EFTA00604340.pdf

Gulfstream Technical Bulletins Report Filters: N401HB MYCMP Log Date - 06 Dec 2016 Analyst: Phone: Keith Bell TYPE: ASC CW Status: ALL Hours Landings 5314.9 1191 Phone Hour Meter 5314.9 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 15449 5245.0 1168 (G550) Aircraft Serial No. 5173 2 Engine Rolls Royce BR700.710C4.11 15448 5245.0 1168 Airworthiness 30 Oct 2007 (G550) Date 1 APU Honeywell RE220 (G550) P-500 1822.5 0 Regulation 91.409f3 TYP I !CAN Source Code Description Effectivity IATAI Status LLogbook Work Order I HRS I LDG Date Cli MM REF M HRS aintenance Notes Cert No ASC ASC 2A Digital Flight Data Recorder This rev cancels ASC 970021 31 CAN CAN 0.0 0 24 Feb 2014 C Airframe Sys Upgrade 002 Dated Dec 5. 2005. Aircraft that have complied with ASC 002 have met the intent of this revision. This ASC has been cancelled by ASC 0028 dated Feb 20. 2008. Mx. Notes: This code has been cancelled. ASC ASC 28 Digital Flight Recorder Cancelled by ASC 970022 31 CAN CAN 0.0 0 24 Feb 2014 C Airframe System Upgrade 002C issued 11121/2008. Mx. Notes: This code has been cancelled. ASC ASC 2C Digital Flight Data Recorder Effectivity: This service 970023 31 CAN CAN 0.0 0 24 Feb 2014 C Airframe System Upgrade (88 Parameters) change is applicable to G500 8 G550 aircraft serial numbers 5001 and subsequent requiring Pan 135 certification. Cancelled by ASC 002D. Mx. Notes: This code has been cancelled. N401HB G550 5173 Technical Bulletins Page 1 o131 06 Dec 2016 2016 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00604340  TYP C/W Source Code Description Effectivity ATA Status iLogbook l Work Order HRS LDG Date C/I MM REF M HRS aintenance Notes Cert No ASC ASC 2D Digital Flight Data Recorder Effectivity: This service 970024 31 OPT 19 Jun 2012 Airframe System Upgrade (88 Parameters) change is applicable to G500 & G550 aircraft serial numbers 5001 and subsequent requiring Pan 135 certification. This revision. ASC 002D cancels and supersedes all previous versions of ASC 002. ASC ASC 8 MAX GROSS WGT 75K GAC-LGB-3 970080 Canx see ASC 008A 11 CAN CPN 9.5 3 07 Mar 2008 C 11 0.00 Airframe PLACARD FP2471 EC3R470L ASC ASC 8A Maximum Gross Weight This revision cancels 970081 CAN CM 2375.8 524 04 Aug 2011 C 0.00 Airframe 75.000 Pounds and supersedes the original version of ASC 008. dated November 4. 2003. Operators of aircraft that have previously complied with ASC 008 shall observe and follow the procedures associated with the use of the placard as described in this revision and return the attached service reply card indicating that ASC 008A was previously complied with. Cancelled see ASC 008B Mx. Notes: Inspected and verified installation of AFM Supplement PIN: G550.2003.01 dated 8/14/2003 in Section 7 ASC ASC 8B Maximum Gross Weight To meet intent of this 970082 OPT CM 2682.7 587 28 Dec 2011 C 0.00 Airframe 75.000 Pounds revision arc that previously cAv ASC 0081008A replace AFMS G550.2003-01 date 8.14-2003 with the AFMS in section II. Mx. Notes: Installed Revision G550.2003.01. Rev. 1 in Flight Manual Supplements binder. N401HB G550 5173 Technical Bulletins Page 2 of 31 06 Dec 2016 2016 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00604341  TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No ASC ASC 9 MAX ZERO FUEL GROSS Eff. Dose: ALL G550 GAC-LGB-3 970090 11 CAN CM 9.5 3 07 Mar 2008 C 11 0.00 Airframe WGT AIRCRAFT. Cancelled FP2471 see ASC 009B EC3R470L ASC ASC 9A Maximum Zero Fuel Gross This service change is 970091 11 CAN CAN 0.0 0 24 Feb 2014 C Airframe Weight 53.500 Pounds - Placard applicable to all Installation Gulfstream G550 aircraft. This revision incorporates a redesigned placard assembly and updates the material list and accomplishment Instructions. This revision upersedes ASC 009. dated November 4. 2003. No further action is required for operators of aircraft that have previously complied with the original issue of ASC 009.Cancelled see ASC 0098 Mx. Notes: This code has been cancelled. ASC ASC 98 Maximum Zero Fuel Gross 970092 OPT CM 3560.8 776 11 Apr 2013 C 0.00 Airframe Weight 53.500 Pounds - Placard Installation Mx. Notes: Previously Complied With: 31712008: 9.5 Hours: 3 Landings ASC 970110 ASC 11 G550 DATA PLATE INSTALL Eft.• Dose.• 5001-5999• 00 OPT CM 0.0 0 31 Oct 2007 C 0.00 Airframe Converts GVSP to G550. "Record ASC" ASC ASC 14 Category II Annunciation cancelled see ASC 970140 34 CAN CAN 0.0 0 24 Feb 2014 C Airframe Activation 14A Mx. Notes: This code has been cancelled. N401HB G550 5173 Technical Bulletins Page 3 of 31 06 Dec 2016 2016 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00604342  TYP C/W Source Code Description Effectivity ATA Status iLogbook l Work Order HRS LDG Date C/I MM REF M HRS aintenance Notes Cert No ASC ASC 14A Category II Annunciation - This ASC replaces 970141 34 OPT 13 Jun 2011 Airframe Activation 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 ASC ASC 33 BONDED HONEYCOMB Eff. Desc: ALL G550 970330 53 OPT 05 Dec 2003 I Airframe PANELS AIRCRAFT. This is a record only ASC which incorporates drawing 1159SB50006 honeycomb floor panel repair-optional. ASC ASC 35A (Part I) EASA / JAA Cart- 970351 Supersedes ASC 035 OPT 10 Nov 2006 I Airframe Basic Requirements ASC ASC 35A (Part 2) EASA / JAA Cert - 970352 Supersedes ASC 035 OPT 10 Nov 2006 I Airframe Basic Requirements ASC ASC 49 Lightning Sensor System This Service Change 970490 34 CAN CAN 0.0 0 03 Aug 2015 C 0.00 Airframe (LSS) Installation is applicable to A/C Serial No# 5001 and Sub. Aircraft that have previously complied with ST No.ST02915AT-D meet the intent of ASC 049. Cancelled by ASC 49A (970491) Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link. N401HB G550 5173 Technical Bulletins Page 4 of 31 06 Dec 2016 O2016 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00604343  TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No ASC 970491 ASC 49A Lightning Sensor System Effectivity: This service 34 CAN CAN 0.0 0 10 Dec 2015 C 0.00 Airframe (LSS) Installation change is applicable to aircraft serial numbers 5001-Subsequent. Aircraft operators who have previously complied with ASC 049 are in compliance with this revision (ASC 049A) and should return the service reply card(s) marked "Previously complied with." Cancelled by ASC 0498 (970492) Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link. ASC ASC 498 Lightning Sensor System Effectivity: This service 970492 34 OPT 09 Dec 2015 I Airframe (LSS) Installation change is applicable to aircraft serial numbers 5001— Subsequent. ASC ASC 52 Planeview Avionics EFF: Acft Serial GAC-LGB-3 970520 31 OPT CAN 9.5 3 12 Mar 2008 C 0.00 Airframe Enhancement Number 5001-5174 FP2471 EC3R470L ASC ASC 53 Comm Management Fnc EFF: 5001 and Sub. 970530 23 CAN CAN 0.0 0 24 Feb 2014 C Airframe Arinc Direct-Datalink cancelled ref ASC 53A Mx. Notes: This code has been cancelled. ASC ASC 53A Communications 5001 and sub. AIC 970531 OPT 05 Dec 2011 Airframe Management Function ARINC Direct - which have previously Datalink Service Provider cAv ASC 53 should signet( this ASC as previously complied with. ASC ASC 61 Synthetic Vision-Primary ASC 907 - GAC 970610 31 CAN CPN APPLETON 930.7 232 30 Jun 2009 C 0.00 Flight Display (SV-PFD) Installation PlaneViewe Master Airframe Operating Software SC5621 Update (SV-PFD) is required for aircraft serial numbers 5001 - 5188. Superceded see ASC 6IA CRS G1FR100Y N4O1HB G55O 5173 Technical Bulletins Page 5 of 31 06 Dec 2016 © 2016 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00604344  TYP CNV Source Code Description Effectivity ATA Status Logbook Work Order HRS LDG Date CA MM REF M HRS aintenance Notes Cert No ASC ASC 61 Aml • Synthetic Vision This service change GAC 970611 CAN CAN APPLETON 33°1 232 30 Jun 2009 C 0.00 Primary Fight Display (SV•PF) amendment is for Airframe information only.This SC5621 amendment replaces pages 1 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 CRS G1FRI00Y ASC ASC 61A Synthetic Vision•Primary This service change 970612 CAN CW 1265.2 296 21 Jan 2010 C 0.00 Airframe Right Display (SV•PFD) Installation revision will supersede the original issue of ASC 061 dated September 8, 2008. incorporate ASC 061 Amt dated December 19.2008 and is now reissued as ASC 061A. Aircraft having previously complied with ASC 061 may continue to operate at version 1.0 with no further action required. Prerequisites: G550 ASC 908 • PlaneView Master Operating Software Update (Cart Fox) Mx. Notes: CNV by Gulfstream. Appleton. Work No. SC 6431 N401HB G550 5173 Technical Bulletins Page 6 of 31 06 Dec 2016 O2016 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00604345  TYP CNV Source Code Description Effectivity ATA Status il Logbook Work Order HRS LOG Date CA MM REF M HRS aintenance Notes Cert No ASC ASC 61A Amt Synthetic Vision - This service change 970613 CAN Cm 1936.8 440 17 Jan 2011 C 0.00 Airframe Primary Fight Display (SV-PFD) amendment is for Installation information only. The installation of ASC 061A is now authorized for aircraft operating under EASA/JAA regulations and an EASA project number has been provided. Additionally. installation of this service change is no longer restricted to Gulfstream Aerospace or General Dynamics Aviation Services (GDAS) facilities. Mx. Notes: This ASC is for Information only. Replacing Instruction paper in ASC 061A ASC ASC 61B Synetic th Vision-Primary This service change 970614 31 OPT Cm 4021.4 896 06 Jan 2014 C 0.00 Airframe Right Display (SV•PFD) Installation applicable to aircraft serial numbers 5001 and subsequent. This aircraft service change revision supersedes ASC 061. Operators of aircraft that have any version of ASC 061 installed require no further action. Operators of aircraft with the original issue of ASC 061 or ASC 061 Amt do not return a service reply card for ASC 061B. Only operators of aircraft with ASC 061A or later installed should complete and return the service reply card indicating "previously complied with'. Mx. Notes: Previously Complied With by ASC Purpose / Discussion Continued Section N401HB G550 5173 Technical Bulletins Page 7 of 31 06 Dec 2016 O2016 Gulfstream Aerospace Corporation. MI Rights Reserved. A General Dynamics Company EFTA00604346  TYP C/W Source Code Description Effectivity ATA Status Logbook Work Order HRS LDG Date Cli MM REF M HRS Maintenance Notes Cert No ASC ASC 63A Wing Fuel Transfer Sys EFF: 5001and 970631 57 CAN CAN 0.0 0 01 Apr 2013 C 0.00 Airframe Mid-Wing Ejector Mod Part 1 Sub.Cancelled by ASC 063B Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link. ASC ASC 63A Wing Fuel Transfer Sys EFF: 5001 and Sub. 970632 57 CAN CAN 0.0 0 01 Apr 2013 C 0.00 Airframe Mid-Wing Ejector Mod Part 2 Cancelled by ASC 063B Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link. ASC ASC 63B Wing Fuel Transfer Sys Effectivity: 5001 and 970633 57 CAN CAN 0.0 0 12 May 2016 C 0.00 Airframe Mid-Wing Ejector Mod Part 1 Sub. Cancelled by ASC 063C (970636) Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link. ASC ASC 63B Wing Fuel Transfer Sys Effectivity: 5001 and 970634 57 CAN CAN 0.0 0 12 May 2016 C 0.00 Airframe Mid-Wing Ejector Mod Part 2 Sub. Cancelled by ASC 063C (970637) Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link. ASC ASC 63B Wing Fuel Transfer Sys Effectivity: 5001 and 970635 57 CAN CAN 0.0 0 12 May 2016 C 0.00 Airframe Mid-Wing Ejector Mod Part 3 Sub. Cancelled by ASC 063C (970638) Mx. Notes: This code has been cancelled. See Compliance Remarks by clicking Show Remarks link. ASC ASC 63C Wing Fuel Transfer Sys Effectivity: This service 970636 57 OPT 12 May 2016 1 Airframe Mid-Wing Ejector Mod Part 1 change is applicable to aircraft 5001 and subsequent. ASC ASC 63C Wing Fuel Transfer Sys Effectivity: This service 970637 57 OPT 12 May 2016 1 Airframe Mid-Wing Ejector Mod Part 2 change is applicable to aircraft 5001 and subsequent. ASC ASC 63C Wing Fuel Transfer Sys Effectivity: This service 970638 57 OPT 12 May 2016 1 Airframe Mid-Wing Ejector Mod Part 3 change is applicable to aircraft 5001 and subsequent. ASC ASC 65 Runway Awareness Advisory EFF: Acft Serial 970650 34 CAN CAN 0.0 0 24 Feb 2014 C Airframe System (FtAAS)•Installation Number 5001 and Sub. Mx. Notes: This code has been cancelled. ASC ASC 65A Runway Awareness This ASC supercedes GAC-LGB-3 970651 34 OPT CM 17.8 5 18 Mar 2008 C 0.00 Airframe Advisory System-Installation ASC 65 FP2471 EC3R470L N4O1HB G55O 5173 Technical Bulletins Page 8 o131 06 Dec 2016 €12016 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00604347  TYP C/W Source Code Description Effectivity ATA Status iLogbook l Work Order HRS LDG Date C/I MM REF M HRS aintenance Notes Cert No ASC 970700 ASC 70 Nose Landing Gear Door EFF: G550 aircraft, GAC-LGB-3 32 MAN CM 9.5 3 26 Feb 2008 C 0.00 Airframe Actuator Modification serial numbers 5001- FP2471 5187I/ NOTE: Mandatory for SIN 5001 - 5177 per CB 58 issued 12/0/2007 EC3R470L ASC ASC 71 Micro Quick Access Recorder Cancelled see ASC GAC-LGB-3 970710 31 CAN CM 22.3 6 24 Mar 2008 C 0.00 Airframe Installation 071A FP2471 Mx. Notes: SATISFIED BY INCORPORATION OF ST01775LA-D EC3R470L ASC ASC 72 Medeco Door Locks 970720 Effectivity 5001.5204 52 OPT 20 May 2008 I Airframe Installation ASC ASC 73 Nose Gear Uplock Hook Concurrent GAC-LGB-5 970730 32 CAN CM 282.0 90 08 Aug 2008 C 0.00 Airframe Spring Replacement requirement = CB 69. SC4484 SiN 5001.5204. EC3R470L ASC ASC 73A Nose Gear Uplock Hook Concurrent 970731 32 MAN CM 815.0 209 14 May 2009 C 0.00 Airframe Spring Replacement Requirement: G550 Customer Bulletin Number 69. SIN 5001- 5204.This revision supersedes ASC 073. dated July 30. 2008. and is now issued as ASC 073A. Aircraft that have previously complied with ASC 073 meet the intent of this revision and should return the attached service reply card indicating that ASC 073 was previously complied with. ASC ASC 74 Dual Brake Metering Valve GAC 970740 32 CAN CM APPLETON 930.7 232 26 Jun 2009 C 0.00 Replacement Airframe SC562I Mx. Notes: SUPERCEDED BY ASC 074k CRS GIFR100Y N401HB G550 5173 Technical Bulletins Page 9 of 31 06 Dec 2016 2016 Gulfstream Aerospace Corporation. All Rights Reserved. A General Dynamics Company EFTA00604348  TYP C/W Source Code Description Effectivity ATA Status L Logbook Work Order HRS LDG Date Cli MM REF M HRS aintenance Notes Cert No ASC ASC 74A Dual Brake Metering Valve This service change GAC 970741 32 OPT CM APPLETON 930.7 232 30 Jun 2009 C 0.00 Replacement revision corrects the Airframe part number for the SC5621 hydraulic line from PIN 11595857960-25 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. CRS G1FR100Y ASC ASC 74A AM1 Dual Brake Metering This service change 970742 OPT CM 2375.8 524 04 Aug 2011 C 0.00 Airframe Valve Replacement amendment corrects the 24 month warranty compliance statement in ASC