(itiiiktrearn MYCMP Phone. Aircraft Make Gulfstream Aircraft Model G550 Aircraft Serial No. 5176 Airworthiness 26 Nov 2007 Date Regulation ELI-EASA Technical Bulletins G-CGUL Report Filters: Log Date - 08 Nov 2014 TYPE: ALL Current TT 3466.5 Analyst: Gar Leaver CW Status: ALL Current Lndgs 953 FA)4 Phone: Current Hr Mtr 3423.6 COMPONENT TIMES Position Logbook Description Serial Number Total Time Total Cycles TSO CSO 1 Engine Rolls Royce BR700.710C4.11 15455 3466.5 953 (G550) 2 Engine Rolls Royce BR700.710C4.11 15456 3466.5 953 (G550) 1 APU Honeywell RE220 (G550) P-503 2044.5 0 Logbook TYP aintenance Notes Code Description Effectivity Airframe 299999 HYDRAULIC REPLENISHING SYSTEM INOPERATIVE Mx. Notes: Hyd replenisher replaced by GS LTN Defect closed 441200 SB GPECSB50001 Cabin System 5365, 5381. 5385 Airframe Level E Firmware Update Cabin service bulletin 449002 GCMS SIB 002 Cabin System Airframe Firmware Update 1.9.1 This Cabin Service Bulletin is applicable to aircraft with GCMS controller firmware version 1.8.4 installed or later approved version. LDG Date IATAI Status C/W Source HRS C/I MM REF M HRS Work Order Cert No gs Itn MAN CM 1012.1 326 19 Feb 2010 C 0.00 OPT 26 Jan 2013 I OPT 08 Aug 2013 I 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

il TYP Logbook Code aintenance Notes Description Effectivity ATA Status CNV Source Work Order Cert No HRS LOG Date C/I MM REF M HRS 449003 Airframe GCMS SB 003 Cabin System Firmware Update 4.4.3.3 This Cabin Service 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. OPT 13 Sep 2013 I Airframe 449004 CSB 003A • Advanced Cabin Server (ACS) System Firmware Update 4A.3.3 This Cabin Service Bulletin revision 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. 23 OPT 21 Feb 2014 G-CGUL G550 5176 Technical Bulletins Page 2 of 164 20 Jan 2015 O2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620792

i lli oe YP book T Code aintenance Notes Airframe 449202 Description Effectivity CSB 002B CPBC Software Installation Effectivity: This Cabin 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. ATA Status CNV Source Work Order Cert No HRS LOG Date CA OPT 11 Dec 2013 I MM REF M HRS Engine 1 880041 ASB BR700.72•A900297 High Pressure Compressor Fairings - Inspection of Upper Left HP Compressor Fairing » Closed by Rev 1. 21 May 2014« Effectivity: Eng SIN 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. CAN CAN Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link 0.0 0 22 May 2014 C 0.00 G-CGUL G550 5176 Technical Bulletins Page 3 of 164 20 Jan 2015 O2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620793

Logbook TYP aintenance Notes 880041 ASB BR700.72•A900297 High Engine 2 (890041) Pressure Compressor Fairings - Inspection of Upper Leh HP Compressor Fairing Code Description Effectivity ATA Status CNV Source Work Order Cert No HRS LOG Date CA MM REF M HRS »Closed by Rev 1. 21 May 2014 « Effectivity: Eng S/N 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. CAN CAN Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link 0.0 0 22 May 2014 C 0.00 Engine 1 880042 ASB BR700.72-A900298 Engine Combustion Fairings • Replacement of Non.Confonning Upper Left. Upper Right and Lower Right Combustion Section Fairings » Closed by Rev 1. 21 May 2014 « Effectivity: Eng S/N 15887 • 15891. This 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. CAN CAN Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link 0.0 0 22 May 2014 C 0.00 880042 ASB BR700.72-A900298 Engine Engine 2 (890042) Combustion Fairings • Replacement of Non-Conforming Upper Left. Upper Right and Lower Right Combustion Section Fairings » Closed by Rev 1. 21 May 2014 « Effectivity: Eng S/N 15887 • 15891. This 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. CAN CAN Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link 0.0 0 22 May 2014 C 0.00 G-CGUL G550 5176 Technical Bulletins Page 4 of 164 20 Jan 2015 O2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620794

L ii _ogbook TYP Code Description Effectivity aintenance Notes Engine 1 880043 Decrease Lives of HP Turbine Discs ASB BR700.72-A900497 TLM Mx. Notes: lives amended as per sb It is recommended this SIB be accomplished on all engines before 2 -28-10 880043 ASB BR700.72-A900497 TLM It is recommended this 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 Engine 1 880044 880044 Engine 2 (890044) Engine 1 880045 880121 Engine 1 ASB BR700.72-A900504 Change of It is recommended this Life Counting Method for Touch-and- SiB be accomplished Go and Overshoot on all engines before 7 -31.10 ASB BR700.72-A900504 Change of It is recommended this 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 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. ATA Status C/W Source HRS LDG Date Cli MM REF M HRS Work Order Cert No REC CM 1007.8 325 14 Feb 2010 C 0.00 REC 1007.8 325 14 Feb 2010 C 0.00 INF CM 1114.2 352 06 Apr 2010 C 0.00 INF CM 1114.2 352 06 Apr 2010 C 0.00 REC 25 Jan 2011 SB BR700-77-101875 - N2 Speed Probes - Introduction of New Attaching Bolts with Shorter Length Effectivity: BR700- 710C4.11 Engines 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. 77 REC 03 Jul 2014 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

Logbook TYP aintenance Notes Code Description Effectivity ATA Status CNV Source Work Order Cert No HRS LDG Date CA MM REF M HRS Engine 2 880121 SB BR700.77-101875 • N2 Speed (890121) Probes • Introduction of New Attaching Botts with Shorter Length Effectivity: BR700- 710G4-11 Engines 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. 77 REC 03 Jul 2014 Engine 1 Alert SB BR700.72-A900509 880200 Replacement of the Fuel Pump Splined Coupling BR700.710A1•10 Engines.Modules M61. 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 CAN CAN 0.0 0 15 Mar 2012 C 0.00 G-CGUL G550 5176 Technical Bulletins Page 6 of 164 20 Jan 2015 O2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620796

TYP Logbook Code Description Effectivity ATA Status CNV Source HRS LOG Date CA MM REF M HRS Work Order 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 Engine 1 SB BR700.72.100981 • LP Impact 880237 Adhesive And Filler Effectivity: Prior to Engines SN 15133 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 880237 SB BR700.72.100981 • LP Impact (890237) Adhesive And Filler Effectivity: Prior to Engines SN 15133 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 880271 SB BR700-72.101144 • Combustion Inner Case And Vanes Effectivity: BR700• 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 72 INF N/A 0.0 0 26 Nov 2007 C 0.00 G-CGUL G55O 5176 Technical Bulletins Page 7 of 164 20 Jan 2015 02015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620797

TYP Logbook Code Description Effectivity ATA Status CNV Source HRS LOG Date CA MM REF M HRS Work Order aintenance Notes Cert No Engine 2 880271 (890271) SB BR700.72.101144 • Combustion Inner Case And Vanes Effectivity: BR700- 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 72 INF NIA 0.0 0 26 Nov 2007 C 0.00 Engine 1 880276 SB BR700.72.101173 • LP / HP Turbine Stator Retainer / Seals NOTE: Prior to Engine Serial Number 15189 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 880276 (890276) SB BR700.72.101173 • LP / HP Turbine Stator Retainer / Seals NOTE: Prior to Engine Serial Number 15189 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 880285 SB BR700.72.101195 • Intermediate Compressor Case NOTE: Prior to Engine Serial Number 15129, 15130 thru 15141, 15145. 15147 thru 15150. 15154 thru 15159. 15162 thru 15195, 15200 thru 15228 and 15231 onwards 72 OPT 14 Dec 2010 I Engine 2 880285 (890285) SB BR700-72.101195 • Intermediate Compressor Case NOTE: Prior to Engine Serial Number 15129, 15130 thru 15141, 15145, 15147 thru 15150, 15154 thru 15159, 15162 thru 15195, 15200 thru 15228 and 15231 onwards 72 OPT la Dec 2010 I Engine 1 880287 SB.BR700•72•101203 • HPC Variable Guide Vanes Actuating Mechanism NOTE: Prior to Engine Serial Number 15124 72 OPT NA 0.0 0 26 Nov 2007 C 0.00 Engine 2 880287 (890287) SB BR700.72.101203 • HPC Variable Guide Vanes Actuating Mechanism NOTE: Prior to Engine Serial Number 15124 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 880296 SB BR700.72.101246 • New LP Compressor Disc NOTE: Prior to Engine Serial Number 15178 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 G-CGUL G550 5176 Technical Bulletins Page 8 of 164 20 Jan 2015 @2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620798

L TYP Logbook Code Description Effectivity ATA Status C/W Source HRS LDG Date Cli MM REF M HRS Work Order aintenance Notes Cert No 880296 Engine 2 (890296) SB BR700.72-101246 - New LP Compressor Disc NOTE: Prior to Engine Serial Number 15178 72 OPT NIA 0.0 0 26 Nov 2007 C 0.00 880301 Engine 1 Alert SB BR700-72-A900509 (Revision 1) Replacement of the Fuel Pump Splined Coupling Revision I of this Non- Modification Service 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 CAN CAN 0.0 0 26 Jun 2012 C 0.00 880301 Engine 2 (890301) Alert SB BR700-72-A900509 (Revision 1) Replacement of the Fuel Pump Splined Coupling Revision 1 of this Non- Modification Service 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 CAN CAN 0.0 0 26 Jun 2012 C 0.00 880302 Engine 1 SB BR700-73-101376 - Combination Of EEC Hardware Standard 73 REC 16 Jul 2002 880302 Engine 2 (890302) SB BR700.73-101376 - Combination Of EEC Hardware Standard 73 REC 16 Jul 2002 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

L TYP Logbook Code Description Effectivity ATA Status C/W Source HRS LDG Date Cli MM REF M HRS Work Order aintenance Notes Cert No 880303 Engine 1 SB BR700.73-101380 - Introduction of an EED with a New Hardware Standard Effectivity: BR700- 710C4.11 Engines / 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 73 REC N/A 0.0 0 26 Nov 2007 C 0.00 880303 Engine 2 (890303) SB 6R70073-101380 - Introduction of an EED with a New Hardware Standard Effectivity: BR700- 710O4-11 Engines / 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 73 REC N/A 0.0 0 26 Nov 2007 C 0.00 880304 Engine 1 SB BR700.73-101386 - Fuel Manifold Damper Wire NOTE: Prior to Engine Serial Number 15181 and from Engine Serial Number 15194 to 15254 73 OPT N/A 0.0 0 26 Nov 2007 C 0.00 880304 Engine 2 (890304) SB BR700.73-101386 - Fuel Manifold Damper Wire NOTE: Prior to Engine Serial Number 15181 and from Engine Serial Number 15194 to 73 OPT N/A 0.0 0 26 Nov 2007 C 0.00 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 Logbook Code Description Effectivity ATA Status CNV Source HRS LOG Date CA MM REF M HRS Work Order aintenance Notes Cert No Engine 1 880305 SB BR700•73.101400 • EEC with S2.1 Software Standard Effectivity: Prior to Engine Serial Number 15166 73 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 880305 (890305) SB BR700•73.101400 • EEC with S2.1 Software Standard Effectivity: Prior to Engine Serial Number 15166 73 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 06 8803 SB BR700•73.101558 (Rev 1) • Fuel NOTE: For engines prior to Engine Serial Number 15328 which do not have the Service Bulletin SB. BR700.73.101496 standard incorporated 73 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Flow Transmitter Engine 2 880306 (890306) SB BR700.73.101558 (Rev 1) • Fuel NOTE: For engines prior to Engine Serial Number 15328 which do not have the Service Bulletin SB. BR700.73.101496 standard incorporated 73 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Flow Transmitter Engine 1 880307 Alert SB BR700.72.A900509 (Revision 2) Replacement of the Fuel Pump Splined Coupling Revision 2 of this Non. Modification Service 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 CAN CAN 0.0 0 26 Jun 2012 C 0.00 G-CGUL G550 5176 Technical Bulletins Page 11 of 164 20 Jan 2015 Ce 2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620801

L TYP Logbook Code Description Effectivity ATA Status C/W Source HRS LDG Date Cli MM REF M HRS Work Order aintenance Notes Cert No 880307 Engine 2 (890307) Alert SB BR700.72-A900509 (Revision 2) Replacement of the Fuel Pump Splined Coupling Revision 2 of this Non- Modification Service 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 CAN CAN 0.0 0 26 Jun 2012 C 0.00 880308 Engine 1 SB BR700-73-101438 External Fuel System Air TubesiFittings NOTE: Prior to Engine Serial Number 15404 73 CAN N/A 0.0 0 26 Nov 2007 C 0.00 880308 Engine 2 (890308) SB BR700.73-101438 External Fuel System Air TubesiFittings NOTE: Prior to Engine Serial Number 15404 73 CAN N/A 0.0 0 26 Nov 2007 C 0.00 880309 Engine 1 Alert SB BR700.72-A900509 (Revision 3) Replacement of the Fuel Pump Splined Coupling Revision 3 of this Non- Modification Service 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 72 GAC LTN CAN CPN BMX000258 3029.7 875 26 Sep 2013 C 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

Logbook TYP aintenance Notes 880309 Alert SB BR700.72•A900509 Revision 3 of this Non- Engine 2 (890309) (Revision 3) Replacement of the Fuel Modification Service 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). Code Description Effectivity ATA Status CNV Source Work Order Cert No HRS LOG Date CA MM REF M HRS 72 CAN CPAr GAC LTN BMX000258 UK.145.00883 3029.7 875 26 Sep 2013 C Engine 1 880311 Alert SB BR700-72-A900509 Revision 4 has been (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.. 72 MAN 25 Aug 2014 I 880311 Alert SB BR700.72-A900509 Revision 4 has been 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.. 72 MAN 25 Aug 2014 I Engine 1 880312 SB BR700.73-101833R2 • Effectivity: See SB. 73 REC 25 Aug 2014 I 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 Gulf stream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620803

TYP Logbook Code Description Effectivity ATA Status CNV Source HRS LOG Date CA MM REF M HRS Work Order aintenance Notes Cert No Engine 1 880312 SB BR700-73.101496 - Engine Electronic Controller See Revision 1 - CMP Code 880313 / 890313 73 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 880312 (890312) SB BR700.73.101496 • Engine Electronic Controller See Revision 1 • CMP Code 880313 / 890313 73 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 880312 (890312) SB BR700-73.101833R2 Introduction of a Revised Drive Shaft Connection for the Fuel Pump Effectivity: See SB. Compliance: RECOMMENDED It is recommended that this Service Bulletin be accomplished on engines at the next engine shop visit maintenance opportunity. 73 REC 25 Aug 2014 I Engine 1 880316 SB BR700.73.101558 - Fuel Flow Transmitter (FFT) NOTE: For engines prior to Engine Serial Number 15328 which do not have the Service Bulletin SB- BR700.73.101496 standard Incorporated 73 OPT 09 Nov 2007 I Engine 2 880316 (890316) SB BR700-73.101558 • Fuel Flow Transmitter (FFT) NOTE: For engines prior to Engine Serial Number 15328 which do not have the Service Bulletin SB- BR700.73.101496 standard Incorporated 73 OPT 09 Nov 2007 I Engine 1 SB BR700-73.101590 - EEC With 880317 S3A Software Also see ASC 058 (970580). 73 REC 19 Mar 2007 I Engine 2 880317 (890317) SB 8R700-73.101590 - EEC With S3.4 Software Also see ASC 058 (970580). 73 REC 19 Mar 2007 I Engine 1 880318 SB BR700.73.101617 • Fuel Flow Transmitter NOTE: Prior to Engine Serial Number 15423. Cancelled ref rev 1 73 CAN N/A 0.0 0 26 Nov 2007 C 0.00 880322 G-CGUL G550 5176 Technical Bulletins Page 14 of 164 20 Jan 2015 492015 Gulf stream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620804

Logbook TYP aintenance Notes Code Description Effectivity ATA Status CNV Source Work Order Cert No HRS LOG Date c/I MM REF M HRS Engine 2 880318 (890318) 880319 Engine 880319 Engine 2 (890319) 880320 Engine 1 SB BR700•73.101617 - Fuel Flow Transmitter NOTE: Prior to Engine Serial Number 15423. Cancelled ref rev 1 880322 SB BR700.73.900463 • Removal of EFF: For engines 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. SB BR700-73•900463 • Removal of EFF: For engines 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. SB BR700.73-900423 - One Time It is recommended that 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 73 CAN N/A 73 REC N/A 0.0 0 26 Nov 2007 C 0.00 73 REC N/A 0.0 0 26 Nov 2007 C 0.00 CAN CAN 0.0 0 09 Sep 2014 C 0.00 0.0 0 26 Nov 2007 C 0.00 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 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620805

TYP Logbook aintenance Notes 880320 SB BR700•73•900423 • One Time It is recommended that 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 Code Description Effectivity ATA Status CNV Source Work Order Cert No HRS LOG Date c/I MM REF M HRS CAN CAN 0.0 0 09 Sep 2014 C 0.00 Engine 1 880324 SB BR700.73-900423R1 -One Time Inspection Of EEC Firebox Assembly For Paint Damage It is recommended that this Non•Modification 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. 73 REC 09 Sep 2014 G-CGUL G550 5176 Technical Bulletins Page 16 of 164 20 Jan 2015 O2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620806

Logbook TYP aintenance Notes 880324 SB BR700-73.900423Rt - One Time It is recommended that 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. Code Description Effectivity ATA Status CNV Source Work Order Cert No HRS LOG Date CA MM REF M HRS 73 REG 09 Sep 2014 I Engine 1 880339 Alert SB 8R70072-A900509 Revision 4 has been (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 72 MAN 25 Aug 2014 I 880339 Alert SB BR700.72-A900509 Revision 4 has been 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 72 MAN 25 Aug 2014 I G-CGUL G550 5176 Technical Bulletins Page 17 of 164 20 Jan 2015 O2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620807

TYP Logbook Code Description Effectivity ATA Status C/W Source HRS LDG Date C/I MM REF M HRS Work Order aintenance Notes Cert No Engine 1 880340 SB BR700.73-101833R2 Introduction of a Revised Drive Shaft Connection for the Fuel Pump Effectivity: See SB. Compliance: RECOMMENDED It is recommended that this Service Bulletin be accomplished on engines at the next engine shop visit maintenance opportunity. 73 REC 25 Aug 2014 I Engine 2 880340 (890340) SB BR700.73-101833R2 - Introduction of a Revised Drive Shaft Connection for the Fuel Pump Effectivity: See SB. Compliance: RECOMMENDED It is recommended that this Service Bulletin be accomplished on engines at the next engine shop visit maintenance opportunity. 73 REC 25 Aug 2014 I Engine 1 880414 SB 6R700-72-101349 - Fuel Shutoff Cable NOTE: Prior to Engine Serial Number 15109 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 880414 (890414) SB BR700.72-101349 - Fuel Shutoff Cable NOTE: Prior to Engine Serial Number 15109 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 880422 SB BR700.72-101414 - HPC Front Case - New Coated Brushes Effectivity: Prior to Engine Serial Number 15146 72 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 880422 (890422) SB BR700.72-101414 - HPC Front Case - New Coated Brushes Effectivity: Prior to Engine Serial Number 15146 72 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 880423 SB 6R700.72-101416 - Accessory Gearbox Line 12 Spacer Effectivity: Prior to Engine Serial Number 15135 71 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 880423 (890423) SB BR700.72-101416 - Accessory Gearbox Line 12 Spacer Effectivity: Prior to Engine Serial Number 71 OPT N/A 0.0 0 26 Nov 2007 C 0.00 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 Logbook Code Description Effectivity ATA Status CNV Source HRS LOG Date CA MM REF M HRS Work Order aintenance Notes Cert No Engine 1 880425 SB BR700.72.101419 • HPC VIGV Actuating Mechanism NOTE: Prior to Engine Serial Number 15148 72 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 880425 (890425) SB BR700•72•101419 • HPC VIGV Actuating Mechanism NOTE: Prior to Engine Serial Number 15148 72 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 880427 SB BR700.72.101421 • LP Turbine Stage Nozzle Guide Seals Effectivity: Engines Prior to Serial Number 15189 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 880427 (890427) SB BR700.72.101421 • LP Turbine Stage Nozzle Guide Seals Effectivity: Engines Prior to Serial Number 15189 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 880428 SB BR700.72.101431 HP Turbine Stage 1 Nozzle Guide Seals EFF: BR700.710A1-10 engines (GV) prior to engine SN 11506/ BR700.710C4- 11engines (G500/G550) prior to engine SN 15277. 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 880428 (890428) SB BR700.72.101431 HP Turbine Stage 1 Nozzle Guide Seals EFF: BR700.710A1.10 engines (GV) prior to engine SN 11506 / BR700.710C4- 11engines (G500/G550) prior to engine SN 15277. 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 880435 SB BR700•72•101460 LP Comp Trim Balance Weights Effectivity: All 72 OPT 28 Apr 2004 Engine 2 880435 (880435) SB BR700.72.101460 LP Comp Trim Balance Weights Effectivity: All 72 OPT 28 Apr 2004 Engine 1 880437 SB BR700.72.101463 • Engine HP Compressor Rear Inner Case GV: Prior to Engine Serial Number 11505 ft G500/ G550: Prior to Engine Serial Number 15229 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 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

Code aintenance Notes Engine 2 (690453) Vane Housing Assembly L TYP Logbook Description Effectivity ATA Status C/W Source Work Order Cert No HRS LDG Date Cli MM REF M HRS Engine 2 880437 SB BR700.72-101463 - Engine HP (890437) Compressor Rear Inner Case GV: Prior to Engine Serial Number 11505 if G500/ G550: Prior to Engine Serial Number 15229 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 880439 SB 6R700-72-101471 - Metco 58 Engine 1 Coated LP Compressor Blades NOTE: Prior to Engine 72 REC N/A Serial Number 15214 0.0 0 26 Nov 2007 C 0.00 880439 SB BR700.72-101471 - Metco 58 Engine 2 (890439) Coated LP Compressor Blades NOTE: Prior to Engine 72 REC N/A Serial Number 15214 0.0 0 26 Nov 2007 C 0.00 Engine 1 880441 SB BR700.72-101474 - Laser Shock Peened LP Compressor Rotor Disc »Cancelled See 72 CAN N/A Code 880581(890581) 0.0 0 26 Nov 2007 C 0.00 880441 SB BR700.72-101474 - Laser Shock »Cancelled See 72 CAN N/A Engine 2 (890441) Peened LP Compressor Rotor Disc Code 880581(890581) 0.0 0 26 Nov 2007 C 0.00 Engine 1 880453 SB BR700-72-101540 - Outlet Guide Vane Housing Assembly Effectivity: Prior to engine SN 15390 and from engine SN 15411 to 15416. Cancelled ref revision 2 880462 72 CAN N/A 0.0 0 26 Nov 2007 C 0.00 880453 SB BR700.72-101540 - Outlet Guide Effectivity: Prior to engine SN 15390 and from engine SN 15411 to 15416. Cancelled ref revision 2 880462 72 CAN N/A 0.0 0 26 Nov 2007 C 0.00 880454 SB BR700.72-101548 - LP Engine 1 Compressor Case NOTE: Prior to Engine 72 OPT N/A Serial Number 15390 0.0 0 26 Nov 2007 C 0.00 880454 SB BR700.72-101548 - LP Engine 2 (890454) Compressor Case NOTE: Prior to Engine 72 OPT N/A Serial Number 15390 0.0 0 26 Nov 2007 C 0.00 880456 SB BR700.72-101550 - Breather Engine 1 Filter. Cover. Tank Covers NOTE: Prior to Engine Serial Number 15360 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 880456 SB BR700.72-101550 - Breather Engine 2 (890456) Filter. Cover. Tank Covers NOTE: Prior to Engine 72 OPT N/A Serial Number 15360 0.0 0 26 Nov 2007 C 0.00 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

L TYP Logbook Code aintenance Notes Description Effectivity ATA Status C/W Source Work Order Cert No HRS LDG Date Cli MM REF M HRS Engine 1 880458 SB BR700.72-101588 - Accesssory Gearbox Module Main Housing NOTE: Prior to Engine Serial Number 15410 and for Engine Serial Numbers 15412 to 15417 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 880458 SB BR700.72-101588 - Accesssory Engine 2 (890458) Gearbox Module Main Housing NOTE: Prior to Engine Serial Number 15410 and for Engine Serial Numbers 15412 to 15417 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 SB BR700.72-101618 - Accessory NOTE: Prior to Engine 880460 72 OPT N/A Engine 1 Gearbox Oil Tank Fill Serial Number 15443 0.0 0 26 Nov 2007 C 0.00 880460 SB BR700.72-101618 - Accessory Engine 2 (890460) Gearbox Oil Tank Fill NOTE: Prior to Engine 72 OPT N/A Serial Number 15443 0.0 0 26 Nov 2007 C 0.00 880461 SB BR700.72-101622 - Lubriclone Engine 1 For The Accessory Gearbox Effectivity: Prior to engine SN 15446. 72 REC N/A 0.0 0 26 Nov 2007 C 0.00 880461 SB BR700.72-101622 - Lubriclone Engine 2 (890461) For The Accessory Gearbox Effectivity: Prior to engine SN 15446. 72 REC N/A 0.0 0 26 Nov 2007 C 0.00 880562 SB BR700.72-900341 HP Engine 1 Compressor Blades Baroscope Module M33.120 (HP 72 REC Compressor Module). 10 Feb 2005 I 880562 SB BR700.72-900341 HP Engine 2 (890562) Compressor Blades Borescope Module M33.120 (HP 72 REC Compressor Module). 10 Feb 2005 I 880567 SB BR700.72-900409 - LP Engine 1 Compressor Case Eff: All BR700.71A I - 10 Engines and All BR700-710C4 -11 Engines 72 REC 19 Sep 2006 I 880567 SB BR700.72-900409 - LP Engine 2 (890567) Compressor Case Eff: All BR700.71A1- 10 Engines and All BR700-710C4 -11 Engines 72 REC 19 Sep 2006 I Engine 1 SB BR700.72-101410 - HP 880572 Alternative Part Number For HP Turbine NOTE: Prior to Engine 72 OPT N/A Serial Number 15134 0.0 0 26 Nov 2007 C 0.00 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 Logbook aintenance Notes Code Description Effectivity 880572 Engine 2 (890572) 880575 Engine I 880575 Engine 2 (890575) 880579 Engine I 880579 Engine 2 (890579) 880581 Engine I SB BR700•72•101410 • HP Alternative Part Number For HP Turbine NOTE: Prior to Engine Serial Number 15134 SB BR700.72.101620 • Accessory Gearbox Module NOTE: For engines which have hardware configuration standard 710C4•11 engraved on the engine data plate SB BR700.72.101620 • Accessory Gearbox Module NOTE: For engines which have hardware configuration standard 710C4•11 engraved on the engine data plate SB BR700.72.900369 • HPT1, NGV & NOTE: See Bulletin 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. SB BR700.72.900369 • HPT1, NGV & NOTE: See Bulletin 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. ATA Status CNV Source HRS LOG Date Cd MM REF M HRS Work Order Cert No 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 72 REC N/A 0.0 0 26 Nov 2007 C 0.00 72 REC N/A 0.0 0 26 Nov 2007 C 0.00 SB BR700.72.101474R1 - Laser Shock Peened LP Compressor Rotor Disc 72 REC 18 Nov 2014 G-CGUL G550 5176 Technical Bulletins Page 22 of 164 20 Jan 2015 O2015 Gulf stream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620812

TYP Logbook Code Description Effectivity ATA Status CNV Source HRS LOG Date c/I MM REF M HRS Work Order aintenance Notes Cert No 880581 SB BR700-72.101474R1 - Laser 72 Engine 2 (890581) Shock Peened LP Compressor Rotor Disc REC 18 Nov 2014 I SB BR700.72.900521 (Pal A) Rev 2 The serial numbers of 880589 Inspection - LP Compressor Annulus the affected LP Engine 1 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 CAN CM 0.0 0 13 Jul 2011 C 0.00 880589 SB BR700.72.900521 (Part A) Rev 2 • The serial numbers of 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 CAN CM 0.0 0 13 Jul 2011 C 0.00 Mx. Notes: see code 890591 G-CGUL G550 5176 Technical Bulletins Page 23 of 164 20 Jan 2015 @ 2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620813

TYP Logbook Code Description Effectivity ATA Status CNV Source HRS LOG Date CA MM REF M HRS Work Order aintenance Notes Cert No SB BR700.72.900521 (Pan B) Rev 2 • The serial numbers of 880590 CAN CAN GAC•LTN 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 CAN CAN GAC•LTN 2354.6 711 19 Apr 2012 C Engine 2 (890590) 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 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620814

L TYP Logbook Code aintenance Notes Description Effectivity ATA Status C/W Source Work Order Cert No HRS LDG Date Cli MM REF M HRS Engine 1 880591 SB BR700.72-900521 (Part A) Rev 1- The serial numbers of Inspection LP Compressor Annulus the affected LP 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 GAC LTN CAN CAN 2047.8 610 13 Jul 2011 C FLO15395 Mx. Notes: set to code 723103 UK.145.00883 Engine 2 880591 SB BR700-72-900521 (Part A) Rev I The serial numbers of (890591) Inspection LP Compressor Annulus the affected LP 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 CAN CPN GAC LTN 2047.8 610 13 Jul 2011 C FLO15395 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 Logbook aintenance Notes Code Description Effectivity ATA Status CNV Source Work Order Cert No HRS LOG Date CA MM REF M HRS Engine 1 880592 SB BR700.72.900521 (Part B) Rev 1- The serial numbers of 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 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 GAC LTN CAN Cm 2047.8 610 15 Jul 2011 C FL015395 Mx. Notes: set to code 723103 UK.145.00883 880592 SB BR700.72.900521 (Part B) Rev 1- The serial numbers of Engine 2 (890592) 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 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 CAN CAN GAC LTN 2047.8 610 15 Jul 2011 C FL015395 Mx. Notes: set to code 723103 UK.145.00883 G-CGUL G550 5176 Technical Bulletins Page 26 of 164 20 Jan 2015 O2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620816

TYP Logbook aintenance Notes Code Description Effectivity ATA Status CNV Source Work Order Cert No HRS LOG Date CA MM REF M HRS Engine 1 880596 SB BR700.72.900521 (Part A) Visual The serial numbers of 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 CAN CAN 0.0 0 17 May 2011 C 0.00 880596 SB BR700-72.900521 (Part A) Visual The serial numbers of 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 CAN CAN 0.0 0 17 May 2011 C 0.00 G-CGUL G550 5176 Technical Bulletins Page 27 of 164 20 Jan 2015 O2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620817

Logbook TYP aintenance Notes Code Description Effectivity ATA Status CNV Source Work Order Cert No HRS LOG Date CA MM REF M HRS Engine 1 880597 SB BR700.72.900521 (Pan B) Eddy Current Inspection • LP Compressor Annulus Fillers 11 is recommended that PART B of this Non• 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 CAN CAN 0.0 0 17 May 2011 C 0.00 880597 SB BR700.72.900521 (Part B) Eddy It is recommended that 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 CAN CAN 0.0 0 17 May 2011 C 0.00 Engine 1 880602 SB BR700.72.900521 (Pan A) Rev 3 • II is recommended that 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 CAN CM 0.0 0 06 Jan 2013 C 0.00 G-CGUL G550 5176 Technical Bulletins Page 28 of 164 20 Jan 2015 O2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620818

L TYP Logbook Code Description Effectivity ATA Status C/W Source HRS LDG Date Cli MM REF M HRS Work Order 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 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. CAN CAN Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link. 0.0 0 07 Mar 2013 C 0.00 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 ii _ogbook TYP Code Description Effectivity aintenance Notes Engine 1 880604 SB BR700.72-900521 (Part A) Rev 4 - It is recommended that 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. 880604 SB BR700-72-900521 (Part A) Rev 4 It is recommended that Engine 2 (890604) 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. Engine 1 880605 SB BR700.72-900521 (Part B) Rev 4 It is recommended that Inspection LP Compressor Annulus PART B of this Non- 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. ATA Status C/W Source HRS LDG Date Cli MM REF M HRS Work Order Cert No REC CPA( GAL Luton BMX000145 UK145.00883 2849.4 832 10 Apr 2013 C 0.00 REC GAL Luton BMX000145 UK145.00883 2849.4 832 10 Apr 2013 C 0.00 REC GAC LTN BMX000380 3307.8 927 24 Mar 2014 C 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

Logbook TYP aintenance Notes 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. Code Description Effectivity ATA Status CNV Source Work Order Cart No HRS LDG Date CA MM REF M HRS UK.145.00883 Engine 1 880610 SB BR700.72.101858 • Introduction of a HP Compressor Stages 7 to 10 Rotor Disc Assembly with Revised Liner Coating Effectivity: BR700- 710G4-11 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). 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 72 OPT 12 Aug 2014 I G-CGUL G550 5176 Technical Bulletins Page 31 of 164 20 Jan 2015 O2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620821

TYP Logbook Code Description Effectivity ATA Status CNV Source HRS LOG Date CA MM REF M HRS Work Order 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 880611 SB BR700.72.101469 R1 - HP Effectivity: GV • prior 72 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 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620822

L TYP Logbook Code Description Effectivity ATA Status C/W Source HRS LDG Date Cli MM REF M HRS Work Order aintenance Notes Cert No 880611 Engine 2 (890611) SB BR700.72-101469 RI HP Compressor Vortex Reducer Ring Effectivity: GV - prior 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. 72 OPT 29Aug 2014 I 880612 Engine 1 SB BR700.72-101476R1 - Introduction of a New Combustion Chamber Without Cooling Ribs Effectivity:GV Engines Prior to Engine Serial 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. 72 OPT 29Aug 2014 I 880612 Engine 2 (890612) SB BR700.72-101476RI - Introduction of a New Combustion Chamber Without Cooling Ribs Effectivity:GV Engines Prior to Engine Serial 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. 72 OPT 29Aug 2014 I 880613 Engine 1 SB BR700.72-101540 R4 Outlet Guide Vane Housing Assembly 72 OPT 29Aug 2014 I 880613 Engine 2 (890613) SB BR700.72-101540 R4 Outlet Guide Vane Housing Assembly 72 OPT 29Aug 2014 I 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 Logbook Code Description Effectivity ATA Status CNV Source HRS LOG Date CA MM REF M HRS Work Order 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 Gulf stream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620824

TYP Logbook Code Description Effectivity ATA Status CNV Source HRS LDG Date CA MM REF M HRS Work Order aintenance Notes Cert No Engine 1 880615 SB BR700.72.101897 • Introduction of an Alternative Standard of HP Compressor Stage 1 Blade Compliance: OPTIONAL This Service Bulletin introduces alternative and fully interchangeable pans. 72 OPT 22 Sep 2014 I Engine 2 880615 (890615) SB BR700.72.101897 • Introduction of an Alternative Standard of HP Compressor Stage 1 Blade Compliance: OPTIONAL This Service Bulletin introduces alternative and fully interchangeable pans. 72 OPT 22 Sep 2014 I Engine 1 882900 SB BRR700.29.900511 Left Engine Hydraulic Tubes and Fittings Note: Bulletin only applies to engine when installed in the left (No.1) position. 72 REC C/W 1787.4 543 08 Mar 2011 C 0.00 Engine 2 882900() SB BRR700.29.900511 Left Engine • Hydraulic Tubes and Fittings Note: Bulletin only applies to engine when installed in the left (No.1) position. 72 REC 08 Dec 2010 I Engine 1 882910 Alert SB BR700.72-A900508 Replacement of HP Turbine Rotor Discs Due to Steel Inclusion BR700.710A1.10 Engine sin 11182. 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. CAN CAN 0.0 0 23 Apr 2013 C 0.00 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 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620825

Logbook TYP aintenance Notes 882910 Alert SB BR700.72-A900508 Engine 2 (892910) Replacement of HP Turbine Rotor Discs Due to Steel Inclusion Code Description Effectivity ATA Status CNV Source Work Order Cert No HRS LOG Date CA MM REF M HRS BR700.710A1.10 Engine sin 11182. 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. CAN CAN Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link. 0.0 0 23 Apr 2013 C 0.00 Engine 1 882911 Alert SB BR700.72,4900508 Rev 1 Replacement of HP Turbine Rotor Discs Due to Steel Inclusion BR700.710A1.10 Engine sin 11182. 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. MAN N/A 22 Apr 2013 G-CGUL G550 5176 Technical Bulletins Page 36 of 164 20 Jan 2015 (O2015 Gulf stream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620826

TYP Logbook Code Description Effectivity ATA Status CNV Source HRS LOG Date c/I MM REF M HRS Work Order 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 Engine Life Management - Fixed 70 OPT N/A 7.2 6 09 Apr 2008 C 0.00 Engine 1 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 • 70 OPT NA, 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 Engine 1 887002 SB BR700.70.900294 • Task Oriented EFF: Section 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 70 OPT CW 7.2 6 09 Apr 2008 C 0.00 G-CGUL G550 5176 Technical Bulletins Page 37 of 164 20 Jan 2015 O2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620827

TYP Logbook Code Description Effectivity ATA Status CNV Source HRS LOG Date CA MM REF M HRS Work Order aintenance Notes Cert No 887002 SB BR700.70.900294 • Task Oriented EFF: Section 1 • Engine 2 (897002) Engine Inspection BR700•710A1-10 (GV) Engines // Section 2. BR700.710C4.11 (G5001 G550) Engines // TASK ORIENTED Maintenance Program Mx. Notes: ENGINE DECLARED TASK ORIENTED 70 OPT cm 7.2 6 09 Apr 2008 C 0.00 887003 SB BR700•70•900412 • BR7I0 Engine 1 Engine Maint Prog Mx. Notes: ENGINE DECLARED TASK ORIENTED EFF: BR700.710A1• 10 (GV) Engines!! BR700-710C4•11 (G5001 G550) Engines 70 OPT CAN 7.2 6 09 Apr 2008 C 0.00 887003 SB BR700-70.900412 • BR710 Engine 2 (897003) Engine Maint Prog Mx. Notes: ENGINE DECLARED TASK ORIENTED EFF: BR700.710A1• 10 (GV) Engines // BR700-710C4•11 (G5001 G550) Engines 70 OPT OW 7.2 6 09 Apr 2008 C 0.00 887186 SB BR700-71.101206 • Power Plant Engine 1 External Drain Tubes And Fitting NOTE: Prior to Engine Serial Number 15111 71 REC N/A 0.0 0 26 Nov 2007 C 0.00 887166 SB BR700.71.101206 - Power Plant Engine 2 (897166) External Drain Tubes And Fitting NOTE: Prior to Engine Serial Number 15111 71 REC N/A 0.0 0 26 Nov 2007 C 0.00 887175 SB BR700.71.101424 • Modified Engine I Installation of Clip Stack Effectivity: BR700- 710C4-11 Engines, which have Service Bulletin SB•BR700-71- 101206 incorporated. Prior to Engine Serial Number 15165 71 REC N/A 0.0 0 26 Nov 2007 C 0.00 887175 SB BR700.71.101424 • Modified Engine 2 (897175) Installation of Clip Stack Effectivity: BR700• 710O1-11 Engines, which have Service Bulletin SB•BR700-71- 101206 incorporated. Prior to Engine Serial Number 15165 71 REC N/A 0.0 0 26 Nov 2007 C 0.00 SB BR700.71.101462 - Extension 887176 Clip with Simplified Design NOTE: Prior to Engine Serial Number 15206 71 Engine OPT 27 Jan 2006 I G-CGUL G550 5176 Technical Bulletins Page 38 of 164 20 Jan 2015 riD 2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620828

TYP Logbook li Code Description Effectivity ATA Status C/W Source HRS LDG Date C/I MM REF M HRS Work Order aintenance Notes Cert No Engine 2 887176 (897176) SB BR700.71-101462 - Extension Clip with Simplified Design NOTE: Prior to Engine Serial Number 15206 71 OPT 27 Jan 2006 I Engine 1 887177 SB BR700.71-101561 - EEC Harness Revised Harness Clipping Effectivity: Prior to engine SN 15352 71 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 887177 (897177) SB BR700-71-101561 - EEC Harness - Revised Harness Clipping Effectivity: Prior to engine SN 15352 71 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 887178 SB BR700.71-101563 - Engine Build Unit (EBU) Harness EFF: from EBU serial number GVSP001 to GVSP124. 71 OPT 23 May 2007 I Engine 2 887178 (897178) SB BR700.71-101563 - Engine Build Unit (EBU) Harness EFF: from EBU serial number GVSP001 to GVSP124. 71 OPT 23 May 2007 I Engine 1 887179 SB 6R700-71-101581 - Oil Drain Tube Support Bracket Effectivity: Prior to Engine Serial Number 15410 and from Engine Serial Number 15412 to 15415 71 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 887179 (897179) SB BR700.71-101581 - Oil Drain Tube Support Bracket Effectivity: Prior to Engine Serial Number 15410 and from Engine Serial Number 15412 to 15415 71 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 887188 SB BR700.71-900384 - Engine Electronic Controller (EEC) Harness Effectivity: For engines which have hardware configuration standard 710C4.11 or 710C4.11/10 engraved on the engine data plate 71 REC 23 May 2007 I Engine 2 887188 (897188) SB BR700.71-900384 - Engine Electronic Controller (EEC) Harness Effectivity: For engines which have hardware configuration standard 710C4.11 or 710C4.11/10 engraved on the engine data plate 71 REC 23 May 2007 I 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

L TYP Logbook Code Description Effectivity aintenance Notes Engine 1 887189 SB BR700.71-900413 - Engine Build Unit (EBU) Harness Effectivity: For engines which have hardware configuration standard 710C4.11 or 71004.11110 engraved on the engine data plate Engine 2 887189 SB BR700.71-900413 - Engine Build (897189) Unit (EBU) Harness Effectivity: For engines which have hardware configuration standard 710C4.11 or 71004.11110 engraved on the engine data plate 887190 SB BR700.71-900336 - Fan Cowl Engine 1 Door Switch Brackets Effectivity: Aircraft &Ns 5023 thru 5028 887190 SB BR700.71-900336 - Fan Cowl Engine 2 (897190) Door Switch Brackets Effectivity: Aircraft &Ns 5023 thru 5028 887195 SB BR700.71-900505 EEC Lane A 710A1.10. 710O4.11 Engine 1 Harness - Inspection prior to tin 15651 887195 SB BR700.71-900505 EEC Lane A 710A1.10. 710O4.11 Engine 2 (897195) Harness • Inspection prior to ern 15651 Engine 1 887257 SB BR700.72-900455 Rev 2 Pt. A Visual Insp LP Compressor Annulus Fillers NOTE: See REVISION 5 CMP CODES 887397.f 897397 Superceded see 880596 887257 SB BR700.72-900455 Rev 2 Pt. A Engine 2 (897257) Visual Insp LP Compressor Annulus Fillers NOTE: See REVISION 5 CMP CODES 887397.f 897397 Superceded see 880596 Engine 1 887258 SB BR700.72-900455 Rev 2 Pt. B Eddy Current Insp LP Compressor Annulus Fillers NOTE: See REVISION 5 CMP CODES 887398.f 897398 Superceded see 880596 ATA Status C/W Source HRS LDG Date Cli MM REF M HRS Work Order Cert No 71 REC 23 May 2007 I 71 REC 23 May 2007 I 88 REC N/A 0.0 0 26 Nov 2007 C 0.00 88 REC N/A 0.0 0 26 Nov 2007 C 0.00 REC CPN 1787.4 543 08 Mar 2011 C 0.00 REC CPN 1787.4 543 08 Mar 2011 C 0.00 72 CAN CPN GAMA20 F080834 206.7 90 20 Aug 2008 C 0.00 72 CAN CPN GAMA20 F080834 206.7 90 20 Aug 2008 C 0.00 72 CAN 28 Feb 2008 I 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 Logbook Code Description Effectivity IATAI Status CNV Source HRS LOG Date CA MM REF M HRS Work Order Ilaintenance Notes Cert No 887258 Engine 2 (897258) SB BR700.72.900455 Rev 2 Pt. B Eddy Current Insp - LP Compressor Annulus Fillers NOTE: See REVISION 5 - CMP CODES 887398 897398 Superceded see 880596 72 CAN 28 Feb 2008 I 887361 Engine 1 SB BR700.73.101415 • Fuel System - Flexble Air Tubes NOTE: GV Engines: Prior to Engine Serial Number 11505 11 G500 & G550 Engines: Prior to Engine Serial Number 15168 and for Engine Serial Numbers 15169 to 15176 73 OPT N/A 0.0 0 26 Nov 2007 C 0.00 887361 Engine 2 (897361) SB BR700.73.101415 • Fuel System - Flexible Air Tubes NOTE: GV Engines: Prior to Engine Serial Number 1150511 G500 & G550 Engines: Prior to Engine Serial Number 15168 and for Engine Serial Numbers 15169 to 15176 73 OPT N'A 0.0 0 26 Nov 2007 C 0.00 887367 Engine 1 SB BR700.73-101443 - Engine Fuel And Control (DEP) NOTE: GV Engines: Prior to Engine Serial Number 11505 11 G500 & G550 Engines: Prior to Engine Serial Number 15228 73 OPT NIA 0.0 0 26 Nov 2007 C 0.00 887367 Engine 2 (897367) SB BR700.73.101443 • Engine Fuel And Control (DEP) NOTE: GV Engines: Prior to Engine Serial Number 1150511 G500 & G550 Engines: Prior to Engine Serial Number 15228 73 OPT N/A 0.0 0 26 Nov 2007 C 0.00 G-CGUL G550 5176 Technical Bulletins Page 41 of 164 20 Jan 2015 O2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620831

TYP Logbook Code Description Effectivity ATA Status CNV Source HRS LOG Date CA MM REF M HRS Work Order aintenance Notes Cert No Engine 1 887391 SB BR700.73.900323 • FMU Connector O-Ring Effectivity: Engine Serial Numbers 15107 thru 15109, 15111, 15114 that 15117, 15120 thru 15130 and 15132 that 15135 71 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 887391 (897391) SB BR700.73.900323 • FMU Connector O-Ring Effectivity: Engine Serial Numbers 15107 thru 15109, 15111, 15114 that 15117, 15120 that 15130 and 15132 that 15135 71 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 8896 73 SB BR700.73•A900451 - Combined Overspeed Shutoff Solenoid NOTE: For engines which have a Fuel Metering Unit (FMU). PM 8061.977 with a FMU Serial Number prior to 15174932 installed 73 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 887396 (897396) SB BR700.73•A900451 - Combined Overspeed Shutoff Solenoid NOTE: For engines which have a Fuel Metering Unit (FMU). PM 8061.977 with a FMU Serial Number prior to 15174932 installed 73 MAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 887397 SB BR700.72.900455 Visual Insp - LP Compressor Annulus Fillers (Part A) It is recommended that PART A of this Non. 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 CAN OW GAL100716 1479.1 446 03 Sep 2010 C 880596/880597 G-CGUL G550 5176 Technical Bulletins Page 42 of 164 20 Jan 2015 O2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620832

L TYP Logbook Code aintenance Notes Description Effectivity ATA Status C/W Source Work Order Cert No HRS LDG Date Cli MM REF M HRS 887397 SB BR700.72-900455 Visual 'lisp It is recommended that Engine 2 (897397) LP Compressor Annulus Fillers (Part PART A of this Non- 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 CAN CAN GAL100716 1479.1 446 03 Sep 2010 C Engine 1 887398 SB BR700.72-900455 Eddy Current- For BR700.710A1-10 LP Compressor Annulus Fillers (Part and BR700.710C4-II 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 CAN CPN GAL100716 1479.1 446 03 Sep 2010 C 887398 SB BR700.72-900455 Eddy Current- For BR700.710A1-10 Engine 2 (897398) LP Compressor Annulus Fillers (Part and BR700.710C4.11 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 CAN CPN GAL100716 1479.1 446 03 Sep 2010 C G-CGUL G550 5176 Technical Bulletins Page 43 of 164 20 Jan 2015 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620833

L TYP Logbook Code Description Effectivity ATA Status C/W Source HRS LDG Date Cli MM REF M HRS Work Order aintenance Notes Cert No Engine 1 887514 SB BR700.75-101097 - Core Air Tubes And Fittings Intro Effectivity: Prior to engine SN 15131 75 OPT N/A 0.0 0 26 Nov 2007 C 0.00 887514 Engine 2 (897514) SB 6R700-75-101097 - Core Air Tubes And Fittings Intro Effectivity: Prior to engine SN 15131 75 OPT N/A 0.0 0 26 Nov 2007 C 0.00 887532 Engine 1 SB BR700.75-900308 - VSV Mechanism Lubrication Effectivity: Prior to Engine Serial Number 15146 75 INF N/A 0.0 0 26 Nov 2007 C 0.00 887532 Engine 2 (897532) SB BR700.75-900308 - VSV Mechanism Lubrication Effectivity: Prior to Engine Serial Number 15146 75 INF N/A 0.0 0 26 Nov 2007 C 0.00 887707 Engine 1 SB BR700-77-101534 - New TGT Probes Effectivity: BR700- 710A1.10 Engines Prior to Engine Serial Number 1150611 BR700.710C4.11 Engines Prior to Engine Serial Number 15308 77 OPT N/A 0.0 0 26 Nov 2007 C 0.00 887707 Engine 2 (897707) SB 6R700-77-101534 - New TGT Probes Effectivity: BR700- 710A1.10 Engines Prior to Engine Serial Number 11506/I BR700.710C4.11 Engines Prior to Engine Serial Number 15308 77 OPT N/A 0.0 0 26 Nov 2007 C 0.00 887708 Engine 1 SB BR700.77-101536 - Turbine Gas Temp (TGT) Harness EFF: Prior to eng SN 15322 and for Engine SN 15330 and 15331, 77 OPT N/A 0.0 0 26 Nov 2007 C 0.00 887708 Engine 2 (897708) SB BR700.77-101536 - Turbine Gas Temp (TGT) Harness EFF: Prior to eng SN 15322 and for Engine SN 15330 and 15331. 77 OPT N/A 0.0 0 26 Nov 2007 C 0.00 887711 Engine 1 SB BR700.77-900329 - N2 Speed Probes Effectivity: N2 speed probes. PIN 889-3.13. with Serial Numbers listed in this SB 77 REC N/A 0.0 0 26 Nov 2007 C 0.00 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 Logbook aintenance Notes Code Description Effectivity ATA Status CNV Source Work Order Cert No HRS LOG Date c/I MM REF M HRS Engine 2 887711 (897711) Airframe 887803 Airframe 887804 Airframe 887839 Airframe 887840 Airframe 887841 SB BR700-77-900329 • N2 Speed Effectivity: N2 speed Probes probes. P/N 889.3.13, with Serial Numbers listed in this SB 77 REC N/A 0.0 0 26 Nov 2007 C 0.00 BR700-78.900535 R3 • TRU Door Actuator (Left) • Inspection of Rod End Assy of the PDA Accomplishment of this SB is optional. 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. OPT 13 Aug 2012 I BR700•78•900535 R3 • TRU Door Actuator (Right) • Inspection of Rod End Assy of the PDA Accomplishment of this SB is optional. 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. OPT 13 Aug 2012 I BR700-78.101512 • Improvements to NOTE: GV Engines: 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: 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: New Y Stop Fitting (Left) Prior to TRU Serial Number 3981 G5001 G550 Engines: Prior to TRU Serial Number 153 78 OPT N/A 0.0 0 26 Nov 2007 C 0.00 78 OPT N/A 0.0 0 26 Nov 2007 C aoo 78 OPT N/A 0.0 0 26 Nov 2007 C aoo G-CGUL G550 5176 Technical Bulletins Page 45 of 164 20 Jan 2015 492015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620835

TYP Logbook Code Description Effectivity ATA Status C/W Source HRS LDG Date Cli MM REF M HRS Work Order Maintenance Notes Cert No Airframe 887842 BR700.78-101516 New Primary Door Lock Actuator (Left) NOTE: Prior to TRU Serial Number 153/ This Bulletin installs PM -02. when this SB is complied with remove the frequency from 887850 and 897850 78 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Airframe 887843 8P700-78.101606 - Introduction of a New T/FI Unit (Left) NOTE: Prior to TRU Serial Number 331 78 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Airframe 887848 BR700.78-900440 - Inspection of TIP Structure Boxes I Connectors (Left) NOTE: See SB for Thrust Reverser Serial Numbers affected 78 REC N/A 0.0 0 26 Nov 2007 C 0.00 Airframe 887850 BR700-78.900350 - Primary Door Lock Actuator - Insp (Left) NOTE: Recurring 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). 78 REC N/A 0.0 0 05 May 2008 C 0.00 Airframe 887851 BR700-78.900443 - Replacement Of T/R Access Doors (Left) NOTE: Left TRU SIN: 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 78 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 887934 SB BR700-79-101449 - Oil Filter Differential Pressure Switch Effectivity: Prior to Engine Serial Number 15198 79 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 887934 (897934) SB BR700.79-101449 - Oil Filter Differential Pressure Switch Effectivity: Prior to Engine Serial Number 79 OPT N/A 0.0 0 26 Nov 2007 C 0.00 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

Logbook TYP aintenance Notes Code Description Effectivity Engine 1 887935 SB BR700•79•101458 • Oil Filter Element Effectivity: Prior to Engine Serial Number 15198 887935 SB BR700•79•101458 • Oil Filter Engine 2 (897935) Element Effectivity: Prior to Engine Serial Number 15198 Engine 1 SB BR700.79.101803R1 887944 Introduction Of New Oil Pump Unit With Improved Gears 887944 SB BR700.79.101803R1 • Engine 2 (897944) Introduction Of New Oil Pump Unit With Improved Gears Engine 1 888010 SB BR700.80.900340 • Air Turbine Starter Oil Level NOTE: For engines 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 Engine 2 (898010) Starter Oil Level NOTE: For engines 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 Engine 1 888011 Valve 888011 SB BR700.80.900427 • Starter Air Engine 2 (898011) Valve ATA Status CNV Source HRS LOG Date CA MM REF M HRS Work Order Cert No 79 OPT N/A 0.0 0 26 Nov 2007 C 0.00 79 OPT N/A 0.0 0 26 Nov 2007 C 0.00 79 REC 29 Aug 2014 I 79 REC 29 Aug 2014 80 REC N/A 0.0 0 26 Nov 2007 C 0.00 80 REC N/A 0.0 0 26 Nov 2007 C 0.00 80 INF N/A 0.0 0 26 Nov 2007 C 0.00 80 INF N'A 0.0 0 26 Nov 2007 C 0.00 G-CGUL G550 5176 Technical Bulletins Page 47 of 164 20 Jan 2015 C2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620837

L TYP Logbook Code aintenance Notes Description Effectivity ATA Status C/W Source Work Order Cert No HRS LDG Date Cli MM REF M HRS Engine 1 888801 SB BR700-73-900153FMU O/S SIO Not Applicable for G550 Engines 88 CAN N/A 0.0 0 26 Nov 2007 C 731005 0.00 888801 Not Applicable for SB BR700.73-900153FMU as sio Engine 2 (898801) G550 Engines 88 CAN N/A 0.0 0 26 Nov 2007 C 731005 0.00 888802 SB BR700.72-900229LP COMP GVI Not Applicable for Engine 1 G550 Engines 88 CAN N/A 0.0 0 26 Nov 2007 C ACB 11A 0.00 888802 Not Applicable for SB BR700.72-900229LP COMP GVI Engine 2 (898802) G550 Engines 88 CAN N/A 0.0 0 26 Nov 2007 C ACB 11A 0.00 888803 SB BR700.72-900229LP COMP NDI Not Applicable for Engine 1 G550 Engines 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 888803 Not Applicable for SB BR700.72-900229LP COMP NDI Engine 2 (898803) G550 Engines 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 888804 SB BR700.72-900229LP COMP NDI Not Applicable for Engine 1 G550 Engines 88 CAN N/A 0.0 0 26 Nov 2007 C ACB 11A 0.00 888804 Not Applicable for SB BR700.72-900229LP COMP NDI Engine 2 (898804) G550 Engines 88 CAN N/A 0.0 0 26 Nov 2007 C ACB 11A 0.00 888805 SB BR700.72-900229 TECH Engine 1 VARIANCE Not Applicable for G550 Engines 88 CAN N/A 0.0 0 26 Nov 2007 C TV1913R 0.00 888805 SB BR700.72-900229 TECH Not Applicable for Engine 2 (898805) VARIANCE G550 Engines 88 CAN N/A 0.0 0 26 Nov 2007 C TV1913R 0.00 Engine 1 888807 SB BRR700.73.101106FMU Not Applicable for G550 Engines 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 888807 SB BRR700.73-101106FMU Engine 2 (898807) Not Applicable for G550 Engines 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 888808 SB BR700.72-100900 NEW CORE Not Applicable for Engine 1 FAIR G550 Engines 88 CAN N/A 0.0 0 26 Nov 2007 C 999822 0.00 888808 SB BR700.72-100900 NEW CORE Not Applicable for Engine 2 (898808) FAIR G550 Engines 88 CAN N/A 0.0 0 26 Nov 2007 C 999822 0.00 G-CGUL G550 5176 Technical Bulletins Page 48 of 164 20 Jan 2015 @ 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620838

L TYP Logbonk Code aintenance Notes Description Effectivity ATA Status C/W Source Work Order Cert No HRS LDG Date CII MM REF M HRS Engine 1 888809 SB BR700.72-101395 METCO Not Applicable for BLADE CO G550 Engines 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 888809 SB BR700-72-101395 METCO Not Applicable for Engine 2 (898809) BLADE CO G550 Engines 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 888810 SB BR700-71-100995 HYD PUMP Not Applicable for Engine 1 RMVL G550 Engines 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 888810 SB BR700.71-100995 HYD PUMP Not Applicable for Engine 2 (898810) RMVL G550 Engines 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 888813 SB BR700-79-900215 R2 PT 1 DPI Not Applicable for Engine 1 SW G550 Engines 88 CAN N/A 0.0 0 26 Nov 2007 C AD 01.01.01 0.00 888813 SB ØR700.79-900215 R2 PT 1 DPI Not Applicable for Engine 2 (898813) SW G550 Engines 88 CAN N/A 0.0 0 26 Nov 2007 C AD 0101.01 0.00 888814 SB BR700-79-900215R2 PT 2 DPI Engine 1 SW CAN N/A 0.0 0 26 Nov 2007 C AD 0101.01 0.00 888814 SB BR700-79-900215R2 PT 2 DPI Engine 2 (898814) SW CAN N/A 0.0 0 26 Nov 2007 C AD 01.01.01 0.00 888815 SB BR700.73-100148 EJECTOR Engine 1 FILTER Not Applicable for G550 Engines 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 888815 SB BR700-73-100148 EJECTOR Not Applicable for Engine 2 (898815) FILTER G550 Engines 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Applicable fo Not r 888816 SB BR700.73-101441 EEC G9.1 SAN 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 Engine 2 (898816) G550 Engines 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 888817 SB BR700.73-900182FMU VALVE- Not Applicable for Engine 1 DSE G550 Aircraft 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 888817 SB BR700-73-900182FMU VALVE- Not Applicable for Engine 2 (898817) DSE G550 Aircraft 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 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

L TYP Logbook Code aintenance Notes Description Effectivity ATA Status C/W Source Work Order Cert No HRS LDG Date Cli MM REF M HRS 888818 SB BR700.72-101473 DFL FAN Not Applicable for Engine 1 BLADES G550 Engines 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 888818 SB BR700.72-101473 DFL FAN Not Applicable for Engine 2 (898818) BLADES G550 Engines 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 888819 SB BR700.72-101144 (Use CMP Engine 1 Code 880271) 72 CAN N/A 0.0 0 26 Nov 2007 C 0.00 888819 SB BR700.72-101144 (Use CMP Engine 2 (898819) Code 880271) 72 CAN N/A 0.0 0 26 Nov 2007 C 0.00 888820 SB BR700-73-101400 EEC 52.1 SAN Engine 1 (Use CMP Code 880305) 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 888820 SB BR700-73-101400 EEC 52.1 SAN Engine 2 (898820) (Use CMP Code 880305) 88 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 888822 Use CMP Code 880422 / 890422 EFF: Engine Serial Numbers prior to SIN 15146 ./ Module M33- 12 (HP Compressor Module 72 CAN N/A 0.0 0 26 Nov 2007 C 0.00 888822 Use CMP Code 880422 / 890422 Engine 2 (888822) EFF: Engine Serial Numbers prior to SIN 15146/ Module M33- 12 (HP Compressor Module 72 CAN N/A 0.0 0 26 Nov 2007 C 0.00 Airframe 897839 BR700.78.101512 - Improvements to NOTE: GV Engines: the Thrust Reverser Pivoting Doors Prior to TRU Serial (Right) Number 398 .// G500 8 G550 Engines: Prior to TRU Serial Number 153 78 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Airframe 897840 BR700.78.101514 TM Fixed NOTE: GV Engines: Structure - Upper Inhibition Bolt Fining Prior to TRU Serial (Right) Number 398// G500 8 G550 Engines: Prior to TRU Serial Number 153 78 OPT N/A 0.0 0 26 Nov 2007 C 0.00 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 Logbook Code Description Effectivity ATA Status C/W Source HRS LDG Date Cli MM REF M HRS Work Order Maintenance Notes Cert No Airframe 897841 BR700.78.101515 Introduction of a New Y Stop Fitting (Right) NOTE: GV Engines: Prior to TRU Serial Number 398/G500! G550 Engines: Prior to TRU Serial Number 153 78 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Airframe 897842 8R700-78.101516 - New Primary Door Lock Actuator (Right) NOTE: Prior to TRU Serial Number 153/ This Bulletin installs P/N -02. when this SB is complied with remove the frequency from 887850 and 897850 78 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Airframe 897843 BR700-78.101606 - Introduction of a New T/R Unit (Right) NOTE: Prior to TRU Serial Number 331 78 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Airframe 897848 BR700J8.900440 - Inspection of T/R Structure Boxes/ Connectors (Right) NOTE: See SB for Thrust Reverser Serial Numbers affected 78 REC N/A 0.0 0 26 Nov 2007 C 0.00 Airframe 897850 BR700-78.900350 - Primary Door Lock Actuator - Insp (Right) NOTE: Recurring 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). 78 REC N/A 0.0 0 05 May 2008 C 0.00 Airframe 897851 8R700-78.900443 - Replacement Of T/R Access Doors (Right) NOTE: Left TRU SIN: 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 78 REC N/A 0.0 0 26 Nov 2007 C 0.00 Airframe 901001 ST02696AT-D PAX OXY CONTROL 35 INF CPN 20.7 1 30 Apr 2008 C 0.00 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 Logbook Code Description Effectivity ATA Status C/W Source HRS LDG Date Cli MM REF M HRS Work Order Maintenance Notes Cert No Airframe 901007 ST02697AT-D EMERGENCY LIGHTING 33 INF CPAr 20.7 t 30 Apr 2008 C 0.00 Airframe 901010 ST02715AT-D EXTERNAL CAMERA Ell' Desc: SECURAPLANE. 23 INF CPAr 20.7 t 30 Apr 2008 C 0.00 Airframe 901022 ST00892LA Emergency Vision Assurance System (EVAS) 25 INF NIA 0.0 0 26 Nov 2007 C 0.00 Airframe 901023 ST02915AT-D LSZ-860 LIGHTNING DETECTOR INF CPAr 20.7 t 30 Apr 2008 C 0.00 Airframe 901024 ST02796AT-D BROAD BAND MULTI LINK SYS (BBML) NOTE: See CMP Codes 262578 and 262548 for ICA Requirements INF CPAr 20.7 t 30 Apr 2008 C 0.00 Airframe 901025 ST02920AT-D SATCOM SYSTEM (MCS-7000) INF NIA 0.0 0 26 Nov 2007 C 0.00 Airframe 901031 ST03290AT-D (ATG) Injection Molded Elec Window Shades 25 INF CPAr 20.7 t 30 Apr 2008 C 0.00 Airframe 901063 ST01957CH.D Airshow Remote Controller NOTE: See CMP Codes 233265 and 233266 for ICA Requirements 23 INF NIA 0.0 0 26 Nov 2007 C 0.00 Airframe 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 COMM AREA NOTE: See CMP Code 252098 for ICA Requirement 25 INF NIA 0.0 0 26 Nov 2007 C 0.00 Airframe 901071 ST02047CH.D MAGNASTAR MCS• 7000 NOTE: See CMP Codes 232134 and 232135 for ICA Requirements INF CPAr 20.7 1 30 Apr 2008 C 0.00 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 Logbook Code Description Effectivity ATA Status C/W Source HRS LDG Date Cli MM REF M HRS Work Order Maintenance Notes Cert No Airframe 901072 ST02048CH.D Airshow 4000 System NOTE: See CMP Code 232165 for ICA Requirement INF CPN 20.7 I 30 Apr 2008 C 0.00 Airframe 901073 ST02049CH.D SECURAPLANE 500 NOTE: See CMP Codes 237225. 237228. 237235. and 232245 for ICA Requirements INF CPN 20.7 I 30 Apr 2008 C 0.00 Airframe 901077 ST03686AT-D Airplane Interior Reference GAC document No. GC5280I A715 for Maintenance Requirements Instructions for Continued Airworthiness dated 610612012. MAN Airframe 901078 ST04289AT-D Aircraft Interior OPT 31 Aug 2013 I Airframe 901355 STO3044AT-D Cabin Custom Interior EFF: G550 5063 ONLY. INF N/A 0.0 0 26 Nov 2007 C 0.00 Airframe 901377 ST03033CH.D True North Simphone System STC ST03033CH-D True North Simphone System. Standard Aero Document No. 1021304. 23 OPT Airframe 901952 ST01952CH.D EXECUTIVE INTERIOR INF N/A 0.0 0 26 Nov 2007 C 0.00 Airframe 901977 ST02196LA-D Fonvard Vestibule Compartment With 1 Additional Crew Seat 25 INF Airframe 901978 ST04260AT-D Installation Of Rockwell Collins Programmable Switch (PSW) OPT 05 Jun 2012 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 Logbook Code Description Effectivity Maintenance Notes ST03781AT-D TrueNonh Simphone Airframe 901979 Airborne Telecommunication 901980 ST04250AT-D Interior Airframe Reconfiguration 901981 ST04246AT-D EMS AMT-700G Airframe SATCOM STC ST04246AT-D Installation of EMS AMT-700G SATCOM Antenna Subsystem. Airframe 901982 ST04261AT-D Airplane Interior Airframe 940040 CE-CSB-5004 CSB 004 (Advanced Effectivity: This Cabin 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. ATA Status C/W Source HRS LDG Date Cli MM REF M HRS Work Order Cert No INF 14 Jun 2010 INF 03 Feb 2012 I INF 08 Dec 2011 INF 44 OPT 24 Oct 2014 5483. Final Phase cut- in starts with serial number 5486 and sub. APU I 950002 RE-220-49-0002 SEALENT GEN ADP 95 OPT N/A 0.0 0 26 Nov 2007 C 0.00 APU 1 957045 SB RE220-49-7045 LOAD CONTROL VALVE 95 OPT N/A 0.0 0 26 Nov 2007 C 0.00 APU 1 957275 RE-220-497275 Repl Deprime Valve. 4140028.2 WM 95 REC N/A 0.0 0 26 Nov 2007 C 0.00 APU I 957282 RE-220-497282 Repalce Inlet Duct & Hardware For Hourrneter 49 REC N/A 0.0 0 26 Nov 2007 C 0.00 APU 957350 RE-220-49-7350 Replace Plug And Oil Filter Element 49 REC N/A 0.0 0 26 Nov 2007 C 0.00 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 Logbook Code Description Effectivity ATA Status C/W Source HRS LDG Date Cli MM REF M HRS Work Order Maintenance Notes Cert No APU I 957359 RE-220-49-7359 Replace T-Wheel PN WE897994.I With WE897994.3 95 REC N/A 0.0 0 26 Nov 2007 C 0.00 APU I 957360 RE-220-49-7360 RPL Fuel Nozzle Bolts. MS9489-06 WI-05 95 REC N/A 0.0 0 26 Nov 2007 C 0.00 APU t 957362 RE-220-49-7362 Replace Lube Pump 95 REC N/A 0.0 0 26 Nov 2007 C 0.00 APU I 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 1 957536 RE-220-49-7536 Replace Atomizer Gasket PN MS9372-031 99 REC N/A 0.0 0 26 Nov 2007 C 0.00 APU 1 957559 RE-220-49.7559 APU EGT MOD 95 OPT N/A 0.0 0 26 Nov 2007 C 0.00 APU I 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 Solenoid Valve 95 OPT N/A 0.0 0 26 Nov 2007 C 0.00 APU I 957689 RE-220-49-7689 Remove/Replace Ignition Exciter 95 OPT N/A 0.0 0 26 Nov 2007 C 0.00 APU I 957690 RE-220-49-7690 Add Deprime Valve EFF: Before SN P-298. Assy, Inerterence Shield 95 REC N/A 0.0 0 26 Nov 2007 C 0.00 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 Logbook Code Description Effectivity Maintenance Notes APU I 957694 RE-220-49-7694 One Time Insp:Replc of Coupling Clamp. T-Bolt APU I 957761 RE-220-49-776I Replace Turbine Bearing Oil Tubes APU I 957771 RE-220-49-777I LOAD CONT VALVE 957772 RE-220-49-7772 Replace Spline APU I Shaft PN WE8979977-3 957775 RE-220-49-7775 Replace Comp APU I Shroud PN W63827383-I 957795 RE-220-49-7795 SURGE CONTROL APU I VALVE 957826 SB RE220-49-7826 Removal / APU I Replace Ignitor Exciter EFF: Before SN# P- 405. 957854 SB RE220-49-7854 Oil Sump Heater- EFF: APU SN#s APU I Replace before P-4 I 4 957863 SB RE220-49-7863 Replace APU I Electronic Control Unit EFF: Before SN# P- 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 APU I Gas Temp Sensor (EGT) P-473. APU I 957935 SB49.7933R5 APU Approved Oils ATA Status C/W Source HRS LDG Date Cli MM REF M HRS Work Order Cert No 95 REC N/A 0.0 0 26 Nov 2007 C 0.00 95 REC N/A 0.0 0 26 Nov 2007 C 0.00 95 OPT N/A 0.0 0 26 Nov 2007 C 0.00 95 REC N/A 0.0 0 26 Nov 2007 C 0.00 95 REC N/A 0.0 0 26 Nov 2007 C 0.00 95 OPT N/A 0.0 0 26 Nov 2007 C 0.00 49 REC N/A 0.0 0 26 Nov 2007 C 0.00 49 OPT NiA 0.0 0 26 Nov 2007 C 0.00 95 REC N/A 0.0 0 26 Nov 2007 C 0.00 49 OPT N/A 0.0 0 26 Nov 2007 C 0.00 49 INF 23 Oct 2014 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

L TYP Logbook Code Description Effectivity aintenance Notes ASC Airframe 970021 ASC 2A Digital Flight Data Recorder Sys Upgrade This rev cancels ASC 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 970022 System Upgrade Airframe Cancelled by ASC 002C issued 11121/2008. ASC Airframe 970023 ASC 2C Digital Flight Data Recorder System Upgrade (88 Parameters) Mx. Notes: This code has been cancelled. Effectivity: This service change is applicable to G500 & G550 aircraft serial numbers 5001 and subsequent requiring Pan 135 certification. Cancelled by ASC 002D. ATA Status C/W Source HRS LDG Date Cli MM REF M HRS Work Order Cert No 31 CAN CAN 0.0 0 26 Nov 2007 C 0.00 31 CAN GAC CPN APPLETON FP549 CRS GIFR100Y 20.7 11 09 Apr 2008 C 0.00 31 CAN CAN 0.0 0 24 Feb 2014 C ASC Airframe 970024 ASC 2D Digital Flight Data Recorder System Upgrade (88 Parameters) Effectivity: This service 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. 31 OPT 19Jun 2012 ASC ASC 4 PACK INLET VALVE Eff. Desc: 5001-5020. 970040 Airframe REPLACE This ASC cancelled ASC 970042 ASC 4A Aml Pack Inlet Valve Airframe Replacement This Service change is for information purposes only. Permits the Intl of 1151582-6 Enviromental Control System. 21 CAN CAN 0.0 0 26 Nov 2007 C 0.00 21 INF PIE 0.0 0 26 Nov 2007 C 0.00 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

L TYP Logbook Code Description Effectivity aintenance Notes ASC Airframe 970070 ASC 7 PDB CONNECTOR INSERTS Eff. Desc: 5017.5022. ASC Airframe 970080 ASC 8 MAX GROSS WGT 75K Canx see ASC 008A PLACARD ASC 970081 ASC 8A Maximum Gross Weight Airframe 75.000 Pounds Mx. Notes: This code has been cancelled. This revision cancels 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 ATA Status C/W Source HRS LDG Date Cli MM REF M HRS Work Order Cert No 24 OPT PIE 0.0 0 26 Nov 2007 C 0.00 11 CAN CM GAC APPLETON FP549 CRS G1FR100Y 20.7 11 09 Apr 2008 C 11 0.00 CAN CAN 0.0 0 24 Feb 2014 C ASC 970082 ASC 8B Maximum Gross Weight Airframe 75.000 Pounds To meet intent of this revision arc that previously cAv ASC 0081008A replace AFMS G550.2003-01 date 8.14-2003 with the AFMS in section II. OPT 26 Oct 2011 ASC Airframe 970090 ASC 9 MAX ZERO FUEL GROSS WGT Eff. Desc: ALL G550 AIRCRAFT. Cancelled see ASC 009B 11 CAN CPN GAC APPLETON FP549 CRS G1FR100Y 20.7 11 09 Apr 2008 C 11 0.00 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

L TYP Logbook Code aintenance Notes ASC Airframe Description Effectivity ATA Status C/W Source Work Order Cert No HRS LDG Date Cli MM REF M HRS 970091 ASC 9A Maximum Zero Fuel Gross Weight 53.500 Pounds - Placard Installation Mx. Notes: This code has been cancelled. This service change is applicable to all 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 11 CAN CAN 0.0 0 24 Feb 2014 C ASC Airframe ASC 98 Maximum Zero Fuel Gross 970092 Weight 53,500 Pounds • Placard Installation OPT ASC Airframe 970110 ASC II G550 DATA PLATE INSTALL Eff. " Dose. 5001-5999. 00 OPT Converts GVSP to G550. "Record ASC" ASC 970140 ASC 14 Category II Annunciation - Airframe Activation Mx. Notes: This code has been cancelled. cancelled see ASC 14A 34 CAN CAN ASC Airframe 970141 ASC I4A Category II Annunciation - Activation This ASC replaces 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 34 OPT 09 May 2011 I 01 Sep 2003 I 0.0 0 24 Feb 2014 C 13 Jun 2011 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 Logbook li Code Description Effectivity ATA Status C/W Source HRS LDG Date C/I MM REF M HRS Work Order aintenance Notes Cert No ASC 970330 ASC 33 BONDED HONEYCOMB Airframe PANELS Eff. Dose: ALL G550 AIRCRAFT. This is a record only ASC which incorporates drawing 1159SB50006 honeycomb floor panel repair-optional. 53 OPT 05 Dec 2003 I ASC ABC 35A (Part I) EASA / JAA Con - 970351 Supersedes ASC 035 Airframe Basic Requirements OPT C GAMA M F090550 564.2 191 02 Jun 2009 C 0.00 ASC ASC 35A (Part 2) EASA / JAA Con - 970352 Supersedes ASC 035 Airframe Basic Requirements OPT C GAMA M F090550 564.2 191 02 Jun 2009 C 0.00 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 Airframe 970461 ASC 46A Navigation Position Lights - LED Navigation Light Installation This revision removes 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. 33 OPT PIE 31 May 2011 ASC 970470 ASC 47 WATER SYSTEM EFFECTIVITY: 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. 38 OPT PIE 0.0 0 26 Nov 2007 C 0.00 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

L TYP Logbook Code Description Effectivity aintenance Notes ASC Airframe 970490 ASC 49 Lightning Sensor System (LSS) Installation This Service Change 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 970530 ASC 53 Comm Management Fnc Airframe Arinc Direct-Datalink Mx. Notes: This code has been cancelled. EFF: 5001 and Sub. cancelled ref ASC 53A ASC Airframe 970531 ASC 53A Communications Management Function ARINC Direct Datalink Service Provider 5001 and sub. AIC which have previously cAv ASC 53 should signet( this ASC as previously complied with. ASC Airframe 970550 ASC 55 WaterMaste Sys Component Eff: Part 1 is applicable Replacement Part 1 to SN# 5001-5099 only. Pan 2. 3. 4 and 5 are applicable to SN# 5001-5084 only. ASC Airframe 970551 ASC 55 WaterMaste Sys Component Eff: Part 1 is applicable Replacement Part 2 to SN# 5001-5099 only. Pan 2. 3. 4 and 5 are applicable to SN# 5001-5084 only. ASC Airframe 970552 ASC 55 WaterMaste Sys Component Eff: Part 1 is applicable Replacement Part 3 to SN# 5001-5099 only. Pan 2. 3. 4 and 5 are applicable to SN# 5001-5084 only. ASC Airframe 970553 ASC 55 WaterMaste Sys Component Eff: Part 1 is applicable Replacement Part 4 to SN# 5001-5099 only. Pan 2. 3. 4 and 5 are applicable to SN# 5001-5084 only. ATA Status C/W Source HRS LDG Date Cli MM REF M HRS Work Order Cert No 34 OPT gs appleton CPN 21.8 12 30 Apr 2008 C 0.00 23 CAN CAN 0.0 0 24 Feb 2014 C OPT 05 Dec 2011 38 OPT PIE 0.0 0 26 Nov 2007 C 0.00 38 OPT PIE 0.0 0 26 Nov 2007 C 0.00 38 OPT PIE 0.0 0 26 Nov 2007 C 0.00 38 OPT PIE 0.0 0 26 Nov 2007 C 0.00 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

L TYP Logbook Code Description Effectivity aintenance Notes ASC Airframe 970554 ASC 55 Water'Waste Sys Component Eff: Part 1 is applicable Replacement Part 5 to SN# 5001.5099 only. Pan 2. 3. 4 and 5 are applicable to SW/ 5001.5084 only. ASC Airframe 970571 ASC 57A • Electrical Lines-Contact Prevention (CB 32 Aml) EFF: 5001.5149 - Ref CB 32 Am 1 - Aircraft having previously complied with ASC 057 meet the intent of this revision. ASC Airframe 970610 ASC 61 Synthetic Vision-Primary Flight Display (SV-PFD) Installation Mx. Notes: This code has been cancelled. ASC 907 - PlaneView@ Master Operating Software Update (SV-PFD) is required for aircraft serial numbers 5001 - 5188. Superceded see ASC 6IA ATA Status C/W Source HRS LDG Date Cli MM REF M HRS Work Order Cert No 38 OPT PIE 0.0 0 26 Nov 2007 C 0.00 24 MAN P/E 03 Sep 2008 I 31 CAN CAN 0.0 0 24 Feb 2014 C ASC ASC 61 Aml- Synthetic Vision Airframe 970611 Primary Flight Display (SV-PF) Mx. Notes: This code has been cancelled. This service change 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 CAN CAN 0.0 0 24 Feb 2014 C 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

il TYP Logbook Code aintenance Notes ASC Airframe Description Effectivity ATA Status CNV Source Work Order Cert No HRS LOG Date CA MM REF M HRS 970612 ASC 61A Synthetic Vision•Primary Flight Display (SV•PFD) Installation Mx. Notes: This code has been cancelled. This service change 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) CAN CAN 0.0 0 24 Feb 2014 C ASC 970613 ASC 61A Amt Synthetic Vision • Aiiirame Primary Fight Display (SV•PFD) Installation Mx. Notes: This code has been cancelled. This service change amendment is for 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. CAN CAN 0.0 0 24 Feb 2014 C G-CGUL G550 5176 Technical Bulletins Page 63 of 164 20 Jan 2015 O2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620853

TYP Logbook li Code Description Effectivity ATA Status C/W Source HRS LDG Date C/I MM REF M HRS Work Order aintenance Notes Cert No ASC Airframe 970614 ASC 618 Synthetic Vision.Primary Flight Display (SV-PFD) Installation This service change 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'. 31 OPT 31 Oct 2011 ASC Airframe 970630 ASC 63 Wing Fuel Transfer Sys Mid- EFF: 5001and Sub. Wing Ejector Mod Ths ASC cancelled see 63A 57 CAN ASC Airframe EFF: 5001and Sub.Cancelled by ASC 0638 Mx. Notes: This code has been cancelled. See Compliance Remarks by cricking Show Remarks link. 970631 57 CAN ASC 63A Wing Fuel Transfer Sys Mid-Wing Ejector Mod Part 1 ASC Airframe 970632 ASC 63A Wing Fuel Transfer Sys Mid-Wing Ejector Mod Part 2 EFF: 5001 and Sub. Cancelled by ASC 0638 57 CAN Mx. Notes: This code has been cancelled. See Compliance Remarks by cricking Show Remarks link. ASC 970633 ASC 638 Wing Fuel Transfer Sys Effectivity: 5001 and Airframe Mid-Wing Ejector Mod Part 1 Sub. 57 OPT ASC ASC 638 Wing Fuel Transfer Sys Effectivity: 5001 and 970634 Airframe Mid-Wing Ejector Mod Part 2 Sub. 57 OPT ASC 970635 ASC 638 Wing Fuel Transfer Sys Effectivity: 5001 and Airframe Mid-Wing Ejector Mod Part 3 Sub. 57 OPT CAN 0.0 0 26 Nov 2007 C 0.00 CAN 0.0 0 01 Apr 2013 C 0.00 CAN 0.0 0 01 Apr 2013 C 0.00 29 Mar 2013 I 29 Mar 2013 29 Mar 2013 I 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

L TYP Logbook Code Description Effectivity ATA Status C/W Source HRS LDG Date Cli MM REF M HRS Work Order aintenance Notes Cert No ASC 970650 Airframe ASC 65 Runway Awareness Advisory EFF: Acft Serial System (RAAS)•Installation Number 5001 and Sub. 34 CAN CAN 0.0 0 26 Nov 2007 C 0.00 ASC 970651 Airframe ASC 65A Runway Awareness This ASC supercedes Advisory System-Installation ASC 65 34 OPT 07 Mar 2008 I ASC 970660 Airframe ASC 66 Auxiliary Power Unit (APLI) Effectivity: SIN 5001- Bond Strap Installation 51591 This or a similar change will be installed in production on aircraft. serial number 5160 and subsequent / Concurrent Requirement: G550 Customer Bulletin 65 49 MAN PIE 07 Apr 2008 I ASC 970691 Airframe ASC 69A Engine Electronic Controller Supercedes ASC 69. (EEC) Upgrade to V1.3/ EECU3000 incorporates SB- BR700.73-101496 Rev 1. Effectivity 5001- 5151. 73 OPT PIE 30 Jul 2008 ASC 970692 Airframe ASC 69A Am1 Engine Electronic The purpose of this 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 73 INF PIE 21 Jan 2009 ASC 970700 Airframe ASC 70 Nose Landing Gear Door EFF: G550 aircraft, Actuator Modification serial numbers 5001- 518711 NOTE: Mandatory for SIN 5001 - 5177 per CB 58 issued 12/10/2007 32 MAN CM GAC APPLETON FP549 CRS G1FR100Y 20.7 II 09 Apr 2008 C 0.00 ASC 970710 Airframe ASC 71 Micro Quick Access Recorder Cancelled see ASC Installation 071A 31 CAN CM GALLTN FL012134 602.6 199 30 Jun 2009 C 0.00 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

Airframe TYP Logbook li Code Description Effectivity ATA Status C/W Source HRS LDG Date C/I MM REF M HRS Work Order aintenance Notes Cert No ASC 970711 ASC 71A Micro Quick Access Airframe Recorder Installation ASC 970720 ASC 72 Medeco Door Locks Airframe Installation Effectivity 5001.5204 ASC 970730 ASC 73 Nose Gear Uplock Hook Airframe Spring Replacement Mx. Notes: This code has been cancelled. Concurrent requirement = CB 69. SiN 5001.5204. ASC 970731 ASC 73A Nose Gear Uplock Hook Concurrent Spring Replacement Requirement: G550 Customer Bulletin 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. 31 OPT PIE 19 Aug 2013 I 52 OPT 20 May 2008 I 32 CAN CAN 0.0 0 24 Feb 2014 C 32 MAN CPN Jet Aviation Geneva GVBTC003 513.0 177 03 Feb 2009 C 0.00 ASC 970740 ASC 74 Dual Brake Metering Valve Airframe Replacement 32 CAN CAN 19 Nov 2008 I 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 Logbook li Code Description Effectivity ATA Status C/W Source HRS LDG Date C/I MM REF M HRS Work Order aintenance Notes Cert No ASC Airframe 970741 ASC 74A Dual Brake Metering Valve Replacement This service change 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. 32 OPT 23 Jan 2009 I ASC Airframe 970742 ASC 74A AM1 Dual Brake Metering Valve Replacement This service change amendment corrects the 24 month warranty compliance statement in ASC 074A. OPT 22 Nov 2010 I ASC 970750 ASC 75 - LED Tail Position Light Airframe Installation Mx. Notes: Superceded by ASC 075A Effectivity: SIN 5001 - 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 33 CAN CAN 2332.2 708 25 Feb 2012 C 0.00 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

L TYP Logbook Code aintenance Notes ASC Airframe Description Effectivity ATA Status C/W Source Work Order Cert No HRS LDG Date Cli MM REF M HRS 970751 ASC 75A - LED Tail Position Light Installation Mx. Notes: See WP FL016369 GiStream Luton for details Effectivity: SIN 5001 -5181. Aircraft operators who have previously complied with ASC 075 should verity proper orientation of the light assembly in accordance with Figure 1. 33 OPT CM 2332.2 708 25 Feb 2012 C 0.00 ASC 970760 ASC 76 PlaneView Avionics Airframe Enhancement (SV-PFD) Elf 5001.5188 31 OPT 15 Sep 2008 I ASC 970761 ASC 76 Am1 PlaneView Avionics Airframe Enhancement (SV-PFD) This amendment is for information only. and restricts the ASC installation to Gulfstream or GDAS facilities. The EASA project number also has been amended. 31 INF 19 Dec 2008 I ASC Airframe 970770 ASC 77 - Decal Installation Remote See 970771 // 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 12 CAN CM 1787.4 543 08 Mar 2011 C 0.00 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 Code Logbook 'Maintenance Notes Description Effectivity IATAI Status CNV Source Work Order Cert No HRS LOG Date cn MM REF M HRS ASC 970771 ASC 77A • Decal Installation- Airframe Remote Oil Servicing Panel Effectivity: This 12 OPT 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 Airframe ASC 78 Potable Water System Purge. SiN 5001.5192 970780 Plackard excluding 5014,5037,5044,5069, 5132,5188,5189,5191. Concurrent requirement CB 71. ASC ASC 79 Main landing Gear 970790 Emergency Line Modification Airframe Concurrent Requirement: 6550 Customer Bulletin Number 72 04 Nov 2011 38 MAN Cm Jet Aviation Geneva GVBTC003 513.0 177 03 Feb 2009 C 0.00 32 MAN CM Jet Aviation Geneva GVBTC003 513.0 177 03 Feb 2009 C 0.00 G-CGUL G550 5176 Technical Bulletins Page 69 of 164 20 Jan 2015 O2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620859

il TYP Logbook Code aintenance Notes ASC Airframe Description Effectivity ATA Status CNV Source Work Order Cert No HRS LOG Date CA MM REF M HRS 970800 ASC 80 Modification - Wing Rear Beam • Flight Spoiler Actuator Attachment Point Concurrent Reqmt:CB 83. This ASC is 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 57 REQ CNJ 1787.4 543 08 Mar 2011 C 0.00 ASC 970801 ASC 80 AM1 Meditation - Wing This service change is 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 57 INF Cm 1787.4 543 08 Mar 2011 C 0.00 G-CGUL G550 5176 Technical Bulletins Page 70 of 164 20 Jan 2015 O2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620860

il TYP Logbook Code Description Effectivity ATA Status CNV Source HRS LOG Date CA MM REF M HRS Work Order 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 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620861

il TYP Logbook Code aintenance Notes ASC Airframe Description Effectivity ATA Status CNV Source Work Order Cart No HRS LDG Date CA MM REF M HRS 970822 ASC 82A AM1 Tail Compartment Ladder • Hinge Pin and Placard Mx. Notes: CM AS ASC082A ALREADY CM. This service change is LTN INF CM 778.0 262 30 Oct 2009 C 0.00 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. ASC ASC 83 PlaneView Avionics 970830 Airframe Enhancement (Cart Fox) This service change is applicable to aircraft serial numbers 5001 - 5274. Cancelled ref ASC 83A ASC 970831 ASC 83A PlaneView Avionics Airframe Enhancement (Cart Fox) Mx. Notes: See FL016471 I FL016474 This service change 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. CAN CAN 0.0 0 28 Sep 2010 C 0.00 OPT CM 2354.3 711 19 Apr 2012 C 0.00 ASC This service change is 970840 ASC 84 Enhanced Navigation 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. CAN CAN 0.0 0 24 Feb 2014 C G-CGUL G550 5176 Technical Bulletins Page 72 of 164 20 Jan 2015 O2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620862

il TYP Logbook Code aintenance Notes ASC Airframe Description Effectivity ATA Status CNV Source Work Order Cert No HRS LOG Date CA MM REF M HRS 970841 ASC 84A Enhanced Navigation Mx. Notes: This code has been cancelled. Prerequisites: G550 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. CAN CAN 0.0 0 24 Feb 2014 C ASC 970842 ASC 848 Enhanced Navigation Airframe This service change 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. 34 OPT 22 Dec 2011 G-CGUL G550 5176 Technical Bulletins Page 73 of 164 20 Jan 2015 O2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620863

L TYP Logbook Code aintenance Notes ASC Airframe Description Effectivity ATA Status C/W Source Work Order Cert No HRS LDG Date Cr' MM REF M HRS 970850 ASC 85 XM Weather Installation Mx. Notes: This code has been cancelled. Prerequisites: G550 ASC 908 - PlaneView Master Operating Software System Software Update (Cert Fox) Cancelled ref ASC 85A CAN CAN 0.0 0 24 Feb 2014 C ASC Airframe 970851 ASC 85A XM Weather Installation This service change 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) OPT 19 Aug 2010 I ASC 970860 ASC 86 Entrained Air Removal Airframe System Installation This service change is applicable to aircraft serial numbers 5001-5102. OPT PIE ASC 970870 ASC 87 Canadian Certification Airframe Requirements OPT 07 Jul 2010 ASC 970890 ASC 89 Stage 4 Noise Standards - Cancelled see ASC Airframe Certification 089A. Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link. CAN CAN 0.0 0 20 Aug 2013 C 0.00 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 Logbook Ilaintenance Notes Code Description Effectivity ASC 970891 ASC 89A Stage 4 Noise Standards • Airframe Certification ASC Airframe 970900 ASC 90 Auxiliary Power Unit (APU) This service change is Enclosure Thermal Barrier applicable to aircraft Installation serial numbers 5001.5249, excluding 5211 and 5225. Cancelled see ASC 90A ASC Airframe 970901 ASC 90 AM1 Auxiliary Power Unit This service change (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 ATA Status CNV Source HRS LOG Date CA MM REF M HRS Work Order Cert No OPT P/E 20 Aug 2013 I CAN CAN 0.0 0 06 Sep 2011 C 0.00 CAN CAN 0.0 0 06 Sep 2011 C 0.00 ASC Airframe 970902 ASC 90A Auxiliary Power Unit (APU) This revision 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. OPT 10 Feb 2011 I G-CGUL G550 5176 Technical Bulletins Page 75 of 164 20 Jan 2015 O2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620865

il TYP Logbook Code aintenance Notes ASC Airframe Description Effectivity ATA Status CNV Source Work Order Cert No HRS LOG Date CA MM REF M HRS 970910 ASC 91 Enhanced Baggage Door Seal System • Installation Mx. Notes: This code has been cancelled. This service change is applicable to G550 aircraft, serial numbers 5001 • subsequent CAN CAN 0.0 0 24 Feb 2014 C ASC Airframe 970911 ASC 91A Enhanced Baggage Door Seal System • Installation This service change is 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." 52 OPT 01 Nov 2011 ASC Akirame 970920 ASC 92 Communication Management Concurrent Req:To Function (CMF) Satcom Direct • activate the datalink 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 [email protected] 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. 23 OPT CM GAC LTN LMX000417 UK.145.00883 2692.3 796 12 Jan 2013 C G-CGUL G550 5176 Technical Bulletins Page 76 of 164 20 Jan 2015 O2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620866

L TYP Logbook Code aintenance Notes ASC Airframe Description Effectivity ATA Status C/W Source Work Order Cert No GAC-LTN FL016471 HRS LDG Date Cli MM REF M HRS 970931 ASC 93A Aileron Cable Fairleads at Sponson Rib Installation This service change is applicable to aircraft 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. 27 OPT CM UK.145.00883 2354.6 711 19 Apr 2012 C ASC Airframe 970940 ASC 94 Landing Gear Door Close - Restrictor 5001.5314. Concurrent requirement CB 110. Cancelled see ASC 094A CAN CAN 0.0 0 28 Jun 2011 C 0.00 ASC Airframe 970941 ASC 94A Landing Gear Door Close Restrictor Mx. Notes: This code has been cancelled. 5001.5314. Concurrent requirement CB 110A. Cancelled see ASC 948 CAN CAN 0.0 0 24 Feb 2014 C ASC Airframe 970942 Aircraft operators who have previously 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 ASC 94B Landing Gear Door Close - Restrictor GAC LTN OPT CAN 2849.4 833 09 Apr 2013 C BMX000145 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

il TYP Logbook Code aintenance Notes ASC 970950 ASC 95 • PlaneView Avionics Effectivity: This 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 Description Effectivity ATA Status CNV Source Work Order Cert No HRS LOG Date C/I MM REF M HRS 31 CAN CAN 0.0 0 25 Apr 2013 C 0.00 ASC 970952 ASC 95B • PlaneView Avionics Effectivity: 5001 - 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. 31 OPT 24 Apr 2013 I ASC 970960 ASC 96 - CPDLC - FANS 1/A Airframe This service change 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. 23 OPT 22 Dec 2011 G-CGUL G550 5176 Technical Bulletins Page 78 of 164 20 Jan 2015 O2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620868

TYP Logbook li Code Description Effectivity ATA Status C/W Source HRS LDG Date C/I MM REF M HRS Work Order aintenance Notes Cert No ASC 970970 ASC 97 - Data Link Recording Airframe Effectivity This service change is applicable to aircraft serial numbers 5309 and subsequent. 31 CAN PIE 22 Dec 2011 ASC 970971 ASC 97A - Data Link Recording Airframe Effectivity: This service change is applicable to aircraft serial numbers 5309 5374. 31 OPT PIE 30 Aug 2012 ASC Airframe 970981 ASC 98 - Retract Braking (Main Wheel De-spin) Brake Metering Valve Upgrade and Hydraulic Flow Control Restrictor Replacement "record only ASC" OPT PIE 18 Mar 2013 I ASC Airframe 970990 ASC 99 - Aileron And Elevator Power Disconnect - Removal This service change is applicable to aircraft serial numbers 5001- 5389. Concurrent Requirement - CB 125. Cancelled see 970991 27 CAN CAN Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link. 0.0 0 01 Apr 2013 C 0.00 ASC 970991 ASC 99A - Aileron And Elevator Airframe Power Disconnect Removal This service change is applicable to aircraft serial numbers 5001- 5389. Concurrent Requirement - CB 125A. OPT CPN GAC LTN 2849.4 833 04 Apr 2013 C BMX000145 UK.145.00883 ASC Airframe 971020 ASC 102 60 Hz Power Generation - 60 Hz Converter Equipment Modification Effectivity: This service change is applicable to aircraft serial numbers 5001.5068. excluding 5003. This or a similar change is installed in production on aircraft serial number 5069 and subsequent. 24 OPT 15 Apr 2014 I ASC 971030 ASC 103 TCAS 7.1 Installation Airframe 5001.5379 OPT 12 Jun 2012 ASC Airframe 971040 ASC 104 Aileron Cade Penetrations at FS 576.5 Floor Beam - Rework This ASC is applicable to aircraft serial numbers 5001- 5404. OPT CPN GAC LTN 2849.4 833 11 Apr 2013 C BMX000145 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

il TYP Logbook Code Description Effectivity ATA Status CNV Source HRS LOG Date CA MM REF M HRS Work Order aintenance Notes Cert No ASC Airframe 971050 ASC 105 • Automatic Dependent Surveillance - Broadcast (ADS-B) Out Installation Effectivity: 5001 - Sub. Prerequisites ASC 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. 34 OPT 24 Apr 2013 I ASC Airframe 971051 ASC 105A • Automatic Dependent Surveillance - Broadcast (ADS-B) Out Installation Effectivity: This service change is applicable to aircraft serial numbers 5001 — subsequent. 34 OPT 25 Jul 2014 ASC Airframe 971060 ASC 106 Fuel Quantity Signal Conditioner - Revision G Software 5001-5409, excluding arc with ASC 63 OPT 08 Feb 2013 I ASC Airframe 971070 ASC 107 • Planeview Avionics Enhancement Effectivity: 5001 - 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. 31 OPT 24 Apr 2013 ASC Airframe 971080 ASC 108 • APU Enclosure Non- Compliant Sealant - Modification Effectivity: This service change is applicable to aircraft serial numbers 5001.5249, excluding 5011, 5225 and 5245. 53 OPT 30 Jul 2014 ASC Airframe 971100 ASC 110 Cockpit Portable Fire Extinguisher • Relocation 5072.5411 CAN CAN 0.0 0 02 Oct 2013 C 0.00 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 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620870

il TYP Logbook Code aintenance Notes ASC Airframe Description Effectivity ATA Status CNV Source Work Order Cert No HRS LOG Date CA MM REF M HRS 971101 ASC 110A (Part 1) Cockpit Portable Fire Extinguisher / Pilot Seat Track Stop - Relocation This ASC is separated into 2 parts. Part I (code 971101), applicable to aircraft serial numbers 5072- 5411. Part II (code 971102), applicable to aircraft serial numbers 5412-5438. OPT 01 Oct 2013 ASC Airframe 971102 ASC 110A (Part 2) Cockpit Portable Fire Extinguisher! Pilot Seat Track Stop - Relocation This ASC is separated into 2 parts. Part I (code 971101), applicable to aircraft serial numbers 5072- 5411. Part II (code 971102), applicable to aircraft serial numbers 5412-5438. OPT PIE 01 Oct 2013 ASC 971110 ASC 111 • Mandates Package Effectivity: Aircraft 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 23 CAN CAN 0.0 0 29 Jul 2014 C 0.00 ASC Airframe 971111 ASC 111A • Communication Navigation (ATA 23 / 34) Mandates Package (CPDLC ADS-B Out) Effectivity: This service change is applicable to aircraft serial numbers 5001 and subsequent. 23 OPT 25 Jul 2014 ASC Airframe 971120 ASC 112 Elevator Hardover Prevention System (HOPS) • Improvement Concurrent GAO LTN OPT CNV 3444.5 949 04 Nov 2014 C 0.00 Requirement G550 BMX000542 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 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620871

il TYP Logbook Code aintenance Notes ASC ASC 113 • Planeview Avionics Effectivity: This service 971130 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 Description Effectivity ATA Status CNV Source Work Order Cert No HRS LOG Date CA MM REF M HRS 31 CAN CAN 0.0 0 18 Sep 2014 C 0.00 ASC 971131 ASC 113A • Planeview Avionics Effectivity: This service 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. 31 OPT 17 Sep 2014 ASC Airframe 971141 ASC 114A • Automatic Dependent Effectivity: This service 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. 34 OPT PIE 25 Jul 2014 ASC Airframe 971160 ASC 116 • Nose Landing Gear (NLG) Effectivity: This Harness • Installation service change is applicable to aircraft serial numbers 5001. 5424. 32 OPT 27 Jun 2014 G-CGUL G550 5176 Technical Bulletins Page 82 of 164 20 Jan 2015 O2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620872

L TYP Logbook Code Description Effectivity aintenance Notes ASC Airframe 971200 ASC 120 - Engine Driven Pump (EDP) Case Drain Hose Routing In Left Pylon Effectivity: This service change is applicable to aircraft serial numbers 5001.5494. This or a similar change will be installed during initial phase manufacturing on aircraft. serial number 5495 and subsequent. ASC 979000 ASC 900 PLANEVIEW MOS UPDATE Eff. Dose: 5001.5029. Airframe ASC 979030 ASC 903 PLANEVIEW MOS UPDATE EFF:500I -5077 Airframe ASC ASC 907 PlaneView Master Operating 979070 Eft 5001.5188 Airframe System Software Update (SV-PFD) ASC Airframe 979071 ASC 907 Am1 PlaneView Master Operating System Software Update (S This amendment is for information only. and restricts the ASC installation to Gulfstream or GDAS facilities. The EASA project number also has been amended. ATA Status C/W Source HRS LDG Date Cli MM REF M HRS Work Order Cert No 29 OPT GAC LTN CM BMX000542 UK.145.00883 3444.5 949 23 Oct 2014 C 31 OPT PIE 0.0 0 26 Nov 2007 C 0.00 31 OPT PIE 0.0 0 26 Nov 2007 C 0.00 31 OPT 15 Sep 2008 I 31 OPT 19 Dec 2008 I 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

il TYP Logbook Code Description Effectivity ATA Status CNV Source HRS LOG Date CA MM REF M HRS Work Order 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 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620874

il TYP Logbook Code aintenance Notes ASC 979090 ASC 909 • PlaneView Master Effectivity: This service 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 Description Effectivity ATA Status CNV Source Work Order Cert No HRS LOG Date C/I MM REF M HRS 31 CAN CAN 0.0 0 25 Apr 2013 C 0.00 ASC Aidrame 979092 ASC 9098 • PlaneView Master Operating System Software Update Effectivity: Serial 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. 31 OPT 24 Apr 2013 I ASC Airframe 979100 ASC 910 • PlaneView Master Operating System Software Update Effectivity: 5001 • 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. 31 OPT 24 Apr 2013 G-CGUL G550 5176 Technical Bulletins Page 85 of 164 20 Jan 2015 O2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620875

L TYP Logbook Code aintenance Notes ASC 979110 ASC 911 - PlaneView Master Effectivity: This service 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 Airframe 979111 ASC 911A • PlaneView Master Operating System Software Update Effectivity: This service 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. 31 OPT 17 Sep 2014 I CB Airframe 980010 CB 1 FIRE DETECT BOX MOUNTING Eff. Desc: 5001.5032. 26 MAN N/A 12 Mar 2004 I 26.15-01 CB Airframe 980020 CB 2 LUBE HORIZ STAB TRIGGER Eff. Desc: 5001.5042. 27 MAN N/A 26 May 2004 I 27-42-01 CB Airframe 980030 CB 3 PT1 WING VORTEX GENS/RIB Eff. Desc: 5001.5051. 57 MAN N/A 05 Aug 2004 I ASC 39 CB Airframe 980031 CB 3 PT2 WING VORTEX GENS/RIB Eff. Desc: 5001.5051. 57 MAN N/A 05 Aug 2004 I ASC 39 CB Airframe 980040 CB 4 AILELEV ACT DAMPER SHAFT Eff. Desc: 5001.5052. 27 MAN N/A 23 Aug 2004 I CB Airframe 980050 CB 5 PDB TERMINAL OVER TORQUE Eff. Desc: 5001.5034. 24 MAN N/A 26 Oct 2004 I ASC41 CB Airframe 980060 CB 6 AILELEV ACT RETROFIT 27 Eff. Desc: ALL G550 ACFT. MAN N/A 0.0 0 26 Nov 2007 C 0.00 Description Effectivity ATA Status C/W Source Work Order Cert No HRS LDG Date Cli MM REF M HRS 31 CAN CAN 0.0 0 18 Sep 2014 C 0.00 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

L TYP Logbook Code Description Effectivity aintenance Notes CB Airframe 980070 CB 7 ELECT DISC BRACKET Eft. Giese: 5001-5042 (12 MOS). CB CB 8 TAIL COMPARTMENT Ell. Desc: 5001-5063 980080 Airframe LADDER (12 MOS). CB . Eff Desc: 5002-5015' 980090 CB 9 RIGHT EER MODIFICATION Airframe EX 5014. CB CB 9A RIGHT ELECTRICAL EQUIP Applies to 5002-5015 980091 Airframe RACK MOD & 5020. CB 980100 CB 10 FLAP LEAD EDGE RIVETS Eft. Giese: 5001-5069. Airframe CB 980110 CB 11 OUTBRD FIX TE RIVETS Eft. Desc: 5001-5051. Airframe CB Airframe 980120 CB 12 WING ANTI-ICE EXHAUST LOUVERS INSP Eft. Dose: 5001- 5005.5008-5024.5026- 5030.5035-5037.5039 & 5044. CB CB 13 PART I FLIGHT CONTROL Effectivity: 5001-5036 980130 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. ATA Status C/W Source HRS LDG Date Cli MM REF M HRS Work Order Cert No 24 MAN N/A 07 Jan 2005 I 25 MAN N/A 07 Jan 2005 25 MAN N/A 20 Jan 2005 I 25 MAN N/A II Feb 2005 I 27 MAN N/A 24 Jan 2005 I 57 MAN N/A 24 Jan 2005 30 MAN N/A 16 Mar 2005 I 31 MAN N/A 22 Mar 2005 I CB Airframe 980131 CB 13 PART 2 FLIGHT CONTROL Effectivity: 5001-5036 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. 31 MAN N/A 22 Mar 2005 I 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 Logbook li Code Description Effectivity ATA Status C/W Source HRS LDG Date C/I MM REF M HRS Work Order aintenance Notes Cert No CB Airframe 980140 CB 14 AILERON FORCE LINK ASSY WIRING-INSP EFF:5001.5072. WING SN 678.767. ONE TIME INSP DUE 12 MOS AFT ISSUE DATE OF THIS BULLETIN AND INCORPORATES VOUGHT SB VAIGV/GVSP-27- PG0098. 27 MAN N/A 23 Jun 2005 I CB Airframe 980151 CB 15A NLG ACTUATOR ROD END INSP EFF:5001-5084. ONE TIME INSP DUE WITHIN 12 MOS OF ISSUE DATE. 32 MAN N/A 21 Nov 2005 I CB Airframe 980160 CB 16 LEFT AND RIGHT STRNG 6 AT FS 955.974 EFF:5001.5047 53 MAN N/A 05 Aug 2005 I CB Airframe 980170 CB 17 INSP. ANTI-SKID CONTROL UNIT EFF: 5044 THRU 5063. TO BE ACCOMPLISHED WITHIN THE NEXT 60 DAYS. 32 MAN N/A 11 Aug 2005 I CB Airframe 980180 CB 18 MODIFICATION-VACUUM TOILET STATUS PANEL EFF: 5001.5059 38 MAN N/A 18 Aug 2005 I CB Airframe 980190 CB 19 INSP/SEALING - OUTBOARD WING RIB REPAIR EFF:5001.5051 TO BE ACCOMPLISHED WITHIN 12 MONTHS OF ISSUE DATE. 57 MAN N/A 18 Aug 2005 I CB Airframe 980200 CB 20 - PREMIUM PACKAGE WIRING HARNESS INSP EFFECTIVITY: SiN 5001.5047 excluding 5014. 5037 and 5044 - Compliance with this CB is to be accomplished within the next 24 Months. 23 MAN N/A 12 Oct 2005 I CB Airframe 980210 CB 21 PT1 INSPECT-FRAME AT FS.377 WITHIN 12 MOS 53 MAN N/A 02 Nov 2005 I CB Airframe 980211 CB 21 PT2 INSPECT-FRAME AT FS.377 WITHIN 12 MOS 53 MAN N/A 02 Nov 2005 I 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 Logbook li Code Description Effectivity ATA Status C/W Source HRS LDG Date C/I MM REF M HRS Work Order aintenance Notes Cert No CB Airframe 980220 CB 22 - NLG DOWNLOCK HARNESS EFFECTIVITY: SiN CONN HDWARE 5001.5094 - ACCOMPLISH WITHIN 150 FLIGHT HOURS 32 MAN N/A 07 Dec 2005 I CB Airframe 980230 CB 23- EMERGENCY PRESSURE TRANSDUCER DECALS. INSP EFF: 5001 THRU 5073. 5077. 5078. 5082. 5083. 5086. AND 5089 EXCLUDING 5014 AND 5037. ACCOMPLISH WITHIN 24 MOS OF ISSUE. 32 MAN N/A 08 Dec 2005 I CB Airframe 980240 CB 24 INSTALL - OXYGEN BOTTLE PHYSICAL BARRIER EFFECTIVITY: 5001- 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. 35 MAN N/A 20 Dec 2005 I CB Airframe 980250 CB 25 - INSP TAIL ANTI-COLL STROBE LT EFFECTIVITY: SiN 5027 - 507911 COMPLIANCE: Compliance with this CB is to be accomplished at the next "Ar check. not to exceed 500 Flight Hours. 33 MAN N/A 11 Jan 2006 CB Airframe 980261 CB 26A MOD-MAIN LANDING GEAR DOORS EFF:5001.5109. COMPLIANCE WITH THIS CUSTOMER BULLETIN REVISION IS TO BE ACCOMPLISHED WITHIN 6 MONTHS. THIS IS A ONE TIME COMPLIANCE. 32 MAN N/A 21 Feb 2006 I 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

il TYP Logbook Code Description Effectivity ATA Status CNV Source HRS LOG Date CA MM REF M HRS Work Order aintenance Notes Cert No CB Airframe 980270 CB 27 REPLACEMENT- AILERON/ELEVATOR ACT LOAD RELIEF BUNGEES EFF:5001.5093. THIS IS A ONE TIME 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. 27 MAN N/A 10 Mar 2006 I CB Airframe 980271 CB 27 AM1 Replace-Aileron / Elevator Act Load Relief Bungees This is a "ONE TIME" 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. 27 MAN N/A 22 Jun 2006 I CB Airframe 980280 CB 28 Lancing Gear Bungee Lube and Rigging-Insp EFF: 5001.5107. THIS IS A ONE TIME INSP. COMPLIANCE WITH THIS CB IS TO BE ACCOMPLISHED WITHIN THE NEXT 6 MONTHS. 32 MAN N/A 30 Mar 2006 I CB Airframe 980290 CB 29 AFT. Emerg Lighting Battery Mount Tray-Mod EFF: G550 SN 5001- 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. 33 MAN N/A 15 May 2006 I G-CGUL G550 5176 Technical Bulletins Page 90 of 164 20 Jan 2015 O2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620880

TYP Code Logbook Ilaintenance Notes CB 980300 Airframe Description Effectivity CB 30 Decompression Vent Panels- insp EFF: G550 5020 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 980310 Airframe Power Supply Connector Due within 12 Mos. EH 5001 thru 5101. excluding 5014.5037,5044,5078, 5083 thru 5092.5094,5095 and 5097 thru 5100. CB CB 32 Electrical Lines Contact 980320 Airframe Prevention-Mod (ASC 57) EFF: 5001.5090, 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 Airframe 980321 CB 32 Aml - Electrical Lines Contact EFF: 5091 -5149- 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 980330 Airframe Window Bonding Strap-Mod EH: 5001 through 5126 "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. IATAI Status CNV Source HRS LOG Date CA MM REF M HRS Work Order Cert No 53 MAN NIA 18 May 2006 31 MAN N/A 25 May 2006 I 24 MAN N A 28 Jun 2006 I 24 MAN N/A 03 Sep 2008 I 34 MAN N/A 17 Jul 2006 G-CGUL G550 5176 Technical Bulletins Page 91 of 164 20 Jan 2015 O2015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620881

il TYP Logbook Code Description Effectivity aintenance Notes CB Airframe 980340 CB 34 Oxy Line Support at F.S. 241• Installation Eff: NC SNif 5002• 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 980350 CB 35 Rudder Stop Botts-Insp Airframe EFF: For NC Serial numbers 5001.5112. This is a 'one time' insp to be accomplished within the next 12 months. CB Airframe 980360 CB 36 Right Pylon Case Drain Line Routing•Mod EFF: G550 5001 through 5121. This custome bulletin is a "One Time" action to be accomplished within the next 12 months. CB 980370 CB 37 (Part I) BBML Operational Airframe Limitation Placard-Insp This is a 2 part Bulletin 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. ATA Status CNV Source HRS LOG Date CA MM REF M HRS Work Order Cert No 35 MAN N/A 03 Aug 2006 I 27 MAN N/A 31 Aug 2006 I 29 MAN N/A 01 Sep 2006 I 11 MAN N/A 25 Sep 2006 I G-CGUL G550 5176 Technical Bulletins Page 92 of 164 20 Jan 2015 02015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620882

il TYP Logbook Code aintenance Notes CB Airframe Description Effectivity ATA Status CNV Source Work Order Cert No HRS LOG Date CA MM REF M HRS 980371 CB 37 (Part 2) BBML Operational limitation Placard-Insp This is a 2 part Bulletin to be accomplished within the next 45 days. Part 1 is a One Time Action, Part 2 if required, ensures incorp of Drawing 11 MAN NIA 25 Sep 2006 I 1159S840091. EFF: SN 5043. 5046, 5053. 5061,5062, 5071, 5076, 5079, 5085, 5089, 5091, 5097, and 5101. CB Airframe 980380 CB 38 Auxiliary Hydraulic Boost Pump•Insp This is a One Time Action to be accomplished "No Later Than Jan 31. 2007. To ensure compliance with Meggitt Airdynamics SB 2006.01. Pump Sn range is 02590318. 29 MAN N/A 25 Sep 2006 I CB Airframe 980390 CB 39 NLG Trunnion PM (Right Side NOTE: EFF: WI Only) 5001 - 5123 II Compliance with this CB is to be accomplished within the next 12 months. 32 MAN N/A 10 Oct 2006 I CB Airframe 980400 CB 40 Mod-Seal Nose Gear Switch 5001.5154 32 MAN N/A 22 Dec 2006 I CB Airframe 980410 CB 41 Battery Chargers • Inspection This is a One Time inspection to ensure compliance with ELDEC SB 8.842.24• 01. Not to exceed 12 months. Accomplish before January 25, 24 MAN N/A 25 Jan 2007 I 2008. G-CGUL G550 5176 Technical Bulletins Page 93 of 164 20 Jan 2015 02015 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620883

L TYP Logbook Code Description Effectivity aintenance Notes CB Airframe 980420 CB 42 lnsp-Trim Valve Servo Pressure Supply Part 1 Part 1 to be 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 980421 CB 42 lnsp Trim Air Valve Servo Airframe Pressure Supply Part 2 Part 1 to be 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 980430 CB 43 lnsp. Water Level Sensor Airframe Harness Pan 1 EFF: 5001 through 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. ATA Status C/W Source HRS LDG Date Cli MM REF M HRS Work Order Cert No 21 MAN N/A 29 Jan 2007 I 21 MAN N/A 29 Jan 2007 38 MAN N/A 14 Feb 2007 I CB 980431 CB 43 lnsp. Water Level Sensor Airframe Harness Pan 2 EFF: 5001 through 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. 38 MAN N/A 14 Feb 2007 I CB 980440 CB 44 Right Eng Integrated Drive Airframe Generator Cable Inst. Mod Effectivity: SIN 5001 through 5136 II This is a "One Time action to be accomplished with in the next 45 days 44 MAN N/A 0.0 0 05 May 2008 C 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

L TYP Logbook Code Description Effectivity ATA Status C/W Source HRS LDG Date Cli MM REF M HRS Work Order 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 980480 CB 48 Wiring Harness Installation Airframe AFT F.S. 660 EFF: SN 5029 through 5079 Excluding 5064. Compliance with this CB is to be accomplished with in 12 months of issue date (June 7. 2007). 24 MAN NIA 07 Jun 2007 I CB 980490 CB 49 Mod-Left And Right Power Airframe Distribution Box (PDB) Effectivity: SIN 5001 - 5150 II This is a 'One Time Action. To be accomplished with in the next 24 months. 24 MAN NIA 25 Jun 2007 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

L TYP Logbook Code aintenance Notes CB Airframe Description Effectivity ATA Status C/W Source Work Order Cert No HRS LDG Date Cli MM REF M HRS 980500 CB 50 Insp- Left Main Ban Lead hist! EFF: SN# 5102 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). 24 MAN N/A 25 Jun 2007 I CB Airframe 980510 CB 51 Broadband Multi-Link (BBML) Antenna Control Unit-Insp EFF: AC SNs 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). 23 MAN N/A 10 Jul 2007 CB 980520 CB 52 Inspection-LP Compressor Airframe Annulus Fillers EFF: Aircraft Serial Numbers 5001 Thru 5160. To be complied with within 90 days from issue date. Update CMP Codes 887256 and 897256 after compliance with CB52. 72 MAN N/A 04 Sep 2007 I CB 980530 CB 53 - Modification - Broadband Airframe Multi-Link Antenna Installation This CB is a ONE 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. 23 CAN N/A 18 Sep 2007 I 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

L TYP Logbook Code Description Effectivity ATA Status C/W Source HRS LDG Date Cli MM REF M HRS Work Order 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 Airframe 980540 CB 54 Wiring Harness At Fuselage Station (FS) 139 - Inspection Eft. A/C SN 5001 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. 24 MAN N/A 04 Oct 2007 I CB Airframe 980550 CB 55 Local Area Network (LAN) Connectors Inspection EFF: 5001.5137 and 5139. This is a *ONE TIME inspection to be accomplished with in the next 12 months. 31 MAN N/A 05 Oct 2007 I CB Airframe 980551 CB 55 AM1 Inspect-Local Area Network Connectors Effectivity sin 5138. due within 12 mos. 31 MAN N/A 11 Aug 2008 I 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 Code Logbook Wiintenance Notes CB 980552 Airframe Description Effectivity IATAI Status CNV Source Work Order CB 55 Am2 Local Area Network (LAN) Aircraft serial numbers 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. 31 MAN NIA Cert No HRS LOG Date 03 Oct 2008 CA MM REF M HRS CB CB 56 Inspection•NLG Downlock 980560 Airframe Switch Mounting Bracket EFF: Aircraft serial numbers 5001 through 5120 excluding 5014, 5044 and 5069 32 MAN N/A 26 Nov 2007 I CB Airframe 980570 CB 57 FMS Wiring Harness Inst at Fuselage Sta 63 Blkhd Effectivity: S/N 5001 through 5151, 5153 and 5155/ Compliance: Compliance with this CB is to be accomplished within the next 90 days. 34 MAN N/A 0.0 0 26 Nov 2007 C 0.00 CB Airframe 9B0580 CB 58 Nose Landing Gear Door Actuator (ASC 070) Effectivity: S/N 5001 through 5177 // Compliance: Compliance with this CB is to be accomplished within the next 12 months./ This CB is a one-time action to incorporate ASC 070. 32 MAN C/IN GAC APPLETON FP549 CRS GIIRI00Y 20.7 11 09 Apr 2008 C aoo 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 Gulf stream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620888

L TYP Logbook Code Description Effectivity aintenance Notes CB Airframe 980591 CB 59A1 Inspection - Main Entry Door EFF: Aircraft Serial Warning Switch Installations Numbers 5001 through 5141 and 5144 through 5146. excluding 5132. CB CB 60 Modification-Tail Compartment EFF: Aircraft serial 980600 Airframe Door Seal numbers 5050 through 5149 CB Airframe 980610 CB 61 Inspection-Feeder Cable Installation At Fuselage Station 687 EFF: Aircraft serial numbers 5003 through 5013, 5015 through 5036. 5038 through 5043. 5045 through 5068. 5070 through 5085 and 5093 CB 980620 CB 62 Inspection-Flap Drive Rod Airframe Installation EFF: Aircraft Serial Numbers 5001 Through 5144. excluding 5132. 5142 and 5143. CB Airframe 980630 CB 63 Inspection-Airshow AS4000 Mounting Tray Connector EFF: Aircraft serial 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 Airframe Nozzles Numbers 5001 Through 5100. CB Airframe 980650 CB 65 Auxiliary Power Unit (APU) Bond Strap Installation (ASC 066) Effectivity: SIN 5001- 51591 This customer 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 ATA Status C/W Source HRS LDG Date Cli MM REF M HRS Work Order Cert No 52 MAN N/A 0.0 0 26 Nov 2007 C 0.00 52 MAN N/A 0.0 0 26 Nov 2007 C 0.00 24 MAN N/A 0.0 0 26 Nov 2007 C 0.00 27 MAN N/A 0.0 0 26 Nov 2007 C 0.00 23 MAN N/A II Feb 2008 I 38 MAN N/A 0.0 0 26 Nov 2007 C 0.00 49 MAN N/A 07 Apr 2008 I 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 Logbook li Code Description Effectivity ATA Status C/W Source HRS LDG Date C/I MM REF M HRS Work Order aintenance Notes Cert No CB Airframe 980660 CB 66 Pt 1 Inspection - Fuel Metering Unit Independent Overspeed Protection Coil Wiring Eff: SeN 5001 51621! Part I is a one time 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. 73 MAN N/A 02 May 2008 I CB Airframe 980661 CB 66 Pt 2 Inspection - Fuel Metering Unit Independent Overspeed Protection Coil Wiring Eft: SiN 5001 -5162/I Part II of this customer 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. 73 MAN N/A 02 May 2008 I CB Airframe 980670 CB 67 Inspection-Fuel Boost Pump Manifolds Aircraft serial numbers 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. 28 MAN N/A 09 May 2008 I CB 980680 CB 68 Replacement-Emergency Airframe Inverter P/N 1.002-0102.1346 Aircraft 5102. 5132. 5151. 5152. 5153. 5156 thru 5161. 5163. 5168. 5170. 5171. Due within 24 months. 24 MAN N/A 11 Jun 2008 CB Airframe Mx. Notes: TO be aligned with 500 hr inspection ref D.Kalsi CB 69 Mod-Nose Gear Uplock Hook 980690 Spring (ASC 73) Due within 12 months. incorporates ASC 73 32 MAN CM Jet Aviation Geneva GV8TC003 513.0 177 03 Feb 2009 C 0.00 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