EFTA01092968.pdf

Gulfstreame 0 MAMBO, COMPANY WO Association WO #: SC13175 WORKORDER: SC13175 Status: Open Planner: STM: Scan Brown Display Steps: Yes COMMENTS: Pm 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 ITEM # : I Airframe Gulfstream GIV Scheduled N423TT ASSOC STATes DISCREPANCY 1.1 Open Return to Service OM (10 or Mom) 1.2 In Progress Inbound/Outbound Inspection 1.2.1 Completed Inbound/Preliminary Inspection 1.2.2 Open Outbound Inspection 1.3 Completed Preflight Inspection 1.4 Completed Comply with Debrief Checklist 1.4.1 Completed Arrival/Debrief 90 Day Due List Review Accomplished. 1.4.2 Completed List Operator's Airworthiness Requirements & Special Documentation Requests. 1.4.3 Completed Review Technical Operations Update prior to return to service for newly released bulletins and advise operator. 1.5 Open Tool Clearance 1.6 In Progress Cover & Protect 1.7 Completed Service Chemical Toilet/Clean Galley 1.8 Completed Arrival/Departure Assist & Video Aircraft 1.9 Open Sample Hydraulic Fluids 1.10 Open Remove Valuables & Secure. 1.11 In Progress Comply with Service Team Manager Checklist 1.12 Open Fluids Used (Oils/Skydrol) - (Materials Only) 1.13 In Progress STM / Quality review of work order and logbook entry prior to departure 1.14 In Progress Towing (Does not include Hangar Moves) 1.15 Completed 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 GAC_WOAssociation.rpt Page: 1 of 15 Gulfstream Proprietary Printed: 4/23/2013 10:31:27Als EFTA01092968  Gulfstreame OINAMICII COMPANY WO Association WO #: SC13175 Mn'EM # : 1 Airframe Gulfstream GIV Scheduled N423TT ASSOC STATUS DISCREPANCY by Hazmat trained authorized GDAS-PBI personnel only. 1.16 Completed Aircraft Cleaning 1.17 Open Billable Consumables & Shop Supplies 1.18 Completed 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 Sit 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 8. 1.19 Open Update Weight & Balance 1.20 Completed 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. GAC_WOAssociation.rpt Page: 2 of 15 Gulfstream Proprietary Printed: 4/23/2013 10:31:27Als EFTA01092969  Gulfstreame OINAMICII COMPANY WO Association WO #: SC13175 Mn'EM # : 1 Airframe Gulfstream GIV Scheduled N423TT ASSOC STATUS DISCREPANCY * 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. 1.21 Completed "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. ASSOC STATUS DISCREPANCY 6.1 Completed RH wing emergency light inop 6., Open While complying with CMP 231001 Avionics-Functional Ramp Test/Inspection found that the #1 HF system does not transmit. 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. HF receives the Int'l 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 CP lamp illuminated. Further troubleshooting required at this time. All work performed JAW G-IV maintenance manual 23.03.00. 6.3 In Progress 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. 6.4 Waiting While complying with CMP 231001 Avionics-Functional Ramp approval (L) Test/Inspection found that the #1 Auto Throttle reports Excessive Friction and Servo Current Failures when tested. 6.5 Waiting While complying with CMP 231001 Avionics-Functional Ramp approval (L) Test/Inspection found that the #2 Auto Throttle reports Servo Current Failure. 6.6 Waiting Performe Cockpit bulb sweep. While complying with CMP 231001 approval (L) Avionics-Functional Ramp Test/Inspection found that the E-Batts switch capsules just left of the co-pilots yoke are partially inop. 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 inop. 6.7 In Progress Squawk from flight test - Standby fuel gauge totalizer is indicateing GAC_WOAssociation.rpt Page: 3 of 15 Gulfstream Proprietary Printed: 4/23/2013 10:31:27Als EFTA01092970  Gulfstreame 0 MAMBO, COMPANY WO Association WO #: SC13175 ASSOC STATUS DISCREPANCY 2001bs lower than the LT and RT fuel gauges and them is a 150Ibs difference between total fuel on EICAS primary and systems page compared to STBY totalizer gauge - EICAS and SYSTEMs page ind same 6.7.1 Open While defueling aircraft noticed that EICAS read 27501bs It and rt and 54001bs total and 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). 6.8 Open Squawk from flight test - LED light burned out on Rate of Climb / FPM (3 digit from LT) on pressurization controller 6.9 Open Squawk from flight test - With both engines and APU running and both converters on DC volts on the Right-Left-AUX or MS selected indicate 47.8VDC 6.10 Open Squawk from flight test - At FL250 with Batteries only, DC volts on ABEX fluctuates 36.9 to 47.9 v 6.11 Open Squawk from flight test RTU I there is a cyan line across display on screen - splits screen in half 6.12 Open Squawk from flight test - On RNAV approach VNAV worked and then became unavailable on approach 6.13 Open Squawk from flight test - Standby engine instrument gauge is indicating all "8888"s on RT HP gauge 6.14 Open Squawk from flight test - HF radios operated normally but NO SELCAL 6.15 Open EGPWS/Terrain database outdated 6.16 Open Squawk from flight test - aft LAV reading light is inop 6.17 Open Squawk from flight test - cabin management display at VIP , galley screen Mop 6.18 Open Squawk from flight test - perform ops test of nose camera 6.19 Open Satphone is Mop ITEM # : 7 Interior ASSOC STATUS DISCREPANCY 7.1 Open Squawk from flight test - FWD LAV water does not pump 7., In Progress Squawk from flight test - LH galley aft cutting board does not latch 7.2.1 Completed Removed galley drawer and galley latch. All work performed IAW GIV MM 25.20.00. 7.3 Open Squawk from flight test - RH #5 window shade does not fully close 7.4 Open Squawk from flight test - pax air gaspers loose, takes two hands to close the outlet 7.5 In Progress Squawk from flight test fwd cabin door angle wing does not hit headliner when closed. 7.5.1 Completed 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. GAC_WOAssociation.rpt Page: 4 of 15 Gulfstream Proprietary Printed: 4/23/2013 10:31:27Als EFTA01092971  Gil Mire a n WO Association DYNAMICS COM ARMY WO #: SC13175 MDIEM # : 8 Mechanical ASSOC STATUS DISCREPANCY 8.1 Completed The No. I engines Outboard igniter plug is worn 8., Completed The No. 2 engines Outboard igniter plug is worn 8.3 Completed 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. 8.4 Completed 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. 8.5 Completed Squawk from flight test - rubber snipping on leading edge of LT and RT MLG doors are torn 8.6 Completed Squawk from flight test - Copilots seat is difficult to move in fore-aft position 8.7 Completed Squawk from flight test - Gear emergency reset handle not safetied (D-ring) 8.8 Open RH - Squawk from flight test - Raps shudder felt when flaps selected to 39 degrees 8.9 Completed Squawk from flight test - screw needs tightening on panel behind pilots seat below OB panel 8.10 In Progress RH - Squawk from flight test - on the ground the flaps would intermittenly move from 20 to 39 degrees and 10 to 20 when selected. 8.11 Open Squawk from flight test - power levers have 1/2 knob split at 15000ft and 80%HP (It lever is fwd) 8.12 Open Squawk from flight test - while climbing through FL 430 with LT Pack OFF the RT Pack was 25psi (should be 27-33psi) 8.13 Open Squawk from flight test - while climbing through FL 430 with RT Pack OFF the LT Pack was 23psi (should be 27-33psi) 8.14 Completed Squawk from flight test - One O2 mask in LAV and LT and RT AFT rear did not drop during test 8.15 In Progress Squawk from flight test - service hydraulic replenisher 8.16 Open 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 8.17 In Progress 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. 8.17.1 Completed Removed APU generator P/N 1159SCAV373.I05 S/N 129A0171 I/A/W GIV AMM 24.01.01 and sent APU out for repair. 8.18 Completed 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. 8.19 Completed Squawk from flight test - There is a soft spot in floor board just fwd of fwd LAV (feels like blowout panel isnt secure) 8.20 Completed Evaluate flaking paint from steel doubler and adjacent structure on UH horizontal stab at panel 38-UPR-4. GAC_WOAssociation Apt Page: 5 of 15 Culfstream Proprietary Printed: 4/23/20B 10:31:27Als EFTA01092972  Gulfstreame OINAMICII COMPANY WO Association WO #: SC13175 Mn'EM # : 8 Mechanical ASSOC STATUS DISCREPANCY Ref to sqk 15.25 8.21 Completed While working sqk 15.26 CMP 551024. Found corrsion and pitting horizontal stabilizer skin at panel 38-UPR-5. 8.21.1 Completed Mechanicaly removed minor surface corrosion and pitting from panel opening mounting flange and cadmium plated exposed surface. All work done IAW GIV SRM 51.13.10. 8.22 Completed While working sqk 15.26 CMP 551023. Found corrsion and pitting horizontal stabilizer skin at panel 39-UPR-5. 8.22.1 Completed Mechanicaly removed minor surface corrosion and pitting from panel opening mounting flange and cadmium plated exposed surface. All work done IAW GIV SRM 51.13.10. 8.23 Waiting RII - While working CMP 551023 sqk 15.25. Found horizontal stab approval (L) thrust blocks to be worn out of limits. 8.24 Completed #2 Engine EPR Rex line chaffing against fixed cowl. (Flagged) 8.25 In Progress #2 Engine has multiple corroded clamps on forward IB area of engine. 8.25.1 Waiting Insp Removed 12 corroded clamps P/N AS12847 and ASI2817 and 5 clamps P/Ns AS12816 and AS12846 and installed 12 NEW clamps P/N AS12847 and AS12817 and 5 clamps P/Ns AS12816 and ASI2846 IAW RR TAY611.8 MM 71.00.00. 8.26 Completed While performing wing HI-lite Collar (left) inspection CMP code 571011 found collar cracked at LBL 44.0 8.27 Completed 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 8.28 Completed While performing wing HI-lite Collar RT inspection CMP code 571012 found a dented fuel line on center wing leading edge. 8.28.1 Completed Cut and removed 6" section with dent from fuel line PIN:l 159P42012-022FP6 at RBS255.5 of R/H wing. Spliced in new 6" section of tubing on fuel line P/N:I 159P42012-022FP6 at RBS255.5 of R/H wing. All work done IAW CAMPS 2507. 8.29 In Progress RII - 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. 8.30 In Progress RII - 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. 8.31 In Progress RII - 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. 8.32 In Progress RII - 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. 8.33 In Progress Found several chips and a soft spot that light can be seen through on the radome nose, under the errosion boot. 8.33.1 Completed Complied with CMP 535005 Radome- Removal/Installation step A. through B.(6). Removed Radome P/N 1159B21040-S7K, S/N 211. GAC_WOAssociationspt Page: 6 of 15 Gulfstream Proprietary Printed: 4/23/2013 10:31:27Als EFTA01092973  Gulfstreame OINAMICII COMPANY WO Association WO #: SC13175 Mn'EM # : 8 Mechanical ASSOC STATUS DISCREPANCY All maintenance performed IAW GIV AMM 53.10.10. 8.34 Waiting FT RH - The RH flap's "C" tracks forward, inboard bearing is bad (I I59SCC228-23) 8.35 Completed RH - The LH flap's "B" tracks AFT, outboard bearing is bad (I I59SCC226-7) 8.35.1 Completed Complied with GIV CMP 275117 wing flap roller (Leftr outboard upper Aft B Track 8-9) - Removal / Installation. steps A to B(2) and B(5)(a) to B(5)(b). Removed defected flap roller P/N: 1159SCC266-7, S/N: NSN. Work done IAW GIV CMP 275117 & GIV M/M 27.06.00. 8.36 In Progress The LH flap track "A" has corrosion 8.36.1 Completed Removed light surface corrosion and pitting from L/H flap track "A" IAW GIV AMM 27.06-00. 8.37 In Progress The LH flap track "B" has corrosion 8.37.1 Completed Removed light surface corrosion and pitting from L/H flap track "B" JAW GIV AMM 27.06-00. 8.38 In Progress The LH flap track "C" has corrosion 8.38.1 Completed Removed light surface corrosion and pitting from L/H flap track "C" IAW GIV AMM 27.06-00. 8.39 In Progress The LH flap track "D" has corrosion 8.39.1 Completed Removed light surface corrosion and pitting from L/H flap track "D" IAW GIV AMM 27.06-00. 8.40 In Progress The RH flap track "A" has corrosion 8.40.1 Completed Removed light surface corrosion and pitting from RIM flap track "A" IAW GIV AMM 27.06-00. 8.41 In Progress The RH flap track "B" has corrosion 8.41.1 Completed Removed light surface corrosion and pitting from Ft/H flap track "B" IAW GIV AMM 27.06-00. 8.42 In Progress The RH flap track "C" has corrosion 8.42.1 Completed Removed light surface corrosion and pitting from RIM flap track "C" IAW GIV AMM 27.06-00. 8.43 In Progress The RH flap track "D" has corrosion 8.43.1 Completed Removed light surface corrosion and pitting from RIM flap track "D" IAW GIV AMM 27.06-00. 8.44 In Progress RII - The LH flap track "B" has play in the fwd attach bolt 8.45 In Progress RII - The RH flap track "B" has play in the fwd attach bolt 8.46 Completed Install prep and seal panels on tail surfaces. See steps for applicable sections. 8.46.1 Completed Preped and sealed panel on vertical stab. Panel edge sealant ready for paint. IAW GIV AMM 20-00-00 8.46.2 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- I, 37-UPR-3, 37-UPR-5 and 37-UPR-7. REF GIV MM 27.00.00 8.47 Completed APU enclosure and apu mount have heavy soot residue GAC_WOAssociation Apt Page: 7 of 15 Culfstream Proprietary Printed: 4/23/2013 10:31:27Als EFTA01092974  Gil Mire a n WO Association DYNAMICS COM ARMY WO #: SC13175 MrrEM # : 8 Mechanical ASSOC STATUS DISCREPANCY 8.48 Completed Squawk from flight test - during climb #2 engine LP went into RED, pilots had to manually pull throttle back 8.49 Open Squawk from flight test - #1 engine was hotter than #2 by 80+ degrees 8.50 In Progress R/H lower wing skin has corrosion near panel 22-Fr-11 8.51 In Progress R/H lower wing skin has corrosion near panel 22-Fr-14 8.52 In Progress R/H lower wing skin has corrosion near panel 22-Fr-15 8.53 In Progress R/H lower wing skin has corrosion near panel 22-Fr-7 8.54 Completed While C/W CMP 275123 sqk 8.34. CMP 275123 preferres that corresponding roller be replaced at same time. 8.55 Completed While C/W CMP 275117 sqk 8.35. CMP 275117 preferres that corresponding roller be replaced at same time. 8.56 Completed While removing R/H wing fuel panel 22-Fr-1 for sqk 15.32. Found ground mesh on panel to be torn. pn 1159WM40076.13 8.57 Waiting FT Squawk from flight test - MED seal was squealing during flight 8.58 Completed Refuel aircraft to 50001bs 8.59 Open During right wing fuel tank leak check Squawk 15.62 found inboard fuel access panel 22-FT-1 missing a screw. 8.59.1 Completed Ordered fuel panel screw p/n- NAS1580V4T10 per GIV IPC 57-20-00. Ref item # 15.62. Awaiting for part. 8.60 Completed CMP GIV 571004 Wing Fasteners - Cadmium Plating Degradation - Check (Right) ITEM # : 9 Pat ASSOC STATUS DISCREPANCY 9.1 Completed Rill lower wing skin has corrosion near panel 22-FT-7 ITEM # : 10 Outstanding Parts. Materials, and /or Services ASSOC STATUS DISCREPANCY 10.1 Waiting Service for Signature for LAV service approval (L) ITEM # : 12 Aircraft Records and Logbook Research Only ASSOC STATUS DISCREPANCY 12.1 Completed Comply with Aircraft Records and Logbook Research 12.1.1 Completed C/W pan of the aircraft avionics equipment inventory list. More inventory required. 12.1.2 Completed Continued with the aircraft avionics equipment inventory list. More inventory required. 12.1.3 Completed Continued with avionics inventory. Need to check with CMP to complete. 12.1.4 Completed Completed GIV Aircraft Avionics Equipment Inventory List. 12.2 In Progress No log entry found for the removal of NLG rod end P/N 1159HM40120-1 and the installation of P/N I 159SCL567-3. Mandatory CB 183 was PCW by Duncan Aviation on 10/24/06. 12.3 Completed No log entry or tag was found for APU Fire bottle cartridge P/N GAC_WOAssociation Apt Page: 8 of 15 Gulfstream Proprietary Printed: 4/23/2013 10:31:27Als EFTA01092975  Gulfstreame 0 MAMBO, COMPANY WO Association WO #: SC13175 ITEM # : 12 Aircraft Records and Logbook Research Only ASSOC STATUS DISCREPANCY AE30903823 S/N AENI.23 Installed on August 3, 2005. 12.4 Completed No log entry was found for NLG Axle Assy. P/N 1159LM40544-7 S/N BFG6056NTW installed on June 3, 1999. 12.5 In Progress No 8130 found for Pilot'& Co-pilot side window attach bolts. Replaced on 12/11/98. 12.6 In Progress No 8130 found for isolator UH Aft Fwd. S/N 2998 installed on 12/11/98. 12.7 In Progress No 8130 found for isolator UH Aft aft S/N 2982 installed on 12/11/98. 12.8 In Progress No 8130 found for isolator R/H Aft Fwd. S/N 2993 installed on 12/11/98. 12.9 In Progress No 8130 found for isolator R/H Aft Aft. S/N 2994 installed on 12/11/98. 12.10 In Progress No 8130 or log entry found for nose wheel steering installed on 10/11/06. 12.11 Open AD74-08-09 R3 Lavatory Paper and Linen Waste Receptacle Enclosure Access Door and Disposal Door Inspection is due in 126.7 Hours ITEM # : 13 APU Borescope ASSOC STATUS DISCREPANCY 13.1 Completed Comply with APU GTCP36-100(G) Borescope 13.2 In Progress RII • Comply with CMP G1V 490001 APU GTCP36-I00(G) - Removal / Installation 13.2.1 Completed Removed APU Per CMP 490001 From A, B 1-14 a-i. All Maintenence Performed In Reference To GIV AMM 49-10-00. 13.2.2 Completed Complied with CMP 490001 APU GTCP36-I00(G) - Removal / Installation steps C-la thin C- lg. All work done IAW GIV Ch.49-10-00. A.F410108 13.3 Open Comply with CMP GIV 490005 APU Enclosure GTCP36.100(G) - Inspection 13.4 Open Comply with CMP GIV 490002 APU GTCP36-I00(G) Ops Test ITEM # : 14 Engine Runs and Borescope ASSOC STATUS DISCREPANCY 14.1 In Progress Comply with Engine Runs and Borescope 14.2 Completed CMP GIV 710019 Powerplant Internal • Inspection 14.3 Completed CMP GIV 710025 Engine Borescope • Inspection 14.3.1 Completed Gained access for Borescope. IAW CMP 710025 paragraph (B) 1-10 14.3.2 Completed Complied with CMP 710025 from step (1 I)(a) through step (5I)(c) IAW the rolls Royce TAY611.8 mm chapter 71.00-00. See squawk 8.3 14.3.3 Completed Complied with CMP 710025 paragraph 53, (A)-(E) I.7, 57-58 (A)- (E). Note could not install other access plugs do to having to order Hylomar. 14.3.4 Completed Left #2 ENG open being that had to order Hylomar and also awaiting GAC_WOAssociationspt Page: 9 of 15 Culfstream Proprietary• Printed: 4/23/2013 10:31:27Als EFTA01092976  Gil NM:Mani . WO Association DYNAMICS COMPANY WO #: SC13175 ITEM # : 14 Engine Runs and Borescope ASSOC STATUS DISCREPANCY possible second opinion from RR 14.3.5 Completed Install all inner and outer engine panels and bore scope plugs IAW Rolls Royce TAY- EMM Chapter 71.00.00. 14.4 In Progress CMP GIV 710031 Engine - Operational Test 14.5 Completed CMP GIV 730001 Fuel Contamination Check (Engine) - Inspection 14.6 Completed CMP GIV 742001 Engine Ignition System - Operational Test 14.7 Completed CMP GIV 742006 Eng I / No. 2 Igniter Plug - Removal / Installation 14.8 Completed CMP GIV 742016 No. 2 Igniter Plug - Inspection 14.9 Completed CMP GIV 774955 CHIP DETECTOR, ENG--INSP 14.10 Completed CMP GIV 792007 Filter, Engine Pressure Oil - Cleaning/Inspection 14.11 Completed CMP GIV 792013 Engine Scavenge Strainers - Inspection 14.12 Completed CMP GIV 710020 Powerplant Internal • Inspection 14.13 Completed CMP GIV 710026 Engine Borescope • Inspection 14.13.1 Completed Gained access for Borescope. IAW CMP 710025 paragraph (B) 1-10 14.13.2 Completed Complied with CMP 710026 from step (I I)(a) through step (51)(c) IAW the rolls Royce TAY611.8 mm chapter 71.00-00. See squawk 8.4. 14.13.3 Completed Install all inner and outer engine panels and bore scope plugs IAW Rolls Royce TAY- EMM Chapter 71.00.00. 14.14 Open CMP GIV 710032 Engine - Operational Test 14.15 Completed CMP GIV 730002 Fuel Contamination Check (Engine) - Inspection 14.16 Completed CMP GIV 742002 Engine Ignition System - Operational Test 14.17 Completed CMP GIV 742008 Eng #2 / No. 2 Igniter Plug - Removal / Installation 14.18 Completed CMP GIV 742018 No. 2 Igniter Plug - Inspection 14.19 Completed CMP GIV 774956 CHIP DETECTOR, ENG—INSP 14.20 Completed CMP GIV 792009 Filter, Engine Pressure Oil - Cleaning/Inspection 14.21 Completed CMP GIV 792014 Engine Scavenge Strainers - Inspection 14.22 Open Related CMP Codes 14.23 Completed CMP GIV 711009 Cowl Latch, Engine (Left) - Rigging 14.24 Open CMP GIV 732001 Engine Acceleration Test / Adjustment 14.24.1 Completed Removed all Ft/H horizontal stabilizer panels required for CMP 551020. All work I.A.W. GIV M/M 55-14-00. 14.25 Open CMP GIV 732005 Engine Deceleration Test / Adjustment 14.26 Open CMP GIV 732049 ENG HANDLE ACU SOLENOID CK 14.26.1 Completed In progress removal of R/H horizontal stabilizer and elevator panels required for CMP 551023 ;Panels on top of Ft/H elevator still need to be removed, for details of panels 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. 14.27 Open CMP GIV 732057 SOLENOID, ENG APPR IDLE-OPS 14.28 Open CMP GIV 732011 GROUND IDLE, ENG-TEST/ADJUST 14.29 Open CMP GIV 732013 APPROACH IDLE, ENG-TEST/ADJ GAC_WOAssociation.rpt Page: 10 of IS Gulfstream Proprietary Printed: 4/23/2013 10:31:27Als EFTA01092977  Gulfstreant DYNAMIC* COMPANY WO Association WO #: SC13175 ITEM # : 14 Engine Runs and Borescope ASSOC STATUS DISCREPANCY 14.30 Open CMP GIV 783013 Thrust Reverser Interlock Feedback System (Left) - Operational Test 14.31 Open CMP GIV 783014 Thrust Reverser Interlock Feedback System (Right) - Operational Test 14.32 Open CMP GIV 783017 MAX REV THRUST, L-OPS TEST/ADJ 14.33 Open CMP GIV 783018 MAX REV THRUST, R-OPS TEST/ADJ 14.34 Open CMP GIV 791033 Oil Level - Check / Service 14.35 Completed CMP GIV 711010 Cowl Latch, Engine (Right) - Rigging 14.36 Open CMP GIV 732002 Engine Acceleration Test / Adjustment 14.37 Open CMP GIV 732006 Engine Deceleration Test / Adjustment 14.38 Open CMP GIV 732050 ENG HANDLE ACU SOLENOID CK 14.39 Open CMP GIV 732058 SOLENOID, ENG APPR IDLE-OPS 14.40 Open CMP GIV 750006 AIRFLOW CONT SYS -TEST 14.41 Open CMP GIV 732012 GROUND IDLE, ENG-TEST/ADJUST 14.42 Open CMP GIV 732014 APPROACH IDLE, ENG-TEST/ADJ 14.43 Open CMP GIV 791034 Oil Level - Check / Service ITEM # : 15 Customer Supplied Due List ASSOC STATUS DISCREPANCY 15.1 In Progress Comply with Customer Supplied Due List 15.1.1 Completed Installed NEW cover as required and painted. Need to be sealed. Work IAW GIV MM 20-00-00. 15.2 Completed CMP GIV 100310 Check Airworthiness Directives 15.3 Completed CMP GIV 100320 AIRWORTHINESS CHECK 15.4 Completed CMP GIV 191108 Review Aircraft Status and Records 15.5 Completed CMP GIV 231001 AVIONICS--FUNC RAMP TEST 15.6 Completed CMP GIV 251114 Pilot and Copilot Seat - Inspection / Lubrication 15.7 Waiting Insp CMP GIV 262045 Fire Bottle (Left Engine) - Hydrostatic Test 15.8 Waiting Insp CMP GIV 262050 Fire Bottle (Right Engine) - Hydrostatic Test 15.8.1 Completed Entered in Error. Step moved to item 15.9.1. 15.9 Completed CMP GIV 270101 Stall Barrier / Angle of Attack System - Ops Test 15.9.1 Completed Complied with CMP 270101 Stall Barrier/AOA System - Operational check Steps B(1) thru B(23) with no discrepancies noted at this time. All work performed IAW G-IV maintenance manual 27.01.01. 15.10 Completed CMP GIV 272038 Rudder Pedals - Lubrication 15.11 Completed RI! - CMP GIV 275009 Flap Actuator Yoke (Left Inboard) - Inspection 15.12 Completed RI! - CMP GIV 275010 Flap Actuator Yoke (Right Inboard) - Inspection 15.13 Completed RI! - CMP GIV 275011 Flap Actuator Yoke (Left Outboard) - Inspection 15.14 Completed RI! - CMP GIV 275012 Flap Actuator Yoke (Right Outboard) - GAC_WOAssociation.rpt Page: I I of 15 Culhaream Proprietary• Printed: 4/23/2013 10:31:27A/i EFTA01092978  GulfstreameOINAMICII COMPANY WO Association WO #: SC13175 Vial; Customer Supplied Due List ASSOC STATUS DISCREPANCY Inspection 15.15 Open CMP GIV 275027 Rap Actuator Bushing (Left) - Service / Lubrication 15.16 Open CMP GIV 275028 Rap Acuator Bushing (Right) - Service / Lubrication 15.17 In Progress CMP GIV 280005 Fuel Control System - Functional Test 15.18 Completed CMP GIV 303005 Pitot Heat System - Operational Test 15.19 Completed CMP GIV 531007 FS 85 Bulkhead - Inspection 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. 15.20 Completed CMP GIV 532007 Fonvard Cabin Compartment Below Floor - Inspection 15.21 Completed CMP GIV 532009 Midcabin Compartment Below Floor- Inspection 15.22 Completed CMP GIV 532011 Aft Cabin Compartment Below Floor - Inspection 15.23 Completed CMP GIV 551019 Horizontal Stabilizer / Elevator (Exterior) (Left) - Inspection 15.23.1 Completed Removed all UH horizontal stabilizer panels required for CMP 551019. All work I.A.W. GIV M/M 55-14-00. 15.23.2 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. 15.24 Completed CMP GIV 551020 Horiz Stabilizer / Elevator (Exterior) (Right) - Insp 15.24.1 Completed Removed all R/H horizontal stabilizer panels required for CMP 551020. All work I.A.W. GIV M/M 55-14-00. 15.24.2 Completed C/W section B thru B(h) of CMP 551020. No discrepancies noted. All work I.A.W. GIV M/M 55.00-00 15.25 Completed CMP GIV 551023 Horizontal Stabilizer / Elevator (Interior / Exterior) (Left) - Inspection 15.25.1 Completed Removed all UH horizontal stabilizer and elevator panels required for CMP 551023. All work I.A.W. GIV MM 55.14.00. 15.25.2 Completed C/W section B thru B(k) of CMP 551023. See sqk 8.23 and8.20 for discrepancies noted. All work I.A.W. GIV MM 55.14.00. 15.26 Completed CMP GIV 551024 Hz Stabilizer/Elevator (Interior/Exterior) (Right) Insp 15.26.1 Completed In progress removal of R/H 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 MM 55.14.00. 15.26.2 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 MM 55.00.00. 15.27 Completed CMP GIV 553005 Vertical Stabilizer / Rudder (External) - Inspection 15.28 Completed CMP GIV 553007 Vertical Stabilizer / Rudder (Internal) - Inspection GAC_WOAssociationspt Page: 12 of 15 Culfstream Proprietary Printed: 4/23/2013 10:31:27Als EFTA01092979  Gulfstreame OINAMICII COMPANY WO Association WO #: SC13175 Customer Supplied Due List ASSOC STATUS DISCREPANCY 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. 15.28.2 Completed Continued removing panels to gain access for inspection. Removed panels 109-LE-2, 109-LH-9, 109-LH-I I, 109-LH-10, 109-RB-I, 109-LH-8, 1I0-LH-1,110-LH-2, I10-LH-3, 110-LH-4, 110-LH-6, l09-LH-7. Work done IAW GIV CMP 553007 & GIV M/M 55-30-00. 15.28.3 Completed Continue with removal of all requiered panels of CMP 553007; And Complied with steps B.(1) thru step B(22).All work done IAW GIV AMM 53-30-00. 15.29 Completed CMP GIV 571011 Wing Front Beam Hi-Lite Collars (Left) - Inspection 15.30 Completed CMP GIV 571012 Wing Front Beam Hi-Lite Collars (Right) - Inspection 15.31 Completed CMP GIV 571025 Wing Tank Interior (Left) - Inspection 15.32 Completed CMP GIV 571026 Wing Tank Interior (Right) - Inspection 15.32.1 Completed Removed R/H wing fuel panels 22-FT-1, 22-FT-2, 22-FT-3, 22-FT-4, 22-FT-5. Work done IAW GIV M/M 28.11.00. 15.33 Open Related CMP Codes 1534 Completed CMP GIV 251109 SEAT ASSEMBLY, PILOT 15.35 Completed CMP GIV 251110 SEAT ASSEMBLY, COPILOT 15.36 Waiting CMP GIV 262025 Engine Fire Bottle (Left) - Removal / Installation Insp/FT 15.36.1 Completed Removed LAI fire bottle P/N 32700022 S/N 06758C2, squibs removed and stored in parts room. I/A/W GIV AMM 26.02.00 15.37 Waiting Insp CMP GIV 262065 Fire Bottle (Left Engine) - Weight Check 15.38 Waiting CMP GIV 262030 Engine Fire Bottle (Right) - Removal / Installation Insp/FT 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 15.39 Waiting Insp CMP GIV 262070 Fire Bottle (Right Engine) - Weight Check 15.40 In Progress RII - CMP GIV 275003 Flap (Left) 15.40.1 Completed Complied with CMP 275003 LEFT FLAP REMOVAIJ INSTALLATION steps A, B and C as required. Work IAW GIV MM 27-06-00. 15.40.2 Completed Remove LH Flap PN 1I59C520005.543 SN 1086 15.41 In Progress RII CMP GIV 275004 Flap (Right) 15.41.1 Completed Complied with CMP 275004 RIGHT FLAP REMOVAIJ INSTALLATION steps A, B and C as required. Work IAW GIV MM27.06.00. 15.41.2 Completed Remove RH flap PN I159C520005.544 SN 1085 15.42 In Progress RII - CMP GIV 275005 Inboard Flap Actuator (Left) - Removal / Installation 15.42.1 Completed Performed CMP code 275005 Remove Inbd Flap Actuator PN GAC_WOAssociationspt