N271UP

Part: ACCESS PANEL — GOUGED (VERTICAL STAB) · airframe 68,219 hrs · 19,655 cycles

RIGHT SIDE LOWER VERTICAL STAB AFT ACCESS PANEL DAMAGEDREPAIRED DAMAGED AREA IAW EO MD11-5530-84606-C

Part: NONE — NONE (FUSELAGE) · airframe 67,799 hrs · 19,441 cycles

INSPECTION TYPE:NA** SDR FILED OPEN**EMERG BATT 1 LO MESSAGE ON EICAS DURING PREFLIGHT CHECK. DEFERRED IAW MEL 33-50-4 DMP 33-50-4 ACCOMPLISHED. REF # M784711 PLACARD APPLIED

Part: SUPPORT BRACKET — CRACKED (LT NR 2 SLAT) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:CL/H I/B WING #2 SLAT TRACK SLOT DOOR AFT SUPPORT BRACKET IS CRACKEDREMOVED FABBED AND INSTALLED SUPPORT BRACKET IAW SRM 51-31-01 DWG ARB1602 AND SRM 51-35-01

Part: STIFFENER — CHAFED (NR 1 NACELLE) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:C#1 PYLON FAIRING ATTACH T ANGLE DEEPLY CHAFED AFT OF PRECOOLERREMOVED , FABBED, AND INSTALLED STIFFNER IAW SRM 51-31-01 DWG AUB7564 AND SRM 51-31-01

Part: WEB — CRACKED (BS 595) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:CR/H AC BAY HAS A CRACKED WEB AT L-34 AT FS 595REMOVED FABBED AND INSTALLED NEW WEB IAW SRM 51-31-01, DRAWING # ACA3804 AND SRM 51-35-01

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CR/H I/B FLAP LOWER SKIN HAS A CRACK XIFH= 134.REPAIRED CRACKED R/H I/B FLAP LOWER SKIN BETWEEN STA. XIFH=133.9 TO 147.3 AND BETWEEN STA. YIFH= 34 TO 78 IAW SRM 57-50-01 REPAIR 1 FIG. 201. (MAJOR)

Part: MOUNT — CORRODED (RT ELEVATOR) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:C2RH O/B HOR STAB #6 HINGE FITTING O/B LUG BUSHING HAS CORROSION.REPAIRED CORRODED HINGE FITTING O/B LUG IAW VT-SAA EA 011-5523-01-A9154 REV I/R AND UPS EO MD11-5520-80624-A (MINOR).

Part: FLOOR PANEL — CORRODED (FWD CABIN) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CFWD CABIN FLOOR PANEL BETWEEN STA 475 - 500.175 AND BETWEEN RBL 62.1 - RBL 73.3 IS CORRODED.REPAIRED FWD CABIN FLOOR PANEL BETWEEN STA 475 - 500.175 AND BETWEEN RBL 62.1 - RBL 73.3 IAW VT-SAA EA 011-5310-01-A9155 REV IR AND UPS EO MD11-5320-80560-A. (MINOR)

Part: FLOOR PANEL — CORRODED (FWD CABIN) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CFWD CABIN FLOOR PANEL BETWEEN STA 475 - 500.175 AND RBL 47.5 - RBL 62.1 IS CORRODED.REPAIRED CORRODED FWD CABIN FLOOR PANEL BETWEEN STA 475 - 500.175 AND RBL 47.5 - RBL 62.1 IAW VT-SAA EA 011-5310-01-A9162 REV. IR AND UPS EO MD11-5320-80651-A. (MINOR)

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CRCB FLOOR PANEL BETWEEN STA. 475-500.175 & BETWEEN X= -73.3 AND X= -107.250 HAS CORROSION.REPAIRED CORRODED FLOOR PANEL IAW VT-SAA EA 011-5320-01-A9167 REV. I/R AND UPS EO MD11-5320-80613-A. (MINOR)

Part: MOUNT — CORRODED (RT ELEVATOR) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:C2RH I/B ELEVATOR #3 BEARING MOUNT FITTING O/B BUSHING HAS CORROSION.REPAIRED CORRODED MOUNT FITTING IAW VT-SAA EA 011-5523-01-A9153 REV I/R AND UPS EO MD11-5520-80625-A (MINOR).

Part: FLOORBEAM — CORRODED (FWD CABIN) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CFWD CABIN FLOOR SUPPORT AT STA 421.578 BETWEEN RBL 65 & RBL 81 IS CORRODED.REMOVED AND REPLACED CORRODED FWD CABIN FLOOR SUPPORT AT STA 421.578 BETWEEN RBL 65 & RBL 81 IAW SRM 51-31-01. (MINOR)

Part: SKIN — GOUGED (LT WING LE) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:C2LH WING L/E SKIN IS GOUGE O/B OF #1 PYLON.REMOVED,FABRICATED AND REPLACED LT L/E SKIN IAW SRM 51-35-01 (MINOR).

Part: SUPPORT — DAMAGED (FWD CARGO) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CFWD. CARGO CEILING SUPPORT HAS DAMAGED FASTENER HOLES BETWEEN STA. 909 TO 1009 AT X= -14.REPAIRED DAMAGED CEILING SUPPORT BETWEEN STA 909 TO 1009 AT X= -14 IAW VT-SAA EA 011 5320-01-A9158 REV. I/R AND UPS EO MD11-5320-80668-A. (MAJOR) REF 8100-9 SIGNED BY S. KANG (AR-605677) DATED 6/12/21.

Part: SEAT TRACK — CRACKED (BS 635) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CFWD. CARGO CEILING AREA SEAT TRACK IS CRACKED AT STA. 635 AND X= -27.5.REPAIRED CRACKED SEAT TRACK BETWEEN STA. 625.0 TO 645.0 AND X= -27.5 IAW SRM 53-00-52 REPAIR 1 FIG. 201. (MAJOR)

Part: STRINGER SPLICE — CRACKED (CENTER CARGO) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CCENTER CARGO LONGERON 44R SPLICE FITTING IS CRACKED AT STA. 5-123.REMOVED, FABRICATED AND REPLACED SPLICE FITTING IAW DWG. A5A7116 AND SRM 51-33-01. (MINOR)

Part: STRINGER — CRACKED (RT WING LE) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CR/H WING FIXED L/E UPPER STRINGER IS CRACKED AT STA. XOS. 667.679.REPAIRED CRACKED R/H WING FIXED L/E UPPER STINGER AT STA. XOS. 667.679 IAW SRM 57-40-03 REPAIR 2 FIG. 202. (MAJOR)

Part: LONGERON SPLICE — CRACKED (CENTER CARGO) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CCENTER CARGO LONGERON 38R SPLICE FITTING AT STA 5-123 IS CRACKED.REMOVED AND REPLACED CRACKED CENTER CARGO LONGERON 38R SPLICE FITTING AT STA 5-123 IAW SRM 51-33-01. (MINOR)

Part: SKIN — GOUGED (RT WING) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:C2RT WING ACCESS PANEL 616ET GOUGE AT UPPER FWD SURFACE.REMOVED,FABRICATED AND REPLACED GOUGED PANEL(SKIN) IAW SRM 51-35-01 AND 51-31-01 (MINOR).

Part: SPAR CAP — CORRODED (RT WING) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CRT WING REAR SPAR UPPER CAP BELOW #3 SPOILER HAS CORROSION.REPAIRED CORRODED RT WING REAR SPAR UPPER CAP AT STA XORS 653.100 IAW VT-SAA EA 011-5700-01-A9140 REV. IR AND UPS EO MD11-5710-80599-A. (MINOR)

Part: SKIN — CORRODED (LT WING) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CLT WING UPPER SKIN BETWEEN XORS 181 - XORS 185 AT STRINGER 16 IS CORRODED.REPAIRED CORRODED LT WING UPPER SKIN BETWEEN XORS 181 - XORS 185 AT STRINGER 16 IAW VT-SAA EA 011-5730-01-A9147 REV. IR AND UPS EO MD11-5730-80654-A. REF. FAA FORM 8100-9 SIGNED BY P. LAU DATED 6/08/21 (MAJOR)

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CR/H WING I/B FLAP CENTER BOX UPPER SKIN IS CRACKED AT STA.XIFH=147.3.REPAIRED CRACKED R/H WING UPPER SKIN AT STA. XIFH= 147.3 AND BETWEEN YIF= 26 TO YIFH= 28 IAW SRM 57-00-01 REPAIR 1 FIG. 201. (MAJOR)

Part: SKIN — CORRODED (LT WING) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CLT WING UPPER SKIN BETWEEN XORS 286.5 - XORS 297 & BETWEEN STRINGER 17 AND FWD SPAR HAS 5 EA AREAS OF CORROSION.REPAIRED CORRODED LT WING UPPER SKIN BETWEEN XORS 286.5 - XORS 297 7 BETWEEN STRINGER 17 AND FWD SPAR 5 EA AREAS IAW VT-SAA EA 011-5730-01-A9143 REV. IR AND UPS EO MD11-5730-80559-A. (MINOR)

Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CL/H I/B FLAP VANE I/B LOWER SURFACE IS DELAMINATEDREPAIRED DELAMINATED L/H I/B FLAP VANE LOWER SURFACE IAW SRM 57-50-80 REPAIR 2 FIG. 201 & SRM 51-62-01 GENERAL. (MAJOR)

Part: SPAR CAP — CORRODED (LT WING) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CLT WING UPPER REAR SPAR CAP AFT FLANGE BETWEEN XORS 561.5 - XORS 576.5 IS CORRODED.REPAIRED CORRODED LT WING UPPER REAR SPAR CAP AFT FLANGE BETWEEN XORS 561.5 - XORS 576.5 IAW VT-SAA EA 011-5710-01-A9159 REV. IR AND UPS EO MD11-5710-80646-A. (MINOR)

Part: SUPPORT ANGLE — CORRODED (RT WING) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:C2RH O/B WING LOWER SUPPORT ANGLE HAS CORROSION AT LWR T/E.REMOVED,FABRICATED AND REPLACED CORRODED SUPPORT ANGLE IAW SRM 51-35-01 AND 51-31-01 (MINOR).

Part: SPAR CAP — CORRODED (RT WING) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CR/H WING REAR SPAR CAP UPPER FLANGE HAS CORROSION BETWEEN STA. XORS. 1042.35 TO 1054.REPAIRED CORRODED R/H WING REAR SPAR CAP UPPER FLANGE BETWEEN STA. XORS. 1042.35 TO 1054 IAW VT-SAA EA 011-5710-01-A9137 REV. I/R AND UPS EO MD11-5710-80666-A. (MAJOR) REF 8100-9 BY S. KANG DATED 06/10/21.

Part: CAP — CORRODED (RT WING) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CR/H WING LOWER CAP HAS CORROSION AT STA. XW= 320.REPAIRED CORRODED R/H WING LOWER CAP BETWEEN STA. XW= 275.230 & XW= 326.730 IAW SRM 57-50-02 REPAIR 9 FIG. 201. (MAJOR)..

Part: DOUBLER — CRACKED (RT WING) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS.667.62 TO 673.76.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 667.62 TO 673.76 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CR/H WING FIXED L/E SPLICE DOUBLER IS CRACKED AT STA. XOS. 667.REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG. ARB3954 AND SRM 51-33-01. (MINOR)

Part: FLOOR PANEL — CORRODED (FWD CABIN) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CFWD CABIN FLOOR PANEL BETWEEN STA 475 - 500 AND BETWEEN LBL 74 - LBL 107 IS CORRODED.REMOVED AND REPLACED CORRODED FWD CABIN FLOOR PANEL BETWEEN STA 475 - 500 AND BETWEEN LBL 74 - LBL 107 IAW SRM 51-31-01 & 51-35-01. (MINOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 661.7 TO 667.62.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 661.7 TO 667.2 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CMAIN CABIN FLOOR PANEL BETWEEN STA. 475.0 & 500.0 AND BETWEEN X= 27.5 TO X= 36.0 HAS CORROSION.REPAIRED FLOOR PANEL IAW VT-SAA EA 011-5320-01-A9164 REV. I/R AND UPS EO MD11-5320-80632-A. (MINOR)

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CRCB FLOOR PANEL HAS CORROSION BETWEEN STA. 475.0 TO 500.0 AND BETWEEN X= -27.5 TO X= -36.0.REPAIRED FLOOR PANEL IAW VT-SAA EA 011-5320-01-A9161 REV. I/R AND UPS EO MD11-5320-80627-A. (MINOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 589.88 TO 594.88.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 589.88 TO 594.88 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: FLOOR PANEL — CORRODED (FWD CABIN) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CFWD CABIN FLOOR PANEL BETWEEN STA 475 - 503 & BETWEEN LBL 19 - LBL 27.5 IS CORRODED.REMOVED AND REPLACED CORRODED FWD CABIN FLOOR PANEL BETWEEN STA 475 - 503 & BETWEEN LBL 19 - LBL 27.5 IAW SRM 51-31-01. (MINOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 692 TO 703.5.REPAIRED CRACKED R/H WING FIXED L/E BEADED DPOUBLER BETWEEN STA. XOS. 692 TO 703.5 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CL/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 661 TO 667.REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 661 TO 667 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CL/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 633 TO 636.REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 633 TO 636 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: SKIN — GOUGED (LT WING LE) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CL/H WING FIXED L/E SKIN IS GOUGED BETWEEN STA. XOS= 1031.669 TO 1044.27.REPAIRED GOUGED L/H WING FIXED L/E SKIN BETWEEN STA. XOS.= 1031.669 TO 1044.27 IAW VT-SAA EA 011-5730-01-A9139 REV. I/R AND UPS EO MD11-5750-80664-A. (MAJOR) REF 8100-9 BY S. KANG (AR-605667) DATED 6/10/21.

Part: SKIN — GOUGED (LT WING) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CL/H WING LOWER L/E SKIN HAS GOUGES BETWEEN STA. XW= 332 TO 344 & YW= 273 TO 280.REPAIRED GOUGED L/H WING LOWER L/E SKIN BETWEEN STA. XW= 332 TO 344 & YW= 273 TO 280 IAW SRM 57-40-01 REPAIR 12 FIG. 201. (MAJOR)

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CRCB FLOOR PANEL BETWEEN STA. 475 AND 500 AND BETWEEN X=0 TO X= 8.5 HAS CORROSION.REPAIRED FLOOR PANEL IAW VT-SAA EA 011-5320-01-A9160 REV. I/R AND UPS EO MD11-5320-80626-A. (MINOR)

Part: SEAT TRACK — CORRODED (FWD CABIN) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CFWD CABIN SEAT TRACK BETWEEN STA 480 - 488 AT LBL 27.5 IS CORRODED.REMOVED AND REPLACED CORRODED FWD CABIN SEAT TRACK BETWEEN STA 421.578 - 625 AT LBL 27.5 IAW SRM 51-31-01 & 51-33-01. (MINOR)

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CRCB FLOOR PANEL BETWEEN STA. 475.0 TO 500.175 AND BETWEEN X= 62.190 AND 73.340 HAS CORROSION.REPAIRED FLOOR PANEL IAW VT-SAA EA 011-5310-01-A9156 REV. I/R AND UPS EO MD11-5320-80633-A. (MINOR)

Part: FORMER — CRACKED (RT WING) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CR/H WING FIXED L/E SPLICE/FORMER IS CRACKED AT STA. XOS. 639.REMOVED, FABRICATED AND REPLACED SPLICE/FORMER IAW DWG. ARB2931 AND SRM 51-33-01. (MINOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 636 TO 643.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 636 TO 643 IAW SRM 57-40-01 REPAIR 15 FIG. 205. (MAJOR)

Part: SPACER — CORRODED (CENTER CARGO) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CLOWER CENTER CARGO BALL RETAINER (WSP1063-3) & SPACER (WSP1062-1) ARE CORRODED.REMOVED, FABRICATED AND REPLACED RETAINER AND SPACER IAW VT-SAA EA 011-5300-01-A9142 REV. I/R AND UPS EO MD11-2550-80661-A. (MINOR)

Part: RETAINER — CORRODED (CENTER CARGO) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CLOWER CENTER CARGO BALL RETAINER (WSP1062-1) & SPACER (WSP1063-3) ARE CORRODEDREMOVED, FABRICATED AND REPLACED RETAINER AND SPACER IAW VT-SAA EA 011-5300-01-A9142 REV. I/R AND UPS EO MD11-2550-80661-A. (MINOR)

Part: RETAINER — CORRODED (CENTER CARGO) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CLOWER CENTER CARGO L/H O/B BALL RETAINER AND SPACER ARE CORRODED.REMOVED, FABRICATED AND REPLACED RETAINER AND SPACER IAW VT-SAA EA 011-5300-01-A9142 REV. I/R AND UPS EO MD11-2550-80661-A. (MINOR)

Part: RETAINER — CORRODED (CENTER CARGO) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CLOWER CENTER CARGO BALL RETAINER (WSP1062-1) & SPACER (WSP1063-3) ARE CORRODED.REMOVED, FABRICATED SPACER AND REPLACED RETAINER AND SPACER IAW VT-SAA EA 011-5300-01-A9142 REV. I/R AND UPS EO MD11-2550-80661-A. (MINOR)

Part: SPACER — CORRODED (CENTER CARGO) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CLOWER CENETR CARGO BALL RETAINER SPACER IS CORRODED.REMOVED, FABRICATED AND REPLACED SPACER IAW VT-SAA EA 011-5300-01-A9142 REV. I/R AND UPS EO MD11-2550-80661-A. (MINOR)

Part: RETAINER — CORRODED (CENTER CARGO) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CLOWER CENYTER CARGO BALL RETAINER (WSP1062-1) & SPACER (WSP1063-3) ARE CORRODED.REMOVED, FABRICATED SPACER AND REPLACED BOTH RETAINER AND SPACER IAW VT-SAA EA 011-5300-01-A9142 REV. I/R AND UPS EO MD11-2550-80661-A. (MINOR)

Part: SPACER — CORRODED (CENTER CARGO) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CLOWER CENTER CARGO BALL RETAINER (WSP1062-1) & SPACER (WSP1063-3) ARE CORRODED.REMOVED, FABRICATED AND REPLACED RETAINER AND SPACER IAW VT-SAA EA 011-5300-01-A9142 REV. I/.R AND UPS EO MD11-2550-80661-A. (MINOR)

Part: RETAINER — CORRODED (CENTER CARGO) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CLOWER CENTER CARGO BALL RETAINER (WSP1062-1) AND SPACER (WSP1063-3) ARE CORRODED.REMOVED, FABRICATED SPACER AND REPLACED BOTH RETAINER AND SPACER IAW VT-SAA EA 011-5300-01-A9142 REV. I/R AND UPS EO MD11-2550-80661-A. (MINOR)

Part: RETAINER — CORRODED (CENTER CARGO) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CLOWER CENTER CARGO BALL RETAINER (WSP1062-1) & SPACER (WSP1063-3) ARE CORRODED.REMOVED, FABRICATED SPACER AND REPLACED RETAINER AND SPACER IAW VT-SAA EA 011-5300-01-A9142 REV. I/R AND UPS EO MD11-2550-80661-A. (MINOR)

Part: SKIN — CRACKED (RT MLG DOOR) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:C2RH MLG DOOR INNER SKIN CRACK 40''FROM FWD END AND 15'' FROM TOP.REPAIRED CRACK MLG DOOR SKIN IAW SRM 52-00-00 FIG 204 (MINOR).

Part: SPACER — CORRODED (CENTER CARGO) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CLOWER CENTER CARGO BALL RETAINER (WSP1062-1) & SPACER (WSP1063-3)ARE CORRODED.REMOVED, FABRICATED AND REPLACED RETAINER AND SPACER IAW VT-SAA EA 011-5300-01-A9142 REVF. I/R AND UPS EO MD11-2550-80661-A. (MINOR)

Part: FLOOR PANEL — DELAMINATED (E/E BAY) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CELECTRICAL COMPARTMENT FLOOR PANEL # ABA8156-11 IS DELAMINATED.REMOVED, FABRICATED AND REPALCED FLOOR PANEL # ABA8156-11 IAW EA 011-5330-01-A9163 REV. I/R AND EO MD11-5330-80647-A. (MAJOR) REF. 8100-9

Part: SPACER — CORRODED (CENTER CARGO) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CLOWER CENTER CARGO BALL RETAINER (WSP1063-3) AND SPACER ARE CORRODSED.REMOVED, FABRICATED SPACER AND REPLACED BOTH RETAINER AND SPACER IAW VT-SAA EA 011-5300-01-A9142 REV. I/R AND UPS EO MD11=2550-80661-A. (MINOR)

Part: RETAINER — CORRODED (CENTER CARGO) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CLOWER CENTER CARGO BALL RETAINER (WSP1062-501) AND SPACER (WSP1063-5) ARE CORRODED.REMOVED, FABRICATED AND REPLACED RETAINER AND SPACER IAW VT-SAA EA 011-5300-01-A9142 REV. I/R AND UPS EO MD11-2550-*80661-A. (MINOR)

Part: RETAINER — CORRODED (CENTER CARGO) · airframe 66,544 hrs · 18,814 cycles

INSPECTION TYPE:2CLOWER CENTER CARGO BALL RETAINER (WSP1062-1) & SPACER (WSP 1063-3) ARE CORRODED.REMOVED, FABRICATED AND REPLACED BOTH RETAINER AND SPACER IAW VT-SAA EA 011-5300-01-A9142 REV. I/R AND UPS EO MD11-2550-80661-A. (MINOR)

Part: FLOORBEAM — CORRODED (BS 392) · airframe 66,541 hrs · 18,812 cycles

INSPECTION TYPE:2CLAVATORY FLOOR SUPPORT IS CORRODED AT STA. 392, Y= 440 AND X= -27.5.REMOVED, FABRICATED AND REPLACED FLOOR SUPPORT IAW DWG. ABA7333 AND SRM 51-31-01. (MINOR)

Part: TRUNNION — CRACKED (NLG) · airframe 66,541 hrs · 18,812 cycles

INSPECTION TYPE:2CNOSE GEAR L/H TRUNNION FITTING IS CRACKED AT STA. 582.5, Z= -114 AND X= 24.REPAIRED CRACKED NOSE GEAR L/H TRUNNION FITTING AT STA. 582.5, Z= -114 AND X= 24 IAW SRM 53-10-14 REPAIR 2 FIG. 202. (MAJOR)

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 66,340 hrs · 18,714 cycles

CAPT REPORTS EMER LIGHTS COME ON WHEN IN ARM POS. DEFFERED IAW MEL 33-50-4 DMP C/W PLACARDED.T/S PER WD 33-51-01. FOUND WIRE BROKEN AT CONNECTOR P1-1756A PIN 5. REPAIRED PER SWPM 20-30-00. OPS CK OK PER MM 33-32-00. THIS CLEARS M738900 DMP REVERSED.

Part: BATTERY PACK — NO TEST (EMERGNCY LIGHTS) · airframe 66,331 hrs · 18,708 cycles

WHEN PREFLIGHT TESTING THE EMERGENCY LIGHTS EMERG LT BAT 1 LO ILLUMINATED. DEFERRED PER MEL 33 50 4 EMERGENCY LT BAT 1 LO DMP C/W M738710R/R'D EMERGENCY LIGHT BATTERY & OPS CK REF MM 33-50-00. OPS CHK GOOD. DMP REVERSED 33-50-1. M738710 CLEARED. EFF SOURCE 33-51-01-05-015.

Part: ACTUATOR — MALFUNCTIONED (RT AILERON) · airframe 65,977 hrs · 18,524 cycles

DIVERSION, NO EMERGENCY DECLARED/EQUIP USED. ONCE AGAIN L2 "AIL DEF DISAG" MESSAGE ON DEPART AFTER SLAT RETRACTION W/SIGNIFICANT ROLL TO THE LEFT. QRH PROCED FOLLOWED. THIS TIME THE MESSAGE REMAINED & AILERON (RT) REMAINED DEFLECTED. DIVERT TO HNL. DEFERRED TAKEOFF DEFLECTED AILERON SYSTEM, IAW MEL 27-13-2-0-1. DMP C/W. R & R INBOARD AILERON DEFLECTION CONTROL ACTUATOR, IAW AMM 27-16-01. OPERATIONS CHECK GOOD.

Part: ACTUATOR — WARNING MESSAGE (AILERON DEFLECT) · airframe 65,546 hrs · 18,358 cycles

ATB, LANDED W/O INCIDENT, UPON SLAT RETRACTION RECEIVED A LEVEL 2 "AIL DEFLECT DISAG". RAN QRH PROCEDURE, DID NOT CORRECT PROBLEM. R & R LEFT INBOARD AILERON DEFLECTION ACTUATOR PER AMM 27-16-01. OPS TESTS GOOD PER AMM 27-16-00-700-801, ALL INDICATIONS NORMAL. IPC 27-11-35-01, #530N.

Part: INDICATOR — INOPERATIVE (L1 DOOR PRESSURE) · airframe 64,912 hrs · 18,128 cycles

L1 PRESSURE LIGHT INOP. DEFERRED IAW MEL 25-61-2 DMP C/W PLACARD INSTALLED.REPLACED REMOTE PRESSURE INDICATOR ASSY. PER MM 25-61-04-401, SYS OPS NORMALLY CLEARS M 708175. ESR 25-61-05-01-165.

Part: LAMP — INOPERATIVE (DOOR INDICATION) · airframe 64,670 hrs · 18,052 cycles

L1 DOOR PRESSURE WAS GOOD, BUT THE LIGHT DOES NOT ILLUMINATE. REPLACED THE LAMP, OPS CHECKED OK.

Part: LINK — BROKEN (LT MLG DOOR) · airframe 63,910 hrs · 17,707 cycles

INSPECTION TYPE:N/AAIR TURNBACK - ON GEAR RETRACTION VIBRATION INCREASING UNTIL VIOLENT SHAKING & VIBRATION AT FULL RETRACTION. EXTENDED GEAR NORMALLY W/VIB SUBSIDING, BUT STILL PRESENTFOUND L/H NLG DOOR LINK MECHANISM BROKEN. R/R DOOR LINK MECHANISM IAW MD11 AMM 32-36-01-000-801. INSTALLED DOOR LINK MECHANISM.

Part: CONNECTOR — DAMAGED (ANTI ICE VALVE) · airframe 63,561 hrs · 17,587 cycles

LEVEL 2 TAIL A-ICE DISAG DURING CLIMBOUT (IN ICING CONDITIONS) COMPLIED WITH QRH DEPARTED ICING CONDITIONS AND LIGHT EXTINGUISHED DUE TO ICING AT DESTINATION MALFUNCTION RESULTED IN DIVERSION. REPLACED TAIL WING ANTI ICE VLV IAW AMM 30 12 01 400 801 P/N ON/OFF 3290278-1 S/N ON 185 S/N OFF 565 PERFORMED OPS TEST TEST FAILED IAW AMM 30 12 00 VLV DISAGREE INDICATION ON FURTHER T/S. PERFORMED WIRING CHECKS. FOUND AT CONNECTOR P1-2609 PIN B WIRE BROKEN. REPLACED PIN B WIRE PN ON/OFF DC65 1655. OPS TEST ALL SATIS NO FAULTS.

Part: RELAY — DEFECTIVE (L1 DOOR) · airframe 63,429 hrs · 17,544 cycles

INSPECTION TYPE:N/A L1 DOOR WILL NOT CLOSET/S PER FIM 52-11-00-101. R/R CLOSE LIMIT SWITCH PER AMM 52-70-04. NO FIX, T/S PER WDM 52-11-01. FOUND R2-177. RELAY BAD. R/R R2-177 RELAY IAW SWPM 20-20-00. OPS CK GOOD. THIS CLEARS M677370.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 63,397 hrs · 17,533 cycles

INSPECTION TYPE:N/A ON EMERGENCY LIGHT PREFLIGHT TEST RECEIVED LEVEL 1 EMERG LT BAT 1 LO. DEF IAW MEL 33 50 4 DMP C/W PLACARD INSTALLED. **SUPPLEMENTAL SDR **R/R BATTERY POWER SUPPLY PER AMM 33-51-01. OPS TEST PASS. SYSTEM OK FOR SERVICE. THIS CLEARS M676836

Part: INDICATOR — INOPERATIVE (L1 DOOR) · airframe 63,386 hrs · 17,522 cycles

INSPECTION TYPE:N/A L-1 DOOR WILL NOT TEST WHEN SLIDE BUTTON PUSHED. L1 DOOR EMERGENCY SLIDE PRESS TO TEST SWITCH HAS BEEN DEFERRED REF MEL 25-61-2. C/W DMP 25-61-2. **SUPPLEMENTAL SDR** R/R REMOTE PSI INDICATOR ASSY ON L1 DOOR IAW AMM 25-61-04. OPS CK GOOD. THIS CLEARS M676008.

Part: SENSOR — MALFUNCTIONED (LE SLAT) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:N/A EMERGENCY DECLARED - SLATS EXTENDED FLAPS 10" TAKE OFF UPON LIFT OFF RECEIVED 4 LEVEL 2 "SLAT DISAG" ALERT (FLAP HANDLE REMAINED IN 10" DETENT) MID FOOT ON AIRSPEED TAPE BECAME DYNAMIC AS THOUGH SLATS RETRACTED UNCOMMANDED RAN QRH PROCEDURE. LANDED W/28" RET (QPER FIM 31-71-07-00-101 FIG 106 PSEU FAULTED "L #4 SLAT B" PROX. SENSOR GL 0558835 7-4-19 REMOVED AND REPLACED L #4 SLAT B SENSOR WITH REF TO MM 2784-03 ACCOMPLISHED ADJ/TEST WITH REF TO MM 27-84-00-501 TEST PASSED IPC 27-84-01-01-030A

Part: TRACK — CRACKED (E&E BAY) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3C FWD. AVIONICS ACCESS DOOR RT TRACK IS CRACKED. REMOVED AND REPLACED TRACK IAW SRM 51-31-01 & 51-33-01. (MINOR)

Part: SKIN — CORRODED (CENTER TANK) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3CCENTER WING TANK UPPER SKIN CORRODED BETWEEN S-14 AND S-15 XCW -46.5.ACCOMPLISHED BLENDOUT REPAIR ON CENTER WING TANK UPPER SKIN BETWEEN STGR 14 AND STGR 15 STA XCW -46.5 PER VT SAA EA# 011-5730-021-A7790 I/R AND UPS EO MD11-5730-72879-A.

Part: SKIN — CORRODED (CENTER TANK) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3CCENTER WING TANK UPPER SKIN HAS CORROSION BETWEEN S-14 AND S-15 XCW 5 TO XCW 9.ACCOMPLISHED BLEND OUT REPAIR ON CENTER WING TANK UPPER SKIN BETWEEN STGR 14 AND STGR 15 XCW 5 TO XCW 9 PER VT SAA EA# 011-5730-01-A7792 I/R AND UPS EO MD11-5730-72878-A.

Part: SKIN — CORRODED (CENTER TANK) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3CCENTER WING TANK UPPER SKIN HAS CORROSION S-14 AND S-15 XCW 81.ACCOMPLISHED BLEND OUT REPAIR ON CENTER WING TANK UPPER SKIN BETWEEN STGR 14 AND STGR 15 XCW 81 PER VT SAA EA#011-5730-01-A7791 I/R AND UPS EO MD11-5730-72891-A.

Part: INTERCOSTAL — CRACKED (FWD CARGO) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3C FWD CARGO LH AFT BULKHEAD ST 6-70 HAS CRACKED INTERCOSTALREMOVED, FABRICATED AND INSTALLED INTERCOSTAL IN FWD CARGO BAY LH SIDE AT STA 6-70 PER MD-11 SRM 51-31-01

Part: FRAME — GOUGED (LH SIDE TAILCONE) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3C LH SIDE FWD TAILCONE CENTER GUIDE PIN WORN INTO FRAMEACCOMPLISHED REPAIR AT LH SIDE FWD TAILCONE PER MD-11 SRM 53-80-07REPAIR 1

Part: SUPPORT BRACKET — CHAFED (LH MLG) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3CLH MLG AFT HYD HOSE /CONDUIT GUIDE IS CHAFFED.ACCOMPLISHED REPAIR ON LH MLG AFT BRAKE HYD HOSE SUPPORT BRACKET ASSY PER VT SAA EA#011-3210-01-A7777 REV I/R AND UPS EO MD-11-3210-66603-A APPENDIX A.

Part: TRUSS FITTING — GOUGED (NR 3 PYLON) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3C#3 ENG FWD MOUNT OTBD SIDE HAS A GOUGED WORN INTO THE L/E.ACCOMPLISHED REPAIR ON #3 PYLON FWD TRUSS FITTING PER VT SAA EA# 011-5410-01-A7780 REV I/R AND UPS EO MD11-5450-72777-A.

Part: SKIN — CORRODED (CENTER TANK) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE: 3C, CENTER WING TANK UPPER SKIN HAS CORROSION AT X=103 AND STRINGER 15.REPAIRED CORRODED CENTER WING TANK UPPER SKINS BETWEEN STRINGER 14 AND 16 AND BETWEEN STRA. XCW=104 AND XCW=-108 IAW VT-SAA EA 011-5730-01-A7814 IR AND UPS EO MD11-5730-72997-A. (MINOR)

Part: SKIN — CORRODED (FUSELAGE) · airframe 63,373 hrs · 17,517 cycles

UPPER AFT SKIN BETWEEN X=104 AND X=-104 HAS AREAS OF CORROSION AT STRINGER 15. REPAIRED THE SKINS BETWEEN STRINGER 14 AND 16 IAW 011-5730-01-A7814 IR AND EO MD11-5730-72997-A.

Part: SKIN — CRACKED (LT WING) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3C, LH WING FIXED L/E SKIN HAS CRACKED FORMER 21 INCHES OTBD OF SLAT TRACK #16REMOVED, FABRICATED AND INSTALLED LH WING FIXED L/E SKIN FORMER PER DWG#ANB2920 AND MD-11 SRM 51-31-01 AND MD-11 SRM 51-35-01

Part: SKIN — CRACKED (LT WING) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3C LT WING FIXED L/E SKIN IS CRACKED AT SLAT TRACK #10 CUTOUT. REPAIRED CRACKED LT WING FIXED L/E SKIN AT SLAT TRACK #10 CUTOUT XOS 661.7174 IAW EA 011-5730-01-A7797 REV. IR AND EO MD11-5730-72886-A. (MAJOR)

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3C LT WING ACCESS PANEL 536AB LANDING 2EA FASTENER HOLES ARE CRACKED. REPAIRED CRACKED LT WING LOWER FUEL ACCESS DOOR LANDING BETWEEN STA. XORS 683.40 - XORS 713.65 2EA FASTENER HOLES IAW EA 011-5730-01-A7796 IR AND UPS EO MD11-5730-72989-A. (MAJOR)

Part: FRAME — WORN (TAILCONE) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3CFWD TAILCONE L/H UPPER GUIDE PIN IS WORN INTO FRAME.REPAIRED FWD TAILCONE L/H FRAME AT UPPER GUIDE PIN IAW MD-11 SRM 53-80-07 REPAIR 1, FIGURE 201. (MINOR)

Part: INTERCOSTAL — CRACKED (FWD CARGO) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3C, LOWER FWD CARGO INTERCOSTAL IS CRACKED BETWEEN STA. 6-10 - 6-30 AND BETWEEN L42L-43L.REMOVED, FABRICATED AND REPLACED INTERCOSTAL ISW DWG. ACA7049 AND SRM 51-33-01. (MINOR)

Part: INTERCOSTAL — CRACKED (FWD CARGO) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3C, LOWER FWD CARGO INTERCOSTAL IS CRACKED BETWEEN STA. 6-30 - 6-50 AND BETWEEN LONGERON 42L - 43L.REMOVED AND REPLACED CRACKED FWD CARGO INTERCOSTAL BETWEEN STA. 6-30 - 6-50 AND BETWEEN LONGERON 42L - 43L IAW MD-11 SRM 51-33-01. (MINOR)

Part: INTERCOSTAL — CRACKED (FWD CARGO) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE: 3C, FWD CARGO AT STA. 6-70 ABOVE LONGERON 43 FOUND INTERCOSTAL (BEAM) CRACKED JUST AFT AFT OF STA. 6-70.REMOVED AND REPLACED CRACKED INTERCOSTAL (BEAM) IN FWD CARGO AT STA. 6-70 ABOVE LONGERON 43 IAW MD-11 SRM 51-33-01. (MINOR)

Part: FLOORBEAM — CRACKED (FWD CARGO) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3CFWD LOWER CARGO FLOOR BEAM IS CRACKED AT STA. 6-70 ABOVE LONGERON 43 RT.REPAIRED CRACKED FWD LOWER CARGO FLOOR BEAM AT STA. Y=6-70, X=-57.5 AND Z=-98 IAW MD-11 SRM 53-40-51 REPAIR 1, FIGURE 202. (MAJOR)

Part: SKIN — CRACKED (RT WING) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3C, R/H OUTERWING LOWER ACCESS DOOR CUT-OUT PANEL LANDING BETWEEN STA. XORS.=683.4 TO XORS.=713.6 HAS 5 FASTENER HOLES CRACKED.REPAIRED R/H OUTERWING LOWER ACCESS DOOR CUTOUT PANEL LANDING BETWEEN STA. XORS.=683.4 TO 713.6 IAW SRM 57-20-02 REPAIR 5 FIG. 202. (MINOR)

Part: FAIRING — CRACKED (NR 1 NACELLE) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3C#1 ENG. PYLON STINGER FAIRING 438ELHAS A CRACKE THRU FASTENER HOLE.REPAIRED #1 ENG. PYLON STINGER FAIRING #438EL IAW SRM 54-55-01 REPAIR 2. (MINOR)

Part: LONGERON — CRACKED (BS 1256) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3CMAIN CABIN LONGERON 27R IS CRACKED AT STA. 1256 UNDER R3 DOOR.REMOVED AND REPLACED CRACKED MAIN CABIN LONGERON 27R BETWEEN STA. 1256 - 1305 IAW MD-11 SRM 51-31-01, 51-33-01 AND 51-35-01. (MINOR)

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3C MAIN CABIN FLOOR BOARD # 263BF HAS EDGE DAMAGE.FABRICATED REPLACEMENT FLOOR BOARD # 263BF IAW UPS EO MD11-5320-27386-C. (MAJOR)

Part: STRINGER — CRACKED (42) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3CCENTER WING FUEL TANK LOWER STRINGER 42 IS CRACKED AT XCW 42.REPAIRED CRACKED CENTER WING FUEL TANK LOWER STRINGER 42 BETWEEN XCW=-34.0 TO XCW=-58.0 IAW MD-11 SRM 57-10-03 REPAIR 1, FIGURE 201. (MAJOR)

Part: STRINGER — CRACKED (CTR WING TANK) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3CCENTER WING TANK STRINGER 52 BETWEEN X=-17 &X=-46 IS CRACKED. REPAIRED CRACKED CENTER WING TANK STRINGER 52 BETWEEN STA. XCW=0.00 & XCW=-32 IAW MD-11 SRM 57-10-03 REPAIR 1, FIGURE 201. (MAJOR)

Part: SKIN — CORRODED (FUSELAGE) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE: 3C, UPPER CENTER SKIN WAS CORRODED BETWEEN STA. XCW=-101 TO XCW=-110 AND ABOVE STRINGER 12. REPAIRED THE SKIN IAW EA 011-5730-01-A7794, REV I/R, AND EO MD11-5730-72977-A. MAJOR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE: 3C, SKIN WAS CORROSION AT STA. IXCW=17.0, STRINGERS 14 & 15. REPAIRED THE SKIN IAW EA 011-5730-01-A7795, REV I/R, AND EO MD11-5710-72976-A. MAJOR.

Part: STRINGER — CRACKED (LT WING) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3CL/H WING UPPER STRINGER #15 IS CRACKED BETWEEN STA. XORS.=433 TO 455.REPAIRED CRACKED L/H WING UPPER STRINGER #15 BETWEEN STA. XORS.=433-455 IAW SRM 57-20-03 REPAIR 3 FIG. 201. (MAJOR)

Part: ATTACH ANGLE — CRACKED (BS 1761) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE :3C, CENTER CARGO COMP. L/H SLOPE PANEL ATTACH ANGLE IS CRACKED AT STA. 1761.REMOVED, FABRICATED AND REPLACED SLOPE ANGLE IAW DWG. ADA0130 AND SRM 51-31-01. (MINOR)

Part: STRINGER — CRACKED (RT WING) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3CRT WING #15 STRIMGER HAS 2 CRACKES.REPAIRED CRACKED RT WING #15 STRINGER BETWEEN XORS=433 & XORS=455 IAW MD-11 SRM 57-20-03 REPAIR 3 FIGURE 201. (MAJOR)

Part: SKIN — CORRODED (BS 1997-2133) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3C, EXTERIOR FUSELAGE SKIN WAS CORRODED BETWEEN BS 1997.75 - 2133, LONGERONS 23R TO 35R. REPAIRED THE SKIN IAW EA 011-5330-01-A7821, REV I/R, AND EO MD11-5330-73013-A. MINOR.

Part: BEAM — CRACKED (LT WING TE FLAP) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3CLT WING O/B FLAP I/B FWD HINGE FAIRING I/B LOWER BEAM IS CRACKED.REMOVED AND REPLACED CRACKED LT WING O/B FLAP I/B FWD HINGE FAIRING I/B LOWER BEAM IAW MD-11 SRM 51-33-01 & 51-35-01. (MINOR)

Part: LONGERON — CRACKED (BS 1877) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3CAFT CARGO COMPARTMENT LONGERON 40R IS CRACKED AT STA. 1877.REPAIRED CRACKED AFT CARGO COMPARTMENT LONGERON 40R BETWEEN Y=1878.5 TO Y=1894.6 IAW VT-SAA EA 011-5310-01-A7786 REV. IR AND UPS EO MD11-5310-72756-A. (MAJOR)

Part: SKIN — CORRODED (FUSELAGE) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3CLT AFT FUSELAGE SKIN BETWEEN STA. 2007 - 2164 AT LOWER FAIRING ATTACHMENT HAS CORROSION.REPAIRED CORRODED AFT FUSELAGE SKIN PANEL BETWEEN STA. 1997.750 TO STA. 2163.685 CANT AND LONGERON 27L TO LONGERON 35L IAW EA 011-5330-01-A7812 REV. IR AND UPS EO MD11-5330-73011-A. (MAJOR)

Part: SKIN — CORRODED (BS 2127-2145) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE: 3C, EXTERIOR FUSELAGE SKIN IS CORRODED BETWEEN BS 2127-2145, LONGERONS 32R TO 35R. REPAIRED THE SKIN IAW EA 011-5330-01-A7805, REV I/R, AND EO MD11-5330-72978-A. MAJOR.

Part: DOOR FRAME — CRACKED (L3 DOOR) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3CL3 DOOR JAMB WEB IS CRACKED AT FWD LOWER CORNER.REPAIRED CRACKED L3 DOOR JAMB WEB FWD LOWER CORNER AT STA. Y=1254 & Z=-18 IAW MD-11 SRM 53-40-15 REPAIR 3, FIGURE 201. (MAJOR)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3C MAIN CABIN AT STA. 1341, LONGERON 15L TEE ANGLE IS CRACKED. REMOVED, FABRICATED AND REPLACED TEE ANGLE AT STA. 1341 AND LONG. 15L IAW DWG. AEA7568 AND SRM 51-350-01. (MINOR)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3C LONG. 15R TEE ANGLE IS CRACKED AT STA. 1341. REMOVED, FABRICATED AND REPLACED TEE ANGLE AT STA. 1341 AND LONG. 15R IAW DWG. AEA7568 AND SRM 51-35-01. (MINOR)

Part: SKIN — CHAFED (BS 1153) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE: 3C, EXTERIOR FUSELAGE SKIN IS CHAFED AT BS 1153, LONGERON 44R. REPAIRED THE SKIN IAW EA 011-5330-A7781, REV I/R, AND EO MD11-5330-72888-A. MAJOR.

Part: PANEL — CRACKED (WING TO BODY) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3CCANTED PANEL CAP IS CRACKED AT STA. 1236 AND Z=-100.REPAIRED CRACKED CANTED PANEL CAP AT STA. 1236 AND Z=-100 IAW UPS EO MD11-5310-72699-A. (MAJOR)

Part: RIB — CRACKED (TE FLAP) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3C RT I/B FLAP O/B HINGE, RIB ON THE AFT LOWER END WHERE IT ATTACHES TO FLAP IS CRACKED. REMOVED, FABRICATED AND REPLACED RIB IAW DWG. ARC2593 AND SRM 51-33-01 & 51-35-01. (MINOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3CL/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS.=437.6 TO 443.8.REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS.=437.6 TO XOS.=443.8 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: PANEL — CRACKED (BS 1236) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3C, LEFT UNDER WING CANTED PANEL CAP IS CRACKED AT STA. 1236.8 AND Z=-100.REPAIRED CRACKED LEFT UNDER WING CANTED PANEL CAP AT STA. 1236.8 AND Z=-100 IAW UPS EO MD11-5310-72700-A. (MAJOR)

Part: FORMER — CRACKED (LT WING) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3CL/H WING FIXED L/E RIB/FORMER IS CRACKED AT STA. XOS.=485.REMOVED, FABRICATED AND REPLACED L/H WING FIXED L/E RIB/FORMER IAW DWG. ARB2931 AND SRM 51-33-01. (MINOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3CL/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS.=443.8-450.0. REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA XOS.=443.8-450.0 IAW VT-SAA EA 011-5730-01-A7788 REV. I/R AND UPE EO MD11-5730-72845-A. (MAJOR)

Part: BEAM — CRACKED (RT WING TE FLAP) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3CRT WING O/B FLAP I/B FWD HINGE I/B LOWER BEAM IS CRACKED.REMOVED AND REPLACED CRACKED RT WING O/B FLAP I/B FWD HINGE I/B LOWER BEAM IAW MD-11 SRM 51-33-01 & 51-35-01. (MINOR)

Part: SKIN — CRACKED (LT WING) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3CL/H WING FIXED L/E LOWER SKIN IS CRACKED AT SLAT TRACK CUT-OUT, STA. XOS=891.REPAIRED CRACKED L/H WING FIXED L/E LOWER SKIN AT STA. XOS.=891 IAW SRM 57-40-02 REPAIR 7 FIG. 201. (MAJOR)

Part: SKIN — CRACKED (RT WING) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3CR/H WING FIXED L/E SKIN IS CRACKED AT SLAT TRACK #10 CUTOUT.REPAIRED CRACKED R/H WING FIXED L/E SKIN AT SLAT TRACK #10 CUTOUT STA. XOS 657 IAW MD-11 SRM 57-40-02 REPAIR 7, FIGURE 201. (MAJOR)

Part: SKIN — CRACKED (RT WING) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3C RT WING FIXED L/E LOWER SKIN IS CRACKED AT STA. XOS.=776.8. REPAIRED CRACKED RT WING FIXED L/E LOWER SKIN AT STA. XOS.=776.8 IAW SRM 57-40-02 REPAIR 7 FIG. 201. (MAJOR)

Part: LANDING — CRACKED (RT WING) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3C RT WING AT STA. XORS.=490 LOWER PANEL LANDING DOUBLER IS CRACKED. REMOVED, FABRICATED AND REPLACED PANEL LANDING IAW DWG. ARB2933 AND SRM 51-33-01 & 51-35-01. (MINOR)

Part: FRAME — GOUGED (RT MLG W/W) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE: 3C, RT MLG W/W FWD LOWER FRAME (FORMER) IS CHAFED AND GOUGED IN RADIUS.REMOVED AND REPLACED DAMAGED RT MLG W/W FWD LOWER FRAME (FORMER) IAW MD-11 SRM 51-31-01 AND 51-33-01. (MINOR)

Part: SLIDE — FAILED (L1 DOOR) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3C DURING OPERATIONAL CHECK OF L1 DOOR SLIDE/RAFT DEPLOYMENT SYSTEM; L1 DOOR SLIDE FAILED TO DEPLOY. SLIDE REPLACED ON TC 4045.

Part: SKIN — CRACKED (RT WING) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3C RT WING FIXED L/E LOWER SKIN IS CRACKED AT STA. XOS=891. REPAIRED CRACKED RT WING FIXED L/E LOWER SKIN AT STA. XOS.=891 IAW SRM 57-40-02 REPAIR 7 FIG. 201. (MAJOR)

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3C RT MLG W/W AFT O/B WALL, 2ND STIFFNER FROM FWD. END IS CRACKED. REMOVED, FABFICATED AND REPLACED STIFFNER IAW DWG. ANB7203 AND SRM 51-33-01 & 51-35-01. (MINOR)

Part: DOUBLER — CRACKED (MLG WW) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3C, CENTER W/W LEFT PUSH ROD FEED THRU CUT-OUT DOUBLER IS CRACKED.REMOVED AND REPLACED DOUBLER IN CTR. W/W IAW SRM 51-33-01. (MINOR)

Part: INTERCOSTAL — CRACKED (LT MLG WW) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3C, L/H MLG W/W INTERCOSTAL BELOW UPPER FWD. BRAKE ACCUMULATOR IS CRACKED.REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG. AEA0218 AND SRM 51-33-01 & 51-35-01. (MINOR)

Part: WEB — CRACKED (BS 1372) · airframe 63,373 hrs · 17,517 cycles

INSPECTION TYPE:3C, R/H OVER WING FUEL TANK UPPER AFT WEB IS CRACKED AT STA. 1372, X=-80 AND Z=-54.REPAIRED CRACKED R/H OVER WING FUEL TANK UPPER AFT WEB AT STA. 1372, X=-80 AND Z=-54 IAW UPS EO MD11-5710-72688-A. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 63,369 hrs · 17,515 cycles

INSPECTION TYPE:3CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED AT XOS.= 625.5 - XOS.= 629.6.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS.= 625.5 TO XOS.= 629.6 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 63,369 hrs · 17,515 cycles

INSPECTION TYPE:3CL/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA, XOS.=692-703.5.REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS.=679.8 TO XOS.=703.5 IAW SRM 57-40-02 REPAIR 15 FIG. 205.

Part: DOUBLER — CRACKED (RT WING) · airframe 63,369 hrs · 17,515 cycles

INSPECTION TYPE:3CR/H WING FIXED L/E BEADED DOUBLER AT STA. XOS 610 - 616 REQUIRES PERMANENT REPAIR. REF. D554979 & D554981.ACCOMPLISHED PERMENENT REPAIR OF R/H WING FIXED L/E BEADED DOUBLER BETWEEN XOS 610 - 616 IAW MD-11 SRM 57-40-02 REPAIR 15, FIGURE 205. (MAJOR)

Part: DOOR — INOPERATIVE (PAX) · airframe 63,180 hrs · 17,433 cycles

L1 DOOR INOP. L1 DOOR DEFERRED IAW MD11 MEL 52-10-3-1-2-1 PLACARD INSTALLED NO DMP DI UPDATED, **SUPLEMENTAL SDR**REPLACED ACTUATOR CONTROL RELAY RE-1777. DOOR OPS CK GOOD PER MM 52-10-01-700-801.

Part: SOLENOID — INOPERATIVE (L1 DOOR) · airframe 63,180 hrs · 17,433 cycles

L1 DOOR INOP. R&R'ED DOOR LOCK PIN RELEASE SOLINOID PER AMM 52-10-06-401 OK FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (L1 DOOR) · airframe 63,083 hrs · 17,393 cycles

INSPECTION TYPE:N/A DOOR L1 DID NOT OPEN AFTER LANDING. CYCLED POWER, OPENED DOOR OPS CK NORMAL, REF AMM 52-11-02.

Part: UNKNOWN — MALFUNCTIONED (CABIN DOOR) · airframe 63,075 hrs · 17,388 cycles

INSPECTION TYPE:N/A LEFT CABIN DOOR WILL NOT OPEN WITH ELECTRIC SWITCH WHEN DOOR IS DISARMED. CYCLED CABIN DOOR CIRCUIT BREAKERS AND OPS CHECKED IAW AMM 52-11-02 OK FOR SERVICE.

Part: GIRT BAR — OUT OF ALIGNMENT (L1 DOOR) · airframe 62,970 hrs · 17,342 cycles

L1 ENTRY DOOR WILL NOT ARM FOR EMERGENCY EXIT. WHEN MOVING THE LEVER TO THE ARM POSITION LEVER BINDS AND WILL NOT GO PAST 1/2 TRAVEL.FOUND GIRT BAR MISS ALIONED WITH DOOR BEAM BRACKETS REALIGNED GIRT BAR HOLE WITH PINON DOOR BEAM BRACKET PER M/M 25-61-01 PERFORMED OPS CHECK OF SLIDE ARMING HANDLE PER MM 52-11-02. OPS CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 62,939 hrs · 17,332 cycles

MAIN ENTRY DOOR (L1) PNEUMATIC BOTTLE LOW.SERVICED L1 DOOR PNEUMATIC STORAGE SYS RESERVIOR IAW AMM 12-25-04-600-801. THIS CLEARS M660786

Part: SIGN — LOOSE (EMERGENCY LIGHTS) · airframe 62,653 hrs · 17,232 cycles

RIGHT FWD ENTRY DOOR EXIT SIGN WAS LOOSE. FWD ENTRY DOOR EXIT SIGN WAS TIGHTENED IAW AMM 33-50-00, OPS CHECKED GOOD.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,484 hrs · 17,186 cycles

EMERGENCY LIGHT TEST FAILED. REPLACED THE POWER SUPPLY IAW 33-51-01-501, TEST FAILED. THE EMERGENCY LIGHTS WOULD NOT GO OFF. INSTALLED THE ORIGINAL POWER SUPPLY. RESEATEDA LOOSE CONNECTOR. OPS CHECKED GOOD IAW AMM 33-50-00.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 62,484 hrs · 17,186 cycles

EMERGENCY LIGHTS INOPERATIVE. REPLACED THE POWER SUPPLY IAW MM 33-51-01-501, TEST FAILED. EMERGENCY LIGHTS WOULD NOT TURN OFF. INSTALLED THE ORIGINAL POWER SUPPLY.

Part: SWITCH — INOPERATIVE (L1 LIFE RAFT) · airframe 62,407 hrs · 17,147 cycles

LIFE RAFT ON THE L1 DOOR WOULD NOT TEST. R & R THE PRESS TO TEST SWITCH ON THE L1 DOOR IAW AMM 25-61-04. OPS TESTED GOOD.

Part: LAMP — INOPERATIVE (PRESS TO TEST) · airframe 62,173 hrs · 17,085 cycles

DURING PREFLIGHT, THE R1 SLIDE WILL NOT TEST. REPLACED THE LAMP IN THE R1 DOOR SLIDE REMOTE PTT INDICATOR IAW MM 25-61-01-400-801. OPS CHECKED NORMAL IAW MM 25-61-04-710-801.

Part: SWITCH — BROKEN (DOOR LIGHT) · airframe 62,125 hrs · 17,056 cycles

L1 DOOR DISARMED LIGHT MODULE BROKEN. REMOVED & REPLACED L1 DOOR DISARMED LIGHT SWITCH MODULE IAW WDM 52-11-01 & OPS CHECKED AMM 52-11-02-410-801 CHECKS ILLEG. EFF SOURCE REF: IPC 52-11-70-01

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,645 hrs · 16,909 cycles

EMERGENCY LIGHT BATTERY 1 LOW, LEVEL 1 ALERT DISPLAYED. REPLACED THE BATTERY PACK IAW AMM 33-51-01. OPS CHECKED OK.

Part: BOTTLE — INOPERATIVE (R1 DOOR) · airframe 61,274 hrs · 16,802 cycles

R1 DOOR BOTTLE NOT IN GREEN RANGE. R & R DOOR RESERVOIR IAW MM 52-11-04-400-801, OPS AND LEAK CHECKED GOOD.

Part: ACTUATOR — FAULTY (L1 DOOR) · airframe 60,632 hrs · 16,637 cycles

FOUND THE L1 ENTRY DOOR ELECTRIC MOTOR SOUNDING STRANGE DURING DOOR OPENING AND DOOR OPERATION SLOW. R & R THE LT FWD PAX DOOR ELECTRIC ACTUATOR IAW AMM 52-11-01, PB 401. OPS TESTED GOOD.

Part: DOOR — UNKNOWN (L1) · airframe 60,612 hrs · 16,634 cycles

L1 DOOR NOT WORKING PROPERLY. CANCELLED DOOR MULTIPLE TIMES. DOORS OPS NORMAL IAW AMM 52-11-02-501. ACFT OK TO CONTINUE.

Part: CABLE — OUT OF ADJUST (L1 DOOR) · airframe 60,534 hrs · 16,619 cycles

INSPECTION TYPE:N/AL-1 DOOR WILL NOT OPEN ELECTRICALLY. ADJUSTED LH CREW DOOR CABLE, CLEANED ACTUATOR ELECTRICAL PLUG AND LUBE TRACK PER AMM 52-11-01-401; OPS TEST OK.

Part: LONGERON — CRACKED (TAILCONE) · airframe 59,247 hrs · 16,313 cycles

INSPECTION TYPE: 2C, FWD END OF LONGERON CRACKED INSIDE EXTENDED TAILCONE, BS 2165. REPAIRED THE LONGERON IAW EA 011-5320-01-A6819 REV IR, AND EO MD11-5320-64445-A.

Part: LUG — CHAFED (THRUST REVERSER) · airframe 59,247 hrs · 16,313 cycles

INSPECTION TYPE: 2C, NR 2 ENGINE, LT FAN REVERSER HAS CHAFE DAMAGE ON THE HINGE BRACKET LUGS. REPAIRED THE DAMAGE IAW EA 011-7830-01-A6828, REV I/R, AND EO MD11-7830-64531-A.

Part: LUG — CHAFED (THRUST REVERSER) · airframe 59,247 hrs · 16,313 cycles

INSPECTION TYPE: 2C, NR 2 ENGINE, LT FAN REVERSER HAS CHAFE DAMAGE ON LOWER HINGE SUPPORT LUG, REPAIRED THE DAMAGE IAW EA O11-7830-01-A6828 REV I/R, AND EO MD11-7830-64531-A.

Part: NOZZLE — CRACKED (NR 1 ENG EXHAUST) · airframe 59,247 hrs · 16,313 cycles

INSPECTION TYPE: 2C, NR 1 ENGINE EXHAUST NOZZLE INNER SKIN CRACKED. REPAIRED THE EXHAUST NOZZLE IAW EA 011-7810-01-A6825, REV IR, AND EO MD11-7810-64529-A.

Part: FASTENER — LOOSE (#2 ENG.) · airframe 59,247 hrs · 16,313 cycles

INSPECTION TYPE: 2C, NR 2 ENGINE INLET COWL LIP SKIN HAS 4 LOOSE FASTENERS AT SPLICE LOCATIONS 2,9 AND 11. INSTALLED BLIND FASTENERS IAW EA 011-5430-01-A6815, REV I/R, AND EO MD11-5430-64427-A.

Part: SKIN — CRACKED (THRUST REVERSER) · airframe 59,247 hrs · 16,313 cycles

INSPECTION TYPE: 2C, NR 2 ENGINE LEFT THRUST REVERSER AFT FIXED INNER BARREL UPPER SKIN CRACKED. REPAIRED IAW EA 011-7830-01-A6817, REV IR, AND EO MD11-7830-64420-A.

Part: VANE — DELAMINATED (RT WING TE FLAP) · airframe 59,247 hrs · 16,313 cycles

INSPECTION TYPE:3C, RT INBD FLAP VANE UPPER AND LOWER SKIN DELAMINATED. REMOVED AND REPLACED THE FLAP VANE IAW AMM 27-50-22.

Part: FITTING — CRACKED (RT WING TE FLAP) · airframe 59,247 hrs · 16,313 cycles

INSPECTION TYPE: 1C, RT OTBD FLAP INTERNAL FITTING CRACKED. REMOVED AND REPLACED THE FLAP IAW AMM 27-50-30.

Part: SPAR CAP — CORRODED (RT WING) · airframe 59,247 hrs · 16,313 cycles

INSPECTION TYPE: 2C, RT WING REAR SPAR UPPER CAP HAS CORROSION BETWEEN XORS 486 - 492. REPAIRED THE SPAR CAP IAW EA 011-5710-01-A6816, REV I/R, AND EO MD11-5730-64428-A.

Part: DOUBLER — CHAFED (RT WING) · airframe 59,247 hrs · 16,313 cycles

INSPECTION TYPE: 2C, RT WING FIXED L/E SKIN REPAIR DOUBLER IS CHAFED BETWEEN XOS 1007.12 AND XOS 1038.04. REPAIRED CHAFED RT WING L/E SKIN REPAIR DOUBLER IAW EA 011-5730-01-A6818, AND EO MD11-5730-64438-A.

Part: DOUBLER — CRACKED (RT WING) · airframe 59,247 hrs · 16,313 cycles

INSPECTION TYPE: 2C, RT WING FIXED L/E BEADED DOUBLER IS CRACKED AT XOS 785. REPAIRED THE DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 205. MAJOR.

Part: SPAR CAP — CORRODED (LT WING) · airframe 59,247 hrs · 16,313 cycles

INSPECTION TYPE: 2C, LEFT WING REAR SPAR UPPER CAP AFT FLANGE CORRODED XORS 551 - 565. REPAIRED THE SPAR CAP IAW EA 011-5710-01-A6821, REV IR, AND EO MD11-5710-64468-A.

Part: SPAR CAP — CORRODED (LT WING) · airframe 59,247 hrs · 16,313 cycles

INSPECTION TYPE: 2C, LEFT WING REAR SPAR UPPER CAP AFT FLANGE CORRODED XORS 1039 - 1049. REPAIRED THE SPAR CAP IAW EA 011-5720-01-A6822, REV IR, AND EO MD11-5710-64477-A.

Part: SKIN — CORRODED (LT WING TE FLAP) · airframe 59,247 hrs · 16,313 cycles

INSPECTION TYPE: 2C, LT WING UPPER FWD SKIN HAS CORROSION IN TWO PLACES XORS 197.2 AND XORS 231, BETWEEN STRINGERS 15-17. REPAIRED IAW EA 011-5730-01-A6814, REV I/R, AND EO MD11-5730-64421-A.

Part: SPAR CAP — CORRODED (RT WING) · airframe 59,247 hrs · 16,313 cycles

INSPECTION TYPE: 2C, RT WING REAR SPAR UPPER CAP HAS CORROSION BETWEEN XORS.542 - 547 AND XORS 556.5 - 572.5. REPAIRED THE SPAR CAP IAW EA 011-5710-01-A6820, REV I/R, AND EO MD11-5710-64472-A.

Part: SPAR — CORRODED (LEFT WING) · airframe 59,247 hrs · 16,313 cycles

INSPECTION TYPE: 2C, LEFT WING UPPER T/E SKIN AND ADJACENT REAR SPAR UPPER CAP AFT FLANGE CORRODED XORS 653 - 672. REPAIRED IAW EA 011-5730-01-A6823, REV IR, AND EO 5710-64482-A.

Part: LUG — WORN (THRUST REVERSER) · airframe 59,247 hrs · 16,313 cycles

INSPECTION TYPE: 1C, NR 3 RT THRUST REVERSER AFT HINGE LUG WORN. REMOVED AND REPLACED THE THRUST REVERSER IAW AMM 78-13-01-400-868.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 58,300 hrs · 16,049 cycles

EMERGENCY LIGHT TEST FAILED. REPLACED EMERGENCY THE BATTERY PACK IAW MM 33-51-01. OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 58,248 hrs · 16,041 cycles

DURING PREFLIGHT, EMERGENCY LIGHT BATTERY LOW ILLUMINATED IAW FIM 33-52-01-00 AND AMM 33-51-01 PFM EMERGENCY LIGHT OER TEST SATIS AND DI M593101 AND MEL 33-50-2 CLOSED.

Part: SEAL — PULLED (PAX DOOR) · airframe 57,920 hrs · 15,962 cycles

DURING CLIMB, THE LEFT ENTRY DOOR HAD VERY LOUD HISSING SOUND WHICH DISSIPATED BY TOP OF CLIMB. FOUND 12 INCHES OF SEAL PULLED OUT OF MCD INSTALLED THE SEAL. PERFORMED PRESSURIZATION OF ACFT, NO NOISE NOTED OK FOR SERVICE IAW MM 21-00-00.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,580 hrs · 15,639 cycles

EMERGENCY LIGHTS BATTERY 1 LOW MESSAGE DURING EMERGENCY LIGHT TEST. IAW FIM 33-51-02-00, FIG 104, BLOCKS 1, 2, 6 AND 7. R & R EMERGENCY LIGHTING BATTERY POWER SUPPLY , OPS CHECK NORMAL, REF AMM 33-51-01, AIPC 33-51-01-05, NR 015.

Part: SKIN — DAMAGED (BS 695) · airframe 55,485 hrs · 15,336 cycles

RIGHT FUSELAGE SKIN DAMAGED AT BS 695, STRINGER 36R, DOUBLER-TRIPLER REPAIR IAW EO MD11-5330-58625-B.

Part: SHEAR TIE — CRACKED (BS 2140) · airframe 54,870 hrs · 15,161 cycles

INSPECTION TYPE: 3C, SHEAR TIE CRACKED BS 2140. R & R THE SHEAR TIE IAW SRM 51-33-01, 51-31-01.

Part: LONGERON CLIP — CORRODED (BS 1687) · airframe 54,870 hrs · 15,161 cycles

INSPECTION TYPE: 3C, LONGERON CLIP CORRODED BEYOND ALLOWABLE LIMITS AT BS 1687 L52. R & R LONGERON CLIP IAW SRM 51-33-01.

Part: TRUNNION — CORRODED (CENTER MLG) · airframe 54,870 hrs · 15,161 cycles

INSPECTION TYPE: 3C, CLG RT SIDE TRUNNION FITTING CORRODED ON UPPER SURFACE SPOTFACES. REPAIRED TRUNNION FITTING IAW EA 011-5310-01-A5850, REV IR AND EO MD11-5310-57837-A.

Part: TRUNNION — CORRODED (CENTER MLG) · airframe 54,870 hrs · 15,161 cycles

INSPECTION TYPE:3C, LT SIDE TRUNNION FITTING CORRODED ON UPPER SURFACE SPOTFACES. REPAIRED TRUNNION FITTING IAW EA 011-5310-01-A5849, REV. IR AND EO MD11-5310-57838-A.

Part: DOUBLER — CRACKED (RT WING) · airframe 54,870 hrs · 15,161 cycles

INSPECTION TYPE: 3C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 628. REPAIRED RT WING BEADED DOUBLER XOS 625-629 IAW SRM 57-40-02, REPAIR 15, FIG 206.

Part: DOUBLER — CRACKED (RT WING) · airframe 54,870 hrs · 15,161 cycles

INSPECTION TYPE: 3C, RIGHT WING FIXED L/E INNER BEADED DOUBLER CRACKED XOS 614. REPAIRED RT WING BEADED DOUBLER, XOS610-616 IAW SRM 57-40-02, REPAIR 15, FIG 206.

Part: DOUBLER — CRACKED (RT WING) · airframe 54,870 hrs · 15,161 cycles

INSPECTION TYPE: 3C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED XOS654. REPAIRED RT WING BEADED DOUBLER XOS653-657 IAW SRM 57-40-02. REPAIR 15, FIG 203.

Part: SHEAR TIE — CRACKED (BS 2084) · airframe 54,870 hrs · 15,161 cycles

INSPECTION TYPE: 3C, SHEAR TIE CRACKED, BS 2084. R & R THE SHEAR TIE IAW SRM 51-33-01.

Part: SKIN — CHAFED (LT WING) · airframe 54,870 hrs · 15,161 cycles

INSPECTION TYPE: 3C, LT WING FIXED L/E EXTERIOR SKIN GOUGED LWS 1030-1046. REPAIRED THE SKIN IAW SRM 57-40-02, REPAIR 5, FIG 201.

Part: DOUBLER — CRACKED (RT WING) · airframe 54,870 hrs · 15,161 cycles

INSPECTION TYPE: 3C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED AT XOS 646. REPAIRED THE DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 203.

Part: SHEAR TIE — CRACKED (BS 2047) · airframe 54,870 hrs · 15,161 cycles

INSPECTION TYPE: 3C, SHEAR TIE CRACKED BS 2047. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT SHEAR TIE IAW DWG AJC7021 AND SRM 51-33-01.

Part: SPAR CAP — CORRODED (LT WING) · airframe 54,870 hrs · 15,161 cycles

INSPECTION TYPE: 3C, LT WING AFT SPAR UPPER CAP AFT FLANGE CORRODED XORS 677-786. REPAIRED CORROSION IAW EA 011-5710-01-A5852, REV IR AND EO MD11-5710-57830-A.

Part: SKIN — CRACKED (BS 535) · airframe 54,870 hrs · 15,161 cycles

INSPECTION TYPE: 3C, FUSELAGE SKIN WAS CRACKED AT THE UPPER AFT CORNER OF RT A/C COMPARTMENT DOOR CUT-OUT, BS 535 L31-32R. REPAIRED THE SKIN IAW SRM 53-20-15, REPAIR 3, FIG 201.

Part: SKIN — GOUGED (RT WING) · airframe 54,870 hrs · 15,161 cycles

INSPECTION TYPE: 3C, RT WING L/E EXTERIOR SKIN GOUGED BETWEEN XOS 1005-1065. REPAIRED THE SKIN IAW SRM 57-40-02 REPAIR 5, FIG 201.

Part: SWITCH — INOPERATIVE (THRUST REVERSER)

IMMEDIATELY AFTER TAKE OFF, RECEIVED A REV 2 PRESSURE FAULT. WARNING DISAPPEARED AND REAPPEARED NUMEROUS TIMES. DUMPED FUEL APPROX 24 MINS, RT LWR SWITCH, S1-8366, INOPERATIVE. LT CENTER ACTUATOR UNLOCK FUNCTION NOT SMOOTHLY. R & R RT LOWER SWITCH IAW AMM 78-34-01. R & R LEFT CENTER ACTUATOR IAW AMM 78-32-02 LEAK CHECK OK. C/O OPS CK OF NR 2 ENG T/R SYSTEM IAW AMM 78-30-01 FOUND SATISFACTORY. PERFORM NR 2 ENG RUN. ACFT OK FOR SERVICE. REF IPC 78-32-91-10, ITEM 307J.

Part: LIGHT — BROKEN (R1 DOOR)

R1 DOOR LEVER EMERGENCY LIGHT ASSY HOUSING BROKEN. R & R R1 DOOR HANDLE EMERGENCY LIGHT IAW AMM 33-52-02.

Part: STRINGER — CRACKED · airframe 52,622 hrs · 14,644 cycles

INSPECTION 1C, CENTER WING LOWER STRINGER 47 HAS THREE CRACKS AT STA XCW= 46.50, 17.00 AND -17.00. ACCOMPLISHED SPLICE REPAIR ON LOWER STRINGER NR 47 AT STA XCW = 46.50, 17.00 AND -17.00 IAW EA 011-5710-01-A5432, REV I/R AND EO 5710-54832-A.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,622 hrs · 14,644 cycles

INSPECTION 1C, STRINGER 52 CRACKED IN UPPER AUX TANK. REPAIRED STRINGER 52 BETWEEN STA XCW-32 AND XCW -64 IAW STASA EA 011- 5710-01-A5433 REV IR AND EO 5710-54836-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 52,622 hrs · 14,644 cycles

1C INSPECTION, LT WING FIXED L/E BEADED DOUBLER FOUND WITH CRACKS BETWEEN XOS 610-625. ACCOMPLISHED REPAIR ON LT WING FIXED L/E BEADED DOUBLER FROM XOS 610-633 IAW EA 011-5730-01-A5425, REV I/R AND EO 5730-54759-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 52,622 hrs · 14,644 cycles

1C INSPECTION, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR STA XOS640. REPAIRED IAW SRM 57-40-02, REPAIR 15, FIG.206.

Part: DOUBLER — CRACKED (LT WING) · airframe 52,622 hrs · 14,644 cycles

1C INSPECTION, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 702. REPAIRED LT WING DOUBLER BETWEEN XOS 698-705 IAW SRM 57-40-02, REPAIR 15, FIG 206.

Part: DOUBLER — CRACKED (LT WING) · airframe 52,622 hrs · 14,644 cycles

1C INSPECTION, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 670 REPAIRED LT WING DOUBLER BETWEEN XOS 667-673 IAW SRM 57-40-02 REPAIR 15, FIG 203.

Part: DOUBLER — CRACKED (LT WING) · airframe 52,622 hrs · 14,644 cycles

1C INSPECTION, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 696. REPAIRED LT WING DOUBLER BETWEEN XOS 692-698 IAW SRM 57-40- 02, REPAIR 15, FIG 206.

Part: DOUBLER — CRACKED (LT WING) · airframe 52,622 hrs · 14,644 cycles

1C INSPECTION, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 646. REPAIRED LT WING DOUBLER BETWEEN XOS 643-648 IAW SRM 57-40-02, REPAIR 15, FIG 203.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHT)

EMERGENCY LIGHT TEST FAILED. R & R EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-01.

Part: FLOOR PANEL — PUNCTURED (BS 1461)

FLOOR PANEL DAMAGED BS 1461, POS 9R. FABRICATED NEW FLOOR PANEL IAW EO 5320-27386-C.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK)

MAIN CARGO DECK FLOOR PANEL DAMAGED. REPAIRED IAW EO 5320-27386-C.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

MAIN CARGO DECK FLOOR PANEL DAMAGED. REPAIR IAW EO 5320-27386-C.

Part: LAMP — INOPERATIVE (DOOR SLIDE)

L1 AND R1 DOOR SLIDE REMOTE PRESS TO TEST INOPERATIVE. REPLACED LAMPS AND REPLACED BATTERIES IAW MM 25-61-400-801. OPS CHECKED GOOD IAW MM 25-61-700-801.

Part: ACTUATOR — LEAKING (ELEVATORS)

HYDRAULIC SYS 3 LEAK, RT INBD ELEVATOR ACTUATOR LEAKING. COMPLETED LMECA 21940 AND 21941. R & R RT INBD ELEVATOR ACTUATOR, REF MM 27-33-20.

Part: ACTUATOR — INOPERATIVE (AILERONS)

ON DEPARTURE, WITH SLAT RETRACTION LEVEL 2 AILERON DEFLECT DISAGREE LT OTBD AILERON STAYED DEFLECTED T/S FOUND LT INBD AILERONS DEFLECTION ACTUATOR INOPERATIVE. R & R LT INBD AILERON DEFLECTION CONTROL ACTUATOR IAW AMM 27-16-01-400-801 A-F. COMPLETED REMAINING STEPS OF INSTALLATION REF MM 27-16-01. RIG CHECKED NORMAL.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 50,559 hrs · 2,637 cycles

INSPECTION TYPE:4C MAIN CABIN FLOORBOARD 263EF HAS ONE PUNCTURE. FABRICATED MAIN CABIN FLOORBOARD IAW EO MD11-5320-27386-C.

Part: FRAME — CRACKED (FS 427.668) · airframe 50,559 hrs · 14,108 cycles

INSPECTION TYPE:4C FRAME AT BS 427.668 APPX 11 O'CLOCK POS IS CRACKED. REPAIRED FUSELAGE DROP CEILING FRAME AT BS 427.668 AT 11:00 POS REF EA 011-5310-01-A4625. REV I/R, EO MD11-5310-50864-A.

Part: DOOR FRAME — CRACKED (R3 DOOR) · airframe 50,559 hrs · 2,637 cycles

INSPECTION TYPE:4C, CRACK IN LIGHTNING HOLE FWD LOWER SIDE OF R3 DOOR FRAME AT BS 1254. REPAIRED LIGHTNING HOLE AT FWD LOWER SIDE OF R3 DOOR IAW SRM 53-40-15, REPAIR 3, FIG 201.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 50,559 hrs · 2,637 cycles

INSPECTION TYPE:4C, FINGER DOUBLER HAS CORROSION ON UPPER SURFACE OF CENTER FUEL TANK AFT END 24" RT OF CENTER LINE. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER (PRODUCTION DOUBLER) ON UPPER SURFACE OF CENTER FUEL TANK AFT END 24 " RT OF CENTERLINE REF DWG APB7241, SRM 51-31-01 AND 51-33-01.

Part: SKIN — DENTED (CTR CARGO DOOR) · airframe 50,559 hrs · 14,108 cycles

INSPECTION TYPE:4C, CENTER CARGO DOOR DENTED ON LOWER EDGE BELOW FWD LOCK PIN WINDOW. REPAIRED DENT AT CENTER CARGO DOOR FWD LOWER CORNER AT APPROX STA 1717 REF STA SA EA 011-5231-01-A4621, REV IR, EO MD11-5230-50845-A.

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 50,559 hrs · 14,108 cycles

INSPECTION TYPE:4C, CENTER CARGO LONGERON SPLICE CRACKED AT L-40L AND STA 5-123. FABRICATED AND REPLACED CENTER CARGO COMPT LONGERON SPLICE AT L-40L AND STA 5-123 SRM 51-33-01, PARA 8.

Part: SKIN — DENTED (FS 1821 L27R) · airframe 50,559 hrs · 14,108 cycles

INSPECTION TYPE:4C, RT FUSELAGE EXTERNAL SKIN DENTED AROUND RIVET HEAD, LOCATED 54' AFT OF AFT CARGO DOOR HINGE. REPAIRED RT FUSELAGE SKIN DENT BETWEEN STA 1821 TO 1841 AND L-27R TO L28R REF SRM 53-00-01, REPAIR 1, FIG 201 EA 01-5330-01-A4615 IR EO MD11-5330-50863A, FIG 201 AND MESSAGE SLH-U PS-13-0076-04B DATED 5/22/2013.

Part: LONGERON SPLICE — CRACKED · airframe 50,559 hrs · 14,108 cycles

INSPECTION TYPE:4C, LONGERON 33LT SPLICE FITTING CRACKED AT STA 5-123. REMOVED, FABRICATED AND INSTALLED REPLACEMENT L33L SPLICE FITTING AT STA 5-123 IAW DWG A5A7112 AND SRM 51-33-01. (MINOR)

Part: STRINGER — CRACKED (RT WING) · airframe 50,559 hrs · 2,637 cycles

INSPECTION TYPE: 4C, RT WING UPPER STRINGER CRACKED AT XORS 623 AT FUEL ACCESS PANEL 635BT. REPAIRED RT WING UPPER STRINGER 12 IAW SRM 57-00-03, REPAIR 5, FIG 202.

Part: STRINGER — CRACKED (RT WING) · airframe 50,559 hrs · 2,637 cycles

INSPECTION TYPE: 4C, RT WING UPPER STRINGER 14 CRACKED AT ACCESS PANEL 634CT AT XORS 506. REPAIRED RT WING UPPER STRINGER IAW SRM 57-00-03, REPAIR 5, FIG 202.

Part: CAP — CORRODED (LT WING) · airframe 50,559 hrs · 14,108 cycles

INSPECTION TYPE:4C, CORROSION ON PANEL LANDING AT PANEL ACCESS 541JB LT WING STA XORS 372 TO 433. REPAIRED LT WING T/E BEAM ASSY LOWER CAP BETWEEN XW314 AND XW373 REF STASA EA 011-5710-01-A4599 IR, EO MD11-5720-50639-A AND FORM 8 110-3.

Part: FAN — INOPERATIVE (E/E BAY)

AVIONICS FAN STARTED EMITTING AN ELECTRICAL MILD BURNING ODOR. AFTER PULLING AVIONICS COMPT COOLING FAN C/B, ODOR WENT AWAY QUICKLY. REPLACED NR 3 AVIONICS COMPT COOLING FAN AMM 21-26-02 IPC REF 21-26- 01-01-400.

Part: SLIDE — MALFUNCTIONED (L1 DOOR)

L1 DOOR SLIDE REMOTE PRESSURE PRESS TO TEST INOPERATIVE. PERFORMED OPS TEST OF THE REMOTE PRESSURE INDICATOR. ALL CHECKED GOOD. DMP REVERSED. WORK DONE IAW 25-61-04-710-801 LIGHT CK & BOTTLE PSI CHECKED GOOD.

Part: LANDING GEAR — MALFUNCTIONED (LEFT)

LEFT MAIN GEAR UNSAFE INDICATION UPON GEAR RETRACTION ON BOTH PRIMARY AND SECONDARY. ACCOMPLISHED CHECKLIST WITH SAME RESULTS. TESTED GEAR SWING SEVERAL TIMES IAW MM 32-31-00-700-803 AND MM 32-32-00-710-803. OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY BATTERY TEST SHOWS BATTERY 1 LOW. R & R EMERGENCY LIGHTS BATTERY POWER SUPPLY IAW MM 33-51-01. EMERGENCY LIGHTS TEST PASSED AND EMERGENCY LIGHTS CHECKED NORMAL.

Part: FMU — INOPERATIVE (NR 3 ENGINE)

AT 17000' GOT NR 3 SEL FADEC ALT, THEN NR 3 RPM LOW FOLLOWED BY FLAMEOUT NR 3. SHUTDOWN ENG 3 IAW QRH. RESTARTED NR 3 IAW QRH NORMAL START. REPLACED NR 3 ENGINE FMU, LEAK AND OPS CHECK OK REF MM 73-21-01-4-2.

Part: VALVE — INOPERATIVE (NR 3 OIL COOLER)

NR 3 ENGINE HIGH OIL TEMPERTURE LEVEL 2 OIL TEMP HIT 162. PERFORMED FIM 79-00-00 THRU FIG 6, BLOCK 6. FOUND CFSD FAULT 351-18 ENG AOC T/M CKT. R & R AIR OIL COOLER VALVE IAW MM 79- 21-01. OPS CHECKS NORMAL, NO LEAKS NOTES. R & R MAIN ENG OIL FILTER & INSPECTED CHIP DETECTORS, NO CONTAMINATION FOUND IAW MM 79-22-05. NO LEAKS.

Part: RIB — CRACKED (RT WING) · airframe 47,816 hrs · 13,441 cycles

INSPECTION TYPE:3C, AFTER REMOVAL OF RT WING PANEL 616ET FOUND L/E INTERNAL RIB CRACKED. FABRICATED AND INSTALLED REPLACEMENT RIB IN RT WING L/E IAW DWG ARB2440, SRM 51-33-01, SRM 51-35-01.

Part: STIFFENER — CRACKED (RT WING) · airframe 47,816 hrs · 13,441 cycles

INSPECTION TYPE:3C, STIFFENER CRACKED IN RT WING L/E INTERIOR AT XORS 562 (XOS667). REPAIRED STIFFENER IN RT WING L/E INTERIOR AT STA XOS667 IAW SRM57-40-03, REPAIR 2, FIG 202.

Part: BATTERY — DISCHARGED (L1 DOOR SLIDE)

AS L1 DOOR REMOTE PRESSURE INDICATOR WILL NOT PRESS TO TEST. CHECKED BOTTLE PRESSURE IAW DMP 25-61-2, STEP 1(A). WIRING CHECK COMPLETED IAW WDM 25-61-01 AND FOUND ELECTRICAL POWER OUTPUT LOW. REPLACED BATTERIES. CHECKED GOOD IAW AMM 25-61-04-4.

Part: FLOORBEAM — DAMAGED (BS 979)

LOWER FWD CARGO BAY FLOORBEAM DAMAGED, BS 979. REPAIRED IAW EO MD11-5310-41454-C.

Part: TRANSMITTER — INOPERATIVE (LT WING TE FLAP)

AFTER TAKEOFF & LANDING GEAR RETRACTED; THE AURAL WARNING "LANDING GEAR AR" SOUNDED CONTINOUSLY. CREW CYCLED GEAR WITH NO SUCCESS. CREW DECIDED TO RETURN TO DEPARTURE. UPON SELECTING THE GEAR DOWN; AURAL WARNING SILENCED. AMTS T/S IAW FRM 31-51-00-1; REPLACED THE LT OTBD FLAP TRANSMITTER IAW MM 27-54-02-4 & PERFORMED OPS/ADJ CHECK OUT IAW MM 27-54-00-5 OPS CK, FOUND OK FOR SERVICE.

Part: CONNECTOR — BROKEN (MLG)

LANDING GEAR AURAL WARNING. IAW FIM 31-51-00-1, FIG 120, STEP 8 R & R CONNECTOR P1-1111 IAW SWPM 20-31-00. ALSO FOUND BROKEN WIRE AT P1-1111 PIN "5". REPAIRED WIRE IAW SWPM 20-10-03. PERFORMED FLAP TRANSMITTER TEST IAW AMM 27-54-00-5. LP 764307 FOR TEST OF LANDING AURAL WARNING HORN.

Part: SKIN — DAMAGED (CARGO DOOR)

CTR CARGO DOOR FUSE SKIN DAMAGED STA 1781. REPAIRED IAW EO MD11-5330-43067-B.

Part: FLOORBEAM — DAMAGED (BS 919)

FLOORBEAM AND STABILIZATION STRAP HAVE OVERSIZE HOLE THROUGH BOTH. FREEZE PLUG HOLE IN FLOORBEAM AND FABRICATED NEW STRAP IAW EOMD11-5310-41455A.

Part: DOOR — INOPERATIVE (FLIGHT DECK)

L1 DOOR JAMMED. RESET L1 DOOR CIRCUIT BREAKER. DOOR OPS CHECKED GOOD IAW AMM 52-11-02-5.

Part: SKIN — CRACKED (LT WING L/E) · airframe 44,984 hrs · 12,733 cycles

INSPECTION TYPE:2C, LT WING L/E SKIN AT TELESCOPIC DUCT CUTOUT CRACKED ON INBD AND OTBD UPPER CORNERS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLR IAW SRM 57-40-01, REPAIR 10, FIG 201.

Part: DOUBLER — CRACKED (LT WING) · airframe 44,984 hrs · 12,733 cycles

INSP TYPE:2C, LT WING L/E COMPT BETWEEN XOS625 AND XOS633 CEILING DOUBLER IS CRACKED AT 4EA FASTENERS. CUT OUT DAMAGE ON LT WING L/E COMPT FROM XOS625 TO XOS633. FABRICATED AND INSTALLED 1 REPAIR DOUBLER, 1 REPAIR FILLER AND 10 REPAIR ANGLES REF SRM 57-40-02, REPAIR 9, FIG 203.

Part: DOUBLER — CRACKED (LT WING) · airframe 44,984 hrs · 12,733 cycles

INSP TYPE:2C, LT WING L/E COMPT CEILING DOUBLER IS CRACKED AT 2EA FASTENERS DIRECTLY ABOVE ANTI-ICE TELESCOPIC DUCT. REMOVED DAMAGED BEADED DOUBLER SECTION FROM LT WING L/E COMPT BETWEEN XOS464 AND XOS470 ABOVE TELESCOPIC DUCT. FABRICATED AND INSTALLED REPAIR DOUBLER, REPAIR FILLER AND 5EA REPAIR ANGLES REF SRM 57-40-02, REPAIR 9, PAGES 201 TO 210.

Part: SKIN — DENTED (BS 372) · airframe 44,984 hrs · 12,733 cycles

INSPECTION TYPE:2C, DEFERED ITEM D-433820: FUSELAGE SKIN DENT AT STA 372 LT AFT SIDE OF FWD E&E DOOR. CUT OUT DAMAGE ON FINGER DOUBLER AND FUSELAGE SKIN DENT AT FS 372 LT AFT SIDE OF FWD E&E DOOR. FABRICATED INTERNAL DOUBLER, SKIN FILLER AND FINGER DOUBLER FILLER AND INSTALLED REF EO MD11-5330-40343-A AND STA SA EA 011-5330-01-A2754.

Part: SLIDE — UNWANTED DEPLOY (L1 DOOR)

EXTERIOR L1 DOOR HANDLE WAS USED TO OPEN THE DOOR. RESET EMERGENCY DEPLOY MECHANISM PER MM 52-10-03-02.

Part: SKIN — MISREPAIRED (TE FLAP) · airframe 42,373 hrs · 12,066 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQUENCE 271-W3-03 HAS EXISTING REPAIR AT LT WING I/B FLAP UPPER SKIN BETWEEN STA XIFH 213.050-219.550 DOES NOT CORRELATE TO MD-11 SRM VOL1 57-20-00 FIG 6. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPLACEMENT REPAIR IAW MD-11 SRM VOL 1 57-10-00 FIG 38 SHT 2.

Part: SKIN — MISREPAIRED (RUDDER) · airframe 42,373 hrs · 12,066 cycles

INSPECTION TYPE:1C REPAIR SEQ 271-S4-02 UPPER AFT RUDDER TIP BETWEEN STA ZV491 AND ZV 487 NOT CORRELATED TO SRM. REMOVED EXISTING REPAIR ON THE UPPER AFT RT RUDDER TIP SKIN BETWEEN ST A ZV491-487. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF EO MD11-5 540-34404-A AND EA 011-5540-01-A1925.

Part: FASTENER — INCORRECT (RT WING) · airframe 42,373 hrs · 12,066 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQUENCE 271-W4-01 RT WING FIXED L/E BETWEEN STA XOS607- XOS 615 EXTERNAL REPAIR DOUBLER BLIND FASTENERS INSTALLED IN LIEU OF SOLID FASTENERS. REMOVED DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SAA EA 011-5730-01-A1933 AND UPS EO MD11-5730-34417-A.

Part: SKIN — MISREPAIRED (RUDDER) · airframe 42,373 hrs · 12,066 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQ 271-S4-03 UPPER AFT RT RUDDER BETWEEN STA ZV484 AA AND STA ZV487 NOT CORRELATED TO SRM. REMOVED EXISTING REPAIR AT UPPER AFT RT RUDDER TIP SKIN BETWEEN STA XV ZV491 AND ZV487. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF EO MD 11-5540-34405-A AND EA 011-5540-01-A1932.

Part: WEDGE — GOUGED (TE FLAP) · airframe 42,373 hrs · 12,066 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQ 271-W4-08 RT INBOARD FLAP T/E WEDGE GRINDING MARKS BETWEEN STA XIFH 183.300 AND XIFH 201.300. REMOVED RT INBOARD FLAP T/E WEDGE BETWEEN STA 183.300 AND 201.300. REPAIRED AND INSTALLED T/E WEDGE REF EO MD11-5750-34399-A, EA 011-5753-01-A1935.

Part: SKIN — MISREPAIRED (TE FLAP) · airframe 42,373 hrs · 12,066 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQUENCE 271-W4-09 EXISTING REPAIR AT RT WING I/B FLAP UPPER SKIN BETWEEN STA XIFH 133.900-140.600 DOES NOT CORRELATE TO MD-11 SRM VOL 1 57-10-00 FIG 33. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPLACEMENT REPAIR IAW MD-11 SRM VOL 1 57-10-00 FIG 39.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 42,373 hrs · 12,066 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQUENCE 271-F1-04 REPAIR BETWEEN STA 1931.500 AND 1942, BETWEEN LONGERON 5L AND 7L DOES NOT CORRELATE TO MD-11 SRM VOL 1 53-20-00 FIG 6. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPLACEMENT REPAIR IAW MD-11 SRM VOL 1 53-20-00 FIG 6 SHT 8 OF 18.

Part: SKIN — GOUGED (RT WING) · airframe 42,373 hrs · 12,066 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQUENCE 271-W4-04 FIXED L/E UPPER SKIN BETWEEN XIS 241- XIS 252 FOUND WITH GOUGE ON REPAIR DOUBLER TOP SURFACE. REMOVED DOUBLER, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SAA EA 011-5730-01-A1927 AND UPS EO MD11-5730-34402-A.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 42,373 hrs · 12,066 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQ 271-F1-02 FOUND GOUGED AND CORRODED EXTERNAL DOUBLER RT AFT FUSELAGE BETWEEN STA 2140 AND STA 2164, L33R AND L35R. REMOVED EXISTING REPAIR AT RT AFT FUSELAGE BETWEEN STA 2140 AND STA 2164, L33R TO L35R AND REPAIRED IAW MD11 SRM VOL 1 53-20-00 FIG 13 SHT 1-5.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 42,373 hrs · 12,066 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQ 271-F1-01 UPON FURTHER EVALUATION ON EFN 271LGPG10 03 NOT CORRELATED TO MD11 SRM 53-20-00 FIG 2 SHT 7. REMOVED EXISTING REPAIR AT FUS STA 1039-1059 L47L-L51L, FABRICATED AND INSTALLED REPLACEMENT REPAIR REF MD11 SRM VOL 1 53-20-00 FIG 2 SHT 5 AND APPLICABLE NOTES IN MD11 SRM VOL 1 53-20-00 PG 1.

Part: DOUBLER — DENTED (FUSELAGE) · airframe 42,373 hrs · 12,066 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQ 271-F1-03 FOUND DENT ON EXTERNAL DOUBLER STA 1921 AND STA 1926 L42L AND L45L. REMOVED EXISTING REPAIR AT AFT CARGO DOOR LOWER FWD CUTOUT FUS STA 1921-1926 AND L42L-L45L, FABRICATED AND INSTALLED REPLACEMENT REPAIR REF RCD 377549 AND MD11 VOL 1 53-50-00 FIG 17 VIEW B AND VIEW C.

Part: FITTING — CRACKED (LT WING) · airframe 39,790 hrs · 11,467 cycles

INSPECTION TYPE-C, LT WING LOWER WINGLET AFT FITTING FOUND CRACKED DURING BOROSCOPE INSPECTION. LT WING WINGLET FWD FITTING REMOVED IAW SRM 51-31-01 V.2R.40 & EOMD 11-57-20-27 680 APP.D. NEW FWD & AFT FITTINGS HOLES PICKED UP IAW SRM 51-31-01V.2 & EO MD11-5720-27680 APP D. NEW NUTPLATES INSTALLED ON FWD & AFT FITTINGS IAW SRM 51-31-01V.2R 40 & EOMD 11-5720-27680 APP D. OK TO INSTALL NEW FWD & AFT FITTING ON LT WING WINGLET.

Part: FITTING — CRACKED (LT WING TE FLAP) · airframe 39,790 hrs · 11,467 cycles

INSPECTION TYPE-C, LT WING OB FLAP STOP BOLT FITTING (SECOND RIB FROM IB) SUSPECT CRACK AS MARKED. HFEC INSP CARRIED OUT IAW NDT SPM R.13 PART 06.10.01.001 ON STOP BOLT FOUND CRACKED AS MARKED. CRACKED STOP BOLT FITTING & ATTACHED PARTS REMOVED IAW SRM 51-31-01V.2 & SRM 51-33-01V.2R.40. NEW STOP BOLT FITTING HOLES PICKED UP IAW SRM 51-31-01&51-33-01V.2R.40. NEW STOP BOLT FITTING PROTECTED IAW SRM 51-21-01V.2R.40. OK TO INSTALL NEW STOP BOLT FITTING.

Part: STRINGER — CRACKED (RT WING) · airframe 39,790 hrs · 11,467 cycles

INSPECTION TYPE-C, RT WING NR 3 FUEL TANK STRINGER NR 11 END SUSPECT CRACK AS MARKED. STR 11 SECTION CUT IAW SRM 57-20-00 FIG.10V.1R.40 & EN1277-08. HFEC C/OUT IAW NDT SPM R.13 PART 06-10-01.001 ON TRIMMED EDGE & FOUND NO CRACK EVIDENT. NEW STRINGER & REP PARTS FAB IAW SRM 57-20-00 FIG.10 V.1R.40. HOLES ON NEW STR 11 & REP PARTS P/UP IAW EN1277-08. NEW STR 11 & REP PARTS, CLIP & REP AREA FASTENERS OK TO INSTALL.

Part: STRINGER — CRACKED (LT WING) · airframe 39,790 hrs · 11,467 cycles

INSPECTION TYPE-C, LT WING FUEL TANK UPPER STRINGER 39 END SUSPECT CRACK. CRACK AT STR 9 LHW SLOTTED OUT IAW SRM 57-20-00 FIG10 V.1R.40.HFEC INSP C/OUT IAW NDTSPM R.13 PART 06-10-01.001 ON SLOTTED OUT AREA FOUND NO CRACK EVIDENT. REP PARTS FAB IAW SRM 57-20-00 FIG.10V.1R.40. REP PARTS HOLES P/UP IAW SRM 57-20-00 FIG.10V.1R.40. OK TO INSTALL REP PARTS STR 9 LT WING SPLICE END & FASTENER AT REPAIR AREA.

Part: STRINGER — CRACKED (RT WING) · airframe 39,790 hrs · 11,467 cycles

INSPECTION TYPE-C, RT WING NR 3 FUEL TANK STRINGER 10 END SUSPECT CRACK AS MARKED. CRACK AT STR 10 OF RHW TANK SLOTTED OUT IAW SRM 57-20-00 IFG.10V.1 R 40. HFEC INSP C/OUT IAW NDT SPM R.13 PART 06.10.01.001 ON SLOTTED A REA FOUND NO CRACK EVIDENT. REP PARTS FAB IAW SRM 57-20-00 FIG.10V.1R.40 REP PARTS HOLES P/UP IAW SRM 57-20-00 FIG.10V.1R.40. OK TO INSTALL REP PARTS STR 10 RHW SPLICE FASTENERS AT REPAIR AREA.

Part: STRUCTURE — CRACKED (RT WING) · airframe 39,790 hrs · 11,467 cycles

INSPECTION TYPE-C, RT WING ANTI-ICE TELESCOPIC DUCT, L/E CUT OUT AREA SUSPECT CRACK AT IB AND OB SIDE AS MARKED. HFEC INSP CARRIED OUT IAW DAC NDT SPM R.13,06-10-01.001 & FOUND CRACK AS MARKED. FASTENERS AT CRACKED AREA REMOVED IAW SRM57-31-01V.2 & SRM 57-33-01 V.2R.40. CRACKED AREA TRIMMED OUT IAW SRM 57-10-00 FIG.43V.1R.40. REP DOUBLER & FILLER FAB IAW SRM 57-10-00 FIG.43 V.1R.40. REP DOUBLER HEAT TREAT TO T62 IAW DPS 7.00-1, HARDNESS 83.83 FOUND WITHIN LIMIT IAW DPS 1.05.

Part: STRINGER — CRACKED (LT WING) · airframe 39,790 hrs · 11,467 cycles

INSPECTION TYPE-C, LT WING FUEL TANK UPPER STRINGER NR 11 END SUSPECT CRACK. STR NR11 SECTION CUT IAW SRM 57-20-00, FIG.10 V.1 REV.40 & EN1277-08. HFEC INSP C/OUT IAW NDT SPM R.13 PART 06-10-01.001 ON TRIMMED AREA FOUND NO CRACK EVIDENT. NEW STRINGER 11L & REP PARTS MACHINED IAW SRM 57-20-00 FIG. 10 V.1 R.40&EN1277-08 USING 10164 & 100425. HOLES ON NEW STR 11 & REP PARTS P/UP IAW EN1277-08. OK TO INSTALL NEW STR 11, REP PARTS, SPLICE END.

Part: ACTUATOR — FAULTY (AILERON)

INSPECTION TYPE:N/A ATB - ON DEPARTURE, LEVEL 2 AILERON DEFLECT DISAGREE. RAN CHECKLIST, LEVEL 2 ALERT RETURNED. T/S PERFORMED AS PER FIM 27-10-00-1 & A/C DATA OBTAINED FROM AMC. FOUND LOB AILERON DEFLECTION ACTUATOR AT FAULT. SAME REPLACED AS PER MM 27-16-00. ALL WITHIN LIMITS.

Part: ACTUATOR — WARNING LIGHT (AILERONS)

ATB - AILERON DEFLECT DISAGREE ALERT ON FLAP RETRACTION. A/C ROLLED RT WITH FLAPS UP. NO EMERGENCY DECLARED. R&R RH I/B AILERON DEFLECT ACTUATOR PER AMM 27-16-01-4 AND FUNCTION TEST C/W PER AMM 27-16-00-5. RESULT NORMAL.

Part: LIGHT — INOPERATIVE (R1 ENTRY DOOR)

INSPECTION TYPE:N/A R1 MAIN ENTRY DOOR SLIDE REMOTE PRESS IND TEST INOP. RELAMPED AND CHECKED NORMAL.

Part: FITTING — DAMAGED (SLAT TRACK) · airframe 35,860 hrs · 10,778 cycles

INSPECTION TYPE:3C LEFT O/B SLAT TRACK FITTING DAMAGED BY SLAT CABLE BETWEEN 5 & 6 SLATS. REPAIRED DAMAGED AREA IAW SAA EA 011-5710-01-A0765 & UPS RAA MD-11-57-20106.

Part: ATTACH FITTING — CRACKED (LT WING LE) · airframe 35,860 hrs · 10,778 cycles

INSPECTION TYPE:3C LEFT WING FIXED LEADING EDGE I/B SLAT TRACK FITTING AT STA XOS 1005 IS CRACKED. REMOVED AND REPLACED LEFT WING FIXED LEADING EDGE I/B SLAT TRACK FITTING AT XOS 1005 IAW MD-11 SRM 51-31-01 & 51-35-01.

Part: ATTACH FITTING — CRACKED (RT WING LE) · airframe 35,860 hrs · 10,778 cycles

INSPECTION TYPE:3C RIGHT WING LEADING EDGE O/B SLAT TRACK NR 5 FITTING IS CRACKED. REMOVED AND REPLACED SLAT TRACK FITTING IAW MD-11 SRM 51-31-01 & 51-35-01.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

FUEL QTY/USED CHK ALERT ILLUMINATED ABOUT 1 HOUR INTO FLIGHT. RUN CHECKLIST AND ISOLATED PROBLEM FUEL LEAK IN TAIL 3500LB DISCREPANCY BETWEEN FUEL BURNED AND FUEL ONBOARD AT BEGINNING OF RUNNING CHECKLIST. REMOVED AND REPLACED TANK 2 RT SIDE COMPENSATOR IAW AMM 28-41-37-4. OPS CHECKED SATIS FUEL QTY TEST CHECKED SATIS. CONNECTOR REINSTALLED SECURED. THIS CLOSES DMI.

Part: SWITCH — INOPERATIVE (L1 DOOR SLIDE)

L1 DOOR SLIDE SWITCH INOP DEFERRED PER MEL 25-61-2. DMP 25-61-2. C/W DOOR SLIDE BOTTLE PRESSURE. VERIFIED IN THE GREEN BAND PRIOR TO DEP FROM PVG. PLACARD INSTALLED. RELAMPED. OPS CHECK GOOD IAW 33-00-00. PLACARD FOR M336276 REMOVED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

LEFT ENTRY DOOR FORWARD EMERGENCY EXIT LIGHT HAS ONE LIGHT OUT. REMOVED AND REPLACED BULB LIGHT. OPS CHECK NORMAL.

Part: GIRT BAR — LOOSE (L1 DOOR)

L1 DOOR GIRT BAR LOOSE. INSTALLED AND SECURED L1 DR GIRT BAR PUSHROD IAW AMM 25-61-01-4.

Part: INDICATOR — INOPERATIVE (COCKPIT)

APPROX T/O 2+30 RECEIVEDD FLASHING IAS COMPARATOR WARNING AND ATS AUTO-PILOT DISENGAGED. OTHER A/PILOT WORKED TEMP UNTIL SAME INDICATIONS AT SAME TIME REC'D FLAP LIMIT ELEV FEEL & WINDSHEAR INOP. PURGED PITOT STATIC SYSTEM CAPTS, F/O AND AUX PER MM 34-11-00; REMOVED AND REPLACED NR 1 CADC PER AMM 34-16-01-4; OPS CHECK GOOD PER 34-16-01-5, P/N 4059060- 901, S/N ON 91070371, S/N OFF 95110701; REMOVED AND REPLACED CAPT & F/O PITOT TUBES PER AMM 34-11-01-02; C/W PITOT STATIC SYSTEM HEATER TEST PER AMM 30-32-00 PER QC REQUEST; SYSTEM OPS CHECK GOOD.

Part: FIRE DETECTOR — FAULTED (NR 3)

INSPECTION TYPE:N/A ON POST FLIGHT FOUND NR 3 FIRE DET FAULT. NEW -A- LOOP PARTIALLY INSTALLED 1848269 REQUIRES COMPLETION & OPS CK FINISHED. INSTALLATION OF -A- LOOP AND OPS CKS GOOD IAW MM 26-11-03. THIS CLEARS M327541.

Part: DOOR — INOPERATIVE (L1)

L1 ENTRY DOOR INOP (CREW PRE-FLT 0038).

Part: ODOR — DETECTED (ACM)

STRONG, ACRID, SULFUROUS ODOR NOTICED BY ACM IN CREW REST MODULE APPROX 1 HOUR INTO FLT. ODOR WAS NOTICED IN COCKPIT WHEN CREW REST MODULE DOOR WAS OPENED. DISSIPATED AFTER 15 MIN. CLEANED UP BY VENDOR, NO ABNORMALITIES FOUND. CONDITION CK'D NORMAL.

Part: FRAME — CORRODED (BS 1801 L52) · airframe 31,968 hrs · 10,123 cycles

INSPECTION TYPE:C2 BILGE STA 1801, LONGERON 52 (BL 0), UPPER CHORD OF FRAME HAS CORROSION AROUND FASTENER. REMOVED CORROSION IAW MD-11 SRM 51-21-01. NDT VERIFIED MATERIAL AFTER CORROSION WAS REMOVED TO BE .070" TO .066" PER NDT SPM 04-00-06. MATERIAL IS WITHIN LIMITS IAW MD-11 SRM 53-00-01 FIG 3. TREAT AND PRIMED IAW MD-11 SRM 51-21-01.

Part: SMOKE GOGGLES — TORN (COCKPIT)

RT COURIER SEAT SMOKE GOGGLE TORN. ORDERED POUCH TO P1 SHELF REPLACED POUCH FOR SMOKE GOGGLE AT RT COURIER SEAT AS REQ FOR SERVICE.

Part: LIGHT — INOPERATIVE (R1 DOOR SLIDE)

R1 DOOR EVAC SLIDE PRESS TO RESET LT INOPERATIVE. RELAMPED AND TESTED SYSTEM PER MM 25-61-04-1. SYS CHECK NORMAL. PLACARD REMOVED.

Part: ELT — ACTIVATED (R-1 DOOR SLIDE)

SUSPECT AIRCRAFT IS TRANSMITTING AN ELT SIGNAL. CONTINUOUS RECEPTION ON 121.5 FROM SDF TO ANC. FOUND R-1 DOOR SLIDE ELT ACTIVATED. REMOVED AND REPLACED R-1 DOOR SLIDE PER AMM 25-61-01. OPS CHECK GOOD.

Part: WARNING LIGHT — ILLUMINATED (R1 SLIDE)

INSPECTION TYPE:N/A, R1 SLIDE LOW PRESS LIGHT INOP. VERIFIED SYS PRESS, OK FOR SERVICE PER DMP 25-61-2.

Part: WINDOW — LEAKING (COCKPIT)

INSPECTION TYPE:N/A 57 MIN INTO FLIGHT, FELT EARS POP AND LOUND NOISE IN COCKPIT FROM F/O WINDOW. F/O WINDOW RE-RIGGED IAW FIM 56-12-01. CLEARANCES SPECIFIED ARE WITHIN LIMITS. LOADS SPECIFIED ARE WITHIN LIMITS. CANNON PLUG ON F/O CLEAR VIEW DEFOG RESEATED.

Part: WINDOW — LEAKING (COCKPIT)

57 MINUTES INTO FLIGHT AT FL320, FLIGHT AIR NOISE EMANATING FROM UPPER LEFT CORNER OF R2 WINDOW. AT 66 MINUTES INTO FLIGHT NOISE BECOMES A WHISTLE SOUND. SOUND BECAME INTERMITTENT FOR REMAINDER OF FLIGHT. REMOVED AND REPLACED RT SLIDING WINDOW AS PER MM 56-12-01. PERFORMED ADJ/TEST IAW MM 56-12-01 PG 501. FOUND SATISFACTORY. THIS CLEARS D281995.

Part: SMOKE GOGGLES — CRACKED (COCKPIT)

RT SUPERNUMERARY SEAT HAS CRACKED SMOKE GOGGLES. REMOVED AND REPLACED SMOKE GOGGLES FOR RIGHT HAND SUPERNUMERARY SEAT.

Part: AXLE — GOUGED (LT MLG)

INSPECTION TYPE:N/A NR 1 AXEL ON LEFT MLG GOUGED ***MRR FILED OPEN***

Part: SKIN — CORRODED (ZONE 316) · airframe 25,166 hrs · 8,794 cycles

INSPECTION TYPE: C, AFT ACCESSORY COMPT ZONE 316 RT FAIRING ATTACHMENT ANCHOR NUT SKIN FOUND CORRODED. RT FAIRING ATTACHMENT ANCHOR NUT SKIN REMOVED AND FOUND OUT OF LIMIT PER SRM 53-00-01 VOL I REV 32. CORROSION BLEND OUT AREA TRIMMED PER EN:10 06-03. HFEC INSP CARRIED OUT PER NDT SPM REV 10 06-10-01-001 & NO CRACKS EVIDENT. FABRICATED REPAIR PARTS, PROTECTED AND INSTALLED AS PER EN: 1006-03.

Part: SUPPORT — CORRODED (RT AILERON) · airframe 25,166 hrs · 8,794 cycles

INSPECTION TYPE: RT WING FWD INBOARD AILERON FOUND CORROSION AT PANEL SUPPORT FROM ST A XW=291 TO XW=373 AS MARK. CORROSION ON PANEL SUPPORT RT WING STA XW291 TO XW373 REMOVED AND PROTECTED IAW SRM 51-21-01 VOLIIREV32. FOUND OUT OF LIMIT IAW SRM 57-00-0 1 VOLIREV 32.OUT OF LIMIT AREA AT PANEL SUPPORT TRIMMED IAW EN1005-0 3. TEE CAP AND REPAIR ANGLES FABRICATED IAW EN1005-03. TEE CAP AND REPAIR ANGLES AND TEE ANGLE INSTALLED IAW EN1005-03.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,166 hrs · 8,794 cycles

INSPECTION TYPE:C SEAT TRACK AT RBL 27.5 BETWEEN STA 791-840 FOUND CORRODED. CORROSION REMOVED AT SEAT TRACK RBL 27.5 STA 791-840 FOUND EXCEED LIMIT AS PER SRM 51-21-01 VOL II REV 32 & 53-70-00 VOL I REV 32. NEW SEAT TRACK & SPLICE REWORKED AS PER SRM 53-70-00 VOL I REV 32, HOLES PICK OUT AND PROTECTED AS PER SRM 51-21-01 VOL II REV 32 & NEW SEAT TRACK & SPLICE FITTING INSTALLED AS PER 53-70-00 VOL I REV 32 AT STA 791-840 RBL 27.5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,166 hrs · 8,794 cycles

INSPECTION TYPE:C SEAT TRACK AT LBL 8.5 BETWEEN 879-899 FOUND CORRODED. CORROSION REMOVED AT STA 879-899 LBL 8.5 & FOUND EXCEED LIMIT AS PER SRM 53-70-00 VOL I REV 32 & 51-21-01 VOL II REV 32. NEW SEAT TRACK & SPLICE FITTING REWORK & HOLES PICKOUT AS PER SRM 53-70-00 VOL I REV 32, PROTECTED AS PER SRM 51-21-01 VOL II REV 32 & NEW SEAT TRACK & SPLICE FITTING INSTALLED AS PER SRM 53-70-00 VOL I REV 32 AT STA 879-899 AT LBL 8.5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,166 hrs · 8,794 cycles

INSPECTION TYPE:C SEAT TRACK AT RBL 8.5 BETWEEN STA 784-939 FOUND CORRODED. CORROSION REMOVED AT SEAT TRACK RBL 8.5 STA 784-939 & FOUND EXCEED LIMIT AS PER SRM 51-21-01 VOL II REV 32 & 53-70-00 VOL I REV 32. NEW SEAT TRACK REWORKED AND HOLES PICK UP AS PER SRM 53-70-00 VOL I REV 32, PROTECTED AS PER SRM 51-21-01 VOL II REV 32 & NEW SEAT TRACK FASTENER INSTALLED AS PER 53-70-00 VOL I REV 32 STA STA 784-939 RBL 8.5

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,166 hrs · 8,794 cycles

INSPECTION TYPE:C SEAT TRACK AT LBL 8.5 BETWEEN STA 791-840 FOUND CORRODED. CORROSION REMOVED AT STA 791-840 LBL 8.5 & FOUND EXCEED LIMIT AS PER SRM 51-21-01 VOL II REV 32 & 53-70-00 VOL I REV 32. NEW SEAT TRACK REWORKED AND HOLES PICKED OUT AS PER AS PER SRM 53-70-00 VOL I REV 32, PROTECTED PER SRM 51-21-01 VOL II REV 32 & NEW SEAT TRACK INSTALLED AS PER SRM 53-70-00 VOL I REV 32 AT STA 791-840 LBL 8.5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,166 hrs · 8,794 cycles

INSPECTION TYPE:C SEAT TRACK AT LBL 8.5 BETWEEN STA 1268-1275 FOUND CORRODED. CORROSION REMOVED AT SEAT TRACK LBL 8.5 AT STA 1268-1275 & FOUND EXCEED LIMIT AS PER SRM 51-21-01 VOL II REV 32 & 53-70-00 VOL I REV 32. NEW SEAT TRACK REWORKED & HOLES PICK OUT AS PER SRM 53-70-00 VOL I REV 32, PROTCTED AS PER SRM 51-21-01 REV 32 VOL II & NEW SEAT TRACK INSTALLED AS PER SRM 51-33-01 VOL II REV 32 AT STA 1268-1275 LBL 8.5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,166 hrs · 8,794 cycles

INSPECTION TYPE: C, SEAT TRACK AT LBL 27.5 BETWEEN STA 824-840 FOUND CORRODED. CORROSION REMOVED AT SEAT TRACK LBL 27.5 AT STA 824-840 FOUND EXCEED LIMIT PER SRM 51-21-01 VOL II REV 32 & 53-70-00 VOL I REV 32. NEW SEAT TRACK & SPLICE REWORKED & HOLES PICK OUT AS PER SRM 53-70-00 VOL I REV 32 & PROTECTED AS PER SRM 51-21-01 VOL II REV 32. NEW SEAT TRACK & SPLICES INSTALLED AS PER SRM 51-33-01 VOL II REV 32 AT STA 824-840 LBL 27.5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,166 hrs · 8,794 cycles

INSPECTION TYPE:C GALLEY FLOORBEAM SUPPORT AT LBL 46 STA 2007 ATTACHMENT FOUND CORRODED. CORROSION AREA REMOVED AT LBL 46 STA 2007 GALLEY FLOORBEAM SUPPORT FOUND EXCEED LIMIT PER SRM 51-21-01 VOL II & 53-00-01 VOL I REV 32. NEW T-CHORD & SPLICE FABRICATED AS PER SRM 53-40-00 VOL I FIG 6 REV 32. SPLICE ANGLE HEAT TREATED AS DPS700-1. NEW T-CHORD & SPLICE ANGLE HOLES PICK OUT PER SRM 51-31-01 VOL II REV 32 & INSTALLED PER 53-40-00 VOL I FIG 6 REV 32.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,166 hrs · 8,794 cycles

INSPECTION TYPE:C SEAT TRACK AT LBL 67 STA 2007 ATTACHMENT BOLT HOLE FOUND CORRODED. CORRODED SEAT TRACK FASTENER REMOVED & SPLICE CUT CARRIED OUT AT ST A1751 X=67 PER SRM 53-70-00 FIG 1 VOL I REV 32. NEW SEAT TRACK AFA7789545 HOLES PICK UP & SPLICE HAT, SPLICE PLATE FABRICATED PER SRM 53-70-00 FIG 1 VOL I & NEW SEAT TRACK AFA7789-545, SPLICE HAT & PLATE INSTALLED AT CABIN STA 1751-2007 X=67 PER SRM 53-70-00 FIG 1 VOL I REV 32.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,166 hrs · 8,794 cycles

INSPECTION TYPE: C, SEAT TRACK AT RBL 75.5 STA 914-946 FOUND CORRODED. CORROSION REMOVED AT SEAT TRACK AT RBL 75.5 STA 914-946 AS PER SRM 51-2 1-01 VOL II REV 32 & FOUND EXCEED LIMIT. NEW SEAT TRACK & SPLICES REWORK AS PER SRM 53-70-00 VOL I REV 32 & HOLES PICKED OUT AS PER SRM 51-21-01 VOL 11 REV 32. NEW SEAT TRACK AND SPLICES INSTALLED AS PER SRM 51-33-01 VOL II REV 32 AT STA 914-946 RBL 75.5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,166 hrs · 8,794 cycles

INSPECTION TYPE:C SEAT TRACK AT RBL 27.5 BETWEEN STA 1264-1273 FOUND CORRODED. CORROSION REMOVED AT SEAT TARCK STA 1264-1273 RBL 27.5 & FOUND EXCEED LIMIT PER SRM 53-70-00 VOL I & 51-21-01 VOL II REV 32. NEW SEAT TRACK REWORKED & HOLES PICKED OUT AS PER SRM 53-70-00 VOL I REV 32, NEW SEAT TRACK PROTECTED AS PER SRM 51-21-01 VOL II REV 32 & NEW SEAT TRACK INSTALLED AS PER SRM 53-70-00 VOL I REV 32 AT STA 1364-1273 RBL 27.5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,166 hrs · 8,794 cycles

INSPECTION TYPE:C SEAT TRACK AT RBL 8.5 BETWEEN STA 1273-1289 FOUND CORRODED. CORROSION REMOVED AT SEAT TRACK STA 1273-1289 RBL 8.5 & FOUND EXCEED LIMIT PER SRM 53-70-00 VOL I REV 32 & 51-21-01 VOL II REV 32. NEW SEAT TRACK REWORKED & HOLES PICK OUT AS PER SRM 53-70-00 VOL I REV 32, SEAT TRACK PROTECTED PER SRM 51-21-01 REV 32 VOL II & NEW SEAT TRACK INSTALLED AS PER SRM 51-33-01 VOL II REV 32 AT STA 1273-1289 RBL 8.5.