DS9 Document EFTA01122767

1E MI BY/B1/ON A GENERAL DYNAMICS COMPANY Tel: (618) 646.8000 ) Jet Aviation St. Louis, Inc. Fax: (618 646-8852 Remit To 24611 NETWORK PLACE CHICAGO, IL 60673-1246 Customer HYPERION AIR 3800 SOUTHERN BLVD SUITE 204 WEST PALM BEACH, FL 33406 PHONE M 561-317-3082 FAX/OTHM Work Order Invoice Invoice Information Invoice No: T00122 Pg. 1 invoice Date: 3/24/11 ColDivILoc 0 3- 0 20 - 1 LCII/DP#My/rDraN D 28 T Aircraft Information AIRCRAFT REG/N#: 909JE MAKE: GULFSTREAM MODEL: II SERIAL: 151 TTime: PRELIMINARY WO Nbr Terms Date In Completed Purchase Order Customer T00122 C.O. D. 2/26/11 HYPEA THIS IS A PRELIMINARY INVOICE ONLY -- VERBIAGE AND DOLLAR AMOUNTS ARE SUBJECT TO CHANGE DUE TO AIRCRAFT STILL IN WORK AND PURCHASE ORDERS BEING INCOMPLETE. 1 Comply with preliminary inspection.: Completed inspection for areas to be worked. *LABOR* CUSTOMER LABOR: ITEM 1 TOTAL AMOUNT: 2 Main inverter intermittent.: Unable to duplicate discrepancy at this time. After 1 hr and several buss xfers. Rechecked ops of inverter unabled to duplicate discrepancy. No further action to be taken. *LABOR* .00 ** .00 545.02 * ITEM 2 TOTAL AMOUNT: 545.02 3 Master warning/caution on copilots side is only "dim" on cancel button.: Observed discrepancy as copilots glareshield master warn light and master caution lights and dim all the time. Unable to match wiring found at lights to any GAC WDM CH 33 or 31 wiring diagram at this time. Waiting for custom out fitter drawings for BKM box installation. Noted that no dwg found for red master warn sw light. Removed glareshield cover and equipment for access to wiring to * *CONTINUED* PROT0 1E MI HYMN A GENERAL DYNAMICS COMPANY Tel: (618) 646-8000 Fax: (618) 646-8852 PRELIMINARY Invoice Date: 3/24/11 ColDivlLoc 0 3 - 0 2 0 -1 LCIUDPR/Ty/pDLN D 28 T Pg. 2 physically run the wires from master warn sw and to access wires at back of switch. Found one loose broken solder joint on open caution switch. Repaired solder joint but did not fix problem. Continued looking into wiring at pilot and copilot annunciator. Found more soldering at annunciators . Resolder, no change. Compared voltages between pilots and copilots annunciators. Found that pin 1 has 28 vdc and pin 2 is the control bright/dim voltage pulse to annunciation. Pilot voltage level changed with brt/dim control. Copilots pin did not. Voltage pulse was at 14-16 volts DC. This control pulse is from BKM box. Gained access to BKM box. Found to bad nutplates on close out panel unable to remove screws. Screws were drilled out. Removed BKM box, called Gulfstream for availability. Received drawing showing interface of BKM box to master warn annunciation. Verified wiring good. Reference M12604-307 for nutplate replacement. Placed BKM serviceable unit on order. Reinstalled remaining screws. Removed from lower edge of glareshield cover. Installed repaired exchange BKM unit, master caution panel and fwd left pedestal closeout. Upon performing operation check found that now the copilot amber caution light is inop will not test. Removed top of glareshield to access disconnect for copilot warn red and caution amber lights and tried to ring lamp to disconnect. Found lamp common to be open. Removed pilot and copilot comp/warn panels and course HDG panels and glareshield itself for access to lamps. Found diode CR234 to be broken. Ordered new diode. Received new diode and installed TAW GAC WDM dwg 37-51-00. Reinstalled glareshield with left and right master warn/caution lights. Ops checked TAW GAC AMM 33-01-01. No defects noted. Reinstalled all removed equipment and panels. *PARTS* PART NUMBER/DESCRIPTION UM QTY LIST AMOUNT PLT1.5M-M EA 100 .07 7.00 TY WRAP PLT2I-M EA 50 .09 4.50 TY WRAP RTV108 EA 1 8.79 8.79 SEALANT T38F-C FT 6 1.10 6.60 SPIROBAND 9BJE53 EA 2 180.00 360.00 DIODE CUSTOMER PARTS: 386.89 * ****CONTINUED**** PROT1 117 RIR= A GENERAL DYNAMICS COMPANY Tel: (618) 646-8000 *LABOR* PRELIMINARY Pg. 3 invoice Date: 3/24/11 ColDiv/Loc 0 3 - 0 2 0 - 1 LC#/DP#/TY/PDLN D 28 T 4,261.99 ITEM 3 TOTAL AMOUNT: 4,648.88 ** 4 Inboard seat at table motor inop. Check reset button.: Investigated inboard seat chair swivel release not working. Verified voltage to chair disconnect. Found circuit breakers under LH double seat (inboard). One circuit breaker tripped. Reset CB. Operate chair and noticed wiring was chafed between entry tube at the base of the chair. Wire was shorting causing CB to pop. Removed both vest holders under both chairs to get better access and bottom seat cushions. During inspection of vest holder noticed unit was pushed up too close to bottom of chair base causing chair base to move hard and causing wiring to chafe. Made record of existing wiring that was chafed. Removed chafed wiring that was burning thru chair pivot axel. Made a new wire harness with extra chafing protection and ops checked the chair swivel release with no defects noted. Reinstalled the removed equipment. *PARTS* PART NUMBER/DESCRIPTION UM QTY LIST AMOUNT ABMS-A-D EA 6 .62 3.72 BASE ACRCO5NEB FT 3 .71 2.13 SLEEVING SIZE 5 ATUM-1/4-0 FT 4 4.14 16.56 SHRINK TUBE PBLK1.00H FT 1 .52 .52 VELCRO PBLK1.001 FT 1 .52 .52 VELCRO 1000-501-D R EA 1 2760.00 2760.00 BKM BOX SERIAL 1 701 31880 EA 1 .23 .23 14 RED TERMINAL 8-31890-1 EA 4 .20 .80 TERMINAL 8-36152-1 EA 4 .20 .80 TERMINAL 8-36154-1 EA 4 .23 .92 TERMINAL CUSTOMER PARTS: 2,786.20 * * •**CONTINUED• PROT2 1E HI NW= A GENERAL DYNAMICS COMPANY Tol: (618) 646.8000 PRELIMINARY *LABOR* Invoice No: 100122 Pg. 4 Invoice Date: 3/24/11 Co/Div/Loc 03-020-1 Lci/DPVTY/PDLN D 28 T 855.61 ITEM 4 TOTAL AMOUNT: 3,641.81 5 Static ports on LH and RH plugged.: Gained access to static tees and disconnected at station 193. Ref ASC 377 for GIIB acft. Purged pilots, copilots and stby. Found some debris. However alternate static was completely clogged. Even with 20 psig per acft MM (GIIB 34-01-00) no movement of any air flow. Troubleshot to alternate static line on RH side of acft to static port. After several times, finally able to get debris in RH alternate static to loosen evidence of insect debris. However airflow between LH and RH alternate static ports was still very much restricted. Disconnected tee at top of cabin for alternate static. Finished removing debris from RH alt static line. LH alternate static at first had low air flow at 20 psig then completely stopped. Many attempts failed to loosen debris in LH alt static line, and then blew out. Found old pieces of static adapter seal lodged in alt static LH. Removed all debris from ASC377 static lines stby/alt pilot/copilot. Reconnected ASC377 tees to acft static system. Have not checked pitot/static for leaks or operation at this time. Complied with functional ops check of pitot/static system by completing the reconnect check alt static check and standby pitot/static leak check, CMPS 3410145, 341048, 341026, 341027 and 341034. *PARTS* PART NUMBER/DESCRIPTION UM 770-3FRD EA INSULATION TAPE *LABOR* ITEM 5 6 Update FMS.: Pilot declines at this time. ITEM 6 7 Pilot altitude hold seems to be controlled from copilot's altimeter. (verify if correct).: Research alt hold operations per GAC dwg CE21134005 block diagram and GAC AFMS CE21134M001 the alt preselector/auto pilot operations for alt, hold will come from the copilots alt via IS&S DADC. No further action to be taken. QTY LIST AMOUNT 1 100.46 100.46 CUSTOMER PARTS: 100.46 * 4,686.24 * TOTAL AMOUNT: 4,786.70 ** TOTAL AMOUNT: .00 ** a • *CONTINUED* PROT3 it MI MAHON A GENERAL DYNAMICS COMPANY Tel: (618) 646-8000 PRELIMINARY *LABOR* Pg. 5 Invoice Date: 3/24/11 ColDivILoc 03-020-1 Lott/Mt/Tv/Row D 28 T 424.83 * ITEM 7 TOTAL AMOUNT: 424.83 ** 8 Ill nav radio head has digits inop on certain numbers.: Removed 91 nav control panel for repair. Installed *1 nay cntrl head IAW AC 43.13 general practices. Reference 8130 for control head corrections. Ops checked IAW AMM GIIB CH 34. *PARTS* PART NUMBER/DESCRIPTION UM QTY LIST AMOUNT 629-7597-014 EA 4 1.58 6.32 SET SCREW 634-3312-001 EA 1 76.92 76.92 FILTER *LABOR* CUSTOMER PARTS: 83.24 * 587.86 * ITEM 8 TOTAL AMOUNT: 671.10 ** 9 RH glareshield flood light has broken terminal.: Removed bad ground terminal for RH glareshield flood light. Replaced terminal and reattached IAW AC 43.13.1B. *LABOR* 10 Cockpit and cabin bulb sweep *LABOR* 999 59.50 * ITEM 9 TOTAL AMOUNT: 59.50 ** 872.00 * ITEM 10 TOTAL AMOUNT: 872.00 ** THIS IS A PRELIMINARY INVOICE ONLY -- VERBIAGE AND DOLLAR AMOUNTS ARE SUBJECT TO CHANGE DUE TO AIRCRAFT STILL IN WORK AND PURCHASE ORDERS BEING INCOMPLETE. ITEM 999 TOTAL AMOUNT: * * * *CONTINUED* .00 ** PROT4 JET A GENERAL DYNAMICS COMPANY Tel: (618) 646-8000 PRELIMINARY TOTAL PARTS: 3,356.79 TOTAL LABOR: 12,293.05 TOTAL OTHER SERVICES: .00 TOTAL SHIPPING/HANDLING CHGS.: 352.12 TOTAL SURCHARGE: 368.79 PAY THIS AMOUNT(USD) 16,370.75 Pg. 6 Invoice Date: 3/24/11 Co/Div/Um 0 3 - 0 2 0 - 1 LCl/DP6/TY/PDLN D 28 T Note: A surcharge has been applied to include the expense of EPA mandated hazardous material disposal and miscellaneous consumables. 12:13:45 VER2 PAY from this Invoice WINSK PROT5