N452PA

Part: ACTUATOR — FAULTED (OUTFLOW VALVE) · airframe 101,102 hrs · 17,094 cycles

OUTFLOW VALVE R EICAS MSG. REMOVED & REPLACED RT OUTFLOW VALVE ACTUATOR ASSY, RT ICU & DIODE IAW AMM 21-31-10/401, 21-31-07/401, SWPM 20-40, AIPC 21-31-01-01 & AIPC 21-31-10-01. OPS CHKD OK.

Part: FIRE WARNING — FALSE ACTIVATION (ZONE 100) · airframe 98,028 hrs · 16,617 cycles

DURING FLIGHT N452PA HAD A MDC FIRE WARNING ALERT. CREW VERIFIED NO FIRE OR SMOKE, CONTINUED TO ANC.(<P>CONFIRM NO SMOKE OR FIRE FROM PREVIOUS LEG. PERFORMED CARGO DET FIRE TEST PER AMM 26-14-00. NO ACTIVE FAULTS PRESENT.</P>)

Part: SMOKE DETECTOR — FALSE ACTIVATION (CREW REST) · airframe 95,137 hrs · 16,174 cycles

CREW REST SMOKE EICAS MSG. NO SMOKE OR FIRE CONFIRMED.(<P>WIRING CHECKED NORMAL PER B747-400 WDM 26-13-31 REV 33. NEED TO REPLACE R/H CREW REST SMOKE DETECTOR. PERFORMED CHECK FLIGHT DECK EQUIPMENT AND CABIN EQUIPMENT. PERFORMED FUMES SMELL CHECK IN BLEED DUCT WITH ENG AND APU RUNNING, CHECKS OK PER B747 FIM 21-00 TASK 810 REV 110. R/R R/H CREW REST SMOKE DETECTOR &AMP; OPS TEST OK PER B747 AMM 26-74-51 REV 110. COMPLETED B747 AMM TASK 05-51-50 REV 110.

Part: RELAY — INOPERATIVE (FUEL PUMP) · airframe 94,955 hrs · 16,130 cycles

FOUND R54 RELAY (#4 FWD) GFI RELAY NOT EQUIP(<P>1) IAW SWPM 20-81-22, 20-20-00 REV. 84, WDM 28-22-31 REV.33 REPLACED #4 FWD GFI RELAY. 2) TRANSFER TO I/C 28-22-03-01 STEP I AND STEP K FOR R54 RELAY TEST AND RESULT WAS SATISFACTORY</P>)

Part: CARGO TRACK — CRACKED (BS 1485) · airframe 94,955 hrs · 16,130 cycles

FND M/D CGO SUBSTITUTE TRACK CRACK AT STA 1485 LBL 75.92(<P>1) PERFORM JOB IAW WORKSHEET #40066 AND DWG #65B38251 SHEET 62 REV A, SHEET 32 REV -, 14440802, SHEET 3 REV B 2) JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: FLOORBEAM — NONE (BS 340) · airframe 94,955 hrs · 16,130 cycles

DEVIATION- DURING PERFORM SB 4453A087 PART 2, AT L/H STA 340 UPPER DECK FLOOR BEAM STRAP HAVE 1 EA FASTENER CAN'T REMOVED.(<P>1) PERFORM JOB IAW EI T2024A53M-246, SEQUENCE A REV 0 2) ACCOMPLISHED EI T2024A53M-246, REV 1 3) JOB COMPLETED AND COND CHK NML.</P>)

Part: DOOR FRAME — CRACKED (BS 2240) · airframe 94,955 hrs · 16,130 cycles

FND DOOR CUTOUT CRACK AT L5 DOOR RELEASE HANDLE AREA, STA 2240, WL 250.(<P>1) PERFORM JOB IAW WORK SHEET #40078 2) JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: FLOORBEAM — CRACKED (BS 980) · airframe 94,955 hrs · 16,130 cycles

FND FLOOR STRUCTURE CRACK AT M/D STA 980 RBL 75.92(<P>1) PERFORM JOB IAW WORKSHEET #40071 AND DWG #65B16004, SHEET 4 REV A , 65B38250, SHEET 17 REV A, SHEET 9 REV B 2) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: SKIN — DEBONDED (RT NR 7 SPOILER) · airframe 94,955 hrs · 16,130 cycles

DISBOND - RH WING #7 SPOILER LWR SURFACE, AT INBD EDGE, T/E EDGE(<P>1) PERFORM INTERIM REPAIR AT #7 SPOILER INBD SIDE T/E AREA, REFER TO EGAT EI T2024A57M-294 REV 1. 2) CONDITION CHECK IS SATISFACTORY</P>)

Part: SKIN — DEBONDED (LT AILERON) · airframe 94,955 hrs · 16,130 cycles

DISBOND - EDGE, LH WING INBD AILERON OUTBD CORNER.(<P>1) PERFORM REPAIR OF DISBOND SKIN AREA AT LH WING INBD AILERON OUTBD SIDE IAW SRM 57-60-01. PLEASE REFER TO THE JOB CARD ATTACHING SHEET FOR DETAILED REWORK INFORMATION. 2) CONDITION CHECK IS SATISFACTORY.</P>)

Part: FLOORBEAM — NONE (BS 340) · airframe 94,955 hrs · 16,130 cycles

DEVIATION- DURING PERFORM SB 4453A087 PART 2, AT R/H STA 340 UPPER DECK FLOOR BEAM STRAP HAVE 1 EA FASTENER CAN'T REMOVED.(<P>1) PERFORM JOB IAW EI T2024A53M-248, SEQUENCE A REV 0 2) ACCOMPLISHED EI T2024A53M-248, REV-1 3) JOB COMPLETED AND COND CHK NML.</P>)

Part: CARGO TRACK — CRACKED (BS 1485) · airframe 94,955 hrs · 16,130 cycles

FND M/D CGO SUBSTITUTE TRACK CRACK AT STA 1485, RBL 75.92(<P>1) PERFORM JOB IAW WORK SHEET NO: 40068 AND DWG NO:14440802, SHEET 3, REV B, 65B38751, SHEET 62 REV A SHET 32 REV-, SHEET 75 REV- 2) JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: FLOORBEAM — NONE (BS 500) · airframe 94,955 hrs · 16,130 cycles

DEVIATION- DURING PERFORM SB 4453A087 PART 2, AT R/H STA 500 UPPER DECK FLOOR BEAM STRAP HAVE 2 EA FASTENER CAN'T REMOVED.(<P>1) PERFORM JOB IAW EI T2024A53M-249, SEQUENCE A REV 0 2) ACCOMPLISHED EI T2024A53M-249, REV 1 3) JOB COMPLETED AND COND CHK NML.</P>)

Part: CARGO TRACK — CRACKED (BS 1720-1730) · airframe 94,955 hrs · 16,130 cycles

FND M/D CGO SUBSTITUTE TRACK CRACK AT STA 1720 ~ 1730, RBL 75.92(<P>1) PERFORM JOB IAW WORKSHEET #40069 AND DWG #65B38751, SHEET 62 REV A, SHEET 32 REV-, SHEET 75 REV-&NBSP; &NBSP;2) JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: SKIN — CHAFED (RT AILERON) · airframe 94,955 hrs · 16,130 cycles

CHAFING - SKIN PNL, RH WING INBD AILERON OUTBD TE AREA(<P>1) PERORM REPAIR OF CHAFING SKIN DAMAGE AT R/H WING INBD AILERON T/E OUTBD SIDE. PLEASE REFER TO THE JOB CARD ATTACHING SHEET FOR DETAILED REWORK INFORMATION. 2) CONDITION CHECK IS SATISFACTORY.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,624 hrs · 15,912 cycles

#1 HYD QUANTITY DROPPING(<P>LOCATED LEAK OF HYDRAULIC LINE AT STA 900. REPAIRED PER GMM 3.24.1 USING A NEW SECTION OF PIPE AND 2 EA RYNGLOC FITTINGS. PRESSURE TESTED, NIL LEAKS. FITTINGS USED PN: R80101T08. AMM 20-11-05 FOR REFERENCE.</P>)

Part: ACM — UNKNOWN (UNKNOWN) · airframe 93,542 hrs · 15,897 cycles

BURNING SMELL & VIBRATION ON FINAL. ISOLATED TO PACK 1. NO INDICATIONS, SHUT OFF PACK(<P>PACK 1 PLACED ON DMI 192433 PER MEL 21-51-01-03 &AMP; DMI 192434 PER 26-16-01-02-01B (DUE TO PACK 1 INOP). PACK 1 DMI 192433 &AMP; FWD LOBE FIRE DETECTION DMI 192434. CHAPTER 5 CONDITIONAL INSPECTION (AMM 05-51-56) CARRIED OUT. LP 1673134 ITEM 3 1SEP23: R/R ACM IAW AMM 21-51-04/401. OPS CHECK GOOD. DMI 192433 CLOSED. LP 1673135 ITEM 4 1SEP23: REACTIVATED SMOKE DETECTORS &AMP; OPS CHECK GOOD IAW AMM 26-16-01-404-008.</P>)

Part: FLAP — DAMAGED · airframe 88,047 hrs

DURING WALK AROUND, FOUND #7 L/E FLAP VARIABLE CAMBER DAMAGED(<P ><SPAN>REPLACED #7 L/E FLAP VARIABLE CAMBER PER AMM 27-81-02/401.&NBSP; PERFORMED FLAP OPS AND FCU GROUND TEST OK PER AMM 27-81-00/801.</SPAN></P> / <P>&NBSP;</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

M/D STA 1778-1800 LBL 33 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1778-1800 LBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

M/D STA 1822-1825 LBL 33 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1822-1825 LBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

M/D - STA 1820 RBL 99 SEAT TRACK FOUND CORROSION(<P>M/D - STA 1820 RBL 99 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

NO.3 PYLON #472ER ACCESS PANEL 1EA FASTENER LOCK PLATE ATT RIVET FOUND BROKEN AND 1EA FASTENER HOLE FOUND WORN(<P>NO.3 PYLON ACCESS PANEL 472ER FASTENER HOLE ELONGATION AREA REPAIRED IAW RI-54-50-15409 REV.A</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

M/D - STA 1880 RBL 99 SEAT TRACK FOUND CORROSION(<P>M/D - STA 1880 RBL 99 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

M/D - STA 1350-1360 RBL 11.33" SEAT TRACK FOUND CORROSION(<P>M/D - STA 1350-1360 RBL 11.33" SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01 CHECKED WITHIN SRM 52-00-52 ALLOWABLE DAMAGE . 1 FIG 101 LIMIT</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

M/D - STA 1470-1480 RBL 11.33 SEAT TRACK FOUND CORROSION(<P>M/D - STA 1470-1480 RBL 11.33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

STA 2231 1EA CRACK WAS FOUND ON REVEAL RUNNING AFT THROUGH THE FASTENER HOLE AND EXTEND TOWARDS THE EDGE(<P>M/D STA 2231 STR 21L - 22L DOOR REVEAL DOUBLER CRACK AREA REPAIRED IAW SRM 53-60-15-2R-3 REPAIR 3. THIS REPAIR IS A PERMANENT REPAIR AND CATEGORY B REPAIR. REPEAT INSP IAW SB 747-53A2450</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

M/D - STA 2117-2120 LBL 11.33 SEAT TRACK FOUND CORROSION(<P>M/D - STA 2117-2120 LBL 11.33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01 CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT&NBSP;</P>)

Part: DUCT — NONE · airframe 87,661 hrs · 14,934 cycles

NO.4 ENG R/H C-DUCT OPEN ACTUATOR ATT FITTING BOLT HOLE FOUND ELONGATED.(<P>NO.4 ENG R/H C-DUCT REPLACED IAW AMM 78-31-01. T/R COWL P/N 683L177G13 CONVERSION TO P/N 683L179G09 REF TO CARD NO. CR.636372</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

M/D - STA 1908 RBL 33 SEAT TRACK FOUND CORROSION(<P>M/D - STA 1908 RBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

M/D - STA 1920 RBL 75.92 SEAT TRACK FOUND CORROSION.(<P>M/D - STA 1920 RBL 75.92 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

M/D - STA 1840 RBL 99 SEAT TRACK FOUND CORROSION(<P>M/D - STA 1840 RBL 99 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

M/D STA 1922 LBL 33 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1922 LBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

RHW O/B FORE FLAP O/B L/E AREA FOUND DELAM(<P>PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07 PAR.5.A REV.94 ,FEB20/2022 AND REFER TO HX PROCESS CARD CONTROL SEQUENCE NO. WO.637467 FOR REPAIR DETAILS</P>)

Part: WEB — NONE · airframe 87,661 hrs · 14,934 cycles

SECT 44 - MAIN DECK FOUND CRACK ON THE WEB OF PRESSURE DECK AT STA 1241 RHS AND LHS 106, CAT C TIME - LIMITED REPAIR(<P>SECT 44 - MAIN DECK PRESSURE DECK AT STA 1241 TO STA 1265 LBL 98- LBL 127 P/N: 65B26630-11 AND STA 1241 TO STA 1265 RBL98-RBL127 WEB P/N: 65B26630-12 REPLACED IAW RI-53-00-15408 REV.A</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

M/D - STA 2196-2198 LBL 11.33 SEAT TRACK FOUND CORROSION(<P>M/D - STA 2196-2198 LBL 11.33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01 CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

M/D STA 1830-1836 RBL 33 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1830-1836 RBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

M/D STA 1270-1278 RBL 11.33" SEAT TRACK FOUND CORROSION.(<P>M/D STA 1270-1278 RBL 11.33" SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 52-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

M/D - STA 1337 RBL 11.33 SEAT TRACK FOUND CORROSION(<P>M/D - STA 1337 RBL 11.33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

M/D STA 1846 RBL 11.33" SEAT TRACK FOUND BROKEN(<P>M/D STA 1766.45 TO STA 1870.45 RBL 11.33" SEAT TRACK REPAIRED IAW SRM 53-00-52-2R-12 REPAIR 12 FIG 201 REV.94 DATE 20FEB 2022</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

BS 2231 1EA CRACK WAS FOUND ON THE FASTENER HOLE AT S25L RUNNING FWD AT 4 O'CLOCK POSITION APPROX 0.040"(<P>&NBSP;STA 2231 STR 25L FRAME STRAP LAYER 1EA FASTENER HOLE OVERSIZE REPAIRED IAW RI-53-60-15406 REV.A</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

M/D - STA 1410-1418 RBL 11.33 SEAT TRACK FOUND CORROSION(<P>M/D - STA 1410-1418 RBL 11.33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

M/D STA 850 - 809 LBL 11.33" SEAT TRACK FOUND CORROSION(<P>M/D STA 805 - 809 LBL 11.33" SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 52-00-52 ALLOWABLE DAMAGE. 1 FIG 101 LIMIT</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

STA 2598 L/H B/H LOWER CORNER 3EA FASTENER HOLE FOUND CRACK AT AFT INNER CHORD(<P>STA 2598 LOWER CORNER LH AFT INNER CHORD 3EA FASTENER HOLE CRACK AREA REPAIRED IAW RI NO: 53-80-15413 REV.A</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

M/D - STA 1877 RBL 33 SEAT TRACK FOUND CORROSION(<P>M/D - STA 1877 RBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

M/D - STA 1920 RBL 99 SEAT TRACK FOUND CORROSION(<P>M/D - STA 1920 RBL 99 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

M/D STA 1290-1298 RBL 11.33" SEAT TRACK FOUND CORROSION(<P>M/D STA 1290-1298 RBL 11.33" SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 52-00-52 ALLOWABLE DAMAGE.1 FIG 101 LIMIT</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

M/D - STA 1777 - 1784 RBL 99 SEAT TRACK FOUND CORROSION(<P>M/D - STA 1777 - 1784 RBL 99 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

NO.2 PYLON 462EL ACCESS PANEL 2EA FASTENER HOLE FOUND WORN(<P>NO.2 PYLON 462EL ACCESS PANEL FASTENER HOLE ELONGATION WORN AREA REPAIRED IAW RI-54-50-15414 REV.A</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

M/D STA 1860 RBL 99 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1860 RBL 99 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

M/D STA 1310-1318 RBL 11.33" SEAT TRACK FOUND CORROSION(<P>M/D STA 1310-1318 RBL 11.33" SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01 CHECKED WITHIN SRM 52-00-52 ALLOWABLE DAMAGE.1 FIG 101 LIMIT&NBSP;</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

NO.4 PYLON 482EL ACCESS PANEL 1EA FASTENER HOLE FOUND WORN(<P>NO.4 PYLON 482EL ACCESS PANEL FASTENER HOLE ELONGATION WORN AREA REPAIR IAW RI-54-50-15415 REV.A</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

U/D STA 740 LH TENSION TIE AFT CHANNEL STARTING FROM THE FASTENER HOLE RUNNING O/B TO THE EDGE FOUND CRACKED APPROX 3/8" IN LENGTH.(<P>U/D STA 740 LBL 55" TO END OF O/B TENSION TIE CHANNEL REPAIRED IAW SRM 53-20-30-2R-1 REPAIR 1. THIS REPAIR IS A PERMANENT REPAIR AND CATEGORY B, REPEAT INSPECTION IAW TABLE 203.</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

LHS CANTED HORI FLANGE OF STA 1241 BULKHEAD FORGED FITTING FOUND CRACK RUNNING I/B AT 3 O/C POSITION AND APPROX 7/8 IN LENGTH AT UPPER SURFACE(<P>FX - STA 1241 L/H O/B CANTED HORI FLANGE OF BULKHEAD FORGED FTG P/N: 65B07920-49 CRACK AREA REPAIRED IAW RI-53-00-15408 REV.A</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

LHW O/B MID FLAP MIDDLE AREA UPPER PANEL 587MT AFT EDGE FOUND BUGLE UP (CORROSION)(<P>LHW O/B MID FLAP MIDDLE AREA UPPER PANEL 587MT AFT EDGE CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01 CHECKED WITHIN SRM 57-53-02-1A-1 LIMIT</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

LHW #11 KRUEGER FLAP O/B LWR CORNER FOUND DELAM(<P>PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-17 PAR.5.G REV.94.FEB20/2022 AND REFER TO HX PROCESS CARD SEQUENCE NO. WO.625865 FOR REPAIR DETAILS</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

M/D - STA 1900 RBL 99 SEAT TRACK FOUND CORROSION(<P>M/D - STA 1900 RBL 99 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

M/D STA 1886-1890 LBL 33 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1886-1890 LBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

BS 2231 2EA CRACK WERE FOUND ON THE FASTENER HOLE AT STR 17L RUNNING AFT AT 9 O'CLOCK POSITION APPROX 0.040"(<P>M/D - STA 2231 STA 17L FRAME STRAP LAYER CRACK AREA REPAIRED IAW RI-53-60-15406 REV.A</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

LH BLG W/W STA 1438-1460 STR 35L INTERCOSTAL FOUND CRACK(<P>LH BLG W/W STA 1438-1460 STR 35L INTERCOSTAL P/N: 65B16948-3 REPAIRED IAW RI-53-00-15421 REV.A</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

NO.3 PYLON 472EL ACCESS PANEL 1EA FASTENER HOLE FOUND WORN(<P>NO.3 PYLON 472EL ACCESS PANEL FASTENER HOLE ELONGATION WORN AREA REPAIRED IAW RI-54-50-15410 REV.A</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

RHS CANTED HORIZONTAL FLANGE OF STA 1241 BULKHEAD FORGED FTG FOUND 2EA CRACK AT 3 O'CLOCK AND 9 O'CLOCK POSITION AND BOTH APPROX 3/16" IN DEPTH AT THE BOTTOM OF FIRST LAYER.(<P>FX - STA 1241 R/H CANTED HORIZONTAL FLANGE BULKHEAD FORGED FTG P/N: 65B07920-50 1EA SCREW HOLE CRACK AREA REPAIRED IAW RI NO: RI-53-00-15408 REV A.</P>)

Part: NONE — NONE · airframe 87,661 hrs · 14,934 cycles

M/D STA 1774-1776 RBL 33 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1774-1776 RBL 33 SEAT TRACK CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)

Part: SHEAR TIE — NONE · airframe 87,661 hrs · 14,934 cycles

1EA CRACK WAS FOUND ON THE RBL 33.99 AND 1EA CRACK WAS FOUND ON THE RBL 57.5 SHEAR TIE AT 1000 FRONT SPAR(<P>STA 1000 RBL 33.99 AND RBL 57.5 SHEAR TIE REPLACED AND INSTALLED IAW EO 4453C024 PART 8 AND PART 9 AND RI 53-00-15419 REV.A, RI 53-00-15420 REV.A</P>)

Part: DOOR — DAMAGED (TAILCONE) · airframe 84,917 hrs · 14,475 cycles

DURING WALK AOUND INSP FOUND TAIL SKID MARKS ON BOTH APU DOORS(<P>REPLACED RH/LH APU DOORS. PERFORMED REPAIR OF TAILCONE AREA PER BOEING SR AND E.O. (OFF PART: PN 65B02771-209, SN TLS23687)</P>)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 84,041 hrs · 14,317 cycles

DURING A-CHECK FUSELAGE SKIN DAMAGE, SIZE 10"L X 5.1"W, AND STRINGER DAMAGED SIZE 1.5" L X 0.3" W. REFER TO RAM FORM N453PA-21-01 AND N453PA-21-02. ACCOMPLISHED A PERMANENT REPAIR TO / THE DAMAGED SKIN (PN: 65B23900-1) BETWEEN STA 2577 TO BSTA 2598 AND STRINGER S-38R TO S-42R PER EO 4453B984 PART 1 AND DAMAGED TO STRINGER S-42R PER EO 4453B984 PART 2.

Part: COMPRESSOR — DAMAGED (NR 1 ENGINE) · airframe 83,811 hrs · 14,273 cycles

DEPARTING KLAX ENG #1 COMPRESSOR STALLED 4 TIMES CLIMING OUT OF APPROX 1000'. QRH PROCEDURES FOLLOWED RESULTING IN NORMAL ENGINE OPERATION.(<P>PERFORMED STALL INSPECTION WITH BOROSCOPE AT HPC 1,6,12,13,14. FOUND DAMAGE AT 12,13,14 BLADES SO DECIDED ENGINE REPLACEMENT IAW AMM 72-00-00-206-050-J00.</P>)

Part: BLEED VALVE — MALFUNCTIONED (ENGINE) · airframe 83,127 hrs · 14,151 cycles

BLEED NR 3 EICAS MESSAGE ON TAKE OFF ROLL. FWD TO MEL 36-11-03, MDDR 140670, CAT C. DEACT NR 3 HP BLEED. REMOVED AND REPLACED HPC (OFF PART: PN 773289-18, SN 200002037) AND HPV, IAW B747 AMM 36-11-00. OPERATIONS CHECK GOOD. THIS CLEARS MDDR 140670.

Part: B-NUT — LEAKING (HYD SYSTEM) · airframe 81,081 hrs · 13,756 cycles

IN FLIGHT HYD QTY LOW, NR 4 INDICATING .34. AFTER LANDING .74. FIM 29-11/884. EXTERNAL LEAK CHECKED IAW AMM 29-11-00 AND FOUND RUNNING LEAK AT GROUND SPOILER CONTROL VALVE B-NUT. TIGHTENED THE B-NUT AND LEAK CHECKED OK. SYSTEM NR 4 SERVICED IAW AMM 12-12-01. SYSTEM NR 4 PRESSURE AND LEAK CHECK OK. AREA CLEANED.

Part: SMOKE DETECTOR — FALSE ACTIVATION (MAIN DECK) · airframe 80,450 hrs · 13,637 cycles

EICAS WARNING "FIRE MN DK MID" DURING CRUISE. VISUALLY VERIFIED FALSE.&NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; ITEM 2: CARGO "CGO DET 8 MN DK" STATUS MESSAGE.&NBSP;(<P STYLE="MARGIN: 0IN; MARGIN-BOTTOM: .0001PT;"><SPAN>ITEM 1: ITEM UNABLE TO DUPLICATE, / PLEASE SEE ITEM 2.</SPAN></P><P STYLE="MARGIN: 0IN 0IN 0.0001PT;"><SPAN>ITEM / 2: CHECKED &AMP; FOUND CMC MSG #26325.&NBSP; FOLLOWED FIM 26-16 TASK 870.&NBSP; / REMOVED AND REPLACED WITH NEW SMOKE DETECTOR ON THE M/D ZONE 8 LOOP B IAW AMM / 26-14-01/401, AND CHECKS OK.&NBSP; MCC NOTIFIED.</SPAN></P>)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,772 hrs · 13,525 cycles

M/D - STA 1480 - 1590 RBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1480 - 1590 RBL 11 SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12.</P>)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,772 hrs · 13,525 cycles

M/D - STA 900 - 920 RBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D STA 900 - 920 RBL SEAT TRACK CORROSION AREA REWORKED AS PER SRM 53-00-52 FIG 101.</P>)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,772 hrs · 13,525 cycles

M/D - STA 980 LBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D - STA 980 LBL 11 SEAT TRACK CORROSION AREA REWORKED AS PER SRM 53-00-52 FIG 101.</P>)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,772 hrs · 13,525 cycles

L/H DOOR 1 FWD DOOR SILL EMERGENCY LIGHT FOUND INOP (L1853).(<P>L/H DOOR 1 FWD DOOR SILL EMERGENCY LIGHT LAMP REPLACED AND OPERATION TEST NORMAL IAW AMM 33-51-05.</P>)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,772 hrs · 13,525 cycles

M/D - STA 1480 RBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1480 RBL 11 SEAT TRACK REPAIRED AS PER RI 53-60-13947 REV A.</P>)

Part: WEB — CRACKED (FUSELAGE) · airframe 79,772 hrs · 13,525 cycles

STA 1241 L/H B/H WEB FOUND CRACK.(<P>STA 1241 L/H B/H WEB CRACK AREA REPAIRED AS PER RI-53-00-13943 REV A.</P>)

Part: WEB — CRACKED (FUSELAGE) · airframe 79,772 hrs · 13,525 cycles

STA 1241 RH B/H WEB FOUND CRACK.(<P>STA 1241 R/H B/H WEB CRACK AREA REPAIRED AS PER RI-53-00-13943 REV A.</P>)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,772 hrs · 13,525 cycles

M/D - STA 1840 LBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D - STA 1840 LBL 11 SEAT TRACK CORROSION AREA REWORKED AS PER SRM 53-00-52 FIG 101.</P>)

Part: FRAME — DAMAGED (FUSELAGE) · airframe 79,772 hrs · 13,525 cycles

FWD CARGO STA 620 LBL 45 FRAME UPPER CHORD DAMAGED.(<P>FWD CARGO STA 620 LBL 45 FRAME UPPER CHORD REPAIRED AS PER SRM 53-20-07-2R REPAIR 11.</P>)

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 79,772 hrs · 13,525 cycles

TAIL SECTION STA 2520 RH LOBE DOUBLER FOUND CRACK.(<P>TAIL SECTION STA 2520 RH LOBE DOUBLER CRACK AREA REPAIRED AS PER RI 53-00-13952 REV A.</P>)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,772 hrs · 13,525 cycles

M/D STA 830 - 950 LBL 11" SEAT TRACK FOUND CORROSION.(<P>M/D STA 830 - 950 LBL 11 SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12.</P>)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 79,772 hrs · 13,525 cycles

FX STA 1840 - 1900 S-42L TO S-43L SKIN DAMAGED.(<P>FX STA 1840 - 1900 S-42L TO S-43L SKIN REPAIRED AS PER SRM 53-00-01-2R-1 AND RI 53-60-13958 REV A.</P>)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,772 hrs · 13,525 cycles

M/D - STA 1120 TO 1140 LBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D - STA 1120 TO 1140 LBL 11 SEAT TRACK CORROSION AREA REWORKED AS PER SRM 53-00-52 FIG 101</P>)

Part: LIGHT — DIM (COCKPIT) · airframe 79,772 hrs · 13,525 cycles

COCKPIT - AISLE EMER LT FOUND DIM.(<P>COCKPIT AISLE EMER LT REPLACED AND TEST NORMAL IAW AMM 33-51-00.</P>)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,772 hrs · 13,525 cycles

L/H DOOR 1 FWD ENTRANCE CEILING EMERGENCY LIGHT FOUND INOP.(<P>L/H DOOR 1 FWD ENTRANCE CEILING EMERGENCY LIGHT LAMP REPLACED AND LAMP TEST NORMAL IAW AMM 33-51-07.</P>)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,772 hrs · 13,525 cycles

M/D - STA 2150 - 2190 RBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D STA 2150 - 2190 RBL 11 SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12.</P>)

Part: SCAVENGE PUMP — CONTAMINATED (NR 1 ENGINE) · airframe 79,498 hrs · 13,446 cycles

SHUT DOWN THE NR 1 ENGINE DUE TO LOW OIL QUANTITY. MAINTENANCE NOTED THAT UPON ARRIVAL, OIL QUANTITY RETURNED TO 18 QUARTS. NO LEAKS FOUND. PERFORMED AN INSPECTION OF THE SCAVENGE SYSTEM FILTERS, FOUND DEBRIS IN THE TRANSFER GEARBOX INLET SCREEN TO THE SCAVENGE PUMP. POWERPLANT ENGINEERING WAS THEN PRESENTED WITH ALL FINDINGS AND THEY CALLED FOR ENGINE TO BE REPLACED. THE NR 1 ENGINE WAS REPLACED IAW MM 71-00-02.

Part: ENGINE — FAILED (NR 1) · airframe 79,498 hrs · 13,446 cycles

NR 1 ENGINE FAILED AT 3500 FT MESSAGE ON APPROACH IN RAIN WITH NAI ON ENGINE RESTARTED AUTOMATICALLY. FOLLOWED FIM 71-00 FIGURE 114 FOR AUTO SHUTDOWN EVENT. ALSO FOLLOWED POWERPLANT ENGINEERING GUIDANCE TO ACCOMPLISH BORESCOPE / INSPECTION FOR INTERNAL DAMAGE. CHECKED NR 1 ENGINES TURBINE EXHAUST AND INLET AREA, NO TROUBLE FOUND PER FIM 71-00 FIG 114. ACCOMPLISHED INSPECTIONS OF CHIP DETECTORS, / SUPPLY AND SCAVENGE FILTERS. NO DEFECTS NOTED. PERFORMED NR 1 ENG HPC 1ST-6TH BSI INPECTION AND CHKED OK BY STK PER AMM 72-00-00. PERFORMED ENGINE IDLE RUN / AND PART POWER RUN SUCCESSFULLY.&NBSP; POWERPLANT ENGINEERING REVIEWED QAR DATA / WITH NO ANOMALIES NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: ACTUATOR — MALFUNCTIONED (CROSS FEED) · airframe 79,197 hrs · 13,380 cycles

FUEL X-FEED 2 STATUS MESSAGE.(<P>FOUND #2 FUEL X-FEED C/B POPPED OUT, C/B RESET AND POPPED AGAIN. REMOVED AND REPLACED #2 FUEL X-FEED ACTUATOR IAW AMM 28-22-01.&NBSP;</P>)

Part: ACTUATOR — MALFUNCTIONED (STEERING) · airframe 76,711 hrs · 12,902 cycles

FLIGHT CREW ABORTED TAKE-OFF DUE TO BODY GEAR STEERING MESSAGE. AIRCRAFT RETURNED TO BLOCKS.&NBSP;(<P>LH BODY GEAR RH STEERING ACTUATOR CHECKED IN LOCKED IN CMC BUT WAS FOUND TO BE EXTENDED. REMOVED AND REPLACED LH BODY GEAR RH STEERING ACTUATOR PER AMM 32-53-11. VERIFIED LOCK FUNCTION NORMAL.&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (NLG STEERING) · airframe 76,685 hrs · 12,898 cycles

FLIGHT CREW ABORTED TAKE OFF IN ANC DUE TO BODY GEAR STEERING WARNING DURING TAKE OFF ROLL.&NBSP; DURING DEBRIEF OF CREW THEY ADVISED THAT MESSAGE DISAPPEARED AFTER THE ABORT.&NBSP; THEY CONTINUED WITH A SUCCESSFUL TAKEOFF WHEN MESSAGE RE-APPEARED SHORTLY AFTER.&NBSP; FLIGHT CREW INFORMED THAT IT WAS A LOW SPEED ABORT AT APPROX. 40 KTS WITH ALL BRAKE TEMP INDICATIONS NORMAL. PLACED ITEM ON DEFERRAL UPON ARRIVAL.

Part: EXTINGUISHER — LEAKING (UPPER DECK) · airframe 70,127 hrs · 11,668 cycles

UPPER DECK WATER FIRE EXTINGUISHER LEAKING. REMOVED AND REPLACED THE WATER FIRE EXTINGUISHER IAW AMM 26-26-02.

Part: DEPRESSOR — TORN (CARGO DOOR) · airframe 69,966 hrs · 11,640 cycles

FOUND LOWER AFT CARGO DOOR DEPRESSOR SEAL TORN LEFT SIDE OF DOOR CUT OUT 10OCLOCK POS. PERFORMED TIME LIMITED REPAIR IAW SRM 53-00-15-2.

Part: ESCAPE REEL — DAMAGED (COCKPIT) · airframe 67,921 hrs · 11,238 cycles

COCKPIT DESCENT DEVICE NR 8, CABLE DAMAGED AND EXTENDED. REMOVED AND REPLACED THE DESCENT DEVICE IAW AMM 25-61-01.

Part: UNKNOWN — ODOR · airframe 67,134 hrs · 11,111 cycles

DURING APPROACH, SMELL OF SMOKE AND LOW HUMMING SOUND NOTED. TURNED OFF PACK 1 AND CONDITION CEASED. FOUND CMC MSG 21189. T/S SUSPECT PACK 1 ACM AT FAULT. DEFERRAL AS PER MEL 21-51-01-02. DUE TO PACK 1 INOP FWD CARGO REMAINS EMPTY PER MEL 26-16-01-02-01B.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 66,588 hrs · 11,008 cycles

ABORTED TAKEOFF LOW SPEED 70 KNOTS DUE TO EICAS MESSAGE ELECTRIC DRIVE 3. TRANSFER TO MDDR 68827 IAW MEL 24-11-01A, CAT B.

Part: SKIN — DAMAGED (LT MLG DOOR) · airframe 65,707 hrs · 10,854 cycles

LEFT BLG INBD STRUT DOOR EXTERIOR SKIN HAS A SCRATCH MARK. LT BLG INBD STRUT DOOR SKIN IS REPAIRED AT BS 1416.5 AREA IAW SRM 52-80-01-2R-1, REPAIR 1, FIG 201.

Part: ATTACH FITTING — CRACKED (VERTICAL TO FUSE) · airframe 65,707 hrs · 10,854 cycles

UPPER LOBE DOUBLER AT THE FUSELAGE AND VERTICAL STABILIZER ATTACH FITTING RT RADIUS UPPER LOBE DOUBLER FOUND CRACK APPROXIMATELY 80MM LONGERON STABILIZER 2403-2524. RT UPPER LOBE DOUBLER AT THE FUSELAGE AND VERTICAL STABILIZER ATTACH FITTING AREA IS REPAIRED IAW GO NO 4453A224-CS, PART 2, REV 4. POST MONITORING INSPECTION IS REQUIRED AS PER GO NO 4453A224-CS, PART 3, REV 4.

Part: SUPPORT — CRACKED (HORIZONTAL STAB) · airframe 65,707 hrs · 10,854 cycles

LEFT HORIZAONTAL STABILIZER OTBD FAIRING AFT PANEL SUPPORT CRACK. LT HORIZONTAL STABILIZER OTBD TIP FAIRING AFT T/E CHANNEL IS REPAIRED IAW HX RE NR R1-55-10-11322, REV A.

Part: MANIFOLD — CHAFED (NR 4 NACELLE) · airframe 657,707 hrs · 10,854 cycles

NR 4 ENGINE, RT CORE COWL AIR COOLING MANIFOLD DEEP CHAFING. NR 4 ENGINE RT CORE COWL AIR COOLING MANIFOLD, PRE-COOLER EXIT DUCT FLANGE REPAIRED IAW ROHR SB TBC 80C2-NAC-71-032.

Part: FITTING — CRACKED (BS 1480-1540) · airframe 65,707 hrs · 10,854 cycles

FS 1480 TO 1540, STR R32 TO R33 CRACK WAS FOUND AT RT LONGERON EXTENSION FITTING CRACK LENGTH .5" APPROXIMATELY AT RADIUS AREA. FS 1480 TO 1540, STR R32 TO R33, RT LONGERON EXTENSION FITTING IS REPAIRED IAW EO NR 4453A818, PART 3, REV 12, POST MODIFICATION INSPECTION IS REQUIRED IAW EO NR 445A818, REV 12, PART 6.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 65,707 hrs · 10,854 cycles

M/D EMERGENCY LIGHT BATTERY PACK CAPACITY CHECK FAILED, LESS THAN 15 MINUTES, POWER PACK REPLACED IAW AMM 33-51-04.

Part: CHANNEL — CRACKED (BS 720) · airframe 65,707 hrs · 10,854 cycles

M/D BS 720 RT SIDE TENSION TIE END OF OTBD CHANNEL CORNER FOUND CRACK. M/DECK, BS 720 RT SIDE TENSION TIE CHANNEL ARE REPAIRED IAW SRM 53-20-30-2R-1, REPAIR 1. SUP: INSPECTION IS REQUIRED IAW SRM 53-20-30-2R-1, REPAIR 1 TABLE NR 3.

Part: ACCESS PANEL — DAMAGED (NR 1 NACELLE) · airframe 65,707 hrs · 10,854 cycles

NR 1 PYLON 452EL ACCESS PANEL, PYLON V/V, LOWER AFT CORNER FASTENER HOLE ELONGATED. NR 1 PYLON 452EL ACCESS PANEL, PYLON V/V, LOWER AFT CORNER HOLE IS REPAIRED IAW HX R1 NR R1-54-00-11338, REV A.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 65,707 hrs · 10,854 cycles

U/D MERGENCY LIGHT BATTERY PACK CAPACITY CHECK FAILED, LESS THAN 15 MINUTES,POWER PACK REPLACED IAW AMM33-51-04.

Part: PANEL — DAMAGED (NR 2 NACELLE) · airframe 65,707 hrs · 10,854 cycles

NR 2 PYLON V/V PANEL 462ER FASTENER HOLE ELONGATED. NR 2 PYLON V/V PANEL 462ER IS REPAIRED IAW HX R1 R1-54-00-11339, REV A.

Part: CHANNEL — CRACKED (BS 720) · airframe 65,707 hrs · 10,854 cycles

M/DECK BS 720 LT SIDE TENSION, THE END OF OTBD CHANNEL CORNER FOUND CRACK. M/DECK BS 720 LT SIDE TENSION THE CHANNELS ARE REPAIRED IAW SRM 53-20-30-2R-1, REPAIR 1. SUP: INSPECTION IS REQUIRED IAW SRM 53-20-30-2R-1, REPAIR 1, TABLE 203.

Part: FLOORBEAM — CRACKED (BS 1900) · airframe 65,707 hrs · 10,854 cycles

AFT CARGO BS 1900, LBL 41, FLOOR STRUCTURE FOUND CRACK. AFT CARGO COMPARTMENT BS 1900, LBL 39 TO LT OTBD FLOORBEAM UPPER CAP IS REPAIRED IAW SRM 53-60-07-2R, REPAIR 6 FIG 201, DETAIL I. ADJACENT INTERCOSTAL IS REPAIRED IAW SRM 51-70-12-06-0.

Part: DUCT — CHAFED (NR 1 ENGINE) · airframe 65,707 hrs · 10,854 cycles

NR 1 ENGINE RT CORE COWL AIR COOLING DUCT INTERNAL EDGE AREA FOUND DEEP CHAFING. NR 1 ENGINE, RT CORE COWL AIR COOLING DUCT INTERNAL EDGE, PRE-COOLER EXIT DUCT. REPAIRED IAW ROHR SB TBC 80C2-NAC-71-032.

Part: SKIN — CORRODED (LT WING TE FLAP) · airframe 65,707 hrs · 10,854 cycles

LT WING OTBD T/E MID FLAP T/E TOP PANEL FOUND CORROSION. LT WING OTBD MID FLAP T/E THE TOP PANEL SUPT AT OTBD AREA CORROSION IS REMOVED. PROTECTED IAW SRM 51-10-02 & 51-20-01 WITHIN SRM 57-53-02-1A-1 ALLOWABLE DAMAGE 1, FIG 101, LIMITATION. BLEND OUT AREA 2" X 1" X O-010" ORG 0.125". 1/3 T/E AREA CORROSION, R & R IAW HXR1NOR1-57-58-11321, REV A.

Part: FLOORBEAM — CRACKED (BS 1840) · airframe 65,707 hrs · 10,854 cycles

AFT CARGO COMPT RT BS 1840, RBL 1 FLOOR SUPPORT BEAM FOUND CRACK. AFT CARGO COMPARTMENT BS 1840, RBL 0 TO RBL 4 FLOORBEAM UPPER CAP IS REPAIRED IAW HX R1, NO R1-53-25-11337, REV A REPEAT INSPECTION IS REQUIRED IAW RT R1 NR R1-53-25-11337, REV A REPEAT INSPECTION IS REQUIERED IAW HX R1 NT R1-53-25-11337, REV A, SHEET 3.

Part: FITTING — CRACKED (BS 1480-1540) · airframe 65,707 hrs · 10,854 cycles

FS 1480 TO 1540, STR L32 TO L33 CRACK WAS FOUND AT LT LONGERON EXTENSION FITTING CRACK LENGTH .3750" APPROXIMATELY AT RADIUS AREA. FS 1480 TO 1540, STR L32 TO L33 LT LONGERON EXTENSION FITTING IS REPAIRED IAW EO NR 4453A818, PART 3, REV 12, POST MODIFICATION INSPECTION IS REQUIRED IAW EO NO 4453A818, REV 12, PART 5.

Part: SENSOR — SHORTED (PROBE HEAT) · airframe 65,309 hrs · 10,788 cycles

HEATER RT TAT, FIM TASK 30-31, TASK 810. T/S FOUND RT TAT SENSOR HEATER INTERNALLY SHORTED TO GROUND. THE SENSOR WAS REPLACED IAW AMM 30-31-00 AND TEST PASSED AND MESSAGE CLEARED.

Part: BRAKE ASSY — FIRE (MLG) · airframe 64,004 hrs · 10,550 cycles

BRAKE/GREASE FIRE MOMENTARILY AFTER BLOCK IN. HOT BRAKE INSPECTION ACCOMPLISHED ON NR 9, NR 10, NR 11 BRAKES IAW MM 5-51-26. NO DEFECTS NOTED. AS PRECAUTION, REPLACED NR 9, NR 10, AND NR 11 TIRES AND NR 9 AND NR 10 BRAKES.

Part: WARNING MESSAGE — ILLUMINATED (THRUST REVERSER) · airframe 63,111 hrs · 10,411 cycles

TAKEOFF ROLL, EICAS MESSAGE FOR NR 4 ENG THRUST REVERSER. REJECTED TAKEOFF AND RETURNED TO BLOCKS,

Part: FIRE WARNING — FALSE ACTIVATION (CARGO BAY) · airframe 62,918 hrs · 10,376 cycles

MAIN DECK FIRE WARNING. QRH PROCEDURE AND ALL CHECK LISTS ACCOMPLISHED. PERFORMED EMERGENCY RETURN. AIRCRAFT LANDED NORMALLY. VISUAL INSPECTION OF MAIN DECK CARGO COMPARTMENT. NO EVIDENCE OF FIRE & SMOKE. AS PRECAUTION, REPLACED NR 8 LOOP A AND B SMOKE DETECTORS IAW AMM 26-14-01 AND AFOLTS WARNING CARD IAW AMM 26-10-01. ALL SYSTEMS OPERATE NORMALLY.

Part: ADC — MALFUNCTIONED (RIGHT) · airframe 62,742 hrs · 10,323 cycles

FLIGHT DIRECTORS ON BOTH SIDES FAILED DURING TAKEOFF AT 200 FT AGL. CYCLED BOTH SWITCHES AND FDS REGAINED OPERATION. FOUND CMC MESSAGE 22877 AND FOLLOWED FIM TASK 22-11, TASK C52. AIR DATA COMPUTER RT REPLACED IAW AMM 34-12-01/401 AND OPS CHECKED GOOD IAW AMM 22-10-00-715-071.

Part: TIRE — FAILED (NR 9) · airframe 62,232 hrs · 10,241 cycles

AFTER LANDING, FOUND NR 9 TIRE MAIN WHEEL TIRE BURST, R & R NR 9 WHEEL ASSY IAW MM 32-45-01, ALSO PERFORMED A CHAPTER 5 INSPECTION ON LOG PAGE 692768, ITEM 7 IAW MM 05-51-34.

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 60,940 hrs · 10,050 cycles

NR 2 ENGINE VIBRATION AT 5.0 DESCENDING THROUGH FL200. VIBE COULD BE FELT AND INCREASED WITH ENGINE POWER. LEVELING AT 16000' AND AS POWER CAME UP HEARD WHAT SOUNDED LIKE 2 ENGINE COMPRESSOR STALLS. ALL INDICATIONS NORMAL EXCEPT FOR NR 2 ENGINE VIBRATION 5.0 AT ALL SETTINGS. ACCOMPLISHED STALL, INSPECTION IAW AMM 72-00-00-206-050-J00. METAL FOUND IN TAIL PIPE AND ON MASTER CHIP DETECTOR. BORESCOPE OF HPC ACCOMPLISHED IAW AMM 72-00-00-206-001-J00 AND FOUND DAMAGE TO THE 1ST, 6TH, 7TH AND 12TH STAGES. AIRCRAFT AOG AND CURRENTLY ARRANGING ENGINE CHANGE FOR CURRENT GROUND TIME.

Part: BEARING — MIGRATED (ELEVATOR) · airframe 59,142 hrs · 9,725 cycles

AUTOPILOT OSCILLATES AT 1500 FT, COUPLED APPROACH DISCONNECTED. GROUND TEST ELEVATOR SERVO PASS AND AUTOLAND & UNIQUE TEST PASS IAW AMM 22-10-00/501. ON INSPECTION IAW FIM 22-10, TASK 843, FOUND RT BEARING OF ELEVATOR CONTROL ROD AT AFT QUADRANT MIGRATED. REPLACED BEARING IAW AMM 27-31-00/001 AND OPS CHECKED OK IAW AMM.

Part: FAN — FAILED (E/E BAY) · airframe 57,878 hrs · 9,495 cycles

E & E COOLING SUPPLY FAN MESSAGE WITH ASSOCIATED ELECTRICAL ODOR. REPLACED FAN AND SYSTEM TESTED NORMAL IAW AMM 21-58-06.

Part: FLOORBEAM — CRACKED (BS 1200) · airframe 57,814 hrs · 9,484 cycles

CABIN BS 1200, LBL 98 TO 127 FLOORBEAM WEB FOUND CRACKED. REPAIRED IAW RI-53-41-10487.

Part: DOOR — DAMAGED (LT MLG) · airframe 57,814 hrs · 9,484 cycles

LT MLG SHOCK STRUT INBD DOOR PANEL, HAS ELONGATED HOLES AND DAMAGED. REPAIRED IAW RI-52-80-10486, REV A.

Part: SKIN — CRACKED (BS 983) · airframe 57,814 hrs · 9,484 cycles

BS 983, STR 38L, AT DRAG SPLICE FITTING AREA FOUND ONE FASTENER HOLE, FOUND A CRACK IN SKIN. SKIN REPAIRED IAW SRM 53-20-01-2R2 REPAIR 2, FIG 201.

Part: ACTUATOR — DAMAGED (MLG) · airframe 56,634 hrs · 9,307 cycles

GEAR MONITOR STATUS MESSAGE. DURING INSPECTION OF MAIN GEAR, MAINTENANCE FOUND THAT THE RT WING GEAR POSITION ACTUATOR ROD END REMOVED FROM SHAFT. R & R RT WING GEAR POSITIONING ACTUATOR IAW AMM 32-11-20. LEAK CHECK GOOD. INSPECTED WING GEAR AND TRUCK AND NO FURTHER DAMAGE NOTED IAW 32-11-00.

Part: NOZZLE — CRACKED (NR 2 ENGINE) · airframe 53,613 hrs · 8,827 cycles

DURING WALKAROUND MAINTENANCE FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, CRACK IS LOCATED AT THE 11 O'CLOCK POSITION ON THE NR 2 ENGINE. THE CRACK IS APPROXIMATELY 10" LONG. AS PER SRM 54-41-30 THE LENGTH OF THE CRACK IS OUT OF LIMITS. DISPOSITION IS TO STOP DRILL THE ENDS OF THE CRACK WITH A 0.125" DIAMETER HOLE, DVI EVERY 3 FLIGHT CYCLES; AND REMOVAL OF THE PART WITHIN 50 FLIGHT CYCLES.

Part: WEB — CRACKED (MLG DOOR) · airframe 52,783 hrs · 8,681 cycles

A CRACK WAS FOUND &NBSP;ON RIGHT BODY GEAR &NBSP; INBOARD AFT DOOR- AFT EDGE CLOSEOUT BEAM WEB. THE SRM 52-80-02 FIGURE 101 DETAIL IV - ALLOWABLE DAMAGE 3 DOESN'T ALLOW FOR A CRACK ON INBOARD AFT DOOR- AFT EDGE CLOSEOUT RIB WEB &NBSP;EO 4452A173 FAA 8110-3 DATED 07JAN13&NBSP; ALLOWS FOR A TIME LIMITED REPAIR &NBSP; IAW SRM 52-80-02-1A-3 FIGURE 101 DETAIL XI.&NBSP.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 51,649 hrs · 8,495 cycles

DAMAGE TO LOWER FORWARD CARGO COMPARTMENT SEAT TRACK AT BS 560, LBL 24.75. THE DAMAGE EXCEEDS THE ALLOWABLE DAMAGE LIMITS AS PER SRM 53-00-53-1A-1. PERFORMED A TIME LIMITED REPAIR AS DESCIBED IN PART 1 OF EO 4453A780 FAA 8110-3 DATED 06 OCT 12.

Part: PDU — FAILED (COCKPIT) · airframe 51,162 hrs · 8,418 cycles

PDU 19L1 HOT AND SMOKING. REMOVED PDU. PDU REPLACED IAW AMM 25-57-01. SYSTEM OPS CHECKED GOOD.

Part: STRUCTURE — DAMAGED (BS 1780) · airframe 51,103 hrs · 8,410 cycles

DAMAGE FOUND TO MDSCD AREA - BS 1780 SIDEWALL TRIM GUTTER DEFORMED AND MOUNT FASTENERS MISSING, DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 OF EO 4425A315 AND FAA 8110-3 DATED 24AUG12 WORK INSTRUCTIONS. REPETITIVE DVIS REQUIRED AND NBSP;AT EVERY 1 FC AND PERMANENT REPAIR PRIOR TO THE ACCUMULATION OF 1,000 FH AFTER PART 1.

Part: RELIEF VALVE — FAULTY (FUEL SYSTEM) · airframe 49,344 hrs · 8,895 cycles

NRT TOWER OBSERVED FLUID STREAMING FROM UNDER THE RIGHT WING. NO NOTICEABLE REDUCTION IN FUEL, HYDRAULIC OR OIL QUANTITIES. (DURING MAINTENANCE WALK AROUND THE RIGHT INBOARD FUEL PRESSURE RELIEF VALVE WAS FOUND TO BE OPEN SLIGHTLY.&NBSP; REMOVED AND REPLACED THE FUEL PRESSURE RELIEF VALVE PER AMM 28-13-05).

Part: RIB — CRACKED (HORIZ STAB) · airframe 48,961 hrs · 8,026 cycles

CRACK ON RIB OF LT HORIZONTAL STABILIZER LEADING EDGE AT STA 151. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM REPAIR DEVIATION RECORD).

Part: RIB — CRACKED (HORIZ STAB) · airframe 48,961 hrs · 8,026 cycles

CRACK ON RIB OF RT HORIZONTAL STABILIZER LEADING EDGE AT STA 518. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM REPAIR DEVIATION RECORD).

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 48,961 hrs · 8,026 cycles

FORWARD MAIN DECK SEAT TRACK WORN AND CHAFING DAMAGE AT SEVERAL LOCATIONS STA 1680&NBSP;- 1800 RBL 11.33. (PERFORMED PERMANENT REPAIR TO SEAT TRACK PER SRM 53-00-52 REPAIR 12 AND INSTRUCTION CONTAINED IN EO 4453A702 AND BOEING&NBSP; REPAIR AND DEVIATION RECORD (RDR)&NBSP; AND SR &NBSP;1-2117061725).

Part: SKIN — WORN (LT WING) · airframe 48,961 hrs · 8,026 cycles

THREE EA FASTENER HOLES WORN ON LT WING LEADING EDGE SKIN AT ILES 653.39. (PERFORMED INTERNAL FLUSH PERMANENT REPAIR PER INSTRUCTIONS IN EO 4457A406 AND BOEING SR 1-2110443013 AND REPAIR AND DEVIATION RECORD RDR).

Part: SKATE ANGLE — CRACKED (NR 3 PLYON) · airframe 48,961 hrs · 8,026 cycles

CRACK ON SKATE ANGLE OF NR 3 PYLON&NBSP; INBOARD FAIRING AT NACELLE STATION 457. (ACCOMPLISHED TIME LIMITED REPAIR PER EO 4454A142 AND BOEING SR 2112722461 AND REPAIR AND DEVIATION RECORD.&NBSP; PERMANENT REPAIR TO BE ACCOMPLISHED PRIOR TO 24 MONTHS).

Part: RIB — CRACKED (HORIZ STAB) · airframe 48,961 hrs · 8,026 cycles

CRACK ON RIB OF LT HORIZONTAL STABILIZER LEADING EDGE AT STA 484. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM REPAIR DEVIATION RECORD).

Part: RIB — CRACKED (HORIZ STAB) · airframe 48,961 hrs · 8,026 cycles

CRACK ON RIB OF LT HORIZONTAL STABILIZER LEADING EDGE AT STA 145 UPPER SIDE. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM REPAIR DEVIATION RECORD).

Part: RIB — CRACKED (HORIZ STAB) · airframe 48,961 hrs · 8,026 cycles

CRACK ON RIB OF LT HORIZONTAL STABILIZER LEADING EDGE AT STA 151 UPPER SIDE. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM RDR).

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,961 hrs · 8,026 cycles

CRACK ON THE FUSELAGE FRAME OF MAIN DECK CARGO COMPARTMENT AT STA 1900, S-12R - S-13R. (PERFORMED REPAIR PER EO 4453A690 WHICH REFERS TO VENDOR ENGINEERING INSTRUCTIONS AND APPROVAL PER BOEING SR SR 1-2110434060 AND FAA 8100-9 FORM).

Part: RIB — CRACKED (HORIZ STAB) · airframe 48,961 hrs · 8,026 cycles

CRACK ON RIB OF LT HORIZONTAL STABILIZER LEADING EDGE AT STA 159. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM RDR).

Part: RIB — CRACKED (HORIZ STAB) · airframe 48,961 hrs · 8,026 cycles

CRACK ON RIB OF LT HORIZONTAL STABILIZER LEADING EDGE AT STA 145, LOWER SIDE. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM REPAIR DEVIATION RECORD).

Part: RIB — CRACKED (HORIZ STAB) · airframe 48,961 hrs · 8,026 cycles

CRACK ON RIB OF RT HORIZONTAL STABILIZER LEADING EDGE AT STA 510. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM REPAIR DEVIATION RECORD).

Part: RIB — CRACKED (HORIZ STAB) · airframe 48,961 hrs · 8,026 cycles

CRACK ON RIB OF LT HORIZONTAL STABILIZER LEADING EDGE AT STA 131. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM REPAIR DEVIATION RECORD).

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 48,961 hrs · 8,026 cycles

CRACK ON THE INTERCOSTAL OF FLOOR STRUCTURE AT STATION 990.5 RBL 99.08 AND WL 200. (PERFORMED PERMANENT REPAIR PER INSTRUCTIONS IN EO 4453A700 AND BOEING SR&NBSP;1-2111730438 AND REPAIR DEVIATION RECORD).

Part: SKIN — DENTED (FUSELAGE) · airframe 48,691 hrs · 8,026 cycles

REPAIR DENT ON LT FUSELAGE SKIN AT STA 710, S-29L & NBSP. DENT MEASURES 8.0" X 1.5" AND IS .210" DEEP. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4453A321 WITH APPROVAL PER 8100-9).

Part: SKIN — NICKED (FUSELAGE) · airframe 48,961 hrs · 8,026 cycles

FOUND SKIN NICK/DAMAGE 1.8" X 2.1" AT STA 2592, S-38R TO S-42R NEAR AFT JACK POINT AREA. (REPAIRED PER&NBSP; EO 4453A699&NBSP;APPROVED BY 8100-9).

Part: RIB — CRACKED (HORIZ STAB) · airframe 48,961 hrs · 8,026 cycles

CRACK ON RIB OF RT HORIZONTAL STABILIZER LEADING EDGE AT STA 501. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM REPAIR DEVIATION RECORD).

Part: WINGLET — DAMAGED (RT WING) · airframe 48,961 hrs · 8,026 cycles

EVIDENCE OF LIGHTNING STRIKE FOUND ON THE UPPER TIP T/E OF RT WINGLET. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4457A405).

Part: SKIN — DENTED (FUSELAGE) · airframe 48,961 hrs · 8,026 cycles

FOUND SKIN DENT AT STA 732, S41L TO S42L &NBSP. (PERMANENT REPAIR ACCOMPLISHED PER EO 4453A706).

Part: SKIN — CRACKED (NR 4 COWLING) · airframe 47,355 hrs · 7,732 cycles

NR 4 ENGINE RT CORE COWL OUTER SKIN HAS A 1 INCH CRACK UNDER PRE-COOLER EXHAUST DUCT. RT CORE COWL OUTER SKIN STOP DRILLED AS PER EO 4471A007 (FAA FORM 8110-3 DATED 08 SEPTEMBER 2011 ISSUED) WITH DVI AT EVERY CYCLE. PERMANENT REPAIR TO BE ACCOMPLISHED &NBSP; WITHIN 20 CYCLES &NBSP).

Part: FAN — MALFUNCTIONED (COCKPIT) · airframe 47,111 hrs · 7,689 cycles

PRIOR TO DEPARTURE, BURNING SMELL REPORTED BY FLIGHT CREW. FOUND EQUIPMENT EXHAUST FAN HOT AND SMELLING BURNT. INSPECTED FAN WITH NO FINDINGS. DEACTIVATED EXHAUST FAN AND DEFERRED ITEM WITH MEL 21-58-4.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 47,111 hrs · 7,689 cycles

PRIOR TO DEPARTURE, BURNING SMELL REPORTED BY FLT CREW. FOUND EQUIP EXHAUST FAN HOT AND SMELLING BURNT. INSPECTED FAN WITH NO FINDINGS. DEACTIVATED EXHAUST FAN AND DEFFERED ITEM WITH MEL 21-58-4.

Part: CDU — MALFUNCTIONED (COCKPIT) · airframe 46,682 hrs · 7,608 cycles

DURING PRE-FLIGHT ELECTRICAL SMELL/SMOKE APPEARED IN FLIGHT DECK AREA. CHECKED E/E COMPARTMENT, FLIGHT DECK, MAIN DECK-FOUND CAPTAINS CDU HAS A STRONG ELECTRICAL SMELL.&NBSP;&NBSP. REMOVED AND REPLACED CDU AS PER AMM 34-61-02/401.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 46,213 hrs · 7,642 cycles

REJECTED TAKEOFF DUE TO OPEN DOOR INDICATION. (ACCOMPLISHED CONDITIONAL INSPECTION AS PER AMM&NBSP;05-51-10 INSPECTION FOR "HIGH ENERGY STOP". AFTER RETURN TO GATE AREA 16 TIRES&NBSP; RELEASED THEIR THERMAL FUSES AND AFTER FURTHER INSPECTION 16&NBSP; BRAKES WERE REPLACED DUE TO HEAT DAMAGE.

Part: DOOR — DELAMINATED (RT WING MLG) · airframe 42,096 hrs · 6,883 cycles

RT WING LANDING GEAR FIXED LOWER STRUT DOOR DELAMINATED. PART ONE TIME LIMITED REPAIR ACCOMPLISHED PER ENGINEERING ORDER 4452A082, WITH FAA 8110-3 DATED 18 JULY 2010. DVI EVERY 15 FLIGHT CYCLES WITH PERMANENT REPAIR PRIOR TO 1000 FLIGHT HOURS AFTER PART ONE WAS ACCOMPLISHED.

Part: WEDGE — DAMAGED (TE FLAP) · airframe 41,104 hrs · 6,737 cycles

FOUND LEFT I/B AFT FLAP T/E WEDGE WITH TEAR / GROUND DAMAGE WITH A DIMENSION OF 7 X 11 X 1.5 INCHES. FLAP TIME LIMITED REPAIR PER EO 4457A248 WITH FAA 8110-3 DATED 07 MAY 2010. INSTALLED EXTERNAL DOUBLER WITH REPEAT INSPECTION AT EVERY 10 FC AND PERMANENT REPAIR AT NEXT A-CHECK PER SRM 51-70-07 AND SRM 57-53-01.

Part: ROLLER — DAMAGED (FO SEAT) · airframe 40,914 hrs · 6,709 cycles

FIRST OFFICER SEAT, LEFT FORWARD TRACK ROLLER ASSEMBLY DAMAGED. ACCOMPLISHED ENGINEERING ORDER 4425A155, WITH FAA 8110-3 DATED 25 APR 2010 PART 1, TIME-LIMITED REPAIR TO INSTALL TEMP BOLT. DVI REQUIRED AT EVERY FLIGHT CYCLE AND PERMANENT REPAIR PRIOR TO 10 FLIGHT CYCLES AFTER PART 1 IS DONE.

Part: SKIN — DENTED (CARGO DOOR) · airframe 40,805 hrs · 6,694 cycles

LOWER AFT CARGO DOOR LOWER AFT CORNER SKIN DENT REPAIR AT BS 1920. DURING C-CHECK AT TPE ACCOMPLISHED PART 2 INTERIM REPAIR IAW ENGINEERING ORDER 44452A072 REV A.

Part: WINGLET — DAMAGED (LT WING) · airframe 40,426 hrs · 6,638 cycles

DURING PARKING OPERATION THE LEFT WINGLET MADE CONTACT WITH THE LEFT WINGLET OF AIRCRAFT N450PA. THE LEFT WINGLET WAS REMOVED IAW CDL 57-28-1 AND AMM 57-28-01. NO FURTHER DAMAGE WAS NOTED.

Part: NOZZLE — CRACKED (NR 3 ENGINE) · airframe 40,244 hrs · 6,610 cycles

ENGINE 3 EXHAUST NOZZLE HAS A CRACK AT THE 12 O'CLOCK POSITION APPROXIMATELY 24 INCHES LONG RUNNING FROM 10 O'CLOCK TO 1 O'CLOCK POSITION, 13 INCHES FROM EDGE OF NOZZLE. TIME LIMITED REPAIR ACCOMPLISHED IAW EO 4478A121 AND FAA 8110-3 DATED 25 FEB 2010. DVI REQUIRED EVERY 3 FLIGHT CYCLES WITH PERMANENT REPAIR TO BE ACCOMPLISHED AT NEXT A-CHECK.

Part: NOZZLE — CRACKED (NR 2 EXHAUST) · airframe 39,750 hrs · 6,534 cycles

NUMBER TWO EXHAUST NOZZLE HAS A CRACK. ENGINEERING ORDER 4478A115 & FAA 8110-3 DATED 19 JAN 2010. ACCOMPLISHED TO STOP DRILL CRACK AS INTERIM REPAIR & DVI EVERY 3 FLIGHT CYCLES. NOZZLE MUST BE REPLACED BEFORE NEXT A-CHECK.

Part: SLEEVE — CRACKED (NR 2 ENGINE) · airframe 37,975 hrs · 6,268 cycles

CRACK FOUND ON NR 2 ENGINE EXHAUST SLEEVE FROM 12 O'CLOCK TO THE 1 O'CLOCK POSITION. NO OTHER DAMAGE FOUND. INTERIM REPAIR ACCOMPLISHED IAW EO 4478A097/FAA 8110-3 DATED 29 AUG09. DETAIL VISUAL INSPECTION DUE EVERY 3 FLIGHT CYCLES AND PERMANENT REPAIR DUE AT NEXT A-CHECK.

Part: STRUCTURE — DENTED (WING) · airframe 37,031 hrs · 6,126 cycles

ON WALK AROUND CHECK, FOUND NR 26 VARIABLE CHAMBER FLAP FOLDING NOSE HAS A DENT 3 INCH BY 1/3 INCH WITH A DEPTH OF 1/4 INCH. TIME LIMITED REPAIR ACCOMPLISHED PER EO 4457A194 PART 1. SEALANT AND ALUMINUM FOIL TAPE APPLIED.

Part: CHILLER — DEFECTIVE (GALLEY) · airframe 35,747 hrs · 5,954 cycles

GALLEY CHILLER MOTOR MAKES GRINDING SOUND AND COMPARTMENT HAS BURNED ELECTRICAL ODOR. REPLACED CHILLER.

Part: FMC — UNSERVICEABLE (RIGHT) · airframe 34,975 hrs · 5,842 cycles

DURING PUSHBACK RIGHT FMC FAILED. "FMC WAS REPLACED AND AIRCRAFT DEPARTED NO FURTHER ISSUES."

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 34,962 hrs · 5,840 cycles

L/E SINGLE DRIVE FLAPS PRIMARY MESSAGE ON FLAP EXTENSION. LEADING EDGE HAD A DELAYED EXTENSION. "PERFORMED GROUND OPERATIONAL CHECK OF THE FLAPS IAW MM 27-81-00. FOUND SYSTEM OPERATES NORMALLY. THE MESSAGE CLEARED AND AIRCRAFT DEPARTED."

Part: CONNECTOR — UNSECURE (NR 2 ENGINE) · airframe 34,832 hrs · 5,820 cycles

RWY 07L HKG REJECTED T/O AT 80 KTS DUE TO NR 2 ENGINE FAILURE TO DEVELOP T/O THRUST SUBSEQUENT RUN-UP ON TAXIWAY MAX N1 68 PERCENT, RETURN TO BLOCKS. ENGINE 2 THRUST REVERSER RIGGING AND READING CHECK CARRIED OUT IAW AMM78-31-00-825-001-J00. RVDT CONNECTOR SECURITY CHECK OK. ENG 2 EEC ALL CONNECTORS RESECURED ENG 2 GROUND RUN AND THROTTLE RESPONSE UP TO 80 PERCENT N1 NORMAL.

Part: SHUTOFF VALVE — DEFECTIVE (NR 1 ENGINE) · airframe 33,989 hrs · 5,684 cycles

NR 1 ENGINE AUTO START FAILED. TROUBLESHOT AND FOUND NR 1 PRSOV DEFECTIVE AMM36-11-04. (K)

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 32,512 hrs · 5,461 cycles

DURING MAINTENANCE, THE RIGHT INBOARD ELEVATOR'S TRAILING EDGE APPROXIMATELY 5 INCHES FROM INBOARD EDGE OF THE ELEVATOR WAS STRUCK AND DAMAGED BY THE CHERRY PICKER. INSPECTED AREA AND ACCOMPLISHED INTERIM REPAIR IAW EO 4455A025.

Part: GASKET — LEAKING (HYD SYSTEM) · airframe 32,512 hrs · 5,461 cycles

ON CLIMB-OUT OF NRT, NR 3 HYDRAULIC SYSTEM WAS LOST. QUANTITY AND PRESSURE DROPPED TO ZERO. FOUND UPPER RUDDER ACTUATOR LEAKING FROM MATING SURFACE OF PROPORTIONAL VALVE AND ACTUATOR. REPLACED GASKET PLATE. NO LEAKS NOTED.

Part: RELIEF VALVE — WRONG PART · airframe 31,680 hrs · 5,338 cycles

RETURN TO BLOCKS DUE TO "BLD 1 OVHT/PRV" EICAS MESSAGE. FINDING THAT THE INCORRECT PRV VALVE WAS DELIVERED, MAINTENANCE SWAPPED THE NR 3 HPSOV WITH NR 1 PRV AND THEN DEFERRED THE NR 3 HPSOV, PER MM 36-11-00.

Part: CIRCUIT CARD — MALFUNCTIONED (POWER SUPPLY) · airframe 28,797 hrs · 4,910 cycles

MASTER WARNING AND FIRE BELL CONTINUOUSLY DISPLAYED ACTIVATED WITH NO ASSOCIATED EICAS OR STATUS MESSAGES. RESEATED MAWEA CARDS AND SYSTEM BITE TESTED OK PER AMM 31-51-00-715-014 AS PRECAUTIONARY REPLACE MAWEA PWR SUPPLY CARDS PER MM 31-51-01 AND C/W MM 31-52-00; OPS SYSTEM FUNCTION TESTED NO FAULTS NOTED. SYSTEM RETURN TO SVC.

Part: UNKNOWN — UNKNOWN (FIRE DETECTION) · airframe 27,997 hrs · 4,790 cycles

MASTER WARNING AND FIRE BELL INTERMITTENT ON TAXI IN. AFTER ENGINE SHUTDOWN AND APU POWER ONLINE THE PROBLEM CEASED. PERFORMED FIRE WARNING SYSTEM OPERATIONAL CHECKS WITH NO DEFECTS NOTED.

Part: LINE — LEAKING (NR 2 ENGINE) · airframe 27,657 hrs · 4,732 cycles

DURING WALK AROUND, CONTINUOUS FUEL DRIP WAS FOUND COMING OUT OF NR 2 ENGINE FUEL DRAIN. CHECKED AND FOUND NAC 298 STATION 93 PYLON AREA FUEL LINE LEAKING. RETIGHTENED LINE AND PERFORMED GROUND ENGINE RUN-UP CHECK. ALL CHECKS OK PER MM 73-11-06 AND 71-00-00.

Part: O-RING — FAILED (HYD SYSTEM) · airframe 25,796 hrs · 4,425 cycles

AT PUSHBACK, FOUND BODY GEAR (LT) TRUCK POSITION ACTUATOR HYDRAULIC FUSE LEAKING. REPLACED PACKING SET OF HYDRAULIC FUSE PER MM 32-13-24. NO LEAK NOTED.

Part: TUBE — CRACKED (NR 3 ENG OIL) · airframe 24,804 hrs · 4,262 cycles

1.5 HOURS INTO FLIGHT, NR 3 ENGINE OIL DROPPED TO 6 QUARTS. REDUCED THRUST TO IDLE, OIL QUANTITY DROPPED TO 4 QUARTS. SHUTDOWN ENGINE. FOUND CRACKED OIL LINE TO LOW OIL PRESSURE SWITCH. REPLACED SAME MM 70-50-00, 71-00-00.

Part: PDU — FAILED (TE FLAPS) · airframe 23,950 hrs · 4,130 cycles

DURING APPROACH, WHEN FLAPS 5 SELECTED, EICAS MESSAGE -FLAPS PRIMARY- THEN EICAS MESSAGE -FLAP DRIVE-. OBSERVED RT OUTBOARD L/E FLAP STUCK. STATUS MESSAGE -LE MULTIDRIVE-. QRH COMPLIED WITH. REMOVED AND REPLACED RIGHT OUTBOARD L/E POWER DRIVE UNIT PER AMM 27-81-03. OPS CHECK NORMAL.

Part: BLADES — DAMAGED (NR 1 ENGINE) · airframe 23,350 hrs · 4,042 cycles

ON CLIMB PASSING FL250, BANG FROM NR 1 ENGINE ALONG WITH SHUDDER. EGT PEAKED 898 DEGREE C. INDICATION RETURNED TO NEAR NORMAL AFTER EVENT. BOROSCOPED NR 1 ENGINE (SN 706222) STAGE 12 BLADES DAMAGED BEYOND LIMITS. ENGINE CHANGE IN PROGRESS.

Part: SEAL — FAILED (COUPLING) · airframe 22,836 hrs · 3,964 cycles

CREW REPORTED AT TOP OF CLIMB (CRUISE) MULTIPLE EICAS MESSAGES -BLEED DUCT L-. REPLACED SEALS AT FLEX COUPLING AT WBL 450 LEADING EDGE PNEUMATIC DUCT PER MM 36-11-02.

Part: CIRCUIT CARD — FAILED (COOLING SYS) · airframe 22,489 hrs · 3,918 cycles

STATUS MESSAGE EQUIPMENT COOLING CARD FAIL. REMOVED AND REPLACED EQUIPMENT COOLING CONTROL CARD PER AM 21-58-05 AND 20-41-02. OPS CHECK NORMAL, NO FAULTS NOTED.

Part: BLADES — BIRD STRIKE (NR 4 ENGINE) · airframe 22,177 hrs · 3,866 cycles

CREW REPORTED JUST AFTER ROTATION, ENGINE NR 4 INDICATED FAN 5.0 VIBRATION. VIBRATION AUDIBLE AND VARIED WITH THRUST SETTING. PERFORMED BIRD STRIKE INSPECTION PER AMM 05-51-202-001. PERFORMED GAS PATH AND CHIP DETECTOR INSPECTION, NIL RESULTS. CHANGED DAMAGED FAN BLADES, OPERATION NORMAL PER AMM 72-31-02-004.

Part: SKIN — DAMAGED (BS 1857-1902) · airframe 21,995 hrs · 3,836 cycles

GROUND EQUIPMENT DAMAGE TO LT SIDE OF AC AT BST 1857 - BST 1902 AT STRINGER 42L. PERMANENT REPAIR CARRIED OUT IAW SRM 747-400F 53-0001 FIG 201.

Part: TIRE — BLOWN (LANDING GEAR) · airframe 21,392 hrs · 3,746 cycles

AT TOP OF CLIMB, CREW REPORTED LOUD BANG FOLLOWED BY EICAS MESSAGE (GEAR DOOR) WITH AC VIBRATION AND AIR NOISE. ACCOMPLISHED MMC 14-7 CHECKLIST DOOR CLOSED, NO VIBRATION OR NOISE, SUSPECT BLOWN TIRE IN LT BODY GEAR WELL, AUTO BRAKE TEMP SENSOR NR 5 FAIL. SOFT LANDING COMPELETED. PERFORMED CONDITIONAL INSP IAW 5-51-34. TIRE BURST. REMOVED AND REPLACED NR 5 AND NR 6 TIRE ASSY IAW MM 32-45-01. BODY GEAR DOOR SYSTEM OPS NORMAL.

Part: PDU — FAILED (LE FLAPS) · airframe 21,014 hrs · 3,682 cycles

ON APPROACH EICAS MSG FLAPS PRIMARY FOLLOWED BY FLAPS DRIVE MSG. TROUBLESHOT THEN REPLACED NR 3 LT L/E PDU IAW MM 27-81-03.

Part: CIRCUIT CARD — FAILED (FIRE WARNING SYS) · airframe 20,505 hrs · 3,594 cycles

FWD CARGO MASTER FIRE WARNING ON GROUND IN MIA. CHECKLIST COMPLETED. FIRE BOTTLES DISCHARGED. FOUND FIRE WARNING CARD A31 AT FAULT. REMOVED A31 CARD PER MM 26-23-00, OPS NORMAL.

Part: GENERATOR — INOPERATIVE (NR 1) · airframe 19,848 hrs · 3,479 cycles

NR 1 GEN ON APU INOP. "CORRECTIVE ACTION": REPLACED NR 1 GENERATOR. OPS CHECK OK PER MM 24-21-03.

Part: DOOR — DELAMINATED (MLG) · airframe 18,256 hrs · 3,219 cycles

RIGHT WING GEAR DOOR O/B HAS DELAMINATION ON AFT LWR EDGE. DOOR REMOVED AND REPAIR ACCOMPLISHED. REINSTALLED DOOR (SERVICEABLE) PER MM 32-12-07.

Part: VALVE — DIRTY (NR 2) · airframe 17,123 hrs · 30,810 cycles

ENGINE NR 2 FUEL VALVE MSG FUEL SPAR VLV 2 STATUS MSG. REMOVED NR 2 FUEL SPAR VALVE. CLEANED SHAFT AND REINSTALLED SPAR VALVE. OPERATION CHECKS OK PER MM 28-22-01.

Part: LINE — LEAKING (FMU) · airframe 17,038 hrs · 3,012 cycles

RETURNED TO BLOCKS DUE TO NR 3 ENGINE FUEL LEAK FROM DRAIN MASK. FOUND NR 3 ENG FUEL LINE FROM PYLON TO FMU LEAKING AT FMU. RETIGHTENED LINE AT FMU, RUN UP AND LEAK CHECK PER 73-11-10.

Part: MANIFOLD — MALFUNCTIONED (NR 2 ENG FUEL) · airframe 16,055 hrs · 2,844 cycles

NR 2 ENGINE FUEL LEAK. REPLACED LT FUEL MANIFOLD PER AMM 73-11-16, PERFORMED ENGINE RUN PER AMM 71-00-00.

Part: DRAIN MAST — LEAKING (NR 3 ENGINE) · airframe 14,807 hrs · 2,629 cycles

AFTER ENGINE START, NR 3 ENGINE LEAKING FUEL, RETURNED TO THE GATE. FOUND FUEL LEAKING FROM DRAIN MAST, AFTER ENGINE START. SUSPECTED LEAK FROM STRUT DRAIN, DISCONNECTED DRAIN PIPE, WET SPAN ENGINE AT IDLE, STILL NO LEAKS EVIDENT, ENGINE COWL SECURED, OK FOR SERVICE.

Part: ENGINE — LEAKING (NR 3) · airframe 13,180 hrs · 2,342 cycles

WHILE STARTING AT GATE NR 3 ENG LEAKING FUEL OUT OF THE BOTTOM MAST AFTER START. FOUND FUEL SUPPLY LINE CONNECTION AT PYLON WET. LOOSENED, REPOSITIONED AND TIGHTENED AS PER 73-11-10, OPS CHECKED ENG PER MM 72-00-00, NO LEAKS NOTED.

Part: CONNECTOR — DIRTY (START VALVE) · airframe 13,097 hrs · 2,325 cycles

STATUS MESSAGE NR 1 ENG START VALVE, ENGINE START VALVE FAILED TO OPEN NORMALLY. CLEANED NR 1 ENGINE START VALVE CONNECTOR. RESECURED & OPS CHECK OK PER MM 80-11-00 PG 501.

Part: TIRE — DAMAGED (NLG) · airframe 13,047 hrs · 2,316 cycles

RIGHT NOSE TIRE HAS LOOSE TREAD BELT. REPLACED TIRE PER MM 32-45-02, COMPLIED WITH TIRE TREAD LOSS INSPECTION PER MM 05-51-34.

Part: O-RING — DISPLACED (NR 1 ENGINE) · airframe 12,588 hrs · 2,235 cycles

NR 1 ENG HAD LOSS OF OIL QUANTITY. ENG SHUT DOWN & RETURN TO MIA. FOUND GEARBOX CRANKPAD COVER O-RING CUT, 50 PERCENT OF RING DISPLACED. REPLACED SAME, RESERVICED ENG OP'S & LEAK CHECK OK.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 12,439 hrs · 2,211 cycles

NR 4 ENG REVERSER STATUS MESSAGE DISPLAYED AFTER LANDING. TRANSFERRED TO DMI 31988 AND MEL 78-31-01 PER DDPG.

Part: SOLENOID — FAILED (NR 3 ENGINE) · airframe 12,190 hrs · 2,168 cycles

NR 3 ENG FAILED TO START. REMOVED AND REPLACED NR 3 HMM SOLENOID SHUT OFF VLV IAW 73-21-20. ENG RUN-UP AND LEAK CK OK.

Part: FAIRING — DELAMINATED (T/E FLAP) · airframe 4,532 hrs · 782 cycles

NR 7 CANOE ASSY, OUTBOARD SIDE AT MID POINT 2 INCH DELAMINATION. REPAIRED PER SRM 51-40-00.

Part: CASTER — CRACKED (MAIN CARGO BAY) · airframe 4,532 hrs · 782 cycles

RT MAIN DECK BS 1725 CASTER TRAY EXTRUSION CRACKED/DAMAGED. REPAIRED PER SRM 51-70-11 FIG 1 & PER MM 25-57-04.

Part: FLOORBOARD — PUNCTURED (FUSELAGE) · airframe 4,532 hrs · 782 cycles

MAIN DECK L/S FLOOR BOARD PUNCTURE BS 1720 LT SIDE. REPAIRED PER SRM 53-00-50.

Part: CASTER — CRACKED (MAIN CARGO BAY) · airframe 4,532 hrs · 782 cycles

MAIN DECK CASTER ASSY AT BS 1900 R/S CRACKED. REPAIRED PER SRM 51-40-00.

Part: GUIDE — DAMAGED (CARGO BAY) · airframe 4,532 hrs · 782 cycles

AFT CARGO COMPT, STA 1820 SIDE GUIDE RAIL DAMAGED LT/SIDE. REPAIRED PER SRM 51-70-12 & MM 25-33-00.

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 4,532 hrs · 782 cycles

MAIN DECK, STA 1920/2040 LEFT SIDE FLOOR PANEL DAMAGED (PUNCTURES). REMOVED AND REPLACED PER MM 53-00-50.

Part: LOCK — DAMAGED (CARGO BAY) · airframe 4,532 hrs · 782 cycles

FWD CARGO COMPT AT STA 650 LOCK ASSY DAMAGED LEFT SIDE. REMOVED AND REPLACED PER MM 25-56-33.