N473MC

Part: ENGINE — MAKING METAL (NR 4) · airframe 119,336 hrs · 21,525 cycles

1.5 HOURS INTO FLIGHT, #4 OIL QUANTITY DROPPED TO 6 QTS. AT ABOUT 2.5 HOURS, QTY SHOWED 0. AT ABOUT 3 HOURS, OIL PRESSURE DROPPED TO 13 PSI AT LANDING. STATUS MESSAGE ENG 4 OIL PRESS(<P>CHECK OIL IND, IND AT 0, VISUALLY CHECK OIL CAPACITY, CAPACITY AT 0. PER MCC INSPECT MAGNETIC CHIP DETECTOR IAW AMM 79-21-00, FOUND CONTAMINATION & LOTS OF METAL DEBRIS. MCC NOTIFIED. LP 1810379 P2: CHK EICAS MSG, ENG LOW OIL PRESS, 0 PSI. AS PER MCC, ADD OIL QTY TO 20, THEN GND CRANK DRY MOTOR, FOUND NO OIL PRESSURE, NO N1 IND IAW AMM 71-00-00. MCC NOTIFIED. LP 1900155 M14: R/R #4 ENG &AMP; OPS &AMP; LEAK CHK NORMAL PER AMM 71-00-02 & W/C 71-099-02-01.

Part: SMOKE DETECTOR — FALSE ACTIVATION (ZONE 100) · airframe 119,019 hrs · 21,457 cycles

ON ARRIVAL, FIRE CGO AFT EICAS MSG, FIRE NOT SUSPECTED. LOOP FAILURES NOTED(<P>R/R SMOKE DETECTORS EQUIPMENT #9129, 9123, 9119 &AMP; 9133 IAW AMM 26-16-01/401 &AMP; IPC 26-16-00-02N. OPS CHK GOOD.</P>)

Part: FIRE WARNING — FALSE ACTIVATION (ZONE 100) · airframe 119,019 hrs · 21,457 cycles

AFT CARGO FIRE WARNING DURING TAXI WITH MOMENTARY STATUS MSG "FIRE DET AFT 2". FIRE CARGO AFT" WARNING DURING TAXI WITH STATUS MSG "CARGO DET AFT 2". TRANSFERRED TO MEL 26-16-01-02-02A MX ACTIONS COMPLIED WITH MDDR 222676. SWAPPED LOWER AFT CARGO SMOKE DETECTOR LOOP A, P/N PPC1200-00, S/N 51450, WITH LOOP B P/N PPC1200-00, S/N 3050 IN ACCORDANCE WITH AMM 26-14-01/401.&NBSP; OPS CHECK GOOD AT THIS TIME. LOOP B MESSAGE CLEARED.

Part: FIRE WARNING — FALSE ACTIVATION (ZONE 100) · airframe 119,010 hrs · 21,452 cycles

AFT CARGO FIRE WARNING DURING TAXI WITH MOMENTARY STATUS MSG "FIRE DET AFT 2". AFT CARGO DETECTOR 1A AND 2A INOP.(<P>PERFORMED OPS CHECK AND GROUND TEST FOR CARGO FIRE DETECTION SYSTEM. THIS CLEARS DMI, PLACARDS REMOVED. 0733Z/JE.&NBSP;</P>)

Part: TIRE — FAILED (MLG) · airframe 117,302 hrs · 21,128 cycles

ABNORMAL VIBRATION ON TAKE OFF BEGINNING APPROX AT 110-120 KNOTS. DECIDED TO CONTINUE. TOWER ADVISED DEBRIS FOUND ON RUNWAY. AFTER LANDING CONFIRMED 2 BLOWN TIRES. #9 & #10 MLG TIRE BLOWN CONDITIONAL INSPECTION C/W PER AMM, FOUND DURING TO RH WING TO BODY FAIRING PANEL 194BR & 194CR. R & R #9, #10, #11 & #12 MLG TIRE ASSY PER AMM 32-45-01 &AMP; IPC 32-45-04. C/W PARTS DEPARTED A/C INSPECTION PER AMM 5-51-58. PERFORMED EA 4453A136, ACCOMPLISHED TIME LIMITS REPAIR PART 1. PART 2 DUE WITHIN 1,000 F/H. TRANSFER TO NON-MEL DMI 212297 & 212298 DUE DATE 20JUL24.

Part: TIRE — FAILED (MLG) · airframe 117,302 hrs · 21,128 cycles

ABNORMAL VIBRATION ON TAKE OFF BEGINNING APPROX AT 110-120 KNOTS. DECIDED TO CONTINUE. TOWER ADVISED DEBRIS FOUND ON RUNWAY. AFTER LANDING CONFIRMED 2 BLOWN TIRES(<P>MX IN WORK WHILE IN AOGD DUE TO #9 AND #10 TIRE FAIL. AOGD ETR: 12JUL24</P>)

Part: LADDER — CRACKED (MAIN DECK) · airframe 117,035 hrs · 21,085 cycles

M/D CREW LADDER #1 STEP FOUND CRACK (COUNT FROM BOTTOM)(<P>#1 STEP REPAIRED AS PER RI-25-00-16893 REV.A. NO FURTHER DEFECTS NOTED.</P>)

Part: DOOR FRAME — CRACKED (BS 800) · airframe 117,035 hrs · 21,085 cycles

1EA HOLE FOUND CRACK AT L2 DOOR FWD CORNER STR 17(<P>&NBSP;INNER CHORD REPAIRED AS PER SRM 53-20-07-2R-12 REPAIR 12 FIG 201 DETAIL II. NO FURTHER DEFECTS NOTED.</P>)

Part: SEAT TRACK — CORRODED (BS 1890-1930) · airframe 117,035 hrs · 21,085 cycles

M/D STA 1900 LBL 75.92 SEAT TRACK CROWN FOUND CRACKED APPROXIMATELY 2"(<P>SEAT TRACK CRACK AREA REPAIRED AS PER SRM 53-00-52-2R-6 REPAIR 6 FIG 201. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — DELAMINATED (LT ELEVATOR TE) · airframe 117,035 hrs · 21,085 cycles

LH I/B ELEVATOR UPPER T/E FOUND DELAMINATION(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-06 PAR 5A. NO FURTHER DEFECTS NOTED.</P>)

Part: STRUCTURE — DAMAGED (BS 320) · airframe 117,035 hrs · 21,085 cycles

CHORD P/N: 65B07942U72 FOUND 11EA FASTENER LOCATION S.E.M.(<P>FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER AS PER RI-53-00-16880 REV.A. NO FURTHER DEFECTS NOTED.</P>)

Part: FITTING — OUT OF ALIGNMENT (BS 290-300) · airframe 117,035 hrs · 21,085 cycles

FITTING P/N: 65B07953U5 FOUND 1EA FASTENER HOLE MISALIGNMENT AND 1EA FASTENER HOLE S.E.M.(<P>1EA FASTENER HOLE INSTALL FREEZE PLUG AND FITTING INSTALLED AS PER RI-53-00-16880 REV.A. NO FURTHER DEFECTS NOTED.</P>)

Part: STRUCTURE — DAMAGED (BS 260) · airframe 117,035 hrs · 21,085 cycles

CHORD P/N 65B07942U16 1EA FASTENER HOLE S.E.M.(<P>CHORD S.E.M. FASTENER HOLE 1EA REPLACED AS PER RI-53-00-16880 REV A. NO FURTHER DEFECTS NOTED.</P>)

Part: SPAR — CRACKED (LT WING) · airframe 117,035 hrs · 21,085 cycles

LHW WS 382.22 O/B MID SPAR AFT SIDE 2EA FASTENER HOLES CRACK(<P>MID SPAR WEB 2EA FASTENER HOLES CRACK AREA REPAIRED AS PER RI-57-20-16903 REV.A. NO FURTHER DEFECTS NOTED.</P>)

Part: SUPPORT BRACKET — BROKEN (RT WING) · airframe 117,035 hrs · 21,085 cycles

R/H WLG WING REAR SPAR - WS 380 STIFFENER ATTACHED SUPPORT BRACKET FOUND BROKEN(<P>SUPPORT BRACKET P/N: 65B12757-4 FABRICATED AS PER DRAWING AND RI NO.RI-57-00-16908 REV.A AND INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.&NBSP;</P>)

Part: INTERCOSTAL — CRACKED (BS 388 S0) · airframe 117,035 hrs · 21,085 cycles

UPPER DECK STA 388 S-0 AREA 1EA CRACK FOUND AT INTERCOSTAL, CRACK THROUGH BETWEEN 2EA FASTENER HOLES(<P>INTERCOSTAL REPAIRED AS PER RI-53-10-16877 REV.A. NO FURTHER DEFECTS NOTED.</P>)

Part: FRAME — CRACKED (BS 2598) · airframe 117,035 hrs · 21,085 cycles

1EA FASTENER HOLE CRACK AT STA 2598 L/H BTN WL 310 AND WL 320 FRAME SUPPORT AREA(<P>FRAME SUPPORT CRACK FASTENER HOLE REPAIRED AS PER RI-53-13-16910 REV.A, REPAIRED IS CAT C. NO FURTHER DEFECTS NOTED.</P>)

Part: FRAME — CHAFED (NR 3 NACELLE) · airframe 117,035 hrs · 21,085 cycles

NO.3 ENG L/H CORE COWL #2 FRAME CHAFING (COUNT FROM FWD)(<P>FRAME REPAIRED AS PER SRM 54-41-02-2R-2 REPAIR 2 FIG 201. NO FURTHER DEFECTS NOTED.</P>)

Part: FITTING — CHAFED (BS 1000 RBL 11) · airframe 117,035 hrs · 21,085 cycles

M/D STA 1000 RBL 11" INTERCOSTAL LUG FITTING FASTENER HOLE CHAFING(<P>CHAFING INTERCOSTAL LUG FITTING REPLACEMENT AS PER IAI DWG: 366-53-15-A2614 SHT.1 ISSUE J. NO FURTHER DEFECTS NOTED.</P>)

Part: STRUCTURE — DAMAGED · airframe 117,035 hrs · 21,085 cycles

CHORD PN 65B07941U111 FOUND 14EA FASTENER HOLES S.E.M.(<P>14EA FASTENER HOLES REPAIRED AS PER RI-53-00-16880 REV A. NO FURTHER DEFECTS NOTED.</P>)

Part: TENSION TIE — CRACKED (BS 920) · airframe 117,035 hrs · 21,085 cycles

L/H STA 920 TENSION TIE FWD CHANNEL UPPER FLANGE AT FRAME AREA CRACK(<P>FWD CHANNEL REPAIRED AS PER RI-53-40-16901 REV.A. NO FURTHER DEFECTS NOTED.</P>)

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 117,035 hrs · 21,085 cycles

U/D STA 490 CEILING PNL EMERGENCY LT ASSY WIRE ATT SCREW FOUND MISSING(<P>U/D STA 490 CEILING PNL EMERGENCY LT ASSY REPLACED IAW AMM 33-51-04. OPS CHK GOOD.</P>)

Part: SUPPORT BEAM — CORRODED (RT WING LE) · airframe 117,035 hrs · 21,085 cycles

RHW L/E FRONT SPAR CAVITY LOWER FIXED PANEL FWD SECTION SUPPORT BEAM FOUND CORROSION AT ILES 480 (#15 KRUEGER FLAP AREA)(<P>SUPPORT BEAM REPAIRED AS PER RI NO. RI-57-41-16871 REV.A. NO FURTHER DEFECTS NOTED.</P>)

Part: FILLER — CRACKED (BS 880) · airframe 117,035 hrs · 21,085 cycles

1EA HOLE FOUND CRACK AT RH STA 880 TENSION TIE FILLER AREA(<P>FILLER REPLACED AS PER RI-53-40-16901 REV.A. NO FURTHER DEFECTS NOTED.</P>)

Part: SUPPORT BEAM — DAMAGED (BS 260-280) · airframe 117,035 hrs · 21,085 cycles

INSTALL SUPPORT BEAM P/N: 141U1193-43 (3EA) AT LH SIDE &AMP; P/N: 141U1193-44 (3EA) AT RH SIDE (BOTH STA 260-280 BETWEEN WL 150 AND WL 170) FOUND BEAMS JOGGLE DEPTH INSUFFICIENT.(<P>TOTAL 6EA TAPERED SHIMS MADE AND INSTALLED AS PER RI-53-00-16880 REV.A. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — CORRODED (BS 1705 S42L) · corrosion level 2 · airframe 117,035 hrs · 21,085 cycles

FUSELAGE EXTERNAL SKIN BS1705 STR 42L FOUND CORROSION.(<P>SKIN CORROSION AREA REPAIRED AS PER SRM 53-00-01-2R-1 REPAIR 1 FIG 201 DETAIL I. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — CRACKED (BS 560 S23L) · airframe 117,035 hrs · 21,085 cycles

SECTION 42 FUSELAGE - LH STA 560 BELOW STR 23 2EA FASTENER HOLE EXTERNAL SKIN FOUND CRACK(<P>SKIN FASTENER HOLES (2EA) CRACK AREA REPAIRED AS PER SRM 53-00-01-2R-13 REPAIR B FIG 201. THIS REPAIR IS CAT B, FOLLOW UP ACTION AS PER SRM 53-00-01-2R-13 REPAIR 13 FIG 201 TABLE II. NO FURTHER DEFECTS NOTED.</P>)

Part: SEAT TRACK — CORRODED (BS 1710-1720) · airframe 117,035 hrs · 21,085 cycles

M/D - STA 1710-1720 RBL 11" SEAT TRACK FOUND CORRORED(<P>CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, BLEND OUT AREA MEASURED: L=3" W=0.7" D=0.017" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED.</P>)

Part: SUPPORT BRACKET — CORRODED (LT WING) · airframe 117,035 hrs · 21,085 cycles

LHW - L/E CAVITY AT WS 1260 SUPPORT BRACKET FOUND SURFACE CORROSION AS MARKED(<P>LHW - L/E CAVITY AT WS 1260 SUPPORT BRACKET REPLACED AS PER AMM 20-51-01. NO FURTHER DEFECTS NOTED.</P>)

Part: TENSION TIE — CRACKED (BS 940) · airframe 117,035 hrs · 21,085 cycles

2EA HOLE FOUND CRACK AT RH STA 940 TENSION TIE FWD CHANNEL, NESTED STRAP, FILLER (3 LOCATIONS)(<P>FWD CHANNEL AND FWD DOUBLER AND FILLER REPAIRED AS PER RI-53-40-16901 REV.A. NO FURTHER DEFECTS NOTED.</P>)

Part: TENSION TIE — CRACKED (BS 960) · airframe 117,035 hrs · 21,085 cycles

1EA HOLE FOUND CRACK AT RH STA 960 TENSION TIE FWD CHANNEL AND AFT CHANNEL(<P>FWD CHANNEL AND AFT CHANNEL REPAIRED AS PER RI-53-40-16901 REV.A. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — CRACKED (BS 540 S23L) · airframe 117,035 hrs · 21,085 cycles

SECTION 42 FUSELAGE - LH STA 540 BELOW STR 23 2EA FASTENER HOLE EXTERNAL SKIN FOUND CRACK(<P>SKIN 2EA FASTENER HOLES CRACK AREA REPAIRED AS PER SRM 53-00-01-2R-13 REPAIR 13 FIG 201. THIS REPAIR IS CAT B, FOLLOW UP ACTION AS PER SRM 53-00-01-2R-13 REPAIR 13 FIG 201 TABLE. NO FURTHER DEFECT NOTED.</P>)

Part: FRAME — CHAFED (NR 2 NACELLE) · airframe 117,035 hrs · 21,085 cycles

NO.2 ENG L/H CORE COWL #2 FRAME CHAFING (COUNT FROM FWD)(<P>FRAME REPAIRED AS PER SRM 54-41-02-2R-2 REPAIR 2 FIG 201, NO FURTHER DEFECTS NOTED.</P>)

Part: SPAR WEB — CRACKED (RT WING) · airframe 117,035 hrs · 21,085 cycles

RHW #3 MAIN TANK MID SPAR WEB AFT FACE BETWEEN WS 382.22 AND WS 411.41 AREA FOUND 2EA FASTENER HOLE CRACK(<P>MID SPAR WEB 2EA FASTENER HOLES CRACK AREA REPAIRED AS PER RI-57-20-16903 REV.A. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 117,035 hrs · 21,085 cycles

LHW I/B T/E MID FLAP UPR SURFACE I/B AFT PNL 577JT AFT EDGE SURFACE CORRODED(<P>PANEL REPAIRED AS PER RI NO: RI-57-53-16875 REV.A. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — DAMAGED (RT WING) · airframe 117,035 hrs · 21,085 cycles

RHW UPPER SURFACE T/E APPROX 48" FROM WINGLET FOUND 1EA LIGHTENING STRIKE MARK(<P>LIGHTENING STRIKE CONDUCTING STRAP FABRICATED AS PER BOEING DWG 112U0700 AND PL. NEW CONDUCTING STRAP INSTALLED AS PER BOEING DWG 112U0700. NO FURTHER DEFECTS NOTED.</P>)

Part: STIFFENER — CRACKED (NLG WW) · airframe 117,035 hrs · 21,085 cycles

CRACK WERE FOUND ON RH NOSE WHEEL WELL SIDE PANEL STA 320-340 WL150 STIFFENER 4EA FASTENER HOLES(<P>STIFFENER REPLACED REFER ATLAS AIR EO 4453A223-1 AND SB 747-53A2562 R.3. NO FURTHER DEFECTS NOTED.</P>)

Part: TENSION TIE — CRACKED (BS 1040) · airframe 117,035 hrs · 21,085 cycles

2EA HOLES FOUND CRACK AT R/H STA 1040 TENSION TIE FWD CHANNEL AND NESTED DOUBLER(<P>FWD CHANNEL AND NESTED DOUBLER REPAIRED AS PER RI-53-40-16901 REV.A. NO FURTHER DEFECTS NOTED.</P>)

Part: DOOR FRAME — CRACKED (BS 800) · airframe 117,035 hrs · 21,085 cycles

1EA HOLE FOUND 2EA CRACKS AT R2 DOOR FWD FRAME STR 17(<P>INNER CHORD REPAIRED AS PER SRM 53-20-07-2R-12 REPAIR 12 FIG 201. NO FURTHER DEFECTS NOTED.</P>)

Part: SUPPORT — CORRODED (LT WING) · corrosion level 2 · airframe 117,035 hrs · 21,085 cycles

LHW UPPER FIXED PANEL 511CTA O/B SUPPORT CHORD FOUND CORRODED.(<P>CORRODED AREA BLENDED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, BLEND OUT AREA MEASURED: L=18" X W=1.6" X D=0.035" WITHIN SRM 57-41-09-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED.</P>)

Part: SEAT TRACK — CORRODED (BS 2090-2190) · airframe 117,035 hrs · 21,085 cycles

M/D STA 2100-2120 RBL 11" SEAT TRACK I/B FLANGE FOUND CRACK(<P>SEAT TRACK CRACK AREA REPAIRED AS PER SRM 53-00-52-2R-12 REPAIR 12 FIG 201. NO FURTHER DEFECTS NOTED.</P>)

Part: STIFFENER — CRACKED (NLG WW) · airframe 117,035 hrs · 21,085 cycles

CRACK WERE FOUND ON LH NOSE WHEEL WELL PANEL STA 320-340 WL140 STIFFENER 5EA FASTENER HOLES(<P>STIFFENER REPLACED REFER ATLAS AIR EO 4453A223-1 AND SB B747-53A2562 R3. NO FURTHER DEFECTS NOTED.&NBSP;</P>)

Part: BEAM — CHAFED (BS 1912 LBL 18) · airframe 117,035 hrs · 21,085 cycles

AFT CARGO STA 1912 LBL 18" CABLE HOLE FOUND CHAFING (CONTACT WITH PDU CONTROL CABLE)(<P>BEAM CHAFING AREA REPAIRED AS PER RI-53-60-16863 REV.A. NO FURTHER DEFECTS NOTED.</P>)

Part: TENSION TIE — CRACKED (BS 900) · airframe 117,035 hrs · 21,085 cycles

1EA HOLE FOUND CRACK AT RH STA 900 TENSION TIE NESTED DOUBLER AREA(<P>NESTED DOUBLER REPAIRED AS PER RI-53-40-16901 REV.A. NO FURTHER DEFECTS NOTED.</P>)

Part: SUPPORT BRACKET — CORRODED (RT WING) · airframe 117,035 hrs · 21,085 cycles

RHW - L/E FRONT SPAR CAVITY LOWER FIXED FAIRING FWD VERT SUPPORT BRACKET FOUND CORROSION NEAR OLES 1564 (#26E L/E SLAT AREA)(<P>RHW - L/E FRONT SPAR CAVITY LOWER FIXED FAIRING FWD VERT SUPPORT BRACKET REPLACED AS PER AMM 20-51-01. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — DELAMINATED (RT WING K FLAP) · airframe 117,035 hrs · 21,085 cycles

RHW #15 K/FLAP EXT SURFACE FOUND DELAMINATION(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED.</P>)

Part: WEB — CRACKED (HORIZONTAL STAB) · airframe 117,035 hrs · 21,085 cycles

EMP L/H HORI STAB TIP FAIRING SUPPORT WEB LWR CHORD FOUND CRACK(<P>LWR CHORD REPAIRED AS PER SRM 55-10-09-2R-13 REPAIR 13 FIG 201. NO FURTHER DEFECTS NOTED.</P>)

Part: FITTING — CHAFED (BS 1000 LBL 11) · airframe 117,035 hrs · 21,085 cycles

M/D STA 1000 LBL 11" INTERCOSTAL LUG FITTING BOLT HOLE CHAFING(<P>CHAFING INTERCOSTAL LUG FITTING REPLACEMENT AS PER IAI DWG: 366-53-15-A2614 SHT.1 ISSUE J. NO FURTHER DEFECTS NOTED.</P>)

Part: DOOR FRAME — CRACKED · airframe 117,035 hrs · 21,085 cycles

M/D L2 DOOR FWD FRAME UPPER CRACK(<P>FRAME UPPER CRACK AREA REPAIRED AS PER SRM 52-10-02-2R-5 REPAIR 5 FIG 201. NO FURTHER DEFECTS NOTED.</P>)

Part: SEAT TRACK — CORRODED (BS 2090-2190) · airframe 117,035 hrs · 21,085 cycles

M/D STA 2140-2160 RBL 11" SEAT TRACK FOUND CORRODED(<P>SEAT TRACK CORROSION AREA REPAIRED AS PER SRM 53-00-52-2R-12 REPAIR 12 FIG 201. NO FURTHER DEFECTS NOTED.</P>)

Part: FITTING — DAMAGED (BS 2598) · airframe 117,035 hrs · 21,085 cycles

ACCOMPLISHMENT OF ATLAS EO 4453B761 PART 1-2 FOUND ALL EXISTING FASTENER HOLES LARGER (8EA) AND FASTENER HOLE CRACK AT L/H FRAME SUPPORT(<P>L/H FWD LWR FTG REPLACED AND L/R FASTENER INSTALLED AS PER RI-53-13-16910 REV.A. NO FURTHER DEFECTS NOTED</P>)

Part: FITTING — DAMAGED · airframe 117,035 hrs · 21,085 cycles

FITTING FOUND 2EA FASTENER HOLES S.E.M.(<P>S.E.M. CONDITION ACCEPTED AS PER RI-53-00-16880 REV A. NO FURTHER DEFECTS NOTED.</P>)

Part: TENSION TIE — CRACKED (BS 980) · airframe 117,035 hrs · 21,085 cycles

2EA HOLES FOUND CRACK AT RH STA 980 TENSION TIE FWD CHANNEL AND NESTED DOUBLER(<P>FWD CHANNEL AND NESTED DOUBLER REPAIRED AS PER RI-53-40-16901 REV.A. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 117,035 hrs · 21,085 cycles

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

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 117,035 hrs · 21,085 cycles

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

Part: SEAT TRACK — CORRODED (BS 1960-1980) · airframe 117,035 hrs · 21,085 cycles

M/D STA 1960-1980 RBL 11" SEAL TRACK FOUND CORRODED(<P>CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, BLEND OUT AREA MEASURED: L=5" W=0.7" D=0.020" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED&NBSP;</P>)

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 117,035 hrs · 21,085 cycles

EMERGENCY LIGHTS BATTERY PACKS M5055 AND M5057 CAPACITY CHECK FAIL(<P>EMERGENCY LIGHTS BATTERY PACKS M5055 AND M5057 REPLACED PER AMM 33-11-00. OPS CHK GOOD.&NBSP;</P> / <P>SN 55565 &AMP; 33111</P>)

Part: CIRCUIT CARD — FAULTED (AFLOTS) · airframe 116,595 hrs · 21,008 cycles

RTO DUE TO AFT CARGO FIRE WARNING DURING T/O ROLL.(<P>REMOVED AND REPLACED AFT CARGO AFOLTS CARD (A32). SYSTEM GROUND TEST PASSED IAW AMM 26-10-01</P>)

Part: START VALVE — FAULTED (NR 2) · airframe 116,445 hrs · 20,984 cycles

ENG 2 LAGGING BEHIND OTHER 3 ON APPLICATION OF TAKEOFF POWER. AIRCRAFT YAWED SLIGHTLY TO THE LEFT, SPEED IN THE 20 TO 30 KNOT RANGE WHEN TAKEOFF REJECTED. #2 START VALVE FOUND NOT CLOSED AND WOULD NOT CLOSE.(<P>START VALVE AND STARTER BOTH REPLACED IAW AMM 80-11-02/401. OPS CHK GOOD.</P>)

Part: START VALVE — FAULTED (NR 2) · airframe 116,445 hrs · 20,984 cycles

REJECTED TAKE OFF DUE TO AIRCRAFT SURGING. LOW SPEED REJECT(<P>#2 START VALVE FOUND NOT FULLY CLOSED, NOT ALLOWING ENG TO ACCELERATE, WITHIN NORMAL PARAMETERS. #2 ENG VALVE REPLACED PER AMM 80-11-02. PERF INLET AND EXHAUST INSP PER AMM 72-00-00, NO DEFECTS NOTED.</P>)

Part: CIRCUIT CARD — FAULTED (AFLOTS) · airframe 116,261 hrs · 20,959 cycles

AFT CARGO FIRE WARNING ON FINAL APPROACH AND AGAIN ON THE GROUND. PRECEDED BY AFT CARGO #2 LOOP A AND AFT CARGO #3 LOOP B STS MSG.(<P>REMOVED AND REPLACED A33 AFOLTS CARD AS PER AMM 26-10-01-004-001. OPS CHECK OK</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 115,174 hrs · 20,687 cycles

BOTH ATC FAILED IN FLIGHT. UNABLE TO ENTER MEXICAN AIRSPACE. DIVERTED TO LAX. ENTERED ON LP 1769776 ITEMS 2 & 3(<P>LOGBOOK PAGE 1769776 ITEM 2 (ATC-LEFT) R/R&NBSP; LH ATC IAW AMM- 34-53-02. OPS CHECK GOOD.</P> / <P>LOGBOOK PAGE 1769776 ITEM 3 (ATC-RIGHT) PERFORMED RH ATC GROUND TEST IAW AMM-34-53-02, MSG CLEARED</P>)

Part: CIRCUIT CARD — UNKNOWN (UNKNOWN) · airframe 114,631 hrs · 20,595 cycles

"FIRE CARGO AFT WARNING" ON TAKEOFF ROLL. REJECTED TAKEOFF, FIRE BELL AND WARNING EICAS INTERMITTENTLY GOING OFF.(<P>REMOVED AND INSTALLED AFT CARGO AFOLTS CARD IAW AMM 26-10-01-004-001 AND 26-10-01-404-006. GROUND TEST PASS.</P>)

Part: CIRCUIT CARD — UNKNOWN (UNKNOWN) · airframe 114,457 hrs · 20,563 cycles

FDE FAULT CARGO DET AFT 2 STATUS MSG.(<P>AFTER VERIFYING THERE WAS NO DANGER, TESTED FIRE LOOP PER DMI 187114 IAW DDG 26-16-01-02A&NBSP; AND APPLIED THE SAME. R/R AFOLPS DATA CARD PER AMM 26-10-01. OPS CHECK GOOD.</P>)

Part: SEAT — UNKNOWN (UNKNOWN) · airframe 113,816 hrs · 20,444 cycles

FIRST OFFICERS SEAT SLID BACKWARDS DURING T/O ROLL(<P>R/R SEAT IAW B747 AMM 25-11-01-401. OPS CKS GOOD&NBSP;</P>)

Part: SMOKE DETECTOR — FAULTED (AFT CARGO) · airframe 113,147 hrs · 20,327 cycles

EICAS, CARGO AFT FIRE ON TAKEOFF. EXTINGUISHED BEFORE FINISHING CHECKLIST. LWR EICAS SHOWN INTERMITTENT STATUS MSG CARGO AFT 1 LOOP A, FAIL AND FAULT MSG REPORT SHOWN 26354. REFER TO SUPPLEMENT FIM 26-16 TASK 892, SMOKE DETECTOR M9121 REPLACED AND MAINTENANCE TESTED NORMAL IAW SUPPLEMENT AMM 26-16-01. LOG 1570449 ITEM #8 REFER TO SUPPLEMENT FIM 26-16 TASK 892 SMOKE DETECTOR M9125 ALSO REPLACED FOR PRECAUTION AND MAINTENANCE TEST RESULT NORMAL IAW SUPPLEMENT AMM 26-16-01.

Part: SMOKE DETECTOR — NONE · airframe 112,395 hrs · 20,184 cycles

FIRE LOWER CARGO AFT WARNING CAME ON PASSING 6000' ON CLIMB AND WENT AWAY. PRIOR TO ACCOMPLISHING QRH AGAIN, CAME ON DURING DESCENT AROUND 4000' AND WENT AWAY PRIOR TO QRH.(<P>INSTALLED SMOKE DETECTOR LWR AFT 2B PER AMM 26-16-01-401-008. PROCEDURE TEST PER AMM 26-16-01-864-018. OPS CHECK GOOD. NO DEFECTS NOTED</P>)

Part: UPLOCK BRACKET — CORRODED · airframe 111,377 hrs · 20,006 cycles

CORROSION FOUND ON RH WLG UPLOCK MECHANISM AFT SUPPORT BRACKET R/R WLG UPLOCK AFT SUPPORT ASSY IAW SRM 51-40-02 PARA 7 & AMM 32-32-08

Part: UPLOCK BRACKET — CORRODED · airframe 111,377 hrs · 20,006 cycles

CORROSION FOUND ON RH WLG UPLOCK MECHANISM FWD SUPPORT BRACKET R/R RH WLG UPLOCK SUPPORT ASSY IAW SRM 51-40-02 PARA 7 & AMM 32-32-08</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

LH STA 2231 FRAME STR 25L 1EA HOLE FOUND CRACK.(<P>M/D STA 2231 STR 25L, 1EA FASTENER HOLE CRACK AREA OVERSIZE REPAIRED IAW RI-53-00-15534 REV B</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

EMP STA 2638 - 2658 STR 17L, APU ACCESS DOOR 317AL CUTOUT FWD UPPER CONNER FOUND EXISTING REPAIR.(<P>EMP STA 2638-2658 STR 15L - 18L, APU ACCESS DOOR 317AL CUTOUT FWD UPPER CORNER EXISTING REPAIR LOCATION RE-DO REPAIRED IAW RI-53-81-15541 REV A.</P>)

Part: BUSHING — NONE · airframe 111,020 hrs · 19,942 cycles

M/D STA 1000 LBL 11.33 FLOOR SUPPORT IB CROSS BOLT HOLE FOUND ENLARGED(<P>M/D STA 1000 LBL 11.33 LUB FTG P/N : 366-53-15-A13641-101 REPLACED IAW SRM 51-10-02 AND P/N : 366-53-15-A1364-103 ATT BUSHING REPLACED IAW SOPM 20-50-03.</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

FX - AIRCON BAY WING CENTER SECTION LOWER SECTION LOWER SURFACE RH O/B CHORD CRACK AT STA 1231 RBL 104.(<P>FX - STA 1231 RBL 104" AIRCON BAY WING CENTER UPPER CHORD P/N : 65B10750-38 CRACK AREA REPAIRED IAW RI-57-00-15529 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

FX - APU TAIL CONE RH STA 2640 - 2680 RIVET FOUND LOOSE.(<P>APU COMPARTMENT STA 2670 - STA 2690 WL 305 - WL 315, ELONGATE FASTENER HOLE REPAIRED IAW RI-53-80-15497 REV B.</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

EO 4453A797 PART 3 - PART 6, SKIN AND BEAR STRAP CRACK AT THE AFT UPPER CORNER OF THE M.E.D 5 CUTOUT - MODIFICATION - SB 747-53A2839.(<P>EO 4453BA797 PART 3 - PART 6, SKIN AND BEAR STRAP CRACK AT THE AFT UPPER CORNER OF THE M.E.D 5 CUTOUT - MODIFICATION - SB 747-53A2839 ACCOMPLISHED.</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

R/H O/B MID FLAP T/E (FROM O/B 7TH) SCREW HOLE FOUND ELONGATED(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5K REV.114 ,FEB 20/2022</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

LHW ILES 1116 L/E NOSE BEAM LOWER CHORD FOUND CRACK.(<P>LHW FIXED L/E NOSE BEAM ILES 1057 - ILES 1116 LOWER CHORD CRACK AREA REPAIRED IAW RI-57-41-15518 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

RHW O/B FORE FLAP T/E 120 FROM O/B FOUND DELAMINATED(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A REV.114 ,FEB 20/2022</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

LHW O/B FORE FLAP L/E 38" FROM I/B FOUND DELAMINATED(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A REV.114 ,FEB 20/2022</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

FX - AIRCON BAY WING CENTER SECTION LOWER SECTION LOWER SURFACE LH O/B CHORD CRACK AT STA 1231 LBL 104.(<P>FX - STA 1231 LBL 104" AIRCON BAY WING CENTER UPPER CHORD P/N : 65B10750-37 CRACK AREA REPAIRED IAW RI-57-00-15528 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

RHW #12 SPOILER LWR SURFACE SEVERAL AREA DISBOND(<P>PERFORMED PERMANENT METAL HOTBOND REPAIR AS PER SRM 51-70-10 REPAIR4 REV.114 ,FEB 20/2022</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

LH BS 800 FRAME AREA, 2EA CRACKS FOUND AT STA 14L. STRAP APPROX 1/8 INCH RUNNING FWD. 1/4 INCH RUNNING AFT.(<P>M/D STA 800 STR 14L. FRAME STRAP P/N : 65B26468-1, 1EA FASTENER HOLE CRACK AREA REPAIRED IAW RI-53-00-15527 REV A.</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

RHW L/E ILES 630 RIB ATT #5 STIFFENER FOUND CRACK(<P>RHW L/E ILES 630 RIB ATT #5 STIFFENER P/N : 65B15696-78 CRACK AREA REPAIRED AND INSTALLED IAW RI-57-00-15540 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

M/D STA 1080 TENSION TIE L/H AFT CHANNEL FOUND CRACK(<P>UPPER DECK STA 1080 L/H TENSION TIE AFT CHANNEL CRACK AREA REPAIRED IAW RI-53-00-15548 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

L/H WLG W/W CTR TANK L/H OVERRIDE / JETTISON PUMP 2EA BONDING JUMPER ATT TO TANK SURFACE AREA CORRODED.(<P>L/H WLG W/W CTR TANK L/H OVERRIDE / JETTISON PUMP 2EA BONDING JUMPER ATT TO TANK SURFACE AREA CORR REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01, WITHIN SRM 57-10-10 ADL 2 FIG 101.</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

LHW O/B AFTER FLAP O/B UPPER PANEL CHAFING(<P>PERFORMED PERMANENT METAL HOTBOND REPAIR AS PER SRM 51-70-10 REPAIR2 REV.114 ,FEB 20/2022</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

R/H WLG W/W CTR TANK R/H OVERRIDE/JETTISON PUMP 2EA BONDING JUMPER ATT TO TANK SURFACE AREA CORRODED.(<P>R/H WLG W/W CTR TANK R/H OVERRIDE/JETTISON PUMP 2EA BONDING JUMPER ATT TO TANK SURFACE AREA CORR REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01, WITHIN SRM 57-10-10 ADL 2 FIG 101.</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

FX - APU TAIL CONE RH FRAME AND UPPER OF WL 310 FOUND CRACKED ( UPR OF PREVIOUS REPAIR AREA )(<P>APU COMP STA 2680.18 RH FRAME ON EXISTING REPAIR SEGMENT CRACK AREA REPAIRED IAW RI-53-80-15504 REV B</P>)

Part: NONE — NONE · corrosion level 2 · airframe 111,020 hrs · 19,942 cycles

M/D - R3 DOOR AFT CUTOUT UPPER CORNER FOUND CORROSION(<P>RH DOOR 3 CUTOUT AFT UPPER CORNER INBOARD FACE CORROSION AREA REPAIRED IAW RI-53-40-15538 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

M/D STA 1800 - 1820 LBL 90 SEAT TRACK CROWN FOUND CORROSION(<P>M/D STA 1800 - 1820 LBL 99 SEAT TRACK CROWN CORROSION REMOVED IAW IAI SRM 51-10-02 AND REPROTECTED IAW IAI SRM 51-20-01, CHECKED WITHIN IAI SRM 53-00-52 ADL 1, FIG 101.</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

RH BS 1480 LONGERON WEB SPLICE AREA CRACK WAS FOUND AT FASTENER HOLE #20 AT BULKHEAD CHORD.(<P>RH BS 1480 LONGERON WEB SPLICE AREA AT FASTENER HOLE #20 CRACKED HOLE REPAIRED AS PER SB 747-53A-2390 REV 1. #20 FASTENER HOLE OVERSIZE (0.500") REPAIRED IAW SB 747-53A2390 REV 1. P.53</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

RH BS 1480 LONGERON WEB SPLICE AREA CRACK WAS FOUND AT FASTENER HOLE #26 AT BULKHEAD CHORD.(<P>RH BS 1480 LONGERON WEB SPLICE AREA AT FASTENER HOLE #26 CRACK HOLE REPAIRED AS PER SB 747-53A2390 REV 1. #26 FASTENER HOLE OVERSIZE ( 0.500" ) REPAIRED IAW SB 747-53A2390 REV 1 P.55.</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

M/D STA 1020 TENSION TIE RH AFT CHANNEL FOUND CRACK(<P>UPPER DECK STA 1020 R/H TENSION TIE AFT CHANNEL CRACK AREA REPAIRED IAW RI-53-00-15548 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

LHW L/E ILES 630 RIB ATT #5 STIFFENER FOUND CRACK(<P>LHW L/E ILES 630 RIB ATT #5 STIFFENER P/N : 65B15696-78 CRACK AREA REPAIRED AND INSTALLED IAW RI-57-00-15539 REV A</P>)

Part: NONE — NONE · corrosion level 2 · airframe 111,020 hrs · 19,942 cycles

U/D STA 680 - 700 STR 12R - STR 13R, FLOOR WEB ATTACHED STIFFENER FOUND HEAVY CORROSION.(<P>U/D STA 685 RBL 80 - RBL 95 WL 307.5 STIFFENER P/N : 65B06144-882 REPLACED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-40-02.</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

LHW ILES 116 L/E NOSE BEAM UPPER CHORD FOUND CRACK(<P>LHW FIXED L/E ILES 1057 - ILES 1116 NOSE BEAM UPPER CHORD CRACK AREA REPAIRED IAW RI-57-41-15518 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

LHW O/B MID FLAP L/E 120" - 125" FROM O/B FOUND DELAMINATED(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A REV.114 ,FEB 20/2022</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

#4 NACELLE STRUT THRUST TANG - COVER PLATE CANNOT BE INSTALLED, DUE TO NO ACCESS ON THE UNDERNEATH AREA.(<P>#4 NACELLE STRUT THRUST TANK - COVER PLATE FASTENER SUBSTITUTION IAW RI-54-00-15545 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

LH BS 900 MOST INNER ROW OF FASTENER HOLES AT TENSION TIE TO FRAME ATTACHMENT LOWER HOLE CRACK WAS FOUND ON FWD CHANNEL RUNNING UP AND DOWN THRU THICKNESS.(<P>STA 900 L/H TENSION TIE FWD CHANNEL 1EA FASTENER HOLE CRACK AREA REPAIRED IAW RI-53-00-15553 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

M/D STA 940 TENSION TIE R/H STRUCTURE FOUND CRACK(<P>UPPER DECK STA 940 R/H TENSION TIE AFT CHANNEL CRACK AREA REPAIRED IAW RI-53-00-15548 REV A</P>)

Part: PANEL — NONE · airframe 111,020 hrs · 19,942 cycles

#2 PYLON VALVE ACCESS PNL #462EL FOUND 2EA SCREWS HOLES ELONGATED(<P>#2 PYLON VALVE ACCESS PNL #462EL P/N : 311U2060-137 FABRICATED AND REPLACED IAW RI-54-50-15536 REV A</P>)

Part: BATTERY PACK — NONE · airframe 111,020 hrs · 19,942 cycles

UPPER DECK L/H DOOR SQUIB PWR SUPPLY BATTERY INOP ( M7037 )(<P>U/D L/H DOOR SQUIB PWR SUPPLY BATTERY PACK REPLACED AND INSTALLATION TEST RESULT NORMAL IAW AMM 52-23-14 REV 104 - 15 MAR 2022</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

U/D EXIT SIGN R/H FOUND WENT OFF IN LESS THAN 15 MINS, M5057 PWR SUPPLY BATTERY NEED REPLACEMENT.(<P>EMERGENCY BATTERY PWR SUPPLY ASSY M5057 REPLACED AND INSTALLATION TEST CARRIED OUT RESULT NORMAL IAW AMM 33-51-04 REV 104, 15MAR2022.</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

L/H BS 900 MOST INNER ROW OF FASTENER HOLES AT TENSION TIE TO FRAME ATTACHMENT UPPER HOLE CRACK WAS FOUND ON FWD CHANNEL RUNNING UP AND DOWN APPROX 0.030 AND 0.040".(<P>STA 900 LH TENSION TIE FORWARD CHANNEL AND FORWARD DOUBLER FASTENER HOLES CRACK AREA REPAIRED IAW RI-53-00-15553 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

LH BS 880 MOST INNER ROW OF FASTENER HOLES AT TENSION TIE TO FRAME ATTACHMENT LOWER HOLE CRACK WAS FOUND ON FWD CHANNEL RUNNING UP THRU THICKNESS.(<P>STA 880 L/H TENSION TIE FWD CHANNEL 1EA FASTENER HOLE CRACK AREA REPAIRED IAW RI-53-00-15553 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

EMP - VERTICAL FIN L/H L/E FIXED PNL AT FS 245 AND FS 270 FAIRING 321D AREA RIVET FOUND LOOSE.(<P>EMP - VERTICAL FIN L/H L/E FIXED PNL AT FS 245 AND FS 270 AREAS LOOSE RIVET REPLACED IAW RI-55-00-15535 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

R/H BS 900 MOST INNER ROW OF FASTENER HOLES AT TENSION TIE TO FRAME ATTACHMENT UPPER HOLE CRACK WAS FOUND ON FWD CHANNEL RUNNING UP AND DOWN THRU THICKNESS(<P>STA 900 RH TENSION TIE FORWARD CHANNEL AND FORWARD DOUBLER FASTENER HOLES CRACK AREA REPAIRED IAW RI-53-00-15553 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

#4 PYLON VALVE ACCESS PNL #482EL FOUND 2EA SCREW HOLE ELONGATED.(<P>#4 PYLON VALVE ACCESS PNL #482EL 2EA SCREW HOLE ELONGATED AREAS REPAIRED IAW RI-54-50-15536 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

M/D STA 940 TENSION TIE L/H AFT CHANNEL FOUND CRACK(<P>UPPER DECK STA 940 LH TENSION TIE AFT CHANNEL CRACK AREA REPAIRED IAW RI-53-00-15548 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

FX - KEEL BEAM PANEL SUPPORT CORROSION CRACK FOUND AT STA 1000 LBL 10" TO RBL 10"(<P>FX - STA 1000 LBL 127" TO RBL 127" KEEL BEAM PANEL ATT SUPPORT CHORD P/N : 69B10098-148 REPLACED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-40-02.</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

RH BS 880 MOST INNER ROW OF FASTENER HOLES AT TENSION TIE TO FRAME ATTACHMENT LOWER HOLE CRACK WAS FOUND ON FWD CHANNEL RUNNING UP AND DOWN THRU THICKNESS.(<P>STA 880 R/H TENSION TIE FWD CHANNEL 1EA FASTENER HOLE CRACK AREA REPAIRED IAW RI-53-00-15553 REV A.</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

U/D EXIT SIGN CTR AND U/D EMER LT AISLE CTR #3 COUNT FROM FWD FOUND WENT OFF IN LESS THAN 15 MINS, M5056 PWR SUPPLY BATTERY NEED REPLACEMENT.(<P>M5056 PWR SUPPLY REPLACED AND INSTALLATION TEST RESULT 'NORMAL' IAW AMM 33-51-04 REV.104, 15MAR2022.</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

M/D STA 960 TENSION TIE L/H AFT CHANNEL FOUND CRACK(<P>UPPER DECK STA 960 L/H TENSION TIE AFT CHANNEL CRACK AREA REPAIRED IAW RI-53-00-15548 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

L/H O/B MID FLAP T/E (FROM I/B 10TH AND 11ST) SCREW HOLE FOUND ELONGATED(<P>&NBSP;PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5K REV.114 ,FEB 20/2022</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

RHW ILES 1116 L/E NOSE BEAM UPPER CHORD FOUND CRACK(<P>RHW FIXED L/E NOSE BEAM ILES 1057 - ILES 1116 UPPER CHORD CRACK AREA REPAIRED IAW RI-57-41-15517 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

STA 2742 STR 46L TO STR 46R FOUND EXISTING REPAIR.(<P>FX - STA 2742 TO STA 2757, STR 46L TO STR 46R, SKIN DOUBLER FOUND EXISITING REPAIRED IAW EGAT E.I NO : E2008A53M-972 REV 02.</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

RHW O/B FORE FLAP L/E 56-58" FROM O/B FOUND DELAMINATED(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A REV.114 ,FEB 20/2022</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

#2 NACELLE STRUT THRUST TANG - COVER PLATE CANNOT BE INSTALLED, DUE TO NO ACCESS ON THE UNDERNEATH AREA(<P>#2 NACELLE STRUT THRUST TANG - COVER PLATE FASTENER SUBSTITUTION IAW RI-54-00-15545 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

LHW O/B MID FLAP L/E 100" - 110"" FROM I/B FOUND DELAMINATED(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A REV.114 ,FEB 20/2022</P>)

Part: SHIELD — NONE · corrosion level 3 · airframe 111,020 hrs · 19,942 cycles

U/D - RH CREW DOOR FWD DRAIN SHIELD LOWER SUPPORT FOUND CORROSION(<P>U/D - STA 666 RBL 95" WL 310, RH CREW DOOR FWD DRAIN SHIELD LOWER CORROSION SUPPORT P/N : 65B25769-12 REPLACED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-40-02.</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

NO.1 ENG R/H CORE COWL EXHAUST DUCT INLET EDGE AREA FOUND CHAFING ( P/N 224-2302-545 )(<P>NO.1 ENG R/H CORE COWL ( P/N : 224-2302-545 S/N : 325001 ) EXHAUST DUCT INLET EDGE CHAFING AREA WELD REPAIRED AND DOUBLER ( P/N : 224M4762-3 )&NBSP; REPLACED IAW EO 1971A278-1.</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

L/H BS 880 MOST INNER ROW OF FASTENER HOLES AT TENSION TIE TO FRAME ATTACHMENT UPPER HOLE CRACK WAS FOUND ON FWD CHANNEL RUNNING UP THRU THICKNESS(<P>STA 880 LH TENSION TIE FORWARD CHANNEL AND FORWARD DOUBLER FASTENER HOLES CRACK AREA REPAIRED IAW RI-53-00-15553 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

RHW O/B FORE FLAP FOUND DELAMINATED(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A REV.114 ,FEB 20/2022</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

#3 NACELLE STRUT THRUST TANG - COVER PLATE CANNOT BE INSTALLED, DUE TO NO ACCESS ON THE UNDERNEATH AREA(<P>#3 NACELLE STRUT THRUST TANG - COVER PLATE FASTENER SUBSTITUTION IAW RI-54-00-15545 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

RHW ILES 1116 L/E NOSE BEAM LOWER CHORD FOUND CRACK(<P>RHW FIXED L/E NOSE BEAM ILES 1057 - ILES 1116 LOWER CHORD CRACK AREA REPAIRED IAW RI-57-41-15517 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

LH WING #1E L/E FLAP O/B LOWER FIXED PANEL FOUND BULGE UP.(<P>LHW L/E NOSE SKIN INSTL SKIN SPLICE STRAP AT OLES 1617.6 TO 1639.0 CORROSION AREA REPAIRED IAW RI-57-41-15493 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

LHW O/B FORE FLAP L/E 64" FROM I/B FOUND DELAMINATED(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A REV.114 ,FEB 20/2022</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

RHW O/B FORE FLAP T/E 70" - 72" FROM O/B FOUND DELAMINATED(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A REV.114 ,FEB 20/2022</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

RHW O/B FORE FLAP T/E 190" FROM O/B FOUND DELAMINATED(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A REV.114 ,FEB 20/2022</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

M/D STA 1060 TENSION TIE L/H AFT L/H AFT CHANNEL FOUND CRACK(<P>UPPER DECK STA 1060 L/H TENSION TIE AFT CHANNEL CRACK AREA REPAIRED IAW RI-53-00-15548 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

STA 1480 RH WEB SPLICE AREA 1 EA CRACK FOUND AT WEB PANEL #14 HOLE RUNNING 7 O'CLOCK APPROX 0.050IN.(<P>STA 1480 RH B/H WEB SPLICE AREA, #14 HOLE WEB PANEL CRACK AREA OVERSIZE ( 0.4057" ) REPAIRED AND BUSHING REPAIRED ( 0.502" ) IAW SB 747-53A2390 REV 1 AND FIG 11.</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

RH BS 1480 LONGERON WEB SPLICE AREA CRACK WAS FOUND AT FASTENER HOLE #21 AT WEB PANEL(<P>RH BS 1480 LONGERON WEB SPLICE AREA FASTENER HOLE #21 CRACKED HOLE REPAIRED AS PER SB 747-53A2390 REV 1, #21 FASTENER HOLE OVERSIZE ( 0.500" ) REPAIRED IAW SB 747-53A2390 REV 1 P.35.</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

#1 NACELLE STRUT THRUST TANG - COVER PLATE CANNOT BE INSTALLED, DUE TO NO ACCESS ON THE UNDERNEATH AREA(<P>#1 NACELLE STRUT THRUST TANG - COVER PLATE FASTENER SUBSTITUTION IAW RI-54-00-15545 REV A</P>)

Part: NONE — NONE · corrosion level 3 · airframe 111,020 hrs · 19,942 cycles

RHW ILES 380 L/E LOWER FIXED PANEL SUPPORT BEAM FOUND CORROSION.(<P>RHW ILES 380 I/B L/E LOWER SURFACE PANEL INSTL SUPPORT BEAM CORROSION AREA REPAIRED IAW RI-57-41-15494 REV A.</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

LH BS 900 MOST INNER ROW OF FASTENER HOLES AT TENSION TIE TO FRAME ATTACHEMENT LOWER HOLE CRACK WAS FOUND ON ALUMINUM DOUBLER.(<P>STA 900 LH TENSION TIE FWD CHANNEL ATT ALUMINUM DOUBLER 1EA FASTENER HOLE CRACK AREA REPAIRED IAW RI-53-00-15553 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

LHW O/B FORE FLAP L/E 20" - 24"" FROM I/B FOUND DELAMINATED(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A REV.114 ,FEB 20/2022</P>)

Part: BUSHING — NONE · airframe 111,020 hrs · 19,942 cycles

M/D STA 1000 RBL 11.33 FLOOR SUPPORT I/B CROSS BOLT HOLE FOUND ENLARGED(<P>M/D STA 1000 RBL 11.33" LUG FTG P/N : 366-53-15-A1364-102 REPLACED IAW SRM 51-10-02 AND P/N : 366-53-15-A1364-104 ATT BUSHING REPLACED IAW SOPM 20-50-03.</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

AFT CARGO STA 1840 - 1850 RBL 85" CEILING PNL SUPPORT FOUND DEFORM.(<P>AFT CARGO COMPT STA 1850 - STA 1851 RBL 85" CEILING SUPPORT CHANNEL P/N : 453U1566-80 DEFORM AREAS REPAIRED IAW RI-25-53-15546 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

M/D STA 1080 TENSION TIE R/H AFT CHANNEL FOUND CRACK(<P>UPPER DECK STA 1080 R/H TENSION TIE AFT CHANNEL CRACK AREA REPAIRED IAW RI-53-00-15548 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

LH BS 1480 LONGERON WEB SPLICE AREA CRACK WAS FOUND AT FASTENER HOLE #16 AT WEB PANEL.(<P>LH BS 1480 LONGERON WEB SPLICE AREA FASTENER HOLE #16 CRACKED HOLE REPAIRED AS PER SB 747-53A-2390 REV 1. #16 FASTENER HOLE OVERSIZE ( 0.4682 ) REPAIRED IAW SB 747-53A2390 REV 1 P.54.</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

RHW I/B MID FLAP L/E FOUND DELAMINATED(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A REV.114 ,FEB 20/2022</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

R/H BS 880 MOST INNER ROW OF FASTENER HOLES AT TENSION TIE TO FRAME ATTACHMENT UPPER HOLE CRACK WAS FOUND ON FWD CHANNEL RUNNING UP AND DOWN THRU THICKNESS(<P>STA 880 RH TENSION TIE FORWARD CHANNEL AND FORWARD DOUBLER FASTENER HOLES CRACK AREA REPAIRED IAW RI-53-00-15553 REV A&NBSP;</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

#3 PYLON VALVE ACCESS PNL #472ER FOUND 1EA SCREW HOLE ELONGATED(<P>#3 PYLON VAVLE ACCESS PNL #472ER 1EA SCREW HOLE ELONGATED AREAS REPAIRED IAW RI-54-50-15536 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

NO.1 PYLON RH NO.1 CORN COWL HINGE FITTING FWD LUG FWD SURFACE FOUND CHAFING(<P>SPOTFACE LUG FACE REQUIRED TO PROVIDE FLAT SURFACE AND FABRICATE CUSTOM WAHSER AS PER RI-54-50-15543 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

RHW O/B FORE FLAP L/E 15" FROM O/B FOUND DELAMINATED(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A REV.114 ,FEB 20/2022</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

STA 2598 HINGE SUPPORT FRAME MOD AND STA 2598 LH LOWER LEFT CORNER MOD DOUBLER FASTENER S.E.M REPAIR.(<P>STA 2598 HINGE SUPPORT FRAME MOD AND STA 2598 LH LOWER LEFT CORNER MOD DOUBLER 1EA FASTENER S.E.M REPAIRED IAW RI-53-00-15537 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

M/D STA 1000 TENSION TIE R/H FWD CHANNEL FOUND CRACK(<P>UPPER DECK STA 1000 R/H TENSION TIE FWD CHANNEL CRACK AREA REPAIRED IAW RI-53-00-15548 REV A</P>)

Part: NONE — NONE · airframe 111,020 hrs · 19,942 cycles

STA 1480 RH WEB SPLICE AREA 1EA CRACK FOUND AT WEB SPLICE PLATE #15 HOLE RUNNING 2 O'CLOCK APPROX 0.050IN.(<P>STA 1480 R/H B/H WEB SPLICE AREA, #15 HOLE WEB SPLICE PLATE CRACK AREA OVERSIZE ( 0.4057" ) REPAIRED AND BUSHING REPAIRED ( 0.502" ) IAW SB 747-53A2390 REV 1 AND FIG 11.</P>)

Part: SEAT TRACK — CORRODED · airframe 111,020 hrs · 19,942 cycles

M/D STA 1820 RBL 77 SEAT TRACK CROWN FOUND CORROSION(<P>M/D STA 1820 RBL 77 SEAT TRACK CROWN CORROSION REMOVED IAW IAI SRM 51-10-02 AND REPORTECTED IAW IAI SRM 51-20-01, CHECKED WITHIN IAI SRM 53-00-52 ADL 1, FIG 101</P>)

Part: SEAT TRACK — CORRODED (BS 1900) · airframe 111,020 hrs · 19,942 cycles

M/D STA 1900 RBL 77 SEAT TRACK CROWN FOUND CORROSION.(<P>M/D STA 1900 RBL 77 SEAT TRACK CROWN CORROSION REMOVED IAW IAI SRM 51-10-02 AND REPROTECTED IAW IAI SRM 51-20-01, CHECKED WITHIN IAI SRM 53-00-52 ADL 1, FIG 101.</P>)

Part: SEAT TRACK — CORRODED · airframe 111,020 hrs · 19,942 cycles

M/D STA 1800 RBL 77 SEAT TRACK CROWN FOUND CORROSION(<P>M/D STA 1800 RBL 77 SEAT TRACK CROWN CORROSION REMOVED IAW IAI SRM 51-10-02 AND REPORTECTED IAW IAI SRM 51-20-01, CHECKED WITHIN IAI SRM 53-00-52 ADL 1, FIG 101</P>)

Part: SEAT TRACK — CORRODED · airframe 111,020 hrs · 19,942 cycles

M/D STA 1840 RBL 77 SEAT TRACK CROWN FOUND CORROSION.(<P>M/D STA 1840 RBL 77 SEAT TRACK CROWN CORROSION REMOVED IAW IAI SRM 51-10-02 AND REPORTECTED IAW IAI SRM 51-20-01, CHECKED WITHIN IAI SRM 53-00-52 ADL 1, FIG 101</P>)

Part: SHEAR WEB — CRACKED · airframe 111,020 hrs · 19,942 cycles

M/D STA 140 LH STR 26 FLOOR WEB FOUND CRACK APPROX 1.3"(<P>M/D STA 140 - STA 160 L/H FLOOR TO SKIN SHEAR WEB CRACK AREA REPAIRED IAW SRM 53-10-51-2R-7 REPAIR 7 REV 114 20 FEB 2022</P>)

Part: NONE — NONE · airframe 110,399 hrs

DISCREPANCY 1. LH HF FAILED IN FLIGHT. DISCREPANCY 2. SATCOM MESSAGE AFTER TAKE OFF. UNABLE TO CROSS PACIFIC OCEAN WITH BOTH INOP.(<P ><SPAN>DISCREPANCY 1. REMOVED AND REPLACD LH HF TRANSCEIVER IAW AMM 23-11-05.&NBSP; DISCREPANCY 2.&NBSP; REMOVED AND REPLACED "THUMB LOCK" ON BEAM STEERING UNIT TRAY IAW AMM 20-11-22.</SPAN></P> / <P>&NBSP;</P>)

Part: TRANSCEIVER — FAULTED (RT HF SYSTEM)

AIR TURNBACK DUE TO INABILITY TO ESTABLISH HF CONTACT.(<P>&NBSP;REMOVED AND REPLACED R/H HF TRANSCEIVER. OPS CK GOOD IAW AMM 23-11-05.</P>)

Part: LINE — LEAKING (HYD SYSTEM) · airframe 109,067 hrs · 19,619 cycles

HYDRAULIC PRESSURE SYSTEM #1 EICAS QUANTITY LOW. REPLACED ELEVATOR ACTUATOR LINE WITH TEMP LINE. TO BE REPLACED ON NEXT A- CHECK. CHECKED CASE DRAIN FILTERS (CLEAN) AND INSTALLED NEW FILTERS.

Part: TRANSCEIVER — FAILED (HF COMMS)

AIR DIVERSION TO ICN - BOTH LH AND RH HF RADIOS FAILED IN CRUISE(<P ><SPAN>REPLACED LH HF TRANSCEIVER. BOTH LH AND RH HF RADIOS OPS CHECK GOOD IAW AMM 23-11-00/501.</SPAN></P> / <P>&NBSP;</P>)

Part: RECEPTACLE — DAMAGED (NR 1 EXTER POWER) · airframe 106,880 hrs · 19,194 cycles

NR 1 EXTERNAL POWER RECEPTACLE DAMAGED. REPAIRED PER EO 4453B956/PART 1. FABRICATED AND INSTALLED INTERNAL REPAIR WASHERS. PERMANENT, CATEGORY B/REPAIR AWAITING DTE.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 106,066 hrs · 18,959 cycles

FOUND EMERGENCY LIGHT BATTERY FUNCTION FAIL, IAW AMM 33-51-04-902-001-001 REV 98. REPLACE EMERGENCY LIGHT BATTERY (M5055) AND CONDITION CHECK NORMAL, IAW SMM 33-51-04-902-001-001 REV 98. PERFORM TEST OF NEW BATTERY, THE RESULT WAS SATISFACTORY.

Part: SPAR — CRACKED (RT WING TE FLAP) · airframe 106,066 hrs · 18,959 cycles

CRACK ON RT WING OUTBOARD MID FLAP REAR SPAR WEB OUTBOARD OF WBL 743.828. REPAIR CRACK AREA, IAW EI NO T2020A57M-2607 REV 1. CONDITION CHECK NORMAL AND JOB COMPLETED.

Part: RIB — CORRODED (LT WING LE) · corrosion level 2 · airframe 106,066 hrs · 18,959 cycles

CORROSION: CHORD, LOWER FACE OF LT WING OUTBOARD LEADING EDGE CAVITY RIB LOWER T CHORD, OLES 1221.05. REMOVED DAMAGED PART, IAW SRM 51-40-02 REV 109. FABRICATE NEW CLIP, IAW EI NO T2020A57M-2613. INSTALL FAB NEW CLIP, IAW BOEING DWG NR 65B07829 SH 3 REV C AND SRM 51-40-02-0G-0 REV 109. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: GUSSET — CORRODED (RT MLG WW) · corrosion level 2 · airframe 106,066 hrs · 18,959 cycles

CORROSION: GUSSET OF RT WING LANDING GEAR WHEEL WELL FWD UNDERWING VAPOR BARRIER AT STA 1240.5, RBL 17.75. REMOVE DAMAGE PART, IAW SRM 51-40-02 REV 109. FAB PART, IAW EI NO T2020A57M-2571 REV 0. INSTALL NEW FAB PART, IAW SRM 51-40-02 REV 109 AND DWG NR 65B10534 SHEET 13 REV D. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: SKIN — DEBONDED (RT WING TE FLAP) · airframe 106,066 hrs · 18,959 cycles

DISBOND, FOUND RT INBOARD MID FLAP UPPER SKIN DISBOND. REPAIR THE RT INBOARD MID FLAP UPPER SKIN, IAW EGAT EI NO T2020A57M-2618 REV 1. CONDITION CHECK IS SATISFACTORY.

Part: SPAR — CRACKED (LT WING TE FLAP) · airframe 106,066 hrs · 18,959 cycles

CRACK ON LT WING OUTBOARD MID FLAP REAR SPAR WEB, OUTBOARD OF WBL 743.828. REPAIRED THE CRACK, IAW EI NO T2020A57M-2605 REV 1. CONDITION CHECK NORMAL AND JOB COMPLETED.

Part: FRAME — CRACKED (BS 134.75) · airframe 106,066 hrs · 18,959 cycles

CRACK: DAMAGE ON RING FRAME UPPER LT SIDE AT STA 134.75 LBL 5, WL 270. ACCOMPLISHED EI NO T2020A53M-2632 REV 1 AND SRM 53-10-08 REPAIR 3 REV 109. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: ACTUATOR — FAILED (NLG) · airframe 105,315 hrs · 18,813 cycles

NR 1 HYDRAULIC SYSTEM LOSS OF FLUID, GEAR DOORS EICAS AFTER TAKEOFF AND GEAR RETRACTION, DURING GEAR RECYCLE, HYD PRESS SYS 1 FOLLOWED BY HYD QTY 1 EICAS. QRH PROCEDURES COMPLIED WITH. REMOVED BROKEN NOSE L/G DOOR ACTUATOR AND INSTALLED NEW NOSE L/G DOOR ACTUATOR & SERVICED HYD FLUID AT NR 1 HYD RESERVOIR. REMOVED AND REPLACED THE NR 1 CASE DRAIN FILTER AND THEN NOSE L/G DOOR ACTUATOR CHECKED, NR 1 HYD QTY CHECKED OK, ERASED FAULT MESSAGE IAW AMM 12-12-01 & 29-21-02. 32-34-14/401. ALSO PERFORMED NOSE GEAR RETRACTION & EXTENSION, OPS WAS NORMAL.

Part: FAIRING — DAMAGED (LT WING K FLAP) · airframe 104,274 hrs · 18,561 cycles

LEFT WING NR 13 KRUEGER FLAP BULLNOSE FAIRING I/B LOWER CORNER DAMAGED. REPAIRED DAMAGED AREA ON I/B LWR CORNER SKIN OF THE KRUEGER FLAP BULLNOSE FAIRING IAW RI-57-44-13644 REV. A.

Part: ACCESS PANEL — DAMAGED (NR 2 NACELLE) · airframe 104,274 hrs · 18,561 cycles

NO.2 PYLON, ACCESS PNL 462FR, FWD LOWER MOUNT SCREW ATT ANCHOR NUT SEAL PLATE MISSING. FABRICATED AND REPLACED ACCESS PANEL 462FR DEPRESSOR SEAL, PN: 311U2542-115 ASSY IAW EO 4454A269 PART 1.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 104,274 hrs · 18,561 cycles

LEFT HORIZONTAL STABILIZER, UPPER SKIN AND UPPER REAR SPAR CHORD ZONE 'B' AREA #8 HOLE FASTENER, HOLE FOUND CRACKED. HORIZONTAL STABILIZER LH SEAL PAN #8 FASTENER CRACK AREA REPAIRED IAW RI-55-10-13670 REV. A.&NBSP;</P>)

Part: SUPPORT — CRACKED (BS 284) · airframe 104,274 hrs · 18,561 cycles

COCKPIT, PILOT L/H FOOT PEDAL AREA, I/B PANEL SUPPORT WEB CRACKED.(<P>REPAIRED PANEL SUPPORT WEB CRACK AREAS IAW RI-53-00-13638 REV. A.&NBSP;</P>)

Part: CARGO TRACK — CORRODED (BS 1880) · airframe 104,274 hrs · 18,561 cycles

FOUND CORROSION ON MAIN DECK CARGO SEAT TRACK STA 1880, LBL 75.92.(<P>MAIN DECK STA 1880, LBL 75.92, CORROSION REMOVED AND RE-PROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN ALLOWABLE DAMAGE LIMIT IAW SRM 53-00-52-1A-1, 1 FIG 101.&NBSP;</P>)

Part: STRUT — CORRODED (LT MLG) · airframe 104,274 hrs · 18,561 cycles

L/H WLG SHOCK STRUT CYLINDER LOWER INNER SURFACE RUSTY.(<P>REPAIRED CORROSION ON INNER SURFACE AREA OF L/H WLG OUTER CYLINDER IAW RI-32-00-13681 REV.A</P>)

Part: FAIRING — DAMAGED (RT WING) · airframe 104,274 hrs · 18,561 cycles

RIGHT WING NR 7 CANOE FAIRING 665EB SCREW HOLE FOUND ELONGATED. FABRICATED A NEW CANOE FAIRING 665EB PANEL IAW EO 4457A693 PART 1.

Part: RETAINER — CRACKED (LT MLG WW) · airframe 104,274 hrs · 18,561 cycles

L/H WLG W/W FWD BULKHEAD, LBL 40, LWR SEAL RETAINER FOUND CRACKED.(<P>L/H WLG W/W FWD BULKHEAD STA 1233, LBL 40, UNDERWING REAR SPAR VAPOR BARRIER SEAL RETAINER CRACK AREAS REPAIRED IAW ATLAS EO 4453B722, PART 1.&NBSP;</P>)

Part: CARGO TRACK — CORRODED (BS 1800) · airframe 104,274 hrs · 18,561 cycles

FOUND CORROSION ON MAIN DECK CARGO SEAT TRACK, STA 1800, LBL 75.92.(<P>MAIN DECK STA 1800, LBL 75.92, SEAT TRACK CORROSION REMOVED AND RE-PROTECTED IAW SRM 51-10-02 AND SRM 51-20-02. CHECKED WITHIN ALLOWABLE DAMAGE LIMIT IAW SRM 53-00-52-1A-1, 1 FIG 101.</P>)

Part: CARGO TRACK — CORRODED (BS 1920) · airframe 104,274 hrs · 18,561 cycles

FOUND CORROSION ON MAIN DECK CARGO, SEAT TRACK STA 1920, LBL 75.92.(<P>MAIN DECK STA 1920, LBL 75.92, SEAT TRACK CORROSION REMOVED AND RE-PROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN ALLOWABLE DAMAGE LIMIT IAW SRM 53-00-52-1A-1, 1 FIG 101.

Part: CARGO TRACK — CORRODED (BS 1840) · airframe 104,274 hrs · 18,561 cycles

FOUND CORROSION ON MAIN DECK CARGO SEAT TRACK, STA 1840, LBL 75.92.(<P>MAIN DECK STA 1840, LBL 75.92, SEAT TRACK CORROSION REMOVED AND RE-PROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN ALLOWABLE DAMAGE LIMIT IAW SRM 53-00-52-1A-1, 1 FIG 101.</P>)

Part: ANGLE — CRACKED · airframe 104,274 hrs · 18,561 cycles

LHW REFUELING PNL STIFFENER ZEE ANGLE FOUND CRACKED.(<P>CRACKED AREA REPAIRED AS PER EO 4457A692.&NBSP;</P>)

Part: WEB — CRACKED (BS 284) · airframe 104,274 hrs · 18,561 cycles

COCKPIT - PILOT R/H FOOT PEDAL AREA I/B PANEL SUPPORT WEB CRACKED. REPAIRED PANEL SUPPORT WEB CRACK AREAS IAW RI-53-00-13638 REV. A.

Part: SEAT TRACK — CORRODED (BS 1860) · airframe 104,274 hrs · 18,561 cycles

FOUND CORROSION ON MAIN DECK SEAT TRACK, STA 1860, LBL 75.92.(<P>MAIN DECK STA 1860, LBL 75.92, SEAT TRACK CORROSION REMOVED AND RE-PROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN ALLOWABLE DAMAGE LIMIT IAW SRM 53-00-52-1A-1, 1 FIG 101.

Part: SEAL — TORN (RT MLG WW) · airframe 104,274 hrs · 18,561 cycles

R/H WLG W/W AFT I/B CUTOUT AREA FOUND 1 EA SEAL TORN.&NBSP;(<P>REMOVED AND REPLACED&NBSP;RH WLG W/W AFT I/B CUTOUT AREA SEAL IAW AMM 20-51-00 AND RI-53-43-13658 REV. A.&NBSP;</P>)

Part: BULKHEAD — CRACKED · airframe 104,274 hrs · 18,561 cycles

RHS BS 2598, AFT INNER CHORD, FOUND CRACK APPROX 1.5".(<P>STA 2598 RH BULKHEAD UPPER AFT INNER, P/N: 65B02505-50 REPLACED IAW SRM 51-10-02 AND RI-53-83-13669 REV. A.&NBSP;</P>)

Part: TORQUE BOX — CORRODED (NR 1 PYLON) · corrosion level 2 · airframe 104,274 hrs · 18,561 cycles

NR 1 PYLON UPPER CAVITY TORQUE BOX SKIN CORRODED, FOUND BETWEEN NAC STA 204.5 AND 249.5. REPAIRED IAW RI-54-00-13660 REV. A.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 101,699 hrs · 18,083 cycles

MAIN DECK SMOKE ON FINAL APPROACH CAUSING "FIRE MAIN DECK". SMOKE DETECTION TEST PASS. NR 1 PACK WATER COALESCER REPLACED. NR 2 WATER COALESCER BAG REPLACED. FOUND MSG 21773, PACK 1 TRIP. DEFERRED PACK 1.

Part: FLAP SYSTEM — LACK OF LUBE · airframe 99,270 hrs · 17,623 cycles

FLAPS PRIMARY CAUTION MESSAGE DURING APPROACH BETWEEN FLAP DEGREES 5 THROUGH 10. INSPECTED PRIMARY FLAPS, GREASED AND LUBED PRIMARY FLAPS. OPS CHECKED GOOD IAW AMM 12-21-20-633-021, 12-21-20-643-040, AND 27-58-01.

Part: FLAP — CORRODED (LT WING) · corrosion level 2 · airframe 97,847 hrs · 17,365 cycles

LT WING I/B MID-FLAP UPPER CENTER SECTION HAS 3EA AREAS OF CORROSION. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 57-53-01-02-01 DETAIL II AND SRM 51-70-10-2R-2 REPAIR 2.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 97,847 hrs · 17,365 cycles

LIGHT BATTERY PACKS FAIL CAPACITY TEST. REMOVED EMERGENCY LIGHT BATTERY PACKS (4EA) IN UPPER DECK AS PER AMM 33-51-04. INSTALLED NEW EMERGENCY LIGHT BATTERY PACKS (2EA) IN UPPER DECK AS PER AMM 33-51-04. OP CK GOOD PER AMM 33-51-04.

Part: PANEL — DELAMINATED (TE FLAP) · airframe 97,847 hrs · 17,365 cycles

LT I/B MID FLAP UPPER ECENTER SECTION PANEL HAS DELAMINATION. REPLACED LT I/B MID FLAP UPPER CENTER SECTION PANEL IAW EA 747-5753-28-A6917 AND EO1957A317.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 97,847 hrs · 17,365 cycles

UPPER DECK LIGHT FOR EMERGENCY DOOR ASSIST BOTTLE REQUIRES SERVICING. REMOVED AND REPLACED UPPER DECK LT EMERGENCY DOOR ASSIST BOTTLE IAW AMM 52-23-13-004-001.

Part: GASKET — CHAFED (LT WING) · airframe 97,847 hrs · 17,365 cycles

GASKET IS CHAFED AND CRACKED ON THE LT WING TRAILING EDGE, JUST INBOARD OF OUTBOARD FLAP INBOARD STOP FITTING. REMOVED GASKET AND FABRICATED AND INSTALLED GASKET AT WS 1084 IAW SRM 51-40-05-0, AND DWG 65B08153, REV W.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 97,847 hrs · 17,365 cycles

FLIGHT DECK EMERGENCY FLASHLIGHT RED LIGHT NOT BLINKING. REMOVED AND REPLACED THE FLASHLIGHT BATTERY PACK IAW AMM 25-60-00-216-005.

Part: FLAP — CHAFED (RT WING) · airframe 97,847 hrs · 17,365 cycles

RT OUTBD AFT FLAP T/E HAS CHAFING. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 51-70-01-2R, 51-70-10-2R AND SRM 51-70-10-2R REPAIR 2 FIG 201.

Part: SHEAR WEB — CRACKED (RT WING) · airframe 97,847 hrs · 17,365 cycles

RIGHT WING FIXED T/E SUPPORT RIB SHEAR WEB IS CRACKED JUST OUTBOARD OF THE NR 8 SPOILER AT WBL 432.65. REPAIRED THE RT WING T/E SUPPORT RIB SHEAR WEB IAW EO4457A169, AND SRM 51-70-13</P>)

Part: SKIN — SEPARATED (RT WING AILERON) · airframe 97,842 hrs · 17,365 cycles

RIGHT WING INBOARD AILERON OTBD T/E CORNER IS SEPARATED. REPAIRED THE RT AILERON OTBD T/E CORNER IAW SRM 51-20-07-0G, FIG 14.

Part: HOSE — DETERIORATED (OXYGEN MASK) · airframe 97,847 hrs · 17,365 cycles

UPPER DECK PORTABLE OXYGEN BOTTLE SUPPLY HOSE IS DETERIORATED. REMOVED AND REPLACED OXYGEN BOTTLE SUPPLY MASK IAW AMM 35-31-00-900-801.

Part: FRAME — GOUGED (NR 2 COWLING) · airframe 97,847 hrs · 17,365 cycles

NR 2 ENGINE OUTBD CORE COWL FRAME GOUGED. FABRICATED AND INSTALLED REPAIR DOUBLER AND REPAIR ANGLE PER SRM 56-41-02-2R-2 FIG 201.

Part: CIRCUIT CARD — DEFECTIVE (SMOKE DETECTION) · airframe 97,847 hrs · 17,365 cycles

CARGO SMOKE DETECTION FAILS OPERATIONAL TEST AND GROUND TEST PER AMM 26-14-00. REMOVED AND REPLACED 4EA CIRCUIT CARDS 1/L PA001, 1/L PA002, 1/LPA004 + 1/L PA005 RECONFIGURED AIRCRAFT TO KIDDE SYSTEM PER AMM 26-11-00. OPS CHECK GOOD.

Part: FLAP — CORRODED (LT WING) · airframe 97,847 hrs · 17,365 cycles

LT WING I/B MID-FLAP UPPER CENTER SECTION HAS 3EA AREAS OF CORROSION. REPARED PER SRM 57-53-01-01-1 AND EO1957A317.

Part: SLIDE — LOW PRESSURE · airframe 97,847 hrs · 17,365 cycles

FLOOR EVACUATION SLIDE GAS RESERVOIR GAUGE POINTER IS BELOW GREEN BAND AT UPPER DECK FWD RT. REMOVED AND REPLACED FLOOR MOUNTED ESCAPE SLIDE IAW AMM 25-68-01-404-005.

Part: EXTINGUISHER — NO TEST (COCKPIT) · airframe 97,159 hrs · 17,235 cycles

COCKPIT FIRE EXTINGUISHER FAIL WEIGHT CHECK. REMOVED AND REPLACED COCKPIT FIRE EXTINGUISHER IAW AMM 26-26-01.

Part: EXTINGUISHER — NO TEST (UPPER DECK) · airframe 97,159 hrs · 17,235 cycles

UPPER DECK FIRE EXTINGUISHER FAIL WEIGHT CHECK. REMOVED AND REPLACED THE FIRE EXTINGUISHER IAW AMM 26-26-01.

Part: LIGHT — INOPERATIVE (LT DOOR) · airframe 94,816 hrs · 16,789 cycles

UPPER DECK BATTERY OK, LIGHT ON LT DOOR INOPERATIVE, RELAMPED NO HELP. ACFT RELEASED IAW MEL 52-30-07, CAT-C MEL RAISED MDDR 69851. M-PROCEDURES COMPLIED WITH, PLACARD INSTALLED.

Part: TIRE — BLOWN (MLG) · airframe 94,528 hrs · 16,727 cycles

ON WALK AROUND, FOUND NR 12 TIRE BLOWN. REPLACED 12 AND 13 TIRE, REF LP 788690. ALSO ACCOMPLISHED CHAPTER 5 INSPECTION IAW 05-51-025 IAW LP 788691/2, DEACTIVATED NR 12 BRAKE AND NR 12 ANTI-SKID.

Part: SKIN — DAMAGED (TE FLAP) · airframe 94,458 hrs · 16,712 cycles

LEFT OTBD FORE FLAP HAS DAMAGE ON LE LOCATED ON OTBD END 10 - 14 INCHES INBD. REMOVED DAMAGED AREA & REPAIRED SAME IAW SRM 51-70-07 PARA 4 C. PREPARED & APPLIED BMS 8-79 & BMR 5-101 REPAIR PLIES IAW SRM 51-70-7 PARA 4 E. LAYERED UP & VACUUMED BAGGED REPAIR IAW SRM 51-70-07 PARA 4 E. CURED REPAIR WITH HOT BONDER 16123181 CAL DUE 23 JULY 2016 IAW SRM PARA 4 G.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 94,261 hrs · 16,675 cycles

AIR TURN BACK. AFTER TAKEOFF, MASTER WARNING FIRE CARGO AFT. QRH PROCEDURES COMPLETED. ACFT RETURNED & MAIN DECK CARGO COMPARTMENT PHYSICALLY CHECKED. NO EVIDENCE OF SMOKE OR FIRE. SUSPECT FAULT OCCURRED DUE TO MOISTURE. STATUS MSG, MD CARGO 15,11,10 LP A, MD CGO 4,9,16 LP B. FOUR SMOKE DETECTORS REPLACED & TESTED OK.

Part: UNKNOWN — SMOKE (LT MLG) · airframe 93,390 hrs · 16,504 cycles

HEAVY SMOKE REPORTED BY OTHER ACFT, EMITTED FROM LT MAIN GEAR;. INSPECTED BRAKE LINES AT MAIN GEARS 1 - 4 & HYD SYSTEMS ON GEARS. FOUND NO LEAKS, NO RUBBED TIRES OR ABRASED TIRES FROM DRAGGING, NO HOT TIRES, NO HOT BRAKES. NO INDICATIONS OF HOT BRAKES OR ANY OTHER INDICATIONS OF A PROBLEM INDICATED IN COCKPIT. ALSO FIRE DEPT READ NO HOT BRAKES OR TIRES ON ACFT. ACFT RELEASED FOR FLIGHT. INSPECTED IAW MM 32-41-15 & MM 32-00-00.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 93,097 hrs · 16,450 cycles

ON TAXI, EICAS WARNING MSG, FIRE MAIN DECK AFT, DISPLAYED. ACCOMPLISHED CHECKLIST, WALK THROUGH BY LOADMASTER, CONFIRMED & FALSE CONDENSATION. ACCOMPLISHED FIRE & OVERHEAT DETECTION SYS OPERATIONAL TEST IAW MM 26-10-00-715-001. ALL TEST PASSED, NO MSGS DISPLAYED. OK FOR SERVICE.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 93,042 hrs · 16,421 cycles

ON BLOCK IN EICAS MSG FIRE MAIN DECK AFT DISPLAYED, INTERMITTENTLY. NO FIRE OBSERVED. FOUND CMC MSG 26336. TESTED SYS IAW 26-16-881, MSG CLEARED & NO EXISTING FAULTS. OK FOR SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (STEERING SYS) · airframe 92,116 hrs · 16,240 cycles

DURING TAKEOFF, ACFT PULLED HARD LT, COULD NOT CONTROL. REJECTED TAKEOFF APPROX 10 KNOTS. PERFORMED CMC BITE TEST, NO MSG NOTED. ACCOMPLISHED ANTI-SKID TEST, BRAKE RELEASE TEST & STEERING TEST, ALL PASSED. DURING BODY GEAR STEERING TEST, SYS FAILED, DURING LT TURN MANEUVER, RETURNED OK. DEACTIVATED B/G STEERING IAW DDG 32-53-01, CAT C, MDDR 59841.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 91,986 hrs · 16,212 cycles

MAIN DECK CARGO AFT FIRE WARNING. VERIFIED NO FIRE PRESENT. PERFORMED TEST OF SYS & OK. MSG CLEARED.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 91,944 hrs · 16,207 cycles

AFT CARGO FIRE WARNING REF LOG ITEMS M10, 11, 12, 13, 14, 15, 16, 18, 19, 21, 22, 23 & 34. REPLACED M9422, M9225, M9227 & M9223 SMOKE DETECTORS. SIGNAL CARD A15 REPLACED. REPLACED SD CONTROLLER. ALL OPERATIONS SATISFACTORY.

Part: FIRE WARNING — FALSE ACTIVATION (CARGO BAY) · airframe 91,849 hrs · 16,190 cycles

AFT CARGO FIRE DURING FINAL. RAN QRH PROCEDURES, CVR PULLED. REMOVED FOUR EACH FORWARD CARGO FIRE BOTTLES AMM 26-23-00. CARGO LOWER AFT COMPARTMENT FIRE SYSTEM IAW FIM 26-16 TASKS, DETERMINED TO BE A FALSE FIRE WARNING. NO EVIDENCE OF SMOKE OR FIRE FOUND. SMOKE DETECTOR SYSTEM CHECKED NORMAL IAW AMM 26-16-00. FIRE EXTINGUISHER SYSTEM CHECKED NORMAL IAW AMM 26-23-00.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 91,717 hrs · 16,167 cycles

AFTER B/O FIRE, MAIN DECK AFT EICAS MSG CONFIRMED. NO FIRE RETURNED TO BLOCKS. PERFORMED CMC FIRE WARNING TEST, SYS CHECKED NORMAL IAW AMM 26-14-00-735-067. NO OTHER MSG NOTED. NOTICED HIGH HUMIDITY, FOG, ON AFT MAIN DECK CAUSING THE AFT FIRE DETECTORS TO ACTIVATE. ACFT OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (EVAC SLIDE) · airframe 91,717 hrs · 16,166 cycles

RIGHT UPPER DECK SLIDE BATTERY TEST SWITCH INOPERATIVE. DOES NOT TEST. R & R RT UPPER DECK DOOR SLIDE BATTERY PACK IAW MM 52-23-14-404-005. OPERATIONS CHECK NORMAL.

Part: BRACKET — DEBONDED (EMERGENCY EXIT) · airframe 91,688 hrs · 16,159 cycles

RIGHT UPPER DECK EMER EXIT LOWER FWD DOOR LINING BRACKET BECAME DISBONDED. REPAIRED LINING BRACKET IAW AMM 25-00-00 801.