N66056

Part: MODULE — FAULTY (ZONE 100) · airframe 96,478 hrs · 13,676 cycles

UNSCHEDUALED STAB TRIM EICAS 7 TIMES DURING FLIGHT WITH AUTOPILOT ON & OFF. FOUND R FSPM FAULT MSG. 27-41076 ON YAW DAMP/STAB TRIM MODULE RIGHT. R & R FLAP/STABILIZER POSITION MODULE IAW AMM 27-58-01-904-001. PERFORMED FSPM TEST, BITE CHECKED GOOD. PERFORMED MCDP TEST 64 & 65, TEST PASSED. YSM BITE TESTED GOOD, NO FAULTS FOUND.

Part: FITTING — FOD (ZONE 800) · airframe 96,092 hrs · 13,619 cycles

DOOR 1R DOES NOT ARM. REMOVED DEBRIS FROM FLOOR FITTING, DOOR ARMS NORMALLY.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 96,037 hrs · 13,611 cycles

EMERGENCY ESCAPE SLIDE PRESSURE LOW 1L PERFORMED VISUAL INSPECTION OF L1 DOOR SLIDE CYLINDER REF AMM 25-66-02 , NEEDLE ON GREEN BAND OK TO CONTINUE.

Part: O-RING — LEAKING (APU FUEL) · airframe 96,037 hrs · 13,611 cycles

FUEL FUMES IN THE CABIN AND COCKPIT CONFIRMED FUEL ODOR COMING FROM BOTH PACKS. T/S TO APU FUEL LEAKING FUEL. APU FIRE HANDLE PULLED. INSPECTED APU, FOUND LEAK AT FUEL LINE. REMOVED AND REPLACED RECIRCULATION AIR FILTERS IAW AMM 21-25-02 AS PRECAUTION IAW AMM 05-51-56-202-001-001 PART D. UPON VISUAL INSPECTION OF THE FUEL CONTROL UNIT, FOUND FUEL SUPPLY TUBE FOR IGV ACTUATOR AND SURGE CONTROL VALVE LEAKING FUEL. REMOVED AND REPLACED PACKINGS ON FUEL TUBES 5, 6, AND 7 IAW AMM 49-31-01/401. OPS AND LEAK CHECK GOOD.

Part: PRESSURE SWITCH — FAULTED (NR 2 ENG FUEL) · airframe 95,997 hrs · 13,605 cycles

R ENG FUEL FILT MSG AFTER LEVEL OFF... ALL OTHER ENG INDICATION NORMAL REF FIM 73-11 FAULT TREE 803 T/SHOOTING, R/H FUEL FILTER REPLACED AS PER AMM 73-11-02 NIL FINDINGS , REPLACEMENT OF FUEL FILTER DIFFERENTIAL TRANSMITTER REQUIRED. FUEL PX SWITCH R & R IAW AMM 73-34-01-024-001. NO LEAKS EVIDENT POST RUN AND NO MAINTENANCE MESSAGES

Part: FUEL SYS — LEAKING (APU) · airframe 94,866 hrs · 13,451 cycles

TOXIC FUMES IN CABIN. APU FUEL LEAK. RAN BOTH PACKS, INSPECTED THE CABIN AND PERFORMED INSPECTION IAW AMM 05-54-56. NO SIGN OF ODOR FUMES THROUGHOUT THE CABIN.

Part: PCA — LEAKING (ZONE 600 ELEVTR) · airframe 94,570 hrs · 13,410 cycles

RIGHT HYD QTY LOW PER CREW DEBRIEF, APPEOX 2 HRS INTO FLT, HYD QTY STARTED TO DECREASE & NOT FLUCTUATE ON ARRIVAL QTY IND SHOWS .39 WITH BRAKES SET MATCHING HYD SERVICE PANAL GAUGE. ON ARRIVAL PERFORMED GVI OF RT MLG, WINGS, & BELLY OF A/C WITH NO NOTIABLE LEAKS FOUND. HYD QTY ON CENTER & LT TANK READS 0.95. SERVICED RT HYD UP TO 0.86 & FOUND HYD LEAK ON RT ELEVATOR. REMOVED MOST OTBD PANEL (345HB) FOR PCA INSPECTION & FOUND NO HYD LEAKS AT MOST OTBD PCA. WHEN HYD RAN & ELEVATORS MOVED FOUND VERY HEAVY MIST FROM MIDDLE PCA ENCLOSURE. AFTER MIDDLE PCA PANEL (345GB) REMOVED & OPERATED SYS AGAIN & FLT CONTROL WAS UNABLE TO DUPE MIST. INSPECTED ALL HYD LINES WITH NO FAULTS. SUSPECT EITHER MIDDLE PCA COLD SOAKED & OR ROD END SEAL. RESEALED & STOPPED HYD LEAK. DUE TO UNABLE TO DUP FAULT WITH MIDDLE PCA SUGGEST MIDDLE PCA REPLACEMENT OR FURTHER TESTING. REMOVED RT SYS, RT ELEVATOR (MIDDLE PCA ) IAW AMM 27-31-05-424-027 , C/W RII REQUIREMENT FOR ATTACH POINT. INSTALLED RT SYS RT ELEVATOR (MIDDLE PCA) IAW AMM 27-31-05-424, OPS & LEAK CKD GOOD.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 93,964 hrs · 13,332 cycles

EMERGENCY LIGHTS OPERATIONAL CHECK FOUND SLIDE AND OVERWING ESCAPE LIGHT EMERGENCY INOPERATIVE NEAR DOOR 4L/H. REMOVED AND REPLACED LAMP FROM SLIDE AND OVERWING ESCAPE LOGHT EMERGENCY NEAR DOOR 4L/H AS PER AMM TASK 33-51-06-902-082. GOOD FOR SERVICE.

Part: IDG — FAULTED (NR 2) · airframe 93,855 hrs · 13,318 cycles

RT GEN OFF. RESET ONCE. FAILED A SECOND TIME. PERFORMED BPCU BITE PER MM 24-11- 00. FOUND MM 24-35002 FOR RIDG PHASE A CURRENT DISAGREE. PERFORMED BPCU BITE PER MM 24-11-00. FOUND R IDG PHASE A CURRENT DISAGREE, MM 24-35002. PERFORMED BPCU BITE PER MM 24-11-00. FOUND R IDG PHASE A CURRENT DISAGREE, MM 24-35002. PERFOMRED BPCU BITE PER MM 24-11-00. FOUND MM 24-35002 "PH A CUR DISAGREE" UNDER R IDG/PFO DPCT. SEE FIM 24-20 T 844 USED FIM 24-20 TASK 844 PART B (REPLACE GCU) REMOVED AND INSTALLED NEW R/H GCU IAW 24-22-02 WITH GEN STILL NOT COMING ONLINE FAILED OPS CHECK. DURING GROUND RUN FOUND WHEN GEN P/BSW IS CYCLED ON ATA 24 MAINT PAGE FREQS COME UP TO 400 THE DROP TO 0. SWAPPED L/H AND R/H ENGINE GCU TO VERIFY NEWLY INSTALLED GCU WASNT BAD FROM STOCK NO HELP. REINSTALLED ALL ORIGINAL GCU'S BACK INTO NORMAL AND REPERFORMED BPCU GROUND TEST IAW 24-22-00 WITH GCU PASSING GROUND TEST AND BPCU PASSING. SUSPECT IDG FAILED. FOLLOWED FIM FOR MESSAGE 24-35002, REMOVED AND REPLACED E2 IDG IAW AMM 24-11-01, LEAK AND OPS CHECK GOOD AT THIS TIME, NO CURRENT MAINTENANCE MESSAGE PRESENT. QC WITNESSED TORQUE OF IDG FEEDER CABLES. VERIFIED INSTALLATION OF NUMBER 2 ENGINE IDG PHASE LEADS PER AMM TASK 24-11-01-404-012-002. I

Part: PUMP — FAULTED (FUEL BOOST) · airframe 88,816 hrs · 12,627 cycles

RIGHT AFT FUEL PUMP FAILED IN FLIGHT DEFECTS NOTED. REF FIM 28-22 FAULT TREE 819. ACCOMPLISHED IDT REQUIREMENTS OF CDCCL BONDING JUMPER SAFETY AND SECURITY. ELECTRICAL BONDING RESISTANCE CHECK WITHIN LIMITS IAW AMM TASK 28-22-03-404-074, AMM TASK 28-22-03-706-014. RIGHT AFT FUEL PUMP. DURING T/S SHOOTING FOUND GFI RELAY K10702 IN P141 PANEL POPPED, R&R RT AFT FUEL BOOST PUMP. REF AMM 28-22-03. OPS AND LEAK IDT BONDING JUMPER INSTALLATION AND BONDING RESISTANCE CHECK REMOVED AND REPLACED GFI RELAY K10702 REF AMM TASK IDT BONDING JUMPER INSTALLATION AND BONDING RESISTANCE CHECKS RESET IT AND OPS CHECKED R AFT PUMP WITH TOTAL FUEL OF 112K CHECKS NOT ACCOMPLISHED AT THIS TIME. PARTS USED: STILL REQUIRED. 28-22-18-400-801. INSPECTION REQUIRED FOR OPS CHECK. STILL REQUIRED.POUNDS FOR 10 MINUTES WITHOUT FAILURE AND NO PRESSURE LIGHT 76-2821-9-9001,QTY :1 ILLUMINATING DURING OPERATION, TESTED MULTIPLE TIMES WITH NO ADD EMP:U383580 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1928071 SN OFF 1921 PUMP, AY-MAIN T OFF 76-2821-9-9001 1921 ON 76-2821-9-9001 0602 PERFORMED OPERATIONAL CHECK OF GFI RELAY K10702 REF AMM TASK 28-22-00-715-696. OPS CHECK GOOD. ACCOMPLISHED IDT REQUIREMENTS OF GFI RELAY K10702.ALI REQUIREMENTS MET IAW AMM TASK 28-22-00-715-696. LEAK AND OPS CK GOOD

Part: STIFFENER — CRACKED (STA 971) · airframe 88,528 hrs · 12,585 cycles

CABIN PRESSURE DECK PNL STA 971 BTN LBL 85.9 AND LBL 97.42 STIFFENER AND L ANGLE FOUND CRACKED TRANSFER REF. NON-ROUTINE HX NRC WO.2534260. CABIN PRESSURE DECK PANEL STA 971 BTN LBL859 TO LBL97.42 STIFFENER AND ANGLE REPLACED AS PER SRM 51-10-02 AND EC/RA NO. 5350-02508 REV-.

Part: STIFFENER — CRACKED (STA 665) · airframe 88,528 hrs · 12,585 cycles

LHW L/E STA 665 FRONT SPAR ATTACH STIFFENER FOUND CRACKED TRANSFER REF. NON-ROUTINE HX NRC WO.2487576. LHW L/E STA 665 FRONT SPAR STIFFENER FABRICATED AND INSTALLED ATTACHED FORM 44-0008 ITEM 1-17 ACCOMPLISHED. IAW RI NO. RI-57-00-16577 (FINAL NO DEVIATION WITH EC/RA NO. REWORKED AREA LEAK CHECK CARRIED OUT AND NO LEAK FOUND IAW AMM 28-11-00. RII INSPECT IS OKAY.

Part: STIFFENER — CRACKED (NR 1 PYLON) · airframe 88,528 hrs · 12,585 cycles

NUMBER 1 PYLON NACELLE STRUT AFT TORQUB BOX (INT) O/B STIFFENER AT NAC. WL 1436 AND NAC STA 265.4-295 FOUND DAMAGE. REPLACED AS PER SRM 51-10-02 AND FASTENER INSTALLED AS PER SRM 51-40-02

Part: TEE FITTING — CORRODED (LH BS955) · airframe 88,528 hrs · 12,585 cycles

TEE FITTING FOUND CORRODED TRANSFER REF. NON-ROUTINE HX NRC WO.2533217. LH BS 955 T FITTING REPLACED AS PER EC/RA NO.5340-02174 REV-. ATTACHED FORM 44-0008 ITEM 1-8 ACCOMPLISHED.

Part: TEE FITTING — CORRODED (RH BS955) · airframe 88,528 hrs · 12,585 cycles

RH BS955 T-FITTING FOUND CORRODED TRANSFER REF. RH STA 955 T FITTING REPLACED AS PER EC/RA NO.5340-02175 REV-.

Part: SHEAR TIE — CORRODED (BULK CARGO) · airframe 88,528 hrs · 12,585 cycles

BULK CARGO COMPT - BELOW FLOOR SHEAR TIE FOUND CORROSION AT STA 1540 BTN S38L-S39L (AS MARK) TRANSFER REF. NON-ROUTINE HX NRC WO.2494482 AND BULK CARGO COMPT BELOW FLOOR SHEAR TIE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 AT STA 1540 BTN S38L AND S39L. AND ATTACHED FORM 44-0008 ITEM 1 TO 12 ACCOMPLISHED.

Part: BEAM — CORRODED (STA325 LBL55) · airframe 87,315 hrs · 12,403 cycles

CABIN FWD WET AREA FOUND CORROSION ON THE TEE CHORD UPPER SURFACE OF PREVIOUS FLOOR BEAM REPAIR AT STA325 LBL55 REFER TO BSH N03 30 PERFORMED FLOOR BEAM REPAIR AT STA325 AS PER ECRA5310-08167 DETA IL STEPS REF TO ATTACHED 44-0008 FORM WORK ACCOMPLISHED BY V9142 47 INSPECTION PERFORMED BY BOEING SHANGHAI QC INSPECTOR JIANG, XIAO XIANG BSH 669. ADD EMP:V914247

Part: BEAM — CORRODED (STA303 LBL46.5) · airframe 87,315 hrs · 12,403 cycles

CABIN FWD WET AREA FOUND CORROSION ON THE TEE CHORD UPPER SURFACE OF PREVIOUS FLOOR BEAM REPAIR AT STA303 LBL46.5 REFER TO BSH N 0329 PERFORMED FLOOR BEAM REPAIR AT STA303 AS PER ECRA5310-08166 DETA IL STEPS REF TO ATTACHED 44-0008 FORM WORK ACCOMPLISHED BY V9142 47 INSPECTION ACCOMPLISHED BY BOEING SHANGHAI QC INSPECTOR JIANG, XIAO XIANG BSH 669. ADD EMP:V914247

Part: SEAL — MISSING (PANEL) · airframe 86,173 hrs · 12,242 cycles

LH MAIN FUEL QTY HARNESS NEEDS SEALING AT BUSSING PLUG AND 2 EACH INTERNAL GROMETS AT RIB FEED THROUGH . REF AMM 28-41-09 INSTALLED BUSSING PLUG AND SEALED GROMET AT PANEL 541JB/HB COMPLETED SEALING GROMETS.

Part: HYDRAULIC LINE — LEAKING (WW) · airframe 83,480 hrs · 11,827 cycles

CENTER HYD QTY DROPPED TO .46RF TWO HOURS INTO FLT WHILE AT CRUISE ...C HYD PRESS NORMAL ON INITIAL WALK AROUND FOUND HYDRAULIC FLUID LEAK, RIGHT WING FOUND CROSS UNION LEAKING REF LPC 32-32-56-03 ITEM 520. REMOVED TRAILING EDGE JUST OUTBOARD OF RIGHT LANDING GEAR. 2 EA PNLS AFT OF GEAR FOR ACCESS. SECURED LINE NO LEAKS NOTED. LEAK ONLY WITH GEAR UP. FOUND HYDRAULIC LINE CROSS UNION OUTBOARD OF RMLG ON REAR SPAR 674BB AND 652CB. CLEANED AREA AND REPLENISHED HYDRAULIC SYSTEM LEAKING WITH GEAR IN UP POSITION. SECURED HYDRAULIC LINE TO REF AMM 12-12-01-613-059. FITTING REF AMM 29-00-99-790-801-C1, PERFORMED HYDRAULIC LEAK CHECK, CHECKS GOOD WITH NO LEAKS NOTED. REINSTALLED PANELS ADD EMP:381113

Part: CONTROL PANEL — UNSERVICEABLE (FLIGHT DECK) · airframe 82,723 hrs · 11,714 cycles

MCP ALTITUDE WINDOW CANT BE CHANGED WITH A/P ON HAVEE TO CLICK O FF A/P AND FD TO CHANGE ALT REPLACED MODE CONTROL PANEL IAW AMM INSTALLATION REFERENCE: TASK 22-11-02-402-008 PERFORMED TEST 04 AND TEST 30 REFERENCE: TASK 22-00-02-742-006-001 OPS CK GOOD ACFT RETAINS FULL CAT CAPABILITY ROTABLE PARTS CHANGE WAS INDICATED - TT # 1877346 SN OFF 2575 PANEL, CONTROL, OFF 99-2211-9-0003 2575 ON 99-2211-9-0003 2925

Part: DRAIN LINE — CRACKED (GALLEY) · airframe 81,843 hrs · 11,546 cycles

B767-25-3-0068 - FWD CARGO L/H STA 480 TO STA 500 SIDE WALL INSI DE, A GALLEY DRAIN LINE, CONNECT RUBBER HOSE FOUND TORN. REF N/R L/P 9130151 AND ORIGINATED BY EMP V896834. FWD CARGO L/H STA 480 TO 500 SIDE WALL AREA GALLEY DRAIN LINE RE PLACED AS PER AMM 20-10-10. ATTACH FORM 44.0008 ITEM 1 TO 30 ACC OMPLISHED. ADD EMP:V896920 UNDER THE FAULTY GALLEY HOSE FOUND EVIDENCE OF SPILLAGE, FWD CARGO LH STA 480 TO STA 500 UNDER SPILL AREA NEED REMOVE FURTHER SLOPE AND SIDEWALL PNLS FOR MORE INVESTIGATION IAW EC2011-01000 REV AB ADD EMP:V898560 PERFORM DEEP CLEAN STA 566-610 AND 632-654+22 LH BELOW FLOOR 20" ADD EMP:V901205 -04.PER FORM DEEP CLEAN STA 544-654A+22 LH SLOPE INTERNAL AREA. ELECT BUNDLES AT LH SIDEWALL INTERNAL STA 478-500 PER SWPM 20-10 BILGE AREA PER ECRA 2011-01000 REV AB. PERFORM DEEP CLEAN ON PERFORM DEEP CLEAN ON STA 434-544 S27L-S37L SLOPE & BELOW FLOOR AREA PER ECRA 2011-01000 REV AB. PERFORM ECRA 2011-0100 GALLEY SPILL 2B (B) IN AFFECTED AREA. FWD CARGO STA 566-610 AND STA 632 -654+22 LH BELOW FLOOR 20" AREA INSPECTED AND NO STRUCTURE CORROSION FOUND.

Part: SHEAR TIE — CORRODED (BS 1417 S38-39L) · airframe 81,843 hrs · 11,546 cycles

SUPPORT TASK - BULK CARGO STA 1417 S38L - S39L POSITION SHEAR TI E FOUND CORROSION. REF N/R L/P 9131387 AND ORIGINATED BY EMP V89 6810. BULK CARGO STA 1417 S38L-39L SHEAR TIE REPLACED AS PER SMR 51-10 -02 AND FASTENER INSTALLED AS PER SRM 51-40-02, DWG 146T1216.ATT ACH MAINTENANCE WORK SHEET FORM 44.0008 ITEM 1 TO 10 ACCOMPLISHE D ( NEW SHEAR TIE LOCAL FABRICATED DETAIL REF NRC L/P9131447 P/N 14T2102-492. ADD EMP:V896816 RII BY HX243351 APPROVED. ADD EMP:V906449

Part: SHEAR TIE — CORRODED (BS 1417 S37-38L) · airframe 81,843 hrs · 11,546 cycles

SUPPORT TASK - BULK CARGO BELOW FLOOR STA 1417 S37L - S38L SHEAR TIE FOUND CORROSION. RER N/R L/P 9131332 AND ORIGINATED BY EMP V896810 BULK CARGO BELOW FLOOR STA 1417 S3TL-38L SHEAR TIE REPLACED AS P ER SRM 51-10-02 AND FASTENER INSTALLED AS PER SRM51-40-02, DWG 1 46T1216 ATTACH MAINTENNACE WORK SHEET FORM 44.0008 ITEM 1 TO 9 A CCOMPLISHED. ADD EMP:V896816 RII BY HX243551. APPROVED ADD EMP:V906449

Part: SHEAR TIE — CORRODED (BS 1417 S39L-R) · airframe 81,843 hrs · 11,546 cycles

SUPPORT TASK - BULK CGO COMPT BELOW FLOOR STA 1417 S39L - S39R P OS SHEAR TIE FOUND CORROSION. REF N/R L/P 9131333 AND ORIGINATED BY EMP V896810 BULK CARGO COMPT BELOW FLOOR (STA 1417 S39L-39R SHEAR TIE REPLAC ED AS PER SRM 51-10-02 AND FASTENER INSTALLED AS PER SRM 51-40-0 2, DWG 146T1216. ADD EMP:V896816 RII BY HX 243551. APPROVED. ADD EMP:V906449

Part: SHEAR TIE — CORRODED (BS 1417 S38 -39L) · airframe 81,843 hrs · 11,546 cycles

SUPPORT TASK - BULK CARGO STA 1417 S38L - S39L POSITION SHEAR TI E FOUND CORROSION. REF N/R L/P 9131387 AND ORIGINATED BY EMP V89 6810. BULK CARGO STA 1417 S38L-39L SHEAR TIE REPLACED AS PER SMR 51-10 -02 AND FASTENER INSTALLED AS PER SRM 51-40-02, DWG 146T1216.ATT ACH MAINTENANCE WORK SHEET FORM 44.0008 ITEM 1 TO 10 ACCOMPLISHE D ( NEW SHEAR TIE LOCAL FABRICATED DETAIL REF NRC L/P9131447 P/N 14T2102-492. ADD EMP:V896816 RII BY HX243351 APPROVED. ADD EMP:V906449

Part: SHEAR TIE — CORRODED (BS 1417 S37-38L) · airframe 81,843 hrs · 11,546 cycles

SUPPORT TASK - BULK CARGO BELOW FLOOR STA 1417 S37L - S38L SHEAR TIE FOUND CORROSION. RER N/R L/P 9131332 AND ORIGINATED BY EMP V896810 BULK CARGO BELOW FLOOR STA 1417 S3TL-38L SHEAR TIE REPLACED AS P ER SRM 51-10-02 AND FASTENER INSTALLED AS PER SRM51-40-02, DWG 1 46T1216 ATTACH MAINTENNACE WORK SHEET FORM 44.0008 ITEM 1 TO 9 A CCOMPLISHED. ADD EMP:V896816 RII BY HX243551. APPROVED ADD EMP:V906449

Part: SKIN — CRACKED (BS 1654-1678) · airframe 81,843 hrs · 11,546 cycles

SUPPORT TASK - EA 5380-01178 REV A OP 003 L/H FUSELAGE SKIN BETW EEN 1654 TO 1678 FOUND 2EA CRACK AT STR 13AL APPROX 3/8" AND 5/8 " IN LENGTH. N/R L/P 9130401 AND ORIGINATED BY EMP V924736 CREATE REPEAT INSPECTION AS PER SRM 53-80-01-2R-7 REPAIRT TABLE 202 DETAIL XIV ADD EMP:V901848

Part: STIFFENER — CRACKED (NLG WW) · airframe 81,843 hrs · 11,546 cycles

SUPPORT TASK - EA5310-07143 REV.D OP 002, AD 2017-17-16 RH NOSE WHEEL WELL VERTICAL STIFFENER ON STA 287 BETWEEN WL 159 AND 185. FOUND CRACK GENERATED AND ACCOMPLISH OP 004. REF N/R L/P 913051 8 . RH NOSE WHEEL WELL VERTICAL STIFFENER ON STA 287 BETWEEN WL 159 AND 185. REPAIR ACCOMPLISHED AS PER EA 5310-07143 REV D OP 004 (WORK DETAIL REFER SEQ 1408).

Part: PANEL — MISSING (RT WING) · airframe 81,843 hrs · 11,546 cycles

PDA 3 UPON ARRIVIAL FOUND PANEL 621FB ON RIGHT WING MISSING. FURTHER DETAILS AWAITED

Part: BRACKET — MISSING (RT MLG) · airframe 81,669 hrs · 11,520 cycles

FOUND AT RH MLG ABOVE TIRE #7 BRACKET LOOSE AND MISSING 1 BLOCK AT ELETRICAL CONDUIT. REF. IPC 32-10-50-01E ITEM 205. PART NEEDED P/N 287T6138-9 ACCOMPLSHED VISUAL INSPECTION AT WIRE CONDUIT, NO DAMAGE FOUND. FABRICATED A CLAMP BLOCK WITH RUBBER MOUNT AS REQUIRED. INSTALLED CLAMP ASSY REF IPC 32-10-50-01E, CHECKED CONDUIT ARE SECURED. ACCOMPLISHED INTERIM REPAIR AS PER EA/RA # 3210-02547. ACCOMPLISH VISUALLY INSPECT THE CLAMP BLOCK FOR SECURITY AND SIGNS OF DETERIORATION DAILY AND ACCOMPLISH PERMANET REPAIR WITHIN 10 DAYS. PART NEEDED M&E 76-3210-3-0007. ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2 DAILY AND ACCOMPLISH PERMANENT REPAIR PER PART 3 WITHIN 10 DAYS. TOMC-APPROVAL FROM SC1ELBYC COMMENT INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: LIGHT — DIM (COCKPIT) · airframe 73,249 hrs · 10,312 cycles

COCKPIT OVERHEAD PORTABLE EMERGENCY EXIT LIGHT FOUND DIM. REPLACED THE LIGHT AND TEST NORMAL IAW AMM 33-51-01

Part: WEB — CRACKED (NR 2 NACELLE) · airframe 73,249 hrs · 10,312 cycles

NR 2 PYLON MID SPAR WEB FOUND CRACKED. REPAIRED IAW SRM 54-55-01, REPAIR 2, FIG 202, DETAIL I.

Part: WEB — CRACKED (NR 1 NACELLE) · airframe 73,249 hrs · 10,312 cycles

NR 1 PYLON NAC STA 223, MID SPAR WEB FOUND CRACKED. REPAIRED IAW SRM 54-55-01, REPAIR 2, FIG 202, DETAIL I.

Part: FLOORBEAM — CORRODED (BS 324) · airframe 73,249 hrs · 10,312 cycles

FLOORBEAM BS 324, LBL 55 FOUND CORRODED. THE CORROSION WAS REMOVED IAW SRM 51-10-02. REPAIRED IAW ECRA 5310-07355, REV.

Part: FLOORBEAM — CORRODED (BS 347) · airframe 73,249 hrs · 10,312 cycles

CABIN FLOORBEAM BS 347, RBL 32 TO 41 FOUND CORRODED. THE CORROSION WAS REMOVED IAW SRM 51-10-02, AND FOUND OUT LIMITS IAW SRM 53-00-51 ALLOWABLE DAMAGE 1, FIG 101. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201, DETAIL I.

Part: ALTIMETER — STUCK (STANDBY POSITION) · airframe 72,915 hrs · 10,264 cycles

STBY ALTIMETER HANGS UP THEN JUMPS 250 FT DURING CLIMB. STBY ALTIMETER REPLACED PER AMM 34-13-06-344-031. ALL INDICATION S NOW NORMAL

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,851 hrs · 10,254 cycles

L2 EXTERIOR EMERGENCY LIGHT INOP. R&R L2 EXTERIOR LIGHT BULB AND SECURED LIGHT ASSEMBLY. VISUAL OPS CHECK OF L2 EXTERIOR LIGHT, CHECKS GOOD. A/C O.K. TO CONTINUE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,851 hrs · 10,254 cycles

FOUND L4 EXTERIOR EMERGENCY LIGHT NOT OPERATING. REMOVED AND REPLACED L4 EXTERIOR EMERGENCY LIGHT BULB AND M739 BATTERY PACK IAW WDM 33-512-15.L4 EXTERIOR EMERGENCY LIGHT VISUALLY OPS CHECK OK, A/C OK TO CONTIN UE.

Part: FLASHLIGHT — INOPERATIVE (L2 DOOR) · airframe 70,290 hrs · 9,891 cycles

2L FWD FACING FLASHLIGHT NOT CHARGING. REPLACED EMERG FLASHLIGHT AT 2L.

Part: MONITOR — FAULTY (HYDRAULIC SYS) · airframe 64,806 hrs · 9,106 cycles

LOST RT HYD FLUID SYS, QTY READS ZERO. NOTE TWO HOURS INTO FLIGHT QTY RETURNED TO NORMAL 1.10. PLACED ON MEL RT HYD QTY INDICATION INOPERATIVE. TROUBLESHOOTING REQUIRED. COMPLIED WITH DDP CHECK BEFORE EACH DEPARTURE FLIGHT IAW FIM 29-11-00-815-899-0-01. R & R HYD QTY MONITOR UNIT M122 IAW AMM 29-33-01. OPERATIONS CHECKED NORMAL & QTY INDICATOR NORMAL. PLACARDS REMOVED, OK TO CONTINUE. ROTABLE PARTS CHANGE WAS INDICATED TT 1762187, SN OFF 00478 MONITOR, HYD QTY OFF 64-2933-9-0001 0478 & ON 64-2933-9-00010437.

Part: UNKNOWN — MULTIPLE FAIL (COCKPIT) · airframe 61,023 hrs · 8,572 cycles

OVERWEIGHT LANDING PERFORMED 366.6 RNWY 04R DUE TO DIVERSION WITH NO CAPTAIN FD FMA SPEED TAPE & ALTITUDE TAPE, NO AUTO THROTTLES & ONE WORKING AUTO PILOT, FIRST OFFICER`S RT. PERFORMED OVER WEIGHT LANDING PHASE 1 OPTION A. ACFT OK TO CONTINUE AMM 25-51-35. RESET LT BUS TIE INDICATION CORRECT PERFORMED TEST 30 AMM 22-00-02 ACFT REMAINS FULL CAPABLE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,498 hrs · 8,235 cycles

EMERGENCY LIGHTS FAILED FUNCTION CHECK AT SEAT 3KL. R & R EMERGENCY LIGHT BATTERY PACK AT SEAT 3KL IAW MM 33-51-07. EMERGENCY LIGHT FUNCTION CHECK PASSED. OPERATIONS NORMAL, OK TO CONTINUE .

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,498 hrs · 8,235 cycles

EMERGENCY LIGHT FUNCTION CHECK FAILED AT SEAT 30KL. R& R EMERGENCY LIGHT BATTERY PACK AT SEAT 30KL IAW MM 33-51-07. EMERGENCY LIGHT FUNCTION CHECK PASSED. OPERATIONS NORMAL, OK TO CONTINUE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,498 hrs · 8,235 cycles

EMERGENCY LIGHT FAILED FUNCTION CHECK AT SEAT 24KL. R & R EMERGENCY LIGHT BATTERY PACK AT SEAT 24KL IAW MM 33-51-07. EMERGENCY LIGHT FUNCTION CHECK PASSED. OPERATIONS NORMAL, OK TO CONTINUE.

Part: SEAT TRACK — CORRODED (BS 1263-1285) · airframe 48,759 hrs · 6,925 cycles

BS 1263-1285 RBL 88 SEAT TRACK CORRODED. SEAT TRACK REPLACED PER ECRA 5320-02046 REV. HFEC FOUND NO CRACKS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,759 hrs · 6,925 cycles

CABIN BS 325 LBL 33 TO RBL 55 FLOORBEAM CORRODED. CABIN BS 325 LBL 64" TO RBL 63" FLOORBEAM REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201 AND HFEC NIL CRACK FOUND ATTACH MAINTENANCE WORK SHEET FORM 44.0008 ITEM 1 TO ITEM 17 ACCOMPLISHED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,759 hrs · 6,925 cycles

CABIN BS 303 LBL 30-33 FLOORBEAM CORRODED. CABIN BS 303 LBL 11" TO LBL 68" FLOORBEAM REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201 AND HFEC NIL CRACK FOUND ATTACH MAINTENANCE WORK SHEET FORM 44.0008 ITEM 1 TO ITEM 24 ACCOMPLISHED.

Part: SUPPORT FITTING — CORRODED (BS 1608) · airframe 48,759 hrs · 6,925 cycles

CABIN BS 1608 LBL 54 AFT GALLEY SUPPORT FITTING FOUND CORRODED. GALLEY SUPPORT FITTING REPLACED AS PER AMM 20-11-00.

Part: SUPPORT FITTING — CORRODED (BS 1582) · airframe 48,759 hrs · 6,925 cycles

CABIN BS 1582 LBL 88 GALLEY SUPPORT FITTING FOUND CORROSION. GALLEY SUPPORT FITTING REPLACED AS PER AMM 20-11-00.

Part: SUPPORT FITTING — CORRODED (BS 1582) · airframe 48,759 hrs · 6,925 cycles

CABIN BS 1582 RBL 88 GALLEY SUPPORT FITTING FOUND CORRSION. GALLEY SUPPORT FITTING REPLACED AS PER AMM 20-11-00.

Part: LIGHT — BROKEN (CABIN) · airframe 46,491 hrs · 6,640 cycles

WALL MOUNTED ESCAPE PATH LIGHT GLY NR 5 LT WALL FACE AFT BROKEN ASSY. REMOVED AND REPLACED WALL MOUNTED ESCAPE PATH LIGHT PER AMM 33- 51-10. OPS CHECK OK.

Part: PCA — LEAKING (ELEVATOR) · airframe 44,121 hrs · 6,342 cycles

C HYD QTY LIGHT CAME ON IN FLIGHT FOUND LT ELEV INBOARD PCA LEAKING. R&R LT ELEV INBRD PCA. PER A/C M/M 27-31-05 UP TO AND INCLUDING STEP 15 OF PG 413, SEE N/R 4457919 FOR COMPLETION OF INSTALLATION AND OPS & LEAK CHECK. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1401989 SN OFF 05285 ACTUATOR, ELEVA OFF 64-2731-9-0001 5285 ON 64-2731-9-0001 5397.

Part: SQUIB — BLOWN (EXTINGUISH SYS) · airframe 42,123 hrs · 6,093 cycles

SQUIB TEST NR 1 DOESN’T COME ON (LIGHT) REF W/C 64-2620-1-7102. REMOVED AND REPLACED FLOW VALVE SQUIBS PER MM 26-23-06. OPS CHECKED OK FWD CARGO.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 34,471 hrs · 5,091 cycles

CABIN - STATION 303 LBL 28 TO 38 FLOOR SUPPORT FOUND CORRODED. CABIN - STATION 303 LBL 28 TO LBL 38 FLOOR SUPPORT REPAIRED PER SRM 53-00-51 FIG 201, REPAIR 1 (UPR SPLICE STRAP ONLY).

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,471 hrs · 5,091 cycles

STATION 325 LBL 25 TO LBL 36 FLOOR SUPPORT FOUND CORRODED. STATION 325 LBL 25 TO LBL 36 FLOOR SUPPORT REPAIRED PER SRM 53-00-51, FIG 201 REPAIR 1, AND HFEC NO CRACK FOUND.

Part: WIRE — BROKEN (OXGEN MASK) · airframe 34,236 hrs · 5,053 cycles

DISCOVERED F/O OX2 MASK COMM WIRE BROKEN, UNABLE TO COMMUNICATE ON. REMOVED AND REPLACED A/C AEROSPACE MASK PER AMM 35-11-51. OPS CHECK OK. P/N 174692N7 TK, ON-1187028, S/N OFF-12871. ROTABLE PARTS CHANGE WAS INDICATED - TT 1187028 S/N OFF 01287 MASK, OXYGEN, C OFF 64-3511-9-9001 2871, ON 64-3511-9-9001 2465.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,791 hrs · 4,864 cycles

DURING EMERGENCY LIGHT OPS CHECK, CENTER ROW SEAT LIGHTS DID NOT COME ON AT SEATS 5D THRU 7D. FOUND BAD POWER SUPPLY ON THE RT SIDE OF A/C AT SEAT ROW 6KL. REMOVED AND REPLACED POWER SUPPLY UNIT PER AMM 33051-07, OPERATION CHECKS GOOD.

Part: FLOORBEAM — CRACKED (BS 246) · airframe 23,556 hrs · 3,555 cycles

INSPECTION FOUND A .75 INCH CRACK IN LOWER FLOORBEAM WEB AT BS 246, BL 0. THE FLOORBEAM WEB WAS REPAIRED IAW ECRA 5310-04566.

Part: FLOORBEAM — CORRODED (BS 325) · airframe 23,556 hrs · 3,555 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT BS 325, LBL 60 TO RBL 60. REPAIRED FLOORBEAM IAW SRM 53-00-51, REPAIR 1, FIGURE 201.

Part: FLOOR SUPPORT — CORRODED (BS 303-325) · airframe 23,556 hrs · 3,555 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 303-325, LBL 30. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 303) · airframe 23,556 hrs · 3,555 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT BS 303, LBL 22 TO 30. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 201, REPAIR 1.

Part: ACM — INOPERATIVE (LEFT) · airframe 20,724 hrs · 3,156 cycles

THE FLIGHT ATTENDANT REPORTED A HAZY SMOKE IN THE FORWARD CABIN THAT WAS DESCRIBED AS CHEMICAL IN NATURE WHLIE CRUISING AT FL 380. THE CABIN BECAME CLEAR AFTER APPROXIMATELY 2-3 MINUTES. THE -L PACK MODE- EICAS MESSAGE DISPLAYED DURING DESCENT TO FL 280. THE LEFT PACK TRIPPED AFTER LANDING. TROUBLESHOOTING FOUND THE LT ACM AT FAULT. THE LT ACM WAS REMOVED AND REPLACED IAW MM 21-51-03. LEAK AND OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,159 hrs · 2,793 cycles

THE COCKPIT EMERGENCY LIGHT DID NOT ILLUMINATE DURING TEST. TWO BATTERIES ON THE COCKPIT EMERGENCY LIGHT PACK WERE REMOVED AND REPLACED IAW MM 33-51-01.