EFTA00796563.pdf

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 Resoludon 1 airfnmeGuirstreeas GSSO 1.1 ',WAN Return To Service al:OrOY4 1.2 In IntoundfOutbaurd Impectnn FrotYrds 1.2.1 Completed IntOundtPrellminary IIMDECti3n Complied with Intoundrivellminary Inspection as per RSQCT 57 rev 24 1.2.2 Open Outbound IngoteU0n 1.3 Waiting Preflight Inspection Complied with creflight impectlon as outlined in RSQCT-113 Rev. 23 approval a.) 1.4 Completed CoraPN with Petrie( Oncklat Complied with Debrief drecklaL 1.4.1 Completed ArriyaVDebref 90 Day De List Review ACCCOWielle 1.4.2 Completed List Cs:orator's Airworthiness Requirements &Simnel Part 91.409 f(3). No other spe0al ckaimentation requests. Documentadon RequeStS 1.5 Waiting Tool Clearance Provided tod clearer= per SOP 1028, all teals eanunted for alnroyal 0.1 1.6 Completed Cover & Protect Covered and PIOteCted as required 1.7 Completed Service Channel Toilet/0ton Galley Told serviced JAW the ground Fending and servicing handbock 14-00-00 Id Completed AfrivaVDeParkre ASSISI & ,Ade0Mot 00mPlete WM interior Inbotrel InSPeCtianGA 3564 (CG) 5/17 and oleo 1.9 Completed Sample RIO-attic Fluids Compiled with Sample Myra-al/lc Ru105 1.10 Completed Remote Valuables & Secure. Secured by customer icon arrival 1.11 Completed Comply with Service Team Manager CheckIst Complied with Service Team Manager Chectist 1.12 Completed Fluids Used (011s/9wdroll • (Materials OrrY) Informalfon Cnly. 1.13 Completed STM Quality review 0l work order and ke/b00k entry CriOr Compiled wile SIN Quality review 0l work order and tobook entry griOr to decorate to departure 1.14 Completed Towing (Does not include Hangar Mores) Tonto as required 1.15 Completed Hazmat - Identey &provide a manifest, and a SritnerS N/A no hatmdt to be loaded. Declaration for Darger0us GOOCIS for all bawdous materials that are loaded aboard any airaaR. FAR Fin 1210r 135 gaeratOrs x111 piovile a hazardous material notinatein letter reputed by FAR 135.505 (e) pax to mantereree at Ohs Repair Station kw FAR 145.206 (a) (b). If there b to be loading of hazardous matelots t shall be complied with by llama trained autheized GAC cern:noel only. 1.16 YMOn9 Moan Donn) alnroval (L) 1.16.1 Open CLEMING LAMING GEAR FCC PAINT 1.17 Completed ConsumaNes & Shop Staples For NUM purposes on,F. LIE Waiting Major Alterations regulatory comp/ante requirements to be approval completed by instaler ea imitated on FM tam 8100-9. 0.1 Copy and paste from attached statements as needed and ern as required. COMPLY WITH REQUIREMENTS OF FAR 25.1301(a) (0). 25.1353(a) and 25.1431(c) (d). COMFUED WITH THE REQUIREMENTS OF FAR 251301(a) (P). 25.1353(a) and 25.1431(0) (d), via GROJIND TEST REPORT-REPORT Ho. CEJO(x%g0f% REV. ), ( IN SUPPORT CS STC )3COCCOM ) and GR4R216.4 REPAIR STATION INTERFERENCE TESTING REQUIREMENTS F057 MAJOR ALTERATIONS COMPUANCE FORM. COMPLY WITH REQUIREMENTS OF FAR 25.1529, INSTRUCTIONS FOR CONTINUED AIRWORTHINESS REF X/C00( MANUAL, P/N %/OW= REV. X, FOR INSTRUCTIONS FOR CONTINUED AIRWORTHINESSAHD EILOCX 8 CC FM FORM 337, DATED )0(/XXIXXXX COMPLY WITH THE WIRE ROUTING REQUIREMENTS OF FM POLICY MM-01-04 MO 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, OIMGE 1CHAPTER 11, SECTION 8. 1.19 WalOn9 Update WCi a Seance approval (1) 1.20 Waiting faience Pant and Were & Etakree Requirements. approval II 500)' 6.21.01AM Gulfstream Proprietary Information Part I N:o EFTA00796563 Work Order: 5C521661 AC: 5173 STM: Chalks Thomas SCC: Julian Brown &pawls All Yellow = Newly Added Items Green = Changed Items (Ready for inspection or completed) from nylons day (or since Friday on Mondays) Assoc Stalin Discrepant/ (1) Reveal scope or aircraft sealer pant totehspftepars, and dtin reptxements reviling in paint reappliatios, and determine area on stir and batanCe. For surfaces :Akre pant is stripped and reapplied or added co top of existing pant on an area greater than 36 square feet the thickness values AO be documented before and after painting . If average oldness %glues remain the seam wore and baba reeincri b net required. For surfaces painted wed an area greater than 36 square feet and before and alter cent thickness average vanes. QC review for pasoble weight end ttlance revision will be regAred. • Thames wit be plottedon an aircraft droning denved from AMM chapter 6 a-other subtle Mach, attached to the week Order and meaStrensantS taken on a two equate foal god. • Reference GAMS 4000, paragraph 3.5.1 for paint restnclicns to fight wird surfaces and RVSM certified aircraft • Reference CAMPS 4000, total average tNduias shed not exceed 6 mils. • Per GAC Mass Properties Engineering, pant thickness of mis equSs .055 pounds per squre foot. Varear QC review, weight change is greater than 2 pounds or .05% of IIAC, the weight and balance report repine rearnaitaton. 1.21 Waiting &exert Ready for Renato Service. At reamed approval inspectsans, to in64e preflirt ropectoss, maintenance (L) tasks, operational & leak checks, related doraimercaocet and deanna activeescompl0te. Contact Realm to Service group when tNs swank is complied with. 1.22 Completed Advise customer of preservation requirements per ATA Advised customer of °ogre and API) preservation requirements. Chapter 10 01 the releant maintenance manuals fa Arframe, Engines, ad MU; review requirements in relation to schedUal Date Po:rimed and later pctental Date Completed; and perform maintenarce or pesovato+ actions as directed by the CuStOmer and documented as a Work Order Squant. 1.23 Completed Pre-Compliance cabn refurbeshment nspecten Complied with Pre-Compliance Sin regsbishment ropecton per 14 CFR part 25. NOTE: SEE APPENDIX 1.29 Completed 04P GSSO 010010-Serree Cater Maintenance !tam Complied with CMP GSSO 010010-know Center Maintenance DIMS= Cheddist Oleddig 1.25 In Comply with lot Codot and Hoe Cabin Progress 1.25.1 Completed Carroty with intend Hat Cockpit LAW RSQCT-26S 0.er-I Complied with inbound Hat Cockpit LAW RSQCT-265 Rev-I 1.252 Completed cow, with MOWN Hot Caton JAW RSQCT-219 Rawl Complied With In0Xeld HOt Cabin JAW PSIZCf:219 Rev-2 1.25.3 Open cow, with outbound Hot Oxkplt LAW RSQCT-265 Rent 1.25.4 Open Comply with citbeund Hot Cabin LAW fISQCT-219 Rev-2 1.26 WaiOng Remand aircraft laps and bag and scared in Seen aPPrOval 9tranSOWS office. 1.27 WaiOng Sales Concesocn appal (1) MODE DR700..7100F31 2.1 Completed Remove LH engne nose cowl and replace with Rots Royce Summary: Removed VII Eng. loaner inlet ant PH:09C0301-019 SN:GYSPIS9 ard instated Rolls Royce provided provided exchange trat. Reference RR Newstts6h: exchange Wet cowl PH: 040/00/019 SN: GVSP13e5V per CW 711002. tiF2013.02. See steps below for detailed week prformed. 2.1.1 Completed Removed VII Eng. lamer inlet cowl PN:0K0081-019 SMGV5P159 and installed customer repated Inlet cowl PP: 04(0001-019514: GVSP134SV per 04P 711002 Ilan 11.1. Reference Rerrowi and Instdletsen Wok page IC. 2.2 Completed CMP GSSO 893131 Alert 5B1311703-73-A9C0383R1 - COMPLIED WITH CMP G550880131 Nat 58 8R700-734.900383R1 Replacement of Non-Conkrmng Parts of the EEC Replawnent d ilInCOnlomeng Part of the EEC Rebox Firebox ASSeMtly. Assembly Taber Not Applicable due to engine SSI: effecthey Only Engine S/N: 15998 with carEguraban standard 7100111 engrawd en data plate. $1,652 Motet No Charge (Rolls-Royce Warranty) (All Cperatas) The intent of this haorbiecclification Service Buletin Is to replace ben EEC firebox assembles that have an inefficient thickness of the retroescent psnt. Effectivity: Reference Rolls.Royce Serra Butetin 80.700-73- x988883 fa effeCtMty Notes: 12/11,011 6:11:03AM Gutfstream Proprietary Information No: EFTA00796564 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 &heckled arid procured theeurob ReffRoyce. Reese place your crow with Ret-Rote Spares sa (6) months m advance and ROMP 'MO need date SO they Can endure parts at:0406:m. CameatcCem Detentes: Cuirstrern viii rrerace Rao. Royce CaparateCare for the three abate en the Custom's behalf. Determination wnat is of is not covered under the mentenzae program will be detenratO by RaluRcyce. My charge, net coated by the CorpoiateCare aceram mll be the Custemsoz rammibilty and %Mast to Gulfs-Cream's standard Terms and Conditons with regard to payment. Sutirressen dl the mote 6 Fecicated on the CorparateCare maintenance program tang in (Dice at the doe a service. 2.3 Completed "'CANCEL"' 04P G550 880466 Alert 58 68700.73• Cannot convey with at this time due to Darts avalabley. $6 emplane due by 31 /AN 2021 (38 rnos remairing). A101981R3 - Irecductico of a New EEC Firebox Assembly nab a Revised Pant System. Customer Ssanatuie: Date: hi ENGINE SA700-71001-11 3.1 Carpkted Rearm NI crane ncee cent and replace with Rots Rate Summary: Removed Rill Eng. boner inlet tea 68040001-020 SN:GYSP171 and installed Rolls Royce provided Pavided enchange tot. Reference RR Newsflast exchange Wet cowl PH: 04C0031-020 SN: G139 Der 04P 711002. NF2013.02. See steps below for detailed work portent& 3.1.1 Canpleted Removed NH Eng. Ceres inlet awl RY:060001-020 SN:GY5P171 and Inetall&I cuRorra offered Inlet cowl PN: 040:031420 SN: 6139 per CMP 711002 Item I I.2 3.2 Canalised CMP G5.50 893131Men SB BR703-73-6907383R1 - COMPLIED WITH CMP e3550 890131 Net 58 BR700-736.900003R1 - Replacement of Nan-Confo-miog Pens of the EEC nepiaonnent of NanConromMts Parts of the EEC Pae%x F9.103x Amend& Assembly Labor Nat Applicable due to engine 5./N: effectivity Engine SM: 15449 ?nth ccroduratico standard 7100i-11 engraved on data plate. 61,652 MatenalS No Charge (RolisitOyce Warranty) (M Operates) The intent of this Non-Modification Service BuTetin is to replace One EEC firebox assembles that have an nuttoent thickness or the evanescent pert Effecbvity: Reference Rolls.Rome Service &ikon 80.700-73- /ROCOCO far effectivity Notes: Parts are theckPol and procured thrown, ROI/Re/CO Pease place your order with Rob-Royce Spares six (6) months in advance arty provide yaw need date so they an enSure parts avaladlty. CapOrateCare Customers affstrearn vin invoice Rolls- Royce Camera-Gore for the cherges above on the Gusts:rods or behalf. Determination what is or is not covered the ym nce ortgram will be detamnol Si RedivRace. M dorms not covered by the CorpaateCare pagan nil be the Custard:es rapcnsibilty and Subject tO Guttman standard rerms and conoloons rah regard to Pareent. Subrnssien of the mode is pralcated on the CorporateCare maintenance pager Ming in force at the bine of scake. 3.3 Competed Cannbalize Y. duct P/N 0480402-005 from NC 5173 la NC strnmann 671, Ref: W.O. 50521837. 49.3.1 Removed to cannibalize 7- duct P/N 04F0402•CCG sin 045513CR, fromNC 5173 for installation onto NC 671 Der RR Eft710 EMM 36-1145 Rev. May 15/16 Removed annbaltred1- Ott P/N 04F0402-005, SM XY4598CR Nam A/C 671 and installed kilo aigianal location an NC 5173 FUH engine per RREMM 36-11-45 Rae. May 15/16 /WA 558135, Due- 6/18. See Stet below. 3.3.1 Convicted Rowed to cannibalize 1- duct P/N 04F0402:035 sin /0459801. from NC 5173 for irate/label onto A/C 671 per RR ER710 DIM 36-1145 Rev. May 15/16 3.3.2 Convicted Install prerbusly renewed cannibalized 1- duct PM See Item 3.3.3 for reinstallation 04804024006 from NC 5173 for NC 671, itecieved dl to install and installed pa PREMM 36-11-45 Rev. May 15/16 3.3.3 Competed Removed tannitialeed 1: duct P/N 0480402-035, SM 704598CR rron: 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 Med( required. Complied with leak check of Y- Ott P/N 0486932-005 on R/II engine with no leas detected per G550 MM 36-11-6 August 31/03. 3.4 Competed "'CANCEL"' CMP 4550 890466 Mert 58 68700.73• Cannot convey with at this time due to Darts avalabley. 56 a:sentence due by 31 /AN 2021 (38 rnOS remairing). Ali/1981R3 - Irooductico 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 InstalLtico Customer Signature' Date: tdrisrzoi7 6:19:01Am Gulfstream Proprietary Information Pat I of29 EFTA00796565 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 :ILO AN Gel/stream Proprietary Information Nrc 4N:9 EFTA00796566 Work Order: SCS21661 AC: 5173 STM: Charles Thomas SCC: Julian Brown Squawks: AD Yellow = Newly Added Items. Green = Changed Items (Ready for inspection or completed) from previous day (or since Friday on Mondays) Assoc stews i DIsexpanot ReeokidOn approwi (L) addedduring debrief 611 Completed Blue 'R FUEL RETURN FAIL' CAS message appeared One Performed heated fuel return memorial check with no defects noted. Al work done per 6550 AMM 28.16-00 dated tour min eight. Crew Aso toted dilettante oil August 30. 2009. temperature was 100 degrees Mous and the left al temeerature was 80 degrees eel:M. Decade resistor box IDe 569366 cal due date 11/18 Added Oaring (letrk4 8.12 Completed Apu endceure has several corroded fasteners bated on Sunurvey: Removed and cleaned areas mond FWD base lave panel 31282F and MT base lower panel 312A2F. encloare base loner access panels Replaced screws PN:MS27039.0609 and washers PN:M1960.108 per Drawing 1159851419 Rev.L Fou4 wile COmPlying with ChIP 491085 * 8.9 See steps below tor full details. 8.12.1 Completed Removed APU asserrbg (Cr access to beer enclosure ps.eb. Ref. GSSO AMM 49e0-00 Rev. 2/15/15 8.122 Completed Removed FWD base rower panel 31282F and AFT base lower panel 312A2F. Removed COrnged hardware and began cleaning panels per Dossing //59851419 Rey. L. 8.12.3 Completed Finished cleanng PhD base lower pond 31282E andMT base lower panel 312A2F Pawing 1159851019 Rev. L. 8.12.4 Completed Installed new hardware on FWD base lower panel 31285 and AFT base lower ps.el 312A2F per Doming /159851419 Rev. L 6.12.5 Completed Installed AM assembly FR • WE38007001 5N • P.500 per 6550 AMM 490060 Rev. 2/15/15. Thies 567921 due O%18 and 562027 due 06/18 6.12.6 Completed Leak died required on MU per 6550 AMM 494300 Feb 15/15. Complied nets leak check of MO per G550 AMM 49-0043 Feb 15/15. Received OK to dose APU panels and completed foal dome. 8.13 Waiting FWD bullet faring (knee panel) ha evidence of erasion at Marmot fwd edge around fwd looking camera and a puncbse reside (1.) of fairing. Areas marked with OW grease Pence Ref. Item 15.1 8.13.1 Ccepleted removed bullet farm camera for faring repair LAW GC515050250 Rev - 8.10 COS Ape Enclosure has large area of distaded coating Removed at Rose and crumtling sections ct COOtlna per eng dep. Ref item 8.17 for PD 2009.17-01 on fwd bh sde of ape endosure. 8.14.1 Completed Request engineering dmosition for APU canpartment has Ref item 8.14.1.1 for eng dope large area 01 fire retardare misprg. 8.14.1.1 Completed Engineern.g dsposton: MRS 891 The coatng it net repairable. Remove any loose or Ref 506238.2022.1.1 mumbling sections of coahng. If applicable remove the ARemate Melva oil Complence authonzaton horn the aircraft records. Reinstate the krnorthiness Orectiye AD 2009-17-01 and op* MM Supplement GS50-2009-03 in accordance with the State Of registry reduirernerts. 8.15 Completed "NOID"IL/Il intgaid roriz.stab. leadre edge has tan "'VOID"' Entered In wrong MC wOrkOrcler rubber sat Rel. Paint Traveler 8.16 Completed " 'VOIDwIrdhl irtgard heriz.stab. Wog edge has torn "'VOID"' Entered In wrong A/C wOrkOrcler rubber seal. Ref. Paint Traveler 8.17 COS OIP 6550 992902 PD 2009-17-01 InsPeChan For Sealant COMPLIED WITH ChiP G550 992902 AD 2039.1741 IrciPeCtiOn Per Sealant Applied To The Exterior Cf The Auxhary Applied To The Exterior Of The Auxthiry loner Out (APU) Ironer Unt (APU) Enclosure ErsCIOSure previougy compiled with in Log Book Entry dated 08/18/09. Ref 8.14.1 erg dspo for remstabng AD 2009.17-1 Veiled KM Sumkment G550-2009-03 was incorportated etc the MM 8.18 COS Wing body faking grew SOWN in dome nut pate at panel Removed and mowed discrepant dome nutdate Ph' NA51474A3 on dottier Phi: 115965201741 and installed doubler 196.48 an 01 wing as marked with tape. per GAC DWG 115%52017 Rev B. REF 13.1.1 8.18.1 Completed Removed discrepant dome r ate PN: NASMINIA3 from Malec PN: 1159852017-11 pa GAC DWG 1159852017 Rey 6. 8.18.2 Completed Install% dome netPlate Par liA514703 On doubler PH: 1159852017.41 and Entailed doubler. Bads Seale/0000er and nu/plate. Week clone per GAC DWG 1159852017 Rev B. 8.19 Waiting Cytn 'AEU Mane Rennet Cm message on APU start. CMC approval fault code 4922222APU (MU ROw Ceeklet SP Short) (L) Ref tens 112 8.19.1 Completed Gained access to 181A1P1 (oh APU Celina). Disconnected pito, inspected and cleaned cannon plug with nO defects noted. Returned Mat to wird confgurabon. MI reverters:me performed tang V/C61 4940-00 June 15/16. 8.20 Completed during panel 196AB nstatation noticed glen spmirg Installed nub:gate PH: ILASI47413 per GAC DWG 1159652017 Rev B. freely. MarkedWM tape IVISROI7 6:2I:01AM Gal/stream Proprietary InformatIon Nee < of 29 EFTA00796567 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 6:21:03AM Gulfstream Proprietary Information port 6 of 29 EFTA00796568 Work Order: 5C521661 AC: 5173 STM: Charles Thomas SCC: Julian Brown squawky Ail Yellow = Newly Added Items Green = Changed Items (Ready for inspection or completed) from nylons day (or since Friday on Mondays) Assoc Stows Dbcrepano, Resokidon COO a Isle .1285-.133$ in. do. per GQIIIAL1)35G at the mare, center part of the depressen to rebore the metered and laelltatecolO 8oritMg. 3 HOT the cob oorked area for cracks (eddy current) anti rernaring materiel tidiness (t Heinle). 4. Inspect the cold worked wee for al caring. 5. Reo.bmIt results to ergamerno for evaluation. mResE742 Paint Outsesnelkm Parts, Materials, and / or Services WalOn0 enineern.3 later cfMrowd (1) 102 Waltin) Back Ordered Parts 407001 (L) 10.3 Waiting Pats Return aP0rovai a.) 11 Follow on CMP Codes / Maintenance Tasks 11.1 Carpleted CMP 6550 711001 Inlet Coal (Left) Removal / Installation COMPLIED WITH CMP 6550 711001 Inlet anti (Left) - Remard / Installation TW 558064 Cal: 08/18 Ref. 2.1 11.2 Completed 04P 6550 711002 Inlet Cowl (Right) Removal / COMPLIED WITH CMP 6550 711002 Inlet OrA1 (Right) - Removal f Instalation Ins0lU9on TW:557274 Cal Cue: 06/18 Ref. 3.1 1V(:557259 Cal Cue: 03/18 11.3 Waiting CMP G550 711019 Coral Door, Engine Lower (Left) 400001 Rel. 'tern 2.1 0.1 11.4 Waiting CMP G550 711020 fore Loner Carl Door (RIM) - Motored Removal f Instalation (1) Ref. 'tern 3.1 11.5 Waling 04P 6550 711021 Upper Cowl Door (Left) Removal/ Motored Installation (1) Ref. item 2.1 11.6 Competed CMP 6550 711022 Upper Cowl Door (Right) • RefrOYN COMPLIED WITH CMP G550 711022 Upper Cowl Door (Right) - RECAMMI Installation Installation Ref. item 3.1 Torque Wrenches used: 557274 Cal die 06/18 557259Cal due 03/18 117 CO0101ete0 OW G550 316024 DISPLAY UNIT, x4 Ref 64 COMPLIED WITH ChIP G550 316024 DISPLAY LIMIT, et on off: 7028140-901 pn on: 7028140-905 sn oft 07092716 sn on: 09125363 11.8 Cc n Ieted CMP G550 221001 PANEL, (LIGHT GUIDANCE(GP-500) Rd COMPLIED win' CMP GSSO 221001 PANEL, FLIGHT GUIGVICE(GP500) 63 pn Ott/00: 7021852-901 sn off. 06030509 sn on: 08080720 11.9 Competed CMP G550 316030 CENTRAL DISPLAY SYS - AM/TEST Ref COMPLIED WITH CMP G550 316030 CEIGRAI. DISPLAY SYS - ADJ/TEST 11.7 11.10 Completed 04P G550 221002 AUTOPILOT-OPERATIONAL TEST Rd COMPLIED WITH CMP 6550 221002 AUTOPILOT- OPERATICNA1 TEST 11,8 11.11 Wang OW G550 330901 SWITCH PANEL x1 (46251) COMPLIED WITH CMP G550 330901 SWITCH PANEL xl approval (VEST. SW PM) (L) 11.12 Wafting CMP G550 330930 SWITCH PANEL x30 (60157) COMPLIED WITH CMP G550 330930 SWITCH PANEL x30 40004 (t/H DIVAN AFT ARM SW PNL) (L) 11.13 Waiting CMP GSSO 330935 SWITCH PANEL 13S (601510) COMPLIED Willi CMP 6550 330935 SWITCH PANEL 135 400001 (WH SEAT ET) (l) 11.14 intiano 04P G5S0 330924 SWITCH PANEL 124 (601511) COMPLIED WITH CMP 6550 330924 SWITCH PANEL 124 Wowed (1) (t/H SEAT 915V MIL) !Lis Waiting OW G550 330904 SWITCH EMEI. T4 (59651) COMPLIED WITH CMP G550 330904 SWITCH PANEL xs approval (1) (FWD LAY SW PNL) 11.16 Wang CMP G550 330925 SWITCH PAM% :25 (60153) COMPLIED WITH CMP G550 330925 SWITCH PANEL :25 a— (L) (VII SEAT *3 SW PNL) 11.17 Waiting CMP 6550 330942 SWITCH PANEL x42 (69652) COMPLIED WITH CMP 6550 330942 SWITCH PANEL TAT 400(04 (L) (AFT LAY SW PNL) 11.18 Waiting 04P G550 330938 SWITCH PANEL 138 (601512) COMPLIED WITH CMP 6550 330938 SWITCH PANEL 138 a00Nval 0.1 (RAI DIVAN LEDGE FWD 51Y PM) 11.19 Waiting 04P 6550 330936 SWITCH PANEL 136 (601511) COMPLIED WITH CMP 6550 330936 SWITCH PANEL 136 Wowed (1) (RAI DIVAN FWD ARM SW PRO 12.M2017 6':2103 AM Gulfstream Proprietary Information Pays 0129 EFTA00796569 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 prevtous day (or since Friday on Mondays) Assoc Status ( DIsaapancy Raolutlon 11.20 Waiting CMP 6550 330905 SWITCH PANEL xS (59652) COMPLIED WITH CMP GSSO 330905 SWITCH PANEL #5 alowerral 0.) (FWD IAV SW PAL) 11.21 Wan) 04P G550 330940 SWITCH PANEL 440 (57153) COMPLIED WITH CMP 6550 330940 SWITCH PANEL 440 Wowed (L) (ENT CABINET SW PML) 11.22 KAMAN 04P 6550 330928 SWITCH PANEL 425 (60155) COMPLIED WITH CMP 6550 330926 SWITCH PANEL 428 a00rOvy (L) (UV DIVAN LEDGE FWD SW Ptti.) 11.23 WalOrg CMP 6550 330927 SWITCH PANB. 427 (60154) COMPLIED WITH CMP 6550 330927 SWITCH PANEL 427 a00rovy (L) (Ull DIVAN FWD MM SW PHL) 11.24 Waiting CMP GSSO 330943 SWITCH PANEL x43 (69653) COMPLIED WITH CMP 6550 330943 SWITCH PANEL x43 a00rovy (l) (AFT LAP SW PAL) 11.25 Waiting CMP G5S0 330933 SWITCH RANA. e33 (