N784UA

Part: BOTTLE — NO DISCREPANCY (ZONE 800) · airframe 112,808 hrs · 14,617 cycles

DR 3L SLIDE GAUGE IN RED INSPECTED DR ASSIST SLIDE BOTTLE GAUGE. ARM IS STILL LOCATED IN GREEN

Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 109,713 hrs · 14,283 cycles

R4 DOOR M33409 BATTERY PACK FOUND LOW CAPACITY DURING TEST REFER HAECO NON-ROUTINE LOG PAGE:9496593,ORIGINATED BY EMP:V903218,SPE C NO.B777-33-3-7019. PERFORMED BY EMP:V903218,REPLACED R4 DOOR M33409 BATTERY PACK AN D C/O NEW BATTERY PACK TEST. THE RESULT NORMAL AS PER AMM 33-51- 06-960-802 REV.101 IDT BY EMP:V905411.

Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 109,713 hrs · 14,283 cycles

M/D R2 DOOR EMERGENCY LIGHT BATTERY PACK M33098 FOUND LOW CAPACI TY DURING CAPACITY CHECK REFER HAECO NON-ROUTINE LOG PAGE:949659 1,ORIGINATED BY EMP:V903218,SPEC NO.B777-33-3-7019. PERFORMED BY EMP:V903218,REPLACED THE M/D R2 DOOR M33098 EMERGEN CY LIGHT BATTERY PACK AND C/O NEW BATTERY PACK TEST THE RESULT N ORMAL AS PER AMM 33-51-06-960-802 REV.101 IDT BY EMP:V905411.

Part: ACCESS PANEL — MISSING (RT NACELLE) · airframe 108,624 hrs · 14,165 cycles

PDA 2 R/H ENGINE STRUT PRESSURE RELIEF DOOR/ACCESS PANEL 443CL FOUND MISSING ON ARRIVAL. PHOTO ADDED. NIL STOCK LHR. CDL APPLIED. DISPATCH DESK: 67 NAME: AC DATE: 19-MAR-24- OK TO PLACE PDA 2 R/H ENGINE STRUT PRESSURE RELIEF DOOR/ACCESS PANEL 443CL FOUND MISSING ON ARRIVAL. ON CDL 54A CDL APPLIED. SDR RAISED #1035496 INSTALLED PYLON ACCESS PANEL REF MM 54-53-01. PLACARD REMOVED

Part: ACCESS PANEL — MISSING (RT NACELLE) · airframe 107,022 hrs · 13,982 cycles

PDA, R/H ENGINE STRUT PRESSURE RELIEF DOOR/ACCESS PANEL 443CL FOUND MISSING ON ARRIVAL. PHOTO ADDED. NIL STOCK LHR. CDL APPLIED. CDL APPLIED. SDR RAISED #1035496 DISPATCH DESK: 67 NAME: AC DATE: 19-MAR-24- OK TO PLACE PDA 2 R/H ENGINE STRUT PRESSURE RELIEF DOOR/ACCESS PANEL 443CL FOUND MISSING ON ARRIVAL. ON CDL 54A.

Part: CIRCUIT CARD — FAILED (STA 287.7) · airframe 106,048 hrs · 13,863 cycles

AI CARD EICAS STATUS WING ANTI-ICE (WAI) CONTROL CARD FAILURE. FIM TASK REF : FIM TASK REFERENCE NOT FOUND CMC MSG# 3018893 FLIGHT STATUS: A INTERMITTENCE CODE: H PH: CRUISE NARRATIVE: ARINC SIGNAL GATEWAY (L EFT), RSCF CARD, ASSY, AIR OFF 27-3011-9-0001 0122 ON 0000 CARD, ASSY, AIR OFF 27-3011-9-0001 0122 ON 27-3011-9-0001 5695 MAT SHOWED ACTIVE FOR MAINT MSG 30-18893. REF FIM 30-11 TASK 815. RPL WAI CONTROL CARD REF MM 30-11-02, OPS TEST GOOD, MSG GONE. VERIFIED PROPER SOFTWARE

Part: FAIRING — BROKEN (BETWEEN BLADES 2) · airframe 102,974 hrs · 13,503 cycles

ENGINE 1, LPC 1ST STAGE FAN BLADE FAIRING (AFT HALF), IN BETWEEN FAN BLADE 20 AND 21, WITH A WHITE DOT ON THE AIRFLOW SURFACE HAS DEPARTED AIRCRAFT. NO EVIDENCE OF FOD, AS INSPECTED FROM OUTSIDE WITH A FLASHLIGHT HAS ENTERED THE CORE. FOUND 3 DAMAGES ON RUBSTRIP AREA AND ACCOUSTIC LINERS, RAISING OTHER LOG PAGES FOR THOSE DAMAGES. PICTURES ADDED

Part: BATTERY — FAILED (LLAR) · airframe 102,516 hrs · 13,452 cycles

B777-33-3-7019 LLAR EMER LIGHT BATTERY CAPACITY CHECK FAIL. TRANSFER REF. NON-ROUTINE HX NRC WO.1582466 AND ORIGINATED BY EMP V898181. LLAR EMER LIGHT BATTERY REPLACED AND TESTED NORMAL AS PER AMM 33-51-06. WORK ACCOMPLISHED BY MECHANIC V898181 INSPECTED BY V896958. IDT INSPECTED OKAY BY HX147282. ADD EMP:V898561

Part: BATTERY — FAILED (L3 M33400) · airframe 102,516 hrs · 13,452 cycles

B777-33-3-7019 DR L3 EMER LIGHT BATTERY M33400 CAPACITY CHECK FAIL. TRANSFER REF. NON-ROUTINE HX NRC WO.1582476 AND ORIGINATED BY EMP V898181. DR L3 EMER LIGHT BATTERY M33400 REPLACED AND TESTED NORMAL AS PER AMM33-51-06. WORK ACCOMPLISHED BY MECHANIC V898181 INSPECTED BY V896958. IDT INSPECTED OKAY BY HX209496. ADD EMP:V898173

Part: BATTERY — FAILED (R3 M33404) · airframe 102,516 hrs · 13,452 cycles

B777-33-3-7019 DR R3 EMER LIGHT BATTERY M33404 CAPACITY CHECK FAIL. TRANSFER REF. NON-ROUTINE HX NRC WO.1582473 AND ORIGINATED BY EMP V898181. DR R3 EMER LIGHT BATTERY M33404 REPLACED AND TESTED NORMAL AS PER AMM33-51-06. WORK ACCOMPLISHED BY MECHANIC V898181 INSPECTED BY V896958. IDT INSPECTED OKAY BY HX209496. ADD EMP:V898558

Part: BATTERY — FAILED (R1 M33094) · airframe 102,516 hrs · 13,452 cycles

B777-33-3-7019 DR R1 EMER LIGHT BATTERY M33094 CAPACITY CHECK FAIL. TRANSFER REF. NON-ROUTINE HX NRC WO.1582468 AND ORIGINATED BY EMP V898181. DR R1 EMER LIGHT BATTERY M33094 REPLACED AND TESTED NORMAL AS PER AMM 33-51-06.WORK ACCOMPLISHED BY MECHANIC V898181 INSPECTED BY V896958. IDT INSPECTED OKAY BY HX209496. ADD EMP:V898558

Part: CHARGER — FAILED (R1 M33094) · airframe 102,516 hrs · 13,452 cycles

B777-33-3-7019 DR R1 EMER LIGHT BATTERY CHARGER M33094 TEST FAIL. TRANSFER REF. NON-ROUTINE HX NRC WO.1668731 AND ORIGINATED BY EMP V898181. DR R1 EMER LIGHT BATTERY CHARGER M33094 REPLACED AND TESTED NORMAL AS PER AMM 33-51-06. WORK ACCOMPLISHED BY MECHANIC V898181 INSPECTED BY V896958. IDT INSPECTED OKAY BY HX209496. ADD EMP:V898558

Part: BATTERY — FAILED (L1 M33424) · airframe 102,516 hrs · 13,452 cycles

B777-33-3-7019 DR L1 EMER LIGHT BATTERY M33424 CAPACITY CHECK FAIL. TRANSFER REF. NON-ROUTINE HX NRC WO.1582477 AND ORIGINATED BY EMP V898181. DR L1 EMER LIGHT BATTERY M33424 REPLACED AND TESTED NORMAL AS PER AMM33-51-06. WORK ACCOMPLISHED BY MECHANIC V898181 INSPECTED BY V896958. IDT INSPECTED OKAY BY HX209496. ADD EMP:V898558

Part: BATTERY — FAILED (R3 M33401) · airframe 102,516 hrs · 13,452 cycles

B777-33-3-7019 DR R3 EMER LIGHT BATTERY M33401 CAPACITY CHECK FAIL. TRANSFER REF. NON-ROUTINE HX NRC WO.1582469 AND ORIGINATED BY EMP V898181. DR R3 EMER LIGHT BATTERY M33401 REPLACED AND TESTED NORMAL AS PER AMM33-51-06. WORK ACCOMPLISHED BY MECHANIC V898181 INSPECTED BY V896958. IDT INSPECTED OKAY BY HX209496. ADD EMP:V898558

Part: CHARGER — FAILED (R2 M33097) · airframe 102,516 hrs · 13,452 cycles

B777-33-3-7019 DR R2 EMER LIGHT BATTERY CHARGER M33097 TEST FAIL. TRANSFER REF. NON-ROUTINE HX NRC WO.1591852 AND ORIGINATED BY EMP V898181. DR R2 EMER LIGHT BATTERY CHARGER M33097 REPLACED AND TESTED NORMAL AS PER AMM 33-51-06. ATTACH FORM 44-0008 ITEM 1 TO 2 ACCOMPLISHED. WORK ACCOMPLISHED BY MECHANIC V898181 INSPECTED BY V896958. IDT INSPECTED OKAY BY HX209496. ADD EMP:V898558

Part: NONE — FAILED (AFT) · airframe 101,444 hrs · 13,301 cycles

*EMERGENCY DECLARED *OUTFLOW VALVE AFT EICAS ADVISORY AUTO CONTROL ON AFT OUTFLOW VALVE FAILED OR MANUAL MODE FOR AFT OUTFLOW VALVE SELECTED. FIM TASK REF : FIM TASK REFERENCE NOT FOUND CMC MSG# 2139040 FLIGHT STATUS: A INTERMITTENCE CODE: M PH: CLIMB. NARRATIVE: AIR SUPPLY & CABIN PRES SURE CONTROLLER (R) REMOVED AND REPLACED AFT ACUATOR CONTROL ASSY REF AMM 21-31-03-400-810-001 ADD EMP:U383471 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1058122 SN OFF 3516 ACTUATOR, CONTR OFF 27-2133-9-0001 3516 ON 27-2133-9-0001 3181

Part: NONE — NONE (PANEL) · airframe 101,379 hrs · 13,292 cycles

RII INSPECTION REQUIRED REFERENCE CARD 27-0520-8-0018 LH WING LEADING EDGE PANELS FOIL MESH INSPECTION REQUIRES INSPECTION BY BACK PER GMM - 03-20-20. ITEMS CLEARED IAW WORK CARD 27-0520-8-0021 . ITEMS HAVE BEEN REPAIRED AND ARE IN COMPLIANCE WITH SRM51-70-14-1A-0 AND RII

Part: NONE — NONE (PANAL 511EB) · airframe 101,379 hrs · 13,292 cycles

PANAL 511EB NEEDS ALUMINUM FOIL TAPE REPAIR IAW AMM TASK 51-27-01-340-801 IN COMPLIANCE WITH SRM 51-70-14-2R AND RII CLEAR TO INSTALL ACP RII INSPECTION OF REPAIR AND EDGE SEAL OK TO INSTALL PANEL REPAIR PANAL TAPE AND ADHESIVE REMOVED IN REFERENCE WITH SRM PANAL TAPE AND ADHESIVE REMOVED IN REFERENCE WITH SRM ALL TAPE INSTALLED TO PANEL AND ADHESIVE WAS APPLIED TO THE RII ACCIDENTLY LEFT OUT IN LAST UPDATE. RE-ENTRY FOR RII. 51-70-14-2R-3 51-70-14-2R-3 EDGES AND HOLES OF ALL TAPE IN ACCORDANCE WITH SRM51-70-14-2R-3. INSTALLED PANEL 511EB AS REQUIED INSPECTION NOT REQUIRED FOR PANEL INSTALLATION

Part: NONE — NONE (PANEL 511MB) · airframe 101,379 hrs · 13,292 cycles

PANAL 511MB NEEDS ALUMINUM FOIL TAPE REPAIR IAW AMM TASK 51-27-01-340-801 IN COMPLIANCE WITH SRM 51-70-14-2R AND RII CLEAR TO INSTALL ACP RII INSPECTION OF REPAIR AND EDGE SEAL OK TO INSTALL PANEL REPAIR PANEL TAPE AND ADHESIVE REMOVED IN REFERENCE WITH SRM ALL TAPE INSTALLED TO PANEL AND ADHESIVE WAS APPLIED TO THE 51-70-14-2R-3. EDGES AND HOLES OF ALL TAPE IN ACCORDANCE WITH SRM51-70-14-2R-3. INSTALLED PANEL 511MB AS REQUIRED. INSPECTION NOT REQUIRED FOR INSTALLATION

Part: NONE — NONE (PANEL 511AB) · airframe 101,379 hrs · 13,292 cycles

PANAL 511AB NEEDS ALUMINUM FOIL TAPE REPAIR IAW AMM TASK 51-27-01-340-801 IN COMPLIANCE WITH SRM 51-70-14-2R AND RII CLEAR TO INSTALL REPAIR IN COMPLIANCE WITH REF SRM 51-70-14-2R-3 AND RII. CLEAR REPAIR TO INSTALL PANAL 511AB TAPE AND ADHESIVE REMOVED IN REF. SRM 51-70-14-2R-3 REPAIR MADE TO PANEL 511AB, REF SRM 51-70-14-2R-3 ADD EMP:U224567 INSTALLED PANEL 511AB AS REQUIRED IMSPECTION NOT REQUIRED FOR PANEL INSTALLATION

Part: NONE — NONE (PANEL 511LB) · airframe 101,379 hrs · 13,292 cycles

PANAL 511LB NEEDS ALUMINUM FOIL TAPE REPAIR IAW AMM TASK 51-27-01-340-801 IN COMPLIANCE WITH SRM 51-70-14-2R AND RII CLEAR TO INSTALL ACP RII INSPECTION OF REPAIR AND EDGE SEAL OK TO INSTALL PANEL REPAIR REMOVED OLD TAPE AND CLEANED PANEL. AWAITING INSPECTION. ALL TAPE INSTALLED TO PANEL AND ADHESIVE WAS APPLIED TO THE RE-ENTRY FOR RII EDGES AND HOLES OF ALL TAPE IN ACCORDANCE WITH SRM51-70-14-2R-3. INSTALLED PANEL AS REQUIRED ACP RII INSPECTION OF REPAIR AND EDGE SEAL OK TO INSTALL PANEL

Part: NONE — NONE (PANEL 511NB) · airframe 101,379 hrs · 13,292 cycles

PANAL 511NB NEEDS ALUMINUM FOIL TAPE REPAIR IAW AMM TASK 51-27-01-340-801 IN COMPLIANCE WITH SRM 51-70-14-2R AND RII CLEAR TO INSTALL ACP RII INSPECTION OF REPAIR AND EDGE SEAL OK TO INSTALL PANEL REPAIR PANEL TAPE AND ADHESIVE REMOVED IN REFERENCE WITH SRM ALL TAPE INSTALLED TO PANEL AND ADHESIVE WAS APPLIED TO THE 51-70-14-2R-3. EDGES AND HOLES OF ALL TAPE IN ACCORDANCE WITH SRM51-70-14-2R-3. INSTALLED PANEL AS REQUIRED ACP RII INSPECTION OF REPAIR AND EDGE SEAL OK TO INSTALL PANEL

Part: NONE — NONE (WING LE) · airframe 101,379 hrs · 13,292 cycles

WING L/E FOIL MESH INSPECTION TO BE ACCOMPLISHED PRIOR TO DEPARTURE. LOCKED UNLOCKED BY TOMC FOR DISPOSITION ITEMS CLEARED IAW WORK CARD 27-0520-8-0021 ITEMS HAVE BEEN REPAIRED AND ARE IN COMPLIANCE WITH SRM51-70-14-1A-0 AND RII

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 101,039 hrs · 13,238 cycles

LLAR BACK-UP LIGHT BATTERY PACK DOESN''T OPERATE DURING FUNCTIONA L TEST REF HAECO NON-ROUTINE NO.9450068,ORIGINATED BY EMP V90535 9,SPEC NO.B777-33-3-7024. PERFORMED BY EMP V905359,REPLACED LLAR POWER SUPPLY BATTERY CHAR GER AND CARRIED OUT LIGHT TEST,THE RESULT WAS NORMAL REF AMM 33- 29-01-960-809 REV92A,IDT BY TA472.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 101,039 hrs · 13,238 cycles

LLAR BACK-UP LIGHT BATTERY PACK DOESN''T OPERATE DURING FUNCTIONA L TEST REF HAECO NON-ROUTINE NO.9446466,ORIGINATED BY EMP V90535 9,SPEC NO.B777-33-3-7024. PERFORMED BY EMP V905359,REPLACED LLAR POWER SUPPLY BATTERY PACK AND CARRIED OUT LIGHT TEST,THE RESULT WAS NORMAL REF AMM 33-29- 01-960-809 REV 92A,IDT BY TA472.

Part: CHARGER — NO TEST (EMERGENCY LIGHTS) · airframe 101,039 hrs · 13,238 cycles

DOOR L3 EMERGENCY LIGHTING BATTERY PACK M33405 DOESN''T OPERATE DURING FUNCTIONAL TEST REF HAECO NON-ROUTINE NO.9450069,ORIGINAT ED BY EMP V905359,SPEC NO.B777-33-3-7015. PERFORMED BY EMP V905359,REPLACED DOOR L3 M33405 BATTERY CHARGER AND CARRIED OUT LIGHT TEST,THE RESULT WAS NORMAL REF AMM 33-51- 06-960-803 REV92A,IDT BY TA472.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 101,039 hrs · 13,238 cycles

DOOR R1 EMERGENCY LIGHTING BATTERY PACK M33094 CAPACITY LOW DURI NG FUNCTIONAL TEST REF HAECO NON-ROUTINE NO.9446470,SPEC NO.B777 -33-3-7015. PERFORMED BY EMP V905359,REPLACED DOOR R1 M33094 BATTERY PACK AN D PERFORMED LIGHT TEST,THE RESULT WAS NORMAL REF AMM 33-51-06-96 0-802 REV 92A,IDT BY TA472.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 101,039 hrs · 13,238 cycles

DOOR L3 EMERGENCY LIGHTING BATTERY PACK M33405 DOESN''T OPERATE D URING FUNCTIONAL TEST REF HAECO NON-ROUTINE NO.9446468,ORIGINATE D BY EMP V905359,SPEC NO.B777-33-3-7015. PERFORMED BY EMP V905359,REPLACED DOOR L3 BATTERY PACK M33405 AN D PERFORMED LIGHT TEST,THE RESULT WAS NORMAL PER AMM 33-51-06-96 0-802 REV 92A,IDT BY TA472.

Part: BATTERY — INOPERATIVE (R3 DOOR) · airframe 97,226 hrs · 12,805 cycles

TEST FOUND RT DOOR 3 EMER BATTERY DM33401 INOP REF NON-ROUTINE NO.9481334 - EA 2500-04866D OP021. REPLACED RT DOOR 3 EMERGENCY LT BATTERY, C/OUT INSTALLATION TEST OF THE NEW BATTERY, THE RESULT FOUND ''NORMAL'' REF AMM 33-51-06- 960-802 REV.86.

Part: BATTERY — DISCHARGED (CABIN) · airframe 97,226 hrs · 12,805 cycles

TEST FOUND EMERGENCY LIGHT M33097 CAPACITY LOW REF NON-ROUTINE NO.9479212 - EA 2500-04866D OP021. REPLACED EMERGENCY LT BATTERY M33097, C/OUT INSTALLATION TEST OF THE NEW BATTERY, THE RESULT FOUND ''NORMAL'' REF AMM 33-51-06-960- 802 REV.86.

Part: LATCH — UNLATCHED (R4 DOOR SLIDE) · airframe 91,717 hrs · 12,191 cycles

R4 DOOR SLIDE PACK COVER UNLATCHED ON ONE SIDE. SECURED THE LATCH.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 91,673 hrs · 12,186 cycles

ON ARRIVAL, RAMP REPORTED SEEING FLAMES AND SMOKE FROM THE LEFT ENGINE ON SHUTDOWN . THE ENGINE FUEL VALVE LT STATUS MESSAGE, FIM PROCEDURE CARRIED OUT IAW 73-22-00-810-801-N00, THE LEFT ENGINE WIRING CHECKED IAW WDM 76-21-71, CHECKED NORMAL. RELAY K76104, REPLACED AS PRECAUTION. FUEL CUTOFF SWITCH CYCLED TO UNLATCH FAULT AND MESSAGE ERASED. ENGINE GROUND IDLE RUNS CARRIED OUT AND ENGINE SHUTDOWN NORMALLY WITH CORRECT INDICATIONS.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHT) · airframe 91,505 hrs · 12,168 cycles

L4 DOOR EMERGENCY LIGHT POWER SUPPLY M33407, FOUND CAPACITY LOW THE POWER PACK WAS REPLACED, TESTED NORMAL IAW AMM 33-51-06.

Part: BULKHEAD WEB — CRACKED (BS 1287) · airframe 91,501 hrs · 12,166 cycles

HORI ZONTAL PRESSURE BULKHEAD WEB BS 1287 BETWEEN RBL18.3 & 25.7. FOUND CRACKED. AREA TRIMMED OUT IAW DWG 524W0008, SHT 8, HFEC IN SPECTION CARRIED OUT IAW NTM PT6 51-00-01, PROC 2, REV 71. NO CRACK WAS FOUND AT TRIMMED AREA, PLUG INSTALLED IAW DWG 624W0008, SHT 8.

Part: FRAME — CRACKED (BS 2370) · airframe 91,501 hrs · 12,166 cycles

RIGHT BS 2370 PIVOT BULKHEAD FORWORD FRAME FOUND CRACKED, ACCOMPLISHED OP 14 OF EA 5380-01113.

Part: BULKHEAD — CRACKED (BS 1287) · airframe 91,501 hrs · 12,166 cycles

HORIZONTAL BULHEAD WEB BS 1287 BETWEEN LBL 18.3, AND 25.7 FOUND CRACKED, THE BULKHEAD WEB FOUND CRACKED. TRIMMED OUT AREA IAW DRAWING 624W0008, SHT 8. HFEC INSPECTION CARRIED OUT IAW NTM PART 6, 51-00-01 PROC 2, REV 71, REV, NO CRACK WAS FOUND AT TRIMMED AREA. PLUG INSTALLED IAW DRAWING 624W0008, SHT 8.

Part: FRAME — CRACKED (BS 2370 BULKHEAD) · airframe 91,501 hrs · 12,166 cycles

LEFT BS 2370 PIVOT BULKHEAD FORWARD FRAME FOUND CRACKED, INSPECTED IAW EA 5380-01113, OP 13.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 91,501 hrs · 12,166 cycles

L1 DOOR EMERGENCY LIGHT BATTERY PACK M33093, FOUND CAPACITY LOW. REPLACED THE BATTERY PACK. TEST CARRIED OUT AND OPS NORMAL IAW AMM 33-51-06.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 91,501 hrs · 12,166 cycles

R4 DOOR EMERGENCY LIGHT POWER PACK M33408 FOUND CAPACITY LOW. THE BATTERY PACK WAS REPLACED. TEST CARRIED OUT, AND OPS NORMAL IAW AMM 33-51-06.

Part: BULKHEAD WEB — CRACKED (BS 1287) · airframe 91,501 hrs · 12,166 cycles

PRESSURE BULKHEAD WEB BS 1287 BETWEEN RBL 11 TO 18.3 FOUND CRACKED. PRESSURE BULKHEAD WEB TRIMMED OFF AND FABRICATED A FILLER IAW ECRA 5310-07340, REV-. HFEC INSPECTION CARRIED OUT IAW NTM INSPECTION CARRIED OUT IAW NTM PART 6,51-00-01 PROC 2 REV 7 REV, NO CRACK WAS FOUND AT TRIMMED AREA.

Part: SKIN — DENTED (CARGO DOOR) · airframe 91,501 hrs · 12,166 cycles

BULK CARGO DOOR DENTED. HF EC ACCOMPLISHED AND FOUND TO BE SMOOTH AND CRACK FREE, WITHIN LIMITS IAW 52-30-01 P112.

Part: COVER — DETACHED (R4 DOOR SLIDE) · airframe 90,939 hrs · 12,104 cycles

SLIDE COVER DETACHED AT THE R4 DOOR, SLIDE COVER INSTALLED.

Part: LIGHT — DAMAGED (CABIN) · airframe 90,772 hrs · 12,087 cycles

EMERGENCY LIGHT IS DAMAGED ON RT AISLE DIVIDER AFT OF BUSINESS CLASS. REPLACED EMERGENCY LIGHT ON RT AISLE DIVIDER AFT OF BUSINESS CLASS. OPS CHECK NORMAL.

Part: COVER — MISSING (CABIN) · airframe 88,934 hrs · 11,878 cycles

EMERGENCY EXIT LIGHTS DAMAGED 121-22B DR-2L FWD LAV 121 2L EXIT LIGHT COVER MISSING. REPLACED EXIT INDICATOR ASSY.

Part: BATTERY — DISCHARGED (R1 DOOR) · airframe 84,996 hrs · 11,435 cycles

DOOR 1R EPAS LIGHTS NOT FLASHING. REPLACED 2 EACH, 9 VOLT BATTERY IAW 51-11-20. LIGHTS OPS CK GOOD.

Part: RECEPTACLE — BURNED (LAVATORY) · airframe 83,370 hrs · 11,252 cycles

LAVATORY 3L BURNING SMELL. ACCOMPLISHED INSPECTIONS IAW MM 05-51-50. FOUND MIRROR LIGHT FWD LAMP RECEPTACLE BURNT & CAUSING ODOR. REMOVED LAMP, DISCONNECTED & SAFETIED BALLAST M004 CONNECTOR IAW STANDARD PRACTICES. COMPLIED WITH MEL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 79,150 hrs · 10,809 cycles

FUSE BELLY SKIN PITTING DAMAGE FROM BS 332 TO 655, STRINGER 45L TO 45R. REPAIRED IAW ECRA 5330-05042. NO PITTING DAMAGE ON THE EXISTING DOUBLER ON BS 508, BETWEEN STRINGER 47R & 48R. THIS REPAIR HAS RECEIVED STAGE 1 APPROVAL VIA FORM 8100-9 DATED FEB 13TH 2015. IF A NEW FORM FINDING NOT ISSUED PRIOR TO FEB 13TH 2017 THE AIR WORTHINESS CERTIFICATE OF THIS ACFT WITH THIS REPAIR IS NO LONGER VALID.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 79,150 hrs · 10,809 cycles

FUSE BELLY SKIN PITTING DAMAGE FROM BS 332 TO 655, STRINGER 45L TO 45R. REPAIRED IAW ECRA 5330-05042. NO PITTING DAMAGE ON THE EXISTING DOUBLER ON BS 508,BETWEEN STRINGER 47R & 48R. THIS REPAIR HAS RECEIVED STAGE 1 APPROVAL VIA FORM 8100-9 DATED FEB 13TH 2015.

Part: UNKNOWN — ODOR (GALLEY) · airframe 78,033 hrs · 10,690 cycles

AFT GALLEY HAS A SLIGHT SMOKEY ODOR. CLEANED ALL WARMING OVENS, COFFEEMAKERS, OVENS & COFFEE WARMERS. RAN ALL ABOVE PLUS CHILLERS. NO SMOKE NOTED OR CIRCUIT BREAKERS TRIPPED. PROCEDURES AMM 05-51-11 & 05-51-50.

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT) · airframe 76,428 hrs · 10,523 cycles

ALL AUTO PILOTS DISCONNECTED & NO LAND 3 STATUS MSG. CMC FAULT DOWNLINKED AUTOPILOT BACKDRIVE RT. BACKDRIVE SYS INOPERATIVE OR DEGRADED DUE TO FAILURE IN RT COLUMN. CREW CYCLED CB AS NO AUTOPILOTS WOULD ENGAGE. THE CYCLING OF THE BREAKER ALLOWED THE AUTOPILOT TO RE-ENGAGE BUT CREW COULD NOT CLEAR THE EICAS STATUS MSG OR THE NO LAND 3 MSG & DECIDED TO RETURN TO THE FIELD. FUEL DUMPED.

Part: UNKNOWN — MALFUNCTIONED (RT ENGINE) · airframe 74,869 hrs · 10,353 cycles

ENG EEC C1 RT ENG CONTROL IS IN A TIME LIMITED DISPATCH CONDITION. ENG CONTROL SYS IS OPERATING WITH REDUCED REDUNDANCY. STATUS MSG 01- NOT ACTIVE CRUISE MODE DEPENDENT. EEC RT ENG T2 SIGNAL DOES NOT AGREE WITH TOTAL AIR TEMPERATURE SIGNALS FROM AIR DATA INERTIAL REFERENCE UNIT & SECONDARY ATTITUDE AIR DATA REFERENCE UNIT. DB EEC RT ENG CH A MSG 02 ACTIVE CRUISE MODE DEPENDENT. MSG 7762082 INACTIVE ER MODE MSG 7762082 ACTIVE ER MODE. AHM SHOWS FIRST LEG THIS FAULT & SHOWED TEMP DIFFERENCE BETWEEN LT & RT ENG. THIS NOSE COWL HAS JUST BEEN REPLACED SO WILL REQUIRE TROUBLE SHOOTING IAW FIM 77-11-815. ON GND BOTH INDICATIONS WITHIN 2 DEGREES OF TAT. PLACARD PLACED NEXT TO EEC SWITCH

Part: FSEU — FAILED (NR 2) · airframe 73,955 hrs · 10,255 cycles

SLAT PRIMARY FAIL EICAS ADVISORY MESSAGE, CYCLED FLAPS & MESSAGE RETURNED. SLATS RETRACTED IN THE SECONDARY MODE. REPLACED NR 2 FSEU IAW AMM, OPERATIONS CHECKED NORMAL. NO FAULTS OR EICAS MESSAGES.

Part: PUMP — ARCED (FUEL SYSTEM) · airframe 73,720 hrs · 10,226 cycles

CTR LT OVRD JETTISON PUMP PIN C FOUND ARCING. CTR LT OVRD JETTISON PUMP REPLACED IAW B777 AMM 28-22-06 & CONNECTOR DM28103 REPLACED IAW SWPM 20-61-19 & WDM 28-22-13.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,704 hrs · 10,225 cycles

ONE EMERGENCY EXIT LIGHT NOT WORKING AT RT AISLE ON WALL SIDE OF THE FWD A4 AFT GALLEY AREA ACROSS THE AISLE FROM PASSENGER DOOR 4RT. RELAMPED, OPERATION CHECKED NORMAL.

Part: CHARGER — FAULTY (CABIN) · airframe 73,704 hrs · 10,225 cycles

EMERGENCY EXIT LIGHTS COME ON, BUT DO NOT STAY ON FOR ONE MINUTE. LOCATED AT LT & RT SIDES OF SEAT ROWS 19 THRU 30, & AT THE RT CEILING FROM ROWS 22 THRU 30. REPLACED BATTERY CHARGER.

Part: BATTERY — FAULTY (FUEL SYSTEM) · airframe 73,197 hrs · 10,170 cycles

FUEL SHUTOFF VALVE BATTERY STATUS MSG. DEF IAW MEL. ACCOMPLISHED FIM 28-22 TASK 842, REPLACED ENG FUEL SPAR VALVE BATTERY IAW MM. OPERATIONS TESTED IAW MM, OPERATIONS NORMAL.

Part: POSITION SENSOR — FAULTY (LE SLAT) · airframe 73,098 hrs · 10,159 cycles

STATUS MESSAGE "FLAP-SLAT CONTROL 2" DISPLAYED. MAT MAINTENANCE MESSAGE 27-21172, SLAT POS SENSOR 2L, FAULTED. FOUND OPEN CKT ACROSS PINS J4 & K4 AT CONN DM27002AC. SUSPECT SENSOR M27203. ACP WIRE CONTINUITY CHECK BETWEEN FSEU 2 BENCH CONNECTOR DM27002 & SLAT POS SENSOR 2L M2 7203. ALL WIRES CHECKED OK IAW FIM 27-82 TASK 816 & WDM 27-88-12. REPLACED LT SLAT POS SENSOR 2L M27203 IAW MM 27-88-03. ACP OPERATIONS TEST MM 27-88-00-710-801 TESTED NORMAL.

Part: COUPLER — FAULTY · airframe 72,628 hrs · 10,106 cycles

FLIGHT CONTROL SYSTEM ANY CONDITION OF THE FLIGHT CONTROL SYSTEM OR IT'S SYSTEM INTERFACES WHICH WOULD PREVENT DISPATCH. FLIGHT CONTROLS SYSTEM BELOW MINIMUM DISPATCH REQUIREMENTS. STATUS MSG01- ACTIVE CRUISE HARD;POWER SUPPLY ASSEMBLY (LEFT) HAS NO OUTPUT ON FLIGHT CONTROLS ARINC 629 BUS (LEFT). DB- PRIMARY FLIGHT COMPUTER (RIGHT) MSG02- ACTIVE CRUISE HARD;POWER SUPPLY ASSEMBLY (LEFT) HAS NO OUTPUT ON FLIGHT CONTROLS 629 BUS (LEFT). MSG-2458811 ACTIVE ER HARD MSG-2458811 ACTIVE ER HARD. MSG 24-58811. REPLACED 629 COUPLER B24101 IAW MM 23-91-01. OPERATIONS CHECKED OK. FLIGHT CONTROL SYSTEM MESSAGE REPLACED ARINC 629 COUPLERS & PSA-LEFT.

Part: VALVE — FAULTY (APU BLEED) · airframe 72,096 hrs · 10,046 cycles

APU BLEED STATUS MESSAGE. REPLACED SURGE VALVE IAW MM 49-53-01. OPS CHECKED OK, NO LATCH MESSAGES. NO LEAKS.

Part: GENERATOR — INOPERATIVE (RT BACK UP) · airframe 71,955 hrs · 10,030 cycles

RIGHT BACKUP GENERATOR INOPERATIVE.

Part: SKIN — DENTED (R4 DOOR) · airframe 71,864 hrs · 10,020 cycles

R4 DOOR OUTER SKIN HAS A DENT LOCATED 25 INCHES UP FROM BOTTOM, 3 INCHES FROM AFT EDGE AND APPROX 8 INCHES LONG.

Part: CONTROL PANEL — FAILED (AUTOPILOT) · airframe 71,738 hrs · 10,006 cycles

MODE CONTROL PANEL LANE 1 OF THE 2 LANES IN AUTOPILOT FLIGHT DIRECTOR SYS (AFDS) MODE CONTROL PANEL (MCP) OR ITS INTERFACE TO THE AFDC HAS FAILED. REPLACED MCP IAW MM, OPS TESTED OK.

Part: ACTUATOR — LEAKING (NR 2 ENGINE) · airframe 71,500 hrs · 9,978 cycles

NR 2 ENGINE STATOR VANE ACTUATOR LEAKING FUEL. REPLACED SVA PER AMM, OPS AND LEAK CHECK NORMAL.

Part: FSEU — FAILED (TE FLAPS) · airframe 71,427 hrs · 9,970 cycles

PRIMARY FLAPS FAILED. FAULT CODE 27-20371, REF 27-51 TASK 801. REPLACED NR 1 FSEU PER MM 27-51-01. PERFORMED TRAILING EDGE FLAP SYSTEM OPS TESTED AND RAN FLAPS TO FULL. MESSAGE DID NOT RETURN.

Part: FSEU — FAULTED (FLAP/SLAT SYS) · airframe 71,222 hrs · 9,944 cycles

FLAP SLAT CONTROL 1 HIGH LIFT CONTROL LANE NR 1 HAS A FAULT. REPLACED FSEU 1. SYSTEM OPS CHECK NORMAL.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 71,169 hrs · 9,939 cycles

STATUS MSG "ENGINE REVERSER R" DISPLAYED. STATUS MSG CAME BACK AGAIN AFTER R-ENG REVERSER OPS. RIGHT ENGINE REVERSER DEACTIVATED PER MEL.

Part: BOLT — MISSING (OXYGEN MASK BIN) · airframe 71,155 hrs · 9,938 cycles

OXYGEN MASKS HAVE DROPPED AT SEATS 9CD. ARMING PINS ARE STILL INSTALLED ON O2 GENERATOR BOTTLES INDICATING THEY HAVE NOT BLOWN. FOUND LEFT CENTER STOW BIN FWD AND AFT PIVOT BOLTS MISSING CAUSING STOW BIN TO CATCH ON O2 DOOR. FORCING DOOR OPEN. REPLACED PIVOT BOLTS AND SECURED O2 DOOR PER MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 71,060 hrs · 9,926 cycles

R1 DOOR EMERGENCY EXIT FLOOR LIGHT LENS IS BROKEN. REPLACED LENS.

Part: BULB — LOOSE (EMERGENCY LIGHT) · airframe 71,060 hrs · 9,926 cycles

R1 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. . BULB LOOSE IN SOCKET.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,060 hrs · 9,926 cycles

EMERGENCY LIGHTS INOPERATIVE AT R1 & L3 DOORS. REPLACED BATTERY PACK. OPS CHECKED OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,060 hrs · 9,926 cycles

LEFT CEILING EMERGENCY LIGHTS FROM DOOR 3L TO ROW 36 ARE INOPERATIVE AND AFT EXIT SIGN ON DOOR 3L IS INOPERATIVE. REPLACED BATTERY PACK AT DOOR 3L, AFT POSITION.

Part: HOUSING — DAMAGED (EMERGENCY LIGHT) · airframe 71,060 hrs · 9,926 cycles

AFT GALLEY CROSS AISLE LEFT EMERGENCY LIGHT INOPERATIVE ON FWD COUNTER UNIT AT FLOOR LEVEL. FOUND LEFT ASSY BROKEN. REPLACED LIGHT ASSY WITH NEW STYLE. CHECKED GOOD.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 70,454 hrs · 9,863 cycles

DURING APPROACH, AN ELECTRICAL ODOR NEAR 1L AND LAV WAS DETECTED. FOUND SOURCE OF ODOR TO BE BALLAST AT CEILING LIGHT ABOVE SEAT 1A, FOUND FLUORESCENT TUBES AT 1A LOOSE AND INTERMITTENT, REMOVED TUBES FROM 1A & 2A CEILING LIGHTS, REMOVED BALLAST AT 1A DISCONNECTED CONNECTOR AND SECURED. REPLACED BALLAST.

Part: WIRE HARNESS — WORN (RT GENERATOR) · airframe 70,029 hrs · 9,820 cycles

GENERATOR DRIVE LIGHT OFF, FOUND WIRES CHAFED AT HARNESS CLAMPS ON WIRE BUNDLE DM24001B. REPLACED WORN WIRE HARNESS. RAN ENGINE, CHECKEDS OKAY.

Part: WIRE HARNESS — CHAFED (GENERATOR SYS) · airframe 70,029 hrs · 9,820 cycles

GEN DRIVE LIGHT OFF, FOUND WIRES CHAFED AT HARNESS CLAMPS ON WIRE BUNDLE DM24001C. REPLACED WIRE HARNESS.

Part: RFU — MALFUNCTIONED (SATCOM) · airframe 70,025 hrs · 9,818 cycles

SATCOM SYSTEM WILL STAY IN SEARCH MODE AFTER LOG OFF AND RE-LOG ON. REPLACED RFU-L M23107 REF WD 23-15-12 PG 5A SHEET 3. NEED OPS CHECK FOR SEVERAL HOURS. ACCOMPLISHED SATCOM SYSTEM OP CHECK REF AMM 23-15-00-501, OPS NORMAL.

Part: PANEL — FAULTY (VHF COMM) · airframe 70,016 hrs · 9,816 cycles

SATVOICE LOST SATCOM VOICE SYSTEM LOGS OFF. ADVISORY CREW COMMENTS: NO SATCOM FOR ENTIRE FLT. NOW 1.5HRS OF FLT. CHRONIC+ETOPS RESTICTED. CENTER VHF TUNING PANEL WAS REPLACED. ACCOMPLISHED GND TEST PER MM, OPS CHECK OKAY.

Part: BATTERY — DISCHARGED (SAT PHONE) · airframe 69,527 hrs · 9,764 cycles

SAT PHONE INOPERATIVE IN CABIN. ON START UP FAULT BALL DISPLAYED ON CTU. TEST EQUIPMENT CHECKED OUT TO RESET CTU AND TROUBLESHOT BUT LAPTOP BATTERY DEAD.

Part: CLAMP — LEAKING (AC BAY) · airframe 69,227 hrs · 9,733 cycles

RIGHT PACK UPPER FLOW CONTROL VALVE LEAKING AT V-BAND CLAMP. REPLACED V-BAND CLAMP, NO LEAKAGE NOTED.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 69,129 hrs · 9,719 cycles

SMELL EMANATING FROM LEFT PACK SMELL IS IN THE REAR OF THE AC AND COCKPIT. NO SMELL IN MID AND FIRST CLASS. IT IS 1HOUR AND 52 MIN SINCE T/O. THE SMELL IS COMING FROM THE LEFT PACK, WITH LEFT PACK OFF SMELL DISSIPATED. ITEM ROLLED FORWARD. POWER AT IDLE, SMELL STRONG IN DESCENT. ACCOMPLISHED NUMEROUS CH ITEMS ASSGINED BY EG. SEE AMIS HISTORY FOR COMPONENTS REPLACED. ACCOMPLISHED BURNOUT ON BOTH AIR CONDITIONING PACKS. NO ABNORMAL ODORS NOTED WITH SFOEG SPECTROMETER ANALYSIS EQUIPMENT.

Part: GENERATOR — FAULTY (NR 1) · airframe 69,129 hrs · 9,719 cycles

STATUS MESSAGE ELEC BACKUP GENERATOR L AFTER SHUTDOWN. CYCLED BACKUP GENERATOR SWITCH, RAN ENGINE, BUG OPERATED NORMALLY MSG RETURNED AFTER SHUTDOWN. REPLACED LEFT ENGINE BACK UP GENERATOR.

Part: START VALVE — FAULTY (APU) · airframe 69,129 hrs · 9,719 cycles

APU AIR START VALVE CYCLES OFF AND ON WITH THE APU RUNNING AND APU BLEED VALVE OFF. THIS SHOWS ON THE AIR PAGE. REPLACED STARTER VALVE REF NEEDS OPS AND LEAK CHECKS. ACP OPS CHECK, NO LEAKS NOTED.

Part: BELLOWS — TORN (AC BAY) · airframe 69,117 hrs · 9,715 cycles

ODOR IN THE CABIN-FD. DUE TO HISTORY OF ODOR IN THE CABIN-FD. REPLACED TORN BELLOW ON FLEXIBLE SURGE DUCT. REF AMM FOR VALVE REMOVED AND REPLACED. REMOVED APU SOV & INSPECTED UPSTREAM & DOWNSTREAM OF VALVE. NO OIL CONTAMINATION NOTED, DUCT CLEAN. RE-INSTALLED APU SOV.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 69,074 hrs · 9,707 cycles

ACRID SMELL IN COCKPIT GOING THRU 14000 DESCENT. ON ARRIVAL NO SMELL IN CABIN , NOR COCKPIT. NO MSG FOUND. ACPD FAULT ISOLATION PROCEDURE PER FIM 21-00 TASKS 808 FOUND ALL NORMAL. NO EVIDENCE OF BIRD STRIKE ON BOTH ENGINE. RUN APU AND PACKS FOR ONE HOUR NO SMELL FELT. ACPD GROUND TEST EQUIPMENT COOLING AND GASPER, BOTH PASSED.

Part: A/C PACK — CONTAMINATED (AC BAY) · airframe 69,013 hrs · 9,696 cycles

FLIGHT CABIN CREW REPORTS ACRID SMOKEY SMELL IN THE FIRST CLASS GALLEY AREA FOR 5 MINS. FOUND STRONG SMELL COMING FROM FIRST CLASS OVEN R11. REPLACED OVEN. ON APPROACH INTO IAD, PURSER REPORTED STRONG ACRID SMELL IN FIRST CLASS AREA, F. FA OPENED OVERHEAD BIN 2C AND REPORTED A VERY STRONG ACRID ODOR FROM BIN. NO SMOKE PRESENT AT ANY TIME ONLY ODOR. FOUND ACFT TO STILL HAVE STRONG ODOR IN CABIN WITH PACKS USING APU AIR. ODOR AT BOTH GND AIR CONDITIONED CONNECTOR, STRONGER FROM RT PACK. CONFIRMED ODOR WITHIN PACKS. ACP'D AIR COND SYS OIL CONTAMINATION REMOVAL WITH UPPER FLOW CONTROL VALVES LOCKED CLOSED. RAN BOTH ENGINES AT POWER PER MM FOR 45 MINS UNTIL ODOR DISSIPATED. REACTIVATED UPPER FCV'S AND RETURNED ACFT TO NORMAL CONDITION. CONDITIONED AIR AT GROUND CONDITIONED AIR CONNECTORS NOW FREE OF OIL ODOR.

Part: CONTROL VALVE — FAULTY (AC BAY) · airframe 69,011 hrs · 9,695 cycles

ELECTRICAL ODOR IN GALLEY, FLIGHT DIVERTED. PILOT BUNK ROOM. TURNED OFF GALLEY POWER. ODOR WENT AWAY IN GALLEY AND BUNK AREA, THEN ADDITIONAL ODOR THROUGHOUT COCKPIT AND CABIN. RAN BLEED AIR, BOTH PACKS AND RECIRC FANS WITH NO ODOR. TURNED ON ALL GALLEY EQUIPMENT FOR 30 MIN WITH NO ODOR. CMC FAULT FOR THE BULK CARGO VENT FAN DOES NOT FOLLOW COMMAND OR IS OVERHEATED. REF DF620 AND COMPLIED WITH FIM TASK 21-00-00-808 J AND K. REF FIM TASK 21-26-802, MESSAGE SHOWED LATCHED, PERFORMED ECS BULK CARGO SYSTEM TEST AND TEST PASSED, MESSAGE UNLATCHED AND CLEARED AFTER TEST. BULK CARGO HEAT TEST ALSO PASS. FAN OPS TEST ALSO PASSED.

Part: MODULE — FAULTY (CABIN LIGHTS) · airframe 66,801 hrs · 9,452 cycles

UNABLE TO CONTROL ZONE CABIN LIGHTING. SWAPPED ZMU NR 1 WITH ZMU NR 3 PER AMM, OK.

Part: OVEN — DIRTY (GALLEY) · airframe 66,581 hrs · 9,428 cycles

BURNING ODOR 2R, NO SMOKE. FOUND PLASTIC BUGS BURNT IN WARMING OVEN W31 CAUSED BURNING ODOR IN THE DOOR 2 AREA. REMOVED BUGS FROM OVEN. NEED TO CLEAN DEBRIS IN THE OVEN OR REPLACE ITSELF. CONSULTED WITH TOMC AND DEACTIVATED W31 OVEN PER MEL PROC. CREW ALSO CONFIRMED THE SITUATION AND READY TO FLIGHT. CLEANED W31 WARMER OVEN AND INSTALLED OVEN RACK ASY., OP'S CK W31. NO SMELL NOTED ON GROUND.

Part: OVEN — DIRTY (GALLEY) · airframe 66,587 hrs · 9,429 cycles

BURNING ODOR 2R. NO SMOKE. ITEM ROLLED FORWARD. FOUND PLASTIC BUGS BURNT IN WARMING OVEN W31 CAUSED BURNING ODOR IN THE DOOR 2 AREA. REMOVED BUGS FROM OVEN. NEED TO CLEAN DEBRIS IN THE OVEN OR REPLACE ITSELF. CONSULTED WITH TOMC AND DE-ACTIVATED W31 OVEN PER MEL PROC. CREW ALSO CONFIRMED THE SITUATION AND READY TO FLIGHT: CLEANED W31 WARMER OVEN AND INSTALLED OVEN RACK ASSY., OP'S CK W31 NO SMELL NOTED ON GROUND.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 66,448 hrs · 9,405 cycles

FLOORBOARD IN FRONT OF LAV 131 IS SPONGY. REPLACED FLOOR PANEL REF SFOOV WRITE UP B3260X.

Part: TOILET — ODOR (LAVATORY) · airframe 66,443 hrs · 9,404 cycles

DOOR 3 LAV ODOR. REPEAT FOUL STENCH FROM AREA OF DR 3 LAVS. FLT 804-27 REPORTS CROSS AISLE FLOOR BETWEEN LAVS AT DOOR 3 IS WET. NEED TO REMOVE TOILET SHROUDS IN LAVS 131 AND 133. CLEAN AREA, INSPECT WASTE LINES BENEATH TOILET ASSEMBLIES INCLUDING RMVL OF CEILING PNLS IN THE AFT PIT. REPLACED BOTH TOILETS, NO LEAKS OPS CHECKED NORMAL.

Part: PSEU — FAULTY (NLG) · airframe 66,386 hrs · 9,395 cycles

STATUS R GEAR DOOR SENSOR. NOSE GEAR UP SENSOR+NOSE GEAR DOOR SENSOR. CMC MSG 1 TO 9 ARE SAME REASON. REPLACED PSEU PER MM. GROUND TEST PASS ALL MSG WAS DISAPPEAR. ALL TEST WITH HYD PRESSURE. NO HYD LEAK FOUND.

Part: HEAT SHIELD — WORN (NR 1 NACELLE) · airframe 66,273 hrs · 9,384 cycles

FOUND NR 1 HEAT SHIELD GAP COVER WORN INTO HEAT SHIELD I/B EDGE AND NR 2 GAP COVER O/B EDGE WORN INTO HEAT SHIELD. REPLACED HEAT SHIELD ASSY.

Part: MODULE — FAULTY (GEAR HANDLE) · airframe 66,230 hrs · 9,380 cycles

ON TAKEOFF GEAR HANDLE WOULDN'T RAISE FOR SEVERAL SECONDS.RAISED ON 3RD REPLACED ALT BRAKE PRESS TRANSDUCER M32225 PER FIM AND REPLACED LANDING GEAR HANDLE MODULE. ALL OPS CHECKS OKAY.

Part: SEAL — LEAKING (LT WING) · airframe 66,141 hrs · 9,372 cycles

FOUND FUEL SEEPAGE UNDER LT WING NR 6 DRIPSTICK PANEL. NO REPAIR PROCEDURE IS NECESSARY, EXAMINE THE FUEL LEAK FREQ TO MAKE SURE IT DOES NOT GET LARGER PER MM. REPLACED SEAL ON NR 6 FUEL STICK PANEL. LT MAIN FUEL TANK. LEAK CHECKS GOOD.

Part: CARPET — DIRTY (CABIN) · airframe 66,117 hrs · 9,370 cycles

CARPET BETWEEN DOORS 3L & 3R SMELLS BAD. CLEANED AND SPRAYED CARPET, CARPET AT LAV AREA NEEDS REPLACEMENT, SEE HISTORY FOR PARTS INFORMATION. CARPET UNABLE TO CLEAN WILL NEED NEW CARPET PCN 025-7129 REF IPC 25-27-01-010Y ITEM 90 PART NOT STOCK. PLEASE ATTEMPT TO REPAIR IF UNABLE PLEASE ASSURE PART IS LOB. LOCAL CLEANING UNSUCESSFUL. STILL SMELLS. NO CARPET LOB. REPLACED CARPET.

Part: PLATE — LOOSE (LT MAIN TANK) · airframe 65,947 hrs · 9,342 cycles

TANK ACCESS PANEL FOR MEASURING STICK LEFT MAIN TANK SEEPING FUEL. RETORQUED PLATE ASSY PER AMM. SYSTEM LEAK CHECKED OKAY.

Part: WARNING MESSAGE — MULTIPLE FAIL · airframe 65,656 hrs · 9,313 cycles

EPR INDICATION (ENGINE) - BLANK MSG01- ACTIVE CRUISE MODE DEPENDENT; PROBE HEAT (L ENG) POWER IS NOT AVAILABLE. DB- ELECTRONIC ENGINE CONTROL (L ENG, CH A) MSG-7361011 ACTIVE ER MODE. ACCCOMPLISHED PROBE HEAT TEST PER FIM 77-11-812 AND FAILED. FOUND 115V AT DM73005A. RESISTANCE AT D71028J 12.3 OHMES. CHECKED FOR SHORTS TO GROUND AND NONE FOUND. CHECKED CONTINUITY THROUGH PLUGS DM73005F TO D71028P AND GOOD AND NO SHORTS. PROBE HEATS DURING TEST, SUSPECT ERU AT FAULT.

Part: CASTING — DAMAGED (NR 1 NACELLE) · airframe 65,326 hrs · 9,265 cycles

NR 1 PYLON AFT FAIRING HEAT SHIELD PAN CASTING AND ITS SEAL RETAINER PN 313W3807-4 WERE FOUND WITH ELONGATED FASTENER HOLE.

Part: HEAT SHIELD — WORN (NR 2 NACELLE) · airframe 65,545 hrs · 9,300 cycles

NR 2 ENG NR 5 HEAT SHIELD HAS WEAR. REPLACED NR 5 HEAT SHIELD.

Part: HEAT SHIELD — WORN (NR 2 NACELLE) · airframe 65,545 hrs · 9,300 cycles

NR 2 ENG NR 3 HEAT SHIELD HAS WEAR. REPLACED HEAT SHIELD SEGMENTS NR 3.

Part: HEAT SHIELD — WORN (NR 2 NACELLE) · airframe 65,545 hrs · 9,300 cycles

NR 2 ENG NR 4 HEAT SHIELD HAS WEAR. REPLACED HEAD SHIELD NR 4.

Part: HEAT SHIELD — WORN (NR 2 NACELLE) · airframe 65,545 hrs · 9,300 cycles

NR 2 ENG NR 2 HEAT SHIELD HAS WEAR. REPLACED HEAT SHIELD SEGMENTS NR 2.

Part: BPU — FAILED (SATCOM) · airframe 65,332 hrs · 9,268 cycles

SATCOM HIGH GAIN FAILED. CHECKED WIRES, NO FAULTS. REPLACED WITH SERVICEABLE LT AND RT BSU AND INSTALLED, TEST OK.

Part: SWITCH — FAULTED (HYD PUMP) · airframe 65,331 hrs · 9,267 cycles

RIGHT HYDRAULIC ENGINE DRIVEN PUMP SOMETIMES WILL NOT DEPRESSURIZE IN FLIGHT. WORKED OK ON GROUND. HYD SYNOPTIC SHOWED EDP SWITCH OFF BUT SYSTEM DID NOT DEPRESSURIZE, SAME RESULT WITH FIRE HANDLE ON LAST FLIGHT. REPLACED WITH NEW SWITCH, TESTED OKAY. CHECKED WIRING AND CHECKED NORMAL. SWAPPED THE LEFT HYDIM CARD AND RIGHT HYDIM CARD & INSTALLATION TEST OKAY.

Part: PAN — DAMAGED (NR 1 PYLON) · airframe 65,326 hrs · 9,265 cycles

NR 1 PYLON AFT FAIRING HEAT SHIELD PAN CASTING NR 1 P/N 313W3821-1 AND ITS SEAL RETAINER PN 313W3807-4 WERE FOUND WITH ELONGATED FASTENER HOLE (1 EACH). REF: AD 2006-19-12. REPAIRED IAW ENGINEERING 777EN-54-0047. ACCOMPLISH OVER-AGING OF HEAT SHIELD PAN CASTING IAW PAGE 1 OF ATTACHMENT BEFORE 26 MAY, 2012. TEXT INCOMPLETE, SEE EVA 81555.

Part: FASTENER — MISSING (NR 1 STRUT) · airframe 65,326 hrs · 9,265 cycles

NR 1 ENG AFT STRUT LOWER FWD HEAT SHIELD FASTENER MISSING (5TH FROM INBD SIDE). INSTALLED MISSING FASTENER REF 777MT 54-UA1. REQUIRES RECHECK AT 3SV AN D REPLACEMENT AT C-CHECK PERMANENT REPAIR WAS MADE BY INSTALLING NEW BOLTS PER 777 MT 54-UA1.

Part: SKIN — DENTED (R4 DOOR) · airframe 65,326 hrs · 9,265 cycles

R4 DOOR HAS A SHALLOW 7 INCH LONG CREASE 4 INCHES FROM AFT EDGE AND 24 FROM BOTTOM. REF FIGURE SRM 52-10-01 PG1 11 FIGURE 103. DAMAGE FOUND TO BE IN AREA B OF FIGURE 103. THE DAMAGE IS DIRECTLY BELOW WINDOW CUTOUT, IN CHEM-MILLED .050 AREA. DEPTH DOES NOT EXCEED 0.014. PERFORMED HFEC, NO CRACKS.

Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 65,326 hrs · 9,265 cycles

LEFT WING REAR SPAR WEB CORRODED BETWEEN IRSS 340 AND 350 AT FUEL PUMP. REMOVED CORROSION, AREA CRACK FREE BY HFEC. FLAP PEENED AREA & AND RESTORED FINISH PER 777EN-57-0219 AND FAA FORM 8100-9.

Part: WIRE — CHAFED (RT WING) · airframe 65,326 hrs · 9,265 cycles

ELECRICAL WIRE CHAFING ON STRINGER RT WING DRY BAY WS 1217 STR L13 JUST FWD OF TANK ACCESS. FIBER SHEATH AND BRAIDED WIRE CONDUIT WORN THROUGH, INNER CONDUIT IS INTACT AND NO VISIBLE DAMAGE TO ELECTRICAL INSULATION OR WIRE. WEAR ON UPPER AFT EDGE OF STRINGER APPROX 0.2' X 0.25'. BLENDED AREA, SHOT PEENED & VERIFIED NO CRACKS BY HFEC. RESTORED FINISH. PER AMECO EN UAL 777EN-57-0220 & BOEING RDR AOJ-UAL-11-0213-04B.

Part: SPAR — CORRODED (RT WING) · corrosion level 2 · airframe 65,326 hrs · 9,265 cycles

RIGHT WING REAR SPAR WEB CORRODED BETWEEN IRSS 340 AND 350 AT FUEL BOOST PUMP. REMOVED CORROSION, AREA CRACK FREE BY HFEC. FLAP PEENED AREA, RESTORED FINISH PER 777EN-57-0218 AND FAA FORM 8100-9.

Part: BOLT — SHEARED (CARGO DOOR) · airframe 65,001 hrs · 9,232 cycles

FOUND FWD CARGO LWR SENSOR BOLTS SHEARED OFF. REPLACED SHEARED BOLTS AND OPS CHECK FWD CARGO DOOR SEVERAL TIMES. VERIFIED ALL INDICATIONS NORMAL.

Part: SDU — FAULTY (SATCOM) · airframe 64,556 hrs · 9,182 cycles

SATCOM VOICE VOICE PORTION OF SATCOM FAILS. ADVISORY MSG06- NOT ACTIVE CRUISE INTERMITTENT; SATELLITE DATA UNIT (LEFT) HAS NO OUTPUT ON DATA TO CMU BUS (429). DB- LEFT AIMS MSG-2360121 ACTIVE ER INTER MSG-2360121 ACTIVE ER HARD MSG-2360131 ACTIVE ER HARD MSG-2360131 ACTIVE ER HARD MSG-2360041 INACTV ER INTER MSG-2368893 INACTV ER INTER. REPLACED SDU PER MM. VOICE & DATA TESTED NORMAL ON GRD.

Part: SDU — MALFUNCTIONED (SATCOM) · airframe 64,536 hrs · 9,180 cycles

CHRONIC SATCOM HI GAIN STATUS, HAS AT LEAST 2 PREVIOUS HITS AND STATUS MSG HAPPENED ABOUT 20 TIMES. COMPLIED WITH REQUIREMENTS IN MEL 2315B. REPLACED SATCOM SDU, OPS CHECK GOOD.

Part: DIPLEXER — FAULTY (SATCOM) · airframe 64,536 hrs · 9,180 cycles

DURING TEST FOR SATCOM SDU REPLACE MAT TEST FAILS LO NOISE AMP-DIPLEXER FOR THE LGA. REPLACED REF AMM. SATCOM TESTS GOOD.

Part: LIFE VEST — IMPROPER PART (CABIN) · airframe 64,450 hrs · 9,172 cycles

NUMEROUS SPARE INFANT LIFE VESTS FOUND ON ACFT AS INCORRECT EFFECTIVITY. REPLACED WITH CORRECT EFFECTIVITY PCN 649-0029 (P/N S71850-6400UAL138).

Part: BATTERY — DISCHARGED (R1 DOOR) · airframe 64,020 hrs · 9,131 cycles

EPAS LIGHT NOT FLASHING DOOR 1R. REPLACED BATTERIES, OPS NORMAL.

Part: CONNECTOR — DAMAGED (IDG) · airframe 63,697 hrs · 9,098 cycles

NR 2 ENG IDG INBOARD BACKSHELL (DM24001A) LOOSE. SECURED LOOSE BACKSHELL.

Part: PCU — LEAKING (RUDDER) · airframe 63,697 hrs · 9,098 cycles

CENTER RUDDER PCU LEAKING HYD FLUID BEYOND MM LIMITS. RUDDER PCU LEAKING HYD FLUID. NEW ONE PLANESIDE, REMOVING. DDK 0835. AS A RESULT OF ACT LOCK INSTALLED, RUDDER DEFLECTED ON PCU LOCK AND DAMAGED SEAL. CENTER PCU. REMOVED CENTER PCU, ACCOMPLISHED DETAILED VISUAL INSPECTION OF CENTER RUDDER ACTUATOR MOUNT POINTS AND ADJACENT STRUCTURE. NO DEFECTS NOTED.

Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 63,176 hrs · 9,044 cycles

FWD CARGO DOOR AFT LOWER CORNER HAS DAMAGE. DAMAGE IS (12 INCHES LONG) WITH SEVERAL RIVET HEADS POPPED. REPAIRED CARGO DOOR DAMAGE & REPLACED DAMAGED FASTENERS PER SRM. NDT COMPLETE, NO CRACKS NOTED. ACCOMPLISHED INSPECTION OF REPAIR, CHECKED OKAY.

Part: SKIN — GOUGED (FUSELAGE) · airframe 62,594 hrs · 8,976 cycles

RAMP REPORTED DAMAGE TO ACFT ONE INCH FWD OF FWD CARGO DOOR BELOW CTR LINE IT APPEARS TO BE A PUNCTURE. DAMAGE IS A GOUGE NOT A PUNCTURE AND IS .375 INCH IN DIAMETER LOCATED .50 INCH FWD OF FWD PIT DOOR ON FUSELAGE SKIN. SKIN THICKNESS IS .200 INCH & DAMAGE IS .056 INCH DEEP, BEYOND ALLOWABLE LIMITS. BLENDED AREA & ACP HFEC INSPECTION, NO CRACKS DETECTED. TREATED & PRIMED. STARTED RPR. RECEIVED FILLER MATERIAL FROM EWR. ALL MATERIAL IS ON HAND. TRIPLER, DOUBLER, AND FILLER HAVE BEEN FABRICATED. INSTALLED REPAIR REF SRM.

Part: IDG — FAILED (RIGHT) · airframe 62,486 hrs · 8,965 cycles

ELECTRICAL GENERATOR SYS RT IDG HAS DISCONNECTED OR A PROTECTIVE TRIP OF THE GENERATOR CONTROL BREAKER HAS OCCURRED OR A PROTECTIVE TRIP OF THE BTB HAS OCCURRED. ELECT GEN OFF RT EICAS MSG AT ENGINE START. RIGHT IDG INOPERATIVE. TRIED SWAPPING GCU 1 AND 2 PER MM, NO HELP STILL HITTING GENERATOR RETURNED GCU 1 AND 2 TO ORIGINAL POSITIONS. REMOVED NR 2 ENG IDG. REPLACED RT IDG PER MM, OPS CHECK NORMAL.

Part: UNKNOWN — SMOKE (BUNKROOM) · airframe 62,449 hrs · 8,961 cycles

CREW REPORT: SMOKE AT LL BUNKROOM AREA. SAMC TEXT: CREW REPORTED THAT THERE WAS A BURNING SMELL AND THAT F/A'S SAW SMOKE. SMOKE CREW REST LWR MSG ON EICAS. UPON RETURN TO GATE, MAINTENANCE WENT ON BOARD AND DOWN INTO THE CREW REST AREA, NO EVIDENCE OF SMOKE WAS SEEN OR BURN SMELL WAS NOTED. EICAS MESSAGE WAS PRESENT IN UPPER EICAS. CHK'D BOTH LLAR HEATERS FOR DEBRIS. CLEANED, REPLACED K26001 IN P110 & LLAR SMOKE DETECTOR, GROUNND TEST CKD OK, RAN BOTH ENGS 5 MINS WITH PKS ON & ISLOLATED, NO FAULTS. EICAS MESSAGE WAS PRESENT IN UPPER EICAS. CHKD BOTH LLAR HEATERS FOR DEBRIS - CLEAN, RPLCD K26001 IN P110 & LLAR SMOKE DETECTOR REF AMM, GND TEST CHECKED OKAY, RAN BOTH ENGS 5 MINS WITH PKS ON & ISOLATED, NO FAULTS.

Part: BATTERY — FAULTY (RIGHT) · airframe 62,392 hrs · 8,953 cycles

FLIGHT CONTROL SYS STATUS MSG WITH ACTIVE MAINTENANCE MSG 24-50242 FCDC BATT RIGHT VOLTAGE IS LOW. THE RIGHT FCDC BATTERY WAS SWAPPED WITH THE LEFT. THE LEFT BATTERY WILL NEED REPLACEMENT. FCDC L BATTERY REPLACED AS PER AMM, TEST CARRIED OUT AS PER AMM, TESTS OKAY.

Part: SHUTOFF VALVE — FAILED · airframe 61,185 hrs · 8,811 cycles

TRIM AIR PRSOV R RIGHT TRIM AIR PRESSURE RELIEF SHUTOFF VALVE (PRSOV) FAILED. STATUS MSG01- ACTIVE CLIMB MODE DEPENDENT; TRIM AIR PRESSURE REGULATING AND SOV (RIGHT) TORQUE MOTOR IS NOT IN COMMANDED POSITION. DB- CABIN TEMPERATURE CONTROLLER (R CHAN2) ITEM CNX PER PLF SHOWS NOT ACTIVE MSG-2124202 ACTIVE CL MODE. REPLACED RIGHT TRIM AIR REG VALVE V21622 PER AMM, OPS CHECK NORMAL.

Part: SHUTOFF VALVE — FAILED · airframe 61,180 hrs · 8,810 cycles

TRIM AIR PRSOV R RIGHT TRIM AIR PRESSURE RELIEF SHUTOFF VALVE (PRSOV) FAILED. STATUS MSG01- ACTIVE CLIMB MODE DEPENDENT; TRIM AIR PRESSURE REGULATING AND SOV (RIGHT) TORQUE MOTOR IS NOT IN COMMANDED POSITION. DB- CABIN TEMPERATURE CONTROLLER (R CHAN2) ITEM CNX PER PLF SHOWS NOT ACTIVE MSG-2124202 ACTIVE CL MODE. MAT TEST RT SYS AIR ON FAILED FOUND RT TRIM AIR PRSOV U-S MEL APPLY RT TRIM PRSOV DE-ACTIVATED CLOSED. REPLACED VALVE.

Part: SHUTOFF VALVE — FAILED · airframe 61,180 hrs · 8,810 cycles

TRIM AIR PRSOV R RIGHT TRIM AIR PRESSURE RELIEF SHUTOFF VALVE (PRSOV) FAILED. STATUS MSG01- ACTIVE CLIMB MODE DEPENDENT; TRIM AIR PRESSURE REGULATING AND SOV (RIGHT) TORQUE MOTOR IS NOT IN COMMANDED POSITION. DB- CABIN TEMPERATURE CONTROLLER (R CHAN2) ITEM CNX PER PLF SHOWS NOT ACTIVE MSG-2124202 ACTIVE CL MODE. MAT TEST RT SYS AIR ON FAILED FOUND RT TRIM AIR PRSOV U-S MEL APPLY RT TRIM PRSOV DE-ACTIVATED CLOSED. REPLACED VALVE PER MM.

Part: AMPLIFIER — MALFUNCTIONED (SATCOM) · airframe 61,180 hrs · 8,810 cycles

SATCOM HGA HPA NEEDS REPLACEMENT. DUE TO REPORTS OF 'SATCOM VOICE' AND 'SATCOM HI GAIN' STATUS MESSAGES WITH CORRELATED MMSG 23-60121, PLZ REPLACE HGA HPA (M23108) (PCN 580-9103) REF MM. UNIT MR23808-92 INSTALLED ON 03JAN11 WAS OBTAINED FROM STOCK TO REPLACE UNIT MR23808-142 ROBBED FOR AIRCRAFT 2629. THERE WERE NO FAILURE MESSAGES PRIOR TO THIS UNIT BEING INSTALLED. ATTACH RFU TAG TO REMOVED UNIT AND SEND TO SFOEG. BAD FROM STOCK RFU NR 220330.

Part: ENGINE — FIRE (APU) · airframe 61,180 hrs · 8,810 cycles

FIRE COMING OUT OF APU EXHAUST REPORTED BY RAMP. SHUT DOWN APU, SMALL FIRE STILL BURNING AT EXHAUST CONE, APPEARED WET WITH OIL. DISCHARGED DRY CHEMICAL EXTINGUISHER DOWN TAILPIPE. MAT REPORTS HIGH EGT WITH APU RUNNING. LOOKED IN TAIL PIPE. T WHEEL TORN UP. REPLACED APU. CLEANED TAIL PIPE IAW MM.

Part: ANTI-ICE VALVE — FAULTY (LEFT) · airframe 60,926 hrs · 8,786 cycles

REPLACED LT M WING ANTI-ICE VALVE IAW MM & CTR AIRFOIL & COWL ICE PROTECTION SYS CARD IAW MM. MESSAGE CLEARED.

Part: CONTROL VALVE — MALFUNCTIONED (LT A/C PACK) · airframe 60,902 hrs · 8,784 cycles

LIGHT HAZE IN COCKPIT, RTFL. LEFT PACK FLOW CONTROL VALVE'S INOP PER CMC DOWNLOADED FAULTS. PER FIM MANUAL REPLACED LEFT PACK ASCPC COMPRESSOR DISCHARGE SENSOR AND PACK TESTS OK. NO LONGER HAZE OR NEW ODORS.

Part: FAN — FAULTY (CABIN) · airframe 60,105 hrs · 8,699 cycles

BURNING ODOR IN CABIN, FLT DIVERTED. INSPECTED CABIN FOR SOURCE, RAN ENG ENGS AND PACKS, OPERATED RECIRC AND GASPER FANS, OPERATED LIGHTS, CHECKED LAVS AND LOWER LOBE. CHECKED CARGO BULK VENT FAN AN D E&E. DEFERRED ENG CARGO VENT FAN. NO OTHER DEFECTS FOUND. REPLACED CARGO VENT FAN. OPS GOOD.

Part: CONTROLLER — FAULTY (CABIN TEMP) · airframe 59,618 hrs · 8,628 cycles

CABIN TEMP IN 1ST CLASS HARD TO CONTROL WHEN SET AT 75 DEGS. IT IS TOO COLD WHEN SET AT 76 DEGS IT GETS TOO HOT. REPLACED CABIN TEMP CONTR. OPS TEST PASSED.

Part: FAN — FAULTY (RECIRCULATION) · airframe 59,579 hrs · 8,624 cycles

MELTING PLASTIC SMELL WAFTS OCCUR FROM BUSINESS CLASS GALLEY OVERHEAD FWD. SPORADIC BURNING ODOR PERSIST, SUSPECT UPPER RECIRCULATION FAN PROBLEM. PREVIOUS HISTORY. IN REF TO BUSINESS GALLEY ODOR UPPER RECIRCULATION FANS HAVE BEEN OFF FOR ABOUT 1.5HRS BUT THE BURNING PLASTIC ODOR IS BACK BUT STILL IN SMALL AMOUNTS. DEACTIVATED FWD UPPER RECIRCULATION FAN. BREAKER PULLED AND COLLARED AT P110 POSITION A21. REPLACED UPPER FWD RECIRCULATION FAN, OPS CHECK GOOD.

Part: LUBRICATION UNIT — MALFUNCTIONED (APU) · airframe 59,535 hrs · 8,619 cycles

APU APUC DETECTED FAULT THAT WOULD CAUSE AUTOMATIC SHUTDOWN OF APU IN UNATTENDED MODE OPS, OR COMPLETE LOSS OF APUC BUSS ACTIVITY (BOTH LT AND RT 629) FOR 3 SECONDS AFTER THE APU MASTER CONTROL SWITCH HAS BEEN IN THE ON POSITION FOR TEN SECONDS. STATUS MSG-4910270 INACTIVE TA MODE. MAG PLUGS WERE CHECKED PER MM AND NO SILVER METAL FOUND. SEVERAL SMALL NON SILVER PARTICLES FOUND ON TURB BEARING PLUG AND TWO SMALL NON SILVER PARTICLES ON MAIN PLUG, NOTHING FOUND ON MID BEARING. GEN PLUG NOT CHECKED. WHEN TRIED STARTING APU AFTER TROUBLESHOOTING OIL PRESSURE STAYED AT 1 AND OIL QTY DID NOT DROP, SUSPECT LUBE CLUSTER. REPLACED APUC AND LUBE CLUSTER. OPERATIONS CHECK NORMAL.

Part: PIN — BENT (CONNECTOR) · airframe 57,946 hrs · 8,411 cycles

PACK FCV L DISPLAYED ON STATUS PAGE RESET AND RE-APPEARS. DEF PER MEL DUE TIME AND NO PART AVAIL AT FRA. REPLACED UPPER LEFT PACK FCV. RAN TEST FAULTED L ECONO COOLING VLV CNTL FOUND BREAKER H23 POPPED ON P110 PANEL. (2) ALREADY REPLACED RELAY K21009 AND BREAKER C21 645, NO HELP. UPPER FLOW CONTROL VALVE MR21563 DASH ON 25 DASH OFF 145. ALREADY REPLACED RELAY K21009 AND BREAKER C21 645, NO HELP. TROUBLESHOTING FOUND BENT PIN ON CANNON PLUG AT UPPER FLOW CONTROL VALVE, WAS ABLE TO STRAIGHTEN. NO MORE POPPED BREAKER. NO MESSAGES NOTED. PACK OPS NORMAL.

Part: CONTROL VALVE — FAULTY (RT A/C PACK) · airframe 57,027 hrs · 8,277 cycles

RIGHT PACK FCV FAULTS. TRIED NEW PACK VALVE, NO HELP. NEW CONTROLLER AND SOFTWARE NO HELP. NEED MORE TIME TO T/S. CTC TO FCV INTERFACE CHECK SHOWS NO VOLTAGE ON PIN 1 AND 2 OF DV21512B. NEEDS FURTHER TROUBLESHOOTING. FOUND VOLTAGE BETWEEN PINS 1 AND 2 AT CONNECTOR DV21512B WITH SWITCH IN OFF AND AUTO POSITION. REPLACED UPPER FCV. OPS AND LEAK CHECKS OK. NO MESSAGES. NO FAULT FOUND ON LAST 3 LEGS, PACK OPS SUCCESSFUL.

Part: OXYGEN SYSTEM — LEAKING (CREW) · airframe 55,313 hrs · 8,039 cycles

CREW OXYGEN LOW. STATUS PAGE SHOWS 500. ACCOMPLISHED LEAK CHECK OF CREW OXYGEN SYSTEM AND FOUND F/O'S MASK STOWAGE BOX LEAKING INTERNALLY. REPLACED STOWAGE BOX.

Part: LIGHT — BROKEN (SEAT 18G) · airframe 55,274 hrs · 8,035 cycles

EMERGENCY PATH LIGHT AT 18G BROKEN. REPLACED ASSY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,593 hrs · 7,954 cycles

EMERGENCY EXIT LIGHT INOP AT SEAT 39 LEFT. RELAMPED, OPS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,645 hrs · 7,830 cycles

FWD EMERGENCY LIGHT IS INOP ON SEAT 8F. RELAMPED, LIGHTING TEST OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,645 hrs · 7,830 cycles

EMERGENCY LIGHT AT SEAT 21D IS INOP. RELAMPED, LIGHT CHECK OK.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 53,291 hrs · 7,786 cycles

SMOKE DETECTED DISPLAYED ON F-A PANEL AT 1L. NO SMOKE, ALL LAVS CHECKED. ACCOMPLISHED LAV SMOKE DETECTION TEST, NO FAULTS FOUND. ALL LAV SMOKE DETECTORS, OP OK.

Part: MODULATING VALVE — FAULTY (BLEED AIR SYS) · airframe 53,060 hrs · 7,751 cycles

LEFT ENGINE BLEED FAN AIR MODULATING VALVE (FAMV) FAILED OPEN OR CLOSED OR LEFT AIR SUPPLY AND CABIN PRESSURE CONTROLLER FAILURE. STATUS MSG-3610531 LATCHED ER MODE MSG-3610531 LATCHED ER MODE, MSG-3610200 ACTIVE CL MODE MSG-3610200 ACTIVE CL MODE. *S/D* REMOVED FAMV FOR NR 1 ENGINE. REPLACED FAMV ON NR 1 ENGINE.

Part: MODULATING VALVE — FAILED (BLEED AIR SYS) · airframe 53,060 hrs · 7,751 cycles

BLEED FAMV L LEFT ENGINE BLEED FAN AIR MODULATING VALVE (FAMV) FAILED OPEN OR CLOSED OR LEFT AIR SUPPLY AND CABIN PRESSURE CONTROLLER FAILURE. STATUS MSG-3610531 LATCHED ER MODE MSG-3610531 LATCHED ER MODE MSG-3610200 ACTIVE CL MODE MSG-3610200 ACTIVE CL MODE. REMOVED FAMV FOR NR 1 ENGINE. REPLACED FAMV ON NR 1 ENGINE.

Part: GIRT BAR — OUT OF ADJUST (R4 DOOR) · airframe 52,238 hrs · 7,647 cycles

MED 4R BINDING DOES NOT OPEN. REMOVED SLIDE BUSTLE FOR ACCESS. ADJUSTED GIRTBAR, DOOR 4R OPENS AND CLOSE NORMAL. SLIDE ARM AND DISARM WITH NO PROBLEM. SECURED BUSTLE.

Part: FILTER — DIRTY (FWD CARGO BAY) · airframe 51,803 hrs · 7,593 cycles

ALL FLIGHT ATTENDANTS FROM BUSS CLASS AFT REPORT STALE STUFFY AIR QUALITY SAMC TEXT: FLT CREW REPORTED MORE THAN 10 F/A'S FELL ILL WITH EFFECTS OF DIZZINESS AND LIGHTHEADED. ONE FLT CREW FELT SAME EFFECTS WHEN TRAVELED TO BACK OF CABIN. F/A'S FROM MID CABIN FELT ILL FIRST AND THEN AFT CABIN F/A'S. ALL FELT BETTER AFTER USING PORTABLE O2. REPLACED 4 EA RECIRC FAN FILTERS IN FWD PIT.

Part: FILTER — UNKNOWN (FWD CARGO BAY) · airframe 51,803 hrs · 7,593 cycles

ALL FLIGHT ATTENDANTS FROM BUS CLASS AFT REPORT STALE STUFFY AIR QUALITY. FLT CREW REPORTED MORE THAN 10 F/A'S FELL ILL WITH EFFECTS OF DIZZINESS AND LIGHTHEADED. ONE FLT CREW FELT SAME EFFECTS WHEN TRAVELING TO BACK OF CABIN. F/A'S FROM MID CABIN FELT ILL FIRST AND THEN AFT CABIN F/A'S. THEY ALL FELT BETTER AFTER USING PORTABLE O2. REPLACED 4 EA RECIRC FAN FILTERS IN FWD PIT.

Part: START VALVE — FAULTY (NR 1 ENGINE) · airframe 50,633 hrs · 7,445 cycles

ENG START VALVE L LEFT STARTER AIR VALVE POSITION DISAGREES WITH COMMANDED POSITION OR STARTER AIR VALVE POSITION INDICATION IS LOST. STATUS MSG01- NOT ACTIVE ENGINE SHUTDOWN MODE DEPENDENT; STARTER AIR VALVE (SAV) (L ENG) IS NOT IN COMMANDED POSITION. *S/D* FOUND FAULTY STARTER VALVE. REPLACED STARTER PER MM 80-11-01, OP CHECK GOOD. AC OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,756 hrs · 7,344 cycles

PED 1L EPAS BATTERY PACK GREEN TEST LIGHTS INOP. *S/D* SUSPECT FAULTY BATTERY. REPLACED 9V BATTERIES IAW MM 52-11-20. AC OK FOR SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 49,409 hrs · 7,303 cycles

AFT SECTION OF EEL STRIP ON SEAT 1F INOP. SUSPECT LOOSE CONNECTION. SECURED CONNECTION OP CHECKED GOOD. AC OK FOR SERVICE.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 49,409 hrs · 7,303 cycles

EMERGENCY AISLE LIGHT IS MISSING LENS ON SEAT 1E. LENS MISSING ON SEAT 2E. SUSPECT FAULTY LIGHT ASSEMBLY. REPLACED 1E EEL LIGHT AND OPS NORMAL. SEAT 2E ALSO TESTS NORMAL. ACFT OK FOR SERVICE.

Part: PANEL — PUNCTURED (T/E FLAP) · airframe 63,507 hrs · 10,432 cycles

OUTBOARD PANEL, ABOVE T/E FLAP PUNCTURED FROM FLAP GUIDE TRACK. SUSPECT FLAP TRACK SNAPPED. REMOVED PANEL AND ROUTED TO SHOP ON R & R NR R16520. REINSTALLED PANEL. ACFT OK FOR SERVICE.

Part: STARTER — FAULTY (APU) · airframe 47,715 hrs · 7,112 cycles

APU APUC DETECTED FAULT THAT WOULD CAUSE AUTOMATIC SHUTDOWN OF APU IN UNATTENDED MODE OPERATION, OR COMPLETE LOSS OF APUC BUSS ACTIVITY (BOTH L AND R 629) FOR 3 SECONDS AFTER THE APU MASTER CONTROL SWITCH HAS BEEN IN THE ON POSITION FOR TEN APU CONTROLLER DETECTED FAULT THAT WOULD CAUSE AUTOMATIC SHUTDOWN OF APU IN UNATTENDED MODE OPERATION, OR COMPLETE LOSS OF APUC BUSS ACTIVITY. REPLACED FAILING ELECTRIC START MOTOR. APU STARTED. NO APUC MESSAGE.

Part: ANTI-ICE VALVE — FAULTY (RT WING) · airframe 46,839 hrs · 7,006 cycles

ICING WING PRIMARY ICE DETECTION SYSTEM (LEFT OR RIGHT ICE DETECTORS) DETECTS ICE, AND THE WING ANTI-ICING (WAI) SWITCH IS OFF. *S/D* REPLACED RIGHT WING ANTI-ICE VALVE PER MM 30-11-03 & ACCOMPLISHED OPS CHECKS PER MM 30-11-00, ALL OPS & INDICATIONS NOW NORMAL.

Part: WIRE — DAMAGED (NLG) · airframe 46,758 hrs · 6,997 cycles

NLG RED SAFETY LIGHT WILL NOT ILLUMINATE WHEN PTT SWITCH IS CLOSED. ALSO, WHEN CLOSING MLG AND NLG DOORS FROM GROUND CIRCUIT BREAKER IN COCKPIT FOR SAFETY VALVE TRIPS. SUSPECT BROKEN WIRE. REPAIRED WIRE IN LT MAIN WHEEL WELL. CLEANED LIGHT SOCKET IN NOSE WHEEL WELL. ACCOMPLISHED LAMP TEST AND OPERATED DOORS, OPS CKS NORMAL. AC OK FOR SERVICE

Part: LIGHT — INOPERATIVE (SEATS 17G, 9F FW) · airframe 43,980 hrs · 6,620 cycles

EMERGENCY LIGHTS INOP AT SEATS 17G, 9F FWD LT & 2F AFT LT. REPLACED EEL LIGHT ASSY'S AT SEATS 17G, 9F-FWD LT, & SEAT 2F-AFT LT. ALL POSITIONS OP CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,980 hrs · 6,620 cycles

DOOR 1L EPAS BATTERY PACK TEST LIGHT IS INOPERATIVE. REPLACED BOTH EPAS 9 VOLT BACKUP BATTERIES AT DOOR 1L AFTER REPL ACEMENT OF DOOR 1L EPAS BATTERY PACK, EPAS TESTED OK. A/C RETURNED TO SERVICE.

Part: LIGHT — DAMAGED (SEAT 1E) · airframe 39,672 hrs · 5,996 cycles

EMERGENCY EXIT LIGHTS DAMAGED AT 1E.

Part: FLT CONTROLS — MALFUNCTIONED (RUDDER) · airframe 37,619 hrs · 5,687 cycles

THREE UNCOMMANDED RUDDER MOVEMENTS ON APPROACH. MECHANICS PERFORMED CAT3 CHECKS PER AMM 22-11-00 PG 501, AMM 22-31-00 AND RUDDER ACTUATOR CONFIDENCE CHECK ON MAT, ALL OPS CHECKS NORMAL. ENGINEERING REVIEWED MAINTENANCE RECORDS AND DOWN LINKED CMC FAULT DATA FOR FLIGHT 958. THERE WERE NO REPORTS OF FAULTED FLIGHT CONTROLS, HYDRAULICS OR INSTRUMENT SYSTEMS THAT COULD CAUSE THIS PROBLEM. THERE ARE NO PRIOR REPORTS IN MAINTENANCE HISTORY FOR RUDDER MOVEMENTS. ENGINEERING SUSPECTS THIS REPORT MAY HAVE BEEN DUE TO AN ATMOSPHERIC ANOMALY. AIRPLANE WILL BE MONITORED FOR ANY SYSTEM MALFUNCTIONS.

Part: LIGHT — INOPERATIVE · airframe 37,416 hrs · 5,663 cycles

EEL LIGHTS AT 1E INOP. REPLACED EEL LIGHT.

Part: ENGINE — BIRD INGESTION (RIGHT) · airframe 36,108 hrs · 5,479 cycles

RT ENG HAD A SMALL POWER SURGE, ALL INDICATIONS NORMAL SHORTLY THEREAFTER AND REMAINED THAT WAY 5 HRS LATER. APPARENTLY THE MM STATES THAT ATMOSPHERIC CONDS (LIGHTNING) COULD CAUSE THIS. THE ACFT WAS IN VICINITY OF LIGHTNING AT THE TIME (AT FL350.) ENGINE REPLACED. SHOP TEARDOWN REVEALED BIRD REMAINS IN LPC. HPC SUFFERED RESULTANT BLADE/STATOR AIRFOIL DAMAGE. BIRD STRIKE MUST HAVE OCCURRED EARLIER, RESULTING IN A LOSS OF SURGE MARGIN. SUBSEQUENT OPERATION IN CLOSE PROXIMITY TO LIGHTNING RESULTED IN A TRANSIENT OPERATING LINE SHIFT SUFFICIENT TO CAUSE THE SURGE.

Part: CHARGER — FAILED (EMERGENCY LIGHT)

MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 24 AND 25 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSY IN THE AFT GALLEY CEILING. OPERATIONAL CHECK GOOD.

Part: SKIN — GOUGED (FUSELAGE) · airframe 30,713 hrs · 4,695 cycles

TWO GOUGES IN EXTERIOR FUSELAGE SKIN AT STA 508 STR 47R-48R. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,615 hrs · 4,679 cycles

AFT EEL LIGHT AT 1E BROKEN IN TWO. REPLACED EEL LAMP ASSY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,567 hrs · 4,499 cycles

SEAT 1E, AFT EMERGENCY LIGHT INOP. RELAMPED.

Part: SKIN — DENTED · airframe 21,946 hrs · 3,384 cycles

BULK CARGO DOOR SKIN FORWARD EDGE AREA HAS DENT. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED DOUBLER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,098 hrs · 2,926 cycles

AFT EMERGENCY PROX LIGHT AT SEAT 1F IS INOP. *S/D* POSSIBLE CAUSE OF AFT EMERGENCY PROX LIGHT AT SEAT 1F FAILURE IS DAMAGE TO THE PROX LIGHT FROM PASSENGER LUGGAGE. EXACT FAILURE CAUSE IS UNKNOWN. REPLACED LIGHT ASSEMBLY. OPS CHECKED GOOD.

Part: CLAMP — FAILED (BLEED AIR SYS) · airframe 17,834 hrs · 2,733 cycles

FORTY MINUTES AFTER TAKE-OFF, FLIGHT HAD MULTIPLE EICAS MESSAGES FOR THEIR RIGHT ENGINE NACELLE VENT VALVE. BLEED LOOP 2 WING R STATUS MSG, BLEED LEAK R, BLEED LOSS R AND PACK R. RESET THE BLEED BUT MESSAGES CAME BACK. RETURNED TO IAD AND LANDED OVERWEIGHT. SUPPLEMENTAL DATA UPDATE FORWARD CLAMP ON RH PACK FLOW CONTROL VALVE FOUND BROKEN. THE HOT AIR LEAKAGE TRIPPED THE OVERTEMP DETECTION SYSTEM CONTRIBUTING TO THE MULTIPLE FLIGHT DECK MESSAGES.CLAMP WAS REPLACED PER AMM 21-51-01.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 17,301 hrs · 2,649 cycles

THE STA 246 FLOORBEAM MID CHORD WAS CRACKED AT LBL 38. THE CRACK IS IN THE CENTER FLANGE. *S/D* CRACKED MID CHORD REPAIRED PER SRM 53-10-51, REPAIR 2, FIG 203.

Part: RADIO — FAILED (COCKPIT HF) · airframe 16,582 hrs · 2,541 cycles

LT AND RT HF TRANSMIT OK BUT NO RECEPTION PER CREW. RTF *S/D* BOTH COUPLERS WERE REPLACED AND TESTED IN THE SHOP. THE RESULT WAS NO FAULT FOUND. ALSO REPLACED WAS THE AUDIO MANAGEMENT UNIT. THE RESULTS OF TESTING ON THIS UNIT ARE NOT YET KNOWN.

Part: STRUCTURE — DAMAGED (AFT FUSELAGE)

MAJOR REPAIR TO AFT LOWER FUSELAGE DUE TO TAIL CONTACTING RUNWAY AT TAKEOFF.

Part: FAN — FAILED (CABIN)

FLIGHT ATTENDANT REPORTED THAT THERE WAS A STRONG ELECTRIC SMELL IN THE AFT CABIN. AN AMBER ALERT WAS DECLARED AND THE FLIGHT DIVERTED INTO MIA MAKING A NORMAL LANDING. *S/D* FOUND THE RIGHT LOWER AIR RECIRCULATION FAN FAILED. FAN WAS REPLACED. SHOP FINDINGS REVEALED THAT RECIRCULATION FAN HAD FAILED BEARINGS WHICH HAS CAUSED ITS MOTOR TO OVERHEAT.

Part: BEARING — FAILED (APU STARTER)

JUST AFTER LEVEL OFF THE RIGHT BACK-UP GENERATOR FAILED. CREW ATTEMPTED TO START APU AND APU FAILED. CREW ELECTED TO RETURN TO MIA. *S/D* APU FAILED TO LIGHT AT 33,000 FT WITH FAULT LIGHT INDICATION ON 17 JAN, 1999. MIA MAINTENANCE REPORTED APUC LATCHED FAULTS 49-11200 AND 49-11110. THESE FAULTS WERE FINALLY CLEARED PER FIM MM REF 49-53-804. THE SAME DAY MIA ACP TWO NORMAL APU STARTS. APU WAS REMOVED. FOUND AIR TURBINE STARTER CLUTCH BEARING (P/N 3616641-1) FAILED.

Part: AURAL WARNING — ACTIVATED (COCKPIT)

CREW REPORTED, ON APPROACH AT 800 FT RECEIVED AURAL WARNING TOO LOW GROUND. GREEN GEAR DOWN LIGHT ON AT ALL TIMES.