N782UA

Part: SLIDE — LOW PRESSURE (ZONE 800) · airframe 113,995 hrs · 14,983 cycles

DOOR 4L SLIDE PRESSURE GAUGE OUT OF GREEN BAND. REMOVED AND REPLACED DOOR 4L ESCAPE SLIDE IAW AMM REF TASK 25-66-01-000-801 & TASK 25-66-01-400-801.

Part: HEAT EXCHANGER — FAULTED (NR 2 ENGINE) · airframe 113,006 hrs · 14,879 cycles

#2 FUEL/OIL COOLER NEEDS REPLACED AS PRECAUTIONARY MEASURE DUE TO FUEL ODOR IN DRAINED IDG OIL. STARTED TO DISCONNECT THE FUEL/OIL COOLER REF AMM 79-21-01 UP TO STEP G. REMOVED #2 ENGINE FUEL/ OIL COOLER REF AMM 79-21-01. INSTALLED NEW ENG 2 FUEL/OIL COOLER TO ENGINE, TORQUED FWD AND AFT MOUNTS. REF AMM TASK 79-21-01-400-801-N00. CONTINUE WITH STEP G(7). PARTIALLY INSTALLED VARIOUS TUBES AND HOSES IN POSITION. CONTINUED INTALLATION OF FUEL/OIL COOLER UP TO STEP (H)(10) REF AMM 79-21-01-400-801-N00 COMPLETED INSTALLATION REF AMM 79-21-01-400-801-N00. PERFORMED IDLE RUN REF AMM 71-00-00, LEAK CHECK GOOD.

Part: IDG — OVERSERVICED (ZONE 400) · airframe 113,006 hrs · 14,879 cycles

ELEC GEN DRIVE R EICAS ADVISORY RIGHT IDG FAULT (LOW INTERNAL OIL PRESSURE).FLIGHT CREW PERFORMED QRH IDG DISCONNECTED,MAINTENANCE PROCEDURE CARRIED OUT. FOUND NR 2 IDG WAS OVER SERVICED. REPLACED ROLS REF AMM 24-11-15. DRAIN EXCESS OIL FROM IDG, RECONNECTED IDG AND PERFORMED IDLE RUN. NEED NEW IDG. REMOVED IDG UP TO SUBTASK 24-11-01-020-004-001 STEP E REMOVE THE PHASE LEADS. REMOVED ENGINE #2 IDG IN REF AMM 24-11-01. INSTALLED NEW IDG UP TO SEC 8, D, 1 OF AMM 24-11-01. ACCOMPLISHED IDT PER GMM 09-10-05 CONTINUE INSTALLATION OF IDG REF AMM 24-11-01 UP TO AND INCLUDING STEP 13 OF THE AMM AFTER FLUSHED ONE MORE TIME, NO FUEL SMELL NOTED. PERFORMED OPS CHECK, LEAK CHECK, AND DISCONNECT CHECK REF AMM 24-11-01, AND 24-11-00. ALL CHECKS GOOD, NO LEAKS.

Part: BATTERY — NO TEST (ZONE 200) · airframe 112,093 hrs · 14,782 cycles

L4 DOOR EMERGENCY LIGHT POWER SUPPLY BATTERY PACK OUT OF LIMIT D URING CAPACITY CHECK - ORIGINATED BY EMP V903218 ON HAECO NR 94 56232, RAISED FROM WORK CARD 85-3351-1-7003. PERFORMED BY EMP V903670, REPLACED THE FR 4L EMERGENCY LT POWER SUPPLY BATTERY PACK M33407 AND C/O TEST, THE TEST RESULT WAS NOR MAL. REF AMM 33-51-06-960-802 REV 103.

Part: AUDIO CONTROL — FAULTED (ZONE 200) · airframe 111,713 hrs · 14,732 cycles

HF1 AND HF2 TUNE BUT UNABLE TO RECEIVE DEBRIEF CREW WHEN THEY BLOCKED IN AND CAPT SAID HE WAS ABLE TO PERFORMED HF VOICE CHECKS WITH COMPANY A/C ON ONSIDE AND OFFSIDE WOULD E...PARTS USED: 27-2351-9-9001,QTY :1 CHANNALIZE AND WAS BARELY ABLE TO HEAR ON ONSIDE HF. F/O DID NOT HF FREQS AND WAS ABLE TO TRANSMIT AND RECIEVE CLEARLY. AHM AND ROTABLE PARTS CHANGE WAS INDICATED - TT # 1662882 SN OFF 0308 DISCLOSE IF SHE COULD HEAR ANYTHING. PERFORMED HF SYSTEM GROUND A/C REPORT FAULT 23-55050 ACTIVE. T/S PER FIM 23-51 TASK 805 AND TEST WITH OPS CHECKS PASSING ON L/H AND R/H SIDE REF PIC. PER FIM DESCRIPTION THIS CAN CAUSE FALSE VOLUME CONTROL WHICH WOULD EXPLAIN WHY CAPT COULD BARELY HEAR ON HF. FOUND F/OBS ACP BUTTONS ALL STICKY. REMOVED AND REPLACED F/OBS ACP IAW AMM 23-51-01 WITH ALL OPS CHECK PASSING AND FAULT NOW SHOWING INACTIVE REF PIC OF FAILURE MESSAGE AND TEST RESULTS. PANEL, AUDIO CO OFF 27-2351-9-9001 0308 ON 27-2351-9-9001 0436

Part: CHARGER — FAILED (R3 M33401) · airframe 106,718 hrs · 14,165 cycles

B777-33-3-7019 DR R3 M33401 EMER LIGHT BATTERY CHARGER DEEP CYCLE TEST FAIL. TRANSFER HX NON-ROUTINE WO.2383416 AND . DR R3 M33401 EMER LIGHT BATTERY CHARGER REPLACED AND TESTED NORMAL AS PER AMM33-51-06.

Part: CHARGER — FAILED (R3 M33404) · airframe 106,718 hrs · 14,165 cycles

B777-33-3-7019 DR L2 M33096 EMER LIGHT BATTERY CHARGER DEEP CYCLE TEST FAIL. TRANSFER HX NON-ROUTINE WO.2383412 AND . DR R3 M33404 EMER LIGHT BATTERY CHARGER REPLACED AND TESTED NORMAL AS PER AMM33-51-06.

Part: BATTERY PACK — FAILED (R4 M33409) · airframe 106,718 hrs · 14,165 cycles

B777-33-3-7019, DR 4R EMER LIGHT BATTERY PACK M33409 CAPACITY CHECK FAILED. TRANSFER HX WO.2449344 AND DR R4 M33409 EMER LIGHT BATTERY AND BATTERY HCARGER REPLACED AND TESTED NORMAL AS PER AMM33-51-06.

Part: BATTERY PACK — FAILED (R1 M33094) · airframe 106,718 hrs · 14,165 cycles

SUPPORT TASK - DR1 RH EMERGENCY BATTERY PACK (M33094) INTERMITTA NT FAULT DURING OPERATIONAL TEST. TRANSFER HX NON-ROUTINE WO.2429821 AND ORIGINATED BY V896963. DR R1 EMER LIGHT BATTERY (M33094) REPLACED AND TESTED NORMAL AS PER AMM33-51-06. WORK ACCOMPLISHED BY V898181 AND INSPECTED BY V896958. IDT INSPECTED BY HX147282 ADD EMP:V896958

Part: BATTERY PACK — FAILED (R3 M33404) · airframe 106,718 hrs · 14,165 cycles

B777-33-3-7019, DR R3 M33404 EMER LIGHT BATTERY DEEP CYCLE TEST FAIL. TRANSFER HX NON-ROUTINE WO.2383399 AND . DR R3 M33404 EMER LIGHT BATTERY REPLACED AND TESTED NORMAL AS PER AMM33-51-06.

Part: BATTERY PACK — FAILED (R3 M33401) · airframe 106,718 hrs · 14,165 cycles

B777-33-3-7019 DR R3 M33401 EMER LIGHT BATTERY DEEP CYCLE TEST FAIL. TRANSFER HX NON-ROUTINE WO.2383408 AND . DR R3 M33401 EMER LIGHT BATTERY REPLACED AND TESTED NORMAL AS PER AMM33-51-06.

Part: CHARGER — FAILED (L# M33400) · airframe 106,718 hrs · 14,165 cycles

SUPPORT TASK - DR 3 LH EMERGENCY POWER SUPPLY ASSY (M33400) INTERMITTENT FAULT DURING OPERATIONAL TEST. TRANSFER HX NON-ROUTINE WO.2429873 AND . DR L3 M33400 EMER LIGHT BATTERY AND BATTERY CHARGER REPLACED AND TESTED NORMAL AS PER AMM33-51-06.

Part: BATTERY PACK — FAILED (R2 M33098) · airframe 106,718 hrs · 14,165 cycles

B777-33-3-7019 DR R2 M33098 EMER LIGHT BATTERY DEEP CYCLE TEST FAIL. TRANSFER HX NON-ROUTINE WO.2383006 AND . DR R2 M33098 EMER LIGHT BATTERY REPLACED AND TESTED NORMAL AS PER AMM33-51-06.

Part: CHARGER — FAILED (L2 M33096) · airframe 106,718 hrs · 14,165 cycles

B777-33-3-7019, DR L2 EMER LIGHT BATTERY PACK M33096 CAPACITY CHECK FAILED. TRANSFER HX NON-ROUTINE WO.2449365 AND . DR L2 M33096 EMER LIGHT BATTERY AND BATTERY CHARGER REPLACED AND TESTED NORMAL AS PER AMM33-51-06.

Part: SKIN — CRACKED (STA1034, S-37L) · airframe 106,718 hrs · 14,165 cycles

SUPPORT TASK : EA5310-06900 REV.D, OP 013 STEP 21.2, 1EA CRACK FOUND APPROX 0.050" IN DEPTH AT FUSELAGE SKIN AT 3 O''CLOCK POSITION. TRANSFER REF.NON-ROUTINE HX NRC WO.2405668 AND . FX SKIN STA 1034 AND S-37L AT UNDERWING LONGERON AREA INTERIM REPAIRED AS PER EC/RA 5330-07172 REV- PART 1. ATTACHED FORM 44-0008 ITEM 1 TO ITEM 23 ACCOMPLISHED.

Part: FITTING — CRACKED (LH ELEVATOR) · airframe 106,718 hrs · 14,165 cycles

SUPPORT TASK - (ADD 2013-08-02) EA 5510-01896 REV C OP 005 - 1EA CRACK FOUND ON LH ELEVATOR O/B ACTUATOR FITTING LOWER I/B SURFACE APPROX 0.375" IN LENGTH AS MARKED. PRINT AND ACCOMPLISH OP 009 OF THIS EA 5510-01806. TRANSFER REF.NON-ROUTINE HX NRC WO.2367727.

Part: UNKNOWN — CRACKED (RH WING) · airframe 106,718 hrs · 14,165 cycles

SUPPORT TASK - EA 5310-06900 REV.D OP 014 STEP 23.7 1EA CRACK FOUND IN RING CHORD AT 7 O''CLOCK POSITION (VIEW LOOKING AFT) APPROX 0.030" IN LENGTH TRANSFER HX NR WO.2403479 AND FX WING CENTER SECTION FRONT SPAR RH RING CHORD 1EA FASTENER HOLE INTERIM REPAIRED AS PER EC/RA 5710-02844 REV.- PART 1. ATTACHED FORM 44-0008 ITEM 1 TO ITEM 22 ACCOMPLISHED.

Part: UNKNOWN — CRACKED (LH WING) · airframe 106,718 hrs · 14,165 cycles

SUPPORT TASK - EA 5310-06900 REV.D OP 013 STEP 23.7 1EA CRACK FOUND RING CHORD AT 9 O''CLOCK POSITION (VIEWING LOOK AFT) APPROX 0.040" IN LENGTH TRANSFER HX NR WO.2403471 AND FX WING CENTER SECTION FRONT SPAR LH RING CHORD 1EA FASTENER HOLE INTERIM REPAIRED AS PER EC/RA 5710-02842 REV.- PART 1. ATTACHED FORM 44-0008 ITEM 1 TO ITEM 22 ACCOMPLISHED.

Part: STRINGER — CRACKED (RH UNDER WING) · airframe 106,718 hrs · 14,165 cycles

SUPPORT TASK - EA5310-06900 REV OP004, RH BUILT-UP UNDERWING LONGERON FOUND CRACK PLEASE ACCOMPLISH OP14 FOR REPLACEMENT. TRANSFER HX NON-ROUTINE WO.2337953 . RH UNDERWING LONGERON REPLACEMENT ACCOMPLISHED PER EA 5310-06900 REV D OP 004

Part: STRINGER — CRACKED (LH UNDER WING) · airframe 106,718 hrs · 14,165 cycles

SUPPORT TASK - EA5310-06900 REV D OP003, LH BUILT-UP UNDERWING LONGERON FOUND CRACK PLEASE ACCOMPLISH OP13 FOR REPLACEMENT. TRANSFER HX NON-ROUTINE WO.2337961. FUSELAGE BS1035 LH UNDERWING LONGERON REPLACED AS PER EA 5310-06900 REV.D OP 013.

Part: SKIN — CRACKED (STA1035) · airframe 106,718 hrs · 14,165 cycles

SUPPORT TASK - EA5310-06900 REV.D OP 014 STEP 21.3, 1EA CRACK WAS FOUND APPROX 0.125" IN LENGTH AT FUSELAGE SKIN SURFACE AT 2 O''CLOCK POSITION. TRANSFER REF.NON-ROUTINE HX NRC WO.2405692 AND . REVISION OF ECRA 5331-03067 PART 2 ON OR BEFORE REACHING 22,165 4,000 FLIGHT CYCLES THEREAFTER. TOTAL FLIGHT CYCLES. REPEAT INSPECTONS AT INTERVAL NOT TO EXCEED GENERATING DIP TO INSPECT FUSELAGE SKIN REPAIR ACCOMPLISHED IN THIS ECRA IN THE AREA OF S37R AND FWD OF STA 1035 PER LATEST OK TO DIP REPAIR BYS37R AND FWD OF STA1035;INSPECT FUSELAGE SKIN TOMC-APPROVAL FROM SC1ELBYC COMMENT REPAIR ACCOMPLISHED BY THIS EC/RA IN THE AREA OF S37R AND FWD OF STA1035 PER LATEST REVISION OF ECRA 5331-03067 PART 2 ON OR BEFORE REACHING 22,165 TOTAL FLIGHT CYCLES. REPEAT THE INSPECTIONS AT INTERVAL NOT TO EXCEED 4,000 FLIGHT CYCLES, THEREAFTER. PER ECRA 5331-03067 PERFORMED INTERIM REPAIR TO 1EA CRACK FOUND APPROX 0.125" IN QC LENGTH AT FUSELAGE SKIN SURFACE AT 2 O''CLOCK POSITION PER HAECO-HKG RI-53-00-16542A AND ECRA 5331-03067 RECORDS UPDATE QC REVIEWED. INIT: 22165 TAFC INIT WILL AUTO ITO TO RIR -0442 RIR: 4000 FC THEREAFTER...SN

Part: FRAME — CRACKED (L3 DOOR) · airframe 106,718 hrs · 14,165 cycles

B777-53-4-7120, DOOR L3 UPPER CORNER CUTOUT FOUND 1EA CRACK. TRANSFER REF. NON-ROUTINE HX NRC WO.2402832 AND FX NO.3 LH PED CUTOUT AFT UPPER CORNER AT STA 1546 AND S17L BEAR STRAP INTERIM REPAIRED AS PER EC/RA 5360-01746 REV- PART 1. ATTACHED FORM 44-0008 ITEM 1-36 ACCOMPLISHED.

Part: UNKNOWN — CRACKED (RH WING) · airframe 106,718 hrs · 14,165 cycles

SUPPORT TASK- EA5310-06900 REV.D OP 014 STEP 23.7 1EA CRACK FOUND LOWER CHROD AT 11 O''CLOCK POS (VIEW LOOKING AFT) APPROX 0.050" IN LENGTH. TRANSFER XH WO.2403488 AND FX WING CENTER SECTION FRONT SPAR RH LOWER CHORD INTERIM REPAIRED AS PER EC/RA 5710-02844 REV.- PART 1. ATTACHED FORM 44-0008 ITEM 1 TO ITEM 28 ACCOMPLISHED. RII INSPECTED OKAY BY HX341008.

Part: UNKNOWN — CRACKED (LH WING) · airframe 106,718 hrs · 14,165 cycles

SUPPORT TASK- EA5310-06900 REV.D OP 013 STEP 23.7 1EA CRACK FOUND LOWER CHORD AT 12 O''CLOCK POS (VIEW LOOKING AFT) APPROX 0.070" IN LENGTH. TRANSFER HX NR WO.2403473 AND . FX WING CENTER SECTION FRONT SPAR LH LOWER CHORD INTERIM REPAIRED AS PER EC/RA 5710-02842 REV.- PART 1. ATTACHED FORM 44-0008 ITEM 1 TO ITEM 28 ACCOMPLISHED.

Part: FLOOR SUPPORT — CRACKED (STA 1287-1308) · airframe 106,718 hrs · 14,165 cycles

SUPPORT TASK- AD 2001-18-09, EA5300-01502 REV.A OP 001- HORIZONTAL PRESSURE DECK WEB CRACK FOUND, PLEASE RELEASE EA5300-01502 REV.OP 002. TRANSFER HX WO.2377581 AND. HORIZONTAL PRESSURE DECK WEB AT STA 1287-1308 BTW LBL18.30-25.70 AND LVL 39.70-46.30 PERMANENT REPAIRED PER ECRA 5310-08235 REV-

Part: TERMINAL — CORRODED (APU FIRE DETECTO) · airframe 103,626 hrs · 13,768 cycles

FIRE APU INSPECTED APU COMPARTMENT FOR SIGNS OF FIRE DAMAGE AS PER AMM REMOVED APU FIRE BOTTLE IAW AMM 26-22-01 DUE TO APU FIRE 49-11-00-200 .FOUND NO EVIDENCE OF FIRE DAMAGE. REMOVED 2 WIRES 00-0609-3-7030, & 40-0366-3-0263, 00-0609-3-6950. BETWEEN DETECTORS. WIRING INSTALLED, OPS CHKS OF APU FIRE DETECTION. C/W. INSPECTION OF APU FIRE DETECTORS FOUND UPR FWD M26008 DET AND REMOVED AND REPLACED WIRES W7291-0001R-16 &W7691-0001R-16 INSTALLED APU FIRE BOTTLE EXTINGUISHER IAW AMM 26-22-01-400. OPS UPPER AFT DETECTOR, WITH HEAVY CORROSION ON TERMINALS . UPON BETWEEN UPPER FWD APU FIRE DET & UPPER AFT APU FIRE CHK AND TEST PASSED. R/R APU FIRE DET SYSTEM IAW AMM 26-15-00/501

Part: ELEVATOR — DAMAGED (LH ELEVATOR) · airframe 101,372 hrs · 13,429 cycles

LEFT ELEVATOR FWD INBD UPPER SURFACE FND HAIL STRIKE DAMAGE REFE R HAECO NON-ROUTINE NO.9472996,ORIGINATED BY EMP:V903300. PERFORMED BY EMP:V903300,LH ELEVATOR FWD I/B UPR SURFACE HAIL STRIKE DAMAGE REPAIRED AS PER SRM 55-20-01-2R-1 REPAIR1 TABLE201 PARA4D AND SRM 51-70-04-2R-2 REPAIR 2 REV.87.

Part: ELEVATOR — DAMAGED (RH ELEVATOR) · airframe 101,372 hrs · 13,429 cycles

RIGHT ELEVATOR FWD INBD UPPER SURFACE FND HAIL STRIKE DAMAGE REF ER HAECO NON-ROUTINE NO.9473140,ORIGINATED BY EMP:V926733. PERFORMED BY EMP:V903300,RH ELEVATOR FWD I/B UPR SURFACE HAIL STRIKE DAMAGE REPAIRED AS PER SRM 55-20-01-2R-1 REPAIR 1 TABLE 2 01 PARA 4D AND SRM 51-70-04-2R-2 REPAIR2 REV.87.

Part: BATTERY PACK — LOW VOLTAGE (M023) · airframe 101,372 hrs · 13,429 cycles

LLAR BACK-UP LIGHT BATTERY PACK M023 LOW VOLTAGE RERER HAECO NON -ROUTINE NO.9472107,ORIGINATED BY EMP:V905336,SPEC NO.B777-33-3- 7024. PERFORMED BY EMP:V905495,REPLACED LLAR BACK-UP LIGHT M023 BATTER Y AS PER AMM 33-51-06-960-802 REV.93 TEST RESULT NORMAL.IDT BY E MP:V905389.

Part: BATTERY PACK — LOW VOLTAGE (M33094) · airframe 101,372 hrs · 13,429 cycles

DR 1R EMERGENCY LIGHT POWER PACK M33094 LOW VOLTAGE REFER HAECO NON-ROUTINE NO.9472105,ORIGINATED BY EMP:V905336,SPEC NO.B777-33 -3-7015. PERFORMED BY EMP:V905495,REPLACED DR 1R EMERGENCY LIGHT M33094 BATTERY AS PER AMM 33-51-06-960-802 REV.93 TEST RESULT NORMAL. IDT BY EMP:V905389.

Part: IDG — MALFUNCTIONED (NR 1 ENGINE) · airframe 100,455 hrs · 13,326 cycles

ELEC GEN SYS L EICAS STATUS IDG HAS DISCONNECTED OR A PROTECTIVE TRIP OF THE GENERATOR CONTR OL BREAKER HAS OCCURRED OR A PROTECTIVE TRIP OF THE BTB HAS OCCU RRED. FIM TASK REF : FIM TASK REFERENCE NOT FOUND CMC MSG# 2431631 FLIGHT STATUS: L INTERMITTENCE CODE: M PH: CRUISE NARRATIVE: GENERATOR CONTROL UNIT (L) COMPLETED AMM 24-11-01-801-001 UP TO UP TO STEP 11 , UNIONS AND FITTINGS LEFT ON OLD IDG TO BE SWAPPED OUT WITH NEW ONE. CONTINUED REMOVING LEFT IDG UP TO STEP I(11)(J) PAGE 9 OF AMM 24-11-01-000-801-001. INSTALLED IDG PER AMM 24-11-01-400-801-001 THROUGH PAR H4. TRACKING INFO ROTABLE PARTS CHANGE WAS INDICATED - TT # 1030378 SN OFF 0460 GENERATOR, MODE OFF 27-2411-9-0001 0460 ON 27-2411-9-0001 0496 TO IDG PER AMM 24-11-01-400-801-001 PAR H 5 AND 6 INSTALLED SAFTY WIRE ON QAD COUPLING AND CONNECTED PHASE LEADS ACCOMPLISHED IDT INSPECTION OF PHASE LEAD INTALLATION PER GMM 09-10-05 AND AMM 24-11-01-400-801-001 COMPLETED INSTALLATION OF LEFT IDG PER MM 24-11-01-400-801-001. SYSTEM TEST OK PER MM 24-11-00-700-801. ADD EMP:040254

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 96,883 hrs · 12,937 cycles

REF NON-ROITINE REF NON-ROUTINE NO.:9475253 - SPEC NO.B777-33-3-7019 - EMERGENCY LT BATT PACK CAPACTITY CHK FOUND D4 LT BATT PACK DM33407 BATT PACK OUT OF LIMIT P/N:ADD717-0 1-100. EMERGENCY LT BATT PACK REPLACED AND EMERGENCY LT TEST CARRIED OUT THE RESULT FOUND ''SATIS'' REF AMM 33-5 1-06-960-802 REV 85.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 96,883 hrs · 12,937 cycles

DATA TRANSFER REF NON-ROUTINE 9475248, SPEC NO.B777-33-3-7019 - EMERGENCY LIGHT BATT PACK CAPACITY CHK FND DR2 RT BATT PACK DM33098 OUT OF LIMIT P/N:ADD717-01-100. PERFORMED EMERGENCY LT BATTERY PACK REPLACED AND EMERGENCY LT TEST CARRIED OUT THE RESULT FND "SATIS" REF AMM 33- 51-06-960-802 REV85.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 96,883 hrs · 12,937 cycles

DATA TRANSFER REF NON-ROUTINE 9475246, SPEC NO:B777-33-3-7019 - EMERGENCY LT BATTERY PACK CAPACITY CHK FND DR2 LIGHT BATT PACK (DM33096) OUT OF LIMIT P/N:ADD717-01-100. PERFORMED EMERGENCY LT BATTERY PACK REPLACED AND EMERGENCY LIGHT TEST CARRIED OUT THE RESULT FOUND "SATIS" REF AMM 33-51-06-960-802 REV85.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 96,883 hrs · 12,937 cycles

DATA TRANSFER REF NON-ROUTINE 9475250, SPEC NO.B777-33-3-7019 - EMERGENCY LIGHT BATT PACK CAPACITY CHK FND DR4 RT BATT PACK DM33409 BATT PACK OUT OF LIMIT P/N:ADD717-01-1 00. PERFORMED EMERGENCY LT BATTERY PACK REPLACED AND EMERGENCY LT TEST CARRIED OUT THE RESULT FND "SATIS" REF AMM 33-51-06-960-802 REV85.

Part: GIRT BAR — OUT OF POSITION (R4 DOOR) · airframe 92,294 hrs · 12,420 cycles

R4 DOOR HARD TO OPEN. ACCOMPLISHED ADJUSTMENT AND TEST IAW AMM 52-11-00, ADJUSTED THE FWD GIRT BAR FITTING, OPS CHECKED OK. REMOVED SAFETY PIN AND RETURNED ACFT TO NORMAL. ACCOMPLISHED GIRT BAR FLOOR FITTING CHECK IAW AMM 52-11-18-200-801, WITNESSED FWD FLOOR FITTING ADJ OTBD 1 NOTCH ON SERRATED PLATE. DOOR OPEN & CLOSES EASILY, NO BINDING. SLIDE PIN A REMOVED, BUSSEL COVER REINSTALLED, EPAS REACTIVATED.

Part: SLIDE — CONTAMINATED (R4 DOOR) · airframe 92,286 hrs · 12,418 cycles

R4 DOOR WILL NOT OPEN. DOOR HANDLE INSIDE AND OUTSIDE ONLY OPENS HALF WAY. LOUD CLUNKING NOISE. FOUND VISIBLE MOISTURE ON BACK OF PACK SLIDE AND IN DOOR SILL. VERIFIED GIRT BAR MECHANISM ADJUSTMENT IAW AMM 52-11-00-820-801 SUBTASK 52-11-00-820-004.

Part: GAUGE — CRACKED (R1 DOOR) · airframe 90,699 hrs · 12,251 cycles

R1 MED EMERGENCY CYLINDER GAGE FOUND CRACKED. PLS NOTE THE REMOVAL PART SHOULD READ R1 DOOR.

Part: SIGN — DAMAGED (EMERGENCY LIGHTS) · airframe 90,699 hrs · 12,251 cycles

FOUND THE L2 DOOR FWD EXIT SIGN DAMAGED. REPLACED THE EXIT SIGN AND OP TESTED NORMAL IAW AMM 33-51-01-960-802, REV 80.

Part: SIGN — DAMAGED (EMERGENCY LIGHTS) · airframe 90,699 hrs · 12,251 cycles

FOUND THE L2 DOOR, FWD EXIT SIGN DAMAGED. REPLACED THE EXIT SIGN AND OP TESTED NORMAL IAW AMM 33-51-01-960-802, REV 80.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 90,699 hrs · 12,251 cycles

RIGHT CEILING AREA EMERGENCY LIGHTT BATTERY HAD LOW CAPACITY. REPLACED THE POWER SUPPLY AND OPS TESTED NORMAL IAW AMM 33-51-06-960-803, REV 80, & AMM 33-51-00-710-801, REV 80.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 90,699 hrs · 12,251 cycles

R1 DOOR EMERGENCY LIGHT BATTERY PACK HAD LOW CAPACITY. REPLACED THE BATTERY PACK AND OP TESTED NORMAL IAW AMM 33-51-06-960-803, REV 80, & AMM 33-51-00-710-801, REV 80.

Part: LIGHT — DAMAGED (GALLEY) · airframe 90,699 hrs · 12,251 cycles

DURING INSTALLATION OF THE EXIT LIGHTS AT THE M1 GALLEY, FOUND ONE LIGHT ASSY DAMAGED. REPLACED THE EMERGENCY LIGHT ASSY, AND TESTED GOOD IAW AMM 33-51-05-960-802, REV 80.

Part: LIGHT — INOPERATIVE (SEAT 44G) · airframe 90,699 hrs · 12,251 cycles

SEAT 44G EMERGENCY LIGHT LIGHT INOPERATIVE. REPLACED THE EMERGENCY LIGHT AND TESTED NORMAL IAW AMM 33-51-05-960-802, REV 80.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 90,699 hrs · 12,251 cycles

RT CEILING AREA EMERGENCY LIGHT BATTERY PACK HAD LOW CAPACITY. REPLACED THE POWER SUPPLY M33094 AND TESTED NORMAL IAW AMM 33-51-06-960-803, REV 80, & AMM 33-51-00-710-801, REV 80.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 90,699 hrs · 12,251 cycles

LEFT SEAT EMERGENCY LIGHT BATTERY PACK HAD LOW CAPACITY. REPLACED THE BATTERY PACK AND TESTED NORMAL IAW AMM 33-51-06-960-802, REV 80, & AMM 33-51-00-710-801, REV 80.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 90,699 hrs · 12,251 cycles

FOUND THE R4 DOOR EMERGENCY LIGHT BATTERY PACK WITH LOW CAPACITY. REPLACED THE BATTERY PACK AND TESTED NORMAL IAW AMM 33-51-06-960-803, REV 80, & AMM 33-51-00-710-801, REV 80.

Part: LIGHT — DAMAGED (GALLEY) · airframe 90,699 hrs · 12,251 cycles

DURING INSTALLATION OF THE EXIT LIGHTS AT THE M1 GALLEY, FOUND ONE LIGHT ASSY DAMAGED. REPLACED THE EMERGENCY LIGHT ASSY, AND TESTED GOOD IAW AMM 33-51-05-960-802, REV 80.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 90,699 hrs · 12,251 cycles

SEAT EMERGENCY LIGHT BATTERY PACK HAD LOW CAPACITY. REPLACED THE BATTERY PACK AND TESTED NORMAL IAW AMM 33-51-06-960-802, REV 80, & AMM 33-51-00-710-801, REV 80.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 90,699 hrs · 12,251 cycles

LEFT CEILING AREA EMERGENCY LIGHT BATTERY PACK HAD LOW CAPACITY. REPLACED THE BATTERY PACK AND OPS TESTED NORMAL IAW AMM 33-51-00-7 10-801, REV 80, & AMM 33-51-06-960-803, REV 80.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 90,699 hrs · 12,251 cycles

FOUND THE SEAT 36G EMERGENCY LIGHT COVER MISSING. REPLACED THE LIGHT ASSY AND TESTED NORMAL IAW AMM 33-51-05-960-802, REV 80.

Part: SIGN — DAMAGED (EMERGENCY LIGHT) · airframe 90,699 hrs · 12,251 cycles

SIGN BASE FOUND BROKEN. REPLACED THE SIGN AND TESTED NORMAL IAW AMM 33-51-01-960-802, REV 80.

Part: LIGHT — BROKEN (CABIN) · airframe 90,699 hrs · 12,251 cycles

PARTITION EMERGENCY LIGHT FOUND BROKEN. REPLACED THE EMERGENCY LIGHT ASSY AND TESTED NORMAL IAW AMM 33-51-05-960-802, REV 80.

Part: LIGHT — MISSING (SEAT 30G) · airframe 89,658 hrs · 12,131 cycles

EMERGENCY LIGHT COVER MISSING AFT OF ROW 30G. REPLACED THE LIGHT ASSY. OP CHECKED NORMAL

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 87,255 hrs · 11,880 cycles

EMERGENCY EXIT LIGHT SIGN AFT OF R3 DOOR AND TWO EMERGENCY CEILING LIGHTS RT SIDE AFT OF R3 DOOR INOPERATIVE. REMOVED AND REPLACED EXIT SIGN AND REPLACED THE LAMPS. ALL LIGHTS STILL INOPERATIVE. WHILE PERFORMING TEST OF EMERGENCY LIGHTS, FOUND THAT THE EXIT LIGHT SIGN AFT OF DOOR , WOULD COME ON ONLY FOR 2 SECONDS. REPLACED THE BATTERY PACK IAW MM 33-51-06 OPS CHECKED GOOD.

Part: CHILLER — FAILED (FWD GALLEY) · airframe 86,510 hrs · 11,786 cycles

FORWARD GALLEY CHILLER LOUD BUZZING NOISE AND STRONG BURNING ODOR. VERIFIED FWD GALLEY CHILLER AT FAULT; HAD FLT. CREW COMPLETE FOR PLACARDED PER ABOVE MEL, C/W DDP, OK FOR SERVICE. M 46-6020-SMOKE ODOR QUESTIONAIRE, COLLARED BOTH FWD GALLEY CHILLER BREAKERS AND DISCONNECTED AND STOWED CHILLER CONNECTOR PLUG. R&R THE CHILLER IAW AMM 25-33-01. ALL OPS OK

Part: SOCKET — BURNED (LAVATORY) · airframe 83,509 hrs · 11,424 cycles

ELECTRICAL SMELL IN CABIN CONSISTENTLY AT LAVATORY AT 2L, NOTICED AT LAVATORY 3L & AROUND ROWS 25 - 27. ACCOMPLISHED AMM 05-51-50, TO STEP C T. FOUND A BURNED SOCKET ON THE MIRROR LIGHT FIXTURE AT DOOR 2L, ISOLATED LIGHT BALLAST FROM THE SOCKET. ALSO USED FIM 21-00-TASK 808. NO FURTHER SOURCES FOUND.

Part: ACTUATOR — FAULTY (LT ENGINE) · airframe 83,329 hrs · 11,406 cycles

CREW REPORTS LT ENG MULTIPLE AUDIBLE SURGES. NR 1 ENG STATOR VANE ACTUATOR REPLACED IAW AMM 75-31-02. ALL ENG TESTS CHECKED NORMAL.

Part: WIRE HARNESS — PINCHED (CABIN) · airframe 81,226 hrs · 11,186 cycles

CREW REPORT, SEAT 1K EXHIBITING SPARKS & AN ELEC ODOR WHEN OPERATED TO THE RECLINE POSITION. FOUND SEAT HARNESS PINCHED & SHORTED. R & R SEAT HARNESS, OPERATIONS GOOD.

Part: PIN — UNSECURE (CABIN) · airframe 78,064 hrs · 10,855 cycles

M2 GALLEY ALL EMER LIGHTS FOUND INOPERATIVE. DURING TROUBLESHOOTING FOUND TERMINAL TB 08 POSITION NR 3 WITH LOOSE PUSHED PIN. SECURED PIN & OPERATIONS CHECKED NORMAL IAW AMM 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,064 hrs · 10,855 cycles

M2 GALLEY FOUR EACH EMER LIGHTS FOUND INOPERATIVE. DURING TROUBLESHOOTING FOUND FOUR EACH EMER LIGHT ASSEMBLIES INOPERATIVE. REPLACED LIGHTS & CHECKED NORMAL IAW AMM 33-51-05 & AMM 33-51-00.

Part: OVEN — MALFUNCTIONED (GALLEY) · airframe 76,730 hrs · 10,711 cycles

CREW REPORTS ELEC BURNING ODOR IN AFT GALLEY. SET MAIN POWER SWITCH ON GALLEY POWER PANEL TO OFF, OPENED CB'S FOR OVENS & CREW REPORTS HOT AIR STILL BLOWING FROM OVENS. REPLACED SUSPECTED OVEN R51. VERIFIED THE CONNECTOR BEHIND THE OVEN, NO IRREGULARITY FOUND. RAN THE OVEN, NO ODOR NOTICED. ALSO CHECKED OTHER COMPONENTS, SUCH AS COFFEE MAKERS, WARMING OVENS AS WELL AS OTHER OVENS IN THE AFT GALLEY. NO ODOR OCCURRED. .

Part: GCU — MALFUNCTIONED (RIGHT) · airframe 74,262 hrs · 10,446 cycles

ELEC GEN SYS RT IDG HAS DISCONNECTED OR A PROTECTIVE TRIP OF THE GEN CONTROL BREAKER HAS OCCURRED OR A PROTECTIVE TRIP OF THE BTB HAS OCCURRED. REPLACED RT GCU.

Part: SEAL — DAMAGED (COCKPIT WINDOW) · airframe 74,181 hrs · 10,435 cycles

FIRST OFFICER`S WINDOW HAS CONSTANT IN UPPER AFT CORNER. REPLACED DAMAGED FIRST OFFICER`S SLIDING WINDOW SEAL IAW MM, IAW SMC 5 FOR LEAK CHECKED.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 73,221 hrs · 10,327 cycles

APU WON'T START BY ELECTRIC STARTER, OK FOR BY PNEUMATIC. APU USEABLE IAW MEL.

Part: GENERATOR — FAULTY (BACK UP) · airframe 73,064 hrs · 10,310 cycles

ELECTRIC BACKUP GENERATOR MESSAGE, RESET ONCE. REPLACED NR 1 ENGINE BACK UP GENERATOR IAW AMM 24-25-01. OPS CHECKED GOOD, NO LEAKS, NO MAINTENANCE MESSAGE.

Part: FILTER — FAULTY (NR 2 ENG IDG) · airframe 72,438 hrs · 10,229 cycles

NR 2 ENGINE IDG FILTER. REPLACED IDG OIL FILTER ELEMENT ON RT ENGINE IDG IAW AMM. REPLACED NR 2 ENG IDG FILTER, NO CONTAMINATION FOUND. NO LEAKS NOTED AFTER ENGINE MOTOR.

Part: IDG — FAULTY (RT ENGINE) · airframe 71,791 hrs · 10,156 cycles

RT ENG IDG OIL FITER "BLOCKED", IDG BODY DELTA PRESSURE INDICATOR- DPI EXTENDED OUT. RIGHT ENGINE START TO DISCONNECT IDG AND ALSO START LT ENGINE CHECKED, NO OTHER MESSAGE. REPLACED RT ENGINE IDG. LEAK AND OPS CHECKED GOOD.

Part: CONTROL PANEL — FAILED (COCKPIT) · airframe 71,036 hrs · 10,078 cycles

ON DEP CTR RADIO WONT DEFAULT TO DATA MODE SUSPECT DCMS FAILURE. MEL COMPLIED WITH. RPL- :ACCOMPLISHED TEST PER MM. FAULTED OBSERVER CONTROL PANEL. REPLACED CONTROL PANEL PER MM.

Part: ISOLATION MOUNT — DAMAGED (FAN) · airframe 70,690 hrs · 10,035 cycles

REMOVED OUTBOARD FAN ASSY AND FOUND FORWARD UPPER ISOLATOR MOUNTS DAMAGED ON BOTH. INSTALLED OUTBOARD LAV GALLEY VENTILATION FAN PER AMM, OPS CHECKED OKAY USING MAT SYSTEM TEST.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 70,690 hrs · 10,035 cycles

NR 1 RIGHT AND LEFT WINDSHIELDS NEED REPLACEMENT. WINDOW LEFT NR 1 DELAMINATING ACROSS TOP. COMPLETED INSTALLATION OF NR 1 RIGHT AND LEFT WINDSHIELDS, IAW MM 56-11-01.

Part: UNKNOWN — ODOR (CABIN) · airframe 70,333 hrs · 10,003 cycles

F/A REPORT ELECTRICAL ODOR FWD OF AFT GALLEY FAXED ELECTRICAL SMELL PAPERWORK TO TOMC. PER TOMC CHECK PACKS ON FULL HOT AND FULL COLD TO ISOLATE SMELL. NO SMELL NOTED. PER TOMC CHECKED ALL AFT CABIN OVERHEAD AND SIDEWALL LIGHTS TO PRECLUDE BALLAST ISSUES. ALL LIGHTS FUNCTION IN ALL MODES. CHECKED E-E COMPARTMENT FOR TRIPPED C-B'S. NON TRIPPED. CHECKED ALL CACP'S PANELS NO ISSUES NOTED. REMOVED CEILING PANELS ABOVE SEATS 43 AND 44 RIGHT FOR INSPECTION REPLACED AFTER INSPECTION.

Part: CONTROL VALVE — FAILED (LT A/C PACK) · airframe 70,246 hrs · 9,989 cycles

CREW REPORTED LEFT PACK TRIPPED. RESET TWICE, NOW HAVE LEFT PACK FLOW CONTROL VALVE MESSAGE. REPLACED LT UPPER FLOW CONTROL VALVE. OPS GOOD.

Part: CARD — MALFUNCTIONED (NR 1) · airframe 70,208 hrs · 9,986 cycles

LSCF ASG CARD L LEFT SYSTEMS CARD FILE (LSCF) ARINC SIGNAL GATEWAY (ASG) RIGHT (R) CARD FAILURE. STATUS MSG01- ACTIVE CRUISE HARD; ARINC SIGNAL GATEWAY (LEFT), LSCF HAS NO OUTPUT ON ANY BUSS MSG-3118801 ACTIVE ER HARD. REPLACED ASG CARD P85A12.

Part: SKIN — DENTED (HORIZ STAB) · airframe 69,261 hrs · 9,885 cycles

ON WALKAROUND FOUND DENT IN RIGHT STABILIZER LEADING EDGE ON INBOARD SIDE OF MID PANEL.

Part: PRECOOLER — RUPTURED (NR 2 ENGINE) · airframe 68,741 hrs · 9,821 cycles

NR 2 ENGINE PRECOOLER, FOUND BOTTOM CORE RUPTURED AND CAUSING DAMAGE TO REVERSER HEAT BLANKETS. BEGAN REMOVING PRECOOLER. REMOVED PRSOV, PRSOV CONTROL PRESSURE SENSE LINE, AND 8TH STAGE THRUST BALANCE DUCT.

Part: CONTROL VALVE — FAULTY (AC BAY) · airframe 68,588 hrs · 9,805 cycles

RIGHT LOWER FCV FAULTS. DUE TO RECENT HISTORY OF RIGHT PACK LOWER FLOW CONTROL VALVE INOP IN FLIGHT, REPLACE LOWER FLOW CONTROL VALVE (PCN 646-9007) RIGHT PACK PER MM. VERIFY PART NUMBER IN IPC PRIOR TO CHANGING. REPLACED RIGHT LOWER CONTROL VALVE PER AMM. MAT TESTED NORMAL. MESSAGE IS GONE.

Part: CLAMP — BROKEN (AC BAY) · airframe 68,588 hrs · 9,805 cycles

CLAMP BROKEN ON AFT END OF LOWER FCV ON RIGHT PACK. INTERIM REPAIRED PER ECRA 2151-01134 INSTALLED CLAMP 160-0143, OPS AND LEAK CHECKED PER MM. INSTALLED NEW CLAMP AFT END OF LOWER FCV ON RIGHT PACK.

Part: START VALVE — FAULTY (RT ENGINE) · airframe 68,403 hrs · 9,784 cycles

ENGINE START VALVE R ON START WITH NO ROTATION. REPLACED START VALVE ON RT ENGINE DRY MOTORED ENG ALL IND NORMAL REF JRH & MM71-00 & REF SMC08.

Part: GCU — FAULTY (NR 1) · airframe 68,317 hrs · 9,771 cycles

ELEC GEN SYSTEM LEFT IDG HAS DISCONNECTED OR A PROTECTIVE TRIP OF THE GENERATOR CONTROL BREAKER HAS OCCURRED OR A PROTECTIVE TRIP OF THE BTB HAS OCCURRED. STATUS MSG01- LATCHED CLIMB MODE DEPENDENT; GENERATOR CONTROL UNIT (L) HAS AN INTERNAL FAULT. DB-GENERATOR CONTROL UNIT (L) MSG-2430031 LATCHD CL MODE REPLACED LEFT GCU PER MM. RAN ENGINE, OPS CHECKED NORMAL.

Part: START VALVE — FAULTY (NR 2 ENGINE) · airframe 68,302 hrs · 9,768 cycles

**RTBL** CREW REPORTS: DURING RT ENGINE START GOT RT ENGINE START VALVE EICAS MSG, ENGINE STARTED NORMAL, CURRENTLY HAVE A START VALVE STS MSG **RTBL** OPBLM TOMC 10SEP12. AHM SHOWS ENGINE START VALVE RT MM MSG 80-61562 (STARTER AIR VALVE IS NOT IN COMMANDED POSITION). START VALVE MESSAGE. REPLACED RT ENG START VLV.

Part: IDG — FAULTY (RT ENGINE) · airframe 68,095 hrs · 9,744 cycles

ELEC GENERATOR SYSTEM RIGHT IDG HAS DISCONNECTED OR A PROTECTIVE TRIP OF THE GENERATOR CONTROL BREAKER HAS OCCURRED OR A PROTECTIVE TRIP OF THE BTB HAS OCCURRED. STATUS MSG01- LATCHED CRUISE MODE DEPENDENT; INTEGRATED DRIVE GENERATOR (R) FREQUENCY IS HIGH. DB-GENERATOR CONTROL UNIT (R) MSG-2431592 LATCHD ER MODE. DUE TO QUICK TURN AND NO SPARE PART AVAILABLE, ITEM DF TO MEL, DDG COMPLIED WITH, PLACARD. REPLACED RIGHT ENGINE IDG PER AMM.

Part: FSEU — FAULTY (NR 2) · airframe 66,989 hrs · 9,613 cycles

FLIGHT EXPERIENCED A PRIMARY FLAPS FAIL. FLIGHT CONTINUED AND MADE A FLAPS 20 LANDING. FLAPS OPERATING IN SECONDARY (ELECTRIC) MODE. CAUTION MSG01-LATCHED DESCENT MODE DEPENDENT; FLAPS MOVE WITHOUT COMMAND. DB- FSEU 2 MSG02- LATCHED DESCENT MODE DEPENDENT; FLAPS MOVE WITHOUT COMMAND. MSG-2720432 LATCHD DC MODE MSG-2720432 LATCHD DC MODE. REPLACED NR 2 FLAP SLAT ELECTRONICS UNIT PER AMM27-51-01 PAGE 401. ERASED STATUS MSG. NOT ACTIVE FAULT AFTER REPLACING AND TEST OF FSEU.

Part: DISPLAY — FAULTY (CABIN) · airframe 66,936 hrs · 9,607 cycles

CAPTAIN’S INBOARD DISPLAY UNIT INOPERATIVE, SWITCHING NO HELP. SWAPPED WITH LOWER EICAS DISPLAY UNIT, OPS CHECK .

Part: UNKNOWN — SMOKE (ENGINE) · airframe 66,457 hrs · 9,553 cycles

EXCESSIVE BLACK SMOKE COMING FROM RT ENGINE FOR 30 SECONDS AFTER SHUTDOWN. ENGINE EXHAUST VISUAL INSPECTION CARRIED OUT. NO FINDINGS. ENGINE RUN CARRIED OUT. ENGINE RAN AND SHUTDOWN SATISFACTORY. NO FURTHER MTC MESSAGES. ENGINE OK FOR SERVICE. RIGHT ENGINE FUEL VALVE HIGH PRESSURE (HP) FUEL SHUTOFF VALVE POSITION DISAGREES WITH COMMANDED POSITION. MAINT REPORTED MM MESSAGE 73-60212, CLEARED MESSAGE, NOT HINGE LATCHED, STATUS MESSAGE INACTIVE, IAW FIM 73-22 TASK 802 PARA "C" PAGE 228. ACCOMPLISHED FIM 73-22 T802. MESSAGE NOT ACTIVE ON ARRIVAL. MESSAGE ERASED AND UNABLE TO REPRODUCE. ENGINE RAN & SHUTDOWN SATISFACTORY. NO FURTHER MTC MESSAGES. OK FOR SERVICE.

Part: SKIN — WORN (NR 2 NACELLE) · airframe 66,191 hrs · 9,521 cycles

NR 2 PYLON CUT OUT FOR ACCESS DOOR 443CL INBD SIDE SKIN TRIPLER P/N 311W3453-5 WORN AT PLATE LATCH CONTACT AREAS. REPAIRED ON DOCK WU Q1849X REQUIRES REPETITIVE INSP FOR WEAR EVERY 30 DAYS AND MUST BE PERMANENTLY PAIRED BY 9-22- 2010 PER UA EVA 73615. REPAIRED SKIN PER AVO2882 01, ACCOMPLISHED ON BASE WU B2763X.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 65,896 hrs · 9,491 cycles

AFT CARGO ZONE 2 FAULTS: DUE TO REPETATIVE NATURE OF AFT CARGO ZONE 2 FAULTS DEFER AFT PIT. REF MEL PROCEDURES 2616T OR REPLACE AFT CARGO SMOKE DETECTOR (M26061). REPLACED LWR CARGO SMOKE DET IN AFT CARGO, TEST PASSED.

Part: CONNECTOR — DIRTY (FUEL SYSTEM) · airframe 65,645 hrs · 9,463 cycles

ENG FUEL VALVE R' STATUS MSG AFTER SHUTDOWN WITH NON ACTIVE MTC MSG 73-60212 RECORDED ON MAT. CHKD AND CLEANED CONNECTORS DM76001C, D71074P, D71024P. CKD WIRES W0625-2950B-16 & W625-2 950W-16, W0629-2950B-16 & W0629-2950W-16. CLEARED MSG AND CYCLED FUEL CUTOFF SW SEVERAL TIMES WITH EEC POWERED, NO MSGS. ACCOMPLISHED ENGINE IDLE RUN PER AMM. START, OPS AND SHUTDOWN NORMAL WITHOUT ANY FAULTS OR MSGS. NO DEFECTS NOTED. NO OPENS OR SHORTS FOUND.

Part: ACTUATOR — FAULTY (NR 2 ENGINE) · airframe 65,474 hrs · 9,448 cycles

R ENG TCC ACTUATOR MAINT MSG 75-60682 'TURBINE CASE CLG AIR VLV ACTR (R ENG) HPT POSITION FEEDBACK IS OUT OF RANGE' HITS FREQUENTLY. REF EG6630-2 REPLACED NR 2 TCC ACTUATOR REF MM. NEEDS EEC GROUND TEST 15. ACCOMPLISHED TEST. OPS CHECKED NORMAL.

Part: CONTROL VALVE — FAULTY (AC BAY) · airframe 65,326 hrs · 9,429 cycles

RT PACK UPPER FCV RPLC. AHM SHOWS MSG 21-24102 WITH 3 HITS IN LAST 7 FLTS FOR UPPER FCV TORQUE MOTOR NOT IN THE COMMANDED POSITION. THIS WILL LEAD TO SERVICE DISRUPTIONS IF LEFT UNCORRECTED. REFERENCE FIM 21-51, TASK 818, CHECK ASSOCIATED WIRE AND CONNECTOR FOR DEFECTS AND IF OK REPLACE THE RT PACK UPPER FCV, V21512, PCN 646-9007. ENTER MESSAGE NUMBER ON REMOVAL TAG. SFOLM 01-06-12. REPLACED RIGHT UPPER FVC.

Part: ENGINE — SMOKE (RIGHT) · airframe 65,256 hrs · 9,420 cycles

WHITE SMOKE COMING FROM RT ENGINE EXHAUST DURING TAXI IN AFTER ENGINE SHUTDOWN REPORTED BY ANOTHER ACFT. AS PRECAUTION CREW CALLED FIRE SERVICES. INBOUND CREW DID NOT OBSERVE ANY ABNORMAL FLIGHT DECK INDICATION. CKD INLET AND EXHAUST NO DISCREPANCIES. MAT SHOWED SINGLE NON ACTIVE MTC MSG 73-60212. ACCMP'D ENGINE RUN UP PER JRH 2-2-1 AND FIM 73-22 TASK 801 NO FAULTS. NO PREVIOUS HISTORY.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 65,068 hrs · 9,403 cycles

DOOR 4R EXTERNAL EMERGENCY LIGHT NOT ILLUMINATED DURING TEST.

Part: FASTENER — LOOSE (NR 1 ENGINE) · airframe 64,867 hrs · 9,383 cycles

NR 1 ENG AT 1 O`CLOCK POS UPPER ACC PANEL HAS ONE LOOSE FASTENER HANGING DOWN. FASTENER WAS REMOVED FROM TOP CENTER OF PANEL, MUST BE REPLACED WITHIN FIFTY HOURS PER MM 72-33-03 CONFIG 1 PAGE 611. REPAIRED WITH EC-RA 7230 -01275. ORIGINAL HARDWARE INSTALLED.

Part: HEAT SHIELD — DAMAGED (NR 2 PYLON) · airframe 64,830 hrs · 9,379 cycles

NR 2 ENGINE NR 3 HEAT SHIELD DAMAGED ON FWD END. REPLACED HEAT SHIELD.

Part: STRIP — DAMAGED (NR 2 ENGINE) · airframe 64,830 hrs · 9,379 cycles

NR 2 ENGINE NR 3 GAP STRIP DAMAGED INBD AFT SIDE. REPLACED GAP STRIP.

Part: HEAT SHIELD — DAMAGED (NR 2 PYLON) · airframe 64,830 hrs · 9,379 cycles

NR 2 ENGINE NR 4 HEAT SHIELD DAMAGED ON FWD END. REPLACED HEAT SHIELD.

Part: COVER — ERODED (NR 1 PYLON) · airframe 64,830 hrs · 9,379 cycles

NR 1 ENG AFT PYLON HEAT SHIELD 3RD GAP STRIP COVER ERODED. REMOVED DAMAGE & CLEANED REF 777MT54-UA2. 22-32 LONG BY 3-32 DEEP.

Part: HEAT SHIELD — DAMAGED (NR 2 ENGINE) · airframe 64,830 hrs · 9,379 cycles

NR 2 ENGINE NR 2 HEAT SHIELD FWD END DAMAGED. NR 2 HEATSHIELD HUNG IN PLACE. NEEDS BOLTS RE-INSTALLED ONE AT A TIME WITH SEALANT APPLIED PER MM PROCEDURES.

Part: VALVE — BINDING (NR 2 TVBC) · airframe 64,567 hrs · 9,349 cycles

NR 2 ENGINE O/B TVBC AIR VALVE POPOUT INDICATOR IN THE CLOSE POSITION. FOUND VALVE BINDING IN CLOSED POSITION. FREED UP VALVE, VALVE OPENS AND CLOSES COMPLETELY. PERFORMED OPERATIONAL CHECK. INDICATOR PIN IN THE EXTENDED POSITION INDICATING VALVE IS NOW OPEN.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 64,493 hrs · 9,339 cycles

STATUS PAGE SHOWED FLIGHT CONTROL STATUS FOR SHORT PERIOD OF TIME. FOUND MSG FAULT CODE 270 071 00. PERFORMED MAT TEST PRIMARY FLIGHT CONTROL SYSTEM TRANSMITTER RESET TEST. PASSED, MSG ALREADY GONE UPON ARRIVAL.

Part: AMPLIFIER — FAULTY (SATCOM) · airframe 64,477 hrs · 9,335 cycles

SATVOICE LOST EICAS, CHRONIC. BOEING AHM REPORTING NUMEROUS MMSG'S RELATED TO HGA HPA. SUGGEST REPLACING HGA HPA (M23108) PCN 580-9103. REPLACED SATCOM HIGH POWER AMP PER MM. CB RESET. MAT TEST PASSED. DECALS REMOVED.

Part: SHUTOFF VALVE — LEAKING (APU) · airframe 64,465 hrs · 9,333 cycles

FOUND UPPER APU SHUTOFF VLV LEAKING ON AFT SPAR LT CENTER TANK. VLV NUMBER M28023. REMOVED APU SHUTOFF ACTUATOR. REPLACED APU SHUTOFF VALVE. RE-INSTALLED APU SHUTOFF ACT. BOTH VALVE AND ACT NEED OPS CHECKS AND STATIC LEAK CHECK. OPS CHECKED APU SHUTOFF VALVE GOOD AND LEAK CHECKED GOOD.

Part: PROBE — FAULTY (FUEL SYSTEM) · airframe 64,465 hrs · 9,333 cycles

FUEL TOTALIZE IS NOT ACCRUED PER PILOT REPORT. REPLACED RT CENTER PROBE NR 2 AND RIGHT MAIN PROBE NR 12. NO FAULTS FOUND.

Part: FAN — FAILED (RECIRCULATION) · airframe 64,360 hrs · 9,316 cycles

GASPERS MAKING SQUEALING SOUNDS NEAR 3L-R. FOUND UPPER AFT RECIRCULATION FAN FAILED. REPLACED AFT UPPER RECIRCULATION FAN ASSY PER MM.

Part: ROD — BENT (L1 DOOR) · airframe 64,383 hrs · 9,320 cycles

CREW REPORTED MAIN ENTRY L1 DOOR IS HARD TO CLOSE. FOUND SECONDARY LIFT ROD BENT. REPLACED ROD & RE-RIGGED DOOR.

Part: PROCESSING UNIT — MALFUNCTIONED (FUEL SYSTEM) · airframe 64,255 hrs · 9,304 cycles

DURING REFUELING, FOUND CENTER FUEL TANK RT REFUEL VLV IND LAMP NON LIGHT. REPLACED WITH NEW FQPU AND FQPU OPERATIONAL TEST OKAY.

Part: PRESSURE SENSOR — FAILED (APU BLEED SYS) · airframe 64,255 hrs · 9,304 cycles

APU FAILED TO START IN FLT. SHUTDOWN SHORTLY AFTER REACHING 100 PERCENT. DIFFERENTIAL PRESSURE SENSOR REPLACED.

Part: BRAKE — DAMAGED (MLG) · airframe 64,243 hrs · 9,303 cycles

BRAKE ASSY FULL OF METAL FROM WHEEL BEARING DAMAGE. BRAKE ASSY MAY ALSO HAVE DAMAGE. NEED TO REPLACE NR 2 FWD BRAKE. REMOVED OLD BRAKE ASSY NR 2 FWD REF MM. NEW BRAKE ASSY IN AREA. INSTALLED SERVICEABLE BRAKE ASSY.

Part: WINDOW — DAMAGED (COCKPIT) · airframe 64,199 hrs · 9,297 cycles

WINDOW (FLIGHT DECK) - SHOWS SIGNS OF DAMAGE. CREW COMMENTS: WHEN SUN ON WINDOW VISION OBSCURED DUE TO PITTING AND SCRATCHES. SAMC TEXT: F/O SIDE WINDOW, 2. REPLACED FLT DECK NR 2 OPERABLE WINDOW ASSY PER MM.

Part: REPAIR — DAMAGED (RT WING) · airframe 64,031 hrs · 9,282 cycles

EDGE OF PATCH LIFTED APPROX 1 INCH. PATCH LOCATED RT WING JUST AFT OF LEADING EDGE SLAT UPPER WING SKIN BETWEEN RIGHT ENGINE AND FUSELAGE. SIZE OF PATCH IS APPROX 7 INCH DIA. IT WAS LEADING EDGE SLAT PANEL. CLEANED AREA AND SECURED BY NEW FASTENER.

Part: CONTROLLER — FAULTY (CABIN TEMP) · airframe 64,019 hrs · 9,281 cycles

AIRPLANE HAS POCKETS OF HOT AND COLD AREAS -TEMP HARD TO CONTROL. REPLACED RT CABIN TEMP CONTROLLER PER MM. OPS NORMAL.

Part: HEATER — WARNING LIGHT (LT PITOT TUBE) · airframe 63,833 hrs · 9,261 cycles

PITOT HEAT LEFT ON EICAS. REPLACED LEFT PITOT ADM PER MM, OPS CHECKED GOOD.

Part: RELAY — FAULTY (PITOT HEAT) · airframe 63,733 hrs · 9,251 cycles

HEAT PITOT L STATUS AND EICAS MSGS. REPLACED RELAY K30312 LEFT PROBE HEATER CONTROL RELAY PER FIM. MAT GROUND TEST PASSED. STATUS MSG DOES NOT SHOW ON LOWER EICAS HEAT PITOT L.

Part: DRAIN — LEAKING (LT WING) · airframe 63,664 hrs · 9,243 cycles

LEFT WING MAIN TANK SUMP DRAIN LEAKING FUEL. MEASURED FUEL LEAK TO BE 42 INCHES LONG FROM SUMP DRAIN AFTER 15 MINUTE EVALUATION. ACCOMPLISHED REPAIR. SEALED AND REPLACED SUMP DRAIN. LEAK CHECK GOOD.

Part: MODULE — FAULTY (COCKPIT) · airframe 63,664 hrs · 9,243 cycles

RIGHT AIMS CABINET LRM MESSAGE ON STATUS. TRIED TO RESET, NO HELP. REPLACED RT AIMS CPM-COMM MODULE (M001) PER FIM AND AMM. LOADED OPS SOFTWARE PER AMM. MSG CLEARED, OPS NORMAL.

Part: WIRE HARNESS — FAULTY (CABIN) · airframe 63,358 hrs · 9,210 cycles

PERSONAL VIDEO DISPLAY - DOES NOT TURN ON 08G CREW COMMENTS: ACRID SMELL WHEN SCREENS FAILED (SEATS 8G + 8H). CONFIRMED. SLAVED IN NEW SPM AND SEB, NO HELP. INVES FOUND CORRODED CONN BETWEEN CABLE RD- KM6453-0808 J1 AND J2 TO CABLE ASSY RD-KM6480-2323 & RD-KM6717-2 323 P2 CONNS. 8GH SEAT IFE INOP. AFFECTED CABLE ASSY CONN DISCONNECTED, COVERED AND STOWED. LISTED PAC CABLE ASSYS REQ REPLACED BY PAC WITH UALMM ASSIST-MIN 1 SHIFT TIME SLOT REQ REPLACED 3 HARNESSES RD-KM6480-2323, RD-KM6453-0808 AND RD-KM6717-2323 AT SEATS 8GH, OPS CHECK GOOD.

Part: MODULE — FAULTY (PITOT HEAT) · airframe 63,055 hrs · 9,174 cycles

HEAT PITOT L LOSS OF LEFT PITOT HEAT. MAT SHOWS MAINT MSG 30-361 21. MEL 3031B PROCEDURES DONE. REPLACED LEFT ADM PER MM.

Part: ACE — MALFUNCTIONED (NR 2) · airframe 62,969 hrs · 9,164 cycles

FLIGHT CONTROL SYS ANY CONDITION OF THE FLIGHT CONTROL SYSTEM OR IT'S SYSTEM INTERFACES WHICH WOULD PREVENT DISPATCH. FLIGHT CONTROLS SYSTEM BELOW MINIMUM DISPATCH REQUIREMENTS, STATUS MSG-2710302 LATCHED TA MODE. REPLACED ACE L2 PER MM. ACE TEST OK. PFC SYSTEM TEST CARRIED OUT ON MAT. FLIGHT CONTROL SYS MSG CLEARED. OPS TEST OF FLAPERON CARRIED OUT OKAY.

Part: POWER SUPPLY — FAULTY (PITOT HEAT) · airframe 62,631 hrs · 9,128 cycles

HEAT PITOT EICAS MESSAGE. REPLACED LEFT POWER SUPPLY ASSEMBLY PER AMM. SYSTEM PASSED MAT TEST AND ALL MESSAGES CLEARED ON EICAS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,455 hrs · 9,105 cycles

EMERGENCY LIGHT ON SEAT 21G IS INOP. REPLACED LIGHT ASSY. OPS CHECKS GOOD.

Part: LENS — MISSING (CACBIN) · airframe 62,455 hrs · 9,105 cycles

EMERGENCY EXIT IDENTIFIER LIGHT MISSING LIGHT LENS AT DOOR 2 LEFT FORWARD LIGHT. INSTALLED EMERGENCY EXIT LIGHT LENS. AREA SECURED.

Part: CONTROLLER — FAILED (APU) · airframe 62,166 hrs · 9,068 cycles

APU BLEED AIR STS MSG. MAINTENANCE MESSAGE: 49-11 290. APU CHECK VALVE FAILED OPEN. VALVE SHOWS XX WHEN CLOSED CORRECT INDICATION WHEN OPEN. SUSPECT VALVE AS STATED. AHM CONFIRMS CHECK VALVE FAILURE (PCN: 295-1003). REPLACED CHECK VALVE AND ALSO APUC. OPS CHECKS GOOD ON GROUND IAW AMM.

Part: TRANSMITTER — FAULTY (POTABLE WATER) · airframe 62,036 hrs · 9,051 cycles

POTABLE WATER SYSTEM SERVICED TO FULL, BUT INDICATIONS SHOW 3 QTR. SERVICED TO FULL, INDICATIONS INOP IN CABIN AND SERVICE PANEL. WHEN CLEARING DEFER ITEM REMOVE DF-CF PLACARD FROM INTERIOR OF BOTH POTABLE WATER SERVICE PANEL. ALL QTY INDICATORS SHOWS 3 QTR, WITH TANKS FULL. MAY REQUIRE SUMMATION UNIT M38004, (566-0143). 1EA 566-02143 RCS 769-56M AT SFOJL HB. REPLACED SUMMATION UNIT 3-23-11, NO HELP. STILL SHOWS 3 QTR FULL. CTR TANK TRANSMITTER WILL NOT CALIBRATE. L+R CALIBRATED. TRANSMITTER 483-2065 IS LOB AFT PIT. WILL NEED TEST CABLE 926-3500 FOR QTY ADJ AFTER TXMTR REPLACED. IF UNABLE TO CALIBRATE REPLACEMENT TRANSMITTER, KNOWN FLEETWIDE ISSUE OF INTERIOR TANK DETERIORATION SUSPECTED. TANK PCN 12

Part: COMPUTER — FAILED (NR 1) · airframe 61,367 hrs · 8,984 cycles

CPM GG (M011) IN LEFT AIMS MOD RESET FAILED, MESSAGE 31-51043, GROUND TEST, RESET MODULE, NO HELP. ACCOMPLISHED MAINT TIP31-041-R2, NO HELP. REPLACED LT AIMS M011, NO HELP. RETURNED BACK ORIGINAL MO11. TRIED TO RESET LT AIMS M001 SAME, RESET FAILED. FOUND L-AMIS HAS NO SOFTWARE OR UNREADABLE. REPLACED L-AMIS M11 FROM STOCK AND LOAD SOFTWARE FROM BINDER IAW MM, NO EXISTING FAULT OR STATUS MESSAGE.

Part: LIGHT — BROKEN (CABIN) · airframe 61,324 hrs · 8,980 cycles

DOOR 2 RT LOWER FWD EMERGENCY EXIT LIGHT ASSY BROKEN. REPLACED LIGHT ASSY AT DOOR 2R, OPS CHECKED OK.

Part: CONTROL VALVE — WARNING MESSAGE (RT A/C PACK) · airframe 60,450 hrs · 8,885 cycles

RIGHT PACK FLOW CONTROL VALVE STATUS MESSAGE. REPLACED RIGHT PACK LWR FLOW CONTROL VALVE PER MM. OPS GOOD.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 60,022 hrs · 8,838 cycles

DOOR 3R EMERGENCY EXIT SIGN LENS COVER MISSING. REPLACED COVER AND OPS NORMAL.

Part: PROCESSOR — FAILED (FUEL QTY) · airframe 59,192 hrs · 8,732 cycles

CTR FUEL TANK RT FILL VALVE DOES NOT OPEN. EXISTING FAULT 28-20050 ON MAT ACTIVE LAST 30 LEGS, REPLACED FQPU, TESTS OK. CENTER FUEL TANK RT FILL VALVE OPS CHECK OK.

Part: FEEDER CABLE — BURNED (APU GENERATOR) · airframe 59,018 hrs · 8,711 cycles

APU GEN INOPERATIVE. DEF DUE TIME. MAINT MESSAGE 24-31733 LATCHED. FOUND M24003-T2 CABLE BURNED OFF AT GEN TERMINAL BLOCK. HARNESS NEEDS REPLACEMENT AND POSSIBLE GENERATOR CHANGE. REPLACED APU GEN AND FEEDER CABLES. RAN APU, APU GEN OPERATES NORMAL.

Part: PUMP — MALFUNCTIONED (FUEL BOOST) · airframe 58,373 hrs · 8,628 cycles

FUEL PUMP R AFT RIGHT AFT FUEL PUMP OUTPUT PRESSURE IS LOW. DEACTIVATED RT AFT PUMP. FAULT MESSAGE 28-12013. FOLLOWED FIM28-22 TASK 821. REPLACED RELAY K28242, TRIED SWITCH S10 AND CARDS M24403A5 & M24403A6, NO HELP. NOW POPS AFT PUMP C-B. INSTALLED ORIGINAL CARDS. SUSPECT R AFT BST PUMP. REPLACED RT AFT BOOST PUMP. LEAK AND OPS CHECK OK.

Part: LIGHT — INOPERATIVE (SEAT 2E) · airframe 58,084 hrs · 8,586 cycles

SEAT 2E FWD EMERGENCY LIGHT INOPERATIVE. REPLACED FWD LIGHT ASSY. OPS CK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,084 hrs · 8,586 cycles

FWD AFT GALLEY AT 4 L&R LT AND RT AISLE EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPS CK GOOD.

Part: WIRE — DAMAGED (CABIN) · airframe 57,984 hrs · 8,571 cycles

SEAT 1E AFT EEL LIGHT INOPERATIVE. REPAIRED EEL LIGHT WIRING SEAT 1E. OPS CHECK GOOD.

Part: FITTING — DAMAGED (THRUST REVERSER) · airframe 57,904 hrs · 8,558 cycles

FOUND HOOPTIE LT ENG RT REVERSER HALF PIT PIN MISSING FROM TIE ROD TO STRAP. EAR BENT AND CRACKED AT COWL END FROM OPEN AND CLOSING COWL WITHOUT BEING HOOKED UP. REPLACED DAMAGED FAIRING FITTING.

Part: PANEL — LEAKING (RT WING) · airframe 57,683 hrs · 8,530 cycles

RUNNING FUEL LEAK FROM FLAME ARRESTER AT RIGHT WING INBOARD OF PYLON NR 2 ENGINE. PANEL 632AB CENTRE TANK DRY BAY ACCESS PANEL AT RIGHT WING REMOVED FOR ACCESS TO LEAK IN DRY BAY. PANEL IS LOCATED INBOARD OF NO 2 ENGINE PYLON. EALED DRY BAY BULKHEAD FITTING. LEAK CKD OK. REBALANCED FUEL LOAD FOR FLIGHT. ACFT BACK IN NORMAL CONFIGURATION.

Part: LIGHT — BROKEN (SEAT 1F) · airframe 57,279 hrs · 8,459 cycles

AFT PATH LIGHT ON SIDE OF SEAT 1F OUT. PATH LIGHT BROKEN OFF. REPLACED EMERGENCY LIGHT ASSY AND CHECKED OK.

Part: PCA — FAULTY (AILERON) · airframe 55,176 hrs · 8,185 cycles

FLIGHT CONTROL SYSTEM STATUS MESSAGE. UNABLE TO RESET. REPLACED AILERON PCA & PRIMARY FLIGHT CONTROL, CHECKED OKAY. OPS SOFTWARE LOADED, ALL MAT TESTS PASSED.

Part: BATTERY — FAILED (APU) · airframe 54,264 hrs · 8,065 cycles

APU BATTERY FAILURE. REPLACED APU BATTERY, CONDITION NORMAL.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 53,896 hrs · 8,016 cycles

THE 1E EEL LIGHT INOP, 1EA LIGHT INOP, ALL OTHERS IN AREA STILL WORK NORMALLY. FOUND PLUG TO AFT EEL STRIP ON SEAT DISCONNECTED. RE-SECURED PLUG AND OPS TEST OF LIGHTS OK.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 53,795 hrs · 8,005 cycles

EMERGENCY LIGHT INOP IN AISLE ABOVE 42G. SUPPLEMENTAL DATA UPDATE TRIED RELAMP NO HELP. LT NUMBER IS L33905. CHECKED ON PLUG AT LT ASSY FOR PWR ON PIN 1 AND NO PWR. GROUND IS OK. RESEATED PLUG ON PWR SUPPLY AT M33409 AT DR 4R. NO TIME TO TROUBLESHOOT FURTHER DUE QUICK TURN. AFTER FURTHER TROUBLESHOOTING, REPLACED PWR SUPPLY M33409, OP NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,795 hrs · 8,005 cycles

EMERGENCY LIGHT INOP OVERHEAD AT AISLE 3L. RELAMPED, OPS NORMAL.

Part: CONTROL UNIT — FAULTY (APU) · airframe 53,558 hrs · 7,972 cycles

APUC IS FAULTY. REPLACED APUC.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,273 hrs · 7,931 cycles

SEAT MOUNTED EMERGENCY EXIT LIGHTS (3EA) INOP AT SEAT LOCATIONS 1E, 3E, AND 3F. RESET POWER 1E AND 3E, OPS NORMAL. REPLACED FWD EEL AT 3F. ALL OPS NORMAL.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 53,273 hrs · 7,931 cycles

EMERGENCY EXIT LIGHTS (ALL) ON AFT GALLEY 440 ARE INOP. REPLACED POWER SUPPLY M33409 AT DOOR 3R. OPS NORMAL.

Part: STARTER — DEFECTIVE (APU) · airframe 52,186 hrs · 7,791 cycles

APU INOP, NO START ON GATE. ATTEMPTED START ON ARRIVAL. NO VOLTAGE DROP ON START, APU DOOR OPEN NORMALLY. WITH APU MAINT SWITCH IN TEST NO FAULTS ON APUC. ACPD FIM 49-40 TASK 812, CONFIRMED RELAY K24494 WORKING PROPERLY AND 28VDC ON TERMINAL E2 AT ELEC STARTER. NEED TO REPLACE ELEC STARTER. REPLACED STARTER. OP CHECKS NORMAL.

Part: GENERATOR — FAULTY (APU) · airframe 52,186 hrs · 7,791 cycles

APU GENERATOR FOUND WITH ONE TERMINAL BLOCK LOOSE AND SIGNS OF OVERHEAT - FOUND DURING FAILED STARTER TROUBLESHOOTING. SUPPLEMENTAL DATA UPDATE NEEDS NEW APU GENERATOR. REPLACED APU GENERATOR. OP CKS GOOD. NO FAULTS.

Part: LIGHT — BROKEN (CABIN) · airframe 51,941 hrs · 7,758 cycles

SEAT 1F EMERGENCY LIGHT BROKEN. REPLACED LIGHT ASSY & CHECKS OKAY.

Part: LIGHT — INOPERATIVE (SEAT 1F) · airframe 51,160 hrs · 7,660 cycles

FLT ATTENDANT REPORTS EEL LIGHT AT SEAT 1F IS INOP. LIGHT FOUND INOPERATIVE. REPLACED LIGHT AT SEAT 1F AFT POSITION. OPS OKAY.

Part: INDICATION SYS — ERRATIC (FUEL QTY) · airframe 50,684 hrs · 7,596 cycles

FUEL QTY SHOWS ERRATIC. RIGHT WING QTY IND.

Part: PROBE — FAULTY (RT WING) · airframe 50,684 hrs · 7,596 cycles

FUEL QTY SHOWS ERRATIC. RT WING QTY IND FLT DIVERTED. CREW COMMENT: AFTER LANDING ALL FUEL QTY IND WORK NORMAL. CHECKED FUEL QTY BY STICK GAUGE. FOUND CMC MSG 28-20123, 28-20127 & 28-20145 CAME ON. TANK UNIT 17, 19 & 9 FAULT. REPLACED RT FUEL PROBES NR 9, 17 & 19.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 50,629 hrs · 7,591 cycles

SEAT 1E 1 EACH EEL INOP. *S/D* FOUND LOOSE CONNECTION. SECURED CONNECTION, OP CHECK GOOD. AC OK FOR SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 50,629 hrs · 7,591 cycles

SEAT 1F BOTH EEL INOP. *S/D* FOUND BROKEN WIRE IN SPLITTER CABLE. REPAIRED WIRE, OP CHECK GOOD. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (SEAT 3E) · airframe 48,792 hrs · 7,376 cycles

FOUND SEAT 3E FWD EEL INOP. REPLACED LIGHT STRIP.

Part: LIGHT — INOPERATIVE (SEAT 22C) · airframe 48,792 hrs · 7,376 cycles

FOUND SEAT 22C EEL INOP. REPLACED LIGHT ASSY.

Part: LIGHT — LOOSE (CABIN) · airframe 48,539 hrs · 7,349 cycles

INSEAT EMERGENCY LIGHTS AT SEAT 1E 2E AND 3E NEED RESECURING.

Part: FITTING — BROKEN (GIRT BAR) · airframe 48,085 hrs · 7,296 cycles

DOOR 4L AFT GIRT FITTING END BROKEN. REPLACED BRACKET. CHECKED DOOR GIRT BAR OPERATION PER 25-66-01 NORMAL. ACFT OK FOR SERVICE.

Part: OXYGEN MASK — FAULTY (COCKPIT) · airframe 47,823 hrs · 7,265 cycles

OXYGEN MASK WILL NOT STAY SNUG WHILE DEPLOYED. SUSPECT BROKEN STRAP. REPLACED DEMO MASK AT LOCATION 217. ACFT OK FOR SERVICE.

Part: RECEIVER — FAULTY (ILS) · airframe 47,681 hrs · 7,248 cycles

RIGHT ILS LOC SIGNAL BAD, MAT SHOWED RT ILS RECEIVER LOC SIGNAL INVALID NO OTHER FAULTS INDICATED CTR AND LT OK. SUSPECT FAULTY ILS. REPLACED RIGHT INSTRUMENT LANDING SYSTEM RECEIVER PER MM 34-31-01. PERFORMED MAT TEST, CK'S GOOD. ACFT OK FOR SERVICE.

Part: APU — MAKING METAL · airframe 46,543 hrs · 7,109 cycles

CREW REPORTS LOUD NOISE FROM AFT CABIN DURING FLT CONTROL CHECK. LOUD NOISE IN AFT CABIN COMES FROM DEMAND ON APU BLEED AIR SYSTEM WHEN STARTING ENGINES. REPLACED APU MASTER CHIP DETECTOR HAD SILVER CHUNKS. ROUTED SCREEN FOR CLEANING. NO BYPASS EXPERIENCED. ELECTRIC STARTER SCREEN WAS TORN IN TWO QUADRANTS BOROSCOPE PLUG NOT BROKEN. IT WAS MISSING AND RED DIRT/SAND PACKED IN HOLE. APU REMOVAL WAS NOT REQUIRED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,517 hrs · 6,981 cycles

EEL LIGHTS INOP AT SEATS 2F AND 3F AFT LIGHTS ONLY. RESPLICED NEW EEL SYSTEM ASSY AT SEATS 2F AND 3F. SYSTEM OK CHECKED OK FOR SERVICE.

Part: FAN — ODOR (CABIN) · airframe 45,486 hrs · 6,978 cycles

FA'S REPORTED FAINT ELECTRICAL ODOR IN CABIN. ODOR MAINLY NOTED BY FIRST CLASS GALLEY TO BUSINESS CLASS AREA. CREW NOTED UPPER RECIRC FAN STATUS MSG. [08-21-07] FOUND FWD UPPER RECIRC FAN C-B POPPED. :REPLACED UPPER RECIRC FAN PER MM 21-25-01. ALSO, REPLACED FILTERS. ACCOMPLISHED LEAK CHK AND OP CHECKED OK FOR SERVICE.

Part: LIGHT — MISSING (CABIN) · airframe 44,119 hrs · 6,799 cycles

SEAT 3F ARMREST EMERGENCY LIGHT MISSING. REPLACED EEL LIGHT ASSY & OPS CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,940 hrs · 6,772 cycles

EMERGENCY SEAT LIGHT OUT AT 1E. *S/D* RELAMPED, EEL SYSTEM TESTED GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 42,604 hrs · 6,583 cycles

SEAT 1E AFT EEL LIGHT AND SEAT 3F FWD EEL LIGHTS INOP. SUPPLEMENTAL DATA UPDATE REPLACED AFT EEL LIGHT ASSEMBLY IN SEAT 1E. REPAIRED EEL LIGHT WIRE IN SEAT 3F. OP CHECKED OK FOR SERVICE.

Part: SMOKE — DETECTED (COCKPIT) · airframe 41,280 hrs · 6,372 cycles

EQUIP COOLING FAN R ON EICAS, ODOR OF SMOKE IN COCKPIT BEFORE EICAS MSG. REPLACED EQUIP COOLING FAN. SYSTEM OP CHECKS OK WITH NO SMOKE OR SMELL. SUSPECT BAD BEARINGS IN FAN OR MOTOR.

Part: CHARGER — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 39,138 hrs · 6,061 cycles

ALL EEL LTS INOP AT AFT GALLEY FWD COMPLEX.

Part: SKIN — DENTED (CARGO DOOR) · airframe 38,469 hrs · 5,946 cycles

DENT WAS FOUND AT SKIN OF BULK CARGO DOOR STA 1916. DAMAGE EXCEEDED LIMIT SO MAJOR REPAIR WAS ACCOMPLISHED. DENT WAS FOUND IN SKIN OF BULK CARGO DOOR STA 1916, WIDTH=1.18" DEPTH=.063". ACP PERM REPAIR PER SRM 52-30-01. REPAIR 12, PARA 4(D). DAMAGED DUE TO IMPACT BY GROUND SUPPORT EQUIPMENT.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,081 hrs · 5,887 cycles

FOUND DENT 3 FT FWD OF DOOR 4L, AND 1 FT BELOW DOOR THRESHOLD. SKIN DENT REPAIRED PER SRM.

Part: LIGHT — DAMAGED (SEAT 3F) · airframe 37,229 hrs · 5,765 cycles

AFT EEL LIGHT AT 3F RIPPED OUT OF SEAT. REPLACED LIGHT ASSY.

Part: INDICATOR — MALFUNCTIONED (FUEL SYSTEM) · airframe 32,643 hrs · 5,114 cycles

DUAL FUEL INDICATION PROBLEM. THIS PROBLEM IS RELATED TO THE THE ISSUE DESCRIBED IN BOEING MAINTENANCE TIP 777-MT28-11, WHERE TWO OR MORE FAULTING TANK UNITS CAN CAUSE MULTIPLE NUISANCE FUEL SYSTEM FAULT MESSAGES. THE CENTER RH TANK UNIT #2 WAS IDENTIFIED AS ONE OF THE TRULY FAULTING PARTS, SO IT WAS REPLACED. THE SECOND TRUE FAULTING TANK UNIT HAS YET TO BE IDENTIFIED, SINCE IT APPARENTLY IS FAULTING INTERMITTENTLY. BUT WHEN IT IS IDENTIFIED, IT WILL BE REPLACED. THE AIRPLANE IS CURRENTLY NOT GENERATING ANY FAULT MESSAGES. THE FUEL QUANTITY PROCESSING UNIT (FQPU) WAS ALSO REPLACED PRECAUTIONARILY.

Part: LIGHT — INOPERATIVE (SEAT 12D) · airframe 32,318 hrs · 5,068 cycles

EMERGENCY LIGHTS INOP AT SEATS 3F, 12D AND 34D. REPLACED LIGHT ASSY'S.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,630 hrs · 4,659 cycles

AFT EMERGENCY LIGHT INOPERATIVE AT SEAT 1E. RELAMPED EMERGENCY LIGHT.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 16,589 hrs · 2,582 cycles

STATION 246 AFT UPPER CHORD AND AFT UPPER CHANNEL CRACKED. STATION 246 FLOORBEAM FWD VERTICAL STIFFENER IS BENT. ALSO COCKPIT FLOOR SUPPORT IS CRACKED AT STATION 244 AT ATTACH AREA FOR STATION 246 FLOORBEAM STIFFENER. *S/D* REPAIRED PER SRM 53-10-51.

Part: ENGINE — MALFUNCTIONED (NR 1 & 2) · airframe 16,175 hrs · 2,517 cycles

N1 INDICATION: ERRATIC WHEN N1 IS ABOVE 9 PERCENT, RT ENGINE. N1 FLUCTUATIONS AFTER T/O. AIR COND PACKS SURGING SOUNDS, SHORTLY AFTER NR 2 ENG. EPR AND N1 STARTED FLUCTUATING NR 2 EPR +- . 07 TO 08 EPR NR 2 N1,+- .3 TO .4. *S/D* AFTER THE HPSOV WAS INOP IN THE CLOSED POSITION, THE ENGINE STILL SURGED-EPR N1, N2. BLEED PRESSURE FLUCUATED WITH THE HPSOV LOCKED CLOSED. THE PRSOV WAS REPLACED AND NO SURGES WERE REPORTED AFTER THE ENGINE RUN-UP. NO ADDITIONAL SURGE OCCURRENCE WERE REPORTED DURING THE FOLLOWING MONTH.

Part: VALVE — OUT OF ADJUSTED (NLG)

ON TAKEOFF, NOSE LANDING GEAR SHOWED DISAGREE. NOSE GEAR APPEARED STUCK DOWN. FLIGHT RETURNED TO ORD, LANDING UNDER AMBER ALERT. *S/D* COULD NOT DUPLICATE MALFUNCTION ON GROUND. REPLACED THE NLG RETRACT ACTUATOR AND NLG LOCK ACTUATOR AS PRECAUTIONARY. SHOP FINDINGS FOUND NO FAULTS WITH ACTUATORS. REPLACED THE NLG SELECTOR BYPASS VALVE (99C55202-101), PERFORMED RIG CHECK OF THE NLG DOOR OPERATED SEQUENCE VALVE LINKAGE AS A FOLLOWUP AT A LATER DATE. THE NLG DOOR OPERATING SEQUENCE VALVE WAS FOUND SLIGHTLY OUT OF ADJUSTED. THIS WAS CORRECTED AND THE AIRCRAFT RETURNED TO SERVICE.