EFTA00609734.pdf
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Gulfstreant
DYNAMISM• COMPANY
Bldg C.-FAX
- West Paint Beach. Florida 33406
PRELIMINARY INVOICE
ParUModel #: GIV
AC Serial No./Tail No.: 1085 / N423TT
Mail Remittance To:
Gulfstream Aerospace Corporation
P.O. Box 730349
Dallas. Texas 75373-0349
Overnight Remiaance To:
Gulfstream Aerospace Corporation (Box # 730349)
Go JP Morgan Chase Bank. NA
ATTN: Dallas National Wholesale Lockbox TX1-0029
14800 Frye Road
Ft. Worth, TX 76155
Wire Remittance To:
Gulfstream Aerospace Corporation
JP Morgan Chase Bank. NA
Chicago, IL 60670
Account No.
Fedwire Routing No.
S.W.I.F.T.
ACII Credit Routing No. (
Bill To: JEGE, INC.
3800 SOUTHERN BLVD
SUITE 204
WEST PALM BEACH, Florida 33406
United States
Title: JEGE, INC.
Invoice Number.
Invoice Date:
Customer ID:
P.O. Number.
Repair Station:
In Date:
Out Date:
Payment Type:
Payment Terms:
FAA CRS PB8R624N
04/01/2013
04/22/2013
Net 30-Open terms
INVOICE SUMMARY FOR WORK ORDER NUMBER: SC13175
Time & Materials
Flat Raw
Total
Labor USD:
$23,939.84
$74,150.00
$98,089.84
Parts USD:
$196,307.51
$0.00
$196,307.51
Services USD:
$1,547.68
$0.00
$1,547.68
Detail Subtotal USD:
$221,795.03
$74,150.00
$295,945.03
Subtotal USD:
$295.945.03
Funds on Deposit USD:
50.00
Total USD:
Pre Test Flight Times /Cycles
Airframe 8563.8 Hrs 3963 Lds
Eng #1 8508.1 TSN 3929 CSN
Eng #2 8528.0 TSN 3935 CSN
Post Test Flight Times / Cycles
Airframe 8567.0 Hrs 3964 Lds
Eng #1 8511.3 TSN 3930 CSN
Eng #2 8531.2 TSN 3936 CSN
$295,945.03
For detail description of the work complied with see the Work Order Detail report.
Unless otherwi
GAC_WorkOrderPreliminaryInvoice.rm
indicated, all financial values listed in this document are in US Dollars (USD).
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EFTA00609734
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Item: 1
Airframe Gulfstream GIV Scheduled N423TT
Team Manager: Sean Brown
Customer Coordinator: Ray Kraber
Pan/Model
GIV
AC Serial No./Tail No.: 1085 / N423TT
TSN/TSO:
CSN/CSO: 3,964
Aircraft Time: 8,567.0
Discrepancy: 1.1
Return to Service EJM (10 or More)
Resolution: ACTT: 8,563.8
LNDS: 3,963
DATE: April XX, 2013
Completed (INSERT TITTLE) inspection accordance with EJM (INSERT AIRCRAFT TYPE) Continuous Airworthiness
Maintenance Program, EJNI Maintenance Procedure Manual and 14 CFR 135.411 (a)(2) and is approved for return to
service.
Authorized RTS Signature
Thomas J. Choynowski, Sr. Airworthiness Inspector
For;
Gulfstream
West Palm Beach, FL 33406
FAA CRS PB8R624N
Discrepancy: 1.2
Inbound/Outbound Inspection
Resolution: Complied with Inbound / Outbound Inspections.
Labor USD:
No Charge
N/ C
Step: 1.2.1
Step: 1.2.2
Completed
Inbound/Preliminary Inspection
Waiting
Outbound Inspection
approval (L)
Discrepancy: 1.3
Preflight Inspection
Resolution: N/A
Discrepancy: 1.4
Comply with Debrief Checklist
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_WorkOrderPrelintinaryInvoicespt
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EFTA00609735
WO8: SC13175
Invoice Number:
Bill To: JEGE, INC.
Resolution: N/A
Step: 1.4.1
Completed
Arrival/Debrief 90 Day Due List Review Accomplished.
Step: 1.4.2
Completed
List Operator's Airworthiness Requirements & Special Documentation Requests.
Step: 1.4.3
Completed
Review Technical Operations Update prior to return to service for newly released
bulletins and advise operator.
Discrepancy: 1.5
Tool Clearance
Resolution: All tooling removed from aircraft.
Discrepancy: 1.6
Cover & Protect
Resolution: Protected aircraft as required for MX as required.
Labor USD:
No Charge
N/ C
Discrepancy: 1.7
Resolution: N/A
Service Chemical Toilet/('lean Galley
Discrepancy: 1.8
ArrivaUDeparture Assist & Video Aircraft
Resolution: C/W as required.
Discrepancy: 1.9
Sample Hydraulic Fluids
Resolution: Sampled Hydraulic Fluids a required.
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_WorkOrderPrelintinaryInvoicespt
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EFTA00609736
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Discrepancy: 1.10
Remove Valuables & Secure.
Resolution:
Discrepancy: 1.11
Comply with Service Team Manager Checklist
Resolution:
Labor USD:
No Charge
N/ C
Discrepancy: 1.12
Fluids Used (Oils/Skydrol) - (Materials Only)
Resolution: Billed Fluids Used (OiLs/Skydrol) - (Materials Only) as required.
Discrepancy: 1.13
STM / Quality review of work order and logbook entry prior to departure
Resolution:
Labor USD:
No Charge
N/ C
Discrepancy: 1.14
Towing (Does not include Hangar Moves)
Resolution: Towed as required for MX.
Billing Method
Hours
Rate
Total
Labor USD:
Time and Material
ST
4.50
@
$118.00
$531.00
Total USD:
$531.00
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_WodcOrderPreliminarylnvoicespt
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EFTA00609737
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Discrepancy: 1.15
HazMat - Identify & provide a manifest, and a Shipper's Declaration for
Dangerous Goods for all hazardous materials that are loaded aboard any
aircraft.
FAR Part 121 or 135 Operators will provide a hazardous material
notification letter required by FAR 135.505 (e) prior to maintenance at
this Repair Station iaw FAR 145.206 (a) (b).
If there is to be loading of hazardous materials it shall be complied with
by Hazmat trained authorized GDAS-PBI personnel only.
Resolution: NM --- No Hazmat onboard aircraft at this time.
Discrepancy: 1.16
Resolution: NM
Aircraft Cleaning
Discrepancy: 1.17
Billable Consumables & Shop Supplies
Resolution: Billed for Shop Supplies and Consumables as required for MX.
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_WoikOrderPreliminarylnvoicespt
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EFTA00609738
Bill To: JEGE, INC.
WO It: SC13175
Invoice Number:
Discrepancy: 1.18
Resolution: NM
Major Alterations regulatory compliance requirements to be completed by installer as indicated on FAA form
8110-3.
Copy and paste from attached statements as needed and edit as required.
COMPLY WITH REQUIREMENTS OF FAR 25.1301 (d), 25.1353(a) and 25.1431(c) (d).
COMPLIED WITH THE REQUIREMENTS OF FAR 25.1301 (d), 25.1353(a) and 25.1431(c) (d), via GROUND
TEST REPORT-REPORT No. CEXXXXXXXX REV. X, ( IN SUPPORT OF STC XXXXXXXXX ) and
GR4R216M REPAIR STATION INTERFERENCE TESTING REQUIREMENTS POST MAJOR
ALTERATIONS COMPLIANCE FORM.
COMPLY WITH REQUIREMENTS OF FAR 25.1529, INSTRUCTIONS FOR CONTINUED
AIRWORTHINESS.
REF XXXXX MANUAL, P/N XXXXXXX REV. X, FOR INSTRUCTIONS FOR CONTINUED
AIRWORTHINESS AND BLOCK 8 OF FAA FORM 337, DATED XX/XX/XXXX.
COMPLY WITH THE WIRE ROUTING REQUIREMENTS OF FAA POLICY ANM-01.04 AND FAR 25.1353
(B)
COMPLIED WITH THE WIRE ROUTING REQUIREMENTS OF FAA POLICY ANM-01.04 AND FAR
25.1353 (B) BY ENSURING ROUTING WAS IN ACCORDANCE AC43.13-1B, CHANGE 1 CHAPTER 11,
SECTION S.
Discrepancy: 1.19
Update Weight & Balance
Resolution:
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_WorkOrderPrelintinaryInvoicespt
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Bill To: JEGE, INC.
WO
SC13175
Invoice Number:
Discrepancy: 1.20
Exterior Paint and Weight & Balance Requirements.
Review scope of aircraft exterior paint touch-up/repairs, and skin replacements resulting in paint reapplication,
and determine affect on weight and balance.
For surfaces where paint is stripped and reapplied or added on top of existing paint on an area greater than 36
square feet the thickness values will be documented before and after painting . If average thickness values remain
the same, weight and balance revision is not required.
For surfaces painted with an area greater than 36 square feet and before and after paint thickness average varies,
QC review for possible weight and balance revision will be required.
* Thickness will be plotted on an aircraft drawing derived from AMM chapter 6 or other suitable sketch,
attached to the work order and measurements taken on a two square foot grid.
* Reference CAMPS 4000, paragraph 3.5.1 for paint restrictions to flight control surfaces and RVSM certified
aircraft.
* Reference CAMPS 4000, total average thickness shall not exceed 6 mils.
* Per GAC Mass Properties Engineering, paint thickness of 5 mils equals .055 pounds per square foot.
* If after QC review, weight change is greater than 2 pounds or .05% of MAC, the weight and balance report will
require recomputation.
Resolution: N/A
Discrepancy: 1.21
Resolution: N/A
"Advise customer of preservation requirements per ATA Chapter 10 of the relevant maintenance manuals for
Airframe, Engines, and APU; review requirements in relation to scheduled Date Promised and later potential
Date Completed; and perform maintenance or preservation actions as directed by the customer and documented
as a Work Order Squawk.
Item: 6
Avionics
Team Manager: Sean Brown
Customer Coordinator: Ray Kraber
Pan/Model
AC Serial No./Tail No.:
TSN/TSO:
CSN/CSO:
Aircraft Time: 8,567.11 / 3,964
Discrepancy: 6.1
RH wing emergency light inop
Resolution: Removed defective bulb RH wing emergency light P/N GE303 nsn. Installed new bulb RH wing emergency light P/N
GE303 nsn. Op's check good. All work was done JAW Gulfstream GIV AMM 33-10-01.
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_WorkOrderPreliminaryInvoicespt
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Bill To: JEGE, INC.
Billing Method
WO #: SC13175
Hours
Rate
Invoice Number:
Total
Labor USD:
Time and Material
ST
4.25
@
$118.00
$501.50
Pans USD:
Time and Material
$28.57
Total USD:
$530.07
Parts:
Ref. No.
Part number:
Description
Quantity
Sell price USD
Extended USD
6.1 #1
303
LAMP
1
$1.75
$1.75
6.1 #2
PRI440-B-1/2
SEALANT, PRC,CARTRIDGE
1
$26.82
$26.82
Discrepancy: 6.2
While complying with CMP 231001 Avionics-Functional Ramp Test/Inspection found that the #1 HF system does
not transmit.
Resolution:
Billing Method
Hours
Rate
Total
Labor USD:
Time and Material
ST
2.25
@
$118.00
$265.50
Total USD:
$265.50
Step: 6.2.1
Completed
Verified discrepancy, performed HF press to test on #1 HF control head and received
codes 19, 27. and 28 with the RT light illuminated. Hi' receives the Intl clock very
clear. When the Press to Talk switch is pressed with the #1 HF system, Fault code 08
appears on the control head with the UP lamp illuminated. Further troubleshooting
required at this time. All work performed 1AW G-IV maintenance manual 23-03-00.
Discrepancy: 6.3
While complying with CMP 231001 Avionics-Functional Ramp Test/Inspection found that the #2 HF system
produces a power surge when press to talk is pressed that causes the external AC power cart to shut down.
Resolution:
Billing Method
Hours
Rate
Total
Labor USD:
Time and Material
ST
0.75
@
$118.00
$88.50
Total USD:
$88.50
Discrepancy: 6.4
While complying with CMP 231001 Avionics-Functional Ramp Test/Inspection found that the #1 Auto Throttle
reports Excessive Friction and Servo Current Failures when tested.
Resolution:
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_WorkOrderPrelintinaryInvoicespt
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Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Discrepancy: 6.5
While complying with CMP 231001 Avionics-Functional Ramp Test/Inspection found that the #2 Auto Throttle
reports Servo Current Failure.
Resolution:
Discrepancy: 6.6
Resolution:
Performe Cockpit bulb sweep. While complying with CMP 231001 Avionics-Functional Ramp Test/Inspection
found that the E-Batts switch capsules just left of the co-pilots yoke are partially loop. Also noted that theupper
half of the first digit on the Differential Pressure Guage is out. The upper half of the Radar Stab IRU select
switch just forward of the IRU MSU are loop.
Discrepancy: 6.7
Resolution:
Step: 6.7.1
Squawk from flight test - Standby fuel gauge totalizer is indicateing 2001bs lower than the LT and RT fuel gauges
and there is a 150lbs difference between total fuel on EICAS primary and systems page compared to STBY
totalizer gauge - EICAS and SYSTEMS page ind same
Waiting
While deluding aircraft noticed that EICAS read 27501bs It and rt and 54001bs total and
approval (L) standby ind read 27501bs It and rt but 44001bs total. The standby ind LOW FUEL light
came on with 26001bs It and rt(suppose to be 6501bs).
Discrepancy: 6.8
Squawk from flight test • LED light burned out on Rate of Climb / FPM (3 digit from LT) on pressurization
controller
Resolution:
Discrepancy: 6.9
Squawk from flight test - With both engines and APU running and both converters on DC volts on the
Right-Left-AUX or ESS selected indicate 47.8VDC
Resolution:
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_WorkOrderPreliminaryInvoicespt
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Rd X
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Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Discrepancy: 6.10
Squawk from flight test - At FL250 with Batteries only, DC volts on ABEX fluctuates 36.9 to 47.9 v
Resolution:
Discrepancy: 6.11
Squawk from flight test - RTU 1 there is a cyan line across display on screen - splits screen in half
Resolution:
Discrepancy: 6.12
Squawk from flight test - On RNAV approach VNAN worked and then became unavailable on approach
Resolution:
Discrepancy: 6.13
Squawk from flight test - Standby engine instrument gauge is indicating all "88118"s on RT HP gauge
Resolution:
Discrepancy: 6.14
Squawk from flight test - HF radios operated normally but NO SELCAL
Resolution:
Discrepancy: 6.15
EGPWS/Terrain database outdated
Resolution:
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_WodcOrderPreliminarylnvoicespt
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EFTA00609743
Bill To: JEGE, INC.
WO ft: SC13175
Invoice Number:
Discrepancy: 6.16
Squawk from flight test - aft LAV reading light is Mop
Resolution:
Discrepancy: 6.17
Squawk from flight test - cabin management display at VIP , galley screen Mop
Resolution:
Discrepancy: 6.18
Squawk from flight test - perform ops test of nose camera
Resolution:
Discrepancy: 6.19
Satphone is inop
Resolution:
Item: 7
Interior
Team Manager: Sean Brown
Customer Coordinator: Ray Kraher
Pan/Model 0:
AC Serial No./Tail No.:
TSN/TSO:
CSN/CSO:
Aircraft Time: 8,567.0 / 3,964
Discrepancy: 7.1
Resolution:
Squawk [ruin flight test - FWD LAV water does not pump
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_WorkOrderPreliminaryInvoicespt
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Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Discrepancy: 7.2
Squawk from flight test - LH galley aft cutting board does not latch
Resolution:
Billing Method
Hours
Rate
Total
Labor USD:
Time and Material
ST
0.87
@
$118.00
$102.66
Pans USD:
Time and Material
$1.86
Total USD:
$104.52
Parts:
Ref. No.
Part number:
Description
Quantity
Sell price USD
Extended USD
7.2#1
MINI-LATCH
SELBY-LATCH WHITE NICKEL
1
$1.86
$1.86
Step: 7.2.1
Completed
Removed galley drawer and galley latch. All work performed IAW GIV MM 25-20-00.
Discrepancy: 7.3
Squawk from flight test - RH #5 window shade does not fully close
Resolution:
Discrepancy: 7,4
Squawk from flight test - pax air gaspers loose, takes two hands to close the outlet
Resolution:
Discrepancy: 7,5
Squawk from flight test - fwd cabin door angle wing does not hit headliner when closed.
Resolution:
Billing Method
Hours
Rate
Total
Labor USD:
Time and Material
ST
2.10
@
$118.00
$247.80
Total USD:
$247.80
Step: 7.5.1
Waiting
Insp
Removed fwd pocket door, inspected pop-up door closeout mechanics, found no defects
at this time, lubricated mechanical areas as required, re-installed fwd door and pop-up
door closeout still would not fully close. Further evaluation is needed. All work
performed IAW GIV MM 25-20-00.
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_WorkOrderPrelintinaryInvoicespt
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EFTA00609745
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Item: 8
Mechanical
Team Manager: Sean Brown
Customer Coordinator: Ray Kraber
Pan/Model #:
AC Serial No./Tail No.:
TSN/TSO:
CSN/CSO:
Aircraft Time: 8,567.0 / 3,964
Discrepancy: 8.1
The No. 1 engines Outboard igniter plug is worn
Resolution: Remove engine #1 ignitor plug #2 P/N Y183-5 S/N 1204. Instaled new engine #1 ignitor plug #2 P/N Y183-5 S/N 12047184.
JAW RR EMM 74-21-03.
Parts USD:
Parts:
Ref. No.
8.1 #1
No Charge
Part number:
Y183-5
Description
PLUG, IGNITOR
N/C
Quantity
Sell price USD
Extended USD
1
$0.00
$0.00
Discrepancy: 81
The No. 2 engines Outboard igniter plug is worn
Resolution: Remove Engine #2 ignitor #2 P/N Y183-5 S/N 0601749. Installed new Engine #2 ignitor #2 P/N Y183-5 S/N 12047194.
JAW RR EMM 74-21-03.
Parts USD:
Parts:
Ref. No.
8.2
No Charge
Part number:
Y183-5
Description
PLUG, IGNITOR
N/C
Quantity
Sell price USD
Extended USD
1
$0.00
$0.00
Discrepancy: 8.3
The Left engine S/N 16291, No.8 combustion liner has a 1.8" crack and part of the crossover tube shroud is
missing. Pictured sent to rolls royce.
Resolution: With further investigation on the No.8 combution liner on the left engine S/N 16291, found the cranks to be within limits
JAW the Rolls Royce TAY611-8 EMM chapter 71.00.00, and no further action is needed.
With further investigation found the crossover tube to only have minor errosion and some carbon build up No further
action is required on this item. All work performed JAW the Rolls Royce TAY611.8 EMM chapter 71.00.00.
Discrepancy: 8.4
The Right engine S/N 16292, No.4 combustion liner has 4 cracks. (1.0", 3.2", 4.0", and 5.6") and over 30 HPT
stage one bases LE cracked. Pictured sent to rolls royce.
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_WorkOrderPreliminaryInvoicespt
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EFTA00609746
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Resolution: With further investigation of the No.4 combution liner of the right engine S/N 16292 found the cracking to only be 25% of
what was originally determined. Total circumferential cracking was found to be less than 40% and no further special
inspections will be needed for this item. All work was performed JAW the Rolls Royce TAY611-8 EMM chapter
71.00.00.
Two HPT stage 1 Blade tips was found to be cracked on the LE with the crack protruding into the airfoil 0.050"
(1.25mm). All work was performed IAW the Rolls Royce TAY611.8 EMM Task 71.00.00.210.001 (9)(a)(iii). Re-Inspect
the blades within 400 hours (8,928.0 TSN) or 400 cycles (4,335 CSN) whichever occurs first. This crack can protrude into
the airfoil up to a length of 0.315" (8.00 mm)
Discrepancy: 8.5
Squawk from flight test - rubber stripping on leading edge of LT and RT MLG doors are torn
Resolution: Removed damaged sections of rubber seal P/N GASl3AN-1.41from around L/H and R/H MLG bays, and installed new
seal P/N GAS13AN-1-41 I/A/W GIV AMM 20-42-00
Billing Method
Hours
Rate
Total
Labor USD:
Time and Material
ST
2.08
@
$118.00
$245.44
Pans USD:
Time and Material
$109.18
Total USD:
$354.62
Parts:
Ref. No.
Part number:
Description
Quantity
Sell price USD
Extended USD
8.5 #1
GASl3AN-1.41
SEAL, BUTTONED STRIP, WHEEL
I
$109.18
$109.18
WELL DOOR (5' SECTION)
Discrepancy: 8.6
Squawk from flight test - Copilots seat is difficult to move in fore-aft position
Resolution: Removed copilot seat and inspected seat track and rollers. Found no defects. Lubed seat track and rollers. Moved seat
fore and aft with satisfactory results. Reinstalled copilot seat. Ref: GIV ALUM 25-11.00.
Billing Method
Hours
Rate
Total
Labor USD:
Time and Material
ST
2.00
@
$118.00
$236.00
Total USD:
$236.00
Discrepancy: 8.7
Squawk from flight test - Gear emergency reset handle not safetied (D-ring)
Resolution: Safetied Gear Emergency Reset Handle (D-ring) IAW GIV AMM 32-00-00.
Billing Method
Hours
Rate
Total
Labor USD:
Time and Material
ST
1.70
@
$118.00
$200.60
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_WoikOrderPreliminarylnvoice.rpt
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Rd X
EFTA00609747
Bill To: JEGE, INC.
WO 9: SC13175
Invoice Number:
Total USD:
$200.60
Discrepancy: 8.8
Squawk front flight test - Flaps shudder felt when flaps selected to 39 degrees
Resolution:
Discrepancy: 8.9
Squawk from flight test - screw needs tightening on panel behind pilots seat below CB panel
Resolution:
Billing Method
Hours
Rate
Total
Labor USD:
Time and Material
ST
0.50
@
$118.00
$59.00
Total USD:
$59.00
Discrepancy: 8.10
Squawk from flight test - on the ground the flaps would intermittenly move from 20 to 39 degrees and 10 to 20
when selected.
Resolution:
Billing Method
flours
Rate
Total
Labor USD:
Time and Material
ST
20.92
@
$118.00
$2,468.56
Total USD:
$2,468.56
Discrepancy: 8.11
Squawk from flight test - power levers have 1/2 knob split at 15000ft and 80%HP (It lever is fwd)
Resolution:
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_WorkOrderPrelintinaryInvoicespt
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Rd X
EFTA00609748
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Discrepancy: 8.12
Squawk from flight test - while climbing through FL 430 with LT Pack OFF the RT Pack was 25psi (should be
27-33psi)
Resolution:
Discrepancy: 8.13
Squawk from flight test - while climbing through FL 430 with RT Pack OFF the LT Pack was 23psi (should be
27-33psi)
Resolution:
Discrepancy: 8.14
Squawk from flight test - One O2 mask in LAV and LT and RT AFT rear did not drop during test
Resolution: Verified that aft left,aft right and lay oxygen masks would not deploy. Adjusted mask lid holding spring clips on all 3
mask boxes. Performed funtional check of the 3 locations. Ops checked good. No further defects noted.
Billing Method
Hours
Rate
Total
Labor USD:
Time and Material
ST
4.36
@
$118.00
$514.48
Total USD:
$514.48
Discrepancy: 8.15
Squawk from flight test - service hydraulic replenisher
Resolution:
Billing Method
Hours
Rate
Total
Labor USD:
Time and Material
ST
1.20
@
$118.00
$141.60
Pans USD:
Time and Material
$319.92
Total USD:
$461.52
Parts:
Ref. No.
P:nt number:
Description
Quantity
Sell price USD
Extended USD
8.15
500B4QT
SKYDROL OIL IN QUART CANS
6
$53.32
$319.92
Discrepancy: 8.16
Squawk from flight test - At FL400 and climbing, RT engine MCI' was 1.79 but could only indicate 1.78 before
LP RPM has an exceedance
Resolution:
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_WorkOrderPreliminaryInvoicespt
Page 16 of 57
Printed: 4/18/2013 11:38:5 IA)
Rd X
EFTA00609749
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Discrepancy: 8.17
While compling with APU GTCP36.100(G) Borescope the following was found.
The plenum is cracked, the nozzle guide vane TE's are erroded and cracked, and the turbine wheel tips are
erroded.
Resolution:
Billing Method
Hours
Rate
Total
Labor USD:
Time and Material
ST
1.47
@
$118.00
$173.46
Services USD:
No Charge
N/ C
Total USD:
$173.46
Services:
Ref. No.
Description
Quantity
Sell Price USD
Extended USD
8.17 #1
REPAIR
1.00
$0.00
$0.00
Part Ref: GTCP36-100G APU (3800062-9-1)
Step: 8.17.1
Completed
Removed APU generator P/N I1598CAV373-105 SIN 129A0171 I/A/W G1V AMM
24-01-01 and sent APU out for repair.
Discrepancy: 8.18
While tightening screw for squawk 8.9 found that the inboard metal protector (located on panel behind copilots
seat) for the coplilots seat is bent and is cutting into copilot seat back rest.
Resolution:
Billing Method
flours
Rate
Total
Labor USD:
Time and Material
ST
1.50
@
$118.00
$177.00
Total USD:
$177.00
Discrepancy: 8.19
Squawk from flight test - There is a soft spot in floor hoard just fwd of fwd LAV (feels like blowout panel isnt
secure)
Resolution: Removed broken clip P/N 159B10732-13 from blowout panel forward of forward lay and replaced with new clip P/N
159B10732-13 IAW GAC Drawing 159B10732.
Billing Method
flours
Rate
Total
Labor USD:
Time and Material
ST
4.91
@
$118.00
$579.38
Pans USD:
Time and Material
$86.10
Total USD:
$665.48
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_WorkOrderPrelintinaryinvoicespt
Page 17 of 57
Printed: 4/18/2013 I I:38:51AP
Flet X
EFTA00609750
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Parts:
Ref. No.
Part number:
Description
Quantity
Sell price USD
Extended USD
8.19 NI
159B10732-13
SPRING CLIP
2
$43.05
$86.10
Discrepancy: 8.20
Evaluate flaking paint from steel doubler and adjacent structure on L/H horizontal stab at panel 38-UPR-4.
Ref to sqk 15.25
Resolution: Cleaned suspect area and after further evaluation found no defects. No further action required. Work perfromed JAW
GIV SRM 51.13.00.
Billing Method
Flours
Rate
Total
Labor USD:
Time and Material
ST
3.40
@
$118.00
$401.20
Total USD:
$401.20
Discrepancy: 8.21
While working sqk 15.26 CMP 551024. Found corrsion and pitting horizontal stabilizer skin at panel 38-UPR-5.
Resolution: Removed minor surface corrosion and pitting from panel opening mounting flange of panel 38-UPR-5, cadmium plated
exposed surface and applied coat of primer. All work done IAW GIV SRM 51-13-10.
Billing Method
Hours
Rate
Total
Labor USD:
Time and Material
ST
733
@
$118.00
$864.94
Labor USD:
Time and Material
OT
0.10
@
$177.00
$17.70
Total USD:
$882.64
Step: 8.21.1
Completed
Nlechanicaly removed minor surface corrosion and pitting from panel opening
mounting flange and cadmium plated exposed surface. All work done lAW GIV SRM
51-13-10.
Discrepancy: 8.22
While working sqk 15.26 CMP 551023. Found corrsion and pitting horizontal stabilizer skin at panel 39-UPR-5.
Resolution: Removed minor surface corrosion and pitting from panel opening mounting flange of panel 39-UPR-5, cadmium plated
exposed surface and applied coat of primer. All work done JAW GIV SRM 51-13-10.
Billing Method
Hours
Rate
Total
Labor USD:
Time and Material
ST
635
@
$118.00
$749.30
Labor USD:
Time and Material
OT
0.92
@
$177.00
$162.84
Total USD:
$912.14
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_WorkOrderPrelintinaryInvoicespt
Page 18 of 57
Printed: 4/18/2013 11:38:5 1 Ali
toe X
EFTA00609751
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Step: 8.22.1
Completed
Mechanical,' removed minor surface corrosion and pitting front panel opening
mounting flange and cadmium plated exposed surface. All work done IAW GIV SRM
51-13-10.
Discrepancy: 8.23
While working CMP 551023 sqk 15.25. Found horizontal stab thrust blocks to be worn out of limits.
Resolution:
Discrepancy: 8.24
#2 Engine EPR Flex line chaffing against fixed cowl. (Flagged)
Resolution: Adjusted orientation of #2 Engine EPR Flex Line IAW GIV AMM 77-01-00.
Billing Method
Hours
Rate
Total
Labor USD:
Time and Material
ST
3.28
@
$118.00
$387.04
Total USD:
$387.04
Discrepancy: 8.25
#2 Engine has multiple corroded clamps on forward IB area of engine.
Resolution:
Billing Method
Hours
Rate
Total
Labor USD:
Time and Material
ST
0.50
@
$118.00
$59.00
Total USD:
$59.00
Discrepancy: 8.26
While performing wing HI-lite Collar (left) inspection CMP code 571011 found collar cracked at LBL 44.0
Resolution: Removed cracked HI-lite Collar at LBL 44.0, and installed new Colter P/N IIST70-8. All maintenance performed IAW
Gulfstream GIV ASC 446 AMI.
Billing Method
Hours
Rate
Total
Labor USD:
Time and Material
ST
0.47
@
$118.00
$55.46
Total USD:
$55.46
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_WorkOrderPrelintinaryInvoicespt
Page 19 of 57
Printed: 4/18/2013 11:38:5 IA)
Ftst X
EFTA00609752
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Discrepancy: 8.27
Resolution:
Labor USD:
Total USD:
While gaining access to cracked Hi-Lite Collar at LBL 44.0 found fasteners wet with hyd fluid at top of wing box
section left and right of BL-0
Billing Method
Houri.
Rate
Total
Time and Material
ST
9.03
@
$118.00
$1,065.54
$1,065.54
Discrepancy: 8.28
Resolution:
Labor USD:
Pans USD:
Total USD:
Parts:
While performing wing HI-lite Collar RT inspection CMP code 571012 found a dented fuel line on center wing
leading edge.
Billing Method
Houri.
Rate
Total
Time and Material
ST
632
@
$118.00
$745.76
Time and Material
$116.32
$862.08
Ref. No.
Part number:
Description
Quantity
Sell price USD
Extended USD
8.28 #1
D10036D06
UNION. PERMASWAGE
1
$51.50
$51.50
8.28 #2
D10036D06
UNION. PERMASWAGE
1
$51.50
$51.50
8.28 #3
6061T6-.375X.028
TUBING, ALUMINUM-3/8
2
$6.66
$13.32
Step: 8.28.1
Completed
Cut and removed 6" section with dent front fuel line PIN:1159N2012-0221/P6 at
RBS255.5 of RIR wing. Spliced in new 6" section of tubing on fuel line
P/N:1159P42012.022FT6 at RBS255.5 of Ral wing. All work done IAN' GAMPS 2507.
Discrepancy: 8.29
While T/S the squawk (8.10) for the flaps moving intermittenly found that the LH outboard flap actuator failed
the Ballnut End Play check. Endplay is .038in., limit is .012in.
Resolution:
Pans USD:
Total USD:
Parts:
Ref. No.
Billing Method
Hours
Rate
Total
Time and Material
$38,000.00
Part number:
$38,000.00
Description
Quantity
Sell price USD
Extended USD
819 11
1159SCC212-15
ACTUATOR.FLAP DRIVE, L-
OUTBOARD
1
$38,000.00
$38,000.00
For detail description of the work complied with see the Work Order Detail report.
GAC_WorkOrderPrelitninaryInvoicespt
Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD).
Page 20 of 57
Printed: 4/15/2013 11:38:5 IA)
Rd X
EFTA00609753
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Discrepancy: 8.30
While T/S the squawk (8.10) for the flaps moving intermittenly found that the LH inboard flap actuator failed the
Ballnut End Play check. Endplay is .057in., limit is .012in.
Resolution:
Billing Method
Hours
Rate
Total
Pans USD:
Time and Material
$38,000.00
Total USD:
$38,000.00
Parts:
Ref. No.
Pail number:
Description
Quantity
Sell price USD
Extended USD
830 /1
II59SCC211-15
ACTUATOR, FLAP DRIVE, INBD
1
$38,000.00
$38,000.00
Discrepancy: 8.31
While T/S the squawk (8.10) for the flaps moving intermittenly found that the RH outboard flap actuator failed
the Ballnut End Play check. Endplay is .061in., limit is .012in.
Resolution:
Billing Method
Houri.
Rate
Total
Pans USD:
Time and Material
$76,000.00
Total USD:
$76,000.00
Parts:
Ref. No.
Part number:
Description
Quantity
Sell price USD
Extended USD
83112
1159SCC212-16
ACTUATOR, FLAP DRIVE, R-
1
$38,000.00
$38,000.00
OUTBOARD
831 N3
1159SCC212-16
ACTUATOR, FLAP DRIVE, R-
I
538,000.00
$38,000.00
OUTBOARD
Discrepancy: 8.32
While T/S the squawk (8.10) for the flaps moving intermittenly found that the RH inboard flap actuator failed
the Ballnut End Play check. Endplay is .030in., limit is .012in.
Resolution:
Billing Method
Hours
Rate
Total
Pans USD:
Time and Material
$38,000.00
Total USD:
$38,000.00
Parts:
Ref. No.
Part number:
Description
Quantity
Sell price USD
Extended USD
83212
I I59SCC211.15
ACTUATOR, FLAP DRIVE, INBD
1
$38,000.00
$38,000.00
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_WorkOrderPrelintinaryInvoicespt
Page 21 of 57
Printed: 4/18/2013 11:38:5IA)
Rd X
EFTA00609754
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Discrepancy: 8.33
Found several chips and a soft spot that light can be seen through on the radonw nose, under the errosion hoot.
Resolution:
Discrepancy: 8.34
The RH flap's "C" tracks forward, inboard bearing is bad (1159SCC228.23)
Resolution: C/W CMP 275123. Removed worn R/H flap "C" track roller P/N 1159SCC228-23. Installed new roller P/N
1159SCC228-23. All work I.A.W. GIV M/M 27-06.00.
Billing Method
Labor USD:
Time and Material
Pans USD:
Time and Material
Total USD:
Parts:
Ref. No.
Part number:
Hours
Rate
ST
2.05
@
$118.00
Description
ROLLER -FLAP
Total
$241.90
$562.00
$803.90
Quantity
Sell price USD
Extended USD
8.34 #1
1159SCC228-23
1
$562.00
$562.00
Discrepancy: 8.35
The LH flap's "B" tracks AFT, outboard bearing is bad (1159SCC226-7)
Resolution:
Billing Method
Hours
Rate
Total
Labor USD:
Time and Material
ST
4.47
@I
$118.00
$527.46
Labor USD:
Time and Material
OT
0.18
@
$177.00
$3L86
Pans USD:
Time and Material
$1,590.32
Total USD:
$2,149.64
Parts:
Ref. No.
Part number:
Description
Quantity
Sell price USD
Extended USD
835 #1
1159SCC426-11
BEARING, FLAP TRACK ROLLER
1
$819.88
$819.88
EXT
835 #2
1159SCC426-9
BEARING. TRACK ROLLER EXT -
1
S770.44
$770.44
FLAP
Step: 8.35.1
Completed
Complied with GIV CMP 275117 wing flap roller (Leftr outboard upper Aft B Track
B-9) - Removal/Installation. steps A to B(2) and B(5)(a) to B(5Xb). Removed defected
flap roller P/N: 1159SCC266-7,
NSN. Work done IAW GIV CMP 275117 & GIV
hl/M 27-06-00.
Discrepancy: 8.36
The LH flap track "A" has corrosion
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_WorkOrderPreliminaryInvoicespt
Page 22 of 57
Printed: 4/18/2013 11:38:5 IA)
toe X
EFTA00609755
Bill To: JEGE, INC.
Resolution:
WO #: SC13175
Invoice Number:
Billing Method
Hours
Rate
Total
Labor USD:
Time and Material
ST
8.50
@
$118.00
$1,003.00
Total USD:
$1,003.00
Step: 8.36.1
Waiting
Insp
Removed light surface corrosion and pitting from IJH flap track "A" IAW GIV AMM
27-06-00.
Discrepancy: 8.37
The LH flap track "B" has corrosion
Resolution:
Billing Method
!lours
Rate
Total
Labor USD:
Time and Material
ST
0.50
@
$118.00
$59.00
Total USD:
$59.00
Discrepancy: 8.38
The LH flap track "C" has corrosion
Resolution:
Billing Method
I lours
Rate
Total
Labor USD:
Time and Material
ST
0.50
@
$118.00
$59.00
Total USD:
$59.00
Discrepancy: 8.39
The LH ❑ap track "I)" has corrosion
Resolution:
Billing Method
Holm
Rate
Tot
Labor USD:
Time and Material
ST
0.50
@
$118.00
559.00
Total USD:
559.00
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_WoikOrderPreliminarylnvoicespt
Page 23 of 57
Printed: 4/18/2013 11:38:5 IA)
Ref X
EFTA00609756
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Discrepancy: 8.40
The RH flap track "A" has corrosion
Resolution:
Billing Method
Hours
Rate
Total
Labor USD:
Time and Material
ST
0.50
@
$118.00
559.00
Total USD:
$59.00
Discrepancy: 8.41
The RH flap track "B" has corrosion
Resolution:
Billing Method
Hours
Rate
Total
Labor USD:
Time and Material
ST
1.50
@
$118.00
$177.00
Total USD:
$177.00
Discrepancy: 8.42
The RH flap track "C" has corrosion
Resolution:
Billing Method
Hours
Rate
Total
Labor USD:
Time and Material
ST
4.33
@
$118.00
$510.94
Total USD:
$510.94
Discrepancy: 8.43
The RH flap track "D" has corrosion
Resolution:
Discrepancy: 8.44
The LH flap track "B" has play in the fwd attach bolt
Resolution:
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_WorkOrderPrelintinaryInvoicespt
Page 24 of 57
Printed: 4/18/2013 11:38:5IA)
Rd X
EFTA00609757
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Billing Method
Houri.
Rate
Total
Labor USD:
Time and Material
ST
3.73
@
$118.00
$440.14
Pans USD:
Time and Material
$481.99
Total USD:
$922.13
Pans:
Ref. No.
Part number:
Description
Quantity
Sell price USD
Extended USD
8.44 #1
1159Wd120235.3
BUSHING
2
$224.66
$449.32
8.44#2
NASI312-23
BOLT
I
$31.42
$31.42
8.44 #3
MS21083NI2
NUT
I
$1.25
$1.2.5
Discrepancy: 8.45
The RH flap track "0" has play in the fwd attach Molt
Resolution:
Billing Method
Houri.
Rate
Total
Parts USD:
Time and Material
$481.99
Total USD:
$481.99
Parts:
Ref. No.
Pan number:
Description
Quantity
Sell price USD
Extended USD
8.45 #1
1159WM20235.3
BUSHING
2
$224.66
$449.32
8.45 #2
NASI312-23
BOLT
I
$31.42
$31.42
8.45 #3
MS21083N12
NUT
1
$1.25
$1.25
Discrepancy: 8.46
Install prep and seal panels on tail surfaces.
See steps for applicable sections.
Resolution:
Billing Method
Hours
Rate
Total
Labor USD:
Time and Material
ST
10.53
@
$118.00
$1,242.54
Labor USD:
Time and Material
OT
0.20
@
$177.00
$35.40
Total USD:
$1,277.94
Step: 8.46.1
Step: 8.46.2
Completed
Preped and sealed panel on vertical stab. Panel edge sealant ready for paint. IAW GIV
AMM 20.00.00
Completed
Sealed panels on the upper vertical on the left and right. Closed left horiz stab trailing
edge panels, taped and ready to seal 37-UPR-1, 37-UPR-3, 37-UPR-5 and 37-UPR-7.
REF G1V MM 27.00.00
Discrepancy: 8.47
APU enclosure and apu mount have heavy soot residue
Resolution:
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_WorkOrderPrelintinaryInvoicespt
Page 25 of 57
Printed: 4/18/2013 11:38:5 IA)
Rd X
EFTA00609758
Bill To: JEGE, INC.
WO #: SCI3175
Invoice Number:
Billing Method
Hour,.
Rate
Total
Labor USD:
Time and Material
ST
4.00
$118.00
$472.00
Total USD:
$472.00
Discrepancy: 8.48
Resolution:
Squawk From night test - during climb #2 engine
went into RED, pilots had to manually pull throttle back
Discrepancy: 8.49
Squawk from flight test - #1 engine was hotter than #2 by 80+ degrees
Resolution:
Discrepancy: 8.50
Resolution:
R/H lower wing skin has corrosion near panel 22-FT-11
Discrepancy: 8.51
Resolution:
Rill lower wing skin has corrosion near panel 22•Ff•14
Discrepancy: 8.52
Resolution:
R/H lower wing skin has corrosion near panel 22-FT-15
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_WorkOrderPreliminaryInvoicespt
Page 26 of 57
Printed: 4/18/2013 11:38:5 IA)
are 3:
EFTA00609759
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Discrepancy: 8.53
Resolution:
R/Ii lower wing skin has corrosion near panel 22-FT-7
Discrepancy: 8.54
While C/W CMP 275123 sqk 8.34. CMP 275123 preferres that corresponding roller be replaced at same time.
Resolution:
Discrepancy: 8.55
While C/W CMP 275117 sqk 8.35. CMP 275117 preferres that corresponding roller be replaced at same time.
Resolution:
Discrepancy: 8.56
While removing R/II wing fuel panel 22-FT-1 for sqk 1532. Found ground mesh on panel to be torn. pn
1159WNI40076-13
Resolution:
Item: 9
Paint
Team Manager: Sean Brown
Customer Coordinator: Ray Kraber
Part/Model it:
AC Serial No./Tail No.:
TSN/TSO:
CSN/CSO:
Aircraft Time: 8,567.0 / 3,964
Discrepancy: 9.1
Ft/H lower wing skin has corrosion near panel 22-FT-7
Resolution: duplicate item to 8.53
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_WorkOrderPreliminaryInvoicespt
Page 27 of 57
Printed: 4/18/2013 11:38:5IA)
Rd X
EFTA00609760
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Item: 10
Outstanding Parts, Materials, and / or Services
Team Manager: Sean Brown
Customer Coordinator: Ray Kraber
ParUModel
AC Serial No./Tail No.:
TSN/TSO:
CSN/CSO:
Aircraft Time: 8,567.0 / 3,964
Discrepancy: 10.1
Service for Signature for LAV service
Resolution:
Services USD:
No Charge
N/ C
Services:
Ref. No.
Description
Quantity
Sell Price USD
Extended USD
10.1 B1
REPAIR AND UPGRADE
1.00
$0.00
$0.00
Item: 12
Aircraft Records and Logbook Research Only
Team Manager: Sean Brown
Customer Coordinator: Ray Kraber
Pan/Model 0:
AC Serial No./Tail No.:
TSN/TSO:
CSN/CSO:
Aircraft Time: 8,567.0 / 3,964
Discrepancy: 12.1
Comply with Aircraft Records and Logbook Research
Resolution: Complied with Aircraft Records and Logbook Research as required. See discrepancies below.
Billing Method
Flours
Rate
Total
Labor USD:
Flat Rate
$13,000.00
Total USD:
$13,000.00
Step: 12.1.1
Completed
CiM, part of the aircraft avionics equipment inventory list. More inventory required.
Step: 12.1.2
Completed
Continued with the aircraft avionics equipment inventory list. More inventory required.
Step: 12.1.3
Completed
Continued with avionics inventory. Need to check with CMP to complete.
Step: 12.1.4
Completed
Completed GIA Aircraft Avionics Equipment Inventory List.
Discrepancy: 12.2
No log entry found for the removal of NLG rod end P/N 1159HM40120-1 and the installation of P/N
1159SCL567-3. Mandatory CB 183 was PCW by Duncan Aviation on 10/24/06.
Resolution:
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_WorkOrderPrelintinaryinvoicespt
Page 28 of 57
Printed: 4/182013 11:38:51M.
Ftst X
EFTA00609761
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Discrepancy: 12.3
Resolution:
No log entry or tag was found for API. Fire bottle P/N AE30903823 S/N AENI.23 installed on 2/28/2005.
Discrepancy: 12.4
No log entry was found for NIA; Axle Assy. P/N 1159LM40544-7 S/N BFG6056NTW installed on June 3, 1999.
Resolution:
Discrepancy: 12.5
No 8130 found for Pilot'& Co-pilot side window attach bolts. Replaced on 12/11/98.
Resolution:
Discrepancy: 12.6
No 8130 found for isolator LJH Aft Fwd. S/N 2998 installed on 12/11/98.
Resolution:
Discrepancy: 12.7
No 8130 found for isolator LH Aft aft S/N 2982 installed on 12/11/98.
Resolution:
Discrepancy: 12.8
No 8130 found for isolator R/H Aft Fwd. S/N 2993 installed on 12/11/98.
Resolution:
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_WorkOrderPrelintinaryInvoicespt
Page 29 of 57
Printed: 4/18/2013 11:38:5IA)
Rd X
EFTA00609762
Bill To: JEGE, INC.
WOO:S(13175
Invoice Number:
Discrepancy: 12.9
No 8130 found for isolator R/II .\ft .\ft. S/N 2994 installed on 12/11/98.
Resolution:
Discrepancy: 12.10 No 8130 or log entry• found for nose wheel steering unitinstalled on 10/11/06.
Resolution:
Discrepancy: 12.11 AD74.08.09 R3 Lavatory Paper and Linen Waste Receptacle Enclosure Access Door and Disposal Door
Inspection is due in 126.7 Hours
Resolution:
Item: 13
APU Borescope
Team Manager: Sean Brown
Customer Coordinator: Ray Kraber
Pan/Model 0:
AC Serial No./Tail No.:
TSN/TSO:
CSN/CSO:
Aircraft Time: 8567.0 / 3,964
Discrepancy: 13.1
Comply with APU GTCP36-100(G) - Borescope
Resolution: Complied with APU GTCP36-100(G) - Borescope Inspection JAW Honeywell GTCP36-100(G) MM 49-20-00. REF Item
8.17 for discrepancies found.
Billing Method
flours
Rate
Total
Labor USD:
Flat Rate
$900.00
Total USD:
$900.00
Discrepancy: 13.2
Comply with CMP GIV 490001 APU GTCP36-100(G) - Removal / Installation
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_WorkOrderPrelintinaryInvoice.rpt
Page 30 of 57
Printed: 4/18/2013 11:38:5 Ali
Rd X
EFTA00609763
Bill To: JEGE, INC.
WO #: SCI3175
Invoice Number:
Resolution: Removed APU GTCP36-100, S/N P-465-C, with 6,449.0 TSN from GIV, N423T1', S/N 1085, IAN the GIV MM chapter
49.10.00.
Billing Method
flours
Rate
Total
Labor USD:
Time and Material
ST
5.00
$118.00
$590.00
Total USD:
$590.00
Step: 13.2.1
Completed
Removed APU Per CMP 490001 From A. BI la ; tin
;
.
Perforincil In
Reference To GIV AMM 49-10-00.
Discrepancy: 13.3
Comply with CMP GIV 490005 APU Enclosure GTCP36-100(C) - Inspection
Resolution:
Discrepancy: 13.4
Comply with CMP GIV 490002 APU GTCP36-100(G) - Ops Test
Resolution:
Item: 14
Engine Runs and Borescope
Team Manager: Sean Brown
Customer Coordinator: Ray Kraber
Pan/Model #:
AC Serial No./Tail No.:
TSN/TS0:
CSN/CS0:
Aircraft Time: 8,567.0 / 3,964
Discrepancy: 14.1
Comply with Engine Runs and Borescope
Resolution:
Billing Method
flours
Rate
Total
Labor USD:
Flat Rate
$14,500.00
Total USD:
$14,500.00
Discrepancy: 14.2
CMP GIV 710019 Powerplant Internal - 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_Work0rderPrelintinaryInvoicespt
Page 31 of 57
Printed: 4/18/2013 11:38:5IA)
Rd X
EFTA00609764
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Resolution: C/W CMP GIV 710019 Powerplant Internal - Inspection I/A/W GIV AMM 71-00-00 No defects noted
Labor USD:
Parts USD:
No Charge
No Charge
N/C
N/C
Discrepancy: 14.3
CMP GIV 710025 Engine Borescope - Inspection
Resolution: COMPLIED WITH CMP GIV 710025 Engine Borescope - Inspection IAW RR TAY EMM 71-00-00.
Labor USD:
Parts USD:
Total USD:
Parts:
Billing Method
No Charge
Time and Material
Flours
Rate
Total
N/C
$332.33
$332.33
Ref. No.
Part number:
Description
Quantity
Sell price USD
Extended USD
143 #1
AS43013-210
ORING
1
$17.72
$17.72
143 #2
A543013-348
ORING
2
$59.74
$119.48
143 #3
KB22748
O-RING
I
$10.51
$10.51
143 #4
PL32M
SEALANT
2
$92.31
$184.62
Step: 143.1
Step: 143.2
Step: 143.3
Step: 143.4
Step: 143.5
Completed
Completed
Completed
Completed
Completed
Gained access for Borescope. IAW CMP 710025 paragraph (B) 1-10
Complied with ChIP 710025 from step (11)(a) through step (51)(c) lAW the rolls Royce
TAY611.8 nun chapter 71.00-00. See squawk 8.3
Complied with ChIP 710025 paragraph 53, (A)-(E) 1-7, 57-58 (A)-(E). Note could not
install other access plugs do to having to order Hylontar.
Left #2 ENG open being that had to order Hy lomar and also awaiting possible second
opinion from RR
Install all inner and outer engine panels and bore scope plugs IAW Rolls Royce TAY-
Ehlhl Chapter 71-00-00.
Discrepancy: 14.4
CMP GIV 710031 Engine - Operational Test
Resolution: COMPLIED WITH CMP GIV 710031 Engine - Operational Test.
Labor USD:
No Charge
N/C
Discrepancy: 14.5
CMP GIV 730001 Fuel Contamination Check (Engine) - Inspection
Resolution: C/W CMP GIV 730001 Fuel Contamination Check (Engine) - Inspection I/A/W RR Tay 611.8 EMM 73-11.03. No defects
noted
For detail description of the work complied with see the Work Order Detail report.
Unless (Ahem'
GAC_WorkOrderPrelintinaryInvoicespt
indicated, all financial values listed in this document are in US Dollars (USD).
Page 32 of 57
Printed: 4/18/2013 11:38:5 IA)
Rst X
EFTA00609765
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Discrepancy: 14.6
CMP GIV 742001 Engine Ignition System - Operational Test
Resolution: COMPLIED WITH CMP GIV 742001 Engine Ignition System - Operational Test. Ops Check Ok. All Maintenence
Performed In Reference To GIV AMM 74-00-00.
Discrepancy: 14.7
CMP GIV 742006 Eng 1 / No. 2 Igniter Plug - Removal / Installation
Resolution: Remove engine #1 ignitor plug #2 P/N Y183-5 SIN 1204. Instaled new engine #1 ignitor plug #2 PIN Y183-5 S/N 12047184.
IAW RR EMM 74-21-03.
Discrepancy: 14.8
CMP GIV 742016 No. 2 Igniter Plug - Inspection
Resolution: COMPLIED WITH CMP GIV 742016 No. 2 Igniter Plug - Inspection. REF item 8 for discrepancies found. Work
performed IAW RR MM 74.21.03.
Discrepancy: 14.9
CMP GIV 774955 CHIP DETECTOR, ENG--INSP
Resolution: C/W CMP GIV 774955 CHIP DETECTOR, ENG--INSP UMW RR Tay 6-11 EMM 77-33-01 No defects noted
Labor USD:
Billing Method
Hours
Rate
Total
No Charge
l'i/ C
Pans USD:
Time and Material
$176.00
Total USD:
$176.00
Parts:
Ref. No.
Part number:
Description
Quantity
Sell price USD
Extended USD
14.9#2
BR49120
RING
4
$11.00
$44.00
14.9 #3
BR49120
RING
12
$11.00
$132.00
Discrepancy: 14.10 CMP GIV 792007 Filter, Engine Pressure Oil - Cleaning/Inspection
Resolution: C/W CMP GIV 792007 Filter, Engine Pressure Oil - 72.01.01. No defects noted
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_WorkOrderPreliminaryInvoicespt
Page 33 of 57
Printed: 4/18/2013 11:38:5IA)
Rd X
EFTA00609766
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Billing Method
Houri.
Rate
Total
Labor USD:
No Charge
N/ C
Pans USD:
Time and Material
$33.25
Total USD:
$33.25
Parts:
Ref. No.
Part number:
Description
Quantity
Sell price USD
Extended USD
14.10 #3
1159CGSK792007
LIENG.OIL FILTER - R&I / 1000-3999
1
S33.25
$33.25
Discrepancy: 14.11 CMP GIV 792013 Engine Scavenge Strainers - Inspection
Resolution: C/W CMP GIV 792013 Engine Scavenge Strainers - Inspection UMW RR Tay 611-8 EMM 72.01.01 No defects noted
Billing Method
Hours
Rate
Total
Labor USD:
No Charge
N/ C
Pans USD:
Time and Material
$195.60
Total USD:
$195.60
Parts:
Ref. No.
Part number:
Description
Quantity
Sell price USD
Extended USD
14.11 #2
KB22722
O-RING
1
$8.40
$8.40
14.11 #3
KB22726
SEAL
I
$8.03
$8.03
14.11 #4
KB22727
O-RING
4
$33.00
$132.00
14.11 #5
KB22730
SEAL
2
$7.62
$15.24
14.11 #6
KB22732
0 RING
I
$31.93
$31.93
Discrepancy: 14.12 CMP GIV 710020 Powerplant Internal - Inspection
Resolution: COMPLIED WITH CMP GIV 710020 Powerplant Internal - Inspection IAW GIV AMM 71.00.00. Ref 8.24 for
descrepancies.
Labor USD:
No Charge
N/ C
Discrepancy: 14.13 CMP GIV 710026 Engine Borescope - Inspection
Resolution: COMPLIED WITH CMP GIV 710026 Engine Borescope - Inspection IAW RR TAY EMM 71.00.00.
Labor USD:
Pans USD:
Billing Method
Flours
Rate
Total
No Charge
Time and Material
N/ C
$147.71
Total USD:
$147.71
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_WorkOrderPrelintinaryInvoicespt
Page 34 of 57
Printed: 4/18/2013 11:38:5 IA)
Rd X
EFTA00609767
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Parts:
Ref. No.
Part number:
Description
Quantity
Sell price USD
Extended USD
14.13 #1
kS43013-210
ORING
1
$17.72
$17.72
14.13#2
AS43013-348
ORING
2
$59.74
$119.48
14.13 #3
KB22748
O-RING
1
$10.51
$10.51
Step: 14.13.1
Step: 14.13.2
Step: 14.13.3
Completed
Gained access for Borescope. lAW CMP 710025 paragraph (B) 1-10
Completed
Complied with CMP 710026 from step (11)(a) through step (51)(c) lAW the rolls Royce
TAY611.8 nun chapter 71.00-00. See squawk 8.4.
Completed
Install all inner and outer engine panels and bore scope plugs 1AW Rolls Royce TAY-
EMM Chapter 71.00.00.
Discrepancy: 14.14 CMP GIV 710032 Engine - Operational Test
Resolution:
Discrepancy: 14.15 CMP GIV 730002 Fuel Contamination Check (Engine) - Inspection
Resolution: COMPLIED WITH CMP GIV 730002 Fuel Contamination Check (Engine) - Inspection. No defects noted IAW RR TAY
611-8 MM 73-11-03.
Labor USD:
No Charge
N/ C
Discrepancy: 14.16 CMP GIV 742002 Engine Ignition System - Operational Test
Resolution: COMPLIED WITH CMP GIV 742002 Engine Ignition System - Operational Test. Ops Check Ok. All Maintenence
Performed In Reference To GIV AMM 74-00-00.
Discrepancy: 14.17 CMP GIV 742008 Eng #2 / No. 2 Igniter Plug - Removal / Installation
Resolution: Remove Engine #2 ignitor #2 P/N Y183-5 S/N 0601749. Installed new Engine #2 ignitor #2 P/N Y183-5 S/N 12047194.
JAW RR EMM 74-21-03.
Discrepancy: 14.18 CMP GIV 742018 No. 2 Igniter Plug - 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_WorkOrderPreliminaryInvoicespt
Page 35 of 57
Printed: 4/18/2013 11:38:5 IA)
Rd X
EFTA00609768
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Resolution: COMPLIED WITH CMP GIV 742018 No. 2 Igniter Plug- Inspection. REF Item 8.2 for discrepancies found. Work
performed IAW RR MM 74.21.03
Discrepancy: 14.19 CMP GIV 774956 CHIP DETECTOR, ENG--INSP
Resolution: COMPLIED WITH CMP GIV 774956 CHIP DETECTOR, ENG—INSP. No defects noted LAW RR TAY 611.8 MM
77-33.01.
Labor USD:
Billing Method
Hours
Rate
Total
No Charge
N/ C
Pans USD:
Time and Material
$176.00
Total USD:
$176.00
Parts:
Ref. No.
Part number:
Description
Quantity
Sell price USD
Extended USD
14.19 #1
BR49120
RING
12
$11.00
$132.00
14.19#2
BR49120
RING
4
$11.00
$44.00
Discrepancy: 14.20 CMP GIV 792009 Filter, Engine Pressure Oil - Cleaning/Inspection
Resolution: COMPLIED WITH CMP GIV 792009 Filter, Engine Pressure Oil - Cleaning/Inspection. No defects noted IAW RR TAY
611-8 MM
Labor USD:
72-01-01.
Billing Method
Houri.
Rate
Total
No Charge
N/ C
Pans USD:
Time and Material
$31.25
Total USD:
$31.25
Parts:
Ref. No.
Part number:
Description
Quantity
Sell price USD
Extended USD
14.20#2
EU18144
WASHER
1
$8.80
$8.80
14.20 #3
KB22782
SEAL
1
$22.45
$22.45
Discrepancy: 14.21 CMP GIV 792014 Engine Scavenge Strainers - Inspection
Resolution: COMPLIED WITH CMP GIV 792014 Engine Scavenge Strainers - Inspection. No defects noted IAW RR TAY 611-8
MM 72-01-01.
Billing Method
Hours
Rate
Total
Labor USD:
Pans USD:
No Charge
Time and Material
N/C
$195.60
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_WorkOrderPrelintinaryInvoicespt
Page 36 of 57
Printed: 4/18/2013 11:38:5 IA)
Rd X
EFTA00609769
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Total USD:
Parts:
Ref. No.
Part number:
Description
Quantity
$195.60
Sell price USD
Extended USD
14.21 #2
KB22722
O-RING
1
$8.40
$8.40
14.21 #3
KB22726
SEAL
1
$8.03
$8.03
14.21 #4
KB22727
O-RING
4
$33.00
$132.00
14.21 #5
KB22730
SEAL
2
$7.62
$15.24
14.21 #6
KB22732
0 RING
1
$31.93
$31.93
Discrepancy: 14.22
Related CMP Codes
Resolution:
Discrepancy: 14.23 CMP GIV 711009 Cowl Latch, Engine (Left) - Rigging
Resolution: CM CMP GIV 711009 Cowl Latch, Engine (Left) - Rigging GIV AMM 71-02-00 No defects noted
Billing Method
Hours
Rate
Total
Labor USD:
Flat Rate
$230.00
Total USD:
$230.00
Discrepancy: 14.24 CMP GIV 732001 Engine Acceleration Test / Adjustment
Resolution:
Step: 14.24.1
Completed
Removed all R/H horizontal stabilizer panels required for CMP 551020. AB work
I.A.W. GIV NUM 55-14-00.
Discrepancy: 14.25 CMP GIV 732005 Engine Deceleration Test / Adjustment
Resolution:
Labor USD:
Parts USD:
Billing Method
Hours
Rate
Total
Flat Rate
No Charge
$460.00
N/ C
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_WorkOrderPrelintinaryInvoicespt
Page 37 of 57
Printed: 4/18/2013 11:38:5 IA)
Ftst X
EFTA00609770
Bill To: JEGE, INC.
WO 8: SC13175
Invoice Number:
Total USD:
$460.00
Discrepancy: 14.26 CMP GIV 732049 ENG HANDLE ACU SOLENOID CK
Resolution:
Step: 14.26.1
Completed
In progress removal of R/H horizontal stabilizer and elevator panels required for CMP
551023 ;Panels on top of R/H elevator still need to be removed, for details of panels
removed refer to the open and close section of the R/1 log book . All work I.A.W. GIV
MAI 55-14-00.
Discrepancy: 14.27 CMP GIV 732057 SOLENOID, ENG APPR IDLE-OPS
Resolution:
Discrepancy: 14.28 CMP GIV 732011 GROUND IDLE, ENG-TEST/ADJUST
Resolution:
Parts USD:
No Charge
N/ C
Discrepancy.: 14.29
CM!)
7321113 APPROACH IDLE, ENG•TEST/ADJ
Resolution:
Discrepancy: 14.30 CMP GIV 783013 Thrust Reverser Interlock Feedback System (Left) - Operational Test
Resolution:
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_WorkOrderPreliminaryInvoicespt
Page 38 of 57
Printed: 4/18/2013 11:38:5IA)
Rd X
EFTA00609771
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Discrepancy: 14.31 CMP GIV 783014 Thrust Reverser Interlock Feedback System (Right) - Operational Test
Resolution:
Discrepancy: 14.32 CMP GIV 783017 MAX REV THRUST, L-OPS TEST/ADJ
Resolution:
Paris USD:
No Charge
N/ C
Discrepancy: 14.33 CMP GIV 783018 MAX REV THRUST, R-OPS TEST/ADJ
Resolution:
Discrepancy: 14.34 CMP GIV 791033 Oil Level - Check / Service
Resolution:
Discrepancy: 14.35 CMP GIV 711010 Cowl Latch, Engine (Right) - Rigging
Resolution: Complied with CMP GIV 711010 Cowl Latch, Engine (Right) - Rigging. No defects noted IAW GIV AMM 71.02.00.
Billing Method
Hours
Rate
Total
Labor USD:
Time and Material
ST
2.65
@
$118.00
$312.70
Total USD:
$312.70
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_WodcOrderPreliminarylnvoice.rpt
Page 39 of 57
Printed: 4/18/2013 11:38:5 IA)
Rd X
EFTA00609772
Bill To: JEGE, INC.
WO 8: SC13175
Discrepancy: 14.36 CMP GIV 732002 Engine Acceleration Test / Adjustment
Resolution:
Invoice Number:
Discrepancy: 14.37 CMP GIV 732006 Engine Deceleration Test / Adjustment
Resolution:
Discrepancy: 14.38 CMP GIV 732050 ENG HANDLE ACU SOLENOID CK
Resolution:
Discrepancy: 14.39 CMP GIV 732058 SOLENOID, ENG AI'PR IDLE-OPS
Resolution:
Discrepancy: 14.40 CMP GIV 750006 AIRFLOW CONT SYS -TEST
Resolution:
Discrepancy: 14.41 CMP GIV 732012 GROUND IDLE, ENG-TEST/ADJUST
Resolution:
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_WorkOrderPrelintinaryInvoicespt
Page 40 of 57
Printed: 4/18/2013 11:38:5 IA)
Ftst X
EFTA00609773
Bill To: JEGE, INC.
WO #: SC13175
Discrepancy: 14.42 CMP GIV 732014 APPROACH IDLE, ENG-TEST/ADJ
Resolution:
Invoice Number:
Discrepancy: 14.43 CMP GIV 791034 Oil Level - Check / Service
Resolution:
Item: 15
Customer Supplied Due List
Team Manager: Sean Brown
Customer Coordinator: Ray Kraber
Pan/Model 0:
AC Serial No./Tail No.:
TSN/TSO:
CSN/CSO:
Aircraft Time: 8,567.0 / 3,964
Discrepancy: 15.1
Resolution:
Comply with Customer Supplied Due List
Billing Method
flours
Rate
Total
Labor USD:
Flat Rate
$39,560.00
Pans USD:
Time and Material
$268.20
Total USD:
$39,828.20
Parts:
Ref. No.
Part number:
Description
Quantity
Sell price USD
Extended USD
15.1 #2
PR I440
-B-2
SEALANT, PRC, CARTRIDGE 6oz
3
$26.82
$80.46
15.1 #3
PR I440
-B-2
SEALANT, PRC, CARTRIDGE 6oz
2
$26.82
$53.64
15.1 #4
PR1440-8-2
SEALANT, PRC, CARTRIDGE 6oz
4
$26.82
$107.28
15.1 #5
PR1440-8-112
SEALANT, PRC,CARTRIDGE
1
$26.82
$26.82
Discrepancy: 15.2
CMP GIV 100310 Check Airworthiness Directives
Resolution: Complied with Airworthiness Directives check as required.
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_WorkOrderPrelintinaryInvoicespt
Page 41 of 57
Printed: 4/18/2013 11:38:5 IA)
Rd X
EFTA00609774
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Discrepancy: 15.3
CMP GIV 100320 AIRWORTHINESS CHECK
Resolution: COMPLIED WITH CMP GIV 100320 AIRWORTHINESS CHECK as required.
Discrepancy: 15.4
CMP GIV 191108 Review Aircraft Status and Records
Resolution: Complied with Aircraft Status and Records Review as required.
Discrepancy: 15.5
CMP GIV 231001 AVIONICS--FUNC RAMP TEST
Resolution: COMPLIED WITH CMP GIV 231001 AVIONICS--FUNC RAMP TEST with discrepancies noted at this time. See items
in section 6 for discrepancies. All work performed LAW G-IV maintenance manual 34-00.00.
Labor USD:
No Charge
N/ C
Discrepancy: 15.6
CMP GIV 251114 Pilot and Copilot Seat - Inspection / Lubrication
Resolution: COMPLIED WITH CMP GIV 251114 Pilot and Copilot Seat - Inspection / Lubrication. No defects noted. Ref: GIV
AMM 25-11-00.
Labor USD:
No Charge
N/ C
Discrepancy: 15.7
CMP GIV 262045 Fire Bottle (Left Engine) - Hydrostatic Test
Resolution:
Billing Method
Hours
Rate
Total
Labor USD:
No Charge
Services USD:
Time and Material
Total USD:
Services:
N/ C
$773.84
$773.84
Ref. No.
Description
Quantity
Sell Price USD
Extended USD
15.7 #1
HYDROSTATIC TEST
1.00
$773.84
$773.84
Pan Ref: 32700022 FIRE BOTTLE, ENGINE - WITHOUT CARTRIGE (HALON 1301)
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_WorkOrderPrelintinaryinvoicesm
Page 42 of 57
Printed: 4/18/2013 11:38:5 IA)
Rd X
EFTA00609775
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Discrepancy: 15.8
CMP GIV 262050 Fire Bottle (Right Engine) - Hydrostatic Test
Resolution:
Billing Method
Hours
Rate
Total
Services USD:
Time and Material
$773.84
Total USD:
$773.84
Services:
Ref. No.
Description
Quantity
Sell Price USD
Extended USD
15.8 #1
HYDROSTATIC TEST
1.00
$773.84
$773.84
Part Ref: 32700022 FIRE BOTTLE, ENGINE - WITHOUT CARTRIGE (HALON 1301)
Step: 15.8.1
Completed
Entered in Error. Step moved to item 15.9.1.
Discrepancy: 15.9
CMP GIV 270101 Stall Barrier / Angle of Attack System - Ops Test
Resolution: COMPLIED WITH CMP GIV 270101 Stall Barrier / Angle of Attack System - Ops Test with no discrepancies noted at
this time. All work performed JAW G-IV maintenance manual 27.01.01.
Labor USD:
No Charge
N/ C
Step: 15.9.1
Completed
Complied with CMP 270101 Stall Barrier/AOA System - Operational check Steps B(l)
that B(23) with no discrepancies noted at this time. All work performed IAW G-IV
maintenance manual 27.01.01.
Discrepancy: 15.10 CMP GIV 272038 Rudder Pedals - Lubrication
Resolution: COMPLIED WITH CMP GIV 272038 Rudder Pedals - Lubrication. No defects noted. Ref: GIV AMM 27.03.00.
Labor USD:
No Charge
N/ C
Discrepancy: 15.11 CMP GIV 275009 Flap Actuator Yoke (Left Inboard) - Inspection
Resolution: COMPLIED WITH CMP GIV 275009 Flap Actuator Yoke (Left Inboard) - Inspection. No defect noted at this time.
Work IAW GIV MM 27.06.00.
Labor USD:
Pans USD:
No Charge
No Charge
N/C
N/C
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_WorkOrderPrelintinaryinvoicespt
Page 43 of 57
Printed: 4/18/2013 11:38:5IM.
Rd X
EFTA00609776
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Discrepancy: 15.12 CMP GIV 275010 Flap Actuator Yoke (Right Inboard) - Inspection
Resolution: COMPLIED WITH CMP GIV 275010 Flap Actuator Yoke (Right Inboard) - Inspection. No defect noted at this time.
Work IAW GIV MM 27-06-00.
Labor USD:
No Charge
Pans USD:
No Charge
N/C
N/C
Discrepancy: 15.13 CMP GIV 275011 Flap Actuator Yoke (Left Outboard) - Inspection
Resolution: COMPLIED WITH CMP GIV 275011 Flap Actuator Yoke (Left Outboard) - Inspection. No defect noted at this time.
Work IAW GIV MM 27-06-00.
Billing Method
Hours
Rate
Total
Pans USD:
Time and Material
$57.60
Total USD:
$57.60
Parts:
Ref. No.
Part number:
Description
Quantity
Sell price USD
Extended USD
15.13 82
ADLFS-4005
BUSHING
I
$57.60
$57.60
Discrepancy: 15.14 CMP GIV 275012 Flap Actuator Yoke (Right Outboard) - Inspection
Resolution: COMPLIED WITH CMP GIV 275012 Flap Actuator Yoke (Right Outboard) - Inspection. No defect noted at this time.
Work IAW GIV MM 27.06.00.
Labor USD:
Pans USD:
No Charge
No Charge
N/C
N/C
Discrepancy: 15.15 CMP GIV 275027 Flap Actuator Bushing (Left) - Service / Lubrication
Resolution:
Discrepancy: 15.16 CMP GIV 275028 Flap Acuator Bushing (Right) - Service / Lubrication
Resolution:
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_WorkOrderPrelintinaryInvoicespt
Page 44 of 57
Printed: 4/18/2013 11:38:5 IA)
Rd X
EFTA00609777
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Discrepancy: 15.17 CMP GIV 280005 Fuel Control System - Functional Test
Resolution:
Discrepancy: 15.18 CMP GIV 303005 Pitot Heat System - Operational Test
Resolution: COMPLIED WITH CMP GIV 303005 Pitot Heat System - Operational Test with no discrepancies noted at this time. All
work performed IAW G-IV maintenance manual 30-03-00.
Labor USD:
No Charge
N/ C
Discrepancy: 15.19 CMP GIV 531007 FS 85 Bulkhead - Inspection
Resolution: COMPLIED WITH CMP GIV 531007 FS 85 Bulkhead - Inspection.No defects noted. All work accomplished IAW GIV
AMM 53-12-00.
Billing Method
Hours
Rate
Total
Labor USD:
No Charge
N/ C
Pans USD:
Time and Material
$6.84
Total USD:
$6.84
Parts:
Ref. No.
Pan number:
Description
Quantity
Sell price USD
Extended USD
15.19 NI
RTV732-3OZ.CLR
SEALANT, CLEAR
I
$6.84
$6.84
Step: 15.19.1
Completed
Complied with steps B(1) thru B(I) of CMP GIV 531007 Instructions. No defects noted.
All work accomplished IAW GIV AMM 53-12-00.
Discrepancy: 15.20 CMP GIV 532007 Forward Cabin Compartment Below Floor - Inspection
Resolution: COMPLIED WITH CMP GIV 532007 Forward Cabin Compartment Below Floor - Inspection with no defects noted. All
work perfeormed IAW. G-IV MM. 53.20.00.
Labor USD:
Parts USD:
Billing Method
Hours
Rate
Total
No Charge
Time and Material
N/ C
$162.66
Total USD:
$162.66
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_WorkOrderPreliminaryinvoicespt
Page 45 of 57
Printed: 4/18/2013 11:38:5 IA)
Flee X
EFTA00609778
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Parts:
Ref. No.
Part number:
Description
Quantity
Sell price USD
Extended USD
15.20 NI
D9100
TAPE, 3 INCH FLAME RETARDANT
1
$162.66
$162.66
Discrepancy: 15.21 CMP GIV 532009 Midcabin Compartment Below Floor - Inspection
Resolution: COMPLIED WITH CMP GIV 532009 Midcabin Compartment Below Floor - Inspection with no defects noted. All work
performed IAW. G-IV MM. 53-30-00
Labor USD:
No Charge
N/ C
Discrepancy: 15.22 CMP GIV 532011 Aft Cabin Compartment Below Floor - Inspection
Resolution: COMPLIED WITH CMP GIV 532011 Aft Cabin Compartment Below Floor - Inspection w ith no defects noted. .‘11 work
performed IAW. G-IV MM. 53.50.00.
Labor USD:
No Charge
N/ C
Discrepancy: 15.23 CMP GIV 551019 Horizontal Stabilizer / Elevator (Exterior) {Left} - Inspection
Resolution: COMPLIED WITH CMP GIV 551019 Horizontal Stabilizer / Elevator (Exterior) (Left) - Inspection. IAW GIV AMM
55-14-00. No defects noted at this time.
Labor USD:
No Charge
N/ C
Step: 15.23.1
Step: 15.23.2
Completed
Removed all L/H horizontal stabilizer panels required for CNIP 551019. All work LA. W.
GIV M/6155.14-00.
Completed
C/W section B thru B(h) of CMP 551019. No discrepancies noted at this time. All work
I.A.W. GIV M/M 55-14.00.
Discrepancy: 15.24 CMP GIV 551020 Horiz Stabilizer / Elevator (Exterior) {Right} - Insp
Resolution: COMPLIED WITH CMP GIV 551020 Horiz Stabilizer / Elevator (Exterior) {Right) - Insp. No discrepancies noted at
time. All work I.A.W. GIV M/M 55.00.00.
Labor USD:
No Charge
N/ C
Step: 15.24.1
Step: 15.24.2
Completed
Removed all R/H horizontal stabilizer panels required for CMP 551020. AU work
I.A.W. GIV M/M 55-14-00.
Completed
(:/W section B thru B(h) of CMP 551020. No discrepancies noted. AU work I.A.W.
MAI 55.00.011
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_WoikOrderPreliminarylnvoice.rpt
Page 46 of 57
Printed: 4/18/2013 11:38:5 IA)
Rd X
EFTA00609779
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Discrepancy: 15.25 CMP GIV 551023 Horizontal Stabilizer / Elevator (Interior / Exterior) (Left) - Inspection
Resolution: COMPLIED WITH CMP GIV 551023 Horizontal Stabilizer / Elevator (Interior / Exterior) (Left) - Inspection. See sqk
8.23 and 8.20 for discrepancies noted. All work I.A.W. GIV M/M 55.14.00.
Labor USD:
No Charge
N/ C
Step: 15.25.1
Step: 15.25.2
Completed
Removed all L/H horizontal stabilizer and elevator panels required for CMP 551023. All
work I.A.W. GIV M/M 55.14.00.
Completed
(:/W section B thru B(k) of CMP 551023. See sqk 8.23 and8.20 for discrepancies noted.
All work I.A.W. GIV M/M 55-14-00.
Discrepancy: 15.26 CMP GIV 551024 Hz Stabilizer/Elevator (Interior/Exterior) (Right) - Insp
Resolution: COMPLIED WITH CMP GIV 551024 Hz Stabilizer/Elevator (Interior/Exterior) (Right) - Insp. See sqk 8.21 and 8.22 for
discrepancies noted. All work I.A.N. GIV M/M 55-00-00.
Labor USD:
No Charge
N/ C
Step: 15.26.1
Step: 15.26.2
Completed
In progress removal of It/11 horizontal stabilizer and elevator panels required for CMP
551023 for details of the panels already removed refer to the open and close section of
the R/I log book. All work I.A.W. GIV M/M 55-14-00.
Completed
Removed remaining required panels for CMP 551024. C/W section B thru B(k) of CMP
551024. See sqk 8.21 and 8.22 for discrepancies noted. All work I.A.W. GIV hf/M
55.00.00.
Discrepancy: 15.27 CMP GIV 553005 Vertical Stabilizer / Rudder (External) - Inspection
Resolution: COMPLIED WITH CMP GIV 553005 Vertical Stabilizer / Rudder (External) - Inspection. REF GIV MM 55-30-00,
CMP 553005. No defects noted.
Labor USD:
No Charge
N/ C
Discrepancy: 15.28 CMP GIV 553007 Vertical Stabilizer / Rudder (Internal) - Inspection
Resolution: COMPLIED WITH CMP GIV 553007 Vertical Stabilizer / Rudder (Internal) - Inspection. IAW GIV AMM 55-30-00. No
defects noted at this time.
Labor USD:
No Charge
N/ C
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_WorkOrderPreliminaryInvoicespt
Page 47 of 57
Printed: 4/18/2013 11:38:5IA)
Rd X
EFTA00609780
Bill To: JEGE, INC.
WO 9: SC13175
Invoice Number:
Step: 15.28.1
Completed
Removed Vertical Stab zone 109 LH trailing edge panels as per CMP GIV 553007.
Continue panel removal to facilitate CMP GIV 553007 Vertical Stabilizer / Rudder
(Internal) - Inspection.
Step: 15.28.2
Completed
Continued removing panels to gain access for inspection. Removed panels 109-LE-2,
I09-LH-9, 109-LH-11, 109-1.H10, 109-RB-1, 109-1.H-8, 110-LH-I,110-LH-2, 110-LH-3,
110-LH-4, 110-LH-5, 110-LH-6, 109-LH-7. Work done JAW G1V CMP 553007 & GIV
Mal 55-30-00.
Step: 15.28.3
Completed
Continue with removal of all requiered panels of CMP 553007; And Complied with
steps B.(I) thru step B(22).All work done IAN' GIV AMM 53-30-00.
Discrepancy: 15.29 CMP GIV 571011 Wing Front Beam Hi-Lite Collars (Left) - Inspection
Resolution: COMPLIED WITH CMP GIV 571011 Wing Front Beam Hi-Lite Collars (Left) - Inspection as per GIV MM 57-11-00.
Reference squawk 8.26.
Labor USD:
No Charge
N/ C
Discrepancy: 15.30 CMP GIV 571012 Wing Front Beam Hi-Lite Collars (Right) - Inspection
Resolution: COMPLIED WITH CMP GIV 571012 Wing Front Beam Hi-Lite Collars (Right) - Inspection as per GIV MM 57-11-00.
Reference item 8.28 for defect.
Labor USD:
No Charge
N/ C
Discrepancy: 15.31 CMP GIV 571025 Wing Tank Interior (Left) - Inspection
Resolution:
Labor USD:
No Charge
N/ C
Discrepancy: 15.32 CMP GIV 571026 Wing Tank Interior (Right) - Inspection
Resolution:
Labor USD:
No Charge
N/ C
Step: 15.32.1
Completed
Removed R/H wing fuel panels 22-FT-1, 22-FT-2, 22-FT-3, 22-FT-4, 22-Fr-5. Work
done IAVVI GIV NI/11 28.11-00.
Discrepancy: 15.33 Related CMP Codes
Resolution:
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_WorkOrderPrelintinaryInvoicespt
Page 48 of 57
Printed: 4/18/2013 11:38:5 IA)
Rd X
EFTA00609781
Bill To: JEGE, INC.
WO ft: SC13175
Invoice Number:
Discrepancy: 15.34 CMP GIV 251109 SEAT ASSEMBLY, PILOT
Resolution: COMPLIED WITH CMP GIV 251109 SEAT ASSEMBLY, PILOT. Removed pilot seat assy. (PN: 1159SCF213-5, SN:
11217) and installed pilot seat assy. (PN: 1159SCF213-5, SN: 11217). Ref: GIV AMM 25-10-00.
Labor USD:
No Charge
N/ C
Discrepancy: 15.35 CMP GIV 251110 SEAT ASSEMBLY, COPILOT
Resolution: COMPLIED WITH CMP GIV 251110 SEAT ASSEMBLY, COPILOT. Removed copilot seat assy. (PN: 1159SCF213.6,
SN: 10980) and installed copilot seat assy. (PN: 1159SCF213-6, SN: 10980). Ref: GIV AMM 25-10-00.
labor USD:
No Charge
N/ C
Discrepancy: 15.36 CMP GIV 262025 Engine Fire Bottle ( Left ) - Remo'
/ Installation
Resolution:
labor USD:
No Charge
N/ C
Step: 15.36.1
Completed
Removed LAI fire bottle PIN 32700022 SAN 06758C2, squibs removed and stored in
parts room. 1/ANt. GIV AMM 26-02-00
Discrepancy: 15.37 CMP GIV 262065 Fire Bottle (Left Engine) - Weight Check
Resolution:
Discrepancy: 15.38 CMP GIV 262030 Engine Fire Bottle (Right) - Removal / Installation
Resolution:
Labor USD:
No Charge
N/ C
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_WorkOrderPreliminaryInvoicespt
Page 49 of 57
Printed: 4/18/2013 11:38:51M
Rd X
EFTA00609782
Bill To: JEGE, INC.
WO It: SC13175
Invoice Number:
Step: 15.38.1
Completed
Removed R/H fire bottle P/N 32700022 S/N 12204C1, squibs removed and stored in
parts room. I/A/W GIV AMM 26-02-00
Discrepancy: 15.39 CMP GIV 262070 Fire Bottle (Right Engine) - Weight Check
Resolution:
Discrepancy: 15.40 CMP GIV 275003 Flap (Left)
Resolution:
Labor USD:
No Charge
N/ C
Step: 15.40.1
Step: 15.40.2
Completed
Complied with CMP 275003 LEFT FLAP REMOVAL/ INSTALLATION steps A, B
and C as required. Work IAW GIV MM 27-06-00.
Completed
Remove 1.H Flap PN 1159C520005-543 SN 1086
Discrepancy: 15.41 CMP GIV 275004 Flap (Right)
Resolution:
Labor USD:
No Charge
N/ C
Step: 15.41.1
Step: 15.41.2
Completed
Complied with CMP 275004 RIGHT FLAP REMOVAL/ INSTALLATION steps A, B
and C as required. Work IAW GIV Mbl27-06-00.
Completed
Remove RH flap PN 1159CS20005-S44 SN 1085
Discrepancy: 15.42 CMP GIV 275005 Inboard Flap Actuator (Left) - Removal / Installation
Resolution:
Labor USD:
No Charge
N/ C
Step: 15.42.1
Completed
Performed CMP code 275005 Remove Inbd Flap Actuator PN 1159SCC2I1-13
SN44-514 steps B-I through B-I0 complete.
Discrepancy: 15.43 CMP GIV 275007 Outboard Flap Actuator (Left) - Removal / Installation
Resolution:
Labor USD:
No Charge
N/ C
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_WorkOrderPreliminaryInvoicespt
Page 50 of 57
Printed: 4/18/2013 11:38:5 IA)
Rd X
EFTA00609783
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Step: 15.43.1
Completed
Performed CMP code 275007 Remove Outbd Flap Actuator PN 1159SCC212-13
5N34-624 steps B-1 through B-I I complete.
Discrepancy: 15.44 CMP GIV 275006 Inboard Flap Actuator (Right) - Removal / Installation
Resolution:
Labor USD:
No Charge
N/ C
Step: 15.44.1
Completed
Complied with CMP 275006 Inboard Flap Actuator (Right) - Removal / Installation
steps A and B. Work lAW GIV N13127-06-00.
Discrepancy: 15.45 CMP GIV 275008 Outboard Flap Actuator (Right) - Removal / Installation
Resolution:
Labor USD:
No Charge
N/ C
Step: 15.45.1
Completed
Complied with CMP 275008 Outboard Flap Actuator (Right) - Removal / Installation
steps A and B. Work lAW GIV MM27.06.00.
Discrepancy: 15.46 CMP GIV 273003 Elevator Free Play - Inspection
Resolution: COMPLIED WITH CMP GIV 273003 Elevator Free Play - Inspection. IAW GIV AMM 27-01-00. No defects noted at
this time.
Labor USD:
No Charge
N/ C
Discrepancy: 15.47 CMP GIV 231114 HF Communications System No. 1 - Operational Check
Resolution:
Discrepancy: 15.48 CMP GIV 231117 HF Communication Antenna - Continuity Check (Installed)
Resolution:
Discrepancy: 15.49 CMP GIV 231155 HF Communication Antenna Assembly - Removal / Installation
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_WorkOrderPrelintinaryInvoicespt
Page 51 of 57
Printed: 4/18/2013 11:38:5 IA)
Rd X
EFTA00609784
Bill To: JEGE, INC.
WO #: SC13175
Resolution:
Invoice Number:
Discrepancy: 15.50 CMP GIV 231115 HF COMM SYS 82-0PS TEST
Resolution:
Discrepancy: 15.51 CMP GIV 280018 Fuel Tank (Left) - Leak Check
Resolution:
Discrepancy: 15.52 CMP GIV 574005 Wing Leading Edge (Left Inboard) - Removal / Installation
Resolution:
Labor USD:
Pans USD:
Total USD:
Parts:
Billing Method
No Charge
Time and Material
Hours
Rate
Total
N/C
$347.34
$347.34
Ref. No.
Part number:
Description
Quantity
Sell price USD
Extended USD
15.52 #1
M83248/I-226
0 RING PACKING-HT61,1.974 ID
6
$1.61
$9.66
S2L-226 S2D-226
1532 #2
M83248/1-230
0 RING PACKING-HTM,2.474 ID
24
$1.26
$30.24
1532 #3
G(;510C300A
GASKET
2
$153.72
$307.44
Step: 15.52.1
Completed
Remove LH wing leading edge gap bands. Remove bottom screws from inbd section of
leading edge and some of the top screws. Removal is in progerss, leading edge can be
removed after all screws are removed.
Discrepancy: 15.53 CMP (NV 574011 Wing Leading Edge (Left Center) - Removal / Installation
Resolution:
Labor USD:
No Charge
N/ C
For detail description of the work complied with see the Work Order Detail report.
GAC_WorkOrderPreliiiiinaryinvoicespt
Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD).
Page 52 of 57
Printed: 4/18/2013 11:38:5 IA)
Rst X
EFTA00609785
Bill To: JEGE, INC.
WO it: SC13175
Invoice Number:
Step: 15.53.1
Completed
Remove gap band 2I-LE-4 ansd center section leading edge from aircraft for Inspection
2ILE-5
Discrepancy: 15.54 CMP GIV 574017 Wing Leading Edge (Left Outboard) - Removal / Installation
Resolution:
Labor USD:
No Charge
Step: 15.54.1
N/ C
Completed
Remove gap bands 21-LE-6 and 211.E-8. Remove outboard section leading edge 211.E-7
from wing.
Discrepancy: 15.55 CMP GIV 574006 Wing Leading Edge (Right Inboard) - Removal I Installation
Resolution:
Labor USD:
Pans USD:
Total USD:
Parts:
Billing Method
No Charge
Time and Material
Flours
Rate
Total
N/C
$134.10
$134.10
Ref. No.
Part number:
Description
Quantity
Sell price USD
Extended USD
15.55 #1
PRI440-B-1/2
SEALANT, PRC,CARTRIDGE
2
$26.82
$53.64
15.55 #2
PR1440-B-1/2
SEALANT, PRC,CARTRIDGE
I
$26.82
$26.82
15.55 #3
PR1440-B-1/2
SEALANT, PRC,CARTRIDGE
2
$26.82
$53.64
Step: 15.55.1
Completed
Remove gap bands 22-LE-2 and 22LE-4 and inbd leading edge screws (except for 4
upper screws).
Discrepancy: 15.56 CMP GIV 574012 Wing Leading Edge (Right Center) - Removal / Installation
Resolution:
Labor USD:
No Charge
N/C
Discrepancy: 15.57 CMP GIV 574018 Wing Leading Edge (Right Outboard) - Removal / Installation
Resolution:
Labor USD:
No Charge
N/C
Discrepancy: 15.58 CMP GIV 280010 Defueling Procedures
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_Work0rderPrelititinaryInvoicespt
Page 53 of 57
Printed: 4/18/2013 11:38:5 IA)
Rd X
EFTA00609786
Bill To: JEGE, INC.
Resolution:
WO ft: SC13175
Invoice Number:
Labor USD:
No Charge
N/ C
Discrepancy: 15.59 CMP GIV 282025 Fuel Pickup Screen (Main Left Wing) - Inspection
Resolution:
Discrepancy: 15.60 CMP GIV 282026 Fuel Pickup Screen (Alternate Left Wing) - Inspection
Resolution:
Discrepancy: 15.61 CMP GIV 571003 Wing Fasteners - Cadmium Plating Degradation - Check ( Left )
Resolution:
Discrepancy: 15.62 CMP GIV 280019 Fuel Tank (Right) - Leak Check
Resolution:
Discrepancy: 15.63 CMP GIV 282027 Fuel Pickup Screen (Main Right Wing) - Inspection
Resolution:
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_WorkOrderPrelintinaryInvoicespt
Page 54 of 57
Printed: 4/18/2013
Rd X
EFTA00609787
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Discrepancy: 15.64 CMP GIV 282028 Fuel Pickup Screen (Alternate Right Wing) - Inspection
Resolution:
Item: 16
Pilots for Conditioned Survey Flight (Pre Test Flight)
Team Manager: Sean Brown
Customer Coordinator: Ray Kraber
Pan/Model
AC Serial No./Tail No.:
TSN/TSO:
CSN/CSO:
Aircraft Time: 8,563.8 / 3,963
Discrepancy: 16.1
Resolution:
Two Pilot's for Condition Survey Flight (Must be performed with Item 14. Engine Runs and Borescope)
Billing Method
Hours
Rate
Total
Labor USD:
Flat Rate
$5,500.00
Total USD:
$5,500.00
Discrepancy: 16.2
Perform Preparation for night Test Traveler
Resolution: Complied with GIV Preparation For Flight Test IAW QAP 9.2, RS-OCT-0217 Rev. 01 and RSQCT-54 Rev. IS, refer to
steps for details.
Billing Method
Hours
Rate
Total
Labor USD:
Time and Material
ST
49.62
@
$118.00
$5,855.16
Labor USD:
Time and Material
OT
0.82
@
$177.00
$145.14
Pans USD:
Time and Material
$213.28
Total USD:
$6,213.58
Parts:
Ref. No.
Part number:
Description
Quantity
Sell price USD
Extended USD
16.2 #1
500B4QT
SKYDROL OIL IN QUART CANS
4
$53.32
$213.28
Step: 161.1
Step: 161.2
Step: 16.2.3
Completed
Complied with Preparation for Flight Test Traveler section C thru Q IAW Flight Test
Traveler
Completed
Complied with most items on the checklist. All work done IAW Traveler Number
RS-QCT-0217 Rev. 01.
Completed
Complied with open items on hot cockpit checklist. All work done IAW Traveler
Number RS-QCT-0217 Rev. 01.
Discrepancy: 16.3
Perform bulb sweep
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_WorkOrderPreliminaryInvoicespt
Page 55 of 57
Printed: 4/18/2013 11:38:5 IA)
Rd X
EFTA00609788
Bill To: JEGE, INC.
WO #: SC13175
Invoice Number:
Resolution: Removed several defective lights bulb's on Cockpit Overhead Panel (COP) P/N OL3335 nsn. Installed new lights bulb's
on Cockpit Overhead Panel (COP) PIN 013335 nsn. Op's check good. All work was done JAW Gulfstream GIV AMM
33.10.01.
Billing Method
Houri.
Rate
Total
Labor USD:
Time and Material
ST
4.00
@
$118.00
$472.00
Paris USD:
Time and Material
$51.50
Total USD:
$523.50
Pans:
Ref. No.
Part number:
Description
Quantity
Sell price USD
Extended USD
163 #1
01_3335
LAMP
10
$5.15
$51.50
Discrepancy: 16.4
Service AC with 18000 Lbs (1700 Gal) of fuel for test Flight.
Resolution: Complied with by Signature.
Billing Method
Flours
Rate
Total
Labor USD:
Time and Material
ST
4.00
@
$118.00
$472.00
Total USD:
$472.00
Discrepancy: 16.5
Return to service EJM for Evaluation Flight.
Resolution: ACTT: 8,563.8
LNDS: 3,963
DATE: April 08, 2013
Completed Preflight Inspection Checklist and other maintenance in accordance with EJM Gulfstream G-IV Continuous
Airworthiness Maintenance Program, EJM Maintenance Procedure Manual and 14 CFR 135.411 (a)(2) and is approved
for return to service.
Randy LaPlace, Sr. Airworthiness Inspector
For Gu[(stream West Palm Beach, FL 33406 FAA CRS PB8R624N
Billing Method
Flours
Rate
Total
Lkor USD:
Time and Material
ST
0.57
@
$118.00
$67.26
Total USD:
$67.26
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_WorkOrderPrelintinaryInvoicespt
Page 56 of 57
Printed: 4/18/2013 11:38:5 IA)
Rd X
EFTA00609789
Bill To: JEGE, INC.
WO 0: SC13175
Invoice Number:
Discrepancy: 16.6
Comply with an outbound inspection for test flight.
Resolution: Complied with an outbound inspection for test flight with no defects noted at this time.
Note: This work order is to remain open with open prebuy inspection items to be worked upon return.
Billing Method
Hours
Rate
Total
Labor USD:
Time and Material
ST
0.56
@
5118.00
566.08
Total USD:
$66.08
Communications concerning disputed debts, including a check or other instrument
tendered as full satisfaction of a debt, must be forwarded to:
Gulfstream Aerospace
Attn: Credit Manager
M/S B•05
PO BOX 2206,
Savannah, GA 31402
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_WorkOrderPrelintinaryInvoicespt
Page 57 of 57
Printed: 4/18/2013 11:38:5IA)
Rd X
EFTA00609790
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| Filename | EFTA00609734.pdf |
| File Size | 2969.0 KB |
| OCR Confidence | 85.0% |
| Has Readable Text | Yes |
| Text Length | 88,862 characters |
| Indexed | 2026-02-11T23:03:34.027531 |