N416MC

Part: TIRE — FAILED (ZONE 700) · airframe 96,652 hrs · 15,864 cycles

#10 MLG TIRE FAILURE ON LANDING. R/R #9 & #10 MLG WHEEL ASSY PER AMM 32-45-01/401 & AIPC 32-45-03-02. FOUND DAMAGE ON RIGHT BODY GEAR DOOR (OUTBOARD). REPLACED DOOR PER AMM 32-14-02. RIGHT BODY GEAR STRUT DOOR DAMAGED. REPLACED PER AMM 32-14-06. DAMAGE AT R/H LONGERON BOX STA 1440-1460. PERFORMED EDDY CURRENT INSPECTION ON RH LONGERON BOX FS 4110-1460 OPEN BOLT HOLES AND INTERNAL STRUCTURE REFERENCE: BOEING NDIM. PART 6 51-00-00 PROCEDURE 4 & 1 REV DATED: NOV 15 2025. NO RELEVANT INDICATION FOUND DURING THE INSPECTION. ACCOMPLISHED EA-4453A239. NO FURTHER DEFECTS NOTED.

Part: SWITCH — INOPERATIVE (ZONE 400) · airframe 96,395 hrs · 15,821 cycles

BLEED 2 OVHT / PRV EICAS MSG. QRH PROCEDURE IND NO NAI AVAILABLE FOR ENG #2.(<P>REMOVED AND REPLACED BLEED 2 OVHT SWITCH REF AMM 36-22-01 &AMP; AIPC 36-22-01-01, OPS CHECK GOOD. NO LEAKS DETECTED. PERFORMED MPA RUN AS REQUESTED, NO FAULTS FOUND REF AMM 71-00-00-715871-J00.</P>)

Part: SWITCH — NO DISCREPANCY (OVERHEAT) · airframe 93,714 hrs · 15,398 cycles

BLD 4 OVHT/PRV EICAS MSG. REPEAT ISSUE SEE LG PAGE 1858928.(<P>MSG 36044. PERFORMED WIRING CHECK BTWN ASCTU &AMP; OVERTEMP SW, RESULT GOOD. R/R ASCTU &AMP; GND TEST / OPS CHECK GOOD PER AMM 36-11-30 &AMP; IPC 36-11-30-01A. ENG RUN UP PERFORMED AND NO DEFECTS NOTED PER AMM 71-00-00</P>)

Part: SWITCH — FAULTED (BLEED TEMP) · airframe 93,714 hrs · 15,398 cycles

BLD 4 OVHT/PRV EICAS MSG. QRH C/W(<P>R/R OVERTEMP SW IAW AMM 36-22-01 &AMP; IPC 36-22-01-01. LEAK &AMP; OPS CHECK GOOD.</P>)

Part: PIN — CORRODED (HYD SYS) · airframe 15,334 hrs · 93,307 cycles

ATB, HYD SYS 4 QTY INDICATION LOW #4. A/C ARRIVED WITH 0.75 ON THE #4 HYD SYS. PLACED LOAD ON SYS WITH NO VISUAL HYD LEAKS ANYWHERE AND A STEADY QTY IND SYS 1 &AMP; 2 ARE AT 1.20 AND 3 AT 0.97.(<P>R/R THE CORRODED PIN, CLEAN &AMP; RECONNECT. C/W FLUID TRANSFER PER AMM 12-12-00. PIN RECONNECT CORRECTED ISSUE. TOP OFF HYD, MX READY.</P>)

Part: FAIRING — DELAMINATED (LT WING TE FLAP) · airframe 92,754 hrs · 15,244 cycles

LHW O/B MID FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED.</P>)

Part: PANEL — CORRODED (MAIN DECK) · airframe 92,754 hrs · 15,244 cycles

M/D BELOW FSK STOWAGE PNL FOUND CORROSION(<P>M/D - BELOW FSK STOWAGE PNL REPAIR IAW FVCI EO - 24090-1, 2A, 3. NO FURTHER DEFECTS NOTED.</P>)

Part: FAIRING — DELAMINATED (LT WING TE FLAP) · airframe 92,754 hrs · 15,244 cycles

LHW O/B MID FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED.</P>)

Part: STRUCTURE — CORRODED (BS 1241) · airframe 92,754 hrs · 15,244 cycles

CENTER SECTION AFT FACE CORROSION ( NEAR RH O/J PUMP BONDING AREA )(<P>CENTER SECTION AFT FACE CORROSION REMOVED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01 AND MEASURED : REMAIN 0.755" ORG 0806, WIDTH 1.4" LENGTH 2" WITHIN SRM 57-10-10-1A-2 ALLOWABLE DAMAGE 2 FIG 101 LIMITS REV 101 DATE 20 JUN 2024</P>)

Part: STRUCTURE — CORRODED (BS 1241) · airframe 92,754 hrs · 15,244 cycles

CENTER SECTION AFT FACE FOUND CORROSION ( NEAR LH O/J PUMP BONDING AREA )(<P>CENTER SECTION AFT FACE CORROSION REMOVED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01 AND MEASURED. REMAIN 0.783" ORG 0.806" WIDTH 1.4, LENGTH 2" WITHIN SRM 57-10-10-1A-2 ALLOWABLE DAMAGE 2 FIG 101 LIMITS REV 101 DATE 20 JUN 2024.</P>)

Part: STRUCTURE — CRACKED (BS 2598) · airframe 92,754 hrs · 15,244 cycles

BS 2598 LH LOWER INNER CHORD 1EA CRACK FOUND ON FASTENER HOLE 2ND LAYER ( COUNT FROM AFT ) AT 2 O'CLOCK POSITION WITH THROUGH THICKNESS CRACK(<P>BS 2598 LH LOWER INNER CHORD 1EA CRACK ON FASTENER HOLE 2ND LAYER ( COUNT FROM AFT ) REPAIRED IAW RI-53-00-16937 REV A. NO FURTHER DEFECTS NOTED</P>)

Part: FAIRING — DELAMINATED (RT TE FLAP) · airframe 92,754 hrs · 15,244 cycles

RHW O/B MID FLAP L/E FAIRING FOUND DELAMINATION(<P><SPAN>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: SKIN — CHAFED (LT TE LFAP) · airframe 92,754 hrs · 15,244 cycles

LHW O/B AFT FLAP UPPER SURFACE O/B AREA FOUND SEVERAL CHAFING MARKS(<P>PERMANENT METAL TO METAL HOTBOND REPAIR AS PER RI NO. RI-57-51-16950 REV.A. NO FURTHER DEFECTS NOTED</P>)

Part: FRAME — UNKNOWN (BS 2231) · airframe 92,754 hrs · 15,244 cycles

MAIN DECK BS 2231 FRAME BETWEEN STRINGERS 15 TO 31 INSPECTION THE SCREW CANNOT BE INSTALLED AFTER MOVED DUE TO BRACKET BLOCKED(<P>MAIN DECK BS 2231 FRAME BETWEEN STRINGERS 15 TO 31 SCREW CANNOT BE INSTALLED. CASE REPAIRED IAW RI-53-60-16951 REV A AND SB 747-53A2450 REV 08. NO FURTHER DEFECTS NOTED</P>)

Part: SUPPORT ROD — DAMAGED (MLG) · airframe 92,754 hrs · 15,244 cycles

LH LDG SUPPORT BEAM O/B UPR SUPPORT ROD ( WS 522 AREA ) FOUND HOLE ELONGATED(<P>LH LDG SUPPORT BEAM O/B UPR SUPPORT ROD ( WS 522 AREA ) ROD FITTING FABRICATED IAW RI-57-22-16946 REV A AND REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 REV 101 DATE 20 JUN 2024. NO FURTHER DEFECTS NOTED.

Part: STRINGER — CRACKED (NR 3 NACELLE) · airframe 92,754 hrs · 15,244 cycles

#3 PYLON - I/B LOWER STRINGER CRACK FOUND AT MOST AFT END AREA (APPROX NAC STA 374) AS MARKED(<P>3 PYLON - I/B LOWER STRINGER REPAIRED AS PER SRM 54-51-02-2R-2 REPAIR 2 REV 101 DATE 20 JUN 2024. NO FURTHER DEFECTS NOTED</P>)

Part: SOCKET — SHORTED (CEILING LIGHT) · airframe 91,545 hrs · 15,058 cycles

VIA SATCOM, CREW REPORTED INFLIGHT ELECTRICAL ODOR CORRESPONDING TO AN UN-COMMANED ILLUMINATION OF CEILING LIGHT IN THE GALLEY / LAV AREA. CREW REPORTED STRONG ODOR, BUT NOTED NO C/B OPENED.(<P>REMOVED UPPER DECK CEILING LIGHT COVER IAW AMM 33-28-01 AND FOUND BURNED / SHORTED LAMP HOLDERS. R/R BURNED BULB AND BULBS IAW AMM 33-28-01 &AMP; SWPM 20-30-00. OPS CHECK GOOD, NO DEFECTS NOTED. OK FOR SERVICE.</P>)

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,200 hrs · 15,000 cycles

M/D STA 1850-1920 LBL 78-99 BALL MAT FLOOR PNL FOUND DAMAGE(<P>THE DAMAGED CASTER PANEL TOP SKIN REPAIR HAS BEEN CARRIED OUT PER EO.4425A500 REV.1</P>)

Part: SHUTOFF VALVE — UNKNOWN (UNKNOWN) · airframe 88,714 hrs · 14,580 cycles

ITEM 1: AIR TURNBACK DUE TO COCKPIT AND UPPER DECK TEMPERATURES CONTINUALLY DROPPING. FLT DECK SET AT 29C, FWD DECK SET AT 15C, UPPER DECK 8C & CREW REST AT 3C.(<P>REMOVED AND REPLACED FWD TRIM AIR SHUTOFF VALVE PER AMM 21-28-04, TEST PASSED.</P>)

Part: ENGINE — STALLED (NR 2) · airframe 86,720 hrs · 14,234 cycles

NR 2 ENGINE N2 VIBRATION 5.0 AND NR 2 COMPRESSOR STALLED ON CLIMB OUT. R & R NR 2 ENGINE IAW WORD CARD 71-099-02-01. OPS CHECK GOOD</P>)

Part: FLAP — CHAFED · airframe 84,432 hrs · 13,881 cycles

LHW O/B AFT FLAP T/E FOUND CHAFING (95" TO O/B). PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94, FEB20/2022</P>)

Part: SKIN — DELAMINATED · airframe 84,432 hrs · 13,881 cycles

LHW I/B FORE FLAP AFTER WEDGE UPPER SURFACE O/B AREA FOUND DELAMINATION (26" TO O/B)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94, FEB20/2022</P>)

Part: FLAP — DELAMINATED · airframe 84,432 hrs · 13,881 cycles

LHW O/B MID FLAP L/E FOUND DELAMINATION (107" TO I/B). PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94 ,FEB20/2022</P>)

Part: BEAM — ELONGATED · airframe 84,432 hrs · 13,881 cycles

AFT CGO STA 1820-1840 MOST RH HORIZ TORQUE TUBE R/H SUPPORT BEARING ATTACHED BEAM FOUND HOLE ELONGATED. HOLE ELONGATED INTERCOSTAL LOCAL FABRICATED AS PER BOEING DWG: 65B06061 & RPL AND INSTALLED AS PER SRM 51-40-02

Part: CURTAIN — TORN · airframe 84,432 hrs · 13,881 cycles

BULK CARGO STA 2160 CURTAIN FOUND LWR AREA TORN. PERMANENT REPAIR CARRIED OUT AS PER RI-25-54-15628 REV.A</P>)

Part: FITTING — DAMAGED · airframe 84,432 hrs · 13,881 cycles

FUSELAGE - LONGERON EXTENSION FITTING - BODY STATION 1480 TO BODY STATION 1540 - STRINGERS S-32 TO S-33 (EO4453A818 5& 6). L/R STA 1480 - STA 1540 LONGERON EXTENSION FITTINGS REPLACEMENT AS PER ATLAS AIR EO4453A818 PART 3 4 AND RI NO. RI-53-00-15644 REV.A

Part: ATTACH BOLT — ELONGATED · airframe 84,432 hrs · 13,881 cycles

AFT CARGO STA 1820-1840 RBL 30" MOST R/H HORIZONTAL TORQUE TUBE L/H SUPPORT BEARING ATT BEAM FOUND BOLT HOLE ELONGATED. LOCAL FABRICATE INTERCOSTAL AS PER BOEING DWG 65B06201 & PART LIST AND DOUBLER AS PER BOEING DWG 69B02959 PL AND NEW PARTS INSTALLED AS PER SRM 51-40-02</P>)

Part: BUSHING — ELONGATED · airframe 84,432 hrs · 13,881 cycles

#3 PYLON TORQUE BOX INNER AREA NAC STA 298.93 BLEED AIR DUCT R/H SUPPORT ROD LWR DUCT SIDE ATTACHED BOLT HOLE FOUND ELONGATION LINE REAM 2EA AFFECTED BUSHING HOLES AND FABRICATE 2 EACH BUSHING AS PER HX RI-36-11-15646 REV A</P>)

Part: HOUSING — CRACKED · airframe 84,432 hrs · 13,881 cycles

RHW I/B FORE FLAP TO MID FLAP MOST O/B LEVER HOUSING FOUND CRACK. LEVER HOUSING REPLACED AS PER SRM 51-10-01 AND NEW HOUSING INSTALLED AS PER SRM 51-40-02

Part: FRAME — CHIPPED · airframe 84,432 hrs · 13,881 cycles

#3 ENG R/H CORE COWL NO.5 FRAME (COUNT FROM FWD) MID LOW SECTION FOUND CHIPPED. FRAME REPAIRED AS PER SRM 54-45-02-2R-1 REPAIR 1 FIG. 201 REV 94, DATE: 20 FEB 2022</P>)

Part: PANEL — CRACKED · airframe 84,432 hrs · 13,881 cycles

LHW TE CAVITY LWR FIXED PANEL CHORD FOUND CRACKED AT WS 1470 CHORD LOCAL FABRICATED AS PER BOEING DWG : 65B08175 AND PART LIST AND CHORD INSTALLED AS PER SRM 51-40-02

Part: ATTACH PLATE — CORRODED · corrosion level 2 · airframe 84,432 hrs · 13,881 cycles

L/H WLG W/W STA 1241 L/H CTR OJ PUMP BONDING ATT SURFACE FOUND CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, BLENDED OUT AREA WITHIN SRM 57-10-10-1A-2 ALLOWABLE DAMAGE 2 FIG 101 LIMITS.

Part: SKIN — CRACKED · airframe 84,432 hrs · 13,881 cycles

#4 ENG R/H CORE COWL LWR AREA OF AIR EXHAUST FOUND 2EA BOLT HOLE CRACKED SKIN 2EA BOLT HOLE CRACK AREA REPAIRED AS PER SRM 54-45-01-2R-4 REPAIR 4 FIG 201</P>)

Part: SPOILER — DENTED · airframe 84,432 hrs · 13,881 cycles

RHW #12 SPOILER FOUND 1EA DENT MARK AS MARKED. PERFORMED METAL HOTBOND REPAIR AS PER SRM 51-70-10 REPAIR 2 AND FIGURE - 203 REV 94 ,FEB 20/2022</P>)

Part: SKIN PANEL — INSTALLED · airframe 84,432 hrs · 13,881 cycles

FUSELAGE - SECTION 46 - BS 1640 TO 1740 LEFT SIDE AT STRINGER 34 - SKIN PANEL INSPECTION -SB 747-53A2487 R4- AD 2002-23-15. SKIN PANEL MODIFICATION AS PER EO NO.4453A036 FIG 3 AND RI NO. RI-53-60-15609 REV.A</P>)

Part: FRAME — CHAFED · airframe 84,432 hrs · 13,881 cycles

APU COMPARTMENT STA 2690 L/H FRAME MID SECTION FOUND CHAFING, FRAME REPAIRED AS PER SRM 53-80-07-2R-1 REPAIR 1 REV 94 DATE 20 FEB 2022</P>)

Part: FLAP — DELAMINATED · airframe 84,432 hrs · 13,881 cycles

LHW O/B FORE FLAP L/E FOUND DELAMINATION (125" TO I/B)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94 ,FEB20/2022</P>)

Part: ATTACH ANGLE — CRACKED · airframe 84,432 hrs · 13,881 cycles

M/D LHS STA 960 S-7 FRAME FWD/ CREASE BEAM LWR ATT ANGLE CRACKED. LOCAL FABRICATED AND P/N NO.65B38488-159 AS PER BOEING DWG: 65B38488 PL AND INSTALLED AS PER SRM 51-40-02</P>)

Part: INDICATOR — FAULT MESSAGE · airframe 84,437 hrs

ENGINE #2 OIL QUANTITY INDICATED 19 PRIOR TO START, 14 AFTER START, 10 AT THE TOP OF THE CLIMB, AND DECREASED TO 7 BY LANDING AFTER 2:51 FLIGHT TIME. RETURNED TO RKSI WITH ENGINE #2 AT IDLE POWER. REMOVED AND REPLACED WITH NO.2 ENG AND THEN LEAK CHECK NORMAL AND RUN UP TEST NORMAL AS PER AMM 71-00-02 AND AMM 71-00-00

Part: FLAP — DELAMINATED · airframe 84,432 hrs · 13,881 cycles

LHW O/B FORE FLAP L/E FOUND DELAMINATION (145" TO I/B). PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94 ,FEB20/2022</P>)

Part: COWLING — GOUGED · airframe 84,432 hrs · 13,881 cycles

#3 ENG R/H CORE COWL MOST AFT FRAME MID LOW SECTION FOUND GOUGE MARK(FRAME REPAIRED AS PER SRM 54-45-02-2R-2 REPAIR 2 FIG.201 REV.94 DATE: 20 FEB 2022</P>)

Part: STRUCTURE — CRACKED · airframe 84,432 hrs · 13,881 cycles

REFER WO.790016 RI-57-00-15623 REV A HFEC OPEN HOLE INSPECTION FOUND R/H I/B FORE FLAP O/B RIB ASSY AT WBL 410.25 AT I/B WEB, I/B LOWER CHORD & O/B LOWER CHORD CRACKED. LOCAL FABRICATE I/B LOWER CHORD AND O/B LOWER CHORD AS PER BOEING DWG: 65B39038 AND PART LIST, WEB LOCAL FABRICATE AS PER RI NO. RI-57-00-15623 REV.A AND NEW I/B LWR CHORD, O/B LWR CHORD WEB INSTALLED AS PER SRM 51-40-02.</P>)

Part: SKIN — DELAMINATED · airframe 84,432 hrs · 13,881 cycles

RHW O/B T/E MID FLAP UPR SURFACE AT AFT AREA 135" FROM O/B EDGE FOUND DELAMINATED. PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94, FEB20/2022

Part: ATTACH PLATE — CORRODED · corrosion level 2 · airframe 84,432 hrs · 13,881 cycles

R/H WLG W/W STA 1241 R/H CTR OJ PUMP BONDING ATT SURFACE FOUND CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, BLENDED OUT AREA WITHIN SRM 57-10-10-1A-2 ALLOWABLE DAMAGE 2 FIG 101 LIMITS

Part: PLATE — MIGRATED · airframe 84,432 hrs · 13,881 cycles

R/H W/W STA 1350 WING LANDING GEAR SUPPORT BEAM SPLICE LOWER PLATE AFT I/B CORNER SHIM MIGRATED. SHIM MIGRATION INSPECTION PER SRM 51-20-08, MOUNT BOLT TORQUE CHECK PERFORMED PER SRM 51-40-04-0G-0, EDGE SEALEANT APPLIED PER AMM 51-31-01.

Part: FLAP — DELAMINATED · airframe 84,432 hrs · 13,881 cycles

LHW O/B MID FLAP L/E FOUND DELAMINATION (55" TO I/B). PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94 ,FEB20/2022</P>)

Part: SKIN — CRACKED · airframe 84,432 hrs · 13,881 cycles

L/H BLG I/B STRUT DOOR SKIN FOUND CRACK. SKIN CRACK AREA REPAIRED AS PER SRM 52-80-01-2R-1 REPAIR 1 FIG 201 REV 94 DATE 20FEB 2022

Part: ATTACH ANGLE — CRACKED · airframe 84,432 hrs · 13,881 cycles

M/D RHS STA 960 S-7 FRAME FWD / CREASE BEAM LWR ATT ANGLE CRACKED. LOCAL FABRICATED ANGLE P/N: 65B38488-159 AS PER BOEING DWG: 65B38488 PL AND INSTALLED AS PER SRM 51-40-02 REV 94 DATE 20FEB2022</P>)

Part: FRAME — CHIPPED · airframe 84,432 hrs · 13,881 cycles

#4 ENG L/H CORE COWL #2 FRAME (COUNT FROM FWD) MID LOW SECTION FOUND CHIPPED (UNDER AREA OF HOLD OPEN ROD) FRAME REPAIRED AS PER SRM 54-45-02-2R-1 REPAIR 1 FIG.201 REV 94, DATE 20 FEB 2022

Part: SPOILER — DENTED · airframe 84,432 hrs · 13,881 cycles

LHW #4 SPOILER FOUND 1EA DENT MARK AS MARKED. PERFORMED METAL HOTBOND REPAIR AS PER SRM 51-70-10 REPAIR 4 AND FIGURE - 201 REV94 ,FEB20/2022

Part: SHEAR TIE — CRACKED · airframe 84,432 hrs · 13,881 cycles

1EA THROUGH THICKNESS CRACK WAS FOUND ON THE LBL 57.5 SHEAR TIE AS MARKED APPROX 13/4" IN LENGTH AT I/B SIDE & 1 1/4" IN LENGTH AT O/B SIDE. CRACK SHEAR TIE REPLACEMENT AS PER ATLAS AIR EO: 4453C024 REV 1 PART5</P>)

Part: WEB — CRACKED · airframe 84,432 hrs · 13,881 cycles

RHW I/B FORE FLAP MOST O/B WBL 410.25 O/B RIB ASSY UPPER CHORD & WEB FOUND CRACKED(<P>LOCAL FABRICATE WEB AS PER RI NO.RI-57-00-15623 REV.A AND REPLACED UPPER CHORD AS PER SRM 51-10-02 AND NEW WEB AND UPPER CHORD INSTALLED AS PER SRM 51-40-02</P>)

Part: FRAME — CHAFED · airframe 84,432 hrs · 13,881 cycles

APU COMPARTMENT STA 2685 L/H FRAME MID SECTION FOUND CHAFING. FRAME CHAFING AREA REPAIRED AS PER SRM 53-80-07-2R-1 REPAIR 1 REV 94, DATE: 20 FEB 2022</P>)

Part: SHEAR TIE — CRACKED · airframe 84,432 hrs · 13,881 cycles

1EA THROUGH THICKNESS CRACK WAS FOUND ON THE LBL 75.92 SHEAR TIE AS MARKED APPROX 1 3/4" IN LENGTH AT I/B SIDE &AMP; 1 1/4" IN LENGTH TO O/B SIDE(<P>CRACK SHEAR TIE REPLACEMENT AS PER ATLAS AIR EO: 4453C024 REV. 1 PART 6</P>)

Part: FLAP — DELAMINATED · airframe 84,432 hrs · 13,881 cycles

LHW O/B FORE FLAP L/E FOUND DELAMINATION (22" TO O/B). PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94 ,FEB20/2022</P>)

Part: FASTENER — CRACKED · airframe 84,432 hrs · 13,881 cycles

EO 4453A821-1 4 FUSELAGE SKIN NOSE WHEEL WELL FORWARD CORNER DOUBLER INSPECTION AND MODIFICATE (SB 747-53A2851) (L/H FASTENERS & WASHERS DEVIATIONS; DOUBLER S.E.M AND R/H FASTENERS & WASHERS DEVIATIONS FASTENER HOLE CRACK (1EA), L/R DOUBLER INSTALLED AS PER BOEING DWG 624U0073 SHT 1 & 2 AND RI NO: RI-53-00-15647 REV.A

Part: FLAP — DELAMINATED · airframe 84,432 hrs · 13,881 cycles

LHW O/B MID FLAP L/E FOUND DELAMINATION (140" TO I/B). PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94 ,FEB20/2022</P>)

Part: FLAP — CHAFED · airframe 84,432 hrs · 13,881 cycles

LHW O/B FORE FLAP T/E UPR SURFACE O/B AREA FOUND CHAFING AS MARKED (3" TO O/B). PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94 ,FEB 20/2022</P>)

Part: SEAT TRACK — CORRODED (BS 2195) · corrosion level 2 · airframe 76,912 hrs · 12,731 cycles

CORROSION DAMAGE ON SEAT TRACK AT STA 2195 RBL 11.33. REPAIR SEAT TRACK, IAW SRM 53-00-52 REPAIR 12 REV 89 AND EI NO T2020A53M-1845 REV 1 DWG 65B38253 SH 54 REV. JOB COMPLETED.

Part: SKIN — DENTED (LT AILERON) · airframe 76,912 hrs · 12,731 cycles

AIRCRAFT DAMAGE LOG PERFORM CONTROL ITEM NUMBER 2707 LEFT AILERON I/B HAS DENT ON LOWER SIDE. CUT OUT THE DAMAGED MATERIAL AND CLEAN, MEASURE THE DAMAGED AREA (L=2", W=2, D=1.5" FROM INBD EDGE 21" FROM AFT EDGE AT INBD 460 OF LH AILERON SIDE. BOND 4 REPAIR PLIES WITH FIRM ADHESIVE, CURE AT 260 DEGREES F FOR 30 MINUTES AND MAINTAIN A MINIMUM VACUUM PRESSURE 22"/HG IAW SRM 57-60-01-2R-1. REFER TO SRM 51-70-07-05-0 REV 88. CONDITION CHECK SAT.

Part: WEB — CANNING (BS 1680) · airframe 76,912 hrs · 12,731 cycles

OIL CANNING DAMAGE ON WEB AT AFT CGO COMPARTMENT NEAR STA 1680, RBL 45.50. REPAIR DAMAGED AREA IAW EI NO T2020A53M-1984 REV 2. JOB COMPLETED AND CONDITION CHECK SATISFIED.

Part: STRUCTURE — CRACKED (BS 1480) · airframe 76,912 hrs · 12,731 cycles

FOUND FLOOR STRUCTURE SUBSTITUTE TRACK CRACK AT STA 1480 RBL 75.92. ACCOMPLISHED IAW SRM 53-00-52-2R-13 REPAIR 13 REV 89 AND DWG NO 65B38251 SH 32 REV - AND DWG NO 144U0802 SH 3 REV B. JOB COMPLETED AND CONDITION CHK SATISFIED.

Part: ACCESS DOOR — DENTED (APU) · airframe 76,912 hrs · 12,731 cycles

4 EA DENT ON SKIN P/N 65B02771-1901 OF APU LH ACCESS DOOR. REPAIRED DAMAGED AREA IAW EI NO T2020A52M-1997 REV 1. APPLY YELLOW DOT NO 32597 FOR DENT AREA #1 AND #2, CONDITION "AS IS". JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: SEAT TRACK — CRACKED (BS 1485) · airframe 76,912 hrs · 12,731 cycles

CRACK DAMAGE ON M/D SUBSTITUTE SEAT TRACK AT STA 1485 LBL 75.92 REPAIRED DAMAGED AREA IAW SRM 53-00-52-2R-13 REPAIR 13 REV 89 AND DWG NO 144420802 SHEET 3 REV B AND DWG NO 65B38251 SHEET 32 REV -. JOB COMPLETED AND CONDITION CHK NORMAL.

Part: STRUCTURE — CRACKED (HORIZONTAL STAB)

CRACK FOUND WEB CRACK AT RT HST TIP HSBL 421.5. REPAIRED DAMAGED AREA, IAW EI NO T2020A55M-1851 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 76,912 hrs · 12,731 cycles

CRACK DAMAGE ON LWR CHORD OF RH HST RIB AT HSBL 421.5. ACCOMPLISHED EI NO T2020A55M-1851 REV 1 THAT ATTACHED TO WD NO. 4824624. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: FLOORBEAM — CORRODED (BS 1920) · corrosion level 2 · airframe 76,912 hrs · 12,731 cycles

CORROSION ON LOWER SURFACE OF FLOOR BEAM UPPER CHORD AT STA 1920 NEAR RBL 102.58. ACCOMPLISHED THE JOB IAW EI NO T2020A53M-1985. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: FLOORBEAM — CORRODED (BS 800) · corrosion level 2 · airframe 76,912 hrs · 12,731 cycles

CORROSION ON FLOOR BEAM UPPER CAP AT STA 800 OUTBD OF LBL 98.58. REPAIR FLOOR BEAM IAW EI NO T2020A53M-2046 REV 1. CONDITION CHECK NORMAL AND JOB COMPELTED.

Part: SPAR — CRACKED (LT WING) · airframe 76,912 hrs · 12,731 cycles

CRACK ON ONE FASTENER HOLE OF LT WING FRONT SPAR WEB COMMON TO LOWER CHORD AT FSSU 676. ACCOMPLISHED EI NO T2020A57M-1947 REV 2. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: DOUBLER — CORRODED (BS 1940-1960) · corrosion level 2 · airframe 76,912 hrs · 12,731 cycles

CORROSION ON DOUBLER SPLICE OF MAIN DECK CARGO COMPARTMENT STRUCTURE, BETWEEN STA 1940-1960, RBL 75.92. REMOVED THE CORROSION DOUBLER SPLICE IAW SRM 51-40-02 REV 88. FABRICATE THE DOUBLER SPLICE IAW EI NO T2020A53-1887 REV. 0. INSTALL THE FABRICATED PART IAW SRM 51-40-02 REV 88 AND DWG NO 65B38251 SH 32, REV -, 65B38251 SH 62 REV A. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: FLOORBEAM — CORRODED (BS 2240) · corrosion level 2 · airframe 76,912 hrs · 12,731 cycles

CORROSION ON FLOOR BEAM UPPER CAP AT STA 2240 BETWEEN LBL 50.00 AND LBL 67.01. ACCOMPLISHED JOB IAW EI NO T2020A53M-1983 REV 1 AND SRM 53-00-51-2R-2, REPAIR 3, REV 89. JOB COMPLETED AND CONDITION CHK NORMAL.

Part: FASTENER — LOOSE (BS 2658-2701) · airframe 76,912 hrs · 12,731 cycles

FOUND FASTENERS LOOSENED ON SKIN OF FUSELAGE FROM STA 2658 TO STA 2701.ACCOMPLISH IAW EI NO T2020A53M-1991 REV 2. JOB COMPLETED AND CONDITION CHK SATISFIED.

Part: SENSOR — FAULTY (APU) · airframe 75,888 hrs · 12,564 cycles

N416MC REQUESTED TO RETURN TO AMS TO TROUBLESHOOT DEFERRED APU BECAUSE OF SCHEDULE AND GROUND SUPPORT EQUIPMENT AVAILABLE AT RIX, OAI. FLIGHT OPERATION REQUEST.(<P>TROUBLESHOOTING CARRIED OUT PER FIM FOR CMC FAULT 49091. CHECKED INLET PLENUM FOR OBSTRUCTIONS FOUND. CHECKED CHIP DETECTORS. FOUND SATISFACTORY. REPLACED N1 SPEED SENSOR IAW AMM 49-61-02. REPLACED DIVERTER VALVE IAW AMM 49-52-04 (OFF PART: PN 3900430, SN F55969), REPLACED APU FUEL FILTER IAW AMM 49-31-00 (OFF PART: PN ACB881F25, NSN). APU OPS CHECK SATISFACTORY IAW AMM 49-11-00.</P>)

Part: FMC — MALFUNCTIONED · airframe 74,769 hrs · 12,357 cycles

DUAL FMC FAIL IMMEDIATELY AFTER TAKEOFF, FAILED 8-10 TIMES ENROUTE.(<P>PERFORMED FMC L &AMP; R GROUND TEST IAW AMM 34-61-00, NO DEFECTS NOTED. PERFORMED FMC L &AMP; R SERVO LOOP GROUND TEST, NO DEFECT NOTED.</P><P>LP 1077093&NBSP; - M6: WHEN GROUND POWER WAS PULLED, PROBLEM REPEATED. REMOVED AND REPLACED L FMC IAW AMM 34-61-01. PERFORMED GROUND TEST IAW AMM 34-61-01, NO DEFECTS NOTED. OFF PART (PN: 4052508-960, SN: 02348927).</P><P>LP 1077094 - M7: REMOVED AND REPLACED R FMC IAW AMM 34-61-01. PERFORMED SOFTWARE CROSSLOAD IAW AMM 34-61-00. PERFORMED GROUND TEST IAW AMM 34-61-00, NO DEFECTS NOTED. PERFORMED AUTOLAND UNIQUE TEST IAW AMM 22-10-00. AIRCRAFT REMAINS CATIIIB.&NBSP;</P>)

Part: OIL SYSTEM — ABNORMAL (NR 4 ENGINE) · airframe 74,601 hrs · 12,328 cycles

#4 ENGINE OIL QTY DECREASED TO 4 QTS, PRECAUTIONARY ENGINE SHUTDOWN.&NBSP;(<P>REMOVED AND REPLACED #4 ENGINE IAW AMM 71-00-02 AND MCS PACKAGE 59263. LEAK AND OPS CHECK GOOD PER AMM 71-00-00.</P>)

Part: TRIM SYSTEM — OUT OF ADJUST (HORIZ STAB) · airframe 74,234 hrs · 12,254 cycles

SLOW SPEED (60 KTS) RTO DUE TO CONFIG STAB EICAS MESSAGE & HORN. NO EXCEEDANCES, ABOVE MIN FUEL. CONTINUED AFTER ADJUSTING STAB TRIM. NOTED BY MAINTENANCE. NO MX ACTION REQUIRED, MCC NOTIFIED.

Part: ACTUATOR — MALFUNCTIONED (CROSSFEED NR 1) · airframe 71,211 hrs · 11,727 cycles

AIR RETURN FOR #1 FUEL CROSSFEED EICAS MESSAGE AND CONSUMPTION NOTED FROM CENTER TANK(<P>REMOVED AND REPLACED ACTUATOR FOR #1 CROSSFEED VALVE PER AMM 28-22-02. ALL OPS CHECKS NORMAL<BR /></P>)

Part: MODULATING VALVE — FAULTY (CABIN TEMP) · airframe 70,556 hrs · 11,617 cycles

STATUS MESSAGE ZONE TEMP WITH ASSOCIATED HIGH FLIGHT DECK TEMPERATURE.(<P>REMOVED AND REPLACED&NBSP; UPPER DECK TRIM AIR MODULATING VALVE PER AMM 21-61-10/401 <BR /></P>)

Part: FITTING — CRACKED (THRUST REVERSER) · airframe 69,845 hrs · 11,489 cycles

NR 4 ENGINE, LT THRUST REVERSER LOWER ACTUATOR HOUSING FITTING FOUND CRACKED. THE ACTUATOR HOUSING WAS REPAIRED IAW CMM 78-32-02, REPAIR 016.

Part: CHANNEL — CRACKED (BS 720) · airframe 69,845 hrs · 11,489 cycles

BS 720, STRINGER 9R, TENSION TIE FWD CHANNEL RADIUS FOUND CRACKED, 0.25 INCH. THE TENSION TIE FWD CHANNEL WAS REPAIRED IAW SRM 53-20-30-2R, REPAIR 1.

Part: SHEAR WEB — CRACKED (RT WING) · airframe 68,256 hrs · 11,201 cycles

RIGHT WING FIXED TRAILING EDGE GROUND SPOILER INBD SUPPORT RIB, WBL 255.69, SHEAR WEB CRACKED. REPAIRED SHEAR WEB IAW EO 4457A169, PART 2, AND SRM 51-70-13-2R-1, FIGURE 201.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 67,026 hrs · 10,962 cycles

NR 1 ENGINE COMPRESSOR STALL ON DEPARTURE DURING CLIMB AT APPROXIMATEY 3000 MSL. OPEN

Part: OVEN — FAILED (GALLEY) · airframe 65,909 hrs · 10,771 cycles

DURING THE MIDDLE OF CRUISE FLIGHT, CREW OBSERVED VOLUMINOUS SMOKE EMITTING FROM THE GRILL PLATE ABOVE THE OVEN, ACCOMPANIED BY A VERY STRONG ELECTRICAL BURNING ODOR. CREW SHUTDOWN ALL ELECTRICITY IN UPPER GALLEY BY PULLING CIRCUIT BREAKERS. SMOKE GENERATION CEASED IMMEDIATELY. ON ARRIVAL TROUBLESHOT AND FOUND OVEN ASSY REAR FAN MOTOR STUCK & BURNING. REPLACED THE OVEN ASSY AND OPS CHECKED OK IAW AMM 25-32-00. INSPECTED UPPER DECK GALLEY UTILITY ELECTRIC CONT. PANEL ALL CONDITION NORMAL.

Part: WARNING MESSAGE — ILLUMINATED · airframe 64,694 hrs · 10,554 cycles

ELEC DRV 1 EICAS ON T/O ROLL AT 70KTS, BRAKE TEMPS MAX 3 AFTER RTO AUTOBRAKE. MX DISC NR 1 IDG PRIOR TO NR 1 ENGINE SHUTDOWN. CARRIED OUT HIGH ENERGY BRAKE INSPECTION, NO DEFECTS NOTED IAW AMM 05-51-10.

Part: ESCAPE ROPE — ABNORMAL (COCKPIT) · airframe 63,242 hrs · 10,305 cycles

COCKPIT DESCENT DEVICE NR 5 EXTENDED. REMOVED AND REPLACED IAW AMM 25-61-01.

Part: ESCAPE ROPE — ABNORMAL (COCKPIT) · airframe 63,242 hrs · 10,305 cycles

COCKPIT DESCENT DEVICE EXTEND. REMOVED AND REPLACED IAW 25-61-01.

Part: ESCAPE ROPE — ABNORMAL (COCKPIT) · airframe 63,242 hrs · 10,305 cycles

COCKPIT DESCENT DEVICE NR 3 EXTENDED. REMOVED AND REPLACED IAW AMM 25-61-01.

Part: ESCAPE ROPE — ABNORMAL (COCKPIT) · airframe 63,242 hrs · 10,305 cycles

COCKPIT DESCENT DEVICE NR 7 EXTENDED. REMOVED AND REPLACED IAW AMM 25-61-01.

Part: ESCAPE ROPE — ABNORMAL (COCKPIT) · airframe 63,242 hrs · 10,305 cycles

COCKPIT DESCENT DEVICE NR 6 EXTENDED. REMOVED AND REPLACED IAW AMM 25-61-01.

Part: ESCAPE ROPE — ABNORMAL (COCKPIT) · airframe 63,242 hrs · 10,305 cycles

COCKPIT DESCENT DEVICE NR 4 EXTENDED. REMOVED AND REPLACED IAW AMM 25-61-01.

Part: ESCAPE ROPE — ABNORMAL (COCKPIT) · airframe 63,242 hrs · 10,305 cycles

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

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 61,855 hrs · 10,048 cycles

UPPER DECK EMERGENCY LIGHT BATTERY PACK (M5169) FAILED THE FUNCTIONAL CHECK, FOUND CAPACITY LOW ,LESS THAN 15 MINIMUM. BATTERY PACK REPLACED IAW AMM 33-51-04.

Part: REVEAL — CRACKED (BS 2231-2237) · airframe 61,855 hrs · 10,048 cycles

L5 DOOR FWD REVEAL DOUBLER CRACKED AT BS 2231-2237 STRINGERS 21- 22L. THE REVEAL DOUBLER REPAIRED IAW SRM 53-6-15-2R-3 REPAIR 3.

Part: CLOSEOUT PANEL — CRACKED (BS 1238-1265) · airframe 61,855 hrs · 10,048 cycles

MAIN DECK LT TRIM AIR DUCT CLOSE PANEL FOUND CRACKED. MAIN PRESSURE DECK BS 1238-1265 LBL 75.92 - LBL 98.58. DAMAGED CLOSE PANEL. REPLACED IAW SRM 51-10-02 AND DWG 65B07992.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,855 hrs · 10,048 cycles

UPPER DECK EMERGENCY LIGHT POWER SUPPLY HAS NO POWER OUTPUT. BATTERY PACK REPLACED IAW AMM 33-51-04.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,368 hrs · 9,788 cycles

EMERGENCY LIGHT INOPERATIVE BATTERY PACK, BS 390, WL 380, RBL 14. R & R POWER SUPPLY IAW 33-51-04 GROUND CHECK NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,368 hrs · 9,788 cycles

EMERGENCY LIGHT INOPERATIVE. BATTERY PACK M5 169 BS: WL 323, RBL 83. PERFORMED EMERGENCY LIGHT OPS CHECK OK AMM 33-51-00.

Part: ACTUATOR — MALFUNCTIONED (MLG DOOR) · airframe 59,932 hrs · 9,699 cycles

EICAS MESSAGE GEAR DOOR AND HYD PRESSURE, SYS 1. REPLACED NOSE GEAR DOOR ACTUATOR IAW AMM 32-34-14-404-012. OPERATION AND LEAK CHECK GOOD. SERVICED NR 1 HYDRAULIC SYSTEM WITH 40 QTS IAW AMM 12-12-01.

Part: ESCAPE REEL — DAMAGED · airframe 59,643 hrs · 9,654 cycles

THREE DESCENT DEVICES DAMAGED. CABLE DAMAGE PULLED FROM REEL. REPLACED NR 7 DESCENT DEVICE. INSTALLED PN 379103D-23, SN 20213 DUE DATE 10-NOV-20.

Part: ESCAPE REEL — DAMAGED · airframe 59,643 hrs · 9,654 cycles

THREE DESCENT DEVICES DAMAGED. CABLE PULLED FROM REEL. REPLACED NR 8 DESCENT DEVICE. INSTALLED PN 379103D-23, SN 13604 DUE DATE 10-NOV-20.

Part: ESCAPE REEL — DAMAGED · airframe 59,643 hrs · 9,654 cycles

THREE DESCENT DEVICES DAMAGED. CABLE PULLED FROM REEL. REPLACED NR 2 DESCENT DEVICE. INSTALLED PN 379103D-23, SN 20495 DUE DATE 10-NOV-20.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 58,588 hrs · 9,488 cycles

HYD QTY LOW 1 EICAS MESSAGE ON SHORT FINAL, FOUND HYDRAULIC LEAK FROM LT WING TO BODY FAIRING AREA LANDING GEAR PRESSURE LINE. INSTALLED TEMPORARY REPAIR FLEX LINE HOSE IAW GMM 3.27.1 AND LEAK CHECKED OK IAW AMM 29-11-00. SYSTEM SERVICED IAW AMM 12-12-01/301. TRACKING WITH NON MEL 59592.

Part: COMPUTER — MALFUNCTIONED (FMC) · airframe 56,603 hrs · 9,131 cycles

DUAL FMC FAILURE FOLLOWED BY RESYNC. ABLE TO ESTABLISH FMC OPERATION NORMAL. DISP NOTIFIED. R & R RT FLIGHT MANAGEMENT COMPUTER AND INSTALLED FMC SOFTWARE THEN GROUND TEST PASSED IAW AMM 34-61-01/401. PERFORMED BOTH FMC LT AND RT GROUND TEST PASS IAW AMM 34-61-00/501, AUTOLAND UNIQUE TEST PASSED IAW AMM 27-00-00/501.

Part: ACTUATOR — LEAKING (MLG DOWNLOCK) · airframe 54,180 hrs · 8,766 cycles

DURING LANDING, HYD SYS NR 1 QTY WENT TO .34 WITH STATUS MESSAGE HYD QTY. DURING INSPECTION FOUND THE RT BODY GEAR DOWNLOCK ACTUATOR LEAKING. REPLACED RT BODY GEAR DOWN LOCK ACTUATOR IAW AMM 32-33-15/401.

Part: FRAME — CRACKED (BS 1480 BULKHEAD) · airframe 54,169 hrs · 8,764 cycles

BULKHEAD FRAME WEB CRACKED AT STA 1480, LBL & NBSP; 110, WL 140, REPAIRED THE DAMAGED AREA IAW EI T2014A53B-2429, REV 2.

Part: SKIN — PUNCTURED (BS 480-488) · airframe 53,635 hrs · 8,676 cycles

PUNCTURE FOUND ON FUSELAGE SKIN AT L1 DOOR LOWER WHICH LOCATED AT BS 480 - 488, STRINGERS 30 - 31L. REPAIRED IAW EO 4453A986.

Part: SKIN — PUNCTURED (BS 435) · airframe 53,635 hrs · 8,676 cycles

PUNCTURE OF DAMAGE FOUND ON FUSELAGE SKIN AT L1 DOOR LOWER WHICH LOCATED AT BS 435, STRINGER 30-31L. FOUND NO INTERNAL DAMAGE TO SURROUNDING FRAME WORK. REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 1. INTERNAL DOUBLER REPAIRED IAW SRM 51-70-13, FIG 201, REPAIR 1, EO 4453A987 ACCOMPLISHED.

Part: FAN — ODOR (EXHAUST) · airframe 51,139 hrs · 8,125 cycles

"EE CLNG" EXHAUST FAN STATUS MESSAGE ACCOMPANIED BY BURNING ODOR. VISUAL AND OPS CHECK C/W. NO FIRE NOTED.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,354 hrs · 7,994 cycles

CABIN-SEAT TRACK CORROSION CRACKED AT STA 1900 LBL 11.33 (CABIN-STA 1870.40-STA 1946.45 LBL11.33. DAMAGED SEAT REPAIRED IAW SRM 53-00-52 REPAIR 12 AND RI NO = RI-53-65-10208 REV A).

Part: ACCESS PANEL — DAMAGED (NR 1 PYLON) · airframe 50,354 hrs · 7,994 cycles

NR 1 PYLON ACCESS PANEL&NBSP; #452ER 1EA LATCH&NBSP; ATT SCREW HOLE ELONGATED AS MARKED (NR 1 PYLON ACCESS PANEL #452ER P/N= 321U2060-40 1 EA ELONGATED HOLE REPAIRED IAW R1-54-00-1027 REV A).

Part: FLAP — DAMAGED (LT WING) · airframe 50,149 hrs · 7,958 cycles

ON WALK AROUND FOUND LEFT WING INBOARD TRAILING EDGE FLAP DAMAGE (ASYMMETRIC). REMOVED AND REPLACED LEFT INB FORE FLAP PER AMM 27-51-02.

Part: SKIN — DAMAGED (LT AILERON) · airframe 50,149 hrs · 7,958 cycles

FOUND LEFT INB AILERON DAMAGED DURING WALK AROUND INSPECTION. REF&NBSP; L.P 525897, M6&NBSP; DAMAGE ON LWR FWD SKIN HAS BEEN BLENDED OUT CLIPS REPLACED ON FWD UPPER CHORD OF THE AILERON RIB PER SRM 57-60-01-1A-1.

Part: CARRIAGE — BROKEN (TE FLAP) · airframe 50,149 hrs · 7,958 cycles

LEFT WING NR 4 SEQUENCE CARRIAGE/TOGGLE ASSY FOUND BROKEN. REMOVED AND REPLACED LEFT WING NR 4 SEQUENCE CARRIAGE / TOGGLE ASSY PER AMM 27-51-23-004-001.

Part: RIB — DAMAGED (LT WING) · airframe 50,149 hrs · 7,958 cycles

LEFT WING RIB STIFFENER INBD COMPARTMENT INBOARD OF LEFT SIDE AILERON IS DAMAGED &NBSP;&NBSP; REPLACED LEFT WING INBD RIB STIFFENER PER SRM 51-40-02&NBSP;.

Part: RIB — DAMAGED (LT WING) · airframe 50,149 hrs · 7,958 cycles

LEFT WING RIB STIFFENER INBD OF AILERON PCP COMPARTMENT HAS DAMAGES TO EDGES&NBSP; (BLENDED ANGLE TRUSS INB OF AILERON PCP COMPARTMENT PER SRM 57-60--2 ALLOWABLE DAMAGE OK FOR SERVICE.&NBSP;&NBSP;).

Part: HYDRAULIC LINE — DENTED (HYDRAULIC SYS) · airframe 50,149 hrs · 7,958 cycles

FOUND NR 1 HYDRAULIC SYSTEM RETURN TUBE NEAR NR 4 FLAP TRACK DENTED UPON INSPECTION OF AREA. REMOVED AND REPLACED NR 1 HYDRAULIC SYSTEM RETURN TUBE IAW AMM 20-11-05.

Part: STIFFENER — DAMAGED (LT WING) · airframe 50,149 hrs · 7,958 cycles

LEFT WING RIB STIFFENER AT WBL 445 FOUND DAMAGED DURING INSPECTION OF THE AREA. WORK IN PROGRESS.

Part: PANEL — DAMAGED (LT WING) · airframe 50,149 hrs · 7,958 cycles

LEFT WING LOWER FIXED TRAILING EDGE&NBSP; PANEL AT WBL 362 THROUGH 445 FOUND DAMAGED DURING INSPECTION OF THE AREA. REMOVED AND REPLACED LOWER TE PANEL ASSY PER SRM 51-70-19.

Part: BUSHING — MISSING (LT WING) · airframe 50,149 hrs · 7,958 cycles

THE LOWER SUPPORT TIE ROD OF THE LEFT OUTBOARD TRAILING EDGE FIXED PANEL AT WBL 426 IS MISSING HARDWARE AS FOUND DURING INSPECTION OF THE AREA. INSTALLED MISSING BUSHING ON LEFT OUTBOARD T/E FIXED PANEL INBOARD LOWER SUPPORT THE ROD PER SRM 57-22-02.

Part: FLAP — DAMAGED (LT WING) · airframe 50,149 hrs · 7,958 cycles

FOUND LEFT WING INBOARD MID FLAP DAMAGED DURING INSPECTION. REMOVED AND REPLACED INB MID (LEFT) FLAP PER AMM 27-51-01.

Part: AILERON — DAMAGED (LEFT) · airframe 50,149 hrs · 7,958 cycles

LEFT INBOARD AILERON DAMAGED. REPAIRS IN WORK. SUPPLEMENTAL TO FOLLOW.

Part: PANEL — DAMAGED (LT WING) · airframe 50,149 hrs · 7,958 cycles

LEFT WING UPPER TRAILING EDGE FIXED PANEL AT WBL 445 FOUND DAMAGED DURING INSPECTION OF AREA. LEFT WING TRAILING WING EDGE UPPER FIXED PANEL REPAIRED PER SRM 57-60-01-1A.

Part: CARRIAGE — WORN (TE FLAP) · airframe 50,149 hrs · 7,958 cycles

LEFT WING&NBSP; INBOARD TRAILING EDGE FLAP NR 4 SEQUENCE CARRIAGE/TOGGLE ASSEMBLY FOUND BROKEN DURING INSPECTION. REFERENCE SDR UIEA2013051300256. REMOVED AND REPLACED LEFT WING NR 4 SEQUENCE CARRIAGE/TOGGLE ASSEMBLY IAW AMM 27-51-23-004-001.

Part: FLAP — DAMAGED (WING) · airframe 50,149 hrs · 7,958 cycles

ON WALK AROUND FOUND LEFT WING INBOARD TRAILING EDGE FLAP DAMAGED (ASYMMETRIC). INSPECTIONS COMPLETED AND REPAIR AND REPLACEMENT OF PARTS OCCURRING AS REQUIRED.

Part: STIFFENER — DAMAGED (LT WING) · airframe 50,149 hrs · 7,958 cycles

LEFT WING RIB STIFFENER INBOARD OF AILERON POWER CONTROL PACKAGE COMPARTMENT AT WBL 446 HAS DAMAGE FOUND DURING INSPECTION OF THE AREA. WORK IN PROGRESS.

Part: CARRIAGE — WORN (TE FLAP) · airframe 50,149 hrs · 7,958 cycles

LEFT WING INBOARD TRAILING EDGE FLAP NR 3 SEQUENCE CARRIAGE/TOGGLE ASSEMBLY FOUND WORN DURING INSPECTION. REMOVED AND REPLACED LEFT&NBSP; WING NR 3 SEQUENCE CARRIAGE/TOGGLE ASSEMBLY IAW AMM 27-51-23-004-001.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 49,794 hrs · 7,897 cycles

STATUS MESSAGE HYD OVERHEAT SYSTEM 1 ACCOMPANIED BY HYD PRESS ENG 1. FOUND HYD EDP LEAKED AT OUTLET PORT. REMOVED AND REPLACED NR 1 HYD EDP PER AMM 29-11-05. SERVICED NR 1 HYDRAULIC SYSTEM PER AMM 12-12-01. OPS AND LEAK CHECK GOOD. MESSAGE CLEARED.

Part: SKIN — DAMAGED (RT WING) · airframe 49,136 hrs · 7,757 cycles

ON WALK AROUND FOUND LIGHTNING STRIKE BURN MARK ON RT WINGLET T/E AT STA 121.637; WLT BL 62.836, MEASURING 2.5" X 1.0". (THE DAMAGE EXCEEDS THE SRM 57-30-01-1A-2 ALLOWABLE DAMAGE 2 - WINGLET SKIN LIMITS. DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR IAW EO 4457A451 PART 1;

Part: PDU — ODOR (MAIN DECK) · airframe 48,881 hrs · 7,717 cycles

DURING CARGO LOADING, ELECTRICAL ODOR FROM MAIN DECK 8R PDU, DEACTIVATED PDU.

Part: WARNING MESSAGE — FALSE ACTIVATION (OVERSPEED) · airframe 44,915 hrs · 7,011 cycles

THERE WAS A MOMENTARY OVERSPEED WARNING DURING AN INSTANCE OF SEVERE TURBULANCE DURING CRUISE. COMPLIED WITH THE SEVERE OR UNUSUAL TURBULANCE INSPECTIONS IAW 05-51-03. NO DEFECTS NOTED.

Part: THRUST REVERSER — DAMAGED (NR 3 ENGINE) · airframe 42,941 hrs · 6,654 cycles

FOUND DAMAGE TO THE NR 3 ENG RT THRUST REV 4 INCHES &NBSP; WIDE&NBSP; BY 2 INCHES LONG & NBSP; FROM A LIGHTNING STRIKE AT 5 O'CLOCK POS. (COMPLIED WITH LIGHTNING STRIKE INSP PER AMM 05-51-13. ACCOMPLISHED &NBSP; EO 4478A184 (FAA FORM 8110-3 DATED 17AUG2011): &NBSP; TIME LIMITED REPAIR PER PART 1. DVI EVERY 5 FC PER PART 2 REQUIRED. PERMANENT REPAIR PRIOR TO 1000 FH PER PART 3.

Part: TENSION TIE — CRACKED (FUSELAGE) · airframe 42,414 hrs · 6,551 cycles

THE FORWARD CHANNEL OF TENSION TIE AT BODY STATION 720 WAS FOUND TO BE CRACKED AT ONE HOLE. ACCOMPLISHED CATEGORY B REPAIR IAW 747-400 SRM 53-20-30 REPAIR 1. REPEAT DETAILED VISUAL INSPECTION REQUIRED EVERY 300 FLIGHT CYCLES ACCORDING TO TABLE 203. TRACKED BY MCI 416-022.

Part: RIB — WORN (MIDFLAP) · airframe 42,414 hrs · 6,551 cycles

RIGHT INBOARD TRAILING EDGE MID-FLAP INBOARD SPRING SEAL RIB FOUND TO BE WORN. SPRING SEAL RIB REPAIRED IAW HX&NBSP; RS 57-55-37144 REV A.

Part: TENSION TIE — CRACKED (FUSELAGE) · airframe 42,414 hrs · 6,551 cycles

THE FORWARD CHANNEL OF&NBSP; TENSION TIE AT BODY STATION 760 WAS FOUND TO BE CRACKED AT 3 HOLES. ACCOMPLISHED CATEGORY B REPAIR IAW 747-400 SRM 53-20-30 REPAIR 1. REPEAT DETAILED VISUAL INSPECTION REQUIRED EVERY 300 FLIGHT CYCLES ACCORDING TO TABLE 203. TRACKED BY MCI 416-023.

Part: SEAL DEPRESSOR — DAMAGED (FUSELAGE) · airframe 41,322 hrs · 6,378 cycles

DURING & NBSP; LOADING OF AIRCRAFT N416MC, & NBSP;THE LOWER, FORWARD CARGO DOOR SEAL DEPRESSOR AND RETAINER AT BS 560 WAS & NBSP; DAMAGED BY & NBSP; THE CARGO LOADER. ACCOMPLISHED INTERIM REPAIR ACCORDING TO PART 1 & NBSP;OF EO 4453A538 &AMP; FAA 8110-3 DATED 29 MAR 11. A DETAILED VISUAL INSPECTION OF THE INTERIM REPAIR IS REQUIRED PRIOR TO & NBSP; EACH FLIGHT CYCLE UNTIL PART 3 PERMANENT REPAIR IS ACCOMPLISHED & NBSP;& NBSP.

Part: FLAP — DAMAGED (LT WING) · airframe 40,521 hrs · 6,260 cycles

BIRD STRIKE INSPECTION REVEALED DAMAGE ON THE LEFT WING, INBOARD, MID FLAP, LEADING EDGE AT WBL 291.5. TIME LIMITED REPAIR ACCOMPLISHED IAW EO 4457A334 AND FAA 8110-3 DATED 30JAN11. DETAILED VISUAL INSPECTION REQUIRED EVERY 25 FLIGHT CYCLES WITH A PERMANENT REPAIR TO BE ACCOMPLISHED PRIOR TO 1000 FLIGHT HOURS.

Part: CONDUIT — DAMAGED (NLG) · airframe 38,033 hrs · 5,878 cycles

NOSE LANDING GEAR ELECTRICAL CONDUIT DAMAGED BY LOADING/UNLOADING TIE DOWN STRAP. PART ONE TIME LIMITED REPAIR ACCOMPLISHED PER ENGINEERING ORDER 4425A167, WITH FAA 8101-3 DATED 18 JULY 2010. DVI EVERY 5 FLIGHT CYCLES AND PERMANENT REPAIR AT NEXT A-CHECK AFTER PART ONE ACCOMPLISHMENT.

Part: STRUCTURE — DAMAGED (RT NACELLE) · airframe 37,504 hrs · 5,806 cycles

NR 4 ENGINE & NBSP; RIGHT CORE COWL DAMAGED DURING MAINTENANCE BY STAND. ACCOMPLISHED TIME LIMITED REPAIR PER ENGINEERING ORDER 4471A058, WITH FAA 8110-3 DATED 15 JUN 2010. DVI EVERY 2 FLIGHT CYCLES WITH PERMANENT REPAIR PRIOR TO 25 FLIGHT CYCLES.

Part: DOOR — DAMAGED (NR 4 PYLON) · airframe 37,504 hrs · 5,806 cycles

NR 4 LEFT PYLON FAIRING DOOR WAS DAMAGED DURING MAINTENANCE BY A WORK STAND. ACCOMPLISHED TIME LIMITED REPAIR PER ENGINEERING ORDER 4454A098, WITH FAA 8110-3 DATED 15 JUNE 2010. DVI EVERY 25 FLIGHT CYCLES WITH PERMANENT REPAIR PRIOR TO 2000 FLIGHT HOURS.

Part: CONDUIT — DAMAGED (RT WING) · airframe 37,187 hrs · 5,761 cycles

RIGHT WING GEAR FLEXIBLE ELECTRICAL CONDUIT DAMAGED. PART ONE TIME LIMITED REPAIR ACCOMPLISHED PER ENGINEERING ORDER 4425A157, WITH FAA 8110-3 DATED 24 MAY 2010. REPEAT DVI EVERY FLIGHT CYCLE AND PERMANENT REPAIR PRIOR TO 25 FLIGHT CYCLES AFTER PART 1 ACCOMPLISHMENT.

Part: DEPRESSOR — DAMAGED (CARGO DOOR) · airframe 34,657 hrs · 5,407 cycles

FOUND LWR AFT CARGO DOOR REAR SIDE UPPER DEPRESSOR SEAL DAMAGED 1/2 X 1/2. REMOVED/SMOOTH DAMAGED AREA AND APPLIED 2 LAYERS OF SPEED TAPE APPLIED IAW PART 1 OF EO 4453A303 IN ADDITION TO FAA 8110-3 ISSUED 5 NOV 2009. VISUAL INSP IS REQUIRED AT EVERY FLIGHT LEG UNTIL A PERMANENT REPAIR CAN BE COMPLETED AT THE ACFT'S NEXT A CHECK.

Part: ACM — DEFECTIVE (NR 1) · airframe 33,108 hrs · 5,176 cycles

IN CRUISE A LOUD RUMBLING WAS HEARD THROUGH THE PACK SYSTEM AND AN ODOR WAS NOTICED COMING THROUGH THE VENTS. CONDITIONAL INSPECTION WAS PERFORMED IAW MM 05-51-56 AND IT WAS CONFIRMED THERE IS A BAD PACK 1 ACM. PACK 1 WAS DEACTIVATED AND DEFERRED IAW MEL 21-51-1.

Part: GROMMET — LOOSE (RUDDER) · airframe 32,432 hrs · 5,084 cycles

PRE TAXI RUDDER CHECK UNSATISFACTORY. FOUND CABLE GROMMET LOOSE AND STICKING ON PULLEY. GROMMET RESECURED AND OP'S CHECKED OK IAW AMM 27-55-00 AND AMM 20-11-07-074-016.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 29,134 hrs · 4,581 cycles

DURING GROUND HANDLING THE TAIL JACK STRUCK THE TAIL SECTION OF THE AIRCRAFT NEAR THE TAIL POST FITTING IN SECTION 48 AT BS 2602. ACCOMPLISHED INTERIM REPAIR ACCORDING TO EO 4453A189, SRM 53-00-01 FIG 201, REPAIR 11. INITIAL AND REPEAT INSPECTIONS TO BE SCHEDULED PER DER 8110-3 DATED 25 JULY 2008. (A)

Part: GIMBAL JOINT — BROKEN (THRUST REVERSER) · airframe 27,830 hrs · 4,373 cycles

DURING ROUTINE INSPECTION OF NR 3 THRUST REVERSER FOUND LT LOWER ACTUATOR MOUNTING BRACKET GIMBAL BROKEN. REMOVED THE NR 3 ENGING LOWER LT ANGLE GEARBOX HOUSING AND BALLSCREW ACTUATOR AS PER AMM 78-31-22, PERFORM DVI INSPECTIONS PER EO NR 4478A065 PRIOR TO EACH CYCLE.

Part: INLET — DAMAGED (NR 3 NACELLE) · airframe 27,571 hrs · 3,213 cycles

DURING THE OIL SERVICING OF THE NR 3 ENGINE DAMAGE OCCURRED TO THE RIGHT SIDE OF THE INLET COWLING AT THE 3 O'CLOCK POSITION. ACCOMPLISHED INTERIM REPAIR PER EO NR 4471A012 PART 1 PER SRM 54-15-01.

Part: ACCESS DOOR — INFLT SEPARATION (NR NACELLE) · airframe 26,437 hrs · 4,158 cycles

NR 4 ENGINE STRUT I/B ACCESS DOOR PARTIALLY LOST IN FLIGHT AND NR 4 ENGINE STRUT O/B ACCESS DOOR PEELED BACK IN FLIGHT. MAJOR REPAIR AND PARTS REPLACEMENT ACCOMPLISHED PER XEO-51-120607, P/N: 323U2304-84, 323U2303-72.

Part: ROLLER TRAY — DAMAGED (CABIN) · airframe 26,383 hrs · 4,151 cycles

ROLLER TRAY AND SEAT TRACK DAMAGE M/D STA 1650-1800. REPAIR ROLLER TRAYS AND SEAT TRACK PER XEO NR 53-111407 SRM 51-70-12 SOYM 20-44-04

Part: DRIVE SYSTEM — FAILED (TE FLAPS) · airframe 25,844 hrs · 4,060 cycles

STATUS MESSAGE LE MULTI DRIVE AND EICAS FLAPS PRIMARY. GOT MSG AFTER EXTENDING FLAPS T/O. RETURNED TO GATE. REMOVED AND REPLACED 3-R L/E DRIVE

Part: ISOLATION VALVE — MALFUNCTIONED (APU) · airframe 25,825 hrs · 4,057 cycles

APU EICAS MESSAGE AFTER T/O. ALSO HEARD LOUD SOUND FROM ABOVE MAIN DECK SIDE CARGO DOOR. AIR TURNBACK. REPLACED APU ISOLATION VALVE, INSEPCTED DUCTS NO DEFECTS NOTED. ACCOMPLISHED PRESSURIZATION CHECK OF CARGO DOOR AND INSPECTED SEALS. NO DEFECTS NOTED, PER MM 36-11-09.

Part: STRUCTURE — LOOSE (THRUST REVERSER) · airframe 25,625 hrs · 4,022 cycles

DURING DAILY CHECK, FOUND NR 1 THRUST REVERSER INNER WIRE MESH BONDING LOOSE AND MISSING BETWEEN 6 AND 10 O'CLOCK POSITIONS. INTERIM REPAIR ACCOMPLISHED AS PER XEO 78-091604/FAA 8110-3.

Part: SUPPORT BRACKET — CRACKED (FUEL SERVICE) · airframe 25,302 hrs · 3,971 cycles

DURING WALK AROUND INSPECTION IN THE LEFT WING FUELING SERVICE PANEL BRACKET SUPPORT CRACK. PERFORMED PART 1 PER XEO 57-082107 AND INTERIM REPAIR APPROVED.

Part: UNKNOWN — UNKNOWN · airframe 24,793 hrs · 3,896 cycles

ON CLIMB-OUT, BLEED HP ENG 4, ENG 4 LOW IDLE, NAI ENG 4 MESSAGES. DEFERRED BLEED HP ENG 4 PER MEL 36-11-3 AND 78-31-1A. DEFERRED NAI 4 MESSAGE PER MEL 30-21-1B

Part: PANEL — MISSING (NR 1 NACELLE) · airframe 22,361 hrs · 3,537 cycles

ON WALK AROUND, FOUND PANEL MISSING ON NR 1 PYLON RIGHT HAND SIDE, PANEL 452 CR. INSTALLED NEW PANEL IAW MM 54-62-00.

Part: FLOORBEAM — DAMAGED (BS 1780) · airframe 22,330 hrs · 3,533 cycles

AFT CARGO COMPARTMENT AFT FLANGE OF FLOORBEAM UPPER CHORD DAMAGED AT STA 1780 RBL 25.75. AFT CARGO COMPARTMENT AFT FLANGE OF FLOORBEAM REPAIRED AS PER SRM 51-70-12 REPAIR 1 AND EO 4453A100.

Part: SEAT TRACK — DAMAGED (BS 1780-1781) · airframe 22,330 hrs · 3,533 cycles

AFT CARGO COMPARTMENT SEAT TRACK CROWN AREA DAMAGED AT STA 1780 RBL 25. AFT CARGO SEAT TRACK REPAIRED IAW SRM 53-00-52 REPAIR NR 10 AND EO NR 4453A100.

Part: MANIFOLD — CHAFED (NR 4 FUEL SYS) · airframe 21,020 hrs · 3,354 cycles

NR 4 ENGINE FUEL NOZZLE MANIFOLD LEAKING AT 12 O'CLOCK POSITION. REMOVED AND REPLACED NR 4 ENGINE RT FUEL MANIFOLD IAW AMM 73-11-10. LEAK CHECK OK.

Part: TIRE — SEPARATED (MLG) · airframe 20,848 hrs · 3,350 cycles

ON TAKEOFF FROM HNL NR 8 TIRE TREAD COMPLETELY SEPARATED FROM MAIN CARCASS CAUSING DAMAGE TO 3 WING TO BODY FAIRINGS AFT OF LT BODY GEAR. HONEYCOMB PANELS 193BL,193CL,193DL INCLUDING WTB FRAMES AT STA1540,1580 & 1620. IMPACT DAMAGE TO ELEC CONDUIT ON RT BLG SIDE BRACE AND CRUSH DAMAGE TO ELECT CONDUIT ON LT BLG IB STEERING ACTUATOR. TIRE REMAINED INFLATED AFTER LANDING.

Part: SKIN — DELAMINATED (MID FLAP) · airframe 18,287 hrs · 2,976 cycles

DURING A-4 CHECK, LEFT HAND INBOARD T/E MID FLAP HAS IMPACT DAMAGE WITH DELAM ON LOWER AFT INBOARD SURFACE AS MARKED. REPAIR CARRIED OUT IAW SRM 51-70-06 AND SRM 57-53-01.

Part: DOOR — MALFUNCTIONED (MLG)

RT BODY GEAR DOOR OPENED AFTER RETRACTION WHEN GEAR LEVER PLACED IN OFF POSITION. STATUS MSG GEAR DOOR GEAR MONITOR. GEAR PINS INSTALLED. PRESSURIZED HYD SYSTEM. OPS CHECKED DOOR IAW MM. ALL INDICATIONS OK IN ALL HANDLE POSITIONS. RT BODY GEAR DOOR DID NOT DROP AT ALL. OK FOR SERVICE. ALL SYSTEMS OPS NORMAL. GEAR PINS REMOVED. (K)

Part: ENGINE — FLAMED OUT (NR 3)

DURING AIRCRAFT DESCENT AT 30000 FT, ENGINE NR 3, NR 4 FLAMED OUT WHILE ENCOUNTERING HEAVY RAIN AND MODERATE TURBULENCE. BOTH ENGINES WERE BACK TO NORMAL AFTER RESTART. THIS CASE IS BEEN DETERMINED AS WEATHER CAUSED IFSD (IN-FLIGHT SHUT DONE) AT OCT/2004. MFG IS GOING TO REVISE THE FADEC VBV SCHEDULE TO OPEN VBV TO PREVENT SEPARATED ICE FROM GETTING INTO HPC/COMBUSTOR AT 1Q/2005.