N476MC

Part: ANGLE — CRACKED (ZONE 100) · airframe 103,250 hrs · 18,818 cycles

FOUND 1 INCH LENGTH CRACK ON RH LONGERON BOX FRAME (PN: 65B15001-80) REPAIRED PER EA 4453A258 PART 1, REQUIRE TO PERFORM REPEAT INSPECTION PER EA 4453A258 PART 2. (14340)(<P>WHEN ACCOMPLISHED REPEAT INSPECTION PER EA 4453A258 PART 2, FOUND CRACK ON CLIP AND REPAIRED CLIP #30 AT STA 1372 WL152 IAW B747-400 SRM 51-70-11-0G-0 FIG 1 AND ENGINEERING MESSAGE EO #4453C602. NO FURTHER DEFECTS NOTED.

Part: SUPPORT FITTING — CRACKED (ZONE 100) · airframe 102,315 hrs · 18,661 cycles

R/H BODY LANDING GEAR WHEEL WELL AREA SUPPORT FITTING CRACK (STA 1372). PERFORMED TIME LIMITED REPAIR PER EA-4453A258 PART 1. NO FURTHER DEFECTS NOTED.

Part: ENGINE — FIRE (NR 1)

N476MC FLT 5Y 8208 AFTER T/O ENGINE # 1 WAS FIRE, SO CREW TAKE THE DECISION TO DIVERT TO GYE. PLS SEE ALSO MSR-14785.

Part: ENGINE — FAILED (NR 1) · airframe 101,396 hrs · 18,505 cycles

ENGINE 1 DUAL FIRE LOOP INDICATION CONFIRMED BY VISUAL OF FLAME COMING FROM INTAKE AND SMOKE OUT EXHAUST AFTER DISCHARGING BOTH FIRE BOTTLES. C/W ENGINE CHANGE PER TASK CARD 71-099-02-01. NO FURTHER DEFECTS NOTED. ORIGINAL SUBMISSION DATE; 6/16/2025.

Part: ENGINE — FIRE (NR 1)

ACFT N476MC FLT 5Y8208 B747C DEPARTED FROM UIO, AFTER DEPART ENG #1 WAS FIRED SO CREW TOOK THE DECISION TO DIVERT TO GYE. ACFT LAND ON GYE, TOWED TO POSITION 13. A RIDING MECHANIC FROM ATLAS IS IN CHARGE OF THE TECHNICAL RELEASE AND WE PROVIDE MECHANIC ASSISTANC

Part: INDICATION SYS — FALSE INDICATION (MAIN TANK) · airframe 100,716 hrs · 18,401 cycles

NO FUEL QTY INDICATION ON MAIN TANK #2.(<P>CONFIRMED NO FUEL LEAKS, DRIP STICK READING ACCOMPLISHED, AND DDG 28-41-01 APPLIED. TRANSFER TO DMI 229181 PER MEL 28-41-01 CAT C DUE DATE 24APR25.</P>)

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 100,695 hrs · 18,396 cycles

MAIN DECK - MAIN DECK FLOOR PANEL SUPPORT MOST O/B AT ABOUT STA 1100-1140 FOUND 2 EA FASTENER HOLE CRACK.(<P>JOB ACCOMPLISHED AS PER EN #3003-25 REV.0. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — CRACKED (ZONE 100) · airframe 100,695 hrs · 18,396 cycles

FUSELAGE - SEC46 SKIN EXTERIOR SURFACE STA1733-1735 S-41R AREA FOUND SKIN CRACKED WITH CORROSION.(<P>JOB ACCOMPLISHED AS PER EN #1023-25 REV.0. FIRST AND SECOND STAGE APPROVAL (APPROVAL FOR STATIC STRENGTH AND INSPECTION THRESHOLD) THE INSPECTION THRESHOLD FOR THIS REPAIR IS PROVIDED BUT FULL COMPLIANCE TO 14 CFR 25.571(B)[25-45] AND 26.43(D) HAS NOT BEEN EVALUATED. NO FURTHER DEFECTS NOTED.

Part: ACM — ODOR (NR 2) · airframe 98,893 hrs · 18,104 cycles

1. DURING APPROACH, LOUD HOWL OR GROAN NOISE FROM BELOW COCKPIT. AFTER LANDING TURNED OFF PACK 2, NOISE STOPPED. 2. PACK 2 EICAS MSG, PACK WILL NOT RESET. 3. TURNING FINAL APPROACH APPROX 3000 FT, BURNING SMELL COMING THROUGH A/C SYSTEM, LESSENED THROUGH LANDING.(<P>CONFIRMED BURNING SMELL FROM PACK 2 PER FIM 21-00 TASK 810 &AMP; AMM 05-51-56. TRANSFER TO DMI 217153 PER MEL 21-51-01-03 CAT C DUE DATE 30SEP24.</P> / <P>LP 1787053 M7: R/R ACM PER AMM 21-51-04. OPS CHECK GOOD. DMI 217153 CLOSED. REF IPC 21-51-04-02 ITEM 35.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 98,771 hrs · 18,087 cycles

DIVERTED, MULTIPLE FLIGHT CONTROL EICAS STATUS MESSAGES(<P>R/R FCE POWER SUPPLY 1R (M7360) IAW AMM 27-09-00 &AMP; AIPC 27-09-04-01A. OPS CHECK GOOD. NIL EXISTING FAULT MSG NOTED. AC-1 DIST C/B STAYED IN SET POSITION.

Part: ELEC CONNECTOR — DIRTY (BLEED INDICATION) · airframe 97,931 hrs · 17,955 cycles

BLEED 3 EICAS MESSAGE(<P>FOUND #2 WIRE ON HPSOV WAS READING 12 MEGA OHMS. REMOVED CANNON PLUG AND CLEANED, RESEATED CANNON PLUG AND FOUND RESISTANCE CHECK TO BE .2 MEGA OHMS WHICH IS NORMAL PER FIM 36-11 TASK 803. NO FURTHER DEFECTS NOTED.</P>)

Part: ACCESS DOOR — DAMAGED (NR 4 NACELLE) · airframe 96,758 hrs · 17,781 cycles

ON POST FLT, FOUND #4 ENG INBD PYLON DAMAGED (SAIL BOAT DOOR)(<P>TEMP REPAIR TO #4 ENG PYLON PANEL COMPLETED PEREA 4454A0080 & SRM 51-70-19-0G-0. SCHEDULED PERMANENT REPAIR UPON AIRCRAFT RETURN TO MIA FROM SCL PRIOR TO THE ACCUMULATION OF 2 F/C AFTER TIME LIMITED REPAIR HAS BEEN ACCOMPLISHED PER EA 4454A0080.

Part: INDICATOR — FALSE INDICATION (CREW OXYGEN) · airframe 96,336 hrs · 17,710 cycles

AIR TURNBACK DUE TO CREW O2 QUANTITY LOW (SUSPECT LEAK)(<P>PERFORMED LEAK CHECK FOR OXY BOTTLES / LINES / ALL MASKS, NO LEAK FOUND. R/R CREW OXYGEN VOLTAGE AVERAGING UNIT AND OPS / IND CHECK GOOD PER AMM 35-41-12.</P>)

Part: NONE — NONE · corrosion level 2 · airframe 7,954,299 hrs · 17,179 cycles

CORROSION ON M/D FLOOR BEAM UPPER CAP NEAR STA 1580 LBL 77 ~ LBL 99(<P>1. ACCOMPLISHED JOB IAW EI NO T2023A53N-170 SEQUENCE A REV0 AND DWG 65B338079 SH9 REV- 2. ACCOMPLISHED FINAL EI NO. T2023A53M-170 REV1 3. CONDITION CHECK NORMAL AND JOB COMPLETED</P>)

Part: NONE — NONE · airframe 93,201 hrs · 17,179 cycles

DEFORM - FOUND FWD CARGO, CARGO TRACK DEFORM NEAR STA 590, RBL 24.75(<P>1. REMOVE THE DAMAGE PARTS IAW SRM 51-40-02 REV96. 2. REPAIR THE DAMAGE AREA IAW EI #T2023A53M-110 REV 2. 3. JOB COMPLETED.</P>)

Part: NONE — NONE · airframe 93,201 hrs · 17,179 cycles

EXISTING UNDOCUMENTED REPAIR DOUBLER ON FUSELAGE SKIN AT STA  1880 BETWEEN S-43L AND S-46L(<P>1. REMOVE EXISTING REPAIR DOUBLER IAW SRM 51-40-02-0G-0 REV96 2. REPAIR SKIN IAW EI NO: T2023A53M-494 REV1 3. ACCOMPLISHED THE REPAIR AREA IAW EI NO: T2023A53M-494 REV2 4. JOB COMPLETED</P>)

Part: NONE — NONE · airframe 93,201 hrs · 17,179 cycles

FND M/D CGO SEAT TRACK CRACK AT STA 940-960 RBL 75.92(<P>1. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 96 2. REPAIRED DAMAGE AREA IAW SRM 53-00-52-2R-13 REPAIR 13 FIG 201 REV 96 3. INSTALLED NEW PARTS IAW SRM 51-40-02-0G-0 REV 96 AND DWG NO: 65B16004 SH4 REV-A AND 65B38250 SH 17 REV A. 65B38754 SH9 REV B AND 65B38250 SH20 REV - 4. CONDITION CHECK NORMAL AND JOB COMPLETED</P>)

Part: FITTING — NONE · airframe 93,201 hrs · 17,179 cycles

CRACK ON FRONT SPAR INTERCOSTAL LUG FITTING AT STA 1000 LBL 11.33(<P>1. REMOVED DAMAGE PARTS IAW SRM 51-40-02-0G-0 REV 96. 2. INSTALL NEW PARTS IAW SRM 51-40-02-0G-0 REV 96 AND EO 4453C024 REV 3 AND EI T2023A53M-134 SEQUENCE B. 3. ACCOMPLISHED EI T2023A53M-134 REV 2. 4. ORIGINAL EI ATTACHING WITH WO 7939908 (162). 5. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: NONE — NONE · corrosion level 2 · airframe 93,201 hrs · 17,179 cycles

CORROSION - FOUND CORROSION ON SKIN INNER SURFACE TOTAL 26EA WHEN PERFORM SB 747-53A2898(<P>1. REMOVED THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV96 2. PERFORMED EI NO T2023A53-135 REV0 3. PERFORMED EI NO T2023A53M-135 REV 1 4. PERFORMED EI NO. T2023A53M-135 REV2 5. PERFORMED EI NO T2023A53M-135 REV3 6. PERFORMED EI NO T2023A53M-135 REV4 7. ACCOMPLISHED EI NO. T2023A53M-135 REV5 8. JOB COMPLETED AND COND CHK NML</P>)

Part: NONE — NONE · corrosion level 2 · airframe 93,201 hrs · 17,179 cycles

CORROSION - FOUND MAIN DECK SEAT TRACK CORROSION AT STA 1928 RBL 98.58(<P>1. REMOVED THE AFFECTED FASTERNER I.A.W SRM 51-40-02 REV-96 2. REPAIRED DAMAGE AREA I.A.W EI NO. T2023A53M-147 SEQUENCE A REV 0. 3. INSTALLED FASTENERS I.A.W SRM 51-40-02 REV9 AND DWG 65B38251 SH 62 REV A AND 65B38251 SH 66 REV- AND 65B38251 SH 67 REV A&NBSP; 4. ACCOMPLISHED EI NO. T2023A53M-147 REV1 5. CONDITION CHECK NORMAL AND JOB COMPLETED</P>)

Part: NONE — NONE · airframe 93,201 hrs · 17,179 cycles

FOUND CVR BEACON BATTERY NEAR DUE AT N6 TIL:1EA(<P>1. IAW AMM 23-71-003-002-001 &AMP; 23-71-03-402-015 REV106 REPLACED CVR UNDERWATER LOCATOR BEACON 2. IAW AMM 23-71-03-712-114 REV106 PERFORMED CVR UNDERWATER LOCATOR BEACON INSTALLATION TEST AND THE RESULT WAS SATISFACTORY.</P>)

Part: NONE — NONE · airframe 93,201 hrs · 17,179 cycles

CHAFING DAMAGE ON LH FUSELAGE SKIN EXTERNAL SURFACE AT STA 980 S-39L(<P>1. REMOVE THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 96 2. ACCOMPLISHED EI NO. T2023A53M-109 REV2 AND INSTALL FASTENERS IAW SRM 51-40-02-0G-0 REV96 AND DWG NO. 140U0999 SH 28 REV- 3/ CONDITION CHECK NORMAL AND JOB COMPLETED</P>)

Part: NONE — NONE · airframe 93,201 hrs · 17,179 cycles

DISBOND - SKIN, #5 SPOILER UPPER SURFACE T/E FOUND DISBOND(<P>1. CUT OUT THE DISBOND AND CLEAN MEASURE THE CUTOUT (L = 5.5", W = 3", 32.5" FROM OUTBD EDGE AT T/E) INSTALL THE REPAIR CORE WITH COMPOUND, CURED AT 250 DEGREE FAHRENHEIT FOR 90 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG AND BOND THE EXTERNAL DOUBLERS WITH FILM ADHESIVE. CURE AT 250 DEGREE FAHRENHEIT FOR 90 MINUTES WITH MINIMUM OF 22IN/HG IAW SRM 57-70-02-2R-1 REV 96, SRM 51-70-10-2R-4 REV 96 AND SRM 51-70-10-2R-0 REV 96. 2. CONDITION CHECK IS GOOD</P>)

Part: NONE — NONE · airframe 93,201 hrs · 17,179 cycles

FOUND MAIN DECK SEAT TRACK WORN OUT STA 1746 RBL 11.33(<P>1. REMOVED THE AFFECTED FASTENER I.A.W SRM 51-40-02 REV 96 2. REPAIRED DAMAGE AREA I.A.W SRM 53-00-52-2R-12 REPAIR 12 FIG 201 REV96 3. INSTALLED NEW FASTENER I.A.W SRM 51-40-02 REV 96 AND DWG NO. 65B38253 SH 49 REV- 4. JOB COMPLETED</P>)

Part: SHEAR TIE — NONE · airframe 93,201 hrs · 17,179 cycles

CRACK ON FRONT SPAR SHEAR TIE AT STA 1000 RBL 57.50(<P>1. REMOVE DAMAGE PARTS IAW SRM 51-40-02-0G-0 REV96 2. INSTALL NEW PARTS IAW SRM 51-40-02-0G-0 REV96 AND EO NO. 4453C024 REV3 AND EI NO: T2023A53M-134 SEQUENCE B 3. ACCOMPLISHED EI NO: T2023A53M-134 REV2 4. JOB COMPLETE AND COND CHK NML</P>)

Part: NONE — NONE · airframe 93,201 hrs · 17,179 cycles

FND M/D CGO SEAT TRACK CRACK AT STA 750. LBL 75.92(<P>1. REMOVED AFFECTED FASTERNERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 96 2. REPAIRED DAMAGED AREA IAW SRM 53-00-52-2R-13 REPAIR 13 FIG 201 REV 96 3. INSTALLED NEW PARTS IAW SRM 51-40-02-0G-0 REV 96 AND DWG NO: 65B38250 SH9 REV B 4. CONDITION CHECK NORMAL AND JOB COMPLETED</P>)

Part: STIFFENER — NONE · corrosion level 2 · airframe 93,201 hrs · 17,179 cycles

CORROSION ON LWR FUSELAGE KEEL BEAM STIFFENER AT STA 1000 WL 90 LBL9(<P>1. REMOVE DAMAGE PARTS IAW SRM 51-40-02-OG-0 REV96 2. INSTALL NEW PARTS IAW SRM 51-40-02-0G-0 REV96 AND DWG NO: 65B01828 SH34 REV-A AND DWG NO: 65B01828 SH44 REV-C 3. JOB COMPLETED AND COND CHK NML</P>)

Part: SHEAR TIE — NONE · airframe 93,201 hrs · 17,179 cycles

CRACK ON FRONT SPAR SHEAR TIE AT STA 1000 RBL 75.92(<P>1. REMOVED DAMAGED PARTS IAW SRM 51-40-02-OG-0 REV96 2. INSTALL NEW PARTS IAW SRM 51-40-02-0G-0 REV96 AND EO NO: 4453C024 REV3 3. JOB COMPLETED</P>)

Part: NONE — NONE · airframe 93,201 hrs · 17,179 cycles

FND M/D CGO FLOOR SEAT TRACK CRACK AT STA 2238 RBL 75.92(<P>1. REMOVED AFFECTED FASTENER IAW SRM 51-40-02-0G-0 REV96 2. REPAIRED DAMAGE AREA IAW SRM 53-00-52-2R-13 REPAIR 13 FIG 201 REV 96 3. INSTALLED NEW FASTENERS IAW SRM 51-40-02-0G-0 REV 96 AND DWG NO: 65B38251 SH33 REV- 4. JOB COMPLETED</P>)

Part: NONE — NONE · airframe 93,201 hrs · 17,179 cycles

WORN OUT- FOUND MAIN DECK SEAT TRACK WORN OUT STA 1110 RBL 11.33(<P>1. REMOVED THE AFFECTED FASTENER IAW SRM 51-40-02-0G-0 REV96 2. REPAIRED DAMAGE AREA IAW EI T2023A53M-130 SEQUENCE A AND SEQUENCE B REV 1 3. INSTALLED FASTENERS IAW SRM 51-40-02-0G-0 REV96 AND NO. 111U0801 SH2 REV D, 14U0801 REV-E 4. ACCOMPLISHED EI NO. T2023A53M-130 REV2 5. CONDITION CHECK NORMAL AND JOB COMPLETED</P>)

Part: SHEAR TIE — NONE · airframe 93,201 hrs · 17,179 cycles

CRACK ON FRONT SPAR SHEAR TIE AT STA 1000 RBL 33.99(<P>1. REMOVED DAMAGE PARTS IAW SRM 51-40-02-0G-0 REV96 2. INSTALL NEW PARTS IAW SRM 51-40-02-0G-0 AND EO NO: 4453C024 REV3 AND EI NO: T2023A53M-134 SEQUENCE B 3. ACCOMPLISHED EI NO: T2023A53M-134 REV2 4. ORIGINAL EI ATTACHING WITH W/O: 7939908(162) 5. JOB COMPLETED AND COND CHK NML</P>)

Part: NONE — NONE · airframe 93,201 hrs · 17,179 cycles

CRACK DAMAGE ON FUSELAGE FRAME WEB AT STA 670 BETWEEN S-34R AND S-35R(<P>1.ACCOMPLISED REPAIR IAW SRM 51-40-02-0G-0 REV 96 AND EI NO T2023A53M-103 REV0 SEQUENCE A 2. ACCOMPLISHED EI NO: T2023A53M-103 REV1 3. JOB COMPLETED AND COND CHK NML</P>)

Part: NONE — NONE · airframe 93,201 hrs · 17,179 cycles

CRACK ON SIDE ANGLE OF NOSE WHEEL WELL TOP PANEL ASSY NEAR STA 300, LBL 30 WL 190(<P>1. ACCOMPLISHED EI NO. T2023A53M-157 REV1 2. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: NONE — NONE · airframe 93,201 hrs · 17,179 cycles

CORROSION DAMAGE ON INNER SIDE OF FUSELAUGE SKIN BETWEEN STA 1720 AND 1740 AT S-45L(<P>1. REPAIR THE DAMAGE AREA I.A.W SRM 53-00-01-2R-1, REV=96 AND EI NO. T2023A53M-057, REV 1 2. JOB COMPLETED AND COND CHECK NML</P>)

Part: NONE — NONE · airframe 93,201 hrs · 17,179 cycles

DEVIATION- DURING PERFORM SB 747-53A2443 REV2 HAVE SHORT EDGE MARGIN(<P>1. ACCOMPLISHED EI NO: T2023A53M-132 REV1 AND 2. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: NONE — NONE · airframe 93,201 hrs · 17,179 cycles

EXISTING UNDOCUMENTED REPAIR ON OUTER SKIN OF AFT CARGO DOOR AT FWD LOWER CORNER BETWEEN STA 1810 AND STA 1823(<P>1. REMOVE EXISTING DOUBLER IAW SRM 51-40-02 RV 96 2. INSTALL REPAIR DOUBLER IAW SRM 51-40-02 REV96 AND EI NO. T2023A52M-121 REV1 3. CONDITION CHECK NORMAL AND JOB COMPLETED</P>)

Part: NONE — NONE · airframe 93,201 hrs · 17,179 cycles

FOUND EXISTING REPAIR DOUBLER ON OUTER SIDE SKIN OF FUSELAGE AT STA 2658 BETWEEN S-11L AND 13L(<P>1. REMOVE THE EXISTING DOUBLER IAW SRM 51-40-02-0G-0 REV 96. 2. PERFORM EI T2023A53M-272 REV 0 SEQUENCE A. 3. ACCOMPLISHED EI T2023A53M-272 REV 1. 4. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: NONE — NONE · airframe 93,201 hrs · 17,179 cycles

PUCH HOLE ON RH FUSELAGE SKIN BETWEEN STA 700 TO STA 720. 5-4R ~ 5-5R(<P>1. REPAIR FUSALAGE SKIN IAW SRM 53-00-01-2R-9 REPAIR 9 FIG 201 REV96 2. COND CHK NML AND JOB COMPLETED</P>)

Part: TUBE — NONE · airframe 93,201 hrs · 17,179 cycles

FOUND FUEL TUBE CHAFING WITH STRUCTURE IN NO.4 FUEL TANK PANEL 646AB(<P>1. IAW AMM 28-22-07-004-072-001 REV106 AND AMM 28-22-07-404-080-001 REV106 RPL TUBE IN NO.4 FUEL TANK AND PFM LEAK TEST RESULT WAS NO LEAK FOUND. 2. COORDINATE WITH THE CLOSE PNL CARD 8017 TALLY-1842 TO CLOSE ACCESS PNL.</P>)

Part: NONE — NONE · airframe 93,201 hrs · 17,179 cycles

FOUND MAIN DECK SEAT TRACK WORN OUT STA 1600 LBL 11.33(<P>1. REMOVED THE AFFECTED FASTENER IAW SRM 51-40-02 REV96 2. REPAIR DAMAGE AREA IAW EI NO. T2023A53M-269 SEQUENCE A REV 0 3. FASTENER INSTALLED IAW SRM 51-40-02 REV96 AND DWG NO. 65B38253 SH48 REV- 4. ACCOMPLISHED EI NO. T2023A53M-269 REV1 5. CONDITION CHECK NORMAL AND JOB COMPLETED</P>)

Part: NONE — NONE · airframe 93,201 hrs · 17,179 cycles

FND M/D CGO FLOOR STRUCTURE CRACK AT STA 1480, LBL 75.92(<P>1. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 96 2. REPAIRED DAMAGE AREA IAW&NBSP; SRM 53-00-52-2R-13 REPAIR 13 FIG 201 REV 96 3. INSTALLED NEW PARTS IAW SRM 51-40-02-0G-0 REV 96 AND DWG NO: 1U4UO8O2 SH 3 REV B AND 65B38251 SH 32 REV AND 65B38251 SH 62 REV A 4. JOB COMPLETED</P>)

Part: NONE — NONE · airframe 93,201 hrs · 17,179 cycles

WORN OUT - FOUND MAIN DECK SEAT TRACK WORN OUT STA 1840 LBL 11.33(<P>1. REMOVED THE AFFECTED FASTENER IAW SRM 51-40-02-0G-0 REV96 2. REPAIR DAMAGE AREA IAW EI NO. T2023A53M-270 SEQUENCE A REV0 3. INSTALLED FASTENERS IAW SRM 51-40-02-0G-0 REV96 AND DWG NO. 65B38253 SH50 REV-A 4. ACCOMPLISHED EI NO T2023A53M-70 REV1 5. CONDITION CHECK NORMAL AND JOB COMPLETED</P>)

Part: NONE — NONE · airframe 93,201 hrs · 17,179 cycles

EXISTING UNDOCUMENTED REPAIR DOUBLER ON SKIN OF FUSELAGE AT STA 2598 FWD SIDE BETWEEN S-26R AND S-42R(<P>1. REMOVED EXISTING DOUBLER IAW SRM 51-40-02-0G-0 REV96 2. ACCOMPLISHED THE SKIN REPAIR IAW EI NO. T2023A53M-433 REV1 AND DWG NO. 65B02698 SH13 REV A 3. CONDITION CHECK NORMAL AND JOB COMPLETED</P>)

Part: NONE — NONE · airframe 93,201 hrs · 17,179 cycles

FOUND AN EXISTING RPR DOUBLER AT FWD CGO DOOR AFT LOWER CORNER NEAR STA 662 S-38R(<P>1. REMOVE EXISTING DOUBLER IAW SRM 51-40-02 REV96 2. INSTALL REPAIR DOUBLER IAW SRM 51-40-02 REV96 AND EI NO: T2023A52M-122 REV1 3. CONDITION CHECK NORMAL AND JOB COMPLETED</P>)

Part: NONE — NONE · airframe 93,201 hrs · 17,179 cycles

WORN OUT - FOUND MAIN DECK SEAT TRACK WORN OUT AT STA 1100, LBL 11.33(<P>REMOVED THE AFFECTED FASTENER IAW SRM 57-00-02-0G-0 REV 96. 2. PERFORM REPAIR IAW EO T2023A53M-191 SEQUENCE A AND SEQUENCE B REV 1. 3 INSTALLED FASTENERS IAW SRM 51-44-02-0G-0 REV 96 AND DWG 111U0801, SH 1 REV B, 111U0801 SH 2, REV B, 111U0801 SH 3 REV 3 AND 111U0801 SH 4 REV J. 4. ACCOMPLISHED EO T2022A53M-191 REV 2. 5. CONDITION CHECK NORMAL AND JOB COMPLETED</P>)

Part: NONE — NONE · airframe 93,201 hrs · 17,179 cycles

EXISTING UNDOCUMENTED REPAIR DOUBLER ON OUTER SKIN OF FUSELAGE AT STA 2598 AFT SIDE BETWEEN S-26R AND S-49R(<P>1. REMOVED EXISTING DOUBLER IAW SRM 51-40-02-0G-0 REV96 2. REPAIR THE SKIN DOUBLER IAW EI NO. T2023A53M-436 REV1 AND DWG NO. 65B02707 SH2 REV1 3. COND CHK NML AND JOB COMPLETED</P>)

Part: NONE — NONE · airframe 93,201 hrs · 17,179 cycles

DEVIATION - PERFORM STA 2598 BULKHEAD MODIFICATION FOUND DEVIATION AT DOUBLER(<P>1. PERFORMED EI T2023A53M-310 REV 0 SEQUENCE A. 2. PERFORMED EI T2023A53M-310 REV 1 SEQUENCE B. 3. PERFORMED EI T2023A53M-384 REV 0 SEQUENCE A. 4. ACCOMPLISHED EI T2023A53M-310 REV 2 AND EI T2023A53M-384 REV 1. 5. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: NONE — NONE · airframe 93,201 hrs · 17,179 cycles

M/D CGO FLOOR STRUCTURE CORROSION AT STA 1860 RBL 117(<P>1. BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02-0G-0 REV96 2. PREFORM NDT INSPECT REFER JOB CARD ATTACHING SHEET NO: 0373340 3. ACCOMPLISHED EI NO: T2023A53M-328 REV1 4. JOB COMPLETED AND COND CHK NML.</P>)

Part: BATTERY — NONE · airframe 93,201 hrs · 17,179 cycles

FOUND EMERGENCY BATTERY (M5169) FUNCTION FAIL(<P>1. IAW AMM 33-51-04-902-001-001 REV107 REPLACED EMEREGENCY LIGHT POWER SUPPLY (M5169) BATTERY 2. IAW AMM 33-51-04-902-001-001 REV 107 PERFORMED POWER SUPPLY BATTERY INSTALLATION TEST AND THE RESULT WAS SATISFACTORY.</P>)

Part: NONE — NONE · airframe 93,201 hrs · 17,179 cycles

GOUGE - SKIN, RH WING INBD AILERON NOSE LE, WBL 502.5 - 514.25(<P>1. PERFORM REPAIR OF GOUGE DAMAGE FOUND ON RH WING INBD AILERON NOSE LE, WBL 502.5 - 514.25. PLEASE REFER TO THE JOB CARD ATTACHING SHEETS FOR DETAILED REWORKING INFORMATION. 2. CONDITION CHECK IS GOOD. WORK PERFORM UNDER SRM 57-60-01-2R-1 REV 95, 51-70-09-0G-0 REV 96 &AMP; SRM 51-70-10-2R-0 REV 96</P>)

Part: UNKNOWN — ODOR (E/E BAY)

DURING LOAD CREW REPORTED SMELL COMING FROM E&E. MX INSPECTED AND PERFORMED FIM 21-00 TASK 810 AND CONDITIONAL INSPECTION IAW AMM 05-51-56. NO FAULTS FOUND. MX VENTED OUT E&E AND FLIGHT DECK SMELL DISSIPATED.

Part: PLATE — CORRODED (BS 2220-2280) · airframe 86,461 hrs · 15,752 cycles

M/D - STA 2220 - 2280 LBL 33-90 FSK BOX PLATEFORM PLATE FOUND CORROSION.(<P>M/D STA 2220 - 2280 LBL 33-90 FSK BOX PLATEFORM PLATE CORROSION AREA REPAIRED AS PER EO&NBSP;4425A641 REV 0&NBSP;</P>)

Part: TENSION TIE — CRACKED (BS 840) · airframe 86,461 hrs · 15,752 cycles

M/D STA 840 RH TENSION TIE FWD CHANNEL FASTENER HOLE FOUND CRACK.(<P>M/D STA 840 RH TENSION TIE FWD CHANNEL FASTENER INSTALLED AS PER SRM 51-40-02.</P>)

Part: SEAT TRACK — CORRODED (BS 1590-1670) · airframe 86,461 hrs · 15,752 cycles

M/D STA 1500 - 1620 LBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1590 - 1670 LBL 11 SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12.</P>)

Part: SEAT TRACK — CORRODED (BS 730 RBL 11) · airframe 86,461 hrs · 15,752 cycles

M/D STA 730 RBL 11 SEAT TRACK FOUND CRACK.(<P>M/D STA 710 - 770 RBL 11 SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12.</P>)

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 86,461 hrs · 15,752 cycles

LHW I/B MID FLAP L/E FOUND DELAMINATION&NBSP;(<P>DELAMINATED AREA PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5.A</P>)

Part: FAIRING — CORRODED (VERTICAL STAB) · airframe 86,461 hrs · 15,752 cycles

EMP - V / STAB TIP FAIRING T/E FAIRING FOUND CORROSION.(<P>EMP - V / STAB TIP FAIRING T/E FAIRING REPLACED AND FASTENER INSTALLED AS PER SRM 51-10-02 AND 51-40-02.</P>)

Part: FRAME — CRACKED (BS 820 S7-12R) · airframe 86,461 hrs · 15,752 cycles

M/D STA 820R S-10R FRAME FASTENER HOLE FOUND CRACK.(<P>M/D STA 820R S-7R TO S-12R FRAME REPAIRED AS PER SRM 53-20-07-2R-2 AND 53-20-07-2R-10.</P>)

Part: SEAT TRACK — CORRODED (BS 2230) · airframe 86,461 hrs · 15,752 cycles

M/D STA 2230 LBL 80 SEAT TRACK AND SUPPORT FOUND CORROSION.(<P>M/D STA 2230 LBL 80 SEAT TRACK AND SUPPORT CORROSION AREA BLAENDED OUT AND REPROTED AS PER SRM 53-00-52-1A-1.</P>)

Part: STRUCTURE — TORN (RT AILERON) · airframe 86,461 hrs · 15,752 cycles

RHW I/B AILERON O/B AFT CORNER FOUND TORN.(<P>RHW I/B AILERON O/B AFT CORNER DAMAGED AREA PERFORMED REPAIR AS PER SRM 51-70-06 PAR 5.G, REV 91, REV DATE : 20 FEB 2021.</P>)

Part: SEAT TRACK — CORRODED (BS 1110) · airframe 86,461 hrs · 15,752 cycles

M/D STA 1110 RBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1000 - 1110 RBL SEAT TRACK REPAIRED AS PER SRM 53-40-52-2R-3.</P>)

Part: SEAT TRACK — CORRODED (BS 665) · airframe 86,461 hrs · 15,752 cycles

M/D - STA 665 RBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D STA 550 - 690 RBL 11 SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12.</P>)

Part: SEAT TRACK — CORRODED (BS 1010-1070) · airframe 86,461 hrs · 15,752 cycles

M/D - STA 1010, 1030, 1052, 1070 LBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D - STA 1000 - 1130 SEAT TRACK REPAIRED AS PER SRM 53-40-52-2R-2.</P>)

Part: SEAT TRACK — CORRODED (BS 2070-2170) · airframe 86,461 hrs · 15,752 cycles

M/D STA 2110 AND 2150 RBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D STA 2070 - 2170 RBL 11 SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12.</P>)

Part: SEAT TRACK — CORRODED (BS 725) · airframe 86,461 hrs · 15,752 cycles

M/D - STA 725 RBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D STA 710-770 RBL 11 SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12.</P>)

Part: TENSION TIE — CRACKED (BS 560) · airframe 86,461 hrs · 15,752 cycles

M/D STA 860 LH TENSION TIE AFT CHANNEL 1EA FASTENER FOUND CRACK.(<P>M/D STA 860 LH TENSION TIE AFT CHANNEL 1EA FASTENER INSTALLED AS PER SRM 51-40-02.</P>)

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 86,461 hrs · 15,752 cycles

LHW I/B AFT FLAP UPPER SURFACE FOUND DELAMINATION&NBSP;(<P>DELAMINATED AREA PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5.A</P>)

Part: SEAT TRACK — CORRODED (BS 1900-1940) · airframe 86,461 hrs · 15,752 cycles

M/D - STA 1900 - 1940 RBL 99 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1900 - 1940 RBL 99 SEAT TRACK CORROSION AREA BLENDED OUT AND REPROTED AS PER SRM 53-00-52-1A-1.</P>)

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 86,461 hrs · 15,752 cycles

RHW I/B FORE FLAP FOUND DELAMINATION(<P>DELAMINATED AREA PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5.A</P>)

Part: SEAT TRACK — CORRODED (BS 870 RBL11) · airframe 86,461 hrs · 15,752 cycles

M/D - STA 870 RBL 11 SEAT TRACK FOUND CRACK.(<P>M/D STA 850 - 950 RBL 11 SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12.</P>)

Part: SEAT TRACK — CORRODED (BS 970) · airframe 86,461 hrs · 15,752 cycles

M/D STA 970 RBL 11 SEAT TRACK FOUND CRACK.(<P>M/D STA 950 - 1000 RBL 11 SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12.</P>)

Part: SEAT TRACK — CORRODED (BS 1570 RBL 11) · airframe 86,461 hrs · 15,752 cycles

M/D - STA 1570 RBL 11 SEAT TRACK FOUND CRACK.(<P>M/D STA 1480 - 1590 RBL 11 SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12.</P>)

Part: TENSION TIE — CRACKED (BS 820) · airframe 86,461 hrs · 15,752 cycles

M/D STA 820 LH TENSION TIE AFT CHANNEL 1EA FASTENER HOLE FOUND CRACK.(<P>M/D STA 820 LH TENSION TIE AFT CHANNEL 1EA FASTENER INSTALLED AS PER SRM 51-40-02.</P>)

Part: SEAT TRACK — CORRODED (BS 1770) · airframe 86,461 hrs · 15,752 cycles

M/D STA 1770 LBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1770 - 1790 LBL 11 SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12.</P>)

Part: SEAT TRACK — CORRODED (BS 1362-1480) · airframe 86,461 hrs · 15,752 cycles

M/D STA 1390, 1414 AND 1447 LBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1362 - 1480 LBL 11 SEAT TRACK REPAIRED AS PER RI-53-40-14506 REV A AND RI-53-40-14483 REV A.</P>)

Part: SEAT TRACK — CORRODED (BS 1130) · airframe 86,461 hrs · 15,752 cycles

M/D - STA 1130 LBL SEAT TRACK FOUND CORROSION.(<P>M/D STA 1000 - 1130 LBL 11 SEAT TRACK REPAIRED AS PER SRM 53-40-52-2R-2.</P>)

Part: SEAT TRACK — CORRODED (CABIN) · airframe 86,461 hrs · 15,752 cycles

M/D STA 2060 - 2080 LBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D STA 2055-2170 LBL 11 SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12.</P>)

Part: SKIN — CORRODED (BS 1715-1720) · airframe 86,461 hrs · 15,752 cycles

FX STA 1715-1720 RH SKIN S-42R TO S-43R FOUND CORROSION.(<P>FX STA 1710 - 1740 RH SKIN S-41R TO S-45R REPAIRED AS PER RI-53-61-14484 REV A.</P>)

Part: SEAT TRACK — CRACKED (BS 1730) · airframe 86,461 hrs · 15,752 cycles

M/D STA 1730 LBL 11 SEAT TRACK FOUND CRACK.(<P>M/D STA 1670 - 1770 SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12.</P>)

Part: WEB — CRACKED (BS 2598) · airframe 86,461 hrs · 15,752 cycles

EMP - STA 2598 RH UPPER WEB FOUND 1EA CRACK APPROX 1/2.(<P>EMP - STA 2598 RH UPPER WEB REPAIRED AS PER RI-53-83-14479 REV A.</P>)

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 86,461 hrs · 15,752 cycles

RHW O/B MID FLAP FOUND DELAMINATION&NBSP;(<P>DELAMINATED AREA PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5.A</P>)

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 86,461 hrs · 15,752 cycles

LHW I/B FORE FLAP L/E FOUND SEVERAL DELAMINATION(<P>DELAMINATED AREA PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5.A</P>)

Part: SEAT TRACK — CORRODED (BS 1950-2055) · airframe 86,461 hrs · 15,752 cycles

M/D STA 1950 LBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1950 - 2055 LBL 11 SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12.</P>)

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 86,461 hrs · 15,752 cycles

RHW I/B MID FLAP FOUND DELAMINATION&NBSP;(<P>DELAMINATED AREA PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5.A</P>)

Part: SEAT TRACK — CORRODED (BS 2040-2055) · airframe 86,461 hrs · 15,752 cycles

M/D STA 2040 AND 2055 LBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1950 - 2055 LBL 11 SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12.</P>)

Part: FRAME — CRACKED (BS 2231) · airframe 86,461 hrs · 15,752 cycles

M/D STA 2231 LH&NBSP; S-16L FRAME FASTENER HOLE CRACK.(<P>M/D STA 2231 LH S-16L FRAME REPAIRED AS PER SRM 53-60-15-2R-5.</P>)

Part: SEAT TRACK — CORRODED (BS 1290) · airframe 86,461 hrs · 15,752 cycles

M/D STA 1290 LBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1290 LBL 11 SEAT TRACK CORROSION AREA BLENDED OUT AND REPROTECTED AS PER SRM 53-00-52-1A-1.</P>)

Part: SKIN — DELAMINATED (LT AILERON) · airframe 86,461 hrs · 15,752 cycles

LHW I/B AILERON LOWER SURFACE O/B EDGE FOUND DELAMINATION.(<P>LHW I/B AILERON LOWER SURFACE O/B EDGE DELAMINATED AREA PERFORMED REPAIR AS PER SRM 51-70-06 PAR.5A.(1), REV 91, REV DATE 20 FEB 2021.</P>)

Part: SKIN — CORRODED (RT WING TE FLAP) · airframe 86,461 hrs · 15,752 cycles

RHW I/B AFT FLAP LOWER SKIN SEVERAL LOCATION FOUND CORROSION.(<P>RHW I/B AFT FLAP&NBSP; REPLACEMENT AS PER AMM 27-51-03.</P>)

Part: TENSION TIE — CRACKED (BS 780) · airframe 86,461 hrs · 15,752 cycles

M/D STA 780 TENSION TIE AFT CHANNEL FASTENER HOLES FOUND CRACK.(<P>M/D STA 780 TENSION TIE AFT CHANNEL FASTENER INSTALLED AS PER SRM 51-40-02.</P>)

Part: SEAT TRACK — CORRODED (BS 1010-1070) · airframe 86,461 hrs · 15,752 cycles

M/D STA 1010, 1050, 1070 RBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1000 - 1110 RBL 11 SEAT TRACK REPAIRED AS PER SRM 53-40-52-2R-3</P>)

Part: SKIN — DELAMINATED (RUDDER) · airframe 86,461 hrs · 15,752 cycles

LOWER RUDDER FOUND DELAMINATION.(<P>LOWER RUDDER DELAMINATED AREA PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5.A, REV 91, REV DATE : 20 FEB 2021.</P>)

Part: SEAT TRACK — CORRODED (BS 1480-1590) · airframe 86,461 hrs · 15,752 cycles

M/D STA 1486 LBL 11.33" SEAT TRACK LOWER FLANGE CORROSION.(<P>M/D STA 1480 - 1590 LBL 11.33 SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12.</P>)

Part: SKIN — CRACKED (L1 DOOR) · airframe 86,461 hrs · 15,752 cycles

NO.1 LH DOOR SKIN UPPER HINGE EXTERIOR DOUBLER FOUND CRACK.&NBSP;(<P>NO.1 LH DOOR SKIN UPPER HINGE CUTOUT REPAIRED AS PER SRM 52-10-01-2R-3</P>)

Part: SKIN — DELAMINATED (LT AILERON) · airframe 86,461 hrs · 15,752 cycles

LHW I/B AILERON UPPER SURFACE FOUND DELAMINATION.(<P>LHW I/B AILERON UPPER SURFACE DELAMINATED AREA PERFORMED REPAIR AS PER SRM 51-70-06 PAR.5.A.(1), REV 91, REV DATE : 20 FEB 2021.</P>)

Part: STEP — CRACKED (MD LADDER) · airframe 86,461 hrs · 15,752 cycles

M/D LADDER #3 STEP FWD CRACK ( COUNT FROM UPPER ).(<P>M/D LADDER #3 STEP CRACK AREA REPAIRED AS PER RI-25-50-14438 REV A.</P>)

Part: SKIN — DELAMINATED (LT AILERON) · airframe 86,461 hrs · 15,752 cycles

LHW I/B AILERON LOWER SURFACE FOUND DELAMINATION.(<P>LHW I/B AILERON LOWER SURFACE DELAMINATED AREA PERFORMED REPAIR AS PER SRM 51-70-06 PAR.5A.(1), REV 91, REV DATE : 20 FEB 2021.</P>)

Part: TENSION TIE — CRACKED (BS 900) · airframe 86,461 hrs · 15,752 cycles

M/D - STA 900 RH TENSION TIE AFT CHANNEL FASTENER HOLE FOUND CRACK.(<P>M/D STA 900 RH TENSION TIE CHANNEL FASTENER INTALLED AS PER SRM 51-40-02.</P>)

Part: SEAT TRACK — CORRODED (BS 2165) · airframe 86,461 hrs · 15,752 cycles

M/D STA 2165 LBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D STA 2055-2170 LBL 11 SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12.</P>)

Part: SKIN — CORRODED (BS 1715-1720) · airframe 86,461 hrs · 15,752 cycles

FX STA 1715-1720 RH SKIN S-42R TO S-43R FOUND CORROSION.(<P>FX STA 1710 - 1750 RH SKIN S-41R TO S-45R REPAIRED AS PER RI-53-61-14484 REV A.</P>)

Part: SEAT TRACK — CORRODED (BS 1590-1670) · airframe 86,461 hrs · 15,752 cycles

M/D STA 1620 - 1640 LBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1590 - 1670 LBL 11 SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12.</P>)

Part: PANEL — CHAFED (LT WING TE FLAP) · airframe 86,461 hrs · 15,752 cycles

LHW O/B AFT FLAP MOST O/B PANEL PREVIOUS PATCH FOUND DEEP CHAFING.(<P>LHW O/B AFT FLAP MOST O/B PANEL CARRIED OUT METAL HOT BOND REPAIR AS PER RI NO. RI-57-55-14467 REV A.</P>)

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 86,461 hrs · 15,752 cycles

LHW I/B ELEVATOR UPPER SURFACE FOUND DELAMINATION&NBSP;(<P>DELAMINATED AREA PERFORMED REPAIR AS PER SRM 51-70-06 PAR.5.A.(1)</P>)

Part: TENSION TIE — CRACKED (BS 860) · airframe 86,461 hrs · 15,752 cycles

M/D STA 860 RH TENSION TIE AFT CHANNEL FASTENER FOUND CRACK.(<P>M/D STA 860 RH TENSION TIE AFT CHANNEL FASTENER INSTALLED AS PER SRM 51-40-02.</P>)

Part: SEAT TRACK — CORRODED (BS 2010-2070) · airframe 86,461 hrs · 15,752 cycles

M/D STA 2030 AND 2055 RBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D STA 2010 - 2070 RBL 11 SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12.</P>)

Part: CIRCUIT CARD — MALFUNCTIONED (FIRE PROTECTION) · airframe 84,271 hrs · 15,270 cycles

AFT CARGO FIRE PROTECTION FIRE ALARM 2 SIGNAL FAIL.(<P>REMOVED AND REPLACED AFT CARGO (33) CIRCUIT CARD IAW AMM 26-10-01 AND OPS CHECK OK.</P>)

Part: HOOK AND LOOP — LOOSE (DECENT DEVICE) · airframe 84,271 hrs · 15,270 cycles

U/D DESCENT HARNESS STORAGE BOX HOOK AND LOOP LOOSE FWD WALL. REMOVED LOOSE HOOK AND LOOP CLEANED AND INSTALLED NEW HOOK AND LOOP AT U/D HARNESS STORAGE BOX PER AMM 20-3001-802-001.

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - RT STA 1241 FWD S4R TO S5R INNER SKIN FOUND CORROSION(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1.</SPAN></P>)

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - SCD ENTRANCE BS 1800, RBL 75 SEAT TRACK FOUND DAMAGE(<P>THE SUBJECT SEAT TRACK REPAIRED IAW&NBSP;<SPAN>HX RI NO:RI 53-45-13390 REV. A.</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - RT STA 1241 FWD S8R TO S9R INNER SKIN FOUND CORROSION&NBSP;(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1.</SPAN></P>)

Part: PANEL — DAMAGED (NR 4 PYLON) · airframe 79,522 hrs · 14,273 cycles

PYLON NR 4 PANEL 482EL 1EA FASTENER HOLE FOUND ELONGATED(<P>THE SUBJECT PANEL REPAIR IAW&NBSP;<SPAN>HX RI NO: RI 54-00-13394 REV. A.&NBSP;</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - RT STA 1241 AFT S6R TO S7R INNER SKIN FOUND CORROSION&NBSP;(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1.</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - LT STA 1241 AFT S1L TO S2L INNER SKIN FOUND CORROSION(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1.</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - LT STA 1241 FWD S-1L TO S-2L INNER SKIN FOUND CORROSION&NBSP;(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1.</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - LT STA 1241 AFT S3L TO S4L INNER SKIN FOUND CORROSION(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1.</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - RT STA 1480 FWD S-1R TO S-2R INNER SKIN FOUND CORROSION(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1.</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - LT STA 1241 FWD S-10L TO S-11L INNER SKIN FOUND CORROSION.(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1.&NBSP;</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - LT STA 1480 FWD S5L TO S6L INNER SKIN FOUND CORROSION(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - RT STA 1241 AFT S2R TO S3R INNER SKIN FOUND CORROSION(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1.</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - LT STA 1480 FWD S-4L TO S-5L INNER SKIN FOUND CORROSION&NBSP;(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1</SPAN></P>)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 79,522 hrs · 14,273 cycles

EMERGENCY LIGHT BATTERY PACK ASSY FOUND LOW CAPACITY(<P>M5170 BATTERY PACK ASSY REPLACED AND TEST NORMAL AS PER AMM 33-51-04</P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - LT STA 1241 FWD S8L TO S9L INNER SKIN FOUND CORROSION&NBSP;(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1.</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - LT STA 1241 FWD S2L O S3L INNER SKIN FOUND CORROSION&NBSP;(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1.</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - RT STA 1241 FWD S6R TO S7R INNER SKIN FOUND CORROSION&NBSP;(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1.</SPAN></P>)

Part: FAIRING — CRACKED (TE FLAP) · airframe 79,522 hrs · 14,273 cycles

RT FLAP TRACK FAIRING NR 5 AFT CHORD O/B AREA FOUND CRACK(<P>THE SUBJECT CHORD REPAIR IAW&NBSP;<SPAN>HX RI NO. RI 57-00-13391 REV. A.</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - LT STA 1241 FWD S7L TO S8L INNER SKIN FOUND CORROSION&NBSP;(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>53-00-01-1A-1.</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - RT STA 1480 FWD S-7R TO S-8R INNER SKIN FOUND CORROSION(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1.</SPAN></P>)

Part: TENSION TIE — CRACKED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

UPPER DECK RT BS 760 TENSION TIE AFT CHANNEL 1 EA HOLE WAS CRACKED.(<P>THE SUBJECT TENSION TIE REPAIR CARRIED OUT I.A.W.&NBSP;<SPAN>SRM 53-20-30-2R-1</SPAN><SPAN>.</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - LT STA 1350 AFT S15L TO S16L INNER SKIN FOUND CORROSION&NBSP;(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1.</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

LT STA 1241 AFT S2L TO S3L INNER SKIN FOUND CORROSION(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1.</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - LT STA 1480 FWD S6L TO S7L INNER SKIN FOUND CORROSION(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1.</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - LT STA 1480 FWD S-2L TO S-3L INNER SKIN FOUND CORROSION(<P>CORROSION BLEND OUT REPAIR IA.&NBSP;<SPAN>SRM 53-00-01-1A-1.</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - LT STA 1480 FWD S-10L TO S-11L INNER SKIN FOUND CORROSION(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1.</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - RT STA 1480 FWD S-2R TO S-3R INNER SKIN FOUND CORROSION(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1.</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - LT STA 1480 FWD S-3L TO S-4L INNER SKIN FOUND CORROSION(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - RT STA 1241 AFT S9R TO S10R INNER SKIN FOUND CORROSION&NBSP;(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1.</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

RT STA 1241 FWD S9R TO S10R INNER SKIN FOUND CORROSION&NBSP;(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1.&NBSP;</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - RT STA 1241 AFT S1R TO S2R INNER SKIN FOUND CORROSION(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1.</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - RT STA 1241 FWD S1R TO S2R INNER SKIN FOUND CORROSION&NBSP;(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1.</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - RT STA 1241 AFT S8R TO S9R INNER SKIN FOUND CORROSION&NBSP;(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1.</SPAN></P>)

Part: SKIN — DAMAGED (LT WING) · airframe 79,522 hrs · 14,273 cycles

LT PYLON NR 2 O/B WING L/E LOWER SEVERAL SCREW HOLE FOUND ELONGATED.(<P>THE SUBJECT AREA L/E NOSE SKIN REPAIR IAW&NBSP;<SPAN>HX RI NO. RI 57-41-13389 REV. A.</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - LT STA 1480 FWD S12L TO S13L INNER SKIN FOUND CORROSION(<P>THE SUBJECT AREA SKIN REPAIR IAW&NBSP;<SPAN>HX RI NO. RI 53-40-13399 REV. A.</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - RT STA 1480 AFT S-13R TO S-14R INNER SKIN FOUND CORROSION&NBSP;(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1.</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - LT STA 1480 FWD S-9L TO S-10L INNER SKIN FOUND CORROSION(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1.</SPAN></P>)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,522 hrs · 14,273 cycles

L1 DOOR AREA EMERGENCY L OPERATIONAL TEST FAIL.(<P>L1 DOOR AREA EMERGENCY LIGHT ASSY REPLACED AND OPERATIONAL TEST AND SYSTEM TEST NORMAL AS PER AMM 33-51-07 AND 35-51-00.</P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - RT STA 1241 AFT S10R TO S11R INNER SKIN FOUND CORROSION&NBSP;(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1.</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - LT STA 1480 FWD S16L TO S17L INNER SKIN FOUND CORROSION(<P>THE SUBJECT AREA SKIN REPAIR IAW&NBSP;<SPAN>HX RI NO. RI 53-40-13399 REV. A.</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - RT STA 1480 FWD S-5R TO S-6R INNER SKIN FOUND CORROSION(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1.</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,522 hrs · 14,273 cycles

M/D - RT STA 1241 FWD S7R TO S8R INNER SKIN FOUND CORROSION&NBSP;(<P>CORROSION BLEND OUT REPAIR IAW&NBSP;<SPAN>SRM 53-00-01-1A-1.&NBSP;</SPAN></P>)

Part: SKIN — CORRODED (FUSELAGE) · airframe 78,255 hrs · 14,043 cycles

SKIN CORRODED 2 EACH LOCATIONS RT BS 1700 - 1740, S44R - S45R. EXTERNAL SKIN DOUBLER REPAIR, INCORPORATING PREVIOUS EXISTING REPAIR RT BS 1710 - 1740, S41R - S46R. CATEGORY B REPAIR.

Part: COOLING FAN — DEFECTIVE (E&E BAY) · airframe 73,701 hrs · 13,219 cycles

CAPTAIN REPORTS STRONG ELECT BURNING SMELL IN COCKPIT. NO VISUAL SMOKE. AIR FILTER FOUND FOULED. CLEANED FILTER, REF AMM 21-58-01. REMOVED AND REPLACED FWD EQUIPMENT COOLING SUPPLY FAN PER AMM 21-58-01. OPS CK GOOD.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,950 hrs · 12,873 cycles

CORROSION ON THE UPPER CAP OF MAIN DECK FLOOR STRUCTURE AT STA 2300, LBL 54 - 65. ACCOMPLISH EI NR T2017A53M-309 REV1. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 71,950 hrs · 12,873 cycles

FOUND SEAT TRACK BROKEN AT STA 1486 RBL 75.92. ACCOMPLISHED SUBSTITUTE SEAT TRACK REPAIR IAW SRM 53-00-52 REPAIR 13 FIG 201 REV 78 2. CONDITION CHECK NORMAL AND JOB COMPLETED.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 71,950 hrs · 12,873 cycles

FOUND TENSION TIE CHANNEL ONE HOLE CRACK AT STA 720 LBL 98. REPAIR TENSION TIE CHANNEL IAW SRM 53-20-30 REPAIR 1 REV 78 & 2. CONDITION CHECK NORMAL AND JOB COMPLETED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,950 hrs · 12,873 cycles

FOUND SEAT TRACK CORROSION AT STA 1913 LBL 11.33 (STA 1893 LBL 11.33). REPAIR THE CORROSION AREA IAW EI NR T2017A53M-306 REV 1 AND DWG 65B38253 SH50 REV1 & 65B38253 SH51 REV A & SRM 53-00-52 REPAIR 12 REV 78 & 2. JOB COMPLETED AND COND CHECK NORMAL.

Part: WIRE — BROKEN (BEACON) · airframe 71,950 hrs · 12,873 cycles

FOUND CVR ULB INOPERATIVE. REPLACED CVR'S ULB AND CONDITION CHECK NORMAL IAW AMM 23-71-03-002-001 & 23-71-03-402-015 REV.88. PERFORMED ULB OPERATIONAL TEST AND THE RESULT WAS SATISFACTORY IAW AMM 23-71-03-712-114 REV.88.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,950 hrs · 12,873 cycles

FOUND LT AFT CORNER OF THE NOSE WHEEL WELL EXTERNAL FUSELAGE SKIN CRACK AT S-44L , STA 490. REPAIR CRACK IAW EI NR T2017A53M-296 REV 1 AND SB 747-53A2305 REV 2. COND CHECK NORMAL AND JOB COMPLETED.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 71,950 hrs · 12,873 cycles

CRACKED M/D CARGO SUBSTITUTE TRACK AT STA 997 LBL 75.92. ACCOMPLISHED SUBSTITUTE TRACK REPAIR IAW SRM 53-00-52 REPAIR 13 FIG 201 REV 78. CONDITION CHECK NORMAL AND JOB COMPLETED.

Part: WIRE — BROKEN (ELECTRICAL) · airframe 71,950 hrs · 12,873 cycles

FWD CARGO CENTER AFT SIDE UNDER FLOOR ELECTRICAL CABLE BS 960 - 980, STRINGER 47L BROKEN. IAW WDM 26-16-17 REV.41 & SWPM 20-30-12 REV.63 SPLICE REPAIRED THE WIRE. IAW AMM 26-16-02-404-010 REV.88 PERFORMED TEST OF EJECTOR AND THE RESULT WAS SATISFACTORY.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,950 hrs · 12,873 cycles

SUPPORT FWD FUSELAGE LT LOWER WING TO BODY FAIRING AT STA 960 - 980 LBL 3 - 4. REMOVE DAMAGED PART IAW SRM 51-40-02-0G-0 REV 18. INSTALL NEW PART P/N 65B06976-5 IAW SRM 51-40-02-0G-0 REV 78 AND DWG NR 65B06976 SH2 REV G. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 71,950 hrs · 12,873 cycles

CRACK DAMAGE ON THE 14843300-5 WEB ASSY AT STA 2598 LBL 37 WL 267. ACCOMPLISHED EI NR T2017A53M-255 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: RECEPTACLE — DAMAGED (FUEL TRANSMITTER) · airframe 71,950 hrs · 12,873 cycles

FOUND THE NR 1 ENGINE FUEL TRANSMITTER RECEPTACLE AND CONNECTOR DAMAGED. IAW SWPM 20-60-06 REV.63 AND WDM 73-33-11 REV.41 REPLACED THE TRANSMITTER RECEPTACLE AND CONNECTOR. IAW AMM 73-33-01-000-801 REV.88 AND AMM 73-33-01-400-801 REV.88 REPLACED FUEL PRESSURE TRANSMITTER.

Part: CONNECTOR — CRACKED (FUEL PUMP) · airframe 71,950 hrs · 12,873 cycles

FOUND NR 3 AFT FUEL BOOST PUMP CONNECTOR CRACK (M31). IAW SWPM 20-61-11 REV 63 REPLACED NR 3 AFT FUEL BOOST PUMP CONNECTOR (M31). IAW AMM 28-22-00-705-106 REV 88 PERFORMED 3 AFT BOOST PUMP OPERATIONAL TEST AND THE RESULT WAS SATISFACTORY.

Part: WIRE — BURNED · airframe 71,950 hrs · 12,873 cycles

FOUND THE WIRE SW4541-236-24R, W4541-237-24B, W4541-213-24R, AND W4541-214-24B BURNED. REPAIRED THE WIRES IAW SWPM 20-30-12 REV.63, WBM 45-34-31, AND 31-35-11 REV.41. PERFORMED WIRING CONTINUITY CHECK AND WAS FOUND SATISFACTORY IAW WDM 45-34-31, AND 31-35-16 REV.41. PERFORMED GROUND TEST IAW AMM 31-35-01-404-004 REV.88 AND FOUND SATISFACTORY. PERFORMED MCP GROUND TEST IAW AMM 22-10-00-745-293 REV.88 AND FOUND SATISFACTORY. PERFORMED CMC GROUND TEST IAW AMM 45-10-00-715-043 REV.88 AND FOUND SATISFACTORY.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,950 hrs · 12,873 cycles

ANGLE, FWD FUSELAGE LOWER WING BODY FAIRING AT STA 920 RBL 3 - LBL 3. REMOVED DAMAGED PARTS IAW SRM 51-40-02-0G-0 REV 78. INSTALLED NEW PARTS IAW SRM 51-40-02-0G-0 REV 78 AND DWG 142U0130 SH1 REV A AND DWG 65N06704 SH2 REV F. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,638 hrs · 12,786 cycles

UPPER DECK EMERGENCY LIGHT INOPERATIVE, CREW REST ENTRY. REPLACED THE LAMPS AND OPS CHECK OK IAW 33-51-07.

Part: FIRE BOTTLE — DISCHARGED (APU BAY) · airframe 71,609 hrs · 12,777 cycles

APU FIRE WARNING AT CRUISE. BOTTLE DISCHARGED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,974 hrs · 12,628 cycles

PRIOR TO SCHEDULED DEPARTURE, ON 24-SEP-2016, THE DATUM AIRPLANE FUSELAGE SKIN WAS FOUND WITH CORROSION CRACKS IN THE VICINITY OF FASTENER LOCATIONS AT BS 1736, ALONG STR 42R, AND AT BS 1731, ALONG STR 42R. SHEET METAL REPAIR EO 4453B268.

Part: CIRCUIT CARD — DEFECTIVE (FIRE WARNING) · airframe 70,186 hrs · 12,442 cycles

EICAS MESSAGE FIRE MAIN DECK ON CLIMBOUT UNTIL SHORT FINAL. REPLACED DIODE CARD A-15 IAW AMM 26-10-01. OPS CHECK OK IAW AMM 26-14-00.

Part: COALESCER BAG — TORN (AC BAY) · airframe 69,934 hrs · 12,384 cycles

MASTER WARNING MAIN DECK FIRE INDICATION. FOLLOWED QRH PROCEDURES, REF LP 769723-M4. PERFORMED MAWEA INPUT MONITORING ON MASTER MONITOR CARD A & B, RESULTS SATISFACTORY. PERFORMED TEST OF SMOKE DETECTION SYS FOR CARGO AREA SYS, RESULTS SATISFACTORY IAW MM 26-10-01, NO MSG NOTED, REF LP 769722-1. INVESTIGATED & NO SMOKE OR FIRE EVIDENCE WAS NOTED. TROUBLE SHOT & FOUND COALESCER BAG WAS TORN ON PACK 3. ALL PACK COALESCER BAGS REPLACED & OK IAW MM 21-51-05.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 69,358 hrs · 12,255 cycles

STATUS MSG, EQUIP SMOKE. COMPLIED WITH CONDITIONAL CHECK OK IAW AMM 05-51-51. NO EVIDENCE OF SMOKE OR FUMES DETECTED. SUSPECT POSSIBLE RELATION TO LOWER EICAS DISPLAY FAIL AT SAME TIME DURING FLIGHT. CHECK & CLEANED EQUIP SMOKE DETECTOR IAW AMM 26-16-51. RAN EQUIP COOLING TEST & OPERATIONS CHECKED NORMAL IAW AMM 21-58-00. LOWER EICAS SCREEN PLACED ON DMI, MDDR 65216.

Part: FUEL FILTER — FAULTY (NR 1 ENGINE) · airframe 67,907 hrs · 11,931 cycles

MULTIPLE EICAS MSGS OF, ENG 1 FUEL FILT IN CRUISE, SELF-CLEAR WITHIN 10 - 15 SECS. STATUS MSG, ENG 1 FUEL FILT, NR 1 ENG FUEL FILTER ELEMENT REPLACED. FUEL LEAK CHECKED WITH ENG GND RUN CUT OUT SATISFACTORY IAW AMM 73-11-02. CMC PLF & EXISTING FAULT REVIEWED NO FAULT ACTIVE.

Part: FUEL FILTER — FAULTY (NR 4 ENGINE) · airframe 67,907 hrs · 11,931 cycles

ENG 4 FUEL FILT IN CRUISE, SELF-CLEAR WITHIN 10 - 15 SECONDS STATUS MSG. ENG 4 FUEL FILT NR 4 ENG FUEL FILTER ELEMENT REPLACED. FUEL LEAK CHECKED CUT OUT & SATISFACTORY IAW AMM 73-11-02. ENG NR 4 GND IDLE RUN TEST PERFORMED IAW AMM 71-00-00. NIL PLF & EXISTING FAULT NOTED.

Part: FUEL FILTER — FAULTY (ENGINE) · airframe 67,907 hrs · 11,931 cycles

INFLIGHT DIVERT DUE TO QRH 7.16, REF TO LP 733225 01 & LP 733226 4. NR 1 & NR 4 FUEL FILTER WERE REPLACED, FUEL LEAK CHECKED SATISFACTORY. ENG 1 & 4 GND IDLE RUN CUT OUT NIL PLF & EXISTING FAULT NOTED IAW AMM 71-00-00.

Part: TIRE — BLOWN (MLG) · airframe 67,115 hrs · 11,755 cycles

ON TAXI OUT, NR 11 TIRE BLEW, BRAKE TEMP 0.0. REPLACED NR 11 MAIN WHEEL IAW AMM 32-45-01, CHECKED OK. ALSO REF LP 744618-20 FOR REPAIRS TO GEAR VIA EO 4432A100 101 102.

Part: WIRE HARNESS — DEFECTIVE (NR 3 ENGINE) · airframe 66,943 hrs · 11,719 cycles

NUMBER 3 ENG EGT INDICATION INTERMITTENTLY & INOPERATIVE. LOST INDICATION TWICE IN FLIGHT, NR 3 ENG EGT LOWER THERMOCOUPLE CABLE HARNESS REPLACED IAW MM 77-21-02-004-001, REF LP 720674. ACCOMPLISHED ENG RUN UP IAW MM 71-00-00 FOR EGT HARNESS REPLACEMENT & ALL INDICATIONS NORMAL.

Part: TIRE — DEFLATED (NR 9) · airframe 66,892 hrs · 11,709 cycles

NUMBER 9 TIRE WENT FLAT ON LANDING. NR 9 TIRE REPLACED IAW AMM 32-45-02 401, REF LOG PAGE 696237 ITEM 4 FOR CHAP 5 INSPECTION.

Part: SKIN — CRACKED (LT WLG DOOR) · airframe 65,547 hrs · 11,477 cycles

LEFT WLG OTBD WW DOOR INNER SKIN OTBD EDGE FOUND CRACKED. REPAIRED IAW R1-52-80-10796 REV A.

Part: SKIN — CRACKED (RT WLG DOOR) · airframe 65,547 hrs · 11,477 cycles

RIGHT WLG OTBD WW DOOR INTER SKIN OTBD EDGE FOUND CRACKED AS MARKED. REPAIRED IAW R1-52-80-10796 REV A.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 65,547 hrs · 11,477 cycles

MAIN DECK L5 DOOR FWD CUT OUT REVEAL FOUND CRACKED. REPAIRED IAW SRM 53-60-15-2R-3 REPAIR 3.

Part: TEE FITTING — CORRODED (LT WING) · corrosion level 2 · airframe 65,547 hrs · 11,477 cycles

LEFT WING TE CAVITY WS 680 FOUND CORROSION, INSIDE 572GB. LT WING TE CAVITY FWD OF NR 5 SPOILER ACTUATOR UPPER TEE CHORD REPAIRED IAW R1-57-51 10815 REV B.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 65,547 hrs · 11,477 cycles

MAIN DECK STATION 1220 RT OTBD BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED DURING RISER DUCT INSPECTION. REPAIRED IAW SRM 53-40-51-2R-5 REPAIR 5.

Part: STRUCTURE — WORN (NR 3 PYLON) · airframe 65,547 hrs · 11,477 cycles

NUMBER 3 PYLON 472ER TWO EACH INDICATOR HOLE FOUND WORN. REPAIRED IAW R1-54-00-10805 REV A.

Part: SKIN — CHIPPED (BALL MAT) · airframe 65,547 hrs · 11,477 cycles

MAIN DECK STATION 1780 - 1840, RBL 55 - 75 BALL MAT SKIN FOUND CHIPPED. REPAIRED TWO LOCATIONS IAW R1-25-55-10798 REV A.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 65,547 hrs · 11,477 cycles

MAIN DECK WHEN REMOVED RT BS 1720 - 1920 UPPER SIDEWALL FOR REPAIR FRAME, FOUND DENT AT BS 1820 STRINGER 12 - 13. MAIN DECK RT BS 1820 STRINGER 11 TO 15 FRAME REPAIRED IAW SRM 53-60-07-2R-5 REPAIR 5.

Part: SKIN — DENTED (LT BLG DOOR) · airframe 65,547 hrs · 11,477 cycles

LEFT BLG INBD STRUT DOOR INNER SKIN FOUND DENT AS MARKED. REPAIRED IAW RI- 52-83-10795 REV A.

Part: CAP — CRACKED (NR 3 COWLING) · airframe 65,547 hrs · 11,477 cycles

NUMBER 3 ENG LT CORE COWL AFT END CAP CRACK FOUND AT CTR PORTION. REPAIRED AS EO NR 1971A092 REV 0.

Part: DOOR — CRACKED (RT WLG) · airframe 65,547 hrs · 11,477 cycles

RIGHT WLG OTBD WW DOOR OTBD EDGE MIDDLE FOUND CRACKED. REPAIRED IAW R1-52-80-10796 REV A.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 65,547 hrs · 11,477 cycles

MAIN DECK STATION 1200 RT OTBD BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED DURING RISER DUCT INSPECTION. REPAIRED IAW R1-53-40-10816 REV A.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 65,547 hrs · 11,477 cycles

MAIN DECK STATION 1200 LT OTBD BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED DURING RISER DUCT INSPECT. REPAIRED IAW R1-53-40-10816 REV A.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 65,547 hrs · 11,477 cycles

MAIN DECK SIDE CARGO AFT OTBD DOOR SILL SKIN FOUND CRACKED. REPAIRED IAW R1-25-55-10793 REV A.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 65,547 hrs · 11,477 cycles

MAIN DECK SIDE CARGO DOOR FWD OTBD DOOR SILL SKIN FOUND CRACKED. REPAIRED 4 LOCATIONS IAW R1-25-55-10807 REV A.

Part: SKIN — CRACKED (BALL MAT) · airframe 65,547 hrs · 11,477 cycles

MAIN DECK STATION 1780 - 1840, LBL 55 - 75 BALL MAT SKIN FOUND PUNCHED MARK & CRACKED. REPAIRED IAW R1-25-55-10798 REV A.

Part: STRUCTURE — WORN (NR 4 PYLON) · airframe 65,547 hrs · 11,477 cycles

NUMBER 4 PYLON 482EL TWO EACH INDICATOR HOLE FOUND WORN. REPAIRED IAW R1-54-00-10805 REV A.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 65,547 hrs · 11,477 cycles

MAIN DECK STATION 545 - 547 RBL 11 SEAT TRACK FOUND ELONGATED. REPAIRED IAW R1-53-25-10814 REV A.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 65,547 hrs · 11,477 cycles

MAIN DECK STATION 1180 RT OTBD BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED DURING RISER DUCT INSPECTION. REPAIRED IAW SRM 53-40-51-2R-8 REPAIR 8.

Part: STRUCTURE — DAMAGED (NR 3 NACELLE) · airframe 65,547 hrs · 11,477 cycles

NUMBER 3 ENG RT CORE COWL UPPER AFT EDGE DEFORMED. REPAIRED IAW SRM 54-45-0-2R-7.

Part: SKIN — CRACKED (BALL MAT) · airframe 65,547 hrs · 11,477 cycles

MAIN STATION 1840 - 1920, LBL 75 - 98 BALL MAT SKIN FOUND CRACKED. REPAIRED IAW R1-25-55-10798 REV A.

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 65,547 hrs · 11,477 cycles

NUMBER 2 ENG RT CORE COWL, EXTERNAL SKIN CRACK FOUND JUST BELOW PRE COOLER EXHAUST GRILL. REPAIRED IAW SRM 54-45-01-2R-4 REPAIR 4.

Part: SKIN — DENTED (RT BLG DOOR) · airframe 65,547 hrs · 11,477 cycles

RIGHT BLG INBD STRUT DOOR INNER SKIN FOUND DENT AS MARKED. REPAIRED IAW RI-52-83-10795 REV A.

Part: STRUCTURE — WORN (NR 1 PYLON) · airframe 65,547 hrs · 11,477 cycles

NUMBER 1 PYLON 452EL ONE EACH INDICATOR HOLE FOUND WORN. REPAIRED IAW R1-54-00- 10805 REV A.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 65,547 hrs · 11,477 cycles

NUMBER 1 PYLON SKIRT FAIRING INBD SKIN CRACK FOUND AT ADP EXHAUST GRILL UPPER AFT SCREW HOLE AREA. REPAIRED IAW R1-54-00-10797 REV A.

Part: DOOR — CRACKED (LT WLG) · airframe 65,547 hrs · 11,477 cycles

LEFT WLG & WW OTBD DOOR, OTBD EDGE MIDDLE FOUND CRACKED. REPAIRED IAW R1-52-80-10796 REV A.

Part: PDU — FAILED (LE FLAPS) · airframe 85,295 hrs · 15,153 cycles

AIR TURN BACK DUE TO FLAPS PRIMARY EICAS MESSAGE AFTER TAKEOFF; APPROXIMATELY AT 10,000 FT, AFTER SELECTING FLAPS "UP". ALT FLAPS DISPLAY HAD AN "X" FOR RIGHT MIDSPAN L/E. R & R R3 L/E DRIVE PDU IAW AMM 27-81-03, ALL OPS NORMAL.

Part: EXHAUST STACK — CRACKED (NR 3) · airframe 60,343 hrs · 10,410 cycles

DURING MX WALK AROUND, FOUND A CRACK ON ENGINE NR 3 PRIMARY EXHAUST NOZZLE LOCATED AT 9 O'CLOCK POSITION AFT EDGE. THE CRACK DIMENSION RUNS 4.7500" LONG CIRCUMFERENTIAL AND LOCATED .7500" FROM THE NOZZLE AFT END. THE CRACK IS DETERMINED TO BE OUTSIDE ALLOWABLE LIMITS IAW SRM 54-41-30. DISPOSITION IS TO PERFORM TIME LIMITED REPAIR BY STOP DRILLING THE CRACK ENDS WITH A 0.125" DIAMETER HOLE, DVI EVERY 3 FLIGHT CYCLES; AND REMOVAL OF THE PART WITHIN 50 FC (FLIGHT CYCLES).

Part: STRUCTURE — CHAFED (RT WING TE FLAP) · airframe 60,080 hrs · 10,360 cycles

RT WING L/E NR 18 VC FLAP LOWER EDGE FOUND CHAFING. REPAIRED IAW R1 NR 57-40-10152, REV A.

Part: FRAME — CHAFED (NR 2 NACELLE) · airframe 60,080 hrs · 10,360 cycles

NR 2 ENG RT CORE COWL INNER FACE NR 2 FRAME FOUND CHAFED. (NR 2 ENG RT CORE COWL INNER FACE NR 2 FRAME CHAFING MARK AREA REPAIRED IAW CN13-0428).

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 60,080 hrs · 10,360 cycles

VERT FIN L/E FAIRING 321H M/D AREA SKIN FOUND DENT AND DAMAGED. (VERT FIN L/E FAIRING 321H, PN 174U11 MID AREA SKIN DENT AREAS REPAIRED IAW R8. R1-55-33-10148).

Part: ACCESS PANEL — DAMAGED (NR 4 NACELLE) · airframe 60,080 hrs · 10,360 cycles

DURING C3 CHECK, DAMAGE TO THE NR 4 PYLON, LT ACCESS PANEL NR 482IL WAS FOUND WITH A CRACK APPROX 6.0" IN LENGTH ON THE LOWER RADIUS AREA. ACCOMPLISHED AN INTERIM REPAIR.

Part: FRAME — CHAFED (NR 1 NACELLE) · airframe 60,080 hrs · 10,360 cycles

NR 1 ENGINE LT CORE COWL NR 2 INTERIOR FRAME FOUND CHAFING MARK. (NR 1 ENG LT CORE COWL NR 2 INTERIOR FRAME CHAFING MARK AREA REPAIRED IAW SRM 54-45-02-2R1, REP 1, FIG 201.)

Part: STOP — LOOSE (NR 1 PYLON) · airframe 60,080 hrs · 10,360 cycles

NR 1 PYLON AFT BULKHEAD OTBD STOP PAD FOUND LOOSE. (NR 1 PYLON AFT BULKHEAD SIDE LOAD FITTING WORN FASTENER HOLES REPAIRED IAW R1 NO R1-5400-10146 REV B.)

Part: SUPPORT CHANNEL — CRACKED (NR 4 NACELLE) · airframe 60,080 hrs · 10,360 cycles

NR 4 PYLON CASE DRAIN MODULE SUPPORT CHANNEL, S/E SIDE FOUND CRACKED.NR 4 PYLON CORE DRAIN MODULE SUPPORT CHANNEL FABRICATED IAW BS NO R1-94-00-10147 AND REPLACED IAW SRM 51-10-02

Part: STRINGER — DAMAGED (BS 160-200) · airframe 60,080 hrs · 10,360 cycles

EO1952A109 DOOR NLD RT STA 160-180 STR 14D, RT STRINGER FOUND DENT. DAMAGED STRINGER REPAIRED IAW R1 NR R1-53-11-10139 AND SRM 53-00-03 REPAIR 4.

Part: SKIN — CRACKED (BS 980 S38L) · airframe 60,080 hrs · 10,360 cycles

DURING C3/A4 CHECK, WHILE UNDERGOING EO 4453A499 (SB 747-53A2444, REV 2/ AD 2001-22-04) INSPECTION, A CRACK WAS DETECTED IN THE FUSELAGE SKIN AT THE 11 AND 5 O'CLOCK POSITION OF A FASTENER HOLE COMMON TO S38L NEAR BS 980. PERMANENT REPAIR ACCOMPLISHED IAW SRM 53-20-01-2R-2, REPAIR 2, FIGURE 201.

Part: SKIN — CRACKED (BS 933 S38R) · airframe 60,080 hrs · 10,360 cycles

FUSELAGE BS 933 STR 38R AT DRAG SPLICE FITTING AREA FOUND ONE FASTENER HOLE CRACKED AT FUSELAGE SKIN. REPAIRED IAW SRM 53-20-01-2R2 REPAIR 2, FIG 201.

Part: ACTUATOR — INOPERATIVE (THRUST REVERSER) · airframe 59,893 hrs · 10,330 cycles

DURING ROUTINE INSPECTION OF NR 2 RT THRUST REVERSER, MX FOUND THE THRUST REVERSER NOT STOWING. AFTER INSPECTION FOUND UPPER BALLSCREW ACTUATOR AT FAULT. PERFORMED A DETAIL INSPECTION OF THE REVERSER HALF IN QUESTION INCLUDING REVERSER CONE BRAKE FUNCTIONAL CHECK, IAW AMM 78-31-00. REMOVAL OF THE DEFECTIVE UPPER ANGLE GEARBOX BALLSCREW ACTUATOR JACKSCREW AND REPLACING IT WITH THE LOWER BALLSCREW ACTUATOR. LOWER ACTUATOR POSITION WILL NOT BE INSTALLED. PERFORMED DEACTIVATION OF THE NR 2 ENGINE THRUST REVERSER IAW DDG 78-31-1.

Part: TRANS PANEL — DAMAGED (THRUST REVERSER) · airframe 59,512 hrs · 10,262 cycles

DURING MX WALKAROUND, FOUND LIGHTNING STRIKE DAMAGE TO THE NR 3 ENGINE RT THRUST REVERSER TRANSLATING COWL, REPAIRED IAW CMM 78-32-31, REPAIR 023.

Part: SKIN — CRACKED (THRUST REVERSER) · airframe 59,111 hrs · 10,178 cycles

CRACK ON THE NR 1 ENGINE LT THRUST REVERSER TRANSLATING COWL OUTER SKIN. PERFORM A TIME LIMITED REPAIR.

Part: SKIN — DAMAGED (WING) · airframe 59,041 hrs · 10,161 cycles

NR 1 FLAP TRACK FAIRING HAS DAMAGE TO THE SKIN, MEASURING 5.375 INCHES LONG, BY 2.5 INCHES WIDE. DAMAGE IS BEYOND THE LIMITS OF SRM 57-53-70, FIG 101 ALLOWABLE DAMAGE 1 AND SRM 51-70-02, FIG 101 ALLOWABLE DAMAGE GENERAL. REPAIRED IAW EO 4457A433.

Part: STRUCTURE — DEFORMED (BS 1780-1920) · airframe 58,942 hrs · 10,140 cycles

MAIN DECK SIDE CARGO DOOR AREA BS 1780 AND 1920 SIDEWALL TRIM AND GUTTER DEFORMED. PERFORMED A TIME LIMITED REPAIR IAW EO 4425A319.

Part: SLEEVE — CRACKED (NR 2 EXHAUST) · airframe 58,813 hrs · 10,116 cycles

DURING MX, FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, APPROX AT 3 O'CLOCK POSITION (RT SIDE) ON THE NR 2 ENGINE. THE CRACK IS APPROX 3" LONG AND IS 1" FROM AFT SIDE OF EXHAUST SLEEVE JUST IN FRONT OF NAC STA 361.923 . IAW SRM 54-41-30 THE DISTANCE BETWEEN THE CRACK AND THE EDGE 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 FC (FLIGHT CYCLES).

Part: RAIL — DEFLATED

TWO ESCAPE RAILS ARE DEFLATED.