an Engine Electronic Controller (EEC) with the part number EECU3000. 02AD and with one of the serial numbers listed the bulletin. 880320 SB BR700.73-900423 - One Time It is recommended that CAN CAN 0.0 0 09 Sep 2014 C 0.00 Engine 1 Inspection Of EEC Firebox Assembly this Non•Modification For Paint Damage Service Bulletin be ocomplished on engines at the next aircraft scheduled maintenance A•Check. If the inspection of the EEC firebox assembly results in the requirement to reject the EEC firebox assembly, record a notice in the engine log book and activate code 880321(890321). The notice must include the information to permit a 500 hours fipon allowance before the EEC firebox assembly is replaced. » Cancelled - See 880324(890324) cc Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link G-CGUL G550 5176 Technical Bulletins Page 15 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620805 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date c/I MM REF M HRS aintenance Notes Cert No 880320 SB BR700•73•900423 • One Time It is recommended that CAN CAN 0.0 0 09 Sep 2014 C 0.00 Engine 2 (890320) Inspection Of EEC Firebox Assembly this Non-Modification For Paint Damage Service Bulletin be ocomplished on engines at the next aircraft scheduled maintenance A-Check. II the inspection of the EEC firebox assembly results in the requirement to reject the EEC firebox assembly, record a notice in the engine log book and activate code 880321(890321). The notice must include the information to permit a 500 hours fly-on allowance before the EEC firebox assembly is replaced. » Cancelled - See 880324(890324) « Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link SB BR700.73-900423R1 -One Time It is recommended that 880324 73 REC 09 Sep 2014 Engine 1 Inspection Of EEC Firebox Assembly this Non•Modification For Paint Damage Service Bulletin be accomplished on engines at the next aircraft scheduled maintenance A•Check. II the inspection of the EEC firebox assembly results in the requirement to reject the EEC firebox assembly, record a notice in the engine log book and activate code 880321(890321). The notice must include the information to permit a 500 hours fty-on allowance before the EEC firebox assembly is replaced. G-CGUL G550 5176 Technical Bulletins Page 16 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620806 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No 880324 SB BR700-73.900423Rt - One Time It is recommended that 73 REG 09 Sep 2014 I Engine 2 (890324) Inspection Of EEC Firebox Assembly this Non-Modification For Paint Damage Service Bulletin be accomplished on engines at the next aircraft scheduled maintenance A-Checic II the inspection of the EEC firebox assembly results in the requirement to reject the EEC firebox assembly, record a notice in the engine log book and activate code 880321(890321). The notice must include the information to permit a 500 hours Ity-on allowance before the EEC firebox assembly is replaced. Alert SB 8R70072-A900509 Revision 4 has been 880339 72 MAN 25 Aug 2014 I Engine 1 (Revision 4) Replacement of the Fuel issued to update the Pump Splined Coupling Effectivity to reflect that engines which have Service Bulletin SB-BR700-73-101833 standard incorporated are no longer affected. See sib for due time requirement. Mx. Notes: CAN PER REV 3 880339 Alert SB BR700.72-A900509 Revision 4 has been 72 MAN 25 Aug 2014 I Engine 2 (890339) (Revision 4) Replacement of the Fuel issued to update the Pump Splined Coupling Effectivity to reflect that engines which have Service Bulletin SB-BR700-73-101833 standard incorporated are no longer affected. See s/b for due time requirement. Mx. Notes. cm PER REV 3 G-CGUL G550 5176 Technical Bulletins Page 17 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620807 TYP C/W Source Code Description Effectivity ATA Status Logbook Work Order HRS LDG Date C/I MM REF M HRS aintenance Notes Cert No SB BR700.73-101833R2 Effectivity: See SB. I 880340 73 REC 25 Aug 2014 Engine 1 Introduction of a Revised Drive Shaft Compliance: Connection for the Fuel Pump RECOMMENDED It is recommended that this Service Bulletin be accomplished on engines at the next engine shop visit maintenance opportunity. 880340 SB BR700.73-101833R2 - Effectivity: See SB. 73 REC 25 Aug 2014 I Engine 2 (890340) Introduction of a Revised Drive Shaft Compliance: Connection for the Fuel Pump RECOMMENDED It is recommended that this Service Bulletin be accomplished on engines at the next engine shop visit maintenance opportunity. 880414 SB 6R700-72-101349 - Fuel Shutoff NOTE: Prior to Engine 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Cable Serial Number 15109 880414 SB BR700.72-101349 - Fuel Shutoff NOTE: Prior to Engine 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890414) Cable Serial Number 15109 SB BR700.72-101414 - HPC Front Effectivity: Prior to 880422 72 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Case - New Coated Brushes Engine Serial Number 15146 880422 SB BR700.72-101414 - HPC Front Effectivity: Prior to 72 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890422) Case - New Coated Brushes Engine Serial Number 15146 SB 6R700.72-101416 - Accessory Effectivity: Prior to 880423 71 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Gearbox Line 12 Spacer Engine Serial Number 15135 880423 SB BR700.72-101416 - Accessory Effectivity: Prior to 71 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890423) Gearbox Line 12 Spacer Engine Serial Number 15135 G-CGUL G550 5176 Technical Bulletins Page 18 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620808 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No SB BR700.72.101419 • HPC VIGV NOTE: Prior to Engine 880425 72 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Actuating Mechanism Serial Number 15148 880425 SB BR700•72•101419 • HPC VIGV NOTE: Prior to Engine 72 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890425) Actuating Mechanism Serial Number 15148 SB BR700.72.101421 • LP Turbine Effectivity: Engines 880427 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Stage Nozzle Guide Seals Prior to Serial Number 15189 880427 SB BR700.72.101421 • LP Turbine Effectivity: Engines 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890427) Stage Nozzle Guide Seals Prior to Serial Number 15189 SB BR700.72.101431 HP Turbine EFF: BR700.710A1-10 880428 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Stage 1 Nozzle Guide Seals engines (GV) prior to engine SN 11506/ BR700.710C4- 11engines (G500/G550) prior to engine SN 15277. 880428 SB BR700.72.101431 HP Turbine EFF: BR700.710A1.10 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890428) Stage 1 Nozzle Guide Seals engines (GV) prior to engine SN 11506 / BR700.710C4- 11engines (G500/G550) prior to engine SN 15277. SB BR700•72•101460 LP Comp Trim 880435 Effectivity: All 72 OPT 28 Apr 2004 Engine 1 Balance Weights 880435 SB BR700.72.101460 LP Comp Trim Effectivity: All 72 OPT 28 Apr 2004 Engine 2 (880435) Balance Weights SB BR700.72.101463 • Engine HP GV: Prior to Engine 880437 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Compressor Rear Inner Case Serial Number 11505 ft G500/ G550: Prior to Engine Serial Number 15229 G-CGUL G550 5176 Technical Bulletins Page 19 of 164 20 Jan 2015 @2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620809 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No 880437 SB BR700.72-101463 - Engine HP GV: Prior to Engine 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890437) Compressor Rear Inner Case Serial Number 11505 if G500/ G550: Prior to Engine Serial Number 15229 880439 SB 6R700-72-101471 - Metco 58 NOTE: Prior to Engine 72 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Coated LP Compressor Blades Serial Number 15214 880439 SB BR700.72-101471 - Metco 58 NOTE: Prior to Engine 72 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890439) Coated LP Compressor Blades Serial Number 15214 880441 SB BR700.72-101474 - Laser Shock »Cancelled See 72 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Peened LP Compressor Rotor Disc Code 880581(890581) 880441 SB BR700.72-101474 - Laser Shock »Cancelled See 72 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890441) Peened LP Compressor Rotor Disc Code 880581(890581) SB BR700-72-101540 - Outlet Guide Effectivity: Prior to 880453 72 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Vane Housing Assembly engine SN 15390 and from engine SN 15411 to 15416. Cancelled ref revision 2 880462 880453 SB BR700.72-101540 - Outlet Guide Effectivity: Prior to (690453) 72 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 Vane Housing Assembly engine SN 15390 and from engine SN 15411 to 15416. Cancelled ref revision 2 880462 880454 SB BR700.72-101548 - LP NOTE: Prior to Engine 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Compressor Case Serial Number 15390 880454 SB BR700.72-101548 - LP NOTE: Prior to Engine (890454) 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 Compressor Case Serial Number 15390 880456 SB BR700.72-101550 - Breather NOTE: Prior to Engine 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Filter. Cover. Tank Covers Serial Number 15360 880456 SB BR700.72-101550 - Breather NOTE: Prior to Engine 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890456) Filter. Cover. Tank Covers Serial Number 15360 G-CGUL G550 5176 Technical Bulletins Page 20 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620810 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No SB BR700.72-101588 - Accesssory NOTE: Prior to Engine 880458 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Gearbox Module Main Housing Serial Number 15410 and for Engine Serial Numbers 15412 to 15417 880458 SB BR700.72-101588 - Accesssory NOTE: Prior to Engine 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890458) Gearbox Module Main Housing Serial Number 15410 and for Engine Serial Numbers 15412 to 15417 SB BR700.72-101618 - Accessory NOTE: Prior to Engine 880460 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Gearbox Oil Tank Fill Serial Number 15443 880460 SB BR700.72-101618 - Accessory NOTE: Prior to Engine 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890460) Gearbox Oil Tank Fill Serial Number 15443 880461 SB BR700.72-101622 - Lubriclone Effectivity: Prior to 72 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 For The Accessory Gearbox engine SN 15446. 880461 SB BR700.72-101622 - Lubriclone Effectivity: Prior to (890461) For The Accessory Gearbox 72 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 engine SN 15446. SB BR700.72-900341 HP Module M33.120 (HP 72 880562 REC 10 Feb 2005 I Engine 1 Compressor Blades Baroscope Compressor Module). 880562 SB BR700.72-900341 HP Module M33.120 (HP 72 REC 10 Feb 2005 I Engine 2 (890562) Compressor Blades Borescope Compressor Module). SB BR700.72-900409 - LP Eff: All BR700.71A I - 880567 72 REC 19 Sep 2006 I Engine 1 Compressor Case 10 Engines and All BR700-710C4 -11 Engines 880567 SB BR700.72-900409 - LP Eff: All BR700.71A1- 72 REC 19 Sep 2006 I Engine 2 (890567) Compressor Case 10 Engines and All BR700-710C4 -11 Engines SB BR700.72-101410 - HP NOTE: Prior to Engine 880572 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Alternative Part Number For HP Serial Number 15134 Turbine G-CGUL G550 5176 Technical Bulletins Page 21 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620811 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date Cd MM REF M HRS aintenance Notes Cert No 880572 SB BR700•72•101410 • HP NOTE: Prior to Engine 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890572) Alternative Part Number For HP Serial Number 15134 Turbine SB BR700.72.101620 • Accessory NOTE: For engines 880575 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine I Gearbox Module which have hardware configuration standard 710C4•11 engraved on the engine data plate 880575 SB BR700.72.101620 • Accessory NOTE: For engines 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890575) Gearbox Module which have hardware configuration standard 710C4•11 engraved on the engine data plate 880579 SB BR700.72.900369 • HPT1, NGV & NOTE: See Bulletin 72 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine I CRIC Borescope for Effectivity If Part 1 is to accomplished within the next 50 flight hours after receipt. Part 2 is to be accomplished within 150 flight hours of Pal 1. Part 3 is to be accomplished within 500 flight hours of Pal 1. 880579 SB BR700.72.900369 • HPT1, NGV & NOTE: See Bulletin 72 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890579) CRIC Borescope for Effectivity //Part 1 is to accomplished within the next 50 flight hours after receipt. Part 2 is to be accomplished within 150 flight hours of Pal 1. Part 3 is to be accomplished within 500 flight hours of Pal 1. SB BR700.72.101474R1 - Laser 880581 72 REC 18 Nov 2014 Engine I Shock Peened LP Compressor Rotor Disc G-CGUL G550 5176 Technical Bulletins Page 22 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620812 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date c/I MM REF M HRS aintenance Notes Cert No 880581 SB BR700-72.101474R1 - Laser 72 REC 18 Nov 2014 I Engine 2 (890581) Shock Peened LP Compressor Rotor Disc SB BR700.72.900521 (Pal A) Rev 2 The serial numbers of 880589 CAN CM 0.0 0 13 Jul 2011 C 0.00 Engine 1 Inspection - LP Compressor Annulus the affected LP Fillers compressor annulus fillers with the part numbers BRR40995. BRR19433, and BRR22626 are in the range from 00001 to 65237. It is recommended that PART A of this Non• Modification Service Bulletin be accomplished on all engines prior to or at the next A-check. This inspection is not applicable for p/n FW77117. Cancelled see rev 3. 880602 Mx. Notes: see code 880591 880589 SB BR700.72.900521 (Part A) Rev 2 • The serial numbers of CAN CM 0.0 0 13 Jul 2011 C 0.00 Engine 2 (890589) Inspection - LP Compressor Annulus the affected LP Fillers compressor annulus fillers with the part numbers BRR40995. BRR19433, and BRR22626 are in the range from 00001 to 65237. It is recommended that PART A of this Non• Modification Service Bulletin be accomplished on all engines prior to or at the next A-check. This inspection is not applicable for p/n FW77117. Cancelled see rev 3.880602 Mx. Notes: see code 890591 G-CGUL G550 5176 Technical Bulletins Page 23 of 164 20 Jan 2015 @ 2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620813 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No SB BR700.72.900521 (Pan B) Rev 2 • The serial numbers of GAC•LTN 880590 CAN CAN 2354.6 711 19 Apr 2012 C Engine 1 Inspection - LP Compressor Annulus the affected LP FL016471 Fillers compressor annulus fillers with the part numbers BRR40995. BRR19433, and BRR22626 are in the range from 00001 to 65237. It Is recommended that PART B of this Non• Modification Service Bulletin be accomplished on all engines prior to or at the next A-check and be repeated once within a further 500 +1- 50 flight hours. This inspection is not applicable for p/n FW77117. cancelled see rev 3. 880603 Mx. Notes: see code 880592 UK.145.00883 880590 SB BR700.72.900521 (Pan B) Rev 2 • The serial numbers of GAC•LTN (890590) CAN CAN 2354.6 711 19 Apr 2012 C Engine 2 Inspection - LP Compressor Annulus the affected LP FL016471 Fillers compressor annulus fillers with the pan numbers BRR40995. BRR19433, and BRR22626 are In the range from 00001 to 65237. It Is recommended that PART B of this Non• Modification Service Bulletin be accomplished on all engines prior to or at the next A-check and be repeated once within a further 500 +1- 50 flight hours. This inspection is not applicable for pin FW77117. cancelled see rev 3.880603 UK.145.00883 G-CGUL G550 5176 Technical Bulletins Page 24 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620814 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No SB BR700.72-900521 (Part A) Rev 1- The serial numbers of GAC LTN 880591 CAN CAN 2047.8 610 13 Jul 2011 C Engine 1 Inspection LP Compressor Annulus the affected LP FLO15395 Fillers compressor annulus fillers with the pan numbers BRR40995. BRR19433 and BRR22626 are in the range from 00001 to 65237. It is recommended that PART A of this Non- Modification Service Bulletin be accomplished on all engines prior to or at the next A-check. Cancelled see revision 2 Mx. Notes: set to code 723103 UK.145.00883 880591 SB BR700-72-900521 (Part A) Rev I The serial numbers of GAC LTN CAN CPN 2047.8 610 13 Jul 2011 C Engine 2 (890591) Inspection LP Compressor Annulus the affected LP FLO15395 Fillers compressor annulus fillers with the pan numbers BRR40995. BRR 19433 and BRR22626 are in the range from 00001 to 65237. II is recommended that PART A of this Non- Modification Service Bulletin be accomplished on all engines prior to or at the next A-check. Cancelled see revision 2 Mx. Notes: set to code 723103 UK.145.00883 G-CGUL G550 5176 Technical Bulletins Page 25 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620815 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No SB BR700.72.900521 (Part B) Rev 1- The serial numbers of GAC LTN 880592 CAN Cm 2047.8 610 15 Jul 2011 C Engine 1 Inspection - LP Compressor Annulus the affected LP FL015395 Fillers compressor annulus fillers with the part numbers BRR40995. BRR19433 and BRR22626 are in the range from 00001 to 65237. It Is recommended that PART B of this Non. Modification Service Bulletin be accomplished on all engines prior to or at the next A-check and be repeated once within a further 500 +1- 50 flight hours. Cancelled see revision 2 Mx. Notes: set to code 723103 UK.145.00883 880592 SB BR700.72.900521 (Part B) Rev 1- The serial numbers of GAC LTN CAN CAN 2047.8 610 15 Jul 2011 C Engine 2 (890592) Inspection - LP Compressor Annulus the affected LP FL015395 Fillers compressor annulus fillers with the part numbers BRR40995. BRR19433 and BRR22626 are in the range from 00001 to 65237. It Is recommended that PART B of this Non- Modification Service Bulletin be accomplished on all engines prior to or at the next A-check and be repeated once within a further 500 +1- 50 flight hours. Cancelled see revision 2 Mx. Notes: set to code 723103 UK.145.00883 G-CGUL G550 5176 Technical Bulletins Page 26 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620816 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No SB BR700.72.900521 (Part A) Visual The serial numbers of 880596 CAN CAN 0.0 0 17 May 2011 C 0.00 Engine 1 Inspection - LP Compressor Annulus the affected LP Fillers compressor annulus fillers with the part numbers BRR40995. BRR19433 and BRR22626 are in the range from 00001 to 65237. It Is recommended that PART A of this Non. Modification Service Bulletin be accomplished on all engines prior to or at the next scheduled maintenance opportunity. Cancelled see 880591 880596 SB BR700-72.900521 (Part A) Visual The serial numbers of CAN CAN 0.0 0 17 May 2011 C 0.00 Engine 2 (890596) Inspection • LP Compressor Annulus the affected LP Fillers compressor annulus fillers with the part numbers BRR40995. BRR19433 and BRR22626 are in the range from 00001 to 65237. It Is recommended that PART A of this Non- Modification Service Bulletin be accomplished on all engines prior to or at the next scheduled maintenance opportunity. Cancelled see 880591 G-CGUL G550 5176 Technical Bulletins Page 27 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620817 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No SB BR700.72.900521 (Pan B) Eddy 11 is recommended that 880597 CAN CAN 0.0 0 17 May 2011 C 0.00 Engine 1 Current Inspection • LP Compressor PART B of this Non• Annulus Fillers Modification Service Bulletin be accomplished on all affected engines at the next scheduled maintenance opportunity and be repeated once within a further 500 +1-50 flight hours. Canceled see 880592 880597 SB BR700.72.900521 (Part B) Eddy It is recommended that CAN CAN 0.0 0 17 May 2011 C 0.00 Engine 2 (890597) Current Inspection - LP Compressor PART B of this Non• Annulus Fillers Modification Service Bulletin be accomplished on all affected engines at the next scheduled maintenance opportunity and be repeated once within a further 500 4-50 flight hours. Canceled see 880592 SB BR700.72.900521 (Pan A) Rev 3 • II is recommended that 880602 CAN CM 0.0 0 06 Jan 2013 C 0.00 Engine 1 Inspection - LP Compressor Annulus PART A of this Non- Fillers Modification Service Bulletin be accomplished on all engines prior to or at the next A-check. This inspection is not applicable for p/n FW77117. Mx. Notes: SEE CODE 880591 G-CGUL G550 5176 Technical Bulletins Page 28 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620818 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No 880602 SB BR700.72-900521 (Part A) Rev 3 - It is recommended that CAN CM 0.0 0 13 Jul 2011 C 0.00 Engine 2 (890602) Inspection LP Compressor Annulus PART A of this Non- Fillers Modification Service Bulletin be accomplished on all engines prior to or at the next A-check. This inspection is not applicable for pin FW77117. Mx. Notes: SEE CODE 890590 SB BR700.72-900521 (Part B) Rev 3 - It is recommended that 880603 CAN CAN 0.0 0 07 Mar 2013 C 0.00 Engine 1 Inspection LP Compressor Annulus PART B of this Non- Fillers Modification Service Bulletin be accomplished on all engines prior to or at the next A-check and be repeated once within a further 500 +1- 50 flight hours. This inspection is not applicable for pin FW77117. Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link. SEE CODE 880590 880603 SB BR700.72-900521 (Part B) Rev 3 It is recommended that CAN CAN 0.0 0 07 Mar 2013 C 0.00 Engine 2 (890603) Inspection LP Compressor Annulus PART B of this Non- Fillers Modification Service Bulletin be accomplished on all engines prior to or at the next A-check and be repeated once within a further 500 +1- 50 flight hours. This inspection is not applicable for pin FW77117. Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link. G-CGUL G550 5176 Technical Bulletins Page 29 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620819 L TYP C/W Source Code Description Effectivity ATA Status ii _ogbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No SB BR700.72-900521 (Part A) Rev 4 - It is recommended that GAL Luton 880604 REC CPA( 2849.4 832 10 Apr 2013 C 0.00 Engine 1 Inspection LP Compressor Annulus PART A of this Non- BMX000145 Fillers Modification Service Bulletin be accomplished on all engines prior to or at the next A-check. This inspection is not applicable for pin FW77117. UK145.00883 880604 SB BR700-72-900521 (Part A) Rev 4 It is recommended that GAL Luton REC 2849.4 832 10 Apr 2013 C 0.00 Engine 2 (890604) Inspection LP Compressor Annulus PART A of this Non- BMX000145 Fillers Modification Service Bulletin be accomplished on all engines prior to or at the next A-check. This inspection is not applicable for pin FW77117. UK145.00883 SB BR700.72-900521 (Part B) Rev 4 It is recommended that GAC LTN 880605 REC 3307.8 927 24 Mar 2014 C Engine 1 Inspection LP Compressor Annulus PART B of this Non- BMX000380 Fillers Modification Service Bulletin be accomplished on all affected engines at the next A-Check and be repeated once within a further 500 +/-50 flight hours. NOTE: Repeat insp. that are not accomplished the inspection interval of 500 +1-50 F/H MI not have complied with the stipulated insp. and will result in further inspections. NrA for prn FW77117. UK.145.00883 G-CGUL G550 5176 Technical Bulletins Page 30 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620820 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LDG Date CA MM REF M HRS aintenance Notes Cart No 880605 SB BR700.72.900521 (Part B) Rev 4 • II is recommended that GAC LTN REC CAN 3307.8 927 24 Mar 2014 C Engine 2 (890605) Inspection - LP Compressor Annulus PART B of this Non• BMX000380 Fillers Modification Service Bulletin be accomplished on all affected engines al the next A-Check and be repeated once within a further 500 +1-50 flight hours. NOTE: Repeat insp. that are not accomplished the inspection interval of 500 +1-50 F/H will not have complied with the stipulated insp. and will result in further inspections. WA for pin FW77117. UK.145.00883 SB BR700.72.101858 • Introduction Effectivity: BR700- 880610 72 OPT 12 Aug 2014 I Engine 1 of a HP Compressor Stages 7 to 10 710G4-11 Engines. (a) Rotor Disc Assembly with Revised For engines, which Liner Coating have hardware configuration standard 710C4-11 engraved on the engine data plate (Service Bulletin SB- BR700.72.101466 standard not incorporated). Module M33.120 (HP Compressor Module). (b) For engines, which have hardware configuration standard 710C4-11/10 engraved on the engine data plate (Service Bulletin SB-BR700-72-101466 standard incorporated). Module M33.120 (HP Compressor Module). Compliance: OPTIONAL G-CGUL G550 5176 Technical Bulletins Page 31 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620821 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No 880610 SB BR700-72.101858 • Introduction Effectivity: BR700- 72 OPT 12 Aug 2014 I Engine 2 (890610) of a HP Compressor Stages 7 to 10 710G4-11 Engines. (a) Rotor Disc Assembly with Revised For engines, which Liner Coating have hardware configuration standard 710C4-11 engraved on the engine data plate (Service Bulletin SB- BR700.72.101466 standard not incorporated). Module M33.120 (HP Compressor Module). (b) For engines, which have hardware configuration standard 710C4-11/10 engraved on the engine data plate (Service Bulletin SB-BR700-72-101466 standard incorporated). Module M33.120 (HP Compressor Module). Compliance: OPTIONAL SB BR700.72.101469 R1 - HP Effectivity: GV • prior 72 880611 OPT 29 Aug 2014 I Engine 1 Compressor Vortex Reducer Ring to Engine Serial Number 11506. G500/550 - see bulletin. Compliance: OPTIONAL - This Service Bulletin introduces a new pan, which should be used when stocks of the pre Service Bulletin part have been used up. G-CGUL G550 5176 Technical Bulletins Page 32 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620822 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No 880611 SB BR700.72-101469 RI HP Effectivity: GV - prior I 72 OPT 29Aug 2014 Engine 2 (890611) Compressor Vortex Reducer Ring to Engine Serial Number 11506. G500/550 see bulletin. Compliance: OPTIONAL This Service Bulletin introduces a new pan. which should be used when stocks of the pre Service Bulletin part have been used up. SB BR700.72-101476R1 - Effectivity:GV Engines 880612 72 OPT 29Aug 2014 I Engine 1 Introduction of a New Combustion Prior to Engine Serial Chamber Without Cooling Ribs Number 11505. G500IG550 -see the bulletin for effectivity. Compliance: OPTIONAL This Service Bulletin introduces a new pan. which should be used when stocks of the pre Service Bulletin part have been used up. 880612 SB BR700.72-101476RI - Effectivity:GV Engines 72 OPT 29Aug 2014 I Engine 2 (890612) Introduction of a New Combustion Prior to Engine Serial Chamber Without Cooling Ribs Number 11505. G500IG550 -see the bulletin for effectivity. Compliance: OPTIONAL This Service Bulletin introduces a new pan. which should be used when stocks of the pre Service Bulletin part have been used up. 880613 SB BR700.72-101540 R4 Outlet 72 OPT 29Aug 2014 I Engine 1 Guide Vane Housing Assembly 880613 SB BR700.72-101540 R4 Outlet 72 OPT 29Aug 2014 I Engine 2 (890613) Guide Vane Housing Assembly G-CGUL G550 5176 Technical Bulletins Page 33 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620823 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No SB BR700.72.101891 • Introduction Effectivity: (1) BR700- 880614 72 OPT 11 Sep2014 I Engine 1 of a Redesigned Gearline 12 710A1-10 Engines Assembly which is Balanced inducing Prior to Engine Serial the Permanent Magnetic Alternator Number 11512. Non- (PMA) Rotor Modular and Module M61.203 (Accessory Gearbox Module). (2) BR700.710C4.11 Engines (a) For engines which have hardware configuration standard 710C4-11 engraved on the engine data plate (Service Bulletin SB- BR700.72.101466 standard not incorporated) only. Prior to Engine Serial Number 16115. Non- Modular and Module M61.205 (Accessory Gearbox Module). 880614 SB BR700.72.101891 - Introduction Effectivity: (1) BR700- 72 OPT 11 Sep 2014 I Engine 2 (890614) of a Redesigned Gearline 12 710A1.10 Engines Assembly which is Balanced inducing Prior to Engine Serial the Permanent Magnetic Alternator Number 11512. Non- (PMA) Rotor Modular and Module M61-203 (Accessory Gearbox Module). (2) BR700.710C4.11 Engines (a) For engines which have hardware configuration standard 710C4.11 engraved on the engine data plate (Service Bulletin SB- BR700.72.101466 standard not incorporated) only. Prior to Engine Serial Number 16115. Non- Modular and Module M61.205 (Accessory Gearbox Module). G-CGUL G550 5176 Technical Bulletins Page 34 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620824 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LDG Date CA MM REF M HRS aintenance Notes Cert No SB BR700.72.101897 • Introduction Compliance: 880615 72 OPT 22 Sep 2014 I Engine 1 of an Alternative Standard of HP OPTIONAL This Compressor Stage 1 Blade Service Bulletin introduces alternative and fully interchangeable pans. 880615 SB BR700.72.101897 • Introduction Compliance: 72 OPT 22 Sep 2014 I Engine 2 (890615) of an Alternative Standard of HP OPTIONAL This Compressor Stage 1 Blade Service Bulletin introduces alternative and fully interchangeable pans. SB BRR700.29.900511 Left Engine Note: Bulletin only 882900 72 REC C/W 1787.4 543 08 Mar 2011 C 0.00 Engine 1 Hydraulic Tubes and Fittings applies to engine when installed in the left (No.1) position. 882900() SB BRR700.29.900511 Left Engine • Note: Bulletin only 72 REC 08 Dec 2010 I Engine 2 Hydraulic Tubes and Fittings applies to engine when installed in the left (No.1) position. Alert SB BR700.72-A900508 BR700.710A1.10 882910 CAN CAN 0.0 0 23 Apr 2013 C 0.00 Engine 1 Replacement of HP Turbine Rotor Engine sin 11182. Discs Due to Steel Inclusion BR700.710C4•11 Engines sin 15791, 15792. 15799, 15801, 15802. Engines must be removed from the aircraft before the affected HP turbine stage 1 and 2 discs have accumulated 3000 cycles since new. Cancelled by Alen SB•BR700-72- A900508 Rev 1. Mx. Notes. This code has been cancelled. See Compliance Remarks by clicking Show Remarks link G-CGUL G550 5176 Technical Bulletins Page 35 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620825 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No 882910 Alert SB BR700.72-A900508 BR700.710A1.10 CAN CAN 0.0 0 23 Apr 2013 C 0.00 Engine 2 (892910) Replacement of HP Turbine Rotor Engine sin 11182. Discs Due to Steel Inclusion BR700.710C4•11 Engines sin 15791, 15792. 15799, 15801, 15802. Engines must be removed from the aircraft before the affected HP turbine stage 1 and 2 discs have accumulated 3000 cycles since new. Cancelled by Alen SB-BR700-72- A900508 Rev 1. Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link. Alert SB BR700.72,4900508 Rev 1 BR700.710A1.10 882911 MAN N/A 22 Apr 2013 Engine 1 Replacement of HP Turbine Rotor Engine sin 11182. Discs Due to Steel Inclusion BR700.710C4•11 Engines sin 15791, 15792. 15799, 15801. 15802. Engines must be removed from the aircraft before the affected HP turbine stage 1 and 2 discs have accumulated 3000 cycles since new. If the Initial Issue of this Non. Modification Service Bulletin is already incorporated, no further Operator action is required with this Revision. G-CGUL G550 5176 Technical Bulletins Page 36 of 164 20 Jan 2015 (O2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620826 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date c/I MM REF M HRS aintenance Notes Cert No 882911 Alert SB BR700.72-A900508 Rev 1 BR700.710A1-10 MAN NIA 22 Apr 2013 I Engine 2 (892911) Replacement of HP Turbine Rotor Engine sin 11182. Discs Due to Steel Inclusion BR700.710C4•11 Engines sin 15791, 15792. 15799, 15801, 15802. Engines must be removed from the aircraft before the affected HP turbine stage 1 and 2 discs have accumulated 3000 cycles since new. If the Initial Issue of this Non. Modification Service Bulletin is already incorporated, no further Operator action is required with this Revision. SB BR700.70.900040 (Rev 11) • EFF: Section 1 • 887001 70 OPT N/A 7.2 6 09 Apr 2008 C 0.00 Engine 1 Engine Life Management - Fixed BR700-710A1-10 (GV) Interval Rework Engines Engines ii Section 3 • BR700-710C4-11 (G500 / G550) Engines // HARD TIME Maintenance Program Mx. Notes: ENGINE DECLARED TASK ORIENTED 887001 SB BR700.70.900040 (Rev 11) • EFF: Section 1 • NA, 70 OPT 7.2 6 09 Apr 2008 C aoo Engine 2 (897001) Engine Life Management • Fixed BR700.710A1-10 (GV) Interval Rework Engines Engines ft Section 3 • BR700.710C4-11 (G500 / G550) Engines // HARD TIME Maintenance Program Mx. Notes: ENGINE DECLARED TASK ORIENTED 887002 SB BR700.70.900294 • Task Oriented EFF: Section 1 • 70 OPT CW 7.2 6 09 Apr 2008 C 0.00 Engine 1 Engine Inspection BR700.710A1.10 (GV) Engines ft Section 2 - BR700.710C4-11 (G500 / G550) Engines TASK ORIENTED Maintenance Program Mx. Notes: ENGINE DECLARED TASK ORIENTED G-CGUL G550 5176 Technical Bulletins Page 37 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620827 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No 887002 SB BR700.70.900294 • Task Oriented EFF: Section 1 • 70 OPT cm 7.2 6 09 Apr 2008 C 0.00 Engine 2 (897002) Engine Inspection BR700•710A1-10 (GV) Engines // Section 2. BR700.710C4.11 (G5001G550) Engines // TASK ORIENTED Maintenance Program Mx. Notes: ENGINE DECLARED TASK ORIENTED SB BR700•70•900412 • BR7I0 EFF: BR700.710A1• 887003 70 OPT CAN 7.2 6 09 Apr 2008 C 0.00 Engine 1 Engine Maint Prog 10 (GV) Engines!! BR700-710C4•11 (G5001G550) Engines Mx. Notes: ENGINE DECLARED TASK ORIENTED 887003 SB BR700-70.900412 • BR710 EFF: BR700.710A1• 70 OPT OW 7.2 6 09 Apr 2008 C 0.00 Engine 2 (897003) Engine Maint Prog 10 (GV) Engines // BR700-710C4•11 (G5001G550) Engines Mx. Notes: ENGINE DECLARED TASK ORIENTED 887186 SB BR700-71.101206 • Power Plant NOTE: Prior to Engine 71 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 External Drain Tubes And Fitting Serial Number 15111 887166 SB BR700.71.101206 - Power Plant NOTE: Prior to Engine 71 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (897166) External Drain Tubes And Fitting Serial Number 15111 SB BR700.71.101424 • Modified Effectivity: BR700- 887175 71 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine I Installation of Clip Stack 710C4-11 Engines, which have Service Bulletin SB•BR700-71- 101206 incorporated. Prior to Engine Serial Number 15165 887175 SB BR700.71.101424 • Modified Effectivity: BR700• (897175) 71 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 Installation of Clip Stack 710O1-11 Engines, which have Service Bulletin SB•BR700-71- 101206 incorporated. Prior to Engine Serial Number 15165 SB BR700.71.101462 - Extension NOTE: Prior to Engine 887176 71 OPT 27 Jan 2006 I Engine Clip with Simplified Design Serial Number 15206 G-CGUL G550 5176 Technical Bulletins Page 38 of 164 20 Jan 2015 riD 2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620828 TYP C/W Source Code Description Effectivity ATA Status ilLogbook Work Order HRS LDG Date C/I MM REF M HRS aintenance Notes Cert No 887176 SB BR700.71-101462 - Extension NOTE: Prior to Engine I 71 OPT 27 Jan 2006 Engine 2 (897176) Clip with Simplified Design Serial Number 15206 887177 SB BR700.71-101561 - EEC Harness Effectivity: Prior to 71 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Revised Harness Clipping engine SN 15352 887177 SB BR700-71-101561 - EEC Harness Effectivity: Prior to 71 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (897177) - Revised Harness Clipping engine SN 15352 887178 SB BR700.71-101563 - Engine Build EFF: from EBU serial 71 OPT 23 May 2007 I Engine 1 Unit (EBU) Harness number GVSP001 to GVSP124. 887178 SB BR700.71-101563 - Engine Build EFF: from EBU serial (897178) Unit (EBU) Harness 71 OPT 23 May 2007 I Engine 2 number GVSP001 to GVSP124. 887179 SB 6R700-71-101581 - Oil Drain Effectivity: Prior to 71 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Tube Support Bracket Engine Serial Number 15410 and from Engine Serial Number 15412 to 15415 887179 SB BR700.71-101581 - Oil Drain Effectivity: Prior to 71 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (897179) Tube Support Bracket Engine Serial Number 15410 and from Engine Serial Number 15412 to 15415 887188 SB BR700.71-900384 - Engine Effectivity: For 71 REC 23 May 2007 I Engine 1 Electronic Controller (EEC) Harness engines which have hardware configuration standard 710C4.11 or 710C4.11/10 engraved on the engine data plate 887188 SB BR700.71-900384 - Engine Effectivity: For 71 REC 23 May 2007 I Engine 2 (897188) Electronic Controller (EEC) Harness engines which have hardware configuration standard 710C4.11 or 710C4.11/10 engraved on the engine data plate G-CGUL G550 5176 Technical Bulletins Page 39 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620829 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No SB BR700.71-900413 - Engine Build Effectivity: For I 887189 71 REC 23 May 2007 Engine 1 Unit (EBU) Harness engines which have hardware configuration standard 710C4.11 or 71004.11110 engraved on the engine data plate 887189 SB BR700.71-900413 - Engine Build Effectivity: For 71 I REC 23 May 2007 Engine 2 (897189) Unit (EBU) Harness engines which have hardware configuration standard 710C4.11 or 71004.11110 engraved on the engine data plate 887190 SB BR700.71-900336 - Fan Cowl Effectivity: Aircraft REC N/A 88 0.0 0 26 Nov 2007 C 0.00 Engine 1 Door Switch Brackets &Ns 5023 thru 5028 887190 SB BR700.71-900336 - Fan Cowl Effectivity: Aircraft 88 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (897190) Door Switch Brackets &Ns 5023 thru 5028 SB BR700.71-900505 EEC Lane A 710A1.10. 710O4.11 887195 REC CPN 1787.4 543 08 Mar 2011 C 0.00 Engine 1 Harness - Inspection prior to tin 15651 887195 SB BR700.71-900505 EEC Lane A 710A1.10. 710O4.11 (897195) Harness • Inspection REC CPN 1787.4 543 08 Mar 2011 C 0.00 Engine 2 prior to ern 15651 SB BR700.72-900455 Rev 2 Pt. A NOTE: See GAMA20 887257 72 CAN CPN 206.7 90 20 Aug 2008 C 0.00 Engine 1 Visual Insp LP Compressor Annulus REVISION 5 CMP F080834 Fillers CODES 887397.f 897397 Superceded see 880596 887257 SB BR700.72-900455 Rev 2 Pt. A NOTE: See GAMA20 72 CAN CPN 206.7 90 20 Aug 2008 C 0.00 Engine 2 (897257) Visual Insp LP Compressor Annulus REVISION 5 CMP F080834 Fillers CODES 887397.f 897397 Superceded see 880596 SB BR700.72-900455 Rev 2 Pt. B NOTE: See 72 887258 CAN 28 Feb 2008 I Engine 1 Eddy Current Insp LP Compressor REVISION 5 CMP Annulus Fillers CODES 887398.f 897398 Superceded see 880596 G-CGUL G550 5176 Technical Bulletins Page 40 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620830 TYP CNV Source Code Description Effectivity IATAI Status Logbook Work Order HRS LOG Date CA MM REF M HRS Ilaintenance Notes Cert No 887258 SB BR700.72.900455 Rev 2 Pt. B NOTE: See 72 CAN 28 Feb 2008 I Engine 2 (897258) Eddy Current Insp - LP Compressor REVISION 5 - CMP Annulus Fillers CODES 887398 897398 Superceded see 880596 SB BR700.73.101415 • Fuel System - NOTE: GV Engines: 887361 73 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Flexble Air Tubes Prior to Engine Serial Number 11505 11G500 & G550 Engines: Prior to Engine Serial Number 15168 and for Engine Serial Numbers 15169 to 15176 887361 SB BR700.73.101415 • Fuel System - NOTE: GV Engines: 73 OPT N'A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (897361) Flexible Air Tubes Prior to Engine Serial Number 1150511G500 & G550 Engines: Prior to Engine Serial Number 15168 and for Engine Serial Numbers 15169 to 15176 887367 SB BR700.73-101443 - Engine Fuel NOTE: GV Engines: 73 OPT NIA 0.0 0 26 Nov 2007 C 0.00 Engine 1 And Control (DEP) Prior to Engine Serial Number 11505 11 G500 & G550 Engines: Prior to Engine Serial Number 15228 887367 SB BR700.73.101443 • Engine Fuel NOTE: GV Engines: 73 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (897367) And Control (DEP) Prior to Engine Serial Number 1150511G500 & G550 Engines: Prior to Engine Serial Number 15228 G-CGUL G550 5176 Technical Bulletins Page 41 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620831 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No SB BR700.73.900323 • FMU Effectivity: Engine 887391 71 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Connector O-Ring Serial Numbers 15107 thru 15109, 15111, 15114 that 15117, 15120 thru 15130 and 15132 that 15135 887391 SB BR700.73.900323 • FMU Effectivity: Engine 71 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (897391) Connector O-Ring Serial Numbers 15107 thru 15109, 15111, 15114 that 15117, 15120 that 15130 and 15132 that 15135 SB BR700.73•A900451 - Combined NOTE: For engines 73 73 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 8896 Overspeed Shutoff Solenoid which have a Fuel Metering Unit (FMU). PM 8061.977 with a FMU Serial Number prior to 15174932 installed 887396 SB BR700.73•A900451 - Combined NOTE: For engines 73 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (897396) Overspeed Shutoff Solenoid which have a Fuel Metering Unit (FMU). PM 8061.977 with a FMU Serial Number prior to 15174932 installed SB BR700.72.900455 Visual Insp - It is recommended that 887397 CAN OW 1479.1 446 03 Sep 2010 C Engine 1 LP Compressor Annulus Fillers (Part PART A of this Non. GAL100716 A) Modification Service Bulletin beaccomplished on engines at the next scheduled aircraft maintenance opportunity and be repeated at maximum intervals of 550 flight hours.Superceded see 880596/880597 G-CGUL G550 5176 Technical Bulletins Page 42 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620832 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No 887397 SB BR700.72-900455 Visual 'lisp It is recommended that CAN CAN 1479.1 446 03 Sep 2010 C Engine 2 (897397) LP Compressor Annulus Fillers (Part PART A of this Non- GAL100716 A) Modification Service Bulletin beaccomplished on engines at the next scheduled aircraft maintenance opportunity and be repeated at maximum intervals of 550 flight hours.Superceded see 8805961880597 SB BR700.72-900455 Eddy Current- For BR700.710A1-10 887398 CAN CPN 1479.1 446 03 Sep 2010 C Engine 1 LP Compressor Annulus Fillers (Part and BR700.710C4-II GAL100716 B) Engines:It is recommended that PART B of this Service Bulletin be accomplished on engines at the next scheduled aircraft maintenance opportunity and be repeated at 500 flight hours +/- 50 flight hours.Superceded see 880596)880597 887398 SB BR700.72-900455 Eddy Current- For BR700.710A1-10 CAN CPN 1479.1 446 03 Sep 2010 C Engine 2 (897398) LP Compressor Annulus Fillers (Part and BR700.710C4.11 GAL100716 B) Engines:It is recommended that PART B of this Service Bulletin be accomplished on engines at the next scheduled aircraft maintenance opportunity and be repeated at 500 flight hours +/- 50 flight hours.Superceded see 880596)880597 G-CGUL G550 5176 Technical Bulletins Page 43 of 164 20 Jan 2015 2015 Gulfstream Aerospace Corporation. 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A General Dynamics Company EFTA00620833 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No 887514 SB BR700.75-101097 - Core Air Effectivity: Prior to 75 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Tubes And Fittings Intro engine SN 15131 887514 SB 6R700-75-101097 - Core Air Effectivity: Prior to (897514) Tubes And Fittings Intro 75 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 engine SN 15131 SB BR700.75-900308 - VSV Effectivity: Prior to 887532 75 INF N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Mechanism Lubrication Engine Serial Number 15146 887532 SB BR700.75-900308 - VSV Effectivity: Prior to 75 INF N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (897532) Mechanism Lubrication Engine Serial Number 15146 887707 SB BR700-77-101534 - New TGT Effectivity: BR700- 77 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Probes 710A1.10 Engines Prior to Engine Serial Number 1150611 BR700.710C4.11 Engines Prior to Engine Serial Number 15308 887707 SB 6R700-77-101534 - New TGT Effectivity: BR700- 77 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (897707) Probes 710A1.10 Engines Prior to Engine Serial Number 11506/I BR700.710C4.11 Engines Prior to Engine Serial Number 15308 SB BR700.77-101536 - Turbine Gas EFF: Prior to eng SN 77 OPT 887708 N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Temp (TGT) Harness 15322 and for Engine SN 15330 and 15331, 887708 SB BR700.77-101536 - Turbine Gas EFF: Prior to eng SN 77 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (897708) Temp (TGT) Harness 15322 and for Engine SN 15330 and 15331. SB BR700.77-900329 - N2 Speed Effectivity: N2 speed 887711 77 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Probes probes. PIN 889-3.13. with Serial Numbers listed in this SB G-CGUL G550 5176 Technical Bulletins Page 44 of 164 20 Jan 2015 €12015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620834 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date c/I MM REF M HRS aintenance Notes Cert No 887711 SB BR700-77-900329 • N2 Speed Effectivity: N2 speed 77 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (897711) Probes probes. P/N 889.3.13, with Serial Numbers listed in this SB BR700-78.900535 R3 • TRU Door Accomplishment of 887803 OPT 13 Aug 2012 I Airframe Actuator (Left) • Inspection of Rod this SB is optional. End Assy of the PDA Rolls•Royce will contact the operator if they are required to CM this SB. Operators must not accomplish this SB unless they are contacted by Rolls• Royce. BR700•78•900535 R3 • TRU Door Accomplishment of I 887804 OPT 13 Aug 2012 Airframe Actuator (Right) • Inspection of Rod this SB is optional. End Assy of the PDA Rolls•Royce will contact the operator if they are required to CM this SB. Operators must not accomplish this SB unless they are contacted by Rolls• Royce. 887839 BR700-78.101512 • Improvements to NOTE: GV Engines: 78 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Airframe the Thrust Reverser Pivoting Doors Prior to TRU Serial (Left) Number 398 /I G500 & G550 Engines: Prior to TRU Serial Number 153 M700.78.101514. TM Fixed NOTE: GV Engines: 887840 78 OPT N/A 0.0 0 26 Nov 2007 C aoo Airframe Structure - Upper Inhibition Bolt Fitting Prior to TRU Serial (Left) Number 39811 G500 & 6550 Engines: Prior to TRU Serial Number 153 BR700-78.101515 - Introduction of a NOTE: GV Engines: 887841 78 OPT N/A 0.0 0 26 Nov 2007 C aoo Airframe New Y Stop Fitting (Left) Prior to TRU Serial Number 3981 G5001 G550 Engines: Prior to TRU Serial Number 153 G-CGUL G550 5176 Technical Bulletins Page 45 of 164 20 Jan 2015 492015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620835 TYP C/W Source Code Description Effectivity ATA Status Logbook Work Order HRS LDG Date Cli MM REF M HRS Maintenance Notes Cert No 887842 BR700.78-101516 New Primary NOTE: Prior to TRU 78 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Airframe Door Lock Actuator (Left) Serial Number 153/ This Bulletin installs PM -02. when this SB is complied with remove the frequency from 887850 and 897850 887843 8P700-78.101606 - Introduction of a NOTE: Prior to TRU 78 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Airframe New T/FI Unit (Left) Serial Number 331 BR700.78-900440 - Inspection of TIP NOTE: See SB for 887848 78 REC N/A 0.0 0 26 Nov 2007 C 0.00 Airframe Structure Boxes I Connectors (Left) Thrust Reverser Serial Numbers affected 887850 BR700-78.900350 - Primary Door NOTE: Recurring 78 REC N/A 0.0 0 05 May 2008 C 0.00 Airframe Lock Actuator - Insp (Left) Frequency is not required if PIN P466A0001.02 Primary Door Lock Actuators have been installed per Rolls- Royce SB-BR700.78- 101516 (CMP Code 887842) Freq is per SB-BR700-78.900350 Pg 5 of 5 C (3). BR700-78.900443 - Replacement Of NOTE: Left TRU SIN: 887851 78 REC N/A 0.0 0 26 Nov 2007 C 0.00 Airframe T/R Access Doors (Left) 156. 158. 160. 162. 164. 166. 168. 170. 172. 174. 176. 178. 184. 186. 190 and 194 / Right TRU SIN: 155. 157. 159. 161. 163. 165. 167. 169. 171. 179. 183. 189 and 191 SB BR700-79-101449 - Oil Filter Effectivity: Prior to 887934 79 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Differential Pressure Switch Engine Serial Number 15198 887934 SB BR700.79-101449 - Oil Filter Effectivity: Prior to 79 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (897934) Differential Pressure Switch Engine Serial Number 15198 G-CGUL G550 5176 Technical Bulletins Page 46 of 164 20 Jan 2015 C12015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620836 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No SB BR700•79•101458 • Oil Filter Effectivity: Prior to 887935 79 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Element Engine Serial Number 15198 887935 SB BR700•79•101458 • Oil Filter Effectivity: Prior to 79 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (897935) Element Engine Serial Number 15198 SB BR700.79.101803R1 887944 79 REC 29 Aug 2014 I Engine 1 Introduction Of New Oil Pump Unit With Improved Gears 887944 SB BR700.79.101803R1 • 79 29 Aug 2014 REC Engine 2 (897944) Introduction Of New Oil Pump Unit With Improved Gears SB BR700.80.900340 • Air Turbine NOTE: For engines 888010 80 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Starter Oil Level that have the Service Bulletin SB•BR700-80- 101018 standard incorporated and on which installed air turbine starters are prior to air turbine starter Serial Number 1204.1438 888010 SB BR700.80.900340 • Air Turbine NOTE: For engines 80 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (898010) Starter Oil Level that have the Service Bulletin SB•BR700-80- 101018 standard incorporated and on which installed air turbine starters are prior to air turbine starter Serial Number 1204.1438 SB BR700.80.900427 • Starter Air 888011 80 INF N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Valve 888011 SB BR700.80.900427 • Starter Air 80 INF N'A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (898011) Valve G-CGUL G550 5176 Technical Bulletins Page 47 of 164 20 Jan 2015 C2015 Gulfstream Aerospace Corporation. 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A General Dynamics Company EFTA00620837 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No Not Applicable for 888801 SB BR700-73-900153FMU O/S SIO 88 CAN N/A 0.0 0 26 Nov 2007 C 731005 0.00 Engine 1 G550 Engines 888801 Not Applicable for SB BR700.73-900153FMU as sio 88 CAN N/A 0.0 0 26 Nov 2007 C 731005 0.00 Engine 2 (898801) G550 Engines Not Applicable for 888802 SB BR700.72-900229LP COMP GVI 88 CAN N/A 0.0 0 26 Nov 2007 C ACB 11A 0.00 Engine 1 G550 Engines 888802 Not Applicable for SB BR700.72-900229LP COMP GVI 88 CAN N/A 0.0 0 26 Nov 2007 C ACB 11A 0.00 Engine 2 (898802) G550 Engines Not Applicable for 888803 SB BR700.72-900229LP COMP NDI 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 G550 Engines 888803 Not Applicable for SB BR700.72-900229LP COMP NDI 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (898803) G550 Engines Not Applicable for 888804 SB BR700.72-900229LP COMP NDI 88 CAN N/A 0.0 0 26 Nov 2007 C ACB 11A 0.00 Engine 1 G550 Engines 888804 Not Applicable for SB BR700.72-900229LP COMP NDI 88 CAN N/A 0.0 0 26 Nov 2007 C ACB 11A 0.00 Engine 2 (898804) G550 Engines SB BR700.72-900229 TECH Not Applicable for 888805 88 CAN N/A 0.0 0 26 Nov 2007 C TV1913R 0.00 Engine 1 VARIANCE G550 Engines 888805 SB BR700.72-900229 TECH Not Applicable for VARIANCE 88 CAN N/A 0.0 0 26 Nov 2007 C TV1913R 0.00 Engine 2 (898805) G550 Engines 888807 SB BRR700.73.101106FMU Not Applicable for 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 G550 Engines 888807 Not Applicable for SB BRR700.73-101106FMU 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (898807) G550 Engines SB BR700.72-100900 NEW CORE Not Applicable for 888808 88 CAN N/A 0.0 0 26 Nov 2007 C 999822 0.00 Engine 1 FAIR G550 Engines 888808 SB BR700.72-100900 NEW CORE Not Applicable for FAIR 88 CAN N/A 0.0 0 26 Nov 2007 C 999822 0.00 Engine 2 (898808) G550 Engines G-CGUL G550 5176 Technical Bulletins Page 48 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. 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A General Dynamics Company EFTA00620838 TYP C/W Source Code Description Effectivity ATA Status L Logbonk Work Order HRS LDG Date CII MM REF M HRS aintenance Notes Cert No SB BR700.72-101395 METCO Not Applicable for 888809 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 BLADE CO G550 Engines 888809 SB BR700-72-101395 METCO Not Applicable for 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (898809) BLADE CO G550 Engines SB BR700-71-100995 HYD PUMP Not Applicable for 888810 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 RMVL G550 Engines 888810 SB BR700.71-100995 HYD PUMP Not Applicable for 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (898810) RMVL G550 Engines 888813 SB BR700-79-900215 R2 PT 1 DPI Not Applicable for 88 CAN N/A 0.0 0 26 Nov 2007 C AD 01.01.01 0.00 Engine 1 SW G550 Engines 888813 SB ØR700.79-900215 R2 PT 1 DPI Not Applicable for SW 88 CAN N/A 0.0 0 26 Nov 2007 C AD 0101.01 0.00 Engine 2 (898813) G550 Engines 888814 SB BR700-79-900215R2 PT 2 DPI CAN N/A 0.0 0 26 Nov 2007 C AD 0101.01 0.00 Engine 1 SW 888814 SB BR700-79-900215R2 PT 2 DPI CAN N/A 0.0 0 26 Nov 2007 C AD 01.01.01 0.00 Engine 2 (898814) SW SB BR700.73-100148 EJECTOR Not Applicable for 888815 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 FILTER G550 Engines 888815 SB BR700-73-100148 EJECTOR Not Applicable for 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (898815) FILTER G550 Engines 888816 SB BR700.73-101441 EEC G9.1 SAN Not Applicable for 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 G550 Engines 888816 Not Applicable for SB 8R700.73-101441 EEC G9.1 SAN 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (898816) G550 Engines 888817 SB BR700.73-900182FMU VALVE- Not Applicable for 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 DSE G550 Aircraft 888817 SB BR700-73-900182FMU VALVE- Not Applicable for 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (898817) DSE G550 Aircraft G-CGUL G550 5176 Technical Bulletins Page 49 of 164 20 Jan 2015 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620839 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No SB BR700.72-101473 DFL FAN Not Applicable for 888818 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 BLADES G550 Engines 888818 SB BR700.72-101473 DFL FAN Not Applicable for 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (898818) BLADES G550 Engines SB BR700.72-101144 (Use CMP 888819 72 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Code 880271) 888819 SB BR700.72-101144 (Use CMP 72 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (898819) Code 880271) SB BR700-73-101400 EEC 52.1 SAN 888820 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 (Use CMP Code 880305) 888820 SB BR700-73-101400 EEC 52.1 SAN 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (898820) (Use CMP Code 880305) EFF: Engine Serial 888822 Use CMP Code 880422 / 890422 72 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Numbers prior to SIN 15146 ./ Module M33- 12 (HP Compressor Module 888822 EFF: Engine Serial Use CMP Code 880422 / 890422 72 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (888822) Numbers prior to SIN 15146/ Module M33- 12 (HP Compressor Module BR700.78.101512 - Improvements to NOTE: GV Engines: 897839 78 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Airframe the Thrust Reverser Pivoting Doors Prior to TRU Serial (Right) Number 398 .// G500 8 G550 Engines: Prior to TRU Serial Number 153 BR700.78.101514 TM Fixed NOTE: GV Engines: 897840 78 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Airframe Structure - Upper Inhibition Bolt Fining Prior to TRU Serial (Right) Number 398// G500 8 G550 Engines: Prior to TRU Serial Number 153 G-CGUL G550 5176 Technical Bulletins Page 50 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620840 TYP C/W Source Code Description Effectivity ATA Status Logbook Work Order HRS LDG Date Cli MM REF M HRS Maintenance Notes Cert No BR700.78.101515 Introduction of a NOTE: GV Engines: 897841 78 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Airframe New Y Stop Fitting (Right) Prior to TRU Serial Number 398/G500! G550 Engines: Prior to TRU Serial Number 153 897842 8R700-78.101516 - New Primary NOTE: Prior to TRU 78 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Airframe Door Lock Actuator (Right) Serial Number 153/ This Bulletin installs P/N -02. when this SB is complied with remove the frequency from 887850 and 897850 897843 BR700-78.101606 - Introduction of a NOTE: Prior to TRU 78 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Airframe New T/R Unit (Right) Serial Number 331 897848 BR700J8.900440 - Inspection of T/R NOTE: See SB for 78 REC N/A 0.0 0 26 Nov 2007 C 0.00 Airframe Structure Boxes/ Connectors (Right) Thrust Reverser Serial Numbers affected BR700-78.900350 - Primary Door NOTE: Recurring 897850 78 REC N/A 0.0 0 05 May 2008 C 0.00 Airframe Lock Actuator - Insp (Right) Frequency is not required if PIN P466A0001.02 Primary Door Lock Actuators have been installed per Rolls- Royce SB-BR700.78- 101516 (CMP Code 887842) Freq is per SB-BR700-78.900350 Pg 5 of 5 C (3). 8R700-78.900443 - Replacement Of NOTE: Left TRU SIN: 897851 78 REC N/A 0.0 0 26 Nov 2007 C 0.00 Airframe T/R Access Doors (Right) 156, 158. 160. 162. 164, 166. 168. 170. 172, 174. 176. 178. 184. 186. 190 and 194 /Right TRU S/N: 155. 157. 159. 161. 163. 165, 167. 169. 171. 179, 183. 189 and 191 901001 ST02696AT-D PAX OXY CONTROL 35 INF CPN 20.7 1 30 Apr 2008 C 0.00 Airframe G-CGUL G550 5176 Technical Bulletins Page 51 of 164 20 Jan 2015 C12015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620841 TYP C/W Source Code Description Effectivity ATA Status Logbook Work Order HRS LDG Date Cli MM REF M HRS Maintenance Notes Cert No ST02697AT-D EMERGENCY t 901007 33 INF CPAr 20.7 30 Apr 2008 C 0.00 Airframe LIGHTING Ell Desc 901010 ST02715AT-D EXTERNAL CAMERA ' : 23 INF CPAr 20.7 t 30 Apr 2008 C 0.00 Airframe SECURAPLANE. ST00892LA Emergency Vision 901022 25 INF NIA 0.0 0 26 Nov 2007 C 0.00 Airframe Assurance System (EVAS) 901023 ST02915AT-D LSZ-860 LIGHTNING INF CPAr 20.7 t 30 Apr 2008 C 0.00 Airframe DETECTOR ST02796AT-D BROAD BAND MULTI NOTE: See CMP t 901024 INF CPAr 20.7 30 Apr 2008 C 0.00 Airframe LINK SYS (BBML) Codes 262578 and 262548 for ICA Requirements ST02920AT-D SATCOM SYSTEM 901025 INF NIA 0.0 0 26 Nov 2007 C 0.00 Airframe (MCS-7000) ST03290AT-D (ATG) Injection Molded t 901031 25 INF CPAr 20.7 30 Apr 2008 C 0.00 Airframe Elec Window Shades ST01957CH.D Airshow Remote NOTE: See CMP 901063 23 INF NIA 0.0 0 26 Nov 2007 C 0.00 Airframe Controller Codes 233265 and 233266 for ICA Requirements 901068 ST04264AT-D Aircell ATG-4000 OPT Airframe 901069 ST02045CH.D AFT LAV SHOWER 25 INF NIA 0.0 0 26 Nov 2007 C 0.00 Airframe 901070 ST02046CH.D FWD GALLERY wiLH NOTE: See CMP 25 INF NIA 0.0 0 26 Nov 2007 C 0.00 Airframe COMM AREA Code 252098 for ICA Requirement ST02047CH.D MAGNASTAR MCS• NOTE: See CMP 901071 INF CPAr 20.7 1 30 Apr 2008 C 0.00 Airframe 7000 Codes 232134 and 232135 for ICA Requirements G-CGUL G550 5176 Technical Bulletins Page 52 of 164 20 Jan 2015 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620842 TYP C/W Source Code Description Effectivity ATA Status Logbook Work Order HRS LDG Date Cli MM REF M HRS Maintenance Notes Cert No NOTE: See CMP I 901072 ST02048CH.D Airshow 4000 System INF CPN 20.7 30 Apr 2008 C 0.00 Airframe Code 232165 for ICA Requirement NOTE: See CMP I 901073 ST02049CH.D SECURAPLANE 500 INF CPN 20.7 30 Apr 2008 C 0.00 Airframe Codes 237225. 237228. 237235. and 232245 for ICA Requirements Reference GAC 901077 ST03686AT-D Airplane Interior MAN Airframe document No. GC5280I A715 for Maintenance Requirements Instructions for Continued Airworthiness dated 610612012. 901078 ST04289AT-D Aircraft Interior OPT 31 Aug 2013 I Airframe 901355 STO3044AT-D Cabin Custom Interior EFF: G550 5063 INF N/A 0.0 0 26 Nov 2007 C 0.00 Airframe ONLY. ST03033CH.D True North Simphone STC ST03033CH-D 901377 23 OPT Airframe System True North Simphone System. Standard Aero Document No. 1021304. ST01952CH.D EXECUTIVE 901952 INF N/A 0.0 0 26 Nov 2007 C 0.00 Airframe INTERIOR 901977 ST02196LA-D Fonvard Vestibule 25 INF Airframe Compartment With 1 Additional Crew Seat 901978 ST04260AT-D Installation Of OPT 05 Jun 2012 Airframe Rockwell Collins Programmable Switch (PSW) G-CGUL G550 5176 Technical Bulletins Page 53 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620843 TYP C/W Source Code Description Effectivity ATA Status Logbook Work Order HRS LDG Date Cli MM REF M HRS Maintenance Notes Cert No ST03781AT-D TrueNonh Simphone 901979 INF 14 Jun 2010 Airframe Airborne Telecommunication ST04250AT-D Interior 901980 INF 03 Feb 2012 I Airframe Reconfiguration ST04246AT-D EMS AMT-700G STC ST04246AT-D 901981 INF 08 Dec 2011 Airframe SATCOM Installation of EMS AMT-700G SATCOM Antenna Subsystem. 901982 ST04261AT-D Airplane Interior INF Airframe CE-CSB-5004 CSB 004 (Advanced Effectivity: This Cabin 940040 44 OPT 24 Oct 2014 Airframe Cabin Server (ACS) System Upgrade Service Bulletin is 4.4.3.9) applicable to aircraft with AC firmware version 4.4.1 installed or later approved version. Serial number effectivity includes 5365. 5381. 5385. 5394. 5395. 5400. 5407. 5418. 5424. 5426. 5446. 5464. 5483. Final Phase cut- in starts with serial number 5486 and sub. 950002 RE-220-49-0002 SEALENT GEN ADP 95 OPT N/A 0.0 0 26 Nov 2007 C 0.00 APU I 957045 SB RE220-49-7045 LOAD CONTROL 95 OPT N/A 0.0 0 26 Nov 2007 C 0.00 APU 1 VALVE RE-220-497275 Repl Deprime Valve. 957275 95 REC N/A 0.0 0 26 Nov 2007 C 0.00 APU 1 4140028.2 WM RE-220-497282 Repalce Inlet Duct & 957282 49 REC N/A 0.0 0 26 Nov 2007 C 0.00 APU I Hardware For Hourrneter RE-220-49-7350 Replace Plug And 957350 49 REC N/A 0.0 0 26 Nov 2007 C 0.00 APU Oil Filter Element G-CGUL G550 5176 Technical Bulletins Page 54 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620844 TYP C/W Source Code Description Effectivity ATA Status Logbook Work Order HRS LDG Date Cli MM REF M HRS Maintenance Notes Cert No RE-220-49-7359 Replace T-Wheel 957359 95 REC N/A 0.0 0 26 Nov 2007 C 0.00 APU I PN WE897994.I With WE897994.3 RE-220-49-7360 RPL Fuel Nozzle 957360 95 REC N/A 0.0 0 26 Nov 2007 C 0.00 APU I Bolts. MS9489-06 WI-05 957362 RE-220-49-7362 Replace Lube Pump 95 REC N/A 0.0 0 26 Nov 2007 C 0.00 APU t 957412 RE-220-49.7412 Replace Gearbox 95 REC N/A 0.0 0 26 Nov 2007 C 0.00 APU I 957413 RE-220-49.7413 Ins!! Spacer 5901 I ABI -150 on GIB Speed Sensor 95 REC N/A 0.0 0 26 Nov 2007 C 0.00 APU I 957428 RE-220-49.7428 INSP EXCITORS 95 OPT N/A 0.0 0 26 Nov 2007 C 0.00 APU I 957524 RE-220-49-7524 RPL FUEL CONT 95 OPT N/A 0.0 0 26 Nov 2007 C 0.00 APU I RE-220-49-7536 Replace Atomizer 957536 99 REC N/A 0.0 0 26 Nov 2007 C 0.00 APU 1 Gasket PN MS9372-031 957559 RE-220-49.7559 APU EGT MOD 95 OPT N/A 0.0 0 26 Nov 2007 C 0.00 APU 1 957570 SB RE220-49-7570 ECU UPGRADE 95 OPT N/A 0.0 0 26 Nov 2007 C 0.00 APU I 957621 RE-220-49-762I DS -1 COMBUSTER 95 OPT N/A 0.0 0 26 Nov 2007 C 0.00 APU I 957659 RE-220-49-7659 Replace Fuel Divider 95 OPT N/A 0.0 0 26 Nov 2007 C 0.00 APU I Solenoid Valve RE-220-49-7689 Remove/Replace 957689 95 OPT N/A 0.0 0 26 Nov 2007 C 0.00 APU I Ignition Exciter RE-220-49-7690 Add Deprime Valve 957690 EFF: Before SN P-298. 95 REC N/A 0.0 0 26 Nov 2007 C 0.00 APU I Assy, Inerterence Shield G-CGUL G550 5176 Technical Bulletins Page 55 of 164 20 Jan 2015 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620845 TYP C/W Source Code Description Effectivity ATA Status Logbook Work Order HRS LDG Date Cli MM REF M HRS Maintenance Notes Cert No RE-220-49-7694 One Time 957694 95 REC N/A 0.0 0 26 Nov 2007 C 0.00 APU I Insp:Replc of Coupling Clamp. T-Bolt 957761 RE-220-49-776I Replace Turbine 95 REC N/A 0.0 0 26 Nov 2007 C 0.00 APU I Bearing Oil Tubes 957771 RE-220-49-777I LOAD CONT VALVE 95 OPT N/A 0.0 0 26 Nov 2007 C 0.00 APU I RE-220-49-7772 Replace Spline 957772 95 REC N/A 0.0 0 26 Nov 2007 C 0.00 APU I Shaft PN WE8979977-3 957775 RE-220-49-7775 Replace Comp 95 REC N/A 0.0 0 26 Nov 2007 C 0.00 APU I Shroud PN W63827383-I RE-220-49-7795 SURGE CONTROL 957795 95 OPT N/A 0.0 0 26 Nov 2007 C 0.00 APU I VALVE SB RE220-49-7826 Removal / EFF: Before SN# P- 957826 49 REC N/A 0.0 0 26 Nov 2007 C 0.00 APU I Replace Ignitor Exciter 405. 957854 SB RE220-49-7854 Oil Sump Heater- EFF: APU SN#s 49 OPT NiA 0.0 0 26 Nov 2007 C 0.00 APU I Replace before P-4 I 4 957863 SB RE220-49-7863 Replace EFF: Before SN# P- 95 REC N/A 0.0 0 26 Nov 2007 C 0.00 APU I Electronic Control Unit 421. Honeywell recommends that this bulletin be accomplished at first return for any cause. at a Honeywell authorized ovhltrepair facility. SB RE220-49-7890 Replace Exhaust EFF: RE220 before SN 957890 49 OPT N/A 0.0 0 26 Nov 2007 C 0.00 APU I Gas Temp Sensor (EGT) P-473. 957935 SB49.7933R5 APU Approved Oils 49 INF 23 Oct 2014 I APU I G-CGUL G550 5176 Technical Bulletins Page 56 of 164 20 Jan 2015 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620846 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No ASC ASC 2A Digital Flight Data Recorder This rev cancels ASC 970021 31 CAN CAN 0.0 0 26 Nov 2007 C 0.00 Airframe Sys Upgrade 002 Dated Dec 5. 2005. Aircraft that have complied with ASC 002 have met the intent of this revision. This ASC has been cancelled by ASC 0028 dated Feb 20. 2008. ASC ASC 2B Digital Flight Recorder Cancelled by ASC GAC 970022 31 CAN CPN APPLETON 20.7 11 09 Apr 2008 C 0.00 System Upgrade 002C issued Airframe 11121/2008. FP549 CRS GIFR100Y ASC ASC 2C Digital Flight Data Recorder Effectivity: This service 970023 31 CAN CAN 0.0 0 24 Feb 2014 C Airframe System Upgrade (88 Parameters) change is applicable to G500 & G550 aircraft serial numbers 5001 and subsequent requiring Pan 135 certification. Cancelled by ASC 002D. Mx. Notes: This code has been cancelled. ASC ASC 2D Digital Flight Data Recorder Effectivity: This service 970024 31 OPT 19Jun 2012 Airframe System Upgrade (88 Parameters) change is applicable to G500 & G550 aircraft serial numbers 5001 and subsequent requiring Pan 135 certification. This revision. ASC 002D cancels and supersedes all previous versions of ASC 002. ASC ASC 4 PACK INLET VALVE Eff. Desc: 5001-5020. 970040 21 CAN CAN 0.0 0 26 Nov 2007 C 0.00 Airframe REPLACE This ASC cancelled ASC ASC 4A Aml Pack Inlet Valve This Service change is 970042 21 INF PIE 0.0 0 26 Nov 2007 C 0.00 Airframe Replacement for information purposes only. Permits the Intl of 1151582-6 Enviromental Control System. G-CGUL G550 5176 Technical Bulletins Page 57 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620847 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No ASC 970070 ASC 7 PDB CONNECTOR INSERTS Eff. Desc: 5017.5022. 24 OPT PIE 0.0 0 26 Nov 2007 C 0.00 Airframe ASC ASC 8 MAX GROSS WGT 75K GAC 970080 Canx see ASC 008A 11 CAN CM APPLETON 20.7 11 09 Apr 2008 C 11 0.00 PLACARD Airframe FP549 CRS G1FR100Y ASC ASC 8A Maximum Gross Weight This revision cancels 970081 CAN CAN 0.0 0 24 Feb 2014 C Airframe 75.000 Pounds and supersedes the original version of ASC 008. dated November 4. 2003. Operators of aircraft that have previously complied with ASC 008 shall observe and follow the procedures associated with the use of the placard as described in this revision and return the attached service reply card indicating that ASC 008A was previously complied with. Cancelled see ASC 008B Mx. Notes: This code has been cancelled. ASC ASC 8B Maximum Gross Weight To meet intent of this 970082 OPT 26 Oct 2011 Airframe 75.000 Pounds revision arc that previously cAv ASC 0081008A replace AFMS G550.2003-01 date 8.14-2003 with the AFMS in section II. ASC ASC 9 MAX ZERO FUEL GROSS Eff. Desc: ALL G550 GAC 970090 11 CAN CPN APPLETON 20.7 11 09 Apr 2008 C 11 0.00 WGT AIRCRAFT. Cancelled Airframe see ASC 009B FP549 CRS G1FR100Y G-CGUL G550 5176 Technical Bulletins Page 58 of 164 20 Jan 2015 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620848 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No ASC ASC 9A Maximum Zero Fuel Gross This service change is 970091 11 CAN CAN 0.0 0 24 Feb 2014 C Airframe Weight 53.500 Pounds - Placard applicable to all Installation Gulfstream G550 aircraft. This revision incorporates a redesigned placard assembly and updates the material list and accomplishment Instructions. This revision upersedes ASC 009. dated November 4. 2003. No further action is required for operators of aircraft that have previously complied with the original issue of ASC 009.Cancelled see ASC 0098 Mx. Notes: This code has been cancelled. ASC ASC 98 Maximum Zero Fuel Gross 970092 OPT 09 May 2011 I Airframe Weight 53,500 Pounds • Placard Installation ASC Eff. Dose. 5001-5999. 970110 ASC II G550 DATA PLATE INSTALL " 00 OPT 01 Sep 2003 I Airframe Converts GVSP to G550. "Record ASC" ASC ASC 14 Category II Annunciation - cancelled see ASC 970140 34 CAN CAN 0.0 0 24 Feb 2014 C Airframe Activation 14A Mx. Notes: This code has been cancelled. ASC ASC I4A Category II Annunciation - This ASC replaces 970141 Activation 34 OPT 13 Jun 2011 Airframe ASC 14. operators who have previously cAv ASC 14 are in compliance with this revision and should return reply card indicating previously complied with. Applies to 5001 and sub G-CGUL G550 5176 Technical Bulletins Page 59 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620849 TYP C/W Source Code Description Effectivity ATA Status ilLogbook Work Order HRS LDG Date C/I MM REF M HRS aintenance Notes Cert No ASC ASC 33 BONDED HONEYCOMB Eff. Dose: ALL G550 970330 53 OPT 05 Dec 2003 I Airframe PANELS AIRCRAFT. This is a record only ASC which incorporates drawing 1159SB50006 honeycomb floor panel repair-optional. ASC ABC 35A (Part I) EASA / JAA Con - GAMA 970351 Supersedes ASC 035 OPT CM 564.2 191 02 Jun 2009 C 0.00 Airframe Basic Requirements F090550 ASC ASC 35A (Part 2) EASA / JAA Con - GAMA 970352 Supersedes ASC 035 OPT CM 564.2 191 02 Jun 2009 C 0.00 Airframe Basic Requirements F090550 ASC 970391 ASC 39 PT2 WING RIB REINFORCE Ell. Desc: 5001.5051. 57 REC PIE 0.0 0 26 Nov 2007 C CB 3 0.00 Airframe ASC ASC 46A Navigation Position Lights - This revision removes 970461 33 OPT PIE 31 May 2011 Airframe LED Navigation Light Installation the LED life limit replacement statement. Operators of aic that have previously complied with ASC 46. should return attached service reply card indicating the ASC was previously complied with. ASC ASC 47 WATER SYSTEM EFFECTIVITY: 970470 38 OPT PIE 0.0 0 26 Nov 2007 C 0.00 Airframe IMPROVEMENT Applicable to SeN 5001 -5013/5015-5099/ NOTE: AC SIN 5090- 5099 will ONLY perform Steps E. I. and J of the "Modification Instructions' portion of this ASC. / This or a similar change will be installed in production S/N 5100 and Subs. G-CGUL G550 5176 Technical Bulletins Page 60 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620850 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No ASC ASC 49 Lightning Sensor System This Service Change gs appleton 970490 34 OPT CPN 21.8 12 30 Apr 2008 C 0.00 Airframe (LSS) Installation is applicable to AIC Serial No# 5001 and Sub. Aircraft that have previously complied with ST No.ST02915AT-D meet the intent of ASC 049. ASC ASC 53 Comm Management Fnc EFF: 5001 and Sub. 970530 23 CAN CAN 0.0 0 24 Feb 2014 C Airframe Arinc Direct-Datalink cancelled ref ASC 53A Mx. Notes: This code has been cancelled. ASC ASC 53A Communications 5001 and sub. AIC 970531 OPT 05 Dec 2011 Airframe Management Function ARINC Direct which have previously Datalink Service Provider cAv ASC 53 should signet( this ASC as previously complied with. ASC ASC 55 WaterMaste Sys Component Eff: Part 1 is applicable 970550 38 OPT PIE 0.0 0 26 Nov 2007 C 0.00 Airframe Replacement Part 1 to SN# 5001-5099 only. Pan 2. 3. 4 and 5 are applicable to SN# 5001-5084 only. ASC ASC 55 WaterMaste Sys Component Eff: Part 1 is applicable 970551 38 OPT PIE 0.0 0 26 Nov 2007 C 0.00 Airframe Replacement Part 2 to SN# 5001-5099 only. Pan 2. 3. 4 and 5 are applicable to SN# 5001-5084 only. ASC ASC 55 WaterMaste Sys Component Eff: Part 1 is applicable 970552 38 OPT PIE 0.0 0 26 Nov 2007 C 0.00 Airframe Replacement Part 3 to SN# 5001-5099 only. Pan 2. 3. 4 and 5 are applicable to SN# 5001-5084 only. ASC ASC 55 WaterMaste Sys Component Eff: Part 1 is applicable 970553 38 OPT PIE 0.0 0 26 Nov 2007 C 0.00 Airframe Replacement Part 4 to SN# 5001-5099 only. Pan 2. 3. 4 and 5 are applicable to SN# 5001-5084 only. G-CGUL G550 5176 Technical Bulletins Page 61 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620851 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No ASC ASC 55 Water'Waste Sys Component Eff: Part 1 is applicable 970554 38 OPT PIE 0.0 0 26 Nov 2007 C 0.00 Airframe Replacement Part 5 to SN# 5001.5099 only. Pan 2. 3. 4 and 5 are applicable to SW/ 5001.5084 only. ASC ASC 57A • Electrical Lines-Contact EFF: 5001.5149 - Ref 970571 24 MAN P/E 03 Sep 2008 I Airframe Prevention (CB 32 Aml) CB 32 Am 1 - Aircraft having previously complied with ASC 057 meet the intent of this revision. ASC ASC 61 Synthetic Vision-Primary ASC 907 - 970610 31 CAN CAN 0.0 0 24 Feb 2014 C Airframe Flight Display (SV-PFD) Installation PlaneView® Master Operating Software Update (SV-PFD) is required for aircraft serial numbers 5001 - 5188. Superceded see ASC 6IA Mx. Notes: This code has been cancelled. ASC ASC 61 Aml- Synthetic Vision This service change 970611 CAN CAN 0.0 0 24 Feb 2014 C Airframe Primary Flight Display (SV-PF) amendment is for information only.This amendment replaces pages I and 3 of 5 of the original issue ASC 061 dated September 15.2008 with new pages 1 and 3 of 5 of this amendment. Superceded see ASC 61A Mx. Notes: This code has been cancelled. G-CGUL G550 5176 Technical Bulletins Page 62 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620852 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No ASC ASC 61A Synthetic Vision•Primary This service change 970612 CAN CAN 0.0 0 24 Feb 2014 C Airframe Flight Display (SV•PFD) Installation revision will supersede the original issue of ASC 061 dated September 8, 2008. incorporate ASC 061 Amt dated December 19. 2008 and is now reissued as ASC 061A. Aircraft having previously complied with ASC 061 may continue to operate at version 1.0 with no further action required. Prerequisites: G550 ASC 908 • PlaneView Master Operating Software Update (Cart Fox) Mx. Notes: This code has been cancelled. ASC ASC 61A Amt Synthetic Vision • This service change 970613 CAN CAN 0.0 0 24 Feb 2014 C Aiiirame Primary Fight Display (SV•PFD) amendment is for Installation information only. The installation of ASC 061A is now authorized for aircraft operating under EASA/JAA regulations and an EASA project number has been provided. Additionally. installation of this service change is no longer restricted to Gulfstream Aerospace or General Dynamics Aviation Services (GDAS) facilities. Mx. Notes: This code has been cancelled. G-CGUL G550 5176 Technical Bulletins Page 63 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620853 TYP C/W Source Code Description Effectivity ATA Status ilLogbook Work Order HRS LDG Date C/I MM REF M HRS aintenance Notes Cert No ASC ASC 618 Synthetic Vision.Primary This service change 970614 31 OPT 31 Oct 2011 Airframe Flight Display (SV-PFD) Installation applicable to aircraft serial numbers 5001 and subsequent. This aircraft service change revision supersedes ASC 061. Operators of aircraft that have any version of ASC 061 installed require no further action. Operators of aircraft with the original issue of ASC 061 or ASC 061 Amt do not return a service reply card for ASC 0618. Only operators of aircraft with ASC 061A or later installed should complete and return the service reply card indicating 'previously complied with'. ASC ASC 63 Wing Fuel Transfer Sys Mid- EFF: 5001and Sub. 970630 57 CAN CAN 0.0 0 26 Nov 2007 C 0.00 Airframe Wing Ejector Mod Ths ASC cancelled see 63A ASC ASC 63A Wing Fuel Transfer Sys EFF: 5001and 970631 57 CAN CAN 0.0 0 01 Apr 2013 C 0.00 Airframe Mid-Wing Ejector Mod Part 1 Sub.Cancelled by ASC 0638 Mx. Notes: This code has been cancelled. See Compliance Remarks by cricking Show Remarks link. ASC ASC 63A Wing Fuel Transfer Sys EFF: 5001 and Sub. 970632 57 CAN CAN 0.0 0 01 Apr 2013 C 0.00 Airframe Mid-Wing Ejector Mod Part 2 Cancelled by ASC 0638 Mx. Notes: This code has been cancelled. See Compliance Remarks by cricking Show Remarks link. ASC ASC 638 Wing Fuel Transfer Sys Effectivity: 5001 and 970633 57 OPT 29 Mar 2013 I Airframe Mid-Wing Ejector Mod Part 1 Sub. ASC ASC 638 Wing Fuel Transfer Sys Effectivity: 5001 and 970634 57 OPT 29 Mar 2013 Airframe Mid-Wing Ejector Mod Part 2 Sub. ASC ASC 638 Wing Fuel Transfer Sys Effectivity: 5001 and 970635 57 OPT 29 Mar 2013 I Airframe Mid-Wing Ejector Mod Part 3 Sub. G-CGUL G550 5176 Technical Bulletins Page 64 of 164 20 Jan 2015 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620854 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No ASC ASC 65 Runway Awareness Advisory EFF: Acft Serial 970650 34 CAN CAN 0.0 0 26 Nov 2007 C 0.00 Airframe System (RAAS)•Installation Number 5001 and Sub. ASC ASC 65A Runway Awareness This ASC supercedes 970651 34 OPT 07 Mar 2008 I Airframe Advisory System-Installation ASC 65 ASC ASC 66 Auxiliary Power Unit (APLI) Effectivity: SIN 5001- 970660 51591 This or a similar 49 MAN PIE 07 Apr 2008 I Airframe Bond Strap Installation change will be installed in production on aircraft. serial number 5160 and subsequent / Concurrent Requirement: G550 Customer Bulletin 65 ASC ASC 69A Engine Electronic Controller Supercedes ASC 69. 970691 73 OPT PIE 30 Jul 2008 Airframe (EEC) Upgrade to V1.3/ EECU3000 incorporates SB- BR700.73-101496 Rev 1. Effectivity 5001- 5151. ASC ASC 69A Am1 Engine Electronic The purpose of this 970692 73 INF PIE 21 Jan 2009 Airframe Controller (EEC) Upgrade to VI.31 amendment is to EECU3000 correct the European Aviation Safety Agency (EASA) Project Number on Page 1 of ASC 069A dated July 30. 2008. This amendment is for information only. Effectivity 5001.5151 ASC ASC 70 Nose Landing Gear Door EFF: G550 aircraft, GAC 970700 32 MAN CM APPLETON 20.7 II 09 Apr 2008 C 0.00 Actuator Modification serial numbers 5001- Airframe 518711 NOTE: FP549 Mandatory for SIN 5001 - 5177 per CB 58 issued 12/10/2007 CRS G1FR100Y ASC ASC 71 Micro Quick Access Recorder Cancelled see ASC GALLTN 970710 31 CAN CM 602.6 199 30 Jun 2009 C 0.00 Airframe Installation 071A FL012134 G-CGUL G550 5176 Technical Bulletins Page 65 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620855 TYP C/W Source Code Description Effectivity ATA Status ilLogbook Work Order HRS LDG Date C/I MM REF M HRS aintenance Notes Cert No ASC ASC 71A Micro Quick Access 970711 31 OPT PIE 19 Aug 2013 I Airframe Recorder Installation ASC ASC 72 Medeco Door Locks 970720 Effectivity 5001.5204 52 OPT 20 May 2008 I Airframe Installation ASC ASC 73 Nose Gear Uplock Hook Concurrent 970730 32 CAN CAN 0.0 0 24 Feb 2014 C Airframe Spring Replacement requirement = CB 69. SiN 5001.5204. Mx. Notes: This code has been cancelled. ASC ASC 73A Nose Gear Uplock Hook Concurrent Jet Aviation 970731 32 MAN CPN Geneva 513.0 177 03 Feb 2009 C 0.00 Spring Replacement Requirement: G550 Airframe Customer Bulletin GVBTC003 Number 69. SIN 5O01- 5204.This revision supersedes ASC 073. dated July 30. 2008. and is now issued as ASC 073A. Aircraft that have previously complied with ASC 073 meet the intent of this revision and should return the attached service reply card indicating that ASC 073 was previously complied with. ASC ASC 74 Dual Brake Metering Valve 970740 32 CAN CAN 19 Nov 2008 I Airframe Replacement G-CGUL G550 5176 Technical Bulletins Page 66 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620856 TYP C/W Source Code Description Effectivity ATA Status ilLogbook Work Order HRS LDG Date C/I MM REF M HRS aintenance Notes Cert No ASC ASC 74A Dual Brake Metering Valve This service change 970741 32 OPT 23 Jan 2009 I Airframe Replacement revision corrects the part number for the hydraulic line from PIN 1159S857960-25 to 11595857960-19. This revision supersedes ASC 074. dated November 19. 2008. and is now issued as ASC 074A. This service change is applicable to aircraft. serial numbers 5001-5209. This or a similar change will be installed in production on aircraft. serial numbers 5210 and subsequent. ASC ASC 74A AM1 Dual Brake Metering This service change 970742 OPT 22 Nov 2010 I Airframe Valve Replacement amendment corrects the 24 month warranty compliance statement in ASC 074A. ASC ASC 75 - LED Tail Position Light Effectivity: SIN 5001 - 970750 33 CAN CAN 2332.2 708 25 Feb 2012 C 0.00 Airframe Installation 5181 This or a similar change will be installed in production on SiN 5182 & Subs fl (NOTE: Two Lights • See CMP Codes 334065 (Upper) and 334066 (Lower)) . Cancelled see ASC 75A Mx. Notes: Superceded by ASC 075A G-CGUL G550 5176 Technical Bulletins Page 67 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620857 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No ASC ASC 75A - LED Tail Position Light Effectivity: SIN 5001 970751 33 OPT CM 2332.2 708 25 Feb 2012 C 0.00 Airframe Installation -5181. Aircraft operators who have previously complied with ASC 075 should verity proper orientation of the light assembly in accordance with Figure 1. Mx. Notes: See WP FL016369 GiStream Luton for details ASC ASC 76 PlaneView Avionics 970760 Elf 5001.5188 31 OPT 15 Sep 2008 I Airframe Enhancement (SV-PFD) ASC ASC 76 Am1 PlaneView Avionics This amendment is for 970761 31 INF 19 Dec 2008 I Airframe Enhancement (SV-PFD) information only. and restricts the ASC installation to Gulfstream or GDAS facilities. The EASA project number also has been amended. ASC ASC 77 - Decal Installation Remote See 970771 // 970770 12 CAN CM 1787.4 543 08 Mar 2011 C 0.00 Airframe Oil Servicing Panel Effectivity: This service change is applicable to aircraft. serial numbers 5001- 5191. excluding aircraft having ASC 063 / 063A. This or a similar change will be installed in production on aircraft serial number 5192 and subsequent. Mx. Notes: work pack FL014715 G-CGUL G550 5176 Technical Bulletins Page 68 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620858 TYP CNV Source Code Description Effectivity IATAI Status Logbook Work Order HRS LOG Date cn MM REF M HRS 'Maintenance Notes Cert No ASC 970771 ASC 77A • Decal Installation - Effectivity: This 12 OPT 04 Nov 2011 Airframe Remote Oil Servicing Panel service change is applicable to aircraft. serial numbers 5001- 5191. excluding aircraft having ASC 063 / 063A. This or a similar change will be installed in production on aircraft serial number 5192 and subsequent. Aircraft operators who have previously complied with ASC 077 are in compliance with this revision and should return the attached service reply card indicating this ASC was previously complied with. ASC ASC 78 Potable Water System Purge. SiN 5001.5192 Jet Aviation 970780 38 MAN Cm Geneva 513.0 177 03 Feb 2009 C 0.00 Plackard excluding Airframe 5014,5037,5044,5069, GVBTC003 5132,5188,5189,5191. Concurrent requirement CB 71. ASC ASC 79 Main landing Gear Concurrent Jet Aviation 970790 32 MAN CM Geneva 513.0 177 03 Feb 2009 C 0.00 Emergency Line Modification Requirement: 6550 Airframe Customer Bulletin GVBTC003 Number 72 G-CGUL G550 5176 Technical Bulletins Page 69 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620859 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No ASC ASC 80 Modification - Wing Rear Concurrent Reqmt:CB 970800 57 REQ CNJ 1787.4 543 08 Mar 2011 C 0.00 Airframe Beam • Flight Spoiler Actuator 83. This ASC is Attachment Point applicable to 5001. 5230. NC in compliance with this mod per drawing 1159S850091 meet the intent of this ASC. Operators of those aircraft should return service card indicating that ASC 080 was previously complied with. After compliance with ASC 80. remove the frequency on code 571200. Adjust next due time from compliance of ASC on codes 571301, 571302.571303• 571304 as they may apply. Mx. Notes: AMENDED TO ALIGN WITH COMPLIANCE OF CB83 ASC ASC 80 AM1 Meditation - Wing This service change is 970801 57 INF Cm 1787.4 543 08 Mar 2011 C 0.00 Airframe Rear Beam - Flight Spoiler Actuator applicable to aircraft Attachment Point serial numbers 5001- 5230. Aircraft in compliance with this modification per drawing 1159SB50091 meet the intent of this ASC. Operators of those aircraft should return the attached service reply card indicating that ASC 080 was previously complied with. See CB 83 AM1 Mx. Notes: WHEN ASC80 INCORPORATED RAISE CODES 571301,571302,571303 & 571304 & DELETE 571200 G-CGUL G550 5176 Technical Bulletins Page 70 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620860 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No ASC ASC 80 AM2 Meditation - Wing This service change 970802 57 INF cm 1787.4 543 08 Mar 2011 C 0.00 Airframe Rear Beam - Flight Spoiler Actuator amendment updates Attachment Point the required man• hours called out in the original issue of ASC 080. dated May 21, 2009. This amendment is for information only. ASC ASC 82 Tail Compartment Ladder - Concurrent 970820 25 CAN CAN 18 Dec 2008 I Airframe Hinge Pin and Placard Requirement: G550 Customer Bulletin Number 80 This service change is applicable to aircraft, serial numbers 5002, 5099, 5100, 5160- 5230 and 5103.6159 having ASC 062. This or a similar change will be installed in production on aircraft serial number 5231 and subsequent. this ASC is canceled by ASC 82A ASC ASC 82A Tail Compartment Ladder • This service change is LTN 970821 25 REQ CM 742.4 251 02 Oct 2009 C 0.00 Airframe Hinge Pin and Placard applicable to aircraft. FLO 12546 serial numbers 5002, 5099. 5100, 5102, 5160.5235, and 5103- 5159 having ASC 062. The original issue of ASC 082. dated December 18, 2008, is canceled and superseded by ASC 082k Operators who have previously complied with ASC 082 must perform Step B. of this revision. Concurrent Requirement:G550 Customer Bulletin Number 80A G-CGUL G550 5176 Technical Bulletins Page 71 of 164 20 Jan 2015 02015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620861 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LDG Date CA MM REF M HRS aintenance Notes Cart No ASC ASC 82A AM1 Tail Compartment This service change is LTN 970822 INF CM 778.0 262 30 Oct 2009 C 0.00 Airframe Ladder • Hinge Pin and Placard applicable to aircraft. FL012675 serial numbers 5002. 5099, 5100, 5102, 5160.5235, and 5103- 5159 having ASC 062. This service change amendment corrects the pan number of clear epoxy paint called out in ASC 082k dated February 27. 2009. This amendment is for information only. Mx. Notes: CM AS ASC082A ALREADY CM. ASC ASC 83 PlaneView Avionics This service change is 970830 CAN CAN 0.0 0 28 Sep 2010 C 0.00 Airframe Enhancement (Cart Fox) applicable to aircraft serial numbers 5001 - 5274. Cancelled ref ASC 83A ASC ASC 83A PlaneView Avionics This service change 970831 OPT CM 2354.3 711 19 Apr 2012 C 0.00 Airframe Enhancement (Cart Fox) revision supersedes the original issue of ASC 083 dated June 4, 2010. All aircraft having previously complied with either the In-Service Evaluation (ISE) or the released version of ASC 083 must comply with this revision. Mx. Notes: See FL016471 I FL016474 ASC This service change is 970840 ASC 84 Enhanced Navigation CAN CAN 0.0 0 24 Feb 2014 C Airframe applicable to aircraft serial numbers 5001 and subsequent.Prerequisit es: G550 ASC 908 - PlaneView Master Operating Software Update (Cart Fox) Cancelled ref ASC MA Mx. Notes: This code has been cancelled. G-CGUL G550 5176 Technical Bulletins Page 72 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620862 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No ASC Prerequisites: G550 970841 ASC 84A Enhanced Navigation CAN CAN 0.0 0 24 Feb 2014 C Airframe ASC 908 • PlaneView8 Master Operating Software Update (Cart Fox). This service change revision cancels and supersedes the original issue of ASC 084 datedJune 4. 2010 and is now reissued as ASC 084A. Aircraft having previously complied with either theln•Service Evaluation (ISE) or the released version of ASC 084 require no further action. Complete and return the service reply cardas "previouslycomplied with" noting the date of installation. Mx. Notes: This code has been cancelled. ASC This service change 970842 ASC 848 Enhanced Navigation 34 OPT 22 Dec 2011 Airframe revision moves the activation of CPDLC functionality to a separate ASC (096) and revises the modification instructions to address changes incorporated to the aircraft during initial phase manufacturing. This service change revision supersedes all previous versions of ASC 084 and is now reissued as ASC 0848. G-CGUL G550 5176 Technical Bulletins Page 73 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620863 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cr' MM REF M HRS aintenance Notes Cert No ASC Prerequisites: G550 970850 ASC 85 XM Weather Installation CAN CAN 0.0 0 24 Feb 2014 C Airframe ASC 908 - PlaneView Master Operating Software System Software Update (Cert Fox) Cancelled ref ASC 85A Mx. Notes: This code has been cancelled. ASC This service change 970851 ASC 85A XM Weather Installation OPT 19 Aug 2010 I Airframe revision cancels and supersedes the original issue of ASC 085 dated June 9. 2010 and is now reissued as ASC 085A. Aircraft having previously complied with either theln- Service Evaluation (ISE) or the released version of ASC 085 require no further action. Complete and return the service reply card as 'previously complied with' noting the date of installation.Prerequisit es: G550 ASC 908 - PlaneView Master Operating Software System Software Update (Ceti Fox) ASC ASC 86 Entrained Air Removal This service change is 970860 OPT PIE Airframe System Installation applicable to aircraft serial numbers 5001-5102. ASC ASC 87 Canadian Certification 970870 OPT 07 Jul 2010 Airframe Requirements ASC ASC 89 Stage 4 Noise Standards - Cancelled see ASC 970890 CAN CAN 0.0 0 20 Aug 2013 C 0.00 Airframe Certification 089A. Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link. G-CGUL G550 5176 Technical Bulletins Page 74 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620864 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date CA MM REF M HRS Ilaintenance Notes Cert No ASC 970891 ASC 89A Stage 4 Noise Standards • P/E 20 Aug 2013 I OPT Airframe Certification ASC ASC 90 Auxiliary Power Unit (APU) This service change is CAN 0.0 0 06 Sep 2011 C 0.00 970900 CAN Airframe Enclosure Thermal Barrier applicable to aircraft Installation serial numbers 5001.5249, excluding 5211 and 5225. Cancelled see ASC 90A ASC ASC 90 AM1 Auxiliary Power Unit This service change 0 06 Sep 2011 C 0.00 970901 CAN CAN 0.0 Airframe (APU) Enclosure - Thermal Barrier amendment corrects Installation the effectivity called out in the original issue of ASC 090.No further action is required for operators of aircraft that have previously complied with the original issue of ASC 090. dated August 30, 2010. This service change is applicable to aircraft serial numbers 5001.5249, excluding 5011 and 5225. Cancelled see ASC 90A ASC ASC 90A Auxiliary Power Unit (APU) This revision 10 Feb 2011 I 970902 OPT Airframe Enclosure - Thermal Barrier supersedes ASC 090, Installation dated August 30, 2010. and ASC 090 AM1, dated September 10, 2010. No further action is required for operators of aircraft that have previously complied with ASC 090 and 090 AM1.This service change is applicable to aircraft serial numbers 5001- 5249. excluding 5011 and 5225. G-CGUL G550 5176 Technical Bulletins Page 75 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620865 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No ASC ASC 91 Enhanced Baggage Door This service change is 970910 CAN CAN 0.0 0 24 Feb 2014 C Airframe Seal System • Installation applicable to G550 aircraft, serial numbers 5001 • subsequent Mx. Notes: This code has been cancelled. ASC ASC 91A Enhanced Baggage Door This service change is 970911 52 OPT 01 Nov 2011 Airframe Seal System • Installation applicable to G550 aircraft, serial numbers 5001 • subsequent. Aircraft operators who have previously complied with ASC 091 are in compliance with this revision (ASC 091A) and should return the service reply card(s) marked "Previously complied with." ASC ASC 92 Communication Management Concurrent Req:To GAC LTN 970920 23 OPT CM 2692.3 796 12 Jan 2013 C Akirame Function (CMF) Satcom Direct • activate the datalink LMX000417 Datalink Service Provider service. Operators will be required to fill out a Satcom Direct FlightDeck Freedom" Customer Service Agreement. Contact Satcom Direct at 321. 777-3000 or email sales@satcomdirect.c om to coordinate a datalink service subscription. Additionally. Operators must submit a cancellation request to their previous service provider. Contact Honeywell's Data Center at 425.685- 8100 or ARINC Direct at 866.321.6060 to discontinue the original subscription. UK.145.00883 G-CGUL G550 5176 Technical Bulletins Page 76 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620866 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No ASC ASC 93A Aileron Cable Fairleads at This service change is GAC-LTN 970931 27 OPT CM 2354.6 711 19 Apr 2012 C Airframe Sponson Rib Installation applicable to aircraft FL016471 serial numbers 5001- 5302. Aircraft operators who have previously complied with ASC 093 are in compliance with this revision and should return the attached service reply card indicating this ASC was previously complied with. UK.145.00883 ASC ASC 94 Landing Gear Door Close - 5001.5314. 970940 CAN CAN 0.0 0 28 Jun 2011 C 0.00 Airframe Restrictor Concurrent requirement CB 110. Cancelled see ASC 094A ASC ASC 94A Landing Gear Door Close 5001.5314. 970941 CAN CAN 0.0 0 24 Feb 2014 C Airframe Restrictor Concurrent requirement CB 110A. Cancelled see ASC 948 Mx. Notes: This code has been cancelled. ASC ASC 94B Landing Gear Door Close - Aircraft operators who GAC LTN 970942 OPT CAN 2849.4 833 09 Apr 2013 C Airframe Restrictor have previously BMX000145 complied with ASC 094A are in compliance with this revision (ASC 0948) and should return the service reply card(s) marked Previously complied with? Mx. Notes: MH - Do at next 3C. circa March 2014 UK.145.00883 G-CGUL G550 5176 Technical Bulletins Page 77 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620867 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date C/I MM REF M HRS aintenance Notes Cert No ASC ASC 95 • PlaneView Avionics Effectivity: This 970950 31 CAN CAN 0.0 0 25 Apr 2013 C 0.00 Airframe Enhancement service change is applicable to aircraft serial numbers 5309 5339. This or a similar change will be installed during initial phase manufacturing on aircraft serial number 5340 and subsequent. Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link ASC 970952 ASC 95B • PlaneView Avionics Effectivity: 5001 - 31 OPT 24 Apr 2013 I Airframe Enhancement 5422. This service change revision supersedes all previous versions of ASC 095 and is now reissued as ASC 0958. Aircraft having previously complied with ASC 095 should upgrade to this latest revision during regularly scheduled maintenance. ASC This service change 970960 ASC 96 - CPDLC - FANS 1/A 23 OPT 22 Dec 2011 Airframe activates the Controller Pilot Data Link Communication (CPDLC) functionality. Aircraft operating under FAA regulations will require FM Airplane Flight Manual (AFM) Revision 30, or later approved version. as a result of this service change. Aircraft operating under EASA /JAA regulations will require G500/G550 AFM Supplement Number EASA.G550-2010.01, or later approved version, as a result of this service change. G-CGUL G550 5176 Technical Bulletins Page 78 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620868 TYP C/W Source Code Description Effectivity ATA Status ilLogbook Work Order HRS LDG Date C/I MM REF M HRS aintenance Notes Cert No ASC Effectivity This service 970970 ASC 97 - Data Link Recording 31 CAN PIE 22 Dec 2011 Airframe change is applicable to aircraft serial numbers 5309 and subsequent. ASC Effectivity: This service 970971 ASC 97A - Data Link Recording 31 OPT PIE 30 Aug 2012 Airframe change is applicable to aircraft serial numbers 5309 5374. ASC ASC 98 - Retract Braking (Main 970981 "record only ASC" OPT PIE 18 Mar 2013 I Airframe Wheel De-spin) Brake Metering Valve Upgrade and Hydraulic Flow Control Restrictor Replacement ASC ASC 99 - Aileron And Elevator Power This service change is 970990 27 CAN CAN 0.0 0 01 Apr 2013 C 0.00 Airframe Disconnect - Removal applicable to aircraft serial numbers 5001- 5389. Concurrent Requirement - CB 125. Cancelled see 970991 Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link. ASC ASC 99A - Aileron And Elevator This service change is GAC LTN 970991 OPT CPN 2849.4 833 04 Apr 2013 C Airframe Power Disconnect Removal applicable to aircraft BMX000145 serial numbers 5001- 5389. Concurrent Requirement - CB 125A. UK.145.00883 ASC ASC 102 60 Hz Power Generation - Effectivity: This service 971020 24 OPT 15 Apr 2014 I Airframe 60 Hz Converter Equipment change is applicable to Modification aircraft serial numbers 5001.5068. excluding 5003. This or a similar change is installed in production on aircraft serial number 5069 and subsequent. ASC 971030 ASC 103 TCAS 7.1 Installation 5001.5379 OPT 12 Jun 2012 Airframe ASC ASC 104 Aileron Cade Penetrations This ASC is applicable GAC LTN 971040 OPT CPN 2849.4 833 11 Apr 2013 C Airframe at FS 576.5 Floor Beam - Rework to aircraft serial BMX000145 numbers 5001- 5404. UK.145.00883 G-CGUL G550 5176 Technical Bulletins Page 79 of 164 20 Jan 2015 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620869 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No ASC ASC 105 • Automatic Dependent Effectivity: 5001 - Sub. 971050 34 OPT 24 Apr 2013 I Airframe Surveillance - Broadcast (ADS-B) Out Prerequisites ASC Installation 9098 — PlaneView Master Operating System Software Update or later. or production equivalent and ASC 084 - Enhanced Navigation Prior to, or at the time this ASC is ordered. ASC ASC 105A • Automatic Dependent Effectivity: This service 971051 34 OPT 25 Jul 2014 Airframe Surveillance - Broadcast (ADS-B) Out change is applicable to Installation aircraft serial numbers 5001 — subsequent. ASC ASC 106 Fuel Quantity Signal 5001-5409, excluding 971060 OPT 08 Feb 2013 I Airframe Conditioner - Revision G Software arc with ASC 63 ASC ASC 107 • Planeview Avionics Effectivity: 5001 - 971070 31 OPT 24 Apr 2013 Airframe Enhancement 5422. ASC 907 — PlaneView MOS Software Update (Gen Echo) or later; or production equivalent. Prior to, or at the time this ASC is ordered. ASC 910 • PlaneView MOS Software Update must be installed in conjunction with this service change. ASC ASC 108 • APU Enclosure Non- Effectivity: This service 971080 53 OPT 30 Jul 2014 Airframe Compliant Sealant - Modification change is applicable to aircraft serial numbers 5001.5249, excluding 5011, 5225 and 5245. ASC ASC 110 Cockpit Portable Fire 971100 5072.5411 CAN CAN 0.0 0 02 Oct 2013 C 0.00 Airframe Extinguisher • Relocation Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link G-CGUL G550 5176 Technical Bulletins Page 80 of 164 20 Jan 2015 @ 2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620870 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No ASC ASC 110A (Part 1) Cockpit Portable This ASC is separated 971101 OPT 01 Oct 2013 Airframe Fire Extinguisher / Pilot Seat Track into 2 parts. Part I Stop - Relocation (code 971101), applicable to aircraft serial numbers 5072- 5411. Part II (code 971102), applicable to aircraft serial numbers 5412-5438. ASC ASC 110A (Part 2) Cockpit Portable This ASC is separated 971102 OPT PIE 01 Oct 2013 Airframe Fire Extinguisher! Pilot Seat Track into 2 parts. Part I Stop - Relocation (code 971101), applicable to aircraft serial numbers 5072- 5411. Part II (code 971102), applicable to aircraft serial numbers 5412-5438. ASC ASC 111 • Mandates Package Effectivity: Aircraft 971110 23 CAN CAN 0.0 0 29 Jul 2014 C 0.00 Airframe (CPDLC / ADS•B Out) 5001 and Sub. Prerequisites ASC 9098 — PlaneView Master Operating System (MOS) Software Update or later, or production equivalent. Cancelled by ASC 111A(971111). Mx. Notes: This code has been cancelled. See Compliance Remarks by ckcking Show Remarks link ASC ASC 111A • Communication Effectivity: This service 971111 23 OPT 25 Jul 2014 Airframe Navigation (ATA 23 / 34) Mandates change is applicable to Package (CPDLC ADS-B Out) aircraft serial numbers 5001 and subsequent. ASC ASC 112 Elevator Hardover Concurrent GAO LTN 971120 OPT CNV 3444.5 949 04 Nov 2014 C 0.00 Airframe Prevention System (HOPS) • Requirement G550 BMX000542 Improvement Customer Bulletin Number 145. This service change is applicable to aircraft serial numbers 5001 • 5468. UK.145.00883 G-CGUL G550 5176 Technical Bulletins Page 81 of 164 20 Jan 2015 02015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620871 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No ASC ASC 113 • Planeview Avionics Effectivity: This service 971130 31 CAN CAN 0.0 0 18 Sep 2014 C 0.00 Airframe Enhancement change is applicable to aircraft serial numbers 5001 — 5473. This, or a similar change. will be Installed during initial phase manufacturing on aircraft serial numbers 5474 and subsequent. Cancelled by ASC 113A(971131). Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link ASC ASC 113A • Planeview Avionics Effectivity: This service 971131 31 OPT 17 Sep 2014 Airframe Enhancement change is applicable to aircraft serial numbers 5001 — 5473. This, or a similar change. will be installed during initial phase manufacturing on aircraft serial numbers 5474 and subsequent. ASC ASC 114A • Automatic Dependent Effectivity: This service 971141 34 OPT PIE 25 Jul 2014 Airframe Surveillance - Broadcast (ADS-B) Out change is applicable to Version 1 Installation aircraft serial numbers 5423. 5429, 5434, 5436 — 5439, 5441. 5443 — 5466. This, or a similar change, will be installed during initial phase manufacturing on aircraft serial numbers 5467 and subsequent. ASC ASC 116 • Nose Landing Gear (NLG) Effectivity: This 971160 32 OPT 27 Jun 2014 Airframe Harness • Installation service change is applicable to aircraft serial numbers 5001. 5424. G-CGUL G550 5176 Technical Bulletins Page 82 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620872 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No ASC ASC 120 - Engine Driven Pump Effectivity: This service GAC LTN 971200 29 OPT CM 3444.5 949 23 Oct 2014 C Airframe (EDP) Case Drain Hose Routing In change is applicable to BMX000542 Left Pylon aircraft serial numbers 5001.5494. This or a similar change will be installed during initial phase manufacturing on aircraft. serial number 5495 and subsequent. UK.145.00883 ASC 979000 ASC 900 PLANEVIEW MOS UPDATE Eff. Dose: 5001.5029. 31 OPT PIE 0.0 0 26 Nov 2007 C 0.00 Airframe ASC 979030 ASC 903 PLANEVIEW MOS UPDATE EFF:500I -5077 31 OPT PIE 0.0 0 26 Nov 2007 C 0.00 Airframe ASC ASC 907 PlaneView Master Operating Eft 5001.5188 979070 31 OPT 15 Sep 2008 I Airframe System Software Update (SV-PFD) ASC ASC 907 Am1 PlaneView Master This amendment is for 979071 31 OPT 19 Dec 2008 I Airframe Operating System Software Update (S information only. and restricts the ASC installation to Gulfstream or GDAS facilities. The EASA project number also has been amended. G-CGUL G550 5176 Technical Bulletins Page 83 of 164 20 Jan 2015 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620873 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS alntenance Notes Cert No ASC ASC 908 PlaneView Master Operating This service change 979080 CAN CAN 0.0 0 24 Feb 2014 C Airframe System Software Update (Cert Fox) installs the PlaneView Master Operating System software EB7031236• 00319 on G550 aircraft serial numbers 5001 • 5274 and EB7031236• 00320 on aircraft serial numbers 5276 • 5285. This ASC must be installed in conjunction with G550 ASC 083. Prerequisites: G550 ASC 907 • PlaneView Master Operating System Software Update pert Echo) Cancelled ref ASC 90M Mx. Notes: This code has been cancelled. ASC ASC 908A PlaneView Master This service change 979081 OPT CM 2354.3 711 19 Apr 2012 C 0.00 Airframe Operating System Software Update revision supersedes pen Fox) the original issue of ASC 908 dated June 4, 2010. All aircraft having previously complied with either the In-Service Evaluation (ISE) or the released version of ASC 908 must comply with this revision. Prerequisites: G550 ASC 907 • PlaneView Master Operating System Software Update pen Echo) Concurrent Requirements: G550 ASC 083A - PlaneView Avionics Enhancement (Cert Fox) must be installed in conjunction with this service change. Mx. Notes: See F1016471 / FLO' 6474 G-CGUL G550 5176 Technical Bulletins Page 84 of 164 20 Jan 2015 02015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620874 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date C/I MM REF M HRS aintenance Notes Cert No ASC ASC 909 • PlaneView Master Effectivity: This service 979090 31 CAN CAN 0.0 0 25 Apr 2013 C 0.00 Aidrame Operating System Software Update change is applicable to aircraft serial numbers 5309 - 5339. This or a similar change will be installed during initial phase manufacturing on aircraft serial number 5340 and subsequent. Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link ASC ASC 9098 • PlaneView Master Effectivity: Serial 979092 31 OPT 24 Apr 2013 I Aidrame Operating System Software Update numbers 5001 • 5422 having ASC 909. ASC 0958 Planeview Avionics Enhancement must be installed in conjunction with this service change. This service change revision supersedes all previous versions of ASC 909 and is now reissued as ASC 9098. Aircraft having previously complied with ASC 909 should upgrade to this latest revision during regularly scheduled maintenance. ASC ASC 910 • PlaneView Master Effectivity: 5001 • 979100 31 OPT 24 Apr 2013 Airframe Operating System Software Update 5422. ASC 907 - PlaneView MOS Software Update (Cart Echo) or later; or production equivalent. ASC 107 • PlaneView Avionics Enhancement must be installed in conjunction with this smite change. G-CGUL G550 5176 Technical Bulletins Page 85 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620875 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No ASC ASC 911 - PlaneView Master Effectivity: This service 979110 31 CAN CAN 0.0 0 18 Sep 2014 C 0.00 Airframe Operating System Software Update change is applicable to aircraft serial numbers 5001 — 5473. This. or a similar change. will be installed during initial phase manufacturing on aircraft serial numbers 5474 and subsequent. Cancelled by ASC 911A(979111). Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link. ASC ASC 911A • PlaneView Master Effectivity: This service 979111 31 OPT 17 Sep 2014 I Airframe Operating System Software Update change is applicable to aircraft serial numbers 5001 — 5473. This. or a similar change. will be installed during initial phase manufacturing on aircraft serial numbers 5474 and subsequent. CB CB 1 FIRE DETECT BOX 980010 Eff. Desc: 5001.5032. 26 MAN N/A 12 Mar 2004 I 26.15-01 Airframe MOUNTING CB 980020 CB 2 LUBE HORIZ STAB TRIGGER Eff. Desc: 5001.5042. 27 MAN N/A 26 May 2004 I 27-42-01 Airframe CB 980030 CB 3 PT1 WING VORTEX GENS/RIB Eff. Desc: 5001.5051. 57 MAN N/A 05 Aug 2004 I ASC 39 Airframe CB 980031 CB 3 PT2 WING VORTEX GENS/RIB Eff. Desc: 5001.5051. 57 MAN N/A 05 Aug 2004 I ASC 39 Airframe CB CB 4 AILELEV ACT DAMPER 980040 Eff. Desc: 5001.5052. 27 MAN N/A 23 Aug 2004 I Airframe SHAFT CB CB 5 PDB TERMINAL OVER 980050 Eff. Desc: 5001.5034. 24 MAN N/A 26 Oct 2004 I ASC41 Airframe TORQUE CB Eff. Desc: ALL G550 980060 CB 6 AILELEV ACT RETROFIT 27 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe ACFT. G-CGUL G550 5176 Technical Bulletins Page 86 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620876 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No CB Eft. Giese: 5001-5042 980070 CB 7 ELECT DISC BRACKET 24 MAN N/A 07 Jan 2005 I Airframe (12 MOS). CB CB 8 TAIL COMPARTMENT Ell. Desc: 5001-5063 980080 25 MAN N/A 07 Jan 2005 Airframe LADDER (12 MOS). CB Eff. Desc: 5002-5015 980090 CB 9 RIGHT EER MODIFICATION ' 25 MAN N/A 20 Jan 2005 I Airframe EX 5014. CB CB 9A RIGHT ELECTRICAL EQUIP Applies to 5002-5015 980091 25 MAN N/A II Feb 2005 I Airframe RACK MOD & 5020. CB 980100 CB 10 FLAP LEAD EDGE RIVETS Eft. Giese: 5001-5069. 27 MAN N/A 24 Jan 2005 I Airframe CB 980110 CB 11 OUTBRD FIX TE RIVETS Eft. Desc: 5001-5051. 57 MAN N/A 24 Jan 2005 Airframe CB CB 12 WING ANTI-ICE EXHAUST Eft. Dose: 5001- 980120 30 MAN N/A 16 Mar 2005 I Airframe LOUVERS INSP 5005.5008-5024.5026- 5030.5035-5037.5039 & 5044. CB CB 13 PART I FLIGHT CONTROL Effectivity: 5001-5036 980130 31 MAN N/A 22 Mar 2005 I Airframe SENSOR INSTALLATION having G550 ASC 2. INSPECTION Part 1 is to be accomplished within the next 12 months. Compliance with Part 2 of this CB. if necessary. is to be accomplished before the next flight following completion of Pan I. CB CB 13 PART 2 FLIGHT CONTROL Effectivity: 5001-5036 980131 31 MAN N/A 22 Mar 2005 I Airframe SENSOR INSTALLATION having G550 ASC 2. INSPECTION Compliance with Part 2 of this CB. if necessary. is to be accomplished before the next flight following completion of Pan 1. G-CGUL G550 5176 Technical Bulletins Page 87 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620877 TYP C/W Source Code Description Effectivity ATA Status ilLogbook Work Order HRS LDG Date C/I MM REF M HRS aintenance Notes Cert No CB CB 14 AILERON FORCE LINK ASSY EFF:5001.5072. WING 980140 27 MAN N/A 23 Jun 2005 I Airframe WIRING-INSP SN 678.767. ONE TIME INSP DUE 12 MOS AFT ISSUE DATE OF THIS BULLETIN AND INCORPORATES VOUGHT SB VAIGV/GVSP-27- PG0098. CB CB 15A NLG ACTUATOR ROD END EFF:5001-5084. ONE 980151 32 MAN N/A 21 Nov 2005 I Airframe INSP TIME INSP DUE WITHIN 12 MOS OF ISSUE DATE. CB CB 16 LEFT AND RIGHT STRNG 6 980160 EFF:5001.5047 53 MAN N/A 05 Aug 2005 I Airframe AT FS 955.974 CB CB 17 INSP. ANTI-SKID CONTROL EFF: 5044 THRU 980170 32 MAN N/A 11 Aug 2005 I Airframe UNIT 5063. TO BE ACCOMPLISHED WITHIN THE NEXT 60 DAYS. CB CB 18 MODIFICATION-VACUUM 980180 EFF: 5001.5059 38 MAN N/A 18 Aug 2005 I Airframe TOILET STATUS PANEL CB CB 19 INSP/SEALING - OUTBOARD EFF:5001.5051 TO BE 980190 57 MAN N/A 18 Aug 2005 I Airframe WING RIB REPAIR ACCOMPLISHED WITHIN 12 MONTHS OF ISSUE DATE. CB CB 20 - PREMIUM PACKAGE EFFECTIVITY: SiN 980200 23 MAN N/A 12 Oct 2005 I Airframe WIRING HARNESS INSP 5001.5047 excluding 5014. 5037 and 5044 - Compliance with this CB is to be accomplished within the next 24 Months. CB CB 21 PT1 INSPECT-FRAME AT 980210 WITHIN 12 MOS 53 MAN N/A 02 Nov 2005 I Airframe FS.377 CB CB 21 PT2 INSPECT-FRAME AT 980211 WITHIN 12 MOS 53 MAN N/A 02 Nov 2005 I Airframe FS.377 G-CGUL G550 5176 Technical Bulletins Page 88 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620878 TYP C/W Source Code Description Effectivity ATA Status ilLogbook Work Order HRS LDG Date C/I MM REF M HRS aintenance Notes Cert No CB CB 22 - NLG DOWNLOCK HARNESS EFFECTIVITY: SiN 980220 32 MAN N/A 07 Dec 2005 I Airframe CONN HDWARE 5001.5094 - ACCOMPLISH WITHIN 150 FLIGHT HOURS CB CB 23- EMERGENCY PRESSURE EFF: 5001 THRU 980230 32 MAN N/A 08 Dec 2005 I Airframe TRANSDUCER DECALS. INSP 5073. 5077. 5078. 5082. 5083. 5086. AND 5089 EXCLUDING 5014 AND 5037. ACCOMPLISH WITHIN 24 MOS OF ISSUE. CB CB 24 INSTALL - OXYGEN EFFECTIVITY: 5001- 980240 35 MAN N/A 20 Dec 2005 I Airframe BOTTLE PHYSICAL BARRIER 5071 r! Compliance with this CB is to be accomplished within the next 24 months./ This CB is a one-time action to ensure incorporation of ASC 048. CB 980250 CB 25 - INSP TAIL ANTI-COLL EFFECTIVITY: SiN 33 MAN N/A 11 Jan 2006 Airframe STROBE LT 5027 - 507911 COMPLIANCE: Compliance with this CB is to be accomplished at the next "Ar check. not to exceed 500 Flight Hours. CB CB 26A MOD-MAIN LANDING GEAR EFF:5001.5109. 980261 32 MAN N/A 21 Feb 2006 I Airframe DOORS COMPLIANCE WITH THIS CUSTOMER BULLETIN REVISION IS TO BE ACCOMPLISHED WITHIN 6 MONTHS. THIS IS A ONE TIME COMPLIANCE. G-CGUL G550 5176 Technical Bulletins Page 89 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620879 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No CB CB 27 REPLACEMENT- EFF:5001.5093. THIS 980270 27 MAN N/A 10 Mar 2006 I Airframe AILERON/ELEVATOR ACT LOAD IS A ONE TIME RELIEF BUNGEES ACTION TO REPLACE THE 1159C20014-5 PN WITH A 1159C20014 5 MOD A OR PN 1159C20014-7. COMP WITH THIS BULLETIN ELIMINATES CHP 5 REQUIREMENTS FOR RECURRING INSP OF BUNGEES. CB CB 27 AM1 Replace-Aileron / This is a "ONE TIME" 980271 27 MAN N/A 22 Jun 2006 I Airframe Elevator Act Load Relief Bungees action to replc all installed PN 1159020014.5 relief bungees with PN 1159C20014-5 Mod A or -7 bungees. Comp with this bulletin will eliminate the GV MM Chapter 5 req for recuMng bungee insp. Within 36 months. CB CB 28 Lancing Gear Bungee Lube EFF: 5001.5107. THIS 980280 32 MAN N/A 30 Mar 2006 I Airframe and Rigging-Insp IS A ONE TIME INSP. COMPLIANCE WITH THIS CB IS TO BE ACCOMPLISHED WITHIN THE NEXT 6 MONTHS. CB CB 29 AFT. Emerg Lighting Battery EFF: G550 SN 5001- 980290 33 MAN N/A 15 May 2006 I Airframe Mount Tray-Mod 5099 Only. This is a one time action to ensure the incorporation of ASC 056. Compliance with this CB is to be done within the next 12 months. G-CGUL G550 5176 Technical Bulletins Page 90 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620880 TYP CNV Source Code Description Effectivity IATAI Status Logbook Work Order HRS LOG Date CA MM REF M HRS Ilaintenance Notes Cert No CB CB 30 Decompression Vent Panels- EFF: G550 5020 980300 53 MAN NIA 18 May 2006 Airframe insp through 5114. This CB is a ONE TIME action, to be accomplished with in the next 12 months of CB issue date (May 18. 2006). CB CB 31 Insp•Modular Avionics Unit Due within 12 Mos. EH 980310 31 MAN N/A 25 May 2006 I Airframe Power Supply Connector 5001 thru 5101. excluding 5014.5037,5044,5078, 5083 thru 5092.5094,5095 and 5097 thru 5100. CB CB 32 Electrical Lines Contact EFF: 5001.5090, This 980320 24 MAN NA 28 Jun 2006 I Airframe Prevention-Mod (ASC 57) is a One Time action to ensure incorporation of ASC 057. Accomplish within the next 250 flight hours, not to exceed 6 months. CB CB 32 Aml - Electrical Lines Contact EFF: 5091 -5149- 980321 24 MAN N/A 03 Sep 2008 I Airframe Prevention-Mod (ASC 57A) This is a One Time action to ensure incorporation of ASC 057. Accomplish within the next 250 flight hours, not to exceed 6 months. CB CB 33 Enhanced Vision System EH: 5001 through 5126 980330 34 MAN N/A 17 Jul 2006 Airframe Window Bonding Strap-Mod "Having" EVS installed. This CB is a "one time" action to ensure incorporation of the G550 ASC 60. Compliance with this CB is to be accomplished within the 110%13 months. G-CGUL G550 5176 Technical Bulletins Page 91 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620881 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No CB CB 34 Oxy Line Support at F.S. 241• Eff: NC SNif 5002• 980340 35 MAN N/A 03 Aug 2006 I Airframe Installation 5086. 5088 and 5090 excluding 5014. This is a One Time" action to be accomplished at the next crew oxygen bottle removal, not to exceed 36 months. CB EFF: For NC Serial 980350 CB 35 Rudder Stop Botts-Insp 27 MAN N/A 31 Aug 2006 I Airframe numbers 5001.5112. This is a 'one time' insp to be accomplished within the next 12 months. CB CB 36 Right Pylon Case Drain Line EFF: G550 5001 980360 29 MAN N/A 01 Sep 2006 I Airframe Routing•Mod through 5121. This custome bulletin is a "One Time" action to be accomplished within the next 12 months. CB CB 37 (Part I) BBML Operational This is a 2 part Bulletin 980370 11 MAN N/A 25 Sep 2006 I Airframe Limitation Placard-Insp to be accomplished within the next 45 days. Part 1 is a One Time Action, Part 2 if required, ensures incorp of Drawing 1159S840091. EFF: SN 5043, 5046, 5053, 5061, 5062, 5071, 5076. 5079, 5085, 5089. 5091, 5097, and 5101. G-CGUL G550 5176 Technical Bulletins Page 92 of 164 20 Jan 2015 02015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620882 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No CB CB 37 (Part 2) BBML Operational This is a 2 part Bulletin 980371 11 MAN NIA 25 Sep 2006 I Airframe limitation Placard-Insp to be accomplished within the next 45 days. Part 1 is a One Time Action, Part 2 if required, ensures incorp of Drawing 1159S840091. EFF: SN 5043. 5046, 5053. 5061,5062, 5071, 5076, 5079, 5085, 5089, 5091, 5097, and 5101. CB CB 38 Auxiliary Hydraulic Boost This is a One Time 980380 29 MAN N/A 25 Sep 2006 I Airframe Pump•Insp Action to be accomplished "No Later Than Jan 31. 2007. To ensure compliance with Meggitt Airdynamics SB 2006.01. Pump Sn range is 02590318. CB CB 39 NLG Trunnion PM (Right Side NOTE: EFF: WI 980390 Only) 32 MAN N/A 10 Oct 2006 I Airframe 5001 - 5123II Compliance with this CB is to be accomplished within the next 12 months. CB 980400 CB 40 Mod-Seal Nose Gear Switch 5001.5154 32 MAN N/A 22 Dec 2006 I Airframe CB This is a One Time 980410 CB 41 Battery Chargers • Inspection 24 MAN N/A 25 Jan 2007 I Airframe inspection to ensure compliance with ELDEC SB 8.842.24• 01. Not to exceed 12 months. Accomplish before January 25, 2008. G-CGUL G550 5176 Technical Bulletins Page 93 of 164 20 Jan 2015 02015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620883 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No CB CB 42 lnsp-Trim Valve Servo Part 1 to be 980420 21 MAN N/A 29 Jan 2007 I Airframe Pressure Supply Part 1 accomplished within the next 90 days. Part 2 if required is to be accomplished 30 days after Part 1. Eft 5001 to 5136 excluding 5126. CB CB 42 lnsp Trim Air Valve Servo Part 1 to be 980421 21 MAN N/A 29 Jan 2007 Airframe Pressure Supply Part 2 accomplished within the next 90 days. Part 2 if required is to be accomplished 30 days after Part 1. Eft 5001 to 5136 excluding 5126. CB CB 43 lnsp. Water Level Sensor EFF: 5001 through 980430 38 MAN N/A 14 Feb 2007 I Airframe Harness Pan 1 5092. excluding 5014. 5037. 5044. 5069 and 5087. pan one is to be accomplished with in the next 12 months. Part 2 is to be accomplished with in 12 months of compliance of Part 1. CB CB 43 lnsp. Water Level Sensor EFF: 5001 through 980431 38 MAN N/A 14 Feb 2007 I Airframe Harness Pan 2 5092. excluding 5014. 5037. 5044. 5069 and 5087. pan one is to be accomplished with in the next 12 months. Part 2 is to be accomplished with in 12 months of compliance of Part 1. CB CB 44 Right Eng Integrated Drive Effectivity: SIN 5001 980440 44 MAN N/A 0.0 0 05 May 2008 C Airframe Generator Cable Inst. Mod through 5136 II This is a "One Time action to be accomplished with in the next 45 days G-CGUL G550 5176 Technical Bulletins Page 94 of 164 20 Jan 2015 C12015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620884 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No CB CB 45 Aux Hyd Boost Pump Circuit EFF: AfC 5001.5096. 980450 29 MAN NIA 0.0 0 05 May 2008 C Airframe Protection. Mod (ASC 059) This is a 'One Time' action to ensure incorporation of ASC 059. To be accomplished with in the next 24 months. Ref ASC 059. CB CB 46 No. 2 ADF Antenna Lead Instl This is a One Time 980460 46 MAN NIA 14 May 2007 I Airframe At F.S. 288 Action to inspect the No.2 ADF antenna lead. Elf: is for 5003 through 5123. 5126. 5127 and 5131. excluding 5014. 5037. 5044. 5069 and 5114. Compliance is due within the next 12 months. CB CB 47 APU Enclosure Sensor Instl - Serial ifs 980470 53 MAN NIA 29 May 2007 I Airframe Insp effected:5002. 5004. 5005, 5008. 5012. 5015.5016. 5018. 5020-5030. 5032- 5034. 5038-5041. 5043, 5045-5056. 5058-5068. 5070- 5074. 5076-5080. 5082-5092. 5095- 5098. 5101.5102. 5104.5106-5124. 5126. and 5128. CB CB 48 Wiring Harness Installation EFF: SN 5029 980480 24 MAN NIA 07 Jun 2007 I Airframe AFT F.S. 660 through 5079 Excluding 5064. Compliance with this CB is to be accomplished with in 12 months of issue date (June 7. 2007). CB CB 49 Mod-Left And Right Power Effectivity: SIN 5001 - 980490 24 MAN NIA 25 Jun 2007 Airframe Distribution Box (PDB) 5150 II This is a 'One Time Action. To be accomplished with in the next 24 months. G-CGUL G550 5176 Technical Bulletins Page 95 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620885 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No CB CB 50 Insp- Left Main Ban Lead hist! EFF: SN# 5102 980500 24 MAN N/A 25 Jun 2007 I Airframe At Wing Anti-Ice Valve through 5118.5124 through 5131. 5133 through 5136. 5140. 5142. 5145. 5146 and 5148. This is a ONE TIME Insp to be accomplished within the next 6 months from Issue Date (June 25. 2007). CB CB 51 Broadband Multi-Link (BBML) EFF: AC SNs 980510 23 MAN N/A 10 Jul 2007 Airframe Antenna Control Unit-Insp 5043.5046.5053.5061. 5062.5071.5076.5079. 5085.5089.5091.5097. 5110.5115.5116.5117. 5118.5120.5121.5124. 5125.5136.5137.5145. 5153 and 5154. Compliance is to be done with in 90 days from issue date (July 10, 2007). CB CB 52 Inspection-LP Compressor EFF: Aircraft Serial 980520 72 MAN N/A 04 Sep 2007 I Airframe Annulus Fillers Numbers 5001 Thru 5160. To be complied with within 90 days from issue date. Update CMP Codes 887256 and 897256 after compliance with CB52. CB CB 53 - Modification - Broadband This CB is a ONE 980530 23 CAN N/A 18 Sep 2007 I Airframe Multi-Link Antenna Installation TIME ACTION, to be accomplished with in the next 6 months. 11 Eff: &Ns 5043, 5046. 5053. 5061. 5062. 5071. 5076. 5079. 5085, 5089. 5091. 5097, 5101. 5104. 5107. 5110. 5115. 5116. 5117. 5118. 5120. 5121. 5124. 5125 and 5136. G-CGUL G550 5176 Technical Bulletins Page 96 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620886 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No CB CB 53A - Modification Broadband This CB is a ONE 980531 23 MAN N/A 16 May 2008 I Airframe Multi-Link Antenna Installation TIME ACTION, to be accomplished with in the next 6 months. Eft: &Vs 5043. 5046. 5053. 5061. 5062. 5071. 5076. 5079. 5085. 5089. 5091. 5097. 5101. 5104. 5107. 5110. 5115. 5116. 5117. 5118. 5120. 5121. 5124. 5125 and 5136. CB CB 54 Wiring Harness At Fuselage Eft. A/C SN 5001 980540 24 MAN N/A 04 Oct 2007 I Airframe Station (FS) 139 - Inspection through 5068 excluding 5014. 5037. 5044. 5064. 5065. 5066 and 5067. To be accomplished with in 250 FIt his and not to exceed 6 months. CB CB 55 Local Area Network (LAN) EFF: 5001.5137 and 980550 31 MAN N/A 05 Oct 2007 I Airframe Connectors Inspection 5139. This is a *ONE TIME inspection to be accomplished with in the next 12 months. CB CB 55 AM1 Inspect-Local Area Effectivity sin 5138. 980551 31 MAN N/A 11 Aug 2008 I Airframe Network Connectors due within 12 mos. G-CGUL G550 5176 Technical Bulletins Page 97 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620887 TYP CNV Source Code Description Effectivity IATAI Status Logbook Work Order HRS LOG Date CA MM REF M HRS Wiintenance Notes Cert No CB CB 55 Am2 Local Area Network (LAN) Aircraft serial numbers 980552 31 MAN NIA 03 Oct 2008 Airframe Connectors • Inspection 5001 through 5137 and 5139. This customer bulletin amendment replaces Page 1 of 6 of Customer Bulletin 55. Aircraft that have previously complied with Customer Bulletin 55 are in ompliance with this customer bulletin amendment.Complian ce with this customer bulletin is to be accomplished no later than August 11. 2009. CB CB 56 Inspection•NLG Downlock EFF: Aircraft serial 980560 32 MAN N/A 26 Nov 2007 I Airframe Switch Mounting Bracket numbers 5001 through 5120 excluding 5014, 5044 and 5069 CB CB 57 FMS Wiring Harness Inst at Effectivity: S/N 5001 980570 34 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe Fuselage Sta 63 Blkhd through 5151, 5153 and 5155/ Compliance: Compliance with this CB is to be accomplished within the next 90 days. CB CB 58 Nose Landing Gear Door Effectivity: S/N 5001 GAC 9B0580 32 MAN C/IN APPLETON 20.7 11 09 Apr 2008 C aoo Actuator (ASC 070) through 5177 // Airframe Compliance: FP549 Compliance with this CB is to be accomplished within the next 12 months./ This CB is a one-time action to incorporate ASC 070. CRS GIIRI00Y CB CB 59 Inspection-Main Entry Door EFF: Aircraft serial 980590 52 MAN NA 19 Dec 2007 I Airframe Warning Switch Installations numbers 5001 through 5139 and 5141 G-CGUL G55O 5176 Technical Bulletins Page 98 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620888 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No CB CB 59A1 Inspection - Main Entry Door EFF: Aircraft Serial 980591 52 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe Warning Switch Installations Numbers 5001 through 5141 and 5144 through 5146. excluding 5132. CB CB 60 Modification-Tail Compartment EFF: Aircraft serial 980600 52 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe Door Seal numbers 5050 through 5149 CB CB 61 Inspection-Feeder Cable EFF: Aircraft serial 980610 24 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe Installation At Fuselage Station 687 numbers 5003 through 5013, 5015 through 5036. 5038 through 5043. 5045 through 5068. 5070 through 5085 and 5093 CB CB 62 Inspection-Flap Drive Rod EFF: Aircraft Serial 980620 27 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe Installation Numbers 5001 Through 5144. excluding 5132. 5142 and 5143. CB CB 63 Inspection-Airshow AS4000 EFF: Aircraft serial 980630 23 MAN N/A II Feb 2008 I Airframe Mounting Tray Connector numbers 5078. 5079. 5084. 5085. 5087. 5088. 5090. 5092. 5097. 5098.5100. 5104. 5105. 5107. 5108, 5111. 5112. 5115, and 5116 CB CB 64 Inspection-Waste Tank Rinse EFF: Aircraft Serial 980640 38 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe Nozzles Numbers 5001Through 5100. CB CB 65 Auxiliary Power Unit (APU) Effectivity: SIN 5001- 980650 51591 This customer 49 MAN N/A 07 Apr 2008 I Airframe Bond Strap Installation (ASC 066) bulletin is a one-time action to ensure incorporation of ASC 066 / Compliance with this customer bulletin is to be accomplished within the next 12 months G-CGUL G550 5176 Technical Bulletins Page 99 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620889 TYP C/W Source Code Description Effectivity ATA Status ilLogbook Work Order HRS LDG Date C/I MM REF M HRS aintenance Notes Cert No CB CB 66 Pt 1 Inspection - Fuel Eff: SeN 5001 51621! 980660 73 MAN N/A 02 May 2008 I Airframe Metering Unit Independent Part I is a one time Overspeed Protection Coil Wiring action to inspect the Combined Overspeed Shutoff Solenoid valve Independent Overspeed Protection coils on the FMU for a cross-wired condition per RR ASB-BR700.73 -A900451 and Woodward SB 83575- 73.005. CB CB 66 Pt 2 Inspection - Fuel Eft: SiN 5001 -5162/I 980661 73 MAN N/A 02 May 2008 I Airframe Metering Unit Independent Part II of this customer Overspeed Protection Coil Wiring bulletin requires replacement of the FMU within 20 flight cycles if the FMU fails the test per the RR ASB-BR700.73- A900451 and Woodward SB 83575- 73.005. CB CB 67 Inspection-Fuel Boost Pump Aircraft serial numbers 980670 28 MAN N/A 09 May 2008 I Airframe Manifolds 5099 through 5141. 5144 and 5145.Compliance with this customer bulletin is to be accomplished at the Wing Tank Internal. BL0 - BL180 Detailed Inspection. 57.00.00 or 3000 landings. whichever occurs first. CB 980680 CB 68 Replacement-Emergency Aircraft 5102. 5132. 24 MAN N/A 11 Jun 2008 Airframe Inverter P/N 1.002-0102.1346 5151. 5152. 5153. 5156 thru 5161. 5163. 5168. 5170. 5171. Due within 24 months. CB CB 69 Mod-Nose Gear Uplock Hook Due within 12 months. Jet Aviation 980690 32 MAN CM Geneva 513.0 177 03 Feb 2009 C 0.00 Spring (ASC 73) incorporates ASC 73 Airframe GV8TC003 Mx. Notes: TO be aligned with 500 hr inspection ref D.Kalsi G-CGUL G550 5176 Technical Bulletins Page 100 of 164 20 Jan 2015 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620890 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No CB CB 70 Replacement-Tee Clips At FS. Due within 24 months. 980700 53 MAN NIA 31 Jul 2008 Airframe 734. Left No. 3 and No.4 Stringers Effectivity 5097 thru 5142. 5144 thru 5151. 5153 thru 5163. 5164 and 5167. CB CB 71 Inspect-Water System Drain sin 5001 thru 5192 gama lab 980710 38 MAN CPN 360.6 141 06 Nov 2008 C 0.00 Airframe Valve excluding 5014. 5037. F081108 5044. 5069. 5132. 5188. 5189. 5191. Due within 90 days. incorporates ASC 78. CB CB 72 Mod-Main Landing Gear AC SIN 5125 thru Jet Aviation 980720 MAN CPN Geneva 513.0 177 03 Feb 2009 C 0.00 Emergency Line (ASC 79) 5182. Incorporates Airframe ASC 79. due within 12 GVBTC003 months CB CB 73 Inspection-Elevator Control sin 5166.5182. due LTN 980730 27 MAN CPN 742.4 251 02 Oct 2009 C 0.00 Airframe Rod Bearings within 12 mos FLOC 546 CB CB 74 Flight Spoiler Actuator SEE CB 74A - GAL-LTN 980740 57 CAN NIA 407.8 157 09 Dec 2008 C 0.00 Airframe Attachment Point - Inspection SUPERCEDED FL0I 1448 11/13/2008 // Effectivity: Aircraft Serial Numbers 5001 through 5210 Compliance with this CB is to be accomplished within the next 90 days G-CGUL G550 5176 Technical Bulletins Page 101 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620891 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No CB CB 74A • Flight Spoiler Actuator Effectivity: Aircraft GALLTN 980741 57 MAN CM 407.8 157 09 Dec 2008 C 0.00 Airframe Attachment Point • Inspection Serial Numbers 5001 FL011448 through 5210! Compliance with this customer bulletin revision Is to be accomplished no later than March 20, 2009. (Per Amt}II Aircraft that have previously complied with CB 74 must comply with this customer bulletin revision with the exception of the static measurement of the spoilers and the fuel leak check called out in Steps II.H and II.M of this document. CB CB 74A Am1• Flight Spoiler Actuator Aircraft serial numbers 980742 57 MAN CM 534.6 184 27 Feb 2009 C 0.00 Airframe Attachment Point - Inspection 5001 through 5210. Aircraft that have previously complied with Customer Bulletin 74A are in compliance with this customer bulletin amendment. This customer bulletin amendment changes the compliance time for all aircraft affected by the original issue of CB 74A to March 30, 2009. Mx. Notes: CB 74A PREVIOUSLY COMPLIED WITH BY GULFSTREAM REF W1O FL011448 9TH DEC 08 CB CB 75 Inspection-Rudder Cable Aircraft serial numbers 980750 27 MAN N/A 04 Nov 2008 I Airframe Guide Bracket 5001 through 5141 and 5144. excluding 5093 and 5132, to be accomplished within the next 24 months. G-CGUL G550 5176 Technical Bulletins Page 102 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620892 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No CB i Aircraft LTN 980760 CB 76 Main Entrance Door Tee Splice serial numbers 6126 52 MAN CNV 742.4 251 02 Oct 2009 C 0.00 Airframe Effect vity: FL012546 through 5185. 5187 and 5202// Compliance with this customer bulletin is to be accomplished within the next 12 months. CB CB 77 • Inspection • Support Effectivity: S/N 5181 • 63 980770 MAN N/A 24 Nov 2008 I Airframe Assembly Panel at Fuselage Station 5185 and 5187 1 44. Nose Wheel Well Compliance with this CB is to be accomplished within the next 6 months / Man-hours for Repair (if required) = 80 Man- hours CB CB 78 - Inspection • HF•9000 Series. Effectivity: S/N 5001 • 980780 23 MAN N/A 25 Nov 2008 I Airframe Fiber Optic Connector Crimping 5158 excluding 5132, 5143, 5152 and 5156/ Compliance with this CB is to be accomplished within the next 12 months / Grounding Ring Installation (if required) = 6 man-hours / Hamess Replacement (if required) = 6 man- hours CB CB 79 Inspection-APU Door Actuator Aircraft serial numbers Jet Aviation 980790 49 MAN CM Geneva 513.0 177 03 Feb 2009 C 0.00 Hardware 5175 through 5188. Airframe 5190. 5192, 5193, GVBTC003 5205 and 5207. Compliance with this customer bulletin is to be accomplished within the next 6 months. G-CGUL G550 5176 Technical Bulletins Page 103 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620893 TYP C/W Source Code Description Effectivity ATA Status ilLogbook Work Order HRS LDG Date C/I MM REF M HRS aintenance Notes Cert No CB CB 80 Mod - Tail Compartment Aircraft serial numbers 980800 25 CAN CAN 18 Dec 2008 I Airframe Access Ladder (ASC 082) 5002, 5099. 5100. 5160 through 5225 and 5103 through 5159 having Aircraft Service Change (ASC) 062. This customer bulletin is a one-time action to ensure incorporation of ASC 082. Compliance with this customer bulletin is to be accomplished within the next 6 months. This CB canceled by CB 80A CB CB 80A Mod Tail Companment Aircraft serial numbers LTN 980801 25 MAN CPN 742.4 251 02 Oct 2009 C 0.00 Airframe Access Ladder (ASC 082A) 5002, 5099. 5100. FLO12546 5102, 5160 through 5233 and 5103 through 5159 having Aircraft Service Change (ASC) 062. This customer bulletin revision cancels and supersedes Customer Bulletin (CB) 80. Aircraft operators who have previously complied with CB 80 must comply with this customer bulletin revision. Compliance with this customer bulletin revision is to be accomplished within the next 6 months. CB CB 81 Divan Seat Belt Anchor Effectivity: Aircraft Jet Aviation 980810 25 CAN CPN Geneva 513.0 177 03 Feb 2009 C 0.00 Installation serial numbers 5001 Airframe through 5206 with GVEITC003 side.fadng divan installed / Compliance: Compliance with this customer bulletin is to be accomplished no later than April 10. 2009 G-CGUL G550 5176 Technical Bulletins Page 104 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620894 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No CB CB 81A - Divan Seat Belt Anchor Aircraft serial numbers gams tab 980811 MAN CPN 562.3 190 19 May 2009 C 0.00 Airframe Installation 5001 through 5206 1090541 with side.fadng divan installed. This customer bulletin revision cancels and supersedes Customer Bulletin (CB) 81. Aircraft operators who have previously complied with CB 81 must comply with this customer bulletin revision. Compliance with this customer bulletin revision is to be accomplished no later than April 24. 2009. CB CB 82 Inspection - Hydraulic System Aircraft serial numbers 980820 29 MAN NIA 29 Apr 2009 I Airframe Accumulator 5023. 5083. 5087. 5091. 5093 through 5100. 5103 through 5106. 5108. 5109. 5121. 5129. 5144. 5161 and 5170. Compliance with this customer bulletin is to be accomplished within the next 12 months. G-CGUL G550 5176 Technical Bulletins Page 105 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620895 i T YP CNV Source Code Description Effectivity ATA Status ill oebook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No CB CB 83 Morification- Wing Rear Beam Applies to 5001.5230. 980830 57 MAN CPN 1787.4 543 08 Mar 2011 C 0.00 Airframe Flight Spoiler Actuator Attachment at in compliance with Point (ASC 80) drawing 1595850091 meet the Intent of ASC 80. Operators of those aircraft should report ASC 80 as p/c/w.This cb is a one-time action to ensure incorporation of ASC 80. Cm this cb within the next: 'A/C with more than 1500 cycles = 6 months. WC having more than 1000. but less than 1500 cycles = 12 months. WC having less than 1000 cycles = 24 months. CB CB 83 AM1 Modification- Wing Rear Applies to 5001.5230. 980831 57 MAN CAN 1787.4 543 08 Mar 2011 C 0.00 Airframe Beam Right Spoiler Actuator afc in compliance with Attachment Point (ASC 80) drawing 1595850091 meet the intent of ASC 80. Operators of those aircraft should report ASC 80 as p/c/w.This cb is a one-time action to ensure incorporation of ASC 80. C/W this cb within the next: WC with more than 1500 cycles = 6 months. 'A/C having more than 1000. but less than 1500 cycles = 12 months. A/C having less than 1000 cycles = 24 months G-CGUL G550 5176 Technical Bulletins Page 106 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620896 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No CB CB 84 Replacement • Accessory Compliance with this 980840 72 MAN NIA 11 Jun 2009 Aidrame Gearbox Pressure Relief Valve customer bulletin is to be accomplished within the next 12 months. This customer bulletin is a onetime action to ensure compliance with Rolls- Royce Service Bulletin SB•BR700-72-900493 (see code 880593). CB CB 84 AM1 Replacement • Accessory This customer bulletin 980841 72 MAN NIA 17 Sep 2009 I Aidrame Gearbox Pressure Relief Valve amendment changes the manpower requirements of the original issue of CB 84 by reducing the man• hours for engine run from 7 to 4 man-hours. removing man-hours for fueling and clarifying man-hours to replace oil. This customer bulletin amendment replaces Pages 1 and 2 of CB 84. Aircraft that have previously complied with CB 84 are in compliance with this customer bulletin amendment. G-CGUL G550 5176 Technical Bulletins Page 107 of 164 20 Jan 2015 C2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620897 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No CB CB 85 Inspection - WINSLOW Life Aircraft serial numbers 980850 MAN NIA 18 Aug 2009 I Airframe Raft 5010, 5019, 5030 and 5087. Compliance with this customer bulletin is to be accomplished before further flight over water. as defined in the following Federal Aviation Regulations (FARs), not to exceed 45 days: FAR Part 91205 • FAR Part 91.509• FAR Part 21.339. FAR Pad 121.340. FAR Part 135.167• FAR Part 25.1415 (Airplanes Certified for Ditching). FAR Part 25.801 CB CB 86 Modification - Sealing of Nose Aircraft serial numbers G/S LTN 980860 32 MAN CAN 1037.5 331 09 Mar 2010 C 0.00 Airframe Wheel Steering Electrical Connectors 5001 through 5232. FL012898 Compliance with this customer bulletin is to be accomplished within the next 12 months. CB CB 87 Global Positioning System Aircraft serial numbers 980870 34 MAN CNV 1787.4 543 08 Mar 2011 C Aidrame Cable Installation at Fuselage Station 5100 through 5215 GAL 110106 139 and 5230. excluding 5205 and 5212. Compliance with this customer bulletin is to be accomplished within the next 24 months. CB 58 CB 88 Baggage Compartment Below Cancelled ref CB 88A. 28 CAN N/A 10 Dec 2009 I Airframe Floor - Overheat Thermal Switch G-CGUL G550 5176 Technical Bulletins Page 108 of 164 20 Jan 2015 ®2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620898 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No CB CB 88A Baggage Compartment sin 5016 - 5173. 980881 26 MAN N/A 11 May 2010 I Airframe Below Floor • Overheat Thermal Compliance with this Switch CB to be accomplished at the next (AMM), Chapter 5 inspection, Task 26.14 01.BaggageCompartm ent Below-Floor Overheat Thermal Switch - Functional Test no later than April 2014.This customer bulletin revision cancels and supersedes Customer Bulletin (CB) 88. If CB 88 previously complied with operators are in compliance with this revision and should return the service reply card marked "Previously complied with." CB CB 89 Replacement - Power Compliance with this 24 MAN C/W 1479.1 446 03 Sep 2010 C Airframe 980890 Distribution Box Contactors, PN customer bulletin is to GALI00716 5912336-3 be accomplished within the next 12 months. Aircraft serial numbers 5004, 5014, 5021, 5027 through 5028, 5037, 5044, 5046, 5049, 5058, 5059, 5073, 5079, 5107, 5109 through 5114,5116, 5118, 5120 through 5139. 5141 through 5156. 5158, 5160 through 5166, 5168 through 5171, 5173 through 5221, 5223, 5224, 5227, 5229, 5230, 5236, 5240 and 5242 G-CGUL G550 5176 Technical Bulletins Page 109 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620899 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No CB CB 90 Inspection - WINSLOW Life Aircraft serial numbers 980900 MAN NIA 981.1 317 03 Feb 2010 C 0.00 Airframe Raft 5001 through 5250 having life raft(s) manufactured by the WINSLOWO LifeRaft Company. Compliance with this customer bulletin is to be accomplished within the next 45 days. Mx. Notes: NOT APPLICABLE AFFECTED LIFERAFTS NOT INSTALLED CB Aircraft serial numbers GiS LTN 980910 CB 91 Modification Nose Jack Point 53 MAN C/W 1037.5 331 09 Mar 2010 C 0.00 Airframe 5001 through 5240 FL012898 and 5245. Compliance with this customer bulletin is to be accomplished within the next 12 months. CB CB 92 Modification Pilot Copilot Aircraft serial numbers 980920 25 MAN CPN 1787.4 543 08 Mar 2011 C Airframe Seat Forward / Aft Adjustment 5001 through 5256. GAL 110106 Control Lever Compliance with this customer bulletin is to be accomplished at the next scheduled 'A Check not to exceed 12 months from the release date of this customer bulletin. G-CGUL G550 5176 Technical Bulletins Page 110 of 164 20 Jan 2015 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620900 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No CB CB 93 Inspection • Horizontal Aircraft serial numbers 980930 27 MAN cm 1787.4 543 08 Mar 2011 C 0.00 Airframe Stabilizer Actuator 5001 through 5239 having Horizontal Stabilizer Actuator (HSA) with SN 305 or subsequent installed. Suspect HSA installations have been identified as any actuator with a serial number of 305 or subsequent installed during initial phase of manufacturing prior to aircraft serial number 5240. or installed on in-service aircraft prior to the AMM revision of October 30. 2006. Compliance with this customer bulletin is to be accomplished within the next 12 months. Mx. Notes: not applicable to hsa s/no 0216 installed. CB 93 was carried out in full see work pack FL014715 itern172 for details...Gulfstream techops advised by email. CB CB 94 Engine (ATA 72), General • Aircraft serial numbers 980940 72 MAN CPAr 1114.2 352 06 Apr 2010 C 0.00 Airframe Change of Life Counting Method for 5001 through 5270. Touch.and.Go and Overshoot (Rolls. This customer bulletin Royce Men SB•BR700-72-A900504) is a onetime action to direct compliance with Rolls•Royce Alert Service Bulletin SB. BR700.72•A900504 (codes 880044/890044). Compliance with this customer bulletin is to be accomplished no later than July 31, 2010. G-CGUL G550 5176 Technical Bulletins Page 111 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620901 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No CB CB 95 Replacement Passenger Seat Aircraft serial numbers 980950 25 MAN N/A 08 Apr 2010 I Airframe Swivel Plate 5058. 5148. 5217 and 5218 through 5245. excluding 5219 and 5242. Compliance with this customer bulletin is to be accomplished within the next 24 months. CB CB 96 Replacement Emergency Aircraft serial numbers 980960 32 MAN CAN 1787.4 543 08 Mar 2011 C Airframe Brake Accumulator and Landing Gear 5001 through 5289. GAL 110106 Emergency Extension Nitrogen Blow- Compliance with this down Bottle Charging Valves customer bulletin is to be accomplished within the next 12 months. CB CB 97 Inspection - Hydraulic Filter Aircraft serial numbers 980970 05 MAN N/A 04 May 2010 I Airframe Element Pan Number AC-B451F-16 5234. 5235 and 5237. Compliance with this customer bulletin is to be accomplished within the next 12 months. CB 980980 CB 98 Repair Right System Aircraft serial numbers 29 CAN CAN 0.0 0 18 Mar 2011 C Airframe Hydraulic Reservoir 5103 through 5182. GAL 110106 Compliance with this customer bulletin is to be accomplished within the next 12 months. Cancelled see CB 98A CB CB 98A Repair Right System Aircraft serial numbers 980981 29 MAN N/A 1787.4 543 08 Mar 2011 C 0.00 Airframe Hydraulic Reservoir 5103 through 5182. Due to parts availability issues. the compliance time has been extended to not later than October 13. 2011. Mx. Notes: N/A by Pan number (1159H50126-31 fitted) CB CB 99 Inspection - Flight Spoiler Aircraft serial numbers 980990 27 MAN N/A 0.0 0 27 May 20 l 0 C Airframe Control Rod. P/N A-GUV10-101 5229 through 5258. excluding 5254 Mx. Notes: Aircraft serial numbers 5229 through 5258. excluding 5254 G-CGUL G550 5176 Technical Bulletins Page 112 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620902 i T YP CNV Source Code Description Effectivity ATA Status ill onbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No CB CB 100 Inspection - Crew Seat Inertia Aircraft serial numbers 981000 25 DEL CAN 0.0 0 07 Jun 2010 C Airframe Reels 5153 through 5217. 5219, 5227, 5237 and 5247 excluding 5205. Compliance with this customer bulletin is to be accomplished within the next 18 months. Manpower: Initial Inspection • 0.5 man-hours Follow-on inspection • 0.5 man-hours per seat Remove/Install inertia reel - 1.0 man-hour per seat. Cancelled see CB 100A CB CB 100 Inspection - Crew Seat Inertia Aircraft serial numbers 981000 25 CAN CAN 0.0 0 08 Jun 2010 C 0.00 Airframe Reels 5153 through 5217. 5219, 5227, 5237 and 5247 excluding 5205. Compliance with this customer bulletin is to be accomplished within the next 18 months. Manpower: Initial Inspection • 0.5 man-hours Follow-on inspection - 0.5 man-hours per seat Remove/Install inertia reel - 1.0 man-hour per seat. Cancelled see CB 100A G-CGUL G550 5176 Technical Bulletins Page 113 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620903 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No CB CB 100A Inspection - Crew Seat Aircraft serial numbers 981001 MAN CM 1787.4 543 08 Mar 2011 C 0.00 Airframe Inertia Reels 5153 through 5217. 5219. 5227. 5237 and 5247 excluding 5205. This customer bulletin revision cancels and supersedes Customer Bulletin (CB) 100. Aircraft operators who have previously complied with CB 100 must comply with this customer bulletin revision. Compliance with this customer bulletin revision is to be accomplished within the next 18 months. CB CB 101 (Part I) Inspection - Portable Aircraft serial numbers game 981010 MAN CM 1562.2 477 29 Oct 2010 C 0.00 Airframe Oxygen Bottle Secondary Mask 5016. 5028. 5033. 1101069 Assembly 5035. 5049. 5060. 5066. 5077. 5083. 5086. 5091. 5095. 5101. 5109. 5113. 5114.5118. 5121. 5124. 5128. 5142. 5146. 5148. 5158. 5163. 5164. 5169. 5171. 5176. 5180. 5183. 5186. 5188. 5189. 5194. 5197. 5202. 5205. 5207. 5212. 5214. 5220. 5223 and 5227.Part I of this customer bulletin is to be accomplished within 90 days.Compliance with Part II of this customer bulletin. if required. is to be accomplished within 24 months Mx. Notes: CB PART 1 CLOUT FOUND INCORRECT PART INSTALLED.PART REMOVED.PART II TO BE COMPLIED WITH G-CGUL G550 5176 Technical Bulletins Page 114 of 164 20 Jan 2015 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620904 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No CB CB 101 (Part II) Inspection • Portable Aircraft serial numbers 981011 MAN cm 1787.4 543 08 Mar 2011 C 0.00 Airframe Oxygen Bottle Secondary Mask 5016, 5028, 5033, Assembly 5035, 5049, 5060, 5066, 5077, 5083, 5086, 5091, 5095. 5101,5109. 5113. 5114, 5118. 5121. 5124, 5128, 5142. 5146, 5148, 5158, 5163, 5164, 5169, 5171, 5176, 5180, 5183, 5186, 5188, 5189, 5194, 5197, 5202, 5205, 5207, 5212, 5214, 5220, 5223 and 5227 Compliance with Part II of this customer bulletin. if required, is to be accomplished within 24 months of the original release date of this customer bulletin. CB CB 102 Modification - Emergency Aircraft serial numbers GAGLTN 981020 MAN CAN 2354.6 711 19 Apr 2012 C Airframe Battery Pack 5001 through 5289. FL016471 Compliance with this CB to be accomplished within the next 24 mos. Securaplane recommends that batteries within 24 mos of the scheduled Pack - Discard (48 month), referenced in the AMM. Chapter 05. Time Limits 05-1040, be kepi in-service and incorporate this customer bulletin at the scheduled 48- month discard time. Batteries not within 24 mos of the Pack • Discard (48 month). must incorporate this CB within next 24 mos Mx. Notes: aligned with 240111 UK.145.00883 G-CGUL G550 5176 Technical Bulletins Page 115 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620905 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No CB CB 103 Inspection - Fasteners at Aircraft serial numbers 981030 MAN CM 1787.4 543 08 Mar 2011 C 0.00 Airframe Fuselage Station 63, Left and Right 5001 through 5257. Butt Line 19 excluding 5131 and 5254. Compliance with this customer bulletin is to be accomplished at the next scheduled AMM Chapter 05 inspection, Air Data System (ADS) Functional / Leak Test (CMP 341304 / 341305/ 341306). no later than 24 months from the original release date of this customer bulletin. Mx. Notes: SET UP WITH CODE 341306 CB CB 104 Inspection • Engine Electronic Aircraft serial numbers 981040 MAN CPAI 1787.4 543 08 Mar 2011 C 0.00 Airframe Controller Lane A Harness 1A 5001 through 5296. This customer bulletin is a one-time action to comply with Rolls- Royce NMSB SBBR700.71.900505. Compliance with this customer bulletin is to be accomplished within 24 months. CB CB 105 Inspection Landing Gear Sasl 5234 - 5267. 981050 CAN N/A 23 Sep 2010 I Airframe Selector Dump Valve excluding 5266. due within 12 mos. Cancelled see CB 105A G-CGUL G550 5176 Technical Bulletins Page 116 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620906 i T YP CNV Source Code Description Effectivity ATA Status ill oebook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No CB CB 105A Inspection • Landing Gear Aircraft serial numbers 981051 MAN NIA 1639.8 497 06 Dec 2010 C Airframe Selector / Dump Valve 5234 through 5267 and 5277. excluding 5266. Compliance with this customer bulletin is to be accomplished within 12 months of the release date of the original customer bulletin dated September 23, 2010. Aircraft operators who have previously complied with CB 105 are in compliance with this revision and should return the service reply card marked Previously complied with? CB CB 106 Fuel Quantity Signal Cancelled see ASC 981060 28 CAN CAN 17 Nov 2010 I Airframe Conditioner to Install Revision F 106A Software CB CB 106A Replacement - Fuel Aircraft serial numbers 981061 28 MAN C/W 1787.4 543 08 Mar 2011 C 0.00 Airframe Quantity Signal Conditioner to Install 5001 through 5192 Revision F Software without ASC 63.This customer bulletin is a one-time action to replace all FOSCs, P/N 367.933.002, not having software Revision F and to incorporate ASC 077 for updated APU oil service. Compliance with this CB revision is required within 24 months from the original issue date of Il-17.2010.A/C having ASC 063 are not affected by this CB. Report this customer bulletin as "N/A. Appliance not installed". G-CGUL G550 5176 Technical Bulletins Page 117 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620907 i T YP CNV Source Code Description Effectivity ATA Status ill onbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No CB CB 107 Inspection - Door Control Aircraft serial numbers 981070 MAN Cm 1787.4 543 08 Mar 2011 C 0.00 Aidrame Valve Hydraulic Lines 5001 through 5268. 5270. 5273 and 5275. Compliance with this customer bulletin is required within 12 months of the release date. CB CB 108. Inspection • Left Engine Effectivity: Aircraft 981080 29 MAN Cm 1787.4 543 08 Mar 2011 C 0.00 Airframe Hydraulic Pressure Line serial numbers 5001 through 5252, 5261and 5265, excluding 5247. Compliance with this customer bulletin is to be accomplished within the next 24 months. CB CB 109 Rework • Vertical Stabilizer Aircraft serial numbers 981090 MAN N/A 08 Jun 2011 Aidrame Access Panel 5290, 5291, 5292, 5293, 5294, 5296. Compliance is required within 36 months of the release date of this customer bulletin. Gulfstream recommends this customer bulletin be accomplished in conjunction with G550 AMM Chapter 05 "3C". Horizontal Stabilizer Actuator • Lubrication G-CGUL G550 5176 Technical Bulletins Page 118 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620908 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No CB CB 110 Modification Landing Gear Aircraft serial numbers 981100 CAN CAN 0.0 0 28 Jun 2011 C 0.00 Airframe Door Close - Restrictor Installation 5001 through 5303. (ASC 094) This customer bulletin is a one-time action to ensure incorporation of ASC 094. Compliance is to be accomplished within 36 months of the release date of this customer bulletin. Gulfstream recommends this customer bulletin be accomplished in conjunction with AMM Chapter 05 "3C" Inspection. Landing Gear Emergency Extension operational test. Cancelled see CB110A Mx. Notes: lined up with code 323901 CB CB 110A Modification Landing Gear Aircraft serial numbers GAC LTN 981101 MAN CM 2849.4 833 09 Apr 2013 C Airframe Door Close - Restrictor Installation 5001 through 5314. BMX000145 (ASC 094) This customer bulletin is a one-time action to ensure incorporation of ASC 094. Compliance is to be accomplished within 36 months of the original release date of this customer bulletin (July 1. 2011). Gulfstream recommends this customer bulletin be accomplished in conjunction with AMM Chapter 5 3C Inspection. Landing Gear Emergency Extension operational test. This customer bulletin revision replaces CB 110. Mx. Notes: Lined up with code 323901 UK.145.00883 G-CGUL G550 5176 Technical Bulletins Page 119 of 164 20 Jan 2015 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620909 i T YP CNV Source Code Description Effectivity ATA Status ill oebook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No CB CB 111 Inspection - Enhanced Vision 5001.5307 with EVS, GAC LTN 981110 MAN Cm 2047.8 610 15 Jul 2011 C Airframe System (EVS) Radome Support Strut. due within 6 months FL015395 PM 1159SCAM561.1 UK.145.00883 CB CB 112 Modification • Tail Aircraft serial numbers GAC•LTN 981120 MAN CAN 2354.6 711 19 Apr 2012 C Airframe Compartment Ladder Attach Fittings 5001 through 5302 FL016471 with Part Number (PN) 1159SCB750 tail compartment ladder. Compliance with this customer bulletin is required within 12 months of the release date. UK.145.00883 CB CB 113 Modification • Broadband Due within 24 months GAL CAMO 981130 MAN N/A 3029.7 875 27 Sep 2013 C 0.00 Airframe Multi-link (BBML) Antenna from release. SIN 5043. 5053, 5058, 5061, 5062, 5071, 5076, 5079, 5085, 5089, 5097, 5101. 5107, 5110. 5115- 5118, 5120. 5121. 5124, 5125, 5136. 5137, 5145, 5153- 5155, 5157, 5159, 5160, 5162, 5164, 5165, 5169, 5180, 5183, 5184, 5194, 5195, 5196, 5206, 5211, 5223, 5235, 5236, 5237, 5240. CB CB 114 Non-Compliance - Stage 3 Aircraft serial numbers 981140 MAN 26Oct 2011 Airframe Noise Certification (ASC 008B) 5001 through 5352 having Aircraft Service Change (ASC) 008 or 008k Compliance with this customer bulletin is required within 12 months of the release date. G-CGUL G550 5176 Technical Bulletins Page 120 of 164 20 Jan 2015 ®2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620910 TYP C/W Source Code Description Effectivity ATA Status ilLogbook Work Order HRS LDG Date C/I MM REF M HRS aintenance Notes Cert No CB CB 115 Inspection Nose Landing Aircraft serial numbers 981150 MAN NIA 04 Nov 2011 Airframe Gear Downlock Swivels. RN LSA14- 5098. 5263 through 15C45 5298. 5300. 5301. 5302. 5303. 5305 through 5318. 5320 through 5325 and 5330. Compliance with this customer bulletin is required within 90 days of the release date. CB CB 116 Inspection - Engine / Auxiliary 5001 - 5352. Due 981160 MAN CPN 2194.0 670 14 Nov 2011 C 0.00 Airframe Power Unit (APU) Fire Bottle Thermal within 90 days Relief Discharge Port Mx. Notes: see F111124 for details CB CB 117 Inspection Flight Data Aircraft serial numbers 981170 CAN 14 Feb 2012 I Airframe Recorder (FDR) and Cockpit Voice 5276 through 5341 Recorder (CVR) Mounting Hardware and 5348. excluding 5305. Compliance with this customer bulletin is required within 12 months of the release date. Cancelled see CBI I7A CB CB 117A Inspection - Flight Data Aircraft serial numbers 981171 MAN N/A 22 Mar 2012 I Airframe Recorder (FDR) and Cockpit Voice 5276 through 5341 Recorder (CVR) Mounting Hardware and 5348. excluding 5305. Compliance with this customer bulletin is required within 12 months of the release date. CB CB 118 Inspection Stringer 6 Compliance with this 981180 MAN 14 Feb 2012 I Airframe Longeron Above Main Entrance Door customer bulletin is required within 12 months of the release date. Aircraft serial numbers 5306 through 5341, 5343. and 5348 G-CGUL G550 5176 Technical Bulletins Page 121 of 164 20 Jan 2015 C12015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620911 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No CB CB 119 Inspection (Part I) - Auxiliary All G550 aircraft 981190 CAN CAN 0.0 0 29 Feb 2012 C 0.00 Airframe Power Unit (APU) Enclosure Thermal having Aircraft Service Barrier Coating Change (ASC) 090. ASC 090 AM1 and/or ASC 090A incorporated. Compliance with Part I of this customer bulletin is to be accomplished within 90 days of release. NOTE: FOLLOWING COMPLIANCE WITH PART I. ADD APPROPRIATE FREQUENCY SCHEDULE TO PART II (981191). Cancelled see 981192 CB CB 119 Inspection (Pan II) • Auxiliary All G550 aircraft 981191 CAN CAN 29 Feb 2012 I Airframe Power Unit (APU) Enclosure Thermal having Aircraft Service Barrier Coating Change (ASC) 090. ASC 090 AM1 and/or ASC 090A incorporated. See CB for inspection interval. Cancelled see 981193 G-CGUL G550 5176 Technical Bulletins Page 122 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620912 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LDG Date CA MM REF M HRS aintenance Notes Cert No CB CB 119A Inspection (Pan I) • Auxiliary Aircraft serial numbers 981192 MAN N/A 2354.5 711 20 Mar 2012 C 0.00 Airframe Power Unit (APU) Enclosure Thermal 5001 through 5249 Barrier Coating having Aircraft Service Change (ASC) 090, ASC 090 AM1 and/or ASC 090A incorporated, excluding 5011, 5225 and 5245. Compliance with Part I of this customer bulletin is to be accomplished within 90 days of release of original CB 119 (2.29.12). NOTE; FOLLOWING COMPLIANCE WITH PART I, ADD APPROPRIATE FREQUENCY SCHEDULE TO PART II (981193). Mx. Notes: N/A as ASC90 not embodied CB CB 119A Inspection (Pan II) • Aircraft serial numbers GAMA 981193 MAN N/A AVIATION 2409.1 723 16 May 2012 Auxiliary Power Unit (APU) Enclosure 5001 through 5249 Airframe Thermal Barrier Coating having Aircraft Service Change (ASC) 090, ASC 090 AM1 and/or ASC 090A incorporated, excluding 5011, 5225 and 5245. NOTE: FOLLOWING COMPLIANCE WITH PART I, ADD APPROPRIATE FREQUENCY SCHEDULE TO PART I. Mx. Notes. NiA as ASC90 not embodied G-CGUL G550 5176 Technical Bulletins Page 123 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620913 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No CB CB 120 Inspection Engine High Aircraft serial numbers GAC-LTN 981200 MAN N/A 2354.6 711 19 Apr 2012 C Airframe Pressure (HP) Fuel Filter Assembly 5280, 5285. 5288. FL016471 Housing Cap Seal r Seal Ring 5292 and 5294. Compliance with this customer bulletin is required within 12 months of the release date. UK.145.00883 CB CB 121 Part I Inspection - Flight SiN 5038. 5079. 5223, 981210 MAN N/A 23 Mar 2012 I Airframe Control Surfaces Paint Thickness 5227, 5237. 5240. 5245, 5246. 5252. 5258, 5261. 5265. 5267, 5283. 5290. 5293, 5294. 5302. 5307, 5311. 5318. 5320 due within 90 days CB CB 121 Part II Inspection Flight SiN 5038. 5079. 5223, 981211 MAN N/A 23 Mar 2012 I Airframe Control Surfaces Paint Thickness 5227, 5237. 5240. 5245, 5246. 5252. 5258, 5261. 5265. 5267, 5283. 5290. 5293, 5294. 5302. 5307, 5311. 5318. 5320 due within 12 months CB CB 122 Replacement - Fuel Boost Sri%) 5001 5340. due GAG-LIN 981220 MAN CAN 2490.4 746 07 Aug 2012 C Airframe Pumps. PeN 1159SCP500-5 within 42 months. CB FL016819 installs PN 1159SCP500.7 (supplier part number 31760.3) Fuel Boost Pumps. Add 500 HRS freq to ATA's 282651. 282652. 282653. and 282654 as applicable. UK.145.00883 G-CGUL G550 5176 Technical Bulletins Page 124 of 164 20 Jan 2015 41)2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620914 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No CB CB 123 Inspection - Rudder Actuator Aircraft serial numbers 981230 CAN NIA 06 Jun 2012 I Airframe Pressure Monitoring Pod Plugs 5001 through 5143. 5156 and 5225. Due within 36 months from date of CB 123 release • &June 2012. Cancelled by CB 123k CB CB 123A Inspection - Rudder Effectivity: Aircraft 981231 MAN NIA 08 Aug 2012 I Airframe Actuator Pressure Monitoring Port serial numbers 5001 Plugs through 5143. 5156 and 5225 with rudder actuators having serial number 0367 and prior. Due within 36 months from date of original CB 123 release • 6 June 2012. CB CB 124 Replacement - Nose Wheel Effectivity: Aircraft GAG LTN 981240 MAN CAA/ 2490.3 746 13 Aug 2012 C Airframe Steering Collar Hardware serial numbers 5001 FL016819 through 5349. Compliance with this customer bulletin is required within 24 months of release date (2 August. 2012). UK.145.00883 CB CB 125 Removal - Aileron and Effectivity: Aircraft 981250 27 CAN CAN 0.0 0 01 Apr 2013 C 0.00 Airframe Elevator Power Disconnect (ASC 099) serial numbers 5001 through 5389. Compliance with this customer bulletin is required within 24 months of the release date (21 August, 2012). Canceled see 981251 Mx. Notes. This code has been cancelled. See Compliance Remarks by ticking Show Remarks link G-CGUL G550 5176 Technical Bulletins Page 125 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620915 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No CB CB 125A Removal - Aileron and Effectivity: Aircraft GAC LTN 981251 MAN CW 2849.4 833 04 Apr 2013 C Airframe Elevator Power Disconnect (ASC 099) serial numbers 5001 BMX000145 through 5389. Compliance with this customer bulletin is required within 24 months of the original issue date (21 August. 2012). UK.145.00883 CB CB 126 Software Modification - Digital Effectivity: Aircraft 981260 31 CAN CAN 0.0 0 01 Apr 2013 C 0.00 Airframe Flight Data Recorder serial numbers 5278 through 5342. Compliance with this customer bulletin is required within 24 months of the release date (22 August. 2012). Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link. CB CB 126A Software Modification - Effectivity: Aircraft 981261 MAN N/A 02 Oct 2012 I Airframe Digital Flight Data Recorder serial numbers 5278 through 5344. Compliance with this customer bulletin is required within 24 months of the release date of CB 126 (22 August. 2012). CB CB 127 Inspection XM Weather Effectivity: Aircraft GAA 981270 MAN N/A AVIATION 2558.6 761 10 Aug 2012 Antenna Doubler Installation serial numbers 5001 Airframe through 5277 with XM Weather antenna. PN 4092744.901.installed prior to October 1. 2010. CAMO CB CB 128 - Inspection - Aft Equipment Effectivity: Aircraft 981280 MAN N/A 11 Oct 2012 Airframe Bay / Engine Pylon Temperature serial numbers 5354 Sensor Switches through 5356. 5358. 5359 and 5362. Due within 24 months G-CGUL G550 5176 Technical Bulletins Page 126 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620916 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No CB CB 129 • Replacement • Elevator Aircraft serial numbers 981290 CAN CAN 0.0 0 16 Jul 2013 C 0.00 Airframe Horn Bearings 5063 through 5160 and 5171. excluding 5123. 5124 and 5133. Compliance with this customer bulletin is required within 24 months from the original issue date of November 8, 2012. Cancelled by CB 129A issued July t6, 2013. Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link CB CB 129A • Replacement - Elevator Aircraft serial numbers 981291 27 REQ N/A 16 Jul 2013 Airframe Horn Bearings 5063 through 5160 and 5171, excluding 5123, 5124 and 5133. Compliance with this customer bulletin is required within 24 months from the original release date of November 8, 2012. Aircraft operators who have previously complied with CB 129 are in compliance with this revision and should return the service reply card marked Previously complied with' . CB CB 130 Aileron Cable Feed-Thru Aircraft serial numbers GAC LTN 981300 MAN OW 2849.4 833 11 Apr 2013 C Airframe Holes at FS 576.5 (ASC 104) 5001 thru 5404. BMX000145 Compliance with this customer bulletin is required within 24 months from the original issue date of November 15. 2012. This customer bulletin requires incorporation of Aircraft Service Change 104. which contains all applicable regulatory agency approval information. UK.145.00883 G-CGUL G55O 5176 Technical Bulletins Page 127 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620917 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No CB CB 131 Inspection - Cabin Window Aircraft serial numbers GAC LTN 981310 MAN CAN 3029.7 875 27 Sep 2013 C Airframe Seals 5150 through 5300. BMX000258 Compliance with this customer bulletin is required within 48 months from the original release date of December 21. 2012. UK.145.00883 CB CB 132 - Flight Controls (ATA 27). CB 132 cancelled see 981320 CAN N/A 16 Jan 2013 1 Airframe Inspection Gust Lock Handle CB 132A. Assembly on Aircraft with ASC 002 CB CB 132A Flight Controls (ATA 27). Aircraft serial numbers 981321 MAN N/A 04 Feb 2013 1 Airframe Inspection Gust Lock Handle 5001 thru 5174 with Assembly on Aircraft with ASC 002 ASC 002 incorporated. Compliance with this customer bulletin is required within 24 months from the original release date of January 16. 2013. This customer bulletin revision replaces CB 132. Aircraft operators who have previously complied with CB 132 are in compliance with this revision and should return the service reply card marked Previously complied with: CB CB 133 - Fire Protection (ATA 26). Cancelled. See 981330 CAN CAN 0.0 0 17 Jan 2013 C 0.00 Airframe Modification - Relocation of Third Revision A. Engine Fire Bottle G-CGUL G550 5176 Technical Bulletins Page 128 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620918 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No CB CB 133A • Fire Protection, Aircraft serial numbers GAL CAMO 981331 MAN N/A 3210.9 909 07 Jan 2014 C 0.00 Airframe Modification • Relocation of Third 5001 through 5294 Engine Fire Bottle with third engine fire bottle installed. Compliance with this customer bulletin is required within 24 months from the original release date of January 16. 2013. Mx. Notes: Third fire bottle not fitted CB CB 134 - Inspection • Tail Cone Effectivity: Aircraft 981340 MAN N/A 14 May 2013 I Airframe Anticollision Light • Fault Indicator 5190 - 5296, 5298. Wiring 5300 - 5304, 5306 • 5325 and 5330. Compliance with this customer bulletin is required within 12 months from the original release date of May 14, 2013. CB CB 135 - Replacement - Main Battery Effectivity: Aircraft 981350 24 CAN CAN 0.0 0 05 Jul 2013 C 0.00 Airframe Chargers serial numbers 5379, 5380, 5382, 5383, 5384. 5391 and 5392. Compliance with this customer bulletin is required within 12 months from the original release date of July 3. 2013. Cancelled ref CB 135A Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link CB CB 135A • Replacement Main Effectivity: Aircraft 981351 24 MAN N/A 05 Jul 2013 Airframe Battery Chargers serial numbers 5379, 5380, 5382, 5383, 5384, 5391 and 5392. Compliance with this customer bulletin is required within 12 months from the original release date of July 3, 2013. G-CGUL G550 5176 Technical Bulletins Page 129 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620919 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No CB CB 136 - Modification - Plug-in Aircraft serial numbers 981360 23 REQ N/A 16 Jul 2013 Airframe Monitors, P/N 7002.260 and 7002- 5255 through 5341 261. Installed with AVDS having Audio Distribution system (AVDS) installed. Compliance with this customer bulletin is required within 24 months from the original issue date of July 16. 2013. CB CB 137 - Inspection • Air Inlet Door Effectivity: Aircraft 981370 49 REO NA 17 Jul 2013 Airframe Actuator 5270, 5271, 5290, 5293 through 5296, 5298 through 5300, 5321 through 5323, 5360, and 5383 This condition is suspected on actuators, PN SVLC-52630.2. serial numbers 437, 438, 462 through 472,499 through 501, 590 through 596 and 599 through 603. Compliance with this customer bulletin is required within 12 months from the original issue date of July 17. 2013. G-CGUL G550 5176 Technical Bulletins Page 130 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620920 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No CB CB 138 • Replacement • Air Inlet Door Effectivity: Aircraft 981380 49 REQ N/A 17 Jul 2013 Airframe Actuator 5347. 5349, 5350, 5352. 5353, 5354 and 5358. This condition affects actuator serial numbers 540, 541, 543. 544. 547, 548 and 549. This customer bulletin is a one•time action to inspect the affected aircraft, verify installation of affected serial numbers and replace the actuators. Compliance with this customer bulletin is required within 12 months from the original issue date of July 17, 2013 CB CB 139- Inspection • Outboard Effectivity: Aircraft 981390 27 MAN N/A 09 Oct 2013 I Airframe Rudder Trim Cable Installation at serial numbers 5388 Fuselage Station 733 through 5404, 5406, 5407. 5410 and 5413. Compliance with this customer bulletin is required within 12 months from the original issue date of October 9. 2013. CB CB 140- Inspection • Fuel Boost Effectivity: Acft SIN 981400 MAN N/A 09 Dec 2013 Airframe Pump Electromagnetic Interference 5254 - 5404. (EMI) Filter Connectors Compliance with this smite bulletin is required within 12 months from the original issue date of December 9. 2013. G-CGUL G550 5176 Technical Bulletins Page 131 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620921 TYP C/W Source Code Description Effectivity ATA Status ilLogbook Work Order HRS LDG Date C/I MM REF M HRS aintenance Notes Cert No CB CB 141 Inspection - Main Landing s/n 5001 thru 5411. GAC LTN 981410 MAN CAN 3444.5 949 21 Oct 2014 Airframe Gear Timers - Striker Arm Shaft 5412. 5414. 5415. BMX000542 5418. 5424. 5428 and 5429. due at next Main Landing Gear Components Detailed Corrosion Inspection (cmp 321003 / 321004) within 48 months from original date of bulletin issue 12.31.2013 UK.145.00883 CB CB 142 - Replacement Motive Flow Effectivity: Aircraft 981420 28 MAN N/A 08 Jan 2014 Airframe Lines for Mid-Wing Fuel Ejector (ASC serial numbers 5189. 063A) 5203. 5279. 5302 and 5314. Compliance with this customer bulletin is required at the next scheduled Aircraft Maintenance Manual (AMM) Chapter 5. Wing TarJc Internal BL 0 — BL 180 — Detailed Inspection. within 48 months from the original issue date of January 8. 2014. CB CB 143 - Inspection Engine Effectivity: Aircraft 981430 72 MAN NA Airframe Removable Fairings - Non- serial numbers 5385 Conformance through 5387 and 5389 through 5393. Compliance with this customer bulletin is required within 12 months from the original issue date of January 9. 2014. not to exceed 500 flight hours after receipt of the respective NMSBs. G-CGUL G550 5176 Technical Bulletins Page 132 of 164 20 Jan 2015 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620922 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No CB CB 144 Inspection - Passenger Effectivity: Aircraft 981440 35 MAN N/A 20 Jan 2014 Airframe Oxygen System - Tube Assembly serial numbers 5365. Bonding 5381. 5385. 5394. 5395. 5400. 5407 and 5418. Compliance with this customer bulletin is required within 12 months from the original issue date of January 20. 2014. CB CB 145 - Elevator Hardover Aircraft serial numbers GAC LTN 981450 MAN CPN 3444.5 949 04 Nov 2014 C Airframe Prevention System (HOPS) 5001 through 5468. BMX000542 Improvement (ASC 112) Compliance with this customer bulletin is required within 24 months from the original issue date of April I0. 2014. UK.145.00883 CB CB 146 - Inspection - Transformer Effectivity: Aircraft 981460 24 MAN N/A 15 May 2014 I Airframe Rectifier Unit (TRU) Feeder Cable serial numbers 5410 Clamp Installation through 5442. 5452 and 5454. excluding 5434 and 5437. Compliance with this customer bulletin is required within 12 months from the original issue date of May 15. 2014. CB CB 147 - Inspection - Right Electrical Effectivity: Aircraft 981470 24 MAN N/A 15 May 2014 I Airframe Equipment Rack (REER) Circuit serial numbers 5365. Breaker Terminals 5394 and 5395.Compliance with this customer bulletin is required within 12 months from the original issue date of May 15. 2014. G-CGUL G550 5176 Technical Bulletins Page 133 of 164 20 Jan 2015 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620923 TYP CNV Source Code Description Effectivity IATAI Status Logbook Work Order HRS LOG Date CA MM REF M HRS Maintenance Notes Cert No CB CB 148 • Inspection • Pressure Relief Compliance with this 981480 MAN NIA 05 Jun 2014 I Airframe Valve Remote Air Filler customer bulletin is required within 12 months from the original issue date of June 5, 2014 CB CB 149 - Inspection • Auxiliary Power Effectivity: Aircraft 981490 49 CAN CAN 0.0 0 05 Aug 20t4 C 0.00 Airframe Unit (APU) Mount Pallet Shimming serial numbers 5001 through 5411. Compliance with this customer bulletin is required within 24 months from the original issue date of July 16, 2014. Cancelled by CB 149A(981491) Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link CB CB 149A • Inspection • Auxiliary Effectivity: Aircraft GAC LTN 981491 49 MAN CM 3444.5 949 23 Oct 2014 C Airframe Power Unit (APU) Mount Pallet serial numbers 5001 BMX000542 Shimming through 5411. Compliance with this customer bulletin is required within 48 months from the original issue date of July 16. 2014. UK.145.00883 CB CB 150 - Modification - Aircraft Main Effectivity: Aircraft 981500 24 CAN CAN 0.0 0 03 Oct 2014 C 0.00 Airframe Battery Chargers serial numbers 5001 through 5482. Compliance with this customer bulletin is required not later than August 15, 2016 as referenced in ELDEC Service Bulletin 8-842- 24-02. Canceled by CB 150A(981501). Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link. G-CGUL G550 5176 Technical Bulletins Page 134 of 164 20 Jan 2015 ®2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620924 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No CB CB 150A - Modification - Aircraft Main Effectivity: Aircraft 981501 24 MAN 03 Oct 2014 I Airframe Battery Chargers serial numbers 5001 through 5482. Compliance with this customer bulletin is required not later than August 15.2016 as referenced in ELDEC Service Bulletin 8.842- 24.02. CB CB 151 Inspection - Cockpit Center Effectivity: Aircraft 981510 27 MAN N/A 11 Sep 2014 I Airframe Pedestal Assembly Gust Lock Bell serial numbers 5354. Crank Bearings 5355. 5357 through 5360. 5362 through 5364. 5366 through 5428. 5430 through 5450. 5452. 5453 and 5455. Compliance with this customer bulletin is required within 24 months from the original issue date of September II. 2014. CB CB 152 - Inspection - Forward Cabin Effectivity: Aircraft 981520 25 MAN N/A 18 Sep 2014 I Airframe Pocket Door Bulkhead at FS 256 serial number 5385. Compliance with this customer bulletin is required within 12 months from the original issue date of September 18. 2014. CB CB 153 - Inspection - Cockpit Effectivity: Aircraft GAC LTN 981530 24 MAN CPN 3444.5 949 23 Oct 2014 C Airframe Overhead Circuit Breaker Panels serial numbers 5072 BMX000542 through 5428. 5430 through 5433 and 5435 through 5446. 5448 and 5454. Compliance with this customer bulletin is required within 24 months from the original issue date of September 18. 2014. UK.145.00883 G-CGUL G550 5176 Technical Bulletins Page 135 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620925 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No CB CB 154 Inspection - Rudder Actuator Effectivity: Aircraft GAC LTN 981540 27 MAN CM 3444.5 949 23 Oct 2014 C Airframe Aft Rod End Attaching Hardware serial numbers 5001 BMX000542 through 5450. Compliance with this customer bulletin is required within 36 months from the original release date of October 16. 2014. UK.145.00883 CB CB 155 - Inspection - Engine Driven Effectivity: Aircraft GAC LTN 981550 29 MAN CM 3444.5 949 23 Oct 2014 C Airframe Pump (EDP) Case Drain Hydraulic serial numbers 5001 BMX000542 Hose - Left Engine Pylon (ASC 120) through 5494. Compliance with this customer bulletin is required within 24 months from the original issue date of October 20. 2014. UK.145.00883 CB CB 156 Replacement - Engine Driven Effectivity: Aircraft 981560 29 MAN 07 Jan 2015 Airframe Pump (EDP) Hydraulic Damper serial numbers 5450 through 5455. 5457 through 5462 and 5466. Compliance with this customer bulletin is required within 18 months from the original issue date of January 7. 2015. AD 990010 ACB 1 WIRING/O2 BOTTLE PART1 Eft. Desc: 5001.5051. 24 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe AD 990011 ACB I WIRING/O2 BOTTLE PART2 Eff. Desc: 5001.5051. 24 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe AD 990020 ACB 2 ASCB NOISE TEST Eff. Desc: 5001.5056. 31 MAN N/A 0.0 0 26 Nov 2007 C 31.41-00 0.00 Airframe AD ACB 3 DE-ACTIVATION-ADEL WITHIN 25HRS.NOT 990030 25 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe WIGGINS FLOOR HEATER SYSTEM TO EXCEED 30 DAYS. G550 5001- 5075 WITH WIGGINS PADS G-CGUL G550 5176 Technical Bulletins Page 136 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620926 TYP C/W Source Code Description Effectivity ATA Status ilLogbook Work Order HRS LDG Date C/I MM REF M HRS aintenance Notes Cert No AD ACB 4A WING RIB EFF:500I -5051 DUE 99W41 57 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe REINFORCEMENT ANGLES 15 DAYS FROM ISSUE DATE. AD ACB 5 INSPECT GOODYEAR NLG Goodyear SB 2005.32 990050 32 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe TIRES -004 - EFF:P:N 217K22-1(Gulfstream P/N: 1159SCL507-1) / Tire SIN Range 22710000 to 22739999 / This bulletin also applies to spare tires operators may have in stock. / Compliance with this Alert CB is to be accomplished by 10125105. AD ACB 6A AIL/ELEV ACT LOAD EFFECTIVITY: S:N 990061 27 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe RELIEF BUNGEES 5001.50931! This ACB cancels and supetcedes ACB 6. NC that have previously complied with ACB 6 must comply with this ACB Revision. /1 Compliance with this ACB revision is to be accomplished within the next 30 Days. AD ACB 7 Pt 1-Inspect Water System 5001.5099.except 990070 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe Valves 5014.5037.5044.5069. Due within 20 hours AD ACB 7 Pt 2-Inspect Water System 5001.5099. except 990071 38 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe Valves 5014,5037.5044.5069 due at next maint opportunity AD ACB 7 Pt 3-Inspect Water System 5001.5099. except 990072 38 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe Valves 5014,5037.5044.5069. Due within 12 mos G-CGUL G550 5176 Technical Bulletins Page 137 of 164 20 Jan 2015 e 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620927 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No AD ACB 8 Modification-Tail Compartment S/N 5100, 5103-5159 gama fab 990080 25 MAN C/W 360.6 141 06 Nov 2008 C 0.00 Airframe Ladder having ASC 62 and F081108 5160.5212. Due within 30 days. AD ACB 9 Operational Limitations • Aircraft serial numbers 53 CAN OW 564.2 191 29 May 2009 C Airframe 990090 Auxiliary Power Unit (APU) 5001 through 5219 excluding 5205 and 5218. Compliance with this alert customer bulletin is to be accomplished within the next 21days.Cancelled see ACB 9A AD ACB 9A • Operational Limitations - 5001 through 5219 GAMA FAB 990091 53 MAN CAN 609.6 211 05 Jul 2009 C 0.00 Airframe Auxiliary Power Unit (APU) excluding 5205 and 5218. This alert customer bulletin revision is a one-time action to incorporate Revision 1 of AFM supplement G550- 2009.03 or JAA-G550. 2009-02, as applicable, into the AFM. Compliance with this alert customer bulletin revision is to be ccomplished within the next 21 days. Mx. Notes. SUPPLEMENT INSERTED INTO AFM G-CGUL G550 5176 Technical Bulletins Page 138 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620928 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No AD ACB 10 Pan I - Inspection - Third Aircraft serial numbers gama 990100 CAN CIW 1639.8 497 07 Dec 2010 C 0.00 Airframe Engine Fire Bottle Installation 5001 through 5308. Compliance with this alert customer bulletin is required with 21 days of the release date. Part I is a one- time action to inspect for. and report. the installation of a third engine fire extinguisher bottle. Part II. if applicable, is a one-time action to remove any mounted spare fire bottles. Mx. Notes: records researched no third bottle found installed AD ACB 10 Pan II - Inspection - Third Aircraft serial numbers gama 990101 CAN NIA 1639.8 497 07 Dec 2010 C 0.00 Airframe Engine Fire Bottle Installation 5001 through 5308. Compliance with this alert customer bulletin is required with 21 days of the release date. Part I is a one- time action to inspect for. and report. the installation of a third engine fire extinguisher bottle. Part II. if applicable. is a one-time action to remove any mounted spare fire bottles. Mx. Notes: not applicable as no third bottle installed G-CGUL G550 5176 Technical Bulletins Page 139 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620929 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No AD ACB 10A Part 1 - Inspection - Third Effectivity: Aircraft 990102 26 MAN CPN 1672.6 505 22 Dec 2010 C 0.00 Airframe Engine Fire Bottle Installation serial numbers 5001 through 5308. Compliance with this alert customer bulletin revision is required with 21 days of the release date of the original alert customer bulletin dated December 6. 2010. Operators who have previously complied with ACB 10 may report this alert customer bulletin as "Previously complied with". Mx. Notes: PCW IAW ACB 10 AD ACB 10A Part 2 - Inspection - Third Effectivity: Aircraft 990103 26 MAN N/A 1672.6 505 22 Dec 2010 C 0.00 Airframe Engine Fire Bottle Installation serial numbers 5001 through 5308. Compliance with this alert customer bulletin revision is required with 21 days of the release date of the original alert customer bulletin dated December 6. 2010. Operators who have previously complied with ACB 10 may report this alert customer bulletin as "Previously complied with". Mx. Notes: NO THIRD BOTTLE FITTED AD FAA AD 2011-01.09 BIE 990109 MAN N/A 1672.6 505 20 Dec 2010 C 0.00 Airframe AEROSPACE PBE PIN 119003.11 IDENTIFICATIONREPLACEMENT Mx. Notes: NOT APPLICABLE TO PBES PIN MR-10039N INSTALLED G-CGUL G550 5176 Technical Bulletins Page 140 of 164 20 Jan 2015 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620930 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No AD ACB 11 - Operational Limitations - 5001 through 5249 990110 49 MAN N/A 2235.2 677 12 Dec 2011 C 0.00 Airframe Auxiliary Power Unit (APU) Enclosure with ASC 090. with Thermal Barrier Coating excluding 5007. 5015. 5024. 5047. 5056. 5057. 5090. 5098. 5115.5160. 5168. 5188. 5202. 5212. 5218. 5233 and 5249. Compliance with this alert customer bulletin is required within 15 days of the release date. Mx. Notes: see F111223 ASC 090 not complied with so NrA AD ACB 12 Operational Limitations - Aircraft serial numbers 990120 MAN 14 May 2012 I Airframe Auxiliary Power Unit (APU) Enclosure 5015. 5057. 5168. with Thermal Barrier Coating - 5188. 5202. 5212 and Expanded Effectivity 5233. Compliance with this alert customer bulletin is required within 15 days of the release date. This alert customer bulletin is a one time action to incorporate Airplane Flight Manual Supplement G550- 2009.03. Revision 1 or JAA.G550.2009.02. Revision 1. as applicable, into the Airplane Flight Manual (AFM). AD EASA AD 2010.0204 Mode S 990204 MAN N/A 1529.8 467 II Oct 2010 C 0.00 Airframe Transponder modificationfrei3lacement Mx. Notes: n/a no affected parts installed AD EASA AD 20090180 RI APU 990980 MAN N/A 1655.9 502 10 Dec 2010 C 0.00 Airframe enclosure firewall inspectiowlimitation Mx. Notes: N/A BY EFFECTIVITY AD 9910001 Cabin Interior STC ST02519CH-D OPT CPN 20.7 1 30 Apr 2008 C 0.00 Airframe G-CGUL G550 5176 Technical Bulletins Page 141 of 164 20 Jan 2015 CO 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620931 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No AD 992204 AD 2002.21.01 Britax Sell Appliances Elf. Desc: (12 MOS). 00 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe AD 8R700 900229 992301 AD 2003.07.11 L ENG FAN DISC Eft. Desc: ALL ACFT. 72 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe REV 5 AD BR700-900229 992302 AD 2003.07.11 R ENG FAN DISC Eft. Desc: ALL ACFT. 72 MAN N/A 0.0 0 26 Nov 2007 C REV 5 0.00 Airframe AD KIDDE 898052 992310 AD 2003.26.14 898052 FIRE BOTTL Elf. Giese: ALL ACFT. 26 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe -26-449 AD 992401 AD 2004.0201 LG Select Dump 32 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe Valve AD AD 2004.22.16 WIRE HARNESS Eli. Desc: 5001.5051 992412 24 MAN N/A 0.0 0 26 Nov 2007 C ACBI 0.00 Airframe CLEAR (25HRS). AD AD 2005.0406 COCKPIT FLIGHT Eft. Dose: 5001.5062 992503 31 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe PANEL DISPLAYS (WITHIN 50 HRS OF 2/23105) REPEAT @ 60 DAY INTERVAL THEREAFTER. ACCOMPLISH TERMINATING ACTION.ASC43& 902.WITHIN 300 HRS OR 90 DAYS. AD AD 2005.16.14 ADEL Wiggins Floor DUE WITHIN 25 FLT 992509 Heater Deactivation 25 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe HRS OR 30 DAYS AFTER EFFECTIVE DATE OF AD. AD AD 2005.20.26 Aviointeriors Model See AD for Initial and 992513 25 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe 312 Seats Repetelive requirements if seats are installed in the Aircraft G-CGUL G550 5176 Technical Bulletins Page 142 of 164 20 Jan 2015 © 2015 Gulfsffeam Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620932 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No AD EASA AD 2005-0001 Insert Gulfstream 992550 MAN NIA 0.0 0 10 Sep 2012 C 0.00 Aidrame IndicatingMaming System • Aerospace Operating procedures and Right Corporation G550 Manual Airplane Flight Manual Revision 2. Dated 12 Jan 2005 into the JANEASA Aircraft Flight Manual. Ref GAC•AC-JAA-G550• OPS-0001. This AD supersedes EASA member state AD number: United Kingdom G-2004- 0033. AD AD 2006.04.13 AFM Procedures, AD 2006.04.13 has 992602 CAN CM 2535.4 756 21 Sep 2012 C 0.00 Airframe Cockpit Displays Malfunction been revised by AD 2006-04-13R1. Mx. Notes: Re-certified compliance at this date. AD AD 2006.04.13 RI AFM Procedure, EFF: GAC Model GAL 992603 99 MAN CM 0.0 0 26 Nov 2007 C 0.00 Airframe Ckpt Displays Malfunction X series NC, certificated in any category. Serial numbers 4001 and sub, and GAC Model GV-SP series NC, certificated in any category. serial numbers 5001 and sub, on which GAC Mod ASC-904 or production equivalent has been incorp. AD AD 2006-11-03 Insp Aileron 8 All GV NC, G500 & 992604 27 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Aidrame Elevator Act. Assy. G550 NC Snits 5001. 5052. Due within 500 hrs after the Eff. date of this AD (June 29, 2006). Related Tech Bulletins: G550 - CB4 G500 • CB4 / GV • CB 123. Terminating Replacement: G550 - CB6 / G500 - CB6 / GV CB124. G-CGUL G550 5176 Technical Bulletins Page 143 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620933 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No AD AD 2006.18.08 Goodyear Aviation This AD 2006.18-08 992608 32 MAN CM 0.0 0 26 Nov 2007 C 0.00 Airframe Tires This AD 2006.18-08 Goodyear Aviation Tires is a one-time inspection of the nosewheel tires to determine if they are within designated serial number range or if replacement is nessary. AD AD 2006.18.13 Aileron HOPS Wire This A.D. "IS NOT' 992609 27 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe Harness Effective till October 13. 2006. Due within 12 months of Effective date. EFF: SN 674- 693. AD AD 2006.1904 Honeywell Effective 10.17-06. 992610 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe International (14 Day) due within 14 days. revise AFM. AD AD 2006.19.04 Honeywell Effective 10.17-06. Jet Aviation 992611 MAN CPN Geneva 513.0 177 03 Feb 2009 C 0.00 International (18 Month) replace ID plates. Airframe within 18 Months. GVBTC003 AD EASA AD 2006-0334 R1 THALES EASA AD 992614 MAN N/A 648.8 225 22 Jul 2009 C 0'00 Airframe COMMUNICATIONS VHF DATA 2006-0334 RI RADIO MODIFICATION Mx. Notes: NOT APPLICABLE AFFECTED EQUIPMENT NOT FITTED AD EASA AD 2006-0220 RECARO EASA AD 992615 MAN N/A 648.8 225 22 Jul 2009 C 0.00 Airframe PASSENGER SEATS INSPECTION 2006-0220 OF SEAT BELT SHACKLE Mx. Notes: NOT APPLICABLE AFFECTED EQUIPMENT NOT FITTED AD EASA AD 2006-0241 CALEDONIAN EASA AD 992616 MAN N/A 648.8 225 22 Jul 2009 C 2006-0241 0.00 Airframe AIRBORNE SYSTEMS AUTO DEPLOYABLE ELT Mx. Notes: NOT APPLICABLE AFFECTED EQUIPMENT NOT FITTED AD 992617 EASA AD 2006-0265 MODE C 8 S EASA AD MAN N/A 648.8 225 22 Jul 2009 C 0.00 Airframe TRANSPONDER CHECK 2006-0265 Mx. Notes: NOT APPLICABLE AFFECTED EQUIPMENT NOT FITTED G-CGUL G550 5176 Technical Bulletins Page 144 of 164 20 Jan 2015 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620934 TYP C/W Source Code Description Effectivity ATA Status ilLogbook Work Order HRS LDG Date C/I MM REF M HRS aintenance Notes Cert No AD EASA AD 20060269 HONEYWELL EASA AD 992618 MAN N/A 648.8 225 22 Jul 2009 C 0.00 Airframe INTERNATIONAL INC MST 67A 20060269 MODE S TRANSPONDER MODIFICATION Mx. Notes: NOT APPLICABLE AFFECTED EQUIPMENT NOT FITTED AD EASA AD 20060375 CARLING EASA AD 992619 MAN N/A 648.8 225 22 Jul 2009 C 0.00 Airframe TECHNOLOGIES SWITCH 20060375 INSPECTION/REPLACEMENT Mx. Notes: NOT APPLICABLE AFFECTED EQUIPMENT NOT FITTED AD EASA AD 20060286 R1 EASA AD 992620 MAN N/A 648.8 225 22 Jul 2009 C 0.00 Airframe INTERTECHNIQUE O2 CYLINDERS 2006-0286 R1 REMOVAUEMPTYING Mx. Notes: NOT APPLICABLE AFFECTED EQUIPMENT NOT FITTED AD 992704 AD 2007.07.12 Honeywell Nav NOTE: Due with 14 AC 34 CAN N/A GETON APP 20.7 11 09 Apr 2008 C 0.00 Computer days of &0711 Airframe Applicable to all FP549 Honeywell NZ-2000 Navigation Computers and all IC-800 Integrated Avionics Computers If Reference: Honeywell Technical Newsletter A23-6111.008. Revision 001. Dated 02+22+2007. Superceded by 992901.This AD does not apply to G500. G550 -(not applicable to Planeview software). CRS G1FR100Y AD EASA AD 2007-0156 HONEYWELL EASA AD 992705 MAN N/A 648.8 225 22 Jul 2009 C 0.00 Airframe INTERNATIONAL COMM UNITS & 2007.0156 TRANSPONDERS MOD/REPLACEMENT Mx. Notes: NOT APPLICABLE AFFECTED EQUIPMENT NOT FITTED G-CGUL G550 5176 Technical Bulletins Page 145 of 164 20 Jan 2015 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620935 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No AD EASA AD 2007-0256 PACIFIC EASA AD 992706 MAN N/A 648.8 225 22 Jul 2009 C 0.00 Airframe SCIENTIFIC SEAT RESTRAINT 2007-0256 SYSTEM PLASTIC ROTARY BUCKLE HANDLE INSPECTION/REPLACEMENT Mx. Notes: NOT APPLICABLE AFFECTED EQUIPMENT NOT FITTED AD AD 2007-12-25 Water Drain / Supply Becomes effective 7-5- 992707 00 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe Valves 07. Within 20 hrs of AD date revise AFM per table 2. Before further flight perform functional checks. Optional Terminating action steps (HI) and (H2) ends requirement for repeat functional checks. AD AD 2007-12-25 Water Drain/Supply Optional Terminating 992708 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe Valves (Terminating Action) action steps (HI) and (H2) ends requirement for repeat functional checks. AD EASA AD 2008-0097 SIGMA AERO EASA AD 992804 MAN N/A 648.8 225 22 Jul 2009 C 0.00 Airframe SEATS 2008-0097 INSPECTION/REPAIRIMODIFICATIO N Mx. Notes: NOT APPLICABLE AFFECTED EQUIPMENT NOT FITTED AD EASA AD 2008-0135 EASA AD 992807 MAN N/A 648.8 225 22 Jul 2009 C 0.00 Airframe AVIOINTERIORS PASSENGER 2008-0135 SEATS BACKREST REPLACEMENT Mx. Notes: NOT APPLICABLE AFFECTED EQUIPMENT NOT FITTED AD EASA AD 2008-0159 HONEYWELL EASA AD 992808 MAN N/A 648.8 225 22 Jul 2009 C 0.00 Airframe INTERNATIONAL INC MST67A 2008-0159 MODE S TRANSPONDER MOD/REPLACEMENT Mx. Notes: NOT APPLICABLE AFFECTED EQUIPMENT NOT FITTED AD EASA AD 2008-0183 FUNKWERK EASA AD 992809 MAN N/A 648.8 225 22 Jul 2009 C 2008-0183 0.00 Airframe AVIONICS TRT800A/TRT800H MODE S TRANSPONDER REPLACEMENT Mx. Notes: NOT APPLICABLE AFFECTED EQUIPMENT NOT FITTED G-CGUL G550 5176 Technical Bulletins Page 146 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620936 TYP C/N/ Source Code Description Effectivity ATA Status Logbook Work Order HRS LDG Date C/I MM REF M HRS Maintenance Notes Cert No AD EASA AD 20080158 R2 FUNKWERK EASA AD 992810 MAN N/A 648.8 225 22 Jul 2009 C 0'00 Airframe AVIONICS TRT600 MODE S 2008-0158 R2 TRANSPONDER REPALCEMENT Mx. Notes: NOT APPLICABLE AFFECTED EQUIPMENT NOT FITTED AD EASA AD 20090097 Rockwell Collins EASA AD 992902 MAN N/A 648.8 225 22 Jul 2009 C 0.00 Airframe Mode S Transponder 2009-0097 inspection/modification Mx. Notes: NOT APPLICABLE AFFECTED EQUIPMENT NOT FITTED AD AD 2009.1701 Inspection For Effectivity: GV-SP 992902 49 MAN CM 686.6 234 22 Aug 2009 C 0.00 Airframe Sealant Applied To The Exterior Of series airplanes. The Auxiliary Power Unit (APU) having serial numbers Enclosure 5001 through 5204. and serial numbers 5206 through 5217. and serial number 5219 // Within 21 days after the effective date of this AD// Perform a general visual inspection of the exterior of the APU enclosure (firewall) to detect overcoat application of sealant on rivets or fillet seals on panel joints, in accordance with the accomplishment instructions of Gulfstream G550 Alert Customer Bulletin 9A including Service Reply Card // Mx. Notes: ACB 9A PREVIOUSLY COMPLIED WITH AD AD 2009.21.10 Avox Systems and Due within 90 days of 992903 CAN CAN 0.0 0 17 Dec 2009 C 0.00 Airframe BE Aerospace Oxygen Cylinder 12.17.09. Superceded Assemblies ref RI. code 992904. AD EASA AD 2009-0173 MODE S 992903 MAN N/A 648.8 225 22 Jul 2009 C 0.00 Airframe TRANSPONDER MODIFICATION/REPLACEMENT Mx. Notes: NOT APPLICABLE AFFECTED EQUIPMENT NOT FITTED G-CGUL G550 5176 Technical Bulletins Page 147 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620937 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No AD AD 2009.21.10 RI Avox Systems and This revision removes 992904 MAN N/A 1012.0 326 21 Feb 2010 C 0.00 Airframe BE Aerospace Oxygen Cylinder certain oxygen cylinder Assemblies part numbers from the applicability. Due within 90 days of 12- 17.09 Mx. Notes: not applicable no affected bottles installed AD EASA AD 2009-0251-E Portable Fire GAMA 992904 MAN N/A 825.4 274 28 Nov 2009 C 0.00 Airframe Extinguishers Halon 1211 (BCF) IdentificationlReplacement Mx. Notes: RECORDS CHECKED NIA TO PIN'S OR SINS INSTALLED AD EASA AD 2009-0180-E APU Revised by EASA AD 992951 MAN NIA 1145.2 362 26 Apr 2010 C 0.00 Airframe Enclosure Inspection 209-0180-R1. Mx. Notes: not applicable by effectivity AD EASA AD US-2009-17.01 APU 992952 MAN 31 Jul 2009 Airframe Enclosure Inspection-AFM (Supplement) Change AD EASA Emergency AD 2009-0251-E - Effectivity: Any aircraft 992956 26 MAN N/A 1145.2 362 26 Apr 2010 C 0.00 Airframe Portable Halon 1211 Fire operated under EASA Extinguishers regulations with Portable Halon 1211 (BCF) fire extinguishers. identified by Finished Goods (FG) part number and serial number (sin) in Appendix 1 of this AD // If any portable fire extinguisher identified as required by paragraph (1) of this AD is listed in Appendix 1 of this AD. before next flight. remove it from the aircraft and replace it with a serviceable unit. Mx. Notes: not applicable no fie bottles installed G-CGUL G550 5176 Technical Bulletins Page 148 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620938 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cr' MM REF M HRS aintenance Notes Cert No AD EASA AD 20090262 RI - Portable Effectivity: Any aircraft 992957 26 MAN NIA 1145.2 362 26 Apr 2010 C 0.00 Airframe Halon 1211 Fire Extinguishers operated under EASA regulations with Portable Halon 1211 (BCF) fire extinguishers. identified by Fire Fighting Enterprises Ltd (FFE) part number and serial number (sin) as identified in FFE ASB 26.115 Appendix 1 or as required by paragraph 1.1 of this AD // Within 30 days of this AD. remove the extinguisher from the aircraft and replace it with a serviceable unit. Mx. Notes: not applicable no He bottles installed AD EASA AD 20090262 Halon 1211 Fire gama lab 992957 MAN CM 837.9 280 15 Dec 2009 C 0.00 Airframe Extinguishers identification/replacement Mx. Notes: AD Part (1)(1.1) bottle identification carried out by records research.No affected bottles found fitted.No further action required AD EASA AD 2010-0003 RI Mode S EASA AD 992958 MAN N/A 1233.7 382 30 May 2010 C 0.00 Airframe Transponder type mode strapping 2010-0003 R1 check/mod. Mx. Notes: not applicable by transponder part number AD EASA AD 20100152 Avox systems ease ad 2010- 992959 MAN NIA 1479.2 446 30 Aug 2010 C 0.00 Airframe O2 mask regulator modification 0152 Mx. Notes: NOT APPLICABLE NO AFFECTED EQUIPMENT FITTED G-CGUL G550 5176 Technical Bulletins Page 149 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620939 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No AD AD 2010.01-03 Fire Fighting Effectivity: Any aircraft 993001 26 MAN N/A 1012.0 326 21 Feb 2010 C 0.00 Airframe Enterprises Limited Portable Halon operated under FAA 1211 Fire Extinguishers regulations, with Portable HaIon 1211 (BCF) fire extinguishers. manufactured by Fire Fighting Enterprises Limited, and not identified in paragraphs (g)(2)(i) and (g)(2)(ii) of the applicable AD. /1 Within 90 days after the effective date of this AD, replace portable Halon 1211 (BCF) fire extinguishers manufactured by Fire Fighting Enterprises Limited with serviceable lire extinguishers, except as provided by paragraph (g)(2) of this AD. Mx. Notes: not applicable no affected bottles installed AD AD 2010-25-05 Rolls Royce HP Effective Jan 13, 2011. 993007 MAN 0.0 0 13 Jan 2011 C 0.00 Engine 1 Turbine Stage 1 Disc Applies to Disc listed in Table 1 of the AD. see 993010/993011 for Stage 2 AD 993007 AD 2010-25.05 Rolls Royce HP Effective Jan 13, 2011. MAN 0.0 0 13Jan 2011 C 0.00 Engine 2 (993008) Turbine Stage t Disc Applies to Disc listed in Table 1 of the AD. see 993010 / 993011 for Stage 2 AD AD 2011.01-09 EVE Aerospace PBE 993009 MAN NA. 1754.7 529 28 Jan 2011 C 0.00 Airframe (PM) 119003-11 Mx. Notes: N/A TO PBE'S P/M MR-10039N INSTALLED G-CGUL G550 5176 Technical Bulletins Page 150 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620940 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No AD AD 2010.2505 Rolls Royce HP Effective Jan 13. 2011. 993010 MAN 0.0 0 13 Jan 2011 C 0.00 Engine 1 Turbine Stage 2 Disc Applies to Disc listed in Table 2 of the AD. see 993007 / 993008 for Stage 1 AD 993010 AD 2010.2505 Rolls Royce HP Effective Jan 13. 2011. (993011) Turbine Stage 2 Disc MAN 0.0 0 13 Jan 2011 C 0.00 Engine 2 Applies to Disc listed in Table 2 of the AD. see 993007 / 993008 for Stage 1 AD AD 2011.2201 Rolls Royce - Touch- Effective November 993016 MAN C.W 2166.4 664 04 Nov 2011 C 0.00 Engine 1 and-go and Overshoot Life Cycle 23. 2011. Once 30 day Counting requirement is c/w. add the second schedule (120 day requirement). this is due from 11.23.11. all BR700-710C4.11 model engines that have hardware configuration standard 710C4.11 engraved on the engine data plate (Service Bulletin SB- BR700.72-101466 standard not incorporated), and all BR700-710C4.11 model engines that have hardware configuration standard 710C4-11/10 engraved on the engine data plate (SB SB-BR700- 72- 101466 standard incorporated Mx. Notes: Previously complied with see EASA AD 201077 G-CGUL G550 5176 Technical Bulletins Page 151 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620941 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No AD 993016 AD 2011.22-01 Rolls Royce • Touch. Effective November MAN cm 2166.4 664 04 Nov 2011 C 0.00 Engine 2 (993017) and.go and Overshoot Life Cycle 23. 2011. Once 30 day Counting requirement is ciw. add the second schedule (120 day requirement), this is due from 11.23-11. all BR700710C4-11 model engines that have hardware configuration standard 710C4-11 engraved on the engine data plate (Service Bulletin SB- BR700.72.101466 standard not incorporated). and all BR700.710C4-11 model engines that have hardware configuration standard 710C4-11/10 engraved on the engine data plate (S8 SB-BR700- 72.101466 standard incorporated Mx. Notes: Previously complied with see EASA AD 2010-77 AD EASA AD 2010.0062 • Re Fighting >>>Superceded by 993050 26 CAN MA 1145.2 362 26 Apr 2010 C 0.00 Airframe Enterprises Limited Portable Halon code 993055«< 1211 Fire Extinguishers Effectivity: Halon 1211 (BCF) fire extinguishers, identified by serial number (s/n) and Part Number (P/N) in Fire Fighting Enterprises Ltd (FFE) Alert Service Buletin (ASB) 26-116 Mx. Notes: not applicable no ffe bottles installed G-CGUL G550 5176 Technical Bulletins Page 152 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620942 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No AD EASA AD2010.0075 • BR700.710 Effectivity: All BR700• gam atab 993051 72 MAN CM 1145.2 362 05 May 2010 C 0.00 Engine 1 Engines - High-Pressure (HP) Turbine 710A1.10 or BR700- Discs Stage 1 and 2 Assembly Life 710C4-11 with Limits • Modification hardware configurations as implied on the AD and equipped with HP Turbine Dics listed in Table 1 or Table 2 of the ADM Applies only to aircraft operated under EASA jurisdiction // Within 1month after the effective date of this AD or upon accumulating the new DSCL as noted in Table 1 or Table 2 of the AD. which ever occures later AD 993051 EASA AD2010-0075 • BR700-710 Effectivity: All BR700• gam afab 72 MAN CM 1145.2 362 05 May 2010 C 0.00 Engine 2 (993061) Engines - High-Pressure (HP) Turbine 710A1.10 or BR700- Discs Stage 1 and 2 Assembly Life 710C4-11 with Limits • Modification hardware configurations as implied on the AD and equipped with HP Turbine Dics listed in Table 1 or Table 2 of the ADM Applies only to aircraft operated under EASA jurisdiction // Within lmonth after the effective date of this AD or upon accumulating the new DSCL as noted in Table 1 or Table 2 of the AD. which ever occures later G-CGUL G550 5176 Technical Bulletins Page 153 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620943 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No AD EASA AD2010.0076 - BR700-710 Effectivity: All BR700- 993052 72 MAN N/A 1145.2 362 26 Apr 2010 C 0.00 Engine 1 Engines High-Pressure (HP) Turbine 710C4.11 with Discs Stage 1 and 2 Assembly Life hardware Limits - Modification configurations as implied on the AD and equipped with HP Turbine Dics listed in Table 1 or Table 2 of the AD!! Applies only to aircraft operated under EASA jurisdiction // Within lmonth after the effective date of this AD or upon accumulating the new DSCL as noted in Table 1 or Table 2 of the AD. which ever occures later Mx. Notes: APPLIES TO M700.710O4-1 1/I 0 WITH SB 72.101466 STANDARD INCORPORATED. AD 993052 EASA A02010.0076 - BR700-710 Effectivity: All BR700- 72 MAN N/A 1145.2 362 26 Apr 2010 C 0.00 Engine 2 (993062) Engines High-Pressure (HP) Turbine 710C4-1I with Discs Stage 1 and 2 Assembly Life hardware Limits - Modification configurations as implied on the AD and equipped with HP Turbine Dics listed in Table 1 or Table 2 of the AD!! Applies only to aircraft operated under EASA jurisdiction // Within 1month after the effective date of this AD or upon accumulating the new DSCL as noted in Table 1 or Table 2 of the AD. which ever occures later Mx. Notes: APPLIES TO 8R700-7104- 11/10 WITH SB 72-101466 INCORORATED G-CGUL G550 5176 Technical Bulletins Page 154 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620944 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No AD EASA AD2010-0077 • BR700•710 Effectivity: All BR700• game tab 993053 MAN CM 1145.2 362 05 May 2010 C 0.00 Engine I Engines - Change of Life Cycle 710A1.10 and BR700• Counting Method for Tounch•and-Go 710CA-11 with and Overshoot hardware configurations as implied on the AD // Applies only to aircraft operated under EASA jurisdiction // Within 4 months after the effective date of this AD accomplish touch- and-go and overshoot calculations per the instructions as defined by Rolls-Royce Deutschland Alert NMSB-BR700.72- A900504 Revision 'paragraph 3.B AD 993053 EASA AD2010-0077 • BR700-710 Effectivity: All BR700• gama fab Engines - Change of Life Cycle MAN CW 1145.2 362 05 May 2010 C 0.00 Engine 2 (993063) 710A1.10 and BR700. Counting Method for Tounch•and-Go 710C4-11 with and Overshoot hardware configurations as implied on the AD // Applies only to aircraft operated under EASA jurisdiction // Within 4 months after the effective date of this AD accomplish touch- and-go and overshoot calculations per the instructions as defined by Rolls-Royce Deutschland Alert NMSB-BR700•72- A900504 Revision 'paragraph 3.B G-CGUL G550 5176 Technical Bulletins Page 155 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620945 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No AD EASA AD 2010.006281 - Fire Effectivity: Halon 1211 993055 26 MAN NIA 1529.8 467 11 Oct 2010 C 0.00 Airframe Fighting Enterprises Limited Portable (BCF) fire Halon 1211 Fire Extinguishers extinguishers. identified by serial number (sin) and Part Number (PIN) in Fire Fighting Enterprises Ltd (FFE) Alert Service Bulletin (ASB) 26.116 issue B II Supercedes code 993050. Mx. Notes: no affected bottles installed AD 993059 EASA AD 2010-0003R2 Mode S This AD revises EASA CAMO MAN N/A 3466.5 953 18 Dec 2014 C 0.00 Airframe Transponder Aircraft Type Mode AD 2010-0003R1 CAMO Strapping Check / Modification dated 11 January UPDATE 2010. The original issue of this AD superseded EASA AD 20070120 dated 03 May 2007. Mx. Notes: NIA BY P/N. HONEYWELL P/N 7517400950 X2 INSTALLED UK.MG.0235 AD EASA AD 2012-0161 Replacement of ref BR700-72- 993095 CAN CAN 0.0 0 23 Sep 2014 C 0.00 Engine 1 the Fuel Pump Splined Coupling A900509 » Cancelled - See 993115(993116) Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link. ref BR700.72-A900509 AD 993095 EASA AD 2012-0161 Replacement of ref BR700-72- CAN CAN 0.0 0 23 Sep 2014 C 0.00 Engine 2 (993096) the Fuel Pump Splined Coupling A900509 » Cancelled - See 993115(993116) Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link. ref BR700.72-A900509 G-CGUL G550 5176 Technical Bulletins Page 156 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620946 TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No AD EASA AD 2012-0166 Engine • High Effectivity: BR700- 993097 MAN N/A 2558.5 761 19 Sep 2012 C 0.00 Engine 1 Pressure Turbine Rotor Disc Stage 1 710A1.10 and BR700• and Stage 2 Life Limit Implementation 710A2-20 engines, all BR700.710C4- 11 engines that have hardware configuration standard 710C4-11 engraved on the engine data plate (RRD SB-BR700.72- 101466 standard not incorporated), or which have hardware configuration standard 710C4-11/10 engraved on the engine data plate (SB-BR700.72. 101466 standard incorporated). Mx. Notes: N/A BY S/N FITTED AD 993097 EASA AD 2012-0166 Engine • High Effectivity: BR700- MAN N/A 2558.5 761 19 Sep 2012 C 0.00 Engine 2 (993098) Pressure Turbine Rotor Disc Stage 1 710A1.10 and BR700• and Stage 2 Life Limit Implementation 710A2-20 engines, all &Ns. BR700.710C4- 11 engines that have hardware configuration standard 71004.11 engraved on the engine data plate (RRD SB-BR700.72- 101466 standard not incorporated), or which have hardware configuration standard 710O1.11/10 engraved on the engine data plate (SB-BR700.72. 101466 standard incorporated). Mx. Notes: N/A BY S/N FITTED G-CGUL G550 5176 Technical Bulletins Page 157 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620947 i T YP CNV Source Code Description Effectivity ATA Status ill oebook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No AD EASA AD 2012-0254 Flight Crew EASA AD 2012-0254 993100 CAN 13 Dec 2012 I Airframe Oxygen Regulator- Identification / Flight Crew Oxygen Operational Procedure / Replacement Regulator. For Flt crew oxy mask regulators, having (PM) MCI0. MF10 and MF20 series. (s/n) as listed in Appendix 1 of this AD. Within 30 days after the effective date of this AD, inspect each flight crew oxygen mask regulator to identify the P/N and SM. Within 12 months after the effective date of this AD, replace each affected mask as required by paragraph (2.1). see rev 1 - 993101 AD EASA AD 2012-0254R1 Right Crew EASA AD 2012-0254 993101 MAN 21 Dec 2012 I Airframe Oxygen Regulator - Identification / Flight Crew Oxy Reg Operational Procedure / Replacement .For Flight crew oxygen mask regulators, having Pal Number (PIN) MC10, MF10 and MF20 series, with serial numbers (s/n) as listed in Appendix 1 of this AD. Within 30 days after the effective date of original issue date (12.13.12) of this AD, inspect each flight crew oxygen mask regulator to identify the P/N and S/N. Within 12 months after the effective date of original AD, replace each affected mask as required by paragraph (2.1). G-CGUL G550 5176 Technical Bulletins Page 158 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620948 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No AD EASA AD 2013.0020 • Safety Belts / superceded ref RI 993102 CAN CAN 0.0 0 14 Mar 2013 C 0.00 Airframe Torso Restraint Systems • Inspection / 993107 Replacement Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link AD AD 2013.03.17 HPT Stage 1 and BR700.710A1.10 and 993103 MAN N/A 2904.4 853 22 May 2013 C 0.00 Engine 1 Stage 2 Disc Replacement 710A2•20 and 710C4- 11 (without Mod 72- 101466) engines with HPT stage 1 or stage 2 disc S/Ns listed in the AD = 3000 cycles. // BR700.710C4.11 (with Mod 72.101466) engines with HPT stage 1 or stage 2 disc &Ns listed in the AD, with hardware config standard 710C4.11 or 710C4-11/10 engraved on engine data plate = 2300 cycles. AD 993103 AD 2013.03.17 HPT Stage 1 and BR700.710A1.10 and MAN N/A 2904.4 853 22 May 2013 C 0.00 Engine 2 (993104) Stage 2 Disc Replacement 710A2-20 and 710C4- 11 (without Mod 72- 101466) engines with HPT stage 1 or stage 2 disc S/Ns listed in the AD = 3000 cycles. BR700.710C4.11 (with Mod 72.101466) engines with HPT stage 1 or stage 2 disc SiNs listed in the AD. with hardware config standard 710C4.11 or 710C4-11/10 engraved on engine data plate = 2300 cycles. AD EASA AD 2013•0020R1 • Safety Belts effective 3-12.13. 993107 CAN CAN 0.0 0 15 Jul 2013 C 0.00 Airframe / Torso Restraint Systems • Inspection Cancelled by EASA / Replacement AD 2013•0020R2 (993110). Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link G-CGUL G550 5176 Technical Bulletins Page 159 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620949 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No AD EASA AD 20110106 Varnish On Comply with action in 993108 25 MAN 14 May 2013 I Airframe Veneered Panels - Inspection r EASA AD 2013.0106. Refurbishment within 7500 hrs or 96 months. whichever occurs first after the effective date of AD (28 May. 2013). See effectivity on AD. AD EASA AD 2013-0020R2 - Safety Belts effective 07-11-2013. 993110 CAN CM 2956.6 861 08 Jul 2013 C 0.00 Airframe r Irmo Restraint Systems - Inspection Cancelled by EASA / Replacement AD 2013-0020R3 (993120). Mx. Notes: Records review carried out AD EASA AD 2014-0142 - Oxygen Mask Due within 24 months. 993113 CAN 18 Jun 2014 Airframe Regulator Inflatable Harness / Hose Cancelled by EASA AD 2014-0142 RI. AD EASA AD 2014.014281 - Oxygen Due within 24 months 993114 MAN 18 Jun 2014 Airframe Mask Regulator Inflatable Harness / from effective date 18 Hose June. 2014. AD 993115 EASA AD 20120161RI Replacement ref SB BR700.72- MAN 19 Sep 2014 I Engine 1 of the Fuel Pump Splined Coupling A900509 AD 993115 EASA AD 20120161RI Replacement ref SB BR700-72- (993116) MAN 19 Sep 2014 I Engine 2 of the Fuel Pump Splined Coupling A900509 AD AD 2011.2402 Gulfstream GV airplanes having 994000 MAN NIA 2264.1 687 27 Dec 2011 C 0.00 Airframe Aerospace Corporation (Third Halon serial numbers (S/Ns) Fire Bottle for Engines) 501 and subsequent. GV-SP airplanes having SiNs 5001 through 5308 inclusive. Mx. Notes: No third engine fire bottle fitted/ confirmed by visual chk. AD AD 2012.0208 - Aviation Effective March 13. 994001 MAN 13 Mar 2012 I Airframe Communication & Surveillance 2012. See AD for Systems. LLC affected pin. Due within 36 months. G-CGUL G550 5176 Technical Bulletins Page 160 of 164 20 Jan 2015 CO 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620950 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No AD AD 74.0849 R3 Lavatory Paper and Eff. Dose: ALL 1000 GAC LTN 994002 25 MAN CIW 2772.7 819 27 Feb 2013 C Airframe Linen Waste Receptacle Enclosure HRS. [GI ref 534030, LMX000558 Access Door and Disposal Door Gil GIIB GM ref Inspection 257530, GIV G300 G400 ref 254001, G350 t G450 ref 2541011 Mx. Notes: SEE CODE 997427 UK.145.00883 AD AD 2012.13.12 Flight Control Surface Within 20 days after 994008 MAN NA 2535.4 756 10 Sep 2012 C 0.00 Airframe Paint Thickness - AFM Revision the effective date of this AD, revise the airplane flight manual (AFM) by incorporating the applicable airplane flight manual supplement (AFMS) specified in paragraph (g)(4) of this AD. Ref CB 121. G550 SINs 5038, 5079, 5223, 5227, 5237, 5240, 5245, 5246, 5252, 5258, 5261, 5265, 5267, 5283, 5290, 5293, 5294, 5302, 5307, 5311, 5318, and 5320. Mx. Notes: N/A by Aircraft S/N AD AD 201243.12 Flight Control Surface Within 90 days after 994009 MAN NIA 2535A 756 10 Sep 2012 C 0.00 Airframe Paint Thickness - Measurement the effective date of this AD, measure flight control surface paint thickness as specified in paragraph (h)(1) of this AD. Ref CB 121. G550 &Ns 5038, 5079, 5223, 5227, 5237, 5240, 5245, 5246, 5252, 5258, 5261, 5265, 5267, 5283, 5290, 5293, 5294, 5302, 5307, 5311, 5318, and 5320. Mx. Notes: N/A by Aircraft S/N G-CGUL G550 5176 Technical Bulletins Page 161 of 164 20 Jan 2015 402015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620951 TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LDG Date CA MM REF M HRS alntenance Notes Cert No AD AD 2012.13.12 Flight Control Surface II. during the 994010 MAN N/A 2535.4 756 10 Sep 2012 C 0.00 Airframe Paint Thickness • Corrective Action measurement required by paragraph (h) of this AD, the average paint thickness is greater than the allowances in CB 121 specified in paragraph (g) of this AD, and is equal to or greater than 13.0 mils: Before further flight, repair. in accordance with a method approved by the Manager, Atlanta ACO, FAA. G550 S/Ns 5038, 5079, 5223, 5227, 5237, 5240, 5245, 5246, 5252, 5258, 5261, 5265, 5267, 5283, 5290, 5293, 5294, 5302, 5307, 5311, 5318, and 5320. Mx. Notes: N/A by Aircraft SIN AD AD 2013.05.13 Rolls-Royce Appfies to BR700- GAC LTN 994011 MAN CAN 875 28 Sep 2013 C Engine 1 Deutschland Ltd & Co KG 710A1.10, all sin and BMX000258 BR700.710C4.11 turbofan engines that have either of the following hardware configuration standards engraved on the engine data plate: (1) Standard -710C4- 11"—RRD Alert Non- Modification Service Bulletin (NMSB) SB- BR700.72-101466 standard not incorporated, or (2) Standard -710C4- 11/10"-RRD Alert NMSB SB-BR700-72- 101466 standard incorporated. Ref AD for compliance times UK.145.00883 G-CGUL G550 5176 Technical Bulletins Page 162 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620952 TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No AD 994011 AD 2013.05.13 Rolls-Royce Applies to BR700- GAC LTN MAN CM 3029.7 875 26 Sep 2013 C Engine 2 (994012) Deutschland Ltd & Co KG 710A1.10. all sin and BMX000258 BR700-710O4.11 turbofan engines that have either of the following hardware configuration standards engraved on the engine data plate: (1) Standard -710C4- 11"-RRD Alert Non- Modification Service Bulletin (NMSB) SB- BR700.72-101466 standard not incorporated. or (2) Standard -710C4- 11/10"-RRD Alert NMSB SB-BR700-72- 101466 standard incorporated. Ref AD for compliance times UK.145.00883 AD Within 36 months after CAMO 994013 AD 2013.22.19 Fuel Boost Pump 28 MAN CM 3466.5 953 18 Dec 2014 C 0.00 Airframe the effective date of CAMO this AD. inspect the UPDATE fuel boost pumps to determine whether Gulfstream P/N 1159SCP500.5 is installed. Mx. Notes: REPLACEMENT REQUIRED PER AD2013.22-19 SECTION (G) CARRIED OUT VIA CB122 - UK.MG.0235 FL016819 - 7 AUG 12AMP REVISED TO INCLUDE ICA REQUIREMENTS GV-GER-0003 PER AD2013.22.19 SECTION (l)(2) AD AD 2014.1801 Rockwell Collins This AD applies to the CAMO 994015 MAN NIA 3466.5 953 18 Dec 2014 C 0.00 Airframe Mode S Transponders TDR-94/TDR- following Rockwell CAMO 94D Collins. Inc. part UPDATE number (P/N) Mode S transponders: (i) TDR- 94: CPN 622-9352- 008. 622-9352-108. 622.9352-308. 622- 9352.408: and (ii) TDR-94D: CPN 622- 9210-008. 622-9210- 108. 622-9210-308. 622.9210-408. Mx. Notes: N/A BY PIN. HONEYWELL P/N 7517400-950 X2 INSTALLED UK.MG.0235 G-CGUL G550 5176 Technical Bulletins Page 163 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620953 TYP C/W Source Code Description Effectivity ATA Status ilLogbook Work Order HRS LDG Date C/I MM REF M HRS aintenance Notes Cert No AD related to FAA AD 74- 997000 PA 2012.336 Lavatories (Italian CAA) MAN 26 Sep 2012 Airframe 08-09R3 AD 997427 AD 74.08.09 R2 Lavatory Inspection Cancelled use 994002 25 CAN CAN 1787.4 543 08 Mar 2011 C 254101 0.00 Airframe Mx. Notes: work pack FL014715 AD AD 2012.26.15 Honeywell effective 1-24-2013. GAL LNT 998000 CAN N/A 2728.9 802 25 Jan 2013 C 0.00 Airframe International G350/450. G5001550. BMX000126 Due within 30 days. CANCELLED BY AD 2012.26-15 r1 (998001). AD Eff. Desc: ALL ACFT 999825 AD 98-24-27 1ST TECH FIRE Bit 26 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe (3MOS). AD Eff. Desc: SEE AD 999831 AD 98.25.10R1 Seat Belt Restraint 25 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe (10HRS). AD AD 2006.1803 Emptesa Brasileira de 999901 MAN 04 Oct 2006 I AD 2006.18.03 Airframe Aeronautica S.A. (EMBRAER) model EMB-145XR G-CGUL G550 5176 Technical Bulletins Page 164 of 164 20 Jan 2015 C12015 Gulfsfream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620954