N296UP

Part: BATTERY — INOPERATIVE (CABIN) · airframe 87,173 hrs · 16,050 cycles

INSPECTION TYPE:NA**SUPPLEMENTAL SDR** EMER LT BATT 1 LO ON PREFLIGHT.REPLACED POWER SUPPLY IAW MM 33-51-01-400-802. OPS CHECK GOOD. THIS CLEARS 782460.

Part: DOOR — INOPERATIVE (DOORS) · airframe 87,155 hrs · 16,047 cycles

INSPECTION TYPE:NAL1 DOOR WAS ON DEFERAL CREW OPENED DOOR UNABLE TO CLOSE BOTH FWD AND AFT LOWER CABLES BROKENINSTALLED FWD & AFT LOWER CABLES ON L1 DOOR PER AMM 52-11-03-400-801 OPS CHECK GOOD

Part: CABLE — BROKEN (L1 DOOR) · airframe 87,146 hrs · 16,042 cycles

L1 DOOR AFT CABLE BROKE.INSTALLED FWD & AFT LOWER CABLES ON L1 DOOR PER AMM 52-11-03-400-801. OPS CHECK GOOD.

Part: SKIN — NONE (RH AC DOOR C/O) · airframe 86,437 hrs · 15,660 cycles

INSPECTION TYPE:N/ART AC DOOR SKIN CUTOUT CRACKED.REPAIRED IAW EO MD11-5330-81636

Part: DOUBLER — CHAFED (BS 1958-1997) · airframe 86,332 hrs · 15,610 cycles

INSPECTION TYPE:S/VINTERNAL DOUBLER HAS DAMAGED HOLES AND CHAFE DAMAGE BETWEEN STA. 1958 TO 1997 AND BETWEEN L48L TO 50L.REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG. AGA7167 AND SRM 51-33-01. (MINOR)

Part: DOUBLER — DAMAGED (BS 1975-1986) · airframe 86,332 hrs · 15,610 cycles

INSPECTION TYPE:SVAFT FUSELAGE SKIN DOUBLER HAS 3EA ELONGATED HOLES BETWEEN STA.1975-1986 LON 48L-49L.REPAIRED 3EA ELONGATED HOLES AT AFT FUSELAGE SKIN DOUBLER BETWEEN STA.1975-1986 LON 48L-49L IAW VT-SAA EA 011-5330-01-A9341 REV I/R AND UPS EO MD11-5330-81536-A (MINOR).

Part: TEAR STRAP — DAMAGED (BS 1921 L50-52L) · airframe 86,332 hrs · 15,610 cycles

INSPECTION TYPE:SV, TEAR STRAP AT STA 1921 BETWEEN LONGERONS 50L & 52 IS CREASED.REPAIRED CREASED TEAR STRAP AT STA 1921 BETWEEN LONGERONS 50L & 52 IAW SRM 53-00-07, REPAIR 1, FIGURE 201. (MAJOR)

Part: SHEAR TIE — CORRODED (BS 1996 L48-50R) · airframe 86,332 hrs · 15,610 cycles

INSPECTION TYPE:SVAFT FUSELAGE SHEAR CLIP HAS EXFOLIATED CORROSION AT STA. Y=1996.75 BETWEEN LON 48R AND LON 50RREMOVED,FABRICATED AND REPLACED CORRODED SHEAR CLIP AT STA. Y=1996.75 BETWEEN LON 48R AND 50R IAW SRM 51-35-01 (MINOR)

Part: SHEAR TIE — DAMAGED (BS 1926 S51-52L) · airframe 86,332 hrs · 15,610 cycles

INSPECTION TYPE:SVAFT FUSELAGE SHEAR TIE HAS AN EXTRA DAMAGE FASTENER HOLE AT STA.1926 BETWEEN LON 51L AND LON 52.REMOVED,FABRICATED AND REPLACED AFT FUSELAGE DAMAGED SHEAR TIE AT STA.1926 BETWEEN LON 51L AND LON 52 IAW SRM 51-33-01 (MINOR).

Part: TEAR STRAP — BROKEN (BS 1942 L50-52L) · airframe 86,332 hrs · 15,610 cycles

INSPECTION TYPE:SVTEAR STRAP AT STA 1942 BETWEEN LONGERONS 50L & 52 IS BROKEN.REPAIRED BROKEN TEAR STRAP AT STA 1942 BETWEEN LONGERONS 50L & 52 IAW SRM 53-00-07, REPAIR 1, FIGURE 201. (MAJOR)

Part: BULKHEAD WEB — DEFLECTION (BS 2007) · airframe 86,332 hrs · 15,610 cycles

INSPECTION TYPE:S/VAFT PRESSURE BULKHEAD WEB HAS DEFLECTION DAMAGE COMMON TO AN EXISTING REPAIR AT STA. 2007 AND BETWEEN X= -10 TO X=10.REPAIRED DAMAGED AFT PRESSURE BULKHEAD WEB AT STA. 2007 AND BETWEEN X= -10 TO X=10 IAW VT-SAA EA 011-5310-01-A9340 REV. I/R AND UPS EO MD11-5310-81567-A. (MAJOR) REF 8100-9 BY S. KANG DATED 9/10/2021.

Part: FILLER — CHAFED (BS 2007 L45L-R) · airframe 86,332 hrs · 15,610 cycles

INSPECTION TYPE:S/VAFT FUSELAGE SKIN FILLER HAS CHAFE DAMAGE AT STA. 2007 AND BETWEEN LONG. 45L TO 45R.REMOVED, FABRICATED AND REPLACED FILLER IAW DWG. AJC7204 AND SRM 51-33-001 & 51-35-01. (MINOR)

Part: DOUBLER — CHAFED (BS 2007-2033) · airframe 86,332 hrs · 15,610 cycles

INSPECTION TYPE:S/VAFT FUSELAGE INTERNAL PRODUCTION DOUBLER HAS CHAFE DAMGE BETWEEN STA. 2007 TO 2033 AND BETWEEN LONG. 45L TO 45R.REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG. AJC7207 AND SRM 51-33-01 & 51-35-01. (MINOR)

Part: LONGERON — DAMAGED (BS1937-1959 L51L) · airframe 86,332 hrs · 15,610 cycles

INSPECTION TYPE:SVAFT CARGO COMPARTMENT LON 51L HAS CHAFE DAMAGE BETWEEN STA.1937.50 TO STA.1959.REPAIRED CHAFED LON 51L BETWEEN STA.1937.50 TO 1959 IAW VT-SAA EA 011-5310-01-A9316 REV I/R AND UPS EO MD11-5310-81418-A (MINOR).

Part: SHEAR TIE — DAMAGED (BS 1942 L51-52L) · airframe 86,332 hrs · 15,610 cycles

INSPECTION TYPE:SVAFT FUSELAGE SHEAR CLIP DAMAGE AT STA. Y=1942.00 BETWEEN LON 51L AND LON 52L.REPAIRED AFT FUSELAGE DAMAGED SHEAR CLIP AT STA. Y=1942.00 BETWEEN LON 51L AND LON 52L IAW SRM 53-00-06 REPAIR 1 FIG 201 REV 68 (MAJOR)

Part: FORMER — CRACKED (RT WING LE) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CRT WING FIXED L/E FORMER AT XOS 912 IS CRACKED.REMOVED AND REPLACED CRACKED RT WING FIXED L/E FORMER AT XOS 912 IAW SRM 51-33-01 & 51-35-01. (MINOR)

Part: TEE FITTING — CRACKED (RT WING TE FLAP) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CRT WING O/B FLAP I/B AFT HINGE FAIRING STRUCTURE TEE BEAM IS CRACKED.REMOVED AND REPLACED CRACKED RT WING O/B FLAP I/B AFT HINGE FAIRING STRUCTURE TEE BEAM IAW SRM 51-33-01 & 51-35-01. (MINOR)

Part: DOUBLER — CRACKED (R/H WING) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CR/H WING FIXED L/E LOWER STRINGER EXISTING REPAIR DOUBLER IS CRACKED AT STA. XOS. 906.5607.REMOVED AND REPLACED CRACKED R/H WING FIXED L/E LOWER STRINGER REPAIR DOUBLER AT STA. XOS. 906.5607 IAW SRM 57-40-03 REPAIR 1 FIG. 201. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CRT WING FIXED L/E SKIN SPLICE DOUBLER AT XOS 906.561 IS CRACKED.REMOVED AND REPLACED CRACKED RT WING FIXED L/E SKIN SPLICE DOUBLER AT XOS 906.561 IAW SRM 51-33-01. (MINOR)

Part: FLOORBEAM — CRACKED (FWD CARGO) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CFORWARD CARGO COMPARTMENT FLOOR BEAM CRACK AT STA.Y= 6-70,X= -57.5 AND Z= -98.REPAIRED CRACKED FWD CARGO COMPT FLOOR BEAM IAW SRM 53-40-51,REPAIR 1,FIG 202,REV 67

Part: FLOORBEAM — CRACKED (FWD CARGO) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CFWD LOWER CARGO FLOOR BEAM AT STA 6-70 & X= 57.50 IS CRACKED.REPAIRED CRACKED FWD LOWER CARGO FLOOR BEAM AT STA 6-70 & X= 57.50 IAW VT-SAA EA 011-5340-01-A9215 REV. IR AND UPS EO MD11-5310-80984-A. REF. FAA FORM 8100-9 SIGNED BY: STEPHEN KANG (AR-605677) DATED 07/12/2021. (MAJOR)

Part: STRINGER — CRACKED (R/H WING) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CR/H WING FIXED L/E UPPER STRINGER IS CRACKED AT STA. XOS. 908.REPAIRED CRACKED R/H WING FIXED L/E UPPER STRINGER BETWEEN STA. XOS. 901.5 TO 912.0 IAW SRM 57-40-03 REPAIR 2 FIG. 202. (MAJOR)

Part: FLOOR PANEL — DELAMINATED (E/E BAY) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CAVIONICS COMPARTMENT FLOOR PANEL DELAMINATED AT AFT CENTER.REMOVED,FABRICATED AND REPLACED AVI COMPT DELAMINATED FLOOR PANEL IAW VT-SAA EA 011-5330-01-A9207 REV I/R AND UPS EO MD11-5330-80933-A (MAJOR).

Part: STRINGER — CRACKED (CENTER BOX) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CCENTER WING BOX STRINGER # 50 IS CRACKED AT STA. XCW -17.REPAIRED CRACKED CENTER WING BOX STRINGER #50 BETWEEN STA. XCW= -5.0 TO 29.0 IAW SRM 57-10-03 REPAIR 1 FIG. 201. (MAJOR)

Part: STRINGER — CRACKED (CENTER WING BOX) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CCENTER WING BOX STRINGER #49 IS CRACKED AT STA. XCW= 17.0.REPAIRED CRACKED CENTER WING BOX STRINGER #49 BETWEEN STA. XCW= 3 TO XCW= 32 IAW SRM 57-10-03 REPAIR 1 FIG. 201. (MAJOR)

Part: DOUBLER — CHAFED (TAIL CONE) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CTAIL CONE R/H UPPER INTERNAL PRODUCTION DOUBLER IS CHAFED.REPAIRED CHAFED TAIL CONE R/H UPPER INTERNAL PRODUCTION DOUBLER IAW UPS EO MD11-5350-66790-B APPENDIX A. (MINOR)

Part: FLOORBEAM — CORRODED (BS 421) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CFWD MAIN CABIN LAV FLOOR SUPPORT HAS HEAVY CORROSION AT STA Y=421.578 BETWEEN X=-65 & X=-81.REMOVED,FABRICATED AND REPLACED CORRODED FLOOR SUPPORT IAW SRM 51-31-01 (MINOR).

Part: FLOOR PANEL — CORRODED (FWD MAIN CABIN) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CFLOOR PANEL WSP0785-501 HAS CORROSION AT POS 4 BETWEEN STA.475-500 AND X=19 TO X=27.REPAIRED CORRODED FLOOR PANEL IAW VT-SAA EA 011-5310-01-A9206 REV I/R AND UPS EO MD11-5310-80887-A (MINOR).

Part: STIFFENER — CORRODED (BS 470) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CAFT AVI COMPT VERTICAL STIFFENER AT STA 470 BULKHEAD BELOW SERVICE DOOR IS CORRODED.REMOVED AND REPLACED CORRODED AFT AVI COMPT VERTICAL STIFFENER AT STA 470 BULKHEAD BELOW SERVICE DOOR IAW SRM 51-33-01. (MINOR)

Part: VENTILATOR PANEL — CRACKED (#1 PYLON) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2C#1 PYLON PANEL 437CR VENTILATOR ASSY IS CRACKED.REPAIRED CRACKED #1 PYLON VENTILATOR ASSY IAW VT-SAA EA 011-5430-01-A9223 REV. IR AND UPS EO MD11-5460-80982-A. REF. FAA FORM 8100-9 SIGNED BY: STEPHEN KANG (AR-605677) DATED 07/12/2021. (MAJOR)

Part: FRAME ANGLE — CRACKED (CARGO) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CCENTER CARGO FRAME ANGLE AT STA 5-113 AND LONGERON 41L IS CRACKED.REMOVED AND REPLACED CRACKED CENTER CARGO FRAME ANGLE AT STA 5-113 AND LONGERON 41L IAW SRM 51-33-01 & 51-35-01. (MINOR)

Part: FLAP — CRACKED (RT WING) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CRT WING O/B FLAP I/B AFT HINGE INTERNAL FITTING HAS A 3" CRACK.REMOVED AND REPLACED CRACKED RT WING FLAP ASSY IAW AMM 27-50-30. (MINOR)

Part: SUPPORT ANGLE — CORRODED (BS 1841 S43L-R) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CAFT CARGO STEP UP BULKHEAD SUPPORT ANGLE CORRODED AT STA.1841 BETWEEN STR 43L &STR 43R.REPAIRED CORRODED SUPPORT ANGLE IAW VT-SAA EA 011-5100-01-A9205 REV I/R AND UPS EO MD11-5100-80871-A (MINOR).

Part: SKIN — CORRODED (RT WING T/E) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CRT WING UPPER SURFACE T/E SKIN CORRODED BETWEEN XORS =779.5-XORS =819.5.REPAIRED CORRODED RT WING UPPER T/E SKIN IAW EA 011-5730-01-A9221 REV I/R AND UPS EO MD11-5710-80892-A (MINOR).

Part: STIFFENER — CRACKED (BS 1841 L47R) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CAFT CARGO STA 1841 BULKHEAD STIFFENER ABOVE LONGERON 47R IS CRACKED.REMOVED AND REPLACED CRACKED AFT CARGO STA 1841 BULKHEAD STIFFENER ABOVE LONGERON 47R IAW SRM 51-33-01. (MINOR)

Part: FRAME ANGLE — CRACKED (BS 1541) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CCENTER CARGO FRAME ANGLE AT STA 1541 AND LONGERON 41L IS CRACKED.REMOVED AND REPLACED CRACKED CENTER CARGO FRAME ANGLE AT STA 1541 AND LONGERON 41L IAW SRM 51-33-01 & 51-35-01. (MINOR)

Part: SUPPORT CHANNEL — CRACKED (VERTICAL-FUSE) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CVERTICAL STAB TO FUSELAGE SUPPORT CHANNEL AT YID 310.35 IS CRACKED.REMOVED AND REPLACED CRACKED VERTICAL STAB TO FUSELAGE SUPPORT CHANNEL AT YID 310.35 IAW SRM 51-35-01. (MINOR)

Part: STIFFENER — CRACKED (BS 1841 L49R) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CAFT CARGO STA 1841 BULKHEAD STIFFENER ABOVE LONGERON 49R IS CRACKED.REMOVED AND REPLACED CRACKED AFT CARGO STA 1841 BULKHEAD STIFFENER ABOVE LONGERON 49R IAW SRM 51-33-01. (MINOR)

Part: RIB — CRACKED (RH MLG W/W) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CRH MLG W/W CUT-OUT RIB CRACK AT FWD O/B JAMB.REMOVED,FABRICATED AND REPLACED CRACKED RIB IAW SRM 51-31-01 AND 51-35-01 (MINOR).

Part: STIFFENER — CRACKED (AFT CARGO) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CAFT CARGO COMPARTMENT STEP UP BULKHEAD STIFFENER CRACK AT STA.1841 STRINGER 46R.REMOVED,FABRICATED AND REPLACED CRACKED STIFFENER IAW SRM 51-33-01 AND 51-31-01 (MINOR).

Part: SKIN — CORRODED (RT WING) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2C, RT WING UPPER SURFACE BETWEEN XORS 97 - XORS 130.4 AND BETWEEN STRINGER 11 & 15 IS CORRODED AROUND FASTENERS.REPAIRED CORRODED RT WING UPPER SURFACE BETWEEN XORS 97 - XORS 130.4 AND STRINGER 11 & 15 IAW EA 011-5730-01-A9216 REV. IR AND UPS EO MD11-5730-80893-A.

Part: SKIN — CRACKED (RT WING) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CRT WING FIXED L/E SKIN IS CRACKED AT SLAT TRACK #14 CUT OUT STA. XOS 891.REPAIRED CRACKED RT WING FIXED L/E SKIN AT SLAT TRACK #14 CUT OUT STA. XOS 891 IAW SRM 57-40-02, REPAIR 7, FIGURE 201. (MAJOR)

Part: SKIN — GOUGED (RT WING) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CRT WING FIXED L/E SKIN UPPER SURFACE BETWEEN XOS 1160 - XOS 1185 IS GOUGED.REPAIRED GOUGED RT WING FIXED L/E SKIN UPPER SURFACE BETWEEN XOS 1160 - XOS 1185 IAW VT-SAA EA 011-5730-01-A9224 REV. IR AND UPS EO MD11-5720-80959-A. (MINOR)

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 86,278 hrs · 15,581 cycles

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

Part: SPAR CAP — CORRODED (LT WING) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CLT WING UPPER T/E PANEL IS BULGED AT REAR SPAR JUST O/B OF #5 SPOILER.REPAIRED CORRODED LT WING REAR SPAR UPPER CAP AFT FLANGE BETWEEN XORS 787 - XORS 826 IAW VT-SAA EA 011-5710-01-A9201 REV. IR AND UPS EO MD11-5710-80889-A. (MINOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CRT WING FIXED L/E BEADED DOUBLER BETWEEN XOS 783 - 789 IS CRACKED.REPAIRED CRACKED RT WING FIXED L/E BEADED DOUBLER BETWEEN XOS 783 - 789 IAW SRM 57-40-02, REPAIR 15, FIGURE 205. (MAJOR)

Part: FORMER — CRACKED (RT WING) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CRT WING FIXED L/E FORMER CRACK JUST I/B OF #9 SLAT TRACK.REMOVED,FABRICATED AND REPLACED CRACKED FORMER IAW SRM 51-33-01 AND 51-31-01 (MINOR).

Part: DOUBLER — CRACKED (RT WING LE) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CRT WING FIXED L/E BEADED DOUBLER BETWEEN XOS 559 - XOS 565 IS CRACKED.REPAIRED CRACKED RT WING FIXED L/E BEADED DOUBLER BETWEEN XOS 559 - XOS 565 IAW SRM 57-40-02, REPAIR 15, FIGURE 205. (MAJOR)

Part: SKIN — GOUGED (L/H WING) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CL/H WING FIXED L/E UPPER SKIN IS GOUGED BETWEEN STA. XOS. 1187 TO 1191.REPAIRED GOUGED L/H WING FIXED L/E UPPER SKIN BETWEEN STA. XOS. 1187 TO 1191 IAW SRM 57-40-01 REPAIR 16. (MAJOR)

Part: SKIN — GOUGED (RT WING L/E) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CRT WING FIXED L/E EXTERIOR SKIN GOUGED BETWEEN STA. XOS 1187- XOS 1191.REPAIRED GOUGED RT WING FIXED L/E EXTERIOR SKIN BETWEEN STA. XOS 1187- XOS 1191 IAW SRM 57-40-01,REPAIR 16 REV 67 (MAJOR)

Part: SPAR CAP — CORRODED (LT WING T/E) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CLT WING UPPER T/E REAR SPAR UPPER CAP HAS CORROSION.REPAIRED CORRODED LT WING SPAR UPPER CAP IAW VT-SAA EA 011-5710-01-A9214 REV I/R AND UPS EO MD11-5710-80891-A (MINOR).

Part: DOUBLER — CRACKED (RT WING) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 537 TO 542.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 537 TO 542 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CRT WING FIXED L/E BEADED DOUBLER BETWEEN XOS 906 - 912 IS CRACKED.REPAIRED CRACKED RT WING FIXED L/E BEADED DOUBLER BETWEEN XOS 906 - 912 IAW SRM 57-40-02, REPAIR 15, FIGURE 205. (MAJOR)

Part: ANGLE — CRACKED (MAIN CABIN) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CMAIN CABIN LON 15L 'T' ANGLE CRACK AT STA.1341.REMOVED,FABRICATED AND REPALCED CRACKED 'T' ANGLE IAW SRM 51-35-01 AND 51-33-01 (MINOR).

Part: ANGLE — CRACKED (BS 1341 L15R) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CMAIN CABIN LON 15R 'T' ANGLE CRACK AT STA.1341.REMOVED,FABRICATED AND REPLACED CRACKED 'T' ANGLE IAW SRM 51-35-01 AND 51-33-01 (MINOR).

Part: DOOR FRAME — CRACKED (BS 1313) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CMAIN CABIN L3 DOOR JAMB AFT LOWER WEB AT STA.1313 & Z= -16.5 IS CRACKED.REPAIRED CRACKED MAIN CABIN L3 DOOR JAMB AFT LOWER WEB AT STA. 1313 & Z= -16.5 IAW SRM 53-40-15, REPAIR 3, FIG 201. (MAJOR)

Part: STRINGER — CRACKED (LT WING) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CLT WING FIXED L/E UPPER STRINGER BETWEEN XOS 789.645 - XOS 801.840 IS CRACKED.REPAIRED CRACKED LT WING FIXED L/E UPPER STRINGER BETWEEN XOS 789.645 - XOS 801.840 IAW VT-SAA EA 011-5710-01-A9220 REV. IR AND UPS EO MD11-5710-80985-A. REF. FAA FORM 8100-9 SIGNED BY: STEPHEN KANG (AR-605677) DATED 07/13/2021. (MAJOR)

Part: SUPPORT BRACKET — CRACKED (HYD ACCUMMULATOR) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CLT MLG W/W SYS #3 HYD ACCUMMULATOR SUPPORT BRACKET CRACK AT LWR END.REMOVED,FABRICATED AND REPLACED CRACKED SUPPORT BRACKET IAW SRM 51-31-01 AND 51-33-01 (MINOR).

Part: FASTENER — LOOSE (NR 2 INLET) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2C#2 ENGINE INLET LIP HAS LOOSE FASTENERS.REPAIRED #2 ENGINE INLET LIP LOOSE FASTENERS IAW VT-SAA EA 011-7110-01-A9204 REV. IR AND UPS EO MD11-7110-80842-A. (MINOR)

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 86,278 hrs · 15,581 cycles

INSPECTION TYPE:2CRH MLG W/W 3RD VERTICAL STIFFENER CRACK AT LWR END.REMOVED,FABRICATED AND REPLACED CRACKED VERTICAL STIFFENER IAW SRM 51-35-01 AND 51-33-01 (MINOR)

Part: DOOR — INOPERATIVE (R1) · airframe 86,027 hrs · 15,437 cycles

INSPECTION TYPE: NA**SDR FILED OPEN** R1 ENTRY DOOR WILL NOT OPEN. DEFERRED R1 ENTRY DOOR IAW MEL 52 10 3 1 2 1 CONTROL #M740124 PLACARD INSTALLED.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 85,806 hrs · 15,331 cycles

EMERGENCY LT BAT LOW LIGHT DURING PREFLIGHT. OK TO CONTINUE PER MEL 33-50-4 DMP COMPLIED WITH. PLACARD INSTALLED.REPLACED EMERGENCY LIGHTING BATTERY POWER SUPPLY PER AMM 33-51-01-401. TEST GOOD, M734125 CLEARED. DMP REVERSED. IPC 33-51-01-05-015

Part: SENSOR — OUT OF ADJUST (RT WING SLAT) · airframe 85,121 hrs · 15,034 cycles

INSPECTION TYPE: NA**EMERGENCY DECLARED AS PRECAUTION. NO EQUIPMENT NEEDED**. DURING CLIMB OUT RECEIVED LEVEL 2 "SLAT DISAG" ALERT AND STICK SHAKER. FOLLOWING SLAT DISAG CHECKLIST WITH FLAPS/SLATS UP/RET, ALERT EXTINGUISHED. FOUND RT LEADING EDGE SLAT SENSOR "A" OF ADJUST SLAT POS SENSOR PER 28-84-03. OPERATIONS CHECK GOOD.

Part: COMPUTER — INOPERATIVE (NR 2 FCC) · airframe 85,023 hrs · 14,973 cycles

FLIGHT CONTROL ANOMOLY IN PITCH USING AUTOPILOT 2 AT ABOUT 1500' ON FINAL. GO AROUND AND EMERGENCY DECLARED SECOND APPROACH SAME PROBLEM AND A/C WAS LANDED MANUALLY. AUTOPILOT 2 INOP PER MEL 22-10-1-0-1 DMP 22-10-1-0-1 ACCOMPLISHED. M714168 ASSIGNED. FCC CHANNEL A INOP ELEVATOR LOAD FEEL LINKED TO M714170. ACCOMPLISHED ELEVATOR RANGE OF MOVEMENT TEST PER AMM 27-30-00-710-802. ALL DIMENSIONS WITHIN RANGE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 84,684 hrs · 14,826 cycles

INSPECTION TYPE:N/AAT 25K ON CLIMBOUT THE F/O WINDSCREEN CRACKED FROM BOTTOM RIGHT MOVING LEFT WHEN I TURNED ON WINDSHIELD ANTI ICE SAW THE ORIGIN POINT SPARKING AND SHUT IT OFF THEN 20 SEC LATER WINDSCREEN SPIDER WEB CRACKED.R&R F/O PANEL ASSEMBLY WINDSHIELD IAW AMM 56-11-01-PG BL 401 CONFIG OPS CK GOOD.

Part: BRACKET — OUT OF ADJUST (ENTRY DOOR) · airframe 84,610 hrs · 14,796 cycles

INSPECTION TYPE:N/AUNABLE TO ARM LEFT ENTRY DOOR & SLIDE BEFORE FLIGHTADJUSTED LEFT DOOR FWD ARMING "ARMED" BRACKET PER AMM 25-61-15

Part: UNKNOWN — LEAKING (RIGHT WING) · airframe 84,039 hrs · 14,519 cycles

INSPECTION TYPE:N/AATB - ON DEPARTURE NOTIFIED OF A POSSIBLE FUEL LEAK IN RIGHT WING..RETURNED FOR UNEVENTFUL LANDING AT SDF. ALL FLUID, PUMPS AND VALVES LOOKED NORMAL (NO# 3 FUEL QY). NO UNSUAL PITCH , POWER OR TRIMPERFORMED DETAILED GVI OF RH WING, INCLUDING FUEL ACCESS PLATES, HYDRALIC COMPONENTS, LINES, FLAPWALL AND AILTNON ACCESS PMLS WITH NO FLUIDS OF ANY TYPE NOTED. RAN ALL THREE ENGINES WITH ALL FUEL SYSTEMS AND HYD. SYSTEM PRESSURIZED ILLEG MM 71-00-00. NO LEAKS NOTED. PERFORMED LEAK TEST OF CROSSFEED

Part: CABLE — BROKEN (L1 DOOR) · airframe 83,388 hrs · 14,289 cycles

INSPECTION TYPE:N/AL1 DOOR FOWARD DRIVE CABLE BROKE. INSTALLED FWD OPEN & CLOSED CABLES PER AMM 52-11-03-400. CABLE TENSION STILL NEEDS TO BE ADJUSTED PER PARA E STEP (2) (7) THRU (10). PERF CABLE TENSIONS & ADJUST DR IAW AMM 52-11-02.

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 83,378 hrs · 14,284 cycles

INSPECTION TYPE:N/AAIR TURN BACK - WHEN WE RAISED LANDING GEAR ON DEPARTURE WE GOT A CONTINOUS "LANDING GEAR" ALL LIGHTS WERE OUT INDICATING GEAR WAS UPREF WDM 32-62-01 APLUS R5-1164B PIN 61 WAS 4K OHMS TO GND WITH FLAPS UP. REPLACED P1-1111 AN LEFT OB FLAP POS. TRANSMITTED PER 27-54-02-401 ACCOMPLISHED REQUIRED TESTS. IPC 27,54-01-01 EQUIP LIST P1-1111

Part: PROXIMITY SENSOR — CONTAMINATED (LE SLAT) · airframe 83,359 hrs · 14,277 cycles

INSPECTION TYPE:N/A DIVERSION - SPEED 230KT ALT GOOD' DURING SLAT EXTENSION AN INTIAL SLIGHT ROLE TO THE RT FOLLOWED BY A ROLE TO THE RT FOLLOWED BY A LVL 2 SLAT DISAG. FOLLOWING QRH SLATS WERE RETRACTED AND A FLAPS 28/RET LAD WAS ACCOMPLISHED. THE SLAT DISAG WAS NOT PREST/S REF FIM 31-71-07-00 BLKS 1-4, FOUND DEBRIS IN LEFT WING SLAT TRACK 3 CONTAMINATING PROX SENSORS. REMOVED DEBRIS AND CLEANED PROX SENSORS. PERFORMED SLAT POS IND OPS CHECK REF AMM 27-84-00 NO FAULTS NOTED AT THIS TIME. SYSTEM OK.

Part: STIFFENER — BENT (RT MLG WW) · airframe 83,357 hrs · 14,276 cycles

INSPECTION TYPE:4C RT WHEEL WELL AFT SIDE VERTICAL STIFFENER IS BENT. REMOVED, FABRICATED, AND INSTALLED RT MLG DOOR JAMB STIFFENER PER SRM 51-35-01 AND SRM 51-31-01.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 83,357 hrs · 14,276 cycles

INSPECTION TYPE:4C RT WHEEL WELL AFT SIDE VERTICAL STIFFENER IS CRACKED. REMOVED, FABRICATED AND INSTALLED RT MLG AFT DOOR JAMB VERTICAL STIFFENER PER SRM 51-31-01 AND SRM 51-35-01.

Part: BEAM — CRACKED (LT WING) · airframe 83,357 hrs · 14,276 cycles

INSPECTION TYPE:4C LT WING LOWER T/E SHELF PANEL HAS VERTICAL T-ANGLE CRACKED JUST AFT OF MLG CUTOUTREMOVED, FABRICATED AND INSTALLED LH WING T/E VERTICAL BEAM PER SRM 51-33-01.

Part: INTERCOSTAL — CRACKED (TAIL CONE) · airframe 83,357 hrs · 14,276 cycles

INSPECTION TYPE:4C TAILCONE LT MIDDLE GUIDE PIN INTERCOSTAL IS CRACKED. REMOVED AND REPLACED CRACKED TAILCONE LT MIDDLE GUIDE PIN INTERCOSTAL IAW SRM 51-35-01. (MINOR)

Part: HINGE — BROKEN (TAILCONE) · airframe 83,357 hrs · 14,276 cycles

INSPECTION TYPE:4C EXTENDED TAILCONE RT SIDE AT STA. CANT.Y=2165.6, X=36.5, AND Z=61.53. REPAIRED EXTENDED TAILCONE AT SAID LOCATION IAW EA 011-5310-01-A7832 REV. I/R AND EO MD11-5310-73209-A. (MINOR)

Part: INTERCOSTAL — CRACKED (TAIL CONE) · airframe 83,357 hrs · 14,276 cycles

INSPECTION TYPE:4C TAILCONE RT MIDDLE GUIDE PIN INTERCOSTAL IS CRACKED. REMOVED AND REPLACED CRACKED TAILCONE RT MIDDLE GUIDE PIN INTERCOSTAL IAW SRM 51-35-01. (MINOR)

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 83,357 hrs · 14,276 cycles

INSPECTION TYPE:4C MAIN CABIN LONGERON 2L SPLICE FITTING IS CRACKED AT STA. 5-123. REMOVED AND REPLACED CRACKED MAIN CABIN LONGERON 2L SPLICE FITTING IAW SRM 51-33-01. (MINOR)

Part: RIVET — LOOSE (NR 2 COWLING) · airframe 83,357 hrs · 14,276 cycles

INSPECTION TYPE:4C #2 ENG. INLET ASSY HAS 1 LOOSE RIVET AT 8:30 POS. REPAIRED #2 ENG. INLET ASSY IAW EA 011-7110-01-A7829 REV. I/R AND EO MD11-7110-73153-A. (MINOR)

Part: DOUBLER — DAMAGED (TAILCONE) · airframe 83,357 hrs · 14,276 cycles

INSPECTION TYPE:4C TAILCONE LT UPPER PRODUCTION DOUBLER IS DAMAGED. REPAIRED DAMAGED TAILCONE LT UPPER PRODUCTION DOUBLER AT STA 2165 & X=36.5 IAW EO MD11-5350-66790-A APPENDIX A. (MINOR)

Part: DOUBLER — DAMAGED (TAILCONE) · airframe 83,357 hrs · 14,276 cycles

INSPECTION TYPE:4C TAILCONE RT UPPER PRODUCTION DOUBLER IS DAMAGED. REPAIRED DAMAGED TAILCONE RT UPPER PRODUCTION DOUBLER AT STA. 2165 & X=-36.5 IAW EO MD11-5350-66790-A APPENDIX A. (MINOR)

Part: DOOR FRAME — CRACKED (LT CLG DOOR) · airframe 83,357 hrs · 14,276 cycles

INSPECTION TYPE:4C LT AFT CLG DOOR FRAME IS CRACKED. REMOVED AND REPLACED CRACKED LT AFT CLG DOOR IAW AMM 32-17-04-400-801. (MINOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 83,357 hrs · 14,276 cycles

INSPECTION TYPE:4C LT WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XIS=276.5 TO XIS=282.4. REPAIRED CRACKED LT WING FIXED L/E BEADED DOUBLER BETWEEN STA. XIS=276.5 TO XIS=282.4 IAW SRM 57-40-05 REPAIR 15 FIG. 205. (MAJOR)

Part: HINGE BRACKET — BROKEN (TE FLAP) · airframe 83,357 hrs · 14,276 cycles

INSPECTION TYPE:4C RT WING O/B FLAP I/B HINGE BRACKET ABOVE LOWER HINGE POINT IS BROKEN. REMOVED, FABRICATED AND REPLACED BRACKET IAW DWG. ARC0504 AND SRM 51-33-01. (MINOR)

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 83,357 hrs · 14,276 cycles

INSPECTION TYPE:4C LT MLG W/W O/B AFT SIDE VERTICAL STIFFENER IS CRACKED. REMOVED AND REPLACED CRACKED LT MLG W/W O/B AFT SIDE VERTICAL STIFFENER IAW SRM 51-33-01 & 51-35-01. (MINOR)

Part: SKIN — DENTED (THRUST REVERSER) · airframe 83,357 hrs · 14,276 cycles

INSPECTION TYPE:4C #1 ENG. O/B T/R TRANSLATING SLEEVE UPPER FWD. CORNER SKIN IS DENTED. REPAIRED #1 ENG. O/B T/R SLEEVE IAW EA 011-7930-01-A7933 REV. I/R AND EO MD11-7830-73171-A. (MINOR)

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 83,357 hrs · 14,276 cycles

INSPECTION TYPE:4C RT MLG W/W O/B AFT SIDE VERTICAL STIFFENER IS CRACKED. REMOVED AND REPLACED CRACKED RT MLG W/W O/B AFT SIDE VERTICAL STIFFENER IAW SRM 51-33-01 & 51-35-01. (MINOR)

Part: DOOR FRAME — CRACKED (CLG DOOR) · airframe 83,357 hrs · 14,276 cycles

INSPECTION TYPE:4C CENTER LANDING GEAR DOOR FRAME IS CRACKED AT FWD. LOWER END. REMOVED AND REPLACED FRAME IAW SRM 51-33-01 & 51-35-02. (MINOR)

Part: INTERCOSTAL — CRACKED (RT MLG WW) · airframe 83,357 hrs · 14,276 cycles

INSPECTION TYPE:4C RT MLG W/W INTERCOSTAL UNDER LOWER AFT BRAKE ACCUMULATOR IS CRACKED. REMOVED AND REPLACED CRACKED RT MLG W/W INTERCOSTAL UNDER LOWER AFT BRAKE ACCUMULATOR IAW SRM 51-33-01. (MINOR)

Part: RECEPTACLE — GOUGED (NR 1 EXHAUST) · airframe 83,357 hrs · 14,276 cycles

INSPECTION TYPE:4C#1 ENGINE EXHAUST NOZZLE O/B CORE COWL AFT LATCH PIN RECEPTACLE IS GOUGED. REPAIRED GOUGED #1 ENGINE EXHAUST NOZZLE O/B CORE COWL AFT LATCH PIN RECEPTACLE IAW EA 011-7810-01-A7834 REV. IR AND EO MD11-7810-73170-A. (MINOR)

Part: INTERCOSTAL — CRACKED (RT MLG WW) · airframe 83,357 hrs · 14,276 cycles

INSPECTION TYPE:4C RT MLG W/W INTERCOSTAL BELOW UPPER AFT BRAKE ACCUMULATOR IS CRACKED. REPAIRED CRACKED RT MLG W/W INTERCOSTAL BELOW AFT BRAKE ACCUMULATOR X=-31.50, Z=-56, BETWEEN Y=1441 AND Y=1461 IAW SRM 53-40-12 REPAIR 3 FIGURE 201. (MAJOR)

Part: SKIN — DENTED (FUSELAGE) · airframe 83,357 hrs · 14,276 cycles

INSPECTION TYPE:4C LT SIDE SKIN DENT AND GOUGED AT STA 330 REQUIRES PERMANENT REPAIR. REPAIRED DENTED & GOUGED LT FUSELAGE SKIN AT STA. 330 ABOVE Z=-2.900 IAW EA 011-5330-01-A7835 REV. IR AND EO MD11-5330-73199-A. (MAJOR)

Part: DOUBLER — NOT REPORTED (RT WING) · airframe 83,338 hrs · 14,267 cycles

INSPECTION TYPE:4C REPLACE RT WING FIXED L/E BEADED DOUBLER REPAIR BETWEEN XOS=551.5 & XOS=555.5. REMOVED AND REPLACED RT WING FIXED L/E BEADED DOUBLER REPAIR BETWEEN XOS=551.5 & XOS=555.5 IAW SRM 57-40-02 REPAIR 15, FIGURE 205. (MAJOR)

Part: BATTERY — DISCHARGED (CABIN) · airframe 82,754 hrs · 14,103 cycles

INSPECTION TYPE:N/A EMER LT BAT 1 LO LIGHT ILLUMINATED DURING TESTING OF EMER LIGHT TEST. EMER PWR SUPPLY BATTERY REPLACED IAW AMM 33-51-01. OPS CK OK. THIS CLEARS M664725

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 82,424 hrs · 13,967 cycles

R1 DOOR BOTTLE PRESSURE WAS LOW. SERVICED THE BOTTLE IAW MM 12-25-04

Part: DOOR — BINDING (L1) · airframe 82,134 hrs · 13,874 cycles

L1 DOOR WILL NOT CLOSE AND SECURE PROPERLY, AFTER BINDING WITH CREW REST MODULER AND RT DOOR IAW MM 52-11-02-400-800, STEPS D2, & F. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 81,659 hrs · 13,736 cycles

EMERGENCY LIGHTS INOP. FOUND THAT EMERGENCY LIGHTS WILL COME ON IN ARM POSITION AND WILL NOT TEST. ORDERED CONTROL RELAY R2-5700 AND CONTROL SWITCH $1-346. PERF T/S IAW FIM 33-51-02-00 AND OPERATIONAL TEST OF EMER LIGHT SYS IAW AMM 33-50-00-700-802. EMER LIGHT TEST PASS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,654 hrs · 13,733 cycles

ON PREFLIGHT LVL EMER LT BAT 1 LOW. REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-51-01 MESSAGE REMAINS. DEFERRAL IAW MEL 33-50-4 DMP C/W DI LOG UPDOWN. PLACARD INSTALLED ESR 33-51-20-01

Part: LATCH — UNSECURE (R1 DOOR) · airframe 80,435 hrs · 13,417 cycles

FOUND THE R1 DOOR LATCH ASSY ON GALLEY FLOOR UNSECURE. SECURED THE LATCH ASSY IAW AMM 20-50-02.

Part: LIGHT — NO TEST (R2 DOOR RAFT) · airframe 80,261 hrs · 13,368 cycles

INSPECTION TYPE:DURING PREFLIGHT R2 DOOR RAFT PRESS PRESS TO TEST DOES NOT ILLUMINATE. DEFER R1 EVAC SLIDE REMOTE P-T-T INDICATION SYSTEM PER MEL 25-61-2 CMP C/W SLIDE PRESSURE IS GOOD. FOUND TERMINAL OF REMOTE IND ASSY PUSHED OUT OF HOUSING; R/R REMOTE PRESS IND ASSY. OPS NORMAL

Part: RETAINER — BROKEN (ESCAPE LINE) · airframe 80,162 hrs · 13,338 cycles

RETAINING STRAP FOR THE CAPTAIN`S EGRESS ESCAPE LINE, BROKEN. SECURED THE ESCAPE LINE. OPS CHECKED OK IAW AMM 25-61-00. ACFT OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 79,614 hrs · 13,193 cycles

DURING PREFLIGHT LVL 1 "EMER LT BATT 1 LO" ILLUMINATED AFTER EMERGENCY LIGHTS TEST. R&R BATTERY SUPPLY IAW AMM 33-51-01-401.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE:3C, CENTER CARGO COMPARTMENT LONGERON 49L HAS CORROSION AT STA 5-123. REMOVED AND REPLACED LONGERON SECTION 49L PER SRM 53-00-05 REPAIR 1, EA 011-5310-01-A6888 I/R AND EO 5310-64959-A.

Part: FLOOR SUPPORT — CRACKED (BS 1962) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, FLOOR SUPPORT AT BS 1962, RBL 10 IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE FLOOR SUPPORT IAW DWG AGA7984, AND SRM 51-35-01.

Part: RIB — BROKEN (NR 8 SLAT) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, RT WING NR 8 SLAT INTERNAL RIB BROKEN. REMOVED AND REPLACED THE SLAT IAW AMM 27-80-30.

Part: SUPPORT FITTING — WORN (L1 DOOR SLIDE) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, L1 DOOR FWD SLIDE MOUNT SUPPORT FITTING HAS DEEP WEAR. REMOVED, FABRICATED, AND REPLACED THE MOUNT SUPPORT FITTING IAW DWG ABA8513, AND SRM 51-35-01.

Part: SIDEWALL SUPPORT — CRACKED (BS 919) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, LOWER FWD CARGO LT SIDEWALL SUPPORT ANGLE IS CRACKED AT BS 919. REMOVED, FABRICATED, AND REPLACED SIDEWALL SUPPORT ANGLE IAW DWG ADA0130, AND SRM 51-35-01.

Part: SIDEWALL SUPPORT — CRACKED (BS 1199) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, LOWER FWD CARGO SIDEWALL SUPPORT ANGLE IS CRACKED AT BS 1199, BETWEEN LONGERONGS 41 - 42R. REMOVED, FABRICATED, AND REPLACED SUPPORT ANGLE IAW DWG ADA0130, AND SRM 51-35-01.

Part: SKIN — CORRODED (BS 2026-2163) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, AFT FUSELAGE EXTERIOR SKIN CORRODED ALONG HORIZONAL STAB FAIRING INTERFACE, RT SIDE, BS 2026 - 2163. REPAIRED IAW EA 011-5330-01-A6893, REV IR, EO MD11-5330-64949, AND SRM 53-70-01, REPAIR 3. MAJOR.

Part: FRAME — CORRODED (BS 1781) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, FRAME LOWER SUPPORT CORRODED BS 1781, LONGERON 50L - 50R. REPAIRED THE FRAME IAW SRM 53-00-07, REPAIR 5, FIG 202. MAJOR

Part: SIDEWALL SUPPORT — CRACKED (BS 1781) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, CENTER CARGO SIDEWALL SUPPORT ANGLE IS CRACKED AT BS 1781. REMOVED, FABRICATED, AND REPLACED THE SIDEWALL SUPPORT IAW DWG AFA0162, AND SRM 51-35-01.

Part: LONGERON — CORRODED (BS 1953-1964) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, LONGERON 43R CORRODED BETWEEN BS 1953 - 1964. REPAIRED THE LONGERON IAW EA 011-5310-01-A6877, REV IR, AND EO MD11-5310-64925-A. MAJOR.

Part: LONGERON SPLICE — CRACKED (BS 1711) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, LONGERON SPLICE 51R CRACKED BS 1711. REMOVED AND REPLACED THE LONGERON SPLICE IAW SRM 51-33-01.

Part: ATTACH BRACKET — CRACKED (FAIRING) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, EXTERIOR FUSELAGE,M RT BODY FAIRING ATTACH BRACKET IS CRACKED AT BS 1661. REMOVED, FABRICATED, AND REPLACED THE ATTACH BRACKET IAW DWG AFA7768, AND SRM 51-33-01.

Part: SIDEWALL SUPPORT — CRACKED (BS 1821) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, CENTER CARGO SIDEWALL SUPPORT ANGLE IS CRACKED AT BS 1821 LT SIDE. REMOVED, FABRICATED, AND REPLACED THE SIDEWALL SUPPORT IAW DWG AFA7295, AND SRM 51-33-01.

Part: ATTACH ANGLE — CRACKED (BS 1361) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, WING TO BODY PANEL ATTACH ANGLE BROKEN AT BS 1361. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT ATTACH ANGLE IAW DWG ANB7143, SRM 51-35-01, AND 51-31-01.

Part: STRINGER — CRACKED (47) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, STRINGER 47 CRACKED. REPAIRED THE STRINGER IAW SRM 57-10-03, REPAIR 1, FIG. 201. MAJOR.

Part: FUEL LINE — DENTED (CENTER TANK) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE:3C, CENTER TANK FUEL DISTRIBUTION PIPE HAD MULTIPLE DENTS. REPAIRED THE FUEL PIPE IAW EA 011-2820-01-A6886, REV IR, AND EO MD11-2820-64869-A.

Part: LONGERON — CORRODED (44L) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, LONGERON 44L CORRODED BETWEEN STATION 5-93 AND 5-123. REPAIRED IAW EA 011-5310-01-A6883, REV IR, AND EO MD11-5310-64922-A. MAJOR.

Part: LONGERON — CORRODED (CENTER CARGO) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, CENTER CARGO BAY LONGERON 48L CORRODED BS 5-93 TO 5-113. REPAIRED IAW EA 011-5310-01-A6890, REV IR, AND EO MD11-5310-64936-A. MAJOR.

Part: ATTACH ANGLE — CRACKED (BS 1281) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, WING-TO-BODY FAIRING ATTACH ANGLE CRACKED BELOW THE R3 DOOR, BS 1281. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT ANGLE IAW DWG ANB7138, SRM 51-35-01, AND 51-31-01.

Part: LONGERON — CRACKED (45 L) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, LONGERON 45L CRACKED AT BS 5-42. REMOVED AND REPLACED THE LONGERON IAW SRM 51-33-01, AND 51-35-01.

Part: VENT LINE — DENTED (FUEL TANK) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, CENTER TANK FUEL PIPE DENTED BETWEEN XCW 17 & 46. REPAIRED THE VENT PIPE IAW EA 011-2820-01-A6887, REV IR, AND EO MD11-2820-64865-A.

Part: FITTING — CORRODED · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, FLOOR FITTING CORRODED. REMOVED AND REPLACED THE FLOOR FITTING REF EO MD11-2520-58701-D

Part: SHEAR TIE — CORRODED (CENTER CARGO) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, CENTER CARGO BAY SHEAR TIE IS CORRODED AT BS 5-73 BETWEEN LONGERONS 48 - 49R. REMOVED, FABRICATED, AND REPLACED THE SHEAR TIE IAW DWG A5A7058-19, AND SRM 51-33-01. (MINOR)

Part: DOUBLER — CHAFED (BS 2165) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, EXTENDED TAILCONE LT SIDE PREVIOUS INTERNAL REPAIR FOUND CHAFED. REMOVED AND REPLACED THE DOUBLER AT BS 2165 IAW EO MD11-5350-64832-A.

Part: STRINGER — CRACKED (RT WING) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, RIGHT WING STRINGER 16 CRACKED BETWEEN XORS 372 & 402. REPAIRED THE STRINGER IAW EA 011-5710-01-A6869, REV IR, AND EO MD11-5710-64900-A. MAJOR.

Part: FRAME — DENTED (BS 655) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, BS 655 FRAME DENTED ADJACENT TO LONGERON 12R. REPAIRED IAW EA 011-5310-01-A6872, REV IR, AND EO MD11-5310-64915-A. MAJOR.

Part: DOOR FRAME — CRACKED (L3 DOOR) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, L3 DOOR FRAME LOWER WEB IS CRACKED AT BS 1254, AND Z=-18. REPAIRED THE DOOR FRAME IAW SRM 53-40-15, REPAIR 3, FIG 201. MAJOR.

Part: LONGERON — CORRODED (BS .1159-1179) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, LONGERON 18R CORRODED BS 1159 - 1179. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT LONGERON IAW DWG AEA0220, AND SRM 51-33-01.

Part: FITTING — CRACKED (LONGERON 19R) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, LONGERON 19R END FITTING CRACKED BETWEEN BS 1139 AND 6-90. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT END FITTING IAW EA 011-5310-01-A6875, REV IR, AND EO MD11-5310-64923-A. MAJOR.

Part: TRUNNION — CRACKED (NLG) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, LEFT NOSE LANDING GEAR TRUNNION FITTING IS CRACKED AT BS 582.5, Z=-114 AND RBL 24. REPAIRED THE TRUNNION FITTING IAW SRM 53-10-14, REPAIR 2, FIG 202. MAJOR.

Part: TEE FITTING — CRACKED (RT WING) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, RIGHT WING T/E SUPPORT TEE CRACKED NEAR OPENING FOR PANEL 641BB. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT TEE IAW DWG ARC0341, AND SRM 51-33-01.

Part: LONGERON — CORRODED (BS 1179) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, LONGERON 16R CORRODED AT BS 1179. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT LONGERON BETWEEN BS 1179 - 1199 IAW DWG AEA7065, AND SRM 51-33-01.

Part: DOOR FRAME — CRACKED (R3 DOOR) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, R3 DOOR FRAME LOWER WEB IS CRACKED AT BS 1254 AND Z=-18. REPAIRED THE DOOR FRAME IAW SRM 53-40-15, REPAIR 3, FIG 201. MAJOR.

Part: LONGERON — CORRODED (BS 1189) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, LONGERON 18R CORRODED BS 1189. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT LONGERON BETWEEN BS 1179 - 1199 IAW DWG AEA0220 AND SRM 51-33-01.

Part: FAIRING — CRACKED (LT WING SLAT) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, LT WING NR 1 SLAT PERFORMANCE FAIRING RIB IS CRACKED AT XIS 150.74. REPAIRED THE SLAT FAIRING IAW EA 011-5750-01-A6856, REV I/R, AND EO MD11-5750-64746-A.

Part: DOUBLER — CRACKED (RT WING) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, RT WING FIXED L/E BEADED DOUBLER IS CRACKED AT XOS 464 - 470.2. REPAIRED THE DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 203. MAJOR

Part: SKIN — CHAFED (RT WING) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, RT WING FIXED L/E SKIN IS CHAFED BEWTEEN XIS 158 & 163. REPAIRED THE RT WING FIXED L/E SKIN IAW EA 011-5730-01-A6861, REV I/R, AND EO MD11-5730-64872-A. MAJOR.

Part: DOOR — DAMAGED (LT WING SLAT) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, LT WING FIXED L/E COMPARTMENT OTBD SLAT MECHANISM DOOR IS DAMAGED. REPAIRED THE SLAT MECHANISM DOOR IAW SRM 57-40-01.

Part: SKIN — CHAFED (LT WING SLAT) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, LT WING NR 8 SLAT INNER SKIN CHAFED AT XOS 1006.8 AND 1021.8. REPAIRED THE SLAT SKIN IAW EA 011-5754-01-A6871, REV I/R, AND EO MD11-5730-64833-A.

Part: SKIN — CHAFED (RT WING) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, RT WING L/E UPPER SURFACE CHAFED REPAIR DOUBLER AT THE NR 1 SLAT. REMOVED AND REPLACED THE DOUBLER IAW SRM 57-40-02, REPAIR 8, FIG. 201. MAJOR

Part: SKIN — CRACKED (NR 3 NOSE COWL) · airframe 79,571 hrs · 13,174 cycles

INSPECTION TYPE: 3C, NR 3 ENGINE INLET NOSE COWL SKIN CRACKED AROUND FASTENERS, 8:00 POSITION. REMOVED AND REPLACED THE 3 INLET COWL IAW AMM 71-11-01.

Part: DOUBLER — CRACKED (LT WING) · airframe 79,568 hrs · 13,172 cycles

INSPECTION TYPE: 3C, LT WING FIXED L/E BEADED DOUBLER IS CRACKED AT XOS 734 - 740. REPAIRED THE BEADED DOUBLER IAW EA 011-5730-01-A6867, REV I/R, AND EO MD11-5730-64853-A. MAJOR.

Part: LONGERON — CRACKED (BS 1531-1551) · airframe 79,568 hrs · 13,172 cycles

INSPECTION TYPE: 3C, LONGERON 48L CRACKED BS 1531 - 1551. REPAIRED THE LONGERON IAW EA 011-5310-01-A6891, REV IR, AND EO MD11-5310-64941-A (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 79,568 hrs · 13,172 cycles

INSPECTION TYPE: 3C, LT WING FIXED L/E BEADED DOUBLER IS CRACKED AT XOS. 789 - 795. REPAIRED THE DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 205. MAJOR.

Part: SKIN — DEFORMED (BS 275) · airframe 79,568 hrs · 13,172 cycles

INSPECTION TYPE: 3C, FORWARD FUSELAGE NOSE SKIN DAMAGED STA. 275 AT BL 0. REPAIRED THE SKIN IAW EA 011-5330-01-A6874, REV IR, AND EO MD11-5330-64805-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 79,568 hrs · 13,172 cycles

INSPECTION TYPE: 3C, LT WING FIXED L/E BEADED DOUBLER IS CRACKED AT XOS. 610 - 616. REPAIRED THE DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 205. MAJOR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,106 hrs · 13,042 cycles

INSPECTION TYPE: 3C, UPPER SKIN HAS CORROSION AT STRINGER 15. REPAIRED THE SKIN IAW EA 011-5730-01-A6876, REV I/R, AND EO MD11-5730-64823-A.

Part: SKIN — DAMAGED (RT WING LE) · airframe 79,096 hrs · 13,036 cycles

DAMAGE TO THE RT WING FIXED LEADING EDGE SKIN. REPAIR IAW EO MD11-5730-63591.

Part: SWITCH — FAILED (L1 DOOR SLIDE) · airframe 78,817 hrs · 12,969 cycles

L1 SLIDE FAILED TO TEST. R & R TEST SWITCH. OPS CHECKED NORMAL IAW AMM 25-61-00

Part: RELAY — INOPERATIVE (R1 DOOR) · airframe 78,060 hrs · 12,778 cycles

R1 DOOR ELECTRIC FUNCTION INOPERATIVE. FOUND STUCK OPEN, PIN AT OPEN LIMIT SWITCH. PERFORMED LUBRICATION OF OPEN PIN ACCESSORY, AMM 12-25-05, REV 86.02. FOUND ALSO BAD LOCK RELEASE, RELAY R2-5325. RELAY R2-5325, REPLACED ACCESSORY WDM 52-11-01, PAGE 5, REV 87. TEST SATISFACTORY DMI CLOSED. PN OFF-ON: 5D0005-1, EFF REF IPC 24-51-71-01, ITEM 179.

Part: BATTERY — DISCHARGED (EVAC SLIDE) · airframe 78,030 hrs · 12,773 cycles

L1 DOOR SLIDE BATTERY DOES NOT TEST. REPLACED LAMPS AND BATTERIES IN L1 SLIDE REMOTE PRESSURE INDICATOR IAW AMM 25-61-04. OPS CK GOOD.

Part: COALESCER BAG — CONTAMINATED (AC BAY) · airframe 77,685 hrs · 12,654 cycles

BAD ACRID ODOR PRESENT ON DESCENT, SUSPECT AIR CONDITIONING SYSTEM. IRRITANT TO EYES, NOSE, AND THROAT OF CREW MEMBERS. DETERMINED RESIDUAL HYD FLUID IN AFT ACCESSORY COMP. CLEANED AREA AND LEAK CHECKED. NO LEAKS NOTED. C/W MM 21-53-00-160-802 FOR ACID DISTRIBUTION DUCTS. R&R 1,2,&3 PACC COALESCER BAGS IAW 21-54-05. RAN ENGS AND APU. OPS CK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 77,600 hrs · 12,626 cycles

EMERGENCY LIGHTS, TEST FAIL. BATTERY LOW, EVEN THOUGH ACFT WAS POWERED FOR SEVERAL HOURS. R & R BATTERY POWER SUPPLY OF EMERGENCY LIGHTS IAW MM 33-51-01-4.

Part: FLAPPER VALVE — STUCK (E/E BAY FAN) · airframe 77,353 hrs · 12,555 cycles

LEVEL 1, AVIONCS FAN OVERHEAD, WARNING DISPLAYED DURING DESCENT. FOUND FWD GROUND CONDITIONED AIR FLAPPER STUCK OPEN, BINDING ON HINGE RETAINER. ADJUST HINGE RETAINER. FLAPPER OPS NORMAL REF MM 21-22-20.

Part: LINE — LEAKING (NR 2 ENGINE) · airframe 77,340 hrs · 12,545 cycles

ENGINE FAIL LIGHT ON T/O ROLL. REJECT ACCOMPLISHED DUE TO ENGINE MONITORING DATA SHOWING LOW PB PRESSURE NR 2 ENGINE, PERFORMED ENGINE CHECK 3, PB SENSE LINES. FOUND NR 2 ENGINE PB FLEX, PN 51U78 HAS SEVERE AIR LEAK. REPLACED LINE, PERFORMED ACCEL/DECEL TEST IAW MM 71-02-04 FOR ALL 3 ENGINES. ALL PARAMETERS NOW NORMAL. ALL PB PRESSURE NORMAL AT APPROXIMATELY 269 PSI.

Part: TRANSDUCER — FAILED (TIRE PRESSURE) · airframe 77,289 hrs · 12,528 cycles

EMERGENCY DECLARED, TIRE FAIL LVL 2 DURING T/O ROLL ON CTR GEAR LT TIRE, FLASHING YELLOW PRESSURE INDICATIONS ON BOTH CTR GEAR TIRES. INDICATION ALT BETWEEN TIRE FAIL AND TIRE DIFF PRESSURE. R & R NR 9 MAIN TIRE PRESSURE TRANSDUCER IAW AMM 32-46-03.

Part: HOOK AND LOOP — LOOSE (LIFE VEST) · airframe 77,271 hrs · 12,521 cycles

CAPTAIN`S LIFE VEST WILL NOT STAY STOWED, FOUND HOOK AND LOOP LOOSE, SECURED THE HOOK AND LOOP.

Part: CYLINDER — OVERSERVICED (LT MLG) · airframe 77,081 hrs · 12,468 cycles

AFTER TAKEOFF, LANDING GEAR WILL NOT RETRACT. MAINTENANCE BLED AIR FROM LT MLG TRUCK BOGIE TRIM CYLINDER IAW AMM 32-37-01. TRUCK BEAM TRIM INTERLOCK OPS TEST GOOD IN IAW 32-37-00.

Part: CONTAINER — DAMAGED (LIFE VEST) · airframe 76,771 hrs · 12,400 cycles

VACUUM PACKAGE AT CREW LIFE VEST IN COURIER AREA DAMAGED. AFFECTED LIFE VEST REPLACED IAW AMM 25-64-01 PB 201, REV 84.02, DATED 12-21-15. PN OFF-ON: P01074-201C, SN OFF: 15040610011, SN ON: 15071900027. EFF REF IPC: 25-64-01-08, ITEM -010B, REV 149.01, DATED 12-08-15.

Part: LIFE VEST — UNSECURE (FLIGHT DECK) · airframe 76,394 hrs · 12,287 cycles

CAPT LIFE PRESERVER WILL NOT STAY IN SEAT COMPARTMENT VELCRO WILL NOT HOLD REPLACED WORN HOOK VELCRO.

Part: SKIN — DAMAGED (TAILCONE) · airframe 76,096 hrs · 12,193 cycles

INSPECTION TYPE:1C, CHAFE DAMAGE TO EXTENDED TAILCONE FWD SKIN INNER SURFACE RT SIDE REPAIRED TAILCONE RT SKIN IAW EA 011-5330-01-A5910, REV IR AND EO MD11-5350-58273-A.

Part: SKIN — DAMAGED (TAILCONE) · airframe 76,096 hrs · 12,193 cycles

INSPECTION TYPE:3C, CHAFE DAMAGE TO EXTENDED TAILCONE FWD SKIN INNER SURFACE LT SIDE REPAIRED TAILCONE LT SKIN IAW EA 011-5330-01-A5910, REV. IR AND EO MD11-5350-58273-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 76,096 hrs · 12,193 cycles

INSPECTION TYPE:3C, LEFT WING FIXED L/E INNER BEADED DOUBLER CRACKED XOS710. REMOVED EXISTING ADJACENT BEADED DOUBLER REPAIR, INSTALLED NEW REPAIR XOS703-714 IAW SRM 57-40-02, REPAIR 15, FIG 206.

Part: SPLICE — CRACKED (LT WING) · airframe 76,096 hrs · 12,193 cycles

INSPECTION TYPE:3C, LT WING FIXED L/E SKIN INNER SPLICE STRAP CRACKED XOS 798. REMOVED, FABRICATED, AND INSTALLED SPLICE DOUBLER IAW DWG ARB3954 AND SRM 51-33-01.

Part: DOUBLER — CRACKED (LT WING) · airframe 76,096 hrs · 12,193 cycles

INSPECTION TYPE:3C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED XOS 756. REMOVED ADJACENT EXISTING REPAIR AND INSTALLED NEW BEADED DOUBLER REPAIR XOS 753-763 IAW SRM 57-40-02, REPAIR 15, FIG 203.

Part: DOOR FRAME — CORRODED (AFT CARGO) · airframe 76,096 hrs · 12,193 cycles

INSPECTION TYPE: 3C, AFT CARGO AFT LOWER DOOR JAMB FRAME HAS CORROSION AT BS 1960. R & R AFT CARGO DOOR AFT LOWER JAMB FRAME AT BS 1960 IAW SRM 51-33-01 AND SRM 51-35-01.

Part: SPAR CAP — CORRODED (LT WING) · airframe 76,096 hrs · 12,193 cycles

INSPECTION TYPE: 3C, LT WING AFT UPPER SPAR CAP AFT FLANGE CORRODED XORS 790. REPAIRED CORRODED SPAR CAP XORS 779-798 IAW EA 011-5710-01-A5912, REV IR AND EO MD11-5710-58325-A.

Part: FORMER — CRACKED (LT WING L/E) · airframe 76,096 hrs · 12,193 cycles

INSPECTION TYPE: 3C, LT WING FIXED L/E FORMER CRACKED XOS 585. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FORMER IAW DWG ARB2931 AND SRM 51-33-01.

Part: FORMER — CRACKED (LH WING L/E) · airframe 76,096 hrs · 12,193 cycles

INSPECTION TYPE: 3C, LT WING FIXED L/E FORMER CRACKED XOS 938. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FORMER IAW DWG ARB1292 AND SRM 51-33-01.

Part: SPAR — CRACKED (LT WING) · airframe 76,096 hrs · 12,193 cycles

INSPECTION TYPE:3C, SILL STRAP CRACKED ALONG LT WING REAR SPAR LOWER SURFACE XORS433. TRANSFERRED FROM 2015080792124. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SILL STRAP IAW DWG ARC7008, SRM 51-33-01, 51-35-01.

Part: SKIN — CRACKED (RT WING) · airframe 76,096 hrs · 12,193 cycles

INSPECTION TYPE:3C, RT WING FIXED L/E EXTERIOR SKIN CRACKED AT NR 12 SLAT TRACK CUT-OUT, XOS 776. REPAIRED RT WING L/E SKIN IAW SRM 57-40-02, REPAIR 7, FIG 201.

Part: SHEAR TIE — CRACKED (BS 2140) · airframe 76,096 hrs · 12,193 cycles

INSPECTION TYPE: 3C, CRACKED SHEAR TIE BS 2104. R & R SHEAR TIE IAW SRM 51-31-01, 51-33-01.

Part: SPAR — CORRODED (RT WING) · airframe 76,096 hrs · 12,193 cycles

INSPECTION TYPE:3C, RIGHT WING AFT SPAR UPPER CAP, AFT FLANGE CORRODED ADJACENT TO NR 2 SPOILER. REPAIR AFT SPAR CAP CORROSION XORS 478-503 IAW EA 011-5710-01-A5913, REV. IR AND EO MD11-5710-58347-A.

Part: SUPPORT — CRACKED (RT WING) · airframe 76,096 hrs · 12,193 cycles

INSPECTION TYPE: 3C, RIGHT WING INBD T/E FALSE SPAR SUPPORT CRACKED AT UPPER END. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SUPPORT, POST IAW DWG ARC0295 AND SRM 51-33-01.

Part: DOUBLER — CRACKED (RT WING) · airframe 76,096 hrs · 12,193 cycles

INSPECTION TYPE:3C, RT WING FIXED L/E INTERIOR BEADED DOUBLER CRACKED XOS 553. REPAIRED THE RT WING BEADED DOUBLER XOS 551-555 IAW SRM 57-40-02, REPAIR 15, FIG 206.

Part: FORMER — CRACKED (RT WING) · airframe 76,096 hrs · 12,193 cycles

INSPECTION TYPE:3C, CRACKED STRAP, FORMER, INSIDE RT WING L/E XOS 585. R & R THE FORMER IAW SRM 51-31-01, 51-33-01.

Part: DOUBLER — CRACKED (RT WING) · airframe 76,096 hrs · 12,193 cycles

INSPECTION TYPE:3C, RT WING FIXED L/E INTERIOR BEADED DOUBLER CRACKED XOS 785. REPAIRED THE RT WING BEADED DOUBLER XOS 783-789 IAW SRM 57-40-02, REPAIR 15, FIG 203.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,892 hrs · 12,121 cycles

EMERGENCY BATTERY 1 LOW. R & R EMERGENCY LIGHT BATTERY IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: LIGHT — BROKEN (L1 DOOR SLIDE) · airframe 75,756 hrs · 12,081 cycles

FOUND L1 DOOR EVAC SLIDE DISARM LIGHT BROKEN. R&R L1 DOOR EVAC SLIDE DISARM LIGHT ASSY IAW WDM 52-11-01. CHECK SATISFACTORY.

Part: WARNING LIGHT — FALSE ACTIVATION (EMERGENCY LIGHTS) · airframe 75,669 hrs · 12,066 cycles

DURING PREFLIGHT TEST, EMERGENCY LT BAT 1 LO ILLUMINATED. ACCOMPLISHED OPS CK OF EMERGENCY LT SYS REF AMM 33-50-00-700-802, OPS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHT BATTERY 1 LOW. R & R EMERGENCY BATTERY POWER SUPPLY AND FUNCTION TEST NORMAL IAW AMM 33-51-01-401.

Part: WARNING MESSAGE — FALSE ACTIVATION (FLAP SYSTEM)

AFTER TAKEOFF, A LEVEL 3 FLAPS DISAGREE. CONFIG PG SHOWED FLAPS 15, FOLLOWED QRH FLAPS EXTENDED NORMALLY. PERFORMED FCC RETURN TO SERVICE TESTS AND FOUND NO FAULTS IAW FIM 22-00-00-101. FLAPS OPS CHECKS NORMAL IAW MM 27-50-00-710.

Part: WARNING MESSAGE — FALSE ACTIVATION (EMERGENCY LIGHTS)

WHILE PERFORMING EMERGENCY LIGHT TEST, AMBER EMERGENCY LIGHT BATTERY LEVEL 1 ALERT DISPLAYED. PERFORMED OPS TEST OF EMERGENCY LIGHT BATTERY POWER SUPPLY IAW MM 33-51-01-700-802. OPS CHECKED GOOD.

Part: SPOILER — MALFUNCTIONED (NR 5)

DURING FLIGHT, WINGS LEVEL, F/O CONTROL YOKE DISPLACED 20DEG LT, CAPT CONTROL YOKE DISPLAYED 5DEG LT, TURN COORDINATOR ALIGNED. WHEN CONTROL YOKE RELEASED, ACFT ROLLS RT. REQUIRES 2.3 UNITS OF LT AILERON TRIM FOR WINGS. FOUND NR 5 RT SPOILER FLOATING C/W FIM 27-60-03, SHEET 1, STEPS 1-3, SYS OK.

Part: BUSHING — WORN (SUPPORT FITTING) · airframe 73,711 hrs · 11,588 cycles

1C INSPECTION, RT WING NR 4 SPOILER OTBD SUPPORT FITTING HAS WORN BUSHING. REPAIRED IAW EA 011-5755-01-A5378, REV I/R AND EO 5740- 54511-A.

Part: STRINGER — CRACKED (LT WING) · airframe 73,711 hrs · 11,588 cycles

1C INSPECTION, LT WING STRINGER 43 CRACKED AT STA XORS 297. REPAIRED IAW EA 011-5710-01-A5336 REV I/R AND EO 5710- 54507-A.

Part: STRINGER — CRACKED (LT WING) · airframe 73,711 hrs · 11,588 cycles

1C INSPECTION, LT WING UPPER STRINGER 13 CRACKED AT STA XORS 298. REPAIRED IAW EA 011-5710-01-A5343, REV I/R AND EO 5710-54510-A.

Part: STRINGER — CRACKED (LT WING) · airframe 73,711 hrs · 11,588 cycles

1C INSPECTION, LT WING LOWER STRINGER 32 CRACKED AT STA XORS 917.2. ACCOMPLISHED SPLICE REPAIR ON LT WING LOWER STRINGER 32 AT STA XORS 917.2 IAW EA 011-5710-01-A5320, REV I/R AND EO 5710-54456-A.

Part: STRINGER — CRACKED (LT WING) · airframe 73,711 hrs · 11,588 cycles

DURING 1C INSPECTION, LT WING STRINGER 37 CRACKED AT XORS 917-948. REPAIRED STRINGER IAW SRM 57-00-03, REPAIR 4, FIG 201 AND 202, DWG SG11570005, REV C AND EO 5710-54051-A.

Part: STRINGER — CRACKED (LT WING) · airframe 73,711 hrs · 11,588 cycles

1C INSPECTION, LT WING UPPER STRINGER 15 CRACKED AT STA XORS 264. ACCOMPLISHED REPAIR ON LT WING UPPER STRINGER 15 AT STA XORS 264 IAW EA 011-5710-01-A5338 AND EO 011-5710-54458-A.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 73,711 hrs · 11,588 cycles

DURING A 1C INSPECTION, LEFT INBD FLAP UPPER SKIN CRACKED NEAR XIFH 165. REPAIRED IAW SRM 57-00-01, REPAIR 1, FIG 201.

Part: STRINGER — CRACKED (LT WING) · airframe 73,711 hrs · 11,588 cycles

1C INSPECTION, LT WING LOWER STRINGER 31 CRACKED AT STA XORS 948 ACCOMPLISHED REPAIR SPLICE ON LT WING LOWER STRINGER 31 AT STA XORS 948 IAW EA 011-5710-01-A5330 AND EO MD11-5710-54457-A.

Part: STRINGER — CRACKED (LT WING) · airframe 73,711 hrs · 11,588 cycles

1C INSPECTION, LT WING STRINGER 15 CRACKED XORS 433-455. REPAIRED IAW EA 011-5710-01-A5335, REV IR AND EO MD11-5710-54422-A.

Part: SKIN — DENTED (BS 849) · airframe 73,711 hrs · 11,588 cycles

1C INSPECTION, FUSELAGE SKIN DENTED AT BS 849 L39-40R. REPAIRED IAW EA 011-5329-01-A5329, REV A AND EO MD11-5330-54445-B.

Part: DOUBLER — CRACKED (LT WING) · airframe 73,711 hrs · 11,588 cycles

DURING A 1C INSPECTION, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 614. REPAIRED IAW SRM 57-40-02 REPAIR 15 FIG 206.

Part: SKIN — DENTED (BS 849) · airframe 73,711 hrs · 11,588 cycles

1C INSPECTION, FUSELAGE SKIN DENTED AT BS 849, L39 -- 40R. REPAIRED IAW EA 011-5329-01-A5329, REV I/R AND EO MD11-5330-54445-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 73,711 hrs · 11,588 cycles

DURING A 1C INSPECTION, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED AT XOS 736. REPAIRED IAW SRM 57-40-02, REPAIR 15, FIG 206.

Part: DOUBLER — CRACKED (LT WING) · airframe 73,711 hrs · 11,588 cycles

DURING A 4C INSPECTION, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED AT XOS 792.35 REPAIRED IAW SRM 57-40-02, REPAIR 15, FIG 206.

Part: DOUBLER — CRACKED (LT WING) · airframe 73,711 hrs · 11,588 cycles

DURING 1C INSPECTION, LEFT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 635. FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 15, FIG 203.

Part: STRINGER — CRACKED (RT WING) · airframe 73,711 hrs · 11,588 cycles

DURING 1C INSPECTION, DISCOVERED RT WING UPPER STRINGER 15 CRACKED BETWEEN XORS 433 - 455. REPAIRED STRINGER IAW EA 011-5710-01-A5331 AND EO MD11-5710-54430-A.

Part: BLEED VALVE — INOPERATIVE (APU)

AFTER SELECTING ANTI-ICE ON ALL THREE ENGINES, WINGS, & TAIL, HAD MULTIPLE MALFUNCTIONS, STARTED WITH AVIONICS FAN OVERRIDE, BLEEDS 1 & 2 OFF, DUCTS 1 & 2 OFF CABIN IN FLOW LOW. REVERSED DMP 49-51-2-2, PERFORMED APU RTS OPS BITE TEST. TEST OK MM 49-00-00-700-801. ACCOMPLISHED APU OPS TEST IAW MM 49-10-00-700-801. NO FAULTS AT THIS TIME.

Part: ACCESS PANEL — MISSING (LT ELEVATOR)

LEFT OTBD ELEVATOR MISSING ACCESS PANEL AT BOTTOM OTBD. INSTALLED HINGE COVER IN REF TO CMM 55-21-02.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 71,563 hrs · 11,002 cycles

INSPECTION TYPE:4C, SPLICE FITTING IS CRACKED IN CENTER CARGO AT STA. 5-123 AND L-39R. FABRICATED AND REPLACED SPLICE FITTING IN CENTER CARGO AT STA 5-123 AND L-39R REF DWG A5A7114 AND SRM 51-33-01, PG 1.

Part: SKIN SPLICE — CRACKED (FUSELAGE) · airframe 71,563 hrs · 11,002 cycles

INSPECTION TYPE:4C, SPLICE FITTING IS CRACKED IN CETER CARGO COMPT AT STA 5-123 AND L-37R. FABRICATED AND REPLACED SPLICE FITTING IN CENTER CARGO COMPT AT STA 5-123 AND L-37R IAW DWG A5A7114-519 AND SRM 51-33-01, PG 1.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 71,563 hrs · 11,002 cycles

INSPECTION TYPE:4C, SPLICE FITTING IS CRACKED IN CENTER CARGO AT STA 5-123 AND L-39R. FABRICATED AND REPLACED SPLICE FITTING AT STA 5-123 AND L39R REF DWG A5A7114 AND SRM 51-33-01 PG 1 AND 31.

Part: LONGERON — CORRODED (BS 1754-1812) · airframe 71,563 hrs · 11,002 cycles

INSPECTION TYPE:4C, LONGERON 46R CORRODED BS 1761-1781. FABRICATED & INSTALLED REPLACEMENT LONGERON SECTION IAW EA 011-5310-01-A4566 REV IR AND EO MD11-5310- 50485-A.

Part: LONGERON SPLICE — CRACKED (34 RIGHT) · airframe 71,563 hrs · 11,002 cycles

INSPECTION TYPE:4C, SPLICE FITTING IS CRACKED IN CENTER CARGO STA 5-123 AND L-34R. FABRICATED AND REPLACED SPLICE FITTING AT STA 5-123 AND L-34R IAW DWG A5A7112 AND SRM 51-33-01, PG 1.

Part: INTERCOSTAL — CRACKED (VERTICAL STAB) · airframe 71,563 hrs · 11,002 cycles

INSPECTION TYPE:4C, APPROX .50" CRACK ALONG AFT EDGE OF INTERCOSTAL PN AJC7582-5 AT TYPICAL LOCATION IN RADIUS OF RELIEF CUT OUT FOR VERT STAB AFT SPAR. REPAIRED INTERCOSTAL (PN AJ7582-5) AT VERT STAB AFT SPAR RELIEF CUT OUT REF SRM 55-30-01, FIG 201 REPAIR 2, STASA EA 011- 5530-01-A4557 REV I/R, EO MD11-5530-50324-A.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 71,563 hrs · 11,002 cycles

INSPECTION TYPE:4C SPLICE FITTING IS CRACKED IN CENTER CARGO COMPT AT STA 5-123 AND L-35R. FABRICATED AND REPLACED SPLICE FITTING IN CENTER CARGO COMPT AT STA 5-123 AND L-35R REF DWG A5A7114 AND SRM 51-33-01, PG 1 AND 31.

Part: DOUBLER — CRACKED (LT WING) · airframe 71,563 hrs · 11,002 cycles

INSPECTION TYPE:4C, LT WING FIXED L/E COMPT BEADED DOUBLER CRACKED AROUND TWO FASTENERS AT XOS 715. REPAIRED LT WING L/E COMPT BEADED DOUBLER AT XOS 715 REF EO -5730-48222-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 71,563 hrs · 11,002 cycles

INSPECTION TYPE:4C, LT WING FIXED L/E COMPT BEADED DOUBLER CRACKED AT XOS 709 INBD OF SLAT TRACK 11. REPAIRED LT WING FIXED L/E COMPT BEADED DOUBLER AT XOS 709 REF EO 5730-48222-A APPROX A.

Part: SWITCH — INOPERATIVE (SLIDE PRESSURE)

RT SIDE DOOR ESCAPE SLIDE PRESSURE TEST LIGHT DOES NOT ILLUMINATE WHEN PUSHED. R & R PRESSURE TO TEST SWITCH IAW MM 25-61-04. OPS CKS OK. THIS CLEARS M487705. PLACARD REMOVED.

Part: LIGHT — INOPERATIVE (PRESSURE TEST)

RIGHT SIDE DOOR ESCAPE SLIDE PRESSURE TEST LIGHT DOES NOT ILLUMINATE WHEN PUSHED. OPEN.

Part: BRAKE DISC — FAILED (NR 1 BRAKE)

FIVE MINUTES AFTER LEVEL OFF, LEVEL 1 "TIRE PRESS LOW" ILLUMINATED WITH NR 1 MAIN TIRE PRESSURE DECREASING ON SYNOPTIC, FOLLOWED WITH A LEVEL 2 "TIRE FAIL" FOR THE NR 1 TIRE. EMERGENCY DECLARED. CONFIRM WITH PILOT NO HIGH ENERGY STOP PFM AND CHECK. NR 1 BRAKE DISC BROKEN & NR 2 BRAKE DISC DAMAGED IAW AMM 32-43-20-4 AND AMM 32-41-01-4 REPLACED NR 1 AND NR 2 BRAKE AND TIRE ASSY, AXLE CHECK BRAKE TEMPERATURE SENSOR AND BTM/TPI TEST ALL CONDITIONS NORMAL IAW AMM 05-56-01-6 PFM HIGH ENERGY STOP INSPECTION CHECK. CONDITION NORMAL.

Part: DOUBLER — CRACKED (LT WING) · airframe 68,855 hrs · 10,311 cycles

INSPECTION TYPE:3C, SPLICE STRAP CRACKED IN LT WING L/E AT STA XOS789. REMOVED, FABRICATED & INSTALLED REPLACEMENT STRAP (DOUBLER) IN LT WING L/E INTERIOR AT STA XOS789 IAW DWG ARB3954, SRM 51-31-01, 51-33-01, 51-21-01.

Part: DOUBLER — CRACKED (LT WING) · airframe 68,855 hrs · 10,311 cycles

INSPECTION TYPE:3C, BEADED DOUBLER CRACKED IN LT WING L/E AT STA XOS .665 REPAIRED BEADED DOUBLER IN LT WING L/E INTERIOR STA XOS661-667 IAW EO-5730-42916-B AND SRM 57-40-02, REPAIR 9, FIG 203.

Part: DOUBLER — CRACKED (LT WING) · airframe 68,855 hrs · 10,311 cycles

INSPECTION TYPE:3C, SPLICE STRAP CRACKED IN LT WING L/E INBD END OF PANEL 526FB AT STA 906. REMOVED FABRICATED AND INSTALLED REPLACEMENT STRAP (DOUBLER) IN LT WING L/E INTERIOR AT STA 906 IAW DWG ARB3954, SRM 51-31-01, 51-33-01 , 51-21-01.

Part: SKIN — CRACKED (LWS 490) · airframe 68,855 hrs · 10,311 cycles

INSPECTION TYPE:3C, LT WING L/E IS CRACKED AT STA XOS490. REPAIRED LT WING L/E SKIN LOWER SURFACE AT XOS490 IAW EO MD11-5730- 45747-A AND STASA EA 011-5730-01-A3638, REV IR.

Part: SKIN — CRACKED (RT WING) · airframe 68,855 hrs · 10,311 cycles

INSPECTION TYPE:3C, CRACK AT INBD CORNER OF FUEL REFUEL/DEFUEL ON DOOR RT WING FIXED L/E AT STA XOS612. REPAIRED RT WING FIXED L/E LOWER SKIN AT STA XOS610 IAW EO-5730- 45707-A AND STA SA EA 011-5730-01-A3631 REV IR.

Part: DOUBLER — CRACKED (LT WING) · airframe 68,855 hrs · 10,311 cycles

INSPECTION TYPE:3C, SPLICE STRAP CRACKED IN LT WING AT STA XOS667. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SPLICE STRAP (DOUBLER) IN LT WING L/E INTERIOR AT STA XOS667 IAW DWG ARB3954, SRM 51-31-01, 51-33-01, 51-21-01.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 68,855 hrs · 10,311 cycles

INSPECTION TYPE:3C, FLOOR PANEL 262LF HAS BROKEN INSERT AND DELAMINATION AS MARKED. REMOVED FABRICATED AND INSTALLED REPLACEMENT FLOOR PANEL 262LF IN MAIN CARGO COMPARTMENT IAW EO MD11-5320-27386-C & DWG AEA0181.

Part: SKIN — DAMAGED (BS 1801 L41R)

FUSELAGE SKIN DAMAGED AT STA 1801, L41R. REMOVED DAMAGE AND REPAIRED IAW EO MD11-5330-35464.

Part: SKIN — DENTED (FUSELAGE)

SKIN DENTED, STA X-13.25. REPAIRED IAW EO MD11-5330-40624-C.

Part: DOUBLER — CRACKED (RT WING) · airframe 68,855 hrs · 10,311 cycles

INSPECTION TYPE:3C, RT WING FIXED L/E COMPT INBD OF SLAT TRACK NR 10 BEADED DOUBLER CRACKED. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS648-653 IAW EO MD11-5730-42916-B AND SRM 57-40-02 REPAIR 9, FIG 203.

Part: DOUBLER — CRACKED (RT WING) · airframe 68,855 hrs · 10,311 cycles

INSPECTION TYPE:3C, RT WING FIXED L/E COMPT INBD OF SLAT TRACK NR 11 BEADED DOUBLER CRACKED 3 PLACES. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS692-708 IAW EO MD11-5730-42916-B AND SRM 57-40-02, REPAIR 9, FIG 203.

Part: FRAME — CHAFED (BS 469 L47-48L) · airframe 65,890 hrs · 9,611 cycles

INSPECTION TYPE:2C, FWD AVIONIC COMPARMENT AT STA 469 LT IN BTWN L47-48. INTERCOSTAL INNER FLANGE HAS 2 EA CHAFE MARKS LT RAM AIR DUCT LOCATION. ACCOMPLISHED REPAIR IAW STA-SA EA 011-5310-01-A2718 I/R AND EO MD11-5310-40036-A.

Part: FINGER DOUBLER — DAMAGED (STA 630 L47L) · airframe 65,890 hrs · 9,611 cycles

INSPECTION TYPE:1C, PERFORM DVI OF EXPOSED STRUCTURE OF SKIN REMOVED FROM STA 595 TO 765 AND L36L TO L48L. FOUND HOLE ENLONGATED AT STA 630 ON FINGER DOUBLER BETWEEN L47L AND L48L. REMOVED DAMAGE ON EXISTING FINGER DOUBLER BETWEEN STA 615 AND STA 635 L47L AND L48L. (FINGER DOUBLER NOT REMOVED) C/W EA 011-5330-01-A2683 I /R AND EO MD11-5330-40019-A.

Part: LONGERON — DAMAGED (FS 739 L46L) · airframe 65,890 hrs · 9,611 cycles

INSPECTION TYPE:2C PERFORMED DVI OF EXPOSED STRUCTURE OF SKIN REMOVED FROM STA 595 TO 765 AND L36L TO L48L. FOUND LONGERON HOLE ENLONGATED AT STA 735 AND L46L. REMOVED LONGERON 46 FROM FS 739-FS 765. FABRICATED REPLACEMENT LONGERON AND INSTALLED REF DWG ACA0150 AND SRM 51-35-01 PG 3 AND SRM 51-33-01 PG 30-32.

Part: LONGERON — DAMAGED (STA 650 L47L) · airframe 65,890 hrs · 9,611 cycles

INSPECTION TYPE:1C, PERFORM DVI OF EXPOSED STRUCTURE OF SKIN FROM STA 595 TO STA 765 AND L36L TO L48L. FOUND L47L WITH ENLONGATED HOLE AT STA 650. REMOVED DAMAGED SECTION OF LONGERON 47L FROM FS 595 TO FS 685. FABRICATED LONGERON REPLACEMENT AND INSTALLED REF SRM 53-20-05 FIG 1 PG 1 AND 2.

Part: SKIN — CHAFED (RT WING) · airframe 65,890 hrs · 9,611 cycles

INSPECTION TYPE:2C, RT WING TOP FWD SURFACE SCAB PATCH IS CHAFED AND HAS 1 EA SLIGHT GOUGE FROM CONTACT. LOCATED BTWN NR1 AND NR2 SLATS, WING STA 230.360 REMOVED DAMAGED DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-40-02, REPAIR 8.

Part: SKIN — GOUGED (LT WING) · airframe 65,890 hrs · 9,611 cycles

INSPECTION TYPE:2C, LT WING UPPER SURFACE HAS A DEEP GOUGE, INBD L/E AT SLAT NR2 POSTION. REMOVED DAMAGE, FABRICATED AND INSTALLED DOULBER IAW SRM 57-40-02, REPAIR 8,

Part: SKIN — DELAMINATED (LT O/B AILERON) · airframe 65,890 hrs · 9,611 cycles

INSPECTION TYPE:2C, LT WING OTBD AILERON LOWER SURFACE, INBD FWD CORNER IS CHIPPED AND DELAMINATED. REMOVED DAMAGE, AND ACCOMPLISHED REPAIR IAW STA-SA EA 011-5751-01-A2684 I/R AND EO MD11-5750-39887-A.

Part: DOUBLER — CRACKED (LT WING L/E) · airframe 65,890 hrs · 9,611 cycles

INSPECTION TYPE:2C, LT WING L/E COMP AT XOS 547, CEILING DOUBLER HAS CRACKS AT 2 EA FASTNERS. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR FILLER, DOUBLER, AND ANGLES IAW SRM 57-40-02 FIG 203, REPAIR 9.

Part: STRUCTURE — CHAFED (LT WING L/E) · airframe 65,890 hrs · 9,611 cycles

INSPECTION TYPE:2C, LT WING L/E AT NR 10 SLAT TRACK CAVITY OPENING, INBD EDGE IS CHAFED AND REPAIR PATCH IS CHAFED. REMOVED PATCH, FABRICATED AND INSTALLED REPAIR DOUBLER IAW STA-SA EA 011-5750-01-A2703 I/R AND EO MD11-5730-40040-A.

Part: DOUBLER — CRACKED (LT WING L/E) · airframe 65,890 hrs · 9,611 cycles

INSPECTION TYPE:2C, LT WING L/E COMPARTMENT AT XOS 758 CEILING DOUBLER IS CRACKED AT FASTNER. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER AND ANGLES IAW SRM 57-40-02, REPAIR 9, FIG 203.

Part: SKIN — DENTED (STA 645 L45L) · airframe 65,890 hrs · 9,611 cycles

INSPECTION TYPE:1C, DEFERED ITEM D-414045 FUSELAGE SKIN DENTED REPAIR STA 645 BETWEEN L45L AND L48L. REMOVED FWD FUSELAGE SKIN BETWEEN STA 595-STA 765 AND L36L-L48L. INSTALLED REPLACEMENT SKIN REF EA 011-5330-01-A2668 AND EO MD11-5330-40019- A.

Part: CONTROL UNIT — INOPERATIVE (COCKPIT)

AFTER ABOUT 42 MINUTES OF FLIGHT TIME, LEVEL 1 EMERGENCY POWER ON DISPLAYED. TRIED TO RECYCLE EMERGENCY POWER SWITCH NO CHANGE. DUMPED 40,000 LBS FUEL FOR RETURN TO DEPARTURE. EPCU FAULT "ADG BATT CTL RLY/INTFC" INDICATED ON CFDS. CURRENT FAULTS, R & R EPCU IAW AMM 24-08-01 IAW FIM PROCEDURE 24-24-06-00. ALSO REPLACED LT EMERGENCY AC BUSS SENSE RELAY AS PRECAUTION. NO CURRENT FAULTS IND. OK TO CONT.

Part: DUCT — DAMAGED (RT WING)

RT WING ANTI-ICE TELESCOPING DUCT OTBD FORMER DAMAGED STA XOS=470.20. REPAIRED IAW EO MD11-5740-36741-B.

Part: DUCT — SEPARATED (RT WING)

WING ANTI ICE DISAGREE ALERT AT ROTATION WITH ENG WING AND TAIL ANTI ICE ON FOR TAKEOFF. ENG NR3 BLEED VALVE WOULD CLOSE AND NR3 PACK FLOW ALERT WOULD ILLUMINATE. FOUND RT WING TELESCOPE DUCT SEPARATED FROM WING DUCT DUE TO MISSING NUT. REPLACED ATTACHING HARDWARE REF IPC 30-11-05 FIG 101 ITEMS 250-265-275.

Part: RCCB — FAILED (ELECT BUSS)

2 FCC DATA FAULTS (2A,2B) HYD 3 PUMP OFF ALERT, AVIONICS FAN OVERRIDE ALERT. FOUND 3 DC BUSS RCCB B1-894 IAW AMM 24-50-01-4 FAILED. ALSO, REPLACED R2-10 AND R2-5153 IAW AMM 24-32-00-5 & SWPM 20-00-09. RAN ENGINES. ALL ELECTRICAL BUSS OPERATED NORMALLY. REF 71-00-00 AND AMM 24-31-0 AND AMM 24-30-00.

Part: OIL SYSTEM — LOW PRESSURE (NR 2 ENGINE)

NR 2 ENGINE IFSD DUE TO LOW OIL PRESSURE. CREW DECLARED AN EMERGENCY. A/C IS OOS FOR ENGINE CHANGE. R & R NR 2 ENGINE REF TC NO 9130. OPS AND LEAK CHECK OK PER TC 9103

Part: LIGHT — NO TEST (DOOR SLIDE)

INSPECTION TYPE:N/A LT CREW ENTRY DOOR SLIDE LIGHT DOES NOT TEST. DI M414285 ASSIGNED. RELAMPED, OPS CHECK GOOD PER MM 25-61-04-5. THIS CLEARS M414285. VERIFIED PLUG AND JACK CONNECTED REF DMP 25-61-2.

Part: SKIN — DAMAGED (FUSELAGE)

INSPECTION TYPE:IN FLC DOOR CUTOUT AFT SIDE, APPROX 3 FEET UP FROM LOWER CORNER DAMAGED SKIN. DAMAGE LOCATED 10 INCHES FROM LOWER AFT CORNER REPAIR. REMOVED DAMAGE AND REPAIRED IAW EO MD11-5330-35746-A.

Part: GIRT BAR — OUT OF POSITION (R1 DOOR)

GIRT BAR ON R1 DOOR HANGING FROM ONE SIDE. REINSTALLED GIRT BAR PER AMM 25-61-15-4. OPS CK GOOD.

Part: PANEL — DELAMINATED (ELEVATOR) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1C PANEL 346BB ON BOTTOM SIDE OUTBD ELEVATOR DELAMINATED. REMOVED DAMAGE FROM RT OUTBD ELEVATOR LE AND REPAIRED RT OUTBD ELEVATOR LE REF MD11 SRM VOL 1 55-90-00 FIG 3 PARA 4A (2) (A) REV 40.

Part: AILERON — DELAMINATED (LT WING) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1C LT OUTBOARD AILERON TRAILING EDGE HAS SMALL DELAMINATED. REMOVED PAD AND FINISH, PREPARED AND APPLIED WET LAY-UP REPAIR IAW IPXA EO MD11-5750-34605-A AND SAA EA 011-5751-01-1791.

Part: WEB — DAMAGED (CARGO BAY) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1C CENTER CARGO AT FS 1787 ABOVE LONGERON 43R HAS 1EA ELONGATED HOLE THRU WEB AND BEAM. REAMED HOLE, FABRICATED AND INSTALLED REPAIR IAW SAA EA 011-5310- 01-A1968 AND IPXA EO MD11-5310-34626-A.

Part: SKIN — MISREPAIRED (RUDDER) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1C REPAIR SEQUENCE NUMBER 296-S4-01, STA ZFR 381.680 TO STA ZFR386.880 DOES NOT CORRELATE TO SRM. REMOVED REPAIR, REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW UPS EO MD11-5540-34577-B AND SAA EA 011-5440-01-A1965 REV A.

Part: SLAT — MISREPAIRED (LT WING) · airframe 633,544 hrs · 9,017 cycles

INSPECTION TYPE:1/C REPAIR SURVEY SEQ 296-W3-13 LT NR 5 SLAT BETWEEN STA XOS 659-662 REPAIR DOUBLER NOT PER SRM. REMOVED, FABBED AND INSTALLED REPAIR DOUBLER IAW UPS EO MD11-5750-3457 6-A AND SAA EA 011-5754-01-A1958.

Part: SKIN — MISREPAIRED (LE SLAT) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQUENCE 296-W4-06 RIGHT NR 8 SLAT BETWEEN STA XOS 1158 - XOS 1173 EXTERIOR EXISTING DOUBLER NOT PER SRM 57-10-00 VOL 1 PG 13 NOTE -1. REMOVED DOUBLER, REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR UPPER AND LOWER SEALS, SPLICE PLATE, SKIN FILLER, BAFFLES, AND SUPPORTS.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQUENCE 296-F1-18 FASTENER SPACING NOT WITHIN THE ALLOWABLE LIMITS IAW SRM 53-20-00 VOL 1 FIG 2 SHEET 1-3. REMOVED, FABRICATED AND INSTALLED 2EA REPAIR DOUBLERS AND 3EA REPAIR FILLERS PER MD11 SRM 53-00-01 FIG 201 SHEET 7 & 8 AND MD11-53-00-01 FIG 1 ITEM 5 AND MD11 SRM 53-00-01 REPAIR 1.

Part: DOUBLER — GOUGED (TE FLAP) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQ 296-W4-13 RT WING INBOARD FLAP UPPER L/E BETWEEN STA X IFH217.399-225.140 EXISTING PREVIOUS DOUBLER GOUGED. REMOVED EXISTING REPAIR (REPAIR SURVEY SEQ 296-W4-13) AT RT WING INBOARD FLAP UPPER L/E BETWEEN XIFH 216.3-XIFH 217.3. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF EO MD11-5750-34564 AND EA 011-5730-01-A19 67.

Part: SKIN — MISREPAIRED (CARGO DOOR) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQ 296-F1-13 NOT IN SRM REPAIRS. REMOVED EXISTING REPAIR ON AFT CARGO DOOR SKIN. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF EO MD11-5230-34640-A AND EA 011- 5231-01-A1952.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1C FOUND BULK CARGO DOOR LOWER AFT CORNER BROKEN (CRACKED). STOP DRILLED L ANGLE ON BULK CARGO DOOR LOWER AFT CORNER. FABRICATED A ND INSTALLED REPAIR DOUBLER REF EO MD11-5230-34644-A AND EA 011-5230- 01-A1966.

Part: SLAT — MISREPAIRED (RT WING) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1/C REPAIR SURVEY SEQ 296-W4-04 RT NR 3 SLAT BETWEEN STA XOS484-490 REPAIR DOUBLER NOT IN SRM. REMOVED, FABBED AND INSTALLED REPAIR DOUBLER IAW UPS EO MD11-5750-345 91-A AND SAA EA 011-5754-01-A1964.

Part: SKIN — MISREPAIRED (LE SLAT) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1/C REPAIR SURVEY SEQ 296-W4-02 AND VALIDATION EO MD11-5100-34211-A ITEM 8 RT WING NR 2 SLAT UNDERSIDE PREVIOUS LARGE DOUBLER 1EA 5/32 CHERRY MAX RIVET HAS ED OF .25. REMOVED, FABBED AND INSTALLED REPAIR DOUBLER IAW UPS EO MD11-5750-34 566-A AND SAAEA 011-5730-01-A1947.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQUENCE 296-F1-12, LT AFT TAIL BODY BETWEEN STA 2007 AND STA 2011, LONGERON 46L AND 48L IS NOT CORRELATED WITH MD-11 SRM AND HAS PITCH AND ED OUT OF TOLERANCE. REMOVED DOUBLER, REAMED 9 HOLES, FABRICATED AND INSTALLED DOUBLER IAW IPXA EO MD11-5330-34588-B AND SAA EA 011-5330-01-A1969 REV A.

Part: STRUCTURE — MISREPAIRED (FUSELAGE) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1C REPAIR SEQUENCE 296-F1-15, LT FWD INTERMEDIATE FUSELAGE BETWEEN STA 999 AND 1019, L42L AND L44L. FASTENERS AND EXT DOUBLER THICKNESS FOUND NOT IAW MD-11 SRM 53-20-00 FIG 6. REMOVED DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLERS IAW MD-11 SRM 53-20-00 FIG 2 SHT 2 REV 40.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQUENCE 296F1-11 RT AFT TAIL BODY BETWEEN STA 2028.750 AND STA 2038.750, LONGERON 39 AND LONGERON 40 IS NOT CORRELATED TO SRM. COMPLIED WITH EO MD-11-5330-34628-A AND EA 011-5330-01-A1955.

Part: SKIN — MISREPAIRED (STA 2007/L43R) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQ 296-F1-10 STA 2007 AND STA 2033.750, L43R-L44R NOT CORRELATED WITH MD11 SRM. REMOVED EXISTING REPAIR (REPAIR SURVEY 296-F1-10) FROM RT AFT FUSELAGE BETWEEN STA 2007-2020 AND L43R-L45R. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF EO MD11-5330-34546 AND EA 011-5330-01-A1945 REV A.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1/C REPAIR SURVEY SEQ 296-F1-09, RT AFT TAIL BODY BETWEEN STA 2007 AND 2011, L 46R - 48L HAS NO SRM AND EDGE DISTANCE OUT OF TOLERANCE. REMOVED, FABBED AND INSTALLED REPAIR DOUBLER IAW UPS EO MD11-5330-345 88-A AND SAA EA 011-5330-01-A1969.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQ 296-F1-02 STA 615 AND 635, L45R-L47R NOT CORRELATED WITH MD11 SRM 53-20-00 VOL 1, FIG 6, EXTERNAL DOUBLER NOT CORRELATED WITH THICKNESS. REMOVED EXISTING REPAIR SURVEY SEQ 296-F1-02 AT STA 624 AND L46R FABRICATED AND INSTALLED REPLACEMENT REPAIR REF EO MD11-5330-34555-A AND EA 011-5330-01-A1944.

Part: PRESSURE PANEL — MISREPAIRED (FUSELAGE) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQ 296-F2-01 NOT CORRELATED TO MD11 SRM. LOCATED AT NOSE LANDING GEAR HORIZONTAL PRESSURE PANEL BETWEEN STA 515 AND STA 535 LBL 4 AND RBL 4. REMOVED EXISTING REPAIR AT STA 515 - 535 BETWEEN X=0.00 AND X=-7.81. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF EO MD11-5310-34608-A AND EA 011-5330-01-A1951.

Part: SKIN — ACTIVATED (SPOILER) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1C LT WING NR 1 SPOILER PANEL LOWER SKIN SURFACE HAS SEVERAL DINGS. REMOVED DAMAGE ON NR 1 SPOILER PANEL LOWER SKIN SURFACE IN 2 AREAS. FABRICATED AND INSTALLED REPAIR DOUBLERS REF MD11 SRM 51-71-00 VOL 2 TABLE 8.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQ 296-F1-08, EXTERNAL DOUBLER IS GOUGED, STA 1801 AND 1821, L34R - L37R. REMOVED EXISTING REPAIR (REPAIR SURVEY SEQ 296-F1-08) AT STA 1801 - 1821 AND L34R-L37R. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF EO MD11-5330-34651-A AND EA 001-5330-01-A1961.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQUENCE 296-F1-07, REPAIR OUTER DOUBLER IS GOUGED STA 1781 AND 1801, L39R-L45R. REMOVED REPAIR DOUBLERS AND FILLERS, FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLERS IAW MD-11 SRM 53-50-00 FIG 17 SHT 3 & 9.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQUENCE 296-F1-05, EXTERNAL DOUBLER IS GOUGED, BETWEEN STA 999 AND STA 1019, L38R-L43R. REMOVED DOUBLERS, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW MD-11 SRM 53-00-15 REPAIR 8 FIG 202 AND FIG 203.

Part: DOUBLER — CRACKED (RT WING) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1C RT WING FIXED L/E 2 EA ARE ON BEADED DOUBLER CRACK AT XOS 667. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER, FILLER, AND ANGLES IAW MD-11 SRM 57-10-00 FIG 27 SHT 1-4.

Part: FASTENER — LOOSE (LE SLAT) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQUENCE 296-W4-07 RT WING NR 8 SLAT BETWEEN STA XOS 1188- XOS 1177 REPAIR DOUBLER HAS LOOSE FASTENERS. REMOVED DOUBLER, CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR UPPER AND LOWER SEALS, SPLICE PLATE, SKIN FILLER, BAFFLES & SUPPORTS IAW IPXA EO MD11-5750-3461-A AND SAA EA 011-5730-A1950.

Part: SKIN — MISREPAIRED (LT WING) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQ 296-W3-02 REPAIR DOUBLER NOT PER SRM LT WING FIXED L/E BETWEEN STA XOS459 - XOS475. REMOVED EXISTING REPAIR (REPAIR SURVEY SEQ 296-W3-02) FROM LT WING FIXED L/E BETWEEN XOS459 AND XOS475. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF EO MD11-5730-34590-A AND EA 011-5730-01-A1942.

Part: DOUBLER — CRACKED (RT WING) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1C RT WING FIXED L/E 2 EA AREA ON BEADED DOUBLER CRACK AT STA 542. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER, FILLER, AND ANGLES IAW MD-11 SRM 57-10-00 FIG 27 SHT 1-4.

Part: SKIN — MISREPAIRED (LT WING) · airframe 633,354 hrs · 9,017 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQUENCE 296-W3-03 REPAIR DOUBLER INSTALLATION USED BLIND FASTENERS IN LIEU OF SOLID FASTENERS LT WING FIXED L/E BETWEEN STA XOS 650-658. REMOVED DOUBLER, REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER, SPLICE DOUBLER, AND FILLER IAW IPXA EO MD11-5730-34634-A AND SAA EA 011-5730-01-A1956.

Part: DOUBLER — GOUGED (RT WING) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQUENCE 296-W4-09 RIGHT WING FIXED L/E UPPER BETWEEN STA XIS 241-XIS 252 REPAIR DOUBLER HAS GOUGE. REMOVED DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER IAW IPXA EO MD11-5730-34184-A AND SAA EA 011-5730-01-A1949.

Part: FLOORBEAM — DENTED (FUSELAGE) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1C TRANSFERRED FROM LP 061825 ITEM 2 REF D402822 - MAIN DECK FLOORBEAM LOWER FLANGE DENTED AT STA 979. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND REPAIR ANGLES IAW UPS EO MD11-5310-33894-B AND SAA EA 011-5310-01-A1941.

Part: FLOORBEAM — DENTED (FUSELAGE) · airframe 63,354 hrs · 9,017 cycles

INSPECTION TYPE:1C TRANSFERRED FROM LP 061825 ITEM 1 REFD402821- MAIN DECK FLOORBEAM LOWER FLANGE DENTED AT STA 939 REF EOMD11-5310-33894-A. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND REPAIR ANGLES IAW UPS EO MD11-5310-33894-B AND SAA EA 011-5310-01-A1940.

Part: RIB — CRACKED (RT WING)

RT UPPER WINGLET ASSY HAS DAMAGED COMPOSITE RIB ON BOTTOM END OF ASSY RIB HAS 2 AREAS CRACKED AT OUTER SKIN. REPAIRED PER EO C-5720-33537-A.

Part: CAP — ERODED (RT WINGLET)

RT UPPER WINGLET CAP HAS EROSION. REPAIRED IAW EO MD11-5720-32859-A.

Part: WINGLET — DAMAGED (RT WING)

RT UPPER WINGLET ASSY HAS DAMAGED COMPOSITE RIB ON BOTTOM END OF ASSY. RIB HAS 2 AREAS CRACKED AT OUTER SKIN ATTACHMENT TO RIB. PART WAS ORIGINALLY INSTALLED ON ACFT. PART WAS TRANSFERRED TO RO SR1417801. REMOVED DAMAGE AND REPAIRED IAW EO C-5720-33537-A.

Part: WINGLET — DAMAGED (RT WING)

RT UPPER WINGLET ASSY HAS 3 DAMAGED AREAS ALONG T/E. REMOVED DAMAGE AND REPAIRED IAW EO C-5720-33537-A.

Part: BOTTLE — LOW PRESSURE (EVAC SLIDE)

INSPECTION TYPE:N/A L1 DOOR SLIDE'S BOTTLE PRESSURE IS LOW PER TEMPERATURE COMPENSATED GREEN BAND ON GAUGE PRESSURE SWITCH IS CLOSED DUE TO LOW PSI. REPLACED L1 DOOR SLIDE ASSY IAW MD-11 MM 25-61-01-4. THIS CLEARS M-391314. PLACARD REMOVED.

Part: BATTERY — DISCHARGED (EVAC SLIDE)

INSPECTION TYPE:N/A L-1 DOOR SLIDE PRESSURE NO PTT REF M388837. REPLACED BATTERIES. OPS CHECKS GOOD PER MM 25-61-04-5. THIS CLEARS M388837, PLACARDS REMOVED.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A EMERGENCY LIGHTING SYSTEM INOP. PERFORMED ADJUSTMENT / TEST IAW 33-50-00-5. SYSTEM OPERATIONAL TEST CHECKED GOOD. THIS CLEARS M388756.

Part: SLIDE — INOPERATIVE (L1 DOOR)

INSPECTION TYPE:N/A L-1 DOOR ESCAPE SLIDE INOP. REMOVED AND REPLACED ESCAPE SLIDE ASSY PER MM 25-61-15-4. THIS CLEARS M388750.

Part: HINGE — CORRODED (T/E FLAP)

INSPECTION TYPE:N/A LT WING O/B FLAP O/B FWD HINGE BARREL NUT UPPER BORE CORRODED. LT WING O/B FLAP O/B FWD HINGE BARREL NUT UPPER BORE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09.

Part: HINGE — CORRODED (T/E FLAP)

INSPECTION TYPE:N/A LT WING O/B FLAP I/B FWD HINGE LOWER MOUNT O/B BORE CORRODED. LT WING O/B FLAP I/B FWD HINGE LOWER MOUNT O/B BORE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08.

Part: HINGE — CORRODED (T/E FLAP)

INSPECTION TYPE:N/A LT WING O/B FLAP O/B FWD HINGE BARREL NUT LOWER BORE CORRODED. LT WING O/B FLAP O/B FWD HINGE BARREL NUT LOWER BORE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09.

Part: HINGE — CORRODED (T/E FLAP)

INSPECTION TYPE:N/A LT WING O/B FLAP I/B FWD HINGE UPPER MOUNT O/B BORE FWD & AFT SPOT FACE CORRODED. LT WING O/B FLAP I/B FWD HINGE UPPER MOUNT O/B BORE FWD & AFT SPOT FACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08.

Part: HINGE — CORRODED (T/E FLAP)

INSPECTION TYPE:N/A LT WING O/B FLAP O/B FWD HINGE LOWER MOUNT O/B BORE CORRODED. LT WING O/B FLAP O/B FWD HINGE LOWER MOUNT O/B BORE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09.

Part: HINGE — CORRODED (T/E FLAP)

INSPECTION TYPE:N/A LT WING O/B FLAP O/B FWD HINGE LOWER MOUNT I/B BORE FWD & AFT SPOTFACE CORRODED. LT WING O/B FLAP O/B FWD HINGE LOWER MOUNT I/B BORE FWD & AFT SPOTFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09.

Part: HINGE — CORRODED (T/E FLAP)

INSPECTION TYPE:N/A LT WING O/B FLAP I/B FWD HINGE LOWER MOUNT O/B BORE FWD & AFT SPOT FACE CORRODED. LT WING O/B FLAP I/B FWD HINGE LOWER MOUNT O/B BORE SPOTFACE CORROSION REMOVED AS PER CMM 57-44-08 AND FOUND WITHIN DWG ARC0502 LIMIT. REPAIR CARRIED OUT AS PER CMM 57-44-08.

Part: HINGE — CORRODED (T/E FLAP)

INSPECTION TYPE:N/A RT WING O/B FLAP O/B FWD HINGE LOWER MOUNT O/B BORE FWD & AFT SPOTFACE CORRODED. RT WING O/B FLAP O/B FWD HINGE LOWER MOUNT O/B BORE FWD & AFT SPOT FACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09.

Part: HINGE — CORRODED (T/E FLAP)

INSPECTION TYPE:N/A LT WING O/B FLAP O/B FWD HINGE UPPER MOUNT I/B BORE FWD SPOTFACE CORROSION. LT WING O/B FLAP O/B FWD HINGE UPPER MOUNT I/B BORE FWD SPOTFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09.

Part: HINGE — CORRODED (T/E FLAP)

INSPECTION TYPE:N/A LT WING O/B FLAP I/B FWD HINGE BARREL NUT LOWER BORE CORRODED. LT WING O/B FLAP I/B FWD HINGE BARREL NUT LOWER BORE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08.

Part: HINGE — CORRODED (T/E FLAP)

INSPECTION TYPE:N/A LT WING O/B FLAP I/B FWD HINGE BARREL NUT UPPER BORE CORRODED. LT WING O/B FLAP I/B FWD HINGE BARREL NUT UPPER BORE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08.

Part: HINGE — CORRODED (T/E FLAP)

INSPECTION TYPE:N/A RT WING O/B FLAP O/B AFT HINGE UPPER MOUNTING CENTER BORE CORRODED. RT WING O/B FLAP O/B AFT HINGE UPPER MOUNTING CENTER BORE CORROSION REMOVED AS PER BSOPM 20-11-02 AND FOUND WITHIN LIMIT AS PER DWG ARC1991.

Part: HINGE — CORRODED (T/E FLAP)

INSPECTION TYPE:N/A RT WING O/B FLAP O/B AFT HINGE I/B PIVOT I/B SPOTFACE CORRODED. RT WING O/B FLAP O/B AFT HINGE I/B PIVOT I/B SPOTFACE CORROSION REMOVED AND REPAIR CARRIED OUT AS PER CMM 57-52-04.

Part: HINGE — CORRODED (T/E FLAP)

INSPECTION TYPE:N/A RT WING O/B FLAP AFT HINGE O/B PIVOT BORE CORRODED. RT WING O/B FLAP O/B AFT HINGE O/B PIVOT BORE CORROSION REMOVED AND REPAIR CARRIED OUT AS PER CMM 57-52-04.

Part: HINGE — CORRODED (T/E FLAP)

INSPECTION TYPE:N/A LT WING O/B FLAP I/B AFT HINGE I/B PIVOT I/B SPOTFACE CORRODED. LT WING O/B FLAP I/B AFT HINGE I/B PIVOT SPOTFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-52-04.

Part: STRUCTURE — CORRODED (AIR CON BAY) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE-C, AIR CON SYS NR 1 COMPARTMENT INTERIOR, AFT BILGE AREA, EXISTING ANGLE DOUBLER FOUND CORRODED. ATTACH CORROSION FRAME SUPPORTS AND RIB REMOVED IAW SR M51-31-01 VII R35. FRAME, SUPPORTS AND RIB CORROSION REMOVED IAW SRM 51-21-01 VII R35. REWORK AREA CLEANED AND REPROTECTED IAW SRM 51-21-01 VII R35. REINSTALLED FRAME,SUPPORTS & RIB ON FUSELAGE AIR CON NR 1 SYS INTERIOR BILGE AREA IAW SRM 51-31-01 VII R35.

Part: HINGE — CORRODED (RT WING TE FLAP) · airframe 61,716 hrs · 5,867 cycles

INSPECTION TYPE:C, RT WING OB FLAP OB FWD HINGE ACTUATOR MOUNTED IB BORE FOUND CORRODED. RT OB FLAP OB HINGE ACTUATOR MOUNTED IB BORE CORROSION REMOVED AND FOUND EXCEED LIMIT IAW CMM57-44-09 PG 602-607 R61.FPI C/O IAW DAC NDT SP R13 PT 08 ON REWORK AREA, FOUND NO CRACK AND NO CORROSION EVIDENT. REWORKED AREA ETCH INSPECTED AND FOUND SATIS IAW EN1298-08.BUSHING FAB IAW EN1298-08. FABRICATED BUSHING INSTALLED IAW EN 1298-08.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR 35 FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 VII REV 35. BORE REAM TO 1.178"DIA, REMAINING BLEND OUT 0.095" DEEP, BOTTOM REMAINING BLEND OUT 0.068"DEEP, FOUND EXCEEDING LIMITS IAW EO MD11-5510-19409M.10X MAGN DVI C/O & FOUND NO CORROSION EVIDENT. REPAIRED BARREL NUT BORE NR 35 RT WAS ACCOMPLISHED IAW EN1254-08 & IS ACCEPTABLE IAW EO MD11-5510-30012A.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE-C, RT HORZ STAB BARREL NUT BORE NR 19 FOUND CORRODED EXISTING REPAIR SLEEVE BUSHING REMOVED. BORE SURFACE CLEANED & MEASURE 1.126" DIA, BOTTOM SURFACE CLEANED & MAT'L THK REMAINING 0.082" MIN, FOUND BORE CLEAN HOLE COND * BORE SIZE EXCEED LIMITS IAW EO MD11-5510-19409 M.10X MAGN DVI C/O & FOUND NO CORROSION EVIDENT. REPAIRED BARREL NUT BORE NR19 RT WAS ACCOMP IAW EN1257-08 & IS ACCEPT IAW EO MD11-5510-30011A.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR 22 FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 VII REV 35. BORE REAM TO 1.067" DIA, REMAINING BLEND OUT 0.040" DEEP, BOTTOM SURFACE REMAINING BLEND OUT 0.055" DEEP, BORE BLEND OUT EXCEED EO LIMITS IAW EO MD11-5 510-19409M.10X MAGN DVI C/O & FOUND NO CORROSION EVIDENT. REPAIRED B/N BORE NR 22 RT WAS ACCOMP IAW EN1253-08 & IS ACCEPT IAW MD11-5510-30011A.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR 16 FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 VII REV 35. BORE REAM TO 1.067"DIA, REMAINING BLEND OUT 0.068" DEEP, BOTTOM SURFACE CLEAN & BORE BLEND OUT, EXCEEDED LIMITS IAW EO MD11-5510-19409M.10X MAGN DVI C/O & FOUND NO CORROSION EVIDENT. REPAIR BARREL NUT BORE NR 16 RT WAS ACCOMPLISHED IAW EN1246-08 & IS ACCEPTABLE IAW EO MD11-5510-30011A.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE-C, LT HORIZ STAB BARREL NUT BORE NR 22 FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 VII REV 35. BORE REAM TO 1.067" DIA, REMAINING BLEND OUT 0.015" DEEP, BOTTOM SURFACE CLEANED, BLEND OUT AT SIDEWALL FOUND OUT OF LIMITS IAW EO MD11-5510-19409M. 10 X MAGNIFICATION DVI C/O & FOUND NO CORROSION EVIDENT. REPAIR BARREL NUT BORE WAS ACCOMP IAW EN1248-08 & IS ACCEPTABLE IAW EO MD11-5510-29971A.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR 31 FOUND CORRODED CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 VII REV35.BORE REAM TO 1.162"DIA, REMAINING BLEND OUT AT BOTTOM RADIUS 0.130" DEEP FOUND EXCEEDING EO LIMIT IAW EO MD11-5510-19409M.10X MAGN DVI FOUND NO CORROSION EVIDENT. REPAIRED BARREL NUT BORE NR31 RT WAS ACCOMPLISHED IAW EN 12 52-08 & IS ACCEPTABLE IAW EO MD11-5510-30012A.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR34 FOUND CORRODED EXISTING SLEEVE BUSHING REMOVED & CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 VII REV 35. BORE REMAINING BLEND OUT 0.030" DEEP, BOTTOM SURFACE CLEANED, BORE BLEND OUT EXCEEDED LIMIT IAW EO MD11-5510-19409M. 10X MAGN.DVI C/O & FOUND NO CORROSION EVIDENT. REPAIRED BARREL NUT BORE NR 34 WAS ACCOMP IAW EN1240-08 & IS ACCEPTABLE IAW EO MD11-5510-30012A.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR 28 FOUND CORRODED, CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 VII REV35. BORE REAMED TO 1.178" DIA, REMAINING BLEND OUT 0.060", BOTTOM REMAINING 0.070" DEEP. BORE BLEND OUT FOUND EXCEEDING LIMITS IAW EO MD11-5510-19409M. 10X MAGNIFICATION DVI C/O & FOUND NO CORROSION EVIDENT. REPAIR BARREL NUT BORE NR 28 RT WAS ACCOMP IAW EN 1239-08 & IS ACCEPT IAW EO MD11-5510-30012-A.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR 8 FOUND CORRODED CORROSION REMOVED AT BARREL NUT BORE IAW SRM 51-21-01 VII REV 35. BORE REAM TO 0.988" DIA REMAINING BLEND OUT 0.095" DEEP, BOTTOM SURFACE CLEANED. BORE BLEND OUT FOUND EXCEEDING LIMITS IAW EO MD11-5510-19409M.10X MAGNIFICATION DVI C/O & FOUND NO CORROSION EVIDENT. REPAIRED BARREL NUT BORE NR8 RH WAS ACCOMP IAW EN 1237-08 & IS ACCEPTABLE IAW MD11-5510-30010A.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR17 FOUND CORRODED. CORROSION REMOVED AT BARREL NUT BORE IAW SRM 51-21-01 VII REV35. BORE REAM TO 1.067"DIA, REMAINING BLEND OUT 0.050", BOTTOM REMAINING, BLEND OUT 0.045" DEEP, FOUND EXCEEDING LIMIT IAW EO MD11-5510-19409M.10X MAGN DVI C/O & FOUND NO CORROSION EVIDENT. REPAIRED BARREL NUT BORE NR 17 RT WAS ACCOMPLISHED IAW EN1229-08 & IS ACCEPTABLE IAW EO MD11-5510-30011A.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE:C CTR CARGO COMPT - UPON REMOVING OF PHENOLIC SPACER AT STATION 5-73,X-33 FOUND FLOORBEAM CRACKED. CRACK BEAM REMOVED AND NEW BEAM P/N AFA0039-5N INSTALLED AS PER SRM 51-31-01 VOL II REV 35.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE-C, LT HORIZ STAB BARREL NUT BORE NR17 FOUND CORRODED. CORROSION AT BARREL BORE REMOVED IAW SRM 51-21-01 VII REV 35. BORE REAM TO 1.067" DIA REMAINING BLEND OUT 0.035", BOTTOM SURFACE CLEANED & BORE FOUND OUT OF LIMIT IAW EO MD11-5510-19409M.10X MANIFICATION DVI C/O & FOUND NO CORROSION EVIDENT. REPAIRED BARREL NUT BORE NR17 LT WAS ACCOMPLISHED IAW EN 1223-08 & IS ACCEPTABLE IAW EO MD11-5510-29971-A.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE-C, LT HORIZ STAB BARREL NUT BORE NR33 FOUND CORRODED CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 VII REV 35. BORE REAM TO 1.178" DIA, REMAINING SIDEWALL BLEND OUT 0.020" DEEP, BOTTOM SURFACE REMAINING BLEND OUT 0.065" DEEP, BLEND OUT AT BORE FOUND EXCEEDING LIMITS IAW EO MD11-5510-19409M. REPAIRED BARREL NUT BORE NR 33 LT WAS ACCOMP LISHED IAW EN 1222-08 & IS ACCEPTABLE IAW EO MD11-5510-29972-A.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR 36 FOUND CORRODED CORROSION AT BORE NR36 RT REMOVED IAW SRM 51-21-01 VII REV 35. BORE REAM TO 2.538" DIA, REMAINING BLEND OUT 0.098" DEEP, BOTTOM REMAINING BLEND OUT 0.150" DEEP, BORE EXCEEDED LIMITS IAW EO MD11-5510-19409M.10X MAGNIFICATION DVI C/O & FOUND NO CORROSION EVIDENT. REPAIRED BARREL NUT BORE NR 36 RT WAS ACCOMP IAW EN1221-08 & IS ACCEPTABLE IAW EO MD11-5510-30009-A.

Part: SPAR — CORRODED (VERTICAL STAB)

INSPECTION TYPE:N/A VERTICAL STABILIZER FRONT SPAR RT AT STA ZFS 353.295 FOUND SURFACE CORROSION. SURFACE CORROSION ON VERTICAL STABILIZER FRONT SPAR RT AT STA ZFS 353.295 REMOVED AS PER SRM 51-21-01 VOL II REV 35. REWORKED AREA MATERIAL ORIGINAL THICKNESS 0.190", MATERIAL REMOVED 0.012", REMAINED THICKNESS 0.178". FOUND WITHIN LIMIT AS PER SRM 55-00-01 FIG 1A VOL I REV 35.

Part: LONGERON SPLICE — CRACKED (BS 1676) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE:C CTR CARGO AT STATION 1676 LONGERON 46 RT LONGERON SPLICE DOUBLER FOUND CRACKED AS MARKED. CRACK SPLICE REMOVED PER SRM 51-33-01 VII REV 35. REPAIR LONGERON SPLICE FAB PER SRM 53-10-00 FIG 2 VI REV 35. NEW SPLICE REWORKED SMOOTH AND REPROTECTED PER SRM 51-21-01 VII REV 35. FPI C/O PER DPS 4.707 REV AW ON NEW SPLICE AND FOUND NO CRACK EVIDENT. SPLICE REPROTECTED PER SRM 51-21-01 V II R35. NEW SPLICE INSTALLED PER SRM 51-33-01 VII REV 35.

Part: WINGLET — DAMAGED (RIGHT)

RT UPPER WINGLET ASSY HAS 3 DAMAGED AREAS ALONG T/E. REPAIRED PER EO C-5720-33537-A.

Part: HINGE — CORRODED (RT WING TE FLAP) · airframe 61,716 hrs · 5,867 cycles

INSPECTION TYPE:C, RT WING OB FLAP OB FWD HINGE BARREL NUT SPOT FACE CORRODED. RT FWD OB FLAP OB HINGE BARREL NUT SPOTFACE CORROSION REMOVED IAW CMM57-44-09 PG 602-607 R61. FPI C/O IAW DAC NDT SPM R13 PT 08 ON REWORKED AREA, FOUND NO CRACK, NO CORROSION EVIDENT. RT FWD OB FLAP OB HINGE BARREL NUT SPOTFACE EVALUATED, FOUND ACCEPTED IAW EN1298-08. REWORKED AREA ETCH INSPECTED, FOUND 'SATIS' IAW EN1298-08.

Part: HINGE — CORRODED (RT WING TE FLAP)

RT WING O/B FLAP O/B FWD HINGE LOWER MOUNT O/B BORE CORRODED. RT WING O/B FLAP O/B FWD HINGE LOWER MOUNT O/B BORE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09.

Part: HINGE — CORRODED (RT WING TE FLAP)

INSPECTION TYPE:N/A RT WING O/B FLAP O/B FWD HINGE ACTUATOR I/B BORE I/B SPOTFACE CORRODED. RT WING O/B FLAP O/B FWD HINGE ACTUATOR I/B BORE I/B SPOTFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE-C, RT HORIZONTAL STABILIZER BARREL NUT BORE NR27 FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 VII REV 35.BORE REAM TO 1.178" DIA,REMAINING BLEND OUT 0.025" DEEP, BOTTOM REMAINING BLEND OUT 0.055" DEEP. BORE BLEND OUT FOUND EXCEEDING LIMITS IAW EO MD11-551 0-19409M. 10X MAG DVI C/O & FOUND NO CORROSION EVIDENT. REPAIRED B/N BO RE NR 27RH WAS ACCOMP IAW EN1209-08 & IS ACCEPT IAW EO MD11-5510-30012A.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE-C, LT HORIZ STAB BARREL NUT BORE NR30 FOUND CORRODED. EXISTING REPAIR BUCKET BUSHING REMOVED IAW EO MD11-5510-19409M. MINOR CORROSION AT BORE REMOVED IAW SRM 51-21-01 VII REV 35. BOTTOM WAS BORED THRU & BORE MEASURED TO 1.255"DIA, REMAINING BLEND OUT 0.040", FOUND BORE EXCEEDED LIMITS IAW EO MD11-5510-19409M. REPAIRED BARREL NUT BORE NR30 LT WAS ACCOMP IAW EN 1202-08 & IS ACCEPTABLE IAW EO MD11-5510-29972A.

Part: HINGE — CORRODED (RT WING TE FLAP)

INSPECTION TYPE:N/A RT OUTBOARD FLAP OUTBOARD FWD HINGE ACTUATOR OUTBOARD BORE OUTBOARD SPOTFACE CORRODED. RT OUTBOARD FLAP OUTBOARD FWD HINGE ACTUATOR OUTBOARD BORE OUTBOARD SPOTFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09.

Part: HINGE — CORRODED (RT WING TE FLAP)

INSPECTION TYPE:N/A RT WING O/B FLAP O/B FWD HINGE FWD MOUNT O/B ATTACHMENT LUG O/B SPOT FACE CORRODED. RT WING O/B FLAP O/B FWD HINGE FWD MOUNT O/B ATTACHMENT LUG O/B SPOTFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE-C, RT HORIZONTAL STABILIZER BARREL NUT BORE NR30 FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 VII REV 35. BORE REAM TO 1.178" DIA REMAINING BLEND OUT 0.040" DEEP, BORE BLEND OUT FOUND EXCEEDING LIMITS IAW EO MD11-5510-19409M.10X MAGNIFICATION DETAIL VISUAL INSP & FOUND NO CORROSION EVIDENT. REPAIRED BARREL NUT BORE NR 30 RT WAS ACCOMPLISHED IAW EN 1210-08 & IS ACCEPTABLE IAW EO MD11-5510-30012-A.

Part: HINGE — CORRODED (RT WING TE FLAP)

INSPECTION TYPE:N/A RT WING O/B FLAP I/B FWD HINGE UPPER MOUNT I/B BORE FWD SPOTFACE CORRODED. RT WING O/B FLAP I/B FWD HINGE UPPER MOUNT I/B BORE FWD SPOTFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08.

Part: STRUCTURE — CORRODED (RT WING TE FLAP)

INSPECTION TYPE:N/A RT WING O/B FLAP O/B FWD HINGE BARREL NUT UPPER BORE CORRODED. RT WING O/B FLAP O/B FWD HINGE BARREL NUT UPPER BORE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09.

Part: HINGE — CORRODED (RT WING TE FLAP)

RT WING O/B FLAP I/B FWD HINGE BARREL NUT LOWER BORE CORRODED. RT WING O/B FLAP I/B FWD HINGE BARREL NUT LOWER BORE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08.

Part: HINGE — CORRODED (T/E FLAP)

INSPECTION TYPE:N/A LT WING O/B FLAP I/B FWD HINGE BARREL NUT SPOT FACE CORRODED. LT WING O/B FLAP I/B FWD HINGE BARREL NUT SPOT FACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08.

Part: STRUCTURE — CORRODED (RT WING TE FLAP)

INSPECTION TYPE:N/A RT WING O/B FLAP O/B FWD HINGE BARREL NUT LOWER BORE CORRODED. RT WING O/B FLAP O/B FWD HINGE BARREL NUT LOWER BORE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09.

Part: HINGE — CORRODED (RT WING TE FLAP)

INSPECTION TYPE:N/A RT WING O/B FLAP I/B FWD HINGE LOWER MOUNT I/B BORE CORRODED. RT WING O/B FLAP I/B FWD HINGE LOWER MOUNT I/B BORE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08.

Part: HINGE — CORRODED (RT WING TE FLAP)

INSPECTION TYPE:N/A RT WING O/B FLAP O/B FWD HINGE UPPER MOUNT FWD SPOTFACE CORRODED. RT WING O/B FLAP O/B FWD HINGE UPPER MOUNT FWD SPOTFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09.

Part: HINGE — CORRODED (RT WING TE FLAP)

INSPECTION TYPE:N/A RT WING O/B FLAP I/B FWD HINGE BARREL NUT UPPER BORE CORRODED. RT WING O/B FLAP I/B FWD HINGE BARREL NUT UPPER BORE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR1 FOUND CORRODED EXISTING SLEEVE BUSHING REMOVED IAW EO MD11-5510-19409M. CORROSION AT BORE REMOVED IAW SRM 51-21-01 VII REV 35. BORE REAM TO 1.549" DIA, REMAINING BLEND OUT 0.050" DEEP, BOTTOM SURFACE CLEANED & REMAINING MAT'L THK CHK MIN. 0.290" THICK. BORE FOUND EXCEEDING LIMITS IAW EO. REPAIRED B/N BO RE NR 01RH WAS ACCOMP IAW EN 1186-08 & IS ACCEPT IAW EO MD11-5510-30008A.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE-C, RT HORZ STAB BARREL NUT BORE NR 24 FOUND CORRODED CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 VII REV 35. BORE REAM TO 1.067"DIA, REMAINING BLEND OUT 0.040" DIA, BOTTOM REMAINING BLEND OUT 0.060" DEEP, BORE FOUND BLEND OUT EXCEEDING LIMITS IAW EO MD11-5510- 19409M.10X MAGN DVI & FOUND NO CORROSION EVIDENT. REPAIRED BARREL NUT BORE NR24 RT WAS ACCOMP IAW EN1238-08 & IS ACCEPT IAW MD11-5510-30011A.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR 21 FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 REV 35. BORE REAM TO 1.067"DIA, REMAINING BLEND OUT 0.083" DEEP, BOTTOM REMAINING BLEND OUT 0.045", BORE BLEND OUT FOUND EXCEEDING LIMITS IAW EO MD11-5510-19409M.1 0X MAGN DVI C/O & FOUND NO CROSSION EVIDENT.REPAIRED AT BARREL NUT BOR E NR 21 RT ACCOMP IAW EN 1234-08 & IS ACCEPTABLE IAW EO MD11-5510-30011A.

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE-C, LT WING OB FLAP IB AFT HINGE LOWER MOUNTING FOUND 02EA BORE RUSTY. LT AFT OB FLAP IB HINGE LOWER MOUNTING FWD & AFT BORE CORROSION REMOVED IAW BSOPM 20-11-02 REV 61.FPI C/O IAW DAC NDT SPM REV 13 PART 0 8 ON REWORKED AREA. FOUND NO CRACK/CORROSION EVIDENT. REWORKED BO RES(02EA) REAMED IAW EN 1288-08.REWORKED AREA ETCH INSPECTED & FOUND SATIS IAW EN 1288-08.BUSHINGS(02EA) FAB & INSTALLED IAW EN 1288-08.

Part: HINGE — CORRODED (TE FLAP)

INSPECTION TYPE:N/A LT WING O/B FLAP I/B AFT HINGE LOWER MOUNTING FOUND 02 EA BORE RUSTY. LT WING O/B FLAP I/B AFT HINGE LOWER MOUNTING 02 EA BORE CORROSION REMOVED AND REPAIRED AS PER EN 1288-08.

Part: HINGE — CORRODED (TE FLAP)

INSPECTION TYPE:N/A LT WING O/B FLAP I/B AFT HINGE UPPER MOUNTING FOUND CENTER BORE CORRODED. LT WING O/B FLAP I/B AFT HINGE UPPER MOUNTING CENTER BORE CORROSION REMOVED AND REPAIRED AS PER EN 1288-08.

Part: LONGERON SPLICE — CRACKED (BS 869 L33L) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE:C FWD CARGO AT STATION 869 LONGERON 33 LT LONGERON SPLICE DOUBLER FOUND CRACKED. CRACK SPLICE REMOVED PER SRM 51-33-01 VII R35. NEW SPLICE REWORKED SMOOTH AND REPROTECTED PER SRM 51-21-01VII R35. FPI C/O PER DPS 4.707 REV AW ON NEW SPLICE AND FOUND NO CRACK EVIDENT. NEW SPLICE ADA8423-501 INSTALLED PER SRM 51-33-01 VII REV 35 AND BOEING DWG ADA8423.

Part: HINGE — CORRODED (RT WING TE FLAP)

INSPECTION TYPE:N/A RT WING O/B FLAP I/B AFT HINGE O/B PIVOT BORE CORRODED. RT WING O/B FLAP I/B AFT HINGE O/B PIVOT BORE CORROSION REMOVED AND REPAIR CARRIED OUT AS PER CMM 57-52-04 REV 61.

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE-C, LT WING OB FLAP IB AFT HINGE UPPER MOUNTING FOUND 06EA BORE RUSTY. LT AFT OB FLAP IB HINGE UPPER MOUNTING IB SIDE BORES(03EA) & OB SIDE BORES (03EA) CORROSION REMOVED IAW BSOPM20-11-02 REV 61.FPI C/O IAW DAC NDT SPM REV 13 PT 08 ON REWORKED AREA & FOUND NO CRACK & NO CORROSION EVIDENT. REWORKED BORES(05EA) REAMED IAW EN1288-08. BUSHING(05EA) FAB AND INSTALLEDIAW EN 1288-08.

Part: HINGE — CORRODED (TE FLAP)

INSPECTION TYPE:N/A RT WING O/B FLAP I/B AFT HINGE I/B AFT HINGE I/B PIVOT I/B SPOTFACE CORRODED. RT WING O/B FLAP I/B AFT HINGE I/B PIVOT I/B SPOTFACE CORROSION REMOVED AND REPAIR CARRIED OUT AS PER CMM 57-52-04 REV 61.

Part: HINGE — CORRODED (RT WING TE FLAP)

INSPECTION TYPE:N/A RT WING O/B FLAP I/B AFT HINGE UPPER MOUNTING CENTER BORE CORRODED. RT WING O/B FLAP I/B AFT HINGE UPPER MOUNTING CENTER BORE CORROSION REMOVED AS PER BSOPM 20-11-02 AND FOUND WITHIN DWG ARC 1984 LIMIT.

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE-C, LT WING OB FLAP IB AFT HINGE UPPER MOUNTING FOUND CENTER BORE CORRODED. LT AFT OB FLAP IB HINGE UPPER MOUNTING CENTER BORE CORROSION REMOVED IAW BSOPM 20-11-02 REV 61 FPI C/O IAW DAC NDT SPM REV 13 PT 08 ON REWORKED AREA & FOUND NO CRACK & NO CORROSION EVIDENT. LT AFT OB FLAP I B HINGE UPPER MOUNTING CENTER BORE FINAL DIA OF 2.020" EVALUATED & FOUND ACCEPTED IAW EN1288-08. FLAP PEENING C/O ON RWK AREA IAW EN1288-08.

Part: HINGE — CORRODED (RT WING TE FLAP)

RT WING O/B FLAP I/B AFT HINGE O/B PIVOT I/B SPOTFACE CORRODED. RT WING O/B FLAP I/B AFT HINGE O/B PIVOT I/B SPOTFACE CORROSION REMOVED AND REPAIR CARRIED OUT AS PER CMM 57-52-04 REV 61.

Part: HINGE — CORRODED (TE FLAP)

INSPECTION TYPE:N/A RT WING O/B FLAP I/B AFT HINGE I/B PIVOT BORE CORRODED. RT WING O/B FLAP I/B AFT HINGE I/B PIVOT BORE CORROSION REMOVED AND REPAIR CARRIED OUT AS PER CMM 57-52-04.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR 09 FOUND CORRODED EXISTING REPAIR SLEEVE BUSHING REMOVED IAW EO MD11-5510-19409M. BARREL NUT BORE SURFACE CLEANED & MEASURED 1.065" DIA,BOTTOM SURFACE CLEANED & MINIMUM THK MEASURED 0.122" THICK, BORE SIZE FOUND OUT OF LIMIT IAW EO MD11-5510-19409M. REPAIRED BARREL NUT BORE NR 09 RT WAS ACCOMPLISHED IAW E N 1185-08 & IS ACCEPTABLE IAW EO MD11-5510-30010-A.

Part: LONGERON — CORRODED (BS 1894 L40R) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE:C AFT CARGO AT STATION 1894 LONGERON 40 RT CORROSION FOUND ON LONGERON AREA AS MARKED. CORROSION LONGERON REMOVED PER SRM 53-10-00 FIG 1 VI REV35. HFEC C/O IAW NDTSPM R13 PT 06.10-01.001 ON TRIMMED EDGE AND FOUND NO CRACK EVIDENT. REPAIR LONGERON AND REPAIR SPLICE FAB PER SRM 53-10-00 FIG 2 VI REV 35 FPI C/O PER DPS 4.707 REV AW ON FABRICATED REPAIR PART AND FOUND NO CRACK EVIDENT. NEW REPAIR SPLICE INSTALLED PER SRM 51-31-01 VII REV 35.

Part: STRINGER — CRACKED (LT WING) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE:C LHW:UPPER FUEL TANK ACCESS NR 534CT INTERIOR COMPT, STRINGER NR 44 END SUSPECT CRACK. HFEC INSP C/O PER DAC NDTSPM R13 06-10-01.001 AND FOUND CRACK APPROX 1/2 INCH. CRACKED AREA AT LHW STRINGER NR 44 END AREA SLOTTED PER SRM 57-2 0-00 V1 FIG 10 R35. NEW REPAIR SPLICE FAB PER SRM 57-20-00 VI FIG 10 R35. NEW FAB REPAIR SPLICE INSTALLED AT LHW ACCESS NR 534CT STRINGER NR 44 END AREA PER SRM 57-20-00 VI FIG 10 R35 AND SRM 51-33-01 VII R35.

Part: HANGER ASSY — BROKEN (BS 602) · airframe 61,716 hrs · 5,867 cycles

INSPECTION TYPE:C, FWD CGO COMPT/ AT STATION 602, LBL 42 FWD BULKHEAD SUPPORT HANGER WITH P/N: ACA0143-7 FOUND BROKEN. FWD CARGO STA 602, LBL 42 FWD BULKHEAD SUPPORT HANGER REMOVED IAW SRM 51 -33-01 VII R35. NEW HANGER FAB IAW EN 1219-08.NEW FAB HANGER HEAT TREAT TO RT 900 CONDITION IAW EN NR 1219-08. HOLES TRANSFERED ONTO NEW FAB HANGER IAW SRM 51-31-01 VII R35. NEW FAB HANGER PRIMED IAW SRM51-21-01 V II R35. NEW HANGER INSTALLED AT FWD CGO IAW SRM 51-33-01 VII REV 35.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE:C AFT FUSELAGE EXTERIOR, RIGHT SIDE AT STA 2033 BETWEEN LONGERONS L39 & L 40, CORROSION FOUND SURROUNDING FASTENER HOLE. ATTACH FASTENERS & INNER SUPPORTS REMOVED PER SRM 51-31-01 V II R35. SKIN CORROSION REMOVED PER SRM 51-21-01 VII R35. DAMAGE SKIN TRIMMED OFF PER SRM 53-20-00 FIG 2. HFEC C/O PER DACNDTSPM R13 PT 06.10.01. 001 ON TRIMMED OFF AREA FOUND NO CRACK EVIDENT. REPAIR PARTS FAB AND INSTALLED PER SRM 53-20-00 FIG 2 VI R35 & SRM 51-31-01 VII R35.

Part: WEB — CORRODED (FUSELAGE) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE:C CABIN LT L27 STA 1946-1986 CHORD WEB AREA FOUND SURFACE CORRODED AS MARKED. LT L27 STA 1946-1986 CORROSION ON WEB SURFACE REMOVED PER SRM 51-21-01 VII R35. CABIN - LT 27 STA 1946-1986 CHORD WEB REMOVED PER SRM 51-31-01 VII R35. NEW WEB FAB PER DWG AGA7145-503 AND INSTALLED PER SRM 51-31-01 VII R35.

Part: SKIN — WORN (RT WING TE FLAP) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE-C, RT WING IB FLAP CTR VANE TRACK CUTOUT SKIN FOUND WORN AS MARKED. REMOVED RT WING IB FLAP VANE IAW AMM27-50-22 REV 53. DAMAGED AREA ON RT WING IB FLAP CTR VANE TRACK CUTOUT SKIN AREA TRIMMED OUT IAW EN NR 1176-08.HF EC INSP C/O ON TRIMMED OUT AREA FOUND NO CRACK EVIDENT. NEW REPAIR DOUBLER & REPAIR FILLER FAB IAW EN NR 1176-08.NEW FAB REPAIR DOUBLER & FILLER INSTALLED AT RT WING IB FLAP CTR VANE TRACK CUTOUT AREA IAW EN NR 1176-08.

Part: STRINGER — CRACKED (RT WING) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE:C RT WING FUEL TANK UPPER STRINGER NR 12 END SUSPECT CRACK, HFEC INSP C/O PER DAC NDTSPM R13 06-10-01.001 AND FOUND CRACK APPROX 10 1/2 INCH. CRACK AREA AT RT WING STRINGER NR 12 END SLOTTED PER SRM 57-20-00 FIG 10 VI R35. NEW REPAIR ANGLES 02 EA FAB PER SRM 57-20-00 FIG 10 VI R35. NEW FAB 02EA REPAIR ANGLES/ATTACHED SP AND SRM 51-33-01 VII R35.

Part: STRINGER — CRACKED (RT WING) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE-C, RT WING FUEL TANK UPPER STRINGER NR 13 END SUSPECT CRACK. HFEC INSPECTED CUTOUT & FOUND CRACK APPROX 10". DAMAGED PORTION RT WING FUEL TANK UPPER STRINGER NR 13 AREA TRIMMED OFF PER EN NR1189-08. HFEC CUTOUT ON TRIMMED EDGE & FOUND NO CRACK EVIDENT. NEW REPAIR STRINGER & 3 REPAIR STRAPS FAB IAW EN NR 1189-08. FPI CUTOUT ON FAB REPAIR FOUND NO CRACK EVIDENT. CAP SEALING CUTOUT ON NEW INSTALLED FASTENER IAW SRM.

Part: SKIN — WORN (LT WING TE FLAP) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE:C, LT WING IB FLAP CTR VANE TRACK CUTOUT SKIN FOUND WORN AS MARKED. REMOVED LT WING IB FLAP VANE IAW AMM27-50-22 R53. CHAFFING MARKS ON LT WING IB FLAP CTR VANE TRACK CUTOUT SKIN AREA BLEND OUT IAW EN NR 1175-0 8. FPI C/O ON REWORKED AREA, FOUND NO CRACK & NO CORROSION EVIDENT. REWORKED AREAS REPROTECTED IAW EN NR 1175-08. LT IB FLAP VANE REINSTALLED IAW MM27-50-22 REV 53.

Part: STRINGER — CRACKED (RT WING) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE:C, RT WING FUEL TANK UPPER STRINGER NR 14 END SUSPECT CRACK. HFEC INSP C/O IAW DAC NDTSPM REV13 06-10-01.001 & FOUND CRACK APPROX 1 13 INCH. SPLICE FITTING AT RT WING FUEL TANK UPPER STRINGER NR 14 AREA REMOVED FOR ACCESS. HFEC INSP C/O, CONFIRM CRACK END & MARKED OUT. DAMAGED PORTION OF RT WING FUEL TANK UPPER STRINGER NR 14 TRIMMED OFF IAW EN NR 1189-08. NEW FAB REPAIR STRINGER & REPAIR STRAP INSTL IAW EN NR1189-08 & SRM.

Part: STRINGER — CRACKED (RT WING) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE:C RT WING FUEL TANK UPPER STRINGER NR 10 END SUSPECT CRACK, HFEC INSP C/O PER DAC NDTSPM R13 06-10-01.001 AND FOUND CRACK APPROX 9 INCH CRACK AREA AT RT WING FUEL TANK UPPER STRINGER NR 10 END SLOTTED OUT PER SRM 57-20-00 FIG 10 VI R35. REPAIR ANGLES 02EA FAB PER SRM 57-20-00 FIG 10 VI R35. NEW FAB 02 EA ANGLES/ATTACHED SPLICE INSTALLED RT WING NR 10 STRINGER NR 10 PER SRM 57-20-00 FIG 10 VI R35 AND SRM 51-33-01 VII R35.

Part: STRINGER — CRACKED (LT WING) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE-C, LT WING FUEL TANK UPPER STRINGER NR14 END SUSPECT CRACK. HFEC C/OUT & FOUND CRACK 11.5" APPROX. DAMAGED PORTION LT WING FUEL TANK UPP STRINGER NR 14 TRIMMED OFF IAW EN NR 1189-08. HFEC CUTOUT FOUND NO CRACK EVIDENT. NEW REPAIR STRINGER & REPAIR PARTS FAB IAW EN NR1189- 08. FPI C/OUT ON FAB PARTS & FOUND NO CRACK EVIDENT. CAP SEALING CUTOUT ON NEW INSTALLED IAW SRM 51-41-01 VOL II REV35.

Part: SEAT TRACK — CORRODED (BS 1961) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE:C CABIN-STA 1961 CURVE SEAT TRACK CROWN AREA, X=-107.25 FOUND CORROSION AS MARKED. CURVE SEAT TRACK CORROSION REMOVED PER SRM 51-21-01VII R35. CORRODED SEAT TRACK REMOVED FROM STA 1831-2007 PER SRM 51-31-01 VII R35. CORRODED SEAT TRACK TRIMMED OFF AT STA 1831-2007 PER SRM 53-70-00 VI FIG R35. HFEC INSP C/O PER DAC NDTSPM 06-10-01.001 R13 ON TRIMMED OUT AREA FOUND NO CRACK EVIDENT. REWORKED SEA TRACK, SPLICE, PLATE INSTALLED PER SRM 51-31-01 VI.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE:C CABIN-STA 6-10 SEAT TRACK CROWN AND BASE AREA, X=8.50 FOUND CORROSION AS MARKED. STA 6-10 SEAT TRACK BASE AREA X=8.5 CORROSION REMOVED PER SRM 51-21-01 VII R35. CABIN EXCEED LIMIT SEAT TRACK FROM STA 6-10 TO STA 6-100 X=8. 50 EXISTING SPLICE REMOVED PER SRM 51-31-01 VII R35. HFEC C/O ON TRIMMED OFF AREA FOUND NO CRACK EVIDENT. NEW SEAT TRACK REWORKED PER SRM 51-70 -00 VI R35. NEW SEAT TRACK INSTALLED PER SRM 51-31-01 VII REV 35.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE:C CABIN STA 1961 CURVE SEAT TRACK CROWN AREA, X=107.25 FOUND CORROSION AS MARKED. CURVE SEAT TRACK CORROSION REMOVED PER SRM 51-21-01 VII R35. ORIGINAL THICKNESS REMOVED AND FOUND EXCEEDED LIMIT PER SRM 53-70-00 VI R35. CORRODED SEAT TRACK TRIMMED OFF FR STA 1831-2007 PER SRM 53-70-00 FIG 7 VI R35. SEAT TRACK SPLICE & SPLICE PLATE FAB PER SRM 53-70-00 VI FIG R35. SEAT TRACK, SEAT TRACK SPLICE & SPLICE PLATE INSTALLED PER SRM 51-31-01 VII R35.

Part: DOUBLER — CRACKED (RT WING) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE:C RT WING FIXED L/E COMPT AT STA XORS 538 APPROX FOUND UPPER DOUBLER CRACKED AS MARKED. DAMAGED AREA AT RT WING FIXED L/E COMPT STA 538 UPPER DOUBLER AREA TRIMMED OFF AS PER SRM 57-10-00 VI FIG 27 R40. NEW REPAIR DOUBLER, REPAIR FILLER & 03EA REPAIR ANGLES FAB PER SRM57-10-00 VI FIG 27 R40. NEW FAB REPAIR DOUBLER, REPAIR FILLER & 3EA REPAIR ANGLES INSTALLED AT RT WING FIXED L/E COMPT STA XORS 538 INTERIOR AREA PER SRM 57-10-00 VI FIG 27 REV 40.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE:C CABIN-BETWEEN STA 879-899, SEAT TRACK CROWN AREA, X=75.25 FOUND SURFACE CORROSION AS MARKED CORROSION AT CABIN BETWEEN STA 879-899 X=75.25 ON SEAT TRACK CROWN SURFACE AREA REMOVED PER SRM51-21-01 V.II R35. EXISTING SEAT TRACK REPAIR SPLICES AT STA 869 AND STA 929 REMOVED PER SRM 51-31-01 V.II R35. HFEC INSP C/O PER DAC NDTSPM R13 06-10-01.001 ON EXISTING TRIMMED OFF FOUND NO CRACK. NEW SEAT TRACK REPAIR SECT AND SPLICE INSTALLED PER SRM51-31-01 V.II R35

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE:C CABIN-STA 839-899 SEAT TRACK CROWN AREA, X=-27.50 FOUND CORROSION AS MARKED. CORROSION AT CABIN STA 839-899 X=-27.5 ON SEAT TRACK CROWN SURFACE AREA REMOVED AS PER SRM 51-21-01 V.II R35. EXISTING SEAT TRACK SPLICE AT STA 816 REMOVED PER SRM 51-31-01 VII R35. HFEC INSP C/O PER DAC NDTSPM R1 3 06-10-01.001 ON TRIMMED OFF AREA AND FOUND NO CRACK. NEW SEAT TRACK REPAIR SECT AND SPLICES INSTALLED PER SRM 51-31-01 V.II REV 35.

Part: FAIRING — GOUGED (TE FLAP) · airframe 61,716 hrs · 8,567 cycles

INSPECTION TYPE:C, RT WING IB FLAP ELEPHANT EAR FAIRING FOUND GOUGED AND DENTED. RT WING IB FLAP, IB FAIRING, REMOVED IAW CMM57-52-03 R61. GOUGED AND DENTED AREAS MEASURED, EVALUATED & FOUND OUT OF LIMIT IAW SRM57-00-01 VI R35. DAMAGED SKIN PORTION ON RT WING IB FLAP IB FAIRING AREA TRIMMED OFF IAW EN NR 1289-08. NEW SKIN PORTION, INTERNAL SPLICE DOUBLER & 02EA REPAIR DOUBLER FAB AND INSTALLED IAW EN NR 1289-08.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 61,716 hrs · 5,867 cycles

INSPECTION TYPE:C, REFERENCE TO EO MD11-5310-27496D, UNABLE TO OBTAIN SUPPORT ASSY ABA7430 -1 OR THE RAW MATERIAL DUE TO LONG LEAD TIME SUPPORT FABRICATED IAW DWG ABA7430 & EN NR 1172-08. FPI C/O IAW DP S 4.707 REV 'AW'. NO CRACK EVIDENT ON FABRICATED FLOOR SUPPORT. FLOOR SUPPORT REPROTECTED IAW SRM51-21-01 VII R35. FLOOR SUPPORT LOCATED & INSTALLED IAW DWG SP11530074 & EN 1172-08 AND REFER EO MD11-5310-2 7496-D.