N642UA

Part: SKIN — DAMAGED (ZONE 600 AILERON) · airframe 131,061 hrs · 20,221 cycles

RT WING OTBD AILERON, WATER INGRESSION FOUND. PERFORMED PERMANENT COMPOSITE REPAIR AT WATER INGRESSION AREA IAW ECRA 5760-01124 REV A.

Part: SKIN — DAMAGED (ZONE 500 AILERON) · airframe 131,061 hrs · 20,221 cycles

LEFT OTBD AILERON HAD WATER INGRESSION. LT OTBD AILERON PERFORRMED PERMANENT COMPOSITE REPAIR AT WATER INGRESSION AREA PER ECRA 5760-01123 REV A.

Part: FMC — FAULTED (ZONE 100) · airframe 130,925 hrs · 20,201 cycles

L FMC FAIL L FMC REPLACED IAW AMM 34-61-01/401 AND FMC CROSSLOAD PERFORMED IAW AMM TASK 34-61-00-342-008-006 REV 145 PERFORMED SUCCESSFULLY REMOVED UNSERVICEABLE PART AND INSTALLED NEW PART

Part: EADI — FAULTED (ZONE 200) · airframe 130,660 hrs · 20,168 cycles

CAPT ADI BLURRED OUT AFTER REACHING CRUISE ALTITUDE PANEL INSTL-PILOTS MAIN (ELECTRONIC ATTITUDE DIRECTOR INDICATOR ONLY) REFERENCE: 34-22-03-02 ONE EACH IN IAD P# 622-5047-101 R/R CAPT ADI MULTICOLOR SCREEN REF. AMM 34-22-03. OPS CHECK GOOD.

Part: ARMING LEVER — FOD (ZONE 800) · airframe 129,941 hrs · 20,083 cycles

DOOR 2L WAS DIFFICULT TO DISARM. DOOR L2 SLIDE ARMING MECHANISM INSPECTED DEBRIS CLEARED FROM THE LOWER FITTING. DOOR ARMING NORMALLY UPON SEVERAL ATTEMPTS. AIRCRAFT FIT FOR FLIGHT

Part: CONTACT — DAMAGED (ZONE 200) · airframe 128,454 hrs · 19,896 cycles

EMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - EMERGENCY LIGHT AT CEILING PANEL ABOVE SEAT 9A INOP. FOUND CONNECTOR DAMAGED. REMOVED AND REPLACED THE EMERGENCY LIGHT CONNECTOR ABOVE SEAT 9A IN REF SWPM 20-61-00. OK FOR SERVICE.PARTS USED: 00-0593-3-4846,QTY :1

Part: SCREW — MISSING (LH WING) · airframe 126,329 hrs · 19,633 cycles

SCREW MISSING LEFT WING GEARBAY TOP. PICTURE IN ATTACHED PICTURE FROM UPPER WING LH SIDE A/C RELEASED IAW EC/RA#5751-01513 INITIATE A DIP TO PERFORM PART 2 AFT EVERY CYCLE AND PART 3 PERMANENT REPAIR WITHIN 2 FLT CYCLES APPROVED FOR 2 CYCLE DIP WITH TAPE INSPECTION PRIOR TO EACH DEPARTURE REF ECRA 5751-01513 TOMC-APPROVAL FROM SC1ELBYC COMMENT TA M&E: 76-9957-8-0360 S/N: 6442 LIMITS, INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS REVIEW.CONTROL #: N/A SOURCE DOCUMENT: EC/RA#5751-01513 TOMC APPROVED: QC REVIEWED CONTROL #:SOURCE DOCUMENT: EC/RA#5751-0 REPETITIVE LABOR HOURS: 0001 GROUND TIME: 0000 TERMINATING LABOR HOURS: 0001 GROUND TIME: 0001 TOMC APPROVED: QC REVIEWED INSTALLED NEW NUTPLATE ON PANEL 551PT REF ECRA 5751-01513 AND AMM 51-40-02 NO FURTHER DEFECT NOTED TOMCQC REV PERFORMED FASTENER PLACED ON DIP PER ECRA. ITEM REPAIRED AFTER ONE FLT CYCLE

Part: SCREW — MISSING (PANEL) · airframe 126,329 hrs · 19,633 cycles

POP SCREW UNDER RIGHT WING ROOT MISSING PLEASE SEE PICTURES SCREW UNDER RIGHT WING ROOT INSTALLED IAM AMM 20-00-00 SATIS SCREW REPLACED

Part: ACTUATOR — LEAKING (THRUST REVERSER) · airframe 125,887 hrs · 19,576 cycles

FUEL LEAKAGE (DROPS) NOTED COMING FROM ENG #1 RH THRUST REVERSER COWL. THE ENGINE #1 WAS OPPENED AND CHECKED, IT WAS FOUND A LEAKAGE ON ROB PART P/N 5830201-111 ACTUATOR TURB VALVE FROM AIRCRAFT 6665 ROBBING A SERVICEABLE COMPONENT FROM AC 6665 #1 ENG - REMOVED ACTUATOR TURBINE CASE COOLING. REMOVED REF AMM 75-24-05/401. IPC 75-25-05-05-55 REMOVED AND REPLACED THE TCC ACTUATOR REF AMM75-24-05/401 NO LEAK NOTED.

Part: DOOR — MISSING (LH ENG PYLON) · airframe 125,852 hrs · 19,572 cycles

PDA 2 PDA : LEFT ENGINE PYLON OUTBOARD NACELLE STRUT PRESSURE RELIEF DOOR MISSING {B767-51-3-6003}. PERFORMED GVI AND IT WAS NOT FOUND ANY DAMAGES ON THE NACELLE INSTALLED. CDL COMPLIED, STICKER INSTALLED. STRUCT AREA, RELEASED CDL 54D DUE NO PARTS AT GRU. STICKER ADD EMP:U409644 DISPATCH DESK: 3385 NAME: J.A. DATE: 22-MAY-24- NOC DESK: 767 NAME: JOHN O DATE: 22-MAY-24- LEFT ENGINE PYLON OUTBOARD NACELLE STRUT PRESSURE RELIEF DOOR MISSING DEFERRED REF CDL 54D THE CORRECT ACCESS DOOR MISSING IS THE STRUT ENGINE MOUNT ACCESS DOOR 436BL PIC ATTACHED. REPLACED LEFT ENGINE PYLON OUTBOARD NACELLE STRUT PR DOOR, PANEL 436BL. REF AMM 54-53-01.

Part: PUMP — MALFUNCTIONED (FUEL SYSTEM) · airframe 125,730 hrs · 19,558 cycles

L AFT FUEL PUMP EICAS MSG L AFT FUEL BOOST PUMP CB POPPED DUE TO LACK OF TIME REQUESTING MEL 2822M FOR AFT FUEL PUMP. PLACED AFT FUEL PUMP ON MEL 2822M, AS REQUESTED. DDP FOLLOWED WITH. APPROVED MEL 2822M IT MUST BE READ L AFT FUEL PUMP INSTEAD OF AFT FUEL PUMP AT DEFERRAL STATEMENT. LEFT AFT BOOST PUMP SWITCH C/B STAYED CLOSED AFTER APPROXIMATELY FUEL LEAKS AROUND LEFT AFT BOOST PUMP REF FIM TASK 28-22 FAULT 5 MINUTES. PERFORMED GENERAL VISUAL INSPECTION NO NOTICEABLE TREE 820. REMOVED LEFT AFT BOOST PUMP CONNECTOR (D1542) TO CHECK FOR LEFT AFT FUEL BOOST PUMP PART NUMBER 76-2821-9-9001 DAMAGE, NO DAMGE NOTED. RESET C/B ON P6 PANEL AND SWITCHED ON

Part: CIRCUIT BREAKER — TRIPPED (FUEL PUMP) · airframe 125,575 hrs · 19,538 cycles

L AFT FUEL PUMP BREAKER TRIPPED WHEN SWITCH SELECTED ON DUE TO LACK OF TIME NEED TO PLACE IT ON MEL. REQUESTING MEL PLACED L AFT FUEL PUMP ON MEL 2822M AS REQUESTED, DDP FOLLOWED 2822M FOR L AFT FUEL PUMP. WITH. F LEFT AFT MAIN FUEL BOOST PUMP ACCOMPLISHED GROUND FAULT INTERRUPTER GFI OPERATIONAL TEST PER AMM 28-22-00-715-969 AND L AFT FUEL PUMP WORKS FINE.

Part: CEILING PANEL — DETACHED (SEAT 33 TO 35) · airframe 125,111 hrs · 19,478 cycles

CONTROL AND PASSENGER CABIN CHECK {B767-25-3-7043} - IT WAS OBSERVED CEILING PANEL NEXT 33D PARTIAL FELL DOWN. THE CEILING PANEL ABOVE SEAT 33 TO 35 A/B HAS BEEN INSTALLED IAW AMM 25-22-01-404-008. ITEM OK FOR FLIGHT

Part: CONTROL PANEL — INTERMITTENT (AUTOPILOT) · airframe 125,035 hrs · 19,464 cycles

MCP ALT SELECTOR WILL NOT SET ALTITUDES. REMOVED AND REPLACED MODE CONTROL PANEL PER AMM 22-11-02-402-008, PERFORMED TEST 30 AS PER AMM 22-00-02 TEST PASS. AC REMAINS FULLY CAT CAPABLE.

Part: SKIN — CORRODED (LT WING LE SLATS) · airframe 124,974 hrs · 19,444 cycles

DOUBLER REPAIR - LEFT WING LEADING EDGE SLATS INTERIOR STRUCTURE CORROSION PREVENTION AND CONTROL PROGRAM (PCP) INSPECTION {B767-57-3-7016} WAS FOUND DENT AND SCRATCH AT SLAT 1/2 UPPER SIDE. PERFORMED REPAIR OF THE #1 SLAT LEADING EDGE SKIN DENTS (#7 THROUGH #11) PER ECRA 5743-01908. ITEM GOOD FOR SERVICE. PERFORMED INSPECTION OF THE REPAIR WHERE THE QC WAS REQUIRED THE #1SLAT LEADING EDGE SKIN AS PER ECRA#5743-01908 FROM STEPS 1 TO 19 FULLY ACCOMPLISHED FROM STEPS 1 TO 3 FULLY ACCOMPLISHED. ITEM OK TO SERVICE.

Part: DOOR SILL — CORRODED (AFT DOOR) · airframe 124,974 hrs · 19,444 cycles

CORROSION NEAR LOWER DOOR SILL - DURING INSPECTION WAS FOUND A CORROSION NEAR LOWER DOOR SILL THE AFT DOOR LH AND RH ON STGR 20RH.

Part: DOOR SILL — CORRODED (AFT) · airframe 124,974 hrs · 19,444 cycles

CORROSION NEAR LOWER DOOR SILL, DURING THE INSPECTION WAS FOUND A CORROSION NEAR LOWER DOOR SILL THE AFT DOOR ON LH SIDE ON STGR 20LH.

Part: SKIN — CRACKED (STA340) · airframe 124,974 hrs · 19,444 cycles

DURING NDT PROCEDURE, IT WAS FOUND 02 HOLES WITH CRACKS INDICATION AT FORWARD DOOR CUTOUT AFT CORNER ON LH SIDE AT STA 340. PERFORM INSPECTION AS REQUIRED ON TABLE 202 FROM SRM AIRPLANE DELIVERY OR 6,000 MAXIMUM FLIGHT CYCLES FROM THE REPAIR INSPECTION INTERVAL IS 3,000 FLIGHT CYCLES. 53-10-01-2R-1. INSPECTION THRESHOLD 37,500 FLIGHT CYCLES AFTER INSTALLATION, WHICHEVER OCCURS LATER AFTER THAT REPEAT PERFORMED REPAIR OF THE FORWARD DOOR CUTOUT AFT CORNER REPAIR I.A.W. SRM 53-10-01-2R-1. THIS IS A CATEGORY B, NECESSARY TO PER SRM 53-10-01-2R-2 REQUIRES REINSPECTION AT 37500 PTC OR 6000 TOMC-APPROVAL FROM SC1ELBYC COMMENT FLIGHT CYCLES FROM REPAIR INSTALLATION REPEAT INSPECTION EVERY 3000 FLIGHT CYCLES. CHECKED REPAIR AT FORWARD DOOR 1L CUTOUT AFT CORNER PER SRM 53-10-01-2R-1 . REPAIR APPROVED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: SKIN — NONE (STA 640 STR 23) · airframe 124,974 hrs · 19,444 cycles

DURING THE AGING AIRCRAFT INSPECTION, WAS FOUND EXTERNAL DOUBLER REPAIR AT STA 640 STR 23 LH SIDE FUSELAGE WITH NO RECORDS. AT STA 632-654 BETWEEN S-26L AND S -29L AS PER PART 2 OF LATEST TOTAL FLIGHT CYCLES. PERFORM REPEAT INSPECTIONS AS PER PART 2 OF 12,000 FLIGHT CYCLES, THEREAFTER. REVISION OF EC5330-07185 ON OR BEFORE AIRCRAFT REACHES 37,500 LATEST REVISION OF EC5330-07185 AT INTERVALS NOT TO EXCEED PERFORMED REPAIR OF THE FUSELAGE SKIN AS PER ECRA # 5330-07185. ACCOMPLISH INITIAL INSPECTION OF THE EXTERNAL REPAIR INSTALLED PERFORMED INSPECTION OF REPAIR PER ECRA 5330-07185.

Part: SKIN — DAMAGED (BS 1109-1134) · airframe 124,974 hrs · 19,444 cycles

DUE TO THE AUTOMATIC DIRECTION FINDER (ADF) AREA STILL HAVE MARKS, GROOVES/SCRATCHES, THIS CAUSED ERROUNEOUS RESULT ON NDT INSPECTION. REWORK THE AREA AS PER APPLICABLE PROCEDURES. MORE DETAILS PICTURES ATTACHED. CLASSIFIED AS MAJOR REPAIR . . NECESSARY TO ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2 OF FLIGHT CYCLES?. ACCOMPLISH REPETITIVE INSPECTIONS PER PART 2 OF S, THEREAFTER. EC/RA 5331-03075 ON OR BEFORE THE AIRCRAFT REACHING 37,500 TOTAL EC/RA 5331-03075 AT INTERVALS NOT TO EXCEED 12,000 FLIGHT CYCLE PERFORMED REPAIR OF THE FUSELAGE SKIN AT STA. 1109 ? 1134, S-1L TO S-1R (UNDER FWD ADF ANTENNA AREA) PER ECRA 5331-03075 PART 1 PERFORMED INSPECTION OF THE REPAIR OF THE FUSELAGE SKIN AT STA. 1109 1134, S-1L TO S-1R (UNDER FWD ADF ANTENNA AREA) PER ECRA 5331-03075 PART 1 . THE REPAIR IS GOOD TO GO.

Part: BOLT — MISSING (PANEL 552HB) · airframe 123,678 hrs · 19,260 cycles

PDA 3 WING TE STRUCTRURE LEFT PANEL 552HB MISSING ONE BOLT. REF. AMM TASK 06-44-00-992-001 ZONE 550 AND 650 ACCESS DOORS AND PANELS. SEE PIC. INSTALLED BOLT IN WING TE STRUCTRURE LEFT PANEL 552HB PER SRM 51-40-02, GOOD FOR SVC,PARTS USED: 00-0593-3-0257,QTY :1

Part: WINDOW — UNKNOWN (FO #2 WNDW) · airframe 122,832 hrs · 19,145 cycles

BIRD STRIKE SUSPECTED RIGHT FRONT NEAR FIRST OFFICERS FEET FOUND EVIDENCE OF BIRD STRIKE BELOW FO #2 WINDOW, RIGHT LANDING LIGHT LENS AND RIGHT INBOARD FLAP. PERFORMED BIRD STRIKE INSP REF AMM 05-51-18-212-001, NO OTHER AREAS AFFECTED. CLEANED, COLLECTED SAMPLES AND INSPECTED AFFECTED AREAS, NO DAMAGE NOTED.

Part: CEILING PANEL — DETACHED (ABOVE AISLE 35/3) · airframe 122,629 hrs · 19,116 cycles

OVERHEAD PANEL 35DEF 36DEF CAME DOWN DURING ARRIVAL. FLT FTT PUS HED UP FOR TAXI IN CEILING PANEL REINSTALLED AND SECURED REF AMM TASK 25-22-01-404-008.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 121,651 hrs · 18,947 cycles

L2 DOOR EMERGENCY EXIT LIGHT POWER SUPPLY (M1561) INOPERATIVE. POWER SUPPLY REPLACED AND TESTED NORML. WORK ACCOMPLISHED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 121,651 hrs · 18,947 cycles

L1 DOOR EMERGENCY LIGHT POWER SUPPLY (M1557) INOPERATIVE. POWER SUPPLY M1557 REPLACED AND TESTED NORMAL

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 121,651 hrs · 18,947 cycles

RH OVERWING EXIT EMER LT PWR SUPPLY (M1554) INOP. POWER SUPPLY (M1554) REPLACED AND TEST NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LGIHTS) · airframe 121,651 hrs · 18,947 cycles

DOOR 1R EMERGENCY LIGHT POWER SUPPLY INOP. POWER SUPPLY (M1552) REPLACED AND TESTED NORMAL. WORK ACCOMPLISHED.

Part: BPCU — FAULTY (NA) · airframe 121,350 hrs · 18,909 cycles

L/R UTILITY BUS LIGHTS ON. UNABLE TO RESET ACCURED AFTER T/O T/S BPCU AND FOUND FAULT CT LOOP GND FAULT IN APU POWER SYSTEM PART OF TEST. FIM FOR CT LOOP GND STATES TO REPLACE APU GENERATOR CONTROLLER. REPLACED BPCU, TEST PASSED, SYSTEM OK FOR SERVICE.

Part: LAVATORY — UNSERVICEABLE (LAVATORY) · airframe 120,997 hrs · 18,864 cycles

LAVATORY SYSTEM REQUIRES SERVICE. LAVATORY SYSTEM SERVICED PER 767-300 AMM 12-17-01, LAVS CHECKED OK PER AMM 38-32-00, CONTINUE IN SERVICE.

Part: EFIS — INOPERATIVE (TCAS) · airframe 120,912 hrs · 18,853 cycles

RIGHT EFIS SYMBOL GEN NOT DISPLAYING TCAS TEST PATTERN ON THE L OWER MFD MEL 3422M REQUIRED. RIGHT EFIS SYMBOL GEN PLACED ON MEL 3422M, DDP C/W. MEL 3422M APPROVED REPLACED COMPUTER EFIS RT. IAW 34-22-01. TEST GOOD AND TCAS TEST IAW 34-45-00 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1913337 SN OFF 1807 COMPUTER, EFIS OFF 75-4182-9-0001 1807 ON 75-4182-9-0001 0760

Part: NONE — COLLAPSED (LH MLG) · airframe 120,200 hrs · 18,758 cycles

LH MLG SHOCK STRUT COLLAPSED AT THE GATE. ACCOMPLISHED LEFT MAIN GEAR SHOCK STRUT SERVICING PER AMM TASK 12-15-01-613-021 TO CONFIRM SHOCK STRUT LEAKING. CONFIRMED LEAKING NEEDS PACK SET REPLACMENT. DELAY BECAUSE LEFT MLG OIL LEAK. ACCOMPLISHED LH M.L.G ACTIVE SEAL REPLACEMENT WITH THE SPARE SEALS I.A.W AMM TASK 32-11-25-962-342. PERFORMED LH SHOCK STRYT SEAL LEAK INSPECTION. NO LEAK FOUND. INSPECTED LH MLG ACTIVE SEAL REPLACEMENT PER AMM 32-11-25-962-342. AIRCRAFT RETURN TO SERVICE. ADD EMP:U288719,U355925

Part: PUMP — FAULT MESSAGE (NA) · airframe 120,190 hrs · 18,757 cycles

CTR L FUEL PUMP EICAS ON TAXI OUT PERFORMED FIM 28-22 FAULT TREE 805 MSG CLEARED. PERFORMED SYSTEM TEST OK.

Part: TRACK — MISSING (TE FLAP) · airframe 119,855 hrs · 18,686 cycles

PDA 2 FOUND TRAILING EDGE FLAP DEFLECTION CONT TRACK BROKEN AND MISSING. (IPC REF 27-51-23-01 ITEM 1) UPDATE TO ADD PICTURES. LEFT OUTBOARD FLAP OUTBOARD EDGE. ADDING PICTURE OF RIGHT SIDE INTACT ASSEMBLY FOR REFERENCE. PERFORMED VISUAL WALK AROUND OF TAIL. NO DAMAGE NOTED ON REMOVED FORWARD END OF BROKEN FLAP TRACK ON LEFT WING. PLACED HORIZONTAL OR VERTICAL STABILIZER. PART IN MAINTENANCE SUPERVISION OFFICE. FORWARD BOLT PLACED WITH NEW TRACK. AFT BOLT REMAINS IN POSITION ON WING. INSPECTION VERIFIED:VERIFIED TORQUE OF ATTACHMENT BOLTS FOR LEFT WING DEFLECTION CONTROL TRACK. INSPECTION WORK PERFORMED BY EMPLOYEE INSPECTED TRACK ATTACH POINTS FOR DAMAGE OR CRACKS. NO INSTALLED LH OUTBOARD FLAP DEFLECTION CONTROL TRACK UP TO STEP VERIFIED TORQUE OF ATTACHMENT BOLTS FOR LEFT WING DEFLECTION INSTALLED NEW OUTBOARD FLAP DEFLECTION CONTROL CARRIAGE PER AMM ADDED ROTABLE PARTS INFO. VERIFIED INSTALLATION AND TORQUE OF OUTBOARD DEFLECTION CONTROL DISCREPENCIES. CLEARED TO INSTALL NEW LEFT WING DEFLECTION D.(6). AMM 27-51-23-424-018 & EC/RA #2750-01787. REQURES OPS CKS CONTROL TRACK 27-52-24-404-020 UP TO STEP #8 SUBTASK 27-51-24-434-011 AND ROTABLE PARTS CHANGE WAS INDICATED - TT # 0942252 SN OFF 9999 TRACK CARRIAGE IAW AMM 27-51-24. CONTROL TRACK. ETC. VERFIED TORQUE. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1148108 SN OFF 1133 ADD EMP:110148AND109211 IPC REFERENCE # 27-51-23 IPC REFERENCE # 27-51-21-01 TASK COMPLETED AS SIGNED ABOVE.

Part: SEAL — MISSING (LT OUTBRD FLAP) · airframe 117,338 hrs · 18,186 cycles

PAX INFORMED US WHEN FLAPS WERE LOWERED ON FINAL A PIECE OF RUBBER CAME OFF LT WING INSPECTED LEFT WING FOR MISSING SEALS. FOUND UPPER SEAL LOCATED NEXT TO OUTBOARD SIDE OF THE INBOARD AILERON MISSING, LOCATED AT APPROX WING STATION 534. REF L/P 6194234 FOR MISSING SEAL AND PDA CAT 2 WRITE UP : PDA 2 FOUND UPPER SEAL OF THE OUTBOARD FLAP INBOARD SIDE NEXT TO INBOARD AILERON MISSING. REF L/P 6192731 FOR CREW WRITEUP(PAX INFOMED US WHEN FLAPS WERE LOWERED ON FINAL A PIECE OF RUBBER CAME OFF LT WING). IPC 57-25-01-05 ITEM 90, 46 INCHES LONG. SEAL MISSING LEFT WING. REPLACED MISSING SEAL USING CMM REFERENCE 57-53-51 AS REFERENCE.LOG CLOSED

Part: CHARGER — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 116,577 hrs · 18,057 cycles

OVERHEAD EMERGENCY EXIT SIGNS AT ROWS 16DEF AND 21DEF ILLUMINATE TEMPORARILY THEN EXTINGUISH. REMOVED AND REPLACED POWER SUPPLY AND BATTERY AT STA 988, REF AMM 33-51-07-402-018-02. OPERATIONS CHECKS NORMAL, REF AMM 33-51-07-402-018-02.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 116,574 hrs · 18,056 cycles

REPLACE EMERGENCY LIGHT BATTERY PACK LOCATED BEHIND 40A AIR GRILL. REPLACED BATTERY PACK 2013-1A, IAW AMM 33-51-03. OPERATIONS CHECKS NORMAL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 116,574 hrs · 18,056 cycles

REF AERSALE CID 513912. EMERGENCY LIGHT BATTERY PACK LOCATED BEHIND CEILING PANEL AT ROW 20ABC HAS NO CHARGE, REF AERSALE CID 513912. REPLACED EMERGENCY LIGHT BATTERY PACK, IAW AMM 33-51-07. OPERATIONS CHECK GOOD, ADD EMP: V931306.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 116,574 hrs · 18,056 cycles

EMERGENCY LIGHT BATTERY PACK LOCATED ABOVE CEILING PANEL ABOVE ROW 1A HAS NO CHARGE. REPACKED AND OPERATIONAL CHECKED EMERGENCY LIGHT BATTERY PACK, IAW AMM 33-51-07. OPERATIONS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 116,574 hrs · 18,056 cycles

REF AERSALE CID 513924. EMERGENCY LIGHT BATTERY PACK LOCATED IN CEILING PANEL ABOVE ROW 2A HAS NO CHARGE, REF AERSALE CID 513924. EMERGENCY LIGHT BATTERY PACK REPLACED AND OPERATIONS CHECKED, IAW AMM 33-51-07. OPERATIONS CHECKED GOOD. WORK ACCOMPLISHED BY V931299 AND INSP BY ASI QC 50 ADD EMP: V931299.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 116,574 hrs · 18,056 cycles

EMERGENCY LIGHT BATTERY PACK AT L1 DOOR F/A SEAT HAS NO CHARGE, REPLACED AND OPERATIONAL CHECKED EMERGENCY LIGHT BATTERY PACK, IAW AMM 33-51-07. OPERATIONS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 116,574 hrs · 18,056 cycles

REF AERSALE CID 513914. EMERGENCY LIGHT BATTERY PACK BEHIND AIR GRILL AT SEAT ROW 21 A HAS NO CHARGE, REF AERSALE CID 513914. REPLACED BATTERY PACK AT SEAT ROW 21A, IAW AMM 33-51-07. OPERATIONS CHECK GOOD.

Part: FUEL CAP — LEAKING (LT WING) · airframe 115,527 hrs · 17,893 cycles

FUEL LEAKING FROM OVERWING FUEL CAP ON LEFT WING. AFTER REMOVING CAP FOUND 70 OF PAINT MISSING FROM FLANGE. CLEANED AND REMOVED ALL PAINT FROM FLANGE, INSTALLED NEW CAP IAW AMM 28-11-04. P/N 38222-3. FUELED LEFT WING TO 40,000 POUNDS, NO LEAKS OBSERVED. A/C OK TO CONTINUE IN SERVICE.

Part: FUEL CAP — LEAKING (LT WING) · airframe 115,271 hrs · 17,857 cycles

FUEL LEAK OBSERVED DURING FLIGHT FROM TOP OF LEFT WING. CAPTAIN TOOK PHOTO DURING FLIGHT SHOWING FUEL COMING FROM LH WING UPPER SURFACE IN THE AREA OF THE OVERWING FUEL CAP. INSPECTED CAP ORING- FOUND INTACT BUT QUITE COMPRESSED. A/C AOG AWAITING NEW CAP FROM LHR. FITTED LH OVERWING FILL CAP IAW AMM 28-11-04 REV 128. P/N 38222-3 M/E 19-2811-3-0007. REFUELED LH WING TO 40700LBS, NOTING GREATER THAN 39,700LBS, REQUIRED TO LEAK CHECK OVERWING CAP. NO LEAKS OBSERVED. A/C OK FOR CONTD SERVICE.

Part: SHUTOFF VALVE — LEAKING (BLEED AIR SYS) · airframe 112,153 hrs · 17,433 cycles

L STRUT DCT LEAK EICAS BLEED VALVE SHUT OFF AS EXPECTED AND CHECKLIST COMPLETED FOUND DUCT LEAK COMMING FROM PRSOV IN LEFT STRUT. REPLACED NR 1 ENG PRSOV PER MM 36-11-09. NEEDS HIGH POWER RUN. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1209042 SN OFF 0010 VALVE, PRES REG OFF 76-3612-9-0002 0010 ON 76-3612-9-0002 3153 PERFORMED 6MIN HIGH POWER RUN, ALL PARAMETERS AND INDICATIONS NORMAL. OK FOR SERVICE.

Part: LENS — MISSING (EXIT SIGN) · airframe 110,902 hrs · 17,272 cycles

OVERHEAD EMERGENCY EXIT SIGN AT ROW 10 RT CABIN HAS THE AFT BLANK LENS ASSY MISSING INSTALLED NEW LENS BLANK ASSY ON AFT FACING CEILING LIGHT FITTING REF IPC 33-51-01-46. IDT RAISED FOR INSPECTION ACP IDT INSPECTION OF EMERGENCY EXIT SIGN PER GMM 09-10-05 & REF IPC 33-51-01-46.

Part: ADC — INOPERATIVE (COCKPIT) · airframe 110,743 hrs · 17,251 cycles

CLMBNG THRU FL240 ALL CA ADC DRIVEN INTSRS FAILED ADC DRIVEN INT SRS FAILED INCL AS/MACH ALT ALT ADC L WAS REPLACED AND INSTALLED IAW AMM 34-12-01-404-006 AND TE ST 30 ACCOMPLISHED SUCCESSFUL, OK FOR SERVICE. ADDING PARTS INFORMATION ROTABLE PARTS CHANGE WAS INDICATED - TT 1319013 SN OFF 9509 IPC REFERENCE 34-12-01-01 COMPUTER, AIR D OFF 76-4113-9-0001 0922 ON 76-4113-9-0001 9509.

Part: SKIN — NOT REPORTED (FUSELAGE) · airframe 110,299 hrs · 17,192 cycles

STA 1329 STR 33L-35L SKIN REPAIR REQUIRE REPAIR DOUBLER -4 MODIFIED TO PICK UP ONE ADDITIONAL FASTENER AT S35L FX SKIN AT STA 1320-1337 AS PER ECRA 5331-02253 REV-.

Part: TEAR STRAP — DEFORMED (FUSELAGE) · airframe 110,296 hrs · 17,191 cycles

STA 1329 PREVIOUSLY DOUBLER REMOVED FOUND STA 1329 STR 34L-35L TEAR STRAP DEFORMED STA 1329 STR 31L TO STR 36L REPAIRED TEAR STRAP AS PER ECRA 5331-02253 REV - AND ATTACHED FORM 44.0008 ITEM 1-26 ACCOMPLISHED.

Part: FLOOR SUPPORT — CRACKED (BS 995-999) · airframe 110,296 hrs · 17,191 cycles

LBL 33 FLOOR SUPPORT WAS FOUND CRACKED CABIN BS 955 TO 999. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 53-00-51, REPAIR 3, FIG 201.

Part: STIFFENER — DEFORMED (BS 967 BULKHEAD) · airframe 110,296 hrs · 17,191 cycles

BS 967, LBL 67, CANTED PRESSURE WEB STIFFENER WAS FOUND DEFORMED. THE STIFFENER WAS REPAIRED IAW SRM 51-70-12, FIG 1.

Part: FLOOR SUPPORT — CRACKED (BS 780) · airframe 110,296 hrs · 17,191 cycles

FLOOR SUPPORT, BS 780, LBL 11, WAS FOUND CRACKED. REPAIRED THE FLOOR SUPPORT IAW SRM 53-00-51, REPAIR 3, FIG 201.

Part: STIFFENER — DEFORMED (BS 967) · airframe 110,296 hrs · 17,191 cycles

BS 967, LBL 67 CANTED PRESSURE WEB STIFFENER WAS FOUND DEFORMED. THE STIFFENER REPAIRED IAW SRM 51-70-12, FIG 1.

Part: FLOOR SUPPORT — CRACKED (BS 995-999) · airframe 110,296 hrs · 17,191 cycles

FLOOR SUPPORT WAS FOUND CRACKED, BS 955 TO 999, LBL 33, FLOOR SUPPORT WAS REPAIRED IAW SRM 53-00-51, REPAIR 3, FIG 201.

Part: FLOORBEAM — CRACKED (BS 780) · airframe 110,296 hrs · 17,191 cycles

BS 780, LBL 11 FLOOR BEAM WAS FOUND CRACKED. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, REPAIR 3, FIG 201.

Part: WEB — CORRODED (BS 1267) · airframe 110,296 hrs · 17,191 cycles

BS 1267, RBL 95, RT FLOOR SUPPORT WEB WAS FOUND CORRODED. THE WEB WAS REPLACED IAW SRM 51-10-02, AND FASTENER INSTALLED IAW SRM 51-40-02.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 108,659 hrs · 16,965 cycles

CLIMBING THRU 5000 FEET RECEIVED A FLAPS EICAS, CONFIG LIGHT, MASTER WARNING AND AURAL WARNING. SPD LIM IN AMBER AT BOTTOM OF SPEED TAPE. EMERGENCY DECLARED. PERFORMED RESISTANCE AND INDUCTACE CHECKS ON PROXIMITY SENSORS S244 AND S266 IAW AMM 32-61-99-706-113, STEP E(2). RESISTANCE S244: 18.2 OHMS; S266: 18.46 OHMS. ACCOMPLISHED FULL STRUT SERVICE IAW AMM 12-15-02. ACCOMPLISHED WARNING SYSTEM TEST IAW AMM31-51-00, ALL TESTS NORMAL NO FAULTS NOTED. ACCOMPLISHED TCAS BITE IAW FIM34-45 TASK 807 AND AMM34-45-00, NO FAULTS NOTED. ACCOMPLISHED STALL WARNING TEST IAW AMM 27-32-00, ALL INDICATIONS NORMAL.

Part: RELAY — FAULTY (ELECTRICAL PANEL) · airframe 108,642 hrs · 16,961 cycles

INTEGRAL LIGHTING ON THE FUEL PANEL EQUIPMENT COOLING PANEL AND PANEL/ FLOOD FLICKERING ON/OFF. EMERGENCY DECLARED. REPLACED RELAY K755. REF WDM 33-13-16. OPS CK NORMAL

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 108,590 hrs · 16,953 cycles

CLIMBING THRU 10K FT, SUDDEN DRAMATIC CHANGE IN NOISE LEVEL, VERY LOUD WIND SOUND WITH LANDING GEAR MONITOR. AIRCRAFT DID NOT PRESSURIZE NORMALLY. EMERGENCY DECLARED. REPLACED CABIN PRESSURE PANEL ASSY IAW AMM 21-31-01. REPLACED THE OUTFLOW VALVE IAW AMM 21-31-03, ALL OPS AND TESTS SATISFACTORY.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 108,577 hrs · 16,950 cycles

FA'S COMPLAINED OF LIGHT HEADED AND NAUSEA, ESP IN BUSINESS CLASS AND 1ST CLASS, ELT LACK OF AIRFLOW AND STRUGGLED WITH BALANCE ISSUES AND FELT THEY WERE IN A CONSTANT TURN, SEVERAL PAX COMPLAINED AS WELL. NO FUMES OR SMOKE WAS NOTED, PRESSURIZATION WAS ROUGH IN TURNS OR FEELING A RAPID DESCENT PRESS, UPON LANDING FA COMPLAINED EARS WERE POPPING IN FLIGHT. EMERGENCY DECLARED. REPLACED CABIN PRESSURE CONTROLLER AUTO 1 ALL OPS CHECKS SATIS REF 21-31-00. REPLACED AUTO CONTROLLER 2 REF AMM21-31-02-004-001 PG401 NO DEFECTS NOTED. BOTH RECIRC FILTERS REMOVED AND REPLACED PER AMM 21-25-02. REPLACED OZONE CONVERTER LEFT REF AMM 21-51-22. REPLACED OZONE CONVERTER RT REF AMM 21-51-22 ALL SATIS.

Part: ALTIMETER — OUT OF TOLERANCE (STANDBY) · airframe 107,616 hrs · 16,811 cycles

AT FLIGHT LEVEL 350 THE STANDBY ALTIMETER SHOWS 35600 FEET PERFORMED STBY ALTIMETER CHECK BY PRESSURIZING PITOT/STATIC SYSTEM IAW AMM 34-11-00. FOUND STBY ALTIMETER STICKING 500'' INCREMENTS AT A TIME. REMOVED AND REPLACED STBY ALTIMETER IAW AMM 34-13-06. NO FURTHER DEFECTS NOTED.

Part: ALTIMETER — OUT OF TOLERANCE (COCKPIT) · airframe 107,545 hrs · 16,802 cycles

STANDBY ALTIMETER OFF BY 500FT AT CRUISE ON THE HIGH SIDE FROM BOTH L AND R ALTIMETERS AT 29.92. R&R STBY ALT REF AMM 34-13-06. OPS CHK GOOD. ACCOMPLISHED NON RII INSPECTION IAW GMM-09-10-05.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 106,196 hrs · 16,588 cycles

L2 DOOR SLIDE PSESSURE GUAGE READING SLIGHTLY LOW. REPLACED THE SLIDE IAW AMM 25-66-01-404-072 ,OPS CHECKED GOOD.

Part: ALTIMETER — MALFUNCTIONED (STANDBY) · airframe 106,196 hrs · 16,588 cycles

STANDBY ALTIMETER 500 FT OFF. READS 32500 WHEN LEVEL 32000 ALTITUDE WITHIN LIMITS PER FIM CHART FIM 34-13-00-990-805 ALTIMETER TOLERANCE CHART.

Part: ALTIMETER — INACCURATE (STANDBY) · airframe 105,800 hrs · 16,525 cycles

STANDBY ALTIMETER 100 FOOT HAND. LAGS BY 500 FEET IN CLIMB. DESCENT AND IN LEVEL FLIGHT. REPLACED STAND BY ALTIMETER IAW AMM 34-13-06, PG 401.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 105,178 hrs · 16,433 cycles

FOUND 20JK, 33JK, AND 37JK SEAT EMERGENCY LIGHTS INOPERATIVE. REPLACED THE LIGHTS AND TESTED NORMAL IAW CMM 25-24-68, REV 2.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 105,178 hrs · 16,433 cycles

EMERGENCY LIGHTS L329 & L738 FOUND INOPERATIVE. REPLACED THE FUSE AND TESTED NORMAL IAW AMM 33-51-00-715-001, REV 196.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 105,178 hrs · 16,433 cycles

EMERGENCY LIGHTS INOPERATIVE, RT SIDE FIRST AND BUSINESS CLASS. REPLACED THE BATTERY PACK AND FOUND NORMAL IAW AMM 33-51-07-422-007-002, REV 196 , AMM 25-25-06-701-801, REV 196, WDM 33-51-12-001, REV 132 & CMM 25-28-72, REV 5.

Part: LIGHT — DAMAGED (CABIN) · airframe 105,178 hrs · 16,433 cycles

EMERGENCY LIGHTS FAILED TEST. REPLACED THE LIGHT ASSY AND TESTED NORMAL IAW AMM 33-51-06-902-082, REV 196, & AMM 33-51-06-902-100, REV 196.

Part: FRAME — CRACKED (FUSELAGE) · airframe 105,178 hrs · 16,433 cycles

A CRACK WAS FOUND IN BS859.5 FRAME INNER CHORD FROM FASTENER HOLE NR 3 AS SHOWN IN "EN PAGE 4 " OF ECRA 5310-07087. REFERENCE ECRA 5310-07087 FOR A MORE DETAILED DESCRIPTION OF CRACK, INTERIM REPAIR ACP

Part: FRAME — CRACKED (BS 903) · airframe 105,178 hrs · 16,433 cycles

A CRACK WAS FOUND ON BOTH THE NR 1 & 5 HOLES AT BS 903.5 FRAME. REPAIRED. CONSIDERED A MAJOR REPAIR IAW ECRA 5310-07106.

Part: FLOORBEAM — CRACKED (BS 764) · airframe 105,178 hrs · 16,433 cycles

FOUND A CRACK IN THE BS 764 FLOORBEAM UPPER HORIZONTAL FLANGE AT LBL 30. REPAIRED IAW ECRA 5320-02762.

Part: FRAME — CRACKED (BS 859) · airframe 105,178 hrs · 16,433 cycles

A CRACK WAS FOUND ON THE NR 2 HOLE OF BS 859.5 FRAME. REPAIRED IAW ECRA 5310-0 7103.

Part: FRAME — CRACKED (FUSELAGE) · airframe 105,178 hrs · 16,433 cycles

WHILE WORKING EA 5310-05292 REV B OP10, A CRACK WAS FOUND IN BS 883.5 FRAME INNER CHORD EMANATING FROM FASTENER HOLE NR 4 AS SHOWN IN "EN PAGE 3" OF ECRA 5310-07095. REF ECRA 5310-07095 FOR A MORE DETAILED DESCRIPTION OF CRACK, INTERIM REPAIR ACP.

Part: FLOORBEAM — CORRODED (BS 287) · airframe 105,178 hrs · 16,433 cycles

CABIN FORWARD ZONE FLOORBEAM UPPER CHORD FOUND CORRODED AT BS 287, RBL 50 - 75 , REPAIRED THE FLOORBEAM UPPER TEE. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 105,178 hrs · 16,433 cycles

CORROSION FOUND ON MAIN DECK BS 325 FLOORBEAM UPPER SURFACE. CATEGORY "A" REPAIR ACCOMPLISHED WITHOUT DEVIATION. REPAIR IS A MAJOR REPAIR PER ECRA. NO FURTHER INSPECTIONS CALLED OUT IN ECRA 5320-02763.

Part: STRAP — CORRODED (FUSELAGE) · airframe 105,178 hrs · 16,433 cycles

FORWARD CARGO DOOR LOWER SILL LOWER FAILSAFE STRAP FOUND CORROSION AT ATTACHED ANCHOR NUT AREA . REPAIR ACCOMPLISHED WITHOUT DEVIATION. REPAIR CLASSIFIED AS MAJOR PER ECRA. NO FURTHER INSPECTION REQUIRED PER ECRA 5320-02760, REPAIR CONSIDERED A CATEGORY "A" REPAIR.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 105,178 hrs · 16,433 cycles

BOTH INNER AND OUTER SKIN OF LT WING OUTBOARD TRAILING EDGE FLAP UPPER PANEL 566KT (113T3140-25) WAS FOUND DELAMINATED. CATEGORY "A" REPAIR ACCOMPLISHED WITHOUT DEVIATION. REPAIR CONSIDERED A MAJOR REPAIR. NO FURTHER INSPECTION REQUIREMENTS PER ECRA 5750-04967.

Part: SOCKET — DEFECTIVE (CABIN) · airframe 104,700 hrs · 16,367 cycles

AFT LEFT DOOR SLIDE EMERGENCY LIGHT INOP. REPLACED THE SOCKET ASSY FOR L397 AFT L DOOR SLIDE LIGHT. OPS GOOD.

Part: CAP — FAILED (RT WING FUEL) · airframe 103,214 hrs · 16,152 cycles

ON ARRIVAL, CAPTAIN HAD SOME PHOTOS FROM FLIGHT WHICH CLEARLY SHOWED FUEL LEAKING FROM OVERWING REFUEL CAP. CAP REPLACED AND REFUEL CAP HOUSING INSPECTED WITH NO FAULTS EVIDENT, CAP REPLACED IAW MM28-11-04 AND TRANSFERRED 40,000LBS OF FUEL TO RIGHT WING FOR LEAK CHECK. WITH 40,000LBS IN TANK AND APU RUNNING FOR 30 MINUTES NO FUEL LEAK EVIDENT. LEFT 40,000 LBS FUEL IN TANK OVERNIGHT (12 HOURS) AND NO LEAK EVIDENT IAW MM 12-11-01/301.

Part: SKIN — DENTED (FUSELAGE) · airframe 99,430 hrs · 15,646 cycles

FUSELAGE SKIN STRINGER 21R, BS 355 SKIN DENT HAD AN INTERIM REPAIR ACCOMPLISHED IAW ECRA 5330-05077. VERIFIED DAMAGE REMOVAL, MANUFACTURED & INSTALLED DOUBLER & TRIPLER IAW SRM 53-10-01 REPAIR 1 DETAIL III & ECRA 5330-05239.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,430 hrs · 15,646 cycles

AFT PIT BILGE, FAIL SAFE STRAP AT STATION 1562 CORRODED BETWEEN STRINGER 39R & 39L. DAMAGE CUT OUT & REPAIR INSTALLED IAW ECRA 5362-1029.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,430 hrs · 15,646 cycles

AFT PIT FRAME STATION 1153, UPPER T CAP CORRODED ON UPPER FLANGE AT RBL 22.5. REPLACED UPPER T CAP IAW SRM 51 -40-02 PARA 70 FIG 12 & DWG 146T1204.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,430 hrs · 15,646 cycles

STATION 303 FLOORBEAM UPPER T CAP CORRODED AT RBL 55. CORRODED SECTION WAS CUT OUT & REPAIR INSTALLED FROM RBL 38 - 90 IAW SRM 53-00-51 FIG 201 REPAIR 1.

Part: BATTERY — DISCHARGED (CABIN) · airframe 99,429 hrs · 15,645 cycles

EMERGENCY EXIT FLOOR LIGHTS INOPERATIVE. AT AFT GALLEY, BETWEEN TWO AFT RT LAVATORIES, & DOOR 2 RT LOWER FWD EXIT SIGN. REPLACED BATTERY M1556 IAW MM 33-51-07. FLOOR EEL OPERATIONS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 99,429 hrs · 15,645 cycles

EMERGENCY EXIT SIGN INOPERATIVE, JUST AFT & ABOVE SEAT ROW 39 RT. REPLACED BATTERY & CHARGER ASSEMBLY REFERENCE SMC 5.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 99,429 hrs · 15,645 cycles

EMERGENCY EXIT LIGHT INOPERATIVE. DOOR 2 RT FWD SILL LIGHT. REPLACED CHARGER & BATTERY IAW AMM 33-51-07.

Part: BATTERY — DISCHARGED (CABIN) · airframe 99,429 hrs · 15,645 cycles

EMERGENCY EXIT LIGHTS INOPERATIVE. CEILING FROM SEAT ROW 29 RT TO AFT RT SIDE OF AFT GALLEY. REPLACED BATTERY & CHARGER ASSEMBLY REFERENCE SMC 5.

Part: BATTERY — DISCHARGED (CABIN) · airframe 99,429 hrs · 15,645 cycles

EMERGENCY EXIT SIGN INOPERATIVE. AFT GALLEY WALL UPPER RT EXIT SIGN. REPLACED BATTERY & CHARGER ASSEMBLY REFERENCE SMC 5.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 97,424 hrs · 15,361 cycles

AFT GALLEY FLOOR EMER EXIT LIGHT INOPERATIVE. SECURED CONNECTOR. AFT GALLEY FLOOR EMER EXIT LIGHT OPERATIONS CHECKED NORMAL.

Part: UNKNOWN — ODOR (CABIN) · airframe 96,014 hrs · 15,163 cycles

RETURN TO BLOCKS FOR AN ELEC ODOR IN THE CABIN.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 95,660 hrs · 15,115 cycles

EXTERIOR EMERGENCY LIGHT LT OVERWING EGRESS LIGHT JUST AFT OF WING IS INOPERATIVE. REPLACED BULB, NO HELP, RELAMPED.

Part: RIB — CRACKED (LT WING) · airframe 95,310 hrs · 15,067 cycles

IAW TASK CARD 656003110 LT WING LOWER RIB ASSEMBLY IS CRACKED. IAW IPC 57-51-52-05 ITEM 410, RIB ASSEMBLY. REMOVED DAMAGE, INSPECTED HFEC TRIM LINE, FABRICATED FILLER & PILOTED HOLES IAW SRM 51-70-12. CONT OF AMIS ITEM 3102041. ACCOMPLISHED HFEC INSPECTION OF EXISTING FASTENER HOLES IAW NDT NTM PART 6 51-00-16, CHECKED GOOD. CONT OF AMIS ITEM 3102053 REMOVED DAMAGE, ACCOMPLISHED TYPICAL EXTRUDED SECTION REPAIR IAW SRM 51-70-12.

Part: HOSE — LEAKING (POTABLE WATER) · airframe 94,813 hrs · 15,000 cycles

POTABLE LEAKING NO PRESS. HOSE REPLACED LEAK CHECKED OK FOR SERVICE.

Part: ACTUATOR — FAULTY (FUEL SYSTEM) · airframe 94,813 hrs · 15,000 cycles

FUEL CROSS FEED VLV LEFT ON & "FUEL CROSS FEED" EICAS MESSAGE DISPLAYED WHEN CROSS FEED SW OPEN OR CLOSED SELECTED. AFT FUEL CROSS FEED VLV IS UNUSUALLY SLOW TO OPERATE. REPLACED ACTUATOR IAW MM.

Part: LIGHT — INOPERATIVE (FIRE WARNING) · airframe 94,795 hrs · 14,997 cycles

AFT CARGO FIRE WARNING LIGHT DOES NOT LIGHT WITH A FIRE TEST.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 94,784 hrs · 14,993 cycles

LT FRONT CEILING EMERGENCY AISLE LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM & OPERATIONS CHECKED GOOD.

Part: SQUIB — FAULTY (EVAC SYSTEM) · airframe 94,784 hrs · 14,993 cycles

EMERGENCY ESCAPE SYSTEM FAILED TEST 2 AT P61 PANEL. R & R NR 7 SPOILER OVERRIDE ACTUATOR SQUIB IAW AMM 25-65-19 & PERFORMED SQUIB TEST IAW AMM 25-65-00 & TEST PASSED FOR TEST 1 & 2.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 94,784 hrs · 14,993 cycles

AFT CABIN LT & CTR LAVATORY EMERGENCY EXIT LIGHT STRIPS INOPERATIVE. R & R M1556 BATTERY PACK IAW AMM 33-51-10, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 94,784 hrs · 14,993 cycles

AFT SEATS 27 - 39 SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. LIGHT ASSEMBLY ON SEAT 32JK & 36JK & REPLACED LIGHT BULBS AT SEAT 39JK & 38AB, OPERATIONS CHECKED GOOD IAW MM 33-51-10.

Part: SPRING — MISSING (NLG) · airframe 94,783 hrs · 14,992 cycles

RT NOSE GEAR DOWN LOCK SPRING MISSING. REPLACED SPRING ASSEMBLY.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 94,592 hrs · 14,968 cycles

PIGTAIL P51 CONNECTOR FELL OFF. P51 CONTROLLER DEF INOPERATIVE. REQUIRES NEW PIGTAIL.

Part: WIRE — DAMAGED (GALLEY) · airframe 94,562 hrs · 14,964 cycles

FLIGHT ATTENDANT REPORTED RECEIVING SHOCKS FROM SEVERAL AFT GALLEY CARTS P51,P52, P53, P61 & P62. CHECKED GALLEY COUNTER TO GROUND, TESTED GOOD. CHECKED P51, P52, P53, P61 & P62, PIGTAILS FOR SHORTS TO COUNTER, FOUND NONE. FOUND PIGTAIL P53 WITH BAD LOCKING COLLAR, APPLIED MEL PULLED & COLLARED N53. SECURED P53 PIGTAIL. R & R PIGTAIL & RESET BREAKER.

Part: CONNECTOR — DAMAGED (LANDING GEAR) · airframe 94,452 hrs · 14,950 cycles

CONNECTOR D1942P PCN 563-1130 DAMAGED. NEEDS REPLACEMENT & TEST IAW 32-61-02 & WDM 32-61-12. R & R CONNECTOR D1942P & PERFORMED OPERATIONS CHECK IAW MM, OPERATIONS CHECKED GOOD.

Part: ACTUATOR — FAULTY (THRUST REVERSER) · airframe 94,436 hrs · 14,948 cycles

LT REVERSER WILL NOT DEPLOY PAST IDLE REVERSE ON LANDING. REPLACED LT INTERLOCK ACT IAW MM, OPERATIONS CHECKED NORMAL.

Part: SHUTOFF VALVE — FAULTY (BLEED AIR SYS) · airframe 94,404 hrs · 14,944 cycles

LT ENG HPSOV STATUS MESSAGE. R & R NR 1 ENG HPSOV IAW MM.

Part: SPRING — BROKEN (NLG) · airframe 94,404 hrs · 14,944 cycles

FOUND LT NLG BUNGEE SPRING BROKEN. REPLACED SPRING IAW MM.

Part: PDU — INOPERATIVE (AFT CARGO) · airframe 94,383 hrs · 14,941 cycles

AFT CARGO POWER DRIVE UNITS 10L AND 8L INOPERATIVE. REPLACED AFT CARGO POWER DRIVE UNITS 10L AND 8L PER AMM.

Part: REGULATOR — DISINTEGRATED (OXYGEN MASK) · airframe 94,326 hrs · 14,935 cycles

FIRST OFFICER`S OXYGEN MASK REGULATOR DISINTEGRATED. R & R FIRST OFFICER`S O2 MASK. LEAK & OPERATIONS CHECKED GOOD, IAW AMM-35-11-51. OK TO CONTINUE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 94,045 hrs · 14,899 cycles

EICAS MESSAGE SPOILERS DISPLAYED. SPOILER LIGHT ILLUMINATED WITH SPOILERS SELECTED UP. LIGHT STAYS ON WITH SPEED BRAKE STOWED. ACP TEST OF SCM 1R MODULE FAULTED PCA XDR 1 OR 12 INT CRUISE. ACP TEST OF SPOILERS ALL OPERATIONS & INDICATIONS NORMAL. TESTED ACP ON MODULE M533 AS PER MM.

Part: STEERING UNIT — FAULTY (SATELLITE SYS) · airframe 93,883 hrs · 14,878 cycles

REPLACED THE SATELLITE COMMUNICATIONS STARBOARD BEAM STEERING UNIT DUE TO SATELLITE DATA UNIT FAULT HISTORY ON NUMEROUS LEGS FOR 'HPR-STBD BSU'. REPLACED STARBOARD BEAM STEERING UNIT. AUDIO CONTROL PANEL INSTALLATION TESTED GOOD.

Part: AMPLIFIER — FAULTY (COCKPIT) · airframe 93,883 hrs · 14,878 cycles

REPLACED THE SATELLITE COMMUNICATIONS LOW GAIN AMPLIFIER M1783 DUE TO NUMEROUS FAULTS IN THE SATELLITE DATA UNIT FAULT HISTORY FOR 'LGA -HPA TX GAIN'. REPLACED LOW GAIN AUDIO MANAGEMENT PANEL, AUDIO CONTROL PANEL INSTALLATION TESTED GOOD.

Part: TRUCK — LEAKING (LT MLG) · airframe 93,761 hrs · 14,862 cycles

LEFT MAIN GEAR LEAKING UNKNOWN FLUID. REPLACED LT MAIN GEAR TRUCK POSITIONER, OPS CHECKED OK.

Part: COFFEEMAKER — SPARKS (GALLEY) · airframe 93,621 hrs · 14,844 cycles

M71 COFFEEMAKER SPARKING. CAPTAIN HAD CIRCUIT BREAKER PULLED. REPLACED COFFEMAKER.

Part: ACTUATOR — LEAKING (RUDDER) · airframe 93,270 hrs · 14,795 cycles

RUNNING HYDRAULIC LEAK OBSERVED FROM THE TAIL AREA. RT HYDRAULIC INDICATING 0.80. FOUND LOWER RUDDER PCA LEAKING. R & R LOWER PCA IAW AMM. RII PERFORMED.

Part: SHIELD — DAMAGED (NLG STEERING) · airframe 93,232 hrs · 14,791 cycles

NOSE GEAR STEERING FIBERGLASS COVER DAMAGE TO LOWER RT CORNER. R & R NOSE GEAR STEERING FIBERGLASS SHIELD.

Part: PAWL — DAMAGED (R1 DOOR HANDLE) · airframe 92,933 hrs · 14,756 cycles

R1 DOOR UNABLE TO OPEN FROM THE INSIDE OR OUTSIDE. HANDLE STUCK IN CLOSED, NOT MOVING. R & R SERVICE DOOR PAWL. OPERATION FROM INSIDE AND OUTSIDE WITH NO PROBLEMS.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 92,876 hrs · 14,750 cycles

FORWARD WINDSHIELD DELAMINATED ON F/O SIDE. INSTALLED R1 WINDOW IAW AMM 56-11-01.

Part: B-NUT — LEAKING (HYD SYSTEM) · airframe 92,866 hrs · 14,749 cycles

HYDRAULIC FLUID LEAKING FROM NR 2 ENGINE STRUT DRAIN. FOUND EVIDENCE OF FLUID IN STRUT AREA. FOUND LEAKING B-NUT AT PYLON AREA. TIGHTENED B-NUT AND RESERVICED SYS IAW MM AND ACCOMPLISHED LEAK CHECK IAW MM 29-00-98, OK.

Part: LATCH — WORN (OVERWING SLIDE) · airframe 92,714 hrs · 14,730 cycles

LEFT SIDE OVERWING SLIDE DOOR HAS A WORN LATCH SLIDER. REPLACED LATCH.

Part: PUMP — INOPERATIVE (HYD SYSTEM) · airframe 92,714 hrs · 14,730 cycles

LEFT ELECTRIC DEMAND PUMP INOPERATIVE IN AUTO AND ON. REPLACED LEFT ELECTRIC PUMP.

Part: SEAL — MISSING (RT PYLON) · airframe 92,511 hrs · 14,704 cycles

A SIX INCH RUBBER SEAL MISSING FROM RIGHT ENGINE INBD PYLON WING ROOT. REPLACED SEAL.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 92,443 hrs · 14,696 cycles

NR 1 ENGINE HYDRAULIC PUMP FOUND LEAKING FLUID. REPLACED EDP PER MM AND CASE DRAIN AND PRESSURE FILTERS PER MM. TEST E AND LEAK CHECKED NORMAL.

Part: VALVE — FAILED (EQUIP COOLING) · airframe 92,392 hrs · 14,689 cycles

EQUIPMENT COOLING 'VALVE' LIGHT ILLUMINATED. 'STBY' SELECTED & 'VALVE' LIGHT REMAINED ILLUMINATED. FOUND FORWARD OVERBOARD VALVE UNSERVICEABLE. REPLACED VALVE PER MM 21-23-08.

Part: VALVE — FAILED (COOLING) · airframe 92,225 hrs · 14,665 cycles

FWD EQUIPMENT VALVE EICAS ON LANDING. AFTER TROUBLESHOOTING FOUND INBOARD SUPPLY VALVE V91 FAULTY. REPLACED EQUIPMENT COOLING VALVE, OPS CHECK GOOD.

Part: DOOR — BROKEN (WS 306) · airframe 92,079 hrs · 14,646 cycles

FIXED LEADING EDGE ICE DOOR AT WS 306, BENEATH LEFT KRUEGER FLAP, BROKEN IN HALF. REMOVED AND REPLACED ICE DOOR AT WS 306.

Part: CONTROL VALVE — FAULTY (RT A/C PACK) · airframe 92,046 hrs · 14,641 cycles

RIGHT A/C PACK OFF LIGHT ILLUMINATED IN AUTO AND STDBY NORMAL. RESETS BUT THEN TRIPS OFF IN BOTH. REPLACE RT A/C PACK TEMP CONTROL VALVE PER MM.

Part: SKIN — TORN (NR 2 PYLON) · airframe 91,101 hrs · 14,504 cycles

NR 2 ENGINE OUTBOARD PYLON FAIRING SKIN TORN 45 DEG APPROX 2.5" X 2.5" AT STN 237 BELOW PANEL 447ERX. ACCOMPLISHED INTERIM REPAIR AS PER ECRA 5453-01057. REMOVED DAMAGED AREA AND PERFORMED COMPOSITE REPAIR TO PANEL REF. ECRA 5453-01057 AND SRM 51-70-10.

Part: SKIN — GOUGED (FUSELAGE) · airframe 90,922 hrs · 14,481 cycles

DURING WALKAROUND MECH NOTICED A GOUGE ON FUSELAGE AFT OF AFT PIT DOOR ON RT SIDE. GOUGE IS 2 INCH LONG AND 0.005 DEPTH, LOCATED ON STA 1351, BETWEEN S29 AND S30 AND 3-4 OFF AN INCH FROM THE CARGO DOOR OPENING, PER LOCAL MECHANIC. DAMAGED AREA BLENDED AND VISUAL INSP CARRIED OUT FOR FURTHER DAMAGE. NONE FOUND. SKIN LOSS 0.005IN, WITHIN SRM LIMITS REF SRM 53-00-01-TABLE 1 PG 102.

Part: COMPUTER — FAULTY (LT EICAS) · airframe 90,748 hrs · 14,459 cycles

LEFT EICAS COMPUTER EICAS MESSAGE. REPLACED EICAS COMPUTER PER MM, OPS CHECKED OKAY.

Part: ENGINE — FAULTY (NR 2) · airframe 90,290 hrs · 14,391 cycles

DUE TO PREVIOUS HISTORY OF RIGHT ENGINE HPSOV MSGS, PERFORM PNEUMATIC HEALTH CHECK OF THE HPSOV-HPC. PER MM 36-00-99-PG 514, STEP C. PAY PARTICULAR ATTENTION FOR SENSE LINE LEAKS. CORRECT ANY DISCREPANCIES FOUND. REMOVED ACCT ECM. REPLACED #2 ENGINE.

Part: LATCH — BROKEN (THRUST REVERSER) · airframe 90,197 hrs · 14,378 cycles

RIGHT ENGINE REVERSER BAND LATCH INBOARD SIDE BROKEN OFF. REPLACED I/B BAND AND LATCH ASSY ON NR 2 ENGINE IAW AMM.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 90,162 hrs · 14,372 cycles

LEFT WING SLIDE EICAS MESSAGE DISPLAYED MOMENTARILY. INSPECTION DOOR COMPARTMENT FOR FAIR, NO ANOMALIES. SQUIB CHECK GOOD. CHECKED DOOR SECURITY.

Part: APU — FAULTY (APU BAY) · airframe 90,088 hrs · 14,361 cycles

APU AUTO SHUTDOWN, FLT DIVERTED. REPLACED APU FMU. PREVIOUS HISTORY. ACP ECU BITE FOUND AUTO SHUTDOWN LOP MESSAGES. DURING LEAK CHECKS FOUND FMU ATTACHMENT FLANGE CASTING LEAKING UNDER PRESSURE FROM HAIRLINE CRACK. REPLACED APU. OPS CHECK, LEAK CHECK NORMAL. REPLACED APU. OPS CHECKS GOOD.

Part: FMU — LEAKING (APU) · airframe 90,088 hrs · 14,361 cycles

APU FMU REQUIRES REPLACEMENT FOR TROUBLESHOOTING OF OIL LEAK. REPLACED APU FMU. ACCOMPLISHED ECU BITE FOUND AUTO SHUTDOWN LOP MSGS. DURING LEAK CHECKS FOUND FMU ATTACHMENT FLANGE CASTING LEAKING UNDER PRESSURE FROM HAIRLINE CRACK. UNABLE TO LOCATE IN IPC ENGINEERING ASSISTANCE REQUIRED. NBRS ON CASTING 99193-3880133-3 OR MFR 5V132 OR CDA-81833. REPLACED APU. OPS CHECK, LEAK CHECK NORMAL.

Part: ENGINE — SURGES (NR 2) · airframe 90,055 hrs · 14,356 cycles

ENGINE SURGE, RETURNED TO FIELD. ENGINE SHUTDOWN 15-20 MINUTES FROM LANDING. METAL FOUND NR 2 ENG TAILPIPE. REPLACED NR 2 ENG.

Part: BRAKE — FIRE (NR 4) · airframe 90,055 hrs · 14,356 cycles

NR 2 ENGINE EEC ISSUE, RTFL SMALL FIRE REPORTED FROM NR 4 BRAKE ASSY, COCKPIT INDICATION 9 UNITS, FUSE DID NOT MELT. REPLACED NR 4 REAR BRAKE ASSY REF MM DUE TO OVERHEAT AND REPORTED BRAKE FIRE.

Part: TIRE — FAILED (NR 3) · airframe 89,845 hrs · 14,327 cycles

NR 3 FWD TIRE WITH TREAD SEPARATION DUE TO RAN FLAT. REPLACED TIRE IAW AMM.

Part: CONNECTOR — DIRTY (LT VSI) · airframe 89,806 hrs · 14,323 cycles

OFF FLAG IN CAPTS VSI. LEFT VSI ELECTRICAL CONNECTOR CLEANED. LEFT AND RIGHT VSI INSTALLATION TEST CARRIED OUT SATISFACTORY AS PER AMM. NO FURTHER FLAGS DISPLAYED.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 89,700 hrs · 14,307 cycles

EMERGENCY LIGHT CONNECTOR BROKEN AT SEAT 36B. REPAIRED EMERGENCY LIGHT CONNECTOR AT SEAT 36B. OPS CHECKED GOOD.

Part: ENGINE — FAILED (LEFT) · airframe 89,673 hrs · 14,302 cycles

AFTER TAKE OFF HEAVY VIBRATION 5.0 UNITS ENG1 SN.727667, THROTTLE PULLED BACK TO IDLE POWER TILL LANDING, FOUND EXTENSIVE DAMAGE TO SEVERAL FAN BLADES, INLET COWL, EXIT GUIDE VANES. NR 1 ENGINE HAS DAMAGE TO FAN EXIT OUTER CASE ALUMINIUM CASTING DAMAGED ON FLANGE AREA ADJACENT TO FAN EXIT GUIDE VANE PLATFORM & LOCATED BETWEEN 8 AND 9 OCLOCK POSITION. DAMAGE MEASURES APPROX 1.75" CIRCUMFERENTIALLY BY 0.25" WIDE AND IS A MAX DEPTH OF 0.080" DEEP. ITEM CFD PER ECRA 7233-01 253 AND REQUIRES REPLACEMENT WITHIN 5 CYCLES. CLEANED AREA. REPLACED NR 1 ENGINE.

Part: TRANSMITTER — FAILED (HYD SYSTEM) · airframe 89,646 hrs · 14,297 cycles

TROUBLESHOT C HYD PRIM 1 INTERMITTENT EICAS MESSAGE ON SHORT FINAL, GEAR DOWN AND DURING TAXI TO GATE. FOUND NO ACTIVE MESSAGE. REF SCHEMATIC 29-00-04. MESSAGE GENERATED FROM S33. PRESSURE TRANSMITTER REPLACED, CHECKED GOOD.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 89,195 hrs · 14,235 cycles

L1 DOOR LOWER EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE WHEN TESTED. LIGHTS OPS CHECKED NORMAL IAW 33-55-00-715-802.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 89,195 hrs · 14,235 cycles

TWO OVERWING EXTERIOR EMERGENCY LIGHTS ONE RT AND LT FORWARD OF AFT EMERGENCY LIGHTS ARE INOPERATIVE. RELAMPED, OPS CHECKED OK.

Part: LINE — LEAKING (LH HYD SYS) · airframe 89,037 hrs · 14,212 cycles

HYD FLUID LEAKING FROM THE LT MLG TRUCK POSITIONING ACTUATOR HOSE. APPROXIMATELY 12 DROPS PER MINUTE. REPLACED LINE PER AMM.

Part: HINGE — LOOSE (OXYGEN MASK DOOR) · airframe 88,995 hrs · 14,207 cycles

OXYGEN MASK HANGING DOWN OVER FC FLIGHT ATTENDANT JUMPSEAT. FOUND PANEL HINGE LOOSE FROM PANEL. REGLUED PANEL PER B767 AMM. STOWED MASKS AND CLOSED PANEL. OK NOW.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 88,591 hrs · 14,153 cycles

4TH EMERGENCY OVERWING EGRESS LIGHT AFT ON LEFT SIDE IS INOPERATIVE. RELAMPED AND SECURED CENTER CONTACT LUG. OP CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,591 hrs · 14,153 cycles

THE 4TH EMERGENCY OVERWING EGRESS LIGHT AFT ON LEFT SIDE IS INOP. RELAMPED, NO HELP. CENTER CONTACT SPRING IS SHOT. NEEDS LIGHT ASSY. NON-STOCK P-N S283T008-45.

Part: LIGHT — BROKEN (CABIN) · airframe 88,591 hrs · 14,153 cycles

DOOR INTERIOR EMERGENCY EXIT LIGHTS THAT SHINES DOWN ON HANDLE IS BROKEN. REPLACED LIGHTS. OPS CHECKED GOOD.

Part: GROUND WIRE — UNSECURE (EQUIPMENT COOLIN) · airframe 88,544 hrs · 14,146 cycles

EQUIPMENT COOLING FAULT ON TAXI OUT. FWD EQUIPMENT VALVE MESSAGE DISPLAYED. SECURED GROUND WIRE AND FAULT CLEARED. SYSTEM OPS CHECKED GOOD.

Part: SHUTOFF VALVE — FAULTY (APU) · airframe 88,491 hrs · 14,140 cycles

NO APU BLEED AIR FOR CABIN APU RUNS ELECT OKAY. REPLACED BLEED VALVE, NO HELP. ACP'D MEL REQUIREMENTS. REPLACED APU SHUTOFF VALVE AND FLOW CONTROL VALVE PER MM. RESET APU CONTROLLER, OPS NORMAL.

Part: CONNECTOR — LOOSE (LT ENGINE) · airframe 88,184 hrs · 14,098 cycles

REF DF 391, LOG12, LOG15 ALL HAVE HISTORY AFT ENG REMOVED AT TPA, HAVE L-R PIMU BITES L ENG TAI HAS HISTORY, L ENG VIB HAS HISTORY, BOTH EEC HAS FAULTS BIT L PIMU FAULTING EEC -PIMU MODE DISAGREE, EEC CHA A&B CAT2, EEC CHA A&B EXTERNAL-DIS DISAGREE, EEC CHA A&B TMC I-F, EEC CHA A&B TRA RNG FAIL BY- 94681 FOUND LT ENG FIREWALL CONNECTOR D04224P ONLY ON ONE TURN, SECURED CONN AND ACP'D MCDP TEST 1, 2, 4, 10, 30, 40 ALL PASSED, RETURNED TO CAT 3 STATUS.

Part: PRESSURE SWITCH — FAULTY (FUEL SYSTEM) · airframe 88,161 hrs · 14,092 cycles

BSTR PUMP LOW PRESS LT-OFF-,SW-OFF-, NO EICAS MSG. POSITION 5 (5=L FWD, 6=L AFT,9=R FWD,10=R AFT).I CENTER BOOST PUMP INOP L-. REPLACE L FWD PUMP PRESSURE SWITCH PER MM, OPS NORMAL.

Part: ACTUATOR — FAULTY (SPOILER) · airframe 88,158 hrs · 14,091 cycles

SPOILER 2 FLOAT WITH RIGHT HYD SYS OFF-REFLY. REMOVED AND REPLACED NR 2 SPOILER PCA IAW MM. LEAK AND OPERATIONAL CHECK GOOD IAW MM.

Part: SWITCH — FAULTY (RAT) · airframe 88,158 hrs · 14,091 cycles

AFTER APU START AT FL350, EICAS RAT UNLOCKED LIGHT ILLUMINATED. SUSPECT RAT DOOR SLIGHTLY OPEN WITH POWER TRANSIENT. NO VIBRATION FELT. REFLY. RMV'D & RPLC'D S369 RAT UP LIMIT SWITCH PER MM. OPS CHECKED GOOD PER MM.

Part: HOUSING — DEFECTIVE (FUEL TANK) · airframe 88,155 hrs · 14,090 cycles

RIGHT FORWARD BOOST PUMP INOP IN RIGHT MAIN FUEL TANK. REPLACED RIGHT MAIN BOOST PUMP HOUSING AND FWD AND AFT BOOST PUMPS OPS CHECK AND LEAK CHECK GOOD.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 88,155 hrs · 14,090 cycles

FWD CARGO STA 560, RBL 18 CORROSION ON 'C' CHANNEL. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW 'C' CHANNEL BETWEEN STA 540 - 560, RBL 18.

Part: STRAP — DAMAGED (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

RT FAILSAFE STRAP AT STA 955 FAILED ULTRA-SOUND TEST. ACCOMPLISHED COA 618451 RT STA 955 FLSF STRP RWK (SB 767-53A100 REV 1).

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

STA 1809.5 AFT BULKHEAD TO STR ATTACH FITTING CRACKED AT STR 36L. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED AFT END ATTACH FITTING.

Part: ATTACH FITTING — BENT (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

FRAME 1809.5 FWD ATTACH FITTING BENT AT STR 36L. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW ATTACH FITTING.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

STR 36R CRACKED AT STA 1809.5 FRAME ATTACH FITTING. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

STA 32L CRACKED AT STA 1809.5 ATTACH FITTING. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

STR 36L CRACKED AT STA 1809.5 FRAME ATTACH FITTING. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

FUSELAGE SKIN FWD OF STA 1809.5 TO STA 1767 DAMAGED BUCKLED STR 39R - 26R. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FILLER, DOUBLER, AND TRIPLER.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

STR 39R CRACKED AT STA 1809.5 FRAME ATTACH FITTING. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER.

Part: ATTACH FITTING — BENT (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

FRAME 1809.5 FWD ATTACH FITTING BENT AT STR 36R. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW ATTACH FITTING.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

FUSELAGE SKIN FWD OF STA 1809.5 TO STA 1767 DAMAGED BUCKLED FROM STR 39L - 26L. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FILLER, DOUBLER AND TRIPLER.

Part: ATTACH FITTING — BENT (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

FRAME 1809.5 FWD ATTACH FITTING BENT AT STR 39R. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW ATTACH FITTING.

Part: ATTACH FITTING — BENT (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

FRAME 1809.5 ATTACH FITTING BENT AT STR 32L FWD. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW ATTACH FITTING.

Part: ATTACH FITTING — BENT (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

FRAME 1809.5 FWD ATTACH FITTING BENT AT STR 39L. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW ATTACH FITTING.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

STR 39L CRACKED AT STA 1809.5 FRAME ATTACH FITTING. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER AND END FITTING.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

FUSELAGE SKIN FWD OF STA 1809.5 TO STA 1767 DAMAGED BUCKLED FROM BL 0 STR 39L - 39R. REPLACED CENTER SKIN.

Part: ATTACH FITTING — BENT (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

FRAME 1809.5 ATTACH FITTING TO STR 36R BENT. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER END FITTING.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

STA 1809 BULKHEAD RIGHT SIDE INBOARD HORIZ HINGE DEFECT INDICATION NOTED ON 2 EA HOLES, 1 LOCATED ON HINGE SECOND ONE DOWN AND 1 LOCATED ON BRACE FIRST INBOARD HOLE. RESULTS FROM NDT, RMV'D FASTENERS, REAMED HOLES, ACCOMP NDT NO CRACKS NOTED, INSTALLED NEW FASTENERS.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

STA 1809.5 AFT BULKHEAD STIFFENER CRACKED BENT AT LBL 8. RMV'D AND RPL'D AFT BULK HEAD STIFFENER AT STA 1809.5, LBL 8.

Part: BULKHEAD — BENT (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

STA 1809.5 AFT BULKHEAD WEB CREASED BENT AT STR 36L TO 36R. MAJOR REPAIR ACCOMPLISHED. RMV'D AND RPL'D STA 1809.5 AFT LWR BULKHEAD WEB.

Part: DISPLAY — INOPERATIVE (COCKPIT) · airframe 88,155 hrs · 14,090 cycles

P-R LOWER ECAM AND F/O DISPLAY UNIT NOT OPERATING. RMV'D & RPLC'D LOWER ECAM DISPLAY UNIT.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

STA 1809.5 AFT BULKHEAD STIFFENER CRACKED, BENT AT RBL 8. MAJOR REPAIR ACCOMPLISHED. RMV'D AND RPL'D AFT BULKHEAD STIFFENER STA 1809.5.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

STA 1809.5 AFT BULKHEAD STIFFENER CRACKED, BENT AT BL 0. RMV'D AND RPL'D AFT BULKHEAD STIFFENER STA 1809.5, BL 0.

Part: FRAME — BENT (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

STA 1725.5 FRAME CHORD BENT-PUSHED IN FWD SIDE OF FRAME STR 30L. REPAIRED FRAME CHORD AT STA 1725.5, STR 30L.

Part: FASTENER — LOOSE (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

STA 1725.5 FRAME FWD SIDE OF FRAME STR 30L HAS RIVETS LOOSE, PUSHING ON ATTACH FITTING. REMOVED FASTENERS AT STA 1725.5, STR 26L AREA, ACCOMPLISHED NDT OF HOLES NO CRACKS NOTED, INSTALLED NEW FASTENERS.

Part: FRAME — BUCKLED (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

FRAME 1809.5 SKIN CHORD BUCKLED FROM STR 36L - 36R. RMV'D AND RPL'D FRAME STA 1809.5.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

FRAME 1809.5 BULKHEAD BENT-BULGED FWD SIDE ABOVE STR 36L - 36R. RMV'D AND RPL'D FRAME FWD CHORD.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

HOLE ELONGATED ON 1809 BULKHEAD LT SIDE CUTOUT AT APPROXIMATELY LBL 27, 15TH HOLE FROM TOP OF LT CUTOUT. RMV'D FASTENER, REAMED HOLE, ACCOMP NDT NO CRACKS NOTED, INSTALLED NEW FASTENER.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

STA 1725.5 EXTERNAL SKIN TORN-BENT AT LAP JOINT AND BUTT JOINT STR 32L. ACCOMPLISHED EXTERNAL SKIN REPAIR PER ECRA 5380-01078.

Part: SKIN — CORRODED (BS 1544, BL 0) · corrosion level 2 · airframe 88,155 hrs · 14,090 cycles

AFT OF CARGO BAY AT BS 1544, BL 0 INTERNAL SKIN IS CORRODED AROUND DRAIN VALVE. MAJOR REPAIR ACCOMPLISHED, REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS OF SRM. TRIMMED OUT DAMAGE AND ACCOMPLISHED NDT OF REPAIR AREA AND OPEN HOLES FOR CRACKS. NONE FOUND. FABRICATED AND INSTALLED DOUBLER AND TRIPLER REPAIR.

Part: SLIDE — UNWANTED DEPLOY (L2 DOOR) · airframe 88,155 hrs · 14,090 cycles

DURING MANUAL OPERATION OF THE DISARM FEATURE FROM THE EXTERNAL HANDLE OF THE L2 DOOR IAW TASKCARD 683301410, THE SLIDE DEPLOYED. REMOVED AND REPLACED SLIDE ASSEMBLY REF AMM. OPS CHECKED GOOD.

Part: FAILSAFE — DAMAGED (BS 955) · airframe 88,155 hrs · 14,090 cycles

LEFT BS 955 FAILSAFE STRAP DAMAGED. ACCOMPLISHED SMC038 FAILSAFE STRAP REWORK ON TASKCARD 3872N00714.

Part: FAILSAFE — DAMAGED (BS 955) · airframe 88,155 hrs · 14,090 cycles

RIGHT BS 955 FAILSAFE STRAP DAMAGED. ACCOMPLISHED REPAIRE ON FAILSAFE STRAP ON TASKCARD 3872N00715.

Part: FLOOR SUPPORT — CORRODED (BS 1510) · corrosion level 2 · airframe 88,155 hrs · 14,090 cycles

AFT LEFT ENTRY DOOR HAS CORROSION INBD OF THRESHOLD ON FLOOR SUPPORT AT BS 1510. FABRICATED AND INSTALLED FILLERS, ANGLE AND PLATE PER ECRA 5360-01178 AND EA PD67- 53-045.

Part: GUARD — CORRODED (L2 DOOR) · corrosion level 2 · airframe 88,155 hrs · 14,090 cycles

L2 DOOR SPLASH GUARD CORRODED AT THE DOOR SILL. FABRICATED AND INSTALLED FILLERS, ANGLE AND PLATE PER ECRA 5360-01178 AND EA PD67- 53-045.

Part: SLIDE — UNSERVICEABLE (CABIN) · airframe 88,155 hrs · 14,090 cycles

LEFT WING OW SLIDE INFLATION HOSE KINKED AND TWISTED OUT OF LIMITS. REMOVED & REPLACED LEFT OVERWING SLIDE.

Part: WIRE — BROKEN (CARGO BAY) · airframe 88,155 hrs · 14,090 cycles

CARGO FIREX BOTTLE 1 AND 2 FAILS, DOES NOT SHOW ON EICAS. NO EICAS CARGO BOTTLE 2 LIGHT. RE-TERMINATED BROKEN WIRE AT D5673P PER SWPM 20-61-16, OPS CHECK GOOD PER AMM 26-23-00 AND TC 612224910.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 88,155 hrs · 14,090 cycles

PASS CABIN FLOOR STRUCTURE AT STA 347, LBL 43 - 49 FLOORBEAM IS CORRODED. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE, FABBED AND REPLACED T-CAP, 2 ANGLES, AND STRAP REPAIR PER SRM 51-40-02 ON NR 3872N00516.

Part: STIFFENER — CRACKED (NLG WW) · airframe 88,155 hrs · 14,090 cycles

NLG WHEEL WELL STA 287 LT VERT STIFFENER CHORD FAILED HFEC INSPECTION. CRACK INDICATION APPROX 55 INCHES ABOVE BOTTOM OF CHORD WHERE MARKED. CUT OUT DAMAGE, FABBED AND INSTALLED FILLER AND ANGLES (3 EA) PER SRM 51-40-02 ON NR 3872N00117.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

PASSENGER CABIN AT STA 1197 RBL 56-80 FLOORBEAM IS SHOWING BARE METAL AROUND FASTENER HOLES AND GOUGES. COUNTER TOP REPLACED BY PEMCO VENDOR (REGENT) IAW 4 FLIGHT CMM 25-30-24, 8130 FURNISHED ON PEMCO NR 3872N00988. INCORRECT ACTION TAKEN FOR PTT 1552114, SHOULD READ, FOUND OUT OF LIMITS, CUT OUT DAMAGED AREA, FABRICATED AND REPLACED 2 EA REPAIR ANGLES, 2 EA STIFFENER SHIMS, 1 EA STIFFENER, AND 1 EA TOP STRAP PER SRM 53-00-51, EA PD67-53-050, AND ECRA 5300-01175 ON NR 3872N00556.

Part: SKIN — DENTED (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

EXT FUSELAGE SKIN DENTED STA 654+110, STR 30L. DENT WITHIN LIMITS, HFEC OF AREA FOUND MATERIAL DISTRESSED. CUT OUT DAMAGE, FABBED AND INSTALLED DOUBLER AND FILLER IAW SRM 53-00-01 AND 51-40-02 ON PEMCO NR 3872N00076.

Part: DOUBLER — CRACKED (NR 1 PYLON) · airframe 88,155 hrs · 14,090 cycles

NR 1 PYLON, PREVIOUS REPAIR ANGLE DOUBLER IS CRACKED AT INBOARD SIDE. REMOVED NR 1 PYLON MIDSPAR CLOSEOUT ANGLE PREVIOUS REPAIR ANGLE DOUBLER-TRIPLER. FABRICATED A REPAIR SPLICE AND STRUCTURAL FILLER AND INSTALLED PER REO G13357, REV A AND UAL EVA 73769 ON NON ROUTINE 20439. RMV'D AFT MID SPAR CLOSE OUT ANGLES P/N 311T3157-1 FOR REPLACEMENT. LOCATED AND INSTALLED NEW CLOSE OUT ANGLE IAW SB 767 54-0080 FIG 16 AS PART OF THE SIP PROJECT.

Part: SKIN — DAMAGED (BS 1373 S27-28R) · airframe 88,155 hrs · 14,090 cycles

AIRCRAFT DAMAGED BY LOADER, DAMAGE AFT OF AFT CARGO DOOR ABOUT 10 INCHES IN FRONT OF EXTERIOR AREA LIGHT. DAMAGE IS LOCATED BETWEEN STRINGER 27R AND 28R. BS 1373. MEASURES 4"X4".350 DEEP, GOUGES ARE .030 AND .060 DEEP. FRAME SHEAR TIE FOUND CRACKED AT BS 1373. REPAIRED FUSELAGE SKIN & SHEAR TIES BY RESTORING THE DISCREPANT LOCATION FOLLOWING EA PD67-53-042 AND ECRA 5360-0119.

Part: SHEAR TIE — DAMAGED (BS 1373 S27-28R) · airframe 88,155 hrs · 14,090 cycles

FOUND SHEAR TIE DAMAGED AT STA 1373 BTWN STRINGERS S27-R AND S28-R. SHEAR TIE HAS 3 SHEARED RIVETS ALONG WITH 5 AND HALF INCH TEAR, WHICH HAS BUCKLED THE FRAME. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW SHEAR TIE PER SRM.

Part: SKIN — DAMAGED (BS 1373 S27-28R) · airframe 88,155 hrs · 14,090 cycles

DURING OPEN UP OF DAMAGED AREA AFT OF THE AFT CARGO DOOR, FOUND BENT FRAME AT STA 1373 BETWEEN STR 27R AND 28R. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR FILLERS (2 EA), STIFFENERS (2 EA), CHANNEL, AND SHEAR TIE PER ECRA 5360-01171 AND EA PD67-53-043 ON NR 3852N00021.

Part: INTERCOSTAL — PUNCTURED (CARGO BAY) · airframe 88,155 hrs · 14,090 cycles

FOUND PUNCTURE IN AFT CARGO PIT INTERCOSTAL AT REAR OF CARGO DOOR OPENING STRINGER 28R LEVEL. APPEARS TO BE UNRELATED TO INITIAL DAMAGE (FOUND WHILST EVALUATING) PUNCTURE IS APPROX 4.5" X 2.5". FABRICATED AND INSTALLED NEW INTERCOSTAL STA 1351 - 1373, STR 28R PER SRM ON PEMCO NR 3852N00007.

Part: FRAME — CORRODED (BS 916 S20L) · corrosion level 2 · airframe 88,155 hrs · 14,090 cycles

CORROSION ON FRAME STA 916, NEAR STR 20L. CORROSION OUT OF LIMITS, FABRICATED AND INSTALLED REPAIR PER SRM ON PEMCO NR 3872N 00597.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 88,155 hrs · 14,090 cycles

PASSENGER CABIN FLOOR STRUCTURE AT BS 287 FROM RBL 40 TO RBL 73 HAS CORRODED FLOORBEAM. MAJOR REPAIR ACCOMPLISHED. RPLC'D T-CHORD, T-CAP, ANGLES AND BRACKET AT STA 287, RBL 31 - RBL 82 PER SRM.

Part: FLOORBEAM — CORRODED (BS 347) · corrosion level 2 · airframe 88,155 hrs · 14,090 cycles

PASSENGER CABIN FLOOR STRUCTURE AT BS 347, BTWN RBL 19 - 40 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. FOUND CORROSION OUT OF LIMITS, FABRICATED AND INSTALLED TEE, STRAPS, AND ANGLES FROM RBL 19 - RBL 60 PER SRM ON NR 3872N00504.

Part: FLOORBEAM — CORRODED (BS 1196.66) · corrosion level 2 · airframe 88,155 hrs · 14,090 cycles

CORROSION ON FLOORBEAM UPPER CAP AT BS 1196.66 ACROSS ENTIRE BEAM IN REAR CARGO.

Part: SKIN — DENTED (BS 440 S25-26R) · airframe 88,155 hrs · 14,090 cycles

FUSELAGE SKIN DENTED BS 440, S25 - 26R. FOUND DENT OUT OF LIMITS. CUT-OUT DAMAGED AREA, INSTALLED DOUBLER AND FILLER IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 88,155 hrs · 14,090 cycles

CORROSION ACROSS TOP OF FLOORBEAM AT STA 1197 IN AFT CARGO COMPARTMENT. REMOVED CORROSION ON TOP OF FLOORBEAM. FOUND TO BE OUT OF LIMITS. REMOVED FLOORBEAM AND FABRICATED NEW FLOORBEAM FROM BAC 1506-3123 7075T651L IAW B767 SRM 53-60-53. ALODINED, PRIMED AND PAINTED IAW MM. INSTALLED NEW FLOORBEAM IAW AT BS 1197 IAW B767 SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

CORROSION ON SEAT TRACK STA 795, LBL 60. MAJOR REPAIR ACCOMPLISHED: RPLC'D SEAT TRACK FROM STA 775 TO 795, LBL 60 PER SRM ON PEMCO NR 3872N00683.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

FLOORBEAM AT BS 654.121 LBL 54 TO 88 HAS DRILL BIT PILOT HOLES PART WAY INTO UPPER CHORD SURFACE. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED FLANGE & FABRICATED REPAIR PARTS IAW B767 SRM 53-00-51. INSTALLED PARTS ON FLOORBEAM AT BS 654 LBL 54 TO LBL 88. NDTM PART 6 51-00-19. ALODINED, PRIMED AND PAINTED PER MM 51-21-10.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 88,155 hrs · 14,090 cycles

CABIN FLOOR STA 334, LBL 40 INTERCOSTAL CRACKED. MAJOR REPAIR ACCOMPLISHED. FABBED AND REPLACED INTERCOSTAL PER SRM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 88,145 hrs · 14,089 cycles

AIRCRAFT HIT BY HILOADER AFT OF AFT CARGO DOOR ABOUT 10 INCHES IN FRONT OF EXTERIOR AREA LIGHT. NDT HI-FREQ EC INSP SKIN AFTER DAMAGE BLENDED. NO CRACKS FOUND. BLEND SKIN DAMAGE AT STA 1373 BTWN S27-R AND S28-R PER SRM. BLENDED OUT GOUGES AND PRIMERED DAMAGE AREA AT STA 1373 PER SRM. DAMAGE TO FUSELAGE AT STATION 1373 BETWEEN STRINGERS 27R AND 28R CAUSED BY CONTACT WITH CARGO LOADER. RE-INSPECTIONS MUST BE ACCOMPLISHED. THE INITIAL DENT MEASURED 4"H X 5"W AND WAS REPAIRED PER THE INSTRUCTIONS ON PEMCO PD 67-53-042 WITHOUT DEVIATION. BY- 29887. ACCOMPLISH THE INITIAL INSPECTION ON OR BEFORE THE AIRCRAFT REACHES 37500 PLANE TOTAL CYCLES. PERFORM REPEAT INSPECTIONS EVERY 3000 CYCLES AFTER REACHING THE THRESHOLD.

Part: A/C PACK — MALFUNCTIONED (RIGHT) · airframe 88,145 hrs · 14,089 cycles

AT GATE RT PACK INOP IN AUTO WITH APU ON WORKS IN SSBY MODE. RT TEMP INOP EICAS MSG INTERROGATED RT PACK CONTROLLER FOUND RAM OUTL ACTR FLAGGED. UNABLE TO RESET REMOVED PLUG ON RAM AIR OUTLET ACTUATOR NOW SYSTEM RESET. PACK IS WORKING NOW IN AUTO MODE BUT DUE TO HISTORY DEFERRED PER MEL 2151K. STANDBY CONTROLLER ALL OK. RT SYSTEM WORKS OK IN STBY MODE.

Part: LIMIT SWITCH — DIRTY (RAT) · airframe 87,968 hrs · 14,067 cycles

RAM AIR TURBINE SHOWS UNLOCKED. EXTENDED RAT AND CLEANED UP LIMIT SWITCH S369. RETRACTED RAT. RAT UNLOCKED LIGHT AND EICAS MESSAGE CLEARED.

Part: PCA — LEAKING (RT ELEVATOR) · airframe 87,968 hrs · 14,067 cycles

RT ELEVATOR INBD PCA IS LEAKING A STEADY STREAM OF HYD. REMOVED PNL FOR ACCESS, PUT PNL IN AFT BULK CARGO COMPARTMENT. REPLACED RIGHT INBD PCA.

Part: CIRCUIT BREAKER — FAULTY (RUDDER RATIO) · airframe 87,896 hrs · 14,057 cycles

RUDDER RATIO LIGHT ILLUMINATED ON THE GROUND. RUDDER RATIO LIGHT CIRCUIT BREAKER RECYCLED LIGHT WENT OUT. ACCOMPLISHED BYTE TEST PER FIM 27-09-00 BLOCK 106B. FOUND PCA FAULT BALL. AFTER RESET OF PCA BALL ON BOTH LEFT AND RTB RRC ACCOMPLISHED TEST PER MM AND TEST PASSED AND NO FAULTS INDICATED.

Part: INDICATOR — INOPERATIVE (LT ENGINE) · airframe 87,796 hrs · 14,041 cycles

LEFT ENGINE VALVE ANNUNCIATOR LIGHT INOPERATIVE. REPLACED INDICATOR LIGHT ASSY. OPS CHECKED GOOD.

Part: CONNECTOR — BROKEN (AC PACK) · airframe 87,695 hrs · 14,028 cycles

LT PACK TEMP CONTROL VLV CONNECTOR BROKEN AND WIRING DISCONNECTED. CONNECTOR D676. PCN 563 -1806 AOG N3982. BY- 8256 : D676 STRAIN RELIEF BROKEN, WIRING INTACT, D678 AT OTHER END OF VLV HAS WIRING PULLED. REPLACED CONNECTOR D676, NEEDS OP CHECK, CONNECTOR D678 WILL BE REPLACED ON SMC17.

Part: WIRE — DAMAGED (AC PACK) · airframe 87,695 hrs · 14,028 cycles

RIGHT PACK DOOR HINGE AREA, WIRE BUNDLE HAS DAMAGED WIRING RUNNING ALONG KEEL BEAM. FOUND WIRE W982-002-20 INSULATION DAMAGE CONDUCTOR STRAND OK, FIX INSULATION. NEED OP CHECK.

Part: DOOR — SEPARATED (ACCESSORY BAY) · airframe 87,695 hrs · 14,028 cycles

LEFT AC BAY DOOR LOST IN FLIGHT. FOUND LEFT AC BAY ACCESS DOOR NOT WITH ACFT UPON ARRIVAL IN ORD. LT PACK BAY ACCESS DOOR 4 EA HINGE ASSY REMOVED DUE TO DAMAGE. BEGAN INSTALLATION OF LT AC BAY DOOR. BEGAN INSTALLING HI-LOKS IN HINGES. REPLACED 4EA DAMAGED HINGES FOR LT AC BAY DOOR. ACCOMPLISH A GENERAL VISUAL INSPECTION OF THE AIRPLANE STRUCTURE FOR ANY ASSOCIATED DAMAGE. REF GNMM 8-0-01-001 P26. VISUAL INSPECTION ACCOMPLISHED AND DAMAGE DOCUMENTED REF GNMM 8-0-01 PG26.

Part: CONTROL UNIT — MALFUNCTIONED (GALLEY) · airframe 87,687 hrs · 14,024 cycles

FWD GALLEY HAS NO POWER. REPLACED ELCU M225, OPS CHECK OF LOAD SHED AND FWD GALLEY POWER OKAY.

Part: CONTROL UNIT — MALFUNCTIONED (GALLEY) · airframe 87,639 hrs · 14,017 cycles

CREW REPORTS NO POWER IN FWD GALLEY. REPLACED FWD GALLEY ELCU M225 AND TESTED OKAY PER MM.

Part: COMPUTER — FAULTY (EICAS) · airframe 87,639 hrs · 14,017 cycles

R IRS ON DC MESSAGE ON ADVISORY PAGE. REPLACED L EICAS COMPUTER PER MM AND LOADED OPC AND OPS SOFTWARE PER MM, MESSAGE CLEARED.

Part: RECEPTACLE — FAULTY (EXTERNAL POWER) · airframe 87,639 hrs · 14,017 cycles

IN CONDUCTING THE BUS POWER CONTROL UNIT TEST PER MM FOUND THAT AIRCRAFT WILL NOT ACCEPT EXTERNAL POWER. FOUND PIN-A OF THE EXTERNAL POWER CONNECTOR LOOSE AND THE INSULATION BETWEEN PIN-A AND PIN-B CRACKED. REPLACED EXTERNAL POWER RECEPTICAL PER MM. SEALANT APPLIED AT 0130 ON 8-20-11 SEALANT TYPE IS SEA3750-14. TEST NEEDS TO BE PERFORMED ON BUS POWER CONTROL UNIT DUE TO UNIT REPLACEMENT. ACCOMPLISHED TEST PER MM.

Part: CONTROL UNIT — MALFUNCTIONED (ELECTRICAL SYS) · airframe 87,639 hrs · 14,017 cycles

UTILITY BUS WILL NOT COME ONLINE. REPLACED BUS POWER CONTROL UNIT, BUSSES NOW ON LINE.

Part: BATTERY — DISCHARGED (MAIN) · airframe 87,639 hrs · 14,017 cycles

TOW CREW REPORTS LOW BATT VOLTAGE. REPLACED MAIN BATTERY, CHECKS GOOD.

Part: CAP — MISSING (WINDSHIELD) · airframe 87,545 hrs · 14,004 cycles

F/O J1 & J4 WINDSHIELD TERMINAL BLOCK MISSING "HIGH VOLTAGE" CAP. FOUND BASE MISSING RETAINING RING. SPLICED IN A NEW HARNESS ASSY. TESTED WINDOW HEAT REF AMM, TESTS OKAY.

Part: OXYGEN BOTTLE — ODOR (CABIN) · airframe 87,522 hrs · 13,995 cycles

MID GALLEY RIGHT AISLE ELECTRICAL BURNING SMELL. SMELL GETS STRONGER THEN DISSIPATES. RAN ALL OVENS, RE-HEATERS, LIGHTS, VIDEOS, AND CHILLERS. NO BURNING SMELL NOTED. CHECKED LAV WATER HEATERS. CH'D ALL CB'S NONE TRIPPED. CHECKED CLOSET LIGHT AND OVERHEAD LIGHTS. CHECKED SEAT ACTUATIONS IN AREA ALL CHECKED NORMAL. FOUND PORTABLE O2 DISPENSING UNIT ON RT SIDE CABINET SMELLED OF ELEC BURN. REMOVED AVIOX O2 PACK.

Part: DUCT — CRACKED (RT A/C PACK) · airframe 87,421 hrs · 13,976 cycles

FOUND RT PACK INBOARD LWR DUCT BETWEEN REHEATER AND HEAT EXCHANGER CRACKED. RIGHT PACK OUTPUT TEMP 58 DEG WILL NOT GO COLDER TEMP VALVE SHOWS 0.00 POSITION DCT PRSS 31. REPLACED DAMAGED DUCT ASSY.

Part: SERVO — FAULTY (AUTOPILOT SYS) · airframe 87,170 hrs · 13,923 cycles

'ELEV SERVO L FAIL' MSG ON MCDP AFTER TEST NR 8. COMPLETED MM FIM 22-00-03 PG 144 MCDP TEST NR 8. TRACED FAULT TREE TO PG 146 BLOCK 210, NEED TO REPLACE LEFT ELEVATOR AUTOPILOT SERVO M21. *NOTE, RPL LEFT FCC FOR TROUBLESHOOTING PER FIM, NO HELP. RE-INSTALLED ORIG L FCC. CONT OF AMIS ITEM 1702003: MCDP TEST NR 1 ON LEFT FCC HAS MSG 'NO INFC L ELEV SURF POS' BELIEVE TO BE RELATED TO TEST NR 8 'ELEV SRVO L FAIL' MSG. REPLACED LEFT ELEVATOR AUTOPILOT SERVO.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 86,803 hrs · 13,870 cycles

EMERGENCY PATH LIGHTS RT AISLE L896, LT AISLE L897, AND CROSS AISLE PATH LIGHT L905 ARE INOPERATIVE. REPLACED RT AISLE PATH LIGHT L896, CHECKED OKAY. REPLACED POWER SUPPLY M1559 FOR L897 AND L905, CHECKED OKAY.

Part: STARTER — LOW (NR 2 ENGINE) · airframe 86,510 hrs · 13,826 cycles

QUANTITY OF OIL DRAINED FROM NR 2 ENG STARTER IS BELOW MINIMUMS IAW MM. STARTER MUST BE CHANGED. REPLACED NR 2 ENGINE STARTER IAW MM.

Part: OIL COOLER — LEAKING (NR 1 ENGINE) · airframe 86,510 hrs · 13,826 cycles

NR 1 ENG HOC. REPLACED FCOC PER MM. NO LEAKS.

Part: ACTUATOR — FAULTY (NLG) · airframe 86,197 hrs · 13,781 cycles

AFTER GEAR RETRACTION WHEN HANDLE SELECTED TO OFF, LDG GEAR MONITOR EICAS MSG AND AIR NOISE AND VIB. GEAR SELECTED TO UP NOISE AND VIB CLEARED. REPLACED NOSE GEAR LOCK ACTUATOR PER MM, CYCLED GEAR AND OPS NORMAL.

Part: ACTUATOR — LEAKING (ELEVATOR) · airframe 85,830 hrs · 13,728 cycles

LT ELEVATOR L ACTUATOR LEAKING. REPLACED ELEVATOR PCA PER MM, OPS NORMAL. CONFIRMED INSTALLATION OF LEFT CENTER SYSTEM ELEVATOR PCA PER MM. LINES SECURE AND ALL BOLTS TORQUED. NO LEAKS NOTED.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 85,594 hrs · 13,689 cycles

AISLE FLOORBOARDS STARTING AT SEAT 1A PAST SEAT 2A DELAMINATED. AT SEAT 1A FLOORBOARD MAKES CRACKING SOUND WHEN PRESSURE APPLIED. DELAMINATED AREA EXCEEDS 3 FT IN LENGTH. REPAIR REQUIRES PICKING UP FASTENERS INBD AND OTBD OF DELAMINATION. EDGE FASTENERS ARE UNDER 1ST CLASS SEAT PODS. CHECKED FLOORBOARD FOR SOFT AREAS OR DELAMINATION AND DETERMINED FLOORBOARD TO BE SERVICEABLE AS IS.

Part: DRAIN — LEAKING (HYD PUMP) · airframe 85,379 hrs · 13,658 cycles

FOUND HYD LEAK FROM NR1 ENG DURING WALK AROUND. FOUND LEAK FROM HYD PUMP PAD WITNESS DRAIN, CLEANED AREA DRY MOTORED ENG FOUND 1 DROP IAW 1 MIN 10 SEC LEAK WITHIN LIMITS IAW MM. HYD QTY NORMAL. ACCOMPLISHED LEAK CHECK OF NR 1 ENGINE HYD PUMP FOR LEAKS, NONE NOTED, STATIC OR AFTER RUN.

Part: PUMP — FAULTY (HYD SYSTEM) · airframe 85,334 hrs · 13,652 cycles

RIGHT HYD EICAS, FLIGHT DIVERTED. PUMP OFF LIGHTS OUT AFTER 10 MINS METAL IN FILTERS CHANGING ENG PUMP & FILTERS. WILL RUN CHANGE FILTERS AGAIN. REPLACED EDP ON NR2 ENGINE DUE TO PUMP FAILURE, LEAKED CHECKED IAW MM, NO LEAKS NOTED.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT) · airframe 85,307 hrs · 13,648 cycles

CAPT FLT DIRECTOR DISAPPEARED WHEN CTR AUTOPILOT WAS DISCONNECTED AND NO AUTOLAND 3 APPEARED. REPLACED LT FCC REF MM, ALL CHECKS OK. PERFORMED CATIII CHECK IAW MM AND ALL OPS NORMAL. ACFT RECERTIFIED TO CATIII STATUS.

Part: ACTUATOR — LEAKING (THRUST REVERSER) · airframe 85,307 hrs · 13,648 cycles

ON ARRIVAL LT HYD QTY INDICATING 14 OPENED LT FAN COWLS TO LET HYD FLUID DRAIN OFF. UNABLE TO DETERMINE SOURCE OF LEAK, BUT SUSPECT THRUST REVERSER ACTUATOR HYD LINE. HYD LEAK COMING FROM LOWER RT NON LOCKING ACTUATOR ON NR1 ENGINE. REPLACED LT ENG RT LOWER NON LOCKING REVERSE ACTUATOR, ALL OPS AND INDS NORMAL.

Part: ISOLATION VALVE — STUCK (LEFT) · airframe 84,947 hrs · 13,598 cycles

LEFT BLEED ISOLATION VALVE ON EICAS AND LT ON OVERHEAD PANEL APPEARS STUCK OPEN. LEFT BLEED ISOLATION VALVE REPLACED IAW AMM. OPS OK.

Part: AUDIO PANEL — FAULTY (COCKPIT) · airframe 84,772 hrs · 13,576 cycles

CAPT BOOM MIC NOT WORKING. REPLACED AUDIO SELECTOR PANEL, OPS CHECKS OKAY.

Part: PRIORITY VALVE — FAULTY (LEFT) · airframe 84,184 hrs · 13,493 cycles

LT ENG PRV EICAS MSG PRIOR TO ENG SHUTDOWN. REPLACED PRV IAW MM, ACCOMPLISHED ENGINE RUN ALL. OPS AND INDICATION NORMAL.

Part: LOGIC CARD — FAULTY (EMERGENCY LIGHTS) · airframe 83,879 hrs · 13,454 cycles

EMERG DOORS LIGHT ON OVERHEAD PANEL WITH LT WING SLIDE DOOR LIGHT ON EICAS. INSPECTED LT WING SLIDE INTERIOR AND EXTERIOR FOUND NO OBVIOUS IRREGULARITIES. SLIDE LIGHT IS OUT AND HAS BEEN FOR 15 PLUS MINUTES. NO HISTORY NOTED. OK FOR SERVICE. INSPECTED LEFT WING SLIDE INTERIOR AND EXTERIOR FOUND NO OBVIOUS IRREGULARITIES. SLIDE LIGHT IS OUT AND HAS BEEN FOR 15 PLUS MINUTES. EXAMINED S198 FOR INTEGRITY AND OPERATION, CHECKS OK. REPLACED PROX CARD NR 4 AND LOGIC CARD NR 5. SYSTEM OPERATION CHECKS OK PER MM. MESSAGE DID NOT REOCCUR. NO HISTORY NOTED. OK FOR SERVICE.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 83,709 hrs · 13,429 cycles

RT ENG BLEED LGT & RT ENG HPSOV EICAS MSG & ACFT ON GND, WITH ENG BLEED SWITCH ON, & ENG RUNNING. LT & RT DUCT PSI ARE. TRIED NEW M860, NO HELP. REINSTALLED ORIGINAL M860. CIRCUIT BREAKER C1340 STILL POPS WITH HPSOV, HPSOV CONTROLLER, PRSOV DISCONNECTED. REPLACED NR 2 ENG FOR TIME. ACCOMPLISHED NR 2 ENG BLEED SYS CHECK FOR ENG CHANGE OPS CHECK. BLEED OPS CKS GOOD. REACTIVATED BLEED SYS IAW MEL.

Part: VALVE — LEAKING (OIL HEAT EXCHANG) · airframe 83,709 hrs · 13,429 cycles

NR 2 ENG AIR-OIL HEAT EXCHANGER VALVE LEAKING FROM CORE. REPLACED NR 2 ENG AIR OIL COOLER. OPS NORMAL.

Part: CLAMP — MISSING (RT NACELLE) · airframe 83,647 hrs · 13,418 cycles

RT ENG FIRE WARNING, RTFL. CAPTAIN RETURNED NR 2 THROTTLE TO IDLE POSITION BY 17,000 AND FIRE WARNING CEASED. FURTHER TEST OF FIREWARNING SYSTEM CHECKED NORMAL & ENG WAS SHUTDOWN PER CREW CHECKLIST. CREW VERIFIED NO FIRE BOTTLES WERE DISCHARGED AND NO FURTHER FIRE WARNINGS OCCURED AFTER NR 2 ENG SHUTDOWN. FOUND E SEAL AND CLAMP MISSING FROM INTERMEDIATE CHECK VALVE, REPLACED PER MM. ACCOMPLISHED FIRE WARNING TEST AND HIGH POWER ENGINE RUN AT 1.50 EPR FOR 3 MINUTES NO DEFECTS NOTED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 83,518 hrs · 13,400 cycles

EMERG EXIT FLOOR LTS FLICKRING LT SIDE BUSINESS NEAR LAV. REPLACED BATTERY PACK IAW MM 33-51-00 DUE TO PREVIOUS HISTORY.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 37AB) · airframe 83,341 hrs · 13,378 cycles

SEAT 37AB O2 MASK DEPLOYED AFTER TAKEOFF. FLT ATTENDENT RESTOWED THEM. MAINTENANCE TO INSPECT SEAT 37A+B O2 MASKS AND CONFIRM GENERATOR NOT FIRED AND FOR PROPER RESTOWING OF MASK AND HOSE ASSEMBLY. INSPECTED O2 GENERATOR, GOOD. RESTOWED O2 MASKS AND LATCHED CLOSED. OK FOR SERVICE.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 82,627 hrs · 13,272 cycles

EMERGENCY EXIT LIGHT ON AT DOOR 2L. REPLACED EMERGENCY BATTERY PACK FOR DOOR 2L.

Part: APU — FAILED · airframe 82,554 hrs · 13,262 cycles

FIRST APU START ATTEMPT APU AUTO SHUTDOWN AT NEAR FULL RPM. LARGE CLOUD ON START THAT SMELLS LIKE OIL. APU LIT-UP AND THEN AUTO SHUTDOWN AFTER 1 TO 2 MINUTES. OPENED APU COMPT AND DID NOT FIND ANY LEAKING COMPONENTS AT THIS TIME. BIT APU ECU FOUND "LOW OIL PSI". SERVICED WITH 3 QTS. ALSO FOUND DELTA P POPPED FOR LUBE FILTER NEXT TO OIL CAP. RESET DELTA P, ATTEMPTED RESTART AFTER SVC OIL, WOULD NOT CRANK AND APU FAULT LIGHT CAME ON. APU ECU NOW SHOWS LOW OIL PRESSURE FLASHING. APU INOPERATIVE.

Part: ADAPTER — BROKEN (VALVE ACTUATOR) · airframe 82,450 hrs · 13,247 cycles

WHILE REPLACING RT ENG SPAR VALVE ACT, THE BOLT FLANGE ON THE MOUNTING ADAPTOR PLATE BROKE OFF. REPLACED THE ADAPTOR PLATE.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 82,450 hrs · 13,247 cycles

EMERGENCY LIGHTS FLASHING ON & OFF. REPLACED BATTERY PACK POWER SUPPLIES M1556 AND M1561 AND TESTED PER MM. GROUND CHECKS NORMAL.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 82,127 hrs · 13,200 cycles

EMERGENCY FLOOR LIGHTS FLICKERED ON OFF SEVERAL TIMES THROUGHOUT FLT IN BUSINESS CLASS. RESECURED LOOSE FLOOR LIGHT CONNECTOR ON RT SIDE OF BUSINESS CLASS CARRIED OUT TEST, ALL SATISFACTORILY.

Part: FSEU — FAULTY (FLAPS) · airframe 82,112 hrs · 13,195 cycles

REPEAT ALT FLAP CHECK FAIL. REPLACED 3 PINS ON ALT FLAP EXTEND MOTOR M547 CONNECTOR, REPLACED FSEU & ALT FLAP EXTEND RELAY, OPS TESTED GOOD.

Part: PROBE — FAILED (ENGINE PT2) · airframe 82,112 hrs · 13,195 cycles

LEFT EEC MODE EICAS AFTER TAKEOFF-RESET OK. T/S IAW MM, REPLACED NR 1 ENGINE PT2 PROBE IAW MM. ACP PT2 PROBE OPS AND LEAK CHECK IAW TEST NR 7 & NR 14 IAW MM. TEST GOOD.

Part: SWITCH — FAULTY (HYD PRESSURE) · airframe 82,112 hrs · 13,195 cycles

STAB TRIM EICAS IMMEDIATELY AFTER TAKEOFF. FOUND HYD PRESSURE SWITCH 528 BAD. REPLACED 528 PRESSURE SWITCH IAW 767MM, OPS CHK GOOD IAW 767MM. OPS CHK GOOD IAW 767MM. REPEAT GRIPE-STAB TRIM EICAS MESSAGE DISPLAYED & STAB TRIM LIGHT ILLUMINATED. TROUBLESHOT MESSAGE. SHOWED STCM FAULT BALL ON M525. FOUND BRAKE PRESSURE SWITCH S1 BAD. REPLACED S1 SWITCH IAW MM & PERFORMED SUCCESSFUL OPS CK.

Part: SWITCH — FAULTY (HYDRAULIC SYS) · airframe 82,111 hrs · 13,194 cycles

RAT UNLOCKED DURING APU BUS PRIORITY CHECK. REPLACED AIRSPEED SWITCH S614 IAW 767 MM AND WDW, PERFORMED RAT DROP IAW 767 MM. OPS TEST GOOD. TROUBLESHOOTING HISTORY, FIRST REPLACED K235 RELAY PER FIM AND WDM, NO HELP. REMOVED CONNECTOR D10434P AND FOUND PINS 1&2 BAD, CAUSING SWITCH TO CLOSE WITH PRESSURE TO 40 KTS. REPLACED AIRSPEED SWITCH S614 PER WDM. SWITCH BAD FROM STOCK. REPLACED S614 AGAIN, AND OPS TEST GOOD PER MM.

Part: MOTOR — FAULTY (LE SLAT) · airframe 82,111 hrs · 13,194 cycles

ALT FLAP SYS FAILED INBOARD CHECK. IND STOPPED HALFWAY BETWEEN 0 AND 1, LEADING EDGE AND TRAILING EDGE DISAGREE. REMOVED AND REPLACED INBOARD SLAT ELECTRIC MOTOR AND TRAILING EDGE FLAP ALTERNATE ELECTRIC MOTOR PER MM. ALT SLAT OPS CHECK GOOD PER MM AND TRAILING EDGE FLAP PDU, OPS CHECK GOOD PER MM.

Part: WEB — CRACKED (PYLON) · airframe 82,111 hrs · 13,194 cycles

NR 1 PYLON INTERNAL MID TORQUE BOX UPPER WEB IS CRACKED AT LEFT DRAIN HOLE. MAJOR REPAIR ACCOMPLISHED. STOP DRILLED 2 EACH CRACKS AND FABRICATED A REPAIR DOUBLER AND FILLERS AND INSTALLED PER SRM.

Part: FEEDER CABLE — CHAFED (NR 1 GENERATOR) · airframe 82,111 hrs · 13,194 cycles

NR 1 ENGINE PYLON GENERATOR FEED CABLES CHAFING ELECTRICAL WIRE BUNDLE LT SIDE MID PYLON AREA. REROUTED GENERATOR CABLES AND WRAPPED WITH HIGH TEMP TEFLON TAPE LACING CORD. NO DAMAGE TO CABLES NOTED. ALL ACCOMPLISHED IAW BSWPM 20-10-13 ON NON ROUTINE 20299 BY MECH-3270 AND INSP QC328.

Part: FEEDER CABLE — CHAFED (NR 2 GENERATOR) · airframe 82,111 hrs · 13,194 cycles

NR 2 ENGINE GENERATOR FEEDER CABLE CHAFING EACH OTHER AT TERMINAL STRIP AT 6:30 POSTITION. REROUTED GENERATOR CABLES AND SECURED WITH HIGH TEMP LACING CORD AND NO DAMAGE TO THE CABLE NOTED. ALL WORK ACP'D IAW GN-MM ON NON ROUTINE 20378.

Part: PUMP — INOPERATIVE (HYD SYSTEM) · airframe 81,430 hrs · 13,095 cycles

CENTER AIR DEMAND HYD PUMP INOP IN AUTO & ON POSITIONS.

Part: RELAY — MALFUNCTIONED (HYD PUMP) · airframe 81,439 hrs · 13,097 cycles

CENTER AIR DEMAND HYD PUMP INOP IN AUTO & ON POSITIONS. FOUND LOW APU BLEED AIR SUPPLY - DF APU BLEED AS PER MEL 3611G. ENGINE NR 1 IDLE RUN ACP AT IAD AND FOUND ADP OP CHECKS NORMAL WITH ENGINE AIR. FOUND LOW APU BLEED AIR SUPPLY - DF APU BLEED AS PER MEL 3611G. ENGINE NR 1 IDLE RUN ACP AT IAD AND FOUND ADP OP CHECKS NORMAL WITH ENGINE AIR. APU BLEED AIR NORMAL, REPLACED RELAY K153. ACCOMPLISHED REF MM, ADP NORMAL, OPS CHECK OK.

Part: WIRE HARNESS — BURNED (CARGO LOADING) · airframe 81,047 hrs · 13,041 cycles

FWD CARGO LOADING SYS INOP. WHILE ID PARTS, RESET SYS CB & SEVERAL BREAKERS POPPED. OPENED FLOOR PANEL TO INSP FOUND BURNED INSULATION & WIRE BUNDLE. STARTED REPAIR TO WIRE BUNDLE. WIRES REPLACED, TEMPORARILY MARKED NR S50 TO NR 59 & PULLED TIED TOGETHER AS TO SEPARATE FROM STILL DAMAGED WIRES. FOUND NR 16 GAUGE ENVIRONMENTAL CRIMPS INSTALLED ON NR 20 GAUGE WIRE. ALSO NR 16 SHRINK INSULATOR NOT SHRUNK DOWN ON NR 20 WIRE AS TO BLOCK WATER INTRUSION THAT PUDDLED ON TOP OF THE INSULATION WHERE WIRES WERE LAYING. REPLACED WIRES & INSTALLED CORRECT SIZE ENVIRONMENTAL CRIMPS. COMPLETED WIRE REPAIRS. ALL FWD PIT LOADING SYS TESTED NORMAL. INSTALLED FLOORBOARD. INSTALLED INSULATION. SECURED WIRES.

Part: LINE — LEAKING (OIL COOLER) · airframe 80,918 hrs · 13,019 cycles

NR 2 ENG FUEL OIL COOLER LINE LEAKING. FOUND A COMBINATION FLEX HARD LINE LEAKING FROM FUEL OIL COOLER, PART AOG'D J3857, LINE IN HAND. LEAK APPEARED TO BE ON THE FLEX PART OF THE LINE APPROX 6 INCHES FROM THE FUEL PUMP CONNECTION. R & R FUEL PUMP INLET TUBE. LEAK CHECKED OK.

Part: PUMP — CRACKED (FUEL SYSTEM) · airframe 80,771 hrs · 12,998 cycles

FOUND MOUNTING FLANGE OF JETTISON PUMP CRACKED. REPLACED RT OTBD JETTISON PUMP. OPS CHECKS NORMAL.

Part: CONTROLLER — FAULTY (APU) · airframe 80,703 hrs · 12,988 cycles

APU AUTO SHUTDOWN. FOUND APU CONTROL UNIT NOT TESTING. REPLACED APU CONTROL UNIT. REPLACED APU STARTER AND APU CRANK RELAY. LATER APU AUTO SHUTDOWN. APU FAULTS DC PWR LOSS.THE NEWLY FITTED CONTROLLER HAD THIS FAULT ON TWO OTHER AIRCRAFT. REPLACED CONTROLLER. SYSTEM TEST AND BITE TEST GOOD.

Part: OVEN — CONTAMINATED (GALLEY) · airframe 80,688 hrs · 12,983 cycles

ON DESCENT BURNING ODOR NEAR BIZ GALLEY. UTILITY BUSES TURNED OFF. ALL PAX CALL LTS ON. WARMING OVEN R11 HAS MOLTEN PLASTIC STUCK TO BOTTOM CAUSING ODOR WHEN HEATED. CLEANED OVEN. INSPECTED E&E, ALL CB'S IN ACFT, NONE POPPED-GALLEY EQPT, CHILLERS, COFFEEMAKER CONNECTORS. RAN ALL GALLEY EQ AND COCKPIT LIGHTS, PACKS, RECIRC FANS, ANTI-ICE SYS, NO ADDITIONAL ODORS. CALL LIGHT CHECK NORMAL. RAN ENGINES & APU, IFE CK OK. NO OTHER FAULTS FOUND.

Part: SKIN — DAMAGED (BS 180.5 S26L) · airframe 80,311 hrs · 12,928 cycles

STATIC DISCHARGE ON CLIMBOUT. SILENT SURGE DETECTED. FOUND 3 LIGHTNING STRIKES JUST AFT OF STA 180.5 JUST ABOVE 27L. DRILLED DAMAGE AND INSTALLED SOLID FASTENER.

Part: FAN BLADE — DAMAGED (RT ENGINE) · airframe 79,786 hrs · 12,849 cycles

RT ENGINE FAN BLADE NR 2 HAS LEADING EDGE IMPACT DAMAGE CAUSING DEFLECTION OF LEADING EDGE. REPLACED NR 2 BLADE AND NR 21 BLADE AND ACP ENG GROUND RUN. NO ABNORMAL VIBRATION; ALL INDICATIONS GOOD.

Part: TRANSCEIVER — FAULTY (HF SYSTEM) · airframe 79,417 hrs · 12,795 cycles

HF TRANSMISSION AND RECEPTION ARE INOP, WEAK, GARBLED INTERMITTENT, ETC. AT ALL CREW STATIONS. (1 = L HF, 2 = R HF). LEFT HF WILL NOT TUNE. REPLACED LT HF COMM TRANSCEIVER FOR TROUBLESHOOTING. REMOVED AND REPLACED LT HF COMM TRANSCEIVER. DID NOT FIX PROBLEM. REPLACED TRANSCEIVER AND SWAPPED CONTROL PANELS, NO HELP. NEEDS COUPLER. REPLACED LEFT HF COUPLER ( M241), OPS CKD GOOD.

Part: SLIDE — DAMAGED (L OVERWING) · airframe 79,132 hrs · 12,751 cycles

LEFT WING SLIDE EICAS AND EMERGENCY DOORS LIGHT FLASHED ON AND OFF INTERMITTENTLY AFTER PUSHBACK. FOUND SLIDE DAMAGED, CAUSING FOREIGN DEBRIS AND LOOSE SLIDE COMPONENTS. REPLACED LEFT OVERWING SLIDE.

Part: MODULE — INOPERATIVE (LT STAB TRIM) · airframe 78,908 hrs · 12,718 cycles

STAB TRIM LIGHT ILLUM ON OVERHEAD PANEL AND EICAS. RESET BOTH SAMS. PERFORMED STAB TRIM TEST PER MEL PROCEDURES AND LEFT PRIMARY TRIM CHANNEL FAILED. NO FAULT BALLS ON THE SAMS. STAB TRIM WORKS WITH FLAPS 5. PROBLEM APPEARS TO BE IN LEFT TRIM LIMIT CIRCUIT. NEED L- STAB TRIM CONTROL MOD. REPLACED LT STCM, NO HELP. FAILS STAB TRIM CUTOFF SWITCHES TEST. REPLACED LT STAB TRIM AIL LOCKOUT MODULE, OP CHECK GOOD.

Part: MODULE — FAULTY (STAB TRIM) · airframe 78,692 hrs · 12,683 cycles

EICAS MSG STAB TRIM DISPLAYED & STAB TRIM LIGHT ILLUMINATED. STABILIZER TRIM RATE NORMAL. FOUND LT STAB TRIM AIL LOCKOUT MOD FAULT. REPLACED LT SAM. COMPLETED MCDP GRND TEST 65 STAB TRIM AND AIL LOCKOUT TEST, ALL TEST PASS. NO FAULT INDICATIONS.

Part: MONITOR — FAULTY (NR 1 ENGINE) · airframe 78,180 hrs · 12,608 cycles

NR 1 ENG EICAS VIB READS HIGH. HIGHEST READING 47 (X.X, RANGE 0.0 TO 5.0, ABNORMAL ON 767-322 IF ABOVE 4.0). EXCESSIVE VIBRATION NOT FELT IN AIRFRAME. CREW COMMENTS: L ENG VIB 4.7 IN CLIMB FOR SEVERAL SECONDS. NO VIB FELT. REPLACED AVM CONDITIONER AND OPS CHECK. VIBRATIONS ON NR 1 ENG WELL WITHIN LIMITS OF MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 77,656 hrs · 12,531 cycles

EXTERIOR EMERGENCY LIGHT AT DOOR 2L INOP. REPLACED LAMP, CHECKED OKAY.

Part: BATTERY — DISCHARGED (CABIN) · airframe 77,656 hrs · 12,531 cycles

LT EXTERIOR EMERGENCY LIGHT, (2ND FROM TRAILING EDGE OF WING) IS INOP. REPLACED BATTERY ASSY, OPS CHECKED OKAY.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 77,656 hrs · 12,531 cycles

LT EXTERIOR EMERGENCY LIGHT AFT OF TRAILING EDGE WING INOP. RELAMPED EMERGENCY LIGHT, CHECKED OKAY.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 77,656 hrs · 12,531 cycles

EMERGENCY LIGHTS FROM ROW 27JK-34JK INOP. FOUND CONNECTOR CHECK BAD FOR SEAT 32JK. PIN PUSHED BACK AND WILL NOT LOCK. DISCONNECTED CONNECTOR CK AT SEAT 32JK. ONE LIGHT AT SEAT 32JK WILL BE INOP. ALL OTHER SYSTEM OPS OK.

Part: STOWAGE BOX — DEFECTIVE (COCKPIT) · airframe 77,105 hrs · 12,451 cycles

CAPT O2 MASK MIC INOP. REPLACED STOWAGE BOX.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 76,945 hrs · 12,428 cycles

EMERGENCY FLOOR LIGHTS AT RIGHT OVERWING EXIT FLICKER ON AND OFF. ARMED EMERGENCY LIGHTS AND RT EEL EXIT LIGHTS CAME ON. REPLACED EEL EMERGENCY POWER SUPPLY M1554, OPS OK.

Part: CONNECTOR — LOOSE (CABIN) · airframe 76,764 hrs · 12,404 cycles

EEL LIGHTING BY LAV 124 COMES ON AND OFF UNCOMMANDED. FOUND SUSPECTED LOOSE CONNECTOR FWD OF LAV 124 AISLE. RESECURED CONNECTOR. CYCLED EMERGENCY LIGHTS AND UNABLE TO REPRODUCE FAULT. CONSIDERED OK FOR FURTHER SERVICE.

Part: ACTUATOR — FAILED (AILERON) · airframe 76,665 hrs · 12,389 cycles

AILERON LOCKOUT LIGHT IS ON. REPLACED RT OUTBOARD AILERON LOCKOUT ACTUATOR.

Part: BATTERY — FAULTY (MAIN) · airframe 76,303 hrs · 12,334 cycles

BATTERY DISCHARGE LIGHT ILLUMINATED. REPLACED SHIP'S BATTERY.

Part: ANGLE — DAMAGED (NR 1 PYLON) · airframe 75,784 hrs · 12,257 cycles

NR 1 PYLON MIDSPAR FITTING CLOSE-OUT ANGLE, 2 EACH INBOARD FASTENER HOLES ARE ELONGATED IN PREVIOUS REPAIR AREA. MAJOR REPAIR ACCOMPLISHED. REMOVED EXISTING REPAIR ANGLES AND FABRICATED A NEW REPAIR DOUBLER AND TRIPLER ANGLE. BOTH HOLES MEASURE .531 INCH AND WITHIN LIMITS OF THIS REPAIR CRITERIA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 75,784 hrs · 12,257 cycles

AFT EMERGENCY LIGHTS AT R-4 AND L-4, EXIT SIGNS INOP. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER. OPS CHECK GOOD.

Part: SOCKET — DIRTY (EXTERIOR) · airframe 75,784 hrs · 12,257 cycles

EXTERIOR EMERGENCY LIGHT AT L-2 DOOR IS INOP. CLEANED LIGHT SOCKET AND OPS CHECKED GOOD.

Part: HOUSING — BROKEN (EVAC SLIDE) · airframe 75,784 hrs · 12,257 cycles

LT OVER WING SLIDE CABLE DISCONNECT HOUSING BROKEN. REMOVED AND REPLACED DISCONNECT HOUSING.

Part: SKIN — DAMAGED (R1 DOOR) · airframe 75,784 hrs · 12,257 cycles

DOOR 1R OUTER SKIN LOWER EDGE DAMAGE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR AT LOWER EDGE.

Part: SLIDE — FAULTY (CABIN) · airframe 75,784 hrs · 12,257 cycles

LT OVERWING SLIDE IS FAULTY.

Part: SLIDE — NO TEST (OVERWING EXIT) · airframe 75,784 hrs · 12,257 cycles

DURING LT OVERWING SLIDE DEPLOYMENT TEST, AFT HATCH STEP FAILED TO DROP DOWN, CABLE KINKED, STEP WILL NOT DROP FREELY. REPLACED AFT SUPPORT CABLE. OPS CHECKS GOOD. SLIDE FAULTY. AFTER CHECKING THE SLIDE SYS OUT, VERIFIED THE BOTTLE PRESSURE AND WHITE DISK WERE CORRECT, THEY WERE PULLED AND SET UP THE SLIDE SYS IAW ROUTINE JIC 6-1950-50-1 0. WITH HYD PWR ON AND SPOILERS UP, THE LT AFT OVERWING HATCH WAS REMOVED, THE SPOILER BLOW DOWN ACTUATOR FIRED, PUSHING 85625, THE INBD SPOILER TO THE DOWN POSITION. LT OVERWING SLIDE COMPARTMENT DOOR OPENED TO THE FULL OPEN POSITION. THIS PULLED THE CABLE THAT ACTUATES THE BOTTLE. AT THE INFLATION BOTTLE, THE BELL CRANK MOVED SLIGHTLY ENOUGH TO PULL THE CABLE FROM THE BOTTLE ONLY ABOUT 1-10TH INCH AND THEN STOPPED. THE WHITE DISK ON THE FRONT OF THE BOTTLE WAS NOW GONE, BUT THE CABLE COULD NOT BE PULLED ANY FURTHER TO OPEN BOTTLE. AFTER DISCONNECTING THE MAIN CABLE FROM THE BOTTLE REGULATOR CABLE AT THE BELLCRANK, THE MAIN CABLE DID MOVE BACK INTO THE CABLE HOUSING. THE SMALL REGULATOR CABLE ON BOTTLE COULD NOT BE MOVED DOWN. REGULATOR CABLE WAS MANUALLY LIFTED UPWARD TOWARD BOTTLE AND WAS EASILY PULLED BACK DOWN BY MX, THE SLIDE 85625 INFLATED. THE SMALL BOTTLE REGULATOR CABLE WAS JAMMED WHEN THE PRESSURE OF THE DOOR OPENING CABLE WAS APPLIED TO THE BOTTLE. FURTHER INVESTIGATION, FOUND THE SLIDE BOTTLE REGULATOR ROTATING-LOOSE, INDEPENDENTLY OF THE BOTTLE.

Part: SWITCH — FAULTY (LT BOOST PUMP) · airframe 75,542 hrs · 12,224 cycles

L FWD FUEL PUMP INDICATES PUMP ON WITH SWITCH OFF AND APU OFF. LIGHT TESTS OK. RESET CONNECTOR ON PRESSURE SWITCH, NO HELP. REPLACED LEFT FWD BOOST PUMP PRESSURE SWITCH. OPS CHECK OK.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 75,015 hrs · 12,144 cycles

DOOR 1L LOWER EXIT LIGHT INOP.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 75,015 hrs · 12,144 cycles

MED CABIN EEL LIGHT AT FRONT OF LAVS LEFT AND RIGHT INOP. FOUND DAMAGED CONNECTORS. REPAIRED LT & RT EMERGENCY LIGHT CABLE CONNECTORS. OP CHECKED OKAY.

Part: FEEDER CABLE — INOPERATIVE (EMERGENCY LIGHT) · airframe 75,015 hrs · 12,144 cycles

FIRST CLASS FWD EEL LIGHT INOP. REPAIRED EMERGENCY LIGHT CABLE. OP CHECKED OKAY.

Part: FUSE — INOPERATIVE (BATTERY) · airframe 74,735 hrs · 12,099 cycles

AIRCRAFT BATTERY IS INOP. AIRCRAFT WILL NOT POWER UP. INSTALLED NEW BATTERY. STILL DID NOT POWER UP. REPLACED INTERLOCK FUSES IN P34 PANEL. CHECKS GOOD.

Part: BLEED VALVE — FAULTED (APU) · airframe 74,611 hrs · 12,082 cycles

APU AUTO SHUTDOWN DURING TAXI OUT. APU AUTO SHUTDOWN DURING TAXI OUT. CONFIRMED APU SURGE BLEED CONTROL VALVE MALFUNCTIONING. REPLACED BLEED VALVE. OPS CHECK OKAY.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 74,543 hrs · 12,072 cycles

EXT EMERGENCY LIGHT JUST AFT OF LT WING INOP. *S/D* FOUND FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (FWD GALLEY) · airframe 74,543 hrs · 12,072 cycles

FWD GALLEY XAISLE EEL LIGHT INOP. *S/D* FOUND FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY, OP CHECK GOOD. AC OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 74,543 hrs · 12,072 cycles

EXT EMERGENCY LIGHT AT DOOR 2L INOP. *S/D* FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (LAVATORY) · airframe 74,543 hrs · 12,072 cycles

EEL LIGHT IN FRONT OF RT MID LAV INOP. *S/D* FOUND FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: VALVE — STUCK (LAVATORY TOILET) · airframe 74,455 hrs · 12,057 cycles

FWD LAV TANK INDICATING FULL. HALF OF LAVS NOW NOT WORKING. ECONOMY LAVATORY BY DOOR 2L TOILET WILL NOT STOP FLUSHING, FOUND STUCK VALVE. USED A WET PILLOW PER SAM. FLUSHED BOTH TANKS THRU SEVERAL TIMES WITH HONEY-BEE AND PRESERVICE. RESET TOILET TANK LOGIC MODULES LIGHTS EXTINGUISHED BOTH SYSTEMS OPS CHECK SATIS. PERFORMED LAVATORY WASTE LEVEL SERVICE CHECK. CHECKS OKAY. CLEANED WATER LEVEL SENSOR. CHECKS OKAY.

Part: IDG — FAULTY (NR 1 ENGINE) · airframe 74,241 hrs · 12,025 cycles

AT TOC HAD LEFT ELEC BUSS POWER PROBLEM OF A TRANSITORY NATURE WHICH MOMENTARILY BLANKED CAPT'S EADI AND EHSI. *S/D* SUSPECT FAULTY BEARING IN IDG. REPLACED NR 1 IDG ASSEMBLY, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 74,048 hrs · 11,993 cycles

LEFT ENGINE STARTED UP WITHIN 95 SECONDS BUT STOPPED ACCELERATING AT 50 PERCENT FOR 10 SECONDS.

Part: TURBINE WHEEL — DAMAGED (NR 1 ENGINE) · airframe 74,039 hrs · 11,990 cycles

NR 1 ENGINE SLOW TO IDLE. REPLACEMENT OF STARTER, IDG, FMU, AND 2.95 BV SOLENOID WERE NO HELP. ENGINE REPLACED. SHOP TEARDOWN REVEALED HEAVY HOT SECTION DISTRESS, ESPECIALLY IN THE HP TURBINE STAGE-1 AND STAGE-2 NOZZLE GUIDE VANES. THE STAGE-1 VANES WERE ON REDUCED BORESCOPE INSPECTION INTERVAL DUE TO LE EROSION. THIS DISTRESS WAS CONSISTENT WITH THE HIGH TIME SINCE LAST ENGINE SHOP REPAIR.

Part: LINE — LEAKING (HYDRAULIC SYS) · airframe 73,761 hrs · 11,952 cycles

LEFT HYDRAULIC QTY BELOW RF (.72). FOUND PRESSURE LINE AT RH WING OUTBOARD SPOILER LEAKING REPLACED LINE WITH FLEX LINE PER GNMM 1-0-13-003 OPS AND LEAK CK OK. AC OK FOR SERVICE.

Part: SIGN — FAULTY (EMERGENCY LIGHTS) · airframe 73,059 hrs · 11,847 cycles

EMERGENCY EXIT LIGHT IN COCKPIT IS ON WHEN SWITCH IS IN ARMED POSITION WHILE ON GROUND. REPLACED PORTABLE EMERGENCY EXIT SIGN ABOVE FLIGHT DECK DOOR PER MM 33-51-01. OPS CHECK GOOD. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 72,696 hrs · 11,796 cycles

EXTERIOR EMERGENCY LIGHT JUST AFT OF LEFT WING INOP. REPLACED LAMP, OP CHECKS OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,696 hrs · 11,796 cycles

EEL LIGHT AT SEAT 35FG INOPERATIVE. REPLACED LAMP, OP CHECKS OK FOR SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 42,781 hrs · 26,831 cycles

FUSELAGE SKIN APPROX STA 280 BETWEEN STR 2L & 3L HAS BLEND MARKS. MAJOR REPAIR ACCOMPLISHED: MFG'D AND INSTALLED REPAIR DOUBLER WITH BLIND FASTENERS.

Part: ASPIRATOR — LEAKING (EVAC SLIDE)

DAMAGED ASPIRATOR, LEAKING.

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 72,049 hrs · 11,708 cycles

LAVATORY 101 SMOKE DETECTOR INOP.

Part: GENERATOR — MALFUNCTIONED (RIGHT) · airframe 71,835 hrs · 11,675 cycles

FLIGHT DIVERTED DUE TO LOSS OF THE RIGHT GENERATOR. EMERGENCY LANDING WAS DECLARED.

Part: PUMP — FAILED (FUEL) · airframe 71,219 hrs · 11,575 cycles

FLIGHT DIVERTED DUE TO LOSS OF RIGHT MAIN FUEL PUMPS. PUMP CONNECTORS WHERE CROSSED. ALSO FOUND FOUND RIGHT AFT BOOST PUMP CKT BK R OUT C371 .REPLACED BREAKER,FOUND WIRE ARCHING ACCOUNT OF SCREW CROSS THREADED. PERFORMED OPS CHECK.

Part: VALVE — STICKING (EXHAUST) · airframe 70,475 hrs · 11,450 cycles

A-C EXPERIENCING EQUIP COOLING FAULTS. V12 OVERBOARD EXHAUST VALVE FOUND TO BE STICKING IN THE PARTIALLY CLOSED POSITION. REPLACED V12 EXHAUST VALVE. DIDN'T SOLVE PROBLEM. :REMOVED & REPLACED EQUIPMENT COOLING OVERHEAT SWITCH. FOUND SUFFICIENT AIR SOURCE IN DUCTING.

Part: FIRE DETECTOR — FAULTY (FWD CARGO BAY) · airframe 69,986 hrs · 11,369 cycles

FWD CARGO DETECTOR NR 2 AND GROUND PROXIMITY SYS STATUS WILL NOT CLEAR. [08-08-07] RESTARTED SYSTEM. FWD CARGO "DET 2" MSG CLEARED. GROUND PROX SYSTEM MESSAGE STILL PRESENT. RESET GLIDESLOPE DISCRETE PER MM34-46-00 MESSAGE CLEARED. MESSAGE REPEATED 8 DAYS LATER. ACCOMPLISHED TEST OF SMOKE DETECTION SYSTEM PER MM 26-16-00 P105. ALL TESTS WERE NORMAL, NO EICAS OR STATUS MESSAGES DISPLAYED. NO HARDWARE CHANGED OR IMPLICAED. AIRCRAFT OK FOR SERVICE.

Part: SENSOR — OUT OF ADJUST (EMERGENCY EXIT) · airframe 69,841 hrs · 11,343 cycles

EMERGENCY DOORS LIGHT ILLUM WITH EICAS MSG POS 11 (05=L EMER DR , 06=R EMER DR, 11=L WING SLIDE, 12=R WING SLIDE). *S/D* FOUND SENSOR FOR DOOR CLOSED, S218 OUT OF ADJUSTMENT. SHIMMED AND ADJUSTED SENSOR PER MM 52-71-00. REACTIVATED DOOR PER MM 25-65-00. OP CHECKED OK FOR SERVICE.

Part: FUEL — LEAKING (RT ENGINE) · airframe 69,598 hrs · 11,303 cycles

NOTICED DURING WALKAROUND INSPECTION RUNNING FUEL LEAK OUT OF UPPER PYLON AREA ON RIGHT ENGINE. [07-31-07] FOUND O-RING ON COUPLING "AS" REF IPC 28-22-07 PAGE17 SPLIT IN TWO PIECES. PACKING WAS WRO INSTALLED REF IPC.FOUND O-RING BETWEEN COUPLING NUT AND ONE RETAINING RING INSTALLED INSTEAD OF IN BETWEEN BOTH RETAINING RINGS. REPLACED PN:MS29513-330 AT FRONT SPAR MAIN FEED LINE COUPLING. LEAK CHECK SATIS. SUSPECT HEAT/COLD CYCLE, VIBRATION & SUBSEQUENT TIGHTENING CAUSED O-RING TO SPLIT.

Part: ODOR — DETECTED (COCKPIT) · airframe 65,557 hrs · 10,630 cycles

NOTIFIED BY TAXI CREW, WHEN AC WAS POWERED UP, ELECTRICAL BURNING SMELL STARTED, AC WAS VENTILATED WITH NO HELP. REPLACED SUPPLY COOLING FAN PER MM ALSO CLEANED FAN FILTER SCREEN. OPS CHECKED. BEARINGS FAILED IN FAN.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 65,557 hrs · 10,630 cycles

FUSELAGE DAMAGED UNDER AFT CARGO DOOR. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR DOUBLERS. REFERENCE UA EVA60460 AND SRM.

Part: ASPIRATOR — UNSERVICEABLE (TUBE NEAR ASPIRA) · airframe 64,046 hrs · 10,416 cycles

DAMAGED ASPIRATOR AND HOLES IN THE OPPOSITE TUBE. ASPIRATOR CAUSED HOLES IN THE TUBE. ALSO, ASPIRATOR HAD A BAD SEAL WHICH MADE IT LEAK. PATCHED THE INFLATION CHAMBER AND REPLACED THE ASPIRATOR. ROOT CAUSE WAS ASPIRATOR PACKED IN SUCH A WAY AS TO ABRADE A HOLE IN SLIDE TUBE DURING NORMAL DOOR OPERATION.

Part: WIRE HARNESS — BURNED (CARGO LOAD SYS) · airframe 64,507 hrs · 10,468 cycles

FWD CARGO PIT LOADING SYSTEM IS POPPING SEVERAL C/B'S. FOUND WIRE HARNESS BURNED AT CLAMP BELOW FLOOR IN FWD PIT STA 650. FWD CARGO PIT LOADING SYS. IS INOP. FOUND WIRE HARNESS BURNT AT CLAMP BELOW FLOOR IN FWD PIT STA.650,JUST RH OF CENTERLINE. PERFORMED WIRE REPAIR. & REPAIRED DAMAGED INSULATION. REPAIRED POWER WIRES FOR 11R, 12L, AND 12R. RESPLICED EACH LINE IN BURNED WIRE BUNDLE FWD PIT. INSTALLED COAX. A/C RETURNED TO SERVICE. SUSPECT CARGO LOADING OPS DAMAGE.

Part: STIFFENER — GOUGED (BS 303) · airframe 64,097 hrs · 10,387 cycles

L-1 DOOR CABLE HAS RUBBED A DEEP GOUGE IN FRAME STIFFENER AFT SIDE OF BS 303 FRAME AT STR 1R. GOUGED SUPPORT MEMBER REPLACED AND INSTALLED PER SRM.

Part: ATTACH ANGLE — CRACKED (BS 246) · airframe 64,097 hrs · 10,387 cycles

FLOORBEAM TO WEB ATTACH ANGLE AT BS 246 APPROX LBL 48, COCKPIT ENTRY STEP IS CRACKED. CRACKED ANGLE REPLACED PER SRM. ANGLE FOUND DURING ROUTINE INSPECTION PROGRAM PER BOEING SERVICE BULLETIN 767-53-0093.

Part: FRAME — CORRODED (BS 1153) · airframe 64,097 hrs · 10,387 cycles

AFT PIT FLOOR FRAME UPPER CHORD AT BS 1153, LBL 24 TO RBL 18 CORRODED ON TOP AND BOTTOM SURFACES. CORRODED FRAME ASSY PIECES REPLACED AND SPLICED PER SRM.

Part: BUSHING — MIGRATED (NR 2 PYLON) · airframe 64,097 hrs · 10,387 cycles

NR 2 ENG PYLON INBOARD MIDSPAR FITTING OUTBOARD LUG BUSHING MIGRATED. NR 2 ENG PYLON INBD MIDSPAR FITTING OUTBD LUG BUSHING WAS FOUND MIGRATED. 4 EACH MIDSPAR BUSHINGS WERE FABRICATED PER SRM 54-53-90, REPAIR 3 & REPLACED PER GN-MM 01-0- 01-013.

Part: SEAT TRACK — CORRODED (BS 1087) · airframe 64,097 hrs · 10,387 cycles

MAIN CABIN STA 1087, SEAT TRACK RBL 88 IS CORRODED. A 20 INCH SECTION OF CORRODED SEAT TRACK REPLACED WITH NEW, PER SRM.

Part: SEAT TRACK — CORRODED (BS 1197-1213) · airframe 64,097 hrs · 10,387 cycles

SEAT TRACK IN MAIN CABIN HAS AREAS OF GOUGES AND CORROSION STA 1197 + 142 TO 1213, 88 RBL. GOUGED SECTIONS OF SEAT TRACK REPLACED WITH NEW, PER SRM.

Part: SEAT TRACK — GOUGED (BS 1302-1325) · airframe 64,097 hrs · 10,387 cycles

AFT CABIN SEAT TRACK GOUGED STA 1302 - 1325 LBL 11. SECTION OF AFT CABIN SEAT TRACK GOUGED BY UNKNOWN ORIGIN. REPAIRED PER SRM.

Part: LATCH — WORN (CABIN)

NR 3 LATCH EDGE MARGIN BEYOND LIMITS. REMOVED AND REPLACED NR 3 LATCH IAW B767 MM 25-65-98.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 63,010 hrs · 10,192 cycles

LANDED ORD UNDER AMBER ALERT DUE TO TRAILING EDGE FLAP INDICATION PROBLEM.

Part: WARNING SYSTEM — ACTIVATED (FLAPS) · airframe 62,849 hrs · 10,166 cycles

ABORTED TAKE OFF DUE TO FLAP CONFIGURATION MESSAGE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,740 hrs · 9,352 cycles

CABIN FLOORBEAM UPPER SURFACE CORRODED, STA 808-813, RBL 57. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM SPLICE.

Part: HINGE — CRACKED (RT TE FLAP) · airframe 57,740 hrs · 9,352 cycles

RT INBD AFT FLAP EXTERNAL HINGE IS CRACKED AT THE MID FLAP AFT SPAR. REPAIRED FITTING WITH ANGLE REPAIR.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 57,905 hrs · 9,380 cycles

LOST RIGHT HYDRAULIC SYSTEM EN ROUTE, CONTINUING TO DESTINATION. LOSS OF PRESSURE DUE TO FAILED NR 2 ENGINE DRIVEN PUMP. PUMP HAS INDICATION OF OVERHEAT CONDITION. NO ADDITIONAL DETAILS FROM OSV REPORTED.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 56,833 hrs · 9,193 cycles

RIGHT SIDE AISLE NEXT TO MID GALLEY 1 EEL LIGHT STRIP SECTION OUT. *S/D* REPLACED CABLE AND SPLICED IN A NEW SECTION.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 56,054 hrs · 9,061 cycles

EXTERIOR EMERGENCY LIGHT INOP AT LT FUSELAGE AFT OF TRAILING EDGE. RELAMPED, CHECKED OK.

Part: WEDGE — DENTED (NR 4 SLAT) · airframe 55,101 hrs · 8,906 cycles

T/E WEDGE DENTED ON UPPER SURFACE OF NR 4 SLAT. MAJOR REPAIR. REPLACED WITH NEW T/E WEDGE.

Part: SPAR — CRACKED (NR 2 PYLON) · airframe 51,314 hrs · 8,272 cycles

NR 2 PYLON UPPER SPAR WEB AT STA 180 IS CRACKED AT RADIUS OF CUTOUT. MAJOR REPAIR ACCOMPLISHED. REPAIRED UPPER SPAR WEB WITH DOUBLER AND ANGLE REPAIR.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,314 hrs · 8,272 cycles

L-ANGLE AND CHANNEL CRACKED BETWEEN STA 325 AND 347 AT RBL 42.69. L-ANGLE ATTACHES TO THE FORWARD END OF C-CHANNEL FLOORBOARD SUPPORT AT RBL 42.69 TO THE STA 325, FLOORBEAM. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW L-ANGLE AND NEW CHANNEL.

Part: SPAR — CRACKED (NR 1 PYLON) · airframe 51,314 hrs · 8,272 cycles

NR 1 PYLON UPPER SPAR WEB CRACKED AT AFT CUTOUT, AFT OUTBOARD RADIUS. MAJOR REPAIR ACCOMPLISHED. REPAIRED WEB W/DOUBLER.

Part: DRIVE UNIT — FAILED (WEATHER RADAR) · airframe 49,582 hrs · 7,981 cycles

WEATHER RADAR FAILED. THE ANTENNA DRIVE UNIT AND FLAT PLATE WERE REPLACED AND SYSTEM OPERATION RESTORED. SHOP TEST OF THE FLAT PLATE FOUND THE UNIT WITHIN SPECS. THE ANTENNA DRIVE UNIT FAILED SHOP TEST.

Part: BATTERY — FAULTY (CABIN) · airframe 47,729 hrs · 7,640 cycles

SMOKE SMELL AT DOOR 1L. FAULTY EMERGENCY EXIT LIGHT CHARGER AND BATTERY WERE REPLACED AT DOOR 1L.

Part: O-RING — LEAKING (PRESSURE SWITCH)

CENTER HYDRAULIC FLUID LOSS. AMBER ALERT. DIVERTED ORD. *S/D* FOUND FLUID LEAKING FROM CENTER PUMP FILTER MODULE DELTA PRESSURE SWITCH. REPLACED ''O'' RING.

Part: AIRFRAME — VIBRATION (CABIN)

CREW REPORTED VIBRATION AND RUMBLING AT RIGHT SIDE OF MID CABIN AREA. STARTED AROUND 320 KTS. RETURNED TO DUS. ETOPS. *S/D* SEQ NR 3272003: CREW FELT AND HEARD NOISE; SUGGESTED LOOSE EXTERIOR PANEL. A/C CK'D FOR OPEN OR LOOSE PNL, DOOR AND LNDG GR DRS, FOUND OK. AC PACKS AND EXHAUST CK'D GOOD, NORMAL OPS. NOTE SEQ NR 6672006 (11/03/97): NR 2 ENG HIGH VIBRATION FELT IN AIRFRAME OR THROTTLE AT HIGH PWR. INSPECTED INLET/EXHAUST, NO DISCREPANCIES. CHIP DETECTORS CHECKED. ENGINE VIBRATION WITHIN LIMITS PER MMOV 77-31-00. ORIGINAL INSPECTIONS FOUND NO PROBLEMS. A/C HAD NO RELATED PROBLEMS FOR 24 DAYS. NO RELATED PROBLEMS FROM 11/03. ISOLATED INCIDENTS, NO FURTHER ACTION.

Part: TR UNIT — INTERMITTENT (RIBBON CABLE)

WEATHER RADAR FAIL ON HSI. DUMPED FUEL, RETURNED TO FIELD, OVERWEIGHT LANDING. *S/D* FOUND WEATHER RADAR TRANSCEIVER FAILED. REPLACED WEATHER RADAR TRANSCEIVER.

Part: BYPASS VALVE — FAILED (TE FLAP)

WHEN RETRACTING FLAPS, TE DISAGREE MSG APPEARED WHEN FLAP HANDLE WAS MOVED FROM 5 DEG TO 1 DEG. RETURNED TO JFK. *S/D* A FAULTY TRAILING EDGE FLAP POWER DRIVE UNIT BYPASS VALVE PREVENTED AFT FLAPS FROM RETRACTING TO THE COMMANDED POSITION. THE FLAP/SLAT ELECTRONICS UNIT SENSED THE DISAGREEMENT BETWEEN THE FLAP LEVER POSITION AND FLAP POSITION AND DROVE THE 'T/E FLAP DISAGREE' CAUTION ALERT MSG TO APPEAR ON EICAS AND THE 'TRAILING EDGE' AMBER LIGHT TO ILLUMINATE. THE BYPASS VALVE ON THE T/E FLAP PDU CONTROL VALVE WAS REPLACED AND TESTED AND THE FLAP/SLAT SYSTEM OPS CHECKED AND VERIFIED NORMAL PER MM.

Part: GASKET — WORN (STAB TRIM)

LEFT HYDRAULIC EICAS MESSAGE AND QUANTITY LIGHT ON OVERHEAD CAME ON DURING TAKEOFF WITH HYDRAULIC QUANTITY INDICATION DROP. *S/D* REPLACED LEAKING STAB TRIM SERVO PLATE GASKET.

Part: BEARING — WORN (LT/RT WING)

INBOARD AILERONS BINDED AT CRUISE ALTITUDE IN THE MANUAL MODE, AND WERE SMOOTH WITH THE AUTOPILOT CONNECTED. THE BEARING WAS GRITTY AND WORN. REPLACED BEARING ON FEEL AND CENTERING SPRING MECHANISM. INSPECTED CABLE RUNS IN E/E BAY AND BOTH LEFT AND RIGHT WING AREAS, ALL CHECK NORMAL.

Part: CONTROLS — LOCKED OUT (AILERON)

AN AILERON LOCKOUT OCCURRED IN FLIGHT. THE EICAS DISPLAY VERIFIED THIS CONDITION. THIS INDICATION WILL BE ADDRESSED BY THE ACCOMPLISHMENT OF BOEING SERVICE LETTER 767-27-081-A.

Part: HARNESS — ARCED (CABIN)

FOUND WIRE BUNDLE ARCING ALONG SIDEWALL FLOOR BETWEEN SEATS 2A AND 3A. FOUND CHAFED WIRES DUE TO CONTACT WITH SIDE WALL GRILL. REPAIRED WIRES. SYSTEM OPS CHECKS OK.