N450PA

Part: TIRE — FAILED (ZONE 700) · airframe 102,134 hrs · 17,135 cycles

#8 MLG BLEW OUT TOWER REPORTED SMOKE & TIRE DEBRIS ON RUNWAY. R & R NR 8 MWA IAW AMM 32-45-01 & IPC 32-45-03-02. C/W BLOWN TIRE CHAP 5 INSP IAW AMM 05-51-25. R & R NR 7 MWA IAW AMM 32-45-01. R & R NLG STEERING CYLINDER IAW AMM 32-53-11. OPS CHKD NORMAL. NO LEAK NOTED. CUTOUT DAMAGED AREA AT BS 148 WTB FRAME LWR FLANGE IAW SRM 51-10-01. PERFORMED NDT AT WT OUT & OPEN BOLT HOLES PER NDTM PT 6 51-00-00. NO FURTHER DEFECTS NOTED. ACCOMPLISHED REPAIR AT LT WTB FAIRING BS 1580 LT IAW SRM 53-00-71 & 51-40-02. PERFORMED NDT AROUND WT OUT & OPEN BOLT HOLES IAW NDTM PT6 51-00-00. NO FURTHER DEFECTS NOTED. R & R NR 8 ANTISKID CONTROL VALVE IAW AMM 32-42-02. OPS CHKD OK. R & R NR 7 BRAKE ASSY IAW AMM 32-41-15. OPS CHKD OK. R & R CONN DV69 IAW WDM 32-42-15. OPS CHKD OK. R & R BSCU IAW AMM 32-42-01. OPS CHKD OK IAW AMM 32-42-001. R & R BRAKE ASSY IAW AMM 32-41-15. OPS CHKD OK. R & R NR 8 MLG BRAKE TEMP SENSOR IAW AMM 32-46-01/401. OPS CHKD OK. REMOVED LT AFT WTB PANEL 193BL IAW AMM 53-51-01. REPAIRED PANEL IAW SRM 51-70-07, 53-00-70 & AMM 51-42-11. REMOVED LT AFT WTB FAIRING PANEL 198CL IAW AMM 53-51-01. REPAIR ACCOMPLISHED IAW SRM 51-70-07 & AMM 51-42-11. REMOVED LT AFT FUSELAGE WTB FAIRING PANEL 193DL & REPAIRED IAW SRM 51-70-07, 53-00-70 & AMM 51-24-11. NO FURTHER DEFECTS NOTED. ORIGINAL SUBMISSION DATE: 11/12/2025

Part: WHEEL — DAMAGED (ZONE 700) · airframe 102,105 hrs · 17,130 cycles

NR 3 MAIN TIRE DAMAGED. REPLACED NR 3 AND 4 MLG WHEEL ASSY IAW AMM 32-45-01/401. PRESS & LEAK CHK OK.

Part: INDICATION SYS — FAULTED (HYD SYSTEM) · airframe 101,813 hrs · 17,089 cycles

FLIGHT CREW REPORTED NR 4 HYD QTY INDICATION ERRATIC IN FLIGHT. PERFORMED WIRING CHECK BETWEEN DW 3112C PIN 2 AND DM7838EA PIN G15, DM 7838BA PIN D15, CHECKS NORMAL. R & R NR 4 HYD IM AND GROUND TEST PASS IAW AMM 29-11-42, WDM 27-62-11 & AIPC 29-11-42-01B, AP-32557. DMI 239827 CLOSED, PLACARD REMOVED.

Part: TIRE — FAILED (ZONE 700) · airframe 101,117 hrs · 16,978 cycles

AT LANDING, #1 TIRE BLEW. FLAT SPOT FOUND. CREW HAD AUTOBRAKE SET AT 4 MINIMUM LEVEL DUE TO NO AUTOSPOILER AND BRAKE ROD. ONCE DISENGAGED, CREW MANUAL BRAKE DID NOT EXCEED LEVEL 2. A/C TAXIED & TOWED IN WITH BLOWN TIRE. R & R #1 MWA IAW AMM 32-45-01/401 & AIPC 32-45-03-02. OPS & LK CHK OK. R/R #1 BRAKE ASSY IAW AMM 32-41-15/401 & AIPC 32-41-15-01A. LEAK CHECK GOOD.: PERFORMED INSPECTION & WIRING CHECK IAW WDM 32-42-14-1, FOUND CONNECTOR DM 48 FOR TRANSDUCER #1 & DM 47 FOR TRANSDUCER #2 WAS IN THE WRONG POSITIONS. SWAPPED BOTH CONNECTORS TO CORRECTED POSITIONS IAW AMM 32-42-04 & WDM 32-42-14-1. NO OTHER DEFECTS NOTED. PERFORMED LT WING GEAR ANTI-SKID TEST IAW AMM 32-42-00-735-779, SYS TEST GOOD. PERFORMED BRAKE SYSTEM BITE GND TEST IAW AMM 32-42-00-715-297, GND TEST GOOD FOR LT WING GEAR. MORE T/S REQ FOR ITEM 3 DISCREPANCY. C/W EO 4432A177 PART 4 ON LT WING GEAR ANTISKID SYS, NO DEFECTS FOUND.

Part: PLATE — DAMAGED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

STEEL PLATE FOUND 3 EA FASTENER HOLE SEM AT UPR DECK RH STA860 TENSION TIE AREA. STEEL PLATE REPLACED CARRIED OUT AS PER RI-53-20-17745 REV.A. NO FURTHER DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D STA 617 - STA 635 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED L:13" X W:0.7" X D:0.006" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED.

Part: SEAT TRACK — SCRATCHED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D SEAT TRACK CTR GUIDE STUD AREA FOUND SCRATCHED AT LBL 11 STA 1430, STA 1450, STA 1470. SCRATCH AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, BLENDED OUT AREA MEASURED L:4' X W:0.7" X D:0.008", WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED.

Part: FAIRING — DELAMINATED (ZONE 600 FLAP) · airframe 100,859 hrs · 16,937 cycles

RIGHT WING O/B MID FLAP L/E FAIRING FOUND DELAMINATION AT O/B 180". PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED.

Part: LUG — CRACKED (ZONE 100) · airframe 100,859 hrs · 16,937 cycles

1 EA CRACK WAS FOUND ON BS 1000 LBL 11.33" INTERCOSTAL LUG FITTING. INTERCOSTAL LUG FITTING REPLACED AS PER ATLAS AIR EO 4453C024 REV.4 PART 3 STEP 3. NO FURTHER DEFECTS NOTED.

Part: WEB — CRACKED (ZONE 500 LE) · airframe 100,859 hrs · 16,937 cycles

LEFT WING L/E FIXED INTERNAL AT INBD ILES 693.5 WEB CRACKED. WEB CRACK AREA REPAIRE AS PER RI-57-41-17749 REV A. NO FURTHER DEFECTS NOTED.

Part: LUG — CRACKED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

1 EA CRACK WAS FOUND ON BS 1000 RBL 11.33 INTERCOSTAL LUG FITTING. INTERCOSTAL LUG FITTING REPLACED AS PER ATLAS AIR EO 4453C024 REV.4 PART 7 STEP 3. NO FURTHER DEFECTS NOTED.

Part: FAIRING — PUNCTURED (ZONE 500 FLAP) · airframe 100,859 hrs · 16,937 cycles

LEFT WING I/B FORE FLAP MID L/E FAIRING FOUND PUNCH HOLE FROM I/B 133". PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. C. NO FURTHER DEFECTS NOTED.

Part: SPLICE STRAP — CRACKED (ZONE 500) · airframe 100,859 hrs · 16,937 cycles

LEFT WING L/E FIXED SPLICE STRAP-LOWER CRACK AT INBD ILES 693.5 AREA. SPLICE STRAP-LOWER CRACK AREA REPAIRED AS PER RI-57-41-17749 REV A. NO FURTHER DEFECTS NOTED.

Part: SEAT TRACK — CHAFED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D STA 1968 TO STA 1970 LBL 11 SEAT TRACK CROWN FOUND CHAFED. CHAFE AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND SMOOTHED OUT AREA MEASURED L:4" X W:03" X D:0.006", WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED.

Part: SEAT TRACK — CHAFED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D STA 1980 TO STA 1985 RBL 11.33" SEAT TRACK CROWN CHAFED. CHAFED AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND SMOOTHED OUT AREA MEASURED L:6" X W:0.3" X D:0.007" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED.

Part: FRAME — CRACKED (ZONE 400) · airframe 100,859 hrs · 16,937 cycles

NR 4 ENG NACELLE LT CORE COWL FRAME NR 2 FOUND CHAFED. FRAME CHAFE AREA REPAIRED IAW SRM 54-45-02-2R-1 REPAIR FIG 201. NO FURTHER DEFECTS NOTED.

Part: PLATE — DAMAGED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

STEEL PLATE FOUND 4EA FASTENER HOLES SEM AT UPR DECK R/H STA 760 TENSION TIE AREA. STEEL PLATE REPLACED CARRIED OUT AS PER RI-53-20-17745 REV.A. NO FURTHER DEFECTS NOTED.

Part: BULKHEAD — CRACKED (ZONE 100) · airframe 100,859 hrs · 16,937 cycles

1 EA CRACK FOUND ON BS 2598 BULKHEAD RH AFT INNER CHORD CRACK AT 3 O'CLOCK POSITION (VIEW LOOKING FWD) CRACK DEPTH APPROX 0.015" FROM FORWARD SURFACE. INNER CHORD CRACK AREA REPAIRED AS PER RI-53-80-17738 REV A. NO FURTHER DEFECTS NOTED.

Part: SEAT TRACK — CHAFED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D STA 1890 TO 1893 LBL 11 SEAT TRACK CROWN FOUND CHAFED. CHAFE AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND CHAFING SMOOTHED OUT AREA MEASURED AS PER SRM 53-00-52-1A-1. WITHIN ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D STA 2200 - STA 2210 LBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED L:4" X W:0.7" X D:0.005" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D STA 687-STA 694 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED: L=8" X W=0.7" X D=0.007" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED.

Part: PLATE — DAMAGED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

STEEL PLATE FOUND 3 EA FASTENER HOLE SEM AT UPR DECK RH STA800 TENSION TIE AREA. STEEL PLATE REPLACED CARRIED OUT AS PER RI-53-20-17745 REV.A. NO FURTHER DEFECTS NOTED.

Part: BULKHEAD — CRACKED (ZONE 100) · airframe 100,859 hrs · 16,937 cycles

1 EA CRACK FOUND ON BS2598 BULKHEAD LH AFT INNER CHORD CRACK AT 3 O'CLOCK POSITION VIEW LOOKING FWD, CRACK DEPTH APPROX 0.080" FROM FORWARD SURFACE. INNER CHORD CRACK AREA REPAIRED AS PER RI-80-17737 REV A. NO FURTHER DEFECTS NOTED.

Part: PLATE — DAMAGED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

STEEL PLATE FOUND 2 EA FASTENER HOLE SEM AT UPR DECK LH STA860 TENSION TIE AREA. STEEL PLATE REPLACED CARRIED OUT AS PER RI-53-20-17745 REV.A. NO FURTHER DEFECTS NOTED.

Part: GUIDE — CORRODED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D STA 1920 - 1980 SCD AFT SIDE GUIDE FOUND CORROSION. CORROSION AREA REMOVED AS PER CMM 25-55-06 AND REPROTECTED AS PER SRM 51-20-01 AND CORROSION REMOVED AREA MEASURE L:13" X W:2" X D:0.028", ORG THICKNESS 0.152" WITHIN CMM 25-55-06 LIMITS. NO FURTHER DEFECTS NOTED.

Part: FRAME — CRACKED (ZONE 400) · airframe 100,859 hrs · 16,937 cycles

#4 ENG R/H CORE COWL FRAME #5 (COUNT FROM FWD) FOUND CRACKED. FRAME CRACK AREA REPAIRED AS PER SRM 54-41-02-2R-2 REPAIR 2 FIG 201. NO FURTHER DEFECTS NOTED.

Part: SEAT TRACK — SCRATCHED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D SEAT TRACK CTR GUIDE STUD AREAS FOUND SCRATCHED AT RBL 11 STA 1611, STA 1631, STA 1772. SCRATCH AREAS SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND SMOOTHED AREA MEASURED L:3" X W:0.7" X D:0.007", WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED.

Part: FAILSAFE — CRACKED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

UPPER DECK LH BS820 TENSION TIE FAIL SAFE CHORD 1EA CRACK FOUND. FAIL SAFE CHORD CRACK AREA REPAIRED AS PER SRM 51-70-11-0G-0. NO FURTHER DEFECTS NOTED.

Part: SEAT TRACK — CHAFED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D STA 2020 TO STA 2026 RBL 11 SEAT TRACK CROWN CHAFED. CHAFED AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND SMOOTHED OUT AREA MEASURED L:7" X W:0.3" X D:0.008", WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG  101 LIMITS. NO FURTHER DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D STA 650 - STA 654 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED L:9' X W:0.7" X D:0.008" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED.

Part: DUCT — CRACKED (NR 2 ENGINE) · airframe 100,859 hrs · 16,937 cycles

NO. 2 ENG - RH C-DUCT OUTER GROOVE UPPER AREA CRACK FOUND. FRAME CRACK AREA REPAIRED AS PER ATLAS AIR EA NO.EA-1978A227 REV.0. NO FURTHER DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D STA 566-STA 592 LBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED: L=15" X W=0.7" X D=0.008" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED.

Part: SEAT TRACK — SCRATCHED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D SEAT TRACK CTR GUIDE STUD AREAS FOUND SCRATCHED AT RBL 11 STA 1370, STA 1390, STA 1410. SCRATCH AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, SMOOTHED AREA MEASURED L:4" X W:0.7" X D:0.008" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED.

Part: BEAM — CRACKED (ZONE 100) · airframe 100,859 hrs · 16,937 cycles

NWW SIDE PANEL HAS 1 EA CRACK FWD AT BEAM RHS WL180 BETWEEN STA 265 AND 280.(<P>CRACKED BEAM REPLACED AS PER BOEING DWG NO.65B07942 & PL & EO 4453A043 REV 11 PART 2 ITEM 3 AND NEW BEAM HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW BEAM INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

FUNCTIONAL TEST EMERGENCY LIGHTS BATTERY PACKS FOR CAPACITY (15 MIN. MINIMUM). FOUND EMERGENCY LT L1533, L5733, L5767 & M4915 WENT OFF IN LESS THAN 15 MINUTES. EMERGENCY LT POWER PACK M5169 REPLACED AND OPERATION CHECKED NORMAL IAW AMM 33-51-04.

Part: WEB — CRACKED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D STA 1200 L/H O/B BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED. INTERCOSTAL WEB CRACK AREA REPAIRED AS PER SRM 53-40-51-2R-9 REPAIR 9. NO FURTHER DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D STA 780, 783 LBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED L=5" X W=0.7", D=0.006" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED.

Part: FAIRING — DELAMINATED (ZONE 600 FLAP) · airframe 100,859 hrs · 16,937 cycles

RIGHT WING I/B AFT FLAP MID L/E FAIRING FOUND DELAMINATION AT O/B 180". PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED.

Part: SKIN — CRACKED (ZONE 800 APU) · airframe 100,859 hrs · 16,937 cycles

APU RIGHT DOOR SKIN AT NR 1 LATCH OPENING AND FWD LOWER FOUND CRACKED AND CHAFING. NR 1 LATCH CUTOUT CRACK & FWD LWR SKIN CHAFING AREA REPAIRED AS PER RI-52-48-17747 REV A. NO FURTHER DEFECTS NOTED.

Part: WEB — CRACKED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D STA 1220 L/H O/B BELOW FLOOR INTERCOSTAL WEB CRACKED. INTERCOSTAL WEB CRACK AREA REPAIRED AS PER SRM 53-40-51-2R-5 REPAIR 5. NO FURTHER DEFECTS NOTED.

Part: FAIRING — DELAMINATED (ZONE 600 FLAP) · airframe 100,859 hrs · 16,937 cycles

RIGHT WING I/B MID FLAP L/E FAIRING FOUND DELAMINATION AT I/B 13". PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D STA 750-STA 783 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED" L=4" X W=0.7" X D=0.007" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED.

Part: WEB — CRACKED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D STA 1180 L/H O/B BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED. INTERCOSTAL WEB CRACK AREA REPAIRED AS PER SRM 53-40-51-2R-8 FIG 8. NO FURTHER DEFECTS NOTED.

Part: WEB — CRACKED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D STA 1180 RH O/B BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED. INTERCOSTAL WEB CRACK AREA REPAIRED AS PER SRM 53-40-51-2R-8 REPAIR 8. NO FURTHER DEFECTS NOTED.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D STA 981 TO 983 LBL 75" SUBSTITUTE TRACK FOUND CRACKED. SUBSTITUTE TRACK CRACK AREA REPAIRED AS PER SRM 53-00-52-2R-13 REPAIR 13 FIG 201. NO FURTHER DEFECTS NOTED.

Part: SEAT TRACK — CHAFED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D STA 646 TO STA 656 LBL 11 SEAT TRACK CROWN FOUND CHAFED. CHAFE AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND SMOOTHED OUT AREA MEASURED L:5" X W:0.3" X D:0.007", WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED.

Part: PLATE — DAMAGED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

STEEL PLATE FOUND 1 EA FASTENER HOLE SEM AT UPR DECK LH STA880 TENSION TIE AREA. STEEL PLATE REPLACED CARRIED OUT AS PER RI-53-20-17745 REV.A. NO FURTHER DEFECTS NOTED.

Part: LONGERON FITTING — CRACKED (ZONE) · airframe 100,859 hrs · 16,937 cycles

LEFT BS 1480 LONGERON EXTENSION FITTING FOUND CRACKED. CRACK LONGERON EXTENSION FITTING REPAIRED AS PER ATLAS AIR EO 4453A818 REV 20 PART 7. NO FURTHER DEFECTS NOTED.

Part: SKIN — DAMAGED (ZONE 500) · airframe 100,859 hrs · 16,937 cycles

LEFT WING L/E FIXED FAIRING BETWEEN INBD ILES 630.46 TO ILES 693.5 SEVERAL FASTENER HOLES FOUND ELONGATED. L/E SKIN REPAIRED AS PER RI-57-41-17749 REV.A. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — CRACKED (ZONE 500 FLAP) · airframe 100,859 hrs · 16,937 cycles

LEFT WING #10 VC FLAP BULLNOSE O/B EDGE FOUND DEFORMED AND CRACKED. O/B EDGE DAMAGE AREA REPAIRED AS PER RI-57-40-17758 REV A. NO FURTHER DEFECTS NOTED.

Part: DOUBLER — CRACKED (ZONE 800) · airframe 100,859 hrs · 16,937 cycles

MAIN DECK - L1 ENTRY DR UPR HINGE DOUBLER FND CRACKED. DOUBLER REPLACED AS PER SRM 51-10-02 AND NEW DOUBLER HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW DOUBLER INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.

Part: SKIN — DAMAGED (ZONE 400) · airframe 100,859 hrs · 16,937 cycles

NR 4 NACELLE NOSE COWL LIP SKIN INTERIOR SURFACE 1 EA FASTENER HOLE ELONGATED. ELONGATE FASTENER HOLE AREA REPAIRED AS PER ATLAS EA-1971A218 REV. 0. NO FURTHER DEFECTS NOTED.

Part: SEAT TRACK — SCRATCHED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D SEAT TRACK CTR GUIDE STUD AREAS FOUND SCRATCHED AT RBL 11 STA 1430, STA 1450 & STA 1470. SCRATCH AREAS SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND SMOOTHED AREA MEASURED L:4" X W:0.7" X D:0.009", WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D STA 546 TO STA 559 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED L:8 X W:0.7" X D:0.007" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED.

Part: BEAM — CRACKED (ZONE 500 LE) · airframe 100,859 hrs · 16,937 cycles

LEFT WING L/E FIXED LOWER BEAM CRACK L/E ILES 693.5 AREA. BEAM REPAIRED AS PER RI-57-41-17749 REV A. NO FURTHER DEFECTS NOTED.

Part: TEE ANGLE — CRACKED (ZONE 400) · airframe 100,859 hrs · 16,937 cycles

NR 3 PYLON O/B INNER MOST LWR TEE CRACKED AT NAC STA 344 APPROX. TEE CRACK AREA REPAIRED AS PER SRM 54-51-02-2R-2 REPAIR 2 FIG 201. NO FURTHER DEFECTS NOTED.

Part: BEAM — CRACKED (ZONE 500 LE) · airframe 100,859 hrs · 16,937 cycles

LEFT WING L/E FIXED INTERNAL AT INBD ILES 693.5 UPPER CHORD CRACKED. UPR CHORD CRACK AREA REPAIRED AS PER RI-57-41-17749 REV A. NO FURTHER DEFECTS NOTED.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D STA753 TO STA757 LBL11" SEAT TRACK FOUND CRACKED. SEAT TRACK CRACK AREA REPAIRED AS PER SRM 53-00-52-2R-12 REPAIR12 FIG 201. NO FURTHER DEFECTS NOTED.

Part: PLATE — DAMAGED (ZONE 100) · airframe 100,859 hrs · 16,937 cycles

STEEL PLATE FOUND 3 EA FASTENER HOLE SEM AT UPR DECK LH STA840 TENSION TIE AREA.(<P>STEEL PLATE REPLACED CARRIED OUT AS PER RI-53-20-17745 REV.A. NO FURTHER DEFECTS NOTED.</P>)

Part: FAIRING — DELAMINATED (ZONE 600 FLAP) · airframe 100,859 hrs · 16,937 cycles

RIGHT WING O/B MID FLAP L/E FAIRING FOUND DELAMINATION AT I/B 12". PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

DOOR L1 FWD EMERGENCY SILL LT L1853 FOUND INOP. DOOR L1 FWD EMERGENCY SILL LT L1853 LAMP REPLACED AND TEST NORMAL IAW AMM 33-51-05.

Part: SEAT TRACK — CHAFED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D STA 1457 TO STA 1461 RBL 11 SEAT TRACK CROWN CHAFING. CHAFING AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND SMOOTHED OUT AREA MEASURED L:7" X W:0.3" X D:0.008", WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D STA 606-STA 624 LBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED: L=8" X W=0.7" X D=0.006" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMTIS. NO FURTHER DEFECTS NOTED.

Part: BEAM — CRACKED (ZONE 100) · airframe 100,859 hrs · 16,937 cycles

NWW SIDE PANEL HAS 1EA CRACK FOUND AT BEAM LHS WL130 BETWEEN STA 320 AND STA 340. BEAM REPLACED AS PER BOEING DWG: 65B07942&AMP;PL AND NEW BEAM HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW BEAM INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.

Part: TENSION TIE — CRACKED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

UPPER DECK LH BS940 TENSION TIE FWD CHANNEL 1 EA CRACK FOUND. TENSION TIE FWD CHANNEL PERFORMED INTERIM REPAIR AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED.

Part: TENSION TIE — CRACKED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

UPPER DECK LH BS820 TENSION TIE FWD CHANNEL 1 EA CRACK FOUND. TENSION TIE CHANNEL REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED.

Part: FAIRING — DELAMINATED (ZONE 500 FLAP) · airframe 100,859 hrs · 16,937 cycles

LEFT WING I/B MID FLAP L/E FAIRING FOUND DELAMINATION AT O/B 70". PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED.

Part: TEE ANGLE — CRACKED (ZONE 400) · airframe 100,859 hrs · 16,937 cycles

NO. 2 PYLON - O/B MOST LOWER TEE CRACK FOUND AT NAC STA 332. TEE CRACK AREA REPAIRED AS PER SRM 54-51-02-2R-2 REPAIR 2 FIG 201. NO FURTHER DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D SEAT TRACK CTR GUIDE STUD AREAS FOUND SCRATCHED AT RBL 11.33 STA 1853 AND STA 1913. SCRATCH AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND SMOOTHED AREA MEASURED L:6" X W:0.7" X D:0.006", WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D STA 872-STA 875 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED: L=6" X W=0.7" X D=0.005" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED.

Part: FAIRING — DELAMINATED (ZONE 600 FLAP) · airframe 100,859 hrs · 16,937 cycles

RIGHT WING O/B MID FLAP L/E FAIRING FOUND DELAMINATION AT I/B 39". PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D STA 570 - STA 593 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED L:6" X W:0.7" X D:0.006" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED.

Part: FAIRING — CHAFED (ZONE 600 FLAP) · airframe 100,859 hrs · 16,937 cycles

RHW I/B AFT FLAP I/B L/E FAIRING FOUND CHAFING. PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5.G. NO FURTHER DEFECTS NOTED.

Part: FRAME — CRACKED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

UPPER DECK TENSION TIE AT RH BS860 1 EA CRACK FOUND. FRAME REPLACED CARRIED OUT AS PER SRM 51-10-02 AND NEW FRAME HOLES AS PER SRM 51-40-05 AND NEW FRAME INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.

Part: PLATE — DAMAGED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

STEEL PLATE FOUND 3 EA FASTENER HOLE SEM AT UPR DECK RH STA840 TENSION TIE AREA. STEEL PLATE REPLACED CARRIED OUT AS PER RI-53-20-17745 REV.A. NO FURTHER DEFECTS NOTED.

Part: TENSION TIE — CRACKED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

UPPER DECK LH BS900 TENSON TIE FWD CHANNEL 1 EA CRACK FOUND. TENSION TIE FWD CHANNEL PERFORMED INTERIM REPAIR AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED.

Part: DUCT — CHAFED (NR 4 ENGINE) · airframe 100,859 hrs · 16,937 cycles

NR 4 ENG RH C-DUCT FWD BLOWOUT DOOR L/E FOUND CHAFING. CHAFING AREA REPAIRED AS PER ST ENGINEERING CMM 78-32-09 REPAIR 5. NO FURTHER DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D STA 730-STA 752 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED: L=6" X W=0.7" X D=0.005" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

MDC - STA 1160 - 1180 LH O/B FLOOR SUPPORT CRACK. FLOOR SUPPORT CRACK AREA REPAIRED AS PER RI-53-40-17764 REV A. NO FURTHER DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 100,859 hrs · 16,937 cycles

M/D STA 545-STA 559 LBL 11 SEAT TRACK CROWN CORRODED. CORRSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED: L=8" X W=0.7" X D=0.007" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED.

Part: PSEU — FAULTED (ZONE 700) · airframe 100,314 hrs · 16,847 cycles

AFTER TAKE OFF, GEAR TILT MESSAGE &AMP; GEAR HANDLE WOULD NOT MOVE PAST OFF.(<P>ADJUSTED LT BLG PROX SWITCH AND TARGET PER B747 AMM 32-61-12-822-019. BODY GEAR OPS CHECK GOOD PER B747 AMM 32-33-715-071. REPLACED PSEU PER B747 AMM 32-09-03-004-001 AND 32-09-03-404-005. OPS CHECK GOOD PER B747 AMM 32-09-03-145-019.</P>)

Part: FAIRING — DELAMINATED (ZONE 500) · airframe 97,845 hrs · 16,453 cycles

LHW I/B MID FLAP I/B 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: LAMP — INOPERATIVE (ZONE 200) · airframe 97,845 hrs · 16,453 cycles

MAIN DECK L1 DR STILL FWD EMER LT INOP.(<P>MAIN DECK L1 DR STILL FWD EMER LT LAMP REPLACED &AMP; OPERATION TEST NORMAL IAW AMM 33-51-05.</P>)

Part: ENGINE — FAULTED (NR 1) · airframe 97,816 hrs · 16,449 cycles

#1 ENGINE IN FLIGHT SHUTDOWN DIVERTED TO ICN.(<P>ACCOMPLISHED WO 134669. R/R #1 ENG IAW WC 71-099-02-01 &AMP; OPS &AMP; LEAK CHECK GOOD IAW AMM 71-00-02.</P>)

Part: NONE — NONE (NONE) · airframe 97,652 hrs · 16,419 cycles

ATB PERFORMED DUE TO COLLAPSED PALLET OF BATTERIES AT POSITION GL.(<P>PER AMM 05-51-15 INSPECTED MCD POSITION GL AREA FOR CHEMICAL SPILL AND FOUND NO SPILLAGE. BATTERIES FOUND TO BE LITHIUM BATTERIES AND NO DEFECTS NOTED. NO DAMAGE OR DEFECTS TO A/C PER AMM 25-59-01 AND 25-58-00.</P>)

Part: BRAKE ASSY — FAILED (NR 12) · airframe 97,524 hrs · 16,398 cycles

#12 BRAKE FAILED ON LANDING(<P>REPLACED #12 BRAKE ASSY PER AMM 32-41-15. OPS &AMP; LEAK CHECK OK</P>)

Part: FLAP SYSTEM — FAULTED (TE FLAP SYS) · airframe 97,513 hrs · 16,396 cycles

UPON DEPARTURE, FLAPS DRIVE. OUTBOARD FLAPS LOCKED AT APPROX F5 POSITION.(<P>PERFORMED FLAPS OPS TEST SEVERAL TIMES PER AMM 27-58-01, CAN'T DUPLICATE FAULT ON GROUND. COMPLETED AP 28370 FOR TE FLAP SYS, FLAP SYS OPS TEST NORMAL

Part: RVDT — FAULTED (TE FLAPS) · airframe 96,948 hrs · 16,317 cycles

DURING FLAP RETRACTION AFTER DEPARTURE, FLAP DRIVE CAME ON EICAS. FLAPS WOULD NOT RETRACT PAST 5DEG ON OUTBOARD FLAPS(<P>R/R RH OUTBOARD RVDT PER AMM 27-58-01. NO FURTHER DEFECTS NOTED.&NBSP;</P>)

Part: ENGINE — LEAKING (NR 4) · airframe 96,480 hrs · 16,249 cycles

NR 4 ENGINE OIL QUANTITY DROPPED TO 2 QTS IN FLIGHT. C/W WO #128800, R & R NR 4 ENGINE, OPS & LEAK CHECKED NORMAL IAW W/C # 71-099-02-01.

Part: GCU — FAILED (NR 1 AC BUSS) · airframe 95,624 hrs · 16,119 cycles

AC 1 BUS FAILED(<P>REMOVED AND REPLACED THE GCU 1 IAW AMM 24-23-01/401. OPS CHK IS GOOD</P>)

Part: SEAL — UNKNOWN (UNKNOWN) · airframe 94,188 hrs · 15,889 cycles

#4 OIL QTY DECREASING IN FLIGHT 1 QUART PER 20 MIN(<P>PERFORMED ENGINE DRAIN INSPECTION IAW AMM 71-71-00, FOUND OIL LEAKING FROM HMM DRAIN LINE. R/R CARBON SEAL AT AGB IAW AMM 72-64-02. R/R HHM IAW AMM 73-21-14. PERFORMED IDLE LEAK CHECK TEST #3 &AMP; #12 EEC ACTUATOR GROUND TEST, NO LEAK NOTED. LEAK CHECK GOOD. OPS CHK GOOD.&NBSP;</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,382 hrs · 15,760 cycles

CRACK - MAIN DECK CGO FLOOR SUBSTITUTE SEAT TRACK AT STA 970 RBL 75(<P>1) REMOVED THE EXISTING REPAIR PART IAW SRM 51-40-02-0G-0 REV 98. 2) REPAIRED DAMAGE AREA IAW SRM 53-00-52-2R-13 REPAIR 13 REV 98. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: SHEAR TIE — UNKNOWN (UNKNOWN) · airframe 93,382 hrs · 15,760 cycles

CRACK - FOUND THE SHEAR TIE CRACK AT STA 1000 RBL 75.92(<P>1) REMOVED THE DAMAGE PART IAW SRM 51-40-02-0G-0 REV 97 AND EO 4453C024 PART 10 REV 3. 2) INSTALL NEW PART IAW SRM 51-40-02-0G-0 REV 97 AND EO 4453C024 PART 10 REV 3. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,382 hrs · 15,760 cycles

CRACK - MAIN DECK CGO FLOOR SUBSTITUTE SEAT TRACK AT STA 990 LBL 75(<P>1) REMOVED THE EXISTING PART IAW SRM 51-40-02-0G-0 REV 98. 2) REPAIRED DAMAGE AREA IAW SRM 53-00-52-2R-13 REPAIR 13 REV 98. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: BATTERY — UNKNOWN (UNKNOWN) · airframe 93,382 hrs · 15,760 cycles

FOUND EMERGENCY LT POWER SUPPLY BATTERY (M5170) AT STA 550 WL323 LBL 83 FUNCTIONAL FAIL(<P>IAW AMM 33-51-04-902-001-001 REV 107 REMOVED AND SENT THE BATTERY FOR REPAIR, AFTER THAT, INSTALLED THE BATTERY AND PERFORMED POWER SUPPLY TEST. THE TEST RESULT WAS GOOD.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,382 hrs · 15,760 cycles

DEVIATION - DURING PERFORMING TASK CARD 4453A087 PART 2 EXISTING CONDITION IS DIFFERENT WITH DWG STA 500 RH SIDE(<P>1) ACCOMPLISHED JOB IAW EI T2023A53M-1557 REV 0. 2) ACCOMPLISHED EI T2023A53M-1557 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,382 hrs · 15,760 cycles

DEVIATION - DURING PERFORMING TASK CARD 4453A087 PART 2 EXISTING CONDITION IS DIFFERENT WITH DWG AT STA 340 RH SIDE(<P>1) ACCOMPLISHED JOB IAW EI T2023A53M-1571 REV 0. 2) ACCOMPLISHED IAW EI T2023A53M-1571 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: ACTUATOR — UNKNOWN (UNKNOWN) · airframe 93,382 hrs · 15,760 cycles

FOUND FUNCTION FAIL AT RH BLG ALTERNATE EXTENSION ROTARY ACTUATOR(<P>1) IAW AMM 32-35-01-004-001 REV 107 AND AMM 32-35-01-404-007 REV 107 R/R RH BLG ALTERNATE EXTENSION ACTUATOR. 2) IAW AMM 32-35-00-715-059 REV 107 PERFORM RH BLG ALTERNATE EXTENSION SYSTEM OPERATIONAL TEST RESULT WAS NORMAL. 3) CONDITION CHECK NORMAL</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,382 hrs · 15,760 cycles

FOUND L5 DOOR FRAME WEB CRACK AT STA 2231 S21L - S22L(<P>1) REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 97. 2) REPAIRED DAMAGE AREA IAW SRM 53-60-15-2R-3 REPAIR 3 REV 97 AND EI T2023A53M-1537 REV 0. 3) INSTALLED FASTENERS IAW SRM 53-60-15-2R-3 REPAIR 3 REV 97 AND EI T2023A53M-1537 REV 0. 4) ACCOMPLISHED IAW EI T2023A53M-1537 REV 1. 5) JOB COMPLETED</P>)

Part: DOUBLER — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 93,382 hrs · 15,760 cycles

WATER FILL CONNECTION AREA DOUBLER CORROSION AT STA 980 S45R - S46R(<P>1) REMOVE DAMAGE PARTS IAW SRM 51-40-02-0G-0 REV 97. 2) INSTALL NEW PARTS SRM 51-40-02-0G-0 REV 97, DWG 142U3780 SHEET 12 REV F, DWG 140U0999 SHEET 30 REV -, DWG 142U0130 SHEET 1 REV A AND DWG 417U2400 SHEET 2 REV -. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,382 hrs · 15,760 cycles

DEVIATION - DURING PERFORMING TASK CARD 4453A087 PART 2 EXISTING CONDITION IS DIFFERENT WITH DWG AT STA 340 LH SIDE(<P>1) ACCOMPLISHED JOB IAW EI T2023A53M-1572 REV 0. 2) ACCOMPLISHED EI T2023A53M-1572 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: SHEAR TIE — UNKNOWN (UNKNOWN) · airframe 93,382 hrs · 15,760 cycles

CRACK - FOUND THE SHEAR TIE CRACK AT LBL 33 STA 1000(<P>1) REMOVED DAMAGE PART IAW SRM 51-40-02-0G-0 REV 97 AND EO 4453C024 PART 4 REV 3. 2) INSTALL NEW PART IAW SRM 51-40-02-0G-0 REV 97 AND EO 4453C024 PART 4 REV 3. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: BRACKET — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 93,382 hrs · 15,760 cycles

FWD LWR WING TO BODY FAIRING PANEL SUPPORT BRACKET SKIN CORROSION STA 920 BL0(<P>1) REMOVE DAMAGE PARTS IAW SRM 51-40-02-0G-0 REV 97. 2) INSTALLED NEW PARTS IAW SRM 51-40-02-0G-0 REV 97, DWG 65B06704 SH2 REV F AND DWG 142U0130 SH1 REV A. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,382 hrs · 15,760 cycles

DEVIATION - DURING PERFORMING TASK CARD 4453A087 PART 2, THE EXISTING CONDITION IS DIFFERENT WITH DWG AT STA 440 LH SIDE(<P>1) ACCOMPLISHED JOB IAW EI T2023A53M-1564 REV 0. 2) ACCOMPLISHED IAW EI T2023A53M-1564 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,382 hrs · 15,760 cycles

CRACK - WEB AND STIFFENER, LH WING INBD FIXED T/E BEAM OUTBD END WBL 429.47(<P>1) PERFORM EI T2023A57M-1568 REV 0. 2) ACCOMPLISHED IAW EI T2023A57M-1568 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL. PN 65B10865-3</P>)

Part: RVDT — NONE · airframe 91,297 hrs · 15,406 cycles

FLAPS DRIVE ON RETRACT ASYMMETRY ON OUTBOARDS(<P>REMOVED AND REPLACED R/H OUTBOARD RVDT TRANSMITTER AT FLAP TRANSMISSION.</P>)

Part: FAIRING — DELAMINATED (RT WING TE FLAP) · airframe 85,308 hrs · 14,560 cycles

RH O/B FORE FLAP L/E FAIRING FOUND DELAMINATION (COUNT FROM I/B EDGE 138.5")(<P>PERFORMED PERMANENT HOT BOND REPAIR AS PER SRM51-70-07 PARA 5.A</P>)

Part: FAIRING — DELAMINATED (LT WING TE FLAP) · airframe 85,308 hrs · 14,560 cycles

LHW O/B FORE FLAP L/E FAIRING FOUND DELAM (COUNT FROM I/B EDGE 42")(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR IAW SRM 51-70-07</P>)

Part: FLOOR PANEL — PUNCTURED (BULK CARGO) · airframe 85,308 hrs · 14,560 cycles

BULK CARGO STA 2040-2060 CENTER FLOOR PANEL FOUND PUNCH HOLE(<P>BULK CARGO COMPT STA 2048 FLOOR PANEL DAMAGED AREA REPAIRED IAW RI-25-54-14646 REV A.</P>)

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 85,308 hrs · 14,560 cycles

RHW #17 VC FLAP BULLNOSE SKIN CHAFE ON O/B EDGE(<P>RHW #17 VC FLAP BULLNOSE SKIN CHAFE ON O/B EDGE DAMAGE AREA TRIM OFF REPAIRED IAW RI-57-00-14635 REV A.</P>)

Part: FAIRING — DELAMINATED (RT WING TE FLAP) · airframe 85,308 hrs · 14,560 cycles

RH O/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED PERMANENT HOT BOND REPAIR AS PER SRM51-70-07 PARA 5.A</P>)

Part: FAIRING — DELAMINATED (LT WING TE FLAP) · airframe 85,308 hrs · 14,560 cycles

LHW I/B FORE FLAP L/E FAIRING FOUND DELAM&NBSP;(<P>PREFORMED PERMANENT COMPOSITE HOTBOND REPAIR</P>)

Part: CHANNEL — CRACKED (HORIZONTAL STAB) · airframe 85,308 hrs · 14,560 cycles

EMP RH HORI STAB TIP FAIRING T/E CHANNEL P/N: 65B03822U12 SUPPORT CRACK(<P>EMP RH HORI STAB TIP FAIRING T/E CHANNEL P/N: 65B03822U12 SUPPORT REPLACED AND INSTALLED IAW RI-55-10-14645 REV B.</P>)

Part: FAIRING — DELAMINATED (LT WING TE FLAP) · airframe 85,308 hrs · 14,560 cycles

LHW I/B MID FLAP L/E FAIRING FOUND DELAM(<P>PREFORMED PERMANENT COMPOSITE HOTBOND REPAIR</P>)

Part: SEAL — PUNCTURED (LT WING TE FLAP) · airframe 85,308 hrs · 14,560 cycles

LHW I/B FORE FLAP COMPRESSION SEAL RIB PUNCTURE(<P>LHW I/B T/E FORE FLAP COMPRESSION SEAL RIB P/N: 65B08466-29 DAMAGED AREAS REPAIRED IAW RI-57-55-14642 REV A.</P>)

Part: FAIRING — DELAMINATED (LT WING TE FLAP) · airframe 85,308 hrs · 14,560 cycles

LHW O/B FORE FLAP L/E FAIRING FOUND DELAM (COUNT FROM I/B EDGE 62")(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR</P>)

Part: PRINTED CKT BOARD — FAULTY (SMOKE WARNING) · airframe 80,039 hrs · 13,658 cycles

MAIN DECK CARGO 11 LOOP B STATUS MSG.(<P STYLE="MARGIN: 0IN; MARGIN-BOTTOM: .0001PT;"><SPAN>MAIN DECK 11 LOOP A AND LOOP B / SMOKE DETECTOR AND AFOLTS CARD REMOVED AND REPLACED IAW AMM</SPAN><SPAN>&NBSP;26-10-0</SPAN><SPAN>, OPS CHECK GOOD. NO FAULTS / NOTED, CARGO INSPECTED, NO IRREGULARITIES NOTED</SPAN><SPAN>&NBSP;IAW AMM 26-14-01 AND 26-10-01.</SPAN></P><P STYLE="MARGIN: 0IN; MARGIN-BOTTOM: .0001PT;"><SPAN></SPAN></P>)

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 79,319 hrs · 13,534 cycles

AT 20,000 FT, NR 1 ENGINE COMPRESSOR STALLED. ENGINE WAS SHUT DOWN. ATB. REMOVED AND REPLACED THE NR 1 ENGINE IAW AMM 71-00-02. PERFORMED IDLE RUN AND LEAK TESTS IAW AMM 71-00-00, OPS CHECKED SATISFACTORY.

Part: TRANSMITTER — FAULTY (TE FLAP) · airframe 77,927 hrs · 13,262 cycles

"FLAP DRIVE" EICAS MESSAGE. (<P>FOUND CMC MSG 27771 REF FIM 27-51 TASK 878, FOUND&NBSP;RT OTBD RVDT TRANSMITTER INCORRECT. REMOVED AND REPLACED RT OTBD TRANSMITTER IAW AMM 27-51-00/401. PERFORMED OPS CHECK IAW AMM TASK 27-58-01-725-050. ALL FLAP POSITION INDICATIONS NORMAL.</P>)

Part: TRANSFORMER — OUT OF LIMITS (TE FLAPS) · airframe 77,793 hrs · 13,242 cycles

FLAPS DRIVE EICAS ON DEPARTURE, OCCURRED ON RETRACTION FROM FLAPS 5 TO FLAPS 1.(<P>DETERMINED&NBSP;L/H OUTBOARD RVDT OUT OF LIMITS. REMOVED AND REPLACED RVDT REF AMM 27-58-01. OPS CHECK OF FLAP SYSTEM OK.</P>)

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 77,566 hrs · 13,205 cycles

AT TAKEOFF, ENGINE 1 OR 2 COMPRESSOR STALL, YAW TO LEFT, SEVERAL LOUD BANGS. #1 ENG ACCELERATED MORE QUICKLY THAN OTHERS. ABORTED TAKEOFF WITH NO LIMITS EXCEEDED. INSPECTED BOTH ENGINE 1 AND 2 FOR DEFECTS. NO DEFECTS FOUND FOR ENGINE 2. FOUND METAL AND DEBRIS IN TAIL PIPE FOR ENGINE 1. REF WO 52350, REMOVED AND REPLACED ENGINE IAW AMM 71-00-02/401. ALL OPS AND LEAK CHECK NORMAL.

Part: WEB — CRACKED (BS 280-286) · airframe 77,516 hrs · 13,197 cycles

COCKPIT-RH (PEDAL) I/B PNL FOUND CRACKED.(<P>COCKPIT-RH (PEDAL) PILOT FWD PANEL SUPPORT WEB CRACK AREA REPAIRED IAW RI-53-00-13578 REV A.<BR /></P>)

Part: SKIN — CORRODED (BS 1003) · airframe 77,516 hrs · 13,197 cycles

M/D STA 1003 STR 12R-13R SKIN INNER SURFACE FOUND CORROSION.(<P>CABIN&NBSP;<SPAN>STA 1003 STR 12R-13R SKIN INNER SURFACE CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED&NBSP; IAW SRM 51-20-01 AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</SPAN></P>)

Part: SKIN — CORRODED (BS 1003) · airframe 77,516 hrs · 13,197 cycles

M/D STA 1003 STR 10L-11L SKIN INNER SURFACE FOUND CORROSION.(<P>CABIN STA 1003 STR 10L-11L SKIN INNER SURFACE CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01 AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.<BR /></P>)

Part: SKIN — CORRODED (BS 1238) · airframe 77,516 hrs · 13,197 cycles

M/D STA 1238 STR 9L-10L SKIN INNER SURFACE FOUND CORROSION.&NBSP;(<P>CABIN&NBSP;<SPAN>STA 1238 STR 9L-10L SKIN INNER SURFACE CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01, AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.&NBSP;</SPAN></P>)

Part: WEB — CRACKED (BS 280-286) · airframe 77,516 hrs · 13,197 cycles

COCKPIT-LH (PEDAL) I/B PNL FOUND CRACKED.(<P>COCKPIT-LH (PEDAL) PILOT FORWARD PANEL SUPPORT WEB CRACK AREA REPAIRED IAW RI-53-00-13578 REV A. <BR /></P>)

Part: SKIN — CORRODED (BS 1483) · airframe 77,516 hrs · 13,197 cycles

M/D STA 1483 STR 18L-19L SKIN INNER SURFACE FOUND CORROSION.(<P>CABIN STA 1483 STR 18L-19L SKIN INNER SURFACE CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01, AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.&NBSP;</P>)

Part: SKIN — CORRODED (BS 1238) · airframe 77,516 hrs · 13,197 cycles

M/D STA 1238 STR 10L-11L SKIN INNER SURFACE FOUND CORROSION.(<P>CABIN&NBSP;<SPAN>STA 1238 STR 10L-11L SKIN INNER SURFACE</SPAN><SPAN>&NBSP;CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED&NBSP; IAW SRM 51-20-01, AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</SPAN></P>)

Part: SKIN — CORRODED (BS 1238) · airframe 77,516 hrs · 13,197 cycles

M/D STA 1238 STR 10R-11R SKIN INNER SURFACE FOUND CORROSION.(<P>CABIN&NBSP;<SPAN>STA 1238 STR 10R-11R SKIN INNER SURFACE CORROSION AREAS SMOOTHED IAW 51-10-02 AND REPROTECTED IAW SRM 51-20-01, AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.&NBSP;</SPAN></P>)

Part: SKIN — CORRODED (BS 1003) · airframe 77,516 hrs · 13,197 cycles

M/D STA 1003 STR 9R-10R SKIN INNER SURFACE FOUND CORROSION(<P>CABIN STA 1003 STR 9R-10R SKIN INNER SURFACE CORROSION AREAS SMOOTHED IAW 51-10-02 AND REPROTECTED IAW 51-20-01 AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.<BR /></P>)

Part: SKIN — CORRODED (BS 1244) · airframe 77,516 hrs · 13,197 cycles

M/D STA 1244 STR 2R-3R SKIN INNER SURFACE FOUND CORROSION.(<P>CABIN&NBSP;<SPAN>STA 1244 STR 2R-3R SKIN INNER SURFACE<STRONG>&NBSP;</STRONG>CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01, AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</SPAN></P>)

Part: TENSION TIE — CRACKED (BS 720) · airframe 77,516 hrs · 13,197 cycles

FOUND CRACK ON UPPER DECK TENSION TIE AREA, FWD CHANNEL, LH BS720 STR L12-L16.(<P>REPAIRED TENSION TIE FWD CHANNEL IAW SRM 53-20-30-2R-2 REPAIR 2.</P>)

Part: BOTTLE — NONE (DOOR SLIDE) · airframe 77,515 hrs · 13,197 cycles

REPLACE U/D RH DOOR SLIDE BOTTLE DUE TO SLIDE DEPLOYMENT TEST. REMOVED AND REPLACED SLIDE BOTTLE IAW AMM 25-68-04.

Part: SEAT TRACK — CORRODED (BS 1451-1462) · airframe 77,516 hrs · 13,197 cycles

M/D RH STA 1451-1462 RBL 11.33" SEAT TRACK FOUND CORROSION.&NBSP;(<P>CABIN-<SPAN>STA 1451-1462 RBL 11.33" SEAT TRACK</SPAN><SPAN>&NBSP;CORROSION AREAS REMOVED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01, AND CHECKED WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.&NBSP;</SPAN></P>)

Part: TENSION TIE — CRACKED (BS 720) · airframe 77,516 hrs · 13,197 cycles

FOUND CRACK ON UPPER DECK TENSION TIE AREA FWD CHANNEL, RH BS720 STR R12 TO R16.&NBSP;(<P>REPAIRED TENSION TIE FWD CHANNEL IAW SRM 53-20-30-2R-2 REPAIR 2.</P>)

Part: SKIN — CORRODED (BS 1244) · airframe 77,516 hrs · 13,197 cycles

M/D STA 1244 STR 0-1R SKIN INNER SURFACE FOUND CORROSION.(<P>CABIN&NBSP;<SPAN>STA 1244 STR 0-1R SKIN INNER SURFACE CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED SRM 51-20-01, AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.&NBSP;</SPAN></P>)

Part: SEAT TRACK — CORRODED (BS 1591-1601) · airframe 77,516 hrs · 13,197 cycles

M/D LH STA 1591-1601 LBL 11.33" SEAT TRACK FOUND CORROSION.(<P>CABIN-STA 1591-1601 LBL 11.33"&NBSP; SEAT TRACK CORROSION AREAS REMOVED IAW SRM 51-10-02 AND RE-PROTECTED IAW SRM 51-20-01. CHECKED WITHIN LIMIT IAW SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101.&NBSP;</P>)

Part: SKIN — CORRODED (BS 1003) · airframe 77,516 hrs · 13,197 cycles

M/D STA 1003 STR 14R-15R SKIN INNER SURFACE FOUND CORROSION.(<P>CABIN STA 1003 STR 14R-15R SKIN INNER SURFACE CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01 AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.<BR /></P>)

Part: SKIN — CORRODED (BS 1003) · airframe 77,516 hrs · 13,197 cycles

M/D STA 1003 STR 7R-8R SKIN INNER SURFACE FOUND CORROSION.(<P>CABIN STA 1003 STR 7R-8R SKIN INNER SURFACE CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01 AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.<BR /></P>)

Part: SEAT TRACK — CORRODED (BS 1820) · airframe 77,516 hrs · 13,197 cycles

M/D LH STA 1820 LBL76" SEAT TRACK FOUND CORROSION.(<P>CABIN-<SPAN>STA 1820 LBL76" SEAT TRACK</SPAN><SPAN>&NBSP;CORROSION AREAS REMOVED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01 AND CHECKED WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.&NBSP;</SPAN></P>)

Part: SKIN — CORRODED (BS 1238) · airframe 77,516 hrs · 13,197 cycles

M/D STA 1238 STR 8R-9R SKIN INNER SURFACE FOUND CORROSION.(<P>CABIN STA&NBSP;<SPAN>1238 STR 8R-9R SKIN INNER SURFACE</SPAN><SPAN>&NBSP;CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01, AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.&NBSP;</SPAN></P>)

Part: SKIN — CORRODED (BS 1003) · airframe 77,516 hrs · 13,197 cycles

M/D STA 1003 STR 9L-10L SKIN INNER SURFACE FOUND CORROSION.(<P>CABIN STA 1003 STR 9L-10L SKIN INNER SURFACE CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01 AND CHECKED WITH SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.<BR /></P>)

Part: SEAT TRACK — CORRODED (BS 1312-1316) · airframe 77,516 hrs · 13,197 cycles

M/D LH STA 1312-1316 LBL 11.33" SEAT TRACK FOUND CORROSION.&NBSP;(<P>CABIN-STA&NBSP;1312-1316 LBL 11.33" SEAT TRACK&NBSP;CORROSION AREAS REMOVED IAW SRM 51-10-02 AND RE-PROTECTED IAW SRM 51-20-01. CHECKED WITHIN LIMIT IAW SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101.&NBSP;</P>)

Part: SKIN — CORRODED (BS 1483) · airframe 77,516 hrs · 13,197 cycles

M/D STA 1483 STR 17L-18L SKIN INNER SURFACE FOUND CORROSION.&NBSP;(<P>CABIN&NBSP;<SPAN>STA 1483 STR 17L-18L SKIN INNER SURFACE CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01, AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.&NBSP;</SPAN></P>)

Part: SEAT TRACK — CORRODED (BS 1880-1920) · airframe 77,516 hrs · 13,197 cycles

M/D LH STA 1880-1920 LBL76" SEAT TRACK FOUND CORROSION.(<P>CABIN-<SPAN>STA 1880-1920 LBL76" SEAT TRACK</SPAN><SPAN>&NBSP;CORROSION AREAS REMOVED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01 AND CHECKED WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</SPAN></P>)

Part: SEAT TRACK — CORRODED (BS 1570-1581) · airframe 77,516 hrs · 13,197 cycles

M/D LH STA 1570-1581 LBL 11.33" SEAT TRACK FOUND CORROSION.(<P>CABIN-STA 1570-1581 LBL 11.33" SEAT TRACK&NBSP;CORROSION AREAS REMOVED IAW SRM 51-10-02 AND RE-PROTECTED IAW SRM 51-20-01. CHECKED WITHIN LIMIT IAW SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101.&NBSP;</P>)

Part: SEAT TRACK — CORRODED (BS 1270-1282) · airframe 77,516 hrs · 13,197 cycles

M/D LH STA 1270-1282 LBL 11.33" SEAT TRACK FOUND CORROSION.(<P>CABIN-STA 1270-1282 LBL 11.33" SEAT TRACK CORROSION AREAS REMOVED IAW SRM 51-10-02 AND RE-PROTECTED IAW SRM 51-20-01. CHECKED WITHIN LIMIT IAW SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101.&NBSP;</P>)

Part: SKIN — CORRODED (BS 1238) · airframe 77,516 hrs · 13,197 cycles

M/D STA 1238 STR 8L-9L SKIN INNER SURFACE FOUND CORROSION.(<P>CABIN&NBSP;<SPAN>STA 1238 STR 8L-9L SKIN INNER SURFACE CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01, AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.&NBSP;</SPAN></P>)

Part: SKIN — CORRODED (BS 1003) · airframe 77,516 hrs · 13,197 cycles

M/D STA 1003 STR 12L-13L SKIN INNER SURFACE FOUND CORROSION(<P>CABIN STA 1003 STR 12L-13L SKIN INNER SURFACE CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01 AND CHECKED WITH SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.<BR /></P>)

Part: BOTTLE — NONE (DOOR SLIDE) · airframe 77,516 hrs · 13,197 cycles

REPLACE RH FLOOR MOUNTED SLIDE DUE TO DEPLOYMENT TEST. REMOVED AND REPLACED FLOOR MOUNTED SLIDE ASSY IAW AMM 25-68-02.

Part: SEAT TRACK — CORRODED (BS 1471-1479) · airframe 77,516 hrs · 13,197 cycles

M/D RH STA 1471-1479 RBL 11.33" SEAT TRACK FOUND CORROSION.(<P>CABIN-STA 1471-1479 RBL 11.33" SEAT TRACK CORROSION AREAS REMOVED IAW SRM 51-10--02 AND RE-PROTECTED IAW SRM 51-20-01. CHECKED WITHIN LIMIT IAW SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101.&NBSP;</P>)

Part: SKIN — CORRODED (BS 1483) · airframe 77,516 hrs · 13,197 cycles

M/D STA 1483 STR 13L-14L SKIN INNER SURFACE FOUND CORROSION.(<P>CABIN&NBSP;<SPAN>STA 1483 STR 13L-14L SKIN INNER SURFACE CORROSION AREAS SMOOTHED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01, AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</SPAN></P>)

Part: RECORDER — NO TEST (FLT DECK) · airframe 69,972 hrs · 11,791 cycles

DFDR ULB TEST FAILED. REPLACED DFDR AND VERIFIED THE NEW DFDR WITH A NEW ULB.

Part: SKIN — CRACKED (BS 2598) · airframe 69,972 hrs · 11,791 cycles

CRACKS ON THE SKIN PANEL, STRINGER 25R AND STRINGER 26R NEAR BS 2598. ACCOMPLISHED EI T2017A53M-1315, REV 2.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 69,972 hrs · 11,791 cycles

FOUND THE EMERGENCY LIGHT POWER SUPPLY BATTERY ASSY FUNCTION BAD IAW AMM 33-51-04-002-009-001 & 33-51-04-402-012-00, REV 89. REPLACED THE POWER SUPPLY AND CHECKED NORMAL IAW AMM 33-51-04-402-012-001, REV 89, STEP D. PERFORMED EMERGENCY POWER SUPPLY TEST AND THE RESULT WAS SATISFACTORY.

Part: FLOORBEAM — CORRODED (BS 2280) · corrosion level 2 · airframe 69,972 hrs · 11,791 cycles

FOUND THE MAIN DECK FLOORBEAM CORRODED AT BS 2280 NEAR THE NR 5 PASSENGER DOOR. REPAIRED THE AREA IAW EI T2017A53M-1222, REV 1.

Part: SUPPORT FITTING — CRACKED (SPOILERS) · airframe 68,872 hrs · 11,791 cycles

CRACK ON THE NR 7 SPOILER SUPPORT FITTING OTBD LOWER FORWARD FLANGE. REPAIRED THE DAMAGED AREA IAW SRM 57-51-13-2R-1, REV 79, AND EI T2017A57M-1316, REV 1. CHECKED NORMAL.

Part: SEAT TRACK — CORRODED (BS 2102) · corrosion level 2 · airframe 69,972 hrs · 11,791 cycles

CORROSION ON THE MAIN DECK SEAT TRACK NEAR BS 2102, LBL 98.58. ACCOMPLISH EI T2017A53M-1244, REV 1. INSTALLED A FASTENER IAW DWG 65B 38-51, SH 62, REV A, SH 63, 64 AND 65 REV.

Part: FLOORBEAM — CORRODED (BS 1500) · corrosion level 2 · airframe 69,972 hrs · 11,791 cycles

FOUND THE MAIN DECK FLOORBEAM CORRODED AT BS 1500, RBL 11.33. REPAIR THE AREA IAW EI T2017A53M-1218, REV 1.

Part: CARGO TRACK — CRACKED (BS 1860-1886) · airframe 69,972 hrs · 11,791 cycles

FOUND AFT CARGO TRACK CRACKED AT BS 1860 - 1886, RBL 45.5. REPAIRED THE AREA IAW SRM 53-00-52-2R-10, REPAIR 10, REV 79, AND DWG 65B06061, SHEET 22, REV D.

Part: RECORDER — MALFUNCTIONED (FLT DECK) · airframe 69,972 hrs · 11,791 cycles

UNABLE TO DOWNLOAD DFDR DATA WITH A HAND HELD DOWNLOADER. REPLACED DFDR AND FOUND ULB EXPIRED DATE TO SHORT IAW AMM 31-31-01-002-001 & 31-31-01-404-004, REV 89. REPLACED ULB AND CONDITION CHECKED NORMAL IAW AMM 31-31-09-002-001 & 31-31-09-402-015, REV 89. PERFORMED ULB OPS TEST AND THE RESULTS WAS SATISFACTORY IAW AMM 31-31-09-702-020, REV 89.PERFORMED GND TEST PER DFDR AND RESULTS SATISFACTORY IAW AMM 31-31-00-745-090, REV 89 .

Part: FLOORBEAM — CORRODED (BS 2240) · airframe 69,972 hrs · 11,791 cycles

FOUND THE MAIN DECK FLOORBEAM CORRODED AT BS 2240, LBL 67. CORROSION REMOVED IAW SRM 51-10-02, REV 79. MEASURED REWORKED AREA ORIGINAL THICKNESS AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 53-00-51-1A-1, FIG 101, DETAIL II, REV 79. REPAIRED IAW SRM 51-20-01, REV 79.

Part: ACTUATOR — FAILED (MLG) · airframe 69,972 hrs · 11,791 cycles

FOUND THE RT BLG ALTERNATE MOTOR FAILED. REPLACED THE ACTUATOR IAW AMM 32-35-01-004-001, REV 89, AND AMM 32-35-01-404-007, REV 89. TESTED NORMAL. CONDITION CHECKED NORMAL.

Part: CARGO TRACK — DAMAGED · airframe 69,972 hrs · 11,791 cycles

FWD CARGO BAY, CARGO TRACK BS 980, RBL 76 DAMAGED. REPAIR THE CARGO TRACK IAW SRM 53-00-52-2R-13, REPAIR 13, REV 79.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 69,972 hrs · 11,791 cycles

CORROSION ON LT WING SKIN. REMOVED CORROSION AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-10-10-1A-2, FIG 101, DETAIL V, REV 79.

Part: SEAT TRACK — CRACKED (BS 1485) · airframe 69,972 hrs · 11,791 cycles

SEAT TRACK BROKEN AT BS 1485, RBL 75.92. REPAIRED THE SEAT TRACK IAW 53-00-52-2R-13, REPAIR 13, REV 79.

Part: FLOORBEAM — CORRODED (BS 2240) · corrosion level 2 · airframe 69,972 hrs · 11,791 cycles

FOUND THE MAIN DECK FLOORBEAM CORRODED AT BS 2240, RBL 67.01. REPAIRED DAMAGED AREA IAW EI T2017A53M-1230, REV 1. CHECKED NORMAL.

Part: FIRE DETECTOR — MALFUNCTIONED (MLG WW) · airframe 69,972 hrs · 11,791 cycles

FOUND WARNING MESSAGE FOR WHEEL WELL FIRE. REPLACED THE W/W FIRE DETECTOR AND CONDITION CHECKED NORMAL IAW AMM-26-17-02-004-001 & 26-17-02-404-012, REV 89. PERFORMED OPERATIONAL TEST OF W/W OVERHEAT DETECTION AND THE RESULTS WAS SATISFACTORY IAW AMM 26-17-00-705-001 REV 89 .

Part: STRUCTURE — DAMAGED (HORIZONTAL STAB) · airframe 69,391 hrs · 11,682 cycles

ON WALK AROUND CHECK, FOUND RT HORIZONTAL STAB TIP AFT FAIRING DAMAGED & MISSING. REPAIRED IAW EO4455A127 PART 3.

Part: OIL SYSTEM — LOW (NR 1 ENGINE) · airframe 64,457 hrs · 10,711 cycles

LOW OIL QUANTITY IN CRUISE. GOT DOWN TO 2 QTS INDICATED. INSPECTED NR 1 ENGINE IAW AMM 72-00-00 AND FOUND LEAKAGE FROM B-SUMP SCAVANGE DRAIN TUBE. R & R NR 1 ENGINE IAW BOOTSTRAP METHOD IAW W/C E2023.

Part: STRUCTURE — CRACKED (LT WING) · airframe 62,380 hrs · 10,381 cycles

LT WING ILES 698 L/E CAVITY NOSE BEAM UPPER CHORD FOUND CRACK, LT WING ILES 693-5 TO ILES 726 L/E CAVITY NOSE BEAM UPPER CHORD IS REPAIRED IAW SRM 57-41-13-2R -2R, REPAIR 2.

Part: STRUCTURE — CRACKED (BS 1000) · airframe 62,380 hrs · 10,381 cycles

BS 1000, LOWER CHORD AT STR 38 AREA FOUND CORROSION CRACK AT CHORD DETAIL REFER ATTACHED FIG, CRACKED HOLE OVERSIZED TO 0.625 AND CRACK FREE. A FREEZE PLUG FABRICATED IAW SRM 51-20-07 AND INSTALLED IAW EO NUMBER.

Part: BRACKET — BROKEN (FIRE DETECTOR) · airframe 62,380 hrs · 10,381 cycles

APU FIRE DETECTOR ASSY BRACKET FOUND BROKE AT APU COMPARTMENT DOOR, REPAIRED APU FIRE DETECTOR ASSY BRACKET IAW EO 4426A069, REV 0.

Part: FLOOR SUPPORT — CRACKED (BS 1200) · airframe 62,380 hrs · 10,381 cycles

M/D BS 1200, RBL 110 FLOOR INTERCOSTAL WEB FOUND CRACK, REPAIRED M/D STA 1200, RBL 110, FLOOR INTERCOSTAL WEB & NBSP; IAW SRM & NBSP; 53-40-51-2R -9, REPAIR 9.

Part: PANEL — CHAFED (BS 1780-1840) · airframe 62,380 hrs · 10,381 cycles

MAIN DECK CARGO CASTER PANEL TOP SURFACE FOUND CHAFE MARK AT RS 780-1840, LBL-33-35, M/D CARGO CASTER PANEL TOP SURFACE IS REPAIRED IAW EO 4425A438.

Part: SKIN — CRACKED (BS 939-991) · airframe 62,380 hrs · 10,381 cycles

FUSELAGE SKIN CRACK FOUND UNDERNEATH RT SIDE LOWER DRAG SPLCE FITTING AT & NBSP; AT BS 980 CRACK APPROX .2500" RUNNING AT 7 O`CLOCK POSITION, FUSELAGE SKIN REPAIRED IAW SRM 53-20-01-2R-2, REPAIR 2 AT BS 991-5 BETWEEN STR 37R-39R AREA.

Part: TENSION TIE — CRACKED (BS 760) · airframe 62,380 hrs · 10,381 cycles

RT BS 760 TENSION TIE INSPECTION AREA FOUND 1 EA FASTENER HOLE CRACK REVEALED AT AFT CHANNEL. RT & NBSP; BS760 TENSION TIE IS REPAIRED IAW SRM 5320-30-TR-1, REPAIR 1. THIS REPAIR IS CLASSIFIED AS A CATEGORY B REPAIR. SUPPLEMENTAL INSPECTION IS REQUIRED IAW SRM 53-20-30-TR-1, REPAIR 1, TABLE 203.

Part: SUPPORT — CHAFED (BS 2484) · airframe 62,380 hrs · 10,381 cycles

STAB COMPT BS 2484 PITOT AND HYDR TUBING SUPPORT LWR FOUND CHAFING. REPAIRED EMP-STAB COMPT STA 2484 PITOT AND HYDR TUBING SUPPORT LWR FLANGE ARE & NBSP; IAW HX RI NO RI-53-80-10915, REV A.

Part: FRAME — CRACKED (BS 980) · airframe 62,380 hrs · 10,381 cycles

FWD CARGO, BS 980, STR 37R-38R FRAME LWR FLANGE CRACK FOUND. REPAIRED FWD CARGO STA 980 RT BETWEEN STR 37R-38R FRAME LWR FLANGE IAW RI NO R153-22-10899, REV A.

Part: PANEL — BROKEN (BS 1860-1920) · airframe 62,380 hrs · 10,381 cycles

M/D CASTER PANEL FOUND BROKE AT BS1860-1920, RBL 11-33, REPAIRED M/D CASTER PANEL AT BS1860-1920 RBL 11-33 IAW EO 4425A437, REV O.

Part: STIFFENER — CRACKED (BS 2658 BULKHEAD) · airframe 62,380 hrs · 10,381 cycles

TAIL COMPT BS 2658 AFT B/H FWD SIDE NR 1 STIFFENER AT LBL 28 FOUND CRACKED, COUNT FROM LWR, TAIL COMPT BS 2658 AFT BULKHEAD FWD SIDE NR 1 STIFFENER AT LBL 28 REPAIRED IAW HX R1-53-83 -10914, REV B.

Part: TIRE — SEPARATED (MLG) · airframe 61,499 hrs · 10,234 cycles

ON WALK AROUND FOUND NR 12 TIRE WITH TREAD SEPARATION. R & R NR 12 WHEEL ASSY IAW AMM 32-45-01. SPIN AND PRESSURE CHECKED GOOD. ALSO, ACCOMPLISHED TREAD LOSS CONDITIONAL INSPECTION IAW AMM 05-51-34-202-001. FOUND DAMAGE TO BODY FAIRING PANEL 194BR AND 194CR, SEPARATE SDR.

Part: ELT — MALFUNCTIONED (UPPER DECK) · airframe 59,476 hrs · 9,870 cycles

RIGHT VHF HAD IRREGULAR SOUND. FOUND UPPER DECK EMERGENCY LOCATION TRASNMITTER TRANSMITTING. R & R UPPER DECK EMERGENCY LOCATION TRANSMITTER IAW AMM 25-65-03-422-052.

Part: COMPUTER — FAILED (FMC) · airframe 57,093 hrs · 9,448 cycles

DUAL FMC FAIL. COMPLIED WITH QRH. R &R LEFT FLIGHT MANAGEMENT COMPUTER IAW AMM 34-61-01. SOFTWARE INSTALLED IAW AMM 34-61-00. PERFORMED GROUND TEST IAW AMM 34-61-00 AND TEST PASSED.

Part: ANGLE — CRACKED (HORIZ STAB) · airframe 54,181 hrs · 8,918 cycles

EMP -RIGHT &NBSP; HORI STAB T/E CAVITY ELEV STA 406.8 WEB ANGLE FOUND CRACK P/N 65B03779-54 ( EMP-RIGHT &NBSP; HORI STAB T/E CAVITY ELEV STA 406.8 CRACKED ANGLE P/N 65B03779-54 FABRICATED AND REPLACED IAW RI NO: RI-55-10-10177 REV A.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 54,181 hrs · 8,918 cycles

FUSELAGE-SECTION 48-FUSELAGE SKIN-BS 2560 BELOW STRINGER 42R-TAIL JACK PAD AREA DENT DAMAGE. CUT OUT REPAIR TAIL JACK PAD AREA FUSELAGE SKIN BS 2560 BELOW STRINGER 42R AS PER SRM &NBSP; 53-80-01 REPAIR 2&NBSP; FIGURE 202 AND RS NO: RI-53-81-10164 REV A.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 54,181 hrs · 8,918 cycles

MAIN DECK- BS 1800-1820 LBL 110 FLOOR SUPPORT BEAM FOUND CRACKED P/N= 65B17951-17. MAIN DECK- BS 1800-1820 LBL 110 FLOOR SUPPORT BEAM FOUND CRACKED P/N= 65B17951-17 REPAIRED IAW RI NO: RI-53-25-10176 REV A.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 54,181 hrs · 8,918 cycles

MAIN DECK-SEAT TRACK CROWN FOUND WORN AT BS 1748-1800 RBL 11". MAIN DECK- BS 1748-1800 RBL 11" DAMAGED SEAT TRACK CROWN REPAIRED IAW RI NO: RI-53-65-10179 REV A. AND RI-53-65-10180 REV A.&NBSP.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 54,181 hrs · 8,918 cycles

MAIN DECK- SEAT TRACK CROWN FOUND WORN AT BS 1748-1800 RBL 11''. MAIN DECK BETWEEN&NBSP; BS 1766.45 TO BS 1810.45 RBL 11'' DAMAGED SEAT TRACK REPAIRED IAW RI NO: RI-53-65-10180 REV A AND RI-53-65-10179 REV A.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 54,181 hrs · 8,918 cycles

MAIN DECK- STA&NBSP;1900 2 LBL 98" TIE DOWN TRACK FOUND BROKEN. MAIN DECK BETWEEN BS 1890.45-1990.45 LBL 98" BROKEN SEAT TRACK REPAIRED IAW RI NO: RI 53-65-10181 REV A.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,181 hrs · 8,918 cycles

MAIN DECK BS&NBSP;1840 LBL 98" TIE DOWN TRACK FLANGE CRACKED. MAIN DECK&NBSP;BETWEEN BS&NBSP;1810.45-&NBSP; BS 1890.45- LBL 98" SEAT TRACK IS & NBSP; REPAIRED IAW RI NO: RI-53-65-10181 REV A.

Part: BRACKET — CRACKED (RT HORIZ STAB) · airframe 54,181 hrs · 8,918 cycles

EMP- RIGHT STABILIZER ELEV STA 426.8 SUPPORT RIB FWD ANGLE BRACKET FOUND CRACK AS MARKED. EMP- RIGHT STABILIZER ELEV STA 426.8 SUPPORT RIB FWD ANGLE WAS FABRICATED AND REPLACED&NBSP;IAW RI NO: RI-55-10-10177 REV A&NBSP.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,181 hrs · 8,918 cycles

MAIN DECK- BS 1770 LBL 11" TIE DOWN TRACK FOUND CRACKED. MAIN DECK AT BS 1766.45 TO BS 1810.45 DAMAGED SEAT TRACK REPAIRED IAW SRM 53-00-52 REPAIR 12 AND RI NO: RI-53-65-10178 REV A.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 54,182 hrs · 8,918 cycles

M/D - BS 1800-1820 LBL 105 - LBL 110 FLOOR SUPPORT BEAM FOUND CRACKED. MAIN DECK BS 1800-1820 LBL 110 FLOOR SUPPORT BEAM IS REPAIRED AS PER RI NO: R1-53-25-10176 REV A.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 54,182 hrs · 8,918 cycles

M/D - SEAT TRACK CROWN FOUND WORN AT BS 1748 RBL 11 TO BS 1800. MAIN DECK AT BETWEEN BS 1730 TO BS 1800 RBL 11 SEAT TRACK IS REPAIRED AS PER RI NO: RI-53-65-10179 REV A AND RI-53-65-10130 REV A.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 54,182 hrs · 8,918 cycles

M/D - BS 1840 LBL 98 TIE DOWN TRACK FLANGE CRACKED. MAIN DECK AT BETWEEN BS 1810 TO BS 1890 LBL 98 SEAT TRACK IS REPAIRED AS PER RI NO: RI-53-65-10181 REV A.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 54,182 hrs · 8,918 cycles

M/D - STA 1900 LBL 96 TIE DOWN TRACK FOUND BROKEN, MARKED. MAIN DECK AT BETWEEN BS 1890 TO BS 1900 LBL 98 SEAT TRACK IS REPLACED AS PER RI NO: RI-53-65-10181 REV A.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 53,793 hrs · 8,858 cycles

PACK 2 EICAS MSG AFTER ENGINE START. QRH COMPLETED. DDG REFER TO REQUIRING M ACTION. RETURNED TO BLOCKS. FOUND NO MSG IN CMC. PERFORMED CMC GROUND TEST. TEST PASS. PACK NR 2 OPERATIONAL TEST NORMAL IAW MM 21-52-00.

Part: COMPRESSOR — STALLED (NR 2 ENGINE) · airframe 748,719 hrs · 1,317 cycles

AT ROTATION, NR 2 ENGINE COMPRESSOR STALLED 4 OR 5 TIMES WITH A FLASH. REDUCED THRUST, ENGINE STABILIZED. CLIMBING THROUGH FL210, EGT NEAR REDLINE, REDUCED THRUST TO IDLE, THEN SHUT ENGINE DOWN TO AVOID OVERTEMP. FOUND LEVER ARM BROKEN, ENGINE REPLACEMENT REQUIRED.

Part: DOOR — DAMAGED (LT WLG) · airframe 52,368 hrs · 8,628 cycles

LEFT WING LANDING GEAR - SHOCK STRUT INBOARD DOOR FAIRING - LEADING EDGE DAMAGE. (REF FIGURE 1).&NBSP;DAMAGE FOUND TO BE BEYOND THE LIMITS OF SRM 52-80-02, FIGURE 101 ALLOWABLE DAMAGE 4 PER SRM 51-70-02, FIGURE 101 ALLOWABLE DAMAGE GENERAL. (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 OF EO 4452A162 AND FAA 8110-3 DATED 30OCT12. SCHEDULE REPEAT INSPECTIONS AT EVERY 5 FC (FLIGHT CYCLES) AND PERMANENT REPAIR PRIOR TO THE ACCUMULATION OF 1,000 FH (FLIGHT HOURS)&NBSP;PER SRM 51-70-17 OR SRM 51-70-07.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 52,213 hrs · 8,600 cycles

DURING WALKAROUND INSPECTION MX ANC FOUND DAMAGE TO THE UNPRESSURIZED AREA OF THE FUSELAGE SKIN AFT OF BS 2560 BELOW STRINGER 42R, CONSISTING OF A DENT MEASURING 0.37 INCH, LONG AND 0.0625 IN DEEP AND SCRATCH&NBSP; 1.25 INCH LONG AND 0.03125 INCH DEEP&NBSP.

Part: SKIN — DAMAGED (BS 1780) · airframe 50,940 hrs · 8,382 cycles

DURING WALKAROUND INSPECTION, DAMAGE FOUND TO BS 1780 SIDEWALL TRIM/GUTTER DEFORMED AND MOUNT FASTENERS MISSING. PERFORMED A TIME LIMITED REPAIR.

Part: PUMP — OVERHEATED (HYD SYSTEM) · airframe 49,955 hrs · 8,184 cycles

NR 1 HYDRAULIC SYSTEM OVERHEAT USING EDP, ADP TURNED ON, ALL FLUID EVENTUALLY LOST FROM NR 1. FOUND EDP TO BE OVERHEATED, INOPERATIVE AND LEAKING. REPLACED EDP AND CORRELATED FILTERS.

Part: NOZZLE — CRACKED (NR 3 ENGINE) · airframe 48,797 hrs · 7,972 cycles

THERE IS A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, BETWEEN THE 10&NBSP;AND 12 O'CLOCK POSITION (LT SIDE) OF THE NR 3 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROXIMATELY 15 INCHES LONG AND IS 13 INCHES FROM AFT SIDE OF EXHAUST SLEEVE JUST IN FRONT OF NAC STA 349.236. CRACK IS OUT OF LIMITS FOUND IN SRM 54-41-30. (A TIME LIMITED REPAIR WAS ACCOMPLISHED IAW&NBSP;EO 4478A205 FAA 8110-3 DATED 28DEC11, PART 1 WITH A&NBSP; DETAILED REPEAT INSPECTION DUE EVERY 3 FLIGHT CYCLES AS PER PART 2. PERMANENT REPAIR DUE PRIOR TO 50 FLIGHT CYCLES.)

Part: THRUST REVERSER — DAMAGED (NR 4 ENGINE) · airframe 46,020 hrs · 7,609 cycles

DURING WALK AROUND INSPECTION FOUND DAMAGE & NBSP; TO NR 4 ENGINE LT AND R&NBSP;/H THRUST REVERSER TRAILING EDGE AT 6 O`CLOCK POSITION. (PER EO 4478A174 PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS WITH A DVI EVERY 1000 FLIGHT HOURS AND A PERMANENT REPAIR AT NEXT C CK).

Part: RING — CRACKED (THRUST REVERSER) · airframe 45,968 hrs · 7,479 cycles

NUMBER 3 ENGINE, RIGHT THRUST REVERSER, FORWARD TORQUE BOX J-RING UPPER SIDE HAS A CRACK. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A78B-911.

Part: ACOUSTIC PANEL — DENTED (NR 4 PYLON) · airframe 45,968 hrs · 7,479 cycles

NUMBER 4 ENGINE NOSE COWL INLET & NBSP; HAS DENTS TO THE ACOUSTIC PANELS AT THE 3, 6 AND 11 O'CLOCK POSITIONS. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A54B-1137, SRM 54-15-01.

Part: ACCESS PANEL — DAMAGED (NR 3 PYLON) · airframe 45,968 hrs · 7,479 cycles

NUMBER 3 ENGINE STRUT FAIRING ACCESS PANEL 472ER HAS ELONGATED FASTENER HOLES. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A54B-1002.

Part: ACOUSTIC PANEL — DENTED (NR 2 PYLON) · airframe 45,968 hrs · 7,479 cycles

NUMBER 2 ENGINE NOSE COWL INLET&NBSP; HAS DENTS TO THE ACOUSTIC PANELS AT THE 3 AND 6 O'CLOCK POSITIONS. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A54B-1136 AND SRM 54-15-01.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 45,968 hrs · 7,479 cycles

MAIN DECK SEAT TRACK IS WORN BEYOND ACCEPTABLE LIMITS AT STATION 1520 RBL 11.33. ACCOMPLISHED PERMANENT REPAIR IAW EIT2011A53B-1107 REV 01.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 45,968 hrs · 7,479 cycles

MAIN DECK SEAT TRACK IS & NBSP; BROKEN & NBSP; FROM STATION 1660 TO 1680 RBL 98.58. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A53B-1108 REV 01.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 45,968 hrs · 7,479 cycles

LOWER SIDE OF AFT CARGO DOOR OUTER SKIN HAS CREASE & NBSP; FROM STATION 1815 TO STATION 1911. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A54B-1002.

Part: FUSE — BLOWN (CABIN) · airframe 45,968 hrs · 7,479 cycles

UPPER DECK EMERGENCY LIGHTING INOPERATIVE AT L1382; M4914; L5731; L5732; L5734 AND L5767. REPLACED 5 FUSES OF POWER SUPPLY IAW AMM 33-51-04-902-001.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 45,968 hrs · 7,479 cycles

FASTENER HOLE ON VERTICAL STABILIZER LEADING EDGE SKIN AT STATION 473 & NBSP; FOUND TO BE ELONGATED. PERMANENT REPAIR ACCOMPLISHED IAW EI T2011A55B-1158.

Part: ACCESS PANEL — DAMAGED (NR 1 NACELLE) · airframe 45,968 hrs · 7,479 cycles

NUMBER 1 ENGINE STRUT FAIRING ACCESS PANEL 452EL HAS FASTENER HOLE ELONGATED. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A54B-1025.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 45,968 hrs · 7,479 cycles

THE SUPPORT AND PANEL SKIN OF THE LEFT LOWER FUSELAGE LONGERON BOX STRUCTURE HAS A CRACK AT STATION 1372, S-35L. ACCOMPLISHED PERMANENT REPAIR IAW SRM 51-70-07-06-0.

Part: RIB — CRACKED (HORIZ STAB) · airframe 45,968 hrs · 7,479 cycles

LEFT HORIZONTAL STABILIZER UPPER AND LOWER SIDES OF THE TIP FAIRING PANEL AT YB428 HAS CRACK DAMAGE TO & NBSP;THE RIB. THE RIB WAS REPLACED AND ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A55B-1161.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 45,968 hrs · 7,479 cycles

THE SUPPORT FOR THE RIGHT LOWER FUSELAGE LONGERON BOX AT STATION 1372, S-35R HAS A CRACK. REWORKED AREA IAW SRM 53-40-05 DETAIL I OF FIG 101. APPLIED SURFACE PROTECTIVE COATING IAW SRM 51-20-01.

Part: RIB — CRACKED (HORIZ STAB) · airframe 45,968 hrs · 7,479 cycles

RIGHT HORIZONTAL STABILIZER LEADING EDGE FAIRING RIB AT STATION 501.103 HAS CRACK ON THE LOWER SIDE. PERMANENT REPAIR ACCOMPLISHED IAW EI T2011A55B-1059.

Part: RIB — CRACKED (HORIZ STAB) · airframe 45,968 hrs · 7,479 cycles

RIGHT HORIZONTAL STABILIZER LEADING EDGE RIB AT STATION 131.946 HAS A CRACK. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A55B-1059.

Part: PANEL — DAMAGED (NR 4 PYLON) · airframe 45,968 hrs · 7,479 cycles

WEAR DAMAGE FOUND ON FASTENER HOLE OF NUMBER 4 ENGINE STRUT FAIRING PANEL 482EL. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A54B-1001 DATED 22APRIL11.

Part: RIB — CRACKED (HORIZ STAB) · airframe 45,968 hrs · 7,479 cycles

LEFT HORIZONTAL STABILIZER LEADING EDGE RIB AT STATION 501.559 HAS A CRACK. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A55B-1059.

Part: RIB — CRACKED (HORIZ STAB) · airframe 45,968 hrs · 7,479 cycles

LEFT HORIZONTAL STABILIZER LEADING EDGE RIB AT STATION 159.109 HAS A CRACK. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A55B-1059.

Part: ACCESS PANEL — DAMAGED (NR 1 PYLON) · airframe 45,968 hrs · 7,479 cycles

CHAFING DAMAGE ON NR 1 ENGINE NACELLE STRUT, INBOARD AFT SIDE OF ACCESS PLATE 452FR. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A54B-958.

Part: BLOWOUT DOOR — WORN (THRUST REVERSER) · airframe 45,968 hrs · 7,479 cycles

NR 3 ENGINE, RIGHT THRUST REVERSER FORWARD AND AFT EDGES OF BLOW OUT DOOR SHOWS WEAR. PERMANENT REPAIR ACCOMPLISHED IAW T2011A78B-1028.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 45,968 hrs · 7,479 cycles

THE EDGE OF THE FUSELAGE SKIN AT STATION 2598, S-42R IS DAMAGED. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A53B-1054.

Part: RIB — CRACKED (HORIZ STAB) · airframe 45,968 hrs · 7,479 cycles

LEFT HORIZONTAL STABILIZER LEADING EDGE RIB AT STATION 527.190 HAS CRACK. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A55B-1059.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 45,968 hrs · 7,479 cycles

BOTTOM OF AFT CARGO DOOR, OUTER SKIN AT STATION 1770 HAS A CRACK. ACCOMPLISHED PERMAMENT REPAIR IAW SRM 52-30-01, REPAIR 2, DETAIL IV, FIGURE 201, SHEET 9.

Part: PANEL — DAMAGED (MAIN DECK) · airframe 45,968 hrs · 7,479 cycles

DADO PANEL AT STATION 1720 OF THE LEFT SIDE OF THE MAIN DECK IS DAMAGED. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A25B-1053.

Part: RIB — CRACKED (HORIZ STAB) · airframe 45,968 hrs · 7,479 cycles

LEFT HORIZONTAL STABILIZER LEADING EDGE RIB AT STATION 441.753 HAS A CRACK. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A55B-1059.

Part: RIB — CRACKED (HORIZ STAB) · airframe 45,968 hrs · 7,479 cycles

RIGHT HORIZONTAL STABILIZER LEADING EDGE RIB AT STATION 159.109 HAS A CRACK. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A55B-1059.

Part: RIB — CRACKED (HORIZ STAB) · airframe 45,968 hrs · 7,479 cycles

LEFT HORIZONTAL STABILIZER LEADING EDGE RIB AT STATION 145.011 HAS A CRACK. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A55B-1059.

Part: FRAME — CRACKED (LT COWLING) · airframe 45,968 hrs · 7,479 cycles

CRACK FOUND ON THE AFT HAT FRAME OF NR 2 ENGINE, LEFT CORE COWL. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A71B-990.

Part: RIB — CRACKED (HORIZ STAB) · airframe 45,968 hrs · 7,479 cycles

LEFT HORIZONTAL STABILIZER LEADING EDGE RIB AT STATION 151.543 HAS A CRACK. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A55B-1059.

Part: DOOR FRAME — CRACKED (NR 1 PYLON) · airframe 45,968 hrs · 7,479 cycles

CRACK ON NR 1 PYLON, RIGHT SIDE, FWD PRESSURE RELIEF DOOR FRAME OF AFT FAIRING. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A54B-1110.

Part: SKIN — ACTIVATED (CARGO DOOR) · airframe 45,968 hrs · 7,479 cycles

FORWARD CARGO DOOR OUTER SKIN AT THE LOWER AFT SIDE HAS CREASE AT STATION 667.5 TO STATION 678. ACCOMPLISHED PERMANENT REPAIR IAW SRM 52-30-01, DETAIL III, REV 59.

Part: RIB — CRACKED (HORIZ STAB) · airframe 45,968 hrs · 7,479 cycles

LEFT HORIZONTAL STABILIZER LEADING EDGE RIB AT STATION 467.384 HAS A CRACK. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A55B-1059.

Part: BLOWOUT DOOR — WORN (THRUST REVERSER) · airframe 45,968 hrs · 7,479 cycles

NR 2 ENGINE RIGHT THRUST REVERSER FORWARD AND AFT EDGES OF BLOW OUT DOOR SHOWS WEAR. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A78B-1028.

Part: RIB — CRACKED (HORIZ STAB) · airframe 45,968 hrs · 7,479 cycles

LEFT HORIZONTAL STABILIZER LEADING EDGE RIB AT STATION 475.928 HAS A CRACK. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A55B-1059.

Part: RIB — CRACKED (FUSELAGE) · airframe 45,968 hrs · 7,479 cycles

LEFT HORIZONTAL STABILIZER LEADING EDGE RIB AT STATION 510.103 HAS A CRACK. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A55B-1059.

Part: RIB — CRACKED (HORIZ STAB) · airframe 45,968 hrs · 7,479 cycles

RIGHT HORIZONTAL STABILIZER LEADING EDGE FAIRING RIB AT STATION 501.559 IS CRACKED ON THE LOWER SIDE. PERMANENT REPAIR ACCOMPLISHED IAW EI T2011A55B-1059.

Part: RIB — CRACKED (HORIZ STAB) · airframe 445,968 hrs · 7,479 cycles

LEFT HORIZONTAL STABILIZER LEADING RIB AT STATION 407.579 HAS A CRACK. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A55B-1059.

Part: BLOWOUT DOOR — WORN (THRUST REVERSER) · airframe 45,968 hrs · 7,479 cycles

NR 1 ENGINE, RIGHT THRUST REVERSER FORWARD AND AFT EDGES OF BLOW OUT DOOR SHOWS SIGNS OF WEAR. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A78B-1026.

Part: RIB — CRACKED (HORIZ STAB) · airframe 45,968 hrs · 7,479 cycles

LEFT HORIZONTAL STABILIZER LEADING EDGE RIB AT STATION 450.297 HAS A CRACK. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A55B-1059.

Part: SKIN — DENTED (FUSELAGE) · airframe 45,968 hrs · 7,479 cycles

FUSELAGE SKIN AT BS 2601.5 BETWEEN S-46R AND S-49R HAS A DENT. ACCOMPLISHED PERMANENT REPAIR IAW SRM 53-00-01, REPAIR 15, DETAIL I, REV 59.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 45,968 hrs · 7,479 cycles

CRACK ON MAIN DECK SEAT TRACK AT STATION 995 RBL 75.92, .8 INCH LONG. PERMANENT REPAIR ACCOMPLISHED IAW 747-400F SRM 53-00-52, REPAIR 13, REV 59.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 45,968 hrs · 7,479 cycles

CRACK ON MAIN DECK SEAT TRACK AT STATION 995 LBL 75.92 ABOUT.8 INCH LONG. PERMANENT REPAIR ACCOMPLISHED IAW 747-400F SRM 53-00-52, REPAIR 13, REV 59.

Part: COWLING — DAMAGED (RIGHT) · airframe 45,418 hrs · 7,391 cycles

DURING THE REPEAT DETAILED VISUAL INSPECTION OF PART 2 OF EO4471A069 IT WAS FOUND THAT THERE WAS ADDITIONAL DAMAGE FOUND TO THE RIGHT CORE COWL. A TIME LIMITED REPAIR WAS ACCOMPLISHED ACCORDING TO REVISION A OF THIS SAME EO &AMP; FAA 8110-3 DATED 28FEB11. REPEAT INSPECTIONS WERE REDUCED FROM 15 FLIGHT CYCLES TO 5 FLIGHT CYCLES. AN INTERIM REPAIR IS REQUIRED AT THE NEXT A CHECK AND A PERMANENT REPAIR IS REQUIRED AT THE NEXT D CHECK.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 45,158 hrs · 7,473 cycles

DURING LOADING OPERATIONS THERE WAS A NOTICEABLE ELECTRICAL SMELL IN COCKPIT. ACCOMPLISHED VISUAL INSPECTION OF ALL IDS, COCKPIT LIGHTING, FMS SYSTEM AND ALL CB PANELS. THERE WERE NO DEFECTS NOTED. EQUIPMENT COOLING TEST WAS ACCOMPLISHED PER AMM 51-58-00 AND TEST PASSED. IT IS SUSPECTED THAT THE ODOR CAME FROM THE PDUS WHILE THE AIRCRAFT WAS BEING LOADED. ALL PDUS OPERATED NORMALLY THROUGHOUT THE LOADING OPERATION.

Part: COWLING — DAMAGED (NR 4 ENGINE) · airframe 45,152 hrs · 7,349 cycles

NUMBER 4 ENGINE LOWER CORE COWL DAMAGED AT 6 O'CLOCK POSITION. TIME LIMITED REPAIR ACCOMPLISHED IAW PART 1 OF EO 4471A069, WITH 8110-3 DATED 07FEB2011. DVI EVERY 15 FLIGHT CYCLES WITH PERMANENT REPAIR DUE PRIOR TO 9000 FLIGHT HOURS AFTER PART 1 IS ACCOMPLISHED.

Part: THRUST REVERSER — DAMAGED (NR 4 ENGINE) · airframe 45,152 hrs · 7,349 cycles

NUMBER 4 ENGINE THRUST REVERSER TRAILING EDGE DAMAGED AT 6 O'CLOCK POSITION. (TIME LIMITED REPAIR ACCOMPLISHED IAW PART 1 OF EO 4478A160, WITH FAA 8110-3 DATED 01FEB2011. A DETAILED VISUAL INSPECTION IS REQUIRED EVERY 1000 FLIGHT HOURS AND A PERMANENT REPAIR TO BE ACCOMPLISHED PRIOR TO 9000 FLIGHT HOURS AFTER THE COMPLETION OF PART 1.

Part: COWLING — ERODED (NR 3 NACELLE) · airframe 43,380 hrs · 7,083 cycles

NR 3 ENGINE RT FAN COWL LEADING EDGE HAS ERROSION DAMAGE -FOUND ON WALKAROUND BY MAINTENANCE.A TIME LIMITED REPAIR WAS ACCOMPLISHED IAW PART 1 OF EO 4471AO64 AND FAA FORM 8110-3 DATED 22 SEPT.2010 WITH DVI EVERY 5 FLIGHT CYCLES AND A PERMENANT REPAIR PRIOR TO 1000 FLIGHT HOURS.

Part: SUPPORT — DAMAGED (FUSELAGE) · airframe 42,759 hrs · 6,982 cycles

BS 1920 MAIN DECK LEFT SIDEWALL SUPPORT STRUCTURE UPPER CORNER WAS FOUND DAMAGED. TIME LIMITED REPAIR WAS ACCOMPLISHED PER ENGINEERING ORDER 4425A173, WITH FAA 8110-3 DATED 30 JULY 2010. DVI REQUIRED EVERY FLIGHT CYCLE WITH PERMANENT REPAIR DUE PRIOR TO 1000 FLIGHT HOURS AFTER PART ONE IS DONE.

Part: STRUCTURE — DAMAGED (NR 4 NACELLE) · airframe 42,029 hrs · 6,876 cycles

NUMBER 4 ENGINE LT &AMP; RT CORE COWLS DAMAGED AT FORWARD EDGE AT 6 O'CLOCK POSITION. TIME LIMITED REPAIR PART ONE ACCOMPLISHED PER ENGINEERING ORDER 4471A057, WITH FAA 8110-3 DATED 08 JUN 2010. DVI EVERY 15 FLIGHT CYCLES AND PERMANENT REPAIR PRIOR TO 50 FLIGHT CYCLES AFTER PART ONE.

Part: COMPRESSOR — DAMAGED (NR 3 ENGINE) · airframe 41,584 hrs · 6,810 cycles

MEMO MESSAGE "VVVVVV" DISPLAYED AT 1515Z AT FL 360, ENGINE 3 N2 VIBRATION AT 5.0. ALL OTHER PARAMETERS WERE NORMAL AND MONITORED. AT APPROXIMATELY 12,000 FT, NR 3 ENGINE FAILED. QRH PROCEDURES ACCOMPLISHED. INSPECTION OF TAILPIPE REVEALED NO METAL. BOROSCOPE INSPECTION OF COMPRESSOR REVEALED DAMAGE TO FIRST STAGE BLADES. ENGINE REPLACEMENT REQUIRED.

Part: SKIN — CRACKED (RT COWLING) · airframe 41,321 hrs · 6,770 cycles

FOUND ON WALK AROUND A 3.5 INCH CRACK ON NR 2 ENGINE RIGHT CORE COWLING OUTER SKIN. TIME LIMITED REPAIR ACCOMPLISHED PER ENGINEERING ORDER 4471A052 WITH FAA 8110-3 DATED 16 APR 2010. DVI TO BE PERFORMED EVERY 3 FLIGHT CYCLES WITH PERMANENT REPAIR AT NEXT A-CHECK.

Part: SKIN — DAMAGED (COWLING) · airframe 41,338 hrs · 6,773 cycles

ON WALK AROUND FOUND DAMAGE TO NR 4 ENGINE RIGHT CORE COWLING OUTER SKIN AT FORWARD EDGE 6 O'CLOCK POSITION. TIME LIMITED REPAIR ACCOMPLISHED PER ENGINEERING ORDER 4471A054 WITH FAA 8110-3 DATED 18 APR 2010 TO TRIM DAMAGE AND APPLY SPEED TAPE. DVI TO BE PERFORMED EVERY 3 FLIGHT CYCLES WITH PERMANENT REPAIR AT NEXT A-CHECK.

Part: WINGLET — DAMAGED (LT WING) · airframe 40,826 hrs · 6,695 cycles

DURING PARKING OPERATION OF N452PA, THE LEFT WINGLET OF N450PA AND DAMAGED IT. THE LEFT WINGLET WAS REMOVED IAW CDL 57-28-1 AND AMM 57-28-01. NO FURTHER DAMAGED WAS NOTED.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 40,820 hrs · 6,694 cycles

MAIN DECK SEAT TRACK FROM BS 1518 THROUGH 1530 LBL 11.33 WAS FOUND DAMAGED. TIME LIMITED REPAIR ACCOMPLISHED PER PART 1 OF EO 4453A341 AND 8110-3 DATED 08MAR10. DVI REQUIRED EVERY 5 FLIGHT CYCLES WITH A PERMANENT REPAIR TO BE ACCOMPLISHED PRIOR TO THE 25TH CYCLE AFTER PART 1.

Part: DEPRESSOR — DAMAGED (CARGO DOOR) · airframe 39,390 hrs · 6,472 cycles

DURING WALK AROUND CHECK THE MAIN DECK, SIDE CARGO DOOR SEAL DEPRESSOR ON THE FORWARD SIDE APPROXIMATELY 1 INCH DOWN FROM TOP WAS FOUND TO BE DAMAGED. TIME LIMITED REPAIR ACCOMPLISHED IAW EO4453A306. FAA 8110-3 WAS ISSUED 10 NOV 09. VISUAL INSPECTION REQUIRED EVERY FLIGHT CYCLE WITH PERMANENT REPAIR TO BE ACCOMPLISHED AT NEXT- A CHECK.

Part: EXHAUST PIPE — CRACKED (NR 3 ENGINE) · airframe 6,180 hrs · 37,399 cycles

DURING WALK AROUND CHECK, A 12 INCH LONG CRACK WAS FOUND AT THE 12 O'CLOCK POSITION 13 INCHES FROM THE TRAILING EDGE OF THE NR 3 ENGINE EXHAUST NOZZLE. "AREA WAS INSPECTED IAW SRM 54-41-30 AND EO 4478A085 WAS ISSUED BY ENGINEERING WITH FAA 8110-3. THE AIRCRAFT DEPARTED WITH NO FURTHER ISSUES."

Part: EXHAUST PIPE — CRACKED (NR 2 ENGINE) · airframe 6,180 hrs · 37,399 cycles

DURING WALK AROUND CHECK, AN 8 INCH LONG CRACK WAS FOUND AT THE 12 O'CLOCK POSITION 13 INCHES FROM THE TRAILING EDGE OF THE NR 2 ENGINE EXHAUST NOZZLE. "AREA WAS INSPECTED IAW SRM 54-41-30 AND EO 4478A086 WAS ISSUED BY ENGINEERING WITH FAA 8110-3. THE AIRCRAFT DEPARTED WITH NO FURTHER ISSUES."

Part: SLEEVE — CRACKED (EXHAUST NOZZLE) · airframe 36,594 hrs · 6,065 cycles

2.5 IN CRACK FOUND ON NR 2 ENG EXHAUST NOZZLE OUTER SLEEVE AT THE TRAILING EDGE AT THE 10 O'CLOCK POSITION. "PER EO 4478A081, STOP DRILLED CRACK AND REPAIR WITHIN 10 FLIGHT CYCLES. FAA 8110-3 ISSUED 15 MAR 09".

Part: TRANSPONDER — MALFUNCTIONED · airframe 35,709 hrs · 5,933 cycles

DURING TAXI OUT CREW WAS UNABLE TO SELECT THE FIRST DIGIT ON TRANSPONDER. MAINTENANCE CONFIRMED THE OPERATION OF THE LEFT AND RIGHT TRANSPONDERS IAW AMM 34-53-00. THE AIRCRAFT DEPARTED WITH NO FURTHER ISSUES.

Part: ENGINE — SURGES (NR 3) · airframe 34,632 hrs · 5,767 cycles

NR 3 ENGINE SURGED ON TAKE OFF ROLL. TAKE OFF ABORTED AT 100 KTS. HIGH ENERGY STOP INSPECTION COMPLETED PER AMM 05-51-10. NO TROUBLE FOUND. ALSO NR 3 ENGINE CIT SENSOR WAS REPLACED AND TESTED OK. ACFT DEPARTED WITH NO FURTHER ISSUES.

Part: ENGINE — FAILED (NR 4) · airframe 33,299 hrs · 5,565 cycles

AT DESCENT, ENGINE NR 4 SHUT DOWN AND RESTARTED 6 TIMES. AFTER THE 6TH RESTART ENGINE SHUTDOWN AND LEFT OFF. AIRCRAFT LANDED SAFELY AND WITHOUT DECLARING EMERGENCY. FOUND NR 4 ENGINE OUT OF BOROSCOPE LIMITS PER AMM. REMOVED AND REPLACED NR 4 ENGINE. (A)

Part: NOZZLE — CRACKED (NR 3 ENGINE) · airframe 32,958 hrs · 5,503 cycles

ON WALK AROUND AFTER ARRIVAL FOUND A CRACK AT 2 O'CLOCK POSITION ON NR 3 ENGINE EXHAUST NOZZLE. PERFORMED INTERIM REPAIR IAW EO 4478A070 WITH DVI EVERY 3 FLIGHT CYCLES.

Part: PDU — MALFUNCTIONED (L/E SLAT) · airframe 32,920 hrs · 5,496 cycles

LEADING EDGE DRIVE, LEADING EDGE MULTI DRIVE STATUS MESSAGES RECEIVED. REPLACED NR 2 RT LEADING EDGE PDU PER MM 27-81-03. OPERATIONAL CHECK NORMAL.

Part: FAIRING — DENTED (WING TO BODY) · airframe 32,490 hrs · 5,434 cycles

LT WING TO BODY FAIRING PANEL 191KL SKIN DENTED EO NR 4453A160 ISSUED AND REQUIRES RE-INSPECTION EVERY 25 FLIGHT CYCLES.

Part: CABLE — DAMAGED · airframe 32,376 hrs · 5,420 cycles

LIGHTNING STRIKE WHILE SITTING ON THE GROUND IN ORD. ALL ELECTRICAL POWER LOST. COMPLETED CONDITIONAL INSPECTION ACCORDING TO MM 05-51-13. REPLACED THE 2 BCUS IAW AMM 24-23-01. ALSO, FOUND BOTH EXTERNAL POWER RECEPTACLE NEUTRAL POWER CABLES DAMAGED. REMOVED SAME CABLES AND DEFERRED EXTERNAL POWER ACCORDING TO MEL 24-41-1.

Part: CARGO TRACK — CRACKED (FUSELAGE) · airframe 32,044 hrs · 5,367 cycles

MAIN DECK CARGO TRACK HAS A CRACK AT BS 1800 LBL 98.5 MEASURING 10.0 INCHES. TIME LIMITED REPAIR WAS ACCOMPLISHED PER EO NR 4453A138 PART 1.

Part: TURBINE BLADES — CRACKED (HPT ROTOR) · airframe 28,578 hrs · 4,853 cycles

ESN 706199 - HPT STAGE 1 BLADES FOUND WITH UNDER PLATEFORM CORROSION AND CRACKS, STAGE 1 P/N 1538M90P12 (80EA).

Part: ENGINE — INOPERATIVE (NR 1) · airframe 28,179 hrs · 4,794 cycles

RETURN TO GATE, NR 1 ENGINE AUTO START EICAS MESSAGE NR 1 ENGINE FAILED TO START, IN AUTO OR MANUAL. UNSUCCESSFUL ENGINE START. PERFORMED VISUAL INSPECTION OF ALL LINES FOR LEAKS, ALL CHECKS NORMAL IAW MM 36-11-00. PERFORMED MANUAL START BY THE CREW. ENGINE STARTED NORMAL IAW MM 80-13-00.

Part: COUPLER — FAILED (HF SYSTEM) · airframe 27,161 hrs · 4,636 cycles

LEFT AND RIGHT HF TRANSMITTERS WENT INOPERATIVE. REPLACED LEFT AND RIGHT HF COUPLERS. OPERATIONAL CHECKS GOOD.

Part: PDU — FAILED (L/E SLAT) · airframe 24,391 hrs · 4,210 cycles

CREW REPORTED (MULTI LE DRIVE) STATUS MESSAGE DISPLAYED WHEN FLAPS RETRACTED. REPLACED NR 3 R/E DRIVE PDU, ALL OPS AND INDICATIONS NORMAL.

Part: BLADES — DAMAGED (NR 4 ENGINE) · airframe 24,172 hrs · 4,179 cycles

REPLACE NR 4 ENGINE DUE TO 7, 8, 9 STAGE BLADE DETERIORATION. REMOVED AND REPLACED NR 4 ENGINE IAW WORK CARDS ENG FUNCTION CHECK AND LEAK CHECK NORMAL.

Part: STATUS MESSAGE — ILLUMINATED (TE FLAPS) · airframe 23,627 hrs · 4,096 cycles

EICAS MESSAGE AFTER PUSHBACK FLAPS PRIMARY AND STATUS MESSAGE LEADING EDGE MULTI DRIVE. RESET FCU CIRCUIT BREAKER, CYCLE ALT MODE SELECT SWITCH. OPS TEST OK PER AMM 27-50-05.

Part: DRIVE UNIT — FAILED (TE FLAPS) · airframe 23,053 hrs · 4,011 cycles

LEFT INBOARD LEADING EDGE FLAPS FAILED TO RETRACT AFTER LANDING, FOLLOWED BY EICAS MESSAGES -FLAPS PRIMARY-, -FLAPS DRIVE- AND -L/E MULTI DRIVE. REPLACED LEFT NR 4 LEADING EDGE PDU; OPS CHECK NORMAL.

Part: MANIFOLD — DEFECTIVE (NR 1 ENGINE) · airframe 23,037 hrs · 4,009 cycles

ON INITIAL CLIMB, AFTER FLAP RETRACTION, EICAS CAUTION MESSAGE OVHT ENG 1 NAC. COMPLIED WITH CHECKLIST AND MESSAGE CLEARED, TRIED TO CONTINUE WITH CLIMB, MESSAGE RETURNED. RETURN TO LAX. REMOVE AND REPLACE NR 1 ENGINE TWELVE SEGMENT LPT COOLING AIR MANIFOLD IAW AMM 75-24-03. SYSTEM OPS CHECK GOOD.

Part: MANIFOLD — FAULTY (NR 1 ENGINE) · airframe 23,037 hrs · 4,009 cycles

ON INITIAL CLIMB, AFTER FLAP RETRACTION, EICAS CAUTION MESSAGE OVHT ENG 1 NAC. COMPLIED WITH CHECKLIST AND MESSAGE CLEARED, TRIED TO CONTINUE WITH CLIMB, MESSAGE RETURNED. RETURN TO LAX. REMOVE AND REPLACE NR 1 ENGINE TWELVE SEGMENT LPT COOLING AIR MANIFOLD IAW AMM 75-24-03. SYSTEM OPS CHECK GOOD.

Part: SHAFT — SHEARED (STARTER) · airframe 22,526 hrs · 3,937 cycles

ENGINE NR 3 STARTER FAILED. REMOVED AND REPLACED NR 3 ENGINE STARTER AND START VALVE PER MM 80-11-01 AND 80-11-02. STARTER SHAFT SHEARED.

Part: BLEED VALVE — DEACTIVATED (NR 3 ENGINE) · airframe 21,880 hrs · 3,833 cycles

RETURNED TO BLOCKS WITH -BLEED PRV ENGINE 3- MESSAGE. NR 3 ENG PRV BLEED VALVE DEACTIVATED PER MEL 36-11-86. ALSO REQUIRED TO LOCK OUT NR 3 REVERSER PER THE MEL.

Part: ODOR — DETECTED (COCKPIT) · airframe 20,367 hrs · 3,604 cycles

ON PREFLIGHT, NOTED ODOR IN COCKPIT. PERFORMED VISUAL INSPECTION IN E/E COMPARTMENT AND COCKPIT PER MM 45-00-00. NO DEFECTS NOTED.

Part: BALL JOINT — CORRODED (T/R GEARBOX) · airframe 20,208 hrs · 3,575 cycles

LOWER RT THRUST REVERSER ANGLE GEARBOX FOUND BALL SCREW CORRODES. REPLACED ANGLE GEAR BOX PER MM 78-31-22.

Part: BALL SCREW — CORRODED (T/R GEARBOX) · airframe 20,208 hrs · 3,575 cycles

UPPER RT T/R ANGLE GEAR BOX FOUND BALL SCREW CORRODED. REPLACED ANGLE GEAR BOX PER MM 78-31-22.

Part: BALL SCREW — LACK OF LUBE (T/R GEARBOX) · airframe 20,208 hrs · 3,575 cycles

LOWER LT T/R ANGLE GEAR BOX FOUND BALL SCREW AT SHOP VISIT FOR LUBRICATION. REPLACED T/R ANGLE GEAR BOX, MM 78-31-22.

Part: SKIN — DENTED (BS 1980-2000) · airframe 20,208 hrs · 3,575 cycles

BULK CARGO DOOR B/T STA 1980-2000 RT CLOSE TO LOWER CUT OUT DENT WAS FOUND 2.28 X 1.46 X 0.075 INCHES. WORK ACCOMPLISHED PER ENGINEERING DISPOSITION RFTA-4177-001. DENT STRAIGHTENED, NO CRACK FOUND.

Part: EXHAUST VALVE — FAILED (E/E COOLING) · airframe 19,891 hrs · 3,521 cycles

EICAS MSG "EQUIP COOLING" AFTER ENGINE START. PERFORMED QRH PROCEDURE "EQUP COOLING" MSG REMAINED DISPLAYED. RETURNED TO GATE. CHECKED COUND CMC MSG 21404 E/E COOLING GROUND EXHAUST VALVE FAILED PART REPLACED IAW MM 21-58-12

Part: CONTROLLER — MALFUNCTIONED (NR 2 ENGINE) · airframe 18,805 hrs · 3,337 cycles

AFTER PUSHBACK AND ENGINE START EICAS MESSAGE BLEED 2 OVERHEAT/PRV APPEARED. RETURNED TO GATE. REPLACED NR 2 ENGINE PRV CONTROLLER PER MM 36-11-20. OPS CHECK OK ON RUN UP PER MM 36-11-00.

Part: LINE — CRACKED (HYD SYSTEM) · airframe 17,732 hrs · 3,167 cycles

LOSS OF NR 3 HYDRAULIC FLUID. TROUBLESHOT AND FOUND NR 3 EDP PRESSURE LINE UNDER THE GAP PANEL CRACKED. REPLACED LINE WITH FLEX LINE PER GMM 3-17-1, COI 450-017. OPS & LEAK CHECK OK PER 20-11-18.

Part: SMOKE — DETECTED (COCKPIT) · airframe 15,465 hrs · 2,763 cycles

THIRTY MINUTES PRIOR TO DEPARTURE, SMELLED SMOKE IN COCKPIT. NO MESSAGE DISPLAYED. INSPECTED LT MEC & REMOVED PANELS 516, 614, 414. NIL EVIDENCE OF ANY BURNING OR SMOKE FOUND, NO C/BS POPPED.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 15,253 hrs · 2,726 cycles

EICAS STATUS MESSAGE; HYDRAULIC PRESSURE 4. TRANSFERED TO DMI NR 32889 IAW MEL NR 29-11-0.

Part: NOZZLE — DENTED (ENGINE EXHAUST) · airframe 14,140 hrs · 2,533 cycles

NR 1 ENGINE EXHAUST NOZZLE HAS A DENT AT 7 O`CLOCK 5.125 LONG .5 INCH WIDE AND .001 INCH DEEP, BEYOND .80 LIMIT. REMOVED AND REPLACED EXHAUST NOZZLE.

Part: WARNING LIGHT — FALSE ACTIVATION (COCKPIT) · airframe 12,513 hrs · 2,247 cycles

EICAS BLEED NR 4 OVERHEAT / PVT MESSAGE DISPLAYED AFTER START. TRANSFERRED ITEM TO DMI 32027 PER DDG MEL 36-11-8B THRUST REVERSER TRANSFERRED TO DMI 32028 PER DDG MEL 78-31-01.

Part: WARNING LIGHT — ILLUMINATED (NR 4 ENGINE) · airframe 12,513 hrs · 2,247 cycles

NR 4 ENG FUEL VALVE MESSAGE. TRANSFERRED TO DMI 32018 AND MEL 73-31-02 PER DDPG.

Part: WARNING LIGHT — ILLUMINATED (NR 4 ENGINE) · airframe 12,213 hrs · 2,196 cycles

NR 4 ENG START BLEED 4 OVERHEAT / PRV MESSAGE STATUS MESSAGE BLEED PRV4. TRANSFERRED TO DMI 31879, MEL 36-11-86 CAT C. ALSO NR 4 REVERSER DEACTIVATED PER MEL REQUIREMENTS.

Part: ENGINE — BIRD INGESTION (NR 4) · airframe 12,207 hrs · 2,193 cycles

NR 4 ENGINE DAMAGE DUE TO BIRDSTRIKE. REMOVED AND REPLACED NR 4 ENGINE AND THE NAI DUCT ON NOSE COWL.

Part: VALVE — INACTIVE (NR 3 ENGINE) · airframe 11,611 hrs · 2,085 cycles

AT PUSHBACK, NR 3 ENGINE DID NOT START. NO FUEL FLOW. REF DMI 31578. REACTIVATED NR 3 ENG FUEL VALVE. EICAS MESSAGE GROUND. NR 3 ENG STARTS, GROUND STARTS NORMAL, IAWMM 71-00-00. DMI CLEARED, PLACARDS REMOVED.

Part: INDICATOR — INOPERATIVE (OIL PRESSURE) · airframe 10,791 hrs · 1,927 cycles

NR 4 ENG OIL PRESSURE INDICATION FAILED AFTER ENG START. RE-PINNED BRKN AND WIRE AT DT679 PIN A. ALSO REMOVED AND REPLACED INOP OIL TRANSMITTER.

Part: START VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 10,538 hrs · 1,878 cycles

ENG NR 2 WOULD NOT START EICAS MESSAGE -ENG NR 2 START VLV-. DEFERRED NR 2 ENG PER DDG START VLV REQUIRED MANUAL START.

Part: PEDAL — DISPLACED (RUDDER) · airframe 9,262 hrs · 1,639 cycles

WITH RUDDER SURFACES NEUTRAL RUDDER PEDALS WERE DISPLACED 1-8 UNITS (RIGHT). OPERATIONAL CHECKED PER AMM 27-21-00. OPS CHECK NORMAL. SUSPECT LARGE LATERAL IMBALANCE AS INDICATED ON W/B FORMS.

Part: RUDDER — MALFUNCTIONED (VERT. STAB) · airframe 8,591 hrs · 1,513 cycles

RUDDER TRAVEL NOT GOING TO LIMITS ON R/H INDICATOR DURING CONTROL CHECK. INSPECTED FWD & AFT RUDDER QUADRANT ASSYS, CABLE SYS., TRIM, CENTERING & FEEL MECHANISM PER MM 27-21-06, 27-21-08 & 27-21-11. ALL OK. PULLED A/C INTO HANGAR. AFTER 30 MIN. SYSTEM OPS CHECKED NORMAL PER MM 27-21-00. SUSPECT POSSIBILITY OF ICE IN AFT QUADRANT AREA DUE TO MOISTURE.

Part: WARNING LIGHT — ILLUMINATED (BLEED OVERHEAT) · airframe 12,577 hrs · 2,260 cycles

BLEED OVERHEAT / PRU EICAS MESSAGE NNC 2.3. GROUND TESTED PER MM 36-11-00 TEST PASSED. NO MESSAGE FOUND ON EICAS WHEN RETURNED TO BLOCKS.

Part: SMOKE DETECTOR — CONTAMINATED (MAIN DECK) · airframe 4,878 hrs · 842 cycles

CENTER FIRE SENSORS ON MAIN DECK INDICATED FIRE 9 HRS INTO FLT. VISUAL INSPECTION REVEALED NO FIRE. CB'S PULLED TO SILENCE ALARM FOR DURATION OF FLT & PERFORMED PERIODIC VISUAL FIRE INSPECTION. CLEANED & DRIED MAIN DECK SMOKE DETECTOR. (DETECTOR CONTAMINATED DUE TO HORSE CHARTER). PERFORMED FIRE SENSOR BITE TEST. ALL PASSED. OK FOR CONTINUED SERVICE.

Part: NOZZLE — CRACKED (#3 ENG EXHAUST) · airframe 4,363 hrs · 754 cycles

#3 ENGINE EXHAUST NOZZLE OUTER SKIN IS CRACKED ON THE RIGHT SIDE TOP. REMOVED & REPLACED EXHAUST NOZZLE AS PER 78-11-01.