N657UA

Part: ADC — FAULTED (ZONE 200) · airframe 127,419 hrs · 19,499 cycles

IAS DISAGREE EICAS MSG. CAPT SIDE SHOWING .785 FO SIDE SHOWING. 815 AT 340 CREW VERBAL. STAND BY IND MATCHED F/O SIDE, CAPT ADC SWITCHED TO ALT AND SYS MATCHED . PERFORMED BITE TEST ON BOTH LEFT AND RIGHT ADC COMP. WITH NO FAULTS. REQ FURTHER T/S. REF FIM 34-11-806 FOR T/S. PERFORMED LOW RANGE AND HIGH RANGE LEAK TEST FOR BOTH PITOT AND STATIC SYSTEM REF AMM 34-11-00-730-805/804/812/811. ALL TEST PASSED. NO AIRSPEED DISCREPANCIES NOTED. R/R CAP. ADC AS PRECAUTIONARY REF AMM 34-12-01. OPS CHECK OK. AIRCRAFT GOOD TO CONTINUE. VERIFIED SECURITY OF QUICK DISCONNECT FITTINGS ON LEFT ADC.

Part: LIGHT — NO TEST (ZONE 200) · airframe 126,526 hrs · 19,381 cycles

OPERATIONAL TEST - EMERGENCY ESCAPE PATH LIGHTING (EEL) SYSTEM PERFORM OPERATIONAL CHECK - 45D AISLE EMERGENCY LIGHT IS DAMAGED. 45D AISLE EMERGENCY LIGHT REPLACED IAW AMM 33-51-10-962-104.

Part: LENS — DETACHED (ZONE 200) · airframe 126,472 hrs · 19,374 cycles

EMERGENCY EXIT SIGN LENS DETACHED, ABOVE AISLE, NEXT TO OVERWING EMERGENCY EXIT DOOR, RT SIDE OF AIRCRAFT, AFT FACING LENS COVER. LENS AND MOUNT WERE NOT BROKEN, JUST UNCLIPPED FROM LIGHT ASSEMBLY, ASSEMBLED BACK TOGETHER IAW AMM 33-51-01-962-028. LIGHT TEST PASSED.

Part: FILTER — ODOR (ZONE 100) · airframe 125,962 hrs · 19,307 cycles

MID TO AFT CABIN HAS MILD TO STRONG FOUL SMELL. REPLACE RECIRC AIR FILTERS REF IPC EQUIPMENT INSTL-CAB. AIR RECIRCULATION REFERENCE: 21-25-01-02. REMOVED AND REPLACED BOTH RECIRC AIR FILTERS PER AMM 21-25-02. PERFORMED OPS CHECK, REF AMM 21-25-02. OPS CHECK GOOD. OKAY TO CONTINUE.

Part: PANEL — CORRODED (ZONE 600) · corrosion level 2 · airframe 125,951 hrs · 19,305 cycles

THERE IS CORROSION ON THE OVERWING FILL PORT CUTOUT OF THE RH WING. CLASSIFIED AS MAJOR REPAIR IAW GMM 03-20-20 AND RII AS PER GMM 09-25-05. REPAIRED THE CORROSION IAW EC/RA 5720-03551. ITEM OK TO SERVICE RT OVERWING FILL PORT CUTOUT WAS REPAIRED AND INSPECTED AS PER EC/RA 5720-03551.

Part: BEAM — CORRODED (ZONE 800) · corrosion level 2 · airframe 125,941 hrs · 19,304 cycles

FORWARD LARGE CARGO DOOR LOWER BEAM BS 562.4 - 575.6. ALL OF STEPS OF ECRA 5233-01037 WERE ACCOMPLISHED WITHOUT DEVIATION.

Part: SKIN — DAMAGED (ZONE 200) · airframe 125,951 hrs · 19,305 cycles

FWD DOOR 1L - FUSELAGE, SCRIBE LINES, GOUGES & DAMAGED FASTENER HOLES. . PERFORMED INTERIM REPAIR IAW EC/RA 5310-08669

Part: FAILSAFE — CORRODED (ZONE 100) · corrosion level 2 · airframe 125,951 hrs · 19,305 cycles

FAIL-SAFE STRAP LOWER SURFACE CORROSION BETWEEN BS 1241 & 1263 MAJOR REPAIR AS PER GMM 03-20-20. PERFORMED INTERIM REPAIR AS PER EC/RA: 5360-01995. ALL THE STEPS OF THE EC/RA 5360-01995 HAVE BEEN INSPECTED. THIS REPAIR IS A PERMANENT SOLUTION WITH INSPECTION REQUIREMENTS.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 125,951 hrs · 19,305 cycles

DURING LOWER LOBE INTERIOR BS 1540 TO 1629, CDP INSPECTION IT WAS FOUND SIGNS OF CORROSION ON SKIN BETWEEN S38L & S39L LOCATED BETWEEN BS 1540 & 1562. PERFORMED INTERIM REPAIR IAW EC/RA 5360-01993, REV A PERFORMED INSPECTION & INTERIM REPAIR WAS ACCOMPLISHED IAW EC/RA 5360-01993, REV A.

Part: SKIN — CRACKED (ZONE 800) · airframe 125,951 hrs · 19,305 cycles

RIGHT FORWARD SERVICE DOOR AFT LOWER CORNER FASTENER HOLE CRACKED. PERFORMED INTERIM REPAIR IAW EC/RA: 5310-08664 ALL STEPS OF INTERIM REPAIR WERE ACCOMPLISHED AS PER EC/RA: 5310-08664 IT. IAW GMM 04-20-05 R1 FORWARD SERVICE DOOR AFT LOWER CORNER FASTENER HOLE CRACK WAS REPAIRED.

Part: TURNBUCKLE — CORRODED (ZONE 800) · airframe 125,022 hrs · 19,183 cycles

L4 DOOR SLIDE REPLACEMENT. FOUND TURNBUCKLES ON FWD SIDE OF DOOR CORRODED. SEE PICS. CLEANED CORROSION IAW AMM 52-11-00-622-107. NO FURTHER DEFECTS NOTED. REAPPLIED CORROSION INHIBITING COMPOUND IAW AMM 51-24-09-377-008. OK TO CONTINUE

Part: LENS — MISSING (ZONE 200) · airframe 124,385 hrs · 19,099 cycles

EMERGENCY LIGHT OPPOSITE LAV B AT GALLEY STOWAGE 227F DAMAGED. EMERGENCY LIGHTING TESTED. ALL LIGHTS WORK BUT CLEAR PLASTIC COVER/LENS IS MISSING. REQUEST DEFERRAL PER MEL 3351C. FWD GALLEY LOWER WALL WHITE EMERGENCY AISLE LT INOP. DEFERRED PER MEL 3351C PART NUMBER REQUIRED:- BR9644-21, M&E 99-3350-3-0008. TAKEN FROM "ESCAPE PATH LIGHTING - SYSTEM LAYOUT" CONFIGURATION DRAWING. UPON BRIEF INSPECTION BEFORE DEFERRING, THE LIGHT LOOKED TO BE HARD WIRED & MAY NEED RE-PINNING OR SOLDERING. INSTALLED NEW LENS COVER. OPS CHECK GOOD. OK TO CONTINUE.

Part: FUEL SYS — OUT OF BALANCE (ZONE 100) · airframe 124,381 hrs · 19,097 cycles

FUEL CONFIG CAS IN CRZ. IMBALNCE OF 1900LBS. FM SUGGESTED POSS FUEL LEAK RTRNED TO LHR. CREW DEBRIEF C/OUT ON A/C RTN - REF MADE TO LP 3937863 - LEFT CTR FUEL PUMP INOP AS PER MEL 2822G. NIL FUEL LEAKS FOUND ON ARRIVAL. CREW BALANCED FUEL INBOUND, LEFT & RIGHT WING TANK BOTH INDICATE 35.8 / CTR TANK INDICATES 0.0. BOTH FLT DECK AND WING GAUGES INDICATE SAME TOTALS. DURING DEBRIEF DISCUSSED FLT CREW INSTRUCTION AND SW POSITION FOR DEPARTURE WITH ALL CREW. SUSPECT A/C DEPARTED WITH NO CROSSFEED VALVE SELECTED TO ON POSITION AS PER FLIGHT CREW INSTRUCTION IN MEL. TOMC INFORMED.

Part: UNKNOWN — ODOR (ZONE 200) · airframe 123,767 hrs · 19,013 cycles

ELECTRICAL SMELL IN CABIN FOLLOWING LIGHTNING STRIKE. CREW REPORTED SMELL IN FWD AND AFT GALLEY AREAS. RAN ENGINES AND PACKS WITH FLIGHT ENTERTAINMENT AND OTHER EQUIPMENT. FLIGHT AND CABIN CREW ON BOARD AND FOUND NO ODORS IN THE CABIN AT THIS TIME REF AMM 05-51-56-940-801-C1.

Part: LENS — MISSING (ZONE 200) · airframe 123,315 hrs · 18,951 cycles

EMERGENCY CEILING LIGHT IN FWD GALLEY ABOVE STOWAGE ZONE 200 LENS CAP IS MISSING. LENS REPLACED IAW AMM 33-51-04-002-001.

Part: CABLE — MISROUTED (OVERWING SLIDE) · airframe 122,689 hrs · 18,868 cycles

LEFT OFF WING SLIDE BOTTLE TRIGGER CABLE BALL FOUND BEHIND RETAINER CLIP TRIGGER CABLE ADJUSTED AS PER AMM 25-65-02-350-811-C2. BALL END NOW SAT CORRECTLY BEHIND THE RETAINER SPRING. RII REQUIRED AS PER GMM 09-25-05 CABLE TRIGGER BALL MECHANISM VERIFIED TO BE INSTALLED CORRECTLY WRT AMM: 25-65-02-350-811-C2. SAFETY PIN FOR THE OFF WING SLIDE BOTTLE CONFIRMED TO BE REMOVED FROM THE VALVE ASSY AND STOWED IN POUCH REF GMM: 09-25-05.

Part: SKIN — DAMAGED (ZONE 100) · airframe 122,001 hrs · 18,777 cycles

DURING ACCOMPLISHMENT NR 2114213 WAS FOUND A DAMAGE ON FUSELAGE SKIN LH SIDE BETWEEN STA 1702 AND 1746.125 , STRINGER 24L AND 26L. ITS NECESSARY TAKE ACTION TO PERFORM A REPAIR IAW SRM. TO PERFORM INSPECTION IAW SRM 53-00-01-2R-12 TABLE 202 & DELIVERY, REPEAT INSPECTIONS AT 12,000 FC INTERVALS. METHOD OF IN EXTERNAL DVI REFERENCE NDT PART 6, 51-00-01 AND FIG202 DETAIL I. TO DETAIL I. THE THRESHOLD INSPECTION IS 37,500 FC AFTER AC D SPECTION IAW SRM 53-00-01-2R-12 TABLE 202. INTERNAL HFEC & TAIL I FIG.202. THRESHOLD INSPECTION IS 37,500 FC AFTER AC D SPECTION IAW SRM 53-00-01-2R-12 TABLE 202. INTERNAL HFEC AND PERFORMED SECTION 48 TAIL CONE, LT FUSELAGE SKIN AREA BETWEEN ST PERFORMED SECTION 48 TAIL CONE, LT FUSELAGE SKIN AREA BETWEEN BS 1702 - 1725 REPAIR IAW ECRA 5380-01397. IT'S NECESSARY A 1702 - STA 1725 REPAIR IAW ECRA 5380-01397. IT'S NECESSARY PER SRM 53-00-01-2R-12 REPAIR 12: PERFORM INSPECTION IAW SRM TOMC-APPROVAL FROM SC1ELBYC COMMENT 53-00-01-2R-12 TABLE 202 & DETAIL I FIG.202. THRESHOLD INSPECTION IS 37,500 FC AFTER AC DELIVERY OR 6000 CYCLES AFTER REPAIR INSTALLATION, WHICHEVER COMES LATER. REPEAT INSPECTIONS AT 12,000 FC INTERVALS. DIP 53-DIP ECRA 5380-01397 DOES NOT LIST THE TERMINATING ACTION OR INSPECTION INTERVALS.

Part: TRANSMITTER — FAULTED (HYD QTY) · airframe 121,882 hrs · 18,762 cycles

LOSS OF L HYD QTY WDM 29-33-11-2. RECONNECTED D38 AND REINSTALLED HYD MON UNIT. INSPECTED LT HYD QTY TRANSMITTER, SUSPECT TRANSMITTER AT FAULT. LT HYD QTY SHOWS 1.00 AT GATE. PERFORMED WIRE HARNESS SHAKEDOWN IAW WDM 29-33-11-2. ALL MEG CHECKED AND CONTINUITY, LT PYLON FROM LEFT HYD QTY TRANSMITTER, NO CHANGE NOTED. MEG CHECKED GOOD. PERFORMED DETAILED VISUAL INSPECTION OF PYLON WIRE, CHECKED ALL PINS ON CONNECTOR D38 WITH HYD MON UNIT REMOVED. NO DEFECTS NOTED. PERFORMED SHAKEDOWN OF PYLON HARNESS CHECKED PINS 1-7 TO GROUND AND EACH OTHER, NO SHORTS NOTED. CHECKED WIRING AGAIN, STILL UNABLE TO DUPLICATE FAULT. NO WIRING DEFECTS. R & R LT HYD QTY TRANSMITER IAW AMM 29-33-02 ,OPS CHECKED GOOD.

Part: HOSE — LEAKING (OXYGEN SYSTETM) · airframe 121,340 hrs · 18,689 cycles

**CHRONIC LVL-2** DUE TO INCREASING FREQUENCY IN CREW O2 SERVICI NG WRITE-UPS, ACCOMPLISH THE FOLLOWING..1) PERFORM CREW O2 LEAK CHECK IAW AMM 35-11-00-795-106. PAY CLOSE ATTENTION TO ALL FITTI NGS AND PROPER STORAGE OF MASKS. LEAK WILL MOST LIKELY BE SMALL. REPLACE ANY MASKS THAT ARE WORN OR DAMAGED. IF AVAILABLE, USE M ARKSMAN ULTRASONIC LEAK DETECTOR M&E: 39-2020-0-5025. THIS TOOL HAS PROVEN TO BE VERY HELPFUL FINDING SMALL LEAKS. CORRECT ANY D EFECTS FOUND...2) PLEASE RECORD THE FIRST AND LAST TESTED PRESSU RE "DROP/HR" OBSERVED IN SIGNOFFS.THANKS! ORDLM PIPERS. CARRIED BY ELB NEED POSITIVE FIX. BEEN GOING ON FOR A WHILE.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 121,089 hrs · 18,655 cycles

LOST NOSE WHEEL STEERING EXITING RUNWAY REF LOGPAGE 7815478 FOR X5 LANDING GEAR DOWNLOCK PIN INSTALLATION AS PART OF AIRCRAFT RETRIEVAL FROM TAXIWAY REF GMM 02-30-20 (2.C.(8)). GVI OF NLG PERFORMED. NIL SIGNS OF HYDRAULIC LEAKS AND STEERING CABLES CHECKED SECURE. TILLER AND RUDDER PEDDLES FUNCTIONED AS PER AMM 32-51-00-735-072 PARAGRAPH H THROUGH TO K AND ALL OPS CHECKED GOOD. NIL PRIOR HISTORY

Part: WARNING MESSAGE — FALSE INDICATION (RUDDER RATIO) · airframe 120,817 hrs · 18,618 cycles

RUDDER RATIO EICAS AFTER TAKEOFF BRIEFED CREW ; NO OVERWEIGHT LANDING,PILOT STATED PLANE FLEW FINE ,JUST EICAS MSG AFTER TAKEOFF PERFORMED FIM TASK RUDDER RATION EICAS MSG 27-21 FAULT TREE PERFORMED YAW DAMPER SYSTEM BITE AS PER FIM 22-21 FAULT TREE 803 804.RUDDER RATIO CONTROL MODULE BITE TEST PER FIM TASK 27-09 AT THIS TIME NO FAULTS WERE OBSERVED AND NO INDICATIONS ON FAULT TREE 814.SAM BITE PROCEDURE 27-09 FAULT TREE 811 AND OVERHEAD PANEL OR EICAS WERE SEEN. SPOILER CONTROL MOD.BITE TEST PER FIM 27-09 FAULT TREE 807.ALSO

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 120,588 hrs · 18,588 cycles

EMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - DOOR 1R EXTERIOR EMERGENCY LIGHT FAILED TO ILLUMINATE. LAMP REPLACED AS PER MM TASK 33-51-06-902-082 PARTS USED: 99-3351-3-0014,QTY :1

Part: MONITOR — FAULTY (STA328, CTR E1/E) · airframe 120,453 hrs · 18,570 cycles

RT HYD QTY ON EICAS DURING TAKE OFF ROLL, EG RECOMMENDS PERFORMING B767 FIM TASK 29-11-00-211-802-C2 IN ORDER TO AID LOCATING THE HYD LEAK. REMOVED AND INSTALLED HYD RES TRANSMITTER ON THE RT RESERVOIR IN REVERENCE TO AMM TASK 29-33-02-004-001. REQUIRES HYD SERVICE & OPS CHECK. AIRCRAFT RETURNED TO GATE INDICATING 1.02 FOR RT HYD SYS. SUSPECT INDICATION PROBLEM. PER FIM 29-11 FAULT TREE 832, REPLACED THE MONITOR, HYD IAW AMM29-33-01. OP CHECK GOOD. SERVICED R SIDE HYDC SYS LEAK CHECK GOOD ON RIGHT SIDE TANK TRANSMITTER. (REF. AMM TASK 12-12-01-613-060)

Part: NOZZLE — LEAKING (WINDSHIELD) · airframe 118,902 hrs · 18,358 cycles

OBSERVED SMOKE/STEAM COMING ACROSS CAPTAINS WINDOWS. 4 SEPERATE OCCURANCES. WX CLEAR. PERFORMED VISUAL CHECK OF TAT PROBE AS WELL AS FUNCTIONAL CHECK OF TAT PROBE HEAT REF AMM 30-33-00-715-010. TEST PASSED, NO DEFECTS NOTED. PERFORMED RAIN REPELLENT OPS CHECK WITH ENGINES RUNNING ABOVE IDLE IN REF. TO AMM 30-43-00 FOUND AIR LEAK COMING FROM BOTH WINDSHIELD RAIN NOZZLES. SYSTEM WAS PREVIOUSLY DEACTIVATED. INSPECTED AND FOUND MOISTURE IN TUBE ASSEMBLY LEADING INTO RAIN REPELLENT SYSTEM REF AIPC 34-12-52-01. PURGED LINE FROM AIPC34-1 2-52-01 ITEM 170 TO 770 UNTIL CLEAR OF MOISTURE. PURGED LINE FRO M ITEM 175 UP TP NOZZLES, NO MOISTURE PRESENT. RECONNECTED AND P ADD EMP:U414805 PERFORMED LEAK CHECK OF PNEUMATIC SYSTEM REF AMM36-00-00. NO LEAK S OR MOISTURE NOTED. PERFORMED TAT PROBE HEAT TEST REF AMM30-33- 00-715-010 NO ISSUES NOTED. RAN ENGINES NO ISSUES NOTED.

Part: SMOKE DETECTOR — NONE (1R & 2R) · airframe 116,382 hrs · 18,009 cycles

2 HALON EXT USED FROM 1R AND 2R HALON EXTINGUISHERS (X2) USED NOT IN STOCK LHR, COMPLIED WITH 2 X HALON FIRE EXTINGUISHERS REQUIRED NIS LHR M&E REQUIREMENTS OF MEL 99-2626-3-0105, COMPLIED WITH REQUIREMENTS OF MEL. APPROVED

Part: PUMP — FAILED (HYD SYSTEM) · airframe 115,540 hrs · 17,894 cycles

SUSPECT LEFT ENGINE DRIVEN HYDRAULIC PUMP FAILURE. PUMP REPLACEMENT REQUIRED. REPLACED LEFT EDP PUMP ASSY IAW AMM 29-11-05-404-029-005 AND PUMP FAILED OPERATIONAL TEST. PERFORMED FIM 29-11 FAULT TREE 805 AND PER SHEET 2 BLOCK 27, SWAPPED OPERATIONAL PRESSURIZATION SHUTOFF ENGINE GROUND IDLE RUN TEST NR 3 IAW AMM 71-00-00-795-003-N00 VALVE FROM RIGHT SYSTEM INTO LEFT POSITION AND DRY MOTOR PERFORMED. EDP OPERATED AND SUPPLIED 2840PSI AT MAX MOTOR. LEFT EDP ASSY REPLACED REF AMM 29-11-05-004-001-005 AND AMM RIGHT SYS RESERVOIR PRESSURIZATION SHUTOFF VALVE REINSTALLED IN 29-11-05-404-029-005. PERFORMED ENGINE DRY MOTOR TEST NR 2 REF ORIGINAL POSITION. PERFORMED FIM PRESSURIZATION SHUTOFF VALVE REPLACEMENT.

Part: INDICATOR — UNSERVICEABLE (RIGHT WING) · airframe 115,360 hrs · 17,869 cycles

FUEL QTY IND EICAS S THE FQIS CANNOT ACCURATELY DETERMINE THE FUEL QUANTITY IN ONE OR MORE FUEL TANKS. R FUEL QTY INDICATOR INOP. NO TOTALIZER VALUE OVERHEAD OR IN FM C ALSO. LOCK FOR POSITIVE FIX, ALSO HISTORY ON LP 3083170 15NOV22 UNLOCKED TO CLEAR REFERENCE L/P 3117850 & 3118047 FOR CORRECTIVE ACTION ; WORK PERFORMED BY TANK TIGERS WO#12249R1272 UALWO# 3060939

Part: DOOR — STUCK (FWD ENTRY DOOR) · airframe 114,741 hrs · 17,783 cycles

FWD ENTRY DOOR WILL NOT RETRACT OPEN DO TO INSIDE FOLDING CEILING PANEL OUT OF SEQUENCE REF AAR N/R 9029568 INSTALLED MISSING BOLT ON OVERCENTER MECHANISM LATCH TUBE.

Part: FLOORBEAM — CRACKED (STA 287, RBL 80) · airframe 114,170 hrs · 17,705 cycles

B767-53-3-7002, CABIN- STA 287, RBL 80 AREA FLOORBEAM FOUND CRACKED TRANSFER REF HXWO 821634 AND ORIGINATED BY EMP V897790 CABIN STA287 RBL33.5 TO RBL82 AREA FLOORBEAM REPAIRED AS PER ECRA5320-02964 REV - ATTACH FORM 44-0008 WORKSHEET ITEM 1 TO ITEM36 ACCOMPLISHED , WORK ACCOMPLISHED BY MECHANIC V897471 INSPECTED BY V898556 RII INSPECTED BY HX156019 ADD EMP:V897897

Part: FLOORBEAM — CORRODED (STA303 LBL24) · airframe 114,170 hrs · 17,705 cycles

B767-53-3-7002 CABIN STA303 LBL24 TO 54 FLOORBEAM FOUND CORROSION TRANSFER REF HXWO 822811 AND ORIGINATED BY EMP V897790 CABIN STA303 LBL46" TO LBL54" FLOOR EAM CORROSION BLEND OUT REPAIR 1 FIG.201 ATTACH FORM 44-0008 WORKSHEET ITEM 1 TO ITEM33 AREA REMAIN 0.040" WIDTH : 1" LENGTHS : 2" ORIG THICKNESS ACCOMPLISHED STA303 LBL24" TO LBL44" WITHIN LIMIT AS PER 0.090" OUT OF SRM53-00-15 ALLOWABLE DAMAGE 1 FIG.101 LIMIT SRM53-00-15 ALLOWABLE DAMAGE 1 FIG.101 WORK ACCOMPLISHED BY FLOOR BEAM STA303 LBL30"-LBL60" REPAIRED AS PER SRM53-00-51-2R-1 MECHANIC V897471 INSPECTED BY V898556 RII INSPECTED BY HX341008 ADD EMP:V896888

Part: SKIN — CRACKED (BS 1438 S38-39R) · airframe 112,902 hrs · 17,460 cycles

B767-53-3-7064 - LOWER HALF FUSELAGE STA 1438 BETWEEN S38R-S39R HAS CRACK REF NRC 9130394, SKIN DAMAGED AREA TRIMMED OFF PER SRM 53-00-01- 2R-29 REAPIR FIG 201. SKIN THICKNESS IS 0.056". HFEC CARRIED OUT PER B767 NTM PART6 51-00-19 REV 125, NO CRACK FOUND. REPAIR DOUB LER INSTALLED PER SRM 53-00-01-2R-29 REPAIR 29 FIG 201 DETAIL 1 CREATED DIP FOR CATEGORY B REPAIR INSPECTION REQUIREMENT PER SRM 53-00-01 REPAIR 29 FIG 201 TABLE V. PER SRM 53-00-01-R2-29 REPAIR 29 TABLE V(5) ACP INITIAL 1 TIME INSPECTION AT 6000 FLIGHT CYCLES AFTER REPAIR INSTALLATION (REPAIR ACP AT 17460 CYCLES) AND ALTERNATIVE 1 INSPECTIONS AT 12000 FLIGHT CYCLES THEREAFTER PER NDT PART 6, 51-00-01. THIS REPAIR IS A: ZONE A-CATEGORY B REPAIR. TOMC-APPROVAL FROM SC1ELBYC COMMENT RECORDS UPDATE............VD TOMC APPROVED : QC REVIEWED. TOMC APPROVED : QC REVIEWED. RECORDS UPDATE............VD INIT: 6000 FC (INIT WILL ITO TO RIR -0607) RIR: 12000 FC...............VD/U353583

Part: SENSOR — FAULTY (LE SLAT) · airframe 110,200 hrs · 16,976 cycles

LEADING EDGE SLAT SYSTEM ALTERNATE LEADING EDGE SLATS PROBLEM WAS ENCOUNTERED BY THE FLIGHT CREW WHICH IS NOT COVERED IN THE FAULT CODE DIAGRAMS. LE SLAT ASYM EICAS MSG DURING FLT LE SLAT ASYM EICAS ALSO ON FINAL. PER TECH SUPPORT FOUND PSEU FAULT WITH PROX SENSOR NO. 284, INBOARD SENSOR ON NO.3 LEADING EDGE SLAT. TARGET GAP AT THIS LOCATION IS AT THE MAX OF INSTALATION RANGE. REMOVED AND REPLACED S284 LEADING EDGE SLAT SENSOR SWITCH. OPS CHECKED GOOD. NO FAULTS FOUND ON PSEU. REF AMM27-88-00, AMM27-88-01.

Part: CONNECTOR — DEFECTIVE (HYDRAULIC SYS) · airframe 109,472 hrs · 16,865 cycles

HYD SYS PRESS -R INTERMITTENT EICAS ALONG WITH FLICKERING BRAKE SOURCE LIGHT(INTERMITTENT. NEED POSITIVE FIX UNLOCK UNLOCKED DEBRIEFED CREW: PILOT REPORTED THAT THEY NOTICED THIS ISSUE AFTER THEY REACHED CRUISE ALTITUDE. PILOT SAW THE BRAKE SOURCE LIGHT FLICKERING ON AND OFF, THEN HEARD A TICKING SOUND ABOVE HER HEAD. SHE NOTICED THE RIGHT SYSTEM DEPMAND PUMP PRESSURE LIGHT AND THE SYSTEM PRESSURE LIGHT FLICKERING ON AND OFF. AS THE PILOT. R WOULD APEAR AND DISAPEAR ALONG WITH THE AUDIBLE CHIME TO WARN THE SYS PRESSURE LIGHT FLICKERED THE EICAS MESSAGE HYD SYS PRESS THE PILOT DID NOT TURN OFF THE RIGHT SYSTEM AS HYDRAULIC PRESSURE INDICATIONS REMAINED NORMAL AND STEADY EVEN AS THE AND THE SYSTEM PRESSURE LIGHT CAME ON, EVEN WITH THE R ENGINE INDICATIONS WERE GOING ON AND OFF. PILOT CYCLED THE EDP TO OFF, PUMP SUPPLYING PRESSURE. WHEN RETURNING TO ORD, PILOT SAYS THE THE SAME PROBLEM. PROBLEM WENT AWAY. THIS ISSUE HAS HISTORY WITH AIR RETURNS FOR REMOVED CONNECTORS D5798P & D76 TO ELEC HYD PUMP RT CONTROL,CHEC KED FOR SHORT & OPEN AT WIRES W572-026,021,W442-002,001 AND W400 -002,001 CHECK OK. OLD PRESS SWITCH CHECKED OK, CONN D76 PIN #2 SHORTED TO BACKSHELL,PINS 3&2 ALSO BREAKING DOWN.REF WDM29-11-22 . LOCKED FOR REPAIR CONFIRMATION UNLOCKED TO CLEAR D5798P. REPLACED CONNECTOR D76 REF WDM 29-11-22 SECURED CONNECTORS D76 & DURING ENG RUN HYD SYS PRESS LIGHT AND BRAKE SOURCE LIGHT DID NOT ILLUMINATE.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 109,434 hrs · 16,859 cycles

WITH THE R ELEC HYD PUMP ON/R LOW PRESSURE SYS. AND BRAKE SOURCE LIGHT CAME ON/FOLLOW QRH. ACMP SHOWS FLUCTUATIONS IN PRESSURE WHEN A LOAD WAS APPLIED. REMOVED ACMP IAW AMM 29-11-01-024-001 AND ORDERED REPLACEMENT VIBRATION MOUNTS AND HARDWARE. REPLACED RIGHT HYDRAULIC PUMP REFERENCE LOG PAGE 3654005. LP 3654005- REMOVED AND REPLACED RIGHT ELEC HYDRAULIC PUMP PER AMM 29-11-01. OPS CHECK GOOD NO LEAKS. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1352928 SN OFF 9029 PUMP, AC MOTOR OFF 75-2914-9-0001 9029 ON 75-2914-9-0001 0379.

Part: PRESSURE SWITCH — INOPERATIVE (HYD SYSTEM) · airframe 109,246 hrs · 16,832 cycles

HYD SYS PRESS R EICAS CAUTION CAME ON IN FLIGHT DEBRIEF CREW RIGHT ELEC PRESS LIGHT FLICKERED AND SYS PRESS LIGH T ILLUMINATED. R ENG HYD PUMP TURNED OFF AND RIGHT ELEC LEFT ON STILL HAD SYS PRESS LIGHT ILLUMINATED. RAN RIGHT ENG FOR 5 MINUT ES NO FAULTS NOTED. RAN R ELECTRIC HYDRAULIC NO FAULTS. REMOVED AND REPLACED S31 EDP PRESSURE SWITCH ON EDP FILTER MODUL E. PERFORMED ENGINE RUN AND NO HYD PRESSURE EICAS CAUTION MESSAGE NOTED WHILE PUTTING LOAD ON RIGHT HYD SYSTEM. ALL WORK PERFORM ED IAW 29-11-17. ALL OPS CHECK NORMAL AND LEAK CHECK GOOD.

Part: STRINGER — CRACKED (BS 1439-1461) · airframe 109,135 hrs · 16,818 cycles

SUPPORT TASK - FX STA1439-1461 STR24R FOUND CRACKED AND PREVIOUS LY REPAIRED (AFTER SKIN DOUBLER REMOVED).REF NR LP 9132054 FX STA1417 TO STA1486 STR24R REPAIRED AS PER ECRA 5331-02466 REV - PART 1 ITEM 1 (STRINGER REPAIR IN CATEGORY A REPAIR) AND SKIN REPAIRED DETAIL REF NRC L/P 9131988.ATTACH MAINTENANCE WORK SHEE T FORM 44-0008 ITEM 1 TO 37 ACCOMPLISHED ADD EMP:V897467 RII BY HX224337,APPROVED

Part: SKIN — DENTED (BS 368) · airframe 109,135 hrs · 16,818 cycles

SUPPORT TASK TAR - LP 6587012 FUSELAGE SKIN DENT BETWEEN STA355 AND STA368 S-22R TO S-23R AFTER MEASURED OF THE DENT, THE DEPTH IS 0.119" LENGTH IS 3.2" AND WIDTH IS 2.1".A/Y IS LESS THAN 30 OUT OF LIMITS AS PER SRM 53-00-01 ALLOWABLE DAMAGE 1, NO APPLICABLE REPAIR FIG FOUND IN SRM DUE TO THE DISTANCE BETWEEN DENT AND CUTOUT ARE LESS THAN 22" PLS ADV REF TO NR LP:9132073 BS 355-368, STR 22R TO S23R,REPAIRED IAW ECRA 5331-02463 AND SRM 53-00-01, REPAIR 10, REF HAECO LP 9132073. DIP CREATED IAW SRM 5300-00-01, RPR 10, TABLE IV, REQUIRING DVI ON OR BEFORE 37,500 ADD EMP:U085164 FC WITH A REPEAT INSPECTION INTERVAL OF 12,000 FC. APPROVED FOR DIP REF ECRA 5331-02463. INSPECTION TO BE ACCOMPLISHED ON OR BEFORE ACFT REACHES 37500 PTC. REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 12000 FLT CYCLES THEREAFTER TOMC-APPROVAL FROM SC1ELBYC COMMENT Q/C REVIEWED. RECORDS UDPATE ..JF Q/C REVIEWED. INIT: 37,500 TAFC (INIT WILL AUTO ITO TO T/A - 0537) T/A : 12,000 FC ..JF

Part: FRAME — CORRODED (BS 977) · airframe 109,135 hrs · 16,818 cycles

B767-53-3-7035 CABIN STA 977 R/H FRAME LWR CORNER FOUND CORRODED REF TO NR LP:9131109 RH FRAME STA 977 CORROSION REPAIRED IAW ECRA 5311-02261. THIS IS A DAMAGE TOLERANCE REPAIR IAW SRM 53-00-06, CAT C, AND REQUIRES REPLACEMENT WITHIN 24 MONTHS OR 3,OOO FC, WHICHEVER OCCURS ADD EMP:U085164 FIRST. ADDITIONAL DVI INSPECTIONS REQUIRED WITHIN 600 FC OR 6 MONTHS OF THIS INSTALLATION, WHICHEVER COMES FIRST. CURRENT FC ARE 16,818. DADO PNLS 242DSW AND 242ESW ARE REQUIRED FOR INSP. APPROVED DIP FOR DAMAGE TOLERANCE REPAIR IAW SRM 53-00-06, CAT C, AND REQUIRES REPLACEMENT WITHIN 24 MONTHS OR 3,OOO FC, WHICHEVER OCCURS FIRST TOMC-APPROVAL FROM SC1ELBYC COMMENT INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE. QC REVIEWED. QC REVIEWED.

Part: SKIN — CRACKED (BS 1605-1629) · airframe 109,135 hrs · 16,818 cycles

SUPPORT TASK TAR - QC PICK UP SHEET - EXTERNAL FUSELAGE REPAIR NOT LISTED FOR INSPECTION FROM AIRCRAFT RECORD BTN BS1605-1629 LWR FUSELAGE RBL 6".PLS ADV REPAIR RECORD OR REPAIR INSTRUCTION REF TO NR LP:9131989 BS 1605-29 REPAIRED IAW ECRA 5331-02462 AND SRM 53-30-01, RPR 29, REF HAECO LP 9131989. DIP CREATED IAW TABLE V, DETAIL I, REQUIRING HFEC INSP BEFORE 37,000 FC AFTER AIRCRAFT DELIVERY OR ADD EMP:U085164 OR 6,000 FC AFTER REPAIR, WHICHEVER COMES LATER. REPEAT HFEC INTERVAL IS 12,000 FC. NDT IAW PART 6, 51-00-01. AIRCRAFT CURRENT FLIGHT CYCLES ARE 16,818. APPROVED DIP REFERENCE ECRA 5331-02462 PART 2 . INSPECTION TO BE ACCOMPLISHED ON OR BEFORE ACFT REACHES 37500 PTC WITH REPEAT INSPECTIONS NOT TO EXCEED 12000 FLT CYCLES THEREAFTER .

Part: SKIN — DENTED (BS 1417-1486) · airframe 109,135 hrs · 16,818 cycles

BS 1417-1486, STR 24R DENT REPAIRED IAW ECRA 5331-02466, REF ELB LP 3408629 AND HAECO NR LP 9132054, DURING HKG 2C VISIT. ECRA 5331-02466 PART 2 REQUIRES INSPECTION ON OR BEFORE 37,500 FC AND REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 12,000 FC. IAW ECRA 5331-02466, DIP CREATED FOR HFEC INSPECTION IAW NDT PART 6, 51-00-01. INSPECT THE SKIN AT THE CRITICAL FASTENER ROW ALONG THE EDGE OF THE DOUBLER. REFER TO 767-300 SRM 53-00-01, RPR 1, FIGURE 201, DETAIL I AND II. ACCOMPLISH AN EXTERNAL DETAILED INSP OF THE RPR DBLR AND A 2-INCH WIDE ZONEAROUND THE RPR IAW SRM 53-00-01, RPR 1, FIG 201, DETAIL I AND III. APPROVED FOR DIP PER ECRA 5331-02466. PART 2 REQUIRES INSPECTION ON OR BEFORE 37,500 FC AND REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 12,000 FC THEREAFTER TOMC-APPROVAL FROM SC1ELBYC COMMENT INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE. QC REVIEWED. QC REVIEWED.

Part: ATTACH ANGLE — DAMAGED (FUSELAGE) · airframe 109,135 hrs · 16,818 cycles

SUPPORT TASK QC PICK UP SHEET - TOOLING MARKS LOCATED ON ATTACH ANGLE AT STA977 AT STRINGER 22L,WL180,ON TOP OF PRESSURE DECK CAUSED BY LEVELING COMPOUND REMOVAL.REF NR LP 9131376 CABIN STA977 S22L PRESSURE DECK LUB ATTACH ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 AND ATTACH FORM 44-0008 ITEM 1 TO 5 ACCOMPLISHED ADD EMP:RII, APPROVED

Part: ATTACH ANGLE — DAMAGED (FUSELAGE) · airframe 109,135 hrs · 16,818 cycles

SUPPORT TASK QC PICK UP SHEET - TOOLING MARKS LOCATED ON ATTACH ANGLE AT STA977 AT STR 22R,WL180,ON TOP OF PRESSURE DECK CAUSED BY LEVELING COMPOUND REMOVAL.REF NR LP 9131377 CABIN STA977 STR22R WL180 ANGLE REPLACED AS PER SRM 51-10-02 AND FASTENER INSTALLED AS PER SRM 51-40-02.ATTACHED FORM 44-0008 ITEM 1 TO 5 ACCOMPLISHED ADD EMP: RII, APPROVED

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 109,135 hrs · 16,818 cycles

B767-53-3-7154 - AFT CGO COMPT L/H TORQUE BOX PNL SUPPORT BOTTOM AREA FOUND CORROSION STA 1285 LBL9-24 FLOOR BEAM AREA.REF TO NR LP:9131604 AFT CGO LH TORQUE BOX PANEL SUPPORT STA1285 LBL40-RBL40 FLOOR BE AM REPLACED AS PER SRM 51-10-02 AND FASTENER INSTALLED AS PER SR M 51-40-02.ATTACH FORM 44-0008 ITEM 1 TO 23 ACCOMPLISHED.(NEW CHORD P/N:146T1210-20 FABRICATED DETAIL REF NRC L/P 9132072) ADD EMP: RII BY, APPROVED

Part: FRAME — CORRODED (FUSELAGE) · airframe 109,135 hrs · 16,818 cycles

B767-53-3-7035 CABIN STA 977 L/H FRAME LWR CORNER FOUND CORRODED REFER TO NR LP:9131108 CABIN STA 977 L/H FRAME OUTER CHORD REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 JUST BETWEEN STR-8L AND STR-22AL NEW CHORD P/N:145T1062-35 GRN H19S244823 ADD EMP: RII IS OK INSPECTED

Part: SKIN — NOT REPORTED (FUSELAGE) · airframe 109,135 hrs · 16,818 cycles

REFERENCE LP#3339628 S/M REPAIR OVER DOOR 1L. REPAIR WAS PREFORM ED PER SRM53-00-01 REPAIR 12. DIP IS REQUIRED FOR REINSPECT. FIR ST REINSPECT IS 6,000 F/C AFTER REPAIR & REPEAT INSP EVERY 9,000 F/C REFERENCE SRM 53-00-01 REPAIR 12 TABLE 202. DIP REQUESTED FOR REINSPECT OF REPAIR OVER DOOR 1L. SRM 53-00-01 RPR 12 TABLE 202 REQUIRES REINSPECT 6,000 F/C AFTER RPR & 9,000 F/C INTERVALS AFTER INITAL INSPECTION. THIS REPAIR WAS ACCOMPLISHED UNDER L/P#33396281 & HAECO NR# 9131 983 &9131992 AT 2C CHECK IN HKG. REQUESTED FOR REINSPECT OF REPAIR OVER DOOR 1L. SRM 53-00-01 RPR 12 TABLE 202 REQUIRES REINSPECT 6,000 F/C AFTER RPR & 9,000 F/C INTERVALS AFTER INITAL INSPECTION. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED. QC REVIEWED. RECORDS UPDATE INIT: 6,000 FC FROM RPR (INIT WILL ITO TO RIR -0528) RIR: 9,000 FC.....BK-245861

Part: WIRE — DAMAGED (CABIN) · airframe 107,954 hrs · 16,653 cycles

DURING CLIMB PAX SAW A FLASH ABOVE ROW 20 FOLLOWED BY SMOKE AND FUMES. REF AMM05-51-56 SMOKE INSPECTION. REMOVED CABIN CEILING PANELS AT 19-20 ABC AND 19-20 KL. CONFIRMED HEAT DAMAGE ON LEFT SIDE CEILING BETWEEN STATION 764 AND 808 REQUIRING FURTHER INVESTIGATION. PHOTOS UPLOADED TO TOCS.

Part: WIRE HARNESS — CHAFED (NR 1 ENGINE) · airframe 107,613 hrs · 16,604 cycles

NR 1 ENG FUEL FLOW FLUCTUATED CONSIDERABLY AFTER APPLYING TO TH RUST INSP WIRING FOUND MULTIPLE WIRES ON HARNESS CHAFFED. CONNECTOR W AS SECURED CHAFFED TO BACK SHELL OF CONNECTOR D11000. RETERMINATED W3510-034-20 AND W3510-302R-20 TO CONNECTOR D11000 AS SWPM 20-10-13. NEED TO PERFORM ENGINE RUN FOR INDICATION OPS CHECK. REF WDM 73-31-11. FOUND W3510-034-20 AND W3510-302R-20 RAN BOTH ENGINES AT VARIOUS SETTINGS. ALL INDICATIONS NORMAL AT THIS TIME.

Part: LIGHT — SHORTED (SEATS 21DEF) · airframe 102,667 hrs · 15,932 cycles

L/H AFT EMERGENY PATH LIGHT ASSEMBLY AT SEAT 21DEF IS SHORTED. RELAMPED 21DEF EMERGENCY PATH LIGHT ASSY-OPS CKS NORMAL

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 101,763 hrs · 15,802 cycles

EMERGENCY LIGHT AT RIGHT AFT LOWER FUSELEAGE IS INOPERATIVE. REPLACED THE LAMP, TESTED OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 101,763 hrs · 15,802 cycles

EMERGENCY LIGHT AT LEFT CEILING ROW 24 WAS INOPERATIVE. REPLACED THE LAMP. OPS CHECKED OK.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 101,763 hrs · 15,802 cycles

EMERGENCY LIGHT ROW 27AB CONNECTOR ON CEILING PANEL DAMAGED. INSTALLED A NEW CONNECTOR IAW SWP 20-61-00, AND WDM 33-51-13. OP CHECKED OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 101,362 hrs · 15,748 cycles

RIGHT SIDE EXTERNAL EMERGENCY LIGHT JUST FORWARD OF AFT CARGO DOOR IS INOPERATIVE. REPLACED THE LAMP, OPS CHECKED OK.

Part: UNKNOWN — ODOR (CABIN) · airframe 100,433 hrs · 15,618 cycles

ELECTRICAL ODOR AND SHORT-LIVED THUMPING SOUND EMANATING FROM THE AFT GALLEY FLOOR. AMM 25-33-00. OPS CK NORMAL OK TO CONTINUE.

Part: ROTARY ACTUATOR — TRIPPED (TE FLAP) · airframe 98,959 hrs · 15,411 cycles

ON FINAL APPROACH TRAILING EDGE DISAGREE. EMERGENCY DECLARED. FIM PROCEDURE 27-90-30 PERFORMED FOR TE FLAP DESAGREE, FDE TE DISAGREE INTERMITTENT INACTIVE FOUND, FSEU BITE PERFORMED IAW A MM 27-51-00-735 NO FAULT CONFIRMED, FLAP ASSY GENERAL VISUAL INSPECTION PERFORMED AND FLAP OPS TEST PERFORMED SEVERAL TIMES NO FAULT CONFIRMED. UPDATE 1/9/17: REPLACED NR 1 AND NR 7 ROTARY ACTUATORS (FOUND TRIPPED) IAW AMM 27-51-22 FOR FINAL FIX.

Part: GCU — FAULTY (E&E BAY) · airframe 98,552 hrs · 15,352 cycles

HEAVY SMOKE ODOR IN THE FLIGHT DECK ONLY, IMMEDIATELY FOLLOWED BY LOSS OF LEFT GEN AND BOTH UTILITY BUSES. FIRE DEPT REPORTED SEEING SMOKE COMING OUT OF E&E COMPT. NO EICAS MESSAGES REPORTED. APU STARTED AND DID NOT PICK LEFT BUS. SUSPECT A SHORT IN E&E. FOUND NR 1 ENG GCU BURNT. REMOVED AND REPLACED GCU AND IDG AND BPCU REF AMM 24-11-01 24-41-03 24-22-02. ALL OPS CHECK GOOD. IDG LEAK CHECK GOOD AND PERFORMED SMOKE OR ODOR IN THE FLIGHT DECK AND OR CABIN CONDITIONAL INSPECTIONS.

Part: FLAP SYSTEM — FALSE ACTIVATION (TE FLAP) · airframe 98,141 hrs · 15,290 cycles

TE FLAP DISAGREE MESSAGE. PERFORMED FLAP/SLAT ELEX UNIT, EMERGENCY DECLARED. BITE CHECKED IAW FIM 27-51 FT 809. NO EXISTING FAULTS DETECTED. EXTENDED FLAP/SLATS SEVERAL TIMES AND FAUL T DID NOT REPEAT. OK TO CONTINUE.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 97,657 hrs · 15,225 cycles

CABIN CENTER SEAT ROW 21 - 23, FLOOR PROXIMITY EMERGENCY LIGHT FOUND DIM. POWER SUPPLY M1209 REPLACED AND TEST CARRIED OUT NORMAL IAW AMM 33-51-07, AND 33-51-10.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 97,657 hrs · 15,225 cycles

CABIN SEAT 4D TO 6D FLOOR PROXIMITY EMERGENCY LIGHT FOUND DIM. CABIN EMER LT BATTERY PACK. REPLACED AND SEAT 4D TO 6D FLOOR PROXIMITY EMER LT TEST CARRIED OUT NORMAL AS PER AMM 33-51-07.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 97,657 hrs · 15,225 cycles

REF NR LP 6201534, 410-0058, B767-54-3-6017 NR 1 PYLON INBD PANEL 436BR CUTOUT SKIN FOUND CRACKED NR 1 PYLON INBD PANEL 436BR CUTOUT SKIN. REPAIRED IAW SRM 54-53-01, REPAIR 7, FIG 201.

Part: FLOOR SUPPORT — CORRODED (BS 1518) · airframe 97,657 hrs · 15,225 cycles

BS 1518 LBL 1, FLOOR SUPPORT FOUND CORRODED BS 1518 LBL 1. FLOOR SUPPORT REPAIRED IAW SRM 53-00-51 REPAIR 2 FIG 201

Part: BATTERY — DISCHARGED (CABIN) · airframe 96,589 hrs · 15,076 cycles

SEAT MOUNTED EMER EXIT LIGHTS INOPERATIVE FROM SEAT ROW 35 RT - 39 RT. REPLACED BATTERY AT M99804 IAW MM 33-51-07 PG 201. OPERATIONS CHECKED NORMAL.

Part: LIGHT — ARCED (CABIN) · airframe 96,322 hrs · 15,035 cycles

ON FINAL APPROACH LIGHT BURNING ODOR NOTED. SMOKE ALARM IN LAVATORY 2R WENT OFF, NO APPARENT FIRE. CAPTAIN STATES MID RT LAVATORY IS WHERE SMOKE DETECTOR ACTIVATED. INSPECTED LAVATORY WATER HEATER, LAVATORY ASSEMBLY, ASSEMBLY ELEC COMPONENTS FOR ANY SIGN OF DAMAGE, NONE FOUND. AREA ABOVE LAVATORY CHECKED, ALL OK. FOUND 1 LIGHT TUBE WITH END CAP DE-ATTACHED, VISUAL EVIDENCE OF ARCING & ELEC SMELL IN END CAP, BOTH TUBES REPLACED IAW AMM 33-26-00. ALL OPERATIONS OK.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 92,036 hrs · 14,458 cycles

LEFT AFT OVERWING EMER PATH LIGHT DIM. REPLACED LIGHT & LENS ASSEMBLY IAW BSWPM 20 - 30-11 & AMM 33-51-06. OPERATIONS CHECKED GOOD IAW AMM 33-51-06.

Part: FRAME — CRACKED (FUSELAGE) · airframe 92,036 hrs · 14,458 cycles

AFT PIT STATION 1197 AT APPROX RBL 32, FRAME WEB IS CRACKED. REMOVED DAMAGE AT FASTENER HOLE LOCATION. FABRICATED A REPAIR DOUBLER & FILLER IAW REO G18376 REV A & INSTALLED IAW ECRA 5310-06276.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 92,036 hrs · 14,458 cycles

CORROSION FOUND ON J CHORD AFT PIT FLOOR STRUCTURE STATION 1197 RBL 3 - 45. REMOVED DAMAGE BY REPLACING AFT PIT FLOOR J CHORD PN 146T1060 2 IAW SRM 51-40-02.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 92,036 hrs · 14,458 cycles

AFT LT EXTERNAL FUSELAGE SKIN REPAIR DOUBLER AT BS 1832.9 TO 1847.9 IS GOUGED. FOUND EXISTING DOUBLER TO BE OUT OF LIMITS. REMOVED REPAIR DOUBLER, FABRICATED A NEW DOUBLER & FILLER. INSTALLED IAW SRM 53-80-01.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 92,036 hrs · 14,458 cycles

AFT RT EXTERNAL FUSELAGE SKIN DOUBLER BS 1832.9 TO 1847 AFT OF RT HORIZONTAL STAB CUT OUT IS GOUGED. REMOVED SKIN DOUBLER, FABRICATED, DRILLED & LOCATED A NEW DOUBLER IAW SRM 53-80-01 REPAIR 3 FIG 201 DETAIL V SHEET 6 OF 7. INSTALLED IAW SRM 53-80-01 & 51-40-02

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 92,036 hrs · 14,458 cycles

AFT CARGO STATION 1197+110, LBL 10 - RBL 36 UPPER J CHORD HAS CORROSION UNDER NUTPLATES. UPPER J CHORD CORRODED BEYOND SRM LIMITS. REMOVED IAW SRM 51-40-02. RECEIVED NEW UPPER J CHORD PN 146T1061-1. LOCATED & DRILLED IAW SRM 51-40-05 & DWG 146T1228 REV A. INSTALLED IAW SRM 51-40-02 & DWG 146T1228 REV A.

Part: FLOORBEAM — MECHANIC ERROR (FUSELAGE) · airframe 92,036 hrs · 14,458 cycles

FLOORBEAM SINGLE FLANGE REPAIR AT BS 764, RBL 34 - 55 REQUIRES EVALUATION FOR PROPER NUMBER OF STRUCTURAL FASTENERS ON THE UPPER STRAP. EVALUATED PREVIOUS REPAIR STRAP & FOUND IMPROPER NUMBER OF FASTENER HOLES INSTALLED. R & R & FABRICATED A NEW REPAIR STRAP & ANGLE. MATERIAL ID FOR ANGLE IS 7075-T6 BAC 1490-2905 EXTRUSION & MATERIAL ID FOR 2 STRAP IS 7075-T6, 063 INCHES, & INSTALLED IAW SRM 53-00-51, REPAIR 2 & 51-40-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 92,036 hrs · 14,458 cycles

MAIN CABIN FLOOR STRUCTURE AT BS 847 & LBL 58, TRANSVERSE FLOORBEAM CORRODED, MID LAVATORY AREA. MATERIAL REMAINING AFTER CORROSION BLEND OUT EXCEEDED SRM 53-50-51. REMOVED DAMAGED FLOORBEAM SECTION, FABRICATED A NEW UPPER CHORD SECTION & INSTALLED IAW SRM 53-00-51 FIG 201 REPAIR 3, MATERIAL ID 1506-2066 7075-T73511 EXTRUSION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 91,884 hrs · 14,437 cycles

EMERGENCY ESCAPE PATH LIGHT L905 INOPERATIVE. EMER LIGHT REPLACED AT MID CROSS AISLE AT FWD COACH BULKHEAD L905 IAW MM 33-51-10.

Part: PIN — SHEARED (EVAC SLIDE) · airframe 90,931 hrs · 14,298 cycles

LEFT OVERWING SLIDE DOOR FWD ALIGNMENT PIN IS SHEARED OFF. REMOVED SHEARED PIN, PIN IS AOG.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,865 hrs · 14,290 cycles

3 EACH AREAS OF CORROSION FOUND AT STATION 1540 IN CTR OF BELLY NEXT TO BELLY DRAIN, JUST FWD & INBD OF OUTFLOW. ACCOMPLISHED REPAIRS AS NECESSARY IAW 5360-01370 & APPLICABLE SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 90,865 hrs · 14,290 cycles

CORROSION DAMAGE ON STRINGER 39R AT STATION 1540. CUT STRINGER TO REMOVED CORROSION DAMAGE

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 90,493 hrs · 14,244 cycles

RIGHT AFT LAVATORY SMOKE DETECTOR HAS NO POWER LIGHT. REPLACED SMOKE DETECTOR.

Part: WARNING SYSTEM — ACTIVATED (HYDRAULIC SYS) · airframe 90,078 hrs · 14,190 cycles

ON SHORT FINAL CTR HYD DEM EICAS CAME ON WITH GEAR SELECTED DOWN & FLAPS 20 SELECTED.

Part: HYDRAULIC LINE — LEAKING (NR 1 ENGINE) · airframe 89,504 hrs · 14,111 cycles

NR 1 ENG WHILE PERFORMING ENGINE RUN FOUND A HEAVY HYD FLUID LEAKING OUT OF LARGE DRAIN MAST. FOUND FAR AFT HYD SUPPLY LINE IN J BOX LOOSE, TIGHTENED LINE. LEAKED CHECKED GOOD & OPERATIONS CHECKED GOOD.

Part: WIRE — LOOSE (CABIN) · airframe 89,342 hrs · 14,087 cycles

DOOR 2L ARCING, RTFL. DUE TO LOOSE WIRING FOUND ON 115VAC SERVICE OUTLET AT DR 2L, REPLACED THE OUTLET.

Part: ISOLATION VALVE — FAULTY (BLEED AIR SYS) · airframe 88,774 hrs · 14,010 cycles

WHILE DOING SERVICE CHECK FOUND LT ISOLATION VALVE LIGHT ON. R & R LT ISOLATION VALVE. OPERATIONS CHECKED GOOD.

Part: COAX — DAMAGED (SATCOM) · airframe 88,772 hrs · 14,009 cycles

SATCOM INOPERATIVE BIT TEST SHOW STBD BSU FAIL LOW GAIN ONLY CIRCUIT BREAKER PANEL P11 H7, H9 PULLED & SAFE TIED. REMOVED & REPLACED STBD BSU IAW AMM 23-25-17, NO HELP. CHECKED FWD & AFT COAX CABLES FROM STBD BSU FOUND CENTER PIN PULLED THRU CONNECTOR AT POS NR 4, M1802 FWD CABLE ASSEMBLY. CAPPED & STOWED COAX AT POS NR 4.

Part: LIGHT — INOPERATIVE (SEAT 14B) · airframe 87,996 hrs · 13,917 cycles

SEAT 14B EMERGENCY LIGHT INOPERATIVE. EMERGENCY LIGHT ASSY REPLACED AND TESTED OK.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 87,996 hrs · 13,917 cycles

SEAT 32A, EMERGENCY LIGHT LENS CRACKED. EMERGENCY LIGHT ASSY REPLACED AND TESTED IAW AMM 33-51-001, TEST OK.

Part: LIGHT — FAULTY (SEAT 33A) · airframe 87,996 hrs · 13,917 cycles

SEAT 33A, EMERGENCY LIGHT DIM, EMERGENCY LIGHT ASSY REPLACED AND LIGHT TEST.

Part: LIGHT — INOPERATIVE (SEAT 39J) · airframe 87,996 hrs · 13,917 cycles

SEAT 39J, EMERGENCY LIGHT INOPERATIVE. EMERGENCY LIGHT ASSY REPLACED AND LIGHT TESTED.

Part: MICROPHONE — DEFECTIVE (COCKPIT) · airframe 87,787 hrs · 13,889 cycles

NR 3 BOOM MICROPHONE IS DEFECTIVE. UNABLE TO TRANSMIT ON 1ST OBS MICROPHONE. REPLACED MIC AT 1ST OBSERVERS SEAT AND TESTED.

Part: MOTOR — FAULTY (TE FLAPS) · airframe 87,755 hrs · 13,885 cycles

FLAPS WILL NOT MOVE ELECTRICALLY. LOWERED FLAPS IAW TASK 27-51-00-862-026, STEP 7 WITH HYDRAULICS. REPLACED ALTERNAT FLAP ELECTRIC MOTOR IAW AMM, UPPER MOUNT BOLT WITH GROUND WIRE IS WRONG PART. PERFORMED ECRA 2751-01436. PERFORMED SYS TEST IAW MM, NO FAULTS FOUND AT THIS TIME.

Part: TRANSMITTER — INACCURATE (HYD QTY) · airframe 87,612 hrs · 13,866 cycles

LEFT HYD QUANT FLUCTUATING BETWEEN 0-98% CHECKED LEFT HYD QTY AT LT PYLON 95 PERCENT. OK TO CONTINUE. REPLACED LEFT HYD QTY TRANSMITTER IAW AMM. SERVICED TO FULL. REINSTALLED SIGNAL WIRE AT P37 PANEL. OPS CK NORMAL.

Part: CIRCUIT CARD — FAULTY (POSIT 1) · airframe 87,477 hrs · 13,849 cycles

FWD EQIPMENT OVERHEAT ON EICAS AT 4000 FT AFTER TAKEOFF. REPLACED ECS FAN CONTROL CARD (M990) AND PERFORMED INSTALLATION TEST IAW MM 21-26-05-401. TEST OP CHECKED GOOD.

Part: CIRCUIT CARD — MALFUNCTIONED (E&E EXHAUST) · airframe 87,477 hrs · 13,849 cycles

LOW AIR FLOW AT E & E EXHAUST DUCT. REPLACED ECS FAN CONTROL CARD (M990) AND PERFORMED INSTALLATION TEST PER MM 21-26-05-401. TEST OP CHECKED GOOD.

Part: O-RING — LEAKING (HYD SYSTEM) · airframe 87,265 hrs · 13,821 cycles

NR 1 ENGINE HYD LEAK. REPLACED BAD O-RING UNDER DPI FOR EDP PRESSURE CASE DRAIN FILTER MODULE IAW AMM.

Part: CIRCUIT CARD — MALFUNCTIONED (DETECTION SYS) · airframe 87,215 hrs · 13,813 cycles

LOWER EICAS RT ENGINE OH LP 2 WILL NOT ERASE. REPLACED RT ENG AFLOTS CARD NR 2 M10274, NO STS MSGS, CONFIRM FIX AFTER ENG RUN REF MM ACCEL, DECEL TEST NR 4. STATUS MESSAGE "RT ENG OH LP 2" WAS STILL PRESENT BEFORE ENG RUN. WOULD NOT ERASE. ENG RUN WAS NOT DONE.

Part: MOTOR — FAILED (FLAP ALTERNATE) · airframe 87,215 hrs · 13,813 cycles

WHILE ACCOMPLISHING FLAP ALTERNATE POWER AND DRIVE TEST, IAW AMM 27-51-00. CIRCUIT BREAKER TRIPPED AT P6-4 D21 ALTERNATE FLAP MOTOR. SUSPECT MOTOR BAD. HEATS UP DURING START THEN BREAKER TRIPS. WIRE CHECKS, FOUND GOOD. T/E ALTERNATE MOTOR REMOVED. REPLACED T/E ALTERNATE FLAP DRIVE IAW MM, OPS CHECKED GOOD.

Part: RELAY — MALFUNCTIONED (THRUST REVERSER) · airframe 86,433 hrs · 13,716 cycles

LEFT THRUST REVERSER DID NOT DEPLOY ON LANDING. PERFORMED THRUST REVERSER OPS CHECK PER MM 78-31-00. LEFT ENG THRUST REVERSER OPERATES NORMAL, NO LEAKS. NO FAULTS ON TR RELAY MODULE. TROUBLESHOT SUSPECT LEFT THRUST REVERSER DEPLOY RELAY. REMOVED AND REPLACED LEFT THRUST REVERSER DEPLOY RELAY PER WDM 78-34-11. OPERATED THRUST REVERSER AGAIN NO FAULTS NOTED. PERFORMED MCDP TEST 30 PER MM 22-00-03, ALL TESTS PASSED, NO MESSAGES NOTED ACFT UPGRADED TO FULLY CAT CAPABLE.

Part: PUMP — FAULTY (HYDRAULIC SYS) · airframe 86,366 hrs · 13,708 cycles

CENTER HYD PUMP EICAS, RTFL REMOVED ADP CONTINUE WITH STEP 3 PAGE 408 OF MM. REPLACED ADP PER AMM. REPLACED HYD ELEC PUMP CTR 2 IAW MM. REMOVED NR 2 CNTR HYD ACMP. REPLACED CASE AND PRESSURE FILTERS AT FILTER MODULE. INSTALLED NR 2 CNTR HYD ELEC PUMP.

Part: ACTUATOR — FAULTY (LEFT) · airframe 86,312 hrs · 13,700 cycles

NEED TO REPLACE LEFT SIDE UPPER LCCA ACTUATOR. REPLACED LEFT HYD SYS LCCA AND ADJUSTED, OPS CHECKED GOOD.

Part: ACTUATOR — FAULTY (FLIGHT CONTROL) · airframe 86,312 hrs · 13,700 cycles

FLT CONTROLS BIND A LITTLE BIT AFTER A LEFT TURN WHEN RETURNING THE CONTROL TO CENTER. REPLACED LY HYD SYS LCCA (FOUND INPUT OUTPUT ROD OUT OF ADJUSTMENT).

Part: LIGHT — BROKEN (CABIN) · airframe 86,311 hrs · 13,699 cycles

SEAT 19B EMERGENCY LIGHT ON SIDE OF SEAT BROKEN. REPLACED LIGHT ASSY.

Part: LIGHT — BROKEN (CABIN) · airframe 86,311 hrs · 13,699 cycles

SEAT 21B EMERGENCY LIGHT ON SIDE OF SEAT BROKEN. REPLACED LIGHT ASSY.

Part: BEARING — BINDING (AILERON) · airframe 86,311 hrs · 13,699 cycles

DURING FLT CONTROL CHECK, FELT BINDING AND HANG UP WHEN FULL CONTROL WHEEL TO THE LEFT. REPLACED AILERON CAM FOLLOWER BEARING.

Part: TOILET — CLOGGED (LAVATORY) · airframe 86,309 hrs · 13,698 cycles

AFT LEFT LAV OVERFLOWING. REMOVED DEBRIS AND UNCLOGGED LAV, OPS CHECKS OKAY.

Part: UNKNOWN — BINDING (FLIGHT CONTROL) · airframe 86,289 hrs · 13,696 cycles

CREW REPORTS DURING FLIGHT CONTROL CHECK TO THE LEFT, CONTROL WHEELS BINDS AND IS SLOW TO RETURN. WORKS NORMALLY TO RIGHT TURN. FLAPS DOWN OR UP. HYD PRESS AND INDICATIONS NORMAL. OPERATED ALL FLIGHT CONTROLS SEVERAL TIMES AND OPERATION FOUND SMOOTH AND NORMAL BOTH WAYS. CABLES IN WHEEL WELLS AND NO OBSTRUCTIONS FOUND.

Part: STATOR VANE — DAMAGED (NR 2 ENGINE) · airframe 86,152 hrs · 13,677 cycles

NR 2 ENGINE STATOR VANE AT 11:30 POS MISSING CHUNK OF LEADING EDGE. REF AMM 72-33-02 DAMAGE STATOR MEASURES BETWEEN .250 AND.500"AXIAL LENGTH" WITHIN LIMITS TAPED AS REQ OK FOR SERVICE.

Part: STATOR VANE — DAMAGED (NR 1 ENGINE) · airframe 86,152 hrs · 13,677 cycles

NR 1 ENGINE STATOR VANE AT 11:30-12:00 POS MISSING CHUNK OF LEADING EDGE REF AMM 72-33-02, DAMAGE STATOR MEASURES BETWEEN .250 AND .500 "AXIAL LENGTH" TAPED AS REQ OK FOR SERVICE.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 86,148 hrs · 13,675 cycles

AT DEPARTURE, CREW REPORTS SMOKE IN CABIN. FIRE DEPARTMENT FOUND NO HOT SPOTS. TROUBLESHOOTING SMOKE IN CABIN CAUSED BY APU, NEED TO REPLACE RECIRCULATION FILTERS.

Part: SCREW — MISSING (NACELLE PANEL) · airframe 86,075 hrs · 13,663 cycles

FOUR SCREWS MISSING FROMM ONE PANEL ON LEFT ENGINE PYLON INBD SIDE ABOVE ENGINE. INSTALLED MISSING SCREWS ON PANEL OK TO CONTINUE.

Part: SLIDING WINDOW — OUT OF ADJUST (COCKPIT) · airframe 86,059 hrs · 13,661 cycles

CAPTAIN'S WINDOW BINDING. ADJUSTED CAPTAIN'S SLIDING WINDOW, OPS CHECKED GOOD.

Part: AUTOPILOT SYS — INOPERATIVE (LEFT) · airframe 85,961 hrs · 13,648 cycles

AUTOPILOT ASA DISPLAYED NO LAND 3 WITH F-D ON. LEFT AUTO PILOT INOPERATIVE.

Part: COMPUTER — FAILED (POSIT 1) · airframe 85,961 hrs · 13,648 cycles

LEFT FCC FAILURE MESSAGE. REPLACED LEFT FCC, OPS CHECKED GOOD.

Part: COUPLER — DAMAGED (HF SYSTEM) · airframe 85,959 hrs · 13,647 cycles

LEFT HF INOPERATIVE. REPLACED NR 1 HF COUPLER REF AMM.

Part: COUPLER — WEAK (HF COMM) · airframe 85,912 hrs · 13,637 cycles

HF TRANSMISSION AND RECEPTION ARE INOP, WEAK, GARBLED INTERMITTENT, ETC. AT ALL CREW STNS.(1 = L HF, 2 = R HF). HF1 WILL NOT TRANSMIT IN FLIGHT, TESTED OK ON THE GROUND. RECEPTION IS NORMAL PROG TEXT: ACCOMPLISH CHRONIC REVIEW, HAS HISTORY. TUNE CYCLE TAKES FROM 15-25 SECS 130138 SHOULD TAKE 4-7 SECS. SUSPECT COUPLER AT FAULT. PCN 530-9045. REMOVED AND REPLACED LEFT HF COUPLER. HF SYSTEM REQUIRES OPS CHECK IAW MM. ACCOMPLISHED CHECK PER MM, CHECKS GOOD.

Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 85,851 hrs · 13,629 cycles

CREW REPORTS OIL SMELL IN FWD CABIN AND FLT DECK AREA IN FLT. ODOR SEEMED TO DISSIPATE WITH LEFT PACK SELECTED OFF. NO SMOKE REPORTED. MAINT TEXT: PER SMOKE ODOR QUESTIONARE-PILOT REPORTS SWEET BURN SMELL MORE LIKE DE-ICING FLUID, OR HYD FLUID THAN FUEL. SOME IMPROVEMENT WITH LEFT PACK OFF. SMELL RETURNED STRONGER DURING DESCENT WITH SAME LEFT PACK OFF CONFIG REF AMM 21-00-00-0200A AND 21-00-21. VISUALLY INSPECTED APU, BOTH ENGINES AND ASSOCIATED DUCTING. RAN APU AND BOTH ENGINES WITH BOTH PACKS ON FULL WARM. SMELL DISSIPATED AFTER ABOUT 45 MINUTES. OK FOR SERVICE.

Part: HEAT EXCHANGER — FAULTY (RT ENGINE) · airframe 85,834 hrs · 13,626 cycles

RIGHT ENGINE EEC C1 STATUS MSG. REMOVED AIR OIL HEAT EXCHANGER AND VALVE ASSY IAW MM 79-21-09 UP TO AND INCLUDING STEP 2 F(5) OF PAGE 404. NEED TO COMPLETE FROM STEP 3 OF PAGE 404 TO END. COMPLETED INSTALLATION EXCEPT FOR 1 SET OF LINE CLAMPS AT 6 O'CLOCK POSITION AND DUCT PANEL. COMPLETED INSTALLATION IAW REF AMM-79-21-09.

Part: GUARD — MISSING (COCKPIT) · airframe 85,781 hrs · 13,618 cycles

CENTER ISOLATION VALVE SWITCH COVER MISSING. REPLACED SWITCH GUARD.

Part: SKIN — DENTED (BS 379 S21-22L) · airframe 85,731 hrs · 13,611 cycles

FUSELAGE DENTED AT BS 379 S21-22L. INSTALLED DOUBLER REPAIR IAW ECRA 5311-01574 & REO-G15687, REV C.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 85,731 hrs · 13,611 cycles

AFT FUSELAGE INTERNAL BULKHEAD T-CHORD CRACKED AT BS 1809.5, LBL 27. MAJOR REPAIR ACCOMPLISHED: FABRICATED A -1 AND -2 ANGLE WITH FILLER AND REPAIRED HORIZONTAL INNER CHORD PER SRM 53-80-08, REPAIR 10.

Part: GUIDE VANE — MISSING (NR 1 ENGINE) · airframe 85,637 hrs · 13,596 cycles

NR 1 ENGINE INLET GUIDE VANE MISSING AT 6 O'CLOCK POSITION. FOUND 1 VANE MISSING AT THE 6 O'OCLOCK POSITION OK TO CONTINUE TO THE NEXT ENGINE SHOP VISIT REF MM-72-33-02.

Part: UNION — LOOSE (RT MLG WW) · airframe 85,605 hrs · 13,592 cycles

WHEEL WELL HYDRAULIC LEAKS. FOUND RIGHT WHEEL WELL FLAP SLAT SHUTOFF VALVE MODULE LEAKING AT THE FLAP PRESSURE PORT LINE UNION. FOUND UNIONS (5)(7) LOOSE, REPLACED PACKING ON BOTH UNIONS.

Part: EEC — FAULTY (NR 1 ENGINE) · airframe 85,530 hrs · 13,581 cycles

STATUS MSGL ENGIINE EEC C1 MAINT TEXT: CREW REPORT PROBLEM ON LEFT ENGINE. BITE CHECK OF PIMU SHOWED EEC CHANNEL A AOC FD-BK FAIL AND EEC CAT 1 CH A AND B. REF PIMU MSG INDEX PAGE 600, MSG NUMBER 351-28 FOR TROUBLESHOOTING INFO DEACTIVATED VALVE IN OPEN POSITION PER MEL CARD 75040. PLUG DISCONNECTED AND SAFTIED AND PLACARD PLACED ON LOWER EICAS. REPLACE NR 1 AIR OIL HEAT EXCHANGER AND VALVE ASSY. REPLACED PER AMM 79-21-09 THROUGH 3 (E), CONTINUE WITH 3(F) PUT AIRPLANE BACK TO ITS USUAL CONDITION. ACCOMPLISHED 3F THROUGH THE END CHECKS OKAY.

Part: PRESSURE SWITCH — FAULTY (HYDRAULIC SYS) · airframe 85,530 hrs · 13,581 cycles

RIGHT ENGINE ELEC HYD DEMAND PUMP DID NOT COME ON IN AUTO OK IN ON POSITION. REF SSM 29-00-03 SHT 1 JUMPERED SWITCH S31 PINS 3 AND 2 AND PUMP OPERATES NORMALLY IN AUTO. REQUIRES SWITCH S31 PCN 481-0076 AND SEAL 750-5644. PUMP AND SYSTEM PRESSURE LT OPS NORMAL. SHOULD STATE PUMP OPS NORMAL IN ON POSITION. DF STICKER PLACED ON ELEC DEMAND PUMP SWITCH. REMOVED AND REPLACED RT ENGINE HYD LOW PRESS SWITCH S31 PER AMM. OPS AND LEAK CHECK STILL NEEDS TO BE ACCOMPLISHED. ALSO SEE DF648 SHT 1 JUMPERED SWITCH S31 PINS 2 AND 3 AND LT OPERATED NORMAL. SUSPECT S31 PCN 481-0076 AND SEAL 750-5644 AT FAULT. COMPLIED WITH MEL. PUMP OPERATED NORMALLY AND SYSTEM PRESSURE LT OPS NORMAL.

Part: CONNECTOR — DAMAGED (HYD PUMP) · airframe 85,530 hrs · 13,581 cycles

RT ENG HYD PUMP LOW PRESSURE LIGHT OUT WHEN RT ELEC DEMAND PUMP IS IN THE AUTO OR ON POSITION, PUMP OPERATION NORMAL. JUMPERED SWITCH S31 PINS 2 AND 3 AND LT OPERATED NORMAL. SUSPECT S31 PCN 481-0076 AND SEAL 750-5644 AT FAULT. PUMP OPERATED NORMALLY AND SYSTEM PRESSURE LT OPS NORMAL.

Part: OIL COOLER — FAULTY (NR 1 ENGINE) · airframe 85,538 hrs · 13,582 cycles

STATUS MSGL ENG A-O VALVE. CREW REPORT PROBLEM ON LEFT ENGINE SEE DF647 BOTH ITEMS RELATED. BITE CHECK SHOWS EEC CH A AOC FD-BK FAIL. AOC VALVE DEACTIVATED PER MEL CARD 75040. VALVE IN OPEN POSITION AND PLUG DISCONNECTED AND SAFTIED. DF PLACARD PLACED ON LOWER EICAS. ABOVE DEACTIVATION FOR DF646. DF646 AND DF647 NEED TO BE WORKED CONCURRENTLY DUE TO THIS CAT 1 FAULT CAUSED BY DF646.

Part: WIRE HARNESS — FAULTY (NR 2 ENGINE) · airframe 85,507 hrs · 13,578 cycles

NEED IDLE RUN TO VERIFY EGT OPS DUE TO W-6 HARNESS REPLACEMENT ON NR 2 ENGINE NR 2 ENGINE EGT, OPS CHECKS OK.

Part: GENERATOR — FAULTY (APU) · airframe 85,381 hrs · 13,562 cycles

APU GENERATOR FIELD OFF. REPLACED APU GENERATOR PER MM.

Part: FILL PORT — STRIPPED (O2 SYSTEM) · airframe 85,029 hrs · 13,514 cycles

CREW O2 BOTTLE FILL PORT HAS STRIPPED THREADS. REPLACED FILL PORT.

Part: DISPLAY — FAILED (SATCOM) · airframe 84,772 hrs · 13,481 cycles

SATCOM STATUS ON LINK STATUS PAGE NO COMMS. SATCOM FAILURE DOES NOT DISPLAY SATCOM LOSS, EICAS MESSAGE SATCOM FAILED AFTER RESETTING CIRCUIT BREAKERS, ACCOMPLISH REVIEW. REPLACED SATCOM DISPLAY UNIT PER MM. GROUND CHECKED NORMAL.

Part: TRAY — WARPED (SAT COM) · airframe 84,757 hrs · 13,479 cycles

SATCOM INOPERATIVE. FOUND PLASTIC COOLING TRAY FOR SAT SDU WARPPED. REPLACED TRAY AND SEAL PCN 160-7204 REF IPC 25-71-41. RETURNED SDU, RFU HGA AND LGA ACCOMP TEST MM23-27-00. NO OTHER ISSUES NOTED. STILL REQUIRES VOICE TEST.

Part: COVER — OUT OF TOLERANCE (EMERGENCY LIGHT) · airframe 84,757 hrs · 13,479 cycles

EMERGENCY LIGHT LENS ABOVE SEAT 2A DAMAGED. REPLACED LENS COVER.

Part: STRUCTURE — DELAMINATED (LT NACELLE) · airframe 84,757 hrs · 13,479 cycles

LEFT ENGINE UPPER PYLON PANEL NOT FLUSH. PANEL FARING MID SECTION FIBERGLASS IS DELAMINATING ON THE FWD LEADING EDGE.

Part: PANEL — DAMAGED (LT NACELLE) · airframe 84,757 hrs · 13,479 cycles

LT ENGINE UPPER PYLON PANEL NOT FLUSH. REPAIRED PANEL IAW ECRA 5430-01932 & SRM 54-53-70.

Part: ENGINE — SURGES (NR 2) · airframe 84,734 hrs · 13,476 cycles

ECM DETECTED A 'SILENT' SURGE (NO CREW GRIPE) AT OR NEAR TOP OF DESCENT AT LOW POWER. THIS IS A RING CASE ENGINE. ACCOMPLISHED PRECAUTIONARY VISUAL CHECKS OF INLET AND EXHAUST AS WELL AS 2.5 BLEED AND 2.9 BLEED OPENINGS FOR DMG OR UNUSUAL MATERIAL. CONFIRM 2.5 BLD NOT DISCONNECTED REF MM71-08-00 FIG 110 CK 10 SHT 2. CK IP CK VALVE REF MM36-11-06 P6XX (IF NEC PCN 643-9217 REF MM36-11-06 PG4XX) AND RELATED DUCTING. CK PIMU FOR RELATED MSGS CK AND COPY OR PRINT EICAS EPCS, PERF PAGES AND EXCEEDANCE PAGE (IF ANY). ACCOMPLISHED EM3514-2 ENG CHECK AS ASSOSIATED MM REF ALL CHECKS OK NO FAULTS NOTED DATA SENT TO ENGINEERING.

Part: OXYGEN MASK — DAMAGED (COCKPIT) · airframe 84,598 hrs · 13,461 cycles

FIRST OFFICERS O2 MASK PRESS TO TEST SWITCH STICKS ON AND O2 CONTINUES TO FLOW. REMOVED AND REPLACED FIRST OFFICER 02 MASK AS PER MM, OPS CHECKED GOOD.

Part: BRAKE — FIRE (MLG) · airframe 84,533 hrs · 13,452 cycles

NR 6 BRAKE FIRE REPORTED. ACCOMPLISHED INSPECTION AND CLEAN UP REF ECRA 0551-01032. NO DAMAGE NOTED. WHEEL ASSY'S 1 ,2, 5 AND 6 REPLACED REF AMM 32-45-01. BRAKE ASSY'S 5 AND 6 REPLACED.

Part: ACTUATOR — LEAKING (RUDDER) · airframe 84,522 hrs · 13,450 cycles

DURING WALK AROUND, MECH NOTICED SIGN OF HYD LEAK FROM APU ACCESS DOOR. ON REMOVAL OF RUDDER ACCESS PANEL, FOUND LOWER PCA LEAKING AT THE ACTUATOR STATIC SEAL. THE LEAK IS APPROX 5 DROP PER MIN AND FOUND WITHIN LIMITS IAW AMM.

Part: AMPLIFIER — FAULTY (NR 1 SATCOM) · airframe 84,258 hrs · 13,415 cycles

SATCOM SYSTEM INOPERATIVE. REPLACED SDU, OPS NORMAL. SATCOM STARTED WORKING AGAIN. REPLACED HIGH POWER AMPLIFIER (LGA).

Part: ADC — FAILED (NR 2) · airframe 84,173 hrs · 13,404 cycles

ADC MECHANICAL ISSUE, FLIGHT DIVERTED. CREW REPORTED AT FL370 FIRST OFFICER'S AIR DATA FLAGS IN VIEW AND THE RUDDER RATIO FAILED. SWITCHED TO FIRST OFFICERS ON STBY AND REGAINED AIR DATA INFO BUT THE RUDDER RATIO IS INOPERATIVE. RT ADC FAIL INDICATOR IN VIEW ON ARRIVAL. TEST 30 CURRENT FAULTS INDICATED RT ADC FAILURE. REPLACED RT ADC PER MM AND ACCOMPLISHED CURRENT FAULT TEST PER MM. NO CURRENT FAULTS NOTED. ACCOMPLISHED RUDDER RATIO CHECKS PER MM, ALL INDICATIONS NORMAL.

Part: RFU — INOPERATIVE (SATCOM) · airframe 83,965 hrs · 13,379 cycles

SATCOM INOPERATIVE. REPLACED RADIO FREQ UNIT.

Part: FEEDER CABLE — SHORTED · airframe 83,965 hrs · 13,379 cycles

F/A SMELLED AN ELECTRICAL ODOR. NOTICED ODOR IN COCKPIT. FOUND PIGTAIL CONNECTOR AT LOCATION P53 LOOSE. REPLACED PIGTAIL.

Part: COMPUTER — FAULTY (AUTOPILOT) · airframe 83,530 hrs · 13,321 cycles

CENTER AUTOPILOT WILL NOT ENGAGE AND FIRST OFFICER FLT DIRECTOR BARS LOST WHEN CENTER FLT DIRECTOR ENGAGED. CENTER FCC INOPERATIVE. REPLACED CENTER FLIGHT CONTROL COMPUTER AS PER AMM. OPS CHECKED NORMAL. ALSO ACCOMPLISHED AUTOPILOT FLIGHT CONTROL TEST AS PER AMM. OPS CHECKED NORMAL.

Part: COMPUTER — FAULTY (AUTOTHROTTLE) · airframe 83,530 hrs · 13,321 cycles

AUTO THROTTLE DISCONNECTED ON SEVERAL OCCASIONS AND UNABLE TO STAY IN ARMED POSITION. REMAINDER OF FLT FLOWN WITH AUTOTHROTTLE OFF. REPLACED THRUST MANAGEMENT COMPUTER AS PER AMM. OPS CHECKED NORMAL.

Part: STARTER — FAULTED (APU) · airframe 83,482 hrs · 13,316 cycles

AFTER LANDING APU WOULD NOT START. THREE ATTEMPTS MAX EGT 777 N40. PRIOR START IN AIR WAS OK. CLEANED CONNECTORS AT IGV, FCU & FUEL FLOW DIVIDER & SOLENOID VALVE PER AMM & MM(S) RESPECTIVELY, CHECKED ALL MAG CD'S PER MM. FOUND CLEAN AND REPLACED APU STARTER MOTOR. REPLACED FUEL FLOW DIVIDER VALVE ASSY. OPERATED APU SEVERAL TIMES PER JRH 2-6-15, OPS NORMAL.

Part: STATOR VANE — DAMAGED (LT ENGINE) · airframe 83,046 hrs · 13,255 cycles

LEFT ENGINE, FOIL COMING OFF OF STATOR VANE. FOUND TAPE REPAIR COMING OFF OF LEADING EDGE. APPLIED TAPE. REPAIRED PER AMM.

Part: WARNING LIGHT — ILLUMINATED (GENERATOR) · airframe 82,793 hrs · 13,222 cycles

CREW ABORTED TAKEOFF AT 78 KTS DUE TO GENERATOR DRIVE LIGHT AND ASSOCATED EICAS MESSAGE. CREW REPORT 6 BRAKES WENT TO "6" THEN DOWN TO '4' BY END OF TAXI BACK TO GATE. WEIGHT WAS 383K, OAT 9DEG C, 1500' PRESS ALT. CONDITIONAL INSPECTION CARRIED OUT SATISFACTORY IAW AMM 05-51-14. NO DAMAGE EVIDENT.

Part: HYDRAULIC LINE — LEAKING (LT MLG) · airframe 82,603 hrs · 13,197 cycles

UNABLE TO RETRACT L MLG, RTFL L MLG EXTENSION RETRACTION LINE LEAKING HYDRAULIC FLUID. REPLACED LINE LEAK CHECK OK WITH LANDING GEAR DOWN AND LOCKED GEAR PINNED AND HANDLE CYCLED. NEED TO JACK AND SWING LANDING GEAR AND CHECK FOR LEAKS IN LT MLG. ACCOMPLISHED GEAR RETRACTION AND EXTENSION, FOUND OPERATION NORMAL.

Part: SEAL — LEAKING (RUDDER PCA) · airframe 82,599 hrs · 13,195 cycles

DURING WALKAROUND, FOUND HYD LEAKING DOWN BOTH SIDES OF TAIL COMPT. CYCLED RUDDER, FOUND UPPR RUDDER PCA LEAKING OUT OF FWD SHAFT SEAL. REMOVED UPPER RUDDER PCA. SHOP REPAIRED ACTUATOR BY REPLACING FWD SHAFT SEALS. WORKING INSTALL.

Part: UNION — LEAKING (HYD LINE) · airframe 82,352 hrs · 13,163 cycles

NR 1 ENG HYDRAULIC LEAK FROM DRAIN. ACCOMPLISHED AMM 71-71-00 P61, HYDRAULIC LEAK IN LT PYLON VIA STRUT DRAIN FROM CTR MOUNT DRAIN LINE. AREA CHECKED. FOUND UNION OF LT HYDRAULIC SYSTEM BETWEEN HYDRAULIC BAY AND PYLON LEAKING UNION RETIGHTENED AND LEAK CHECK PERFORMED. NO MORE LEAK.

Part: PUMP — UNKNOWN (NR 2 ENGINE) · airframe 82,219 hrs · 13,145 cycles

NR 2 ENG FUEL PUMP REPLACEMENT.

Part: RUB STRIP — LOOSE (NR 2 ENGINE) · airframe 82,170 hrs · 13,139 cycles

NR 2 ENG RUB STRIP LOOSE LEADING EDGE OF REV COWL. INTERIM REPAIR ACCOMPLISHED PER ECRA 7111-01296. CLEANED AREA WITH SOLVENT PER GPM. APPLIED 3 LAYERS OF ALUMINUM TAPE 2524-2-0200 TO DISCREPANT AREAS. TAPE TO BE RE-INSPECTED EVERY 25 HOURS BEGINNING PTT 82195 AND TO BE PERMANENTLY REPAIRED WITHIN 75 FLT HOURS OR BY PTT 82245. ** MF8627 CREATED TO MONITOR **

Part: COMPUTER — FAULTY (RIGHT) · airframe 81,990 hrs · 13,115 cycles

R EICAS CMPTR STATUS. REPLACED RT EICAS COMPUTER. DOWNLOADED DATA PER MM. OPS CKS OKAY.

Part: ACTUATOR — FAULTY (AILERON) · airframe 81,973 hrs · 13,112 cycles

AILERON LOCK-OUT, RTFL. REPLACED RIGHT AND LEFT AILERON LOCKOUT ACTUATORS REF MM. LOCKOUT ACTUATOR AND MECHANISM TEST GOOD ON RIGHT AND LEFT SIDE.

Part: RUB STRIP — DAMAGED (THRUST REVERSER) · airframe 81,633 hrs · 13,065 cycles

NR 2 ENG O/B REV RUBSTRIP DAMAGED AND LOWER GUIDE CHANNEL WORN. REPLACED NR 2 ENG OTBRD REV RUBSTRIP. WAITING ON GUIDE CHANNEL ON AOG. REPLACED NR 2 ENGINE OUTBOARD GUIDE CHANNEL. GUIDE CHANNEL REQUIRES SEALANT APPLICATION.

Part: ACTUATOR — UNKNOWN (AILERONS) · airframe 81,624 hrs · 13,064 cycles

AILERON LOCKED LIGHT ON AT HIGH SPEED. EICAS MESSAGE AILERON LOCKOUT DISPLAYED. OUTBD AILERONS INDICATED NORMAL - LOCKED OUT. ANNUNCIATION DISPLAYED FOR APPROX 10 SECONDS. ACCOMPLISHED FIM 27-11-00 F104 AND FAULT BALLS FOR 'ADC' ON RIGHT SAM AND 'R AIL LOCK ACT' ON LEFT SAM BOTH RESET. ACCOMPLISHED FUNCTIONAL TEST OF AILERON LOCKOUT REF MM AND ALL OPS AND INDICATIONS GOOD, NO FAULT BALLS PRESENT. DUE TO PREVIOUS HISTORY OF AILERON LOCK EICAS MESSAGES REPLACE BOTH LT AND RT AILERON LOCK ACTUATORS PCN 563-9035 REF MM 27-11-44 OPBLM HANN DEC 18, 2011.

Part: FAIRING — MISSING (NR 2 ENGINE) · airframe 81,049 hrs · 12,990 cycles

NR 2 ENGINE MID SPAN SHROUD PANEL MISSING AT THE 8 O'CLOCK POSITION. INSTALLED MISSING INTERMEDIATE CASE FAIRING AT THE 8 O'CLOCK POSITION AS REQUIRED.

Part: FAIRING — DAMAGED (TE FLAP) · airframe 81,049 hrs · 12,990 cycles

RIGHT WING INBD MID FLAP FAIRING DAMAGED FROM ENGINE MID SPAN SHROUD. DAMAGE MEASURES APPROX 4" IN LENGTH BY 2.5" IN WIDTH. DAMAGE GOES INTO THE HONEYCOMB. REMOVED MID FAIRING AND AFT FAIRING PER CDL 57H. MID FAIRING IN ORD MM SHEETMETAL SHOP FOR REPAIRS AND AFT FAIRING IN SMC OFFICE. COMPLETED REPAIRS, PRIMED PAINTED AND RE-INSTALLED. CYCLED FLAPS, OPS CHECKS GOOD.

Part: TUBE — UNKNOWN (NR 2 ENGINE) · airframe 81,006 hrs · 12,983 cycles

NR 2 ENG DRAIN SYS TUBES ARE REMOVED FROM BOTH SIDES OF THE J-BOX AND SECTION OF RT SIDE. INSTALLED REMOVED TUBES.

Part: TUBE — OBSTRUCTED (NR 2 ENGINE) · airframe 81,006 hrs · 12,983 cycles

NR 2 ENG DRAIN SYS TUBES FROM J-BOX BOTH LEFT AND RIGHT SIDES ARE OBSTRUCTED. REPLACED OBSTRUCTED TUBES.

Part: CIRCUIT CARD — FAILED (SCC) · airframe 80,632 hrs · 12,932 cycles

AFTER EXTERNAL POWER PULLED, "EICAS SCC" STATUS MESSAGE DISPLAYED AND WILL NOT ERASE. REPLACED EICAS SCC CARD PER MM.

Part: WINDOW — SCRATCHED (COCKPIT) · airframe 80,626 hrs · 12,929 cycles

CAPTAIN'S NR 1 WINDOW IS SCRATCHED AND IS UNSERVICEABLE. VISIBILITY AFFECTED. REMOVED & INSTALLED WINDOW PER MM.

Part: LAMP — INOPERATIVE (SQUIB TEST) · airframe 80,590 hrs · 12,924 cycles

LEFT SQUIB TEST INOPERATIVE. RELAMPED AND CYCLED SWITCH, TEST NORMAL.

Part: PRESSURE SWITCH — FAULTY (APU) · airframe 80,277 hrs · 12,881 cycles

APU AUTOSHUTDOWN ON THE GROUND. REPLACED GEN OIL PRESSURE DIFFERENTIAL SWITCH PER MM, OPS NORMAL.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 80,224 hrs · 12,874 cycles

ELECTRICAL SMELL IN COCKPIT, FLIGHT DIVERTED. CREW REPORTED INTERMITTENT ELECTRICAL ODOR IN FLT DK. UTILITY BUSSES TURN OFF, ACFT DIVERT TO KEF. CK'D WINDOW HEAT TERMINALS FOR ANY DISCREPENCIES. NONE NOTED. CHECKED AND OPERATED RECIRC FANS FOR ANY DISCREPANCIES OR ODORS, NONE NOTED. OPERATED EQUIPT COOLING SYSTEM. NO ODORS NOTED. CREW REPORTED FOOT AND SHOULDER HEAT OFF AT TIME OF REPORTED ODOR. CHECKED FLIGHT DECK AND E AND E COMPARTMENT FOR ANY TRIPPED CIRCUIT BREAKERS OR ODORS. NONE NOTED. (NFF)

Part: INDICATOR — FAULTY (ADI) · airframe 80,172 hrs · 12,867 cycles

FLT CREW REPORTING CAPT ADI BLANKING OUT, SWITCH TO ALT POSITION AND ADI ERRATIC. CAPT HSI ALL NORMAL. REPLACED THE CAPT'S EADI. INDICATIONS OK IN NORMAL AND ALTERNATE.

Part: HEAT SHIELD — FAILED (NR 2 ENG OIL) · airframe 79,947 hrs · 12,837 cycles

NR 2 ENG OIL TANK HEAT SHIELD HAS DETERIORATED. REPLACED HEAT SHIELD.

Part: MONITOR — DEFECTIVE (HYDRAULIC SYS) · airframe 79,947 hrs · 12,837 cycles

HYDRAULIC QUANTITY MONITOR UNIT NEEDS REPLACEMENT. REPLACED HYD QTY MONITOR.

Part: ACTUATOR — LEAKING (NR 1 ENGINE) · airframe 79,895 hrs · 12,829 cycles

NR 1 ENG VSV ACT HAS HISTORY OF FLUID LEAKS. NEED TO REPLACE THE VSV. REPLACED PER MM.

Part: TRANSMITTER — FAILED (HYD SYSTEM) · airframe 79,887 hrs · 12,826 cycles

LEFT HYD QTY INDICATION. REPLACED LT HYD QTY TRANSMITTER AMM 29-33-02. R AND E WORKING SIGNAL WIRE OF PTU. AFTER TRANSMITTER WAS REPLACED FOUND DIODE BLOCK R397 WITH BRUNDY TERMINAL JAMMED IN POSITION "C". WIRE TO POSITION "C" WAS BROKEN OFF AND TIED BACK. SUGGEST REPLACED DIODE BLOCK AND RE-PIN WIRE. BLK-563-1685 OR 540-0004 123076 CONTACT PCN-585-0047 OR 585-1581 OR 562-6048. PARTS NIS ORD. 26JUL ORD INF- :DIODE 561-1804 LOB IN CKPIT. 26JUL ORD INF- :CONNECTOR 585-1581 ALSO LOB'D.

Part: WARNING LIGHT — ILLUMINATED (LT HYD QTY) · airframe 79,887 hrs · 12,826 cycles

LEFT HYD QTY INDICATION.

Part: FILTER — DEFECTIVE (APU) · airframe 79,947 hrs · 12,837 cycles

APU AUTO SHUTDOWN THREE TIMES. APU INOP GENERATOR FILTER FAULT. REPLACED LUBE AND GENERATOR SCAVENGE OIL FILTER PER MM. ALSO SERVICED OIL, ADDED 1 QT. RAN APU AND LEAK CHECKED FILTER, NO LEAKS NOTED. RAN APU FOR 45 MIN. APU DID NOT AUTO SHUTDOWN.

Part: ACTUATOR — MALFUNCTIONED (RUDDER) · airframe 79,393 hrs · 12,749 cycles

RUDDER OUT OF RIG 5 UNITS TO LEFT. WORKING RDR RIG. MEASURED RUDDER ACTUATOR INDEX POSITIONS FOR LEFT, CENTER AND RIGHT HYDRAULIC SYSTEMS. WHEN ALL SYSTEMS PRESSURIZED, INDEX IS SLIGHTLY TO THE LEFT OF PLATE. WHEN RIGHT SYSTEM PRESSURIZED ONLY, RUDDER TRAILING EDGE IS 1.468" RIGHT OF INDEX. CENTER SYSTEM PRESSURIZED ONLY, RUDDER TRAILING EDGE IS 0.39" TO LEFT OF INDEX. LEFT SYSTEM PRESSURIZED ONLY, RUDDER TRAILING EDGE IS CENTER RUDDER PCA (LEFT SYSTEM). OPERATIONAL TESTS NORMAL. BOTH UPPER AND LOWER RUDDER PCAS WITHIN LIMITS AND OPS TESTED NORMAL.

Part: HEAT SHIELD — DETERIORATED (NR 2 ENGINE) · airframe 79,359 hrs · 12,744 cycles

NR 2 ENG, OIL TANK HEAT SHIELD DETERIORATED. REPLACED NR 2 ENG OIL TANK HEATSHIELD.

Part: ACTUATOR — LEAKING (RUDDER) · airframe 79,222 hrs · 12,723 cycles

L HYD LOW ON TAXI IN RF .63 INDICATED. FOUND CENTER RUDDER PCA LEAKING ACTUATOR. APPLIED SEALANT ON THE ACTUATOR. LEAKING 26 DROP PER MN WITHIN LIMITS AS PER AMM. OK TO CONTINUE. ACCESS PANEL 324JL.

Part: CONNECTOR — UNSECURE (AC PACK) · airframe 79,055 hrs · 12,698 cycles

RT PACK TRIPPED OFF AT GATE WHILE ON APU. SECURED CONNECTOR ON R PACK CPRSR OUT OVHT, OPS CHECKS OKAY. CLEANED CONNECTORS TO 490 AND 190 TEMP BULBS.

Part: O-RING — FAULTY (NR 1 ENGINE OIL) · airframe 78,852 hrs · 12,666 cycles

NR 1 ENG OIL CONSUMPTION. INSPECTED ENG. FOUND OIL IN COWLINGS AND AROUND OIL PUMP AND CHIP DETECTORS. CLEANED OIL PUMP AND COATED EXTERIOR OF PUMP WITH DYE CHECK DEVELOPER. RAN ENG FOR 5 MIN. FOUND OIL LEAKING FROM OIL PUMP PARTING SURFACE WITH GEAR BOX. ALSO AFT 3 CHIP DETECTOR PROBES LEAKING - IDENTIFIED AS: ANGLE GB, NR 3 AND 4 COMPT. REPLACED ALL 4 MCD ASSEMBLIES AND ASSOCIATED O-RINGS ON MAIN OIL PUMP, RAN AND LEAK CHECKED ENGINE NR 1, NO FURTHER LEAKAGE NOTED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 78,782 hrs · 12,651 cycles

EMERGENCY ESC PATH LIGHTS L896 AND L910 ARE INOP. REPLACED PWR SUPPLIES M1553 AND 1561, PATH LIGHTS TEST OKAY.

Part: FSEU — FAULTY (NR 1) · airframe 78,680 hrs · 12,638 cycles

FLAP-SLAT ELEC STATUS AND TRAILING ASYMMETRIC EICAS CAME ON WHILE SELECTING FLAPS 5. REPLACED FLAP SLAP ELEC UNIT AND ASYMMETRY RELAY K351 IN P36. RAN FLAPS AND SLAPS UP AND DOWN SEVERAL TIMES. ALSO ACCOMPLISHED VISUAL INSPECTION ON T/E FLAP TORQUE TUBES, ACTUATORS, GEAR BOXES AND POSITION TRANSMITTERS. NO FAULTS NOTED. REPLACED SLAT HYD PRESSURE SWITCH AS PER MM. REPLACED OUTBOARD LEFT TRAILING EDGE FLAP POSITION TRANSMITTER 473 PER MM.

Part: INDICATOR — INTERMITTENT (COCKPIT) · airframe 78,659 hrs · 12,634 cycles

RT MAIN FUEL IND AND TOTAL INTERMITTENT. REPLACED COCKPIT FUEL QTY INDICATOR PER MM, OP CHECKS GOOD.

Part: ACTUATOR — OUT OF ADJUST (BLEED VALVE) · airframe 78,607 hrs · 12,625 cycles

NR 2 ENGINE, STATIC LEAK UNDER ANGLE GEAR BOX. REMOVED AND REPLACED NR 5 FAN EXIT LINER IAW B767-300 AMM. REMOVED, REPLACED AND ADJUSTED THE 2.5 BLEED VALVE ACTUATOR IAW AMM AND CONNECTED ELECTRICAL CONNECTOR IAW AMM. OPS AND LEAK CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 955, LBL 12) · airframe 78,607 hrs · 12,625 cycles

RII-CANTED DECK STATION 955, LBL 12 IS CORRODED AT THE SEAM OUTBOARD OF THE RIB. MAJOR REPAIR ACCOMPLISHED: REPAIRED ALL CORROSION IN CANTED DECK AREA PER EA PD WITHOUT DEVIATION.

Part: CONNECTOR — SHORTED (SEAT 23H AUDIO) · airframe 78,605 hrs · 12,624 cycles

PASSENGER AT 23H COMPLAINED OF BEING SHOCKED FROM THE AUDIO JACK. REPLACED AUDIO JACK AT 23H. 23H AUDIO OPS CHECK OK.

Part: VALVE — FAULTED (NLG STEERING) · airframe 78,363 hrs · 12,591 cycles

NOSE STEERING CHECK. DUPLICATED AND ISOLATED STICKING STEERING TO METERING VALVE. REPLACED IAW AMM. STICKING ISSUE RESOLVED, BUT NEW VALFE FAILED OPS CK. INTERMITTENTLY HARD TO MAKE RT TURNS. SUSPECT BAD VLV FROM STOCK. REPLACED METERING VALVE AGAIN, NO HELP. STEERING IS SLOW IN BOTH DIRECTIONS FROM FULL TILLER TURN BACK TO NEUTRAL. CONFIRMED 3000 PSI TO METERING VALVE USING A PRESS GAUGE AT VALVE. RE-INSTALLED ORIGINAL VALVE. STEERING FORCE AND RETURN TO NEUTRAL. NOW NORMAL WITH THE EXCEPTION ORIGINAL PROBLEM, STEERING STICKING. SECOND VALVE ALSO BAD FROM STOCK. NLG STEERING SUMMING MECHANISM COVER REMOVED FOR ACCESS TO METERING VALVE REPLACED. PLACED IN COCKPIT. RE-INSTALLED COVER.

Part: ROD — WORN (NR 1 STARTER) · airframe 78,264 hrs · 12,578 cycles

ENG NR 2 STARTER DUCT SUPPORT RODS WORN. REPLACED STARTER DUCT SUPPORT RODS.

Part: BOTTLE — READS LOW (L2 DOOR SLIDE) · airframe 78,264 hrs · 12,578 cycles

2L DOOR SLIDE BOTTLE PRESSURE LOW. MED 2L SLIDE-RAFT CYLINDER PRESSURE GAUGE INDICATOR IS BELOW TEMP COMPENSATOR GREEN BAND. REPLACED DOOR 2L ESCAPE SLIDE PACK PER MM. INSPECTED DR 2L ESCAPE SLIDE INSTALLATION IAW MM.

Part: SHROUD — DETERIORATED (NR 2 ENGINE) · airframe 78,264 hrs · 12,578 cycles

ENG NR 2 OIL TANK HEAT SHROUD DETERIORATED BEYOND LIMITS. REPLACED ENG NR 2 OIL TANK HEAT SHIELD.

Part: CONTACT — DIRTY (EMERGENCY LIGHT) · airframe 78,208 hrs · 12,569 cycles

RT EMERGENCY LIGHT AT T/E OF WING IS INOP. CLEANED CONTACT, OPS CHECKED GOOD.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 77,067 hrs · 12,411 cycles

LEFT SIDE COAX FEED THRU AT AFT PRESSURE BULKHEAD WAS LEAKING. SEALANT PR1458-B2 APPLIED TO AREA. NO FURTHER LEAKS.

Part: GCU — FAULTY (NR 3) · airframe 76,865 hrs · 12,379 cycles

BPCU FAULT APU GCU. REPLACED APU GCU, NO HELP. REPLACED APU GCU, NO HELP. WHEN LT GEN SELECTED APU GEN OFF LT ILLUM AND WOULD NOT COME BACK ON LINE. FREQS AND VOLTS GOOD. CYCLED CB FOR APU GEN CONT, NO HELP. REPLACED NR 1 ENG IDG AND BPCU. ALL AUTOMATIC SWITCHING OF GENERATORS, OPS CHECK NORMAL.

Part: GCU — FAULTY (LT ENGINE) · airframe 76,861 hrs · 12,377 cycles

LT ENG GEN DID NOT COME ONLINE AUTOMATICALLY AFTER ENG START. HAD TO MANUALLY SELECT GEN ON. REPLACED GCU & BPU FOR NR1 ENG. OPS NORMAL.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 76,861 hrs · 12,377 cycles

SEAT 37J, EMERGENCY LIGHT LENS BROKEN. REPLACED BROKEN EMERGENCY LIGHT LENS SEAT 37J.

Part: STARTER — FAULTY (NR 2 ENGINE) · airframe 75,890 hrs · 12,238 cycles

AFTER PUSHBACK CREW STATES NR 2 ENG DID NOT START IN IGNITION NR 2. N2 ROSE AND FELL BACK DOWN TO 5 PERCENT AND BOUNCED TO 8 PERCENT THEN BACK TO 6 PERCENT ON SECOND START. REPLACED NR 2 ENG STARTER AND START VALVE. RAN AND LEAK CHECKED ENG. ENG 2 OPS CKD NORMAL.

Part: WIRE — SHORTED (CONTROL SWITCH) · airframe 75,743 hrs · 12,217 cycles

EDP (ENGINE DRIVEN PUMP) HYD PWR. POS 2O1=L,O2=R) EDP HYD LOW PRESS LGT ILLUM. EICAS MSG DISPLAYED (LT,RT) HYD PRIM PUMP. EICAS MSG (LT,RT) HYD SYS MAINT (WAS, WAS NOT) DISPLAYED. CREW COMMENTS: PUMP AND SYS LO PSI LIGHT ON WITH R ELEC DEMAND SWITCH IN AUTO OR ON. FOUND WIRE SHORTING ON FRAME AT THE ELEC CONTROL PRESS SWITCH 532. AT THE CONNECTOR D75. SPLICED NEW WIRE REF STD WIRING PRACTICE MANUAL 20-30-12 AND SYS OPERATES NORMAL. LOCATION AT RT PYLON SAIL TAIL HYD COMPARTMENT.

Part: TRANSMITTER — FLUCTUATES (HYD SYSTEM) · airframe 75,658 hrs · 12,206 cycles

LT HYD QTY FLUCTUATING. REMOVED AND SECURED PTU SIGNAL WIRE AND WILL REQUIRE RECONNECTION IAW MEL ITEM. SYS IS INOP IAW MEL. QUANTITY VERIFIED. QTY NORMAL AND LOW PRESSURE LIGHT IS OPERATIVE. REPLACED LT HYD TRANSMITTER IAW MM. NO LEAKS NOTED. RECONNECTED WIRE TO PTU SIGNAL.

Part: TRIM SYSTEM — MALFUNCTIONED (HORIZ STAB) · airframe 75,489 hrs · 12,180 cycles

CREW REPORT: STAB TRIM EICAS ON TAXI OUT. CYCLED STAB TRIM CTRL C/B'S NO HELP, CYCLED FLT CTRL ELEC LT & RT 1&2 C/B'S FAULT CLEARS & STAYS OUT WHEN MOVING CAPT'S ELECT STAB TRIM SWITCHES. LIGHT & EICAS MSG RETURN WHEN F/O'S STAB TRIM SWITCHES ARE USED. STAB APPEARS TO TRIM AT NORMAL RATE.

Part: LAMP — INOPERATIVE (CABIN LIGHTS) · airframe 75,254 hrs · 12,147 cycles

LIGHT IN LAVATORY BUSINESS CLASS RT SIDE, LIGHT INOP. RELAMPED.

Part: LINE — LEAKING (FLEX HYD) · airframe 74,965 hrs · 12,108 cycles

FOUND HEAVY HYD LEAK AT RT MLG DURING WALK AROUND. LEAK ISOLATED ON A BROKEN HYD FLEX LINE ON THE TOP RT OF MLG ON A FLEX HYD LINE PN 00624-AC127J-0300SS OR AS4624J-0300SS AT 3000 PSIG 275F AS4623*. FLEX HYD LINE REPLACED IAW AMM. LEAK CHECK PERFORMED, NO LEAK. MOST OF THE HYD LEAK WAS CLEANED BUT SOME REMAINING TRACES OF FLUID MAY APPEAR IN THE RT MLG AREA.

Part: SWITCH — DEFECTIVE (RAM AIR TURBINE) · airframe 74,629 hrs · 12,063 cycles

RAT FAILED TO MANUALLY DEPLOY, DURING OPS CHECK RELATED TO KORRY SWITCH REPLACE COA 617952. REMOVED AND REPLACED RAT DEPLOY SWITCH S4 PER BACO SB. OPS CHECK OF RAT CHECKED GOOD, MANUAL DEPLOYMENT GOOD PER MM ON NON ROUTINE 21815.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 74,629 hrs · 12,063 cycles

EXTERIOR EMERGENCY LIGHT AT R-4 DOOR INOP. RELAMPED AFT RT EMERGENCY LIGHT AND OPS CHECK GOOD.

Part: ACTUATOR — CRACKED (NR 7 SPOILER) · airframe 74,628 hrs · 12,062 cycles

NR 7 SPOILER ACTUATOR SIDE HSG IS CRACKED. RUNNING LEAK AT 1 DROP IAW SECOND. ACTUATOR ON AOG NR Y1799. REPLACED NR 7 SPOILER ACTUATOR, OPS CHECKS GOOD.

Part: FAN — INADEQUATE (POSITION LT) · airframe 74,525 hrs · 12,047 cycles

ELECTRICAL ODOR IN COCKPIT, FLT DIVERTED. TURNED OFF UTILITY BUSS (LT & RT). ODOR STARTED CLEARING. NO SMOKE OR FIRE IAW CREW. FOUND LT RECIRC FAN IMPELLER CONTACTING FAN HSG AND RECIRC FAN CB POPPED. REPLACED FAN. RAN ALL PNEUMATICS SYS, ELECTRICAL SYS FOR 1.5 HRS. NO ODORS, SMELLS FOUND.

Part: GCU — FAULTY (LT GENERATOR) · airframe 74,442 hrs · 12,030 cycles

LT GEN LIGHT OFF. DUE TO SEVERAL REPORTS ON LT GEN FIELD LIGHT ON. ACCOMPLISH ELECTRICAL HARNESS CHECK IAW MM. ACCOMPLISH BPCU BITE TEST IAW FIM AND CORRECT ANY PROBLEMS. IF NO PROBLEMS FOUND, REPLACE LT GEN GCU IAW MM. REPLACED GCU. ACP HARNESS CK UP TO PYLON. LEFT GEN LIGHT OFF. DUE TO SEVERAL REPORTS ON LT GEN FIELD LIGHT ON PLEASE ACCOMPLISH ELECTRICAL HARNESS CHECK IAW MM. ACCOMPLISH BPCU BITE TEST IAW FIM AND CORRECT ANY PROBLEMS. IF NO PROBLEMS FOUND PLEASE REPLACE LT GEN GCU IAW MM. REPLACED GCU. ACP HARNESS CK UP TO PYLON.

Part: HEATER BLANKET — BURNED (NR 2 ENGINE) · airframe 73,980 hrs · 11,962 cycles

SHIELD ASSY NR 2 ENGINE BURNED AND FALLING APART. REPLACED HYD HEAT SHIELD BLANKET AND SECURED. ALL OKAY.

Part: CONTROLLER — FAULTY (COCKPIT TEMP) · airframe 73,412 hrs · 11,881 cycles

FLT DECK TEMP CONTROL FAILED TO CONTROL DESIRED TEMP IN 'AUTO' OR 'MAN'. CREW COMMENTS: FLT DECK IS IN FULL HOT MANUAL & IT IS JUST BARELY COMFORTABLE. REPLACED FLIGHT COMPARTMENT TRIM MODULATING VALVE. DID NOT FIX PROBLEM. VALVE SHOWS FULL HOT, WITH COLD AIR COMING OUT OF GASPERS. REPLACED ZONE TEMP CONTROLLER AND TESTS OKAY.

Part: CONTROLLER — INOPERATIVE (COCKPIT TEMP) · airframe 73,344 hrs · 11,870 cycles

COCKPIT TEMP SELECTOR INOP LIGHT ON IN AUTO. INSTALLED NEW ZONE TEMP CONTROLLER. INOP LIGHT EXTINGUISHED. OPS NORMAL.

Part: AMPLIFIER — FAULTY (SATCOM) · airframe 73,185 hrs · 11,849 cycles

SATCOM SYS INTERMITTENT. TRANSCEIVER MOVING FROM LTR. PART WILL ARV 1900 ZRH. FBO TO REPLACE PART. ERTS WILL BE UPDATED WHEN PART IN AMT HANDS. NR1 HF TRANSCEIVER REPLACED AND TESTED OK. REPLACED HIGH POWER HGA, LGA AND LOW NOISE DUPLEXER LGA. SATCOM SYS BITE FAULTED HGA, SUSPECT BAD HGA INSTALLED. SATCOM SYS BITE HAS AN INTERMITTENT FAULT ON THE HIGH GAIN AMP. EVERY 10 TO 20 MIN FAULT APPEARS AND GOES OUT. ORDERED HI GAIN AMP UNDER OSTF F1907 FOR IAD 30DEC. REPLACED SATCOM HIGH GAIN AMP IAW MM, CKS OK.

Part: LATCH — FAULTY (OVERWING SLIDE) · airframe 72,880 hrs · 11,806 cycles

LT OVERWING COMPARTMENT DOOR INTEGRATOR TORQUE CHECK EXCEEDS 175 INCH POUNDS. INSTALLED 2 EA NEW DOOR LATCHES FOR THE LT OVERWING SLIDE COMPT DOOR AND OPS CHECKS GOOD.

Part: LATCH — FAULTY (OVERWING DOOR) · airframe 72,880 hrs · 11,806 cycles

RIGHT OVERWING COMPARTMENT DOOR INTEGRATOR TORQUE EXCEEDS 175 INCH POUNDS. REPLACED 4 EA RT OVERWING COMPARTMENT DOOR LATCHES. RIG CHECKS GOOD.

Part: STIFFENER — CRACKED (BS 246 LBL 20) · airframe 72,880 hrs · 11,806 cycles

STA 246 FLOORBEAM FWD SIDE VERT STIFFENER CRACKED AT LBL 20. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW STIFFENER.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 72,759 hrs · 11,785 cycles

EDP HYD OVHT LIGHT ILLUMINATED EICAS MSG (L,R) PRIM HYD OVHT DISPLAYED. PUMP WAS DEACTIVATED. POS 2 (01=L,02=R). CREW COMMENTS: R PRIM HYD PUMP OVHT SHUT OFF PUMP OVHT CAUTION EXTINGUISHED AFTER 12MIN 20SEC. SUPPLEMENTAL DATA UPDATE, FOUND NR 2 ENGINE (EDP) LEAKING HYD FLUID. REPLACED (EDP). OPS CHECKED RT HYD QUANTITY AND PRESSURE. OPS CHECKED GOOD AFTER ENG PUMP WAS REPLACED. REPLACED CASE DRAIN AND PRESSURE AND RETURN FILTERS, OPS GOOD.

Part: CHARGER — FAULTY (MAIN BATTERY) · airframe 72,759 hrs · 11,785 cycles

MAIN BATTERY CHARGER STATUS MESSAGE WON’T CANCEL. REPLACED MAIN BATTERY CHARGER, OP CHECKS OKAY.

Part: LINE — LEAKING (HYDRAULIC SYS) · airframe 72,336 hrs · 11,724 cycles

HYD FLUID LEAKING FROM PYLON AREA OVER TAIL PIPE. HAVE HYD LEAK NR 2 ENG PYLON OVER TAIL PIPE. NR 2 ENG & PYLON CLEANED UP, LOOKING FOR LEAK. FOUND HYD LEAK FROM A PRESSURE LINE IN THE FWD SAILTAIL INTO THE PYLON. RESEARCHING LINE VERY LIMITED ACCESS. REMOVED DAMAGED HYD LINE. NEW LINE ON AOG Q1265. REMOVED AND REPLACED LEAKING LINE, CHECKED CONNECTIONS FOR SECURITY AND LEAKS. NO LEAKS.

Part: VALVE — LEAKING (NR 1 ENGINE) · airframe 72,336 hrs · 11,724 cycles

FUEL LEAKING BOTTOM OF NR 1 ENGINE. REPLACED NR 1 ENG FUEL DISTRIBUTION VALVE. OP CHECKS OKAY.

Part: VALVE — FAULTED (CABIN TEMP) · airframe 72,181 hrs · 11,702 cycles

EICAS MESSAGE: AFT CABIN TEMP, ZONE TEMP BITE. ACCMP'D TEMP CTL BITE. AFT TRIM VALVE FAULT SHOWN. REPLACED TRIM VALVE. ALL OPS AND INDICATIONS NORMAL.

Part: LINE — LEAKING (OIL COOLER) · airframe 72,155 hrs · 11,698 cycles

FUEL LEAK FROM AIR NR 2 ENG AIR-OIL COOLER. FOUND FUEL LINE LEAKING AT BOTTOM OF AIR OIL HEAT EXCHANGER ASSY, RE-TORQUED FITTING, NO HELP. SUSPECT LINE OR FITTING ON ASSY BAD. COMPLETED LINE INSTALLATION. REPLACED A/O COOLER VALVE.

Part: PCU — LEAKING (AILERON) · airframe 72,135 hrs · 11,694 cycles

RIGHT INBOARD AILERON PCA LEAKING. RIGHT INBOARD AILERON ACT LEAKING 8 DROPS PER MIN. NEEDS AILERON PCU REPLACED. REPLACED INBOARD RIGHT AILERON PCU. OPS CHECK GOOD. NO LEAKS FOUND.

Part: PROBE — FAULTY (PITOT) · airframe 71,025 hrs · 11,518 cycles

L AUX PITOT MESSAGE DISPLAYED AFTER ENGINE START. REPLACED L AUX PITOT PROBE. OP CHECKS OKAY.

Part: CABLE — DEFECTIVE (HF COMM) · airframe 70,550 hrs · 11,449 cycles

HF TUNING CAUSING INTERFERENCE. REPLACED MCABLE W243-01CX- BA6903 FROM D4003J TO D4839J REF WDM 23-11-11 PG 1.HF RADIO TEST OK.

Part: DUCT — FAILED (APU) · airframe 70,314 hrs · 38,842 cycles

APU ONLY PUTTING OUT 11 PSI ON ENG START. NOTABLE TO START ENGS. *S/D* TEE DUCT FWD OF SURGE FAILED. REPLACED AND OPS CHECK APU PNEUMATICS. DUCT PRESS NORMAL.

Part: ANTI-ICE VALVE — FAULTY (LT ENGINE) · airframe 69,229 hrs · 11,257 cycles

LEFT ENG A-I VALVE LIGHT ILLUMINATED WITH SWITCH IN OFF POSITION. REPLACED ANTI-ICE VALVE & CONNECTOR. OPS CHECK NORMAL.

Part: DOOR — CRACKED (THRUST REVERSER) · airframe 69,195 hrs · 11,252 cycles

NR 1 ENGINE HAS A CRACKED THRUST REVERSER BLOCKER DOOR LOCATED AT THE 11 O'CLOCK POSITION (AFT OF FAN EXIT GUIDE VANES). BLOCKER FAN REVERSER SLEEVE DOOR REMOVED.

Part: PUMP — FAULTY (CENTER AUX TANK) · airframe 67,076 hrs · 10,946 cycles

RIGHT MAIN FUEL QTY DECREASED WHILE FEEDING FROM CTR TANK. *S/D* SUSPECT FAULTY AUX OVERRIDE PUMP. REPLACED PUMP PER MM 28-22- 05, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: OXYGEN MASK — LEAKING (FIRST OFFICER'S) · airframe 67,035 hrs · 10,940 cycles

F/O O2 MASK LEAKING FROM HEADBAND. *S/D* FOUND MASK LEAKING. REPLACED MASK, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: IDG — FAULTY (NR 1) · airframe 66,885 hrs · 10,911 cycles

NR 1 ENG IDG FAILED DISC RESET TEST DOES NOT RESET MANUALLY AT DISC RING. *S/D* SUSPECT FAULTY BEARING. REPLACED IDG, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: LAMP — DISCONNECTED (EMERGENCY LIGHT) · airframe 66,885 hrs · 10,911 cycles

SEAT 9J EMERGENCY LIGHT INOP. *S/D* FOUND LOOSE CONNECTION. SECURED CONNECTION, OP CHECK GOOD. AC OK FOR SERVICE.

Part: PANEL — CORRODED (BS 955) · airframe 66,885 hrs · 10,911 cycles

MAIN CABIN STA 955, UPPER SURFACE OF WING BOX PANEL CORRODED AT LBL 36. REMOVED CORROSION DAMAGE TO CENTER WING BOX PANEL AT LBL36, TRIMMED THE FLOORBEAM LOWER CHORD AND THE UPPER WING SKIN. FABRICATED A FILLER FOR THE WING SKIN CUT-OUT, A -1 AND -4 FILLER, -2 DOUBLER, AND -3 TRIPLER AND I NSTALLED. REPAIRED THE REAR SPAR UPPER CHORD WITH A REPAIR ANGLE, SPLICE REPAIRED THE 85625 LOWER CHORD AND FABBED AND INSTALLED FLOOR BEAM SPLICE FITTINGS AND FLOORBEAM WEB DOUBLER.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,885 hrs · 10,911 cycles

LEFT SIDE A&B ZONE CEILING EMERGENCY AISLE LIGHTS ARE INOP. *S/D* FOUND FAULTY BATTERY PACK. REPLACED BATTERY PACK, OP CHECK GOOD. AC OK FOR SERVICE.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,885 hrs · 10,911 cycles

LEFT AND RIGHT AFT DOORS EMERGENCY EXIT LIGHTS ARE INOP. *S/D* FOUND FAULTY FUSE. REPLACED FUSE, OP CHECK GOOD. AC OK FOR SERVICE.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHT) · airframe 66,885 hrs · 10,911 cycles

L1 DOOR EMERGENCY EXIT LIGHT IS INOP. *S/D* FOUND FAULTY POWER SUPPLY. REPLACED POWER SUPPLY, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: SKIN — DAMAGED (BS 465 S36L-38R) · airframe 66,885 hrs · 10,911 cycles

LOWER EXT FUSELAGE SKIN CREASED AT BS 465 STR 36L TO 38R. REPAIRED SKIN CREATED CF9055 TO FOLLOW UP INSPECTION. AC OK FOR SERVICE.

Part: CONNECTOR — DAMAGED (NR 1 HYD SYS) · airframe 66,885 hrs · 10,911 cycles

NR 1 ENG PYLON HYD BAY CONNECTOR D02134 SADDLE CLAMP IS MISSING.

Part: WIRE — CHAFED (NR 1 PYLON) · airframe 66,885 hrs · 10,911 cycles

NR 1 ENG PYLON HYD BAY WIRE W390-082-18 IS CHAFED. REPLACED WIRE. OPS CHECKS GOOD.

Part: WIRE — DAMAGED (NR 1 NACELLE) · airframe 66,885 hrs · 10,911 cycles

NR 1 ENG PYLON HYD BAY WIRE AT CONNECTOR D00 036 PIN 2 (SWITCH S310) IS HEAT DAMAGED. FOUND WIRE AT CONNECTOR D00036 PIN 2 (SWITCH S310) IS HEAT DAMAGE. REPLACED WIRE AT D00036P PER BSWPM 20-61-11 AND WDM 29-32-11. OPS CHECKS GOOD

Part: SKIN — DENTED (NR 3 SLAT) · airframe 66,885 hrs · 10,911 cycles

NR 3 SLAT REMOVED FROM A-C 6352. SLAT DENTED 56 INCHES FROM INBOARD END. DAMAGED CAUSE IN WIND STORM.

Part: WIRE — CHAFED (NR 1 NACELLE) · airframe 66,885 hrs · 10,911 cycles

NR 1 ENG PYLON HYD BAY WIRE W390-082-18 IS CHAFED.

Part: CLAMP — MISSING (CONNECTOR) · airframe 66,885 hrs · 10,911 cycles

NR 1 ENG PYLON HYD BAY CONNECTOR D02134 SADDLE CLAMP IS MISSING. REPLACED CONNECTOR DO2134P SADDLE CLAMP. OPS CHECKS OF NR 1 ENG HYD PRESSURE INDICATION CHECKS NORMAL.

Part: SLAT — DAMAGED (NR 3) · airframe 66,885 hrs · 10,911 cycles

NR 3 SLAT REMOVED FROM A-C 6352. SLAT DENTED 56 INCHES FROM INBOARD END. DAMAGED CAUSE IN WIND STORM. INSTALLED REPAIRED SLAT.

Part: HEATING ELEMENT — BURNED (WATER TANK LINE) · airframe 66,885 hrs · 10,911 cycles

ELECTRICAL HEATER TAPE HAS BURNED THROUGH ON AFT WATER TANK LINE STA 1650 STR 27R AFT CARGO COMPARTMENT. REPLACED HEAT TAPE OP CHECKED GOOD. AC OK FOR SERVICE.

Part: GROUND WIRE — CHAFED (NR 1 HYD PUMP) · airframe 66,885 hrs · 10,911 cycles

NR 1 HYD PUMP WIRE IS CHAFED DOWN TO PRIMARY CONDUCTOR. REPLACED GROUND WIRE PER B 767 WDM 29-11-12, SWPM 20-10-11, AND 20-20-12. OPS CHECKED ELECT HYD PUMP PER MM29-11-00, OP CHECK GOOD. AC OK FOR SERVICE.

Part: WIRE — DAMAGED (SHUTOFF VALVE) · airframe 66,885 hrs · 10,911 cycles

NR 1 PYLON PRSOV VALVE WIRES W306-68-18 AND W306-71-18 DAMAGED. REPLACED WIRES W306-68-18 ANSD W306-71-18 PER B767 WDM 36-11-51 AND BSWPM 20-30-12. REPLACED CONNECTOR D22 PER WDM 36-11-51. OPS CHECKS GOOD. AC OK FOR SERVCICE.

Part: SPAR — CRACKED (NR 1 NACELLE) · airframe 66,885 hrs · 10,911 cycles

NR 1 ENG PYLON TOP, BELOW ACCESS 441DT, RT SIDE, UPPER SPAR WEB CRACKED AT EXISTING REPAIR, CRACK NOT TERMINATED. REMOVED THE EXISTING REPAIR. FABRICATED AND INSTALLED A DOUBLER, RADIUS FILLER, AND REPAIR FILLER.

Part: STRINGER — CORRODED (BS 785.9) · airframe 66,885 hrs · 10,911 cycles

FWD PIT BS 785.9, S-39R STRINGER END FITTING IS CORRODED. REPLACED STRINGER END FITTING. INSTALLED FITTING.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 66,885 hrs · 10,911 cycles

NR 1 PYLON STRUT I/B SIDE STRUT ACCESS HOLE FOR PANEL 416BR AFT UPPER CORNER SKIN IS CRACKED. STOP DRILLED CRACK. FABRICATED & INSTALLED 2EA DOUBLERS. HFEC INSP, NO CRACK PAST STOP DRILL.

Part: BUSHING — OUT OF POSITION (NR 2 PYLON) · airframe 66,885 hrs · 10,911 cycles

NR 2 PYLON INBOARD MID SPAR FITTING BUSHING MIGRATED .030 NO CORROSION OR ROTATION.

Part: BUSHING — OUT OF POSITION (NR 1 PYLON) · airframe 66,885 hrs · 10,911 cycles

NR 1 PYLON INBOARD MID SPAR FITTING BUSHING MIGRATED .035 NO CORROSION OR ROTATION.

Part: SPRING — WEAK (SERVICE DOOR) · airframe 66,885 hrs · 10,911 cycles

AFT RT SVC DOOR DEPLOYMENT BAR GAS SPRING IS WEAK. FOUND WEAK GAS SPRING IN DEPLOYMENT BAR SERVICE DOOR. REPLACED GAS SPRING IAW MM 25-66-03. AC OK FOR SERVICE.

Part: SPRING — WEAK (SERVICE DOOR) · airframe 66,885 hrs · 10,911 cycles

AFT LT SVC DOOR DEPLOYMENT BAR GAS SPRING IS WEAK. REPLACED GAS SPRING IAW MM 25-66-03. AC OK FOR SERVICE.

Part: WEB — CRACKED (NR 2 PYLON) · airframe 66,885 hrs · 10,911 cycles

NR 2 PYLON UPPER WEB CRACKED, NAC STA 182 AT FWD OUTBD CORNER OF FEED THROUGH CUTOUT. FOUND CRACKED WEB SUSPECT NORMAL AC OPERATION. REPAIRED CRACK IAW SB 767-54-0091 FIG 10. AC OK FOR SERVICE.

Part: GUARD — CORRODED (FUSELAGE) · airframe 66,885 hrs · 10,911 cycles

MAIN CABIN FLOOR SUPPORT ANGLE SPLASH GUARD HAS CORROSION AT BS 285 AND RBL 83. REMOVED & REPLACED SPLASH GUARD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 66,885 hrs · 10,911 cycles

MAIN CABIN FLOOR SUPPORT ANGLE -SPLASH GUARD- HAS CORROSION AT BS 285 AND RBL 83.

Part: FLOORBEAM — CRACKED (BS 246 LBL11) · airframe 66,885 hrs · 10,911 cycles

MAIN CABIN FLOORBEAM AT BS 246, AFT FACE UPPER ANGLE CRACKED, LBL 11. *S/D* FOUND UPPER CHORD CRACKED. REMOVED DAMAGE, FABRICATED NEW UPPER CHORD AND INSTALLED IAW SRM 53-10-51.

Part: FLOORBEAM — CORRODED (BS 805 LBL 11) · airframe 66,885 hrs · 10,911 cycles

CORROSION FOUND AT BS 805, LBL 11, UNDER MAIN CABIN FLOOR. *S/D* SUSPECT MOISTURE CONTAMINATION. CUT OUT DAMAGED SECTION OF T-CAP SPLICED IN NEW SECTION PER SRM 53-00-51, SRM 51-20-01 AND SRM 51-40-02. AC OK FOR SERVICE.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 66,885 hrs · 10,911 cycles

E&E COMPARTMENT AT STA 246 FLOORBEAM AND LBL 40 HAS CRACKED VERTICAL STIFFENER. REPLACED CRACKED STIFFENER. FABRICATED & INSTALLED NEW REPAIR.

Part: STRUCTURE — DAMAGED (LT NLG DOOR) · airframe 66,885 hrs · 10,911 cycles

LT FWD NLG DOOR SKIN HAS A LIGHTNING STRIKE APROX 17 INCHES AFT OF LEADING EDGE OF DOOR AND 7.75 INCHES FROM INBOARD EDGE OF DOOR. *S/D* FOUND LIGHTNING STRIKE IN NOSE LANDING GEAR DOOR. REMOVED DAMAGE TO LT FWD NLG DOOR AND INSTALLED COMPOSITE REPAIR PER SRM 52-80-02. PAINTED PER GN-MM 5-0-4-020. AC OK FOR SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,885 hrs · 10,911 cycles

CABIN FLOORBEAM AT BS 805, RBL 11 IS CORRODED. REMOVED DAMAGE, FABRICATED NEW REPAIR AND INSTALLED IAW SRM 53-00-51 AND SRM 51-40-02. AC OK FOR SERVICE.

Part: FLOORBEAM — WORN (MAIN CABIN UPPER) · airframe 66,885 hrs · 10,911 cycles

MAIN CABIN FLOORBEAM UPPER SURFACE HAS WEAR MARKS AROUND FASTENER HOLE AT BS 764 BETWEEN RBL 20 AND RBL 54. *S/D* SUSPECT TOOLING MARKS. REMOVED DAMAGE AREA, FABRICATED AND INSTALLED REPAIR IAW SRM 53-00-51 FIG 201 TABLE I. AC OK FOR SERVICE.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,885 hrs · 10,911 cycles

STA 303, RBL 88.5, CRACK ON FLOORBEAM. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED T-CHORD, REPAIR SPLICE & STRAP.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 66,885 hrs · 10,911 cycles

MAIN CABIN UNDER FLOOR, INTERCOSTAL UPPER ANGLE CRACKED BETWEEN BS 742 AND BS 764, AND RBL 40. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW ANGLE (P/N OA00002UD).

Part: SHUTOFF VALVE — FAULTY (NR 1 ENGINE) · airframe 66,885 hrs · 10,911 cycles

NR 1 ENG PRSOV FAILED HEALTH CHECK REFERENCE PRESSURE LOW. *S/D* DURING HEALTH CHECK FOUND PRESSURE REGULATING SHUT OFF VALVE FAULTY. REPLACED PRSOV. AC OK FOR SERVICE.

Part: POWER CABLE — DAMAGED (EMERGENCY LIGHTS) · airframe 65,772 hrs · 10,727 cycles

EEL ADJACENT TO DR 1R INOP. REPAIRED POWER CABLE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,367 hrs · 10,667 cycles

FWD LEFT OVERWING EMERGENCY LIGHT INOP. RELAMPED.

Part: SKIN — DENTED (BS 1373) · airframe 65,367 hrs · 10,667 cycles

EXTERIOR FUSELAGE SKIN AT BS 1373 AND STR 28R DENTED. MAJOR REPAIR ACCOMPLISHED: CUT-OUT DAMAGE TO EXTERNAL FUSELAGE AND FABRICATED REPAIR DOUBLERS AND FILLERS AND INSTALLED. REMOVED CRACKED SHEAR TIE AND FABRICATED A NEW -818 SHEAR TIE AND INSTALLED.

Part: HOSE — COLLAPSED (EVAC SLIDE) · airframe 65,357 hrs · 10,666 cycles

RIGHT EMERGENCY EXIT SLIDE INFLATION HOSE IN THE HYDRAULIC SERVICE BAY IS COLLAPSED AND SPONGY. REPLACED HOSE ASSY. HYDRAULIC SPLASH DURING SERVICING MAKES CONTACT WITH HOSE & PARTIALLY DISSOLVES IT, BECOMING SPONGY. HOSE THEN IS PRONE TO COLLAPSING.

Part: OXYGEN BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 65,357 hrs · 10,666 cycles

O2 BOTTLE AT DOOR 2R LOW. SUSPECT FAULTY VALVE. REPLACED O2 BOTTLE AT DOOR 2R. ACFT OK FOR SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 65,357 hrs · 10,666 cycles

ON ARRIVAL FOUND SKIN DAMAGE AFT OF REAR CARGO DOOR. SUSPECT AC DAMAGE FROM GROUND EQUIPMENT. CUT-OUT DAMAGE TO EXTERNAL FUSELAGE AND FABRICATED REPAIR DOUBLERS AND FILLERS AND INSTALLED PER SRM 53-00-01, FIG. 201.REMOVED CRACK SHEAR 85625 TIE AND FABRICATED A NEW -818 SHEAR TIE PER BAC DWG 140T2103 AND INSTALLED PER SRM 51-40-2. AC OK FOR SERVICE.

Part: ANTI-ICE VALVE — INOPERATIVE (NR 2 ENGINE) · airframe 65,128 hrs · 10,633 cycles

EICAS MSG ENG-ANTI ICE DISPLAYED. REPLACED NR 2 ENG ANTI ICE VALVE, AND OP CHECKED PER MM 30-21-03 -401. CHECKS GOOD.

Part: ASPIRATOR — UNSERVICEABLE (EVAC SLIDE)

ASPIRATOR LEAKING. REPLACED ASPIRATOR AND SLIDE. ACFT OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (CABIN TEMP) · airframe 63,851 hrs · 10,441 cycles

CREW COMMENTS: TEMPS VERY DIFFICULT IN COCKPIT, FIRST, BUS CLASSES.

Part: BALLAST — FAULTY (GALLEY LIGHT) · airframe 63,649 hrs · 10,403 cycles

FWD GALLEY OVERHEAD LIGHT EMITTED ODOR WHILE ON BUT WENT AWAY. LEFT IT OFF FOR REMAINDER OF FLIGHT. 10-9-07 REPLACED BALLAST M660, OP CHECKS OK.FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 63,557 hrs · 10,388 cycles

GEAR DISAGREE LIGHT ILLUM WHEN GEAR WAS EXTENDED FOLLOWED BY TAIL SKID LIGHT.

Part: OVEN — FIRE (GALLEY) · airframe 63,294 hrs · 10,343 cycles

GALLEY OVEN R42 CAUGHT ON FIRE. FIRE EXTINGUISED WITH HALON. REPLACED R42 GALLEY OVEN. OPS CKS OK. SUSPECT SHORT IN HEATING ELEMENT.

Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 63,176 hrs · 10,325 cycles

FUSELAGE DAMAGED BELOW BULK CARGO DOOR. 08-31-07 ACP'D MAT'L LOSS INSP USING ULTRASONIC THICKNESS TESTER ON REPAIRED SKIN DAMAGE BELOW BULK CARGO DOOR. BLENDED DAMAGED AREA. REPAIR OK PER EVA 70500 IS FAA APPROVED VIA FAA 8100-9 FORM. AIRCRAFT OK FOR RETURN TO SERVICE. SUSPECT DAMAGE DUE TO CONTACT BY GROUND SERVICE EQUIPMENT.

Part: LENS — INOPERATIVE (FIRE WARNING) · airframe 62,737 hrs · 10,254 cycles

RED FIRE WARNING LIGHT DOES NOT ILLUMINATE WHEN TESTED. [07-27-07] REPLACED FIRE ANNUNICATOR LENS ASSY. OP CHECKS NORMALLY.

Part: ENGINE — SURGES (NR 2) · airframe 61,935 hrs · 10,106 cycles

NR 2 ENGINE SILENT SURGE. [SUP 05-18-07] REPLACED NR 2 ENG ELECTRONIC ENGINE CONTROL PER AMM 73 -21-04. RT ENG PIMU HAD 'EEC CH-A T29 RNG FAIL' REF SMC 2. REF LOG 1 DURING ENG RUN AFTER REPLACE OF EEC FOUND PIMU FAULT 'EEC CH-A T29 RNG FAIL'. REPLACED NR 2 ENG LEFT 2.9 BLEED VALVE THERMOCOUPLE PER AMM 75-32-06, ENGINE CKS GOOD. A/C RETURNED TO SERVICE.

Part: CIRCUIT CARD — INOPERATIVE (RIGHT) · airframe 61,620 hrs · 10,045 cycles

RIGHT FUEL CUT OFF SWITCH FIRE TEST INOPERATIVE. [SUP 4-20-07] AFTER TROUBLESHOOTING FOUND LOGIC TEST FIRE OVERHEAT CARD M10274 AT FAULT. REPLACED CARD PER MM26-10-0 1, OP CHECKS GOOD. RETURN TO SERVICE.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHTS) · airframe 60,922 hrs · 9,932 cycles

EEL STRIP LEFT FWD CABIN INOPERATIVE. REPAIRED EEL CABLE. A/C OK FOR SERVICE.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 60,862 hrs · 9,923 cycles

EMERGENCY FLOOR LIGHT IN FIRST CAM OUT OF TRACK. FOUND 2 EEL STRIPS INOP AT FWD DOOR AND CROSSOVER. REPAIRED HARNESSES PER GNMM 2-0-15-005. ALL GROUND CHECKS GOOD.

Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 60,424 hrs · 9,825 cycles

NR 2 PYLON MIDSPAR FITTING CLOSE OUT ANGLE, OUTBOARD SIDE, INBOARD FASTENER HAS CRACK INDICATION APPROX .75 INCH LONG LOCATED AFT SIDE. STOP DRILLED THE CRACK AND ACCOMPLISHED HIGH FREQ EDDY CURRENT INSP. CRACK CONTAINMENT CONFIRMED. FABRICATED REPAIR SPLICE STRAP AND FILLER AND INSTALLED. OK FOR SERVICE. CLOSEOUT ANGLE SUBJECT OF AD NOTE, AD2005-19-23. VIBRATION & HEAT EXACERBATE FATIGUE LEADING TO EARLY CRACKING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,557 hrs · 8,903 cycles

LEFT SIDE FIRST CLASS EEL STRIPS INOP.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHT) · airframe 54,262 hrs · 8,855 cycles

EMERGENCY LIGHTS L900, L908 AND L976 ON WITH SW IN ARMED POSITION. BATTERY PACK NOT HOLDING CHARGE. REPLACED OK.

Part: ENGINE — OVERHEATED (NR 2) · airframe 54,248 hrs · 8,852 cycles

RETURNED TO THE FIELD DUE TO HIGH OIL TEMPERATURE ON NR 2 ENGINE. REPLACED FUEL/OIL COOLER BYPASS VALVE SOLENOID. TESTED OK AFTER REPLACEMENT.

Part: HINGE FITTING — DAMAGED (FLAPS) · airframe 54,101 hrs · 8,824 cycles

LT INBD FLAP CENTER HINGE FITTING LINE INBD SIDE DAMAGED. LEFT INBOARD FLAP CENTER HINGE FITTING FOUND DAMAGED ON INBOARD SIDE. REPAIRED PER SRM 57-53-02.

Part: SKIN — CORRODED (CENTER WING) · airframe 54,101 hrs · 8,824 cycles

BS 955 CENTER WING BOX UPPER SKIN AT RBL 3 AT AFT SPAR CORRODED, SKIN SPLICE FITTING AND AFT SPAR. CORROSION CAUSED BY MOISTURE IN THE AREA. BLENDED WING SKIN, FABRICATED REPAIR SHIM BETWEEN SKIN AND FITTING, BLENDED SPAR CHORD, AND FABRICATED MODIFIED FITTING P/N 145T8657-2 PER TIMCO REO (EVA) G10657, REV C, AND UA-EVA-50419 ON NON ROUTINES J7557R, G4070J, G4036J, G4043J AND G7128I.

Part: SKIN — DENTED (CARGO DOOR) · airframe 54,101 hrs · 8,824 cycles

DENT IN BULK CARGO DOOR, .5 INCHES BELOW EXISTING EXTERNAL REPAIR DOUBLER. INTERIM REPAIR PER EVA MOC1-8779A. ACCOMPLISH A DETAILED, EXTERNAL VISUAL INSPECTION EVERY 'A' CHECK UNTIL NEXT 'C10' CHECK. INTERIM REPAIR PER EVA MOC1-8779A. ACCOMPLISH A DETAILED, EXTERNAL VISUAL INSPECTION EVERY 'A' CHECK UNTIL NEXT 'C10' CHECK. MF4762 CREATED TO MONITOR.

Part: LATCH — WORN (CABIN)

LT O/W SLIDE DOOR LATCH FAILS EDGE MARGIN CHECK (NR 3 LATCH). REPLACE LATCH IAW 767, MM 25-65-98.

Part: ASPIRATOR — LEAKING (SLIDE/RAFT)

THE ASPIRATOR LEAKING BY BARREL. REPLACED ASPIRATOR.

Part: IDG — VIBRATION (LT ENGINE) · airframe 51,064 hrs · 8,333 cycles

DIVERTED WHEN LEFT ENGINE INDICATED IDLE FUEL FLOW AND IDLE THRUST. SHOP FOUND LOG PISTON FAILURE ON REMOVED LT IDG. CORRESPONDENCE BETWEEN COMPONENTS ENGINEERING, POWER PLANT ENGINEERING, SUNDSTRAND, AND PWA, INDICATES THERE IS A POTENTIAL ANOMALY FOR A WORN IDG TO INTRODUCE NOISE INTO THE N2 SPEED TRANSDUCER THROUGH THE ENGINE GEARBOX DUE TO UNSTEADY LOADING BY THE IDG. IT IS SURMISED THAT AN UNSTEADY N2 SIGNAL TO THE ENGINE FADEC MAY ACCOUNT FOR THE INABILITY OF THE ENGINE TO ACCELERATE.

Part: AUTOTHROTTLE SYS — MALFUNCTIONED (COCKPIT) · airframe 48,087 hrs · 7,835 cycles

FLIGHT ABORTED TAKEOFF AT 100 KTS DUE TO AUTOTHROTTLE INDICATION. RETURNED TO BLOCKS. THRUST MANAGEMENT COMPUTER WAS REMOVED AS A PRECAUTION. UNIT CHECKED OK IN THE SHOP. MCDP FAULT DATA DID NOT RECORD ANY TMC-RELATED FAULTS DURING THE EVENT. REASON FOR THE ANOMALOUS AUTO-THROTTLE INDICATION IS UNKNOWN.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 49,049 hrs · 7,993 cycles

EEL LIGHTS BLINKING FROM ROWS 20 TO 28 CHECKED SYSTEM PER WDM33-51-11 & 33-51-14, SPLICES SM42, SM41,SM5 OVER M1559 OK. SPLICES SM44, SM43 & SM45 OVER M1556 ALSO OK.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 47,568 hrs · 7,738 cycles

CRACK ON FWD UPPER PYLON SKIN INSIDE ACCESS PNL 432BR, NR 1 ENG. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: LINE — FAILED (HYD SYSTEM) · airframe 47,519 hrs · 7,727 cycles

C-HYDRAULIC SYSTEM QTY SLOWLY DECREASING. LEFT MAIN GEAR HYDRAULIC LINE FOUND LEAKING AT UPPER TRUNNION LOCATION. RESERVICED CENTER SYSTEM TO NORMAL. RYNGLOK REPAIR ACCOMPLISHED ON BRAKE HYDRAULIC LINE/TUBE. SPECIFIC HYDRAULIC LINE AND CAUSE OF LEAK NOT IDENTIFIED. SERVICE BULLETIN 767-32-0162 IS RELATED TO HYDRAULIC LEAK EVENTS IN THIS AREA. DUE TO LACK OF PART IDENTIFICATION, UNABLE TO DETERMINE IF THIS EVENT RELATED TO SPECIFIC SERVICE BULLETIN APPLICATION.

Part: SCREW — LOOSE (BEARING RETAINER) · airframe 47,217 hrs · 7,675 cycles

NR 2 ENGINE FLAMEOUT. FLAME OUT WAS CAUSED BY FUEL LEAK AT THE AIR/OIL COOLER MUSCLE LINE. THE FUEL MUSCLE LINE WAS REPLACED AND THE ENGINE WAS REMOVED WITH IN 25 CYCLES DUE TO A SURGE ABOVE 1.25 EPR CAUSED BY THE FLAME OUT. THE MUSCLE LINE FAILED DUE TO VIBRATION CAUSED BY THE ANGLE GEARBOX. THE ANGLE GEARBOX HAD THREE BEARING RETAINING SCREWS LOOSE AND ONE HAD FALLEN OUT. ROOT CAUSE OF THE FAILURE APPEARS TO BE INSUFFICIENT RETENTION OF THE AB4 BEARING RETAINING SCREWS. THE ADDED ADDITION OF LOCKING LIQUID WILL BE USED ON FUTURE BUILDS IN THE ANGLE GEARBOX.

Part: SWITCH — FAILED (CABIN PRESSURE) · airframe 46,456 hrs · 7,548 cycles

FWD EQUIP OVERHEAT MSG DISPLAYED. THE CABIN PRESSSURIZATION CONTROL MODULE M17, ROTARY SWITCH FAILED. THE SWITCH WAS REPLACED.

Part: BATTERY — DAMAGED (MASTER) · airframe 46,022 hrs · 7,471 cycles

MAIN BATTERY CHARGER STATUS MESSAGE. MAIN BATTERY REPLACED. SHOP REPORTS THE BATTERY WAS COMPLETELY DISCHARGED. BATTERY WAS PROCESSED THROUGH THE OVERHAUL CYCLE AND PASSED ITS ACCEPTANCE TEST.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 43,259 hrs · 7,012 cycles

EMERGENCY EXTERIOR LIGHT INOPERATIVE, AFT OF RIGHT WING. RELAMPED LIGHT.

Part: PUMP — LEAKING (RT ENGINE) · airframe 41,523 hrs · 6,702 cycles

LOSS OF HYDRAULIC FLUID FROM RIGHT SYSTEM. REPLACED RIGHT ENGINE HYD PUMP DUE TO LEAK BETWEEN MATING SEAM. ACP ENG RUN, NO LEAKS NOTED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,418 hrs · 6,681 cycles

AFT PIT T-CAP CORRODED AT BODY STATION 1175, BL 0 TO RBL 40. MAJOR REPAIR ACCOMPLISHED. REPAIRED AND INSTALLED FLOORBEAM T-CAP.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,418 hrs · 6,681 cycles

AFT PIT T-CAP CORRODED BODY STATION 1285, LBL 40. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM T-CAP.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,418 hrs · 6,681 cycles

AFT PIT T-CAP CORRODED BODY STATION 1207 AND RBL 40. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM T-CAP.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,418 hrs · 6,681 cycles

CABIN STATION 825-850, RBL 34, TRANSVERSE BEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. REPAIRED BEAM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,418 hrs · 6,681 cycles

AFT PIT FLOORBEAM T-CAP CORRODED BODY STATION 1241, RBL 44. MAJOR REPAIR ACCOMPLISHED. REPAIRED AND INSTALLED T-CAP.

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 41,418 hrs · 6,681 cycles

CABIN FLOORBEAM UPPER SURFACE GOUGED NEXT TO GALLEY FITTING AT BODY STATION 807, RBL 29. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED FLOORBEAM SPLICE DOUBLER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,418 hrs · 6,681 cycles

BS 852, LBL 34, FLOORBEAM CORRODED, MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM SECTION AND SPLICES.

Part: SPAR — CRACKED (NR 2 PYLON) · airframe 41,418 hrs · 6,681 cycles

NAC STA 221, NR 2 ENGINE PYLON, AFT UPPER SPAR WEB IS CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR PARTS.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 41,418 hrs · 6,681 cycles

BS 786, LBL 12, FLOORBEAM CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW FLOORBEAM SECTION.

Part: SKIN — CHAFED (FUSELAGE) · airframe 41,418 hrs · 6,681 cycles

BS 1809.5, LT FUSELAGE AT HORIZONTAL STABILIZER, LOWER SURFACE SKIN CHAFFED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER AND FILLER.

Part: SPAR — CRACKED (NR 2 PYLON) · airframe 41,418 hrs · 6,681 cycles

NAC STA 221, NR 2 ENGINE PYLON, UPPER SPAR WEB, IS CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR PARTS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,418 hrs · 6,681 cycles

BS 830-870, RBL 11, WL 200, UPPER CHORD CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM REPAIR.

Part: SKIN — CHAFED (FUSELAGE) · airframe 41,418 hrs · 6,681 cycles

BS 1809.5, RT EXTERIOR FUSELAGE, HAS EXCESSIVE CHAFFING AT LOWER BANANA FAIRING. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER AND FILLER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,418 hrs · 6,681 cycles

BS 1300 LBL 40-44 T-CAP FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP REPAIRS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,418 hrs · 6,681 cycles

CABIN FLOORBEAM UPPER SURFACE CORRODED AT BS 800-825, RBL 54. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 41,418 hrs · 6,681 cycles

BS 287 FLOORBEAM CRACKED, LEFT HAND SIDE. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR PARTS.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 41,418 hrs · 6,681 cycles

BS 287 FLOORBEAM CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR PARTS.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 41,418 hrs · 6,681 cycles

BS 400-420, STRINGER 36R-30R SKIN DOUBLER HAS BLIND FASTENERS. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,418 hrs · 6,681 cycles

BS 790, LBL 11, WL 200 TOP OF FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR PARTS AND SPLICES.

Part: INDICATOR — OUT OF TOLERANCE (COCKPIT) · airframe 40,704 hrs · 6,544 cycles

EICAS MSG TRAILING EDGE FLAP DISAGREE DISPLAYED. EMERGENCY DECLARED. LANDING WAS UNEVENTFUL. TEMPORARY INTERRUPTION IN THE FLAP/SLAT ELECTRONICS UNIT (FSPM) CAUSED A DISAGREE INDICATION TO GENERATED ON EICAS DISPLAY. ONE TIME DISRUPTION OF SYSTEM. ACCOMPLISHED FSEU BITE TEST PER MM AND NO FAULTS FOUND. FLAP INDICATOR EXHIBITED A SPLIT IN THE FLAP INDICATION NEEDLES GREATER THAN ALLOWED. SUBJECT FLAP INDICATOR WAS REPLACED AND CHECKED PER APPLICABLE MM. FLAP SYSTEM WAS OPERATIONALLY CHECKED SEVERAL TIMES PER APPLICABLE MM. ALL OPS CHECKS NORMAL.

Part: LIGHT — BROKEN (L1 DOOR) · airframe 38,135 hrs · 6,118 cycles

DOOR 1L EMER EXIT LIGHT IS BROKEN.

Part: LIGHT — BROKEN (L1 DOOR) · airframe 38,135 hrs · 6,118 cycles

DOOR 1L EMER EXIT LIGHT IS BROKEN.

Part: LINK — MISSING (LT MLG) · airframe 36,944 hrs · 5,923 cycles

LT MAIN LANDING GEAR HAS EVIDENCE OF CONTACTING UPPER WING PANEL DURING RETRACTION. *S/D* STABILIZING LINK WAS FOUND MISSING, ALLOWING UPSTOP FTG TO ROTATE FREELY, THEREBY CAUSING A PRELOAD BETWEEN GEAR AND GEAR DOOR. THIS CAUSED THE OVER-RETRACTION. LINK WAS POSSIBLY LEFT OFF DURING BRAKE ROD INSPECTION.

Part: WEB — CRACKED (NR 2 PYLON) · airframe 36,509 hrs · 5,843 cycles

NR 2 PYLON UPPER WEB AT IDG CABLE HOLE ACCESS HAS TO CRACKS. INSTALLED REPAIR DOUBLER REF: 54-53-02.

Part: WEB — CORRODED (FUSELAGE) · airframe 36,509 hrs · 5,843 cycles

AFT PIT BS 1280 RBL 18 FLOOR WEB CORRODED. INSTALLED REPAIR DOUBLER REF: SRM 51-70-13 FIGURE 01.

Part: WEB — CRACKED (NR 1 PYLON) · airframe 36,509 hrs · 5,843 cycles

NR 1 PYLON UPPER WEB AT IDG CABLE HOLE ACCESS HAS 2 CRACKS AT NP HOLES. INSTALLED REPAIR DOUBLER REF: SRM 54-53-02.

Part: WEB — CRACKED (NR 1 PYLON) · airframe 36,509 hrs · 5,843 cycles

NR 1 PYLON WEB CRACKED AT OUTBOARD DRAIN HOLE JUST FORWARD OF IDG CUTOUT INSIDE PANEL 441DT. INSTALLED REPAIR DOUBLER REF: SRM 54-53-02.

Part: ENGINE — LEAKING (NR 2) · airframe 35,348 hrs · 5,637 cycles

ON ROLLOUT, FLIGHT ATTENDANTS IN MID SECTION SMELLED SMOKE IN GALLEY / LAVATORY AREA. AIRCRAFT RETURNED TO FIELD. SUPPLEMENTAL DATA UPDATE CHECKED CARBON FILTERS IN FWD CARGO PIT AND MIXER AREA, NO FAULTS NOTED. ACCOMPLISHED HIGH POWER ENGINE RUN AND NO SMOKE VISIBLE. A STATIC OIL LEAK WAS NOTICED AT NR 2 ENGINE - CLEANED OUT RESIDUAL OIL. NO FURTHER DISCREPANCIES NOTED.

Part: SQUIB — WILL NOT TEST (LT WING EXIT) · airframe 35,061 hrs · 5,587 cycles

LEFT WING EMERGENCY EXIT SQUIB WILL NOT TEST.

Part: CONTROL PANEL — INOPERATIVE (RUDDER TRIM) · airframe 34,271 hrs

RUDDER TRIM INOP. DIVERTED DEN. *S/D* REPLACED RUDDER TRIM CONTROL PANEL (P/N: 233T6201-21).

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 33,446 hrs · 5,287 cycles

APPROXIMATELY 30 LIGHTNING STRIKES ON THE LEFT HAND SIDE STARTING FROM STA 785.9 FWD TO RADOME. HITS ARE ON CROWN, AROUND DOOR 1L AND BELOW CAPTS 3 & 2 WINDOWS AND ON RADOME, RT SIDE. RTF. OVERWEIGHT LANDING. *S/D* LIGHTNING STRIKE ON LEFT HAND SIDE OF AIRCRAFT WHILE CLIMBING THROUGH 10,000 FEET. AIRCRAFT LANDED 20,000 LBS OVERWEIGHT. COMPLETED PHASE 1 EXAMINATION PER MM. COMPLETED LIGHTNING INSPECTION PER PER MM. ALL HITS MARKED WITH GREASE PENCIL. REPAIRED DAMAGED AREAS PER SRM.

Part: ENGINE — FAILED (WING)

ENGINE FAILURE ON TAKEOFF. DUMPED FUEL. AMBER ALERT.

Part: CONNECTOR — FAILED (RADAR SYS)

WEATHER RADAR FAILED AFTER DEPARTING JFK. DIVERTED TO IAD DUE TO THUNDERSTORMS EN ROUTE. *S/D* THE WEATHER RADAR TRANSCEIVER (P/N 622-5122-103, MR43114 - 2032) WAS REPLACED AT IAD. THE SYSTEM OPS CHECKED NORMAL. UPDATE: 7/12/99 THE COAX CONTACT INSERT ON THE TRANSCEIVER BENCH CONNECTOR D391A WAS DAMAGED AND WOULD NOT MAINTAIN CONTACT. REPLACED CONNECTOR INSERT, SYSTEM OPERATIONALLY CHECKED OK.

Part: VALVE — FAILED (CABIN)

FL330 CABIN RATE BEGAN TO CLIMB AT MORE THAT 2,000 FEET PER MINUTE. ATTEMPTED AUTO MODE TO NR 2 MANUAL CABIN, STILL CLIMBING WITH OUTFLOW FULLY CLOSED. THE O2 MASKS DEPLOYED. DIVERTED TO RNO. *S/D* UPPER PRESSURE RELIEF VALVE (MR21313, SN OR DASH 2690) REPLACED AT SFO ON 16MAY99. THE PRESSURE RELIEF VALVE WAS SENT TO ALLIED SIGNAL FOR TESTING. PRELIMINARY TESTS SHOW THE VALVE FAILED OPEN AND WOULD NOT RESEAT. THE OUTFLOW VALVE (MR21314 DASH 10) WAS ALSO REMOVED AT SFO. BOTH THE OUTFLOW VALVE AND THE OUTFLOW VALVE ACTUATOR WERE FOUND WITHIN LIMITS BY THEIR RESPECTIVE COMPONENT SHOP.

Part: VALVE — FAILED (CABIN)

FL330 CABIN RATE BEGAN TO CLIMB AT MORE THAT 2,000 FEET PER MINUTE. ATTEMPTED AUTO MODE TO NR 2 MANUAL CABIN, STILL CLIMBING WITH OUTFLOW FULLY CLOSED. THE O2 MASKS DEPLOYED. DIVERTED TO RNO. *S/D* UPPER PRESSURE RELIEF VALVE (MR21313, SN OR DASH 2690) REPLACED AT SFO ON 16MAY99. THE PRESSURE RELIEF VALVE WAS SENT TO ALLIED SIGNAL FOR TESTING. PRELIMINARY TESTS SHOW THE VALVE FAILED OPEN AND WOULD NOT RESEAT. THE OUTFLOW VALVE (MR21314 DASH 10) WAS ALSO REMOVED AT SFO. BOTH THE OUTFLOW VALVE AND THE OUTFLOW VALVE ACTUATOR WERE FOUND WITHIN LIMITS BY THEIR RESPECTIVE COMPONENT SHOP.

Part: OIL — DECREASED (RT ENGINE)

RIGHT ENGINE OIL QUANTITY DECREASED TO 1 QUART. AIRCRAFT DIVERTED TO YQX. ENGINE WAS NOT SHUT DOWN. *S/D* SUSPECT LEAK AT NR 3 BEARING OIL SCAVENGE TUBE UPPER B-NUT. NO DEFECTS WERE FOUND. POSSIBLE INSTALLATION OR TORQUING ERROR. REVIEWED INSTALLATION AND TORQUING PROCEDURES WITH SHOP MECHANICS.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY EXIT LIGHTING (EEL) STRIP WAS INOPERABLE FROM SEAT 11G THROUGH RIGHT SIDE OF THE MID GALLEY. REPAIRED ASSEMBLY PER MM 2-0-15-5. OPERATIONS CHECK NORMAL.

Part: CHECK VALVE — FAILED (RT PACK)

THE RIGHT PACK WAS NOISY AND CAUSING A VIBRATION IN THE FORWARD CABIN DURING THE FLIGHT. THE AIRCRAFT DIVERTED TO JFK. *S/D* THE NOISE AND VIBRATION WAS CAUSED BY A LOOSE FLAPPER IN THE SUPPLY FAN CHECK VALVE. THE CHECK VALVE WAS REPLACED PER MM 21-58-02, OPERATIONS CHECK NORMAL.

Part: FIRE WARNING — MALFUNCTIONED (ENGINE)

AIRCRAFT RETURNED TO THE FIELD AT SFO UNDER AMBER ALERT DUE TO A FIRE BELL AURAL WARNING. *S/D* THE ENGINE FIRE DETECTION SYSTEM CAUSED THE AURAL WARNING. A BITE TEST WAS PERFORMED AND INDICATED NO FAULTS. THE M1000 BELL CHIME MODULE WAS REPLACED AS A PRECAUTION. THIS MODULE WAS DETERMINED TO BE SERVICEABLE AND WAS RETURNED TO SERVICE. NO OTHER FAULTS HAVE BEEN INDICATED SINCE THIS INCIDENT.

Part: POWER CABLE — FAILED (CABIN)

FOUND INOPERABLE EMERGENCY EVACUATION LIGHT STRIP FROM SEAT 11E BACK TO 19E. FOUND SIDEWALL CONNECTOR DAMAGED. REPLACED COMPLETE POWER CABLE FROM SIDEWALL TO LIGHT STRIPS. OPERATIONS CHECK INDICATES EEL NOW FULLY OPERATIONAL.

Part: EEL — INOP (CABIN)

EMERGENCY ESCAPE PATH LIGHTING INOP AT GALLEY. REPLACED LIGHT, CHECKS OK.