EFTA00796534.pdf

Work Order: 5C521661 AC: 5173 STM: Charles Thomas SCC: Julian Brown Squawks: Ni Yellow = Newly Added Items, Green = Changed Items (Ready for inspection or completed) from prevtous day (or since Friday on Mondays) Assoc Status Discrepancy Resoludon 1 airfnmeGuirstreeas GSSO 1.I Wdttng Return To Service aCnrOvat (1.) 1.2 In IntoundfOutbaurd Impectnn Progress 1.2.1 Competed IntOunerellminary IFISDOCti3n Comp led xlth IntounOPYcglmInacy Inspection as per RSQCT 57 rev 24 1.2.2 Open Outbound InspecUon 1.3 Waiting Preflight Inspection Complied with creflight impectlon as outlined in RSQCT-113 Rev. 23 0(04 a.) 1.4 Completed CoraPh with Detrid Oncklat Complied with Detrid drecklaL 1.4.1 Completed ArriyaVDebref 90 Day De List Revell ACCCOWielle 1.4.2 ComMeted List C9eratoes Matt Tress Relultements &Special Part 91.409 f(3). N3 Other special documentation requests. Documentadon RequeStS 1.5 Waiting Tool Clearance Provided bed dearence per SOP 1028, all teals eanunted for alnrowd 0.1 1.6 Completed Cover & Protect Covered and NOteded as required 1.2 Completed Service Channel Toilet/0ton Galley Told serviced JAY( the ground herding and servicing hardback 14-00-00 Id Completed AfrIvaVDeParttre ASSISI & MOO Nroart Complete with interior inbotrel InSfiedianGA 3564 (CG) 5/17 and oleo 1.9 Completed SamPie Mircratglt Fluids Compiled ulM Sample MydraiAlt Flutlf 1.10 Completed Remote Valuables & Scare. Secured by customer soon arrival 1.11 Completed Comply with Service Team Manager Check1st Complied with Service Team Manager Chectist 1.12 Completed Molds Used (011s/9ttdr0) • (Materials Or4) Informaoon Cy*. 1.13 Completed SIM / Quality review 01 week Order and ite/bOOk con plot Compiled xiith SIN/Quality reviewof work order and logbook entry PIN to depantre to departure 1.14 Completed Towing (Dees not include Hangar Mores) TOMO as required 1.15 Completed Hazinat - Identey & provide a manifest, and a SriggerS N/A no hatmat to be loaded. Declaration for Dangerous Goods for all hazardous materials that are loaded aboard any airaaR. FAR Pin 121 Of 135 Operators x111 proud° a hazardous material noting= letter reputed by FAR 135.505 (e) pax to mantereree at Ohs Repair Station tax FAR 145.206 (a) (b). If there b to be loading of hazardous matelots e shall be complied with by llama trained autheized GAC personnel orgy. 1.16 Waltin9 Moan Donn) adarowd (L) 1.16.1 Open CLEM1NG LAMING GEAR Fit PAINT 1.17 Completed Consumades & Shop Staple' FOr bl1Yg purposes tined. 1.18 Waiting Major Alteratnns regulatory comp/ once requirements to be approval completed by initaler ea notated on FM Pam 8100-9. 0.1 Copy and paste from attached statements as needed and eat as moulted. COMPLY WITH REQUIREMENTS OF FAR 25.1301 (a) (0). 25.1353(a) and 25.1431(c) (d). COMPUED WITH THE REQUIREMENTS OF FAR 251301(a) (b). 25.1353(a) and 25.1431(0 (d). via GROAD TEST REPORT-REPORT Ho. CE)0(x)O3Ca REV. X, ( IN SUPPORT CS STC =Mean ) and GR4R216.4 REPAIR STATION INTERFERENCE TESTING REQUIREMENTS P057 MAJOR ALTERATIONS COMPUANCE FORM. COMPLY WITH REQUIREMENTS OF FAR 25.1529, INSTRUCTIONS FOR CONTINUED AIRWORTHINESS REF X)COCK MANUAL, P/N X)0(x)03( REV. X, FOR INSTRUCTIONS FOR CONTINUED AIRWORTHINESS AND BLOOM 8 CC FM FORM 337, DATED nifix)UXXXX COMPLY WITH THE WIRE ROUTING REQUIREMENTSOF FM POLICY MM-01-04 AND FAR 25.1353 (8) COMPLIED WITH THE WIRE ROUTING REQUIREMENTS OF FM POLICY MM-01-04 AND FM 25.1353 (13) By ENSURING ROUTING WAS IN ACCORDANCE AC43.13-11, CHANGE 1CHAPTER 11, SECTION 8. 1.19 Vann) Update WCi a Balance aPPrOwil (1) 1.20 Waiting Catena Pant and Were & Stan Requirements. aPPrOyal LI 15,2017 6.21.0S AM Gulfstream Proprietary Information Nrc I of 2"0 EFTA00796534 Work Order: 5C521661 AC: 5173 STM: Chart Thomas SCC: Julian Brown Squawks: All Yellow = Newly Added Items Green = Changed Items (Ready for inspection or completed) from previous day (or since Friday on Mondays) Assoc Stalin Discrepant/ ResOkiliOn (L) Reyes scope or aircraft caterer pant touthspftepars, and Son replxements reviling in paint reapplication, dd determine arieCt on weir and batriCe. For surfaces where paint is stripped and reapplied or added on top of existng pant on Si area greater than 36 square feet tne thickness values will be documented before and after painting . If average thickness values remain the 'erne, sestet and balm review S not required. For surfaces painted wed an area greater than 36 square feet and before and alter pant tricnwss average vanes. QC review for pantile weight end blame revision will be reettred. • Tholosess wit be plotted on an aircraft droning derived from AMM chapter 6 or Weer sutable netch, attached to the work order and meastrements taken on a two glare foot grid. • Reference CAMPS 9000, paragraph 3.5.1 for paint restriclions to right control surfaces and RYSM certified aircraft • Reference CAMPS 9000, teal average thidness shall not (Steed 6 mils. • Per GAC Mass Propene= Engineering, pant thickness of 5 rids equSs .055 pounds per squre foot. Vane QC revs% night charge is greater than 2 pounds or .05% of MAC, the weight and balance report wig repute reoamwtaton. 1.21 Waiting Aircraft Ready Co. Rotten to Service. Al reCured approval inspections, to include preflign espectins, maintenance (L) tasks, 'secrets:anal & Ionchecks, related dowmenabco, and clearing activitiescomplete. Contact Return to Service group when Oh swank is complied with. 1.22 Completed Advise customer of °reser...Won requirements per ATA Advised customer of °ogre and PA) preservation requirements. Chapter 10 of the releant maintenance manuals rot • Engines, and MU; renew requirements en relation to schedled Date Pronned and later ',dental Date Completed; and perform maintenance 0, cresovaten actions as directed by the CuStOmer and documented at a Work Order Squeak. 123 Completed Pre-Compliance cabn refurbishment inspecbco Complied with Pre-Compliance cabin nkstishment Section per 14 CM part 25. NOTE: SEE APPENDIX 1.29 Completed CMP GSSO O1OO1O-Service Cater Maintenance Indexton Complied with CMP GSSO O1OO1O-San= Center Maintenance India:ton Cheddist Cheddig 1.25 In Comply with Het Cockpe and Ha Cabin Progress 1.25.1 Completed Comply with intern Hot Codmit LAW RSQCT-26S flat-I Complied with inbound Hot Cockpit LAW RSQCT-265 flat-I 1.25.2 Completed Coney with intoinO Hot Caton JAW RSQCT•219 Rawl Complied with Intent Not Cabin JAW PSZCf.219 PAN-2 1.25.3 Open Comply with osaound Not Cockpit LAW RSQCT•265 Rev.' 1.25.4 Open Comply with ciAtcund Mot Cain LAW RSQCT-219 Rev-2 1.26 Waiting Removed aircraft laptop and bag and sensed in Seen Moroni 94ansons office. 0.) 1.27 Waiting Sales Conceseco Wowed (L) 2 OMNI elt70071001-11 2.1 Completed Remove LH engne nose covA and replace with Rots Royce Summary: Retraced Lill Eng. loaner into cowl PN:O4CO3O1-O19 SN:GVSPIS9 and instated Rot Royce provided Padded ex hange snit Reference RR Newstbish: exchange inet cowl PH: 0401031-019 511: GV5P1345V per CW 711002. liF201302. See steps below fa detailed work palormed. 2.1.1 Completed Removed Lill Erg. toner inlet cowl PN:O9O2O31-O19 SN:GVSP159 and Installed customs.' 'waned Inlet cowl PH: 0400001-019 5th: GV5P134SV per OSP 711002 Item 11.1. Reference Removal and Installation book page IC. 2.2 Completed CMP GSSO 893131 Alert SO 8127D3-73-A912O383R1 COMPLIED woe CMP GS5O 880131 Alert 58 W00-734500383R1 Replacement of Non-Conkemng Pats of the EEC Replamment of NOnCOnlOmling Parts of the HC Re%x Firetp3x Assembly. AS9eMtly Labor Not Appinstle due to engine Sin: effectMly Oily Engem Sint: 15998 wth corfnutation standard 7100111 engumed On data plate. $1,652 Matenals. it Charge (Rolls-Royce Warranty) (AI • perators) The Intent of this Mon•ModificatIon Service SWOP, Is to replace EC-C firebox assembles that have an inglficient thickness of the rittroescent part Effecbvity: Reference Rolls.Rcsee Semite Etuletin 80.700-73- A900083 for effectMty Notes: 12113,2017 6:21:O5AM Gut/stream Proprietary Information Pace ;a 2.9 EFTA00796535 Work Order: 5C521661 AC: 5173 STM: Chart Thomas SCC: Julian Brown Squawks: Au Yellow = Newly Added Items Green = Changed Items (Ready for inspection or completed) from previous day (or since Friday on Mondays) Assoc Stalsas Discrepancy Resolution Pans are savaged arid procured thrash kenRoyce. Reese place your or with Relts-Rote Spares sin (6) months m advance and preekle 'MO need date SO OX'y Can endure parts aroilaff my. CapzeatcCem Detentes: Carstrern viii Frerace Rao. Royce CaparateCare for the rheas abate en the CusternerS behalf. Determination wnat is of is not covered under the maintenance program will be detenratO by Ralefface. My charge, net conered b, the CorporoteCare pagan mil be the Custemsoz raperoibilty and %Mast to Gulfs-Cream's standard Terms and Conditons with regard to payment. Sutirresseon dl the mote 6 Fecicated on the CorparateCare maintenance program tang in (Dice at the Ome a service. 2.3 Completed "'CANCEL"' 04P G550 880466 Alert 58 EIR700.73 Cannot compete with at this time due to Darts avalabley. $6 emplane due by 31 /AN 2021 (38 rnos remaining). A101981R3 - Introduce= of a New EEC Firebox Asscrady nab a Revised Pant System. Customer Ssanatuie: Date: hi ENGINE 8R700-710C4-11 3.1 Cemented Rai-me NI crane ncee cent and replace with Rots Rate Summery: Removed Rill Eng. boner inlet men fr4:040001-020 SN:GVSP171 and installed Rolls Royce provided Panda/ exchange alt. Reference RR Newsflast exchange Viet cowl PH: 04C0031-020 SN: G139 Der 04P 711002. NF2013.02. See steps below for detailed work portent& 3.1.1 Completed Removed NH Eng. Ironer inlet awl MV:0K0001-020 SN:GV5P171 and InetalleO cuRorror offered Inlet cowl PN: 040:031420 SN: 6139 per CMP 711002 Item I I.2 3.2 Canalised CMP MO 893131Men SB BR703-73-A907383R1 - COMPLIED WITH CMP e3550 890131 Net 58 BR700-734.900083R1 - Replacement of Nan-Confirmiog Pens of the EEC nepiaonnent of NanConromM9 Parts of the EEC Pae%x F9.103x Astra:17 Assembly Labor Nat Applicable due to engine 5./N: effectivity Engine S/N: 15449 oath ccroguratico standard 7100i-11 engraved on data plate. 61,652 MatenalS ism Charge (RolisitOyce Warta*) (Ail Operates) The intent of this Non-Modification Service BuTetin is to replete One EEC firebox assembles that have an nuttoent thickness or the evanescent pert Effecbvity: Reference Rolls.Roroe Service &ikon 80.700-73- /ROCOCO far effectivity Notes: Parts are SCheckPol and procured thrown, ROBROW:e. Pease place your order with Rob-Royce Spares six (6) months in advance arty provide yea need date so they an ensure parts avaladlty. CapOrateCare Customers affstrearn vin invoice Rolls- Royce ComordeCrre for the cherges above on the Gust:Nodsor behalf. Determination what is or is not covered the maintenance ortgram will be detamnol by Rale-Royce. My dorms not covered by the CorpaateCare pagan nil be the Custard:es Deem:relay and Subject toGuttman standard Terms an conoloons rah regard to percent. Suldrnssien of the riveKe is preocated co the CorporateCare of maintenance pager being in force at the lime stake. 3.3 Competed CannbalizeY•• duct P/N 0480402-005 from NC 5173 la NC strnmann 671, Ref: W.O. 50521837. 49.3.1 Removed to cannibalize duct P/N 04F0402•CCG 045513CR, fromNC 5173 for installation onto NC 671 Der RR Eft710 EMM 36-1145 Rev. May 15/16. Removed embalmed V- ea P/N 04F0402-005, Sill )04598CA from A/C 671 and installed kilo aigianal location an NC 5173 FUH engine per RREMM 36-11-45 Rev. May 15/16 1WIr 558135, Due- 6/18. See Stet below. 3.3.1 Convicted Removed to cannibalize 1- duct P/N 04F0402.035 sin /0459801. from NC 5173 for irate/label onto A/C 671 per RR ER710 BAH 36-1145 Rev. May 15/16 3.3.2 Convicted Install provizeusly rowed cannibalized duct P/N See Item 3.3.3 for reinstallation 04804024006 from NC 5173 for NC 671, itecieved el to install and installed pa ;REHM 36-11-45 Rev. May 15/16 3.3.3 Competed Removed tannlinaleal`b duct P/N 0480402-035, S/N 704598CR from NC 671 and rotated into onnianal location on NC 5173 RH engine per RREMM 36-1145 Rev. May 15/16 TWA 558135, Due- 6/18 3.3.4 Competed Leak deed required. Complied with leak check of Y- Ott P/N 0486932-005 on R/II engine with no leas detected per 6550 MM 36-11-6 August 31/03. 3.4 Competed "'CANCEL"' CMP 4550 890466 Meet 58 ER700.73• Cannot convey with at this time due to Darts avalabley. 56 a:sentence due by 31 /AN 2021 (38 mad remaining). A101981P3 - Irooducten of a New EEC Firebox Assembly with a Revised Pant System. Cogent, Signature: Date: APU RE220 Tochnkal Bulletins (ASC, CB, SB, AD, ACB) 5.1 COMMete0 "•CAUCEL• • 'CsIc Cs550 9/1162 ASC 1168 Nose Landing Customer elects ro alien at this bme. Gear (MS) Karnes • InstalLtecn Customs Signature' Date: ivisnoi7 6: i es Am Gulfstream Proprietary Information Pat I of1.9 EFTA00796536 Work Order: 5C521661 AC: 5173 ST/4: Charles Thomas SCC: Julian Brown Squawks: All Yellow = Newly Added Items, Green = Changed Items (Ready for inspection or completed) from previous day (or since Friday on Mondays) Assoc Status Discrepancy Resolution 6 /Monks 6.1 Completed Customer request to comp/y nth Registration change to Ref Rein 20.1 fa no* performed 112121E. Notes: Need 05< update for restrawn3 transponder etc. Pete Rawsen has ordered the wife Sri. 6.2 Watbng Customer request custom &midst be 'staled on DU. aooroval (l) Pease hold watt receipt ol Me custom ACL. 6.3 Completed Plight GLadarce Panel backichong does not Muir/rote for Sinewy: nicht 00s. Confirm NW Carved Item Renewed flight pub:lance panel (on: 7021852.901 sn: 06030509) and replaced wen repaired flight pub:lance Panel (on: 7021852.901 sn: 080130720) and performed Autopla operatenal deck with no defects noted. Ahnork done ref CMP G550 221002 item 11.10 and GSSO CMP 22100 kern 11.8. See steps baby/ fa work performed. 6.3.1 Completed Removed night gullance panel (on: 7021852.901 sn: %030509) and replaced WM repaired Pr guidance panel (pn: 7021852401 en: 08080720) with no defects noted. NI work dad per GSSO CMP 221001. Ref tern 11.8 for CMP RIM. 6.3.2 Completed Performed Auteibt operational ONNk with nodefects noted. Al work done ref CMP G550 221002 item 11.10. 6.4 Completed DU 24 mop. Swapped with DU 23 and problem (phoned. Removed defative DU and repliced nth notified DU (p.: 7028140-905 sn: 09125363) aid performed operation:1 deck with no defects noted. All work done Per 6550 CND 316024 and CMP 316030. Rel Items 11.7 and 11.9. 6.5 In Custard request to update ROAS settings. Progress 6.5.1 Completed Created one Settings and Riggrhas Der GER 5767 6.6 WAIN Customer requests to update the anhow 4000 aircraft zoomed photo wth the new blue paint sdierre and to add the (L) company logo. Logo to be worded by the Catania. Ref tern 20 1.16 7 Interior 7.1 Completed •••CANCEL•• 'Customer request to remove and replace or- Customs elects no action at this brae. SOW NW. YAM customer Selected Nees: Demon has samples for customer Customer Signature: Date: 7.2 WAN Fwd oxket door hande loose and Orals door operation. aooroval (L) 7.3 'Hsiang Lent hande for on pressure S scotching varier on as approval treSSure 000r (C8528041000) (L) Nathaniel 8.1 Completed "'VOID—Customer request to replace nose and man Otoicate Entry. REF ITEM 25.1 FOR TIRE REPLACEMENT des 8.2 Completed Replace Lil & RH Engem Cows ( to be supplied by Rots- Ref dens 2.1 & 3.1 foe wok performed Royce). Notes: Comorate Care item 8.3 In Customer request full dewing arid operatimal checks of the Progress Lavatory tank end sistan. 8.3.1 Completed Removed, cleaned, nspecte0, and reinstalled tftradOok sensors P61:7700395-001 LM SN:07.G-170]. and R/H 511:07- G-167 per CMP 380015/383024, and CMP 38(031/380032. Ref. Warns. 11.44,11.45,11.46,11.98. 8.4 Completed Customer request to irooect all exterior sense° door latches Sunny: Installed New latch P/N 145000-2•102-142 per BP 1159851110 Rev G to the external MED switch seroce for seryirstality end replace one discrepant latch en the door. Completed inspection of di sense door Latches per G550 MM 53-00-00 )une 15/16 and found no father external MED snatch prvire door diserepanes. (See steps below for a detail of work performed) 8.4.1 Completed Remtreed discrepant latch On the eternal MED switch Senkerlar Per ED 1159651110 Rev G. 8.4.2 Completed Installed New latch P/N 16000-2-102-142 per OP 1159851110 Rev G to the eternal MED swath service doer. Competed inspecdonol al exterior seroce door latches per 6550 MM 530000 Acne 15/16 and 6550 MM 5240.00 October 30/06 irking no further discrepsioes. 8.4.3 Completed Request paint onexternal MED switch Nate door die to The aircraft is getting fill Trap/paint (ref kern 13.1). The MED service {low latch wil be painted at this time. new latch Installation 8.5 Open Customer request to Cheek water system IndtatROS 8.5.1 Completed Complied with potable water tank soNix per G550 AlO4 38-1401 March 31/17. No indication on external pond noted throughout entire service. 8.6 Completed CMP G550 275019 Flap Actuator Travel Nut (Left) - COMPLIED WITH CMP G550 275019 Flap Actuator Travel Not (Left) - Lubrisabco Lubrication 8.7 Completed 04P G550275020 Rio Actuator Travel Nut (Right)- COMPLIED WITH CMP G550275020 Flap Actuator Travel NUt (Right) • tteaca0on Lubrication 8.8 Completed •••V011)•••CMP 6550 274202 Ilarnotal Stabnzer Vod - Cupleate of item 23.11. Actuator - Lubication 8.9 Completed 04P 6550 491005 PAl Embus:0 FS 767 • P5 797. Zonal COMPLIED WITH CMP G550 491005 APIA Enclosure FS 767 FS 797: Zonal InSPeCtian Inspection 8.10 Waibng Customer requests 12 spare aircraft keys. 12.15.2017 6 :lid AN Gel/stream Proprietary Information Nrc 4N:9 EFTA00796537 Work Order: SC521661 AC: 5173 STM: Charles Thomas SCC: Julian Brown Squawks: All Yellow = Newly Added Items, Green = Changed Items (Ready for inspection or completed) from previous day (or since Friday on Mondays) Assoc Status . Discrepancy Resolution approval (L) Addeddorbo debrief 811 Completed Blue R FUEL RETURN FAIL' CAS message appeared one Perknned boated fuel return operaVonal check wet no defects noted. Al work done oar 6550 AMR 28.16-00 dated rair Into Might. Crew also noted Mat the rut NI August 30. 2009. temperature was 100 degrees odour and the left al temperature was 80 degrees atm,. Decade reastcr box ID* 568366 cal due date 11/18 Added during debrief 8.12 Completed Apu enclosure ha sward corroded fasteners basted as Suninary: Removed and cleaned areas around FWD base low panel 31262F and AFT base lower panel 312A2F. errJostre base loser amen panels Replaced screws PN:M527039.0008 arid washers Rt:A/4960)08 per Droning 115%51419 Rev.L Foetid Wile On:tying AIM CMP491005 • 8.9 See steps belOw be full Stalk. 8.12.1 Completed Removed MU assembly for access to loner erdame pleb. Ref. G550 AMM 49-00-00 Rev. 2/15/15 8.12.2 COMOleted Removed FWD base lower panel 31282F and MT base lower panel 312AZF. Removed corroded hardware and began cleaning pat per Drarang 1159851419 Rev. L. 8.12.3 Completed finished demng FAD base kw panel 31283 and AFT base lower panel 312AZF Crewing 1159851419 Rev. L. 8.12.4 Completed Installed new hardware on FWD base lower panel 3128/F and AFT base loner panel 312A2F per Drawrg 1159851419 Rev. L 8.12.5 Completed Installed MU assembly FN WE3800700-1 SN - P-500 per G550 ANN 4900-00 Rev. 2/15/15. Tess 567921 due 09/18 and 562027 due 06/18 832.6 Completed Leak the* required on MU per 6550 MOM 494340 Feb 15/15. Complied welt leak died of AA) per G550 ASIM 49420-00 Feb 15/15. Received OK to dose APU panels and completed final closure. 8.13 Waiting FWD bullet faring (knee panel) ha evidence of erase" at approval fwd edge around fwd lolling contra and a puncbse Side 0.) of faring. Areas marked with blue grease pencil Ref. Item 15.1 8.13.1 [Depleted removed billet fairrg camera for faring repair LAW 60515050250 Rev 8.14 Completed Apu Enclosure has large area of dd0eded coating ReM0001al hose and crumbling sections of COOtrg per eng disco Ref Kern 8.17 be PD 2009-17-01 fwd I/h ade of apu enclosure. 8.14.1 [Depleted Request engineering disposition for MU compartment has Ref item 8.14.1.1 kr eng depo large area of nre retardant missing. 8.14.1.1 Completed Ergineerrg dspostnn: MR11 6391 The ombrig is not repairable. Remove any best a Ref 506238.20.22.1.1 bumbling seniors of coa0ng. If applicable remove Me Atemate Method of Complarce autharizaton from the arcade records. Renstate the Annorthiness Drecbm AD 2009.17-01 end eforkAFM Supplement 6550-2009-03 in accordance with the state of registry regulleMertS. 8.15 Completed "'VOID"'UH aboard hOrq.Stab. leadrg edge has torn "'VOID"' Entered In wrongNC verkOKI0e rubber seal. R0f. Paint Treed& 8.16 Completed " •VOID"'R/H irtrzerd Iell.sta0. kedIrg edge has torn "'VOID"' Entered In wrongNC workeder rubber seal. R0f. Paint Traveler 8.17 Completed 04P 6550 992902 PD 2009-17-01 Inspect/3n FOr Sealant COMPUED WITH CMP G550 992902 A0 2%9.17-01 Inspection For Sealant Applied To me DiXerlar Of The Aollary Applied To The Exterior a The Auxilary Paver Unt (APU) Power Urn (APU)Erdoare ErKIOSure. PrevlOuSly templed vnth in Log Book EMI, dated 08/18/09. Ref 8.14.1 erg dspo for remstaong AD 2009-17-I Verified AFM Supplement 050-2009-03 was incorportated into the MM 8.18 Completed Wing body fairing XICOI seYmrKi In done not Mate at panel Renewed and rePtXed diSCMpant dome nutplate Pit: NAS1474A3 on 004.0/W PK 1199652017.41 and instated doubler 19648 aft of wing as marked with tape. per GAC DWG 1159852017 Rev 6. REF 13.1.1 8.18.1 Completed Removed discrepant dome nutpeate PV: NAS1474A3 from doubler Pit: 1159652017.41 per GAC DWG 11591352017 Rev 6. 8.18.2 Completed Installed dame nutPlae 11A514740 on doubler PM: 1159852017.41 and installed doubler. Back sea% elottler and nutplate. Work done per GAC DWG 1159852017 Rev B. 8.19 Waiting Cyan 'MU Mart Reamed' Cas message on MU start. DC approval fault code 4922222APU (APU Row Cevider Sir Short) (L) Ref tern 8.12 8.19.1 Completed Gained access to 181A1P1 ( on APU Goers). Dsoonnected pug, Inspected and cleaned came, plug with no defects noted. Returned aircraft to angered cafgurabco. All OUVOSIMIXC performed song WWI 49-60-00 June 15/16. 8.20 Completed during panel 196A$ nstalation noticed were somrg Installed nuts, ate PM: MAS1474A3 per GAC DWG 1159652017 Rev 8. freely. Marked with tape 12, 15,2017 6.21.0S AM Gulfstream Proprietary Information NeeSNW EFTA00796538 Work Order: 5C521661 AC: 5173 STM: Charks Thomas SCC: Julian Brown Squawks: All Yellow = Newly Added Items Green = Changed Items (Ready for inspection or completed) from previous day (or since Friday on Mondays) Assoc Status I Diserepaney ReerWiliOn Ref kern 8.18 821 Compiete1 R/H elevator trim tab upper surface nas 3 areas of possible Strnmarr. Removed CI Omar urn tab PM: 1159C552095-423 5/Il: 373. Cleaned. pepped and repaired all Wee deaamnWon. Rd. Item 13.1 surface discrepancies. Reference Engineering *%O. in SOW 8.21.3. Installed Fuls eievator ten tab Pitt 1159352095-423 S/N: 373 Ref. DIP GSSO 273024 Items 11.56 See correspondrg steps for detals of work performed. 1W 560349 Cal 12/2017 8.21.1 Completed Removed R/H elevator trim tab FIN: 1159C582095-423 S/N: 373 per OW4550 273024. Ref. Item 11.56 8.212 Completed NOT Inspection mowed on marked SPOt NOT performed Tap test inspection on R/H elevator trim tab upper surface per GAC AIDTP 2.1 rev 7 09/16/2015 No relevant incicabons noted at MS tele 8.213 Completed Engineerng Cispouton for three surface discrepanoes: Refer to Steps 1 thna 6. I. Solent dean the three areas using dean cheesecloth weer, wet wen HoproPil Alcohol. Continue until rapers 'then dean. Do not use synthetc or shop toted wiper ~torah. 2. $4 all wee locations sand ON surroundng paint using • tamde paper anti a solid paint base exist. 3. At the two locations next to the grandrog jumpers carefully sand off the dry fit cloth to expose the carbon pir. Do not Leger art nto carton Alms. TraOSS« Claret remaining wein the rattle snail be acceptable. 1. Heat areas sp to 120 to 140F for at least 20 minutes. After reacting this lolo time and while heat is WI berg apeled, surface wet areas wen Epon 828/ DTA (GAC I ISAA2 GAC117G1 respectlx<v). S. Renacne heat source and :plow surface ta air mol to room temperature. Phalan at 70 to 95F trail the attache gels MaKII slop take dace after 4 hr,. 6. Na other action required shoe NC mil be undergoing repaint. This is inn, repay. MR8 NO. E064 8.21.4 Completed Rhea cleaned tie tree discrepant areas. At all three locations sailed off surrounding paint. At the two batons reed to the mounting jumpers carefuly sanded off the dry F/G Mtn to expose the carbon ply. Heated areas to 120 to 140F tor at least 20 minutes Solace coated areas with Epan 828 / DTA (GAC11SAA2 / GAC117G1 respectively). Reference ergineerrg dsposstion in step 8.213 821.5 Completed Installed R/H elevator blm tab P/N: 115%552095423 S/N: 373 per RIP 6550 273024. Ref. IS 11.561W 560348 Cal 12/2017 8.22 ritteg Horizontal stabiles R/II hoist plug stopped. aP)rosel Ref. 13.1 (L) 8.23 Completed ull Flap Traded 1/8 Roller is worn beyond lints per Replaced NI %pi? Triads Mt I/B Roller with new roller, P/N KRF233012FT, LAW CIP G550275037 and Drawing 6550 MIM 273000 Rev. march 31117 1159055420 Rev G Ref. 13.2 8.24 Completed MI flap Track Aft I/O Roller is worn beyond Imes per Sirrimay: Removed Rill Flap 'V Traded outboard bracket Replaced NH Flap 11' Track AR 1/B it with new 6550 AMM 27.5000 Rev. MarCh 31/17 roller, FIN XRF233012FT. Installed R/H Flap 'Er Track Mt aboard bracket. Work performed per ChIP 6550 275038 and Draning 1159C554220 Reg G. Ref. 13.2 See steps below far detakd week performed. 8.24.1 Completed RemOved R/H Rart TraCk Mt outboard bracket Replaced WH Nap Traded 1/8 Wier with nor role, P/N 80233012Ft per DIP GSSO 275038 and Drawing 11591354220 Rev G 8.242 Completed Redved ok to Install and Instated R/H Flap Track "V AFT OM roller ntting. Bolts Still require torque and fang rewires sealant per 1159C554220 Rev G. 8.243 Completed Oct require torque and fang requires sealant per Torpred toOltS On fitting and sealed per 1159C5524220 Rev. G 1159(554220 Rev G. Torque Wrench* 558039 CAL: 08/ 18 825 Completed R/H Hap track 0/8 roller bracket for track has shipped Upon further imestigaton round R/H Flap Track B' 0/8 ROter Bracket hardware to be stepped and ~rates are out tolts. bot roles/nutplates may require clearing out. functioning property_ Instated and torqued NEW hardware per 2741-05 Rev. November 15117. Ref/ism 8.24 826 In While conveying wit paint strip lund dar in right fuselage Progress at GYPS 694.000, skin P/N 115%51316. Impression is approximately C wide by r high and .012' deep. Rel 13.1.2 8.26.1 Completed Request NDT to Chetk for cracks at discrepant area. POttrmed Eddy Current Insp.:than per GAC NOW 3.0 (REV 7 SEP 2015). No <redo noted at the bele. Equprnere Used: Hartet 5005 GACD 555039 (cal due 12/17) and SID. 560706 (no cal reg.) 6262 Open Request engineering dive for repar of dent In the right fuselage. 8.26.2.1 Completed Preliminary Engneerng Csspastten: Christa Kerby, MR81E742 I. Gain access to the Wen« Side of the dented skin Visually inspect the dscrepant area for any additional d iamaten to surroundng structure 2. Cold work the dxrcpart area per the procedures in SR 1077 to restore the skn to surrouncing contour 4/..005 irs 12/151011 6:21:0S AM Gulfstream Proprietary Information port 6 of 29 EFTA00796539 Work Order: 5C521661 AC: 5173 STM: Charles Thomas SCC: Julian Brown Squawky AS Yelloiv = Newly Added Items; Green = Changed Items (Ready for inspection or completed) from previous day (or since Friday on Mondays) Assoc Stan —al Disawanogr Resolution Dill a hde .1285-.1335 in. de. per GQIIIAL1)35G at the sharp, center part of the depress= to relieve the retard aid tartrate celd "sonde° 3. HOT the cold worked area for cracks (eddy current) and remanng matend thane's (ultrasonic). 4. Inspect the cold waked area for al canning. 5 Rea*nit results to engineers; sar evaluation. mRe4/742 9 Paint 10 Outstorialksp Parts, Materials, and / or Services 10.1 Wang Enginee rs tater aPProved (1) 10.2 Wattles, Back Ordered PartS approval (L) 10.3 Waiting Pats Return a0Orcwar a.) 11 Follow on CMP Codes / Maintenance Tasks 11.1 Completed CmP 6550 711001 Inlet Cool (Left) Remota I Instaltstian COMPLIED WITH CMP 6550 711001 Inlet Coal (Left) - Remard / Installation TW 558064 Cal: 08/1E Rel. 2.1 11.2 Completed CMP 6550 711002 Inlet Coal (Right). Removal / COMPLIED WITH CMP 6550 711002 Inlet Carl (Right) - Removal f Instalaten Installation TW:557274 Cal Due: 06/18 Ref. 3.1 1V(:557259 Cal Due: 03/18 11.3 Waiting CMP 6550 7110190ml Door, Engine Lower (Left) (I.)0(04 Rel. Item 2.1 11.4 Waiting CMP 6550 711020 Engine Loner Carl Door (Part) - approval Removal f Instalatian 0.1 Rel. Item 3.1 11.5 Wattles, CMP 6550 711021 Upper Cowl Door (Left) Rerrograli approval Installation (L) Ref. Han 2.1 11.6 Comokte0 04P 6550 711022 Upper Cowl Door (Right) • Rerno4 COMPLIED WITH CMP G550 711022 Upper Cowl Door (Right) - Removal InetallatiOn InetallatiOn Ref. item 3.1 Torque Virendies used: 557274 Cal die 06/18 557259Cal due 03/18 1I.7 COmOlne0 04P G550 316024 DISPLAY UNIT, a4 Ref 64 COMPLIED WITH CMP G550 316024 DISPLAY I.X4IT, x4 pn off: 7028140-901 PO on: 7028140-905 sn oft 07092716 sn ore 09125363 11.8 Completed CMP G550 221001 PANEL, (LIGHT GUIDANCOGP-500) Rd COMPLIED WITH CMP 6550 221001 PANEL, FLIGHT GU@VICE(GPS00) 63 Po OlflOn: 7021852-901 sn off: 06030509 sn an: 090130720 1I.9 Completed CMP 6550 316030 CENTRAL DISPLAY SYS - AD)/TEST Ref COMPLIED WITH CMP G550 316030 CElfIRM. DISPLAY SYS - ADJ/TEST 11.7 11.10 Completed 04P G550 221002 AUTOPILOT—OPERATIONAL TEST Ref COMPLIED MTh [MP 6550 221002 AUTOPILOT—OPERATICNAL TEST 11.8 11.11 Waiting 04P G550 330901 SWITCH PANEL xl (48251) COMPLIED WITH CMP G550 330901 SWITCH PANEL 11 approval (VEST. SW PHL) (L) 11.12 Waiting 04P G550 330930 SWITCH PANEL X30 (60157) COMPLIED WITH CMP G550 330930 SWITCH PANEL 130 00rOyal (t/H DIVAN AFT ARM SW PHL) (L) 11.13 Waiting CMP G5S0 330935 SWITCH PANEL 135 (601510) COMPLIED WITH CMP 6550 330935 SWITCH PANEL ar3S a00rOyal (R/H SEAT 93) a.) 11.14 /long CMP G550 330924 SWITCH PANEL 124 (601511) COMPLIED WITH CMP 6550 330924 SWITCH PANEL 124 Wowed (1) (VH SEAT al SW MIL) 11.15 Waren, 04P G550 330904 SWITCH PANEL X4 (59651) COMPLIED WITH CMP G550 330904 SWITCH PANEL xe Wowed (1) (FWD LAV SW PNL) 11.16 Wang CMP G550 330925 SWITCH PANEt. X25 (60153) COMPLIED WITH CMP G550 330925 SWITCH PANEL 125 angrOyal (L) (Lill SEAT *3 SW PftL) 11.17 Waiting 04P 6550 330942 SWITCH PANEL 142 (69652) COMPLIED WITH CMP G550 330942 SWITCH PANEL : 42 angrOyal (L) (AFT LAV SW PHL) 11.18 Waiano 04P G550 330938 SWITOI PAHO. 138 (601512) COMPLIED WITH CMP 6550 330938 SWITCH PANEL 138 angrOyal a.) ( I4 DIVAN LEDGE FWD StY PM) 11.19 Waiano 04P G550 330936 SWITCH PANEL 136 (601511) COMPLIED WITH CMP 6550 330936 SWITCH PANEL 136 approval (1.1 (WI4 DIVAN FWD ARM SW PHL) 12, M2011 agIDS AM Gulfs:beam Proprietary Information Nos, of 29 EFTA00796540 Work Order: SC521661 AC: 5173 STAN: Charles Thomas SCC: Julian Brown Squawks: All Yellow = Newly Added Items, Green = Changed Items (Ready for inspection or completed) from previous day (or since Friday on Mondays) Assoc Status DIsaspancy Resolution 11.20 Waibng CMP GSSO 330905 SWITOI PANEL IS (59652) COMPLIED WITH CMP GSSO 330905 SWITCH PANEL 15 aPoroyal (FWD IAV SW PHL) 11.21 Walarg 04P 6550 330940 SWITCH PANEL X40 (57153) COMPLIED WITH CMP 6550 330940 SWITCH PANEL # 4.0 aPoroyal (L) (ENT CABINET SW PHI) 11.22 Walarg CMP 6550 330928 SWITCH PANEL 128 (60155) COMPLIED WITH CMP 6550 330928 SWITCH PANEL :28 aCIProyal (L) (Ull DIVAN LEDGE FWD SW PM) 11.2