Gulfstreame

Gulfstreame WO Association 0 MAMBO, COMPANY 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 STATUS DISCREPANCY 1.1 Open Return to Service OM (10 or More) 1./ In Progress Inbound/Outbound Inspection 12.1 Open Outbound Inspection 1.5 Open Tool Clearance 1.6 In Progress Cover & Protect 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) 1.17 Open Billable Consumables & Shop Supplies 1.19 Open Update Weight & Balance ITEM # : 6 Avionics ASSOC STATUS DISCREPANCY 6.1 Open While complying with CMP 231001 Avionics-Functional Ramp Test/Inspection found that the #1 HF system does not transmit. 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 tint 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_WOAssociationspt Page: I of 6 Gulfstream Proprietary Printed: 4/23/2013 10:23: I 7Als EFTA01114167 Gulfstreame WO Association 0 MAMBO, COMPANY WO #: SC13175 ASSOC STATUS 6.7.1 Open 6.8 Open 6.9 Open 6.10 Open 6.11 Open 6.12 Open 6.13 Open 6.14 Open 6.15 Open 6.16 Open 6.17 Open 6.18 Open 6.19 Open Satphone is Mop ITEM # : 7 Interior ASSOC STATUS 7.1 Open 7.1 In Progress 7.3 Open 7.4 Open 7.5 In Progress DISCREPANCY 2001bs lower than the LT and RT fuel gauges and there is a 150Ibs difference between total fuel on EICAS primary and systems page compared to STBY totalizer gauge - EICAS and SYSTEMs page ind same 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). Squawk from flight test - LED light burned out on Rate of Climb / FPM (3 digit from LT) on pressurization controller 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 Squawk from flight test - At FL250 with Batteries only, DC volts on ABEX fluctuates 36.9 to 47.9 v Squawk from flight test RTU 1 there is a cyan line across display on screen - splits screen in half Squawk from flight test - On RNAV approach VNAV worked and then became unavailable on approach Squawk from flight test - Standby engine instrument gauge is indicating all "8888"s on RT HP gauge Squawk from flight test - HF radios operated normally but NO SELCAL EGPWS/Terrain database outdated Squawk from flight test - aft LAV reading light is inop Squawk from flight test - cabin management display at VIP , galley screen Mop Squawk from flight test - perform ops test of nose camera DISCREPANCY Squawk from flight test - Squawk from flight test - Squawk from flight test - Squawk from flight test - close the outlet Squawk from flight test - headliner when closed. ITEM # : 8 Mechanical ASSOC STATUS 8.8 Open 8.10 In Progress FWD LAV water does not pump LH galley aft cutting board does not latch RH #5 window shade does not fully close pax air gaspers loose, takes two hands to fwd cabin door angle wing does not hit DISCREPANCY RII - Squawk from flight test - Raps shudder felt when flaps selected to 39 degrees RII - Squawk from flight test - on the ground the flaps would intermittenly move from 20 to 39 degrees and 10 to 20 when selected. GAC_WOAssociationspt Page: 2 of 6 Culfstream Proprietary• Printed: 4/23/2013 10:23:17Als EFTA01114168 Gulfstreame WO Association OINAMICII COMPANY WO #: SC13175 Mn'EM # : 8 ASSOC STATUS Mechanical DISCREPANCY 8.11 Open Squawk from flight test - power levers have 1/2 knob split at I5000ft 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) 8.15 In Progress Squawk from flight test - service hydraulic replenisher 8.16 Open Squawk from flight test - At FL400 and climbing, RT engine MCI' was 139 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. 8.23 Waiting RII - While working CMP 551023 sqk 15.25. Found horizontal stab approval (L) thrust blocks to be worn out of limits. 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 AS 12847 and AS 12817 and 5 clamps P/Ns AS12816 and AS12846 and installed 12 NEW clamps P/N AS12847 and AS12817 and 5 clamps P/Ns AS 12816 and AS12846 IAW RR TAY611.8 MM 71-00-00. 8.29 In Progress RH - 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 RH - 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 RH - 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 RH - 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. 8.34 Waiting FT RII - The RH flap's "C" tracks forward, inboard bearing is bad (I I59SCC228-23) 8.36 In Progress The LH flap track "A" has corrosion 8.37 In Progress The LH flap track "B" has corrosion 8.38 In Progress The LH flap track "C" has corrosion 8.39 In Progress The LH flap track "D" has corrosion 8.40 In Progress The RH flap track "A" has corrosion 8.41 In Progress The RH flap track "B" has corrosion 8.42 In Progress The RH flap track "C" has corrosion 8.43 In Progress The RH flap track "D" has corrosion GAC_WOAssociation.rpt Page: 3 of 6 Gulfstream Proprietary Printed: 4/23/2013 10:23:17Als EFTA01114169 Gil Mire a n DYNAMICS COM ARMY WO Association WO #: SC13175 MDIEM # : 8 ASSOC STATUS 8.44 8.45 8.49 8.50 8.51 8.52 8.53 8.57 8.59 In Progress In Progress Open In Progress In Progress In Progress In Progress Waiting FT Open ASSOC STATUS 10.1 Waiting approval (L) ITEM # : 12 ASSOC STATUS 12.2 In Progress 12.5 In Progress 12.6 In Progress 12.7 In Progress 12.8 In Progress 12.9 In Progress 12.10 In Progress 12.11 Open ITEM # : 13 ASSOC STATUS 13.2 In Progress 13.3 Open 13.4 Open Mechanical DISCREPANCY RH - The LH flap track "B" has play in the fwd attach bolt RII - The RH flap track "B" has play in the fwd attach bolt Squawk from flight test - #1 engine was hotter than #2 by 80+ degrees R/H lower wing skin has corrosion near panel 22-FT-11 R/H lower wing skin has corrosion near panel 22-FT-I4 R/H lower wing skin has corrosion near panel 22-FT-I5 R/H lower wing skin has corrosion near panel 22-FT-7 Squawk from flight test - MED seal was squealing during flight During right wing fuel tank leak check Squawk 15.62 found inboard fuel access panel 22-FT- I missing a screw. Outstanding Parts, Materials and I or Send DISCREPANCY Service for Signature for LAV service Aircraft Records and Logbook Research Only DISCREPANCY No log entry found for the removal of NLG rod end P/N 1159HM40120-I and the installation of P/N I 159SCL567-3. Mandatory CB 183 was PCW by Duncan Aviation on 10/24/06. No 8130 found for Pilot'& Co-pilot side window attach bolts. Replaced on 12/11/98. No 8130 found for isolator UH Aft Fwd. S/N 2998 installed on 12/11/98. No 8130 found for isolator UH Aft aft S/N 2982 installed on 12/11/98. No 8130 found for isolator R/H Aft Fwd. S/N 2993 installed on 12/11/98. No 8130 found for isolator R/H Aft Aft. S/N 2994 installed on 12/11/98. No 8130 or log entry found for nose wheel steering installed on 10/11/06. AD74-08-09 R3 Lavatory Paper and Linen Waste Receptacle Enclosure Access Door and Disposal Door Inspection is due in 126.7 Hours APU Borescope DISCREPANCY RII - Comply with CMP G1V 490001 APU GTCP36-100(G) - Removal / Installation Comply with CMP GIV 490005 APU Enclosure GTCP36.100(G) 100(G)- Inspection Comply with CMP G1V 490002 APU GTCP36-100(G) Ops Test GAC_WOAssociation.rpt Page: 4 of 6 Culfstream Proprietary Printed: 4/23/2013 10:23:17Ali EFTA01114170 Gil NM:Mani . DYNAMICS COMPANY WO Association WO #: SC13175 ITEM # : 14 ASSOC STATUS Engine Runs and Borescope DISCREPANCY 14.1 In Progress Comply with Engine Runs and Borescope 14.4 In Progress CMP GIV 710031 Engine • Operational Test 14.14 Open CMP GIV 710032 Engine - Operational Test 14.22 Open Related CMP Codes 14.24 Open CMP GIV 732001 Engine Acceleration Test / Adjustment 14.25 Open CMP GIV 732005 Engine Deceleration Test / Adjustment 14.26 Open CMP GIV 732049 ENG HANDLE ACU SOLENOID CK 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 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, LOPS 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 14.36 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 ASSOC STATUS Customer Supplied Due Lis DISCREPANCY 15.1 In Progress Comply with Customer Supplied Due List 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 15.15 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 15.33 Open Related CMP Codes 15.36 Waiting CMP GIV 262025 Engine Fire Bottle (Left) - Removal / Installation Insp/Fr 15.37 Waiting Insp CMP GIV 262065 Fire Bottle (Left Engine) • Weight Check GAC_WOAssociation.rpt Page: 5 of 6 Culfstream Proprietary• Printed: 4/23/2013 10:23:1 7Als EFTA01114171 Gil Mire a n DYNAMICS COM ARMY WO Association WO #: SC13175 ITEM # : 15 ASSOC STATUS Customer Supplied Due List DISCREPANCY 15.38 Waiting CMP GIV 262030 Engine Fire Bottle (Right) - Removal / Installation Insp/FT 15.39 Waiting Insp CMP GIV 262070 Fire Bottle (Right Engine) - Weight Check 15.40 In Progress RI! - CMP GIV 275003 Flap (Left) 15.41 In Progress RI! - CMP GIV 275004 Flap (Right) 15.42 In Progress RII - CMP GIV 275005 Inboard Flap Actuator (Left) - Removal I Installation 15.43 In Progress RII - CMP GIV 275007 Outboard Rap Actuator (Left) - Removal / Installation 15.44 In Progress RII - CMP GIV 275006 Inboard Flap Actuator (Right) - Removal / Installation 15.45 In Progress RI! - CMP GIV 275008 Outboard Flap Actuator (Right) - Removal / Installation 15.47 Open CMP GIV 231114 HF Communications System No. 1 - Operational Check 15.48 Open CMP GIV 231117 HF Communication Antenna - Continuity Check (Installed) 15.49 Open CMP GIV 231155 HF Communication Antenna Assembly - Removal / Installation 15.50 Open CMP GIV 231115 HF COMM SYS #2.OPS TEST 15.52 In Progress CMP GIV 574005 Wing Leading Edge (Left Inboard) - Removal/ Installation 15.53 In Progress CMP GIV 574011 Wing Leading Edge (Left Center) - Removal / Installation 15.54 In Progress CMP GIV 574017 Wing Leading Edge (Left Outboard) - Removal / Installation 15.55 In Progress CMP GIV 574006 Wing Leading Edge (Right Inboard) - Removal / Installation 15.56 In Progress CMP GIV 574012 Wing Leading Edge (Right Center) - Removal / Installation 15.57 In Progress CMP GIV 574018 Wing Leading Edge (Right Outboard) • Removal / Installation ITEM # : 16 ASSOC STATUS 16.1 In Progress Pilots for Conditioned Survey Right (Pre Test Right) DISCREPANCY Two Pilot's for Condition Survey Flight (Must be performed with Item 14. Engine Runs and Borescope) GAC_WOAssociation.rpt Page: 6 of 6 Gulfstream Proprietary• Printed: 4/23/2013 10:23: I 7Als EFTA01114172