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FBI VOL00009
EFTA00811141
64 pages
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Bill To: Plan D, LLC. WO #: SC52166I Invoice Number: 5517132452 Discrepancy: 23.34 CMP G550 262620 Portable Halon Fire Extinguisher (Aft Cabin) - Removal / Installation Resolution: EOMPLIED WITH CMP G550 262620 Portable Halon Fire Extinguisher (Aft Cabin) - Removal / Installation Billing Method Hours Rate Total Pans USD: Time and Material S3.15 Total USD: S3.15 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 2334 MI 14776 STRAP AND CLAMP ASSY 1 $3.15 $3.15 Discrepancy: 23.43 CMP G550 351222 Passenger Oxygen Cylinder (No. 2)- Removal / Installation Resolution: COMPLIED WITH CMP G550 351222 Passenger Oxygen Cylinder (No.2)- Removal / Installation Billing Method Hours Rate Total Labor USD: No Charge NI C Pans USD: Time and Material S5.31 Total USD: S5.31 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 23.43 in hIS21044C08 NUT SELF LKG-CRES.PASS1VATED 1 $0.41 $0.41 23.43 62 hIS21044C3 NUT 1 $4.90 $4.90 Item: 24 Discrepancies related to Miscellaneous CMPTasks (Exhibit 3) - (Ref. Item C 13 of Proposal ID# 7039702 ROO) Team Manager: Customer Coordinator: Charles Thomas Julian Brown ParttModcl AC Serial No/Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: Discrepancy: 24.3 2 Bruce Batts failed cap check and require replacement. Refer to items 31.1 and 33.1. Resolution: Ordered and recieved New Bruce Batts. Ref Items 23.35 and 23.37 Billing Method Hours Rate Total Pans USD: Time and Material $2,810.64 Total USD: $2,810.64 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 243 #1 2013-BR BATTERY. EMERGENCY LIGHTS 2 51,40532 $2,810.64 Discrepancy: 24.4 (1) passanger 02 mask has a broken valve and (1) passenger 02 mask has a broken lanyard. Ref 23.44 Resolution: Removed and replaced (2ea.) o2 masks. PN On/Off: 289-601-224-1 Ref. G550 Atom 35-25-01 dated June 15,2016 Billing Method Hours Rate Total Labor USD: Time and Material ST 6.50 (t! 5146.00 S949.00 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). riAC_RevenueSquawksInvoicc.rpt v3 Page 41 of 64 Printed: 3/7/2018 3:15:05PM tit W. EFTA00811181
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Bill To: Plan D, LLC. WO #: SC52166I Invoice Number: 5517132452 Pans USD: Time and Material $159.46 Total USD: $1,108.46 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 24.4 #1 289-601-224-I MASK 2 579.73 S159.46 Discrepancy: 24.5 One light bulb from "No smoking" light on cabin PSU #5 LI1 and One light bulb from "No smoking" light on cabin PSU #1 RH did not illuminate during test Ref. 23.44 Resolution: Removed and replaced light bulb from "No smoking" light on cabin PSU #5 LH and light bulb from "No smoking" light on cabin PSU #1 RH. Ops ck good. PN on/off GE387 Parts USD: Total USD: Pans: Billing Method Hours Rate Total Time and Material $3.50 $3.50 Ref. No. Pan number: Description Quantity Sell price USD Extended USD 24.5 #1 GE387 BULBS/A GE387 10 5035 $3.50 Item: 25 Replace all Main and Nose tires - (Ref. Item C 1.5 of Proposal ID# 7039702 ROO) Team Manager: Customer Coordinator Charles Thomas Julian Brown Pan/Model AC Serial NoJTail No.: TSN/TSO: CSNJCSO: Aircraft Time: Discrepancy: 25.1 Remove and Replace all main and nose landing gear tires. Resolution: Summary: Removed all MLC wheel assemblies (4ea.) and NI.0 (2ea.) and routed to back shop for lire changes and NUT. reference items 34,35,36,37,38 and 39 for work performed in the back shop. Received wheels after tire change and installed on aircraft, Reference items 11.58 thru 11.61 for NILC wheel assembly WI CMPs and 11.93 and 11.94 for NLG w heel ass). R/I CMPs See steps below Billing Method Hours Rate fowl Labor USD: Flat Rate 52.686.00 Pans USD: Flat Rate 515.350.00 Total USD: 518,036.00 Step: 25.1.1 Completed Removed main wheels (4) and routed to back shop. Ref items 11.58 thru 11.61 Step: 25.1.2 Completed Removed nose wheels per 6550 CNIP 324001 and G550 CMP 324002 and routed to back shop for tire replacement. Step: 25.1.3 Completed Installed red wheels on NLG per AMM 6550 32-41-01 rev 3131/17 TW: 560296 Cal Due: 04/18 Step: 25.1.4 Completed Removed IJH and R/H NLG red wheels. Received ok to install and Installed L/H NLG Wheel Assy P/N 1159150400-37 SiN 508117 per CMP 6550 324002. Received ok to install and installed R/H NLG Wheel Assy P/N 1159/50400-37 S/N 508217 per ChIP 6550 324003. Serviced 14/H and R/H NIG Wheels to 120PS1 per 6550 AMM 12-33-01 Rev. June 20/13. Step: 25.1.5 Completed Installed main wheels (4) IAW 6550 CMPs 324003.324004.324005. and 324006. Ref items 11.58 thru 11.61 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). GAC_RevenueSquawksInvoiceept v3 Page 42 of 64 Printed: 3/7/2018 3:15:05PM tit W. EFTA00811182
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Bill To: Plan D, LLC. WO 1r: SC521661 Invoice Number: 5517132452 Rem: 26 CUSTOMER PROPERTY OUT TO VENDOR Team Manager: Customer Coordinator. Charles Thomas Julian Brown S/N: N/A TSWISO: N/A CSN/CSO: N/A Aircraft Time: N/A Discrepancy: 26.1 SEND BLOW DOWN BOTTLE TO SUPPLIER FOR HYDROSTATIC TEST AND RETURN TO AIRCRAFT CUSTOMER PROPERTY AC 5173 TN - N415LM REQUESTED RETURN DATE - 11/9 Resolution: Recleved Blow Down Bottle Billing Method Hours Rate Total Services USD: Flat Rate 5270.60 Total USD: 5270.60 Services: Ref. No. Description Quantity 26.1 41 HYDROSTATIC TEST Part Ref: 1159SCH233-II BOTTLE, NITROGEN - BLOW DOWN BOTTLE 1.00 Discrepancy: 26.2 SEND 02 BOTTLE TO SUPPLIER TO COMPLY WITH HYDROSTATIC TEST AND RETURN TO AIRCRAFT CUSTOMER PROPERTY AC 5173 TN - N415LM REQUESTED RETURN DATE - 11/11 Resolution: Recleved O2 Bottle. Billing Method Hours Rate Total Services USD: Flat Rate 52,527.80 Total USD: 52,527.80 Services: Ref. No. Description Quantity 26.2 41 HYDROSTATIC TEST Pan Ref: 805983-IS BOTTLE, OXYGEN 1.00 Discrepancy: 26.3 SEND 02 MASK TO SUPPLIER FOR RESTORE/RECERTIFY AND RETURN TO AIRCRAFT CUSTOMER PROPERTY AC 5173 TN - N415LM REQUESTED RETURN DATE 11124 Resolution: Recleved O2 Mask Billing Method Hours Rate Total Services USD: Flat Rate 52392.50 Total USD: $2.392.50 Services: Ref. No. Descripiion Quantity 26381 REPAIR Part Ref: A1O0-15-158 MASK, OXYGEN, CREW 1.00 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). GAC_RevenueSquawksInvoice.rpt v3 Page 43 of 64 Printed: 3/7/2018 3:15:05PM tit kW EFTA00811183
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Bill To: Plan D, LLC. WON: SC521661 Invoice Number: 5517132452 Discrepancy: 26.5 SEND 18 EA LIFE VEST TO THE SUPPLIER FOR RESTORE AND RETURN TO AIRCRAFT CUSTOMER PROPERTY AC 5173 TN - N415LSI REQUESTED RETURN DATE - 2/20 PN - 63600-105 SN - L784996, L748997, L784998, L784999, L785000, L785001, L785002, L785003, L785004, L785006, L785007. L785008, L785009, L785010 AND L785011 PN - 63600-505 SN - L785711, L745141, L785710 Resolution: Received 18 each repaired life vests Billing Method Hours Rate Total Services USD: Time and Material $884.17 Total USD: 5884.17 Services: Ref. No. Description Quantity Sell Price USD Extended USD 26.5 NI REPAIR 1.00 5884.17 S884.17 Part Ref: AC5173LIFEVESTKIT LIFE VEST KIT Discrepancy: 26.6 SEND CUP HOLDERS AND DOOR HANDLE TO QUAKER CITY TO BE PLATED QCP588 SATIN BLUSHED WHITE GOLD AND RETURN TO AIRCRAFT CUSTOMER PROPERTY AC 5173 TN - N415LM REQUESTED RETURN DATE - 2/26/2018 Resolution: Received plated cup holders. 2/22/18- Per the PO in Corridor It is tracking for 2-26 confirmed by Courtney. CC Billing Method Hours Rate Total Services USD: Time and Material $1,500.00 Total USD: $1,500.00 Services: Ref. No. Description Quantity Sell Price USD Extended USD 26.6 #1 PLATING 1.00 50.00 S0.00 Part Ref: AC5173PLATINGKIT KIT 26.682 EXPEDITE FEE 1.00 $1,500.00 $1,500.00 26.683 PLATING 1.00 50.00 S0.00 Part Ref: AC5173PLATINGKIT KIT Item: 27 AIRCRAFT BATTERY (FCS EBIIA BATTERY & MAIN SHIP BATTERY) Team Manager: Charles Thomas Customer Coordinator: Julian Brown PartModcl N: 1159SCAV519-1 S/N: 0905200069DDF TSN/TS0: N/A CSN/CS0: N/A Aircraft Time: Na For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). GAC_RevenueSquawksInvoice.rpt v3 Page 44 of 64 Printed: 3/7/2018 3:15:05PM tat W. EFTA00811184
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Bill To: Plan D, LW. WO #: SC521661 Invoice Number: 5517132452 Item: 28 AVIATION BATTERY TYPE - CORE (FCS EBIIA BATTERY & MAIN SIIIP BATTERY) Team Manager: Customer Coordinator: Charles Thomas Julian Brown Pan/Model #: 5317C1I-1 S/N: 09052001067B3 TSN/TS0: N/A CSN/CS0: N/A Aircraft Time: N/A Item: 29 FAIRING ASSY, BULLET, FWD Team Manager: Customer Coordinator: Charles Thomas Julian Brown Part/Model #: 1159C51152024-405 S/N: N/A TSN/TS0: N/A CSN/CS0: N/A Aircraft Time: N/A Discrepancy: 29.1 FWD BULLET FAIRING (KNEE PANEL) HAS EVIDENCE OF EROSION AT FWD EDGE AROUND FWD EDGE AROUND FWD LOOKING CAMERA AND A PUNCTURE INSIDE OF FAIRING. AREAS !WAKED WITH BLUE GREASE PENCIL. IRAN AND RETURN TO AIRCRAFT CUSTOMER PROPERTY AC 5173 TN - N415LM REQUESTED RETURN DATE - 11/17 Resolution: Repaired satcom radome. Reference: Engineering dispo In step 29.2.1.1 and B/P 1159C51152024 Rev.D 1/17/06 Engineering dispos in steps 29.3.8 and 29.3.10. FWD BULLET Part# ->1159CS1152024-405 Seel ->NFA Final finish FAIRING will apply at service center. Billing Method Hours Rate Total Labor USD: Time and Material ST 68.78 (a $146.00 $10,041.88 Labor USD: Time and Material ST 1.02 (-a $222.00 $226.44 Pans USD: Time and Material $2,318.91 Total USD: $12,587.23 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 29.1 #1 LSSQW00-0460 LIGHTNING DIVERTER I $772.97 $772.97 29.1#2 LSSQW00-0460 LIGHTNING DIVERTER I $772.97 $772.97 29.1#3 ISSQW00-0460 LIGHTNING DIVERTER I $772.97 $772.97 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). GAC_RevenueSquawkslnvoice.rpt v3 Page 45 of 64 Printed: 3/7/2018 3:15:05PM tit kW EFTA00811185
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Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Step: 29.1.1 Completed Incoming Inspection Step: 29.1.2 Completed Teardown Step: 29.13 Completed Inspection Step: 29.1.4 Completed Rework Step: 29.1.5 Completed Assembly Step: 29.1.6 Completed Test Step: 29.1.7 Completed Refinish Step: 29.1.7.1 Completed Made Mytar Step: 29.1.7.2 Completed Apply IOP2-3 anti-static coating Step: 29.1.7.3 Completed Strip-Sand and prime with 3012 / D-8003 Hi-Bu0d.Apply 10P2-3 Anti-Static.Re-prime with 3012. Step: 29.1.7.4 Completed Apply IOP2-3 Anti-Static. Perform resistivity test. Step: 29.1.8 Completed Outgoing Imagery Discrepancy: 29.2 Erosion along the leading edge and diverter strips. Resolution: Repaired erosion along the leading edge and replaced all diverter strips. Reference: Engineering dispo in step 29.2.1.1 and B/P 1159CSII52024 Rev. D.1/17/06. Billing Method Hours Rate Total Labor USD: Time and Material ST 2.00 @ 5222.00 5444.00 Total USD: 5444.00 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). GAC_RevenueSquawksInvoice.rpt v3 Page 46 of 64 Printed: 3/7/2018 3:15:05PM tit kW EFTA00811186
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Bill To: Plan D, LLC. WO Si: SC521661 Invoice Number: 5517132452 Step: 29.2.1 Completed Request engineering evaluation for repair of erosion. Step: 29.2.1.1 Completed Engineering disposition: Remove lightning diverter and hardware as required. Sand eroded areas smooth. Scuff sand minimum 1.50in around areas to be repaired. removing all glossy surfaces, to prepare for wet lay up. Fabricate two plies using plies of 161/181sts le dry fiberglass cloth. Size plies to ensure coverage of eroded and sanded regions. Ply #1 should extend at least 1.00in beyond the reworked area and Ply #2 should extend at least .50in beyond Ply al. except plies may end at edge of part where applicable. Saturate Plies 1 and 2 with Shell Epon 828/DTA or Hysol EA956A/B mixed per manufacturer's instructions. Lay up rework areas with Ply #1 and Ply #2 ensuring adequate overlap as specified above. Cure plies under vacuum bag at 75-95°F for at least 12 hours, or under vacuum bag at 75-95°F for at 2-3 hours followed by 3 hours at 130-140°F. Remove vacuum hag and sand smooth. Visually inspect reworked area: if required. fill and fair using 11>sol EA960F and sand to contour. If required, install lightning diverter as described below. Touch up with primer and paint to match customer topcoat, as required. Lightning diverter installation: Prepare surface to be bonded per CAMPS 8210: scuff sand then solvent wipe with MEN or acetone followed by isopropyl alcohol. Apply GAA100BDI0 or GAAI00BD03 adhesive and position diverter per 1159C5H52024. Cure under vacuum bag for 7 days at room temperature, or 2-3 hours at room temperature followed by 2 hours at 130-140°F. Step: 29.2.2 Completed REMOVED PAINT/PRIMER FROM DISCREPANT FWD AREAS AND SOLVENT CLEANED. THEN FABRICATED AND INSTALLED 2 PLIES OF STYLE 181 FIBERGLASS WET USING EPON 828fDTA. VACUUM BAGGED AND CURED. REF ENGINEERING DISPO STEP 29.2.1.1 Step: 29.2.3 Completed Removed and replaced all diverter strips(P/N LSSQW00-0460). Reference: B/P 1159O:1152024 Rev. D Released I/17/06. Discrepancy: 29.3 Puncture on LAI Inner surface. Resolution: Repaired puncture on Lill Inner surface. Reference: Engineering dispos in steps 29.3.8 and 29.3.10. Billing Method Hours Rate Total Labor USD: Time and Material ST 18.00 €2; 5222.00 $3,996.00 Total USD: 53,996.00 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). GAC_RevenueSquawksInvoice.rpt v3 Page 47 of 64 Printed: 3/7/2018 3:15:05PM tat kW EFTA00811187
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Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 ( moulded Request engineering evaluation for repair of inner skin puncture. ( moult:Ertl Request NDT to perform tap test of inner skin puncture. ( moult:Ertl Preliminary Engineering Disposition: Refer to pic in the "files" tab for suspect location of contact area. Place a soft compressible material (clay, repro-rubber. etc.) that will retain location and determin if this is the contact area. Install fwd bullet fairing and attach with B/P hardware. Remove fairing and take pits of suspect contact area. Resubmit pies via Corridor to engineering for evaluation. MRB No. E064 ompleted Per preliminary engineering disposition placed a soft compressible material (repro-rubber) on the contact area. Installed fwd bullet fairing and attach with B/P hardware. Removeed fairing and took pits of suspect contact area. Resubmited pies to engineering. ompleted Preliminary Engineering Disposition: Refer to pic in the" Files" tab drill a No. 30 at the location shown. Take a measurement from the inner surface of outer skin to the outer surface of inner skin. Resubmit results to engineering for Final disposition. MRS No. F.064 Completed Resubmit engineering after measurement from the inner surface of outer skin to the outer surface of inner skin is .240" Completed Preliminary Engineering Disposition: Refer to attachment in the "Files" tab: using the smallest clean up diameter. represented by the red dash line, trim out the discrepant section of inner skin and associated core down to the bond surface of outer skin. Do not undercut the outer skin or incorporate core ramp at this time. Measure, document, and resubmit resulting clean up dia. MRB E064 Completed Final Engineering Disposition: Rework per Steps I thru 13. NOTE. -Steps 9 thru 13 are in 29.3.9. Cutout of the inner skin and core removal is acceptable. Proceed with following rework: I. Refer to "Files" Powerpoint attachment Section A-A in 29.3.7. Incorporate core ramp that starts from edge of cutout extending .25 to .35 inches beyond cutout. At the lower EOP it is acceptable for the chamfer to extend onto the solid laminate. 2. Straighten out folded over core cells and remove loose cells. Vacuum out debris. 3. Pot core ramp with Magnobond 68-3. Cure at 70 to 95F' until potting has a harden surface. Do not touch sanded surfaces with bare hands. wear clean cotton gloves. 4. Solvent clean using fresh cheesecloth wipers wet with MEK or Isopropyl Alcohol an area extending at least 2.0 inches beyond cutout or to EOP. whichever is closer. Continue until wipers remain clean. Do not use synthetic or shop towel wiper materials. Also solvent clean a corresponding area on outer skin. 5. Sand off excess potting. Sand inner bond surface to remove core stubble and any glossy surface finish, also extend sanding around skin cutout over an area extending from lower EOP or at least 2.0 inches beyond edge of cutout to expose the outer fiberglass (F/G) ply. Vacuum out debris. Traces of paint, primer. etc. remaining within the F/G weave shall be acceptable. 6. Sand correspond outer skin surface in the same way. 7. On inner skin add two plies of dry Style 181 (F/C). Orientation of both plies is optionaL It is acceptable to dart F7G to allow working out wrinkles. Stagger darts so they do not overlap onto each other. Saturated plies with Epon 828 / DTA or EA956 MB. Refer to SRM 51-34-00 Table 1 and SRM 51078-10 Repair Technique 7. 8. Refer to Files tab in 29.3.7. Ply I shall overlap .50 to .80 inch onto the inner surface. Ply 2 shall overlap Ply 1 by .50 to .80 inches. Disposition continues in 29.3.9 MRB No. E064 Step: 29.3.9 Completed Final Engineering Disposition Continued from 29.3.8. 9. On outer surface add like plies centered over cutout. 10. Install a breather pack and vacuum bag. refer to SRM51-78-10 Repair Technique 8. Perform a vacuum leak check by pulling full vacuum (min 21 inches of Hg) until bag is pulled tight. Disconnect vacuum source and verify max leakage rate does not exceed 5 inches of Hg within 5 minutes. II. Cure at 70 to 95F until adhesive gels which should take at least 4 hours. 12. After cure remove bag and sand off excess adhesive and F7G. Tap test outer and inner skin within repair area to verify no voids and I or disbands exist. Also visually verify no ply separations exist. 13. On outer surface apply Finish 3012 (CAMPS 3116) followed by anti-static paint and customer topcoat. Ensure applied anti-static paint overlaps onto the existing anti-static paint. On inner surface no finish is required unless dry surfaces exist and if so apply Finish 3012 to entire repaired surface. This is a minor repair. MRB No. E064 Step: 293.1 Step: 293.2 Step: 2933 Step: 29.3.4 Step: 29.3.5 Step: 293.6 Step: 293.7 Step: 293.8 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). GAC_RevenueSquawksInvoice.rpt v3 Page 48 of 64 Printed: 3/7/2018 3:15:05PM tit W. EFTA00811188
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WO tr: SC521661 Invoice Number: 5517132452 Bill To: Plan D, LLC. Step: 293.10 Completed Made core ramp and potted core with Magnobond 68-3. Cured at 70 to 95F until potting has a harden surface. Solvent cleaned, sanded off excess potting. Sanded inner bond surface and extend sanded around skin cutout over an area. On inner and outer skin added two plies of dry Style 181 (FIG). Saturated plies with Epon 828 / DTA. Install vacuum bag, performed a vacuum Ink cheek and cured at 70 to 95F. After cured remove bag and sand off excess adhesive and F/6. Tap tested outer and inner skin within repair area to verified no voids and I or disbands exist. Also visually verified no ply separations exist. Work reference:Engineering dispo in steps 29.3.8 and 29.3.10. Item: 30 Addition of a SIIADE MASTER at the Right-Hand #2 VIP Seat - (Ref. Item B 1.1 of Proposal ID#7038565 ROO ) Team Manager: Customer Coordinator Charles Thomas Julian Brown Part/Model #: AC Serial No/Tail No.: TSWISO: CSN/CSO: Aircraft Time: Discrepancy: 30.2 CMP G550 330934 SWITCH PANEL #34 (Ref. 30.1) Resolution: COMPLIED WITH CUP G550 330934 SWITCH PANEL #34 PN OFF: 2501-2-110Q588A SN OFF: 31B3J PN ON: 2501-2-714Q588A SN ON: 48NOHIC Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Item 31 BATTERY, EMERGENCY LIGHTS Team Manager: Customer Coordinator Charles Thomas Julian Brown Pan/Model #: 2013-BR S/N: B8662 TSWISO: N/A CSN/CSO: N/A Aircraft Time: N/A Item: 32 BATTERY, EMERGENCY LIGHTS Team Manager: Charles Thomas Customer Coordinator: Julian Brown Part/Model #: 2013-BR S/N: B8663 TSNffSO: N/A CSN/CSO: N/A Aircraft Time: N/A Item: 33 BATTERY, EMERGENCY LIGHTS Team Manager: Customer Coordinator Charles Thomas Julian Brown Part/Modcl #: 2013-BR S/N: B8660 TSN/TSO: N/A CSN/CSO: N/A Aircraft Time: N/A Item: 34 MAIN WHEEL Team Manager: Customer Coordinator: Charles Thomas Julian Brown PartfIsiodcl #: 1159SCL503-9 S/N: 5159FX TSNEISO: N/A CSN/CSO: N/A Aircraft Time: 54022 11725 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). GAC_RevenueSquawksInvoice.rpt v3 Page 49 of 64 Printed: 3/7/2018 3:15:05PM tit W. EFTA00811189
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Bill To: Plan D, LLC. WO #: SC521681 Invoice Number: 5517132452 Item: 35 MAIN WHEEL ASSEMBLY Team Manager: Charles Thomas Customer Coordinator. Julian Brown Pan/Model #: 1159SCL503-7 S/N: 5167FP TSN/TS0: N/A CSN/CS0: N/A Aircrafaime: 5402.8 11225 Item: 36 MAIN WHEEL Team Manager: Customer Coordinator Charles Thomas Julian Brown Part/Modcl #: 1159SCL503-9 S/N: 5I75GC TSNEIS0: N/A CSN/CS0: N/A Aircraft Time: 5402.8 / 1225 Item: 37 MAIN WHEEL ASSEMBLY Team Manager: Charles Thomas Customer Coordinator: Julian Brown Pan/Model #: 1159SCL503-7 S/N: 5188FP TSNEIS0: N/A CSN/CS0: N/A Aircraft Time: 5402.8 11225 Item: 38 NOSE WHEEL/TIRE ASSEMBLY-MOUNTED 1159L50400-37 Team Manager: Customer Coordinator Charles Thomas Julian Brown Part/Modcl #: 1159SCL505-7111TD S/N: 5082FZ TSN/TS0: N/A CSN/CS0: N/A Aircraft Time: 5402.8 Item: 39 NOSE WHEEL/TIRE ASSEMBLY-MOUNTED 1159L50400-37 Team Manager: Customer Coordinator: Charles Thomas Julian Brown Part/Model #: 1159SCL505-7MTD S/N: 5081EZ TSNfIS0: N/A CSN/CS0: N/A Aircraft Time: 5402.8 Item: 40 Customer Requested Due List Items as of 02/15/18 Team Manager: Charles Thomas Customer Coordinator Julian Brown Part/Modcl #: AC Serial No/Tail No.: N/A / N/A TSWIS0: N/A CSN/CS0: Aircraft Time: N/A Discrepancy: 40.1 CMP G550 231108 Airshow 4000 Sys Components - GVI Resolution: COMPLIED WITH CMP G550 231108 Airshow 4000 Sys Components - GVI Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.2 CMP G550 231113 Securaplane 500 Components - GVI Resolution: COMPLIED WITH CMP G550 231113 Securaplane 500 Components - Billing Method I lours Rate Total Labor USD: Flat Rate $152.00 Total USD: 5152.00 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). DAC_RevenueSquawksInvoicc.rpt v3 Page 50 of 64 Printed: 3/7/2018 3:15:05PM tit kW EFTA00811190
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Bill To: Plan D, LLC. WO SC521661 Invoice Number: 5517132452 Discrepancy: 40.3 CMP G550 232158 Airshow 4000 Above Floor - Visual Inspection Resolution: COMPLIED WITH CMP G550 232158 Airshow 4000 Above Floor - Visual Inspection Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.4 CMP G550 240108 Fwd Emergency Battery - BITE / Battery Level Test Resolution: COMPLIED WITH CMP O550 240108 Fwd Emergency Battery - BITE / Battery Level Test Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.5 CMP G550 240109 Aft Emergency Battery - BITEJBattery Level Test Resolution: COMPLIED WITH ChIP G550 240109 Aft Emergency Battery - BITE! Battery Level Test Billing Method Hours Rate Total Labor USD: Flat Rate $152.00 Total USD: 5152.00 Discrepancy: 40.6 CMP G550 251006 Crew Scats Inertia Reel (Pilot) - Operational Test Resolution: cOMPLIED WITH CMP O550 251006 Crew Seats Inertia Reel (Pilot) - Operational Test Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.7 CMP G550 251007 Crew Scats Inertia Reel (Copilot) - Operational Test Resolution: cOMPLIED WITH CMP G550 251007 Crew Seats Inertia Reel (Copilot) - Operational Test Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.8 CMP G550 251008 Crew Scats Inertia Reel (Observer) - Operational Test Resolution: COMPLIED WITH CMP O550 251008 Crew Seats Inertia Reel (Observer) - Operational Test Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.9 CMP G550 251016 Crew Seat Restraints (Pilot) - Detailed Inspection Resolution: COMPLIED WITH CMP G550 251016 Crew Seat Restraints (Pilot) - Detailed Inspection Billing Method Hours Rate Total Labor USD: Flat Rate $152.00 Total USD: $152.00 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). GAC_RevenueSquawksInvoice.rpt v3 Page 51 of 64 Printed: 3/7/2018 3:15:05PM tat W. EFTA00811191
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Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Discrepancy: 40.10 CMP G550 251017 Crew Seat Restraints (Copilot) - Detailed Inspection Resolution: COMPLIED WITH CMP G550 251017 Crew Seat Restraints (Copilot) - Detailed Inspection Billing Method Hours Rate Total Labor USD: Flat Rate SI 52.00 Total USD: 5152.00 Discrepancy: 40.11 CMP G550 251018 Crew Seat Restraints (Observer) - Detailed Inspection Resolution: COMPLIED WITH CMP G550 251018 Crew Seat Restraints (Observer) - Detailed Inspection Billing Method Hours Rate Total Labor USD: Flat Rate 51 52.00 Total USD: 5152.00 Discrepancy: 40.12 CMP G550 252102 Passenger Seats Restraints - Detailed Inspection Resolution: COMPLIED WITH CMP 6550 252102 Passenger Seats Restraints - Detailed Inspection Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.13 CMP G550 252104 Passenger Seats Inertia Reels - Operational Test Resolution: COMPLIED WITH CMP G550 252104 Passenger Seats Inertia Reels - Operational Test Billing Method Hours Rate Taal Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.14 CMP G550 256019 EVAS System (Left) - Periodic Inspection Resolution: COMPLIED WITH CMP G550 256019 EVAS System (Left) - Periodic Inspection Billing Method Hours Rate Taal Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.15 CMP G550 256020 EVAS System (Right) - Periodic Inspection Resolution: COMPLIED WITH CMP G550 256020 EVAS System (Right) - Periodic Inspection Billing Method Hours Rate owl Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.16 CMP 6550 256205 Life Vest - Restore For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). GAC_RevenueSquawksInvoice.rpt v3 Page 52 of 64 Printed: 3/7/2018 3:15:05PM tat W. EFTA00811192
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Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Resolution: The Squawk for this specific task shall be signed off as " Verified compliance of CMP 256205 under vender work order number SAPO17-08768 dated Feburaury 20 2018. This documentation is for CMP data base update only - no maintenance accomplished by GAC." COMPLIED WITH ChIP G550 256205 Life Vest - Restore Life Vests Restored P/N: 63600-105 S/N :L784996 P/N: 63600-105 S/N :L784997 P/N: 63600-105 S/N :L784998 P/N: 63600-105 S/N :L784999 P/N: 63600-105 S/N :L785000 P/N: 63600-105 S/N :L785001 P/N: 63600-105 S/N :L785002 P/N: 63600-105 S/N :L785003 P/N: 63600-105 S/N :1.785004 P/N: 63600-105 SIN A.785006 P/N: 63600-105 SIN :L785007 P/N: 63600-105 SIN :L785009 P/N: 63600-105 SIN :L785010 P/N: 63600-105 S/N :L785011 Billing Method Hours Rate I oial Labor USD: Flat Rate 5304.00 Total USD: 5304.00 Discrepancy: 40.17 CMP G550 256404 Defibrillator Battery - Inspect / Check Resolution: COMPLIED WITH CMP G550 256404 Defibrillator Battery - Inspect I Check Billing Method Hours Rate Total Labor USD: Flat Rate 51 52.00 Total USD: 5152.00 Discrepancy: 40.18 CUP 6550 256407 Defibrillator Electrode Pads - Inspection Resolution: COMPLIED WITH CMP G550 256107 Defibrillator Electrode Pads - Inspection Billing Method Hours Rate Total Labor USD. Flat Rate 51 52.00 Total USD: 5152.00 Discrepancy: 40.19 •""DELETE*** ChIP G550 256438 - LIFE KIT Resolution: Equipment not installed in aircraft, customer email approving deletion is on file Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.20 ChIP G550 261302 APU (Fire) Shutdown Circuit - Operational Test Resolution: COMPLIED WITH CMP G550 261302 APU (Fire) Shutdown Circuit - Operational Test Billing Method Hours Rate Total Labor USD Flat Rate $304.00 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). GAC_RevenueSquawksInvoice.rpt v3 Page 53 of 64 Printed: 3/7/2018 3:15:05PM tit W. EFTA00811193
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Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Total USD: 5304.00 Discrepancy: 40.21 CMP G550 262122 Engine and APU Fire Extinguishing Firing Circuitry (Left Engine) - Integrity Test Resolution: COMPLIED WITH CMP G550 262122 Engine and APU Fire Extinguishing Firing Circuitry (Left Engine) - Integrity Test multlmeter 556315 due date:9/18 Billing Method Hours Rate Total Labor USD: Flat Rate 5228.00 Total USD: 5228.00 Discrepancy: 40.22 CMP G550 262123 Engine and APU Fire Extinguishing Firing Circuitry (Right Engine) - Integrity Test Resolution: COMPLIED WITH CMP G550 262123 Engine and APU Fire Extinguishing Firing Circuitry (Right Engine) - Integrity Test multlmeter 556315 due date:9/18 Billing Method Hours Rate Total Labor USD: Flat Rate 5304.00 Total USD: 5304.00 Discrepancy: 40.23 CMP G550 262124 Engine Fire Bottle Pressure Switch (Left) - Operational Test Resolution: COMPLIED WITH CMP G550 262124 Engine Fire Bottle Pressure Switch (Leib- Operational Test Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.24 CMP G550 262125 Engine Fire Bottle Pressure Switch (Right) - Operational Test Resolution: COMPLIED WITH CMP G550 262125 Engine Fire Bottle Pressure Switch (Right) - Operational Test Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.25 CMP G550 262126 Engine and APU Fire Extinguishing Firing Circuitry (API) - Integrity Test Resolution: COMPLIED WITH CMP G550 262126 Engine and APU Fire Extinguishing Firing Circuitry (APU) - Integrity Test multimeter 556315 due date:9/18 Billing Method Hours Rate -lotal Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.26 CMP 6550 262605 Portable I lalon Fire Extinguisher (Cockpit) - Visual Inspection Resolution: COMPLIED WITH CMP G550 262605 Portable Halon Fire Extinguisher (Cockpit) - Visual Inspection For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). riAC_RevenueSquawksInvoice.rpt v3 Page 54 of 64 Printed: 3/7/2018 3:15:05PM rut ma EFTA00811194
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Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: $152.00 Discrepancy: 40.27 CMP 6550 262626 Portable union Fire Extinguisher (Aft Cabin) - Visual Inspection Resolution: COMPLIED WITH CMP 6550 262626 Portable Haien Fire Extinguisher (Aft Cabin) - Visual Inspection Billing Method Hours Rate Total Labor USD: Flat Rate $152.00 Total USD: $152.00 Discrepancy: 40.28 CMP 6550 262646 Portable I lalon Fire Extinguisher (Aft Lavatory) - Visual Inspection Resolution: COMPLIED WITH Cup G550 262646 Portable Halton Fire Extinguisher (Aft Lavatory) - Visual Inspection Billing Method Hours Rate Total Labor USD: Flat Rate $152.00 Total USD: $152.00 Discrepancy: 40.29 CMP 6550 271011 Aileron Control and Trim Cables in Main Wheel Wells! Wing hailing Edge - Detailed Inspection Resolution: COMPLIED WITH CMP G550 271011 Aileron Control and Trim Cables in Main Wheel Wells / Wing Trailing Edge - Detailed Inspection Tensiometer 66853 Due Date 5/18 Billing Method Hours Rate Total Labor USD: Ma Rate $304.00 Total USD: $304.00 Discrepancy: 40.30 CMP G550 272108 Rudder Control and Trim Cables in Main Wheel Well / Tail Compartment - Detailed Inspection Resolution: COMPLIED WITH CUP G550 272108 Rudder Control and Trim Cables in Main Wheel Well / Tail Compartment - Detailed Inspection Billing Method I lours Rate Total Labor USD: Flat Rate $304.00 Total USD: 5304.00 Discrepancy: 40.31 CMP G550 273100 ELEVITRIM CABLE(6IVVW/TAIL)-INSP Resolution: COMPLIED WITH CMP G550 273100 ELEV/TRIM CABLE(MWW/TAIL)-INSP Billing Method Hours Rate Total Labor USD: Flat Rate $912.00 Total USD: $912.00 Discrepancy: 40.32 CMP G550 276105 SPEEDBRAKE CABLE(111WW/WING)INSP For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). GAC_RevenueSquawksInvoice.rpt v3 Page 55 of 64 Printed: 3/7/2018 3:15:05PM tat W. EFTA00811195
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Bill To: Plan D, LLC. WO /I: SC521661 Invoice Number: 5517132452 Resolution: COMPLIED WITH CMP G550 276105 SPEEDBRAICECABLE(MWW/WING)INSP Tensiometer 66853 Due Date 05/18 Billing Method Flours Rate Total Labor USD Flat Rate $912.00 Total USD: $912.00 Discrepancy: 4033 CMP 6550 282606 Engine Feed Dual Wall Fuel Line (Left) - Detailed Inspection Resolution: COMPLIED WITH CMP G550 282606 Engine Feed Dual Wall Fuel Line (Left) - Detailed Inspection Billing Method Hours Rate Total Labor USD: Flat Rate $152.00 Total USD: $152.00 Discrepancy: 4034 CMP 6550 282607 Engine Feed Dual Wall Fuel Line (Right) - Detailed Inspection Resolution: COMPLIED WITH CMP G550 282607 Engine Feed Dual Wall Fuel Line (Right) - Detailed Inspection Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 4035 CMP O550 282608 APU Feed Dual Wall Fuel Line - Detailed Inspection Resolution: COMPLIED WITH CMP G550 282608 APU Feed Dual Wall Fuel Line - Detailed Inspection Billing Method Hours Rate Total Labor USD: Flat Rate $152.00 Total USD: $152.00 Discrepancy: 4036 CMP G550 282609 Engine heated Return Feed Dual Wall Fuel Line (Left) - Detailed Inspection Resolution: COMPLIED WITH CMP 6550 282609 Engine Heated Return Feed Dual Wall Fuel Line (Left) - Detailed Inspection Billing Method Hours Rate Total Labor USD: Flat Rate $152.00 Total USD: $152.00 Discrepancy: 4037 CMP G550 282610 Engine Heated Return Feed Dual Wall Fuel Line (Right) - Detailed Inspection Resolution: COMPLIED WITH CMP 6550 282610 Engine I kated Return Feed Dual Wall Fuel Line (Right) - Detailed Inspection Billing Method I lours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 4038 CMP G550 282629 Engine Fuel Shut-off Valve (Left) - Operational Check Resolution: COMPLIED WITH ChIP G550 282629 Engine Fuel Shut-off Valve (Left) - Operational Check Billing Method Hours Rate Total Labor USD Flat Rate 5152.00 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). GAC_RevenueSquawksInvoice.rpt v3 Page 56 of 64 Printed: 3/7/2018 3:15:05PM tat W. EFTA00811196
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Bill To: Plan D, LLC. Total USD: WO #: SC521661 Invoice Number: 5517132452 $152.00 Discrepancy: 40.39 CMP G550 282630 Engine Fuel Shut-off Valve (Right) - Operational Check Resolution: COMPLIED WITH CMP G550 282630 Engine Fuel Shut-off Valve (Right) - Operational Check Billing Method Hours Ratc Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.40 CMP G550 291501 Hydraulic System Shut-off Valve (Left) - Operational Test Resolution: COMPLIED WITH CMP G550 291501 Hydraulic System Shut-off Valve (Left) - Operational Test Billing Method Hours Rate Total Labor USD: Flat Rate 5304.00 Total USD: 5304.00 Discrepancy: 40.41 CMP G550 291502 Hydraulic System Shut-off Valve (Right) - Operational Test Resolution: COMPLIED WITH CMP G550 291502 Hydraulic System Shut-off Valve (Right) - Operational Test Billing Method Hours Rate Total Labor USD: Flat Rate 5304.00 Total USD: $304.00 Discrepancy: 40.42 CMP G550 313002 DFDR - Functional Test Resolution: COMPLIED WITH CMP 6550 313002 DFDR - Functional Test See step below for details of work performed. Billing Method Hours Ratc Total Labor USD: Flat Rate $608.00 Total USD: $608.00 Step: 40.42.1 Completed Comply with FDR data report from download a% placed on thumbdrne Discrepancy: 40.43 CMP G550 316205 FDR FAIL MESSAGE-OPS TEST Resolution: COMPLIED WITH CMP G550 316205 FDR FAIL MESSAGE-OPS TEST Billing Method Hours Rate Total Labor USD: Flat Rate $76.00 Total USD: $76.00 Discrepancy: 40.44 CMP 6550 319013 Red Disk Honeywell! Jeppesen - Aerospace, Communication, Navigation Data, (28 Day Interval) Resolution: COMPLIED WITH CMP 6550 319013 Red Disk Honeywell I Jeppesen - Aerospace, Communication, Navigation Data. (28 Day Interval) Expires: 28Nlar2018 Billing Method Hours Rate -total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). GAC_RevenueSquawksInvoice.rpt v3 Page 57 of 64 Printed: 3/7/2018 3:15:05PM tit W. EFTA00811197
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Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Discrepancy: 40.45 CMP 6550 319014 Blue Disk Honeywell / Jeppesen - Electronic Terminal Charts, Geopolitical Boundaries, Airport Information Obstacle Data (14 Day Interval) Resolution: COMPLIED WITH ChIP G550 319014 Blue Disk Honeywell / Jeppesen - Electronic Terminal Charts, Geopolitical Boundaries, Airport Information Obstacle Data (14 Day Interval) Expires: 14Mar2018 Billing Method flours Rate Total Labor USD Fiat Rate $152.00 Total USD: $152.00 Discrepancy: 40.46 CMP G550 319016 Green Disk Honeywell! Jeppesen - Terrain Data (On condition or Six Month Interval) Resolution: COMPLIED WITH CMP G550 319016 Green Disk Honeywell / Jeppesen - Terrain Data (On condition or Six Month Interval) Billing Method Hours Rate Taal Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.47 CMP G550 321005 Main Landing Gear (Left) - Lubrication Resolution: COMPLIED WITH CMP G550 321005 Main Landing Gear (Left) - Lubrication Labor USD: Billing Method Hours Rate Taal Flat Rate 5304.00 Total USD: 5304.00 Discrepancy: 40.48 CMP G550 321006 Main Landing Gear (Right) - Lubrication Resolution: COMPLIED WITH CMP G550 321006 Main Landing Gear (Right) - Lubrication Billing Method Hours Rate Total Labor USD: Flat Rate 5304.00 Total USD: 5304.00 Discrepancy: 40.49 CMP G550 322004 Nose Landing Gear - Lubrication Resolution: COMPLIED WITH CMP G550 322004 Nose Landing Gear - Lubrication Billing Method Hours Rate Total Labor USD: Flat Rate $304.00 Total USD: $304.00 Discrepancy: 40.50 CMP 6550 322306 Nose Landing Gear Bungee - Lubrication Resolution: COMPLIED WITH CMP G550 322306 Nose Landing Gear Bungee - Lubrication Billing Method Hours Rate Total Labor USD: FM Rate $456.00 Total USD: $456.00 Discrepancy: 40.51 CMP G550 323037 Main Landing Gear Bungee (Left) - Lubrication For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). GAC_RevenueSquawksInvoice.rpt v3 Page 58 of 64 Printed: 3/7/2018 3:15:05PM tut Me EFTA00811198
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Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Resolution: COMPLIED WITH CMP 6550 323037 Main Landing Gear Bungee (Left) - Lubrication TW 568539 Due 2/19 TW 567919 Due 01/19 Billing Method Hours Rate Total Labor USD: Flat Rate 5456.00 Total USD: 5456.00 Discrepancy: 40.52 CMP 6550 323038 Main Landing Gear Bungee (Right) - Lubrication Resolution: COMPLIED WITH CMP 6550 323038 Main Landing Gear Bungee (Right) - Lubrication TW 568539 Due 2/19 TW 567919 Due 01/19 Billing Method Hours Rate Total Labor USD: Flat Rate $608.00 Total USD: $608.00 Discrepancy: 40.53 CMP G550 325202 Nose Wheel Steering Collar Assembly! Slave Gear - Lubrication Resolution: COMPLIED WITH CMP G550 325202 Nose Wheel Steering Collar Assembly / Slave Gear - Lubrication Billing Method Hours Rate Total Labor USD: Flat Rate $76.00 Total USD: $76.00 Discrepancy: 40.54 CMP G550 491007 APU Enclosure Thermal Blanket I Coating - General Visual Inspection Resolution: COMPLIED WITH ChIP G550 491007 APU Enclosure Thermal Blanket / Coating - General Visual Inspection Reference items 8.14 and 8.17 Billing Method Hours Rate Total Labor USD: Flat Rate Parts USD: Time and Material Total USD: Pans: Ref. No. Pan number: $760.00 510.45 $770.45 Quantity Sell price USD Extended USD 40.54 MI NAS1580C3T12 BOLT 52.09 $10.45 Discrepancy: 40.55 CMP 6550 491300 APU Compartment Drain Collectors - General Visual Inspection Resolution: COMPLIED WITH CMP G550 491300 APU Compartment Drain Collectors - General Visual Inspection Billing Method Hours Rate Total Labor USD: Flat Rate $304.00 Total USD: $304.00 Discrepancy: 40.56 CMP 6550 491301 Auxiliary Power Unit Turbine Plenum Drains - Operational Test For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). riAC_RevenueSquawksInvoice.rpt v3 Page 59 of 64 Printed: 3/7/2018 3:15:05PM tat W. EFTA00811199
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Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Resolution: COMPLIED WITH CMP G550 491301 Auxiliary Power Unit Tbrbine Plenum Drains - Operational Test Billing Method Hours Rate Total Labor USD: Flat Rate 5456.00 Total USD: 5456.00 Discrepancy: 40.57 CMP G550 523003 Baggage Compartment Door Seal - Detailed Inspection Resolution: COMPLIED WITH ChIP G550 523003 Baggage Compartment Door Seal - Detailed Inspection Air Regulator: 556959 Cal Due:06/I8. Billing Method Hours Rate Total Labor USD: Flat Rate $608.00 Total USD: $608.00 Discrepancy: 40.58 CMP G550 523004 Baggage Compartment Door Seal Air Supply Moisture Drain Orifice - Detailed Inspection Resolution: cOMPLIED WITH CMP 6550 523004 Baggage Compartment Door Seal Air Supply Moisture Drain Orifice - Detailed Inspection Labor USD: Billing Method Hours Rate Total Flat Rate 5304.00 Total USD: 5304.00 Discrepancy: 40.59 CMP G550 523008 Baggage Door Seal Check Valve - Operational Test Resolution: COMPLIED WITH CMP G550 523008 Baggage Door Seal Check Valve - Operational Test Ale Regulator: 556959 Cal Due: 06/18. Billing Method Hours Rate Total Labor USD: Flat Rate $456.00 Total USD: $456.00 Discrepancy: 40.60 CMP G550 527001 Main Entrance Door Secondary Handle Lock Switch and Circuitry - Operational Test Resolution: COMPLIED WITH CMP 6550 527001 Main Entrance Door Secondary Handle Lock Switch and Circuitry - Operational Test Billing Method Hours Rate Total Labor USD: Flat Rate 5912.00 Total USD: 5912.00 Discrepancy: 40.61 CMP G550 531005 External Lower Fuselage FS -4 thru FS 758 View From Ground - Zonal Inspection Resolution: COMPLIED WITH CMP G550 531005 External Lower Fuselage FS -4 thru FS 758 View From Ground - Zonal Inspection Billing Method Hours Rate total Labor USD: Flat Rate 5304.00 Total USD: 5304.00 Discrepancy: 40.62 CMP 6550 531055 Aft Cabin Below Floor FS 632 - FS 684 - Zonal Inspection For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). GAC_RevenuaquawksInvoice.rpt v3 Page 60 of 64 Printed: 3/7/2018 3:15:05PM tat W. EFTA00811200