EFTA00620791.pdf

(itiiiktrearn Technical Bulletins Report Filters: G-CGUL MYCMP Log Date - 08 Nov 2014 Analyst: Gar Leaver TYPE: ALL CW Status: ALL Current TT 3466.5 Current Lndgs 953 Phone. FA)4 Phone: Current Hr Mtr 3423.6 COMPONENT TIMES Aircraft Make Gulfstream Position Logbook Description Serial Number Total Time Total Cycles TSO CSO Aircraft Model G550 1 Engine Rolls Royce BR700.710C4.11 15455 3466.5 953 (G550) Aircraft Serial No. 5176 2 Engine Rolls Royce BR700.710C4.11 15456 3466.5 953 Airworthiness 26 Nov 2007 (G550) Date 1 APU Honeywell RE220 (G550) P-503 2044.5 0 Regulation ELI-EASA TYP C/W Source Code Description Effectivity IATAI Status Logbook Work Order HRS LDG Date C/I MM REF M HRS aintenance Notes Cert No HYDRAULIC REPLENISHING gs Itn MAN CM 1012.1 326 19 Feb 2010 C 0.00 Airframe 299999 SYSTEM INOPERATIVE Mx. Notes: Hyd replenisher replaced by GS LTN Defect closed 441200 SB GPECSB50001 Cabin System 5365, 5381. 5385 OPT 26 Jan 2013 I Airframe Level E Firmware Update Cabin service bulletin 449002 GCMS SIB 002 Cabin System This Cabin Service OPT 08 Aug 2013 I Airframe Firmware Update 1.9.1 Bulletin is applicable to aircraft with GCMS controller firmware version 1.8.4 installed or later approved version. G-CGUL G550 5176 Technical Bulletins Page 1 of 164 20 Jan 2015 © 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620791  TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date C/I MM REF M HRS aintenance Notes Cert No GCMS SB 003 Cabin System This Cabin Service 449003 OPT 13 Sep 2013 I Airframe Firmware Update 4.4.3.3 Bulletin is applicable to aircraft with AC firmware version 4.4.1 installed or later approved version. Serial number effectivity includes 5365, 5381, 5385, 5394, 5395, 5400, 5407 and 5418. Final Phase Production cut- in starts with serial number 5424. CSB 003A • Advanced Cabin Server This Cabin Service 449004 23 OPT 21 Feb 2014 Airframe (ACS) System Firmware Update Bulletin revision 4A.3.3 supersedes CSB 003 Rev. — and Rev A is now re-issued as CSB 003A Rev. B. Aircraft having complied with CSB 003 will only accomplish Preferred Method Steps A.9 through A.17 or Alternate Method Steps B.28 through B.32, Return to Service testing and Service . Serial number effectivity includes 5365, 5381. 5385. 5394, 5395, 5400. 5407, 5418 and sub. with firmware ver. 4.4.1 or later version. G-CGUL G550 5176 Technical Bulletins Page 2 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620792 i T YP CNV Source Code Description Effectivity ATA Status lli oebook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No CSB 002B CPBC Software Installation Effectivity: This Cabin 449202 OPT 11 Dec 2013 I Airframe Instructions Service Bulletin is applicable to aircraft with GCMS controller firmware version 1.8.4 installed or later approved version. Serial number effectivity includes 5365, 5381. 5385. 5394, 5395, 5400. 5407, 5418 and 5424 Final Phase Production cut•in starts with serial number 5426 and Sub. 24 month compliance is for Warranty at Gutfstream G650 Authorized Warranty Facility. ASB BR700.72•A900297 High » Closed by Rev 1. C 880041 CAN CAN 0.0 0 22 May 2014 0.00 Engine 1 Pressure Compressor Fairings - 21 May 2014« Inspection of Upper Left HP Effectivity: Eng SIN Compressor Fairing 15887 • 15899. This SB must be accomplished on the affected eng within 500 flight hours after receipt of this SB. For eng SIN 15887 • 15891 only. it is recommended that this SB is accomplished at the same time as SB 72-A900298. Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link G-CGUL G550 5176 Technical Bulletins Page 3 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620793  TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No 880041 ASB BR700.72•A900297 High »Closed by Rev 1. CAN CAN 0.0 0 22 May 2014 C 0.00 Engine 2 (890041) Pressure Compressor Fairings - 21 May 2014 « Inspection of Upper Leh HP Effectivity: Eng S/N Compressor Fairing 15887 • 15899. This SB must be accomplished on the affected eng within 500 flight hours after receipt of this SB. II For eng S/N 15887 15891 only, it is recommended that this SB is accomplished at the same time as SB 72-A900298. Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link ASB BR700.72-A900298 Engine » Closed by Rev 1. C 880042 CAN CAN 0.0 0 22 May 2014 0.00 Engine 1 Combustion Fairings • Replacement 21 May 2014 « of Non.Confonning Upper Left. Upper Effectivity: Eng S/N Right and Lower Right Combustion 15887 • 15891. This Section Fairings SB must be accomplished on the affected eng within 500 flight hours after receipt of this SB. II It is recommended that this SB is accomplished at the same time as SB 72. A900297. Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link 880042 ASB BR700.72-A900298 Engine » Closed by Rev 1. C CAN CAN 0.0 0 22 May 2014 0.00 Engine 2 (890042) Combustion Fairings • Replacement 21 May 2014 « of Non-Conforming Upper Left. Upper Effectivity: Eng S/N Right and Lower Right Combustion 15887 • 15891. This Section Fairings SB must be accomplished on the affected eng within 500 flight hours after receipt of this SB. II It is recommended that this SB is accomplished al the same time as SB 72. A900297. Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link G-CGUL G550 5176 Technical Bulletins Page 4 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620794 L TYP C/W Source Code Description Effectivity ATA Status ii _ogbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No ASB BR700.72-A900497 TLM It is recommended this 880043 REC CM 1007.8 325 14 Feb 2010 C 0.00 Engine 1 Decrease Lives of HP Turbine Discs SIB be accomplished on all engines before 2 -28-10 Mx. Notes: lives amended as per sb 880043 ASB BR700.72-A900497 TLM It is recommended this REC 1007.8 325 14 Feb 2010 C 0.00 Engine 2 (890043) Decrease Lives of HP Turbine Discs SiB be accomplished on all engines before 2 -28-10 Mx. Notes: lives amended as per sb 880044 ASB BR700.72-A900504 Change of It is recommended this INF CM 1114.2 352 06 Apr 2010 C 0.00 Engine 1 Life Counting Method for Touch-and- SiB be accomplished Go and Overshoot on all engines before 7 -31.10 880044 ASB BR700.72-A900504 Change of It is recommended this INF CM 1114.2 352 06 Apr 2010 C 0.00 Engine 2 (890044) Life Counting Method for Touch-and- SIB be accomplished Go and Overshoot on all engines before 7 -31.10 SB BR700.72-900517 LP Compressor 710A1.10 sin 11275 880045 REC 25 Jan 2011 Engine 1 Annulus Fillers DFL and 11276 w/ SB- BR700.72-101699. 710C4.11 s/n 15129. 15179. 15180. 15181. 15413. 15425 wf SB- BR700.72-101699. 880121 SB BR700-77-101875 - N2 Speed Effectivity: BR700- 77 REC 03 Jul 2014 Engine 1 Probes - Introduction of New 710C4.11 Engines Attaching Bolts with Shorter Length prior to Engine Serial Number 16074. which have the Service Bulletin SB-BR700.72- 101588 standard incorporated. Compliance - RECOMMENDED It is recommended that this Service Bulletin be accomplished on engines when the engine or module is disassembled for refurbishment or overhaul. G-CGUL G550 5176 Technical Bulletins Page 5 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620795  TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LDG Date CA MM REF M HRS aintenance Notes Cert No 880121 SB BR700.77-101875 • N2 Speed Effectivity: BR700- 77 REC 03 Jul 2014 Engine 2 (890121) Probes • Introduction of New 710G4-11 Engines Attaching Botts with Shorter Length prior to Engine Serial Number 16074. which have the Service Bulletin SB-BR700-72- 101588 standard incorporated. Compliance - RECOMMENDED It Is recommended that this Service Bulletin be accomplished on engines when the engine or module is disassembled for refurbishment or overhaul. Alert SB BR700.72-A900509 BR700.710A1•10 0 880200 CAN CAN 0.0 15 Mar 2012 C 0.00 Engine 1 Replacement of the Fuel Pump Engines.Modules M61. Splined Coupling 148. M61.158. M61- 162. M61.168. M61- 169. M61.176. M61- 179. M61.184. M61- 188, M61.190. M61- 195, M61.196. M61- 197 and M61.203. BR700.710C4.11 Engines. (a) For engines which have hfw config standard 71004.11 engraved on data plate (SB-BR700.72-101466 standard not 'acorn). Modules M61.187 and M61.205 (AccesGearbox Module). (b) For eng which have hfw config 710C4- 11/10 engraved on data plate SB•BR700- 72-101466 incorp. Module M61.202 Ganz see revl 890300 G-CGUL G550 5176 Technical Bulletins Page 6 of 164 20 Jan 2015 O2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620796  TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No 880200 Alert SB BR700.72-A900509 BR700.710A1-10 CAN CAN 0.0 0 15 Mar 2012 C 0.00 Engine 2 (890200) Replacement of the Fuel Pump Engines.Modules M61. Splined Coupling 148. M61.I58. M61- 162. M61.168. M61- 169. M61.176. M61- 179. M61.184. M61- 188. M61.190. M61- 195, M61.196. M61- 197 and M61.203. BR700.710C4.l1 Engines. (a) For engines which have h/w config standard 7100441 engraved on data plate (SB-BR700.72-101466 standard not incorp). Modules M61.187 and M61.205 (AccesGearbox Module). (b) For eng which have hive config 710C4- 11/10 engraved on data plate SB.BR700- 72-101466 incorp. Module M61.202 Canx see rev1 890300 SB BR700.72.100981 • LP Impact Effectivity: Prior to 880237 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Adhesive And Filler Engines SN 15133 880237 SB BR700.72.100981 • LP Impact Effectivity: Prior to 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890237) Adhesive And Filler Engines SN 15133 880271 SB BR700-72.101144 • Combustion Effectivity: BR700• 72 INF N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Inner Case And Vanes 710A1.I0 Engines / Prior to Engine Serial Number 11498 // BR700.710C4.// Engines / Prior to Engine Serial Number 15113 and Engine Serial Numbers 15114 and 15115 G-CGUL G55O 5176 Technical Bulletins Page 7 of 164 20 Jan 2015 02015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620797  TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No 880271 SB BR700.72.101144 • Combustion Effectivity: BR700- 72 INF NIA 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890271) Inner Case And Vanes 710A1.10 Engines/ Prior to Engine Serial Number 11498 // BR700.710C4.11 Engines / Prior to Engine Serial Number 15113 and Engine Serial Numbers 15114 and 15115 SB BR700.72.101173 • LP / HP NOTE: Prior to Engine 880276 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Turbine Stator Retainer / Seals Serial Number 15189 880276 SB BR700.72.101173 • LP / HP NOTE: Prior to Engine 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890276) Turbine Stator Retainer / Seals Serial Number 15189 SB BR700.72.101195 • Intermediate NOTE: Prior to Engine 72 OPT 14 Dec 2010 I Engine 1 880285 Compressor Case Serial Number 15129, 15130 thru 15141, 15145. 15147 thru 15150. 15154 thru 15159. 15162 thru 15195, 15200 thru 15228 and 15231 onwards 880285 SB BR700-72.101195 • Intermediate NOTE: Prior to Engine I 72 OPT la Dec 2010 Engine 2 (890285) Compressor Case Serial Number 15129, 15130 thru 15141, 15145, 15147 thru 15150, 15154 thru 15159, 15162 thru 15195, 15200 thru 15228 and 15231 onwards SB BR700•72•101203 • HPC Variable NOTE: Prior to Engine 72 OPT 880287 . NA 0.0 0 26 Nov 2007 C 0.00 Engine 1 Guide Vanes Actuating Mechanism Serial Number 15124 880287 SB BR700.72.101203 • HPC Variable NOTE: Prior to Engine 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890287) Guide Vanes Actuating Mechanism Serial Number 15124 SB BR700.72.101246 • New LP NOTE: Prior to Engine 880296 72 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Compressor Disc Serial Number 15178 G-CGUL G550 5176 Technical Bulletins Page 8 of 164 20 Jan 2015 ®2015 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00620798  TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No 880296 SB BR700.72-101246 - New LP NOTE: Prior to Engine (890296) 72 OPT NIA 0.0 0 26 Nov 2007 C 0.00 Engine 2 Compressor Disc Serial Number 15178 880301 Alert SB BR700-72-A900509 Revision I of this Non- CAN CAN 0.0 0 26 Jun 2012 C 0.00 Engine 1 (Revision 1) Replacement of the Fuel Modification Service Pump Splined Coupling Bulletin has been issued to change the Manpower from 4 hours to 10 hours and to include the old standard of fuel pump splined coupling. PIN BRR52639. Superceded see revision 2 - code 880307 880301 Alert SB BR700-72-A900509 Revision 1 of this Non- CAN CAN 0.0 0 26 Jun 2012 C 0.00 Engine 2 (890301) (Revision 1) Replacement of the Fuel Modification Service Pump Splined Coupling Bulletin has been issued to change the Manpower from 4 hours to 10 hours and to include the old standard of fuel pump splined coupling. PIN BRR52639. Superceded see revision 2 - code 880307 880302 SB BR700-73-101376 - Combination 73 REC 16 Jul 2002 Engine 1 Of EEC Hardware Standard 880302 SB BR700.73-101376 - Combination 73 REC 16 Jul 2002 Engine 2 (890302) Of EEC Hardware Standard G-CGUL G550 5176 Technical Bulletins Page 9 of 164 20 Jan 2015 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620799  TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No SB BR700.73-101380 - Introduction Effectivity: BR700- 880303 73 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 of an EED with a New Hardware 710C4.11 Engines / Standard For engines which have hardware configuration standard 710C4.11 or 710C4- 11/10 engraved on the engine data plate (Service Bulletin R SB- BR700.72-101466 standard not incorporated). Prior to Engine Serial Number 15105. Orig Issue: 08/09/2002 / Rev 1: 09/11/2002 880303 SB 6R70073-101380 - Introduction Effectivity: BR700- 73 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890303) of an EED with a New Hardware 710O4-11 Engines / Standard For engines which have hardware configuration standard 710C4.11 or 710C4- 11/10 engraved on the engine data plate (Service Bulletin R SB- BR700.72-101466 standard not incorporated). Prior to Engine Serial Number 15105. Orig Issue: 08/09/2002 / Rev 1: 09/11/2002 SB BR700.73-101386 - Fuel Manifold NOTE: Prior to Engine 880304 73 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 Damper Wire Serial Number 15181 and from Engine Serial Number 15194 to 15254 880304 SB BR700.73-101386 - Fuel Manifold NOTE: Prior to Engine 73 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890304) Damper Wire Serial Number 15181 and from Engine Serial Number 15194 to 15254 G-CGUL G550 5176 Technical Bulletins Page 10 of 164 20 Jan 2015 2015 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00620800  TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No SB BR700•73.101400 • EEC with Effectivity: Prior to 1 880305 73 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine S2.1 Software Standard Engine Serial Number 15166 880305 SB BR700•73.101400 • EEC with Effectivity: Prior to 73 REC N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890305) S2.1 Software Standard Engine Serial Number 15166 SB BR700•73.101558 (Rev 1) • Fuel NOTE: For engines 8803 73 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 1 06 Flow Transmitter prior to Engine Serial Number 15328 which do not have the Service Bulletin SB. BR700.73.101496 standard incorporated 880306 SB BR700.73.101558 (Rev 1) • Fuel NOTE: For engines 73 OPT N/A 0.0 0 26 Nov 2007 C 0.00 Engine 2 (890306) Flow Transmitter prior to Engine Serial Number 15328 which do not have the Service Bulletin SB. BR700.73.101496 standard incorporated Alert SB B