N644UA

Part: DOOR — MISSING (NR 2 NACELLE) · airframe 131,017 hrs · 20,140 cycles

DURING EPDSC WALKAROUBD FOUND MISSING NACELLE STRUT ACCESS DOOR ON INBOARD SIDE OF ENGINE 2. REPLACED ENGINE 2 NACELLE STRUT ACCESS DOOR REF IPC 54-52-01-01. NO OTHER DAMAGE NOTED UPON INSPECTION.

Part: SLIDE — NO DISCREPANCY (ZONE 800) · airframe 130,774 hrs · 20,110 cycles

BOTH AFT ENTRY DOORS SLIDE PRESSURE GAUGES NOT IN GREEN BAND DOOR 2L, NEEDLE IS WITHIN TOLERANCE. DOOR 2R IS 2 WIDTH NEEDLES ABOVE. GO CONDITION IAW AMM 25-66-99-702-001 (D) IN SERVICE, OBSERVE THE RELATIVE POSITION OF THE NEEDLE TO THE BACKGROUND COLOR. IF THE YELLOW NEEDLE IS OVER GREEN OR ABOVE GREEN, THE BOTTLE IS STILL PROPERLY CHARGED (GO CONDITION).

Part: RELAY — FAULTY (ZONE 900) · airframe 130,484 hrs · 20,074 cycles

AIR TURN BACK DUE TO BOTH FWD LAVS AND ONE AFT LAV NOT FLUSHING IN AIR (FWD SYS). LAV FLUSH CONTROL RELAYS K2311 AND K2310 SWAPPED FOR TROUBLESHOOTING PURPOSES (WDM 38-32-11-1.1)AIRCRAFT PUT IN AIR MODE AND ALL LAVS FLUSHED CORRECTLY. REMOVED AND REPLACED RELAYS K2310 AND K2311 PER WDM 38-32-11-1.1, TOILET SERVICED BY VENDOR AND PERFORMED OPERATIONAL TEST OF ALL TOILETS PER AMM 38-32-00-725-142, FOUND SATISFACTORY ON GROUND. AIRCRAFT OK FOR SERVICE.T

Part: POWER UNIT — NO DISCREPANCY (ZONE 900) · airframe 130,222 hrs · 20,041 cycles

ALL GALLEY POWER INOPERATIVE AFTER ENGINES SHUT DOWN AND PARKING BRAKES APPLIED. GALLEY POWER REINSTATED, .BPCU READ OUT C/O NO FAULTS DETECTED, GALLEY POWER STILL AVAILABLE,

Part: BOTTLE — NO DISCREPANCY (ZONE 800) · airframe 129,896 hrs · 20,002 cycles

2L/2R SLIDE PRESSURE IN THE RED. THE PRESSURE GAUGE NEEDLE ON THE INFLATION CYLINDER IS IN THE GREEN BAND, OR ONE NEEDLE WIDTH ABOVE THE GREEN BAND. AS PER AMM SUBTASK 25-66-01-216-008

Part: TRANSMITTER — FAULTED (HYD SYSTEM) · airframe 129,862 hrs · 19,996 cycles

RTO DUE TO EICAS R HYD QUANTITY REMOVED AND REPLACED RH HYDRAULIC SYSTEM RESEVOIR FLUID QUANTITY TRANSMITTER IAW AMM 29-33-02. OPS AND LEAK CHECK GOOD.

Part: NONE — NONE (NONE) · airframe 129,257 hrs · 19,922 cycles

2L AND 2R SLIDE SIGHT GAUGES APPEAR ABOVE GREEN BAND PERFORMED DOOR 2L AND 2R INFLATION PRESSURE CHECK REFERENCE AMM TASK 25-66-02-206-001 SUBTASK 25-66-02-226-011 AND CHECK GOOD.

Part: SLIDE — NO DISCREPANCY (ZONE 800) · airframe 128,936 hrs · 19,883 cycles

DOORS 2L AND 2R SLIDE PRESSURE GUAGES INDICATE IN THE RED. PERFORMED CHECK REF. AMM TASK 25-66-99-702-001, GOOD FOR SERVICE.CK REF.

Part: STRAP — CORRODED (ZONE 100) · corrosion level 2 · airframe 128,861 hrs · 19,875 cycles

DURING ACCOMPLISHMENT OF REPAIR, WAS FOUND FRAME STRAP AT STA 1540 WITH CORROSION. UPDATE GENERATED DUE REPAIR ACCOMPLISHMENT, CLASSIFIED AS MAJOR REPAIR. FILLED OUT ESFR INFORMATION, IT'S NECESSARY QC REVIEW AND APPROVAL TO GENERATE ESFR NUMBER. VERIFIED THE ESFR AND NO WAS FOUND DISCREPANCY, BY QC PERFORMED INTERIM REPAIR ON THE TEAR STRAP STA 1540 PN 146T3242-11 AS PER EC/RA #5360-01948 PART B AND PART C STEP 13. IT WAS INITIATED A NEW DIP BY LOG PAGE 4720209. VERIFIED THE STEPS AND NO WAS FOUND DEVIATION.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 128,861 hrs · 19,875 cycles

DURING ACCOMPLISHMENT OF REPAIR, WAS FOUND S-37L DAMAGED AT STA 1540. PICTURES ATTACHED. UPDATE GENERATED DUE REPAIR ACCOMPLISHMENT, CLASSIFIED AS MAJOR REPAIR. FILLED OUT ESFR INFORMATION, IT'S NECESSARY QC REVIEW AND APPROVAL TO GENERATE ESFR NUMBER. VERIFIED THE ESFR AND NO WAS DEVIATION, BY QC PERFORMED INTERIM REPAIR AT STRINGER 37LH AND BETWEEN STA 1562/ STA 1540 AS PER EC/RA #5360-01948 PART A STEP 2,3 AND PART C STEP 14. IT WAS INITIATED A DIP BY LOG PAGE 4720209. VERIFIED THE STEPS AND NO WAS FOUND DEVIATION.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 128,861 hrs · 19,875 cycles

DURING INSPECTION WAS FOUND CORROSION AT BULK CARGO COMPARTMENT AT STRINGER 38LH AND BETWEEN STA 1562/ STA 1540. PICTURES ATTACHED UPDATE GENERATED DUE REPAIR ACCOMPLISHMENT, CLASSIFIED AS MAJOR REPAIR. FILLED OUT ESFR INFORMATION, IT'S NECESSARY QC REVIEW AND APPROVAL TO GENERATE ESFR NUMBER. VERIFIED THE ESFR AND NO WAS FOUND DEVIATION, BY QC PERFORMED INTERIM REPAIR AT STRINGER 38LH AND BETWEEN STA 1562/ STA 1540 AS PER EC/RA #5360-01948 PART A STEP 1, 3 AND PART C STEP 14. IT WAS INITIATED A DIP BY LOG PAGE 4720209. VERIFIED THE STEPS AND NO WAS FOUND DISCREPANCY.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 128,861 hrs · 19,875 cycles

CORROSION FOUND ON BULK CARGO COMPARTMENT FUSELAGE SKIN AT LAP SPLICE STRINGER 36LH BETWEEN STA 1540 AND 1540 PLUS 7". CLASSIFIED AS MAJOR REPAIR. FILLED OUT ESFR INFORMATION, IT'S NECESSARY QC REVIEW AND APPROVAL TO GENERATE ESFR NUMBER. VERIFIED THE ESFR AND NO WAS FOUND DISCREPANCY, BY QC PERFORMED INTERIM REPAIR ON THE FUSELAGE SKIN BTW STA 1540/1562 AT S-36L AND STRINGERS S-37L & S-38L AS PER EC/RA #5360-01948. VERIFIED THE STEPS NO WAS FOUND DISCREPANCY. REF ECRA 5360-01948, PLANNING TO CONTACT ENGINEERING AFTER 20 MONTHS BUT BEFORE 24 MONTHS FOR INSPECTIONS REQUIREMENTS AND INSTRUCTIONS, AND PERMANENT REPAIR. REF ECRA 5360-01948, "PLANNING TO CONTACT ENGINEERING AFTER 20 MONTHS BUT BEFORE 24 MONTHS FOR INSPECTIONS REQUIREMENTS AND INSTRUCTIONS, AND PERMANENT REPAIR.

Part: SQUIB — NO TEST (ZONE 800) · airframe 128,778 hrs · 19,862 cycles

OFF WING ESCAPE SYSTEM EMERGENCY SLIDE SQUIB 1 AND 2 NOT TESTING. REMOVED AND REPLACED LEFT AND RT OFF WING ESCAPE SYSTEM EMERGENCY BATTERIES REF AMM 25-65-17 OPS CK GOOD.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 128,330 hrs · 19,808 cycles

ROW 10 OVERHEAD EMER EXIT LIGHT INOP ADJUSTED OVERHEAD EMERGENCY EXIT COVER LIGHT AT ROW 10 AND PERFORMED OPERATIONAL TEST EMERGENCY LIGHTS AS PER AMM 33-51-00.OPERATIONAL TEST SATISFACTORY IS TIME.

Part: PROXIMITY SWITCH — FAULTED (CARGO DOOR) · airframe 125,672 hrs · 19,473 cycles

MULTIPLE EICAS EMEG DOOR CARGO DOORS AND ENTRY DOORS. PRESSURIZATION WAS ERRATIC DURING THIS HISTORY ON PSEU UNIT, ASSY, PRO OFF 76-3260-9-0005 0634 ON 76-3260-9-0005 1064 UNIT, ASSY, PRO OFF 76-3260-9-0005 0634 ON 0000 FOUND PSEU S/N = 0634 FAULTED FOR SAME DISCREPANCY ON PREVIOUS AIRCRAFT. REMOVED AND REPLACED PSEU (M162) PER AMM 32-09-04/401. OPS CHECK GOOD. REF LOGPAGE 8049281 FOR PRESSURIZATION ERRACTIC SIGN OFF. PARTS USED: 76-3260-9-0005,

Part: WASTE TANK — DISCONNECTED (AFT CARGO PIT) · airframe 125,595 hrs · 19,463 cycles

BLUE JUICE SPILL: WAS REPORTED THAT WASTE TANK WAS SERVICED WHEN SUMP TANK WAS DISCONNECTED CAUSING BLUE JUICE TO SPILL INTO THE AFT EQUIPMENT AREA, INSULATION BLANKETS SOAKED AND HUMAN WASTE FOUND IN AREA. NEW INSULATION AND WASTE TANK. REMOVED WASTE TANK AND INSPECTED AREA. LARGE AMOUNTS OF BLUE REF EC/RA 2011-01000 JUICE AND HUMAN WASTE IN WASTE TANK AREA. REMOVED SOAKED INSULATION AND ATTEMPTED TO CLEAN. FURTHER CLEANING, DISINFECTING AND CIC NEEDS TO BE ACCOMPLISHED BEFORE INSTALLING . PLUG ASSY BROKE OFF WAS SUCKED INTO TANK, CAUSING INITIAL FAULT. PLUG P/N 32500-01306.AFT CARGO PIT STA 1220 BACK TO STA 1540

Part: PROCESSOR — FAULTED (FUEL QTY) · airframe 125,424 hrs · 19,443 cycles

FUEL LEAK OUTBD LEFT ENGINE FUEL VIEWED BY PASSENGER LEAKING FROM UPPER SURFACE OF WING NEAR LEADNG EDGE OF OUTBOARD AILERON WHERE AILERON MEETS UPPER WING SURFACE. CORROBORATED BY VIDEO TAKEN BY CREW. WING UNDER SURFACE NEAR AILERON WET WITH FUEL. CREW STATED AROUND 600LBS OF FUEL PERFORMED VISUAL INSPECTION ON TOP OF THE LEFT WING JUST FORWARD OF THE OUTBOARD AILERON AND FOUND A PANEL TO BE CRACKED AND FOUND THE HEADS OF MULTIPLE RIVETS TO BE SHEARED OFF. FURTHER TROUBLE SHOOTING AND REPAIR WILL BE NECESSARY BY SHEETMETAL OR LOSS. COMPOSITE SHOP REMOVED PANEL 561QB TO INSPECT INSIDE OF WING UNDER DAMAGED PANEL. FOUND BOTTOM OF PANEL TO BE CRACKED IN SEVERAL LOCATIONS, MISSING SEVERAL FASTENERS, AND LIFTING FROM SPAR. PANEL EXTENDS PAST SPAR TO FUEL TANK, SEAL BETWEEN PANEL AND SPAR WAS BROKEN FRM LIFTING CAUSING FUEL LEAK. SAW FUEL SEEP FROM AREAS WHERE SEAL WAS VISUALLY BROKEN. POSSIBLE FUEL LEAK FROM LH WING OTBD TRAILING EDGE FWD OF OTBD AILERON WORK TO ACCOMPLISHED REF LP 7755331. FOUND NO FUEL AT CRACKED PANEL .PANEL IS LOCATED OUTBD OF DRYBY. SUPECT FUEL CAME FROM SURGE TANK . PERFORMED FIMS 28-21. 803 AND FIM 28-21. 822. NO FUEL WENT TO SURGE TANK. VTO AND OVERFILL . TEST GOOD. REF LP 7741639, FUEL LEAKING FROM LH WING UPPER TRAILING EDGE FWD OF OTBD AILERON. ACCOMPLISHED FUEL SCAVENGE SYSTEM TEST PER AMM: 28-22-00-735-723. NO DEFECTS, NO LEAKS NOTED. ACCOMPLISHED FIM TASK 28-21 TREE 803, FUEL SPILL AT SURGE TANK, NO DEFECT, NO LEAKS NOTED. ACCOMPLISHED FIM 28-21 FAU

Part: OVEN — SMOKE (GALLEY) · airframe 125,276 hrs · 19,425 cycles

OVEN 109 STARTED SMOKING WHEN TURNED ON PERFORMED INSPECTION PER AMM 05-51-56-940-801-C1. FOUND BURNED CREW REPORTED OVEN 109 NOISY WHILE OPREATING. FOOD IN OVEN. CLEANED OVEN 109 PER AMM 25-31-00. OPS CK OK. NO MORE SMOKE PRESENTS. REPLACED OVEN 109. OPS CK OK.REF AMM 25-31-00.

Part: FSEU — FAULTY (STA 328) · airframe 124,130 hrs · 19,252 cycles

SPD 190 SELECTED F20 AND GOT TE FLAP DISAGREE EICAS. RAN CHKLST. DID NOT CLEAR. LOG LOCKED FOR POSITIVE FIX, IAH NOTIFIED. FLIGHT CREW DECLARED EMERGENCY LANDING UNLOCKED: FSEU AND M838 CARD REPLACED, NUMEROUS OPS TEST WITH NO FAULTS LOCKED T/S PER FIM 27-51 TASK 809, ALL FAULTS, INFO., AND PARTS REPLACED PER FIM STATED IN THE LOGPAGE. DEBRIEFED CAPT: AT 190KIAS MOVED FLAP LEVER FROM FL5 TO FL20, TE FLAP DISAGREE APPEARED AFTER BOTH NEEDLES REACHED FL20. RAN DISAGREE CHECKLIST, DID NOT CLEAR. DISAGREE CHECKLIST DRIVES TO TE ASYMMETRY CHECKLIST, MSG STILL DID NOT CLEAR. PER FIM 27-51 TASK 809 FOUND FAULT MSGS 27-51333, 27-51332 AND 27-51102. REMOVED AND REPLACED FSEU REF AMM 27-51-01-404-130 OPS CHECKS GOOD NO FAULTS NOTED AT THIS TIME. REMOVED AND REPLACED LEFT FSPM, OPS CHECKS GOOD NO FAULTS AT THIS TIME. CYCLED L/E NOTE ALSO ACCOMPLISHED FIM TASK 27-51 TASK 810 AGAIN NO FAILURES AFTER COMPONENT CHANGE OUT. ANOTHER NOTE THE FSPM WAS THE M839 CARD. WHILE COMPLETING ALT DRIVE TESTING VISUALLY CONFIRMED THAT THE FLAP BYPASS VALVE OPERATION WAS SMOOTH AND NO SIGNS OF STICKING AS THIS HAS BEEN A KNOWN ISSUE ON OTHER 767 SERIES FLAP ISSUES IN PAST. MODULE, FLAP ST OFF 76-2754-9-0001 2812 ON 0000 MODULE, FLAP ST OFF 76-2754-9-0001 2812 ON 76-2754-9-0001 2556 UNIT, FLAP SLAT OFF 76-2751-9-0010 1609 ON 76-2751-9-0010 1132 UNIT, FLAP SLAT OFF 76-2751-9-0010 1609 ON 0000 SLATS AND T/E FLAPS ELECTRICALLY AND HYDRAULICLLY OVER 3 TIMES EACH SHOWING NO FAULT

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 124,078 hrs · 19,246 cycles

SELECTED FLAPS 20 WITH FLAP HANDLE IN 20 DETENT AT 190KIAS. TE E DGE FLAPR DISAGREE. VERBAL FROM CREW. BOTH FLAP POS NEEDLES WERE AT 20 DEG TOGETHER BITE CHECK COMPLETED PICS ADDED WHEN DISAGREE MSG CAME UP FOUND THE ALT FLAP SWITCH PLACED IN 20 DEG FLAPS POSITION. MECHANIC WHO DEBRIEFED THE FLIGHT CREW SAID THERE WAS NO MENTION PLACED SWITCH IN "NORMAL" POSITION AND OPERATED FLAPS SEVERAL OF THE SWITCH BEING MOVED. NO PREVIOUS WRITE UPS. OK TO TIMES WITHOUT A DISAGREE MESSAGE. PERFORMED FIM 27-51 FAULT TREE CONTINUE. 809 . GROUND TEST INDICATED NO EXISTING FAULTS. THE LEAD ACCOMPLISHING THE CHECKLIST. DEBRIEF FROM INBOUND CREW AT 19Z ON 08NOV FOR CLARIFICATION: CREW FOLLOWED FM CHECKLIST AND LOWERED FLAPS TO 20 IN ALTERNATE, THAT IS WHY ALT FLAP SW WAS FOUND IN POSITION 20. ADDITIONALLY THE TE FLAP DISAGREE OCCURRED THREE TIMES IN THE PROCESS OF ACCOMPLISHING THE CHECKLIST.

Part: COMPUTER — FAILED (STA 328) · airframe 123,599 hrs · 19,175 cycles

AUTO THROTTLE WOULD NOT ENGAGE ON TAKEOFF ROLL. PICTURE FROM INSTALLED TMS ADDED. PERFORMED FIM 22-02 TASK 801. PERFORMED TMS SYSTEM TEST, TMS OPS TEST AND MCDP GROUND TEST 52 AS PER AMM 22-32-00. TMS COMPUTER FAILED. THRUST MANAGEMENT COMPUTER REPLACED PER AMM 22-31-01, INSTALLATION TEST PASSED. A/C DOWNGRADED TO "NO AUTOLAND" IN LOG 5779127.

Part: UNKNOWN — UNKNOWN (STA1725.5/S-7R) · airframe 122,269 hrs · 18,987 cycles

INSPECT THE FUSELAGE SKIN AND CHORD STRAP REPAIR INSTALLED AT STA 1725.5 AND S-7R, PER LATEST REVISION OF ECRA 5380-01359 PART 2 BEFORE THE AIRCRAFT REACHES 37,500 TOTAL FLIGHT CYCLES. REPEAT THE INSPECTIONS AT INTERVALS NOT TO EXCEED 6,000 FLIGHT CYCLES THEREAFTER. GENERATED A DTA/DIP PER ECRA 5380-01359 PART 1.2. REF EC 5380-01359, INSPECT THE FUSELAGE SKIN AND CHORD STRAP TOMC-APPROVAL FROM SC1ELBYC COMMENT REPAIR, INSTALLED AT STA 1725.5 AND S-7R, PER LATEST REVISION OF ECRA 5380-01359 PART 2 BEFORE THE AIRCRAFT REACHES 37,500 TOTAL FLIGHT CYCLES. REPEAT THE INSPECTIONS AT INTERVALS NOT TO EXCEED 6,000 FLIGHT CYCLES THEREAFTER. REVIEWED RECORDS UPDATE QC REVIEWED INIT: BEFORE 37,500 TAFC WILL ITO TO RIR (-0782) RIR: EVERY 6,000 FC. LT

Part: SKIN — UNKNOWN (BULK CRGO DR) · airframe 122,269 hrs · 18,987 cycles

SUPPORT TASK TAR- EA 5100-02345 REV E OP 18 BULK CGO DOOR EXTERNAL STRUCTURE FOUND REINFORCING REPAIR AT AFT MIDDLE , PLS PROVIDE PERVIOUS REPAIR RECORD OR HISTORY FOR EVALUATION. TRANSFER NR WO.1715150 AND ORIGINATED BY V896921. BULK CARGO DOOR EXTERNAL SKIN AT AFT MIDDLE INTRIM REPAIRED AS PER ECRA5236-01031 REV - PART 1 ATTACH FORM 44-0008 ITEM 1 TO ITEM 31 ACCOMPLISHED WORK ACCOMPLISHED BY MECHANIC V897381 INSPECTED BY V896888 RII INSPECTED BY HX185167 ADD EMP:V897008

Part: DOOR — CRACKED (LH FWD DR) · airframe 122,269 hrs · 18,987 cycles

SUPPORT TASK - EA 5315-01152 OP 001 LH FWD ENTRY DOOR CUTOUT AFT LOWER CORNER 1EA FASTENER HOLE FOUND CRACK AT 10''O''CLOCK ON BEAR STRAP LAYER WITH APPROX 1/8" IN DEPTH - TRANSFER REFER NON-ROUTINE WO.1671977 AND ORIGINATED BY V924732 DOOR 1L CUTOUT AFT LOWER CORNER BEAR STRAP DOUBLER INTERIM REPAIRED AS PER ECRA 5315-01195 REV PART 1 ATTACHED FORM44-0008 ITEM 1 TO ITEM 47 ACCOMPLISHED BY MECH V897381 AND INSPECTED BY V896919 RII INSPECTED OKAY BY HX 203084 ADD EMP:V896920

Part: FITTING — UNKNOWN (STA808&S13R) · airframe 122,269 hrs · 18,987 cycles

INSPECT THE REPAIRED AREAS AT FUSELAGE STA 808 & S13R PER THE LATEST REVISION OF ECRA 5350-02481 PART 2 ON OR BEFORE 29-APR-2024 GENERATED A DTA/DIP PER ECRA 5350-02481 PART 1 ITEM 2. REF EC 5350-02481, INSPECT THE REPAIRED AREAS AT FUSELAGE STA808 TOMC-APPROVAL FROM SC1ELBYC COMMENT & S13R PER THE LATEST REVISION OF ECRA 5350-02481 PART 2 / ON OR BEFORE 29-APR-2024 REVIEWED RECORDS UPDATE QC REVIEWED T/A: 29APR24...SN

Part: SKIN — CRACKED (RH FWD DR) · airframe 122,269 hrs · 18,987 cycles

SUPPORT TASK - EA 5315-01152 - OP002 - RH FWD ENTRY DOOR CUTOUT AFT LOWER CORNER 1EA FASTENER HOLE FOUND CRACK AT 8''O''CLOCK ON FUSELAGE SKIN LAYER WITH THROUGH THICKNESS - TRANSFER REFER NON-ROUTINE WO.1671967 DOOR 1R CUTOUT AFT LOWER CORNER FUSELAGE SKIN REPAIRED AS PER SRM 53-10-01-2R-1 REPAIR 1 FIG 201 DETAIL III ATTACH FORM44-0008 ITEM 1 TO ITEM 45

Part: UNKNOWN — CORRODED (STR38L-38R) · airframe 122,269 hrs · 18,987 cycles

SUPPORT TASK AAI INSPECTION FOUND BULK CARGO COMPT BS1560 NEAR BILGE AREA HAVE SIGN OF CORROSION TRANSFER REF HXWO 1703431 AND ORIGINATED BY EMP V896948 BULK CARGO COMPT BS1560 BILGE AREA BETWEEN STR38L AND STR38R SHEAR TIE REPLACED AS PER SRM51-10-02 AND INSTALLED AS PER SRM51-40-02 ATTACH FORM 44-0008 ITEM 1 TO ITEM 27 ACCOMPLISHED WORK ACCOMPLISHED BY MECHANIC V897381 INSPECTED BY V898550 RII INSPECTED BY HX341008 ADD EMP:V896888

Part: NONE — NONE (L GEN DRIVE) · airframe 120,529 hrs · 18,726 cycles

L GEN DRIVE EICS ON INITIAL POWER ADVANCE ON TOFF ITEM DEFERRED IAW MEL 2400E LEFT GEN SYSTEM INOP ITEM DEFERRED IAW MEL 2200E LEFT GEN SYSTEM INOP DISPATCH DESK: 66 NAME: BC DATE: 07-SEP-22- NOC DESK: 767 NAME: ANDRE DATE: 07-SEP-22- MEL 2400E APPROVED STORED. C/W REQUIRED IDT INSPECTION FOR LEFT ENG IDGINSTALL REF AMM 24-11-11. BPCU SHOWS LEFT IDG HIGH RISE TEMP. PREVIOUS LEGS FAULTS OF LOW REMOCED AND REPLACED IDG ON NUMBER ONE ENGINE PER AMM 24-11-11. PERFORMED LEAK CHECK ON IDG NUMBER 1 ENGINE, NO LEAK FOUND OIL PRESSURE WITH ASSOCIATED HIGH RISE TEMP AND SERVICE IDG ALSO NEED TO PREFORM OPS AND LEAK CHECK ADD EMP:U393360 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1092538 SN OFF 1546 GENERATOR, INTE OFF 76-2411-9-0002 1546 ON 76-2411-9-0002 1199 PERFORMED OPERATIONAL TEST FOR THE LEFT IDG IAW AMM 24-11-00-715-005. ALL TESTS PASSED. C/W REQUIRED IDT INSPECTION FOR LEFT ENG IDG INSTALL REF AMM 24-11-11.

Part: NONE — NONE (N/A) · airframe 118,620 hrs · 18,448 cycles

SPOILERS LIGMT ILLUMNTED OVERHEAD AFTER ENG START NO EICAS MSG. PERFORMED TEST PER AMM 27-61-00 SYSTEM OK NO MORE MENSSAGES.

Part: SLAT — SEPARATION (LE SLAT) · airframe 116,726 hrs · 18,025 cycles

PDA 1 REF L/P 6664565 PASSENGER REPORTED A 4" DELAMINATION ON LE SLAT INITIALLY. ON ARRIVAL INTO EWR MX FOUND THE DMG AREA TO BE 16" X 10" . PER GMM 02-30-95 TABLE 1 THE DMG FALLS INTO CATEGORY 1. FURTHER DETAILS AWAITED

Part: SCREW — MISSING (NR 2 NACELLE) · airframe 116,340 hrs · 17,939 cycles

PDA 3 FOUND 2 SMALL SCREWS MISSING FROM RIGHT ENG PYLON INBORD SIDE REPLACED 2 MISSING SCREWS AS REQ OK TO CONTINUE

Part: SKIN — CORRODED (BS 1540-1545) · airframe 116,167 hrs · 17,905 cycles

B767-53-3-7058 - BULK CGO STA1540 TO 1545 CTR BOTTOM DRAIN VALVE AREA SKIN FOUND CORROSION.REF NR LP 9130687 BULK CGO STA1540 TO STA1545 BETWEEN S39L AND S39R FUSELAGE SKIN REPAIRED AS ECRA 5361-01084 REV- PART 1 INTERIM REPAIR AND ATTAC H FORM 44-0008 MAINTENANCE WORKSHEET ITEM 1 TO 36 ACCOMPLISHED ADD EMP:V897490 RII BY HX185167,APPROVED ACCOMPLISH THE INSPECTION PER LATEST ECRA 5361-01084 PART 2 ON OR BEFORE REACHING 37,500 TOTAL FLIGHT CYCLES. SEPRATE DIP LOG 6222081 CREATED TO CONTACT ENGINEERING AFTER AIRCRAFT REACHES 35 000 BUT BEFORE 35,500 CYCLES FOR THE INSPECTION REQUIREMENTS BULG CARGO STA 1540 BETWEEN S39L & S39R SKIN CORROSION REPAIRED PER ECRA 5361-01084 PART 1. REPAIR IS APPROVED AS PERMANENT PROV IDED PART 2 INSPECTION REQUIREMENTS ARE COMPLIED WITH. INSP LOG 6222081 CREATED FOR INSPECTION PER ECRA 5361-01084 PART 2 ON OR BEFORE REACHING 37,500 TOTAL FLIGHT CYCLES RII BY HX185167,APPROVED

Part: SKIN — CORRODED (BS 1540) · airframe 116,167 hrs · 17,905 cycles

CORROSION DAMAGE WAS FOUND ON FUSELAGE INTERNAL SKIN, PN 1146T3241-12, JUST AFT OF STA 1540 BETWEEN S39L & 39R IN THE AREA WHERE A DRAIN VALVE AND AN EXISTING REPAIR EXIST. AMOUNT OF MATERIAL REMOVED TO CLEAN THE DAMAGE EXCEEDS LIMIT 0.15T IAW 767-300 SRM 53-00-01 ALLOWANBLE DAMAGE 1. REF FIG 1 OF RI-53-00-14514 REV A.

Part: SKIN — CORRODED (BS 1540-1545) · airframe 116,167 hrs · 17,905 cycles

B767-53-3-7058 - BULK CGO STA1540 TO 1545 CTR BOTTOM DRAIN VALVE AREA SKIN FOUND CORROSION.REF NR LP 9130687 BULK CGO STA1540 TO STA1545 BETWEEN S39L AND S39R FUSELAGE SKIN REPAIRED AS ECRA 5361-01084 REV- PART 1 INTERIM REPAIR AND ATTAC H FORM 44-0008 MAINTENANCE WORKSHEET ITEM 1 TO 36 ACCOMPLISHED ADD EMP:V897490

Part: FRAME — DAMAGED (CARGO DOOR) · airframe 116,167 hrs · 17,905 cycles

B767-06-3-7007 BULK CGO DOOR INTERNAL LOWEST FRAME FOUND CHIPPED REF NR LP 9130524 BULK CGO DOOR INTERNAL LOWEST FRAME REPLACED AND INSTALLED AS PER SRM 51-10-02 AND SRM 51-40-02 AND ATTACH FORM 44-0008 MAINTENANCE WORKSHEET ITEM 1 TO 24 ACCOMPLISHED ADD EMP:V897532 RII BY HX203084,APPROVED BULK CGO DOOR INTERNAL LOWEST FRAME REPLACED AND INSTALLED AS PER SRM 51-10-02 AND SRM 51-40-02 AND ATTACH FORM 44-0008 MAINTENANCE WORKSHEET ITEM 1 TO 24 ACCOMPLISHED ADD EMP:V897532

Part: OVEN — UNSECURE (GALLEY) · airframe 110,752 hrs · 17,175 cycles

AIR RETURN AND DECLARED EMERGENCY DUE TO CREW REPORTING IN CLIMBOUT A FWD GALLEY OVEN (109) BECAME DETACHED AND SLID OUT OF POSITION. FLT ATTD MANAGED TO PUSH BACK INTO PLACE, BUT UNABLE TO SECURE IT IN PLACE. MX INSPECTED OVEN AND OPS CHKED. NO FAULTS NOTED.

Part: OVEN — UNSECURE (FWD GALLEY) · airframe 110,714 hrs · 17,170 cycles

AIR RETURN DUE TO OVEN WORKING ITSELF LOOSE. TOMC REQUESTS OVEN 109 TO BE REPLACED DUE TO HISTORY. REPACED OVEN 109 AS REQUESTED PER TOMC AS PER REF AMM 25-31-00. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1219170 SN OFF 1080 OVEN, STEAM, OFF 99-2534-9-0002 1080 ON 99-2534-9-0002 0054.

Part: INDICATOR — DEFECTIVE (COCKPIT) · airframe 107,651 hrs · 16,771 cycles

GAUGE SHOWED TE FLAP ASSYM. NO EICAS MSG L FLAP SHOWED 30 R FLAP OUT OF THE WHITE ARC T/S PER FIM 27-58-00-815-803, FSEU BITE TEST OK. REMOVED AND REPLACED FLAP POSITION INDICATOR. CYCLED FLAPS SEVERAL TIMES NO DEFECTS NOTED ALL INDICATIONS NORMAL. ROTABLE PARTS CHANGE WAS INDICATED - TT 1304723 SN OFF 9015 INDICATOR, TE F OFF 76-2754-9-9001 9015 ON 76-2754-9-9001 0455.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 106,902 hrs · 16,660 cycles

EMER EXIT LIGHT DOOR 1L BLINKING. REPLACED BATTERY PACK M1557. OP CK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 105,854 hrs · 16,515 cycles

EMERGENCY LIGHTS DISARMED LIGHT BULB INOPERATIVE. REPLACED THE BULB. OPS NORMAL.

Part: SPAR — CRACKED (NR 2 PYLON) · airframe 105,747 hrs · 16,499 cycles

NR 2 PYLON UPPER SPAR WEB FOUND CRACKED AT HYD CASE DRAIN TUBE THROUGH CUTOUT. REPAIR ACCOMPLISHED IAW EC/RA 5410-01857, REV-, PART 1, STEP 1.

Part: SKIN — WORN (BS 1582-1605) · airframe 105,747 hrs · 16,499 cycles

WEAR ON EXTERIOR LT FUSELAGE SKIN AT VERTICAL STABILIZER TO FUSELAGE INTERFACE AREA BS 1582 TO 1605.5. INTERIM REPAIR ACCOMPLISHED IAW ECRA 5330-06139, PART 1, STEP 1.

Part: FRAME — CORRODED (BS 1584) · airframe 105,747 hrs · 16,499 cycles

AFT BULKHEAD LOWER SUPPORT FRAME SURFACE AT BS 1584, LBL 10 FOUND CORRODED. INTERIM REPAIR ACCOMPLISHED IAW PART 1, STEP 1, IAW ECRA 5310-07 168.

Part: SKIN — DAMAGED (BS 1582 - 1605) · airframe 105,747 hrs · 16,499 cycles

WEAR MARK ON EXTERIOR RT FUSELAGE SKIN AT VERTICAL STABILIZER TO FUSELAGE INTERFACE AREA BS 1582 - 1605.5. INTERIM REPAIR ACCOMPLISHED IAW ECRA 5330-06139, PART 1, STEP 1.

Part: SKIN — SCRATCHED (BS 1788-1809) · airframe 105,747 hrs · 16,499 cycles

LOWER EMPENAGE SKIN BS 1788 - 1809 STRINGER 30 - 32L, FOUND SCRATCHED. REPAIRED IAW SRM 53 -00-01, REPAIR 6, FIG 201.

Part: FAILSAFE — CORRODED (BS 1562) · airframe 105,747 hrs · 16,499 cycles

AFT OF BULK CARGO BAY SUPPORT FRAME LOWER FAIL SAFE AT BS 1562, BL 0, FOUND CORRODED. INTERIM REPAIR ACCOMPLISHED IAW ECRA 5310-07173, PART 1, STEP 2.

Part: STRINGER — CRACKED (FWD CARGO) · airframe 105,747 hrs · 16,499 cycles

FWD CARGO BAY LOWER DOOR SILL UPPER STRINGER FOUND CRACKED. THE STRINGER WAS REPLACED IAW SRM 51-10-02 AND AMM 20-11-00.

Part: WEB — CORRODED (BS 1576) · airframe 105,747 hrs · 16,499 cycles

BULK CARGO BS 1576, BL 0 BILGE, VERTICAL SUPPORT FACE FOUND CORRODED. THE VERTICAL SUPPORT WEB AND TWO ANGLES REPLACED IAW SRM 51-10-02, AND INSTALLED IAW SRM 51-4 0-02.

Part: FAILSAFE — CORRODED (BS 566) · airframe 105,747 hrs · 16,499 cycles

FWD CARGO BAY DOOR SILL LOWER STRINGER LOWER FAIL SAFE STRAP FOUND CORRODED AT BS 566. THE FAIL SAFE STRAP WAS REPAIRED IAW ECRA 5310-07172, REV.

Part: SHEAR WEB — CORRODED (POWER DRIVE ATTA) · airframe 105,747 hrs · 16,499 cycles

FWD CARGO BAY 4R POWER DRIVE UNIT ATTACH SHEAR WEB FOUND CORRODED. REPLACED IAW SRM 51-10-02 AND SRM 51-40-02.

Part: ANGLE — CORRODED (CARGO DRIVE) · airframe 105,747 hrs · 16,499 cycles

FWD CARGO BAY 5C POWER DRIVE UNIT AFT ANGLE SURFACE FOUND CORRODED. THE AFT ANGLE WAS REPLACED IAW SRM 51-10-02, AND SRM 51-40-02.

Part: PANEL — CORRODED (BS 544) · airframe 105,747 hrs · 16,499 cycles

FWD CARGO BAY RT TORQUE PANEL HAD SURFACE CORROSION AT BS 544. THE TORQUE PANEL WAS REPLACED.

Part: STRINGER — CORRODED (DOOR SILL) · airframe 105,747 hrs · 16,499 cycles

FWD CARGO DOOR SILL LOWER STRINGER WAS FOUND CORRODED AT BS 478 - 610. THE STRINGER WAS REPLACED IAW SRM 51-10-02 AND SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 287) · airframe 105,747 hrs · 16,499 cycles

CABIN BS 287, RBL 37-76 FLOORBEAM FOUND CORRODED. REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201.

Part: NUT PLATE — CORRODED (FWD CARGO) · airframe 105,747 hrs · 16,499 cycles

FWD CARGO BAY 8R POWER DRIVE UNIT AFT NUT PLATE AREA FOUND CORROSION FWD CARGO COMPT 8R POWER DRIVE UNIT AFT SUPPORT WEB REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02.

Part: WEB — CORRODED (BS 456-478) · airframe 105,747 hrs · 16,499 cycles

SUPPORT WEB FOUND CORRODED AT FWD CARGO BS 456 - 478, RBL 40. THE SUPPORT WEB WAS REPLACED IAW SRM 51-10-02 AND SRM 51-40-02.

Part: CHANNEL — CORRODED (BS 544-566) · airframe 105,747 hrs · 16,499 cycles

FWD CARGO BAY PDU 7R INBD MOUNTING SUPPORT CHANNEL FOUND CORRODED AT BS 544 - 566. THE SUPPORT CHANNEL WAS REPLACED IAW SRM 51-10-02, AND SRM 51-40-02.

Part: SUPPORT — CORRODED (BS 566-577) · airframe 105,747 hrs · 16,499 cycles

FWD CARGO BAY BS 566 - 577, RBL 37 TORQUE PANEL OTBD LOWER SUPPORT FOUND CORRODED. REPLACED IAW SRM 51-10-02 AND SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 1482) · airframe 105,747 hrs · 16,499 cycles

M/D AFT ZONE BS 1482, RBL 54 FLOORBEAM UPPER TEE CORRODED. REPAIRED IAW SRM 53-00-51, REPAIR 2, FIG 201.

Part: FLOORBEAM — CORRODED (BS 632) · airframe 105,747 hrs · 16,499 cycles

FWD CARGO BAY FLOORBEAM FOUND ANCHOR NUTS AREA CORRODED, BS 632 LBL 18 - 28. REPAIRED IAW SRM 51-10-02 AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 786-890) · airframe 105,747 hrs · 16,499 cycles

FLOOR SUPPORT CORRODED BS 786 - 890, RBL 54. REPAIRED IAW SRM 53-00-51, FIG 201, REPAIR 3.

Part: STRINGER — CRACKED (BS 1439) · airframe 105,747 hrs · 16,499 cycles

FOUND STRINGER 9L, BS 1439 CRACKED, REPAIRED THE STRINGER IAW SRM 53-00-03, FIG 201, REPAIR 1.

Part: SKIN — CORRODED (BS 1307) · airframe 105,747 hrs · 16,499 cycles

DEEP BLEND OUT UNDER LOCK FASTENER HEAD EXPOSING PART OF COUNTERSINK THAT HAS LIGHT CORROSION UNDERNEATH ON UPPER FUSELAGE CROWN SKIN BS 1307 JUST OUTBOARD OF STRINGER 1R REPAIRED THE SKIN IAW SRM 53-00-01, REPAIR 29, FIG 201

Part: ANGLE — CORRODED (BS 566-588) · airframe 105,747 hrs · 16,499 cycles

FWD CARGO BAY FWD OF PDU 8R INBD SUPPORT ANGLE FOUND CORRODED, LOWER SURFACE BS 566 - 588, RBL 24. THE ANGLE WAS REPLACED IAW SRM 51-10-02 AND SRM 51-40-02.

Part: CHANNEL — CORRODED (BS 500) · airframe 105,747 hrs · 16,499 cycles

FWD CARGO BAY PDU 4R AFT SUPPORT MOUNTING SUPPORT CHANNEL FOUND CORRODED BS 500. REPLACED IAW SRM 51-10-02, AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 524-541) · airframe 105,747 hrs · 16,499 cycles

FWD CARGO BAY BS 524 TO 541, RBL 33 FLOOR SUPPORT FOUND CORRODED. REPLACED IAW SRM 51-10-02 AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 583) · airframe 105,747 hrs · 16,499 cycles

FWD CARGO BAY BS 583, RBL 33 FLOOR SUPPORT FOUND CORRODED. REPLACED IAW SRM 51-10-02, AND SRM 51-40-02.

Part: COVER — CRACKED (FWD CARGO) · airframe 105,747 hrs · 16,499 cycles

FWD CARGO BAY PDU 3R OTBD SUPPORT PLATE COVER FOUND CORRODED AND CRACKED. REPLACED IAW SRM 51-10-02 AND SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FWD CARGO BAY) · airframe 105,747 hrs · 16,499 cycles

FWD CARGO BAY PDU 7R OTBD AFT MOUNTING LOWER INTERCOSTAL FOUND CORRODED. THE INTERCOSTAL WAS REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02

Part: SUPPORT CHANNEL — CORRODED (BS 478-500) · airframe 105,747 hrs · 16,499 cycles

FWD CARGO BAY TORQUE BOX PANEL SUPPORT CHANNEL FOUND CORRODED AT BS 478 - 500. REPLACED IAW SRM 51-10-02, AND SRM 51-40-01.

Part: FLOOR SUPPORT — CORRODED (BS 544-566) · airframe 105,747 hrs · 16,499 cycles

FWD CARGO BAY BS 544 - 566, RBL 36 FLOOR SUPPORT CORRODED. REPLACED IAW SRM 51-10-02 AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 502) · airframe 105,747 hrs · 16,499 cycles

FWD CARGO FLOOR SUPPORT FOUND CORRODED BS 502.51, RBL 38. REPLACED IAW SRM 51-10-02, AND SRM 51-40-02.

Part: WEB — CORRODED (BS 478-497) · airframe 105,747 hrs · 16,499 cycles

FWD CARGO BAY BS 478 TO 497, RBL 30 FLOOR SUPPORT WEB FOUND CORRODED. REPLACED IAW SRM 51-10-02, AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 588-610) · airframe 105,747 hrs · 16,499 cycles

FWD CARGO BAY BS 588 TO 610, RBL 33 FLOOR SUPPORT FOUND CORRODED. REPLACED IAW SRM 51-10-02 AND SRM 51-40-02.

Part: SHEAR TIE — CORRODED (BS 1540) · airframe 105,747 hrs · 16,499 cycles

AFT OF BULK CARGO COMPT - SHEAR TIE FOUND CORRODED AT BS 1540, STRINGERS 39L - 39R, THE SHEAR TIE WAS REPLACED IAW SRM 51-10-02 AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 512) · airframe 105,747 hrs · 16,499 cycles

FWD CARGO FLOOR SUPPORT UPPER SURFACE WAS CORRODED AT BS 512.15, RBL 38. REPLACED IAW SRM 51-10-02 AND SRM 51-40-02.

Part: SUPPORT — CORRODED (BS 520) · airframe 105,747 hrs · 16,499 cycles

FWD CARGO BAY BS 520, RBL 42 LATERNAL SUPPORT OTBD FOUND CORRODED AT THE DOOR SILL. REPLACED IAW SRM 51-10-02 AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 522-544) · airframe 105,747 hrs · 16,499 cycles

FWD CGO COMPT BS 522 TO 544, RBL 24.75 FLOOR SUPPORT WAS FOUND CORRODED. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-02, AND INSTALLED IAW SRM 51-40-02.

Part: SUPPORT ANGLE — CORRODED (BS 512-519) · airframe 105,747 hrs · 16,499 cycles

FWD CARGO BAY BS 512 - 519, RBL 40 NO. 5R PDU OTBD MOUNTING SUPPORT ANGLE FOUND CORRODED. THE MOUNTING SUPPORT ANGLE WAS REPLACED IAW SRM 51-10-02, AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 478-500) · airframe 105,747 hrs · 16,499 cycles

FWD CARGO BAY BS 478 TO 500, RBL 23 FLOOR SUPPORT FOUND CORRODED. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-02, AND INSTALLED IAW SRM 51-40-02.

Part: SKIN — CORRODED (BS 1307) · airframe 105,747 hrs · 16,499 cycles

DEEP BLEND OUT UNDER LOCK FASTENER HEAD EXPOSING PART OF COUNTERSINK THAT HAD LIGHT CORROSION UNDERNEATH ON UPPER SURFACE FUSELAGE CROWN SKIN BS 1307 OTBD OF STRINGER 1R. THE AREA WAS REPAIRED IAW SRM 53-00-01, RPR 29, FIG 201.

Part: SKIN — SCRATCHED (BS 654) · airframe 105,747 hrs · 16,499 cycles

BS 654+30 - 654+36, STRINGERS 4L - 5L SKIN FOUND SCRATCHED. THE SKIN WAS REPAIRED IAW SRM 53-00-01, REPAIR 14, FIG 201.

Part: SPLICE — CHAFED (FUEL SYSTEM) · airframe 105,725 hrs · 16,497 cycles

LT ENG FUEL FILTER EICAS. EMERGENCY DECLARED. FOUND WIRE W3508-005-18 PIN A ON CONNECTOR D10996 CHAFING TO GRD ON AN EXISTING SPLICE 24 INCHES FROM PLUG D4232P. REMOVED AND REPLACED DAMAGED SPLICE IAW SWPM 20-10-13, 20-30-12 & WDM 73-34-11. PERFORMED HIGH POWER RUN OF NR 1 ENGINE WITH NO MESSAGES NO OTHER FAULTS NOTED.

Part: PRESSURE SWITCH — FAULTY (NR 1 ENGINE) · airframe 105,707 hrs · 16,493 cycles

AT TOP OF CRUISE GOT A L ENG FUEL FILTER EICAS. EMERGENCY DECLARED. T/S PER FIM 73-34 FAULT TREE 803. CHANGED NR 1 ENG FUEL FILTER REF AMM 73-11-02. LEAK CHK GOOD. MSG DID NOT RETURN ON IDLE RUN. R&R NR 1 ENG FUEL PUMP DIFFERENTIAL PRESSURE SWITCH PER AMM 73-34-01. LEAK AND OPS CHECK NORMAL. NO MSG. SHOWING AT THIS TIME.

Part: LENS — BROKEN (CABIN) · airframe 105,592 hrs · 16,476 cycles

EMERGENCY EXIT LIGHT LENS IS BROKEN AT SEAT 20J. INSTALLED NEW EMERGENCY EXIT LIGHT LENS.

Part: PIN — LOOSE (CABIN) · airframe 104,846 hrs · 16,370 cycles

EMER LIGHT AT SEAT 39J INOP WHEN TESTED. ADDITIONAL EMERGENCY LIGHTS INOP AT SEATS 27J, 28J, AND 34J RELAMPED, NO HELP. LIGHT SOCKET TESTED OK. SECURED LOOSE EMERGENCY SEAT LIGHT CONNECTIONS AT 27J, 28J AND 34J, FOUND PUSHED PIN AT SEAT LIGHT CONNECTOR FOR 39J, RESECURED, ALL SEAT EMERGENCY LIGHTS OPERATIONAL CHECK OK REF MM33-51-10 .

Part: LAMP — LOOSE (EMERGENCY LIGHT) · airframe 104,772 hrs · 16,361 cycles

MID LEFT SIDE FWD EMERGENCY EXIT DOOR LAMP OUT. REPOSITIONED THE LAMP, OPS CHECKED GOOD

Part: SKIN — PUNCTURED (LT ELEVATOR) · airframe 103,842 hrs · 16,230 cycles

LEFT INBD ELEVATOR UPPER SURFACE PUNCTURED. REPAIRED IAW ECRA5520-01503.

Part: FAILSAFE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,472 hrs · 15,744 cycles

MAJOR REPAIR, AFT PIT STATION 1562 FAIL SAFE STRAP WAS FOUND CORRODED, BETWEEN STRINGER 38L & 38R. REPAIR WAS ACCOMPLISHED IAW ECRA 5362-01030.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,472 hrs · 15,744 cycles

CORROSION IN AFT CARGO COMPARTMENT ON FRAME 1197.66 T CAP LOWER SURFACE RBL 38 AT NUTPLATE. R & R T CAP AT BS 1197.66, LBL 46 TO RBL 46 IAW SRM 51-40-02 & DWG 146T1226.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,472 hrs · 15,744 cycles

MAJOR REPAIR, AFT PIT STATION 1220, SHEER TIE CORRODED AT BL 0. SHEAR TIE WAS REPLACED IAW SRM 51-40-05, SRM 51-30-01 & DWG 140T2102.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,472 hrs · 15,744 cycles

CORROSION BS 1540, LBL 6 AFT CARGO FLOOR ON WEB & SHEAR TIE. CORROSION ON SHEAR TIE R & R IAW SRM 51-40-02 & DWG 146T1222 & 140T2102. NO CORROSION NOTED ON WEB.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,472 hrs · 15,744 cycles

CORROSION BS 1540, RBL 6 AFT CARGO FLOOR BILGE SHEAR TIE. R & R SHEAR TIE IN AFT CARGO BS 1540, RBL 6 IAW SRM 51-40-02 & DWG 146T122 2 & 140T2102.

Part: OXYGEN MASK — NO TEST (CABIN) · airframe 100,172 hrs · 15,702 cycles

DURING OXYGEN MASK MANUAL DROP TEST MASK BOX DOORS AT 7HC, 8AB & 34KJ DID NOT OPEN IAW AMM 35-21-00 STEP 2E. SEATS 7HC, 8AB ADJUSTED. SEAT 34KJ CURRENTLY DF398. DROP TEST GOOD ON 7HC & 8AB.

Part: LANYARD — MISSING (OXYGEN MASK) · airframe 100,172 hrs · 15,702 cycles

DURING OXYGEN MASK MANUAL DROP TEST, THE AFT RIGHT FLIGHT ATTENDANT MASKS DROPPED & IT WAS NOTED THAT THE ACTIVATION LANYARD WAS MISSING & THAT THE MASK LANYARD RINGS WERE NOT ATTACHED TO THE OXYGEN GENERATOR FIRING PIN. IAW AMM 35-21-00 STEP 2E. INSTALLED ACTIVATION LANYARD & SECURED MASK RINGS IAW AMM 35-21-10.

Part: OXYGEN GEN — MISSING (CABIN) · airframe 100,172 hrs · 15,702 cycles

DURING OXYGEN MASK MANUAL DROP TEST THE AFT LEFT FLIGHT ATTENDANT MASKS DROPPED & IT WAS NOTED THAT THE OXYGEN GENERATOR WAS MISSING. REPLACED OXYGEN MODULE LEFT AFT POSITION IAW AMM 35-21-10. TEST OF PASSENGER OXYGEN MASKS AMM 35-21-00. OPERATIONAL CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 100,156 hrs · 15,700 cycles

EMERGENCY EXIT FLOOR, EMER EXIT INOPERATIVE. JUST FWD OF MID SEAT ROW 19. REPLACED BATTERY M1559 IAW MM 33-51-07. OPERATIONS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 100,156 hrs · 15,700 cycles

EMERGENCY EXIT FLOOR EMER EXIT INOPERATIVE AT MID LT LAVATORY. REPLACED BATTERY M1559 IAW MM 33-51-07. OPERATIONS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 100,156 hrs · 15,700 cycles

SEAT MOUNTED EMER EXIT LIGHTS INOPERATIVE FROM SEAT ROWS 19 RT - 22 RT. REPLACED POWER SUPPLY M1209 IAW MM 33-51-07. OPERATIONS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 100,156 hrs · 15,700 cycles

EMERGENCY EXIT LIGHT, EXIT SIGNS INOPERATIVE AT 2 EA LT OVERWING EXIT DOORS. REPLACED BATTERY M1559 IAW MM 33-51-07. OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 98,915 hrs · 15,537 cycles

MID LAVATORY 111 LT SIDE EMER EXIT LIGHT STRIP IS INOPERATIVE. SECURED CONNECTION. OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 97,745 hrs · 15,381 cycles

EMERGENCY EXIT LIGHT INOPERATIVE AT AFT GALLEY FLOOR. SECURED CONNECTION. OPERATIONS CHECKED NORMAL.

Part: FASTENER — CORRODED (FUSELAGE) · airframe 96,849 hrs · 15,256 cycles

DURING LIGHTNING STRIKE INSPECTION IAW SMC 179 FOUND CORRODED HARDWARE LOCATED BELOW THE PILOT'S FWD NR 1 WINDSHIELD CLEANED LIGHT CORROSION & PAINTED IAW GPM 5-0-4-024.

Part: IRU — MALFUNCTIONED (RIGHT) · airframe 95,854 hrs · 15,118 cycles

IRS 3 ON POS IAW 2 - 4 SHOWED AN INCREASING ACTUAL MILEAGE THROUGHOUT THE FLIGHT. DIS OF IRUS WAS GROSSLY DIFFERING IN BEARING. UP TO 140 DEGREES DIFFERENCE RT INERTIAL IAW UNIT FAILS REMOVAL CHECK IAW FIG 107B, REPLACED RT IRU IAW AMM34- 21-401. ALSO PERFORMED MCDP TEST 30 IAW AMM 22-00-03 117. OPERATIONS CHECKED GOOD ACFT REMAINS FULL CAT CAPABLE AUTO LAND

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 95,760 hrs · 15,106 cycles

EXTERIOR EMERGENCY LIGHT AT DOOR 1LT IS INOPERATIVE. RELAMPED EXT DOOR 1LT EMERGENCY LIGHT, OPERATIONS CHECK OK IAW MM 33-51-00.

Part: LATCH — OUT OF SEQUENCE (CARGO DOOR) · airframe 95,760 hrs · 15,106 cycles

WHILE PERFORMING TASK CARD 682205001 AFT CARGO DOOR OPERATIONS CHECK, CARGO DOOR LOST POWER, BITE CHECKED PSEU F LAGGING SENSOR S209. FOUND LATCH ACT OUT OF SEQUENCE. ONLY RETRACTS HALFWAY, WILL NOT RETRACT ELEC OR MANUALLY TO LIFT DOOR SO IT CAN BE CLOSED.

Part: VALVE — FAULTY (FUEL SYSTEM) · airframe 95,626 hrs · 15,085 cycles

FUEL BURNS FROM RT TANK WITH RT CTR PUMP ON. WITH CROSS FEED VLV OPEN & LT CTR PUMP FEEDING RT ENG, NO MORE FUEL BURNS FROM RT TANK. APPEARS RT CTR PUMP DOES NOT OVERRIDE RT MAIN TANK PUMPS TO FEED THE RT ENG. PROBLEM FOUND TO BE THE RT WING OTBD FILL VLV, REPLACEMENT ACCOMPLISHED.

Part: FUEL — LEAKING (LT ENGINE) · airframe 95,585 hrs · 15,080 cycles

1 FUEL LEAK FROM VICINITY OF LT ENG 2.5 BLEED VLV.

Part: VALVE — OUT OF ADJUST (AC BAY) · airframe 95,530 hrs · 15,071 cycles

FWD EQUIPMENT VLV EICAS & OVERHEAD EQUIPMENT COOLING VLV CYCLING ON & OFF, COMPLIED WITH MEL 2158U. CLOSED OVERBOARD VLV & DEACTIVATED IAW MEL 2158S. PERFORMED ADJUSTMENT TEST ON FWD EQUIPMENT VLV IAW AMM 21 58 00 CONFG 3, NO FAULTS NOTED ALL CHECKED GOOD.

Part: VALVE — MALFUNCTIONED (E&E BAY) · airframe 95,483 hrs · 15,065 cycles

FWD EQPT VLV EICAS & OVERHEAD EQPT COOLING VLV CYCLING ON & OFF. COMPLIED WITH MEL 2158U, CLOSED OVERBOARD VLV & DEACTIVATED IAW MEL 2158S.

Part: LIGHT — INOPERATIVE (RT WING) · airframe 95,435 hrs · 15,058 cycles

RT WING NAV LIGHT BULB INOPERATIVE. PLACED RT GREEN NAV LIGHT ON MEL 3343B.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 95,288 hrs · 15,034 cycles

FOUND CREASE ON FRAME 228 LAP SEAM STATION 222.4 TO 230.5 AT LAP SPLICE STRINGER 21L. THE DENT IS LOCATED IN THE RVSM CRITICAL AREA. REPAIRED IAW ECRA 5310-05971 REO 617052 REV B.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 95,288 hrs · 15,034 cycles

LT SIDE FIRST & BUSINESS CLASS SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY PACK LOCATED AT STATION 988, WL 203 & LBL 92 IAW B767 AMM 33-51-07 & OPERATIONS CHECKED GOOD ON NON-ROUTINE 23120.

Part: SKIN — DENTED (FUSELAGE) · airframe 95,288 hrs · 15,034 cycles

RT FUSELAGE SKIN DENTED AT STATION 654+66, STRINGER 29R. EVALUATED DENT & FOUND TO BE WITHIN LIMITS OF SRM 53-00-01. DENT WIDTH 2.65, DEPTH.054 & A OVER Y RATIO 49. DENT IS SMOOTH & CRACK FREE, OK TO ARCHIVE. ^18JAN GSO RPR RE-EVALUATED DENT AT S CHECK & FOUND CREASE DEFECT OUT OF LIMITS IAW SRM 53-00-01, DETAIL III, FIG 101. CUT-OUT DAMAGED SECTION 085625 OF SKIN, FABRICATED & INSTALLED A REPAIR DOUBLER & FILLER IAW SRM 53-00-01, REPAIR 14 IAW SRM TABLE V.

Part: SKIN — DENTED (FUSELAGE) · airframe 95,288 hrs · 15,034 cycles

EVALUATED FUSE SKIN BETWEEN BS 320 - 478 LT BETWEEN STRINGER 21L TO 23L. FOUND TWO DENTS AT BS 471 & STRINGER 23L OUT OF LIMITS IAW SRM 53-00-01. DENT CROSSES STRINGER 23L, NO OTHER DEFECTS NOTED. CUT OUT DAMAGED AREA OF SKIN AT BS 471 & STRINGER 23L. FABRICATED & INSTALLED A REPAIR DOUBLER & FILLER IAW SRM 53-00-01, REPAIR 1 ON NON-ROUTINE 22505.

Part: VALVE — OPEN (AC BAY) · airframe 94,996 hrs · 14,996 cycles

FWD EQUIPMENT VLV IN THE OPEN POSITION.

Part: WINDOW — DAMAGED (COCKPIT) · airframe 94,814 hrs · 14,973 cycles

LOUD SQUEAL COMING FROM CAPTAINS SIDE WINDOW. INTERIM REPAIR ACP IAW MM.

Part: ACTUATOR — LEAKING (NR 2 ENGINE) · airframe 94,576 hrs · 14,942 cycles

NR 2 ENG VSV ACTUATOR LEAKING FUEL FROM SIDE COVER. REMOVED & INSTALLED NR 2 ENG VSV ACTUATOR IAW AMM.

Part: VALVE — BLOWN (APU) · airframe 94,478 hrs · 14,929 cycles

APU SURGE VALVE HAS DUCT THAT IS BLOWN.. REPLACED SURGE VALVE & DUCT. APU OPERATION NORMAL.

Part: PRESSURE SWITCH — FAULTY (APU) · airframe 94,478 hrs · 14,929 cycles

APU AUTO SHUTDOWN ECU SHOWS "GEN FILTER" IN 2 OF THE LAST 4 SHUTDOWNS. IAW FIM49-11-00 CONF 2 PG 146 ITM2 SWITCH NEEDS TO BE CHECKED FOR RESISTANCE. PCN 481-1503 ORDERED. IAW AMM 49-27-15, AMM 49-27-03, AMM 49-27-04, CHECKED CHIP DETECTOR FOUND OK. REPLACED GEN FILT DIFF P SWITCH & CHANGED GEN FILTER. APU OPERATES NORMALLY.

Part: SWITCH — FAULTY (ELECTRICAL SYS) · airframe 94,378 hrs · 14,916 cycles

UNABLE TO RESET RT UTILITY SWITCH. R & R RT UTILITY BUS SWITCH, OPERATIONS CHECKED NORMAL.

Part: CIRCUIT CARD — NOT SEATED (E&E BAY) · airframe 94,312 hrs · 14,909 cycles

FWD EQUIP VALVE EICAS AFTER ENGINE START. ACCOMPLISHED FIM TASK 21- 58-00 FIG 105 STEPS 1 THRU 3. RESEATED EQUIP IND CARD M867 & CHECKED ALL VALVE OPENINGS. RESEATED PLUG ON V91. MESSAGE & VALVE LIGHT CLEARED & NOW IN AUTO & STBY VALVE LIGHT REMAINS EXTINGUISHED & WORKS NORMALLY WHEN ACCOMPLISHING N2 SPEED CARD TEST.

Part: RIVET — MISSING (NR 2 COWLING) · airframe 94,149 hrs · 14,887 cycles

NR 2 ENG LT CORE COWL HAS 3 MISSING RIVETS BETWEEN 8 & 9 O'CLOCK POSITION.

Part: VALVE — OUT OF POSITION (E&E BAY) · airframe 94,140 hrs · 14,886 cycles

FWD EQUIPMENT VALVE MESSAGE ON EICAS. EQUIPMENT COOLING IN AUTO POSITION ACP'D P61 EQUIPMENT COOLING GROUND TEST. SMOKE & OVERHEAT MESSAGES SHOWN IAW TEST & SMOKE LIGHT OVERHEAD. VALVE LIGHT EXTINGUISHED ONCE VALVES REPOSITIONED. VALVE LIGHT REMAINED OUT AFTER TEST. CYCLED SWITCH TO STANDBY, VALVE LIGHT CYCLED ON THEN OFF. RETURNED TO AUTO & LIGHT OFF. NO HISTORY NOTED & SYSTEM CHECKED GOOD.

Part: COMPUTER — MALFUNCTIONED (EICAS) · airframe 94,079 hrs · 14,878 cycles

RT EICAS STATUS MESSAGE AFTER LANDING. REPLACED EICAS COMPUTER IAW AMM & TESTED SATISFACTORY.

Part: SEAL — MISSING (RT AILERON) · airframe 93,918 hrs · 14,856 cycles

REPORT OF PIECE OF RUBBER COMING OFF WING DURING LANDING. FOUND ON RT AILERON INBD SIDE, UPPER SEAL MISSING REPLACED SEAL WITH PN 10.60754-221 IAW AMM 27-10-00.

Part: WARNING MESSAGE — ILLUMINATED (SMOKE DETECTOR) · airframe 93,895 hrs · 14,853 cycles

FORWARD CARGO DETECTOR 1 STATUS MESSAGE WILL NOT CLEAR.

Part: AMPLIFIER — FAULTY (COCKPIT) · airframe 93,879 hrs · 14,851 cycles

SATCOM VOICE. ACCOMPLISHED MM23-25-00 FAULT ISOLATION. 'HGA HPA INACTIVE' DISPLAYED ON CDU. VERIFIED POWER AT HPA. M1782, HGA HPA HAS 'POWER SUPPLY FAULT' LIGHT ILLUMINATED. REPLACED HPA PER MM. TESTED SYSTEM PER MM, OPS CHECKED NORMAL.

Part: COMPUTER — FAILED (RIGHT) · airframe 93,879 hrs · 14,851 cycles

EICAS DISAGREE STATUS MESSAGE WILL NOT CLEAR ON LOWER DISPLAY. FOUND RT EICAS COMPUTER FAILING. ITEM TRANSFERRED IAW 3141H. REPLACED EICAS COMPUTER AND LOADED OPC & OPS SW REF MM, GROUND TEST NORMAL.

Part: WARNING MESSAGE — ILLUMINATED (AILERONS) · airframe 93,798 hrs · 14,840 cycles

"AILERON LOCK" ILLUMINATED AT LOW SPEED. EICAS MESSAGE AILERON LOCKOUT DISPLAYED. OTBD AILERONS DID NOT INDICATE NORMAL-LOCKED OUT-BOTH. CARRIED OUT TEST IAW MM 27-11-44 & FIM 27-11-00 ALL OPS & INDICATIONS NOW OK.

Part: FASTENER — MISSING (WING PANEL) · airframe 93,619 hrs · 14,818 cycles

WALKAROUND MULTIPLE FASTENERS LOOSE, MISSING UNDERWING PANELS BOTH SIDES, OTBD EA MLG STRUT. INSTALLED NEW FASTENERS ON UNDERWING PANELS.

Part: SEAL — LEAKING (NR 1 STARTER) · airframe 93,488 hrs · 14,801 cycles

LEFT ENGINE SHOWS SIGNS OF OIL LEAKAGE. FOUND NR 1 ENG STARTER QUAD COUPLING SEAL LEAKING. REPLACED SEAL AND REFITTED QUAD COUPLING IAW AM. LEAK TEST ACTIONED IAW AMM 71-00-00, TEST 5 OK. NO LEAKS OBSERVED.

Part: ALTIMETER — MALFUNCTIONED · airframe 93,482 hrs · 14,800 cycles

CAPTAIN'S ALTIMETER FROZEN. PERFORMED FUNCTIONAL TEST OF THE LEFT ADC TEST PASSED ALSO PERFORMED TEST 30 IAW AMM, TEST PASSED, NO FAULT NOTED AT THIS TIME.

Part: DOOR — UNSECURE (RAT) · airframe 93,422 hrs · 14,792 cycles

RAM AIR TURBINE UNLOCKED. FOUND RAT DOOR EXTENDED 1 .5". CYCLED RAT. ALL INDICATIONS NORMAL.

Part: TRANSCEIVER — FAULTY (NR 2 VHF) · airframe 93,406 hrs · 14,790 cycles

NR 2 VHF HAS LOUD, STATIC HUM. REPLACED NR 2 VHF TRANSCEIVER.

Part: OIL SYSTEM — LEAKING (LT ENGINE) · airframe 93,373 hrs · 14,786 cycles

OIL DRIPPING FROM LT ENGINE. BOTTOM HALF OF TAILPIPE COVERED IN OILY SHEEN. CLEANED OIL FROM AREA AND BREATHER OUTLET HOLE. OPENED CORE COWL AND NO ACTIVE LEAK NOTED. COMPLIED WITH OIL CONSUMPTION CHECK REF AMM. NO EXCESS OIL CONSUMPTION NOTED ON PLN OIL IN AMS DIS.

Part: FAN — FAILED (AFT EQUIP) · airframe 93,199 hrs · 14,762 cycles

STATUS MESSAGE AFT EQUIPMENT EXHAUST FAN NR 1 DISPLAYED ON STATUS PAGE. PERFORMED TROUBLESHOOTING IAW FIM 21-26-00. FOUND CIRCUIT BREAKER FOR EQUIPMENT COOLING FAN NR 1 TRIPPED, UNABLE TO RESET. REPLACED RECIRCULATION FAN, OPS CHECKS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 93,190 hrs · 14,761 cycles

EMERGENCY AISLE LIGHT AT ROW 38KJ INOPERATIVE. REPLACED LAMP IAW AMM. OPS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 93,190 hrs · 14,761 cycles

EMERGENCY SLIDE LIGHT AT R2 DOOR INOPERATIVE. REPLACED LAMP IAW AMM, OPS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 93,190 hrs · 14,761 cycles

EMERGENCY SLIDE LIGHT AT L1 DOOR INOPERATIVE. REPLACED LAMP IAW MM 33-51-06-902-082. OPS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 93,190 hrs · 14,761 cycles

EMERGENCY AISLE LIGHT AT ROW 35AB IS INOPERATIVE. REPLACED LAMP, OPS CHECKED NORMAL.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT ROW 19K) · airframe 93,143 hrs · 14,754 cycles

CABIN OXYGEN MASK DEPLOYED AT 19K. REPACKED OXYGEN MASK IAW MM 35-21-00-501 & 35-21-10-532-116.

Part: B-NUT — LOOSE (HYD LINE) · airframe 93,099 hrs · 14,747 cycles

DURING WALKROUND CHECK, NOTICED HYD LEAK ON RT MAIN GEAR BOGIE TILT ACTUATOR. FOUND HYD CONNECTION B-NUT LOOSE. NUT TIGHTENED CORRECTLY. OPS TESTED GOOD. NO LEAKS. OK FOR SERVICE.

Part: STARTER — FAILED (LT ENGINE) · airframe 93,060 hrs · 14,742 cycles

DURING LEFT ENGINE START, NO N2 ROTATION, HAD GOOD DUCT PRESSURE DROP AND START VALVE INDICATION, TRIED TWICE, NO HELP, RESET "D19" CIRCUIT BREAKER NO HELP, NO N2 ROTATION. REPLACED STARTER IAW MM. REPLACED STARTER VALVE MM. PERFORMED MOTORING OF ENGINE 1.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 92,893 hrs · 14,718 cycles

RIGHT ENGINE HYDRAULIC LEAK FROM AFT STRUT. ACCOMPLISHED PERMANENT REPAIR IAW DWG 272T3100 AND IAW MM 20-10-09. ACCOMPLISHED LEAK CHECK ALL NORMAL.

Part: AUDIO PANEL — FAULTY (CAPTAIN'S) · airframe 92,702 hrs · 14,698 cycles

CAPTAIN'S AUDIO PANEL NOT ILLUMINATED. REPLACED CAPTAIN`S AUDIO CONTROL PANEL IAW MM, OPS OK.

Part: CONTROL PANEL — FAULTY (CAPTAIN'S AUDIO) · airframe 92,639 hrs · 14,690 cycles

CAPTAIN'S RADIO LOUD SIDE TONE EVERY TIME KEYED. REPLACED CAPTAIN`S AUDIO CONTROL PANEL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 92,557 hrs · 14,680 cycles

BUSINESS CLASS CROSS AISLE LIGHT INOP IN FULL OK IN DIM. RELAMPED OKAY.

Part: BLADE — NICKED (NR 1 ENGINE) · airframe 92,459 hrs · 14,668 cycles

NR 1 ENGINE FIRST STAGE FAN BLADE NICKED ON LEADING EDGE APPROX 12 INCHES FROM OUTBOARD END WITH A DEPTH OF .010. ACCOMPLISHED FIRST BLEND ON BLADE IAW AMM 72-31-02. ACCOMPLISHED HFEC AS REQUIRED REF NDT MANUAL PART 6 72-31-401. NO CRACKS FOUND.

Part: COMPUTER — INOPERATIVE (RIGHT) · airframe 92,105 hrs · 14,619 cycles

F/O'S HEADING FLIGHT DIRECTOR INOPERATIVE. REPLACED RIGHT FCC, SYSTEM CHECKED OK PER MM 22-10-00, AIRCRAFT IS AUTOLAND CAPABLE.

Part: COMPUTER — FAILED (RT EICAS) · airframe 92,009 hrs · 14,606 cycles

RIGHT EICAS COMPUTER SOFTWARE LOADING FAILURE. REPLACED RIGHT EICAS COMPUTER AND TESTED FOUND NORMAL.

Part: VALVE — FAILED (NR 2 ENGINE) · airframe 92,009 hrs · 14,606 cycles

NR 2 ENGINE FAN AIR VALVE PNEUMATIC HEALTH CHECK FAILED AS PER FCD 3611-01233. NR 2 ENGINE FAN AIR VALVE REPLACED & BITE TEST CARRIED OUT AS PER AMM 36-11-16 & RESULT NORMAL.

Part: SHUTOFF VALVE — FAILED (PNEUMATIC) · airframe 92,009 hrs · 14,606 cycles

NR 2 ENGINE HPSOV PNEUMATIC HEALTH CHECK FAILED AS FCD 3611-01233. NR 2 ENGINE HPSOV PNEUMATIC HEALTH CHECK FAIL AS FCD 3611-01233 NR 2 ENGINE HPSOV REPLACED & INSTALLATION TEST CARRIED OUT AS PER AMM. RESULT NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 91,924 hrs · 14,595 cycles

FORWARD EQUIPMENT VALVE EICAS MESSAGE. PERFORMED FIM TASK 21 58 00 FIGURE 104. NO FAULTS FOUND, SYSTEM CHECKED GOOD. OK TO CONTINUE.

Part: STRUT — CRACKED (ENGINE) · airframe 91,515 hrs · 14,538 cycles

INSPECTION FOUND ONE INCH CRACK AFTER STRESS RELIEF AND FPI, WELDED STRUT IAW 72-54-01 RU02 REPAIR C.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 91,465 hrs · 14,531 cycles

EMERGENCY LIGHT INOPERATIVE AT MID LAV LEFT AISLE. REPLACED LIGHT. TESTED OK. ACCOMPLISHED IDT INSPECTION OF REPLACED FLOOR EMERGENCY LIGHT STRIP.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 91,465 hrs · 14,531 cycles

EMERGENCY CEILING FLOOD LIGHT INOPERATIVE 13AB RECONNECTED CONNECTOR, OPERATIONAL TESTED GOOD.

Part: VALVE — FAULTY (TRIM AIR) · airframe 91,433 hrs · 14,527 cycles

FWD CABIN TEMP EICAS, UNABLE TO OPEN VALVE EVEN IN MANUAL. PULLED CIRCUIT BREAKERS H2 & H5. REPLACED THE AUXILARY FORWARD TRIM AIR MODULATING VALVE (V152) IAW AMM. ACCOMPLISHED OPS TEST IAW AMM, ALL CHECKED GOOD.

Part: MOTOR — INOPERATIVE (HYD SYSTEM) · airframe 91,323 hrs · 14,507 cycles

HYDRAULIC MOTOR GENERATOR (HMG) INOPERATIVE AND DEACTIVATED. HYDRAULIC MOTOR GENERATOR (HMG) HAS BEEN DEFERRED IN COMPLIANCE WITH MEL CARD 29060. REACTIVATED SYSTEM PER MEL 2911G AND 2425A.

Part: SENSOR — FAULTY (COCKPIT TEMP) · airframe 91,307 hrs · 14,505 cycles

FLIGHT DECK TEMP CONTROL PROBLEMS. REPLACED FLT DECK ZONE TEMP SENSOR PER MM 21-61-08 & REPLACED FLT DECK ZONE DUCT SENSOR, BOTH SENSORS BITE TEST GOOD.

Part: CONTROLLER — FAULTY (CABIN TEMP) · airframe 91,206 hrs · 14,491 cycles

NEED TO REPLACE ZONE TEMP CONTROLLER DUE TO FWD, MID, ZONE TEMP FAULT. VERY ERRATIC ON ECS PAGE. VERY ERRATIC ON ECS PAGE. REPLACED ZONE TEMP CONTROLLER. FWD AND MID CABIN TEMPS ROSE TO 76 AFTER 30 MIN AT 69. MOVED CTRL SLIGHTLY, NOW BACK TO 69. FWD AND MID INDICATE INOP,NO ECS PAGE TRIM VALVE POSITION VALUES FOR AUX FWD,FWD,AUX MID,MID.FLIGHT DECK TRIM AIR WORKS IN MANUAL,INOP IN AUTO. AFT INDICATES OK. REPLACED K238 RELAY. REPLACED ZONE TEMP CONTROLLER, OPS CHECK AND BITE NORMAL.

Part: MODULATING VALVE — FAULTY (NR 1) · airframe 91,188 hrs · 14,488 cycles

COCKPIT COLD. COCKPIT TRIM AIR VALVE IND SHOWS FULL HOT AND COLD AIR IS BLOWING INTO COCKPIT. REMOVED AND REPLACED FLT DECK TRIM AIR MODULATING VALVE, OPS CHECK GOOD.

Part: REGULATOR VALVE — FAULTY (TEMP CONTROL) · airframe 91,169 hrs · 14,485 cycles

DIFFICULT TO CONTROL CABIN AND COCKPIT TEMPS, HAD TO SWITCH BETWEEN AUTO AND TRIM AIR OFF. REPLACED TRIM AIR REG VALVE. BECAUSE NO FAULTS WERE FOUND, REMOVED BOTH TRIM AIR CHECK VALVES, FOUND OK AND INSTALL PROPER, ALSO CHECKED SENSE LINE ON TRIM AIR REG VALVE.

Part: CONTROLLER — FAULTY (TEMP CONTROL) · airframe 91,161 hrs · 14,484 cycles

FLT DECK TEMP CONTROL FULL WARM AND VALVE SHOWS FULL WARM BUT ONLY PUTS OUT COLD AIR. SAMC TEXT: PER VERBAL FROM FLT CREW. COLD TEMPS IN BOTH COCKPIT AND CABIN. STANDBY W-NO HELP. STANDBY ON DID HELP BRING TEMPS UP. ACP BITE CHECKS ON ZONE TEMP AND AUX TEMP CONTROLLERS ZONE TEMP CONTROLLER FAILED AND REPLACED REF MM AND ACP TESTS. ALL ZONE TEMPS OKAY.

Part: COVER — MISSING (RUDDER) · airframe 91,018 hrs · 14,463 cycles

DURING PRE DEPARTURE WALKAROUND FOUND UPPER RUDDER HINGE COVER MISSING. NEEDS 1 EA 173T2011-7 BOND, 2 EA FASTENER HL97DU6 REF IPC 55-40-55-0001 ITEMS 774, 777. WILL REQUIRE 2 SHIFT SLOT MUST REMOVE UPPER AND PARTLY LOWER PANEL ABOVE AND BELOW UPPER RUDDER HINGE COVER, HAVE FASTENERS WILL ATTACH TO IPC WILL NEED OUT OF STOCK ORDER FOR PANEL 173T2011-7 BOND ASSY.

Part: LINE — LEAKING (LT HYD SYSTEM) · airframe 90,675 hrs · 14,418 cycles

LEFT HYD QTY EICAS INFLIGHT WITH RF 0.48. FOUND HYD LINE IN LEFT SAIL TAIL LEAKING. INSTALLED NEW LINE AND OPS CHECKED. NO LEAKS.

Part: BLOCKER DOOR — DAMAGED (THRUST REVERSER) · airframe 90,171 hrs · 14,350 cycles

LEFT ENGINE BLOCKER DOOR FOUND DAMAGED AT THE 3 O'CLOCK POSITION. RADIAL CRACK APPROX 3 INCHES. BLOCKER DOOR AND DRAG LINK REMOVED IAW MM 78-31-15. INSTALLED BLOCKER DOOR AND DRAG LINK IAW AMM 78-31-14 AND AMM 78-31-15. OPS CHECKED OK.

Part: SENSOR — FAULTY (STALL WARNING) · airframe 90,156 hrs · 14,348 cycles

AIRSPEED INDICATOR FLUX, RTFL. ACCOMPLISHED LEFT ADC BITE PROC PER FIM 34-12-00. THE FAULT DISPLAY INDICATES 1. PLEASE REPLACE LEFT ANGLE OF ATTACK SENSOR PER MM. RPL'D LT ANGLE OF ATTACK PER MM, OPS NORMAL. REPLACED LEFT ADC PER MM. ALL INDICATIONS NOW NORMAL. ACCOMPLISHED MCDP TEST 30 PER MM 22-00-02, NO CURRENT FAULTS INDICATED. SEE SMC 4 FOR FURTHER WORK TO BE ACCOMPLISHED.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 89,991 hrs · 14,325 cycles

DOOR 1R SLIDE PRESSURE LOW. REPLACED SLIDE. ACCOMPLISHED PER MM AND R II METHOD 1 PIN. REMOVED SLIDE WITHIN DATE AND GIRT BAR IS ALIGNED AND PRESSURE IS NORMAL

Part: BRAKE — FAILED (MLG) · airframe 89,959 hrs · 14,321 cycles

NEED RIGHT TILLER TO TAXI, PULLS LEFT. TROUBLESHOT PER FIM 32-51-00. REPLACED NR 6 BRAKE PER AMM.

Part: BRACKET — CRACKED (WINDOW) · airframe 89,861 hrs · 14,309 cycles

AT DEPARTURE TIME, CAPTAIN UNABLE TO SECURE SLIDING COCKPIT WINDOW. SUPPLEMENTAL DATA UPDATE, ADJUSTED NR 2 CAPTAIN WINDOW, CHECK NO LEAK. LOWER CARRIAGE BRACKET ITEM NR 365 P NR 141T4883-501, -9, OR -15 IS CRACKED AT CAPTAIN'S SLIDING WINDOW. SEE IPC 56-11-04-001C PG6 AND PG19. ITEM ON AOG K4828 DELIVERY TO LSVC.

Part: WINDOW — STUCK (COCKPIT) · airframe 89,861 hrs · 14,309 cycles

AT DEPARTURE, CAPTAIN UNABLE TO SECURE SLIDING COCKPIT WINDOW. ADJUSTED NR 2 CAPTAIN WINDOW, CHECKED, NO LEAKS.

Part: ISOLATION VALVE — FAULTY (THRUST REVERSER) · airframe 89,845 hrs · 14,306 cycles

NR 2 ENGINE THRUST REVERSER FAULT. REPLACED NR 2 THRUST REVERSER MOTORIZED ISOLATION VALVE IAW.

Part: COMPUTER — FAILED (AUTOTHROTTLE) · airframe 89,590 hrs · 14,269 cycles

AUTOTHROTTLE WILL NOT STAY ENGAGED IN VNAV OR FLCH. REMOVED AND REPLACED THRUST MANAGEMENT COMPUTER AS PER AMM, OPS CHECKED GOOD. PERFORMED TEST 30 AS PER AMM, ACFT RESTORED TO FULL CAPACITY CAT STATUS.

Part: SKIN — MISREPAIRED (BS 14301461) · airframe 88,677 hrs · 14,145 cycles

EXTERNAL FUSELAGE SKIN AT BS 1430-1461 JUST BELOW CARGO DOOR WAS FOUND MISREPAIRED. REPAIRED SKIN IAW EA PT67-53-003 AND ECRA 5360- 01191. ACCOMPLISHED NDT OF AREA. NO CRACKS FOUND. ACCOMPLISHED INSURANCE CUT. FABRICATED AND INSTALLED EXTERNAL FILLER, DOUBLER AND TRIPLER REPAIR REF EA AND ECRA.

Part: LIGHT — INOPERATIVE (SEATS 37-38) · airframe 88,677 hrs · 14,145 cycles

EMERGENCY EXIT AISLE LIGHT AT SEATS 37-38 RT SIDE IS INOP. REPLACED SEAT EMERGENCY EXIT LIGHT REF AMM 33-51-10. OPS CHECKED GOOD.

Part: LINE — DAMAGED (POTABLE WATER) · airframe 88,677 hrs · 14,145 cycles

POTABLE WATER SUPPLY LINE RUNNING FROM STA 1375 TO 1550 HAS A BURN MARK ASSOCIATED WITH RIBBON HEATER TAPE B110 AT BS 1420. REMOVED AND REPLACED DAMAGED WATER LINE IAW AMM 38-10-00 AND SRM 51-40-02. PERFORMED LEAK CHECK TEST IAW 38-10-00. CHECKED GOOD. HEATER TAPE B110 REPLACED AND OPS CHECKED ON UAL JIC 4162R136

Part: SKIN — DENTED (BS 331 S30L) · airframe 88,677 hrs · 14,145 cycles

DENT ON FUSELAGE AT BS 331 STRINGER S30L FOUND OUT OF SRM LIMITS. TRIMMED OUT DAMAGE IAW EA PT67-53-005 AND ECRA 5310-05483. ACCOMPLISHED NDT. NO CRACKS FOUND. ACCOMPLISHED INSURANCE CUT PER EA FABRICATED AND INSTALLED EXTERNAL DOUBLER AND FILLER REPAIR REF EA AND ECRA.

Part: TERMINAL BLOCK — DAMAGED (WINDOW HEAT) · airframe 88,677 hrs · 14,145 cycles

WINDOW EICAS MESSAGE DISPLAYED. INOPERATIVE LIGHT DID NOT EXTINGUISH WHEN SWITCH WAS RECYCLED TO OFF THEN ON. BITE CHECKED, CONTROLLER FAULTED. FOUND DAMAGED TERMINAL BLOCKS ON WIRE HARNESS, HARNESS BRITTLE, TROUBLESHOOTING FOUND RECESSED PINS 2 AND 3 ON CONNECTOR D5870P. REPLACED CONNECTOR D5870P IAW SWPM 20-61-00, OPS CHECKED GOOD. WINDOW HEAT SYSTEM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 88,677 hrs · 14,145 cycles

EMERGENCY EXIT LIGHT ASSY L-288 AT R1 DOORWAY INOPERATIVE. REMOVED AND REPLACED LAMP. OPS CHECKED GOOD.

Part: FLOORBEAM — CORRODED (BS 287) · corrosion level 2 · airframe 88,677 hrs · 14,145 cycles

FWD CABIN BS 287 FLOORBEAM UPPER TEE CORRODED. REMOVED DAMAGED TEE IAW SRM 53-00-51 NR 1. ACCOMPLISHED NDT, NO CRACKS FOUND. FABRICATED AND INSTALLED UPPER TEE IAW SRM 53-00-51 FIG 201 REPAIR NR 1. MAJOR REPAIR.

Part: STRINGER — MISREPAIRED (BS 1453 S38L) · airframe 88,677 hrs · 14,145 cycles

STRINGER 38 LEFT MISREPAIRED AT BS 1453. FABRICATED AND INSTALLED STRINGER REPAIR, SRM 53-00-03 FIG 201 REPAIR 2 DETAIL 4. MAJOR REPAIR

Part: LIGHT — INOPERATIVE (SEAT 34AB) · airframe 88,677 hrs · 14,145 cycles

EMERGENCY EXIT LIGHT AT SEAT 34AB INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSY FOR SEAT. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (SEAT 34AB) · airframe 88,677 hrs · 14,145 cycles

EMERGENCY EXIT LIGHT AT SEAT 34AB INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSY FOR SEAT REF AMM 33-51-10. OPS CHECKED GOOD REF AMM33- 51-00.

Part: FLOORBEAM — CORRODED (BS 287) · corrosion level 2 · airframe 88,677 hrs · 14,145 cycles

FWD CABIN BS 287 AND RBL 20, FLOORBEAM TEE CORRODED. REMOVED DAMAGE AND FABRICATED AND INSTALLED TEE REPAIR REF SRM 53-00-051 FIG 201 REPAIR 1.

Part: FRAME — CORRODED (BS 1241 S34R) · corrosion level 2 · airframe 88,677 hrs · 14,145 cycles

AFT CARGO PIT, FRAME AT BS 1241 AND STR 34R, INNER CHORD CORRODED. REMOVED CORROSION & FOUND MATERIAL LOSS OUT OF SRM LIMITS. REMOVED EXISTING TEE. FABRICATED & INSTALLED NEW TEE. MAJOR REPAIR.

Part: SPAR — CRACKED (NR 1 NACELLE) · airframe 88,677 hrs · 14,145 cycles

NR 1 PYLON FWD UPPER SPAR WEB OUTBOARD DRAIN HOLE CRACKED AT OUTBOARD DRAIN HOLE AT NAC STA 156. STOP DRILLED CRACK. ACCOMPLISHED NDT, NO CRACKS FOUND. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 54-53-01 REPAIR 10.

Part: FLOORBEAM — CORRODED (BS 287) · corrosion level 2 · airframe 88,677 hrs · 14,145 cycles

FWD CABIN BS 287 FLOORBEAM UPPER TEE CORRODED. REMOVED DAMAGED TEE AT BS 287 RBL 37-70 IAW SRM 53-00-51 REPAIR 1. ACCOMPLISHED NDT FOR CRACKS. NONE FOUND. FABRICATED AND INSTALLED UPPER TEE REPAIR REF SRM 53-00-51 FIG 201 REPAIR 1.

Part: FRAME — CORRODED (BS 1197 S34L) · corrosion level 2 · airframe 88,677 hrs · 14,145 cycles

AFT CARGO PIT, FRAME INNER CHORD CORRODED AT BS 1197+88 AND S34L. REMOVED DAMAGE AND FOUND MATERIAL LOSS OUT OF SRM LIMITS. REMOVED DAMAGED UPPER TEE SECTION IN ENTIRETY. FABRICATED AND INSTALLED NEW UPPER TEE REF SRM51-40-02.

Part: SKIN — MISREPAIRED (BS 1447 S37L) · airframe 88,677 hrs · 14,145 cycles

SKIN BS 1447, STR 37L MISREPAIRED. CUT OUT DAMAGE, FABRICATED AND INSTALLED HAT CHANNEL AND ANGLES PER SRM 53-00-03, FIG 201, RPR 2, TYPE IV. PERFORMED HFEC PER NDTM 51-00-16, PRT 6, NO CRACKS NOTED.

Part: STRINGER — CORRODED (BS 1434 S36L) · corrosion level 2 · airframe 88,677 hrs · 14,145 cycles

STRINGER 36L IS CORRODED AT BS 1434. FABRICATED AND INSTALLED STRINGER, CHANNEL, AND ANGLE.

Part: SKIN — DENTED (BS 395 S35-36L) · airframe 88,677 hrs · 14,145 cycles

FUSELAGE DENTED AT BS 395 BETWEEN STRINGERS 35-36L. EVALUATED DENT & FOUND OUT OF LIMITS. CUT-OUT DAMAGE & ACCOMPLISHED NDT FOR CRACKS. NONE FOUND. FABRICATED & INSTALLED EXTERNAL DOUBLER & FILLER REPAIR REF SRM. MAJOR REPAIR

Part: CONTROLLER — FAULTY (APU) · airframe 88,632 hrs · 14,139 cycles

APU DID NOT START ON TAXI IN TWO ATTEMPTS. COMPLIED WITH MEL. RPL'D APUC.

Part: CONNECTOR — UNSECURE (COCKPIT) · airframe 88,611 hrs · 14,134 cycles

BOTH SIDE WINDOW HEATS INOPERATIVE. SECURED CONNECTOR ON CAPTS SIDE WINDOW, CKS OKAY. F/O SIDE DEFERRED. FAULTS SENSOR 2. RPL'D WINDOW; FOUND SENSOR BAD. ACCMP'D WINDOW HEAT TEST 2RT. WINDOW HEAT TEST FAILS. CONTROLLER MITE SHOWS SENSOR 2 FAULT. PRIMARY SENSOR WIRE HAS INTERMITTENT OPEN AT WINDOW TERMINAL CONNECTOR (COIL HARNESS CONNECTOR). NEED TO SWAP TO SPARE SENSOR WIRE AT TERMINAL BLOCK. ACP SWAP TO SPARE SENSOR ON TB322 FO (PARTIAL). SWAPPED SENSORS, OPS CHECK GOOD.

Part: WINDOW — DEFECTIVE (COCKPIT) · airframe 88,617 hrs · 14,135 cycles

VERY LOUD SQUEALING COMING FROM REAR FIRST OFFICER WINDOW NR 3. LOUDEST SQUEAL & LOUD AIR LEAK COMING FROM BTWN 1ST OFFICER'S WINDOWS 2 & 3. CARRIED OUT INSPECTION OF WINDOWS 2 & 3 ON 1ST OFFICER'S SIDE. BULB SEAL & RETAINER TRACK CLN'D & NO FAULTS EVIDENT. SMALL SECTION OF BULB SEAL AT AFT FACE 6" UP FROM BOTTOM CORNER APPEARS TO HAVE MIGRATED OUT OF CHANNEL FOR APPROX HALF INCH. RESEATED BULB SEAL. WINDOW ASSEMBLY EDGE APPEARS CLEAN & IN GOOD CONDITION. CHK'D OPERATION OF NO2 DIRECT VISION WINDOW & CLOSES & OPENS NORMALLY WITH NO EXCESSIVE FORCE REQUIRED. EXTERNAL INSP CONFIRMS THIS WINDOW IS SEATED NORMALLY. RETORQUED RETAINING BOLTS ON NO3 FIRST OFFICERS WINDOW. RMV'D WINDOW & INSTALLED NEW WINDOW

Part: COMPUTER — FAILED (AUTOPILOT SYS) · airframe 88,589 hrs · 14,132 cycles

CAPTIN FLT DIRECTOR NO ROLL MODE SEL RT FLT DIR ROLL MODE RETURNS NO LAND 3 BOTH POSITIONS. REPLACED LEFT SIDE FLT COMPUTER PER MM. NO LAND 3 ON AUTOLAND STATUS ANNUNCIATOR. REPLACED LEFT FLIGHT CONTROL COMPUTER IAW MM. ACP'D TEST PER MM. GRND CK NORMAL. ACFT RETURNED TO CAT III STATUS.

Part: THRUST REVERSER — DAMAGED (NR 2 ENGINE) · airframe 88,403 hrs · 14,108 cycles

NR 2 ENG LT REVERSER DAMAGED. THREE DAMAGED AREAS, TWO IN SLEEVE ACCOUSTICAL SKIN AND ONE ON INNER BARREL ACCOUSTICAL SKIN, MOST LIKELY DAMAGED FROM PREVIOUS BLOCKER DOOR OR FAIRING DEPARTURE. DENT IN SLEEVE 1.375" X 1.875" X .125" A-Y=11, CREASE IN SLEEVE 11' X .375" X .063" WOULD REQUIRE THRU-BOLTED DOUBLER. GOUGE IN BARREL 2" LONG 80 PERCENT MATERIAL LOSS. ACCMP'D INTERIM REPAIR, RECHECK AT 100HRS AND ACP PERMANENT REPAIR AT CK.

Part: PUMP — FAILED (LT ENGINE) · airframe 87,789 hrs · 14,029 cycles

LEFT ELECTRIC HYDRAULIC PUMP SHOWS NO PRESSURE INDICATED WHEN IN AUTO OR ON, ENGINE RUNNING OR NOT. REPLACED LT ENGINE EDP PRESSURE CASE DRAIN FILTER MODULE PER MM, OPS CK IS NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (STAB TRIM) · airframe 87,663 hrs · 14,013 cycles

STAB TRIM EICAS MESSAGE ON CLIMBOUT. APPEARS TO WORK NORMALLY. NO EICAS MESSAGE PRESENT ON ARRIVAL CHECKED BOTH STAB TRIM AND AILERON LOCKOUT MODULES FOR FAULT BALLS. NONE PRESENT.

Part: MONITOR — FAULTY (HYDRAULIC SYS) · airframe 87,464 hrs · 13,984 cycles

RT HYD SYSTEM FAILURE, RTFL. PERFORMED FIM PROCEDURES IAW FIM29-11-00 INDICATION STILL ZERO SUSPECTED BAD QTY MONITOR OR QTY TRANSMITTER. NO PARTS AT EZEJL CHECKED QTY VISUAL ON RT HYD RESERVOIR SHOWS FULL. NO EXTERNAL INDICATION OF HYD FLUID LOSS. RT RESERVOIR WAS FOUND FULL AND RT PUMP PRESSURE INDICATIONS OPS NORMAL. REPLACED MONITOR IAW AMM. ALL TEST PASSED. SYSTEM WORKS OKAY.

Part: CABLE — BURNED (GALLEY) · airframe 87,239 hrs · 13,952 cycles

NEW TECH CART CABLE P61 PINS BURNT AND PUSHED BACK. REPLACED CABLE PER MM, OP CHECKS OKAY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 87,239 hrs · 13,952 cycles

CENTER AISLE EMERGENCY LIGHT AT MED 1L CLOSET INOPERATIVE. RELAMPED, OP CHECKED GOOD.

Part: BLADE — CRACKED (NR 1 ENGINE) · airframe 86,843 hrs · 13,898 cycles

DURING HFEC INSPECTION FOUND CRACK IN THE MIDSPAN SHROUD ON BLADE NR 1 AND NR 3 IN NR 1 ENGINE. REPLACED NR 1 ENGINE FAN BLADES NR 1 & 19 NR 3 & 21.

Part: SERVO VALVE — LEAKING (NR 2 SPOILER) · airframe 86,670 hrs · 13,866 cycles

NR 2 SPOILER ACTUATOR LEAKING. REPLACED NR 2 SPOILER ELECTRO SERVO VALVE & GASKET PLATE PER MM, LEAK CHECKS OKAY.

Part: COUPLER — FAULTY (HF COMM) · airframe 86,643 hrs · 13,862 cycles

RT HF (NR 2 SYSTEM) TUNES WHENEVER MIC IS KEYED. PLZ RPLC THE ANT COUPLER PER MM. PCN 530-9045, PLZ CHECK WITH ONLINE IPC FOR PROPER EFFECTIVITES. REPLACED RT COUPLER PER MM. CHECKS OKAY. THERE HAVE BEEN 6 WRITEUPS OF SIMILAR OCCURRENCES. SAMC DEFERRED DUE TO NO TIME TO REPLACE HF COUPLER PER LM1684.

Part: ANTENNA — FAILED (WX RADAR SYS) · airframe 86,334 hrs · 13,818 cycles

WXR FAIL ON EHSI, FLT DIVERTED. WHEN TEST SELECTED, "ANT RT" DISPLAYED UNDER WX RADAR FAIL ON ESHI. RESET WX RADAR CB GRID F2, NO HELP. ALSO TRIED PWS OFF, TILT IN MAN OR AUTO, GAIN IN AUTO OR MAX, ALL NO HELP. FOUND ANTENNA FAILURE AFTER TRANSCEIVER BITE PROCEDURE FOUND ANTENNA FAILURE. REPLACED ANTENNA.

Part: BATTERY — FAULTED (EMERGENCY LIGHTS) · airframe 86,093 hrs · 13,782 cycles

A CABIN APPEARANCE TEAM FOUND DURING AN INTERIOR SWEEP 2 EMERGENCY EXIT LIGHTS INOP AT DOORS 2L AND R. REPLACED BATTERY AND CHARGER ASSY PER MM, LAMPS OP NORMAL.

Part: PRESSURE SWITCH — FAULTED (STAB TRIM) · airframe 86,041 hrs · 13,773 cycles

RIGHT AUTOPILOT INOP DUE TO RIGHT STABILIZER TRIM CHANNEL FAULT. REPLACED PRESSURE SWITCH ON RT STCM.

Part: MODULE — MALFUNCTIONED (LT STAB TRIM) · airframe 86,041 hrs · 13,773 cycles

STABILIZER TRIM EICAS WITH ASSOCIATED TRIM LIGHT ILLUMINATED. ACCOMPLISHED CK OF STABILIZER TRIM SYSTEM AND FOUND LEFT CHANNEL FAULT. LEFT SAM SHOWED STCM AND PRESS SWITCH FAULTS. RESET BOTH SAMS, NO HELP. ALSO REPLACED LEFT SAM NO HELP. LEFT NEW UNIT INSTALLED. MR22167-92 OFF, -17 ON, IN LEFT POSITION. FOUND LEFT SAM FAILED, REPLACED LEFT SAM, NO OTHER FAULTS INDICATED. LEFT SYSTEM FUNCTIONS NORMAL.

Part: MODULE — FAULTY (AILERONS) · airframe 85,904 hrs · 13,753 cycles

AILERON LOCKOUT EICAS, RTFL. REPLACED R FCC PER MM. PERFORMED SATISFACTORY CAT III CHECK PER MM22-10-00. REPLACED RT STAB TRIM AILERON LOCK MODULE. SYSTEM CHECKS OK AT THIS TIME. MESSAGE CLEARED. ACFT RETURNED TO CAT III SERVICE.

Part: CONTROL VALVE — FAULTY (AC BAY) · airframe 85,903 hrs · 13,752 cycles

DURING BITE TEST OF LEFT PACK CONTROLLER TEMP CONTROL VALVE LIGHT ILLUMINATED. REPLACED LEFT PACK TEMP CONTROL VALVE, OPS CHECK NORMAL.

Part: ACTUATOR — LEAKING (AILERON) · airframe 85,903 hrs · 13,752 cycles

HYD LEAK AT RT OUTBOARD AILERON. REPLACE OUTBOARD AILERON INBOARD ACTUATOR. NEED TO COMPLETE INSTALLATION OF NEW ACTUATOR (INBOARD POSITION). BEGIN AT MM. REPLACED ACTUATOR IAW MM.

Part: HEAT EXCHANGER — DAMAGED (AC BAY) · airframe 85,903 hrs · 13,752 cycles

LT PACK SECONDARY HEAT EXCHANGER BOTTOM FWD END HAS PIECE BROKEN OFF. STARTED HEAT EXCHANGER CHANGE. STOPPED AT STEP (F). REMOVED PRIMARY, SECONDARY HEAT EXCHANGERS AND PLENUM FOR ACM AS AN ASSEMBLY. NEED TO COMPLETE INSTALLATION. ACCOMPLISHED UP TO AND INCLUDING PAR 3F(2)D. COMPLETED INSTALLATION. OPS CHECK NORMAL.

Part: CONTROL VALVE — FAULTY (AC BAY) · airframe 85,903 hrs · 13,752 cycles

RT PACK TRIPPED ON TAKEOFF ROLL. REPLACED PACK CONTROLLER ALSO FOUND HOT AIR OUTLET B-NUT LOOSE, SECURED NUT AND GROUND CHECK NORMAL. RT PACK TRIPPED AGAIN ON TAXI OUT. ACCOMPLISHED BITE TEST REF MM. REPLACED 490 DEG SWITCH. UNABLE TO RUN PACK DUE TO OTHER WORK ON A/C NEEDS OPS CHECK. RAN NR 2 ENGINE PACK OFF LIGHT. ILLUMINATES AS SOON AS NR 2 THROTTLE IS ADVANCED. TRIED NEW FLOW CONTROL LOGIC CARD, NO HELP. OPS CHECKS GOOD. RT PACK OUTLET TEMP INDICATING MINUS TEMPS WHEN OPERATED ON ENGINE BLEEDS AT FLT IDLE AND ABOVE. REPLACED PACK OUTLET TEMP BULB IAW MM, NO HELP. RPL'D RIGHT PACK TEMP CONTROL VALVE. RPLC'D RT FLOW CONTROL VALVE FOR T-S PER MM (P/N 396462-2; SERIAL 74). OPS CHECKS GOOD.

Part: UNKNOWN — MALFUNCTIONED (AC BAY) · airframe 85,724 hrs · 13,715 cycles

R PACK OFF LIGHT WITH ENGINE POWER PUSHED TO TAKEOFF. OFF LIGHT GOES OUT WITH POWER REDUCED. SAMC TEXT: FAULT OCCURRED TWICE ON TAKEOFF ROLL. ABORT WAS AT VERY SLOW SPEED, 20KTS. PER CREW PACK OFF AT 1.1 EPR SETTING. ACCOMPLISH HIGH PWR ENG RUN PER JRH TO 1.3 EPR FOR 5 MINUTES, ALL BLEED & PACK PARAMETERS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,503 hrs · 13,683 cycles

INTERIOR EMERGENCY CEILING LIGHT INOP ABOVE SEAT ROW 32AB. REPLACED LAMP, CHECKED, OKAY.

Part: BEARING — LOOSE (NLG DOOR) · airframe 85,466 hrs · 13,678 cycles

LT AFT NOSE GEAR DOOR LOOSE AT AFT ATTACH POINT. REMOVED DOOR. REPLACED AFT DOOR MOUNT BEARING PER GNMM. RE-INSTALLED PER MM.

Part: TUBE — LEAKING (FUEL PUMP) · airframe 85,268 hrs · 13,643 cycles

FUEL TRANSFERING FROM RT TANK TO CENTER APPROX 400LBS-HR. FOUND CRACKED FUEL FEED 'WYE' AT OUTPUT OF RIGHT OVERRIDE PUMP IN CENTER TANK. TUBE WAS TEMP REPAIRED. PUMP OPS CHECKED AND LEAK CHECKED GOOD. Y SUPPLY PIPE OFF RT CENTER TANK BOOST PUMP HOUSING REMOVED. DYE PENETRANT INSPECTED PER DWG, NO CRACKS NOTED AFTER WELD REPAIR.

Part: PANEL — DAMAGED (COCKPIT) · airframe 85,174 hrs · 13,628 cycles

THE "A" PILLAR BETWEEN FWD WINDSHIELD & SLIDING WINDOW IS COMING APART BY HANDLE PRODUCING SHARPNESS. THE "A" PILLAR PADDING AT HANDLE IS DAMAGED AND FOAM IS EXPOSED, INTERIM REPAIR WITH TAPE PADDING IS SERVICEABLE. REPLACED CO-PILOT PANEL.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 84,991 hrs · 13,603 cycles

LT AFT CABIN FLOOR EEL LIGHT INOP AFT OF ROW 39AB, IN FRONT OF LAV. RECONNECTED EEL STRIP, CHECKS GOOD.

Part: EXCITER — DAMAGED (NR 1 ENGINE) · airframe 84,991 hrs · 13,603 cycles

NR 1 ENG EXCITER A HAS CARBON TRACK INSIDE SLEEVE AND IGNITER CABLE SLEEVE IS CRACKED. REPLACED EXCITER.

Part: ACTUATOR — LEAKING (RUDDER) · airframe 84,926 hrs · 13,595 cycles

DURING ETOPS PRE-DEPARTURE CHECK FOUND HYDRAULIC LEAK COMING FROM VERTICAL FIN. SUSPECT LEAK COMING FROM RUDDER ACTUATORS. FOUND HYDRAULIC LEAK COMING FROM CENTER RUDDER PCA ACTUATOR. FOUND LEAK WITHIN LIMITS AS PER AMM. LT HYD SYSTEM SERVICED TO FULL.

Part: OXYGEN MASK — CRACKED (OXYGEN SYSTEM) · airframe 84,782 hrs · 13,573 cycles

OXYGEN MASK 2L NEEDS TO BE REPLACED, IT IS CRACKED. REPLACED MASK.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 84,775 hrs · 13,571 cycles

EMERGENCY LIGHTS FLASHING ON AND OFF DURING ENTIRE FLIGHT. UNABLE TO DUPLICATE FLASHING EMERGENCY LIGHTS. REPLACED POWER SUPPLY M1561 AT STA 1362 PER MM. LIGHTS OP CHECKED OKAY.

Part: VALVE — FAULTY (BLEED AIR SYS) · airframe 84,714 hrs · 13,561 cycles

RT DUCT PRESS FLUCTUATES-SURGING DURING CLIMB FROM 15-35 PSI. CHRONIC HPSOV VALVE IS SEC CLOSED. REPLACED PRV REPLACED PRECOOLER CONTROLLER. OPS CHECKS OK. NO FAULTS. RE-ACTIVATED HP VALVE.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 84,443 hrs · 13,517 cycles

EMERGENCY LIGHTS FLICK ON & OFF AT 2L. ACCOMPLISHED OPS TEST IAW MM. SYS PASSED OK. NO FAULTS FOUND OR HISTORY NOTED.

Part: CONTROLLER — FAULTY (CABIN TEMP) · airframe 84,315 hrs · 13,497 cycles

CREW REPORTED PACKS IN AUTO, MID AND FWD CAB TEMP EICAS MESSAGES WITH INOP LIGHTS. TURNING OFF TRIM AIR HAD NO AFFECT ON CABIN TEMPS. PLACED PACKS IN STBY "N". TEMPS STILL FLUCTUATED. PLACED LT PACK BACK IN AUTO, PACK TRIPPED DUE TO OVERHEAT, RESET PACK. CAN ONLY CONTROL TEMPS BY SWITCHING BETWEEN STBY "N","C" AND "W". CREW REPORTED TEMPS STABILIZED SOMEWHAT IN STBY "W". REPLACED FAIL AUX PACK CONTROLLER IAW MM, OPS CHECK STATUS NORMAL. ALSO CLEANED ALL ZONE TEMP FILTERS.

Part: GUIDE VANE — DELAMINATED (RT ENGINE) · airframe 84,247 hrs · 13,488 cycles

RT ENG 6 O'CLOCK FAN EXIT GUIDE VANE DELAMINATED. REMOVED EXIT GUIDE VANE AS PER MM. APPLIED SEALANT AND SPEED TAPE AS REQUIRED.

Part: SENSOR — FAULTY (FWD LAVATORY) · airframe 84,186 hrs · 13,481 cycles

FWD WASTE TANK FAILURES. DUE TO NUMEROUS LAV FAILURES IN FLIGHT PLEASE COMPLETE THE FOLLOWING CALLOUT BEFORE FURTHER REVENUE FLIGHT. REPLACE BOTH POINT LEVEL SENSORS ON THE FWD WASTE TANK CHECK ALL CONNECTORS AND WIRES ASSOCIATED WITH THE WASTE TANK LEVEL SENSORS AND REPAIR AS NEEDED. REPLACED THE LOGIC CONTROL UNIT FOR THE FWD WASTE TANK AND CHECK ALL CONNECTORS AND WIRING ASSOCIATED WITH THE LOGIC CONTROL UNIT. REPLACED BOTH SENSORS AND LCU IAW MM. REPLACED AFT TANK LCM, CHECKS OKAY

Part: ANTI-ICE VALVE — FAULTY (RT ENGINE) · airframe 84,186 hrs · 13,481 cycles

RT ENG ANTI-ICE VALVE LIGHT ILLUMINATED WITH SWITCH OFF. REPLACED RT ENG ANTI-ICE VALVE IAW MM.

Part: STOWAGE BOX — FAULTY (COCKPIT) · airframe 84,044 hrs · 13,462 cycles

CAPTS O2 MASK MIKE INOPERATIVE. ROBBED SECOND OBSERVER O2 COMPARTMENT BOX FOR CAPT SIDE. BAD BOX IS AT SEAT BEHIND CAPTAIN. WIRES ARE DAMAGED AT CONNECTOR ON BOX. BOX ASSY (PCN 649-0001) ON AOG U6179. REPLACED O2 BOX, TESTED OKAY.

Part: WIRE — DAMAGED (HYDRAULIC SYS) · airframe 84,032 hrs · 13,459 cycles

CREW REPORTS RT HYD DEMAND PUMP EICAS MSG ALONG WITH RT DEM PUMP OVERHEAT LIGHT ILLUMINATED. SUPPLEMENTAL DATA UPDATE, CREW TURNED PUMP OFF PER IRREG PROCEDURE. ACCOMPLISHED FIM 29-11-00 FIG 119. FOUND SHORT TO GROUND BETWEEN D922 PIN 3 AND D4054J PIN 38. WHEN SHAKING WIRING AT FWD SAILBOAT AREA WIRE WOULD GO INTERMITTENTLY TO GRND. FOUND DAMAGED INSULATION NEXT TO UPPER FWD CLAMP. REPAIRED WIRING PER GNMM AND SHAKE CHECK OKAY. PUMP OPS AND MSG NORMAL.

Part: COUPLER — FAULTY (HF COMMS) · airframe 83,909 hrs · 13,440 cycles

RIGHT HF COMMUNICATION SYSTEM INOPERATIVE. DEFERRED PER SAMC. REPLACED FIRST OFFICER’S AUDIO SELECT PANEL. UNABLE TO TRANSMIT OR RECEIVE ON R-HF. POSSIBLE HF COUPLER M242 (530-9045). WILL NEED A 2 SHIFT SLOT FOR THE COUPLER CHANGE. TWO RT HF TRANSCEIVERS ALREADY REPLACED IN DEC. REQUESTED 2 SHIFT SLOT FOR COUPLER REPLACED. REPLACED HF COUPLER PER MM. SYSTEM CHECKS OK ON GROUND.

Part: LIGHT — FAULTY (AUDIO PANEL) · airframe 83,909 hrs · 13,440 cycles

FIRST OFFICER’S AUDIO PANEL BACK LIGHTING INOP. REPLACED FIRST OFFICER’S AUDIO SELECT PANEL, OP CHECKS GOOD.

Part: HEAT EXCHANGER — CRACKED (LT A/C PACK) · airframe 83,762 hrs · 13,420 cycles

LEFT PACK MAKING LOUD NOIS. FOUND CRACK ON PRIMARY HEAT EXCHANGER MEASURES APPX 4" LONG BY 2" WIDE. REMOVED HEAT EXCHANGER AND PLENUM ASSEMBLY. REPLACED LT PACK PRIMARY HEAT EXCHANGER AIAW MM. SYSTEM OPS NORMAL WITH NO LEAKS DETECTED.

Part: PRIORITY VALVE — FAULTY (RT ENGINE) · airframe 83,668 hrs · 13,405 cycles

RT ENG PRV EICAS AND BLEED LIGHT ON OVERHEAD WHEN 2 ENG SHUTDOWN. COULD NOT CLOSE THE PRIORITY VALVE. REPLACED IAW MM. OPS CHECK OK.

Part: OIL TANK — DAMAGED (RT ENGINE) · airframe 82,782 hrs · 13,277 cycles

RIGHT ENGINE MAIN OIL TANK SMASHED IN AT AFT LOWER SIDE OF TANK. ROUTED AND SECURED WIRING ABOVE OIL TANK. COMPLETED SECURING OF WIRE BUNDLE.

Part: B-NUT — LOOSE (THRUST REVERSER) · airframe 82,782 hrs · 13,277 cycles

NR 2 ENGINE OTBD REVERSER LOCKING ACTUATOR (CTR) LEAKING HYD FLUID. REPLACED LEAKING SEAL AND TIGHTENED LOOSE B-NUT. OPS CK IAW MM, NO LEAKS NOTED.

Part: SENSOR — FAILED (COCKPIT) · airframe 82,641 hrs · 13,256 cycles

FLAP EICAS WARNING MESSAGE / NOSE A-G DISAGREE STATUS MESSAGE ALSO DISPLAYED, FLIGHT DIVERTED. FOUND S266 SENSOR FAILED. REPLACED TESTED OKAY.

Part: FAIRING — MISSING (THRUSTE REVERSER) · airframe 82,592 hrs · 13,248 cycles

RT ENGINE OUTBOARD REVERSER HAS A PIECE OF MISSING FAIRING. FAIRING IS LOCATED AFT OF LOWER BLOCKER DOOR (5:30 O'CLOCK) AND MISSING PIECE IS 6.5 INCH LONG BY 2 INCH WIDE. REQUIRES PERMANENT REPAIR, PICTURES ON RVI WEB SITE. DEFERRED REVERSER INOP. APPLIED SPEED TAPE REPAIR PER MM. REAPPLIED TAPE TO AREA. IPC NOT CLEAR ON PANEL ID. POSSIBLE PART PCN 181-7618 REF IPC. FAIRING REPAIRED AND REPLACED FAIRING. FAIRING IS SECURED. REINSTALLED LOWER BLOCKER DOOR. REACTIVATED NR 2 REVERSER, NR 2 THRUST REVERSER OPS CK'S GOOD.

Part: BRAKE — FIRE (NR 2) · airframe 82,012 hrs · 13,166 cycles

NR2 FWD BRAKE FAILED ON LANDING. AFTER SLIDE DEPLOYMENT AT DOOR 1R, REMOVED SLIDE ASSY AND CLOSED DOOR. REPLACED SLIDE-RAFT AT DOOR 1R. ALSO REPLACED BRAKE. OPS NORMAL.

Part: FUEL LINE — DAMAGED (NR 2 ENGINE) · airframe 81,944 hrs · 13,156 cycles

NR 2 ENGINE FUEL LINE FROM FUEL-OIL COOLER 'FUEL OUT' LINE TO FUEL PUMP INSULATION DAMAGED. REMOVED FUEL LINE. COMPLETED INSTALLATION, LEAK CHECKED GOOD. REPLACED FUEL PUMP. OPS & LEAK CHECKED GOOD.

Part: LOCKOUT — MALFUNCTIONED (STAB TRIM) · airframe 81,888 hrs · 13,146 cycles

L FMC FAILURE & STAB TRIM EICAS, RTFL. STAB TRIM LIGHT ON O/H AS WELL AS EICAS MESSAGE. REPLACED STAB TRIM - AILERON LOCKOUT MODULE. ACP MCDP TEST 65. TEST OK. ACCOMPLISHED STAB TRIM CONTROL OPS TEST IAW MM. ALL TESTS PASSED.

Part: SELECTOR PANEL — MALFUNCTIONED (NR 1) · airframe 42,462 hrs · 11,748 cycles

LOWER EICAS TURNED PINK IN DESCENT. POSSIBLE PART "PANEL EICAS CONTROL". REPLACED EICAS DISPLAY SELECT PANEL, OPS CHECK ABOUT 3 HOURS, NO FAULTS & DISPLAY COLORS NORMAL.

Part: RELAY — DEFECTIVE (ELECTRICAL SYS) · airframe 81,752 hrs · 13,123 cycles

Y PWR AFTER TAKEOFF CYCLED UTIL BUSSES AND POWER RESTORED. REPLACED AIR-GND TIME DELAY RELAYS M1164 & M1163 WDM. ALSO SWAPPED ELEC SYS PNL ON P5 M10063 WITH ACFT 6457. ACP LOAD SHED CHECK GRND CHECKED NORMAL.

Part: PIN — BENT (GALLEY CONNECTOR) · airframe 81,733 hrs · 13,118 cycles

LOSS OF GALLEY POWER. REPLACED THE RT ENGINE GENERATOR CIRCUIT BREAKER, NO HELP. REPLACED RELAY K101 & K103 AS A PRECAUTION. FOUND BENT PIN IN CONNECTOR D4034P PIN 25. STRAIGHTEN PIN-WIRE W018-069-22, CHECKS GOOD FROM M116 BUSS POWER CONTROL UNIT M116 CONNECTOR D278B C12 TO D4034P PIN 25. PROBLEM WITH GALLEY LOAD SHED. HISTORY INDICATES IT HAPPENS AFTER TAKEOFF. ON GROUND, GALLEY SHED SHIFTED FROM GROUND POWER TO APU POWER. UTILITY BUSS RESET WITH UTILITY BUSS SWITCHES NORMAL IN CONFIGURATION NOTED. CONCURS WITH INFORMATION IN MM. NO FURTHER ACTION REQUIRED.

Part: MODULE — FAULTY (BLEED AIR SYS) · airframe 81,733 hrs · 13,118 cycles

LEFT ENG DUCT LEAK LIGHT CAME ON, ON TAXI. REPLACED THE AIR SUPPLY BITE MODULE IAW MM. ACCOMPLISHED LEAK CHECK IAW MM.

Part: HOSE — DISCONNECTED (A/C PACK) · airframe 81,686 hrs · 13,110 cycles

LT PACK BLEED LEAK LIGHT ON WITH LT PACK ON. LT ENG BLEED OFF. FOUND HOLE IN HOSE OFF ACM DUCT REPLACED.

Part: WINDOW — LEAKING (COCKPIT) · airframe 81,686 hrs · 13,110 cycles

CAPT SLIDING WINDOW LEAK. HISSING LEAK ONLY BECAME EVIDENT AT 7.0 PSI DIFF PRESSURE. AREA OF HISSING COMING FROM AREA AROUND WINDOW LOCK LATCH HANDLE. CONFIRMED WITH AMT'S THAT PERFORMED INITIAL PRESSURE TEST A TYPO WAS MADE REGARDING PRESSURE READING DURING TEST. MAX PRESSURE ACHIEVED WAS 3.5 AND WINDOW HISSING BEGAN AT 3.0 PSI. REPLACED WINDOW ASSY & PRESSURIZED TO 4 PSI, NO NOISE.

Part: RELAY — FAILED (GALLEY POWER) · airframe 81,546 hrs · 13,090 cycles

NO GALLEY POWER IN FIRST AND COACH AFTER TAKEOFF. CYCLING RT UTILITY BUS RESTORES POWER. RPLCD RELAY K10109. REPLACED BPCU. ALSO REPLACED ELCU M225 AND M226, TESTS OKAY.

Part: RECEPTACLE — DAMAGED (GROUND POWER) · airframe 81,435 hrs · 13,071 cycles

RAMP PERSONNEL REPORTS GND POWER RECEPTACLE APPEARS DAMAGED. EXT POWER PINS WERE SEVERELY BENT AND TOUCHING THE ALIGNMENT SHROUD. STRAIGHTENED PINS AS BEST AS POSSIBLE. MAY NOT BE USEABLE AT NEXT STATION. RAMP SVC UNABLE TO CONNECT EXT PWR IN SFO DUE TO BENT PINS. IF PINS ARE STRAIGHT ENOUGH RECEPTACLE MAY BE USABLE AND THIS ITEM SIGNED OFF. PANEL DOOR WAS ALSO BENT AND NEEDS STRAIGHTENING. GOT PINS STRAIGHT, GROUND POWER IS WORKING, TRIED STRAIGHTENING DOOR, STILL NEEDS MORE HELP OR POSSIBLY NEW DOOR.STRAIGHTENED DOOR, DOOR CHECKS, FLUSH AND TIGHT.

Part: SEAL — LEAKING (NR2 WINDOW ASSY) · airframe 81,405 hrs · 13,064 cycles

NR 2 WINDOW ASSY AIR LEAKS (NOISY) POSITION 2 (2=2L ,5=2R). INTERIM REPAIR IAW MM. APPLIED TAPE TO WINDOW, NEED TO ACCOMPLISH PERMANENT REPAIR IAW AMM AT FIRST AVAILABLE MX OPPORTUNITY. OK IAW SAMC. REPLACED PRESSURE SEAL. OP CHK'D NORMAL.

Part: HANDLE — OUT OF RIG (COCKPIT WINDOW) · airframe 81,343 hrs · 13,056 cycles

CAPT WINDOW LEAK & SQUEAL IS LOUD & EXTREMELY DISTRACTING. NOISE COMING FROM STOWAGE HANDLE. RIGGED LOWER LINK ARM ASSY. ALSO FAYING SEALANT WAS APPLIED TO ENTIRE SEAL, PRESSURIZED ACFT AND NO LEAKS. CK'D ALL OTHER RIGS AND ALL FELL INTO LIMITS.

Part: BULB — FAULTY (EMERGENCY LIGHTS) · airframe 81,335 hrs · 13,055 cycles

EXIT PATH LIGHT FLICKERING AT DOOR 1L. SECURED BULB, OPS CHK NORMAL.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHTS) · airframe 81,328 hrs · 13,054 cycles

EMERGENCY EXIT FLOOR STRIPS AND EXIT LIGHT AT DOOR 1L ON INTERMITTANTLY WITH SW IN ARM. CLEANED POWER SUPPLY CONNECTOR M1208, OPS CKS GOOD.

Part: ACTUATOR — LEAKING (NLG STEERING) · airframe 81,326 hrs · 13,053 cycles

RT NOSE WHEEL STEERING ACTUATOR LEAKING. REPLACED RT NOSE WHEEL STEERING ACTUATOR. OPS CHECKED AND LEAK CHECKED. OPS CHECKED GOOD AND NO LEAKAGE NOTICED.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 81,326 hrs · 13,053 cycles

SEVERAL EXT EMERGENCY EXIT LIGHTS INOP ON TEST. RELAMPED LIGHT ASSY AT FWD ENTRY DOOR & REPLACED BATTERY CHARGER AT POSITION M737. OPS CHECKED GOOD

Part: GENERATOR — FAULTY (APU) · airframe 81,314 hrs · 13,051 cycles

APU SHUTSDOWN. NO FAULT LIGHT. NO ABNORMAL INDICATIONS. IAW T-S REPLACED APU FLOW SENSITIVE MODULE, NO HELP. REPLACED GCU IAW AMM, NO HELP. REPLACED BPCU IAW AMM, NO HELP. RESTORED ORIGINAL UNIT. CKD GEN FEEDERS AND LUGS. ALL OK. RUN APU WITH 70 PERCENT OF LOAD FOR 30 MINUTES THEN DROP OFF LINE TRIED TO RECONNECT SHOW APU FIELD OPEN MOMENTARY WHILE TRIED TO RECONNECT APU GEN. R & R APU GENERATOR IAW MM. OPS CHECKS NORMAL. RESET SYS CRANK APU WITH NO FAULTS. REPLACED LOW OIL TEMP SWITCH AND STARTED SEVERAL TIMES, OPS CKS NORMAL.

Part: INDICATOR — FAULTY (FUEL QTY) · airframe 80,432 hrs · 12,922 cycles

O-H FUEL PANEL-FUEL TEMP INOPERATIVE. REPLACED OVERHEAD FUEL QUANTITY PANEL. ACCOMPLISHED FUEL QUANTITY BITE CHECK.

Part: PRESSURE SWITCH — UNKNOWN (UNKNOWN) · airframe 80,179 hrs · 12,886 cycles

PUMP OFF AND LP LGT ON BUT NO EICAS MSG. TRIED S72 PRESSURE SWITCH NO HELP, TRIED OVERHEAD PANEL, NO HELP, REPLACED K190 CONTROL RELAY NO HELP. ISOLATED CIRCUIT BETWEEN S5 TO S72 & BOTH EICAS CMPTS, WIRES CHKS OK. REF FIM 28-22-00 FIG 111 BOX 2, 28VDC PRESENT, ACP'D BOX 24, NO HELP, NEED MORE TROUBLESHOOTING. R & R FWD BOOST PUMP PRESS SWITCH S72. RT WW FWD OF MLG BULKHEAD, FUEL LEAKING FROM B-NUT OF HEAT EXCHANGER LINE HAVE A RUNNING LEAK. CLEANED OUT OLD SEALANT & RESEAL WITH 12 HOUR CURE TIME. RT WW FWD OF GEAR BULKHEAD SEALED, 2 EA KINKED FUEL LINES. BOTH LINES INSTALLED. NEEDS TANK CLOSE-UP & LK CHKS. ACCOMPLISHED CLOSEUP & LK CHK OF RT MAIN FUEL TANK.

Part: LIGHT — DAMAGED (SEAT 8B) · airframe 79,613 hrs · 12,806 cycles

SEAT MOUNTED EMERGENCY LIGHT DISCONNECTED AND WIRES STOWED DUE TO INCOMPLETE REPAIR OF FOOT REST AT SEAT 8B. REPAIRED DISCONNECTED WIRES. LIGHT TESTS NORMAL.

Part: DUCT — RUPTURED (ANTI-ICE SYSTEM) · airframe 79,255 hrs · 12,754 cycles

ON ARRIVAL FOUND WING ANTI ICE BLOW OUT PNL DISINTEGRATED AT THE LT WING STA 523AT. FURTHER T-S SHOWED COMPOSITE DUCT RUPTURED AT STA 523 AT JOINING METAL DUCT. REPLACED TAI DUCT. DISCONNECTED AND RECONNECTED SLAT CONTROL ROD AT BOTH ENDS OF SLAT NR 4. ACCOMPLISHED RII INSPECTION PER METHOD 1 ON INSTALLATION AND OPERATION OF SLAT NR 4, ALL OPS AND IND NORMAL. RECONNECTED AND LEAK CHECKED WING ANTI ICE DUCTS (INTERSTITIAL DUCTS). OK FOR SVC.

Part: ANTI-ICE VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 79,205 hrs · 12,746 cycles

EICAS MSG ENG ANTI-ICE DISPLAYED AND ENG ANTI-ICE VALVE LIGHT REMAINED ILLUM WITH SWITCH ON, POSITION 2. CREW COMMENTS: AFTER ENG START HAD TO CYCLE SWITCH SEVERAL TIMES AND BOOST POWER TO EXTINGUISH REPEAT. REPLACED NR 2 ENGINE ANTI-ICE VALVE, RAN ENGINE. NO STATUS MESSAGES AND OPS CHECKED GOOD.

Part: SEALANT — DAMAGED (CENTER TANK) · airframe 78,984 hrs · 12,708 cycles

FUEL LEAK FROM L PACK BAY AT 20DPM. CENTER FUEL TANK UNDER PANEL 193PL LT WING TO BODY FAIRING STATION 955.10 REAR SPAR CENTER TANK FASTENERS LEAKING. FOUND LEAK AT AFT SPAR BELOW AND JUST FWD OF LOWER LEFT BATHTUB FITTING. FOUND INTERNAL LEAK, REMOVED DAMAGED SEALANT AND RESEALED. LEAK CHECK OF AREA IS OKAY.

Part: WIRE — SPARKS (GALLEY CART) · airframe 78,561 hrs · 12,639 cycles

AFT GALLEY PIGTAIL P51 SPARKED WHEN REMOVED & C/B POPPED OUT. P51 PIGTAIL REPLACED. GALLEY CART OPS CHECK OKAY.

Part: POTABLE WATER — EMPTY · airframe 78,403 hrs · 12,618 cycles

NO WATER QUANTITY AND PRESSURE, RTFL. SHORTLY AFTER DEPARTURE, CREW NOTIFIED CHIDD AND SAM THAT THE POTABLE WATER SYSTEM APPEARED TO BE EMPTY. MAINT CONFIRMED NO WATER IN MID LAVS-GALLEYS AND AFT LAVS-GALLEYS. WATER QTY IND RESERVICED WATER AND BLED SYSTEM. CHECKED FOR LEAKS AND NONE FOUND. CONFIRMED WATER FLOW AT ALL POSITIONS AND QTY INDICATOR STEADY AT FULL.

Part: CONTROL PANEL — FAULTY (AUDIO SYSTEM) · airframe 78,304 hrs · 12,598 cycles

NR 1 AUDIO SELECTOR PANEL LIGHTING FAULTY. CREW COMMENTS: LIGHTS ON ALL SELECTOR SWITCHES ON CAPTS VHF PANEL ARE INOP. 2ND OBSERVER FLIGHT & SERVICE INTERPHONE SWITCHES INOP. FLT INTERPHONE FROM FRONT TO COCKPIT DOES NOT WORK. REPLACED CAPT AUDIO SELECTOR PANEL, OPS CHECK GOOD.

Part: PANEL — DAMAGED (LE SLAT) · airframe 77,738 hrs · 12,507 cycles

RIGHT SIDE WING LEADING EDGE SLAT NR 12 LINKAGE FAIRING PANEL NR 24 DAMAGED. SLATS OPERATE NORMALLY. PANEL REMOVED AND PLACED IN LOB BOX. REMOVED AND REPLACED SLAT NR 12 LINKAGE PANEL.

Part: COMPUTER — FAULTY (RT EICAS) · airframe 77,718 hrs · 12,505 cycles

RIGHT EICAS COMPUTER INOPERATIVE. REPLACED RT EICAS COMPUTER.

Part: VALVE — FAILED (FUEL SYSTEM) · airframe 76,674 hrs · 12,348 cycles

FUEL CONFIG MESSAGE. FLIGHT DIVERTED. REPLACED CHECK VALVE ASSEMBLY. NO UNWANTED FUEL TRANSFER NOTED.

Part: PUMP — FAULTY (FUEL SYSTEM) · airframe 76,667 hrs · 12,347 cycles

FUEL IMBALANCE. FLIGHT DIVERTED. FUEL CONFIG LIGHT ILLUMINATED DUE MORE THAN 2000 POUNDS DIFFERENCE BETWEEN RT AND LT MAIN TANKS WHILST FEEDING FROM THE CENTRE TANKS. CHKD STICK READINGS VERSES GAUGES-NO DISCREPANCY FOUND, PROCESSOR NO FAULTS OPS CHK PUMP IND ALL OK, INDICATION SYSTEM GOOD, REPLACED OVERRIDE PUMP WITH KNOWN GOOD PUMP FROM RT JETT PUMP POS. REPLACED JETT PUMP WITH NEW ITEM DURING REPLACEMENT RT JETTISON PUMP SLEEVE AS TWO WINDOW TYPE THEREFORE INSTALLED FUEL PUMP P/N 5006286F. OVERRIDE PUMP SLEEVE NOTED AS 4 WINDOW TYPE AND INSTALLED 5006286D PUMP. ACP'D OPS CHECKS OF BOTH PUMPS AND ALL GOOD. ACP'D CROSSFEED CHECK AND ALL GOOD.

Part: INDICATOR — FLUCTUATES (FUEL QTY) · airframe 76,542 hrs · 12,326 cycles

FUEL QTY INDICATORS FLUCTUATING. RTFL. REPLACED FUEL QTY PROCESSOR. REPLACED COCKPIT FUEL QTY INDICATION PANEL. PERFORMED BITE. CHECKED OK.

Part: ASPIRATOR — LEAKING (EVAC SLIDE) · airframe 76,069 hrs · 12,259 cycles

SLIDE ASPIRATOR BARREL LEAKING. CAUSE IS UNKNOWN. REPLACED ASPIRATOR.

Part: OXYGEN SYSTEM — LOW PRESSURE (CREW O2) · airframe 75,959 hrs · 12,244 cycles

CREW OXYGEN PRESSURE BELOW 3SVC LIMITS (1.610 PSI). SERVICED CREW OXYGEN SYSTEM. OP CHECKS OKAY.

Part: OXYGEN SYSTEM — LOW PRESSURE (CREW O2) · airframe 75,959 hrs · 12,244 cycles

CREW OXYGEN PRESSURE BELOW 3SVC LIMITS (1.610 PSI). SERVICED CREW OXYGEN SYSTEM. OP CHECKS OKAY.

Part: PUMP — FAULTY (RIGHT) · airframe 75,379 hrs · 12,168 cycles

ONE HOUR AFTER TAKEOFF, FUEL CONFIG LIGHT WITH RT TANK 4000 LBS LESS THAN LT. REPLACED RT FUEL OVERRIDE PUMP. OPS CHECK GOOD.

Part: O-RING — DAMAGED (EVAC SLIDE)

LOW BOTTLE PRESSURE. LEAKING AROUND GAUGE ADAPTER. R&R O-RING.

Part: O-RING — UNSERVICEABLE (SLIDE INDICATOR)

LOW BOTTLE PRESSURE. LEAKING AROUND GAUGE ADAPTER. R & R O-RING.

Part: HYDRAULIC LINE — LEAKING (AILERON PCU) · airframe 75,196 hrs · 12,144 cycles

HYD LEAK FROM LT OTBD AILERON PCU HYD LINE. TUBE REPAIRED WITH FITTING. LEAK CHECK ACCOMPLISHED. LT HYD SYS SERVICED TO GREEN BAND.

Part: OVEN — CONTAMINATED (GALLEY) · airframe 75,156 hrs · 12,139 cycles

ELECTRICAL ODOR IN CABIN. FLIGHT DIVERTED. DOOR AREA HEATER CB PULLED R12 ON OVERHEAD P11 PANEL TO SEE IF ODOR GOES AWAY. THERE IS NO SIGN OF ANY SMOKE. REPLACED RT AFT DOOR HEATER. WARMING OVEN DIRECTLY BELOW W51 HAD MELTED PLASTIC INSIDE CAUSING BURNED ODOR IN AFT GALLEY. CLEANED OUT OVEN AND RAN FOR SEVERAL HOURS. CHECKS OK. REPLACED OVEN.

Part: OVEN — ODOR (FWD GALLEY) · airframe 75,105 hrs · 12,133 cycles

ELECTRICAL ODOR REPORTED IN AFT GALLEY. NO ODOR WITH GALLEY POWER OFF. CHECKED IN CEILING ABOVE AFT GALLEY ALL OK. FOUND WARMING OVEN W51 HAD MELTED PLASTIC INSIDE AND STRONG BURNED ODOR. CLEANED OVEN. RAN FOR SEVERAL HOURS. CHECKED OK.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 75,062 hrs · 12,127 cycles

DOOR 1R PRESSURE GAUGE IS BELOW THE GREEN BAND. REPLACED SLIDE.

Part: SWITCH — FAILED (RT ENG TAI PRESS) · airframe 74,930 hrs · 12,109 cycles

RIGHT ENG TAI PROBLEM. REPLACED RT ENG TAI PRESSURE SWITCH S525. RAN ENGINE AND OPS CHECK NORMAL. REACTIVATED SYSTEM.

Part: CHARGER — FAULTY (APU BATTERY) · airframe 74,909 hrs · 12,105 cycles

APU AUTO SHUT DOWN. TAXI CREW TRIED STARTING IT SEVERAL TIMES WITH NO START, BIT OF APU CONTROLLER SHOWED NO ACCEL IN POSITION 1 AND OVERTEMP IN POSITION 4 THRU 5. REPLACE APU BATTERY CHARGER. APU SLOW TO GET TO SPEED AND DUCT PRESSURE 10 PSI.

Part: PRESSURE SENSOR — INOPERATIVE (LT BOOST PUMP) · airframe 74,900 hrs · 12,104 cycles

LEFT AFT BOOST PUMP PRESSURE LIGHT INOP. REPLACED LEFT AFT BOOST PUMP PRESSURE SWITCH.

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 74,380 hrs · 12,026 cycles

RT BLEED FAULT. RTFL. REPLACING PRSOV. RIGHT ENGINE BLEED LIGHT ILLUMINATED WITH BLEED SWITCH ON. REPLACED PRSOV. ACCOMPLISHED IDLE RUN, BLEED PRESSURE NORMAL. BLEED SWITCH-NORMAL OPERATION.

Part: RELAY — DAMAGED (CABIN) · airframe 74,287 hrs · 12,008 cycles

RELAYS K417 AND K383 IN P-19 PANEL SHOW SIGNS OF OVERHEATING. REMOVED AND REPLACED RELAYS. PERFORMED A GOOD OPS CHECK OF THE NS-FSB SIGNS AND OPS CHECK OF L-1 DOOR.

Part: RELAY — DAMAGED (P-19 PANEL) · airframe 74,287 hrs · 12,008 cycles

RELAYS K417 AND K383 IN P-19 PANEL SHOW SIGNS OF OVERHEATING. REMOVED AND REPLACED RELAYS. PERFORMED A GOOD OPS CHECK OF THE NS-FSB SIGNS AND OPS CHECK OF L-1 DOOR.

Part: WIRE HARNESS — CORRODED (APU POWER) · airframe 74,287 hrs · 12,008 cycles

APU POWER CABLE (W236-006-1-0) HAS A CORRODED SPLICE CAUSING OVERHEAT AT BS 1783-1800 IN EMPENNAGE COMPARTMENT BELOW HORIZ STAB RIGHT SIDE. REMOVED AND REPLACED HARNESS ASSY. INSTALLED ASSOCIATED SPLICES FOR HARNESS. OPS CHECK OF APU GENERATOR GOOD.

Part: TERMINAL — OVERHEATED (CABIN) · airframe 74,287 hrs · 12,008 cycles

P19 PANEL, T180 AND T184 TERMINAL LUGS SHOW SIGNS OF OVERHEATING. REMOVED AND REPLACED TERMINAL LUGS. OPS CHECK GOOD OF FWD INDIRECT CEILING LIGHTS AND SIDEWALL LIGHT.

Part: SPRING — WEAK (L1 DOOR) · airframe 74,287 hrs · 12,008 cycles

L1 DOOR GAS SPRING WEAK. REMOVED AND REPLACED GAS SPRING. OPS CHECK GOOD.

Part: CABLE — FRAYED (AFT RT OVERWING) · airframe 74,287 hrs · 12,008 cycles

AFT RT OVERWING HATCH STEP AFT CABLE FRAYED. REPLACED CABLE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,287 hrs · 12,008 cycles

LIGHT BAR (EEL) AT AFT GALLEY. REPLACED EEL STRIP. OPS CHECKS GOOD.

Part: SHEAR TIE — DEFECTIVE (FUSELAGE) · airframe 74,287 hrs · 12,008 cycles

STA 368 BETWEEN STR 7L AND 8L IS OUT OF TOLERANCE. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED SHEAR TIE.

Part: SPRING — FAULTY (R2 DOOR SLIDE) · airframe 74,287 hrs · 12,008 cycles

CABIN DOOR R2 SLIDE DEPLOYMENT BAR FAILS TO RETURN FROM 90 DEGREES. REPLACED GAS SPRING. OPS CHECKS GOOD.

Part: HOUSING — CRACKED (LT OVERWING) · airframe 74,287 hrs · 12,008 cycles

LT OVERWING DISCONNECT HOUSING IS CRACKED. REPLACED DISCONNECT HOUSING. FREEDOM OF MOVEMENT. CHECKS GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 74,266 hrs · 12,003 cycles

BROKEN EEL LIGHTING RIGHT SIDE IN FIRST CLASS. REPLACED BROKEN ELCTRO LUMINESCENT LIGHT STRIP & POWER RIBBON. REPLACED PLASTIC COVER AND SYSTEM. OPS CKS OKAY.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 74,120 hrs · 11,982 cycles

EMERGENCY LIGHTS AT SEAT 14B COVERED BY DUCT TAPE REPAIR IN AREA. FOUND COVER IS MISSING. REPLACED EMERGENCY LIGHT TRACK COVER. LIGHTS OPS CHECK NORMAL.

Part: BOTTLE — LOW (OXYGEN SYS) · airframe 73,979 hrs · 11,962 cycles

CREW OXYGEN PRESSURE BELOW 3SVC REQUIRED LIMITS (1.620 PSI). UNIT FOUND UNDERSERVICED. SERVICED O2 TO FULL. OPS CHECK GOOD.

Part: CAP — DISLODGED (EMERGENCY LIGHT) · airframe 73,662 hrs · 11,910 cycles

EMERGENCY EXIT LIGHTS LOOSE L AISLE 1ST CLASS. *S/D* FOUND LOOSE END CAP LIGHT ASSEMBLY. INSTALLED END CAP. AC OK FOR SERVICE.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 73,396 hrs · 11,872 cycles

RIGHT INBOARD MID AND AFT T/E FLAP HAS DAMAGE TO LOWER SURFACE. ALSO LOWER WING PANEL (652CB) WAS PUNCTURED AND HAS INTERIM REPAIR ACCOMPLISHED.

Part: BARREL — UNSERVICEABLE (EVAC SLIDE)

LEAKING BARREL. REPLACED BARREL. READY FOR SERVICE.

Part: CHILLER — TRIPPED (FWD GALLEY) · airframe 73,209 hrs · 11,843 cycles

SMOKE POSSIBLY ELECTRICAL IN BUSINESS GALLEY IN FLT. ALL POWER TO GALLEY SECURED. *S/D* FOUND CHILLER CIRCUIT BREAKER TRIPPED. REPLACED MID FWD GALLEY CHILLER, OP CHECK GOOD. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,155 hrs · 11,836 cycles

LEFT EXT EMERGENCY LIGHT AFT OF WING INOP.

Part: LIGHT — INOPERATIVE (CAVIN) · airframe 73,155 hrs · 11,836 cycles

EEL LIGHT AT SEATS 5EF INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,155 hrs · 11,836 cycles

EEL LIGHT IN FRONT OF LAV 103 INOP.

Part: WARNING LIGHT — ILLUMINATED · airframe 72,143 hrs · 11,667 cycles

NR 2 ENG 'ENG CONTROL' MESSAGE APPEARED ON EICAS WITH EEC IN NORMAL MODE. RECURRED ON SUBSEQUENT FLIGHT.

Part: EEC — MALFUNCTIONED (NR 2 ENGINE) · airframe 72,143 hrs · 11,667 cycles

NR 2 ENG 'ENG CONTROL' MESSAGE APPEARED ON EICAS WITH EEC IN NORMAL MODE. RECURRED ON SUBSEQUENT FLIGHT. *S/D* REPLACED NR 2 ENGINE EEC ALTERNATOR, EEC AND N1 TRANSDUCER. OPS CHECK NORMAL.

Part: DISPLAY — FAILED (COCKPIT) · airframe 71,772 hrs · 11,610 cycles

RTFL DUE TO FAILURE OF THE MULTI-FUNCTION CONTROL DISPLAY UNIT.

Part: PANEL — CRACKED (T/E FLAP) · airframe 71,709 hrs · 11,601 cycles

RIGHT OUTBOARD FLAP OUTBOARD WRAP AROUND PANEL AT OUTBOARD SIDE UNDER AUX TRACK HAS CRACK. DURING A CHECK FOUND RH OUTBOARD FLAP OUTBOARD FLAP GUIDE BROKEN AND MISSING. SENT LEADING EDGE PANEL 666FT TO SHOP 273 FOR REPAIR. REPLACED RT OUTBOARD FLAP DEFLECTION TRACK REF 27-51-24. REINSTALLED REPAIRED PANEL 666FT. AC OK FOR SERVICE.

Part: LAMP — DIRTY (EMERGENCY LIGHTS) · airframe 71,709 hrs · 11,601 cycles

RIGHT OVERWING EEL AND ROWS 16 THRU 26 EEL INOP. CLEANED, DRIED AND REINSTALLED LAMPS.

Part: HYDRAULIC SYSTEM — MALFUNCTIONED (LEFT) · airframe 70,710 hrs · 11,459 cycles

LOSS OF LEFT HYDRAULIC SYSTEM ON ENGINE START.

Part: BLADE — BENT (HPC) · airframe 70,220 hrs · 11,381 cycles

6TH STAGE HPC BLADE HAS BENT AND DISTORTED IMPACT DAMAGE 0.5 INCH FROM BLADE TIP. LENGTH OF DAMAGE 0.5 AND BEND IS .125 INCH.

Part: SWITCH — FAULTY (EMERGENCY LIGHTS) · airframe 69,775 hrs · 11,310 cycles

AFT ATTENDANT EMERGENCY LIGHT SWITCH LIGHT INOP. 10-9-07 EMERGENCY LIGHT SWITCH CONNECTED BACKWARDS. REWIRED SWITCH PER WDM 33-51-11, OP CHECK OK

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,775 hrs · 11,310 cycles

LEFT FWD GALLEY AISLE EEL LIGHT INOPERATIVE. 10-9-07 REPLACED LAMP, OP CHECKS OK.

Part: SWITCH — FAULTY (EMERGENCY LIGHTS) · airframe 69,775 hrs · 11,310 cycles

EMERGENCY EXIT LIGHTS ON W- SWITCH IN ARMED POSITION. 10-19-07 REPLACED FLT DECK AND AFT FLT ATTEND. SWITCHES REF WD 33-51-11 PG.1D OPS CKS GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 69,740 hrs · 11,302 cycles

ENTIRE FIRST CLASS EEL LIGHTS INOP LEFT SIDE AND X AISLE. 10-9-07 RECONNECTED AND SECURED FEEDER CONNECTOR.OPS CHECKED EEL LIGHTS, OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,740 hrs · 11,302 cycles

EEL LIGHTS INOP RIGHT SIDE ROWS 15 THRU 27. 10-9-07 REPLACED SHORTED EEL LAMP. ALL EEL OP CHECKS OK.

Part: PANEL — PUNCTURED (L/E SLAT) · airframe 69,273 hrs · 11,216 cycles

LEFT LEADING.EDGE SLAT NR 1 CLOSURE PANEL HAS 3 INCHES PUNCTURE, CRACKED, APPROX 20 INCHES FROM INBOARD EDGE. PERFORMED TEMPORARY REPAIR PER ENGINEERING VARIATION AUTHORITY. SLAT TO BE PERMANENTLY REPAIRED WITHIN 300 HOURS. PUNCTURE CAUSED BY GROUND EQUIPMENT CONTACT.

Part: LIGHT — DAMAGED (CABIN) · airframe 69,219 hrs · 11,205 cycles

FLOOR EEL STRIP AT DOOR 1L CLOSET HAS BEEN DAMAGED AND IS INOP. [08-14-07] REPAIRED EEL STRIP AT DOOR 1L CLOSET.

Part: BRACKET — BROKEN (LEFT IDG) · airframe 68,698 hrs · 11,113 cycles

PER FLT CREW - LEFT GENERATOR DRIVE LIGHT ILLUMINATED, IDG DISCONNECTED AND APU POWERING BUSS. SERVICED LT IDG, FOUND SERVICE CONNECTION FITTING BRACKET BROKEN AND DRAIN FITTING POPPET NOT COMPLETELY SEATING. REPLACED POPPET AND WELDED BRACKET FOR INTERIM REPAIR. DPI NOT POPPED. RESET IDG AND RAN ENGINE AT THE GATE. ALL PARAMETERS NORMAL AND NO LEAKS NOTED.

Part: ENGINE — OVERHEATED (RIGHT) · airframe 68,608 hrs · 11,099 cycles

RTFL DUE TO RIGHT ENGINE BLEED OVERHEAT INDICATION. [07-10-07] REPLACED FAN AIR VALVE AND FAN AIR TEMP SENSOR, PERFORMED HIGH POWER RUN, PS CK OK . AIRCRAFT OK FOR SERVICE.

Part: CABLE — OUT OF POSITION (CABIN) · airframe 68,162 hrs · 11,021 cycles

EMERGENCY FLOOR LIGHTING STRIP NEAR 1B COMING UP. POSITIONED CABLE IN THE CORRECT PLACE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,905 hrs · 10,972 cycles

EEL LIGHT LEFT A-ZONE INOPERATIVE. REMOVED AND REPLACED CHARGER AND BATTERY PER MM 33-51-07 AND EEL SYSTEM OP CHECKS GOOD.

Part: BRACKET — CRACKED (BS 246) · airframe 67,905 hrs · 10,972 cycles

PULLEY SUPPORT BRACKET CRACKED FWD FACE OF BS 246 FLOORBEAM AT RBL 14. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED BRACKET STIFFENER.

Part: FASTENER — MISSING (GIRT BAR) · airframe 67,905 hrs · 10,972 cycles

LEFT FWD ENTRY DOOR, FWD GIRT BAR FITTING MISSING FASTENER, FOUND DURING PRELIMINARY INSPECTION. [SUP 5-1-07] INSTALLED LT FWD ENTRY DOOR, FWD GIRT BAR FITTING FASTENER RETAINER. A/C OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,905 hrs · 10,972 cycles

LIGHT STRIP IN FRONT OF THE FWD CLOSET IS INOP.

Part: SPRING — WEAK (SLIDE GIRT BAR) · airframe 67,905 hrs · 10,972 cycles

LEFT AFT MED DEPLOYMENT BAR GAS SPRING IS WEAK. [SUP 4-24-07] AFTER TROUBLESHOOTING FOUND WEAK GAS SPRING. REPLACED GAS SPRING PER MM 25-66-03. DEPLOYMENT BAR HAS PROPER SPRING TENSION. AIRCRAFT OK FOR SERVICE.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 67,539 hrs · 10,907 cycles

OVERWING EXIT EMERGENCY LIGHTS FLASHING WITH EMERGENCY LIGHTS ARMED. REPLACED EEL BATTERY PACK AT ROW 17A. EEL SYSTEM OP CHECKED OK FOR SERVICE.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 67,450 hrs · 10,884 cycles

FOUND EMERGENCY EXIT LIGHTS CAME ON ONCE IN FLIGHT IN LEFT REAR OF CABIN. REPLACED BATTERY PACK AT POWER SUPPLY M739. EEL OPS CK OK

Part: CONNECTOR — DIRTY (EMERGENCY LIGHTS) · airframe 67,446 hrs · 10,884 cycles

FOUND EEL LIGHTS COME ON INTERMITTENTLY AT SEATS 15 THRU TO REAR OF AIRCRAFT, LEFT AISLE. CLEANED CONNECTOR AT EMERGENCY EXIT LIGHT BATTERY CHARGER OUTBOARD OF SEAT 18A. LIGHTS OPERATE NORMALLY.

Part: CHECK VALVE — STUCK (RT FUEL TANK) · airframe 67,398 hrs · 10,872 cycles

FUEL CONFIG LIGHT ON AND RT MAIN TANK QTY INCREASED TO 42.6 WHEN LEFT READS 40.4. TTL READS 127.3 AND FMC CALC READS 124.1. FUEL AT DEPT READ 126.6. [5-1-07] REPLACED RT FUEL TANK COMPENSATOR & EMITTER. ALSO, SUSPECT RT MAIN INTANK HARNESS. REPLACED RT MAIN INTANK HARNESS & SUMMING PLUG. SEALED & RETURNED TO SERVICE. FUEL TANK IMBALANCE STILL PARTIALLY INDICATED UNTIL 26MAR07. A/C INPUT TO GSO FOR C13 VISIT 27MAR07. PERFORMED FUEL TANK FLAME ARRESTOR MOD. NO RECURRENCE OF FUEL IMBALANCE AFTER C13 VISIT. SUSPECT TANK WORK/ MOD ACTIVITY RELIEVED A PARTIALLY STUCK FUEL CHECK VALVE.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 64,042 hrs · 10,337 cycles

LANDED AT ORD UNDER AMBER ALERT DUE TO ILLUMINATED FLAP DISAGREE LIGHT.

Part: FLAP TRACK — SHEARED (TE FLAPS) · airframe 63,497 hrs · 10,245 cycles

FRACTURE OF LT OTBD T/E FLAP DETECTION CONTROL TRACK. LT OTBD T/E FLAP DEFLECTION CONTROL TRACK IS COMPLETELY SHEARED JUST AFT OF TIE ROD SUPPORT LUG. PER BOEING, THIS TYPE OF INCIDENT IS UNUSUAL, BUT NOT UNCOMMON. BOEING HAS RELEASE SB 767-27-0184 TO EXAMINE SUPPORT LUG AREA FOR CRACKING & CORRECTIVE MEASURES IF FOUND. TELEX 1-167172191 GOES FURTHER TO EXPLAIN THAT THE CRACKING IS UNRELATED TO THE TRACK ATTACH FITTINGS THAT ARE THE SUBJECT OF BOEING SB 767-57-0069. BOEING SERVICE BULLETIN 767-27-0184 STATES THAT FRACTURE OF THE DEFLECTION CONTROL TRACK DOES NOT AFFECT THE SAFETY OF FLIGHT.

Part: TRACK — SEPARATED (TE FLAPS) · airframe 63,497 hrs · 10,245 cycles

LEFT OUTBOARD FLAP DEFLECTION CONTROL TRACK HAS SEPARATED AT FWD END.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 62,879 hrs · 10,139 cycles

NR 1 PYLON INBOARD FWD STRUT SKIN CRACKED AT PANEL 416BR CUTOUT RADIUS. IT WAS PROBABLY CAUSED BY FATIGUE. THE SKIN WAS REPAIRED PER SRM 54-53-01 WITH -1 AND -2 DOUBLERS.

Part: BUSHING — CORRODED (NR 1 PYLON) · airframe 62,879 hrs · 10,139 cycles

NR 1 PYLON UPPER LINK FITTING, OUTBOARD LUG REQUIRES REWORK DUE TO INBOARD LUG REWORKED. BUSHING REPLACEMENT DUE CORRODED BUSHING. BOTH LUGS MUST BE REWORKED AS A PAIR. REWORKED AND BUSHINGS WERE REPLACED DUE TO CORROSION. BUSHINGS WERE REPLACED PER SRM 54-53-90 AND LUGS WERE REWORKED PER MM 54-51-93.

Part: BUSHING — ROTATED (NR 1 PYLON) · airframe 62,879 hrs · 10,139 cycles

NR 1 PYLON DIAGONAL BRACE FITTING AT STRUT ATTACH, FWD INBOARD AND OUTBOARD BUSHINGS HAS EVIDENCE OF ROTATION IN THE BORE. NR 1 PYLON DIAGONAL BRACE FITTING AT STRUT ATTACH, FWD INBD AND OUTBD BUSHINGS HAVE EVIDENCE OF ROTATION IN THE BORE. MIGRATION CAUSE IS UNKNOWN. THEY WERE REPLACED PER SRM 54-53-90.

Part: BUSHING — WORN (NR 1 PYLON) · airframe 62,879 hrs · 10,139 cycles

NR 1 PYLON UPPER LINK FITTING, INBOARD LUG, OUTBOARD BUSHING LIP FRETTED. NR 1 PYLON UPPER LINK FITTING, INBD LUG, OUTBD BUSHING LIP FRETTED. IT WAS PROBABLY CAUSED BY TOLERANCE BUILD UP. BUSHING WAS REPLACED PER SRM 54-51-93.

Part: BUSHING — LOOSE (NR 2 PYLON) · airframe 62,879 hrs · 10,139 cycles

NR 2 PYLON OUTBOARD MIDSPAR FITTING, INBOARD LUG BUSHING MOVES IN BORE. NR 2 PYLON OUTBD MIDSPAR FITTING, INBD LUG BUSHING MOVED IN THE BORE. BUSHING MIGRATION CAUSE IS UNKNOWN. IT WAS REPLACED WITH AN OVERSIZED BUSHING PER SRM 54-53-90

Part: FRAME — CORRODED (BS 654, LBL4) · airframe 62,879 hrs · 10,139 cycles

FRAME TOP CAP CORRODED AT BS 654+121, LBL42, FWD CARGO PIT. MAJOR REPAIR TO FRAME TOP CAP PER SRM AS PERMANENT REPAIR.

Part: BUSHING — MIGRATED (NR 1 PYLON) · airframe 62,879 hrs · 10,139 cycles

NR 1 PYLON INBD MIDSPAR FITTING, INBD AND OUTBD LUG BUSHINGS MIGRATED. NR 1 PYLON INBD MIDSPAR FITTING, INBD AND OUTBD LUG BUSHINGS WERE MIGRATED. CAUSE OF BUSHING MIGRATIONS IS UNKNOWN. BUSHINGS WERE REPLACED PER MM 54-53-90.

Part: BUSHING — MIGRATED (NR 1 PYLON) · airframe 62,879 hrs · 10,139 cycles

NR 1 PYLON OUTBD MIDSPAR FITTING OUTBD LUG, BUSHING IS MIGRATED. NR 1 PYLON OUTBD MIDSPAR FITTING OUTBD LUG, BUSHING WAS MIGRATED. THE BUSHING MIGRATION IS UNKNOWN. IT WAS REPLACED PER SRM 54-53-90.

Part: BUSHING — MIGRATED (NR 2 PYLON) · airframe 62,879 hrs · 10,139 cycles

NR 2 PYLON DIAGONAL BRACE FITTING FWD-STRUT ATTACH, INBD SIDE BUSHING IS MIGRATED. NR 2 PYLON DIAGONAL BRACE FITTING FWD-STRUT ATTACH, INBD SIDE BUSHING WAS MIGRATED. BUSHING MIGRATION CAUSE IS UNKNOWN. THE BUSHING WERE REPLACED PER SRM 54-53-90.

Part: BRACKET — CRACKED (LT WING KRUEGER) · airframe 62,879 hrs · 10,139 cycles

LT WING KRUEGER FLAP INBD OF NR 1 PYLON, ROTARY ACTUATOR OUTBD SUPPORT BRACKET IS BUCKLED AND CRACKED. BRACKET FAILURE WAS DUE TO FATIGUE. PART WAS REPLACED.

Part: STIFFENER — CRACKED (FLOORBEAM) · airframe 56,939 hrs · 9,173 cycles

CRACK IN U-STIFFENER BS 246, APPROX RBL 75, FWD SIDE OF FLOORBEAM. FABRICATED & INSTALLED STIFFENER.

Part: HINGE — CRACKED (TE FLAP) · airframe 56,939 hrs · 9,173 cycles

RIGHT INBOARD FLAP-CENTER EXTERNAL HINGE FITTING IS CRACKED ON INBOARD AND OUTBOARD FLANGES AT THE TOP. REPAIRED HINGE WITH REPAIR ANGLES AND FILLERS.

Part: GENERATOR — INOPERATIVE (LEFT) · airframe 56,865 hrs · 9,155 cycles

RETURN TO FIELD DUE TO L-GENERATOR INOP. TEARDOWN REVEALED THAT THE DIFFERENTIAL AND CLUSTER GEARS WERE SEVERELY DAMAGED BEYOND REPAIR. IT APPEARS THAT SOME KIND OF CONTAMINATION WAS INTRODUCED WHICH EITHER INTERRUPTED/DILUTED THE OIL SUPPLY TO ONE OF THE CLUSTER GEARS, OR DAMAGED THE PLATING ON THE SHAFT RESULTING IN LARGE AMOUNTS OF METAL INTRODUCED IN-BETWEEN BEARING SURFACES. THE CONTAMINATION COULD HAVE BEEN FUEL (OR SOME OTHER CONTAMINATE WHICH LOWERED THE VISCOSITY OF THE OIL), OR SOME OTHER FOREIGN PARTICLE(S) INTRODUCED EARLY IN THE UNITS LIFE. NO FUEL SMELL WAS NOTED BY TECHNICIAN DURING TEARDOWN. THE UNIT IS UNDERGOING A COMPLETE OVERHAUL.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 51,447 hrs · 8,226 cycles

EMERGENCY FLOOR LIGHTING, FLASHING ON AND OFF ON LEFT SIDE OF ECONOMY SECTION BETWEEN ROWS 18-26. FOUND CONNECTOR PLUG LOOSE AND RECONNECTED IT. SYSTEM CHECKED OK.

Part: RELAY — BURNED OUT (EMERGENCY LIGHTS) · airframe 51,024 hrs · 8,167 cycles

FLOOR EMERGENCY LIGHTS ON LEFT SIDE OF COACH CYCLED ON AND OFF THREE TIMES WITH COCKPIT SWITCH IN ARMED POSITION. EMERGENCY LIGHTS ALT TRANSFER RELAY "K868" REQUIRES REPLACEMENT. REPLACED RELAY.

Part: SKIN — DENTED (FUSELAGE) · airframe 50,696 hrs · 8,111 cycles

DENT IN SKIN JUST BELOW SKIN LAP AT STA 272, STRINGER 17R. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALLED.

Part: DOOR — DAMAGED (RAM AIR INLET) · airframe 46,953 hrs · 7,428 cycles

EN ROUTE CREW REPORTED SIGNIFICANT VIBRATION AND DIVERTED TO DENVER. LT RAM AIR INLET DOOR SECTION FOUND MISSING. DOOR WAS REMOVED AND SYSTEM WAS DEFERRED PER CDL 21BA. DOOR P/N 213T3010-1 AND ASSOCIATED HARDWARE WERE REPLACED AT DEN.

Part: CONTROL VALVE — OUT OF RIG (ENGINE) · airframe 44,727 hrs · 7,047 cycles

WEATHER RADAR INOP. DIVERTED TO MCO DUE TO T-STORMS IN MIA AREA. *S/D* ENGINE WAS REPLACED DUE TO OVERTEMP. DURING ENGINE PRE-REPAIR RUN, FOUND ENGINE VANE BLEED CONTROL (EVBC) WAS OUT OF TRIM. EVBC WILL BE OVERHAULED.

Part: LIGHT — DAMAGED (CABIN) · airframe 43,823 hrs · 6,900 cycles

LT EMERGENCY EXIT LIGHTING (EEL) IN FIRST CLASS IS DAMAGED.

Part: CONTROLLER — INOPERATIVE (RUDDER TRIM) · airframe 42,932 hrs · 6,750 cycles

RUDDER TRIM INOP. JETISONED FUEL, RTF.

Part: ENGINE — LEAKING (NR 2) · airframe 41,803 hrs · 6,566 cycles

NR 2 ENGINE OIL QTY DECREASED TO 0 IN FLIGHT OIL TEMP & PRESSURE OK. LOGBOOK READS LOST 2 QTS AN HOUR, THE LAST 2.5 HOURS OF FLT. ON DESCENT WITH THROTTLES RETARDED OIL TEMP BEGAN TO RISE AND ENGINE VIBRATION WAS AT 1.7. AFTER ENGINE SHUTDOWN AT THE GATE OIL QTY READS 9 QTS. *S/D* THE SUBJECT ENGINE WAS REMOVED FROM AIRCRAFT 6644-2 ON OCTOBER 1,2000 IN ORD FOR OIL IN THE TAILPIPE AND ABOVE NORMAL OIL CONSUMPTION. A FULL ENGINE BORESCOPE WAS PERFORMED WITH SPECIAL ATTENTION FOR OIL WETTING IN THE HPC AND HPT. REVEALED NO UNSERVICEABLE CONDITIONS AND NO OIL WETTING. OIL FILTER AND CHIP DETECTORS WERE CLEAN.THE NUMBER 3 BEARING DRAIN LINE WAS FOUND CLEAN AND DRY. OIL SYSTEM PRESSURE CHECKS WERE ACCOMPLISHED

Part: SKIN — DAMAGED (FUSELAGE)

FUSELAGE DAMAGED BY PORTABLE AIRSTAIR. DAMAGE LOCATED BETWEEN BS 246 AND BS 434 STRINGERS S17L AND S26L. *S/D* REPLACED SKIN PANEL 141T3330-109, STRINGER 22L BS 297 TO 363 (141T3001-71) AND BS 363 TO 434 (141T3001-69) PER 767-300 SRM 51-40-02 (APPLICABLE PAGES ONLY). REPAIR RECORDED ON MRA NR 114.

Part: PROX CARD — FAILED (E & E COMPT)

ON TAKEOFF ROLL 100 KT, FLAP CONFIG WARNING LIGHT ON EICAS AND HORN. CONTINUED TAKEOFF. FALSE STICK SHAKER AT 170 KTS AND L/E SLAT ASYM ON EICAS. COULD NOT RETRACT SLATS WITH FLAP HANDLE UP. EXTENDED FLAPS USING ALTERNATE SYSTEM. LANDED FLAPS 20 DEG AT 330,000 POUNDS. *S/D* FAULTY LOGIC FROM THE PSEU CAUSED FALSE WARNING INDICATIONS DURING TAKEOFF INCLUDING FLAP CONFIGURATION, SLAT ASYMMETRY AND STALL WARNING. WHEN THE SLAT ASYMMETRY INDICATION WAS SENSED BY THE FLAP/SLAT ELEC UNIT FSEU. SLATS WERE POSITIONED ELECTRICALLY. REPLACED M14 PROX CARD AND M10 DRIVER CARD ASSEMBLIES IN PSEU AND THE S300 SLAP POSITION SENOR SWITCH PER MM.

Part: ACTUATOR — FAILED (MLG UPLOCK)

LEFT MAIN LANDING GEAR REMAINED DOWN AFTER TAKEOFF. RETURNED TO FIELD. *S/D* MLG DRAG BRACE LOCK ACTUATOR FAILED. INTERNAL PISTON RETENTION NUT WAS NOT INSTALLED CORRECTLY. REPLACED ACTUATOR.

Part: COMPRESSOR — STALLED (NR 2 ENGINE)

NR 2 COMPRESSOR STALL SHORTLY AFTER TAKEOFF. FLAMES REPORTED, FIRE BOTTLES DISCHARGED, ENGINE SHUTDOWN. EMERGENCY DECLARED. RETURNED TO FIELD, OVERWEIGHT LANDING WITHOUT INCIDENT. *S/D* THIS ENGINE EXPERIENCED A GROUP 3 SURGE EVENT. GROUP 3 SURGES ARE THE RESULT OF EXCESSIVE BLADE TIP CLEARANCE IN THE REAR STAGES OF THE HIGH PRESSURE COMPRESSOR. THIS ENGINE WAS REMOVED FOR HIGH PRESSURE COMPRESSOR REFURBISHMENT.

Part: IRU — MISALIGNED (E/E BAY)

THE AIRCRAFT RETURNED, DUE TO A FLIGHT MANAGEMENT COMPUTER NAVIGATION DISCREPANCY. *S/D* FLIGHT RECORDER DATA INDICATED THAT THE FMC POSITION WAS APPROXIMATELY 34 NM NORTHEAST OF THE ACTUAL POSITION AFTER PUSHBACK. THE IRU WAS MISALIGNED, OPERATIONS CHECKED NORMAL AFTER REALIGNMENT.

Part: PRESS REG VLV — MALFUNCTIONED (RT ENGINE)

ABORTED TAKEOFF DUE TO RIGHT ENGINE PRESSURE REGULATING VALVE EICAS MESSAGE WITH BLEED CAUTION LIGHT. ACCOMPLISHED CHECK OF ALL VALVES ON THE RIGHT ENGINE. ALL WIRES WERE ALSO INSPECTED AND FOUND SECURE. OPERATIONS CHECK NORMAL. THERE HAVE BEEN NO FURTHER DISCREPANCIES INDICATED. NO PARTS WERE REMOVED.

Part: WINDOW — DEFECTIVE (RT COCKPIT)

AIRCRAFT RETURNED TO FIELD DUE TO FIRST OFFICER WINDOW LEAK. *S/D* UPDATE A DEFECTIVE FIRST OFFICER WINDOW CAUSED THE AIR LEAK. REPLACED WINDOW AND PRESSURIZED AIRCRAFT, NO LEAKS NOTED.

Part: CONNECTORS — LOOSE (CABIN)

FORWARD CROSS AISLE EEL STRIP INOPERABLE. REPLACED CONNECTORS ON EEL STRIPS, OPERATIONS CHECK NORMAL.

Part: OIL PRESS TUBE — CRACKED (NR 1 ENGINE)

CREW REPORTS NR 1 ENGINE OIL QUANTITY WENT TO '0'. ENGINE SHUTDOWN AND WINDMILLED FOR APPROX 30 MINUTES. OIL PRESSURE DURING WINDMILL 4-6 PSI. SUPPLEMENTAL DATA UPDATE: ANGLE GEARBOX OIL PRESSURE LINE CRACKED CAUSING LOSS OF OIL QUANTITY. REPLACED OIL PRESSURE LINE.