N451PA

Part: HINGE FITTING — CRACKED (ZONE 500 SPOILER) · airframe 101,546 hrs · 17,006 cycles

CRACK - FITTING, INBD LWR SIDE OF LH WING #6 SPOILER MID HINGE FITTING(<P>1) REPAIRED DAMAGE AREA IAW W/S 50588 &AMP; SRM 57-51-13-2R-1 REV 104. 2) CONDITION CHK NORMAL AND JOB COMPLETED.</P>)

Part: SKIN — CORRODED (ZONE 100) · airframe 101,546 hrs · 17,006 cycles

CORROSION ON LH FUSELAGE OUTER SKIN NEAR STA 1700, S42L(<P>1) REMOVED FASTENERS IAW SRM 51-40-02-0G-0 REV 104. 2) REPAIR DAMAGE SKIN IAW EI T2025A53M-1733 REV 104. 3) JOB COMPLETED AND CONDITION CHK NORMAL</P>)

Part: NOT ENTERED — NOT REPORTED (ZONE 100) · airframe 101,546 hrs · 17,006 cycles

CMR REQUEST CLARIFICATION FUSELAGE FASTENERS TYPE ON RH BODY SKIN NEAR STA 440, S26R(<P>1) ACCOMPLISHED EI T2025A53M-1774 REV 1. 2) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: SKIN — CORRODED (ZONE 100) · airframe 101,546 hrs · 17,006 cycles

CORROSION - SKIN, LH AFT LWR FUSELAGE SKIN STA 1732, S42L(<P>1) REPAIR THE DAMAGE IAW SRM 53-00-01-2R-1 REV 104 &AMP; W/S 50620. 2) CONDITION CHK NORMAL AND JOB COMPLETED</P>)

Part: SKIN — DAMAGED (ZONE 500 FLAP) · airframe 100,781 hrs · 16,886 cycles

LH INBOARD AFT FLAP DAMAGE OUT OF LIMITS 12" LENGTH AND 9" WIDTH UPPER SURFACE AND 10" LENGTH AND 5" WIDTH LOWER SURFACE.(<P>PERFORMED PERMANENT REPAIR IAW EA-1957A224, SRM 57-53-01-2R-1 AND SRM 51-70-07-0G-0. NO FURTHER DEFECTS NOTED.</P>)

Part: CONTROL UNIT — FAILED (ZONE 700) · airframe 100,693 hrs · 16,872 cycles

RIGHT MAIN BODY GEAR TIRE FAILURE ON TAKEOFF FROM HKG.(<P>REMOVED AND REPLACED BRAKE CONTROL UNIT AND R/H BODY GEAR ANTI SKID MODULE. REMOVED AND REPLACED #9 &AMP; #10 MAIN WHEEL ASSEMBLIES. PERFORMED THE FOLLOWING CONDITIONAL INSPECTIONS:</P> / <P>SINGLE FLAT / BLOWN TIRE, WHEEL WELL BURST TIRE, PARTS DEPART A/C, HARD / OVERWEIGHT / HIGH DRAG SIDE, LOAD CONDITION. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.</P> / <P>&NBSP;</P> / <P>&NBSP;</P>)

Part: CURTAIN — TORN (ZONE 200) · airframe 100,596 hrs · 16,853 cycles

BULK CARGO STA 2160 CURTAIN FOUND TORN(<P>PERMANENT REPAIR CARRIED OUT AS PER RI-25-54-17582 REV. A. NO FURTHER DEFECTS NOTED</P>)

Part: FAN — FAILED (ZONE 100) · airframe 98,205 hrs · 16,488 cycles

POSSIBLE BURNING ELECTRICAL SMELL IN FLIGHT DECK WHILE A/C ON GROUND(<P>FOUND FWD EQPT COOLING SUPPLY FAN HEATED &AMP; SMALL BURNT SMELL SO R/R EQPT COOLING SUPPLY FAN. OPS &AMP; SMELL CHECK GOOD PER AMM 21-58-01/401 &AMP; IPC 21-58-01-01. CONDITION CHECK NORMAL PER AMM 5-51-56/201.</P>)

Part: LIGHT — SPARKS (COCKPIT) · airframe 97,555 hrs · 16,388 cycles

CO PILOTS FLOOD LIGHT SPARKS AND SMOKE.(<P>REPAIRED WIRING AS PER SWPM 20-10-13, REPLACED MAP LIGHT AS PER AMM 33-15-00. OPS CHECK GOOD</P>)

Part: PUMP — FAULTED (HYD SYSTEM) · airframe 96,491 hrs · 16,220 cycles

HYD PRESS SYS 1 CAUTION MSG IN FLIGHT. BOTH ENG AND DEMAND PUMP ON SYSTEM 1 INOP(<P>R/R #1 ENG DRIVEN PUMP. REMOVED &AMP; INSPECTED ALL SYS 1 HYD FILTERS, NO CONTAMINATION OR DISCREPANCIES FOUND. ENGINE IDLE RUNS &AMP; LEAK CHECK NORMAL. REF LP 1797125 M5: R/R ADP 1, OPS AND LEAK CHK OK PER AMM 29-11-08-401. REF LP 1797125 M6: R/R #1 ENG DRIVEN PUMP IAW AMM 29-11-05. ENGINE IDLE TEST RUN AND LEAK CHECK NORMAL IAW AMM 71-00-00. THIS ACTION CLEARS DMI #206802. PLACARD REMOVED.</P>)

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 96,448 hrs · 16,214 cycles

LHW T/E I/B MID FLAP L/E FOUND BIRD STRIKE(<P>LHW T/E I/B MID FLAP L/E BIRD STRIKE AREA, PERFORMED TIME LIMIT REPAIR AS PER EA-1957A0103 REV 0. NO FURTHER DEFECTS NOTED.</P>)

Part: BATTERY — UNKNOWN (UNKNOWN) · airframe 94,440 hrs · 15,909 cycles

FOUND ALL EMERGENCY LIGHT BATTYER ASSY FUNCTION FAIL. TT23 EACH(<P>1) IAW AMM 33-51-04-902-001-001 REV 108 REPLACED ALL EMERGENCY LIGHT BATTERY ASSY, CONDITION CHECK NORMAL. 2) IAW AMM 33-51-04-902-001-001 REV 108 PERFORMED INSTALLATION TEST OF ALL EMERGENCY LIGHT BATTERY. THE RESULT WAS SATISFACTORY</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,440 hrs · 15,909 cycles

FOUND L5 DOOR WEB CRACK AT STA 2231 S21L - S22L(<P>1) REPAIRED DAMAGE AREA IAW SRM 51-40-02-0G-0 REV 98 &AMP; EI T2023A53M-2634 REV 0. 2) ACCOMPLISHED EI T2023A53M-2634 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,440 hrs · 15,909 cycles

FOUND FLOOR STRUCTURE SUBSTITUTE TRACK CRACK AT STA 2060-2100 LBL 75.92(<P>1) REPAIR DAMAGE AREA IAW SRM 53-00-52-2R-13 REV 98. 2) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,440 hrs · 15,909 cycles

DEVIATION - DURING PERFORMING EO 4453A087 PART 2 STA 340 RH UPPER CHORD STRAP HAVE 1 EACH FASTENER CAN'T REMOVE(<P>1) PERFORM JOB IAW EI T2023A53M-2577 SEQUENCE A REV 0. 2) ACCOMPLISHED EI T2023A53M-2577 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,440 hrs · 15,909 cycles

EXISTING REPAIR AT AFT CGO DOOR OUTER SKIN FWD LOWER EDGE(<P>1) PERFORM JOB IAW EI T2023A52M-2623 SEQUENCE E REV 4. 2) ACCOMPLISHED EI T2023A52M-2623 REV 5. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,440 hrs · 15,909 cycles

DEVIATION - DURING PERFORMING EO 4453A087 PART 2 RH FRAME STA 500 HAVE 2 EACH FLUSH FASTENER(<P>1) PERFORM JOB IAW EI T2023A53M-2564 SEQUENCE A REV 0. 2) ACCOMPLISHED EI T2023A53M-2504 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,440 hrs · 15,909 cycles

DEVIATION - DURING PERFORMING EO 4453A087 PART 2 STA 340 LH UPPER CHORD STRAP HAVE 1 EACH FASTENER CAN'T REMOVE(<P>1) PERFORM JOB IAW EI T2023A53M-2576 SEQUENCE A REV 0. 2) ACCOMPLISHED EI T2023A53M-2576 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: SHEAR TIE — UNKNOWN (UNKNOWN) · airframe 94,440 hrs · 15,909 cycles

CRACK - FOUND SHEAR TIE CRACK AT STA 1000 RBL 57/5(<P>1) REMOVED DAMAGE PART IAW SRM 51-40-02-0G-0 REV 98. 2) INSTALLED NEW SHEAR TIE IAW EI T2023A53M-2465 REV 0, EI ATTACHING TO W/O: 8745973. 3) ACCOMPLISHED EI T2023A53M-2465 REV 1, EI ATTACHING TO WO: 875973 &AMP; EO 4453C024 PART 9 REV 3. 4) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,440 hrs · 15,909 cycles

DEVIATION - DURING PERFORMING EO 4453A087 PART 2, STA 360 RH UPPER CHORD STRAP HAVE 2 EACH EXISTING FASTENER WAS 1/4"(<P>1) PERFORM JOB IAW EI T2023A53M-2628 SEQUENCE A REV 0. 2) ACCOMPLISHED EI T2023A53M-2628 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: LAMP — UNKNOWN (UNKNOWN) · airframe 94,440 hrs · 15,909 cycles

FOUND SLIDE LIGHT LAMP INOP AT UPPER DECK RH SIDE(<P>1) IAW AMM 33-51-10-962-001 REV 108 REPLACED LIGHT LAMP AT UPPER DECK RH SIDE, CONDITIONAL CHECK NORMAL. 2) IAW AMM 33-51-10-402-005 REV 108 PERFORMED LIGHT TEST OF SLIDE LIGHT. THE RESULT WAS SATISFACTORY</P>)

Part: SHEAR TIE — UNKNOWN (UNKNOWN) · airframe 94,440 hrs · 15,909 cycles

CRACK - FOUND SHEAR TIE CRACK AT STA1000 LBL 57.5(<P>1) REMOVED THE DAMAGE PART IAW SRM 51-40-02-0G-0 REV 98. 2) INSTALL NEW SHEAR TIE IAW EI T2023A53M-2465 REV 0. 3) ACCOMPLISHED EI T2023A53M-2465 REV 1 &AMP; EI 4453C024 PART 5 REV 3. 4) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,223 hrs · 15,728 cycles

APU FIRE ON EICAS, QRH PROCEEDURE PERFORMED SUCCESSFULLY, RETURN TO BLOCK.(<P>PERFORMED INSPECTION PER AMM 49-11-00-206-029, NO EVIDENCE OF APU FIRE OR DAMAGE NOTED.</P>)

Part: SEQUENCE VALVE — UNKNOWN · airframe 93,068 hrs · 15,703 cycles

NOSE GEAR DOES NOT REMAIN STOWED AFTER RETRACTION(<P>COMPLIED WITH ACTION PLAN 24223. JACKED AIRCRAFT AND PERFORMED MULTIPLE GEAR SWINGS WITH NO FAULTS. PERFORMED CONFIDENCE FLIGHT WITH NO FAULTS.</P>)

Part: VALVE — UNKNOWN · airframe 93,068 hrs · 15,702 cycles

NOSE GEAR FAIR TO FULLY RETRACT AND STOW(<P>REF 744 AMM 32-34-00, PERFORMED TROUBLESHOOTING AND REPLACED NOSE LANDING GEAR DOOR. OPERATED SEQUENCE VALVE AS PER 744 AMM 32-34-05/401 AND OPS CHECKED NIL EFFECTIVED. ITEM REMAINS OPEN AND CONTINUE TO LP 1779115 M7</P> / <P>LP 1779115 ITEM 7: CONTINUE T/S, REPLACED NOSE GEAR LOCK ACTUATOR AS PER 744 AMM 32-34-03/401 STILL NIL EFFECTIVATED, FURTHER T/S AND REPLACED NOSE LANDING GEAR OPERATED SEQUENCE VALVE AS PER 744 AMM 32-34-07/401.</P>)

Part: SEQUENCE VALVE — UNKNOWN · airframe 93,069 hrs · 15,704 cycles

LOG PAGE 1779113 ITEM # 2 NOSE GEAR FAIL TO FULLY RETRACT AND STOW.(<P>REF 744 AMM 32-34-08. PERFORMED TROUBLESHOOTING AND REPLACED NOSE GEAR DOOR OPERATED SEQUENCE VALVE AS PER 744 AMM 32-34-05/401, OPS CHECKED NIL EFFECTIVE. LP 1779115 ITEM #7: AMM 32-34-00/001 CONTINUE T/S &AMP; REPLACED NOSE GEAR LOCK ACTUATOR AS PER 744 AMM 32-34-03/401, STILL NIL EFFECTIVE. FURTHER T/S AND REPLACED NOSE LANDING GEAR OPERATED SEQUENCE VALVE AS PER 744 AMM 32-34-07/401. LOG PAGE ITEM #8: NOSE LANDING GEAR AND DOOR EXTENSION AND RETRACTION OPERATIONAL CHECKED GOOD AS PER 744 AMM 32-34-00/501. SYSTEM OKAY TO RETURN TO SERVICE.</P>)

Part: ACTUATOR — UNKNOWN · airframe 93,067 hrs · 15,701 cycles

ON GEAR RETRACTION EICAS GEAR INDICATOR WOULD GO FROM GEAR UP TO DOWN IN TRANSIT. SOUNDED LIKE NOSE GEAR AREA HAD GRINDING NOISE WHEN IN TRANSIT. CROSS HATCH DISPLAYED. TRIED CYCLING ONCE WITH SAME INDICATION. LEFT THE GEAR DOWN, DUMPED FUEL, AND RETURNED TO HKG. GOT GEAR MONITOR STS MSG WHILE DUMPING.(<P>REMOVED AND REPLACED NOSE LANDING GEAR RETRACT ACTUATOR PER AMM 32-34-01.&NBSP;</P>)

Part: NONE — NONE · airframe 90,541 hrs · 15,302 cycles

HYD PRESS SYS 1 STATUS MESSAGE(<P>PER FIM MESSAGE 29038, REPLACED #1 HYDIM CIRCUIT CARD A20 IAW AMM 29-11-42-004-001. OPS CHECK GOOD, NO FAULTS NOTED</P>)

Part: FIRE DETECTOR — WARNING MESSAGE · 15,093 cycles

FIRE MAIN DECK AFT EICAS WARNING MESSAGE INTERROGATED CMC. FOUND MAIN DECK ZONE 12 FIRE DETECTOR LOOP A& B FAIL. PERFORMED FIRE TEST IAW AMM 26-14-00/501. TEST PASSED. MESSAGE CLEARED, NO FAULTS PRESENT.

Part: HANDLE — FAULTY · airframe 88,851 hrs · 15,029 cycles

LANDING GEAR HANDLE WOULD ONLY MOVE UP WITH OVERIDE SWITCH TRANSFERRED TO MDDR 164088 IAW MEL 32-31-01, CAT C.

Part: FLOW SENSOR — INOPERATIVE · airframe 88,647 hrs

EQUIPMENT COOLING EICAS MSG CAME ON DURING CLIMB RAN CHECKLIST &AMP; MSG CAME BACK(<P>REMOVED / REPLACED FLIGHT DECK LOW FLOW DETECTOR IAW ATLAS AIR AMM 21-28-02</P>)

Part: SEAT TRACK — DAMAGED (BS 1800-1820) · 14,583 cycles

M/D STA 1780, 1800 AND 1820 LBL 77 SEAT TRACK CROWN FOUND DAMAGE(<P><SPAN>M/D STA 1750-1870 LBL 77 SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-6</SPAN></P>)

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · 14,583 cycles

MAIN DECK OVERDOOR EMERGENCY LIGHT FOUND INOP. MAIN DECK EMERGENCY LIGHT POWER SUPPLY BATTERY ( M5170 ) REPLACED AND OPERATIONAL TEST RESULT NORMAL AS PER AMM 33-51-04 REV 101,15 MAR 2021.

Part: SKIN — DELAMINATED (LT TE FLAP LE) · 14,583 cycles

LHW I/B FORE FLAP L/E COUNT FROM O/B 4.5FT FOUND DELAMINATED(<P><SPAN>CARRIED OUT COMPOSITE HOTBOND REPAIR&NBSP;</SPAN></P>)

Part: RIB — CRACKED (HORIZONTAL STAB) · 14,583 cycles

EMP - RH H/STAB TIP FAIRING #3, #4 RIB FOUND CRACK(<P><SPAN>EMP - RH RH H/STAB TIP FAIRING #3, #4 RIB CRACKED AREA REPAIRED AS PER SRM 55-10-09-R2-12</SPAN></P>)

Part: SKIN — DELAMINATED (LT TE FLAP LE) · 14,583 cycles

LHW I/B MID FLAP L/E COUNT FROM #4 FLAP TRACK TO O/B 3FT FOUND 1EA DELAMINATED(<P><SPAN>CARRIED OUT COMPOSITE HOTBOND REPAIR</SPAN></P>)

Part: GUIDE — CRACKED (BS 1900)

AFT CARGO L/H SIDE GUIDE RAIL AT STA 1900 AREA FOUND CRACK. AFT CARGO L/H SIDE GUIDE RAIL AT STA 1900 CRACK AREA REPAIRED AS PER RI-25-50-14871 REV A&NBSP;</SPAN></P>)

Part: SUPPORT CHANNEL — CRACKED (HORIZONTAL STAB) · 14,583 cycles

EMP-R/H HORIZONTAL STAB T/E WEDGE SUPPORT U CHANNEL FOUND CRACKED. REPLACE NEW CHANNEL WITH ADHESIVE FILM.

Part: SKIN — WORN (LT WING TE FLAP) · 14,583 cycles

LHW-O/B AFT FLAP O/B UPPER PANEL #588IT FOUND WORN AT 2 PREVIOUS REPAIR. CARRIED OUT METAL HOTBOND REPAIR.

Part: DOOR FRAME — DAMAGED (NLG DOOR AREA) · 14,583 cycles

NLG FWD L/R CORNER STA 240. DOUBLER INSTALL ( MOD ). NLG FWD L/R CORNER STA 240 L/R DOUBLER INSTALLED AS PER RI-53-00-14828 REV A</SPAN></P>)

Part: REVEAL — CRACKED (L5 DOOR FRAME) · 14,583 cycles

M/D #5L DOOR FWD CUTOUT REVEAL FOUND CRACK. M/D #5L DOOR FWD CUTOUT REVEAL CRACK AREA REPAIRED AS PER SRM 53-60-15-2R-7</SPAN></P>)

Part: SKIN — DENTED (BS 2595 S25-26R) · 14,583 cycles

EMP - TAIL JACK POINT SKIN FOUND DENT MARK ( STA 2595 S-25R TO S-26R ). EMP TAIL JACK POINT SKIN DENT AREA REWORKED AS PER RI-53-14813 REV A</SPAN></P>)

Part: ACTUATOR — MALFUNCTIONED (LT MLG STEERING) · 14,573 cycles

EICAS MESSAGES GEAR DISAGREE, GEAR TILT, GEAR DOOR, GEAR MONITOR, FLAP CONTROL, AND NO LAND 3.(<P>REPLACED LH BODY GEAR STEERING ACTUATOR, LH INBRD GEAR STOP AND BOTH BRACKETS. REPLACED LH INBRD AND OUTBRD WING GEAR DOORS. REPLACED LH BODY GEAR SHOCK STRUT. REPLACED UPPER AND LOWER TRAILING EDGE FLAP TORQUE TUBES. REPAIRED RH WING DOOR PUNCTURE. PER&NBSP;<SPAN>SRM 52-80-01-2R.</SPAN></P>)

Part: ENGINE — VIBRATION (NR 3) · airframe 82,105 hrs · 13,884 cycles

ENGINE NR 3 SHOWED FAN VIBRATION OF 5.0 UNITS AT LIFT OFF, NO VIBRATION FELT. PERFORMED VISUAL INSPECTION AND BORESCOPE, DEFECTS FOUND. REMOVED AND REPLACED ENGINE, IAW AMM 71-00-02/401.

Part: RELAY — MALFUNCTIONED (THRUST REVERSER) · airframe 81,881 hrs · 13,849 cycles

REJECTED TAKEOFF AT 35 KNOTS FOR ENGINE 2 REV STATUS MESSAGE REMAINED.DMI 133482 RAISED, MEL 78-31-01A APPLIED, CAT 'C'. MAINT PROCEDURES CARRIED OUT. R/R RELAY IAW AMM 78-36-07. OPS CHECK GOOD.

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 81,834 hrs · 13,842 cycles

GEAR TILT STATUS MESSAGE (REMOVED AND REPLACED RT BODY / GEAR ACTUATOR HYD IN HOSE ASSEMBLE).

Part: THRUST REVERSER — MALFUNCTIONED (NR 2 ENGINE) · airframe 78,514 hrs · 13,240 cycles

DURING TAKEOFF ROLL, EICAS ALERT, NR 2 ENGINE THRUST REVERSER MESSAGE. ABORTED TAKEOFF, APPROX 70 KNOTS INDICATED. CMC SHOWS ENG 2 REVERSER PRESSURE SW FAIL, MSG NO. 78353. APPLIED MEL 78-31-01A, CAT 'C', ACCOMPLISHED HIGH ENERGY STOP INSPECTION, NO DAMAGE FOUND IAW AMM 05-51-10-202-001.

Part: DOUBLER — DELAMINATED (TE FLAP) · airframe 78,243 hrs · 13,199 cycles

LT WING, O/B AFT FLAP, UPPER PNL, EXISTING REPAIR - DOUBLER FOUND DELAMINATED. PERFORMED PERMANENT REPAIR OF LT WING O/B AFT FLAP, UPPER O/B PANEL #588IT AS PER HX RI NR RI-57-00-13720 REV A.

Part: ACCESS PANEL — CHAFED (TE FLAP) · airframe 78,243 hrs · 13,199 cycles

LT WING O/B AFT FLAP, O/B ACCESS PANEL #588IT, FOUND DEEP CHAFING FROM O/B 15", AS MARKED. PERFORMED PERMANENT REPAIR OF LT WING O/B AFT FLAP, O/B ACCESS PANEL #588IT AS PER HX RI NR. RI-57-00-13720 REV A.

Part: ENGINE — NOT REPORTED (NR 3) · airframe 75,320 hrs · 12,685 cycles

RTO RUNWAY 25L, @ 80 KTS. DOUBLE POP ON #3 ENGINE, EGT 736 AT IDLE, TAXI TO THE GATE. OIL PRESSURE NORMAL.(<P>REMOVED AND REPLACED #3 ENGINE IAW EO WORK CARDS 71-099-02-01, LEAK AND RUN UP CHECKS WERE NORMAL</P>)

Part: SHAFT — SHEARED (OIL SCAV PUMP) · airframe 75,320 hrs · 12,685 cycles

#3 ENGINE OIL PRESSURE DECREASED TO 98 PSI IN FLIGHT, AND THEN 38 PSI AT IDLE. "ENG 3 OIL FILTER" EICAS MESSAGE. RAN QRH PROCEDURE, AND SHUT DOWN ENG 3.&NBSP;(<P>COMPLIED WITH POST WINDMILL INSPECTION IAW B747 AMM 72-00-00-206-059-J00, AND FIM TASK 71-00 A07 "ENG 3 OIL FILTER" MESSAGE. NO DEFECTS NOTED, PERFORMED ENGINE RUN PER 71-00-00-962-003-J00. OIL PRESSURE GOOD.&NBSP; &NBSP;ON NEXT ENGINE START PILOTS REPORTED NO OIL PRESSURE RISE. T/S AND FOUND&NBSP; #3 ENG LUBE AND SCAVENGE PUMP SHAFT SHEARED. REMOVED AND REPLACED PUMP IAW&NBSP; 79-21-03. DRAINED AND REPLACED ENGINE OIL, AND FLUSHED ACCESSORY GEARBOX. PERFORMED DRY MOTOR IDLE AND POWER RUN IAW B747 AMM 71-11-00. OIL PRESSURE GOOD.&NBSP;</P>)

Part: FLOORBEAM — CORRODED (BS 980) · corrosion level 2 · airframe 70,411 hrs · 11,774 cycles

CORROSION ON THE UPPER ANGLE OF MAIN DECK FLOORBEAM AT BS 980 NEAR LBL 85. ACCOMPLISH EI T2017A53M-1837, REV 2. CHECKED NORMAL.

Part: FITTING — CORRODED (BS 1500) · corrosion level 2 · airframe 70,411 hrs · 11,774 cycles

FOUND MAIN DECK FITTING CORRODED BS 1500, LBL 81. REPLACED THE FITTING IAW AMM 20-51-01-912-008, REV 90. CONDITION CHECKED NORMAL.

Part: PLATE — CORRODED (LT WING) · corrosion level 2 · airframe 70,411 hrs · 11,774 cycles

CORROSION ON PLATE LT WING L/E TO FRONT SPAR CAVITY AT OLES 1305.14. REMOVED THE DAMAGED PART IAW SRM 51-40-02, REV 80. INSTALLED THE PLATE IAW SRM 51-40-02, REV 80, AND DWG 65B11862 SH2, REV F 3. CONDITION CHECKED NORMAL.

Part: SEAT TRACK — BROKEN (BS 961-980) · airframe 70,411 hrs · 11,774 cycles

FOUND SEAT TRACK BROKEN AT BS 961, RBL 76.92 AND BS 980, RBL 75.92. REPAIRED IAW SRM 53-00-52-2R-13, REPAIR 13, REV 80. CONDITION CHECKED NORMAL.

Part: FLOORBEAM — CORRODED (BS 1500) · corrosion level 2 · airframe 70,411 hrs · 11,774 cycles

CORROSION ON THE FLOORBEAM UPPER ANGLE NEAR BS 1500, RBL 23. ACCOMPLISHED EI T2017A53M-1890, REV 1 & 2. CONDITION CHECKED NORMAL.

Part: FLOORBEAM — CORRODED (BS 460) · corrosion level 2 · airframe 70,411 hrs · 11,774 cycles

CORROSION ON THE FLOORBEAM UPPER ANGLE OF MAIN DECK CARGO AT BS 460, NEAR LBL 105. ACCOMPLISHED EI T2017A53M-1839, REV 2.

Part: SKIN — CORRODED (L5 DOOR) · corrosion level 2 · airframe 70,411 hrs · 11,774 cycles

CORROSION ON THE INNER SKIN UPPER OF LT SIDE NR 5 MAIN ENTRY DOOR. ACCOMPLISH EI T2017A52M-1879, REV 1. CONDITION CHECKED NORMAL.

Part: FITTING — CORRODED (BS 1640) · corrosion level 2 · airframe 70,411 hrs · 11,774 cycles

FOUND MAIN DECK FITTING CORRODED BS 1640, LBL 39.69. REPLACED THE FITTING IAW AMM 20-51-01-912-008, REV 90. CONDITION CHECKED NORMAL.

Part: BULKHEAD — DAMAGED (BS 2376) · airframe 70,411 hrs · 11,774 cycles

AFT PRESSURE BULKHEAD FWD FACE HAD ONE DENT AND A SCRATCH BS 2376, WL 212, LBL 65. REPAIRED IAW SRM 53-80-08, REPAIR 7, REV 80. CONDITION CHECKED NORMAL.

Part: SKIN — CORRODED (L5 DOOR) · corrosion level 2 · airframe 70,411 hrs · 11,774 cycles

CORROSION ON THE INNER SKIN UPPER OF L5 DOOR. ACCOMPLISHED EI T2017A52M-1879, REV 1.

Part: PLATE — CORRODED (LT WING) · corrosion level 2 · airframe 70,411 hrs · 11,774 cycles

CORROSION ON PLATE, LT WING L/E TO FRONT SPAR CAVITY AT OLES 1425.31. REMOVED DAMAGED PART IAW SRM 51-40-02, REV 80. INSTALLED THE PLATE IAW SRM 51-40-02, REV 80, AND DWG 65B11862, SH2, REV F. CONDITION CHECKED NORMAL.

Part: SKIN — NICKED (BS 1034) · airframe 70,411 hrs · 11,774 cycles

FOUND A NICK IN SKIN BETWEEN STRINGERS 6L & 7L, BS 1034. REPAIRED IAW SRM 53-00-01-2R-9, REV 80. CHECKED NORMAL.

Part: BRACKET — CORRODED (BS 920) · corrosion level 2 · airframe 70,411 hrs · 11,774 cycles

CORROSION ON THE SUPPORT BRACKET LOWER FUSELAGE WING TO BODY FAIRING BS 920, BL 0. REMOVED THE PART IAW SRM 51-40-02-0G-0, REV 80. INSTALLED A NEW PART IAW SRM 51-40-02-0G-0, REV 80, DWG 65B06704, SHEET 2, REV F, AND DWG 142U0130, SHEET 1, REV A3. CONDITION CHECKED NORMAL.

Part: FLOORBEAM — CORRODED (BS 460) · corrosion level 2 · airframe 70,411 hrs · 11,774 cycles

CORROSION ON THE FLOORBEAM UPPER ANGLE OF MAIN DECK CARGO AT BS 460, NEAR LBL 105. ACCOMPLISHED EI T2017A53M-1839, REV 2. CONDITION CHECKED NORMAL.

Part: FLOORBEAM — CORRODED (BS 2100) · corrosion level 2 · airframe 70,411 hrs · 11,774 cycles

FOUND FLOORBEAM CORRODED AT BS 2100, LBL 86.67. REPAIRED IAW SRM 53-00-51-2R-3, REPAIR 3, REV 80, DWG 65B38105, SHEET 10, REV -, AND DWG 65B21441, SHEET 8, REV C. CHECKED NORMAL.

Part: SEAT TRACK — BROKEN (BS 984) · airframe 70,411 hrs · 11,774 cycles

FOUND SEAT TRACK CRACKED AT BS 984 LBL 76.92. REPAIRED IAW SRM 53-00-52-2R-13, REPAIR 13, REV 80. CONDITION CHECKED NORMAL.

Part: SEAT TRACK — BROKEN (BS 1485) · airframe 70,411 hrs · 11,774 cycles

FOUND SEAT TRACK BROKEN AT BS 1485, RBL 75.92. REPAIRED IAW SRM 53-00-52-2R-13, REPAIR 13, REV 80. CONDITION CHECKED NORMAL.

Part: FITTING — CORRODED (BS 2060) · corrosion level 2 · airframe 70,411 hrs · 11,774 cycles

FOUND MAIN DECK FITTING CORRODED BS 2060, LBL 81. REPLACED THE FITTING IAW AMM 20-51-01-912-008, REV 90. CONDITION CHECKED NORMAL.

Part: SEAT TRACK — BROKEN (BS 1523) · airframe 70,411 hrs · 11,774 cycles

FOUND SEAT TRACK BROKEN AT BS 1523, LBL 77. REPAIRED AREA IAW SRM 53-00-52-2R-13, REPAIR 13, REV 80. CONDITION CHECKED NORMAL.

Part: LINE — LEAKING (OIL SYSTEM) · airframe 67,885 hrs · 11,334 cycles

EICAS MESSAGE NR 3 ENG OIL PRESSURE, QUANTITY READ ZERO. INSPECTED AND FOUND THAT OIL LEAK FROM THE NR 3 ENG MAIN FUEL PUMP DRAIN LINE. SERVICED THE OIL SYS AND CAPPED MAIN FUEL PUMP DRAIN LINE THEN NO OIL LEAK NOTED AND OIL QTY NORMAL AFTER ENG RUN CHECK IAW AMM 71-71-00/601. PERFORMED NR 3 ENG RUN CHECK AND OIL PRESSURE INDICATION CHECKED OK IAW AMM 79-32-00/501, AND AMM 71-00-00/501.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 67,005 hrs · 11,181 cycles

AFTER TAKEOFF, CREW OBSERVED STEADY HYDRAULIC FLUID LOSS IN SYSTEM NR 4. HYDRAULIC LOSS CONTINUED TO .67 WITH SYS DEPRESSURIZED. AFTER INSPECTION , MAINTENANCE NOTED NO FLUID LOSS IN NR 4 SYSTEM. QTY WAS FULL AFTER ACFT LANDED. MAINTENANCE FOUND THE PNEUMATIC HEAD PRESSURE LINE TO THE NR 4 RESERVOIR LEAKING. THE LINE WAS REPLACED AND THE NR 4 HYD QTY INDICATION FOR THE NR 4 SYS WAS DEFERRED. A NEW QTY TRANSMITTER WAS ORDERED FOR THIS.

Part: WARNING MESSAGE — ACTIVATED (THRUST REVERSER) · airframe 65,982 hrs · 10,983 cycles

LOW SPEED REJECT DUE TO ENGINE 2 REVERSER EICAS APPPLIED MEL 78-31-01A. CAT "C". MAINTENANCE PROCEDURE COMPLETED.

Part: ESCAPE REEL — DAMAGED (COCKPIT) · airframe 64,232 hrs · 10,642 cycles

COCKPIT DESCENT DEVICE NR 4 HAS CABLE EXTENDED. R & R NR 4 COCKPIT DESCENT DEVICE IAW AMM 25-61-01.

Part: ESCAPE REEL — DAMAGED (COCKPIT) · airframe 64,232 hrs · 10,642 cycles

COCKPIT DESCENT DEVICE NR 6 HAS CABLE EXTENDED. R & R COCKPIT DESCENT DEVICE IAW AMM 25-61-01.

Part: ESCAPE REEL — DAMAGED (COCKPIT) · airframe 64,232 hrs · 10,642 cycles

COCKPIT DESCENT DEVICE NR 8 HAS CABLE EXTENDED. R & R COCKPIT DESCENT DEVICE IAW AMM 25-61-01.

Part: ESCAPE REEL — DAMAGED (COCKPIT) · airframe 64,232 hrs · 10,642 cycles

COCKPIT DESCENT DEVICE NR 5 HAS CABLE EXTENDED. R & R DESCENT DEVICE IAW AMM 25-61-01.

Part: ESCAPE REEL — DAMAGED (COCKPIT) · airframe 64,232 hrs · 10,642 cycles

COCKPIT DESCENT DEVICE NR 7 HAS CABLE EXTENDED. R & R NR 7 DESCENT DEVICE IAW 25-61-01.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 63,511 hrs · 10,518 cycles

ODOR FROM INSIDE COCKPIT, LIKE VINYL BURNED. INSPECTED INSIDE, E1, E2 RACK BOTH SIDE TUNNEL, SUPPLY FAN, EXHAUST FAN, INSIDE COCKPIT, INSIDE LT PFD AND RT PFD, UPPER AND LOWER EICAS ALL CDU OK IAW MM 05-51-56-200-801, ENGINE RUN CHECKED IAW MM 71-00-00-862-003.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 62,914 hrs · 10,416 cycles

LEFT WING - NR 6 SPOILER ACTUATOR SUPPORT FITTING FOUND CRACKED AT OTBD LOWER FLANGE, LT WING - NR 6 SPOILER ACTUATOR SUPPORT FITTING OTBD LOWER FLANGE CRACK AREA REPAIRED IAW SRM 57-51-13-2R-1, REPAIR 1.

Part: SKIN — DENTED (MLG DOOR) · airframe 62,914 hrs · 10,416 cycles

RIGHT MLG INBD AFT STRUT DOOR EXTERNAL OUTER SKIN FOUND DENT, RT BLG INBD AFT STRUT DOOR EXTERNAL OUTER SKIN DENT AREAS AND DAMAGED RIB REPAIRED IAW R1-52-80-11002, REV B.

Part: PANEL — DAMAGED (NR 3 NACELLE) · airframe 62,914 hrs · 10,416 cycles

NR 3 PYLON, RT EXHAUST NOZZLE UPPER SKIRT PANEL 1 EA HOLE FOUND ELONGATED, NR 3 PYLON RT SKIRT FAIRING SKIN ELONGATED FASTENER HOLE REPAIRED IAW R1-54-50-11007.

Part: FRAME — DAMAGED (NR 2 NACELLE) · airframe 62,914 hrs · 10,416 cycles

NR 2 ENGINE LT CORE COWL FRAME HOLD OPEN ROD BRACKET MOUNT HOLE 3 EA ELONGATED. NR 2 ENGINE LT CORE COWL FRAME HOLD OPEN ROD BRACKET, MOUNT HOLE ELONGATED AREAS. REPAIRED IAW SRM 51-70-11: EO 4471A153, REV 0.

Part: SHEAR TIE — CRACKED (BS 980) · airframe 62,914 hrs · 10,416 cycles

FWD CARGO -BS 980, STR 37R -STR 38R FWD FRAME SHEAR TIE FOUND CRACKED AT RADIUS, FWD CARGO COMPARTMENT BS 980 RIGHT BETWEEN STR 37R TO STR 38R FRAME SHEAR TIE IS REPAIRED IAW R1: R1-53-22-11018.

Part: HINGE FITTING — CRACKED (NR 7 SPOILER) · airframe 62,914 hrs · 10,416 cycles

RT WING REAR SPAR NR 7 SPOILER MID HINGE FITTING OTBD LOWER 3EA RIVET HEAD CRACKED. RT WING REAR SPAR NR 7 SPOILER ACTUATOR SUPPORT FITTING CRACKED AREA REPAIRED IAW R1-57-51-11009.

Part: ACCESS PANEL — CHAFED (NR 3 NACELLE) · airframe 62,914 hrs · 10,416 cycles

NR 3 PYLON, ACCESS PANEL NR 472ER, 2EA FASTENER HOLES FOUND CHAFED. NR 3 PYLON - ACCESS PANEL NR 472ER, 2EA DAMAGED HOLE REPAIRED IAW R1-54-57-11016, REV A.

Part: DOOR SILL — CRACKED (BS 1850) · airframe 62,914 hrs · 10,416 cycles

SCD FWD DOOR SILL FOUND CRACKED, M/D-SCD FWD DOOR SILL WALKWAY PANEL CRACKED AREA, REPAIRED IAW R1-25-55-10998.

Part: SUPPORT BEAM — CHAFED (NR 1 NACELLE) · airframe 62,914 hrs · 10,416 cycles

NR 1 PYLON, NR 3 FAN COWL SUPPORT BEAM RT LOWER SURFACE FOUND DEEP CHAFING, NR 1 PYLON, NR 3 FAN COWL SUPPORT BEAM, RT LOWER SURFACE DEEP CHAFING AREAS REPAIRED IAW R1-54-50-11008.

Part: CHANNEL — CRACKED (BS 760) · airframe 62,914 hrs · 10,416 cycles

U/D BS 760 RT TENSION TIE AFT CHANNEL, 2 EA FASTENER HOLES FOUND CRACK. U/D BS 760, RT TENSION TIE FWD CHANNEL AND AFT CHANNEL CRACK AREAS REPAIRED IAW SRM 53-20-30-2R-1 REPAIR 1. THIS REPAIR IS CLASSIFIED AS A CATEGORY B REPAIR.

Part: DOOR SILL — CRACKED (BS 1862-1867) · airframe 62,914 hrs · 10,416 cycles

AFT DOOR SILL FOUND CRACK, M/D SIDE CARGO AFT DOOR SILL PANEL CRACK AREAS REPAIRED IAW R1-25-55-10997.

Part: CHANNEL — CRACKED (BS 760) · airframe 62,914 hrs · 10,416 cycles

U/D BS 760, LT TENSION TIE FWD CHANNEL 1 EA FASTENER HOLES FOUND CRACKED IN 6 AND 12 O/C POSITION, BOTH 0.030" LENGTH. U/D BS 760, LT TENSION TIE FWD CHANNEL AND AFT CHANNEL CRACK AREAS REPAIRED IAW SRM 53-20-30-2R-1, REPAIR. THIS REPAIR IS CLASSIFIED AS A CATEGORY B REPAIR.

Part: CHANNEL — CRACKED (BS 720) · airframe 62,914 hrs · 10,416 cycles

U/D BS 720, LT TENSION TIE FWD CHANNEL CRACKED AT RADIUS APPROXIMATELY 0.375" LONG. U/D BS 720, LT TENSION TIE FWD CHANNEL AND AFT CHANNEL CRACK AREAS. REPAIRED IAW SRM 53-20-30-2R-1, REPAIR 1. THIS REPAIR IS CLASSIFIED AS A CATEGORY B REPAIR.

Part: SKIN — CRACKED (RT WING) · airframe 62,914 hrs · 10,416 cycles

RIGHT WING LOWER L/E TIP AT NR 15 K-FLAP OTBD ARM CUTOUT FOUND CRACK, RT WING L/E INBD ILES 514 HOSE BEAM LOWER BEAM CRACK AREA REPAIRED IAW R1-57-41-11011.

Part: SKIN — CRACKED (BS 939-991) · airframe 62,914 hrs · 10,416 cycles

RT SIDE BS 980 DRAG SPLICE LOWER FITTING AT STR 38R CRACK FOUND ON SKIN LAYER UNDER FITTING, CRACK RUNNING DOWNWARD AT 6 O'CLOCK POSITION THROUGH THICKNESS, FUSELAGE SKIN IS REPAIRED IAW SRM 53-20-01-2R-2. REPAIR 2 AT BS 939.5 TO 991.5 BETWEEN STR 37R-39R AREA. THIS REPAIR IS CLASSIFIED AS A CATEGORY B REPAIR.

Part: CHANNEL — CRACKED (BS 720) · airframe 62,914 hrs · 10,416 cycles

U/D BS 720 RT TENSION TIE FWD CHANNEL CRACKED AT RADIUS APPROX 0.375" LONG. U/D BS 720 RT TENSION TIE FWD CHANNEL AND AFT CHANNEL CRACK AREAS REPAIRED IAW SRM 53-20-30-2R-1, REPAIR 1. THIS REPAIR IS CLASSIFIED AS A CATEGORY B.

Part: ACCESS PANEL — CHAFED (NR 3 NACELLE) · airframe 62,914 hrs · 10,416 cycles

NR 3 PYLON, ACCESS PANEL NR 472EL, 2EA FASTENER HOLES FOUND CHAFED. NR 3 PYLON, ACCESS PANEL NR 472EL DAMAGED. FASTENER HOLES REPAIRED IAW R1-54-57-11017, REV A.

Part: ACTUATOR — BROKEN (LT MLG) · airframe 61,163 hrs · 10,133 cycles

ON POST FLIGHT WALK AROUND, FOUND LT WING LANDING GEAR TRUCK POSITION ACTUATOR BROKEN AT BOTH ENDS. R & R LT WING GEAR TRUCK POSITION ACTUATOR IAW AMM 32-11-20-404-010.

Part: OVEN — FAILED (GALLEY) · airframe 61,161 hrs · 10,132 cycles

OVEN CONTROL PANEL HOT WITH C/B PULLED. ODOR OF BURNED PLASTIC. PERFORMED OVEN OPS CHECK AND CHECKED OK. NO PLASTIC ODOR IAW AMM 25-32-00. ACCOMPLISHED CONDITIONAL INSPECTION IAW AMM 05-51-56. NO OTHER ITEMS FOUND.

Part: CONNECTOR — BURNED (RUDDER) · airframe 56,805 hrs · 9,446 cycles

RUDDER RATIO STATUS MESSAGE AND RUDDER RATIO SINGLE ADVISORY MESSAGE APPEARED DURING TRANSIT CHECK. TROUBLESHOOTING FOUND E1-2 SHELF WIU 1420 CONNECTOR D1288A PINS; A1 AND A2 BURNED. RELOCATED PINS TO A6 AND A7 OF SAME CONNECTOR IAW EO 4424A053, REV 0. RUDDER RATIO SYSTEM OPS CHECK NORMAL IAW AMM 27-21-00.

Part: WIRE — BURNED · airframe 56,805 hrs · 9,446 cycles

RUDDER RATIO STATUS MESSAGE AND RUDDER RATIO SINGLE ADVISORY MESSAGE APPEARED DURING TRANSIT CHECK. CIRCUIT BREAKER FOR THE RUDDER RATIO CHANGER CONTROL WAS FOUND TO BE TRIPPED AND WOULD NOT RESET. FURTHER INVESTIGATION FOUND WIRES AND POSTS IN THE WIRE INTEGRATION UNIT (WIU) WERE FOUND BURNED.

Part: STRUCTURE — CRACKED (BS 1220) · airframe 54,857 hrs · 9,038 cycles

BS 1220, RBL 110 BELOW FLOOR INTERCOASTAL WEB, FOUND CRACKED. REPAIRED IAW SRM 53-40-51-2R-5, REPAIR 5.

Part: INTERCOSTAL — CRACKED (BS 1180) · airframe 54,857 hrs · 9,038 cycles

BS 1180, RBL 107 INTERCOSTAL WEB CRACKED. INTERCOSTAL WEB REPLACED.

Part: INTERCOSTAL — CRACKED (BS 1200) · airframe 54,857 hrs · 9,038 cycles

BS 1200, RBL 107, INTERCOSTAL WEB CRACKED. INTERCOSTAL WEB REPLACED.

Part: ROLLER — CRACKED (RT WING TE FLAP) · airframe 54,857 hrs · 9,038 cycles

RT WING INBD MID FLAP, ONE ROLLER PLATE FOUND CRACKED AT UPPER RADIUS AT WBL 164.6. ROLLER PLATE REPLACED IAW SRM 51-10-02 AND SRM 51-40-02 AND EO NR: 1927A123, PART 8.

Part: INTERCOSTAL — CRACKED (BS 1180) · airframe 54,857 hrs · 9,038 cycles

M/D BS 1180, RBL 107 INTERCOSTAL CRACKED. INTERCOSTAL REPLACED.

Part: RETAINER — DAMAGED (LT WING PYLON) · airframe 54,857 hrs · 9,038 cycles

LEFT WING NR 2 PYLON UPPER L/E ILES 652.37 NOSE SKIN AND SEAL RETAINER NEAR SEVERAL FASTNER HOLES FOUND ELONGATED. REPAIRED IAW R1 NO: R1-57-41-10275, REV A.

Part: INTERCOSTAL — CRACKED (BS 1200) · airframe 54,857 hrs · 9,038 cycles

BS 1200, RBL 107 INTERCOSTAL WEB CRACKED. INTERCOSTAL WEB REPLACED IAW RI NO: R1-53-41-10274, REV A.

Part: STRUCTURE — CRACKED (BS 1220) · airframe 54,857 hrs · 9,038 cycles

BS 1220, LBL 110 BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-51-2R- 5, REPAIR 5.

Part: ACTUATOR — FAILED (CABIN PRESSURE) · airframe 53,962 hrs · 8,888 cycles

AIRCRAFT WOULD NOT HOLD PRESSURIZATION. PERFORMED OUTFLOW VALVE L, R QRH ITEMS TO NO AVAIL. REMOVED AND REPLACED LEFT OUTFLOW VALVE ACTUATOR AS PER AMM 21-21-07. OPERATIONAL CHECK GOOD AS PER AMM 21-31-07.

Part: CONTROL UNIT — FAILED (CABIN PRESSURE) · airframe 53,962 hrs · 8,888 cycles

AIRCRAFT WOULD NOT HOLD PRESSURIZATION. PERFORMED OUTFLOW VALVE LEFT AND RIGHT QRH ITEMS TO NO AVAIL. REMOVED AND REPLACED LEFT OUTFLOW VALVE INTERFACE CONTROL UNIT AS PER AMM 21-31-10. OPERATIONAL CHECK GOOD AS PER AMM 21-31-10.

Part: SIDEWALL PANEL — DAMAGED (MAIN CARGO BAY) · airframe 52,663 hrs · 8,662 cycles

DURING MAINTENANCE WALKAROUND IN NRT, MAINTENANCE FOUND THE MAIN DECK - RIGHT BS 1710 SIDEWALL PANEL DAMAGED; TEAR 14.0 INCHES LONG X 5.0 INCHES WIDE. AS PER AMM 25-52-01-308-062, THE DAMAGE EXCEEDS THE REPAIR LIMITS. DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS (IN ACCORDANCE WITH THE AMM 25-59-01-206-001).

Part: SEAL DEPRESSOR — DAMAGED (FUSELAGE) · airframe 52,030 hrs · 8,537 cycles

DAMAGE TO THE LOWER LOBE - FWD CARGO DOOR - BS 670 SEAL DEPRESSOR FOUND MEASURING 0.280 IN. X 0.250 IN. AND LOCATED 3.0 INCHES FORM THE SEAL DEPRESSOR SPLICE AREA. DAMAGE WAS DETERMINED TO BE BEYOND THE REPAIR LIMITS IN ACCORDANCE WITH THE SRM 53-00-15, FIGURE 201, REPAIR 2. (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 OF EO 4453A789, FAA 8110-3 DATED 12NOV12 AND TO SCHEDULE REPEAT INSPECTIONS AT EVERY 5 FC AND PERMANENT REPAIR PRIOR TO THE ACCUMULATION OF 1,000 (FLIGHT HOURS) AFTER PART 1.)

Part: HINGE — CORRODED (FUSELAGE) · airframe 51,982 hrs · 8,530 cycles

DURING WALKAROUND INSPECTION IN PVG, A/C ACCESS PANEL HINGE FOUND WITH CORROSION DAMAGE. TIME LIMITED REPAIR ACCOMPLISHED PER EO 4453A785. REPEAT INSPECTIONS EVERY FLIGHT CYCLE. PERMANENT REPAIR REQUIRED PRIOR TO THE ACCUMALATION OF 25FLIGHT CYCLES.

Part: TRIM PANEL — DAMAGED (MAIN CARGO BAY) · airframe 51,653 hrs · 8,474 cycles

DAMAGE FOUND TO MAIN DECK SIDE CARGO DOOR AREA AT & NBSP; BS 1780 SIDEWALL TRIM/GUTTER.

Part: OIL SYSTEM — LOW (NR 1 ENGINE) · airframe 50,719 hrs · 8,289 cycles

SHUTDOWN NR 1 ENGINE AS A PRECAUTION DUE TO LOW OIL QUANTITY. TWO QUARTS REMAINED. SHUTDOWN TIME 16:40Z. FIRE SWITCH NOT PULLED. REMOVED AND REPLACED ENGINE 1 IDG BLANKING PLATE AND PLUG. SERVICED ENGINE IAW AMM 12-13-03. POST WINDMILL INSPECTION IAW 72-00-00 COMPLETED AND NO ISSUES.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,586 hrs · 8,266 cycles

CREW REST COMPARTMENT EMERGENCY LIGHT INOPERATIVE, DEFECTIVE LIGHT BULB. REPLACED AND OPERATIONAL TESTED NORMAL.

Part: LENS — BROKEN (CABIN) · airframe 49,750 hrs · 8,121 cycles

FOUND LT OUTBD&NBSP; LANDING LIGHT LENS WAS BROKEN. (ACCOMPLISHED TIME LIMITED REPAIR PER&NBSP;EO 4433A034 AS DESCRIBED IN PART 1 WORK INSTRUCTIONS.&NBSP; PART 2 INSPECTION REQUIRED EVERY FLIGHT. PERMANENT REPAIR BY REPLACING THE DAMAGED LENS COVER ASSY PRIOR TO THE ACCUMULATION OF 25 FLIGHT CYCLES IS REQUIRED).

Part: PIN — DEFECTIVE (WIU) · airframe 47,918 hrs · 7,838 cycles

ELECTRIC FLIGHT CONTROLS {PSM} LEFT 2 AC, DC CIRCUIT BREAKERS FOUND&NBSP; POPPED AND WILL NOT RESET. NON-FDE CMC MSG 27506A NOTED. (PRELIMINARY INSPECTION FOUND WIRE WRAP PINS 15A AND 15E OF WIU TO BE MAKING CONTACT. CONTACT CAUSED THE RECEPTACLE TO DISCOLOR. REPLACEMENT OF AFFECTED PARTS IN PROGRESS. SUPPLEMENTAL TO THIS SDR WILL BE SUBMITTED ONCE JOB IS COMPLETE.)

Part: RIB — CRACKED (HORIZ STAB) · airframe 47,181 hrs · 7,713 cycles

THE TOP OF RIB AT STATION 151.548 OF THE LEADING EDGE OF THE LEFT HORIZONTAL STABILIZER IS CRACKED. REPAIRED RIB IAW EI T2011A55B-1968 REV 1. NO FURTHER ACTION REQUIRED.

Part: RIB — CRACKED (HORIZ STAB) · airframe 47,181 hrs · 7,713 cycles

RIB AT STATION 510.103 OF THE LEADING EDGE OF THE RIGHT HORIZONTAL STABILIZER IS CRACKED. RIB REPAIRED IAW EI T2011A55B-1964 REV 1. NO FURTHER ACTION REQUIRED.

Part: RIB — CRACKED (HORIZ STAB) · airframe 47,181 hrs · 7,713 cycles

LOWER SIDE OF RIB AT STATION 510.103 OF THE LEADING EDGE OF THE LEFT HORIZONTAL STABILIZER IS CRACKED. REPAIRED RIB IAW EI T2011A55B-1964 REV 1. NO FURTHER ACTION REQUIRED.

Part: RIB — CRACKED (HORIZ STAB) · airframe 47,181 hrs · 7,713 cycles

RIB AT STATION 433.210 OF LEADING EDGE OF LEFT HORIZONTAL STABILIZER IS CRACKED. REPAIRED RIB IAW EI T2011A55B-1954 REV 1. NO FURTHER ACTION REQUIRED.

Part: RIB — CRACKED (HORIZ STAB) · airframe 47,181 hrs · 7,713 cycles

RIB AT STATION 159.109 OF THE LEADING EDGE OF THE RIGHT HORIZONTAL STABILIZER IS CRACKED. REPAIRED RIB IAW EI T2011A55B-1971 REV 1. NO FURTHER ACTION IS REQUIRED.

Part: RIB — CRACKED (HORIZ STAB) · airframe 47,181 hrs · 7,713 cycles

RIB AT STATION 138.478 OF THE LEADING EDGE OF THE LEFT HORIZONTAL STABILIZER IS CRACKED. REPAIRED RIB IAW EI T2011A55B-1967 REV 1. NO FURTHER ACTION REQUIRED.

Part: RIB — CRACKED (HORIZ STAB) · airframe 47,181 hrs · 7,713 cycles

RIB AT STATION 527.190 OF THE LEADING EDGE OF THE RIGHT HORIZONTAL STABILIZER IS CRACKED. REPAIRED RIB IAW EI T2011A55B-1966 REV 1. NO FURTHER ACTION REQUIRED.

Part: RIB — CRACKED (HORIZ STAB) · airframe 47,181 hrs · 7,713 cycles

RIB AT STATION 467.384 OF THE LEADING EDGE OF THE RIGHT HORIZONTAL STABILIZER IS CRACKED. REPAIRED RIB IAW EI T2011-158 REV 1. NO FURTHER ACTION REQUIRED.

Part: RIB — CRACKED (HORIZ STAB) · airframe 47,181 hrs · 7,713 cycles

THE TOP SIDE OF THE RIB AT STATION 501.559 OF THE LEFT HORIZONTAL STABILIZER IS CRACKED. REPAIRED RIB IAW EI T2011A55B-1960 REV 1. NO FURTHER ACTION REQUIRED.

Part: RIB — CRACKED (HORIZ STAB) · airframe 47,181 hrs · 7,713 cycles

TOP SIDE OF RIB AT STATION 510.103 OF THE LEADING EDGE OF THE LEFT HORIZONTAL STABILIZER IS CRACKED. REPAIRED RIB IAW EI T2011A55B-162 REV 1. NO FURTHER ACTION REQUIRED.

Part: RIB — CRACKED (HORIZ STAB) · airframe 47,181 hrs · 7,713 cycles

RIB AT STATION 131.946 IF THE LEADING EDGE OF THE LEFT HORIZONTAL STABILIZER IS CRACKED. REPAIRED RIB IAW EI T2011A55B-1972 REV 1. NO FURTHER ACTION REQUIRED.

Part: RIB — CRACKED (HORIZ STAB) · airframe 47,181 hrs · 7,713 cycles

RIB AT STATION 518.646 OF THE LEADING EDGE OF THE RIGHT HORIZONTAL STABILIZER IS CRACKED. REPAIRED RIB IAW EI T2011A55B-1965 REV 1. NO FURTHER ACTION REQUIRED.

Part: RIB — CRACKED (HORIZ STAB) · airframe 47,181 hrs · 7,713 cycles

RIB AT STATION 159.109 OF THE LEADING EDGE OF THE LEFT HORIZONTAL STABLIZER IS CRACKED. REPAIRED RIB IAW EI T2011A55B-170 REV 1. NO FURTHER ACTION REQUIRED.

Part: RIB — CRACKED (HORIZ STAB) · airframe 47,181 hrs · 7,713 cycles

BOTTOM OF RIB AT STATION 501.559 OF THE LEADING EDGE OF THE LEFT HORIZONTAL STABILIZER IS CRACKED. REPAIRED RIB IAW EI T2011A55B-161 REV 1. NO FURTHER ACTION REQUIRED.

Part: RIB — CRACKED (HORIZ STAB) · airframe 47,181 hrs · 7,713 cycles

RIB AT STATION 458.841 OF THE LEADING EDGE OF THE RIGHT HORIZONTAL STABILIZER IS CRACKED. REPAIRED RIB IAW EI T2011A55B-157 REV 1. NO FURTHER ACTION REQUIRED.

Part: RIB — CRACKED (HORIZ STAB) · airframe 47,181 hrs · 7,713 cycles

RIB AT STATION 458.841 OF THE LEADING EDGE OF THE LEFT HORIZONTAL STABILIZER IS CRACKED. REPAIRED RIB IAW EI T2011A55B-1956 REV 1. NO FURTHER ACTION REQUIRED.

Part: RIB — CRACKED (HORIZ STAB) · airframe 47,181 hrs · 7,713 cycles

RIB AT STATION 501.559 OF THE LEADING EDGE OF THE RIGHT HORIZONTAL STABILIZER IS CRACKED. REPAIRED RIB IAW EI T2011A55B-159 REV 1. NO FURTHER ACTION REQUIRED.

Part: RIB — CRACKED (HORIZ STAB) · airframe 47,181 hrs · 7,713 cycles

RIB AT STATION 450.297 OF THE LEADING EDGE OF THE RIGHT HORIZONTAL STABILIZER IS CRACKED. REPAIRED IAW EI T2011A55B-1955 REV 1. NO FURTHER ACTION REQUIRED.

Part: RIB — CRACKED (HORIZ STAB) · airframe 47,181 hrs · 7,713 cycles

LOWER PART OF RIB AT STATION 151.548 OF THE LEADING EDGE OF THE LEFT HORIZONTAL STABILIZER IS CRACKED. REPAIRED RIB IAW EI T2011A55B-169 REV 1. NO FURTHER ACTION REQUIRED.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 47,677 hrs · 7,801 cycles

LOWER AFT CARGO COMPARTMENT AT STA 1880 R/S HAS 7 INCH CRACK ON SEAT TRACK. IAW EO 4453A656 PART 1 A TIME LIMITED REPAIR WAS ACCOMPLISHED WITH PART 2, A REPETATIVE INSPECTION EVERY 5 CYCLES AND PART 3 PERMANENT REPAIR TO BE ACCOMPLISHED A NEXT A CHECK.

Part: BLOWOUT DOOR — WORN (THRUST REVERSER) · airframe 47,181 hrs · 7,713 cycles

BLOW OUT DOOR AT 6 O`CLOCK POSITION ON NR 2 ENGINE, RIGHT THRUST REVERSER IS WORN ON THE LEADING & NBSP; AND THE TRAILING EDGES. REPAIR ACCOMPLISHED TO BOTH EDGES AS PER EO 4478A191.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 47,181 hrs · 7,713 cycles

MAIN DECK SEAT TRACK & NBSP; AT STATION & NBSP; 997 RBL 75.92 HAS A 1 INCH CRACK. REPAIR ACCOMPLISHED AS PER SRM 53-00-52 REPAIR 13 REV 60.

Part: REVEAL — CRACKED (CABIN) · airframe 47,181 hrs · 7,713 cycles

PANEL REVEAL OF L1 ENTRY DOOR SURROUND STRUCTURE AT STATION 440 WL 213 HAS A .35 INCH CRACK. ACCOMPLISHED REPAIR AS PER EIT2011A53B-1931.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,181 hrs · 7,713 cycles

EXFOLIATION CORROSION (LEVEL 2) WAS FOUND ON DOUBLER ON LOWER FUSELAGE SKIN AROUND WATER FILL CONNECTION AT BS 983, RBL 17. AFFECTED DOUBLER WAS REPLACED AS PER EI T2011P53B-2052.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 47,181 hrs · 7,713 cycles

MAIN DECK SEAT TRACK IS WORN BEYOND LIMITS AT STATION 1650 RBL 11.33. ACCOMPLISHED REPAIR AS PER EI T2011A53B-2046 REV 1.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 47,181 hrs · 7,713 cycles

LOWER EDGE OF MAIN DECK SIDE CARGO DOOR AT & NBSP;STATION 1803 WL 193 HAS GOUGE AND & NBSP; DEFORM DAMAGE ON OUTER SKIN. THE DAMAGE IS OVER & NBSP; SRM LIMITS & NBSP. ACCOMPLISHED REPAIR AS PER EI T2011A52B-2001 REV 1.

Part: PANEL — BROKEN (MAIN DECK) · airframe 47,181 hrs · 7,713 cycles

AFT CORNER OF MAIN DECK DADO PANEL AT LEFT STATION 1720 IS BROKEN. ACCOMPLISHED REPAIR AS PER EI T2011A25B02003.

Part: SLEEVE — DENTED (NR 4 EXHAUST) · airframe 47,181 hrs · 7,713 cycles

OUTER SURFACE OF NR 4 ENGINE EXHAUST SLEEVE HAS 5 DENTS THAT ARE OVER SRM LIMITS. ACCOMPLISHED REPAIR AS PER EI T2011A54B-1994 REV 1.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,181 hrs · 7,713 cycles

EMERGENCY LIGHT BATTERIES EQUIPMENT NUMBERS M5169 & AMP; M5170 ARE & NBSP; INOPERATIVE. BOTH BATTERY PACKS REPLACED IAW AMM 33-51-04-902-001-001 REV 72. BOTH TESTED NORMAL.

Part: FAIRING — WORN (LT COWLING) · airframe 47,181 hrs · 7,713 cycles

NR 2 ENGINE LEFT CORE COWL'S TITANIUM FAIRING HAS WEAR DAMAGE THAT IS OUT OF SRM LIMITS. ACCOMPLISHED REPAIR AS PER EO 4478A192.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 47,181 hrs · 7,713 cycles

MAIN DECK SUBSTITUTE SEAT TRACK AT STATION 1970 LBL 75.92 HAS A 2 INCH CRACK. ACCOMPLISHED REPAIR AS PER SRM 53-00-52 REPAIR 13 REV 60.

Part: DOOR — DAMAGED (CARGO BAY) · airframe 47,181 hrs · 7,713 cycles

AFT LOWER EDGE OF LOWER AFT CARGO & NBSP; DOOR AT STATION 1915 HAS MINOR DEFORMATION DAMAGE & NBSP. REPAIR ACCOMPLISHED AS PER EI T2011A52B REV 2.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 47,181 hrs · 7,713 cycles

MAIN DECK SEAT TRACK AT STATION 995 LBL 75.92 HAS A 1.5 INCH CRACK. ACCOMPLISHED REPAIR AS PER SRM 53-00-52 REPAIR 13 REV 60.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 47,181 hrs · 7,713 cycles

INTERCOSTAL OF MAIN DECK FLOORING AT STATION 990.5 RBL 99 WL 200 IS CRACKED. ACCOMPLISHED REPAIR AS PER EI T2011A53B-2035 REV 1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 47,181 hrs · 7,713 cycles

THE INTERCOSTAL OF THE BULK CARGO FLOOR STRUCTURE AT STATION 2060 TO & NBSP; 2080 LBL 29.375 HAS 2 CRACKS EACH AT .5 INCH. ACCOMPLISHED REPAIR AS PER EI T2011A53B-2011 REV 1.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 47,181 hrs · 7,713 cycles

MAIN DECK SEAT TRACK WORN BEYOND LIMITS AT STATION 1855 LBL 11.33. ACCOMPLISHED REPAIR AS PER EI T2011A53B-2046 REV 1.

Part: SLEEVE — DAMAGED (NR 1 EXHAUST) · airframe 47,181 hrs · 7,713 cycles

NR 1 ENGINE EXHAUST SLEEVE OUTER SKIN HAS SEVERAL DENTS AND NICKS BETWEEN NSTA 318 &AMP; NSTA 349. BAC APPROVED LEAVING ALL DENTS AS IS SINCE THEY ARE WITHIN ALLOWABLE LIMITS IAW SRM 54-51-30-1A-1 DETAIL VI. NICKS WERE REPAIRED AS PER EI T2011A54B-1997.

Part: DOOR — DEFORMED (CARGO BAY) · airframe 47,181 hrs · 7,713 cycles

FORWARD LOWER EDGE OF LOWER AFT CARGO DOOR WAS FOUND TO BE DEFORMED AT STATION 1827. ACCOMPLISHED REPAIR AS PER EI T2011A52B-1927.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 46,990 hrs · 7,679 cycles

BIRD STRIKE &NBSP; TO NOSE AREA DURING CLIMBOUT. (BIRD STRIKE CONDITIONAL INSPECTION COMPLIED WITH AS PER AMM 05-51-14-202-001 &NBSP;&NBSP; RADOME TIME LIMITED REPAIR CARRIED OUT AS PER EO 4453A617 PART 1 &NBSP; WITH A FAA 8110-3 FORM ISSUED ON 20 AUGUST 2011. PER EO 4453A617 AS PER EO 4453A617 PART 2 ACCOMPLISH REPEAT INSPECTIONS EVERY 5 CYCLES WITH PERMANENT REPAIR WITHIN 2000 FLIGHT HOURS AS PER PART 3).

Part: FAIRING — DAMAGED (LT WLG DOOR) · airframe 45,598 hrs · 7,452 cycles

LEFT WING GEAR DOOR FAIRING DAMAGE. TIME LIMITED REPAIR ACCOMPLISHED IAW EO 4452A121.

Part: LENS — DAMAGED (CABIN) · airframe 42,854 hrs · 7,135 cycles

DURING WALK AROUND INSPECTION FOUND LT OUTBOARD LANDING LIGHT LENS COVER ASSEMBLY DAMAGED. TIME LIMITED REPAIR ACCOMPLISHED AS PER EO 4433AO25.

Part: CONTROL PANEL — MALFUNCTIONED (EFIS) · airframe 42,702 hrs · 7,011 cycles

LT EFIS CONTROL EICAS AND STATIS MESSAGE CIRCUT BREAKER POPPED WITH SMOKE AND FUMES FROM LT EFIS CONTROL. REMOVED AND REPLACED LT EFIS AS PER AMM 31-61-02 OPERATIONAL CHECK HAD STATIS MESSAGE #31460. ITEM DEFERRED ON LOG PAGE #435034.

Part: CONTROL UNIT — FAILED (EICAS) · airframe 42,702 hrs · 7,011 cycles

LEFT EICAS AND STATUS MESSAGE CIRCUIT BREAKER POPPED WITH SMOKE AND FUMES FROM LT EFIS CONTROL. REMOVED AND REPLACED LT EFIS CONTROL AS PER AMM 31-61-02. OPERATIONAL CHECK RETURNED STATUS MESSAGE NR 31460. ITEM DEFERRED ON LOG PAGE 435034.

Part: CONTROL PANEL — MALFUNCTIONED (EFIS) · airframe 42,702 hrs · 7,011 cycles

LT EFIS CONTROL EICAS AND STATIS MESSAGE CIRCUIT BREAKER POPPED WITH SMOKE AND FUMES FROM LT EFIS CONTROL. REMOVED AND REPLACED LT EFIS CONTROL AS PER AMM 31-61-02. OPERATIONAL CHECK RETURNED STATIS MESSAGE 31460 ITEM DEFERRED ON LOG PAGE 435034.

Part: THRUST REVERSER — DAMAGED (NR 2) · airframe 41,480 hrs · 6,825 cycles

LOWER BALLSCREW REMOVED FROM LEFT SLEEVE OF THE NR 2 THRUST REVERSER. TIME LIMITED REPAIR ACCOMPLISHED PER AMM 78-31-00-& NBSP; EO 4478A133 AND FAA 8110-3 DATED 27 JUNE 2010. NOTE: DETAILED VISUAL INSPECTION IS DUE EVERY FLIGHT CYCLE UNTIL PERMANENT REPAIR IS ACCOMPLISHED PRIOR TO 50 FLIGHT CYCLES.

Part: SKIN — CRACKED (COWLING) · airframe 40,531 hrs · 6,681 cycles

FOUND ON WALK AROUND 1-.5 INCH CRACK ON NR 4 ENGINE RIGHT CORE COWLING OUTER SKIN. TIME LIMITED REPAIR ACCOMPLISHED PER ENGINEERING ORDER 4471A053 WITH FAA 8110-3 DATED 18 APR 2010. DVI TO BE PREFORMED EVERY 3 FLIGHT CYCLES WITH PERMANENT REPAIR AT NEXT A-CHECK.

Part: FLANGE — DAMAGED (WING) · airframe 40,370 hrs · 6,656 cycles

ENGINEERING ORDER 4457A139 REVISION "A" WITH FAA 8110-3 DATED 30 MARCH 2010 FOR ACCOMPLISHMENT OF PERMANENT REPAIR TO THE FIXED LEADING EDGE LOWER CHORD FLANGE AT ILES 817.51. THIS EO IS CLASSIFIED AS MAJOR.

Part: PANEL — CRACKED (WING) · airframe 37,652 hrs · 6,263 cycles

DURING WALK AROUND CHECK THE LEFT LOWER LEADING EDGE PANEL IN FRONT OF THE FUELING PANEL DOOR WAS FOUND CRACKED. TIME LIMITED REPAIR ACCOMPLISHED IAW EO 4457A227 AND FAA 8110-3 DATED 22JAN10. DVI REQUIRED EVERY A-CHECK WITH PERMANENT REPAIR TO BE ACCOMPLISHED AT NEXT C-CHECK.

Part: DEPRESSOR — DAMAGED (CARGO DOOR) · airframe 38,689 hrs · 6,418 cycles

DURING WALK AROUND CHECK THE MAIN DECK, SIDE CARGO DOOR SEAL DEPRESSOR ON THE FORWARD AND AFT SIDES WERE FOUND TO BE DAMAGED AT THE TOP CORNERS. TIME LIMITED ACCOMPLISHED IAW EO 4453A308. FAA 8110-3 ISSUED 15 NOV 2009. DVI REQUIRED EVERY FLIGHT CYCLE WITH PERMANENT REPAIR TO BE ACCOMPLISHED AT NEXT A-CHECK.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 38,111 hrs · 6,333 cycles

DURING CRUISE FLIGHT R1 WINDOW ARCED AND THE OUTER LAYER OF WINDOW DELAMINATED. WINDOW AND WINDOW HEAT CONTROLLER REPLACED IAW AMM 56-11-01.

Part: SLEEVE — CRACKED (NR 2 ENGINE) · airframe 37,678 hrs · 6,266 cycles

CRACK FOUND ON THE NR 2 ENGINE EXHAUST SLEEVE AT THE 12 O'CLOCK POSITION DURING WALK AROUND INSPECTION. INTERIM REPAIR ACCOMPLISHED IAW EO 4478A096 ISSUED PER FAA 8110-3 DATED 27 AUG 09. DETAILED VISUAL INSPECTION DUE EVERY 3 FLIGHT CYCLES UNTIL NEXT A-CHECK WHERE A PERMANENT REPAIR OR REPLACEMENT IS DUE.

Part: STRUCTURE — DAMAGED (MLG DOOR) · airframe 36,977 hrs · 6,162 cycles

DURING WALK AROUND INSPECTION FOUND BIRD STRIKE DAMAGED TO THE LE OF THE LEFT WING GEAR DOOR. "TEMP. REPAIR PER EO 4452A093 AS PER SRM 51-70-07 WITH DVI INSP AT EVERY 5 FLT CYCLES AND PERMANENT REPAIRS AT THE NEXT A- CHECK."

Part: SKIN — DAMAGED (TE FLAP) · airframe 36,968 hrs · 6,160 cycles

ON POST FLIGHT WALKAROUND FOUND LEFT INBOARD FLAP MISSING PIECE OF SKIN. "DAMAGE FOUND TO BE WITHIN LIMITS AS PER SRM 51-70-02. PERFORMED TIME LIMITED REPAIR IAW SRM 57-53-01/51-70-17. REQUIRED DIVE CYCLES WITH PERMANENT REPAIR NEXT "A" CHECK."

Part: BLADES — DAMAGED (ENGINE FAN) · airframe 36,698 hrs · 6,123 cycles

CREW REPORTED VIBRATION FROM NR 1 ENGINE ON CLIMB. CREW DUMPED FUEL AND RETURNED TO LAX. FOUND EVIDENCE OF BIRD STRIKE IN NR 1 ENGINE INLET. ACCOMPLISHED BIRD STRIKE INSPECTION PER AMM 72-00-00 AND 05-51-14. REPLACED 7 DAMAGED FAN BLADES PER AMM 72-31-02.

Part: BLEED VALVE — MALFUNCTIONED · airframe 35,857 hrs · 6,002 cycles

CREW REPORTED VIA ACARS EXPERIENCED BLEED PROBLEMS. "ICN MAINTENANCE TROUBLESHOT TO THE NR 2 PRSOV. DEACTIVATED VALVE AND DEFERRED THE ITEM PER DDG 36-11-1."

Part: RVDT — FAULTY (TE FLAP) · airframe 34,892 hrs · 5,858 cycles

DURING CLIMBOUT OF NRT, CREW EXPERIENCED SEVERE WIND SHEAR AND A FLAP ASYMMETRY PROBLEM. OUTBOARD TRAILING EDGE FLAPS WOULD NOT RETRACT PASSED 5 DEGREES. AIRCRAFT RETURNED TO NRT. CONDITIONAL INSPECTIONS FOR HIGH ENERGY STOP AND SEVERE TURBULENCE WERE ACCOMPLISHED IAW AMM 05-51-03 AND 05-51-10. DURING TROUBLESHOOTING OF THE FLAP ISSUE THE RIGHT OUTBOARD FLAP RVDT WAS FOUND TO BE FAULTY AND REPLACED.

Part: START VALVE — FAILED (NR 1 ENGINE) · airframe 32,532 hrs · 5,519 cycles

DURING PUSHBACK AND ENGINE START NR 1 STARTER CUTOUT MESSAGE APPEARED. AIRCRAFT RETURNED TO BLOCKS. START VALVE WAS REPLACED, BUT NO HELP. ITEM WAS THEN DEFERRED IAW MEL 80-11-1. NO OTHER ISSUES. (A)

Part: WARNING LIGHT — ILLUMINATED · airframe 32,216 hrs · 5,474 cycles

DURING PUSHBACK AND ENGINE START "HYD DEM 3" STATUS MESSAGE APPEARED. AIRCRAFT CAME BACK TO BLOCKS. "ITEM WAS DEFERRED IAW MEL 29-11-2-2. NO OTHER ISSUES. (A)

Part: PANEL — CRACKED (LT WING) · airframe 32,090 hrs · 5,453 cycles

LEFT WING INBOARD FIXED PANEL FORWARD OF THE INBOARD FUELING PANEL CRACKED 3 INCHES LONG. ACCOMPLISHED PART 1 OF EO 4457A142. STOP DRILLED CRACK AND APPLIED SPEED TAPE OVER AFFECTED AREA.

Part: ENGINE — FAILED (LEFT) · airframe 31,652 hrs · 5,373 cycles

AT 3000' ON FINAL, A LOUD BANG WAS HEARD ON THE LEFT SIDE OF THE AIRCRAFT, FOLLOWED BY 2 MORE TIMES. ENGINE VIBRATIONS EXCEEDED ON NR 2, ALL ENGINE INDICATIONS THEN APPEARED NORMAL. NR 2 ENGINE CHANGE.

Part: SENSOR — MALFUNCTIONED (NR 2 ENGINE) · airframe 31,341 hrs · 5,318 cycles

AIR TURN BACK DUE TO NR 2 ENGINE SURGING N1, N2, EGT PARAMETERS ON TAKEOFF AND CONTINUED THROUGH CLIMB-OUT AND CRUISE, N1 +/- 5%, N2 +/- 5%, EGT +/- 40. TROUBLESHOT AND FOUND A BAD T2.5 SENSOR. REMOVED AND REPLACED SAME. OPERATIONAL CHECK NORMAL DURING ENGINE RUN.

Part: STRUCTURE — DENTED (HORIZONTAL STAB) · airframe 30,912 hrs · 5,245 cycles

DURING GROUND HANDLING AND PREFLIGHT WALK AROUND FLIGHT CREW FOUND 3 DENTS TO THE LEFT LEADING EDGE OF THE HORIZONTAL STABILIZER. AN INTERIM REPAIR WAS COMPLETED WITH A DVI EVERY 5 FLIGHT CYCLES AS PER MA A45510-01:01 AND SRM 55-10-01 FIG 201.

Part: SEAT TRACK — CRACKED (BS 1850-1862) · airframe 30,447 hrs · 5,171 cycles

MAIN CARGO DECK SEAT TRACK CRACKED AT STATION 1850-1862 RBL 11.33. SCL ACCOMPLISHED INTERIM REPAIR AND MIA ACCOMPLISHED PERMANENT REPAIR PER MA A4 5300-10-00.

Part: APU — AUTO SHUTDOWN · airframe 30,229 hrs · 5,132 cycles

RECEIVED "APU" AND "APU DOOR" STATUS MESSAGES AND APU AUTO SHUTDOWN FOLLOWING ENGINE START. RETURN TO BLOCKS AND APPLIED MEL 49-11-1 AND 49-15-1A. MAINTENANCE ACTION WAS ACCOMPLISHED AS PER THE DDG.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 28,448 hrs · 4,847 cycles

CAPT'S L1 WINDSHIELD CRACKED ON OUTER PANE ORIG IN PVG. REMOVED AND REPLACED WINDSHIELD BOR PART FROM KOREAN AIR PER AMM REF 56-11-01-404-016.

Part: PUMP — LEAKING (NR 2 ENGINE) · airframe 27,280 hrs · 4,643 cycles

HYDR ENG NR 2 ON EICAS DISPLAY. FOUND EDP LEAKING AND SHAFT SHEARED. REMOVED AND REPLACED EDP AND INSTALLED COVER PLATE P/N G29003-1 PER AMM 29-11-05 P 201. DEFERRED PER MEL 29-1-1-C. LEAKS CHECK OK.

Part: SUPPORT TUBE — DAMAGED (FUEL ACCESS DOOR) · airframe 26,277 hrs · 4,491 cycles

LT WING FIXED L/E PANEL DAMAGED AT REFUEL ACCESS PANEL DOOR. REPLACED FIXED L/E SUPPORT RODS FORWARD OF REFUEL PANEL DOOR. ACCOMPLISHED TIME LIMITED, INTERIM REPAIR TO SKIN AND RIB IAW MA A4 57-41-01:01.

Part: HANDLE — UNSECURE (DOOR) · airframe 26,012 hrs · 4,451 cycles

HIGH SPEED REJECT DUE TO OVERHEAD DOOR OPEN INDICATION. INSIDE HANDLE WAS AJAR. CHECKED OPERATION OF HANDLE AND HATCH. OPERATION NORMAL.

Part: COMPRESSOR — DAMAGED (NR 3 ENGINE) · airframe 25,714 hrs · 4,406 cycles

DURING TREND MONITORING OF NR 3 ENGINE, A SHIFT IN PARAMETERS WAS NOTICED. AN INSPECTION ON THE NR 3 ENGINE WAS REQUESTED AND THE AIRCRAFT WAS DIVERTED TO PIK FOR A BORESCOPE INSPECTION. INSPECTED NR 3 ENGINE AND FOUND 11TH STAGE DAMAGE. REMOVED AND REPLACED NR 3 ENGINE PER POLAR WORK CARDS P71-00-00-1A/2A, P71-71-002A, P78-34-02-2A, P7200-101, P7100-002.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 25,095 hrs · 4,301 cycles

CREW REPORTED BURNT TURBINE OIL SMELL EMITTED THROUGH GASPERS IN COCKPIT. VISUALLY INSPECTED FOR EVIDENCE OF OIL LEAKS IN APU, ALL ENGINES, AND ALL PACKS WITH NOTHING FOUND. PERFORMED OPERATIONAL CHECKS OF ALL PACKS PER MM 21-51-10, NO TROUBLE FOUND.

Part: UNKNOWN — SMOKE (CABIN) · airframe 24,923 hrs · 4,276 cycles

ON TAXI OUT, SMOKE WAS NOTICED ON UPPER DECK. CREW REST SMOKE DETECTOR ACTIVATED AND UPPER DECK AIR SUPPLY BUTTON ILLUMINATED. COCKPIT AND LOWER DECK WERE CLEAR OF SMOKE. AFTER A FEW MINUTES, SMOKE/ODORS DISAPPEARED AND AIR SUPPLY RESET. NO FURTHER PROBLEMS. INSPECTED EVIDENCE OF OIL LEAK IN APU. NO TROUBLE FOUND. NO EVIDENCE FOUND WITH ALL 3 PACKS RUN, AND NO EVIDENCE SMELL OF SMOKE PER AMM 49-12-00.

Part: TIRE — FAILED (MLG) · airframe 24,341 hrs · 4,190 cycles

NR 11 TIRE BLOWN ON LANDING CAUSING DAMAGE TO BODY STATION 1480 BULKHEAD TO BODY STATION 1540. DENT REPAIRED PER B747-400 SRM 53-00-01 & APPROVAL PER FAA FORM 8110-3. ALL WORK LISTED ON FAA FORM 337.

Part: STEERING SYS — WARNING MESSAGE · airframe 23,606 hrs · 4,080 cycles

CREW REPORTED -BODY GEAR STRG- AND -BODY GEAR STRG SYS- STATUS MESSAGES DISPLAYED. RETURNED TO BLOCKS. OPENED MEL 32-53-1.

Part: ACTUATOR — FAILED (STEERING) · airframe 23,606 hrs · 4,808 cycles

CREW REPORTED EICAS MESSAGE -CONFIG GEAR CTR- DURING TAKEOFF AT APPROX 30 KTS. REPLACED RT BODY GEAR, LT ACTUATOR PER MM 32-53-11. OPS AND LEAK CHECK OK. ACCOMPLISHED HIGH ENERGY STOP INSPECTION PER MM 05-51-10.

Part: WIRE HARNESS — FAILED (OIL SYSTEM) · airframe 21,683 hrs · 3,789 cycles

OIL TEMP INDICATION INOP AFTER NR 2 ENGINE START - RTB. REMOVED AND REPLACED W-13 (BLUE) WIRING HARNESS PER AMM 73-21-18. OPS TEST GOOD.

Part: ACTUATOR — FAILED (RT WLG) · airframe 21,379 hrs · 3,737 cycles

WHILE PERFORMING ALTERNATE EXTENSION OF WING GEAR, RIGHT WING GEAR WOULD NOT EXTEND AFTER 2MIN 30SEC. REMOVED AND REPLACED RIGHT WING DOWNLOCK ACTUATOR IAW MM 32-32-15-404-006. PERFORMED RETRACTION TEST AND ALT EXTENSION CHECK IAW MM 32-36-00-715-203. OPS CHECK NORMAL.

Part: CONTROLLER — MALFUNCTIONED (NR 3 ENGINE) · airframe 19,591 hrs · 3,447 cycles

STATUS MESSAGE NR 3 ENG PRV / OVHT. (RETURN TO BLOCK) DEFERRED PER MEL 36-11-8C.

Part: SKIN — DELAMINATED (RT FLAP) · airframe 18,867 hrs · 3,335 cycles

DELAMINATION OF LEADING EDGE OF RT OUTBD FORE FLAP FOUND NOT TO BE WITHIN SRM LIMITS FOR CONTINUED SERVICE. RT OUTBD FORE FLAP REPLACED PER MM 27-51-05.

Part: ENGINE — VIBRATION (NR 4) · airframe 17,898 hrs · 3,154 cycles

EXCEEDANCE REPORT ON ENGINE NR 4 VIBRATION, .4 AFTER ENGINE START. REPLACED NR 4 ENGINE DUE TO VSV LEVER ARM BROKEN ON 5TH STAGE IAW P71-00-001A/2A POLAR ENGINE CHANGE WORK CARDS.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 17,501 hrs · 3,087 cycles

ON WALK AROUND FOUND PUNCTURE DAMAGE ON OUTERSKIN OF BULK CARGO DOOR. DAMAGE WAS .7500 ROUND IN DIAMETER 10 INCHES FROM FRONT EDGE, 6 INCHES FROM LOWER EDGE. REPAIRED PER SRM 52-00-01. COI 451-008 RAISED FOR INTERIM REPAIR.

Part: GENERATOR — MALFUNCTIONED · airframe 17,394 hrs · 3,068 cycles

CREW REPORTED RETURN TO BLOCKS DUE NR 2, 3 AND 4 GENERATORS WOULD NOT PARALLEL. RESET SPLIT SYSTEM BREAKER, PERFORMED BCU-1 AND BCU-2 SYSTEM GROUND TEST PER MM 24-11-00. ALL OPS NORMAL.

Part: BLEED VALVE — DEFECTIVE (NR 2 ENGINE) · airframe 17,308 hrs · 3,054 cycles

NR 2 ENGINE BLEED EICAS MESSAGE. REMOVED AND REPLACED NR 2 PRV PER 36-11-19. OPS CHECK NORMAL.

Part: ENGINE — BIRD INGESTION (NR 1) · airframe 16,769 hrs · 2,962 cycles

BIRD INGESTION INTO NR 1 ENG AT ROTATION. ENG SHUT DOWN. PERFORMED BIRD STRIKE INSPECTION PER MM 05-51-14. REPLACED ENG PER PAC: P71-00-00-1A AND P71-00-00-2A.

Part: STARTER — FAILED (NR 2 ENGINE) · airframe 16,643 hrs · 2,939 cycles

NR 2 ENGINE NO ROTATION ON START. REPLACED STARTER MOTOR PER MM 80-11-02.

Part: SEAL — NICKED (NR 2 STARTER) · airframe 16,643 hrs · 2,939 cycles

SECONDARY ENGINE EXCEEDANCE DUE WITH LOW NR 2 ENG OIL QTY DOWN TO 4 GALS. A/C RETURNED TO SHJ. INSPECTED ENG NR 2, FOUND STARTER MOTOR SHAFT SEAL NICKED AND OIL LEAK. REPLACED SEALS & ENG RUN/LEAK CHECKED PER MM 80-11-02.

Part: FAN — MALFUNCTIONED (E/E BAY) · airframe 13,977 hrs · 2,467 cycles

MULTIPLE CMC STATUS MESSAGES PRIOR TO DEPARTURE, ZONE TEMPRATURE, E/E COOLING & GEAR MONITORING. GEAR MONITORING MESSAGE CLEARED, DEFERRED ZONE TEMPERATURE MEL 21-61-8A, DEFERRED E/E COOLING FAN PER MEL 21-58-6.

Part: TUBE — LEAKING (HYD SYSTEM) · airframe 13,552 hrs · 2,400 cycles

STATUS MESSAGE, "HYD PRESSURE ENG 2." INSTALLED FLEX LINE IN PLACE OF RIGID LINE AND SECURED, OPS AND LEAK CHECK OK IAW MM 29-00-00 AND SERVICED HYD LEVEL TO FULL.

Part: AILERON — MALFUNCTIONED · airframe 12,194 hrs · 1,785 cycles

AFTER ENG START CREW REPORTED AILERON INDICATION PROBLEMS DURING FLT CNTRL CHECK. CONFIRMED W/ VISUAL OPERATION THAT THE CONTROL SURFACES LOOKED NORMAL, DEFERRED IAW MEL 27-18-1

Part: SKIN — GOUGED (FUSELAGE) · airframe 9,693 hrs · 1,700 cycles

AFT FUSELAGE SKIN AT STA 2392 THRU 2394 DEEP GOUGE. CUT OUT DAMAGE, FABRICATED & INSTALLED REPAIR DOUBLER & FILLER AS PER SRM 53-00-01 FIF 201.

Part: CONTROLLER — FAULTY (1R WINDOW) · airframe 8,669 hrs · 1,514 cycles

AFTER TWO HOURS OF FLT SMOKE WAS OBSERVED COMING FROM RT SIDE COCKPIT. AOM PROCEDURE COMPLIED W/. SMOKE SOURCE TRACED TO LWR AREA OF NUMBER 1 RT WINDOW. WINDOW HEAT 1R SWITCHED OFF, SMOKE STOPPED. AREA OF GREASE WAS OBSERVED ALONG LWR PART OF WINDOW. REMOVED AND REPLACED 1R WINDOW HEAT CONTROL UNIT AS PER MM 30-41-01. OPS CHECKS NORMAL.

Part: A/C PACK — ODOR (COCKPIT) · airframe 8,662 hrs · 1,513 cycles

DURING CRUISE OILY ODOR WAS NOTICED ON FLT DECK FOLLOWED BY LITE SMOKE FROM F/O'S AC VENT. AOM PROCEDURE COMPLIED WITH, A/C DESCENDED TO FL29 AS A PRECAUTION WITH CREW ON 02. SMOKE CLEARED FOLLOWING COMPLETION OF PROCEDURE WITH INTERMITTANT INCREASED ODOR. PERFORMED INSPECTION FOR OIL CONTAMINATIONS AS PER MM 21-00-01-802, NO OIL FOUND IN DUCTS PER PACK 1, 2, 3 PER MM 21-51-05 -201. NO LEAKS OR FURTHER ODOR WITH 3 PACKS RUNNING.

Part: SKIN — DENTED (LWR CARGO DOOR) · airframe 4,920 hrs · 840 cycles

LOWER AFT EDGE SKIN OF AFT LWR CARGO DOOR DENTED IN BY CONTACT WITH GROUND EQUIPMENT. TRANSFERRED TO COI #451-013 PER MX CTRL (JOHN). NO FURTHER DISCREPANCIES NOTED. OK FOR CONTINUED SERVICE. COMPLETED REPAIR AT NEXT STATION (MIA) ON AFT CARGO DOOR PER SRM 52-00-01, P 209. COI #451-013 CLEARED.

Part: SERVICE DOOR — BROKEN (LT WING) · airframe 4,379 hrs · 748 cycles

AT SCL ARRIVAL FOUND LT WING LT FUELING PANEL DOOR BROKEN. TRANSFERRED TO CDL 28876 AS PER CDL 57-31-1. CAUSE IS UNDER INVESTIGATION. REMOVED DOOR AND COVERED WITH HIGH SPEED TAPE.

Part: SEAT TRACK — CRACKED (FWD CARGO COMPT) · airframe 4,208 hrs · 720 cycles

FORWARD CARGO COMPARTMENT BS 560 - RBL - 45, WL - 118 SEAT TRACK CRACKED. REPAIRED BY SPLICED IN SECTION OF SEAT TRACK IAW 400F SRM 53-00-52, PG 251

Part: SEAT TRACK — CRACKED (FWD CARGO COMPT) · airframe 4,208 hrs · 720 cycles

FORWARD CARGO COMPARTMENT BS 560 - LBL - 225, WL 118 SEAT TRACK CRACKED. REPAIRED BY SPLICED IN SECTION OF SEAT TRACK IAW 400 SRM 53-00-52, PG. 251

Part: GCU — FAILED (NR 1 ENGINE) · airframe 3,787 hrs · 646 cycles

FIVE SECONDS AFTER LIFT OFF, EICAS MESSAGE APPEARED: ELEC AC BUS - NR 1 AC BUS BECAME ISOLATED AND UNPOWERED. WOULD NOT RESET PER NNL ELEC AC BUS CHECKLIST. FOUND NR 1 GCU DIFFERENTIAL LOCK OUT. REPLACED NR 1 GCU WITH KLM LOAN PART. CARRIED OUT CMC GROUND TEST & OPS CHECK ON ENG RUN. ALL SATISFACTORY.