N67058

Part: WARNING MESSAGE — ILLUMINATED (ZONE 800) · airframe 89,132 hrs · 12,442 cycles

AFTER ENG START, LEFT AFT ENT DOOR MSG DISPLAYED LEFT AFT ENTRY DOOR UPPER EICAS LEFT AFT ENTRY DOOR DISPLAYED. AFT LEFT ENTRY DOOR VERIFIED CLOSED AND TARGET NEAR PLACED ON MEL. VERIFIED DOOR L2 IS CLOSED ON INSIDE AND OUTSIDE HANDLE IS RECESSED AND IN PLACE.

Part: ANTI-ICE VALVE — FAULTED (RT ENGINE) · airframe 89,032 hrs · 12,427 cycles

RIGHT ENG ANTI ICE LIGHT REMAINS ILLUM AFTER COMPLETION OF NON NORMAL PROCEDURE. ORDERED ENGINE TAI VALVE M&E NUMBER 75-3023-9-0001 AND WING AND ENGINE ANTI ICE CONTROL PANEL M&E NUMBER 64-3112-9-9010 AND PLACED IN COCKPIT FOUND RH ENGINE INLET THERMAL ANTI ICE PRESSURE SWITCH TO SHOW SIGNS OF CORROSION, REMOVED AND REPLACED RH ENGINE INLET THERMAL ANTI ICE PRESSURE SWITCH IN REF TO AMM 30-21-01. ALSO PERFORMED TAI VALVE TEST IN REF TO AMM 30-21-03-404-022. OPS CHECK GOOD, NO FURTHER DISCREPANCIES NOTED.

Part: O-RING — DETERIORATED (ZONE 100) · airframe 88,616 hrs · 12,371 cycles

SIGNIFICANT FUEL SMELL THROUGHOUT CABIN WHILE DOING EXTERIOR WALKAROUND FOUND APU LEAKING FUEL. UPON FURTHER INSPECTION FOUND FUEL LINES GOING TO APU FUEL CONTROL LEAKING FUEL. REMOVED FUEL TUBES TO FUEL CONTROL UNIT. FOUND O-RINGS DETERIORATED. REPLACED O-RINGS AND REINSTALLED FUEL TUBES IAW AMM 49-31-01. OPS AND LEAK CHECKS GOOD. NO FUEL SMELL NOTED IN CABIN. REMOVED AND REPLACED RECIRCULATION AIR FILTER IAW AMM REF TASK 21-25-02-004-020-001. NO ODOR IN CABIN WITH APU AND PACKS RUNNING.

Part: BLEED VALVE — FAULTED (NR 1 ENGINE) · airframe 87,429 hrs · 12,216 cycles

L ENG OVERHEAT ON CLIMBOUT WITH ASSOCIATED BLEED OFF AND PACK OF F. COULD NOT RECOVER PERFORMED FIM 26-11 FAULT TREE 807. SEE L/P 4678470 FOR REPLACEMENT OF # 1 ENGINE FAN AIR VALVE (DUE TO HIGH PRECOOLER OUT DUCT TEMPERATURE) AS PER MM-36-11-16/401. RAN # 1 ENGINE AT POWER. ALL CHECKS GOOD

Part: UNKNOWN — ODOR (CABIN) · airframe 86,951 hrs · 12,153 cycles

ELECTRICAL BURNING SMELL IN FWD GALLEY AND COCKPI T GALLEY AREA INSPECTED IAW AMM 05-51-56,REV 143, NO FINDINGS, NOR MAL SMELLCOCKPIT AREA INSPECTED IAW AMM 05-51-56,REV 143,ALL C /B PANELS P11 OPENED, INSPECTED AND CLOSED IAW AMM, NO FINDINGS , ADDITIONAL INSPECTION C/OUT BEHIND P5 PANEL WITH BRIGHNESS OF LIGHTS IN NORMAL POSITION, NO ABNORMAL SMELL AND NO FINDINGS, CONDITION GOOD NOW, SMELL

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 86,532 hrs · 12,101 cycles

EMERGENCY LIGHTS SIGNS FROM DOOR L1 AND R1 DOES NOT COMES ON PERFORMED FIM 33-51 TASK 803 IT WAS FOUND BATTERY PACK FROM 1208 WITHOUND LOAD, REPLACED IT AS REF 33-51-07-022-005-001, ITEM OK

Part: DOOR — MISSING (ZONE 600) · airframe 85,776 hrs · 12,003 cycles

PDA 2 SLAT # 8, TELESCOPING DUCT TAI SEAL DOOR MISSING PICTURES ATTACHED SDR ACCOMPLISHED NO SDR OR PDA REQUIRED DUPLICATE WRITE UP, REF LP 9419899

Part: ACCESS DOOR — MISSING (NR 2 NACELLE) · airframe 84,786 hrs · 11,861 cycles

PDA 2 NACELLE STRUT ACCESS DOOR ( PANEL #436AR ) MISSING, INBOARD OF ENG 1 PYLON. UPDATED WITH PICTURE. UPDATED WITH SUBMITTED ESDR REPORT. UPON LANDING WITH NO REPORTED EMERGENCY REPORTED, FOUND #1 ENG INBD NACELLE ACCESS DOOR 436AR MISSING UPON ROUTINE WALK AROUND INSP. REF IPC 54-53-01-16 ITEM 448, MFG P/N 311T1065-97SD. REF ECRA 5450-02589 FOR MFG SUPPLIER. M&E P/N 64-5450-3-0028. INSTALLED NEW PANEL 436AR, REF AMM 54-53-01. P

Part: PUMP — FAILED (LT BOOST) · airframe 83,208 hrs · 11,645 cycles

L AFT FUEL PUMP EICAS WITH L AFT FUEL BOOST PUMP CB POPPED. RECENT HISTORY SHOWS GFI K10703 WAS REPLACED BUT THAT COULD BE I DEBRIEFED CREW AND STATED THAT CB POPPED. BOOST PUMP OUT OF STOCK M&E 76-2821-9-9001. LT AFT PUMP OPS ON GFI K10705 CIRCUIT. DUE FLT DIVERSION AT CRUISE. LOCATION P6-3 GRID G15. , REPLACED LEFT AFT MAIN TANK FUEL BOOST PUMP REF. AMM 28-22-03-004-051 & 28-22-03-404-074. SOLD INSPECTION BUY-OFF TO INSPECTOR. OPERATIONAL CHECK GOOD. NO LEAKS NOTED.

Part: ACCESS PANEL — MISSING (LT WING) · airframe 83,182 hrs · 11,640 cycles

FOA LEADING EDGE SLAT 1 UNDER WING ACCESS PANEL MISSING. CONFIRMED 521AJB LEADING EDGE SLAT MECHANISM LUBRICATION ACCESS LEADING EDGE SLAT LINKAGE FAIRING PANELS INSTALLED. PARTS CDL FOLLOWED, INOP. DOORS MISSING. INSPECTED AREA NO DAMAGES FOUND. CHKD ALL WING INFORMED NSU AT GRU.

Part: AMU — POWER LOSS (STA 434, E4 RACK) · airframe 81,740 hrs · 11,448 cycles

LOST POWER TO ALL 3 RADIO CONTROL PANELS, NO COMMS IN REF TO TOMC LOCKED LOGPAGE 6273058: FOUND AUDIO MANAGMENT UNIT LOOSE IN RACK. PULLED AMU AND INSPECTED UNIT AND RACK AND FOUND NO DEFECTS NOTED. REINSTALLED AMU, CLOSED BREAKERS. ALL POWER RETURNED AND TEST CALL SAT TO TOWER. PER AMM 23-51-05 UPDATE WITH PICTURE OF UNSERCURE AMU . REPLACE AMU AT THE REQUEST OF TOMC REF LOGS 6274081 AND 6273058 . REMOVED AND REPLACED AMU, OPS CK GOOD NO FURTHER DEFECTS NOTED AT THIS TIME PER AMM 23-51-05. OVERWEIGHT LANDING WEIGHT 361.000 300FPM TOUCHDOWN COMPLIED WITH PHASE 1A AND 1B OVERWEIGHT LANDIND INSPECTIONS, NO DEFECTS NOTED PER AMM 05-51-01. THE TOMC CONTROLLER AND SENIOR MANAGER CONCUR THAT THE AIRCRAFT CAN BE RELEASED BACK TO SERVICE AFTER EXPERIENCING A DIVERSION OR AIR TURN BACK DUE TO A MECHANICAL REASON.

Part: B-NUT — LEAKING (LH MLG) · airframe 80,359 hrs · 11,249 cycles

C HYD QTY EICAS C. THE CENTER HYDRAULIC RESERVOIR QUANTITY IS LOW. NOTE: HYD AUTO E VENT C QTY .48 SERVICED CTR SYSTEM HYDRAULIC RESERVOIR TO DETERMINE IF QTY INDICATION ERROR. INDICATION CHECKED GOOD. VISUAL WALK AROUND INSPECTION SHOWS LEAK AT AREA ABOVE TOP OF L/H MLG. FOUND LH MLG RETRACT ACTUATOR UP HYDRAULIC HOSE NUT SEVERELY LEAKING WHEN THE GEAR HANDLE IS PUT INTO THE UP POSITION. UP HYDRAULIC HOSE NUT WAS LOOSE RESULTING IN THE LEAK. TIGHTENED UP HOSE NUT AND PERFORMED ACTUATOR INSTALLATION TEST PER AMM 32-32-01. OPS CHECK GOOD AT THIS TIME, NO MORE LEAKAGE NOTED AT THIS TIME. AIRCRAFT RETURNED TO RIGINAL CONFIGURATION.

Part: FMC — INOPERATIVE (RIGHT) · airframe 79,826 hrs · 11,165 cycles

R FMC FAIL AND FMC MSG EICAS REMOVED AND REPLACED RIGHT FLIGHT MANAGEMENT COMPUTER REF. AMM 34-61-01, CHECKS GOOD. PARTS USED: 1819614,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1819614 SN OFF 9674 COMPUTER, FLT M OFF 19-3461-9-0004 9674 ON 19-3461-9-0004 9495

Part: BEAM — CORRODED (STA 303 LBL 50) · airframe 79,668 hrs · 11,139 cycles

CABIN FWD WET FLOOR BEAM FOUND CORROSION AT STA 303 LBL 50 CARRIED OUT THE FLOOR BEAM REPAIR AT CABIN FWD WET FLOOR BEAM ST A303 LBL50 AS PER EC/RA5310-08148.DETAIL PER BSH N0746

Part: SKIN — DAMAGED (STA 1502 & 1518) · airframe 79,668 hrs · 11,139 cycles

BULK CARGO EXISTING DOUBLER REPAIR RIVET INSTALLED POOR CONDITIO N AT STA1518-1502S-25L AS PER JC 64-5300-1-2562 STALLED ON FUSELAGE SKIN BETWEEN STA 1502 & 1518 AND S24L & 25L EACHING 30,000 TOTAL FLIGHT CYCLES. REPEAT THE INSPECTION AT INT HAS BEEN APPROVED AS CATEGORY B REPAIR. PER THE LATEST REVISION OF ECRA 5360-01698 PART 2 ON OR BEFORE R ERVAL NOT TO EXCEED 12,000 FLIGHT CYCLES, THEREAFTER. THE REPAIR REPLACED THE EXISTING REPAIR AND TRIMMED A PORTION OF TEAR STRAP PER ECRA. 5360-01698. PER ECRA 5336-01698 INSPECT THE REPAIR IN PER ECRA 5360-01698:INSPECT THE REPAIR INSTALLED ON FUSELAGE TOMC-APPROVAL FROM SC1ELBYC COMMENT SKIN BETWEEN STA 1502 & 1518 AND S24L & 25L PER THE LATEST REVISION OF ECRA 5360-01698 PART 2 ON OR BEFORE REACHING 30,000 TOTAL FLIGHT CYCLES. REPEAT THE INSPECTION AT INTERVAL NOT TO EXCEED 12,000 FLIGHT CYCLES, THEREAFTER. QC REVIEWED QC REVIEWED INIT : 30000 TAFC RIR : 12000 FC (INIT WILL ITO TO RIR) --HK/U391876 RECORDS UPDATE--HK

Part: BEAM — CORRODED (STA325) · airframe 79,668 hrs · 11,139 cycles

CABIN FWD WET FLOOR BEAM FOUND CORROSION AT STA325 LBL50 AS PER JC64-5310-1-2602

Part: UNKNOWN — MALFUNCTIONED (LE SLAT) · airframe 79,597 hrs · 11,126 cycles

ON APPROACH DURING FLAP EXTENSION LE SLAT DISAGR EE EICAS MESSAG E. EICAS MSG LE SLAT SHUTDOWN, REF B767-4 FIM 27-81 TASK 815, FSEU BITE SHOWS LE OUTBOARD PDU RVDT MSG NMBR 27-81041 PERFORMED FIM TASK 27-51-00-815-809.. CLEARED FAULT ON PSEU AND OPERATED FLAPS SERVERAL TIMES ALL OPS CHECKED GOOD NO HISTORY ... REF AMM 27-81-11 AND FIM TASK 27-51-00-815-809

Part: LINE — LEAKING (HYD SYSTEM) · airframe 74,586 hrs · 10,401 cycles

MAIN (LEFT, RIGHT, AND CENTER) HYDRAULIC SYSTEMSC HYD QTY DECREASED TO ____. QTY STABLE WITH SYSTEM PUMPS OFF CENTER HYD QTY DECREASED TO .46. IT ROSE TO .54 AND IS STABLE. UPON INSPECTION OF CENTER HYD QTY LOSS WITH STABLE HYD PRESSURE FOUNDED THE MLG RETRACT ACTUATOR RETURN LINE LOOSE AND LEAKING HYD FLUID. TIGHTEN HYD LINE AS PER AMM 32-32-01. OPS AND LEAK CHECK GOOD. OK TO CONT. SERVICED THE CENTER HYD SYSTEM TO WITHIN LIMITS PER AMM 12-12-01-301. OK TO CONT.

Part: LAVATORY — MALFUNCTIONED · airframe 72,116 hrs · 10,053 cycles

LAVATORIES E, G, AN J TOILETS BACKING UP AND NOT FLUSHING AFTER SERVICING OPS CHECKED OK.

Part: LIGHT — LOOSE (SEAT 24F) · airframe 71,083 hrs · 9,917 cycles

SOME WIRES HANGING DOWN FROM SEAT 24F. FOUND EMERGENCY LIGHT ASSY LOOSE, SECURED THE LIGHT ASSY, OPS CHECKED GOOD.

Part: INDICATOR — LEAKING (HYD SYSTEM) · airframe 69,758 hrs · 9,734 cycles

CENTER HYDRAULIC SYSTEM LEAK. RAN THE CHECKLISTS AND LANDED WITH QTY AT .28. EMERGENCY DECLARED. FOUND FWD DPI ON CENTER ACMP FILTER MODULE LEAKING UNDER HEAD PRESSURE. R & R THE FWD DPI IAW AMM 29-11-18. SERVICED THE CENTER HYDRAULICS TO FULL, CLEANED AREA AND PERFORMED LEAK CHECK. DPI LEAK CHECKED GOOD, NO OTHER LEAKAGE NOTED.

Part: SLIDE — UNWANTED DEPLOY (R2 DOOR) · airframe 69,204 hrs · 9,653 cycles

R2 DOOR SLIDE DEPLOYED . FLIGHT ATTENDANT ACCIDENTALLY DEPLOYED THE SLIDE. REPLACED SLIDE IAW AMM 25-66-01 AND IPC 25-66 -01

Part: OVEN — SMOKE (MID GALLEY) · airframe 69,097 hrs · 9,639 cycles

GALLEY OVEN INOPERATIVE, FILLS WITH SMOKE AFTER 2 MINUTES OF USE MID GALLEY, CYCLED THE CIRCUIT BREAKER. OVEN GROUND CHECKED NORMAL.

Part: ALTIMETER — OUT OF LIMITS (STANDBY POSITION) · airframe 68,797 hrs · 9,595 cycles

STBY ALTIMETER STICKY IN CLIMB AND DESCENT JUMPS 500 FEET AT A TIME REMOVED AND REPLACED STBY ALTIMETER IAW AMM 34-13-06.

Part: MODULE — FAULTY (RIGHT) · airframe 67,645 hrs · 9,433 cycles

AFTER T/O GOT ALT DISAGREE EICAS. F/O WAS 3 TO 500 FT BELOW CAP T SIDE AND FLUCTUATING. EMERGENCY DECLARED. REMOVED AND REPLACED RT ADM PER 34-26-03-401. GRND CKS OK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 60,536 hrs · 8,456 cycles

SUPPORT TASK, EXTERIOR EMER LIGHTS AT 1L, 1R & 2R INOPERATIVE. REPLACED EMER LIGHT BATTERY IAW AMM 33-51-07-022- 005-0-01. OPERATIONS CHECKED GOOD IAW AMM 33-51-07-201-022-005-0-01.

Part: BATTERY — DISCHARGED (CABIN) · airframe 60,536 hrs · 8,456 cycles

SUPPORT TASK, SEAT 21F RT EMER LIGHT INOPERATIVE. REPLACED BATTERY FOR EMER LIGHT AT SEAT 21F RT IAW AMM 33-51-07. OPERATIONS CHECKED GOOD IAW AMM 33-51-07-201-022-005- 0-01.

Part: WIRE — SHORTED (CABIN) · airframe 54,696 hrs · 7,667 cycles

AFTER REPLACING EMERGENCY LIGHT BATTERIES SHIP SET FOUND EMERGENCY LIGHTS ON SEAT 5, 6 & 7 EMERGENCY LIGHT WILL NOT ILLUMINATE DURING TEST. R & R BATTERY CHARGER EQUIP LIST NBR M6757 SN OFF 16326 & SN ON 9250 AS PRECAUTIONARY IAW AMM TASK 33-51-0 7-002-014-0-001 & 33-51-07-402-018-0-001. SEAT 6D RT AFT LIGHT WIRES SHORTED & SEAT 7D LT FWD LIGHT WIRES SHORTED. R & R LIGHT ASSEMBLY, OPERATIONS CHECKED GOOD DELAY TM FOR 229 MINS. PN FOR LIGHT ASSEMBLY BR9644-11.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 54,109 hrs · 7,584 cycles

DURING PREFLIGHT EMERGENCY LIGHTS CENTER AISLE LIGHTS ON SEAT GROUP WOULD NOT LIGHT UP POS 4-5-6D DUE TO PREVIOUS PROBLEMS. BATTERY CHARGER M06757 REPLACED IAW AMM 33-51-07-022-005-001 PN ON D717-02-030 SN ON 16326,PN OFF D717-02-030, SN OFF 15714. PERFORMED EMERGENCY LIGHTS OPEN TEST IAW AMM 33-51-00-715-001 SATIS

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 53,082 hrs · 7,451 cycles

EMERGENCY EXIT LIGHTS AT 1L AND 1R FLASH DURING FLIGHT. OPS CHECK OF CABIN EMERGENCY LIGHTS C/O IAW AMM 33-51-0 0-715-200 AND AMM 33-51-00-715-001, ALL SATISFACTORY. FOR FURTHER REPORT AS REQUIRED.

Part: OXYGEN MASK — DISCONNECTED (FLIGHT DECK) · airframe 50,255 hrs · 7,065 cycles

CAPTAIN`S O2 MASK CAME DETACHED FROM HOSE WHILE STOWING MASK AFTER USE. CREW OXY PRESSURE DEPLEATED. HOSE TIED IN KNOT TO PREVENT COMPLETE LOSS. R & R CAPTAIN`S O2 MASK WITH SERVICEABLE ASSY. O2 MASK AND MIC CHECKED NORMAL. CREW O2 SERVICED.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 48,119 hrs · 6,812 cycles

ROW 18/21 EMERGENCY LIGHTS INOPERATIVE. FOUND ROW 18 UNPLUGGED. RECONNECTED, CHECKED NORMAL.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 47,343 hrs · 6,714 cycles

CABIN BS 1241-1400 RBL 88 SEAT TRACK FOUND CORRODED. SEAT TRACK CORROSION REMOVED AS PER SRM51-10-02 BLEND OUT AREA D:0.040"X W:2.6"X L:3" SEVERAL LOCATION OUT OF SRM 53-00-52 ALLOWABLE DMG 1 FIG 101 LIMIT AND CORROSION SEAT TRACK REPAIR AS PER ECRA 5320-02051 REV- AT BS 1208 TO BS 1408 RBL 88.

Part: FLOORBEAM — CORRODED (BS 325) · airframe 47,343 hrs · 6,714 cycles

BS 325 RBL 55-56 FLOORBEAM FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-10-02, BLEND AREA D:0.037" (ORG 0.080) W:1"X L:2"X FOUND OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101 LIMITS AND FLOORBEAM REPAIRED AS PER SRM 53-00-51 FIG 201 REPAIR 1.

Part: FLOORBEAM — CORRODED (BS 325) · airframe 47,343 hrs · 6,714 cycles

BS 325 LBL 24-56 FLOORBEA, FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02, BLEND OUT AREA D:0.035"(ORG 0.090")X W:1" L:3". FOUND OUT OF LIMITS IAW SRM 53-00-51 REPAIR FIG 201.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 47,343 hrs · 6,714 cycles

CABIN BS 303-325 LBL 30 FLOOR SUPPORT FOUND CORRODED. CABIN BS 303-325 LBL 30" FLOOR SUPPORT CORROSION REMOVED AS PER SRM 51-10-021 BLEND OUT AREA D:0.032" X ORG.0.071" X W:1"X L:3" OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101. LIMIT AND CORRODED SUPPORT REPLACED AS PER SRM 51-10-02 AND NEW SUPPORT INSTALLED AS PER SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,343 hrs · 6,714 cycles

CABIN BS 303 LBL 18" -60" FLOOR SUPPORT FOUND CORRODED. CABIN BS 303 LBL 6" TO 65" FLOORBEAM UPPER FLANGE REPAIRED AS PER SRM 53-00-51 REPAIR + FIG 201 AND HFEC NIL CRACK FOUND. ATTACH MAINTENANCE WORKSHEET FORM 44.0008 ITEM 1 TO ITEM 27 ACCOMPLISHED.

Part: CONTROL PANEL — FALSE ACTIVATION (FIRE CONTROL) · airframe 39,601 hrs · 5,725 cycles

NEED TO CHANGE APU/CARGO FIRE CONTROL PANEL. R & R APU/CARGO FIRE CONTROL PANEL IAW AMM 26-22 -03. OPS CHECK GOOD. NO FAULTS NOTED AT THIS TIME. ROTABLE PARTS CHANGE WAS INDICATED - TT 1399482, SN OFF 00032, IPC REF PANEL, ASSY - A OFF 64-3111-9-9009 0032 ON 64-2622-9-9001 0019.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 9,943 hrs · 1,548 cycles

THE M732 EMERGENCY LIGHT POWER SUPPLY FAILED FUNCTIONAL TEST PER WORK CARD 64-3350-1-7100. REMOVED AND REPLACED EMERGENCY POWER SUPPLY AND BATTERY PACK IAW MM 33-51-07.