N496MC

Part: TRANSCEIVER — FAILED (WX RADAR SYSTEM) · airframe 103,296 hrs · 17,357 cycles

WX RT SYS & RT WXR FAIL STATUS MSG DISPLAYED. ATB, R & R RT WXR R/T RACK IAW AMM 34-43-03. OPS CHECK GOOD. R & R RH WXR TRANSCEIVER IAW 34-43-02, SYSTEM TEST OKAY.

Part: TRANSCEIVER — FAILED (WX RADAR SYS) · airframe 103,299 hrs · 17,358 cycles

WEATHER FAIL ND MESSAGE &AMP; WXR ATT(<P>R/R LH WXR TRANSCEIVER IAW AMM 34-43-02 AND WXR RADAR PEDESTAL IAW 34-43-00. SYSTEM TEST GOOD PER 34-43-00</P>)

Part: PDU — BURNED (NR 1) · airframe 103,210 hrs · 17,341 cycles

PDU NR 1 FOUND BURNED. REMOVED PDU NR 1, INSTALLED BLANKING PLATE, AND DEFERRED PDU NR 1. PERFORMED CONDITIONAL INSPECTION IAW AMM 05-51-56-200-801, NO FURTHER DEFECTS FOUND. TRANSFER TO DMI 238867 PER MEL 25-57-01 CAT D DUE DATE 23JAN26.

Part: SKIN — DAMAGED (ZONE 100) · airframe 102,957 hrs · 17,288 cycles

RIGHT LOWER AFT FUSELAGE SKIN DAMMAGE FWD OF AFT LOWER CARGO DOOR. REPAIR TO DAMAGE AT FS 1802, STR 35R C/W IAW EO 4453C592 PART 1 CATEGORY C IAW SRM 53-00-01. REPEAT VISUAL INSP DUE EVERY 250 F/C. TRANSFERRED TO NON-MEL 237259. LP 1915290 M14: PERMANENT REPAIR CATEGORY B REPAIR ACCOMPLISHED ON FUSELAGE SKIN (P/N:65B07008-7) AS PER BMN TLS-TLS-26-0058 AND SCO-TLS-26-0010 AND APPROVED PER FAA FORM 8100-9 STAGE 1 & 2. (W/O 146589 EO4453C592 9RTN 8017-1035) & NR 0007). NO FURTHER DEFECTS NOTED. DMI 237259 CLOSED.

Part: SPOILER — DAMAGED (ZONE 500) · airframe 101,274 hrs · 16,958 cycles

DURING LOADING, FOUND #5 SPOILER DAMAGED/PARTIALLY MISSING.(<P>R/R LEFT WING SPOILER #5 IAW B747 AMM 27-62-01/401. OPS CHECKED GOOD. NO DEFECTS NOTED. IPC REF: 27-11-01-01.</P>)

Part: RVDT — FAULTED (ZONE 500) · airframe 100,833 hrs · 16,875 cycles

FLAP DRIVE EICAS MESSAGE WITH SELECTION OF FLAPS 5 ON APPROACH(<P>PER FIM 27-51 TASK 878. R/R LH OUTBD FLAP TRANS RVDT IAW AMM 27-58-01 REV 112, ADJUSTED AND OPS CHECKED GOOD.&NBSP;</P>)

Part: TRANSCEIVER — FAILED (WX RADAR) · airframe 100,376 hrs · 16,797 cycles

RIGHT SIDE WXR FAIL IN FLIGHT (LH DEFERRED)(<P>SWAPPED RH WITH LH TRANSCEIVER AS THIS WAS NOT THE REASON FOR DEFERRAL. TESTED GOOD PER AMM 34-43-02</P>)

Part: FLOOR SUPPORT — CRACKED (BS 1000) · airframe 98,092 hrs · 16,371 cycles

M/D STA 1000 RBL 75" FLOOR HAT SECTION FOUND CRACKED(<P>&NBSP;HAT SECTION CRACK AREA REPAIRED AS PER SRM 53-00-52-2R-13 REPAIR 13 FIG 201. NO FURTHER DEFECTS NOTED</P>)

Part: SEAT TRACK — CRACKED (BS 1600-1620) · airframe 98,092 hrs · 16,371 cycles

M/D - STA 1600-1620 RBL 11" SEAT TRACK O/B FLANGE FOUND CORROSION CRACK(<P>SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12 REPAIR 12 FIG 201. NO FURTHER DEFECTS NOTED</P>)

Part: SEAT TRACK — CRACKED (BS 980-1000) · airframe 98,092 hrs · 16,371 cycles

FWD CARGO BS 980-1000 RH S/W UPPER AREA FND M/D FLOOR SEAT TRACK RBL 98.58 CORROSION DAMAGE(<P>SEAT TRACK REPAIRED AS PER RI-53-40-16817 REV A. NO FURTHER DEFECTS NOTED</P>)

Part: FITTING — CRACKED (BS 1000) · airframe 98,092 hrs · 16,371 cycles

1EA CRACK WAS FOUND ON BS 1000 RBL 11.33" INTERCOSTAL LUG FITTING APPROX 1" IN LENGTH(<P>CRACK INTERCOSTAL LUG FITTING REPLACED AS PER ATLAS AIR EO 4453C024 REV 3 PART 7. NO FURTHER DEFECTS NOTED</P>)

Part: SEAT TRACK — CORRODED (BS 1920-1940) · airframe 98,092 hrs · 16,371 cycles

M/D - STA 1920-1940 RBL 11" SEAT TRACK FOUND CORRODED(<P>SEAT TRACK CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DENTED (LT MLG DOOR) · airframe 98,092 hrs · 16,371 cycles

DENT LOG D-3-21 - LH BODY GEAR O/B W/W DOOR FWD OUTBOARD (DOOR 754) 77" FROM LEADING EDGE DENT D2 1/4"X 2 1/4" X 7/32 DEEP WITHIN LIMIT IAW SRM 52-80-01-1A-3(<P>SKIN REPAIR AS PER SRM 52-80-01-2R-1 REPAIR 1 FIG 201. NO FURTHER DEFECTS NOTED</P>)

Part: BEAM — CRACKED (NR 1 NACELLE) · airframe 98,092 hrs · 16,371 cycles

#1 PYLON INBD SKIRT BEAM AFT STRUT ADP AIR OUTLET UPPER FND PYLON PANEL FASTENER HOLES CRACKED (2 LOCATIONS)(<P>SKIN 2EA FASTENER HOLES REPAIRED AS PER RI-54-51-16818 REV A. NO FURTHER DEFECTS NOTED</P>)

Part: SEAT TRACK — CRACKED (BS 1920-1940) · airframe 98,092 hrs · 16,371 cycles

M/D - STA 1920-1940 LBL 11" SEAT TRACK FOUND CRACK(<P>SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12 REPAIR 12 FIG 201. NO FURTHER DEFECTS NOTED</P>)

Part: SEAT TRACK — CRACKED (BS 1780-1800) · airframe 98,092 hrs · 16,371 cycles

M/D - STA 1780-1800 LBL 11" O/B FLANGE FOUND CORROSION CRACK(<P>SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12 REPAIR 12 FIG 201. NO FURTHER DEFECTS NOTED</P>)

Part: LADDER — CRACKED (CREW) · airframe 98,092 hrs · 16,371 cycles

M/D - CREW LADDER #7 STEP FWD & AFT AREA FOUND CRACK (FROM BOTTOM)(<P>CRACK STEP FWD AND AFT AREA REPAIRED AS PER RI-25-50-16803 REV A. NO FURTHER DEFECTS NOTED</P>)

Part: SHEAR TIE — CRACKED (BS 1000) · airframe 98,092 hrs · 16,371 cycles

1EA CRACK WAS FOUND ON BS 1000 RBL 75.92 SHEAR TIE APPROX 0.875"  LENGTH(<P>CRACK SHEAR TIE REPLACED AS PER ATLAS EO 4453C024 REV 3 PART 10. NO FURTHER DEFECTS NOTED</P>)

Part: TENSION TIE — CRACKED (BS 860) · airframe 98,092 hrs · 16,371 cycles

LH BS 860 UPR DECK TENSION TIE 1EA FASTENER HOLE FOUND CRACK ON AFT CHANNEL(<P>AFT CHANNEL REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED</P>)

Part: SHEAR TIE — CRACKED (BS 1000) · airframe 98,092 hrs · 16,371 cycles

1EA CRACK WAS FOUND ON BS 1000 RBL 33.99 SHEAR TIE APRROX 1.250" LENGTH(<P>&NBSP;CRACK SHEAR TIE REPLACED AS PER ATLAS EO 4453C024 REV 3 PART 8 AND RI-53-14-16804 REV A. NO FURTHER DEFECTS NOTED</P>)

Part: CLOSEOUT PANEL — CRACKED (BS 1241 LBL77-99) · airframe 98,092 hrs · 16,371 cycles

M/D - STA 1241 LBL 77-99 CLOSEOUT PANEL FOUND CRACK (APPROXIMATE 6")(<P>CRACK CLOSEOUT PANEL REPLACED AS PER SRM 51-10-02 AND NEW CLOSEOUT PANEL HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW CLOSEOUT PANEL INSTALLED AS PER SRM 51-40-02&NBSP;</P>)

Part: RIVET — DAMAGED (VERTICAL STAB) · airframe 98,092 hrs · 16,371 cycles

V/STAB L/H AUX SPAR TO FRONT SPAR PNL SURFACE FND 1EA BURN MARK RIVET (STA 245 FRONT SPAR RIVET)(<P>BURN MARK RIVET REPLACED AS PER RI-55-30-16816 REV A. NO FURTHER DEFECTS NOTED</P>)

Part: STIFFENER — CRACKED (NLG WW) · airframe 98,092 hrs · 16,371 cycles

LH NOSE WHEEL WELL SIDE PANEL STA 265 TO 280 WL 170 STIFFENER 1EA HOLE CRACK. APPROX 3/8" IN LENGTH(<P>CRACK STIFFENER REPLACED AS PER ATLAS AIR EO 4453A043 REV 10 PART 2 STEP 2 AND STEP 3</P>)

Part: SHEAR TIE — CRACKED (BS 1000) · airframe 98,092 hrs · 16,371 cycles

1EA CRACK WAS FOUND ON BS 1000 RBL 57.50 SHEAR TIE APPROX 1.250" LENGTH(<P>CRACK SHEAR TIE REPLACED AS PER ATLAS EO 4453C024 REV 3 PART 9 AND RI-53-14-16805 REV A. NO FURTHER DEFECTS NOTED</P>)

Part: SEAT TRACK — CRACKED (BS 1780-1800) · airframe 98,092 hrs · 16,371 cycles

M/D STA 1780-1800 RBL 11" SEAT TRACK FOUND CRACK.(<P>SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12 REPAIR 12 FIG 201. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DENTED (RT ELEVATOR) · airframe 98,092 hrs · 16,371 cycles

RH I/B ELEVATOR FOUND DENT(<P>PERFORMED REPAIR IAW SRM 51-70-06 PAR 5.A (1) AT DENT AREA. NO FURTHER DEFECTS NOTED</P>)

Part: PANEL — DAMAGED (BS 1720) · airframe 98,092 hrs · 16,371 cycles

M/D - STA 1720 L/H DADO PANEL FOUND DAMAGE(<P>DAMAGE AREA REPAIRED AS PER RI-25-21-16797 REV A. NO FURTHER DEFECTS NOTED</P>)

Part: FITTING — CRACKED (BS 1000) · airframe 98,092 hrs · 16,371 cycles

1EA CRACK WAS FOUND ON BS 1000 LBL 11.33" INTERCOSTAL LUG FTG APPROX 1"(<P>CRACK INTERCOSTAL LUG FTG REPLACED AS PER ATLAS AIR EO 4453C024 REV 3 PART 3. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 98,092 hrs · 16,371 cycles

LHW O/B FORE FLAP FOUND DELAMINATED(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-17 PAR 5.A.(1). NO FURTHER DEFECTS NOTED</P>)

Part: DOOR — CHAFED (NR 1 NACELLE) · airframe 98,092 hrs · 16,371 cycles

#1 ENG RH CORE COWL PRESSURE RELIEF DOOR INTERNAL UPPER FND 1EA FRAME CHAFING(<P>FRAME CHAFING AREA REPAIRED AS PER EO 1971A308 REV 0. NO FURTHER DEFECTS NOTED&NBSP;</P>)

Part: PANEL — CRACKED (BS 1940) · airframe 98,092 hrs · 16,371 cycles

M/D STA 1940 L/H DADO PANEL FOUND CRACK(<P>CRACK AREA REPAIRED AS PER RI-25-21-16795 REV A. NO FURTHER DEFECTS NOTED</P>)

Part: TENSION TIE — CRACKED (BS 860) · airframe 98,092 hrs · 16,371 cycles

LH BS 860 UPR DECK TENSION TIE 1EA FASTENER HOLE FOUND CRACK ON FWD CHANNEL(<P>FWD CHANNEL REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED</P>)

Part: NOT REPORTED — CRACKED (BS 2231 S23L) · airframe 98,092 hrs · 16,371 cycles

2EA CRACK WERE FOUND ON LH BS 2231 S23L FASTENER HOLE(<P>CRACK AREA REPAIRED AS PER SRM 53-60-15-2R-2 REPAIR 2 FIG 201 DETAIL II, THIS REPAIRED IS CAT B. NO FURTHER DEFECTS NOTED</P>)

Part: ANGLE — CORRODED · corrosion level 2 · airframe 90,140 hrs

CORROSION - ANGLE, LOWER FUSELAGE INSIDE OF WING TO BODY FAIRING NO. 191DAL AT STA 960 TO STA 985, LBL 4(<P>REMOVED DAMAGE PART IAW SRM 51-40-02 REV 94. INSTALL NEW PART IAW SRM 51-40-02 REV 94 ANF DWG # 65B06976 SH 2 REV G. JOB COMPLETED AND COND CHK NML.</P>)

Part: SKIN — DENTED (RT SPOILER) · airframe 90,140 hrs

DENT - RH WING INBD #8 SPOILER UPPER SKIN(<P>CUT OUT THE DAMAGE MATERIAL AND CLEAN.MEASURE THE DAMAGE SIZE L=2.6", W=1.5", 2/3" FROM INBD EDGE, 2" FROM AFT EDGE. BOND REPAIR FILLER AND DOUBLER WITH FILM ADHESIVE. CURE AT 250 DEGREES F FOR 120 MINS. MAINTAIN MINIMUM VACUUM PRESSURE. IAW SRM 57-70-02-2R-1. COND CHK NML.</P>)

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 90,140 hrs

FOUND MD FLOOR STRUCTURE SUPPORT CORROSION AT STA 2376, RBL 16(<P>REMOVED DAMAGE PART IAW SRM 51-40-02 REV 94. INSTALLED NEW PART IAW SRM 51-40-02 REV 94 AND DWG #65B38754 SH 8 REV A. JOB COMPLETED AND COND CHK NML.</P>)

Part: WEB — CRACKED (BS 1480) · airframe 90,119 hrs

CRACK ON THE WEB OF STA 1480 BULKHEAD FRAME AT LBL 80 AND WL 120(<P>REPAIRED DAMAGED AREA IAW EI #T2022A53M-710 REV 1. CONDITION NORMAL AND JOB COMPLETED</P>)

Part: SKIN — CORRODED (BS 840) · corrosion level 2 · airframe 90,119 hrs

CORROSION - SKIN SURFACE LWR FUESLAGE INSIDE OF WING TO BODY FAIRING AT STA 840, S-44L &AMP; S-45L(<P>REM0VE DAMAGE AREA FASTENERS IAW SRM 51-40-02 REV 94. ACCOMPLISH <SPAN>EI # T2022A53M-746 REV 1 &AMP; DWG #142A3544 SHEET 7 REV B AND DWG #142A3784 SHEET 12 REV F. JOB COMPLETED &AMP; COND CHK NORMAL.</SPAN></P>)

Part: SEAT TRACK — CORRODED (BS 960-980) · corrosion level 2 · airframe 90,119 hrs

CORROSION ON MD SEAT TRACK BETWEEN STA 960 AND 980, LBL 11.33(<P>PERFORMED SEAT TRACK REPAIR IAW<SPAN>EI # T2022A53M-788 REV 1. INSTALL REPAIR IAW SRM 51-40-02 REV 94 AND DWG #65B38252 SHEET 14 REV . JOB COMPLETED &AMP; COND CHK NORMAL.</SPAN></P>)

Part: STRAP — CRACKED · airframe 90,119 hrs

CRACK DAMAGES ON THE STRAP AND INNER CORD OD STA 2231 FRAME AT S-16L &AMP; S-17L(<P>ACCOMPLISHED THE REPAIR IAW&NBSP;<SPAN>EI # T2022A53M-748 REV 1 AND SRM 53-60-15-2R-2 REPAIR 2 REV 94 AND DWG #65B0500 SH 19 REV D. JOB COMPLETED AND COND CHK NORMAL.</SPAN></P>)

Part: NONE — NONE · airframe 90,119 hrs

MISSING RECORD OF EXISTING REPAIR DOUBLER ON FUSELAGE SKIN BETWEEN STA 460 &AMP; STA 480, S-37R &AMP; S-39R(<P>PERFORMED FUSELAGE SKIN REPAUR DOUBLER IAW SRM 51-40-02 REV 94 &AMP;&NBSP;<SPAN>EI # T2022A53M-841 REV 1. JOB COMPLETED AND COND CHK NORMAL.</SPAN></P>)

Part: TRACK — CORRODED · corrosion level 2 · airframe 90,140 hrs

FOUND MD SUBSTITUTE TRACK CORROSION AT STA 720 LBL 75.92(<P>ACCOMPLISHED THE REPAIR IAW SRM 53-00-52-2R-13 REPAIR 13 REV 94, DWG# 65B38250 SH 17 REV A &AMP; SH 9 REV B. COND CHK NML AND JOB COMPLETED.</P>)

Part: SEAT TRACK — CORRODED (BS 2060) · corrosion level 2 · airframe 90,119 hrs

CORROSION DAMAGE ON THE SEAT TRACK OF MD BETWEEN STA 2060 &AMP; STA 2110.45 AT LBL 98.58.(<P>REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02 REV 94. ACCOMPLISHED&NBSP;<SPAN>EI # T2022A53M-704 REV 2 AND SRM 53-02-52-2R-6 DETAIL III REV 94. REINSTALLED FASTENERS IAW SRM 51-40-02 REV 94. COND CHECK NORMAL AND JOB COMPLETED.</SPAN></P>)

Part: SEAT TRACK — CRACKED (BS 2268) · airframe 90,119 hrs

FOUND CRACK DAMAGE ON CROWN OF SEAR TRACK OF MD AT STA 2268, LBL 33.99(<P>REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02 REV 94. REPAIRED DAMAGED AREA IAW SRM 53-00-52-2R-6 REPAIR 6 REV 94 &AMP; <SPAN>EI # T2022A53M-720 REV 1. INSTALLED FASTENERS IAW SRM 51-40-02 REV 94. JOB COMPLETED AND COND CHK NORMAL.</SPAN></P>)

Part: SKIN — CORRODED · airframe 90,119 hrs

CORROSION DAMAGES ON INNER SURFACE OF FUSELAGE SKIN DURING PERFORMING INSP PER SB 747-53A2878(<P>REPAIR DAMAGE AREA IAW EI NO. T2022A53M-636 REV 2. JOB COMPLETED</P>)

Part: WEB — CRACKED (BS 1480) · 14,993 cycles

CRACK ON THE WEB OF STA 1480 BULKHEAD FRAME AT RBL 110 AND WL 150(<P>REMOVE FASTENERS IAW SRM 51-40-02 REV 94. PERFORM WEB REPAIR IAW EI # T2022A53M-716 REV 1. COND CHK NORMAL AND JOB COMPLETED.&NBSP;</P>)

Part: SKID SHOE — CORRODED · airframe 90,140 hrs

CORROSION - MD CGO FUSELAGE SKIN AREA AT STA 1000 FWD S-16R TO S-17R(<P>ACCOMPLISHED&NBSP;<SPAN>EI # T2022A53M-636 REV 2. ATTACHED TO W/O 6828148. JOB COMPLETED.</SPAN></P>)

Part: FLOORBEAM — CORRODED (BS 2240) · corrosion level 2 · airframe 90,119 hrs

REPAIR CORROSION ON FLOOR BEAM UPPER CAP AT STA 2240 BETWEEN LBL 67.01 &AMP; LBL 90(<P>REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02 REV 94. REPAIR DAMAGE AREA IAW SRM 53-00-51-2R-3 REPAIR 3 REV 94 AND&NBSP;<SPAN>EI # T2022A53M-727 REV 1. INSTALLED FASTENERS IAW SRM 51-40-02-REV 94 AND DWG #65B38112 SHEET 13 REV 4. JOB COMPLETED &AMP; COND CHK NORMAL.</SPAN></P>)

Part: FLOORBEAM — CORRODED (BS 1500) · corrosion level 2 · airframe 90,119 hrs

FOUND MD FLOOR BEAM CORROSION AT STA 1500, RBL 90(<P>ACCOMPLISHED EI #T2022A53M-734 REV 2 AND DWG #65B38075 SHEET 11. JOB COMPLETED</P>)

Part: TRACK — CRACKED · airframe 90,140 hrs

CRACK - SUBSTITURE TRACK, MID CGO COMPT UNDER FLOOR AT B.S 995, LBL 75.92(<P>ACCOMPLISHED THE REPAIR IAW SRM 53-00-52-2R-13 REPAIR 13 REV 94 &AMP; DWG # 65B38250 SH 9 REV B. &AMP; 65B16004 SH 4 REV A. COND CHK NML &AMP; JOB COMPLETED.</P>)

Part: FLOORBEAM — NOT REPORTED · 14,995 cycles

DEVIATION FOUND DURING PERFORMING SB 4453A087 PART 2 ON UPPER DECK FLOOR BEAM(<P>ACCOMPLISHED JOB IAW EI # T2022A53M-820 REV 1. JOB COMPLETED AND COND CHK NML.</P>)

Part: INTERCOSTAL — CORRODED · corrosion level 2 · airframe 90,140 hrs

FOUND BULK CGO SLOPING SIDEWALL STRUCTURE INTERCOSTAL CORROSION AT STA 1960 - 1980, S-38R(<P>REMOVED DAMAGE PART IAW SRM 51-40-02 REV 94. INSTALL NEW INTERCOSTAL IAW SRM 51-40-02 REV 94 AND DWG #65B04652 SH 2 &AMP; DWG #65B04153 SH 13 REV B &AMP; 146U3009 SH 4 REV D. JOB COMPLETED AND CONDITION CHK NML.</P>)

Part: SQUIB — NO TEST (FIRE EXINGUISHER) · 14,987 cycles

FIRE EXT SQUIB TEST CH A INOP(<P>TRANSFERRED TO MDDR 160810 PER MEL 26-21-01-01, CAT C. DUE DATE 14 FEB 22.</P> / <P>5 FEB 22 - ICN - MAWEA POWER CB RECYCLED AND CARGO FIRE SYSTEM PERFORMED IAW AMM 26-23-00/501.</P>)

Part: ACTUATOR — MALFUNCTIONED (CNTR GEAR STEERI) · airframe 83,162 hrs · 13,798 cycles

MASTER WARNING FOR CONFIG GEAR CTR BODY GEAR STR CTR ON TAKE OFF, REJECTED TAKEOFF. REMOVED AND REPLACED THE RIGHT BODY GEAR STEERING ACTUATOR IAW AMM 32-53-11-404-010. OPS CHECKED GOOD. OK FOR SERVICE.

Part: FLOORBEAM — CORRODED (BS 1500) · corrosion level 2 · airframe 82,485 hrs · 13,672 cycles

FOUND THE MAIN DECK CARGO FLOORBEAM CORRODED AT BS 1500, LBL 12 TO 15. REPAIRED DAMAGED AREA IAW SRM 53-00-51 REPAIR 3, REV 88, AND EI T2020A53M-1457, REV 2, AND DWG 65B38075 SH 11, REV -, SH 12 REV -, SH 13 REV A.

Part: CARGO TRACK — CORRODED (BS 1790-1990) · corrosion level 2 · airframe 82,485 hrs · 13,672 cycles

CORROSION FOUND ON THE M/D CARGO TRACK BETWEEN BS 1790 AND 1990, LBL 98.58. REPAIRED THE DAMAGED AREA IAW SRM 53-00-52, REPAIR 5, DETAIL III, REV 88, AND EI T2020A53M-1476, REV 3, AND DWG 65B38251 SH 04, REV -, SH 65 REV -, 65B38306 SH6 REV A.

Part: SKIN — CRACKED (BS 980) · airframe 82,485 hrs · 13,672 cycles

A CRACK WAS FOUND ON THE FUSELAGE SKIN UNDER THE DRAG SPLICE FITTING NEAR BS 980 STRINGER 38R. REPAIRED THE DAMAGED AREA IAW SRM 53-20-01-2R-2, REPAIR 2, REV 88, AND EI T2020A53M-1510, REV 2, AND EI T2020A53M-1419, REV 1, ATTACHED TO W/O 4641182.

Part: SKIN — CORRODED (BS 1720) · corrosion level 2 · airframe 82,485 hrs · 13,672 cycles

CORROSION FOUND ON THE UPPER SURFACE OF THE FUSELAGE SKIN PANEL AT BS 1720, BL 0. REPAIRED THE DAMAGED AREA IAW EI T2020A53M-1455, REV 2.

Part: SKIN — CRACKED (BS 980) · airframe 82,485 hrs · 13,672 cycles

CRACK ON SKIN PANEL UNDER THE DRAG SPLICE FITTING AT STA 980 S-38L. REPAIRED DAMAGED AREA IAW SRM 53-20-01-2R-2, REPAIR 2 REV 88, EI T2020A51M-1482 REV 1, AND T2020A53M-1419 REV 1. CONDITION CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 82,485 hrs · 13,672 cycles

FOUND EMERGENCY LIGHT BATTERY PACK M5169 INOPERATIVE. IAW AMM 33-51-04-902-001 REV 98, REPLACED M5169 EMERGENCY LIGHT BATTERY PACK. IAW AMM 33-51-04-902-001-001, REV 98. PERFORMED AN EMERGENCY LIGHT TEST, AND THE RESULT WAS SATISFACTORY.

Part: WIRE — BROKEN (APU IGNITION) · airframe 82,485 hrs · 13,672 cycles

FAULT HISTORY REPORT FOUND APU IGNITION UNIT STUCK ENERGIZED CMC MSG: 49078. IAW FIM 49-11 TASK 879 REV 98 AND WDM 49-11-16 REV 48 AND SSM 49-11-01 REV 48 PERFORMED WIRE CONTINUITY AND INSULATION CHECK. FOUND WIRE W7242-008-20 BROKEN. IAW SWPM 20-30-11 REV 13 AND SWPM 20-03-19 REV 73 AND WDM 49-11-16 REV 48, REPLACED W7242-008-20. IAW WDM 49-11-16 REV 48 PERFORMED COND CHECK AND RESULT WAS SATISFACTORY. IAW AMM 49-11-00-705-017 REV 98 PERFORMED GROUND TEST OF APU AND RESULT WAS SATISFACTORY.

Part: SEAT TRACK — CORRODED (BS 830-870) · corrosion level 2 · airframe 82,485 hrs · 13,672 cycles

FOUND CORROSION ON THE MAIN DECK CARGO SEAT TRACK BETWEEN BS 830 AND 870, LBL 11.33. REPAIRED DAMAGED AREA IAW SRM 53-00-52, REPAIR 12, DETAIL III, REV 88, AND DWG T2020A53M-1484, REV 1, AND DWG 65B8352 SH 13, REV -.

Part: SEAT TRACK — CORRODED (BS 1973-2085) · corrosion level 2 · airframe 82,485 hrs · 13,672 cycles

CORROSION - FOUND M/D CGO SEAT TRACK CORROSION AT BS 1973, 2003, 2052-2055, 2080-2085, RBL 11.33. REPAIRED DAMAGED AREA IAW SRM 53-00-52 REPAIR 12 DETAIL I REV 88, EI T2020A53M-1489 REV 2, AND DWG 65B38253 SH 51 REV A, SH 52 REV A, SH 53 REV -. CONDITION CHECKED NORMAL.

Part: SKIN — BROKEN (RT WING AILERON) · airframe 82,485 hrs · 13,672 cycles

RT WING INBD AILERON UPPER SURFACE SKIN WBL 514 AREA BROKEN. REMOVED THE DAMAGED MATERIAL AREA AT INBD AILERON OUTBD EDGE AFT EDGE AND CLEAN BONDED WITH REPAIR, CURED THE RESIN AT 150 DEGREES F FOR 180 MINUTES, MAINTAINED PRESSURE IAW SRM 57-00-01-2R-1 REFER TO SRM 51-70-06-0G REV 85. CHECK CONDITION WAS SATISFACTORY.

Part: CARGO TRACK — CORRODED (BS 510-750) · corrosion level 2 · airframe 82,485 hrs · 13,672 cycles

CORROSION FOUND ON THE MAIN DECK CARGO TRACK BETWEEN BS 510 AND 570, RBL 11.33. REPAIRED DAMAGED AREA IAW SRM 53-00-52-2R-12 DETAIL I AND EI T2020A53M-1473 REV 1 AND DWG 65B38252 SH 9 REV -, SH 10 REV -, SH 11 REV -, SH 12 REV -.

Part: STRUCTURE — CORRODED (BS 1237-1477) · corrosion level 2 · airframe 82,485 hrs · 13,672 cycles

FOUND MAIN DECK CARGO UPPER CHORD CORRODED AT BS 1267 TO 1271, 1330, 1364, 1368, 1383 -1384, 1403 - 1404, 1477, RBL 11. REMOVE THE DAMAGED PART IAW SRM 51-40-02 REV 88. INSTALL NEW PART IAW SRM 51-40-02 REV 88 AND DWG 65B24600 SH 18 REV B, SH 19 REV C, SH 20 REV B. CHECKED NORMAL.

Part: SEAT TRACK — CORRODED (BS 1050-1265) · corrosion level 2 · airframe 82,485 hrs · 13,672 cycles

CORROSION DAMAGE FOUND ON THE MAIN DECK SEAT TRACKS BETWEEN BS 1050 AND 1265, LBL 11. REPAIRED THE DAMAGED AREA IAW SRM 53-40-52, REPAIR 3, FIG 201, REV 88, AND EI T2020A53M-1472, AND DWG 11140801, SHEET 01, REV B.

Part: SEAT TRACK — CORRODED (BS 705-728) · corrosion level 2 · airframe 82,485 hrs · 13,672 cycles

CORROSION FOUND ON THE MAIN DECK CARGO SEAT TRACK AT BS 705 AND 728, RBL 11. REPAIRED DAMAGED AREA IAW SRM 53-00-52, REPAIR 12, DETAIL I, REV 88, AND EI T2020A53M-1473, REV 1, THAT ATTACHED TO W/O 4641285, AND DWG 65B38252 SH 10, REV -, SH 11 REV -, SH 12 REV -.

Part: STRUCTURE — CORRODED (BS 1268-1477) · corrosion level 2 · airframe 82,425 hrs · 13,672 cycles

CORROSION - FOUND M/D CGO UPPER CHORD CORROSION AT STA 1268, 1297, 1328, 1395-1396, 1435, 1477, LBL 11.(<P>REMOVE DAMAGED PART IAW SRM 51-40-02 REV 88. INSTALLED NEW PART IAW SRM 51-40-02 REV 88 AND BOEING DWG 65B24600 SH 18 REV B AND SH 19 REV C AND SH 20 REV B. JOB COMPLETED AND CONDITION CHECK NORMAL.&NBSP;</P>)

Part: SEAT TRACK — CORRODED (BS 510-750) · corrosion level 2 · airframe 82,485 hrs · 13,672 cycles

CORROSION - FOUND M/D CARGO SEAT TRACK CORROSION BETWEEN BS 510 AND 750, LBL 11.33. REPAIRED DAMAGED AREA IAW SRM 53-00-52 REPAIR 12 DETAIL II REV 88, EI T2020A53M-1483 REV 1, AND DWG 65B3D252 SH 9 REV -, SH 10 REV -, SH 11 REV -, SH 12 REV -. CONDITION CHECKED NORMAL.

Part: SEAT TRACK — CORRODED (BS 1050-1265) · corrosion level 2 · airframe 82,485 hrs · 13,672 cycles

CORROSION DAMAGE FOUND ON THE MAIN DECK SEAT TRACKS BETWEEN BS 1050 AND 1265, RBL 11. REPAIRED DAMAGED AREA IAW SRM 53-40-52-2R-3, REPAIR 3, FIG 201, REV 88, AND EI T2020A53M-1472, REV 2, AND DWG 11140801, SHEET 01, REV B. ORIGINAL EI T2020A53M-1472, REV 2 ATTACHING W/O 4641219 (540).

Part: SEAT TRACK — CORRODED (BS 750-930) · corrosion level 2 · airframe 82,485 hrs · 13,672 cycles

CORROSION - FOUND M/D CGO SEAT TRACK CORROSION BETWEEN BS 750 AND 930 RBL 11.33. REPAIRED DAMAGE AREA IAW SRM 53-00-52 REPAIR 12 DETAIL III (STA 830), DETAIL I (STA 930) REV 88 AND EI T2020A53M-1478 REV 1 AND DWG 65B38252 SH 12 REV -, SH 13 REV -, SH 18 REV B.

Part: SKIN — CORRODED (BS 1680) · corrosion level 2 · airframe 82,485 hrs · 13,672 cycles

CORROSION FOUND ON THE INNER FUSELAGE SKIN, AFT CARGO COMPARTMENT BS 1680, STRINGERS 50L TO 51R. REPAIRED THE DAMAGED AREA IAW EI T2020A53M-1426, REV 3.

Part: SEAT TRACK — CORRODED (BS 1530-1620) · corrosion level 2 · airframe 82,485 hrs · 13,672 cycles

CORROSION - FOUND M/D CARGO SEAT TRACK CORROSION AT STA 1530, 1570, AND 1620, LBL 11.33. REPAIRED DAMAGED AREA IAW SRM 53-00-52-2R-12 DETAIL 1 REV 88, EI T2020A53M-1480 REV 1, AND DWG 65B38253541 REV A, SH 47 REV -, SH 48 REV -, SH 49 REV -.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 81,439 hrs · 13,487 cycles

DOOR 1L DOOR SILL LIGHTS AND NEARBY OUTER DOOR LIGHTS FOUND NOT ILLUMINATED.(<P>EMERGENCY POWER SUPPLY BATTERY ASSY (M5170) REPLACED AND OPERATIONAL TEST CARRIED OUT. RESULT NORMAL IAW&NBSP;<SPAN>AMM 33-51-04.</SPAN></P>)

Part: ADC — MALFUNCTIONED · airframe 80,979 hrs · 13,394 cycles

REJECTED TAKE OFF AT 85 KTS DUE TO NO AIRSPEED ON F/O SIDE.&NBSP;(<P>REMOVED AND REPLACED ADC IAW AMM 34-12-01, OPS CHECK NORMAL AT THIS TIME.</P><P>ITEM M2: DUE TO REJECTED TAKEOFF, PERFORMED HIGH ENERGY STOP INSPECTION IAW AMM 32-12-01. ALSO PERFORMED TIRE INSPECTION IAW AMM 32-12-01. NO DEFECTS NOTED AND TIRES WITHIN LIMITS. OPS NORMAL AT THIS TIME.</P>)

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 78,924 hrs · 13,035 cycles

FUEL IMBALANCE. 2-3 EICAS WHEN USING CENTER TANK FUEL. FUEL GETS MOVED INTO MAIN TANK. CAUSED UNBAL EICAS.&NBSP; AFTER CENTER TANK AT APPROX 1.2/1.3 BALANCED 2/3. AT THAT POINT, THE FUEL TOTALIZER STARTED DROPPING BELOW, CALC UP TO 2.2/3 LESS. CENTER TANK DID NOT EMPTY UNTIL DESCENT. TANK 3 LEVEL VARIED BETWEEN .7 TO .6, REF TANK 2. TOTALIZER STEADILY DROPPED.&NBSP;(<P>PERFORMED FQIS TEST THROUGH CMC PER AMM 28-41-00. TEST PASSED. FOLLOWED FIM TASK 28-22-15. NO DEFECTS NOTED. FOLLOWED FIM TASK 28-43 TASK 812. CENTER TANK SCAVENGE PUMP, OPS CHECK NORMAL PER AMM 28-15-01. FQIS TEST PASSED PER AMM 28-20-01. NO DEFECTS NOTED.&NBSP;</P><P />)

Part: RUB STRIP — CORRODED (THRUST REVERSER) · airframe 76,869 hrs · 12,497 cycles

RUBSTRIP ASSY CORRODED. NR 1 ENG RT THRUST REVERSER T/E AT THE R1 POSITION. REMOVE AND REPLACED IAW SRM 51-40-02, REV 82.2,

Part: NOT REPORTED — CORRODED (BS 1220-1480) · airframe 76,069 hrs · 12,499 cycles

CORROSION LOCATIONS FOUND DURING SB 747-53A-878. REPAIR THE DAMAGE AREA IAW EI T2018 AS3M-2232 REV.3

Part: SKIN — DAMAGED (BS 2529) · airframe 76,069 hrs · 12,499 cycles

SCRATCHES WITH SHARP EDGE DENT ON SEC 48 FUSELAGE SKIN NEAR BS 2529.6 BETWEEN STRINGERS 46L AND 51L. REPAIRED THE DAMAGE IAW SRM 53-00-01-2R-1, REV 82, AND EI T2018 53M-2412, REV 1.

Part: FLOORBEAM — CORRODED (BS 1771) · airframe 76,069 hrs · 12,499 cycles

AFT CGO BAY FLOORBEAM BS 1771, LBL 25 - LBL 45 CORRODED. REMOVED AND REPLACED IAW SRM 51-40-02, REV.82, DWG 65806061542, REV R, AND DWG NO.65806061, SH3, REV.P.

Part: STIFFENER — CORRODED (BS 1460) · airframe 76,069 hrs · 12,499 cycles

CORROSION FOUND ON THE RT BODY GEAR STIFFENER AT BS 1460. REMOVED AND REPLACED IAW SRM 51-40-02-06-0, REV 82. EI T2018A53M-2359, REV 01, AND DWG 65815069, SH 6, REV.R 547 REV G.

Part: FLOORBEAM — DAMAGED (BS 1590) · airframe 76,069 hrs · 12,499 cycles

AFT CARGO BAY FLOORBEAM BS 1590, RBL 25 - RBL 45 DAMAGED. REMOVED AND REPLACED IAW SRM 51-40-02-061-0, REV 82, DWG 65B06061, SH2, REV R AND SRM 51-40-02-061-0, REV 82.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,069 hrs · 12,499 cycles

FOUND THE EMERGENCY LIGHT FUNCTION ABNORMAL IN THE UPPER DECK AREA. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY M5168 IAW AMM 33-51-04-902-001-001, REV 42 AND PERFORMED AN EMERGENCY LIGHT TEST. RESULT WAS SATISFACTORY.

Part: SPOILER — LACK OF LUBE (NR 7) · airframe 72,758 hrs · 11,947 cycles

DURING DECENT, 280 AIR SPEED, AT 15,000 FT, WITH RIGHT AUTOPILOT ENGAGED, EXTENDED THE SPEED BRAKES SLOWLY, THE AIRCRAFT TURNED 6 DEGREES TO THE LEFT. PERFORMED OPS CHECK ON SPOILER SYSTEM AND FOUND THE NR 7 SPOILER WAS SLOW TO EXTEND. ACCOMPLISHED LUBRICATION OF NR 7 SPOILER PANEL IAW AMM 12-00. PERFORMED FUNCTIONAL AND OPS CHECKS IAW AMM 27-61 AND THE AUTOLAND UNIQUE TEST WAS SUCCESSFUL.

Part: ACM — SEIZED (NR 3) · airframe 72,657 hrs · 11,924 cycles

UPON GEAR EXTENSION, EXPERIENCED GRINDING SOUND AND ACRID ODOR IN FLT DECK. FOUND PACK 3 SEIZED. REMOVED AND REPLACED THE ACM IAW AMM REF 21-51-04. OPERATIONAL CHECKED NORMAL IAW AMM 21-00-00-201.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,862 hrs · 11,173 cycles

FOUND BRACKET CORROSION AT FUSELAGE STA 920, BL0. REPLACED BRACKET, PN: 69B01805-3, 2EA IAW SRM 51-40-02-0G-0, REV 76 AND DWG NR 142U0130, SH1 REV A, DWG 65B06704, SH2, REV F. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 68,862 hrs · 11,173 cycles

CRACK ON MAIN DECK SEAT TRACK NEAR STA 1800, RBL 98.58. REPAIRED THE CRACKED SEAT TRACK IAW SRM 53-00-52, REPAIR 6, FIG 201, ALTERNATIVE 1, REV 76, EI T2016A53M-1359, REV 1. FASTENER IDENTIFICATION IAW DWG 65B38251, SH66. REV AND DWG 45741062, REV A. CONDITION CHECK NORMAL AND JOB COMPLETED.

Part: REPAIR — DEFORMED (CARGO DOOR) · airframe 68,862 hrs · 11,173 cycles

DEFORM ON EXISTING REPAIR AT FORWARD LOWER CORNER OF AFT CARGO DOOR SKIN. REPAIR DAMAGE AFT CARGO DOOR IAW EI T2016A52M-1338, REV 1. CONDITION CHECK NORMAL AND JOB COMPLETED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,862 hrs · 11,173 cycles

FOUND BEAM M/D, FLOORBEAM UPPER CAP HAD CORROSION AT STA 2160, LBL 2. EI T2016A53M-1372, REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,862 hrs · 11,173 cycles

FOUND BRACKET CORROSION AT FUSELAGE LOWER AREA BETWEEN STA 970 AND STA 980, BL3. REPLACED ANGLE IAW DWG 65B06976 ID0002, REV G AND SRM 51-40-02-0G-0, REV 76. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 68,862 hrs · 11,173 cycles

FOUND EMERGENCY LIGHTS DID NOT STAY ON FOR 15 MINUTES, X325, X326, M4914, L1382, L5730, L5731, L5732, L5734 IAW AMM 33-51-04-002-009-001 AND 33-51-04-402-012-001, REV 86. REPLACED POWER SUPPLY IAW AMM 33-51-04-402-012-001, REV 86 PERFORMED INSTALLATION TEST OF POWER SUPPLY AND THE RESULT WAS SATISFACTORY.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,862 hrs · 11,173 cycles

FOUND SEAT TRACK CORROSION AT STA 2190, RBL 11.35. PERFORMED SEAT TRACK REPAIR IAW EI T2016A53M-1347, REV 3. CONDITION CHECK NORMAL AND JOB COMPLETED.

Part: BRACKET — DAMAGED (FUSELAGE) · airframe 68,862 hrs · 11,173 cycles

FOUND M/D CARGO FLOOR SUBSTITUTE SEAT TRACK BRACKET AT STA 2010, LBL 75.92. ACCOMPLISHED REPAIR DAMAGE AREA IAW SRM 53-00-52. REPAIR REV 76 AND NR 65B38251, SHEET 32, REV AND SRM 51-40-02, REV 76. JOB COMPLETED AND CONDITION CHECK SATISFIED.

Part: MODULE — FAULTY (EXTINGUISH SYS) · airframe 68,862 hrs · 11,173 cycles

FOUND LOWER CARGO FIRE BOTTLE B, CHANNEL 2 CONNECTOR VOLTAGE ABNORMAL DURING TEST IAW AMM 26-21-01-004-001 AND 26-21-01-404-006, REV 86. REPLACED FIRE MODULE AND CONNECTION CHECK NORMAL IAW AMM 26-21-01-734-305, REV 86 PERFORMED FIRE CONTROL MODULE INSTALLATION TEST AND RESULT WAS SATISFACTORY.

Part: SKIN — DENTED (FUSELAGE) · airframe 68,262 hrs · 11,173 cycles

DENT FOUND ON RT FUSELAGE SKIN AT BS 510 BETWEEN S-40R TO S-41R. REPAIR DAMAGED FUSELAGE SKIN IAW T2016A53M-1325, REV 1. CONDITION CHECK NORMAL AND JOB COMPLETED.

Part: ACTUATOR — FAILED (MLG) · airframe 68,862 hrs · 11,173 cycles

THE LT WING LANDING GEAR ALTERNATE EXTENSION SYS ELECTRICAL ACTUATOR FUNCTION FAILED IAW AMM 32-36-01-004-001, REV 86, AMM 32-36-01-404-009, REV 86 REPLACED ELECTRICAL ACTUATOR IAW 32-36-06-705-009, REV 86, PFM OPERATION TEST RESULT WAS NORMAL. CONDITION CHECK SATISFACTORY.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,862 hrs · 11,173 cycles

FOUND CORROSION AT UPPER CAP OF MAIN DECK FLOORBEAM AT STA 2260, LBL 23. REPAIRED CORROSION AT UPPER CAP OF MAIN DECK FLOORBEAM AT STA 2260, LBL 23 IAW EI T2016A53M-1373, REV 1. CONDITION CHECK NORMAL AND JOB COMPLETED.

Part: WEB — CORRODED (RT WING) · corrosion level 2 · airframe 68,862 hrs · 11,173 cycles

CORROSION ON THE WEB OF RT WING OTBD L/E NEAR OLES 1536. REPAIR DAMAGE AREA IAW EI T2016A57M-1352, REV 1, DWG 65B10652, SHEET 8, REV AND DWG 65B12736, SHEET 4, REV B. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: ACTUATOR — BROKEN (SPOILER) · airframe 65,162 hrs · 10,406 cycles

BLOCK TURN BACK, LT SPOILER INDICATION DOES NOT MOVE FOR FLIGHT CONTROL CHECK. FOUND NR 4 SPOILER ACTUATOR ROD BROKEN. R & R NR 4 SPOILER ACTUATOR. OPERATIONAL & LEAK CHECKED OK IAW MM 27-61-05. LEFT SPOILER INDICATION OPERATES NORMAL.

Part: DRIVE UNIT — FAULTY (LE FLAP) · airframe 64,043 hrs · 10,182 cycles

DURING CRUISE HAD LE FLAP IN-TRANSIT, MAGENTA INDICATION, & 280KT IAS LIMIT OR SPEED DISPLAYED. STATUS MSG FLAP SYS MON. TURNED WAI TO ON, INDICATION WENT AWAY AFTER APPROX 2 MIN, THEN EICAS MSG FLAPS CONTROL & EXPANDED DISPLAY SHOWING LE SENSOR INOPERATIVE. R & R LE L3 FLAP DRIVE UNIT IAW AMM 27-81-03. OPERATIONAL CHECKED GOOD & NO FAULT PRESENT AT THIS TIME. FDU SERVICED IAW AMM 12-13-12-603-801.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,242 hrs · 9,839 cycles

EMERGENCY LIGHT OPERATION TEST FAILED AT MD CARGO L1 DOOR, NEXT TO STAIR WAY. LIGHT BULB REPLACED & OPERATION TEST CARRIED OUT, RESULT NORMAL.

Part: LENS — DEFECTIVE (CABIN) · airframe 62,242 hrs · 9,839 cycles

LEFT DOOR 1 CEILING EMERGENCY LIGHT LENS COVER FOUND POOR CONDITION. LT DOOR CEILING EMERGENCY LIGHT LENS COVER REPLACED & OPERATIONS CHECKED FOUND NORMAL IAW AMM 33-51-00.

Part: FLOOR SUPPORT — CRACKED (BS 1000) · airframe 60,417 hrs · 9,467 cycles

FLOOR SUPPORT CRACKED BS 1000, LBL 75.92. REPAIRED CRACK DAMAGE IAW SRM 53-00-52-2R-13, REPAIR 13.

Part: SKIN — CRACKED (BS 1735) · airframe 60,060 hrs · 9,396 cycles

DURING WALK AROUND A .75" CRACK WAS FOUND ON THE RT SIDE OF THE ACFT. FUSELAGE SKIN AT STATION 1735, S-42R. EO 4453A892 DOCUMENTS A CATEGORY B PERMANENT REPAIR ACCOMPLISHED IAW THE SRM 53-00-0, REPAIR 15, FIG 201. PART 2 OF THE EO REQUIRES AN INITAL HFEC INSPECTION AT 15,000 FLIGHT CYCLES WITH REPEAT HFEC INSPECTIONS PRIOR TO EVERY 6000 FLIGHT CYCLES.

Part: TRANSMITTER — FAILED (TE FLAPS) · airframe 59,110 hrs · 9,240 cycles

EICAS FLAPS DRIVE, DURING RETRACTION FROM 20 TO 10. OTBD T/E FLAPS STOPPED. SEEMED LT T/E FLAP REMAINED LOWER THAN RT. EXPANDED VIEW AND STATUS T/E FLAPS INDICATED. APPROX 50-55 MIN INTO FLT. EXPANDED VIEW EXTINGUISHED AND SYS APPEARED NORMAL. DURING HOLDING AND IN LANDING CONFIGURATION RETRACTED FLAPS FROM 25 TO 20. FLAPS DID NOT RETRACT TO 20 AND EXPANDED VIEW WAS NOT INDICATED. LOWERED FLAPS TO 25. REMAINED CONFIGURED FOR LANDING. FLAPS RETRACTED OK ON GROUND. (R & R LT OTBD T/E FLAP RVDT IAW AMM 27-58-01. OPS CHECK WAS GOOD IAW AMM 27-58-01/725-050. C/O L,C,R FCC TEST AND PASSED IAW AMM 27-51-00.)

Part: COMPUTER — FAILED

UNABLE TO ENGAGE ANY OF THE THREE AUTOPILOTS, CMC SHOWS AILERON SERVO C/FCC- C /FCC FAIL. R & R CENTER AND LEFT FCC IAW AMM 22-11-01-004-026. PERFORMED CMC TEST ON CENTER AND LT FCC PASSED REF 22-11-01 ALSO PERFORMED AUTOLAND UNIQUE TEST PASSED.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 58,436 hrs · 9,117 cycles

RT WING INBD AFT T/E FLAP DAMAGED AT WBL 178.46. PREPARED CLEANED AND REPAIRED AREA OF DAMAGE ON RT WING INBD AFT FLAP T/E AT STATION WBL 178.48 IAW SRM 57-51-01-2R1-1. REPAIR 1, FIG 201 SHEET 4 AND 8. IAW 250 DEGREE F; CORE. SRM 51-70-01.

Part: ROLLER — LOOSE (LT WING TE FLAP) · airframe 56,625 hrs · 8,786 cycles

LT WING INBD FOREFLAP, OTBD TRACK FWD UPPER FLIGHT LOAD ROLLER LOOSE WITH VERTICAL MOVEMENT WHEN TRACK GOES IN AND OUT. R & R BEARINGS IAW SB 747-57-2107; PERFORMED T/E SYSTEM OPS CHECK OK. FLAPS RETRACTION AND EXTENSION SEVERAL TIMES NORMAL IAW AMM 27-51-00.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 56,625 hrs · 8,786 cycles

RIGHT WING OTBD FOREFLAP LEADING EDGE WITH CHAFING DAMAGE. PREPARED, CLEANED AND REPAIRED RIGHT OTBD FORE FLAP LEADING EDGE DAMAGE IN LOCATIONS WBL 820.750, 818.00 IAW SRM 57-53-01-2R-1. REPAIR 1, FIGURE 201 SHEETS 5, 6, 9, 10 IAW 250 F CORE SRM 51-70-02.

Part: INTERCOSTAL — CRACKED (BS 1220) · airframe 55,701 hrs · 8,626 cycles

MAIN DECK, BS 1220, LBL 98-127 INTERCOSTAL WEB FOUND CRACKED. INTERCOSTAL WEB REPAIRED IAW SRM 53-40-51, REPAIR 5 AND RS NR R-53-41-3748, REV A.

Part: INTERCOSTAL — CRACKED (BS 1220) · airframe 55,701 hrs · 8,626 cycles

MAIN DECK, BS 1220, RBL 98-127 INTERCOSTAL WEB FOUND CRACKED. INTERCOSTAL WEB REPAIRED IAW SRM 53-40-51, REPAIR 5 AND RS NR R-53-41-37348, REV A.

Part: CHANNEL — CRACKED (BS 760) · airframe 55,701 hrs · 8,626 cycles

MAIN DECK, BS 760 RT TENSION TIE AFT CHANNEL CRACKED. CHANNEL REPAIRED IAW SRM 53-20-30-2R-1, REPAIR 1.

Part: CHANNEL — CRACKED (BS 740) · airframe 55,701 hrs · 8,626 cycles

MAIN DECK, BS 740 RT TENSION TIE FWD CHANNEL FOUND CRACKED. CHANNEL FASTENER HOLES REPAIRED IAW EO 4453A301 PART 2, STEP 5 AND SB T47-53A2502, FIG 11.

Part: NOZZLE — CRACKED (EXHAUST) · airframe 54,212 hrs · 8,367 cycles

DURING MX WALKAROUND, MX FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, BETWEEN APPROX THE 10 TO 12 O'CLOCK POSITION (LT SIDE) ON THE NR3 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 11" LONG AND IS 13" FROM AFT SIDE OF EXHAUST SLEEVE JUST IN FRONT OF NAC STA 349.236 IAW SRM 54-41-30 THE LENGTH OF THE CRACK IS OUT OF LIMITS. STOP DRILLED ENDS OF CRACK WITH A 0.125" DIAMETER HOLE.

Part: ACOUSTIC LINER — DAMAGED (THRUST REVERSER) · airframe 53,695 hrs · 8,271 cycles

DURING MX WALKAROUND AT MX FOUND DAMAGE TO THE NR 3 ENGINE THRUST REVERSER ACOUSTIC MESH. PERMANENT REPAIR WILL BE PERFORMED ON THE LT T/R PRIOR TO THE NEXT C-CHECK OR HIGHER AFTER PART 1.

Part: STRUCTURE — DAMAGED (BS 260) · airframe 51,840 hrs · 7,944 cycles

DURING LOADING OPERATIONS, THROUGH THE NOSE CARGO DOOR, LOADER DROPPED CAUSING DAMAGE TO BS 260, LBL10.75 &AMP; RBL 10.75, WL 195.8 - CANTED BULKHEAD STIFFENERS (2 EA.), CONSISTING IN EDGE CRACKS MEASURING 1.5 AND 2.5 INCHES LONG (REF FIG 1). DAMAGE TO THE STIFFENERS EXCEEDS THE SRM 53-10-08-1A-2 ALLOWABLE DAMAGE LIMITS.(DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS, INITIATE REPETITIVE DVIS AT EVERY 5 FC (FLIGHT CYCLES) AND PERMANENT REPAIR PRIOR TO THE ACCUMULATION OF 2,000 (FLIGHT HOURS) AFTER PART 1 IAW THE SRM 51-70-11.)

Part: ENGINE — VIBRATION · airframe 51,546 hrs · 7,922 cycles

ON TAKE-OFF ROLL, ENGINE VIBE 4 SHOWED 5.2. FELT A VIBRATION WHEN SELECTING MAX THRUST (VISUALLY INSPECTED INLET/EXHAUST OF ENGINE, MAG CHIP DETECTOR AND & NBSP; ENGINE LPT AREA COMPONENTS AMD VIBRATION PICKUP CONNECTOR & NBSP; ALL IAW FIM 71-00. PERFORMED BORO INSP OF HPC 1ST, 5TH,9TH AND 12TH STAGES, AND 1ST, 2ND, STAGE HPT IAW MM 72-00-00. FOUND ALL WITHIN MM LIMITS)

Part: SLEEVE — CRACKED (EXHAUST NOZZLE) · airframe 51,067 hrs · 7,818 cycles

DURING MX WALKAROUND, MX FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, STARTING AT APPROX THE 9 O'CLOCK POSITION ON THE NR 3 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 3" LONG AND IS APPROX .5" FROM THE T/E OF THE NOZZLE. IAW 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 0.098" DIAMETER HOLE, DVI EVERY 3 FLIGHT CYCLES; AND REMOVAL OF THE PART WITHIN 50 FC (FLIGHT CYCLES).)

Part: FLOORBOARD — DAMAGED (BS 400) · airframe 50,786 hrs · 7,797 cycles

DURING CARGO LOADING AT HSV; MX FOUND DAMAGE TO THE MAIN DECK FLOORBOARD AT BS 400, RBL 15 (REF FIG 1). THE DAMAGE IS 1.5 INCHES LONG AND ABOUT 0.125 INCH WIDE. (PART 1: REMOVE LOOSE MATERIAL AND CLEAN UP THE EDGES OF THE DAMAGED FLOOR PANEL SRM 51-20-01. SEAL THE DAMAGED AREA USING SPEED TAPE AND SEALING RESIN IAW SRM 53-00-50, FIG 101, NOTE C. PART 2 OF THIS EO ACCOMPLISHES REPETITIVE DETAILED INSPECTIONS OF THE PART 1 REPAIR TO ENSURE CONTINUED AIRWORTHINESS. ACCOMPLISH PART 3 OF THIS EO AT THE NEXT A-CHECK AFTER PART 1. PERMANENT REPAIR IAW PART 3 OF THIS EO TERMINATES THE PART 2 INSP.)

Part: EEC — MALFUNCTIONED (NR 1 ENGINE) · airframe 50,575 hrs · 7,735 cycles

AFTER ENGINE START, NR 1 ENGINE WENT TO IMMED T/O THRUST UNCOMMAND. ENGINE SHUTDOWN PERFORMED. FAULT CONFIRMED ON GROUND RUN, 101 PERCENT IN EEC NORMAL MODE. EEC ALT MODE SELECTED AND ENG RUN C/O SATIS. NR 1 ENG ECU REPLACED IAW AMM.

Part: COMPRESSOR — SMOKE (POTABLE WATER) · airframe 50,030 hrs · 7,668 cycles

DURING OFFLOAD, LOADMASTER NOTED SMOKE COMING OUT OF THE RT SIDE VENT AT STA 850. ISOLATED SMOKE TO POTABLE WATER COMPRESSOR, INSPECTED GENERAL AREA AND NO ABNORMALITIES FOUND. POTABLE WATER COMPRESSOR INOPERATIVE AND POTABLE WATER SYS DEACTIVATED.

Part: STRUCTURE — DENTED (BS 1820) · airframe 44,080 hrs · 6,640 cycles

DURING WALK-AROUND INSP, DAMAGE WAS FOUND TO THE LOWER LOBE - BS 1820, WL 188 - LOWER AFT CARGO DOOR CONSISTING OF A DENT. LENGTH: 10 IN. WIDTH: 2.0 IN. DEPTH:0.175 (REF. FIG 1). THE DAMAGE IS OUT OF THE SRM 52-30-01, FIG 101, ALLOWABLE DAMAGE 1, DETAILS XI AND XII.

Part: SKIN — DAMAGED (RT STAB) · airframe 49,402 hrs · 7,537 cycles

DURING DEICING ON 19DEC2010, THE R STABILIZER FIXED T/E PANEL WAS STRUCK AT STABILIZER BL 418. THE DAMAGE MEASURES APPROX 1.375 INCH DEEP BY 1.500 INCH WIDE AS SHOWN IN FIG 1. (THE REPAIR IAW PART 1, THE REPETITIVE INSP IAW PART 2 ARE APPROVED BY DER ON THE 8110-3 DATED 19DEC2010. THE PERMANENT REPAIR IAW PART 3 IS APPROVED IAW THE SRM.)

Part: FLOORBOARD — GOUGED (BS 1520-1580) · airframe 49,040 hrs · 7,476 cycles

DURING WALK AROUND INSP, MX FOUND GOUGES/DAMAGE TO THE MAIN DECK - FLOORBOARDS (2 EA) BS1520 - BS1580, LBL68.0 (REF FIG 1). (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS, INITIATE REPETITIVE DVIS AT EVERY 1000 FH (FLIGHT HOURS) AND PERMANENT REPAIR PRIOR TO, OR AT THE NEXT C-CHECK AFTER PART 1 IAW THE SRM 53-00-50, REPAIR 1.)

Part: RIB — BROKEN (LT WING) · airframe 47,752 hrs · 7,255 cycles

DURING A-CHECK, THE 69B12755-5 STIFFENER ON THE LT WING T/E RIB WBL515 WAS FOUND TO HAVE A BROKEN OUT SECTION DUE TO INTERFERENCE WITH THE LT WING OTBD MID-FLAP INBD END GUIDE ROLLER. (THE STIFFENER IS MADE FROM 0.063 INCH CLAD 2024-T3 IAW DWG 69B12755. PART 1, IS TO BE DONE TO PROVIDE AN EXTRA MEASURE OF CLEARANCE AFTER CHECKING AND IF NEEDED RIGGING THE FLAPS, A NEW STIFFENER WILL BE FABRICATED WITH LESS FLANGE WIDTH. PART 2, IS TO BE ACCOMPLISHED EVERY 1000 FLIGHT HOURS TO ENSURE THAT NO FURTHER CONTACT IS MADE BETWEEN THE GUIDE ROLLER AND STIFFENER UNTIL PART 3, PERMANENT REPAIR IS ACCOMPLISHED AT THE NEXT SCHEDULED C-CHECK.)

Part: SKIN — DAMAGED (BS 2360-2484) · airframe 46,988 hrs · 7,140 cycles

DURING D-CHECK IN TPE, WRINKLES WERE FOUND IN THE 65B02697-122, BS 2360-2484, S-23L TO -46L SKIN (SEE FIG 1 AND 2) WHILE THE TAIL WAS UNSUPPORTED. (FASTENERS WERE REMOVED FROM THE WRINKLED AREA AND SHIMS WERE INSTALLED TO REMOVE THE WRINKLES.)

Part: UNKNOWN — UNKNOWN (FLT CONTROLS) · airframe 44,109 hrs · 6,668 cycles

FLYING WITH AUTOPILOT OFF, EXTENDED SPEEDBRAKES TO FLIGHT DETENT, ACFT ROLLED HARD LEFT, INTERMITTENT. WITH AUTOPILOT ENGAGED, EXTENDED SPEEDBRAKES TO FLIGHT DETENT, YOKE MOVES RIGHT APPROX 2 UNITS TO MAINT WING LEVEL, ALSO INTERMITTENT. ACCOMPLISHED VISUAL INSP OF SPOILERS, NO DEFECTS, GROUND OPS CHECK OF SPOILERS IAW AMM OK. ACCOMPLISHED GROUND, OPS CHECK OF SPEEDBRAKE SEQUENCE MECHANISM IAW AMM, SHEAR PINS NORMAL, PERFORMED RIG CHECK, ALL NORMAL.

Part: SKIN — CRACKED (RT NACELLE) · airframe 43,924 hrs · 6,614 cycles

RT NR3 CORE COWL UPPER AFT AREA FAIRING OUTER SKIN AT NAC STATION 296.25 TO 304.5 HAS A 8.250 INCH CRACK. TIME LIMITED REPAIR WAS ACCOMPLISHED IAW SRM 51-40-02-06-0 AND EO 4471A043. TO INSPECT OR ACCOMPLISH PERMANENT REPAIR NEXT A-CHECK.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 43,924 hrs · 6,614 cycles

MAIN DECK SIDE DOOR AREA AT LT, FS 1806.95 TO 1809.95, LBL99 SEAT TRACK CROWN LUG HAS A 3.0 INCH CRACK. PERMANENT REPAIR ACCOMPLISHED IAW SRM 53-00-52-2R-6 REPAIR 6 AND EO 4453A271.

Part: SEAT TRACK — CRACKED (BS 1806.95) · airframe 43,924 hrs · 6,614 cycles

MAIN CARGO SIDE DOOR AREA - SEAT TRACK LUG CRACKED AT FS 1806.95 LBL 99 NEXT TO ROLLOUT STOP ASSY. NR 1 POSITION."PERMANENT REPAIR PERFORMED IAW THE SRM 53-00-52-2R-6, REPAIR 6."

Part: FAIRING — CRACKED (NR 3 NACELLE) · airframe 43,924 hrs · 6,614 cycles

ENG 3 OTBD CORE COWL UPPER AFT AREA FAIRING HAS A CRACK. ON THE AFT UPPER EDGE. DUE TO NO STOCK FOR THE PANEL, DISPOSITION WAS TO ACCOMPLISH A TIME LIMITED REPAIR BY WELDING THE CRACK IAW STANDARD PRACTICES AND REPLACEMENT OF FAIRING WITHIN THE NEXT 2A CHECK.

Part: FAIRING — CRACKED (NR 3 NACELLE) · airframe 43,924 hrs · 6,614 cycles

ENG 3 OTBD CORE COWL UPPER AFT AREA FAIRING HAS A CRACK. ON THE AFT UPPER EDGE. DUE TO NO STOCK FOR THE PANEL, DISPOSITION WAS TO ACCOMPLISH A TIME LIMITED REPAIR BY WELDING THE CRACK IAW STANDARD PRACTICES AND REPLACEMENT OF FAIRING WITHIN THE NEXT 2A CHECK.

Part: FAN — FAILED (E/E BAY) · airframe 42,795 hrs · 6,403 cycles

ON "TAXI IN" THERE WAS AN ODOR OF ELECTRICAL BURNING IN THE COCKPIT. ALSO, E/E COOLING FAN STATUS MESSAGE. FOUND E/E FAN FAILED AND DEFERRED FAN PER MEL 21-58-4. ALSO, PERFORMED CONDITIONAL INSPECTION PER AMM 05-51-56. NO FURTHER TROUBLE FOUND. NO PARTS CHANGED AT THIS TIME.

Part: SKIN — DAMAGED (RT WING AILERON) · airframe 42,732 hrs · 6,395 cycles

THE PURPOSE OF THIS EO IS TO RECORD A MAJOR REPAIR. DURING C-CHECK INSP; DAMAGE WAS FOUND TO THE RT INBD AILERON UPPER SURFACE OTBD T/E CORNER MEASURING 0.5 IN. X 1.0 IN. (REF FIG 1). PERMANENT REPAIR PERFORMED IAW THE SRM 51-70-06 FIG 5.1. ACCOMPLISH REPAIR TO THE RT INBD AILERON UPPER SURFACE OTBD T/E CORNER DAMAGE IAW SRM 51-70-06 FIG 5 (REF FIG 1). RESTORE ACFT TO A SERVICEABLE CONFIGURATION.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 42,732 hrs · 6,395 cycles

ACCOMPLISH REPAIR TO THE LT INBD AFT FLAP, LOWER SURFACE INBD FWD AREA OF DELAMINATION IAW SRM 57-53-01 FIG 201,SRM 51-70-07 (REF FIG 1). ACCOMPLISH REPAIR TO THE RT INBD FORE FLAP, INBD T/E LOWER SURFACE DAMAGE IAW SRM 57-53-01, FIG 201, RPR 1 TABLE I AND THE SRM 51-70-07 (REF FIG 2). ACCOMPLISH REPAIR TO THE RT INBD MID FLAP UPPER SURFACE AT OTBD T/E DELAMINATION IAW THE SRM 57-53-01, FIG 201,AND SRM 51-70-07, FIG 5. (REF FIG 3). ACCOMPLISH REPAIR TO THE RT OTBD AFT FLAP T/E LOWER EXTERNAL SURFACE AREA OF DELAMINATION IAW SRM 57-53-01 FIG 201, SRM 51-70-07 FIG. 5. (REF FIG 4). ACCOMPLISH REPAIR TO THE RT OTBD FORE FLAP L/E WORN/DELAMINATED AREAS IAW SRM 57-53-01 FIG 201, SRM 51-70-07 (REF FIG 5). ACCOMPLISH REPAIR TO THE LT INBD FORE FLAP DAMAGE IAW SRM 57-53-01 FIG 201,AND THE SRM 51-70-07 (REF FIG 6). ACCOMPLISH REPAIR TO THE LT INBD FORE FLAP L/E MID AREA PUNCTURE/DAMAGE IAW SRM 57-53-01 FIG 201, SRM 51-70-07 (REF FIG 7).

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 41,915 hrs · 6,297 cycles

CREW REPORTED EQUIPMENT SMOKE STATUS MESSAGE DISPLAYED AFTER LANDING. EXISTING FAULTS REVIEWED , NO RELATED FAULTS NOTED. EQUIPMENT TEST WITH NO FAULTS RESULTS. ACFT WAS RELEASED WITH NO FURTHER MESSAGES.

Part: PANEL — PUNCTURED (BS 1660-1680)

AFT CARGO COMPARTMENT TORQUE BOX TOP PANEL AT STA 1660 TO 1680 RT SIDE FOUND PUNCTURED AT 2 LOCATIONS. TORQUE BOX TOP PANEL REPAIRED IAW EO. (K)

Part: SUPPORT BEAM — CRACKED (CARGO DOOR) · airframe 36,614 hrs · 5,511 cycles

MAIN DECK CARGO SIDE DOOR AREA, SUPPORT BEAM BETWEEN STA 1820-1840 AND 1840-1860 LBL 102.250, CRACKED AND DENTED. PERMANENT REPAIR ACCOMPLISHED AS PER ATLAS AIR XEO 53-110607, BOEING DRAWING 65B17951 AND FAA FORM 8100-9.

Part: SEAT TRACK — CRACKED (BS 1850-1920) · airframe 36,614 hrs · 5,511 cycles

MAIN DECK CARGO SIDE DOOR AREA, SEAT TRACK DAMAGED AND CRACKED AT STA 1850 AND 1920, LBL 99.0. PERMANENT REPAIR ACCOMPLISHED AS PER B747-400 SRM 53-00-52 FIG 201, REPAIR 6. REFERENCE ATLAS AIR XEO NR 53-110607.

Part: STRUCTURE — ERODED (LT NACELLE) · airframe 36,614 hrs · 5,511 cycles

NR 2 ENGINE LT FAN COWL L/E HAS 78.0 INCH AREA OF EROSION AT L/E. PERMANENT REPAIR ACCOMPLISHED AS PER B747-400 SRM 54-21-01, REPAIR 6. REFERENCE ATLAS EO NR 4471A009.

Part: ACCESS PANEL — DAMAGED (THRUST REVERSER) · airframe 36,000 hrs · 5,394 cycles

NR 1 ENGINE REVERSER RIGHT SIDE LOWER AFT SECTION TENSION LATCH ACCESS PANEL SEVERAL RIVETS MIGRATED. REMOVED AND REPLACED MIGRATED RIVETS IAW SRM 51-40-02.

Part: COWL FASTENER — DAMAGED (THRUST REVERSER) · airframe 36,000 hrs · 5,394 cycles

NR 1 ENGINE REVERSER LEFT SIDE TRANSLATING COWL FWD SECTION LOWER HALF HAS SEVERAL RIVETS MIGRATED. REMOVED AND REPLACED LOOSE AND MIGRATED RIVETS IAW SRM 51-40-02.

Part: SKIN PANEL — DENTED (THRUST REVERSER) · airframe 36,000 hrs · 5,394 cycles

NR 1 ENGINE REVERSER RIGHT SIDE THRUST REVERSER FIXED AFT SECTION BEAVER TAIL OUTER SKIN PANEL DENTED. REWORKED DENTED AREA IAW SRM 51-70-01.

Part: COWL FASTENER — MIGRATED (THRUST REVERSER) · airframe 36,000 hrs · 5,394 cycles

NR 1 ENGINE REVERSER RIGHT SIDE TRANSLATING COWL OUTER SKIN FORWARD SECTION SEVERAL RIVETS MIGRATED. REMOVED AND REPLACED LOOSE AND MIGRATED RIVETS IAW SRM 51-40-02.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 36,000 hrs · 5,394 cycles

RIGHT WING OUTBOARD FORE FLAP HAS DELAMINATION FROM WBL 804-WBL 817. REPAIRED RIGHT OUTBOARD FOREFLAP LEADING EDGE AT WBL 804 TO WBL 817 IAW SRM 51-70-07 AND ATLAS XEO 57-091507.

Part: BLOWOUT PANEL — BROKEN (THRUST REVERSER) · airframe 36,000 hrs · 5,394 cycles

NR 1 ENGINE REVERSER LEFT SIDE LOWER FORWARD SECTION FORWARD END OF BLOW OUT PANEL SIDE SUPPORT BRACKET SECTION DAMAGED. REMOVED BROKEN RIVETS AND REPLACED WITH NEW RIVETS IAW SRM 51-40-02.

Part: FAN — ODOR (E/E BAY) · airframe 34,316 hrs · 5,069 cycles

ELECTRICAL ODOR IN THE COCKPIT. T/S FOUND E/E COOLING SUPPLY FAN FAILED CAUSING ODOR. DEACTIVATED E/E COOLING SUPPLY FAN IAW DDPG 21-28-06 AS PER MAINTENANCE ACTION PERFORMED.

Part: UNKNOWN — UNKNOWN (JETTISON PUMP) · airframe 33,899 hrs · 4,991 cycles

AFTER BLOCK OUT, MAIN TANK NR 2 FWD OVERRIDE/JETTISON PUMP FAIL STATUS MESSAGE DISPLAYED. OPENED MEL 28-31-2C, COMPLIED WITH DDG.

Part: UNKNOWN — UNKNOWN (FUEL) · airframe 33,763 hrs · 4,969 cycles

AT PUSHBACK OFF BLOCKS, RECEIVED STATUS MESSAGE FUEL OVRD 2 FWD. DEFER PER MEL 28-31-2.

Part: STRUCTURE — CHAFED (CARGO DOOR) · airframe 33,765 hrs · 4,971 cycles

AFT LWR CARGO DOOR LWR FWD CORNER MINOR CHAFING V-SHAPE .125 INCH. INTERIM REPAIR FROM ENGINEERING PER DER-ISSUED FAA 8110-3.

Part: SEAT TRACK — CRACKED (BS 1905-1920) · airframe 33,656 hrs · 4,953 cycles

LOWER AFT CARGO COMPARTMENT SEAT TRACK BETWEEN STA 1905-1920, RBL 25 CRACKED. SEAT TRACK REPLACED AS PER SRM 53-00-52.

Part: SEAT TRACK — CRACKED (BS 1905-1920) · airframe 33,656 hrs · 4,953 cycles

LOWER AFT CARGO COMPARTMENT SEAT TRACK CRACKED STA 1905-1920, RBL 45. SEAT TRACK REPLACED AS PER SRM 53-00-52.

Part: WARNING MESSAGE — ILLUMINATED · airframe 32,766 hrs · 4,816 cycles

CREW REPORTED "ANTI-SKID" EICAS MESSAGE DISPLAYED AT ENGINE START. OPENED MEL NR S 32-42-1-1, 32-41-1-A, AND 32-42-4-1A.

Part: PDU — INOPERATIVE · airframe 32,550 hrs · 4,780 cycles

LE SINGLE DRIVE STATUS MSG NR 3 LED INOP PNEUMATICALLY. REPLACED LE PDU.

Part: SHIM — MIGRATED (CARGO DOOR) · airframe 31,293 hrs · 4,545 cycles

C-4 & A-4 CHECK AT PIK., FWD CARGO DOOR FWD ACTUATOR ARM FITTING HAS MIGRATING SHIMS. AFT CARGO DOOR AFT ACTUATOR ARM FITTING HAS MIGRATING SHIMS. ENGG HAS GENERATED XEO 53-081406 PART-1 OF XEO 53-081406 HAS ALREADY ACCOMPLISHED DURING C-CHECK AT PIK ON 15TH AUG 2006. PART-2 (DVI) WILL BE ACCOMPLISHED EVERY 2A CHECK UNTIL ACCOMPLISHMENT OF PART-3. PART-3 IS SCHEDULE PERMANENT REPAIR AT THE NEXT C-CHECK.

Part: SHIM — MIGRATED (CARGO DOOR) · airframe 31,293 hrs · 4,545 cycles

C-4 & A-4 CHECK AT PIK. AFT PIT DOOR HINGE SEGMENTS 1 THRU 12 HAVE MIGRATING SHIMS. AS PER BOEING MESSAGE 1-218612791-2 DATED 11TH AUG 2006, XEO 52-081106 GENERATED. PART-1 ACCOMPLISHED DURING C-CHECK AT PIK. PART-2 WILL BE ACCOMPLISHED (DVI) EVERY 2A CHECK UNTIL ACCOMPLISHED OF PART-3. PART-3 IS SCHEDULE PERMANENT REPAIR AT NEXT C-CHECK.

Part: SKIN — DAMAGED (FORE FLAP) · airframe 31,293 hrs · 4,545 cycles

N496MC AT PIK FOR MSG C-4 & A-4 CHECK. AS PER N/R 39, ON INDUCTION OF A/C FOUND LT I/B T/E FORE FLAP LEADING EDGE DAMAGED, I/B OF NR 3 CANOE. OFF S/N 000532. RECT:LT, I/B T/E FORE FLAP REPLACED AS PER AMM 27-51-02. ON P/N 65B39011-93C & ON S/N 000492.

Part: SEAT TRACK — TORN (BS 1430-1442) · airframe 30,216 hrs · 4,361 cycles

MAIN DECK SEAT TRACK BETWEEN STATION 1430 AND 1442, LBL 99, 12 INCH SECTION OF SEAT TRACK WAS TORN AND DAMAGED. SEAT TRACK WAS PERMANENT REPAIRED PER SRM 53-00-52 FIG 201, REPAIR 6 AND REFERENCE XEO 53-051206.

Part: FMC — FAILED (COCKPIT) · airframe 26,777 hrs · 3,825 cycles

CREW REPORTED RT FMC INOP. REPLACED RT FMC- MM 34-61-01. ALL OPS NORMAL.

Part: CONNECTOR — CONTAMINATED (OIL PRESS XMITTR)

ON TAXI OUT NR2 ENGINE OIL PRESSURE DROPPED BELOW RED LINE-ENGINE SHUTDOWN. T/S IAW MM. CLEANED OIL PRESSURE TRANSMITTER CONNECTOR. ENGINE GROUND RUN PERFORMED ALL WORKING NORMAL. (K)

Part: CONNECTOR — DIRTY (OIL TEMP SENSOR) · airframe 23,232 hrs · 3,221 cycles

NR 2 ENGINE OIL ITEM INDICATION. CLEANED ELECTRICAL CONNECTOR ON OIL TEMPRATURE SENSOR, NR 2 ENGINE INDICATION OK, IAW AMM 71-00-00.

Part: TRANSMITTER — FAILED (NR 1 ENGINE OIL) · airframe 22,905 hrs · 3,168 cycles

LOSS OF ENGINE NR 1 OIL PSI INDICATION ON LWR EICAS DURING CLIMB, NO EICAS MSG RECD OIL INDICATION HAD BEEN NORMAL THROUGHOUT TAXI. REPLACED NR 1 OIL PRESSURE TRANSMITTER PER MM 79-32-01. OPS CHECK ON RUN OK.

Part: WARNING LIGHT — ILLUMINATED (APU DUCT) · airframe 22,404 hrs · 3,074 cycles

AFTER PUSHBACK APU DUCT LEAIL STATUS MESSAGE DISPLAYED. OPENED MEL 49-11-1-1.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 21,385 hrs · 2,901 cycles

STATUS MESSAGE FUEL JET-B. DEFERRED PER MEL 28-31-4-1, PLACARDS INSTALLED.

Part: HOSE — LOOSE (HYD SYSTEM) · airframe 21,090 hrs · 2,847 cycles

LOSS OF HYD FLUID, SYSTEM NR 1 ENG PUMP SELECTED OFF. SYSTEM NR 1 PRESS NORMAL TO COMPLETION OF FLIGHT. FOUND PRESS HOSE AT EDP LOOSE. TIGHTENED HOSE/LINE PER MM 29-11-08. NO LEAKS NOTED PER MM 71-00-00.

Part: ACTUATOR — MALFUNCTIONED (DOOR LATCH) · airframe 20,961 hrs · 2,824 cycles

MAIN DECK SIDE DOOR WILL NOT CLOSE IN ELECTRICAL OR MANUAL MODE. REMOVED AND REPLACED LATCH ACTUATOR PER MM 52-32-09.

Part: ACTUATOR — FAILED (CARGO DOOR) · airframe 20,399 hrs · 2,723 cycles

ON ARRIVAL UNABLE TO OPEN SIDE CARGO DOOR MANUALLY. DOOR LATCH SYS PREVIOUSLY DEFERRED. REPLACED DOOR LATCH ACTUATOR PER MM 52-00-00, OPS CHECK NORMAL. DEFERRAL CLEARED.

Part: DISPLAY — FAILED (COCKPIT) · airframe 20,383 hrs · 2,719 cycles

EXTERNAL POWER FAILED TWICE. WHEN RESTORED, FO'S PFD REMAINED BLANK. SWAPPED LOWER EICAS DISPLAY WITH FO'S PFD AND DEFERRED IAW MEL 31-61-1. DMI AUTH. NR 32082.

Part: WARNING LIGHT — FALSE INDICATION (EICAS) · airframe 20,183 hrs · 2,686 cycles

ON PUSHBACK ACARS DIDN'T BLOCK OUT. SENSORS INDICATED DOOR OPEN. EICAS INDICATED DOOR CLOSED. ALL DOORS CYCLED AND PHYSICALLY CHECKED CLOSED, EICAS INDICATED ALL DOORS CLOSED.

Part: PDU — MALFUNCTIONED (NR 3) · airframe 19,887 hrs · 2,639 cycles

STATUS MESSAGE L/E MULTIDRIVE. REPLACED NR 3 L/E PDU, OPS CHECK NORMAL PER MM 27-81-00.

Part: SOLENOID VALVE — MALFUNCTIONED (HMU) · airframe 19,860 hrs · 2,635 cycles

RETURNED TO BLOCKS. ENG. NR 3 FAILED TO START DUE TO 0 FUEL FLOW (NO EICAS MESS.) REPLACED NR 3 ENG. HMU FUEL SOLENOID VALVE. OPS CHECK OK IAW MM 73-21-00.

Part: SENSE LINE — LOOSE (NR 3 ENGINE) · airframe 19,637 hrs · 2,599 cycles

START FAILURE NR 3 ENGINE - RETURN TO BLOCKS. INSPECTED NR 3 ENGINE, FOUND CDP SENSE LINE AT EEC LOOSE. CLEANED AND PROPERLY SECURED CDP LINE. ENGINE RUN ACCOMPLISHED WITH ALL PARAMETERS NORMAL.

Part: ENGINE — SHUTDOWN (NR 3) · airframe 19,446 hrs · 2,560 cycles

NR 3 ENGINE SHUTDOWN DUE TO NO OIL QTY - FL 350 OIL PRESSURE 45. DURATION OF SHUTDOWN - 45 MINUTES. REMOVED AND REPLACED NR 3 ENGINE PER MM 71-00-00 AND ATLAS MX JOB CARD A71710GTI. ENGINE OPS CHECK GOOD PER MM 71-00-00.

Part: SLIDE — FAILED (CABIN) · airframe 18,777 hrs · 2,425 cycles

RIGHT UPPER DECK SLIDE ASSY FAILED TO DEPLOY DURING MC CHECK. NEW SLIDE INSTALLED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 18,718 hrs · 2,414 cycles

DURING ENG START NR 4 ENG AUTO START EICAS MESSAGE STARTER VLV LIGHT FAILED TO EXTINGUISH WITH SWITCH PUSHED IN. ITEM DEFERRED PER MEL 80-11-01.

Part: CIRCUIT CARD — FAULTY (FIRE WARNING) · airframe 16,403 hrs · 1,987 cycles

ON LANDING ROLL EICAS MSG APPEARED -APU FIRE LOOP A-, -APU FIRE LOOP B- AND APU BOTTLE LOW-. NO INTERIOR OR EXTERIOR INDICATIONS OF FIRE. DE-ACTIVATED APU PER AMM 49-11-00-042-064 AND DEFERRED PER DDPG 49-11-01.

Part: SKIN PANEL — PUNCTURED · airframe 13,983 hrs · 1,577 cycles

Fuselage Skin damaged from BS 460 to 480 from between Stringer 38R and 39R by cargo container during loading operation. Stringers 38R and 39R at this location deformed by container. Damaged skin area trimmed out. Damaged area of stringer 38R trimmed out. Stringer 39R was straightened. Area NDT inspected after straightening. No cracks found. Repair doublers, fillers and stringer repair sections fabricated and installed per standard practices. Briles fasteners used in fuselage skin repair IAW SRM 53-00-03 Figure 204