N282UP

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,245 hrs · 18,466 cycles

**EMERGENCY DECLARED**ANTI SKID FAIL AS PER FIM 32-40-11-00 STEP #2 RESET CB ANTI SKID CONTROL SYST 1 AND 2. ALERT DOES NOT SHOW, SYST OK

Part: DRIVE CHAIN — INOPERATIVE (DOOR) · airframe 90,820 hrs · 18,198 cycles

INSPECTION TYPE:PS1REF M808022, L1 MAIN ENT DR, DRIVE CHAIN FOR AIR MOTOR. REF WAN #3794454. R&R AIR DRIVE MOTOR CHAIN WILL REQUIRE PARTIAL DISASSEMBLY OF AIR DRIVE MOTOR. 2 AMTS 6 HOURS. M808022 REMAINS. PARTS IN PFMINSTALLED CABIN DR PWR DRIVE MECH ROLLER CHAIN IAW AMM 52-11-08. NO DMPTO REVERSE. PLACARD REMOVED. THIS CLEARS M808022. ESR: AEPL ENG DWG #7595071

Part: DOOR — WARNING MESSAGE (DOORS) · airframe 90,820 hrs · 18,198 cycles

INSPECTION TYPE:NABTB DUE TO LVL1 ALERT CABIN DOOR FWD R DISPLAYEDFOUND SAFETY STRAP ON OUTSIDE OF FWD RH SERVICE DOOR. REMOVED STRAP AND OPC DOOR. OPC GOOD IAW AMM 52-11-02

Part: BATTERY — LOW (CABIN) · airframe 90,674 hrs · 18,125 cycles

PILOT REPORTS EMERGENCY BATTERY 1 LOW. DEFERRED IAW MEL 33-50-4. PLACARD INSTALLED DMP ACCOMPLISHEDR&R EMERGENCY LIGHTING BATTERY POWER SUPPLY IAW AMM 33-51-01-401. OPS CHECK GOOD. PLACARD REMOVED. THIS CLEARS M805906. DMP REVERSED. IPC 33-51-10-01-008

Part: LIGHT — BROKEN (DOOR ARMING) · airframe 90,075 hrs · 17,804 cycles

INSPECTION TYPE:NAL1 DOOR "DOOR DISARMED" LIGHT BROKEN.R&R'D L1 DOOR LIGHT ASSY L2-1361. REF. IPC 52-11-70-01-170 & SWPM 20-20-03. OPS CHECK REF. AMM 52-11-02-010-801.

Part: NOT REPORTED — INOPERATIVE (ENGINE) · airframe 89,494 hrs · 17,481 cycles

ATB, ON DEPARTURE AND AIRBORNE WE RECEIVED ENG #2 EVM COMP HI LEVEL 1 ALERT 4 TIMES EXCEEDING 4 UNITS FOR A DURATION LESS THAN 30 SECONDS ONCE POWER REDUCED AT FIRST LEVEL OFF AT 8000' NO MORE ALERTS ALL OTHER INDICATIONS NORMALREMOVED FAN BLADES PER MM 72 31 02 000 868 LUBRICATED FAN BLADES PER MM 72 31 02 640 801 INSTALLED FAN BLADES PER MM 72 31 02 400 868. REMOVED ENGINE ESN 723858 PER TC HH 3/14/222 0986333 REPLACED #2 ENGINE PER T.C. 9103 IPC M-7100-53395-A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,386 hrs · 17,447 cycles

INSPECTION TYPE:N/AEMERGENCY PWR OFF LIGHT IS INOPRELAMPED EMERGENCY PWR OFF LIGHT IAW BOEING SWPM 20-84-18 OPS CHK GOOD

Part: LONGERON — NONE (CENTER CARGO) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:C3CENTER CARGO HAS A CRACK LONGERON 39R BETWEEN R/H STA 5-113 TO 1541.REPAIRED CRACKED LONGERON 39R BETWEEN STA Y=1531 AND Y=1561 IAW MD11 SRM 53-00-05 REPAIR 1 FIGURE 201/202 (MAJOR)

Part: SHIELD — CRACKED (UNDER LAVATORY) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:3CLAVATORY UNDER FLOOR SHIELD (WEB) IS CRACKED.REMOVED, REPAIRED SHIELD (WEB) AT THE LAVATORY UNDER FLOOR AREA IAW MD11 SRM 51-35-01 AND 51-33-01 (MINOR)

Part: SEAT TRACK — CORRODED (FWD CABIN) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:1CFORWARD MAIN CABIN SEAT TRACK CORRODED AT STA 475 X=-17.000.REMOVED,FABRICATED AND REPLACED CORRODED SEAT TRACK IAW MD-11 SRM 51-33-01 AND 51-21-01 (MINOR).

Part: FLOOR SUPPORT — CORRODED (FWD MAIN CABIN) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:1CMAIN CABIN LAV FLOOR SUPPORT CORRODED BETWEEN STA.Y=392-Y=440 AND X=-8.5-X=-27.5.REMOVED AND REPLACED CORRODED MAIN CABIN LAV FLOOR SUPPPORT BETWEEN STA.Y=392-Y=440 AND X=-8.5-X=-27.5 IAW MD11 SRM 51-31-01 AND 51-33-01 (MINOR).

Part: PAN — GOUGED (MAIN CARGO DOOR) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:3CMAIN CARGO DOOR FWD FRAME/PAN HAS 2EA GOUGES.REMOVED ,FAB, INSTALL FRAME/PAN ON THE FWD SIDE OF MAIN CARGO DOOR IAW MD11 SRM 51-35-01 AND SRM 51-33-01. (MINOR)

Part: NONE — CORRODED (AVI. COMP.) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:3CAVI. COMP. AFT DOOR BELOW DOOR JAMB AT STA X=3, VERTICAL STIFFNER IS CORRODED.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. NCA6042 AND SRM 51-33-01. (MINOR)

Part: NONE — NONE (CARGO DOOR) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:1CUPPER CARGO DOOR AFT DOOR PAN GOUGE AT STA. Y=765.375 AND BETWEEN STA. Z=30.0-Z=40.0.REPAIRED GOUGED UPPER CARGO DOOR AFT PAN AT STA. Y=765.375 AND BETWEEN STA.Z=30.0-Z=40.0 IAW VT-SAA EA011-5230-01-A9459 REV I/R AND UPS EO MD11-5230-82754-A BY P.LAU (AR-830967) DATED 02/02/2020 (MAJOR).

Part: ANGLE — NONE (BANJO AREA) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:3C#2 PYLON BANJO FITTING LWR SUPPORT ANGLE IS CRACK.REMOVED AND REPLACED SUPPORT ANGLE IAW MD11 SRM 51-31-01 (MINOR)

Part: NONE — NONE (L4 DOOR) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:1CL4 DOOR LOWER HORIZONTAL BEAM NO.6 CRACK AT AFT SIDE.REMOVED,FABRICATED AND REPLACED CRACKED HORZ BEAM WITH ALTERNATE MATERIAL IAW VT-SAA EA011-5210-01-A9456 REV I/R AND UPS EO MDII-5210-82714-A BY P.LAU (AR-830967) DATED 01/28/2022 (MAJOR).

Part: INTERCOSTAL — CRACKED (#2 PYLON) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:3C#2 PYLON CARRY THRU REAR SPAR INTERCOSTAL IS CRACKED AT STA. YID= 375, XID= 7.1 AND ZID= 65.REPAIRED CRACKED #2 PYLON CARRY THRU REAR SPAR INTERCOSTAL AT STA. YID= 375, XID= 7.1 AND ZID= 65 IAW SRM 55-30-02 REPAIR 7 FIG. 203. (MAJOR)

Part: NONE — CRACKED (L-3 DOOR WEB) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:3CL-3 DOOR JAMB INNER SKIN REPAIR DOUBLER IS CRACKED BETWEEN STA. 1250.75 & 1256.75.REPAIRED CRACKED L-3 DOOR JAMB INNER SKIN BETWEEN STA. 1250.75 & 1256.75 IAW VT-SAA EA 011-5310-01-A9471 REV. I/R AND UPS EO MD11-5310-82750-A. (MAJOR) REF. FAA FORM 8100-9 BY S. KANG (AR-605677) DATED 02/01/2022.

Part: NONE — NONE (CABIN) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:1CMAIN CABIN R-3 PLUG DOOR AFT JAMB WEB(INNER SKIN) CRACK AT STA.Y=1307 & Z=-17.5.REPAIRED MAIN CABIN R-3 PLUG DOOR AFT JAMB CRACKED WEB(INNER SKIN) AT STA.Y=1307 & Z=-17.5 IAW MD-11 SRM 53-40-15,REPAIR 3 FIG 201,REV.68.01 (MAJOR).

Part: STRINGER — NONE (CENTER WING TANK) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:1CCENTER WING TANK LOWER STRINGER 47 CRACK AT XCW=0.00 AND XCW=-59.00.REPAIRED CRACKED CENTER WING TANK LOWER STRINGER 47 AT XCW=0.00 AND XCW=-59.00 IAW VT-SAA EA011-5710-01-A9458 REV I/R AND UPS EO MD11-5740-82574-A BY PHILLIP LAU (AR -830967) DATED 08/21/2017 (MAJOR).

Part: LONGERON — CORRODED (CENTER CARGO) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:3C, CENTER CARGO LONGERON 44R HAS CORROSION AT STA. 5-118.REPAIRED CORRODED LONGERON 44R BETWEEN STA. 5-93 & 5-123 IAW EA 011-5310-01-A9466 REV. I/R AND EO MD11-5310-82764-A. (MAJOR)

Part: NONE — CRACKED (AFT CARGO) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:3CAFT CARGO VERTICAL STIFFNER AT STA. 1841 AND RBL 36 IS CRACKED.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. AGA7170 AND SRM 51-33-01. (MINOR)

Part: STRINGER — CRACKED (CENTER TANK) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:3CCENTER WING TANK STRINGER 48 IS CRACKED BETWEEN STA. XCW= 35.1 TO XCW= 58.6.REPAIRED CRACKED CENTER WING TANK STRINGER BETWEEN STA. XCW= 35.1 TO XCW= 58.6 IAW SRM 57-10-03 REPAIR 1 FIG. 201. (MAJOR)

Part: STRINGER — NONE (CENTER AUX TANK) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:C3UPPER CENTER AUX TANK STRINGER 40 IS CRACK BETWEEN STA XCW=17 AND XCW=81.REPAIRED CRACK STRINGER 40 IN CENTER AUX TANK BETWEEN STA XCW=34.5 AND XCW=56.5 IAW VTSAA EA 011-5710-01-A9464 REV I/R AND UPS EO MD11-5710-82745-A. FAA 8100-9 SIGNED BY P.LAU (AR-830967) (MAJOR)

Part: LONGERON — CORRODED (CENTER CARGO) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:3CCENTER CARGO LONGERON 45R IS CORRODED AT STA. 5-118.REPAIRED CORRODED CENTER CARGO. LONGERON 45R BETWEEN STA. 5-93 & 5-123 IAW VT-SAA EA 011-5310-01-A9465 REV. I/R AND UPS EO MD11-5310-82761-A (MAJOR)

Part: STRINGER — NONE (CENTER WING TANK) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:3CCENTER WING UPPER FUEL TANK STINGER #40 IS CRACK AT STA XCW=-46.5.REPAIRED CRACKED STRINGER #40 AT STA XCW=-34.5 AND XCW=-56.5 IN THE CENTER UPPER FUEL TANK IAW MD11 EA 011-5710-01-A9460 REV I/R AND UPS EO MD11-5710-82747-A FAA FORM 8100-9 SIGNED BY P. LAU (AR-830967) DATED 1/27/22 (MAJOR)

Part: NONE — CRACKED (AFT CARGO) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:3CAFT CARGO COMP. VERTICAL STIFFNER IS CRACKED AT STA. 1841 AND LBL 26.REMMOVED, FABRICATED AND REPLACED STIFFNER IAE DWG. AGA7170 AND SRM 51-33-01. (MINOR)

Part: RETAINER — NONE (CENTER CARGO) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:1CCENTER CARGO COMPARTMENT FLOOR SUPPORT RETAINER CRACK AT LWR BULKHEAD STA.1501 LBL 19''.REMOVED,FABRICATED AND REPLACED CRACKED SUPPORT ANGLE RETAINER IAW MD-11 SRM 51-31-01 AND SRM 51-35-01 (MINOR).

Part: NONE — CORRODED (MAIN CABIN) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:3CMAIN CABIN FLOOR PANEL BETWEEN STA. 475 TO 500.175 AND X= -47.5 & X= -75.2501 HAS CORROSION.REPAIRED FLOOR PANEL IAW VT-SAA EA 011-5320-01-A9463 REV. I/R AND UPS EO MD11-5320-82699-A. (MINOR)

Part: FLOOR PANEL — CORRODED (,MAIN CABIN) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:3CMAIN CABIN FLOOR PANEL HAS CORROSION BETWEEN STA. 4754 TO 500.175 AND X=0 & X= -8.5.REPAIRED FLOOR PANEF IAW VT-SAA EA 011 5320-01-A9463 REV. I/R AND UPS EO MD11-5320-82653-A. (MINOR)

Part: NONE — CORRODED (FWD CABIN) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:1CFWD MAIN CABIN FLOOR PANEL WSP0785-501 HAS CORROSION BETWEEN STA Y=475.000-Y=503.175 & X=-8.50-X=-17.00.REMOVED AND REPLACED CORRODED FLOOR PANEL IAW SRM 51-31-01 AND 51-35-01 (MINOR).

Part: ANGLE — NONE (FWD CARGO COMPT) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:1CFWD CARGO COMPARTMENT SUPPORT ANGLE CRACK AT STA.979 BETWEEN LON 41L-38L.REMOVED,FABRICATED AND REPLACED CRACKED ANGLE IAW SRM 51-35-01 AND 51-33-01 (MINOR).

Part: ANGLE — NONE (FWD CARGO COMPT) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:1CFWD CARGO COMPARTMENT SUPPORT ANGLE CRACK AT STA.959 BETWEEN LON 41L-38L.REMOVED,FABRICATED AND REPLACED CRACK ANGLE IAW 51-35-01 AND 51-33-01 (MINOR).

Part: ANGLE — NONE (FWD CARGO COMPT) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:1CFWD CARGO COMPARTMENT SUPPORT ANGLE CRACK AT STA.899 BETWEEN LON 41L-38L.REMOVED,FABRICATED AND REPLACED CRACKED ANGLE IAW SRM 51-35-01 AND 51-33-01 (MINOR).

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:3CMAIN CABIN FLOOR PANELHAS CORROSION BETWEEN STA. 475 TO 500.175 AND X= -27.5 & X= -36.REPAIRED FLOOR PANEL IAW VT-SAA EA 011-5320-01-A9468 REV. I/R AND UPS EO MD11-5320-82679-A. (MINOR)

Part: ANGLE — NONE (FWD CARGO COMPT) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:1CFWD CARGO COMPARTMENT SUPPORT ANGLE CRACK AT STA.939 BETWEEN LON 41L-38L.REMOVED,FABRICATED AND REPLACED CRACKED ANGLE IAW SRM 51-35-01 AND 51-33-01 (MINOR).

Part: PANEL — NONE (COURIER AREA) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:C3FLOOR PANEL WSP0785Y501 BETWEEN STA 475.000 AND STA 500.175 AND X=0 X=8.5 HAS CORROSION.REMOVED AND REPLACE FLOOR PANEL WSP0785Y501 IAW MD11 SRM 51-31-01 (MINOR)

Part: NONE — CRACKED (FWD. CARGO) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:3CFWD. CARGO COMP. WEB LOCATED BETWEEN L/H VERTICAL BEAMS STA. 979 & 999 IS CRACKED.REMOVED, FABRICATED AND REPLACED WEB/DOUBLER IAW DWG. AAM7465 AND SRM 51-35-01. (MINOR)

Part: INTERCOSTAL — NONE (MAIN CABIN) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:3CMAIN CABIN FLOOR WEB/INTERCOSTAL BETWEEN STA. 1341-1364 AT RBL 46 IS BROKEN.REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG. AEA7204 AND SRM 51-35-01. (MINOR)

Part: DOUBLER — CRACKED (R/H WING) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:3CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 551.51 TO 555.58.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 551.51 TO 555.58 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: ANGLE — CORRODED (WING) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:3CCENTER WING BOX EXTERNAL ANGLE AT R/H AFT BEAR CLAW IS CORRODED.REMOVED AND REPLACED ANGLE IAW SRM 51-31-01. (MINOR)

Part: SKIN — DAMAGED (R/H WING) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:3CR/H WING FIXED L/E SKIN HAS IMPACT DAMAGE AT STA. XOS. 1063.REPAIRED DAMAGED R/H WING FIXED L/E SKIN AT STA. XOS. 1063 IAW VT-SAA EA 011-5730-01-A9455 REV. I/R AND UPS EO MD11-5730-82770-A. (MAJOR) REF. FAA FORM 8100-9

Part: FLOOR PANEL — CORRODED (FWD CABIN) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:3CFWD CABIN FLOOR PANEL WSP0786-501 HAS CORROSION BETWEEEN STA. Y=475.000-Y=503.175 AND X=-17.00-X=27.5.REMOVED AND REPLACED CORRODED FLOOR PANEL IAW SRM 53-21-10 AND 51-21-01 (MINOR).

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:3CR/H A/C COMP. AT STA. 605, INTERCOSTAL IS CRACKED.REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG. ACA3804 AND SRM 51-33-01. (MINOR)

Part: SKIN — NONE (FWD LWR CARGO) · airframe 89,374 hrs · 17,440 cycles

INSPECTION TYPE:3CFWD LWR CARGO DOOR HAS A DENT BETWEEN STA Y=954.8 TO 957.8 AND INTERCOSTAL PLANE C . DENT IS (3"X 2.5" X.176" DEEP)REPAIRED DENT AT THE FWD LWR CARGO DOOR BETWEEN STA Y=954.8 TO 957.8 AND INTERCOSTAL PLANE C IAW MD11 EA 011-5200-01-A9469 REF I/R AND UPS EO MD11-5230-82683-A. FAA FORM 8100-9 SIGNED BY P.LAU (AR-830967) DATED 01/27/22 (MAJOR)

Part: BEAM — CHAFED (TAIL CONE) · airframe 89,369 hrs · 17,438 cycles

INSPECTION TYPE:3CTAIL CONE HORZ. BEAM REPAIR DOUBLER HAS CHAFE DAMAGE.REMOVED, FABRICATED AND REPLACED DOUBLER IAW SRM 53-00-00 REPAIR 1, FIG. 201. (MINOR)

Part: NONE — BROKEN (DOOR) · airframe 89,296 hrs · 17,404 cycles

INSPECTION TYPE:N/A** SUPPLEMENTAL SDR **L1 DOOR AFT CABLE TENSIONER BROKEN, AFT CABLE BROKEN. DEFERRED PER MEL 52-10-2-2-1 CONTROL NUMBER ASSIGNED M766187. FYI CABLE NOT BROKEN PLASTIC COATING PEELED OFF CABLE ONLY.INSTALLED / ROUTED L1 CABLE TO STEP 1A PER AMM 52 11 03. INSTALLED AFT LOWER CABLE REF AMM 52 11 03. OPS CK GOOD REF AMM 52 11 02. THIS CLEARS M766187, PLACARD REMOVED, DMP REVERSED. ESR IPC 52 11 05 05.

Part: NONE — LOW PRESSURE (CABIN) · airframe 89,139 hrs · 17,344 cycles

INSPECTION TYPE:N/A** SUPPLEMENTAL SDR**ON PREFLIGHT FOUND L1 DOOR BOTTLE PRESSURE BELOW GREEN BAND. PLACARDED L1 DOOR INOP IAW MEL 52-10-3-1-2-1-1, M-763027 ASSIGNED. NOTE: DOOR MAYBE OPERATED FOR NORMAL INGRESS AND EGRESS ON THE GROUND. EXTENDED OVERWATER OPERATIONS PROHIBITED.SERVICED L1 ENTRY DOOR PNEUMATIC STORAGE AIR RESERVOIR REF AMM 12-25-04. THIS CLEARS M763027.

Part: NONE — NONE (CABIN) · airframe 89,103 hrs · 17,335 cycles

INSPECTION TYPE:N/A** SUPPLEMENTAL SDR**CLIMBING THROUGH FL 310, LEVEL 1 CRG FLO FWD DISAG. PLACED FWD CARGO COMPARTMENT VENTILATION FAN ON MEL I/A/W 21-24-1C/W FIM 21-27-03-00 FOUND SENSOR SCREEN 132BR IN FWD CARGO PUT PLUGGED WITH DEBRIS CLEANED SCREEN SVS CKS OK THIS CLEARS M762383.

Part: SKIN — DAMAGED (L1 DOOR) · airframe 88,381 hrs · 17,154 cycles

INSPECTION TYPE:N/AL1 CREW ENTRY DOOR HAS DAMAGE EXTERNAL SKIN AT TOP CENTER EDGE.REPAIRED DOOR PER EO MD11-5210-80278.

Part: COVER — INOPERATIVE (L1 DOOR) · airframe 88,327 hrs · 17,141 cycles

L1 DOOR DOOR INOP- DUE TO DOOR HINGE SPRING WORN. DEFFERRED PER MEL 52-10-3-1-2-1 ASSIGNED CONTROL M-751262 PARTS REQ 360673 PLACARDE INSTALLED.INSTALLED NAV SERVICEABLE LWR COVER PER AMM 25-23-07-401. M751262 CLOSED. PLACARD REMOVED. ESR 52-11-14-05 ITEM 00-125

Part: WARNING LIGHT — FALSE ACTIVATION (L1 DOOR) · airframe 88,179 hrs · 17,095 cycles

L1 DOOR DISARM LIGHT ON DOOR PANEL WILL NOT EXTINGUISH. R & R S1-1090 IAW WDM 52-11-01. OPS CK OK. REF MM 52-11-02-601.

Part: SLIDE — DETACHED (PAX DOOR) · airframe 88,148 hrs · 17,079 cycles

LEFT ENTRY DOOR EMERGENCY SLIDE FELL OUT WHILE OPENING DOOR WITH NORMAL TOGGLE SWITCH. DEFERRED IAW MEL 52 10 3 1 2 1 1 PLACARD INSTALLED.INSTALLED L1 SLIDE/RAFT IAW AMM 25-61-15-400-801 & CONTAINER IAW AMM 25-61-01-400-801. M747780 CLOSED. PLACARD REMOVED. IPC 25-61-05-01-080R.

Part: WIRE — SPARKS (GALLEY) · airframe 87,899 hrs · 16,943 cycles

EMERGENCY DECLARED, O2 MASK DROPPED BUT NOT DONNED - LANDED UNEVENTFULLY - AC OOS** ON DESCENT SPARK FROM BEHIND GALLEY AREA RPRTD BY ACM SMOKE & FUMES NOTED. AFT CB'S FROM GALLEY PULLED SMOKE & FUMES SUBSIDED. GROUND SERVICE BUS C/B POPPED AFTER LANDING. MAIN DR WOULDN'T OPEN ELECTRICALLY. FOUND 115VAC GRD SERVICE WIRING SHORTING TO GROUND AT 9G WALL ATTACH POINT AT 1 O'CLOCK POSITION. REPAIRED WIRING PER EO MD11-2450-79830A. OPS CKS GOOD.

Part: BLOCK — CORRODED (CLG) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CCENTER LANDING GEAR PILLOW BLOCK R/H AFT HOLE HAS CORROSION.REPAIRED CORRODED CENTER GEAR PILLOW BLOCK R/H AFT HOLE IAW SRM 53-40-14 REPAIR 1 FIG. 201. (MINOR)

Part: FITTING — DAMAGED (LT MLG TRUNNION) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CLT MLG TRUNNION FITTING FWD UPPER LUGS ARE GOUGED.REPAIRED DAMAGED LT MLG TRUNNION FITTING FWD UPPER LUGS IAW VT-SAA EA 011-5710-01-A8050 REV. IR AND UPS EO MD11-5710-75719-A. (MINOR)

Part: HINGE — DAMAGED (LT HORIZ STAB) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CL/H HORZ. STAB. T/E LOWER ACCESS DOOR COVER HINGE TEMP. REPAIR REQUIRES PERMANENT REPAIR.ACCOMPLISHED PERMANENT REPAIR OF L/H HORZ. STAB. T/E LOWER ACCESS DOOR COVER HINGE IAW VT-SAA EA 011-5520-01-A8054 REV. I/R AND UPS EO MD11-5510-75657-A. (MAJOR)

Part: FRAME — CRACKED (TAILCONE) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CFWD TAILCONE R/H AFT FRAME IS CRACKED IN O/B RADIUS BELOW UPPER LATCH FITTING.REPAIRED CRACKED FWD TAILCONE R/H AFT FRAME BELOW UPPER LATCH FITTING IAW MD-11 SRM 53-80-07 REPAIR 4. (MINOR)

Part: CROSSBEAM — CHAFED (TAILCONE) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CFWD TAILCONE FWD FLOOR CROSS BEAM HAS SEVERAL AREAS OF CHAFING.REPAIRED CHAFED FWD TAILCONE FWD FLOOR CROSS BEAM IAW MD-11 53-00-00 FIG. 210. (MINOR)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CCENTER CARGO L/H SLOPE PANEL SUPPORT ANGLE IS CRACKED AT STA. 1601.REMOVED, FABRICATED AND REPLACED SUPPORT ANGLE AT STA. 1601 IAW DWG. ADA0130 AND SRM 51-33-01. (MINOR)

Part: DOOR SILL — CRACKED (RT WING) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CR/H WING OUTER T/E LOWER ACCESS DOOR SILL IS CRACKED AT STA. XORS.= 469.375.REPAIRED CRACKED R/H WING OUTER T/E LOWER ACCESS DOOR SILL AT STA. XORS.= 469.375 IAW VT-SAA EA 011-5720-01-A8039 REV. I/R AND UPS EO MD11=5720-60372-C. (MINOR)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CCENTER CARGO R/H SLOP PANEL SUPPORT ANGLE IS CRACKED AT STA 1561.REMOVED AND REPLACED CRACKED CENTER CARGO R/H SLOP PANEL SUPPORT ANGLE AT STA. 1561 IAW MD-11 SRM 51-33-01 & 51-35-01. (MINOR)

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CCENTER CARGO BETWEEN STA. 1721 TO 1741 AND L51 R/H TO L51 L/H HAS CORRODED FINGER DOUBLER.REMOVED, FABRICATED AND REPLACED FINGER DOUBLER BETWEEN STA 1721 TO 1741 AND L 51R TO 51L IAW DWG AGA7809 AND SRM 51-35-01. (MINOR)

Part: DOOR SILL — CRACKED (RT WING) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CR/H WING OUTER T/E LOWER ACCESS DOOR SILL IS CRACKED AT STA. XORS.= 411.250.REPAIRED CRACKED R/H WING OUTER T/E LOWER ACCESS DOOR SILL AT STA. XORS.= 411.250 IAW VT-SAA EA 011-5720-01-A8039 REV. I/R AND UPS EO MD11-5720-60372-C. (MINOR)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CCENTER CARGO L/H SLOPE PANEL SUPPORT ANGLE IS CRACKED AT STA. 1593.REMOVED, FABRICATED AND REPLACED SUPPORT ANGLE IAW DWG. ADA0130 AND SRM 51-33-01. (MINOR)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CCENTER CARGO L/H SLOPE PANEL SUPPORT ANGLE IS CRACKED AT STA. 1581.REMOVED, FABRICATED AND REPLACED SUPPORT ANGLE AT STA. 1581 IAW SRM 51-33-01. (MINOR)

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CCENTER CARGO L/H SLOPE PANEL SUPPORT ANGLE IS CRACKED AT STA. 1621.REMOVED AND REPLACED CRACKED CENTER CARGO L/H SLOPE PANEL SUPPORT ANGLE AT STA. 1621 IAW MD-11 SRM 51-33-01 AND 51-35-01. (MINOR)

Part: LONGERON — CORRODED (FUSELAGE) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CCENTER CARGO LONGERON 47 L/H IS CORRODED BETWEEN STA 1771-1791.REPAIRED CORRODED CENTER CARGO LONGERON 47 L/H BETWEEN STA. 1771-1791 IAW SRM 53-00-05 REPAIR1 FIG. 201. (MAJOR)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CCENTER CARGO L/H SLOPE ANGLE IS CRACKED AT STA. 1681.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. ADA0130 AND SRM 51-33-01. (MINOR)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CCENTER CARGO L/H SLOPE PANEL ATTACH ANGLE IS CRACKED AT STA. 1721.REMOVED, FABRICATED AND REPLACED ANGLE AT STA. 1721 IAW DWG. ADA0130 AND SRM 51-31-01. (MINOR)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CCENTER CARGO L/H SLOPE PANEL SUPPORT ANGLE IS CRACKED AT STA. 1661.REMOVED, FABRICATED AND REPLACED SUPPORT ANGLE AT STA. 1661 IAW DWG. ADA0130 AND SRM 51-33-01. (MINOR)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CCENTER CARGO COMPARTMENT L/H SLOPE PANEL SUPPORT ANGLE IS CRACKED AT STA. 1701.REMOVED AND REPLACED CRACKED CENTER CARGO COMPARTMENT L/H SLOPE PANEL SUPPORT ANGLE AT STA. 1701 IAW MD-11 SRM 51-33-01 AND 51-35-01. (MINOR)

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CCENTER CARGO LONGERON 48 R/H SPLICE FITTING IS CRACKED BETWEEN STA. 1581-1601.REPAIRED CRACKED LONGERON 48 R/H SPLICE FITTING BETWEEN STA. 1581-1601 IAW VT-SAA EA 011-5310-01-A8042 REV. I/R AND UPS EO MD11-5310-60454-C. (MAJOR)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CCENTER CARGO L/H SLOPE PANEL SUPPORT ANGLE IS CRACKED AT STA. 5-52.REMOVED, FABRICATED AND REPLACED ANGLE AT STA. 5-52 IAW DWG. ADA0130 AND SRM 51-33-01. (MINOR)

Part: SPAR CAP — CORRODED (RT WING) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CR/H WING REAR SPAR UPPER CAP AFT FLANGE HAS CORROSION BETWEEN STA. XORS.= 763.0-826.5.REPAIRED CORRODED R/H WING REAR SPAR UPPER CAP AFT FLANGE BETWEEN STA. XORS.= 763-826.5 IAW VT-SAA EA 011-5710-01-A8057 REV. I/R AND UPS EO MD11-5740-75653-A. (MINOR)

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CFWD. CARGO FLOOR BEAM IS CRACKED AT STA. 6-70, Z=-98 AND BETWEEN X=-37 & X=-64.REPAIRED CRACKED FLOOR BEAM AT STA. 6-70, Z=-98 AND BETWEEN X=-37 TO X=-64 IAW VT-SAA EA 011-5310-01-A8053 REV. I/R AND UPS EO MD11-5310-75857-A. (MAJOR)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CCENTER CARGO COMPARTMENT L/H SLOPE PANEL SUPPORT ANGLE IS CRACKED AT STA. 1741.REMOVED AND REPLACED CRACKED CENTER CARGO COMPARTMENT L/H SLOPE PANEL SUPPORT ANGLE AT STA. 1741 IAW MD-11 SRM 51-33-01 AND 51-35-01. (MINOR)

Part: STIFFENER — CRACKED (RT WING) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CRT WING L/E STIFFENER AT O/B SIDE OF PANEL 618FB IS CRACKED.REMOVED AND REPLACED CRACKED RT WING L/E STIFFENER AT O/B SIDE OF PANEL 618FB IAW MD-11 SRM 51-33-01 AND 51-35-01. (MINOR)

Part: RIB — CRACKED (RT WING) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CRT WING FIXED L/E RIB (FORMER) IS CRACKED AT XOS=584.8912.REPAIRED CRACKED RT WING FIXED L/E RIB (FORMER) AT XOS=584.8912 IAW MD-11 SRM 57-00-00 REPAIR GENERAL, FIGURE 204. (MAJOR)

Part: DOUBLER — WORN (RT WING) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CR/H WING FIXED L/E SKIN REPAIR DOUBLER HAS DEEP WEAR BETWEEN STA. XIS= 163.4 AND 164.972.REMOVED, INSPECTED AND REPLACED R/H WING FIXED L/E SKIN REPAIR DOUBLER BETWEEN STA. XIS= 163.4 TO 164.972 IAW VT-SAA EA 011-5740-01-A8035 REV. I/R AND UPS EO MD11-5720-75779-A. (MAJOR)

Part: SPAR CAP — CORRODED (LT WING) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CL/H WING REAR SPAR UPPER CAP AFT FLANGE HAS CORROSION FWD. OF #3 SPOILER O/B END.REPAIRED CORRODED L/H WING REAR SPAR UPPER CAP AFT FLANGE BETWEEN STA. STA. XORS.= 551-650 IAW VT-SAA EA 011-5710-01-A8045 REV. I/R AND UPS EO MD11-5710-75647-A. (MINOR)

Part: FILLER — CORRODED (LT WING) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CLT WING T/E PANEL HAS BULGE FWD OF I/B AILERON.REPAIRED CORRODED LT WING T/E SPACER FILLER BETWEEN XORS 414 TO XORS 420 IAW VT-SAA EA 011-5700-01-A8051 REV. IR AND UPS EO MD11-5710-75648-A. (MINOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CLT WING FIXED L/E SKIN SPLICE DOUBLER AT XOS 789 IS CRACKED.REMOVED AND REPLACED CRACKED LT WING FIXED L/E SPLICE DOUBLER AT XOS 789 IAW MD-11 SRM 51-33-01. (MINOR)

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CLT WING O/B FLAP I/B FWD HINGE FAIRING FWD I/B SUPPORT CLIP IS CRACKED.REMOVED AND REPLACED CRACKED LT WING O/B FLAP I/B FWD HINGE FAIRING FWD I/B SUPPORT CLIP IAW MD-11 SRM 51-33-01. (MINOR)

Part: SKIN — CORRODED (LT WING) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CL/H WING UPPER FWD. SKIN HAS CORROSION BETWEEN STA. XORS,=222.65 TO 230.6.REPAIRED CORRODED L/H WING UPPER FWD. SKIN BETWEEN STA. XORS.= 222.65 TO 230.6 IAW VT-SAA EA 011-5730-01-A8038 REV. I/R AND UPS EO MD11-5730-75670-A. (MINOR)

Part: SPAR CAP — CORRODED (LT WING) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CL/H WING REAR SPAR UPPER CAP AFT FLANGE HAS CORROSION FWD. # 2 SPOILER.REPAIRED CORRODED L/H WING REAR SPAR UPPER CAP AFT FLANGE BETWEEN STA. XORS.= 551-650 IAW VT-SAA EA 011-57140-01-A8045 REV. I/R AND UPS EO MD11-5710-75647-A. (MINOR)

Part: LANDING — CRACKED (LT WING) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CL/H WING FIXED L/E LOWER STRINGER (PANEL LANDING) IS CRACKED AT STA. XOS.= 906.5607.REPAIRED CRACKED L/H WING FIXED L/E LOWER STRINGER AT STA. XOS.= 906.5607 IAW SRM 57-40-03 REPAIR 1 FIG. 201. (MAJOR)

Part: INTERCOSTAL — CRACKED (NR 2 PYLON) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2C#2 PYLON CARRY THRU REAR SPAR INTERCOSTAL IS CRACKED AT STA. YID= 375, XID= -7.1 AND ZID= 65.REPAIRED CRACKED #2 PYLON CARRY THRU REAR SPAR INTERCOSTAL AT STA. YID= 375, XID= -7.1 AND ZID= 65 IAW SRM 55-30-02 REPAIR 7 FIG. 204. (MAJOR)

Part: SPAR CAP — CORRODED (LT WING) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CL/H WIING REAR SPAR UPPER CAP HAS CORROSION FWD. OF #3 SPOILER I/B END.REAPIRED CORRODED L/H WING REAR SPAR UPPER CAP AFT FLANGE BETWEEN STA. XORS.= 551-650 IAW VT-SAA EA 011-5710-01-A8045 REV. I/R AND UPS EO MD11-5710-75647-A. (MINOR)

Part: SKIN — CRACKED (LT WING LE) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CL/H WING L/E LOWER SKIN IS CRACKED AT STA. XOS= 776.REPAIRED CRACKED L/H WING L/E LOWER SKIN AT STA. XOS.= 776 IAW SRM 57-40-02 REPAIR 7 FIG. 201. (MAJOR)

Part: BEAM — CRACKED (L3 DOOR) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CMAIN CABIN L3 PLUG DOOR LOWER FWD STOP FITTING (BEAM) IS BROKEN OFF.REMOVED AND REPLACED BROKEN MAIN CABIN L3 PLUG DOOR LOWER STOP FITTING (BEAM) IAW MD-11 SRM 51-33-01. (MINOR)

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CCENTER CARGO INTERMEDIATE FUSELAGE STA. BETWEEN STA. 1721 TO 1741 AND L=51R TO L51L INTERNAL RING DOUBLER HAS HEAVY CORROSION.REMOVED, FABRICATED AND REPLACED RING DOUBLER BETWEEN STA. 1721 TO 1741 AND L51R TO L51L IAW DWG. AGA7808 AND NGA6314 AND SRM 51-33-01. (MINOR)

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CR-3 DOOR JAMB INNER SKIN (WEB) IS CRACKED AT STA. 1256.75 AND Z=60.REPAIRED CRACKED R-3 DOOR JAMB INNER SKIN (WEB) AT STA. 1256.75 AND Z=60 IAW VT-SAA EA 011-5310-01-A8034 REV. I/R AND UPS EO MD11-5310-75793-A. (MAJOR)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CMAIN CABIN LONGERON 15 R/H "T" ANGLE IS CRACKED AT STA. 1341.REMOVED, FABRICATED AND REPLACED LONG. 15 R/H "T" ANGLE AT STA. 1341 IAW DWG. AEA7568 AND SRM 51-31-01. (MINOR)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CPREVIOUS MAJOR REPAIR AT LOWER FWD CARGO DOOR CUTOUT AFT SIDE HAS EDGE DAMAGE.REPAIRED DAMAGED PREVIOUS MAJOR REPAIR AT LOWER FWD CARGO DOOR CUTOUT AFT SIDE IAW VT-SAA EA 011-5330-01-A8036 REV. IR AND UPS EO MD11-5330-75654-A. (MINOR)

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CL-3 DOOR JAMB WEB (INNER SKIN) IS CRACKED AT STA. 1254 AND Z=-18.REPAIRED CRACKED L-3 DOOR JAMB WEB (INNER SKIN) AT STA. 1254 AND Z=-18 IAW SRM 53-40-15 REPAIR 3 FIG. 201. (MAJOR)

Part: DOOR FRAME — CRACKED (BS 1313) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CMAIN CABIN L-3 DOOR JAMB WEB IS CRACKED AT STA. 1313 AND Z=-15.REPAIRED CRACKED L-3 DOOR JAMB WEB AT STA. 1313 AND Z=-15 IAW SRM 53-40-15 REPAIR3 FIG. 201. (MAJOR)

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CRT MLG W/W O/B AFT AREA LOWER VERTICAL STIFFNER IS CRACKED.REMOVED AND REPLACED CRACKED RT MLG W/W O/B AFT AREA LOWER VERTICAL STIFFNER IAW MD-11 SRM 51-35-01. (MINOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CL/H WING L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS.= 633.4 TO 636.8.REPAIRED CRACKED L/H WING L/E BEADED DOUBLER BETWEEN STA. SOX.= 633.4 TO 636.8 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: SUPPORT WEB — CRACKED (FUSELAGE) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CCENTER ACCESSORY COMP. AT STA. 6-90 R/H CIELING SUPPORT WEB IS CRACKED.REMOVED, FABRICATED AND REPLACED WEB IAW DWG. ADA7652 AND SRM 51-33-01. (MINOR)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CCAC AT STA. 6-90 , FLOOR AREA R/H SUPPORT ANGLE IS CRACKED.REMOVED, FABRICATED AND REPLACED SUPPORT ANGLE IAW DWG. AAN7185 AND SRM 51-33-01. (MINOR)

Part: SKIN — CRACKED (THRUST REVERSER) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2C#1 ENG. I/B T/R AFT FIXED INNER BARREL SKIN IS CRACKED.REPAIRED #1 ENG. I/B T/R AFT FIXED INNER BARREL UPPER SKIN IAW VT-SAA EA 011-7830-01-A8032 REV. I/R AND UPS EO MD11-7830-755551-A. (MINOR)

Part: SKIN — CRACKED (THRUST REVERSER) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2C#3 ENG. L/H T/R AFT FIXED INNER BARRELL UPPER SKIN IS CRACKED AT STA. NAC=194 & 11:00 POS.REPAIRED #3 ENG. L/H T/R FIXED INNER BARRELL UPPER SKIN IAW VT-SAA EA 011-7830-01-A8301 REV. I/R AND UPS EO MD11-7830-75553-A. (MINOR)

Part: SKIN — CRACKED (THRUST REVERSER) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2C#3 ENG. R/H T/R AFT INNER BARREL UPPER SKIN IS CRACKED AT STA. NAC=194 & 1:00 POS.REPAIRED CRACKED #3 ENG. R/H T/R IAW VTSAA EA 011-7830-01-A8030 REV. I/R AND UPS EO MD11-7830-75552-A. (MINOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CR/H WING L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS.= 759.1 TO 763.6.REPAIRED CRACKED R/H WING L/E BEADED DOUBLER BETWEEN STA. XOS. = 759.1 TO 763.6 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CL/H WING L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS.= 610.8 TO 621.6.REPAIRED CRACKED L/H WING L/E BEADED DOUBLER BETWEEN STA. XOS.= 610.8 TO 621.6 IAW SRM 57-40-05 REPAIR 15 FIG. 205. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CR/H WING L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS.= 584.8 TO 589.8.REPAIRED CRACKED R/H WING L/E BEADED DOUBLER BETWEEN STA. XOS.= 584.8 TO 589.8 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CL/H WING L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS.= 653.0 TO 658.REPAIRED CRACKED L/H WING L/E BEADED DOUBLER BETWEEN STA. XOS.= 653.0 TO 658 IAW SRM 57-40-02 REPAIR 15 FIG.205. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 86,131 hrs · 16,185 cycles

INSPECTION TYPE:2CR/H WING L/E BEADED DOUBLER IS CRACKED BEYTWEEN STA. XOS.= 768.2 TO 772.8.REPAIRED CRACKED R/H WING L/E BEADED DOUBLER BETWEEN STA. XOS.= 768.2 TO 772.8 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: HANDLE — INOPERATIVE (LANDING GEAR) · airframe 86,055 hrs · 16,150 cycles

INSPECTION TYPE:N/AATB - LEFT MAIN GEAR PRI/SEC GEAR IND. RED WGEAR HANDLE UFOUND THE LEFT DOWN LOCK LINK REQUIRED LUBRCIATION. ACCOMPLISHED PER AMM 12-21-00 CYCLED GEAR SEVERAL TIMES. NORMAL RETRACTION REF AMM 32-00-00-501

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 85,351 hrs · 15,847 cycles

LVL 1 EMER LT BAT 1 LO ON PREFLIGHT. R & R AND TESTED EMERGENCY LIGHTING BATTERY IAW MM 33-51-01-401 AND MM 33-51-10-01, ITEM 08.

Part: CONTROL UNIT — MALFUNCTIONED (ELECTRICAL SYS) · airframe 85,146 hrs · 15,757 cycles

INSPECTION TYPE:N/A **AIR TURN BACK** WHILE IN CRUISE, WE GOT MULTIPLE LEVEL 1 ALERTS GEN 1,2,3 OFF THAT LASTED FOR ONE SECOND THEN WOULD GO BACK NORMAL. WE CYCLED THE SYSTEM CONTROLLER WITH NO CHANGE. R/R EPCU ASSY AS PER AMM 24-08-01/401. PERFORMED EPCU RTS AS PER AMM24-08-01/501. TEST PASS WITH NO RELATED FAULT MSG NOTED. PERFORMED #1, #2 AND #3 ENGINE RUN AS PER AMM71-00-00. ALL PARAMETERS NORMAL.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 84,472 hrs · 15,505 cycles

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

Part: LAMP — INOPERATIVE (MASTER CAUTION) · airframe 84,448 hrs · 15,499 cycles

FIRST OFFICER`S MASTER CAUTION LAMP INOPERATIVE. REPLACED THE LAMP.

Part: CONTROL PANEL — MALFUNCTIONED (APU) · airframe 84,114 hrs · 15,385 cycles

FIRE WARNING TEST CONTINUOUSLY ON. R & R THE APU CONTROL PANEL IAW AMM 49-04-01-000-801, AND 49-04-01-400-801. OPS TESTED IAW 49-10-00-700-801, OPS NORMAL.

Part: ENGINE — FIRE (NR 3) · airframe 83,888 hrs · 15,315 cycles

RETURNED TO BLOCKS DUE TO A FIRE ON THE NR 3 ENGINE DURING PUSH & START. ACCOMPLISHED K ALER K182779, AND EO 4000-7100-69656-A. ENGINE OK FOR SERVICE.

Part: RETAINING CLIP — BROKEN (LIFE VEST) · airframe 83,641 hrs · 15,230 cycles

INSPECTION TYPE:PS-1, LIFE STOWAGE COMPARTMENT DOOR SUPER SEATS LEFT AND CTR RETAINING CLIPS BROKEN. R&R LIFE VEST STOWAGE COMPARTMENT BETWEEN LEFT AND CTR SUPER SEATS, REF AMM 25-64-01-201.

Part: RUDDER — CORRODED (UPPER AFT) · airframe 82,752 hrs · 15,012 cycles

INSPECTION TYPE: 4C, UPPER AFT RUDDER CORRODED UNDER EXTERIOR SKIN. REMOVED AND REPLACED THE RUDDER IAW AMM 27-20-30, P/B 401.

Part: HINGE — CRACKED (HORIZONTAL STAB) · airframe 82,752 hrs · 15,012 cycles

INSPECTION TYPE: 4C, LT HORIZONTAL STAB T/E ACCESS COVER, LOWER DOOR HINGE IS CRACKED AT XE 178, & XE 180. REPAIRED THE HINGE IAW EA 011-5520-01-A7154, REV I/R, AND EO MD11-5520-67620-A.

Part: PANEL — CRACKED (LT ELEVATOR) · airframe 82,752 hrs · 15,012 cycles

INSPECTION TYPE: 3C, LT INBD ELEVATOR L/E FAIRING PANEL LOWER SURFACE AT ATTACH ANGLE WAS FOUND CRACKED, OTBD OF ACTUATOR. ACCOMPLISHED A PERMANENT REPAIR IAW EA. 011-5520-01-A7147, REV IR, AND EO MD11-5520-67625-A. MAJOR.

Part: SPAR CAP — CRACKED (LT WING) · airframe 82,752 hrs · 15,012 cycles

INSPECTION TYPE: 3C, LEFT WING LOWER REAR SPAR CAP CRACKED AT XORS 1085. REPAIRED THE SPAR CAP IAW SRM 57-20-10, REPAIR 1, FIG. 201, SRM 51-38-01, FIG 15, AND SRM 51-38-01, GENERAL, PAR 6 D, REV 64. MAJOR.

Part: SPAR CAP — CRACKED (LT WING) · airframe 82,752 hrs · 15,012 cycles

INSPECTION TYPE: 3C, LEFT OUTER WING UPPER REAR SPAR CAP IS CRACKED BETWEEN XORS 1082.3 AND 1090. REPAIRED THE SPAR CAP IAW EA 011-5710-01-A7131, REV I/R, AND EO MD11-5710-67636-A. MAJOR.

Part: STIFFENER — CRACKED (BS 1841) · airframe 82,752 hrs · 15,012 cycles

INSPECTION TYPE: 4C, AFT CARGO COMPARTMENT BILGE VERTICAL STIFFENER CRACKED AT BS 1841, LBL 20. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-31-01, AND 51-33-01.

Part: STIFFENER — CRACKED (BS 1841) · airframe 82,752 hrs · 15,012 cycles

INSPECTION TYPE: 4C, AFT CARGO BILGE VERTICAL STIFFNER CRACKED AND HAS SHEARED RIVETS AT BS 1841, RBL 20. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-33-01, AND 51-35-01.

Part: LUG — GOUGED (THRUST REVERSER) · airframe 82,752 hrs · 15,012 cycles

INSPECTION TYPE: 4C, NR 2 ENGINE RT THRUST REVERSER UPPER TRACK LUG GOUGED. REPAIRED THE LUG IAW EO MD11-7830-67388-A.

Part: SKIN — CHAFED (TAIL CONE) · airframe 82,752 hrs · 15,012 cycles

INSPECTION TYPE: 4C, TAIL CONE UPPER FWD LT INTERNAL SKIN DOUBLER CHAFED. REPAIRED IAW EA 011-5350-01-A7110, REV IR, AND EO MD11-5350-67365-A.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 82,752 hrs · 15,012 cycles

INSPECTION TYPE: 4C, LT INBD FLAP EXTERIOR SKIN GOUGED AT TWO PLACES, FLAP VANE CENTER TRACK CUT OUT. REPAIRED THE SKIN IAW EA. 011-5753-01-A7115, REV IR, AND EO MD11-5750-67448-A.

Part: SKIN — CHAFED (RT WING) · airframe 82,752 hrs · 15,012 cycles

INSPECTION TYPE: 4C, RIGHT WING DROOP L/E SKIN AT THE OTBD XDLE 329.774 HAS CHAFED. REPAIRED THE RT WING DROOP L/E SKIN IAW SRM 57-40-01, REPAIR 15, FIG 202. MAJOR.

Part: SKIN — CHAFED (LT WING L/E) · airframe 82,752 hrs · 15,012 cycles

INSPECTION TYPE: 4C, LT WING L/E LOWER SKIN PANEL CHAFED JUST INBD OF THE NR 3 SLAT AT NR 1 PYLON. REMOVED THE SKIN PANEL, FABRICATED REPLACEMENT SKIN PANEL AND INSTALLED IAW DWG ARB2363 AND SRM 51-35-01 & 51-33-01.

Part: RIB — CRACKED (LT WING L/E) · airframe 82,752 hrs · 15,012 cycles

INSPECTION TYPE: 4C, LT WING L/E RIB CRACKED JUST INBD OF THE NR 9 SLAT TRACK.REMOVED CRACKED RIB JUST I/B OF NR 9 SLAT TRACK, FABRICATED A REPLACEMENT RIB AND INSTALLED IAW DWG. ARB2931 AND MD-11 SRM 51-33-01.

Part: CHAIN DRIVE — FAILED (L1 DOOR) · airframe 81,823 hrs · 14,778 cycles

L1 DOOR BINDS WHEN CLOSING. DOOR STARTS DOWN AND BINDS AFTER MOVING ONE OR TWO INCHES, PIECES OF CHAIN FELL TO THE FLOOR IN THE COURIER AREA. REMOVED & REPLACED REAR CHAIN ASSY ON L1 DOOR IAW AMM 52-11-09, OPS CHECKED GOOD. ACFT OK FOR SERVICE

Part: SOLENOID — INOPERATIVE (L1 DOOR LOCK) · airframe 81,424 hrs · 14,704 cycles

L1 DOOR INOPERATIVE PRIOR TO DEPARTURE. REMOVED AND REPLACED L1 DOOR LOCK RELEASE SOLENOID IAW AMM 52-10-06.

Part: ACTUATOR — INOPERATIVE (L1 DOOR) · airframe 81,382 hrs · 14,692 cycles

L1 DOOR INOPERATIVE ELECTRICALLY. REPLACED CABIN DOOR ELECTRIC ACTUATOR IAW AMM 52-11-01.

Part: RELAY — INOPERATIVE (L1 DOOR) · airframe 81,373 hrs · 14,690 cycles

L1 DOOR ELECTRICAL OPENING INOPERATIVE. TROUBLESHOT IAW FIM 52-11-00, R & R THE DOOR CONTROL RELAY, OPS NORMAL.

Part: WEB — CRACKED (BS 1372) · airframe 81,347 hrs · 14,679 cycles

INSPECTION TYPE: SV, OVER WING UPPER FUEL TANK AFT WEB CRACKED BS 1372 AT X=80. REPAIRED CRACKED WEB IAW EA 011-5710-01-A6913 REV IR, AND EO MD11-5710-65091-A. MAJOR.

Part: WEB — CRACKED (BS 1372) · airframe 81,347 hrs · 14,679 cycles

INSPECTION TYPE: SV, OVER WING UPPER FUEL TANK AFT WEB CRACKED BS 1372 AT X=-80. REPAIRED CRACKED WEB IAW EA 011-5710-01-A6913, REV IR AND EO MD11-5710-65091-A. MAJOR.

Part: LIMIT SWITCH — MALFUNCTIONED (R2 DOOR) · airframe 80,494 hrs · 14,498 cycles

R2 DOOR INOPERATIVE. EXERCISED R1 DOOR DOWN LIMIT SWITCH S1-244. DOOR OPS NORMAL IAW AMM 52-10-01-201

Part: SOLENOID — FAULTED (L1 DOOR) · airframe 79,410 hrs · 14,277 cycles

L1 DOOR FAILED TO OPERATE WITH INTERIOR & EXTERIOR SWITCH. TROUBLESHOT SYS AND R & R THE L1 DOOR LOCK PIN RELEASE SOLENOID IAW MM 52-10-06-000 & - 400. OPS NORMAL IAW 52-11-02.

Part: RELAY — INOPERATIVE (L1 DOOR) · airframe 79,405 hrs · 14,273 cycles

L1 DOOR STUCK OPEN AND WILL NOT CLOSE ELECTRICALLY FROM OUTSIDE OR INSIDE SWITCH. MOVED DOOR MANAULLY A FEW INCHES ABLE TO CLOSE DOOR ELECTRICALLY THE REST OF THE WAY. R & R THE L1 DOOR RELAY LOCK RELEASE R2-5324 IAW WDM 52-11-01. DOOR OPS CHECKED GOOD IAW MM 52-10-01.

Part: TEE FITTING — DEFORMED (WING) · airframe 79,010 hrs · 14,181 cycles

INSPECTION TYPE: SERVICE, CENTER AUXILIARY TANK TEE FITTING FOUND DEFORMED WITH OVERSIZED, OUT-OF-ROUND FASTENER HOLES AT XCW0, STR 52. REMOVED FABRICATED AND INSTALLED REPLACEMENT TEE FITTING IAW EA 011-5710-01-A6444, REV IR AND EO MD11-5710-61836-A, MAJOR.

Part: REPAIR — LEAKING (WING) · airframe 79,010 hrs · 14,181 cycles

INSPECTION TYPE:SERVICE, CENTER WING TANK LOWER STR 52 SPLICE REPAIR LEAKING AT XCW = 17. REPAIRED LEAK IAW EA 011-5710-01-A6444, REV IR AND EO MD11-5710-61836-A, MAJOR.

Part: BOTTLE — BLOWN (L1 DOOR) · airframe 78,764 hrs · 14,122 cycles

FOUND L1 ENTRY DOOR EMERGENCY BOTTLE BLOWN, SERVICED THE BOTTLE IAW MM 12 25 04. PERFORMED. OPS CHECKED GOOD IAW MM 52 11 02. OK FOR SERVICE.

Part: TIRE — LEAKING (NLG) · airframe 78,678 hrs · 14,099 cycles

LEFT NOSE TIRE HAD LOW PRESSURE. EMERGENCY DECLARED. R & R LEFT NOSE WHEEL ASSY IAW AMM 32-42-01-401

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 78,236 hrs · 13,972 cycles

EMERGENCY BATTERY LOW TAB 1. REPLACED EMEREGENCY LIGHT POWER SUPPLY IAW MM 33-51-01. OPS TEST GOOD IAW 33-51-01-200.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 78,236 hrs · 13,972 cycles

EMERGENCY LIGHT TEST FAIL EMERGENCY LEFT BATTERY 1 LOW MESSAGE. RETESTED EMERGENCY LIGHT SYS IAW AMM 33-50-00. ALL TESTS PASSED.

Part: LONGERON — CORRODED (L38 LEFT) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, CENTER CARGO LONGERON 38L HAS CORROSION BETWEEN BS 5-53 AND 5-93. ACCOMPLISHED PERMANENT REPAIR ON CENTER CARGO LONGERON 38L FROM BS 5-53 TO 5-93 IAW SRM 53-00-05, REPAIR FIG 201/202.

Part: DOUBLER — CORRODED (R3 DOOR) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:C3, R-3 DOOR INTERNAL DOUBLER HAS CORROSION BETWEEN BS 1240 TO BS 1305, LONGERON 11R TO 15R. REPAIRED CORRODED R-3 DOOR INTERNAL DOUBLER BETWEEN BS 1240 TO 1305 LONGERON 11R TO 15R IAW EA 011-5330-01-A6161, REV I/R AND EO 5330-60274-A,

Part: SKIN — CRACKED (RIGHT WING) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE: 3C, RT WING LOWER FUEL ACCESS DOOR SKIN LANDING HAS THREE CRACKS AT FASTER HOLES BETWEEN XORS 683.4 AND 713.6. ACCOMPLISHED 3 EA BUSHING REPAIRS ON RT WING LOWER FUEL ACCESS DOOR SKIN LANDING BETWEEN XORS 683.4 AND 713.6 IAW SRM 57-20-02, REPAIR 5, FIGURE 201.

Part: ACCESS PANEL — CRACKED (LEFT WING) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, LT WING LOWER FUEL ACCESS DOOR SKIN LANDING HAS 4 EA CRACKS AT FASTENER HOLES BETWEEN BS XORS 683.4 AND 713.6. ACCOMPLISHED 4 EA BUSHING REPAIRS ON LT WING LOWER FUEL ACCESS DOOR SKIN BETWEEN BS XORS 683.4 AND 713.6 IAW SRM 57-20-02 REPAIR 5, FIG 201.

Part: FITTING — CRACKED (BS 1278) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, CENTER LOWER AUXILIARY FUEL TANK ANGLE FITTING CRACKED AT BS 1278 BETWEEN L42L AND L43L. R & R CENTER LOWER AUXILIARY FUEL TANK ANGLE FITTING IAW SRM 51-33-01 AND 51-35-01.

Part: BARREL — GOUGED (THRUST REVERSER) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, NR 3 ENGINE OTBD T/R INNER ACOUSTIC BARREL GOUGED. ACCOMPLISHED REPAIR ON NR 3 ENG OTBD T/R INNER ACOUSTIC BARREL IAW EA 011-7830-01-A6169, REV I/R AND EO MD11-7830-60351-A.

Part: STRINGER — CRACKED (RT WING) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, RT WING STR NR 12 CRACKED BETWEEN BS XORS 623 AND XORS 653. ACCOMPLISHED PERMANENT REPAIR ON RT WING STR 12 FROM NS XORS 623 TO XORS 653 IAW SRM 57-00-03, REPAIR 5, FIG 202.

Part: SKIN — DAMAGED (RT AILERON) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, CHAFE DAMAGE IN RT OTBD AILERON L/E SKIN AT BS XOA878. REPAIRED NOTED CHAFE DAMAGE IAW EA 011-5750-01-A6160, REV IR AND EO MD11-5750-60267-A.

Part: STRINGER — CRACKED (LEFT WING) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE: 3C, LEFT WING STRINGER NR 9 HAS 12" CRACK BETWEEN BS XORS 799.4 AND XORS 826.5. ACCOMPLISHED PERMANENT REPAIR ON LT WING STRINGER NR 9 FROM BS XORS 799.4 TO XORS 826.5 IAW SRM 57-00-03, REPAIR 5, FIGURE 202.

Part: FITTING — CORRODED (MAIN CABIN) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, RCB FLOOR FITTING NR 8 HAS CORROSION ON TOP FLANGE BS 488 X= - 47.5. ACCOMPLISHED BLEND REPAIR ON RCB FLOOR FITTING NR 8 BS 488 X=-47.5 IAW EA 011-5310-01-A6176 REV I/R AND EO 5340-60281-A.

Part: STRINGER — CRACKED (RIGHT WING) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, RT WING STRINGER 14 CRACKED BETWEEN BS XORS 506 AND 538. ACCOMPLISHED PERMANENT REPAIR ON RT WING STR 14 FROM BS XORS 506 TO 538 IAW SRM 57-00-03. REPAIR 5, FIGURE 201.

Part: FITTING — GOUGED (MAIN CABIN) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, RCB FLOOR FITTING NR 6 HAS CORROSION ON UPPPER AND LOWER SURFACE, PERFORMED BLEND REPAIR ON RCB FLOOR FITTING NR 6 UPPER AND LOWER SURFACE IAW EA 011-5310-01-A6175, REV I/R AND EO MD11-5340-60352-A.

Part: INTERCOSTAL — CRACKED (FWD CARGO BAY) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, FORWARD CARGO INTERCOSTAL CRACKED AT BS 6-50 ABOVE L42R. R & R FORWARD INTERCOSTAL IN FORWARD CARGO AT BS 6-50 ABOVE L42R IAW SRM 51-35-01 AND SRM 51-33-01.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, CENTER WING TANK LOWER STR 47 CRACKED AT XCW17, -17, -46.5. REPAIRED STR 47 IAW EA 011-5710-01-A6145, REV IR AND EO MD11-5740-60443-A.

Part: PLATE — CRACKED (BS 1159) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, TRUSS PLATE CRACKED ALONG TOP OF L27R IN CAC AT BS 1159. REMOVED, FABRICATED AND INSTALLED REPLACEMENT TRUSS PLATE IAW DWG AFA7605 AND SRM 51-33-01.

Part: FITTING — CORRODED (MAIN CABIN) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, RCB WALL FLOOR FITTING NR 4 HAS CORROSION ON LOWER SURFACE. PERFORMED BLEND REPAIR ON RCB WALL FLOOR FITTING NR 4 LOWER SURFACE IAW EA 011-5310-01-A6175, REV I/R AND EO MD11-5340-60352-A.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, CENTER WING TANK LOWER STR 52 CRACKED AT XCW=17.00. REPAIRED STR 52 IAW EA 011-5710-01-A6146, REV. IR AND EO MD11-5710-60429-A.

Part: STRINGER — CRACKED (RT WING) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:C3, RT WING STRINGER RUN-OUT NR 13 HAS A CRACK APPROXIMATELY 18" LONG AT BS XORS.562 TO 593. REPAIRED CRACKED RT WING STR RUN-OUT AT BS XORS.562 TO 593 IAW EA 011-5710-01-A6154, REV I/R AND EO MD11-5710-60282-A.

Part: SKIN — GOUGED (HORIZONTAL STAB) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, LT HORIZONTAL STABILIZER L/E HAS MULTIPLE SKIN NICKS AND GOUGES ACCOMPLISHED LT HORIZONTAL STABILIZER L/E BLEND REPAIR IAW EA 011-5510-A6180, REV I/R AND EO 5510-60353-A.

Part: SKIN — GOUGED (HORIZONTAL STAB) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, LT HORIZONTAL STABILIZER OTBD L/E SECTION HAS SEVERAL NICKS AND GOUGES ON INBD END. REPAIRED GOUGED LT HORIZONTAL STABILIZER L/E SECTION IAW EA 011-5510-01-A6177, REV I/R AND EO MD11-5510-60450-A.

Part: FITTING — CORRODED (MAIN CABIN) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, RCB WALL FLOOR FITTING NR 5 HAS CORROSION ON UPPPER AND LOWER SURFACE. PERFORMED BLEND REPAIR ON RCB WALL FLOOR FITTING NR 5 IAW EA 011-5310-01-A6175 REV I/R AND EO 5340-60352-A.

Part: INTERCOSTAL — CRACKED (FWD CARGO) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, FORWARD CARGO INTERCOSTAL CRACKED BS 6-50 TO 6-70 ABOVE LONGERON 42L. R & R FORWARD CARGO INTERCOSTAL AT BS 6-50 T0 6-70 ABOVE LONGERON 42L IAW SRM 51-33-01 AND SRM 51-31-01.

Part: SKIN — CORRODED (BS 1229-1239) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, CENTER WING UPPER SKIN HAS CORROSION BS 1229 TO BS 1239 XCW -24 TO XCW 8 AT STR 15 ACCOMPLISHED BLEND REPAIR ON CENTER WING UPPER SKIN BS 1229 TO BS 1239 XCW -24 TO XCW 8 AT STR 15 IAW EA 011-5710-01-A6170, REV I/R AND EO 5730-60305-A.

Part: LONGERON — CORRODED (BS 1381) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, MAIN CABIN LONGERON 16R AT BS 1381 HAS CORROSION. R & R LONGERON 16R AT BS 1381 IAW SRM 51-33-01, PG. 30.

Part: NUT PLATE — BROKEN · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3 CONE BROKEN NUTPLATE INSIDE RCB BASE RECTIFIED BROKEN NUTPLATE CONDITION EA 011-5310-01-A6142, REV IR AND EO MD11-5320-60382-A.

Part: LONGERON — CORRODED (BS 1481-1501) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, MAIN CABIN LONGERON 18L, BS 1481 TO 1501 HAS CORROSION. R & R MAIN CABIN LONGERON 18L AT BS 1481 TO 1501 IAW SRM 51-33-01 AND DWG AEA0020.

Part: LONGERON — CORRODED (BS 1381-1401) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, MAIN CABIN LONGERON 18L HAS CORROSION AT BS 1381 TO BS 1401. REMOVED, FABRICATED AND INSTALLED NEW MAIN CABIN LONGERON 18L AT BS 1381 TO BS 1401 IAW SRM 51-33-01, SRM 51-31-01 AND DWG DWF AEA0220-555.

Part: LONGERON — CORRODED (BS 1361) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, INTERRUPTED LONGERON 25R CORRODED AT BS 1361. REMOVED CORROSION IAW SRM 51-21-01, 53-00-00, FIG 205.

Part: LONGERON — CORRODED (BS 1401-1421) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, MAIN CABIN LONGERON 18L HAS CORROSION AT BS 1401 TO 1421. R & R MAIN CABIN LONGERON 18L, BS 1401 TO BS 1421 IAW SRM 51-33-01 AND DWG AEA0220.

Part: SKIN — CORRODED (BS 1256-1276) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, CENTER WING UPPER SKIN HAS CORROSION BS 1256-1276, XCW 114 BETWEEN STR 10-11 ACCOMPLISHED REPAIR ON CENTER WING UPPER SKIN BS 1256-1276 XCW 114 BETWEEN STR 10-11 IAW EA 011-5730-01-A6171, REV I/R AND EO MD11-5330-60302-A. THIS REPAIR DETERMINED TO BE MINOR IAW REPAIR.

Part: LONGERON — CORRODED (BS 1401-1421) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE: 3C, MAIN CABIN LONGERON 18R HAS CORROSION BS 1401 TO 1421. REMOVED, FABRICATED AND REPLACED MAIN CABIN LONGERON 18R BS 1401 TO 1421 IAW SRM 51-33-01 AND DWG DAC AEA0220.

Part: STRINGER — CRACKED (RT WING) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, RT WING LOWER STR 44R CRACKED BETWEEN BS XORS 506 TO XORS 538. ACCOMPLISHED PERMANENT REPAIR ON RT WING LOWER STR 44 IAW SRM 57-00-03, FIG 201, REPAIR 4.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, MAIN CABIN RCB FLOOR PANEL HAS CORROSION BS 490 TO 500 X=-27.5 TO X= 32. ACCOMPLISHED BLEND REPAIR ON MAIN CABIN RCB FLOOR PANEL BS 490 TO 500 X=-27.5 TO X= -32 IAW EA 011-5310-01-A6163, REV I/R AND EO MD11-5310-60278-A.

Part: STRINGER — CRACKED (RT WING) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, RIGHT WING STR 10 CRACKED BETWEEN BS XORS 737.5 AND XORS 772.5. ACCOMPLISHED PERMANENT REPAIR ON RT WING STRINGER 10, BS XORS 737.5 AND BS XORS 772.5 IAW SRM 57-00-3, FIG 202, REPAIR 5.

Part: STRINGER — CRACKED (LT WING) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, LT WING STR 6 CRACKED BETWEEN BS XORS 1012-1042. REPAIRED LT STR 6, XORS 1012-1042 IAW EA 011-5700-01-A6157, REV IR AND EO MD11-5710-60437-A.

Part: LONGERON — CORRODED (BS 1441-1461) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, INTERRUPTED LONGERON 18L CRACKED AND CORRODED BETWEEN BS 1441 - 1461. REMOVED, FABRICATED AND INSTALLED REPLACEMENT LONGERON 16L, STA 1441-1461 IAW DWG AEA0220, SRM 51-33-01, 51-35-01, 51-21-01.

Part: SKIN — CORRODED (FUSELAGE) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, CENTER WING UPPER CENTER SKIN CORRODED BS XCW 101-118, S10 - S13. REPAIRED CENTER WING SKIN CORROSION IAW EA 011-5730-01-A6171, REV. IR AND EO MD11-5330-60302-A.

Part: LONGERON — CORRODED (BS 1321-1341) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE: 3C, MAIN CABIN LONGERON 25R AT BS 1321 TO 1341 HAS CORROSION. R & R LONGERON IAW SRM 51-33-01, PG 30.

Part: SKIN — CORRODED (FUSELAGE) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, CENTER WING UPPER SKIN HAS CORROSION ABOVE STR 4 BETWEEN XCW 101 AND 118 ACCOMPLISHED BLEND REPAIR ON CENTER WING UPPER SKIN ABOVE STR 4 BETWEEN XCW 101 AND 118 EA 011-5710-01-A6167, REV I/R AND EO MD11-5730-60289-A.

Part: LONGERON — CORRODED (BS 1441) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, LONGERON 25L CORRODED AT BS 1441. REMOVED CORROSION IAW SRM 51-21-01 AND 53-00-00, FIG 205.

Part: SKIN — CORRODED (BS 1236) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, CENTER WING UPPER SKIN HAS CORROSION AT BS 1236 BETWEEN XCW -101 AND XCW -118. ACCOMPLISHED BLEND REPAIR ON CENTER WING UPPER SKIN BS 1236 BETWEEN XCW -101 AND XCW -118 IAW EA 011-5710-A6168, REV I/R AND EO 5730-60291-A.

Part: SKIN — CORRODED (FUSELAGE) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, CENTER WING UPPER SKIN CORRODED BS XCW 114 S10-S11. REPAIRED NOTED CORROSION IAW EA 011-5730-01-A6171 REV IR AND EO MD11-5330-60302-A.

Part: LONGERON — CORRODED (BS 1401-1421) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, LONGERON 16L CORRODED BETWEEN BS 1401-1421. REMOVED CORROSION IAW SRM 51-21-01 AND 53-00-00, FIG 205.

Part: SKIN — CORRODED (BS 1229-1239) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C CENTER WING UPPER SKIN BS 1229 TO BS 1239 XCW -83 TO XCW -87 HAS CORROSION ACCOMPLISHED BLEND REPAIR ON CENTER WING UPPER SKIN BS 1229 TO BS 1239 BETWEEN XCW -83 AND XCW -87 IAW EA 011-5754-01-A6166, REV I/R AND EO MD11-5730-60292-A.

Part: LONGERON — CORRODED (BS 1341-1361) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, MAIN CABIN LONGERON 25R HAS CORROSION BS 1341 TO 1361. ACCOMPLISHED BLEND REPAIR ON MAIN CABIN LONGERON 25R, BS 1341 TO 1361 IAW SRM 53-00-00, FIG 205.

Part: LONGERON — CORRODED (BS 1381-1401) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE: 3C, MAIN CABIN LONGERON 16L HAS CORROSION BS 1381 TO 1401. REMOVED, FABRICATED AND REPLACED MIN CABIN LONGERON 16L, BS 1381 TO 1401 IAW SRM 51-33-01 AND DWG AEA0220.

Part: FINGER DOUBLER — CORRODED (BS 1376) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, CORRODED FINGER DOUBLER ON UPPER SURFACE OF CENTER WING IN MAIN CABIN SUBFLOOR, BS 1376, RBL 41. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FINGER DOUBLER IAW DWG ARB7241, SRM 51-33-01, 51-35-01, 51-21-01.

Part: SKIN — CORRODED (BS 1229-1239) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, SUB FLOOR CENTER WING BOX UPPER SKIN AT BS 1229-1239, RBL10 TO RBL 18 HAS SEVERAL AREAS OF HEAVY CORROSION. ACCOMPLISHED PERMANENT BLEND REPAIR TO UPPER FWD CENTER WING SKIN AT XCW -24 TO XCW 8 AT STR 15 IAW EA 011-5710-01-A6170, REV I/R AND EO MD11-5730-60305-A.

Part: FRAME — CORRODED (BS 1561) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, MAIN CABIN FRAME AT BS 1561 HAS CORROSION BETWEEN L1R AND L3R, ACCOMPLISHED BLEND REPAIR ON MAIN CABIN FRAME BS 1561 BETWEEN L1R AND L3R IAW SRM 53-00-00, FIG 205.

Part: FRAME — CORRODED (MAIN CABIN) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, MAIN CABIN FRAME AT BS 5-113 HAS CORROSION BETWEEN L3R AND L5R. ACCOMPLISHED BLEND REPAIR ON MAIN CABIN FRAME BS 5-113 BETWEEN L3R AND L5R SRM 53-00-00, FIGURE 205.

Part: SUPPORT STRAP — CORRODED (RT WING TE FLAP) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, RT WING INBD FLAP OTBD FAIRING SUPPORT STRAP CORRODED. R & R RT WING INBD FLAP, OTBD FAIRING SUPPORT STRAP AT BS XW 254 IAW SRM 51-35-01 AND DWG ARC2540.

Part: LONGERON — CRACKED (MAIN CABIN) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE: 3C, MAIN CABIN LONGERON 25R CRACKED AT BS 5-123 ACCOMPLISHED REPAIR ON MAIN CABIN LONGERON 25R FROM BS 5-123 TO 1541 IAW SRM 53-00-05, REPAIR 1, FIG 201/202.

Part: SKIN — CORRODED (BS 1971-2163) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:C3, RT SIDE EXTERIOR AFT FUSELAGE SKIN FROM BS 1971 TO BS 2163 HAS CORROSION IN SEVERAL PLACES. REPAIRED CORRODED RT SIDE AFT FUSELAGE SKIN BETWEEN BS 1971 TO BS 2163 IAW EA 011-5330-01-A6182, REV I/R AND EO MD11-5330-60284-A,

Part: FITTING — DAMAGED (MAIN CABIN) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:C3, RIGID CARGO BARRIER SIDE FITTING NR 6 HAS HEAVY WEAR, CHAFE DAMAGE. REPAIRED RIGID CARGO BARRIER SIDE FITTING NR 6 IAW VT-SAA, EA 011-5310-01-A6164, REV I/R AND EO MD11-5340-60397-A.

Part: FORMER — CRACKED (LT WING) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, CRACKED FORMER IN LT WING FIXED L/E AT BS XORS 455. REMOVED FABRICATED AND INSTALLED REPLACEMENT FORMER IAW DWG ARB 7762, SRM 51-35-01, 51-33-01.

Part: SEAT TRACK — CRACKED (BS 635) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, MAIN CABIN FLOOR SEAT TRACK CRACKED AT BS 635, LB L74. REPAIRED THE SEAT TRACK IAW SRM 53-00-52, REPAIR 1, FIG. 201.

Part: STANCHION — CORRODED · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, CENTER ACCESSORY COMPARTMENT, VERTICAL STANCHION HAS HEAVY CORROSION AT BS 6-79 ABOVE LONGERON 43L. REPAIRED CORRODED VERTICAL STANCHION AT BS 6-79 ABOVE LONGERON 43L IAW EA 011-5310-A6156-A AND EO MD11-5340-60270-A.

Part: TRACK — GOUGED (L1 DOOR) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, L1 DOOR CEILING BOGIE TRACK GOUGED. ACCOMPLISHED REPAIR ON L1 CEILING BOGIE TRACK IAW VT-SAA, EA 011-5320-01-A6184, REV I/R AND EO MD11-5210-60404-A.

Part: INTERCOSTAL — CRACKED (BS 1761) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, CENTER CARGO INTERCOSTAL CRACKED AT BS 1761 BETWEEN L43L AND L44L. R & R CENTER CARGO INTERCOSTAL AT BS 1761 BETWEEN L43L AND L44L IAW SRM 51-33-01 DWG ACA7049.

Part: FITTING — DAMAGED (MAIN CABIN) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:C3, RIGID CARGO BARRIER SIDE FITTING NR 1 HAS HEAVY WEAR/CHAFE DAMAGE. REPAIRED RIGID CARGO BARRIER SIDE FITTING NR 1 IAW EA 011-5310-01-A6172, REV I/R AND EO MD11-5340-60398-A.

Part: SKIN — CORRODED (BS 2153-2163) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:C3, LT SIDE EXTERIOR FUSELAGE SKIN HAS CORROSION BETWEEN BS 2153 TO 2163.685 AND BETWEEN LONG. 33L TO 35L. REPAIRED CORRODED LT SIDE EXTERIOR FUSELAGE SKIN BETWEEN BS 2153 TO 2163.685 AND BETWEEN LONG.33L TO 35L IAW MD 11-SRM 53-70-01, FIG 201, REPAIR 3 REV 61.

Part: INTERCOSTAL — CRACKED (BS 1531) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE: 3C, CENTER CARGO INTERCOSTAL CRACKED BS 1531 BETWEEN L43L AND L44L. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IN CENTER CARGO BS 1531 BETWEEN L43L AND L44L IAW SRM 51-33-01 AND DAC DWG A5A7085.

Part: CLEVIS — CRACKED (R3 DOOR FRAME) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, FUSELAGE R3 DOOR FWD FRAME STOP NR 5 CLEVIS CRACKED BS 1250-1256. REPAIRED DOOR JAMB CLEVIS IAW EA 011-5300-01-A6192 REV IR AND EO MD11-5310-60447-A.

Part: FITTING — DAMAGED (CARGO BARRIER) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:C3, RIGID CARGO BARRIER SIDE FITTING NR 13 HAS HEAVY WEAR, CHAFE DAMAGE. REPAIRED RIGID CARGO BARRIER SIDE FITTING NR 13 IAW VT-SAA, EA011-5310-01-A6164, REV I/R AND EO-5340-60397-A. (MINOR).

Part: FRAME — CORRODED (BS 1561) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, MAIN CABIN FRAME AT BS 1561 HAS CORROSION BETWEEN L2L AND L4L ACCOMPLISHED BLEND REPAIR ON MAIN CABIN FRAME BS 1561 BETWEEN L2L AND L4L IAW SRM 53-00-00, FIGURE 205.

Part: FITTING — DAMAGED (MAIN CABIN) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:C3, RIGID CARGO BARRIER SIDE FITTING NR 17 HAS HEAVY WEAR/CHAFE DAMAGE. REPAIRED RIGID CARGO BARRIER SIDE FITTING NR 17 IAW VT-SAA EA 011-5310-01-A6173 REV I/R AND EO MD11-5340-60356-A.

Part: LONGERON SPLICE — CRACKED (CENTER CARGO) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, CENTER CARGO LONGERON 39R SPLICE FITTING CRACKED BS 5-132. R & R CENTER CARGO LONGERON 39R SPLICE FITTING AT BS 5-132 IAW SRM 51-33-01 AND 51-31-01.

Part: LONGERON — CORRODED (BS 1601-1621) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:C3, CENTER CARGO COMPARTMENT, LONGERON 48R AT BS 1601 TO 1621 HAS EXFOLIATION CORROSION. REPAIRED CORRODED LONGERON 48R AT BS 1601 TO BS 1621 IAW EA011-5310-01-A6153 REV I/R AND EO MD11-5310-60453-A.

Part: RIB — CRACKED (RT WING) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, RT CRUISE PERFORMANCE FAIRING IS CRACKED ON WEB/RIB. REPAIRED RT CRUISE PERFORMANCE FAIRING WEB/RIB IAW EA 011-5754-01-A6178, REV I/R AND EO MD11-5750-60451-A.

Part: RIB — CORRODED (RUDDER) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, CORRODED RIB, AMC7292-33 INSIDE UPPER FWD RUDDER L/E AT BS ZFR450. REMOVED FABRICATED AND INSTALLED REPLACEMENT RIB IAW DWG AMC7292 AND SRM 51-35-01.

Part: RIB — CRACKED (LT WING) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:C3, LT CRUISE PERFORMANCE FAIRING OTBD WEB/RIB IS CRACKED. REPAIRED LT CRUISE PERFORMANCE FAIRING OTBD WEB/RIB IAW EA 011-5754-01-A6159 REV. I/R AND EO MD11-5750-60452-A.

Part: BEAM — CHAFED (R3 DOOR) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE: 3C, R3 DOOR HAS CHAFE DAMAGE ON NR 7 BEAM, AFT SIDE ACCOMPLISHED BLEND REPAIR ON R3 DOOR NR 7 BEAM AFT SIDE IAW EA 011-5200-01-A6165, REV I/R AND EO 5210-60286-A.

Part: STIFFENER — CRACKED (LT WING) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, INNER STIFFENER CRACKED AT LT WING L/E PANEL 516ET. REMOVED, FABRICATED AND INSTALLED REPLACEMENT STIFFENER IAW DWG ARB2440 AND SRM 51-35-01.

Part: CLOSEOUT PANEL — CRACKED · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, 13 CRACKS ALONG RCB WALL LOWER FWD CLOSE-OUT. REPAIRED RCB IAW EA 011-5310-01-A6142, REV IR AND EO MD11-5320-60382-A.

Part: BEAM — CHAFED (R3 DOOR) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, R3 DOOR HAS CHAFE DAMAGE ON BEAM NR 7 ACCOMPLISHED BLEND REPAIR ON R3 DOOR NR 7 BEAM IAW EA 011-5200-01-A6165, REV I/R AND EO 5210-60286-A.

Part: SKIN — CORRODED (LT WING) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, LT WING UPPER SKIN CORRODED ALONG T/E XORS1042. REPAIRED NOTED CORROSION BTEWEEN BS 1057-1067 IAW EA 011-5710-01-A6174, REV IR AND EO 5730-60295-A.

Part: SUPPORT FITTING — DAMAGED (L1 DOOR) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, L1 DOOR ESCAPE SLIDE AFT SUPPORT CHAFE DAMAGE. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SLIDE SUPPORT IAW DWG ABA 8513, SRM 51-33-01, 51-35-01.

Part: COUPLER — CHAFED · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, ELEVATOR LOAD FEEL MOMENT ARM CHANGER COUPLER ARM CHAFE DAMAGE. REPAIRED CHAFE DAMAGE TO NOTED ARM IAW EA 011-2730-01-A6181, REV IR AND EO MD11-2730-60303-A.

Part: STIFFENER — CRACKED (NR 2 NACELLE) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, 2 PYLON AFT FAIRING 457JR FWD. UPPER WEB IS CRACKED. REPAIRED CRACKED NR 2 PYLON AFT FAIRING WEB IAW EA 011-5450-01-A6183 -A AND EO MD11-5440-60412-A.

Part: FITTING — CRACKED (NR 1 SLAT) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE :3C, RT WING NR 1 SLAT INNER FITTING CRACKED AT BS XW151. R & R RT WING NR 1 SLAT INNER FITTING AT BS XW151 IAW SRM 51-35-01 AND 51-33-01.

Part: STRINGER — CRACKED (RT WING) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, RT WING L/E STRINGER CRACKED BETWEEN BS XOS 584.891 AND BS XOS 589.888. REPAIRED RT WING L/E STR BETWEEN BS XOS 584.891 AND 589.888 IAW EA 011-5754-01-A6152-IR AND EO MD11-5730-60355-A.

Part: FORMER — CRACKED (RT WING) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE: 3C, RT WING FIXED L/E FORMER CRACKED XOS 996. REMOVED FABRICATED AND INSTALLED REPLACEMENT FORMER IAW DWG ARB2920, SRM 57-00-00, 51-33-01, 51-35-01.

Part: DOUBLER — CRACKED (RT WING) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, RT WING FIXED L/E BEADED DOUBLER CRACKED BS XOS 783.23 TO 789.64. ACCOMPLISHED PERMANENT REPAIR ON RT WING FIXED LEADING BEADED DOUBLER BS XOS 783.23 TO 789.64 IAW SRM 57-40-02, FIG 203, REPAIR 15.

Part: RIB — CRACKED (NR 1 SLAT) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, LT NR 1 SLAT RIB WEB CRACKED AT BS XIS 151.2578. ACCOMPLISHED PERMANENT SPLICE REPAIR ON LT NR 1 SLAT WEB AT BS XIS 151-2578 IAW EA 011-5754-01-A6158, REV I/R AND EO MD11-5750-60269-A.

Part: FORMER — CRACKED (RT WING) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, RT WING FIXED L/E FORMER CRACKED XOS 996. REMOVED FABRICATED AND INSTALLED REPLACEMENT FORMER IAW DWG ARB 2920, SRM 57-00-00, 51-35-01, 51-33-01.

Part: DOUBLER — CRACKED (LT WING) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, LT WING L/E INTERNAL BEADED DOUBLER HAS SEVERAL CRACKS AT BS XOS 633 -XOS 636. REPAIRED CRACKED LT WING INTERNAL BEADED DOUBLER AT BS XOS 633-XOS 636 IAW EA011-5700-01-A6155, REV I/R AND EO MD11-5730-60378-A.

Part: SKIN — CHAFED (RT WING) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE: 3C, RT WING FIXED L/E LOWER SKIN REPAIR DOUBLER IS CHAFED. REPAIRED CHAFED RT WING LOWER L/E SKIN REPAIR DOUBLER IAW EA 011-5740-01-A6191, REV I/R AND EO MD11-5720-60453-A.

Part: SPAR CAP — CORRODED (RT WING) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE: 3C, RT WING REAR SPAR UPPER CAP HAS CORROSION BETWEEN XORS 482.15 - XORS 498.45 AND XORS 510.05 - XORS 515.35. ACCOMPLISHED BLEND REPAIR ON RT WING REAR SPAR UPPER CAP FROM BS XORS 482.15- XORS 498.45 AND XORS 510.05 - XORS 515.35 IAW EA 011-5710-01-A6147, REV I/R AND EO MD11-5710-60266-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, LT WING BEADED DOUBLER TEMP REPAIR XOS 653-658 REQUIRES REPLACEMENT. INSTALLED NEW TEMP REPAIR LT WING BEADED DOUBLER XOS 653- XOS 658 IAW SRM 57-40-02. REPAIR 15, FIG 206.

Part: SPAR CAP — CRACKED (RT WING) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:30, RT WING LOWER SPAR STRAP CAP, STRAP IS CRACKED AT BS XORS. 411.250, AND XORS.480.250. ACCOMPLISHED REPAIR ON RT WING LOWER SPAR CAP STRAP AT BS XORS 411.250 AND XORS 480.250 IAW EA 011-5700-01-A6143, REV I/R AND EO MD11-5720-60732-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED XOS 610-616. R & R BEADED DOUBLER REPAIR IAW SRM 57-40-02, REPAIR 15, FIG 206.

Part: DOUBLER — CRACKED (LT WING) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED XOS 616- XOS 621. R & R BEADED DOUBLER REPAIR IAW SRM 57-40-02, REPAIR 15, FIG 206.

Part: DOUBLER — CRACKED (RT WING) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED XOS 760 -XOS 768. R & R BEADED DOUBLER REPAIR IAW SRM 57-40-02, REPAIR 15, FIG 206.

Part: DOUBLER — CRACKED (RT WING) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED XOS 768-772. R & R BEADED DOUBLER REPAIR IAW SRM 57-40-02, REPAIR 15, FIG 206.

Part: DOUBLER — CRACKED (RT WING) · airframe 78,198 hrs · 13,965 cycles

INSPECTION TYPE:3C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED XOS 584-589. R & R BEADED DOUBLER REPAIR IAW SRM 57-40-02, REPAIR 15, FIG 206.

Part: STIFFENER — CORRODED (BS 1967) · airframe 78,114 hrs · 13,942 cycles

INSPECTION TYPE: 3C, CORRODED STIFFENER INSIDE AFT CARGO DOOR FRAME BS 1967. R & R STIFFENER IAW SRM 51-33-01.

Part: SKIN — CORRODED (FUSELAGE) · airframe 78,114 hrs · 13,942 cycles

INSPECTION TYPE:3C, CENTER WING UPPER SKIN CORRODED BETWEEN XCW 101- XCW 118 ABOVE STRINGER 4, REPAIRED NOTED CORROSION IAW EA 011-5710-01-A6167, REV IR AND EO 5730-60289-A.

Part: WARNING MESSAGE — FALSE ACTIVATION (EMERGENCY LIGHT) · airframe 77,073 hrs · 13,693 cycles

EMERGENCY LIGHT BATTERY 1 LOW. OPS CHECK C/O IAW AMM 33-51-01, REV 83.01. FOUND SATISFACTORY.

Part: INDICATOR — OBSTRUCTED (L1 DOOR SLIDE) · airframe 76,919 hrs · 13,654 cycles

L1 SLIDE PRESSURE NOT VISABLE. CLEARED VIEWING GLASS.

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 76,471 hrs · 13,542 cycles

RIGHT INBD FLAP HAS CRACKED CLOSURE RIB ON OTBD END. 6 INCH CRACK LOCATED IN THE RADIUS OF THE UPPER TEE CAP. REPAIR IAW EO MD11-5750-57645.

Part: NONE — NONE (NONE) · airframe 75,807 hrs · 13,404 cycles

LEVEL 1 EMERGENCY LIGHT BATTERY 1 OPERATIVE, FORMED OPERATION TEST IAW AMM 33-50-00. OPS CK GOOD.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

FLOOR PANEL DAMAGED. FABRICATED A NEW FLOOR PANEL IAW EO 5320-27386-C.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 75,121 hrs · 13,222 cycles

INSPECTION C01, CHAFING DAMAGE ON UPPER SKIN OF LT WING INBD FLAP VANE INBD, AFT SIDE. REPAIR DAMAGE AREA IAW RE SRM 57-50-80, REPAIR 2, PARA 2.A, REV.56

Part: LIGHT — DAMAGED (CABIN)

FOUND L1 DOOR EMERGENCY LIGHT COVER BROKEN. EMERGENCY LIGHT CHANGED IAW AMM 33-27-01-05, REV 79.01.

Part: SPRING — BROKEN (CEILING PANEL)

L1 ENTRY DOOR DROP CEILING PANEL HAS A BROKEN SPRING. NEW SPRING INSTALLED IAW AMM 25-23-23-4, REV 79.01.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

PDC INSPECTION, DURING PRE FLIGHT CHECK FOUND EMERGENCY LIGHT BATTERY LOW 1 MESSAGE. R & R POWER SUPPLY IAW MM 33-51-01-401, TESTED IAW MM 33-51-01-501, FOUND SATISFACTORY.

Part: STRINGER — CRACKED (LT WING) · airframe 72,847 hrs · 12,594 cycles

DURING 2C, LEFT WING CRACKED AT STRINGER 41 ACCESS THRU NR 1 TANK, 536AB ACCOMPLISHED PERMANENT REPAIR IAW EA 011-5710-01-A4861 REV I/R AND UPS EO MD11-5710-52032-A. FOR 8100-9 SIGNED BY B.V.TRAN DATED 09/04/2013

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 72,847 hrs · 12,594 cycles

2C INSPECTION, LEFT INBD FLAP VANE IS CHAFED INTO COMPOSITE MATERIAL ON UPPER INBD SIDE. ACCOMPLISHED PERMANENT REPAIR IAW SRM 57-50-80, REPAIR 2, PARA2 A (2) (A) (5) WET LAY UP.

Part: WEB — CRACKED (LT WING) · airframe 72,847 hrs · 12,594 cycles

DURING 2C, LT WING FUEL TANK WEB LIGHTNING HOLE OTBD DOUBLER CRACKED AT STA XORS 345, BETWEEN STRINGERA 44 AND 45. REPAIRED LT WING FUEL TANK LIGHTNING HOLE OTBD DOUBLER AT STA XORS 345 BETWEEN STGR. 44 AND 45 REF STASA EA 011-5710-01-A4882 REV I/R, UPS EO MD11-5710-52048-A AND 8100-9.

Part: STRINGER — CRACKED (LT WING) · airframe 72,847 hrs · 12,594 cycles

DURING 2C INSPECTION, LEFT WING STRINGER 16 CRACKED IN BAY BETWEEN XORS 372-402. REPAIREDSTRINGER IAW EA 011-5710-01-A4875, REV IR AND EO MD11-5710-52020-A, FAA 8100-9.

Part: STRINGER — CRACKED (LT WING) · airframe 72,847 hrs · 12,594 cycles

INSPECTION TYPE:2C, LT WING STRINGER 15 CRACKED WITH ACCESS THRU 1 TANK PANEL 533AT ACCOMPLISHED PERMANENT REPAIR IAW EA 011-5710-A4867 REV I/R AND EO MD11-5710-52030-A.

Part: STRINGER — CRACKED (LT WING) · airframe 72,847 hrs · 12,594 cycles

DURING 2C INSPECTION, LEFT WING, STRINGER 11 CRACKED IN BAY BETWEEN XORS 683 -713. REPAIRED STRINGER IAW SRM 57-00-03, REPAIR 5, FIG 202.

Part: DOUBLER — CRACKED (LT WING) · airframe 72,847 hrs · 12,594 cycles

INSPECTION TYPE:2C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 654. REPAIRED LT WING INNER BEADED DOUBLER BETWEEN XOS 653-658 IAW SRM 57-40-02, REPAIR 15, FIG 202.

Part: DOUBLER — CRACKED (LT WING) · airframe 72,847 hrs · 12,954 cycles

INSPECTION 2C, LEFT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 669. REPAIRED IAW SRM 57-40-02. REPAIR 15, FIG 203. (MAJOR)

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 72,847 hrs · 12,594 cycles

DURING 2C INSPECTION, RT INBD FLAP, INBD WEDGE, UPPER SKIN HAS TWO CREASES NEAR XIFH 192. REPAIRED RT INBD FLAP, INBD WEDGE UPPER SKIN IAW SRM 57-00-01, REPAIR 1, FIG. 201.

Part: DOUBLER — CRACKED (LT WING) · airframe 72,847 hrs · 12,594 cycles

INSPECTION 2C, LEFT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 620. REPAIRED IAW SRM 57-40-02, REPAIR 15, FIG 202. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 72,847 hrs · 12,594 cycles

INSPECTION 2C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 615. REPAIRED IAW SRM 57-40-02. REPAIR 15, FIG 202. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 72,847 hrs · 12,954 cycles

INSPECTION 2C, LEFT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 666. REPAIRED IAW SRM 57-40-02, REPAIR 15 FIG 203. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 72,847 hrs · 12,594 cycles

INSPECTION 2C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 700 REPAIRED IAW SRM 57-40-02, REPAIR 15, FIG. 203. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 72,847 hrs · 12,594 cycles

INSPECTION TYPE:2C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS760. REPAIRED RT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS 760 - 768 IAW SRM 57-40-02. REPAIR 15, FIG 206.

Part: DOUBLER — CRACKED (RT WING) · airframe 72,847 hrs · 12,594 cycles

INSPECTION TYPE: 2C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 768. REPAIRED RT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS 768-772 IAW SRM 57-40-02, REPAIR 15, FIG 206. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 72,847 hrs · 12,594 cycles

INSPECTION TYPE:2C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 587. REPAIRED IAW SRM 57-40-02. REPAIR 15, FIG. 202. (MAJOR)

Part: TRUNNION — CRACKED (NLG WW) · airframe 72,847 hrs · 12,594 cycles

2C INSPECTION, APPROX .70" CRACK AT LT TRUNNION FITTING AT BS 582, X=24 AND Z=-114. REPAIRED LT TRUNNION FITTING IAW SRM 53-10-14, REPAIR 2, FIG 202.

Part: SPAR CAP — CORRODED (LT WING) · airframe 70,476 hrs · 11,946 cycles

INSPECTION TYPE:3C, LT WING REAR SPAR UPPER CAP AFT FLANGE CORRODED BETWEEN XORS 744-785. REPAIRED LT WING REAR SPAR UPPER CAP AFT FLANGE BETWEEN XORS 744-785 IAW STA SA EA 011-5710-01-A4035 REV IR & EO MD11-5710-47737-A.

Part: SKIN — CHAFED (RT WING) · airframe 70,476 hrs · 11,946 cycles

INSPECTION TYPE: 4C, RT WING FIXED L/E ANTI-ICE CUT OUT REPAIR DOUBLER CHAFED AT OTBD EDGE AND BENT AT INBD CORNER. REPAIRED RT WING FIXED L/E ANTI-ICE DUCT CUT OUT AT XOS464-XOS470, REF STASA, EA 011-5730-01-A4037 I/R, EO MD115730-47775-A AND 8100-9.

Part: SKIN — DAMAGED (LT WING) · airframe 70,476 hrs · 11,946 cycles

INSPECTION TYPE:3C, LT WING FIXED L/E OVER NR 1 PYLON HAS EDGE DAMAGE 3 PLACES. REPAIRED LT WING FIXED L/E EXTERIOR SKIN AT XDLE330 IAW STA SA EA 011- 5730-01-A4040 REV IR AND EO MD11-5730-47739-A.

Part: DOUBLER — CRACKED (RT WING) · airframe 70,476 hrs · 11,946 cycles

INSPECTION TYPE:3C, RT WING FIXED L/E COMPT BEADED DOUBLER CRACKED AT APPROX STA XOS620. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS625-629 IAW SRM 57-40-02, REPAIR 9, FIG 203 & EO MD11-5730-42916-D.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 70,476 hrs · 11,946 cycles

INSPECTION TYPE:3C, LT INBD FLAP UPPER SKIN DENTED 60" FROM T/E 85" FROM INBD END. (XIFH 202) REPAIRED LT INBD FLAP UPPER SKIN IAW SRM 57-00-01, REPAIR 1, FIG 201.

Part: DOUBLER — CRACKED (LT WING) · airframe 70,476 hrs · 11,946 cycles

INSPECTION TYPE: 3C, CRACKED BEADED DOUBLER IN LT WING L/E AT STA 795 (XOS901-906) REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS901-906 IAW SRM 57-40-02, REPAIR 9 FIG 203 & EO MD11-5730-42916-D.

Part: DOUBLER — CRACKED (LT WING) · airframe 70,476 hrs · 11,946 cycles

INSPECTION TYPE:3C, CRACKED BEADED DOUBLER IN LT WING L/E AT STA 787.5 (XOS891-896) REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS891-896 IAW SRM 57-40-02, REPAIR 9, FIG 203 & EO MD11-5730-42916-D.

Part: SKIN — CHAFED (LT WING) · airframe 70,476 hrs · 11,946 cycles

INSPECTION TYPE:3C, LT WING FIXED L/E EXTERIOR SKIN CHAFED BY CONTACT WITH NR 8 SLAT BETWEEN STA XOS1185 & XORS 1093 CANTED. REPAIRED LT WING FIXED L/E EXTERIOR SKIN BETWEEN STA XOS1185 & XORS 1093 CANTED IAW STA SA EA 011-5730-01-A4024, REV IR & EO MD11-5730- 47778-A, FAA 8100-9.

Part: DOUBLER — CRACKED (LT IWNG) · airframe 70,476 hrs · 11,946 cycles

INSPECTION TYPE: 3C, CRACKED BEADED DOUBLER IN LT WING L/E AT SAT.774 (XOS879-883) REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS879-883 IAW SRM 57-40-02 REPAIR 9, FIG.203 & EO MD11-5730-42916-D.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHT BATTERY 1 LOW. R & R EMERGENCY LIGHT BATTERY IAW MM 33-51-01-4.

Part: CHARGER — MALFUNCTIONED

LEVEL ONE BATTERY DISCHARGING ALERT. DIVERSION PERFORMED FIM 24-30-00-810-803, FIG 104, SHT 1. EPCS SHOWS NO FAULTS. RETURN TO SERVICE IAW MM 24-30-02-5. NO FAULTS NOTED. OK FOR SERVICE

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 67,950 hrs · 11,304 cycles

INSPECTION TYPE:4C, MAIN CABIN FLOORBOARD 263BF IS DAMAGED (OFF ACFT INSP FINDING). FABRICATED AND INSTALLED REPLACEMENT FLOORBOARD 263BF REF MD11-5320-27386- C.

Part: LONGERON SPLICE — CRACKED (STA.1625 L14R) · airframe 67,950 hrs · 11,304 cycles

INSPECTION TYPE:4C, CRACK IN LONERON SPLICE IN UPPER MAIN CARGO STA.1625 L14R REMOVED, FABRICATED, & INSTALLED REPLACEMENT SPLICE FITTING EO MD11-5310-42361-A AND STA EA 011-5340-01-A3038, REV. IR

Part: STRINGER — CRACKED (RT WING) · airframe 67,950 hrs · 11,304 cycles

INSPECTION TYPE:4C, RT WING NR 3 TANK UPPER STRINGER CRACKED THROUGH ACCESS 636AB, 2ND STRINGER FROM FWD SPAR. REMOVED DAMAGE, AND REPAIRED IAW SRM 57-00-03, REPAIR 5, FIG 201.

Part: DOOR FRAME — CRACKED (FS 1256) · airframe 67,950 hrs · 11,304 cycles

INSPECTION TYPE:4C, R3 DOOR JAMB FWD WEB IS CRACKED AT LOWER LIGHTENING HOLE. FABRICATED & INSTALLED REPAIR SRM 53-40-15, REPAIR 3, FIG.201.

Part: LONGERON — CORRODED (BS 1521) · airframe 67,950 hrs · 11,304 cycles

INSPECTION TYPE:4C, CTR CARGO COMPT LT LONGERON 43 AT SPLICE AREA UNDER SURFACE CORRODED BET STA 1521 AND 1541. REMOVED DAMAGE, AND REPAIRED IAW STA-SA EA 011-5310-01-A2995 I/R AND EO MD11-5310-2343-A.

Part: STRINGER — CRACKED (LT WING) · airframe 67,950 hrs · 11,304 cycles

INSPECTION TYPE:4C, LT WING L/E STRINGER AND REPAIR DOUBLER ARE CRACKED AT INBD END OF PANEL 526FB UNDER HINGE. REMOVED DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-40-03, REPAIR 1, FIG 201.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 67,950 hrs · 11,304 cycles

INSPECTION TYPE:4C, RT WING INBD FLAP LOWER SKIN DENTED BETWEEN STA XIFH 133.9 & 140.6. FABRICATED & INSTALLED REPLACEMENT SKIN SECTION REF SRM 57-50-01, REPAIR 1 FIG 201.

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 67,950 hrs · 11,304 cycles

INSPECTION TYPE:4C, RT WING L/E BEADED DOUBLER IS CRACKED AT XOS 644-648. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SRM 57-40-02 REPAIR 9, FIG. 203.

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 67,950 hrs · 11,304 cycles

INSPECTION TYPE:4C, RT WING L/E BEADED DOUBLER HAS 3 CRACKS AT XOS 651-656. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SRM 57-40-02 REPAIR 9, FIG. 203.

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 67,950 hrs · 11,304 cycles

INSPECTION TYPE:4C, RT WING FIXED L/E COMPARTMENT OTBD OF SLAT TRACK NR 11, BEADED DOUBLER FOUND CRACKED AT XOS 748-734. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW MD-11-57-40-02 REPAIR 9, FIG. 203.

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 67,950 hrs · 11,304 cycles

INSPECTION TYPE:4C, RT WING L/E BEADED DOUBLER IS CRACKED AT XOS 637-643 REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.

Part: SKIN — CRACKED (RT WING L/E) · airframe 67,950 hrs · 11,304 cycles

INSPECTION TYPE:4C, RT WING L/E SKIN CRACKED AT NR 14 TRACK CUTOUT. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SRM 57-40-02. REPAIR 7, FIG. 201.

Part: SKIN — CRACKED (RT WING L/E) · airframe 67,950 hrs · 11,304 cycles

INSPECTION TYPE:4C, RT WING L/E SKIN CRACKED AT NR 12 TRACK CUT OUT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 7, FIG. 201.

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 67,950 hrs · 11,304 cycles

INSPECTION TYPE:4C, RT WING L/E BEADED DOUBLER IS CRACKED AT XOS 611-616. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02 REPAIR 9, FIG 203.

Part: SKIN — CHAFED (LWS 464-470) · airframe 67,950 hrs · 11,304 cycles

INSPECTION TYPE:4C, LT WING TELESCOPIC DUCT CUT-OUT REPAIR DOUBLER IS CHAFED REMOVED DAMAGED REPAIR DOUBLER. FABRICATED AND INSTALLED NEW REPAIR IAW SRM. 57-40-01, REPAIR 10, FIG 201.

Part: DOUBLER — CRACKED (LT WING L/E) · airframe 67,950 hrs · 11,304 cycles

INSPECTION TYPE:4C, LT WING L/E COMPARTMENT, ACCESS THRU OTBD OF PANEL 518FB, CEILING AREA BEADED DOUBLER CRACKED AT XOS 542-546. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG. 203.

Part: DOUBLER — CRACKED (LT WING L/E) · airframe 67,950 hrs · 11,304 cycles

INSPECTION TYPE:4C, LT WING L/E COMPARTMENT, OTBD OF ACCESS 519CB, CEILING AREA, BEADED DOUBLER FOUND WITH CRACKS. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW 57-40-02 REPAIR 9, FIG. 203.

Part: DOUBLER — CRACKED (LT WING L/E) · airframe 67,950 hrs · 11,304 cycles

INSPECTION TYPE:4C, LT WING L/E COMPARTMENT THRU ACCESS 519CB OTBD FUEL RECEPTACLE OTBD SIDE CEILING AREA, BEADED DOUBLER FOUND WITH CRACKS. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SRM 57-40-02 REPAIR 9, FIG. 203.

Part: DOUBLER — CRACKED (LT WING L/E) · airframe 67,950 hrs · 11,304 cycles

INSPECTION TYPE:4C, LT WING L/E COMPARTMENT THRU ACCESS 519CB, INBD FUEL RECEPTACLE OTBD SIDE, CEILING AREA, BEADED DOUBLER FOUND WITH CRACKS. XOS 625- 633.5. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG. 203.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS)

"EMERGENCY LIGHT BATTERY 1 LOW" MESSAGE DURING EMERGENCY LIGHT TEST. T/S IAW FIM 33-51-00-1, REV NR 67, NOV 01/2010. EMERGENCY LIGHT TEST PASSED. SUSPECT BATTERY WAS NOT FULLY LOADED. PLACARD REMOVED. THIS CLOSES DMI.

Part: WIRE — FAILED (RT MLG)

ON CONFIG SYNOPTIC-RT FWD INNER TIRE PRESSURE DATA TIRE SYMBOL MISSING. BRAKE TEMP NORMAL. RT FWD OUTER TIRE BRAKE TEMP SYMBOL MISSING ALONG WITH BRAKE PAD SYMBOL. TIRE PRESSURE NORMAL. EMERGENCY DECLARED, FOUND RT MLG ELECTRIC CONDUIT/WIRING DAMAGED AT FWD END OF TRUCK, BETWEEN NR3 AND NR4 MAIN WHEEL ASSYS. R & R WIRE/CONDUIT ASSY IAW CMM 32-10-02. PERFORMED CAT 3 RTS OF ASCU & BTM/TPI SYS. ALL TESTS PASSED. ALL WIRE TERMINATIONS IAW WDM 32-45-02 AND 32-46-02.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS)

EMER LIGHT SYS TEST INOP. R & R EMER POWER SUPPLY BATTERY IAW MM 33-51-01-5. OPS CKS GOOD IAW MM 33-51-01-5.

Part: SKIN — MISREPAIRED (RT WING AILERON) · airframe 65,421 hrs · 10,704 cycles

INSPECTION TYPE:1C, REPAIR SURVEY SEQ NR 282-W4-08 RT WING IB AILERON LOWER SKIN APPROX BETWEEN STA XIA375-359 PREVIOUS REPAIR FASTENERS NOT IAW SRM 57-10-00, FIG 1, VOL 1. INSTALLED NAS1097AD4 IN LIEU OF NAS1097AD5. REMOVED INCOMING SKIN PANEL, FABRICATED AND INSTALLED REPLACEMENT SKIN PANEL REF SRM 57-60-01, REPAIR 1, REV 42.

Part: SKIN PANEL — ACTIVATED (BS 1750 L41R) · airframe 65,421 hrs · 10,704 cycles

INSPECTION TYPE:1C, REPAIR SURVEY SEQ NR 282-F1-02 BETWEEN STA 1746-1761 L40R-L42R APPROX REPAIR IS NOT IAW SRM 53-50-00 REV39 VOL 1 FIG 17 WRONG DOUBLER THICKNESS, WRONG PITCH, WRONG E.D. REMOVED EXISTING REPAIR, ENLARGED DAMAGE CUT-OUT, FABRICATED AND INSTALLED REPAIR REF STASA EA 011-5330-01-A2175 AND EO MD11-5330- -36745-A.

Part: SKIN — MISREPAIRED (BS 816 L42L) · airframe 65,421 hrs · 10,704 cycles

INSP TYPE:1C, REPAIR SURVEY SEQ NR 282-F1-07 BETWEEN STA 808-824 L41L-L42L REPAIR HAS WRONG PITCH AND IS LOCATED ON RVSM AREA IAW 53-01-00 FIG 201. REMOVED INCOMING REPAIR, CUT OUT DAMAGE, FABRICATED AND INSTALLED NEW REPAIR REF STASA EA 011-5330-01-A2169 AND EO MD11-5330-36756-A.

Part: SKIN — MISREPAIRED (BS 799 L16R) · airframe 65,421 hrs · 10,704 cycles

INSP TYPE:C1, REPAIR SURVEY SEQ NR282-F1-08 (R2 DOOR PLUG) BETWEEN STA 808-791 L16R AND BEAM NR7 REPAIR DOUBLER HAS WRONG PITCH IAW SRM 52-10-01 REPAIR 3 FIG 201 REV42. REMOVED OLD REPAIR, CORRECTED OLD DAMAGE CUT-OUT, FABRICATED AND INSTALLED NEW REPAIR SRM 52-10-01 REPAIR NR 3.

Part: SKIN — MISREPAIRED (BS 832 L42L) · airframe 65,421 hrs · 10,704 cycles

INSPECTION TYPE:1C, REPAIR SURVEY SEQ NR 282-F1-06 BETWEEN STA 824-840 L41L-L43L. REPAIR NOT CORRELATED WITH SRM 53-00-01 REP.8, FIG 201, SHEET 6 WRONG DOUBLER MATERIAL, WRONG THICKNESS, WRONG PITCH, AND IS LOCATED IN RVSM AREA IAW SRM 53-01-00. GAINED ACCESS TO REPAIR AREA, REMOVED EXISTING REPAIR, FABRICATED & INSTALLED NEW REPAIR REF STASA EA 011-5330-01-A2179 AND EO MD11- 5330-36748-A. RESTORED AREA.

Part: STRINGER — CRACKED (RT WING) · airframe 65,421 hrs · 10,704 cycles

INSPECTION TYPE:1C, RT WING FIXED L/E COMP'T SPLICE STRAP SUPPORT STRINGER CRACKED AT STA XOS666, TRIMMED DAMAGE FROM HORIZ FLANGE AND REWORKED VERTICAL FLANGE EDGE OF NOTED STRINGER. FABRICATED AND INSTALLED SECTION REPAIR STRAP REF STA EA 011-5720-01-A2170 AND EO MD11-5720-36672-A.

Part: SUPPORT — CRACKED (RT WING) · airframe 65,421 hrs · 10,704 cycles

INSP TYPE:1C, RT WING FIXED L/E COMP'T SPLICE STRAP SUPPORT CRACKED AT STA XOS789 CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR STRAP AND FILLER REF STASA EA 011-5720-01-A2178 AND EO MD11-5720-36726-A

Part: STRINGER — CRACKED (LT WING) · airframe 65,421 hrs · 10,704 cycles

INSPECTION TYPE:1C, LT WING FIXED L/E COMP'T SPLICE STRAP STIFFENER CRACKED AT STA XOS 666. TRIMMED AND REWORKED STIFFENER FLANGES, FABRICATED AND INSTALLED REPLACEMENT SECTION REPAIR STRAP AND FILLER REF STA SA EA 011-5720-01- A2171 AND EO MD11-5720-36671.

Part: SKIN — GOUGED (LT WING) · airframe 65,421 hrs · 10,704 cycles

INSPECTION TYPE:1C, LT WING FIXED L/E APPROX BETWEEN STA XOS 1185-1191 WELD REPAIR GOUGE. GAINED ACCESS, DETERMINED THAT NOTED DAMAGE WAS ADJACENT TO INCOMING WELD REPAIR. REPAIRED NOTED DAMAGE BY WELDING REF STA SA EA 011-5740- 01-A2191 AND EO MD11-5730-36722-A. RESTORED AREA.

Part: SKIN — GOUGED (LT WING) · airframe 65,421 hrs · 10,704 cycles

INSP TYPE:C1, REPAIR SURVEY SEQ NR 282-W3-03 LT WING BETWEEN STA XIS210-229 FIXED L/E PREVIOUS REPAIR DOUBLE GOUGED. REMOVED OLD REPAIR, FABRICATED AND INSTALLED REPAIR IAW EA 011- 5730-01-A2172 & EO 5730-36689-A.

Part: SKIN — GOUGED (RT WING) · airframe 65,421 hrs · 10,704 cycles

INSP TYPE:C1, REPAIR SURVEY SEQ NR 282-W4-01 RT WING FIXED L/E APPROX BETWEEN STA XIS 154-168, PREVIOUS DOUBLER GOUGED. REMOVED OLD REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER REF STASA EA NR 011-5730-01-A2174, REV IR & EO MD11-5730-36706-A.

Part: SKIN — GOUGED (NR 1 SLAT) · airframe 65,421 hrs · 10,704 cycles

INSP TYPE:C1, REPAIR SURVEY SEQ NR 282-W3-01 LT WING NR1 SLAT APPROX BETWEEN STA XIS 173-196 FLUSH REPAIR FILLER GOUGED. REMOVED EXISTING REPAIR, CORRECTED OLD DAMAGE CUT-OUT, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-01, REPAIR 11, FIG 201.

Part: SKIN — GOUGED (RT WING) · airframe 65,421 hrs · 10,704 cycles

INSP TYPE:C1, REPAIR SURVEY SEQ NR 282-W4-02 RT WING FIXED L/E UPPER SKIN, APPROX BETWEEN STA XIS 240-253 PREVIOUS REPAIR DOUBLER IS GOUGED. REMOVED OLD REPAIR DOUBLER, ENLARGED DAMAGE CUT-OUT, FABRICATED AND INSTALLED DOUBLER AND FILLER REF SRM 57-40-02 FIG 201 REPAIR 8.

Part: SKIN — CRACKED (LT WING) · airframe 65,421 hrs · 10,704 cycles

INSP TYPE:1C LT WING TELESCOPIC DUCT SPRING DOOR CUT-OUT CRACKED AT BOTH UPPER CORNERS. GAINED ACCESS TO AREA, CUT-OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER AND FILLERS REF SRM 57-40-01, REPAIR 10, FIG 201, RESTORED AREA.

Part: UNKNOWN — FUMES (COCKPIT)

FUMES IN COCKPIT. INSPECTED INTERIOR LIGHTING, WINDOW HEAT OPERATION, RAN ALL 3 PACKS, RAN ENGINES, CHECKED CIRCUIT BREAKERS, NO FAULTS FOUND.

Part: POWER SUPPLY — DEFECTIVE (CABIN)

INSPECTION TYPE:N/A "EMER LT BAT 1 LO" ALERT DISPLAYED. REMOVED AND REPLACED EMER LT BATT PWR SUPPLY IAW 33-51-01-4. OPS CHECKS GOOD. OK FOR CONTINUED SERVICE.

Part: WEDGE — CRACKED (TE FLAP)

INSPECTION TYPE:N/A RIGHT I/B AFT FLAP T/E SPLIT FROM IN TO 15 INCHES O/B. REPAIRED PER EO MD11-5750-34526-A.

Part: FLOORBOARD — DELAMINATED (AFT CARGO BAY)

FLOOR BOARD DELAM. FABRICATED AND REPLACED FLOOR BOARD IAW EO MD11-5320-27386-A.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 62,845 hrs · 10,011 cycles

INSPECTION TYPE:2C RCB FLOOR PANEL 8 HAS CORROSION ON UPPER SURFACE. PROCURED NEW FLOOR PANEL.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 62,845 hrs · 10,011 cycles

INSPECTION TYPE:2C RCB FLOOR PNL 10 HAS CORROSION ON UPPER SURFACE. PROCURED AND DRILLED NEW FLOOR PANEL IAW MD-11 SRM 51-31-01.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 62,845 hrs · 10,011 cycles

INSPECTION TYPE:2C RCB FLOOR PANEL 4 HAS CORROSION ON UPPER SURFACE. PROCURED AND DRILLED NEW FLOOR PANEL IAW MD-11 SRM 51-31-01.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 62,845 hrs · 10,011 cycles

INSPECTION TYPE:2C RCB FLOOR PANEL 7 HAS CORROSION ON UPPER SURFACE. PROCURED NEW FLOOR PANEL.

Part: STRAP — CRACKED (LT WING) · airframe 62,845 hrs · 10,011 cycles

INSPECTION TYPE:2C LT WING SPLICE STRAP AT L/E WING STA 683 IS CRACKED. REMOVED, FABRICATED, AND INSTALLED SPLICE STRAP IAW DWG ARB3954 MD-11 SRM 51-35-01, 51-31-01, 51-33-01.

Part: STRAP — CRACKED (LT WING) · airframe 62,845 hrs · 10,011 cycles

INSPECTION TYPE:2C LT WING SPLICE STRAP AT LEADING EDGE WING STA 562 IS CRACKED WHERE MARKED. REMOVED AND REPLACED SPLICE STRAP IAW SRM 51-31-1, 51-21-1, 51-33-1.

Part: STRAP — WORN (GIRT BAR)

L1 GIRT BAR STRAP WORN. SLIDE INOP. SLIDE DEFERRED PER MEL 52-10-3-2, M375594 ASSIGNED. INSTALLED L1 SLIDE ASSY PER 25-61-01-4 AND 25-61-15-4.

Part: SLIDE — INOPERATIVE (R1 DOOR)

R1 DOOR SLIDE INOP M361751 ISSUED. REMOVED AND REPLACED RT DOOR SLIDE ASSY IAW MD11 MM 25-61-01-4. OPS CHECK OK. THIS CLEARS M361751.

Part: SKIN — GOUGED (FUSELAGE) · airframe 59,014 hrs · 4,344 cycles

INSPECTION TYPE:C FUSELAGE SKIN CENTER CARGO DOOR AFT JAMB GOUGE REPAIR. REF DMI# D350923. CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR DOUBLER, TRIPLER, AND FILLER IAW MD-11 SRM 53-50-00 FIG 17. REPAIRED ON NRC 082034.

Part: SKIN — DAMAGED (BS 1850-1941) · airframe 57,007 hrs · 9,015 cycles

INSPECTION TYPE:SP D337809: FUSELAGE SKIN DAMAGE TO THE AFT LOWER FUSELAGE SKIN STA 1850 THRU STA 1941 BETWEEN LONGERONS 51L AND 51R. COMPLY WITH WAN 1176489. CUT OUT DAMAGED AREAS OF FUSELAGE SKIN FROM STA 1850 THRU STA 1941 BETWEEN L51L AND L51R. FABRICATED REPAIR PARTS AND INSTALLED IAW MD-11 SRM 53-20-00 FIG 2, CLASS 1 AND BOEING MESSAGE 1-2499221532-2.

Part: SKIN — DAMAGED (BS 1850-1941)

AIRCRAFT SUSTAINED SKIN DAMAGE TO THE AFT LOWER FUSELAGE BS 1850-1941 BETWEEN LONGERONS 51L - 51R FROM TAIL STRIKE. A/C WAS FERRIED TO SAA 9015. TRANSFERRED TO NRC 876642. ACCOMPLISHED INTERIM REPAIR IAW EO MD11-5330-25590. ITEM DEFERRED D 337809 ISSUED.

Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHT)

WITH EMERG LT SW IN ARM POS, EMERG LTS CAME ON IN SUPERNUMERARY AREA. EMERG LIGHTING SYS PLACARDED PER MEL 33-50-4. UPDATED DI LOG AND ISSUED M333406. PLACARD INSTALLED. T/S C/O R/R SWITCH S1-346 NO HELP. CHECKED WIRING IAW WDM 33-51-01 FOUND WIRE BROKEN OF ON P1-1756A PIN 5. USED SPARE PIN ON CONNECTOR TO REPAIR AND CONNECT WIRE. ORIGINAL SWITCH INSTALLED. OPS TEST SATISFACTORY. THIS CLOSES DMI.

Part: A/C PACK — ODOR

REPEAT WRITE UP. REF LP 640979. DURING INITIAL CLIMB TO CRUISE ALTITUDE HEARD AND FELT RUMBLING TYPICALLY ASSOCIATED WITH A PACK, LASTING ONLY A FEW SECONDS. APPROXIMATELY 3 HOURS INTO FLIGHT SMELLED UNUSUAL ODOR. NR 1 PACK DEFERRED IAW MEL 21-51-1-0-1. DMP CARRIED OUT. FOUND FAIRING BROKEN IN INLET DOOR. REMOVED INLET DOOR & BROKEN FAIRING PER MM 21-55-01-4. INSTALLED NEW FAIRING & EXISTING INLET DOOR REF MM 21-55-01. OPS CK GOOD.

Part: A/C PACK — ODOR

SMOKE FUMES OF ELECTRICAL, AIR COND OR UNKNOWN ORIGIN. CHECK LIST PERFORMED FOR FAINT SMELL FROM A/C. CLEARED AFTER PACK 1 SECURED, LOUD HAMMERING NOISE FROM A/C SPACES UNDER COCKPIT. REMOVED AND CLEANED PACK NR 1, 2, 3 COALESCER BAGS PER MD11 AMM 21-54-05-2. RE-INSTALLED PER SAME. OPERATED ALL 3 PACKS INDIVIDUALLY AND SIMULTANEOUSLY. OPS CHECK OK PER MD11 AMM 21-53-20-5. NO DEFECTS NOTED. A/C OK FOR SERVICE.

Part: A/C PACK — ODOR (NR 1)

INSPECTION TYPE:N/A NR 1 PACK RUMBLES AND HAS BAD ODOR SMELL. TURNED OFF PACK NR 1 AND ODOR RUMBLE CLEARED. PERFORMED RTS ON NR 1 ACC WITH ALL PASS. NO RUMBLE NOTICED. RAN PACK NR 1 ON GROUND FOR 45 MINUTES WITH NO ODOR/SMELL NOTICED BY BOTH MECHANICS. A/C IS OK FOR SERVICE.

Part: PLACARD — MISSING (BATTERY PACK)

INSPECTION TYPE:PS3 EMERGENCY LIGHT SYS BATTERY PACK HAS NO DUE DATE STICKER OR OTHER EVIDENCE OF LAST RESTORATION. REMOVED AND REPLACED EMERGENCY LIGHTS RECHARGEABLE BATTERY POWER SUPPLY IAW MM 33-51-01-4. ADJ/TEST CHECK GOOD IAW AMM 33-51-01-5.

Part: STRUCTURE — CORRODED (EMPENNAGE) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE 22 LEFT FOUND BEARING WITH SURFACE CORROSION ON SIDE & BOTTOM AREA. CORROSION REMOVAL C/OUT & FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. BARREL NUT HOLE NR 22 LT BORE REWORKED PER EN1032-06. FAB SLEEVE BUSHING PER EO MD11-5510-19409-K, FIG-5. APPLIED SEALANT PR1422B1/2 BLEND OUT AREA & S/ BUSHING PER EO MD11-5510-19409-K. REPAIR ACCOMPLISHED AT BARREL NUT HOLE 22 LEFT PER EO MD11-5510-19409-K & EN1032-06, FOUND SATIS.

Part: STRUCTURE — CORRODED (EMPENNAGE) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE 19 LEFT FOUND BEARING WITH SURFACE CORROSION ON SIDE & BOTTOM AREA. CORROSION REMOVAL C/OUT & FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. BARREL NUT HOLE 19 LEFT BORE & BOTTOM REWORKED PER EN1033-06. FAB SLEEVE BUSHING PER EO MD11-5510-19409-K, FIG-5. APPLIED SEALANT PR1422B1/2 BLEND OUT AREA & S/BUSHING PER EO MD11-5510-19409-K. REPAIR ACCOMPLISHED AT BARREL NUT HOLE 19 LEFT PER EO MD11-5510-19409-K & EN1033-06, FOUND SATIS.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C EMPENNAGE-BARREL NUT HOLE NR 34 LT FOUND BEARING WITH SURFACE CORROSION ON THE SIDE AND BOTTOM AREA. CORROSION REMOVAL C/OUT AFFECTED AREA PER SRM51-21-01.V2.R38, FOUND BLEND OUT EXCEEDED LIMIT PER MD11-5510-19409-K, REPAIR SLEEVE BUSHING FAB PER MD11-5510-19409-K, APPLIED SEALANT PR1422B 1/2 ON SLEEVE BUSHING AND BORE AREA. INSTALLED REPAIR SLEEVE BUSHING ON B/N HOLE NR 34LH BORE. REPAIR ACCOMPLISHED AT B/N HOLE NR 34LH PER EN 1040-06 AND 1029-06, FOUND SATIS.

Part: STRUCTURE — CORRODED (EMPENNAGE) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE 16 LEFT FOUND BEARING WITH SURFACE CORROSION ON SIDE & BOTTOM AREA. CORROSION REMOVAL C/OUT & FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. BARREL NUT HOLE 16 LEFT BORE & BOTTOM REWORKED PER EN1022-06. FAB SLEEVE BUSHING PER EO MD11-5510-19409-K, FIG-5. APPLIED SEALANT PR1422B1/2 BLEND OUT AREA & S/BUSHING PER MD11-5510-19409-K. REPAIR ACCOMPLISHED AT BARREL NUT HOLE 16 LEFT PER EO MD11-5510-19409-K & EN1022-06, FOUND SATIS.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 55,014 hrs · 8,680 cycles

EMPENNAGE-BARREL NUT HOLE NR 31 LT FOUND BEARING WITH SURFACE CORROSION ON SIDE AND BOTTOM AREA. CORROSION REMOVAL C/OUT ON B/N HOLE NR 31 LT FOUND EXCEEDED LIMIT PER SRM 51-21-01V2R.38. REPAIR BUSHING FAB PER MD11-5510-19409-K FIG 5. PR 1422 B 1/2 SEALANT APPLIED AND REPAIR BUSHING INSTALLED IAW MD11-5510-19409-K. REPAIR CARRIED OUT AT BARREL NUT BORE IS ACCEPTABLE IAW EN1040-06, FOUND SATIS.

Part: SKIN — CHAFED (LT WING) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C LHW UPP SURFACE FIXED L/E AREA AT STA XRO 1192 APP (ON TOP LT NR 8 SLAT O/B EDGE AREA) FOUND CHAFF MARK. CHAFF MARK PER A/M DISCREPANCY BLENDED AND PROTECTED PER SRM 51-21-01.V2. R38.ORI THK 0.065,MAT REMOVED 0.031" FOUND EXCEEDED LIMIT. DAMAGED AREA TRIMMED DIA 1 1/2 BY 4 PER EN1042-06. HFEC INSP C/OUT, FOUND SATIS. NO CRACK EVIDENT. REPAIR SKIN FAB AND MAT USE 6061-0-0.063" BARE PER EN1042-06 REPAIR, WELDING AND GRINDING PER EN1042-06, FOUND JOB ACCOMPLISHED, SATIS.

Part: STRUCTURE — CORRODED (EMPENNAGE) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE 26 LEFT FOUND BEARING WITH SURFACE CORROSION ON SIDE & BOTTOM AREA. CORROSION REMOVAL C/OUT & FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. BARREL NUT BORE & BOTTOM REWORKED PER EN1031-06. FAB SLEEVE BUSHING PER EO MD 11-5510-19409-KF.F.5. APPLIED SEALANT PR1422B1/2 BLEND OUT AREA & S/BUSHING PER EO MD11-5510-19409-K. REPAIR ACCOMPLISHED AT BARREL NUT HOLE 26 LT PER EO MD11-5510-19409-K & EN1031-06, FOUND SATIS.

Part: STRUCTURE — CORRODED (EMPENNAGE) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE 20 LEFT FOUND BEARING WITH SURFACE CORROSION ON SIDE & BOTTOM AREA. CORROSION REMOVAL C/OUT & FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. BARREL NUT HOLE 20 LEFT BORE & BOTTOM REWORKED PER EN1024-06. FAB SLEEVE BUSHING PER EO MD11-5510-19409-K,FIG-5. APPLIED SEALANT PR1422B1/2 BLEND OUT AREA & S/BUSHING PER MD11-5510-19409-K. REPAIR ACCOMPLISHED AT BARREL NUT HOLE 20 LEFT PER EO MD11-5510-19409-K & EN1024-06, FOUND SATIS.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE NR 08 LT FOUND BEARING WITH SURFACE CORROSION ON SIDE & BOTTOM AREA. CORROSION REMOVAL CUTOUT & FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. B/N BORE & BOTTOM REWORKED PER EN 1643-05. FAB SLEEVE BUSHING PER EO MD 11-5510-19409-K, FIG 5. APPLIED SEALANT PR1422B 1/2 BLEND OUT AREA & S/BUSHING PER EO MD11-5510-19409-K. REPAIR ACCOMPLISHED AT B/N HOLE NR 08 LT PER EO MD11-5510-19409-K & EN 1643-05, FOUND SATISFACTORY.

Part: STRUCTURE — CORRODED (EMPENNAGE) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE 23 LEFT FOUND BEARING WITH SURFACE CORROSION ON SIDE & BOTTOM AREA. CORROSION REMOVAL C/OUT & FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. BARREL NUT HOLE 23 LEFT BORE & BOTTOM REWORKED PER EN1025-06. FAB SLEEVE BUSHING PER EO MD11-5510-19409-K, FIG-5. APPLIED SEALANT PR1422B1/2 BLEND OUT AREA & S/BUSHING PER EO MD11-5510-19409-K. REPAIR ACCOMPLISHED AT BARREL NUT HOLE 23 LEFT PER EO MD11-5510-19409-K & EN1025-06, FOUND SATIS.

Part: STRUCTURE — CORRODED (EMPENNAGE) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE NR 17 LEFT FOUND BEARING WITH SURFACE CORROSION ON SIDE & BOTTOM AREA. CORROSION REMOVAL C/OUT & FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. BARREL NUT HOLE 17 LEFT BORE & BOTTOM REWORKED PER EN1023-06. FAB SLEEVE BUSHING PER EO MD11-5510-19409-K, FIG-5. APPLIED SEALANT PR1422B1/2 BLEND OUT AREA & S/BUSHING PER EO MD11-5510-19409-K. REPAIR ACCOMPLISHED AT BARREL NUT HOLE PER EO MD11-5510-19409-K & EN1023-06, FOUND SATIS.

Part: ANGLE — CRACKED (TE FLAP) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C AFTER I/B FLAP O/B SEGMENT REMOVAL, FOUND FWD O/B SEGMENT MOST O/B AFT END 01/EA ANGLE CRACKED. THE ABOVE MENTIONED CRACKED AREA ANGLE REMOVED PER SRM 51-35-01.V.2R.38. NEW T-FAB & MAT USED S2931361X7075T6511 PER EN1063-06. HFEC C/OUT FOUND NO EVIDENT OF CRACK AT FAB T-ANGLE REWORKED AREA, REPAIR ACCOMPLISHED PER EN1063-06. NEW TEE HOLES TRANSFERRED & NEW TEE INSTALLED PER SRM 51-21-01V.2.R38.

Part: BEARING — CORRODED (ZONE 300) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C EMPENNAGE-BARREL NUT HOLE NR 36 LT FOUND BEARING WITH SURFACE CORROSION ON SIDE AND BOTTOM AREA. CORROSION REMOVAL C/OUT ON AFFECTED AREA PER SRM 51-21-01.V2.R38, FOUND BLEND OUT EXCEEDED LIMIT PER MD11-5510-19409-K FIG5. REPAIR SLEEVE BUSHING FAB PER MD11-5510-19409-K, APPLIED SEALANT PR1422B 1/2 ON SLEEVE AND AFFECTED BORE AREA. INSTALLED REPAIR SLEEVE BUSHING ON B/N HOLE NR 36 LT BORE, REPAIR ACCOMPLISHED AT B/N HOLE NR 36LH PER EN 1617-05, FOUND SATIS.

Part: SKIN — DENTED (L/E SLAT) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C LEFT WING INBOARD NR 1 SLAT HAS DENT AS MARKED. LEFT WING INBOARD NR 1 SLAT DENT (QTY/01/EA) EVALUATED FOUND EXCEEDED PER SRM LIMIT. HFEC CUTOUT FOUND NO EVIDENT OF CRACK. DENT AREA FASTENERS REMOVED AS PER SRM 51-35-01V.2.R.38. DENT AREA SKIN TRIMMED PER SRM 57-10-00.F33. V.1.R.38. REPAIR ANGLE FAB USING MAT 7075-0-0.050 PER SRM 57-10-00 FIG 33 SHT 2. REPAIR ACCOMPLISHED AT NR 1 SLAT LEFT WING PER EN1041-06, FOUND SATISFACTORY.

Part: FUEL TANK — CORRODED (CENTER) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C, CABIN-UPPER SURFACE OF UPPER CTR FUEL TANK AROUND FASTENERS HEAD AT STA 1159-1209X=97.70 TO 107.00 FOUND CORROSION. FASTENERS AT UPPER SURFACE CTR F/TANK AT STA1159-1209 REMOVAL FOR ACCESS. CORROSION REMOVAL C/OUT PER SRM51-21-01.V2.R38, FOUND EXCEEDED LIMIT. C/OUT MAGNIFIED V/INSP AND FPI FOUND SATIS. FLAP PEENING C/OUT ON REWORKED AREA PER CMM20-11-01.R51, IAW EN1009-06. INSTALL FASTENERS AND REPAIR ACCOMPLISHED PER EN1009-06, FOUND SATIS.

Part: SKIN — CHAFED (L/E SLAT) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C RHW DROOP L/E SLAT LWR I/B EDGE FOUND CHAFING MARK. CHAFING MARK BLENDED AND PROTECTED PER SRM51-21-01.V2.R.38.ORI THK 0.069 MAT REMOVED 0.055", REMAIN MAT THK 0.014", FOUND EXCEEDED LIMIT. REWORKED AREA EDGE TRIMMING FOUND REMAIN MAT THK 0.035". FASTENER EDGE DISTANCE IS 0.312" AND FASTENER HOLE SIZE IS 0.157" WITHIN LIMIT PER EN1005-06. RE WORK ACCOMPLISHED PER EN1005-06, FOUND SATIS.

Part: STRUCTURE — CORRODED (EMPENNAGE) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE 09 LEFT FOUND BEARING WITH SURFACE CORROSION ON SIDE & BOTTOM AREA. CORROSION REMOVAL C/OUT & FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. BARREL NUT HOLE 09 LEFT BORE & BOTTOM REWORKED PER EN 1622-05. FAB SLEEVE BUSHING PER EO MD11-5510-19409-K,F-5. APPLIED SEALANT PR1422B1/2 BLEND OUT AREA & S/BUSHING PER EO MD11-5510-19409-K. REPAIR ACCOMPLISHED AT BARREL NUT HOLE 09 LEFT PER EO MD11-5510-19409-K & EN1622-05, FOUND SATIS.

Part: BEARING — CORRODED (ZONE 300) · airframe 55,014 hrs · 8,680 cycles

EMPENNAGE-BARREL NUT HOLE NR 33 LT FOUND BEARING WITH SURFACE CORROSION ON SIDE AND BOTTOM AREA. CORROSION REMOVAL C/OUT AFFECTED AREA PER SRM 51-21-01.V2.R38, FOUND BLEND OUT EXCEEDED LIMIT PER MD11-5510-19409-K, REPAIR SLEEVE BUSHING FAB PER MD11-5510-19409-K, APPLIED SEALANT PR1422B 1/2 ON SLEEVE AND BORE AREA. INSTALLED REPAIR SLEEVE BUSHING ON B/N HOLE NR 33 LT BORE. REPAIR ACCOMPLISHED AT B/N HOLE NR 33 LT PER EN 1040-06, FOUND SATIS.

Part: STRUCTURE — CORRODED (EMPENNAGE) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE 21 LEFT FOUND BEARING WITH SURFACE CORRODED ON SIDE & BOTTOM AREA. CORROSION REMOVAL C/OUT & FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. BARREL NUT 21 LEFT & BOTTOM REWORKED PER EN 1637-05. FAB SLEEVE BUSHING PER EO MD11-5510-19409-K,F.5. APPLIED SEALANT PR1422B1/2 BLEND OUT AREA & FAB S/BUSHING PER EO MD11-5510-19409-K. REPAIR ACCOMPLISHED AT BARREL NUT HOLE 21 LEFT PER EO MD11-5510-19409-K & EN1637-05, FOUND SATIS.

Part: STRUCTURE — CORRODED (EMPENNAGE) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE 12 LEFT FOUND BEARING WITH SURFACE CORROSION ON SIDE & BOTTOM AREA. CORROSION REMOVAL C/OUT FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. BARREL NUT 12 LEFT BORE & BOTTOM REWORKED PER EN1623-05. FAB SLEEVE BUSHING PER EO MD11-5510-19409-K.F-5. APPLIED SEALANT PR1422B1/2 BLEND OUT AREA & S/BUSHING PER EO MD11-5510-19409-K. REPAIR ACCOMPLISHED AT BARREL NUT HOLE 12 LEFT PER EO MD11-5510-19409-K & EN1623-05, FOUND SATIS.

Part: STRUCTURE — CORRODED (EMPENNAGE) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE 02 LEFT FOUND BEARING WITH SURFACE CORROSION ON SIDE & BOTTOM AREA. CORROSION REMOVAL C/OUT & FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. BARREL NUT HOLE 02 LEFT BORE & BOTTOM REWORKED PER EN 1640-05. FAB SLEEVE BUSHING PER EO MD11-5510-19409-K. APPLIED SEALANT PR1422B1/2 BLEND OUT AREA & S/BUSHING PER EO MD11-5510-19409-K. REPAIR ACCOMPLISHED AT BARREL NUT HOLE 02 LEFT PER EO MD11-5510-19409-K & EN1640-05, FOUND SATIS.

Part: STRUCTURE — CORRODED (EMPENNAGE) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE 18 LEFT FOUND BEARING WITH SURFACE CORROSION ON SIDE & BOTTOM AREA. CORROSION REMOVAL C/OUT & FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. BARREL NUT HOLE 18 LEFT BORE & BOTTOM REWORKED PER EN1636-05. FAB SLEEVE BUSHING PER EO MD11-5510-19409-K, FIG-5. APPLIED SEALANT PR1422B1/2 BLEND OUT AREA & S/BUSHING PER EO MD11-5510-19409-K. REPAIR ACCOMPLISHED AT BARREL NUT HOLE 18 LEFT PER EO MD11-5510-19409-K & EN1636-05, FOUND SATIS.

Part: STRUCTURE — CORRODED (EMPENNAGE) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE 15 LEFT FOUND BEARING WITH SURFACE CORROSION ON SIDE & BOTTOM AREA. CORROSION REMOVAL C/OUT & FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. BARREL NUT HOLE 15 LEFT BORE & BOTTOM REWORKED PER EN1635-05. FAB SLEEVE BUSHING PER EO MD11-5510-19409-K,F-5. APPLIED PR1422B1/2 BLEND OUT AREA & S/BUSHING PER EO MD11-5510-19409-K. REPAIR ACCOMPLISHED AT BARREL NUT HOLE 15 LEFT PER EO MD11-5510-19409-K & EN1635-05, FOUND SATIS.

Part: BEARING — CORRODED (ZONE 300) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C EMPENNAGE-BARREL NUT HOLE NR 30 LT FOUND BEARING WITH SURFACE CORROSION ON SIDE AND BOTTOM AREA. CORROSION REMOVAL C/OUT AFFECTED AREA PER SRM51-21-01.V2.R38, FOUND BLEND OUT EXCEEDED LIMIT PER MD11-5510-19409-K, REPAIR SLEEVE BUSHING FAB PER MD11-5510-19409-K, APPLIED SEALANT PR1422B 1/2 ON SLEEVE AND BORE AREA. INSTALLED SLEEVE BUSHING ON B/N HOLE NR 30 LT BORE. REPAIR ACCOMPLISHED AT B/N HOLE NR 30 LT PER EN 1040-06 AND EN 1638-05, FOUND SATIS.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 55,014 hrs · 8,680 cycles

EMPENNAGE-BARREL NUT HOLE NR 1 LT FOUND WITH SURFACE CORROSION ON SIDE AND BOTTOM AREA. CORROSION REMOVAL C/OUT AFFECTED AREA PER SRM 51-21-01.V2.R38, FOUND BLEND OUT EXCEEDED LIMIT PER MD11-5510-19409-K, REPAIR SLEEVE BUSHING FAB PER MD11-5510-19409-K, APPLIED SEALANT PR1422B 1/2 ON SLEEVE AND BORE AREA. INSTALLED REPAIR SLEEVE BUSHING ON B/N HOLE NR 1 LT BORE. REPAIR ACCOMPLISHED AT B/N HOLE NR 1 LT PER EN 1626-05, FOUND SATIS.

Part: FUEL TANK — CORRODED (CENTER) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C CABIN, CORROSION ON UPPER SURFACE OF UPPER CTR FUEL TANK AROUND FASTENER HEAD AT STA1209-1239 X=+.97 TO+107. FASTENERS REMOVED FOR ACCESS AT STA1209-1239, CORROSION REMOVAL C/OUT PER SRM 51-21-01.V2.R38, FOUND EXCEEDED LIMIT. C/OUT MAGNIFIED V/INSP AND FPI FOUND SATIS. FLAP PEENING C/OUT ON REWORKED AREAS PER CMM20-11-01R.51, IAW EN1009-06. INSTALL FASTENERS AND REPAIR ACCOMPLISHED PER EN1009-06, FOUND SATIS.

Part: FUEL TANK — CORRODED (CENTER) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C CABIN, CORROSION ON UPPER SURFACE OF OF UPPER CTR FUEL TANK AT STA 1239 -1253 X=-107. FASTENERS AT UPPER SURFACE CTR FUEL TANK AT STA 1239-1253X=-107, REMOVED PER SRM 51-31-01 AND 51-33-01 V.2.R.38. CORROSION REMOVAL C/OUT PER SRM 51 -21-01V2.38, FOUND EXCEEDED LIMIT. C/OUT MAGNIFIED V/INSP AND FPI FOUND SATIS. FLAP PEENING C/OUT ON REWORKED AREAS PER CMM20-11-01.R51, IAW EN10 08-06. INSTALL FASTENERS AND REPAIR ACCOMPLISHED PER EN 1008-06, F/SATIS.

Part: LONGERON — CORRODED (BS 2007) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C AFT CABIN, CORROSION ON LONGERON 27 AT STA 2007 X=27.5 CORROSION ON LONG 27 T-CHORD AT STA 2007 X=27.50. REMOVED PER SRM 51-21- 01V2.R37 AND FOUND OUT OF LIMIT PER SRM 53-40-00V1 FIG7 R.37.ORI THK=0.12 5" MAT REMOVED 0.040".STA 2007 BULKHEAD T-CHORD REMOVED PER SRM 51-31-0 1V.2R.37. T-CHORD FAB PER DWG NJC 6040 USING MAT S2924410. NEW T-CHORD INSTALLED PER SRM 51-31-01 V2R.37, FOUND SATIS.

Part: FRAME — CORRODED (BS 1960) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C AFT CARGO COMPT AT STA 1960 LONGERON 45 LT FRAME WITH SURFACE CORROSION. CORROSION AT AFT CARGO COMPT REMOVED PER SRM 51-21-01.V.2.R.38. FOUND EXCEEDED LIMIT. FPI C/OUT FOUND NO CRACK EVIDENT. REPAIR DOUBLER FAB PER EN1 036-06, USING MAT 7075-0-0.071"(CLAD ALU SHT) REPAIR DOUBLER PICK UP HOLES & REPAIR BUSHING FAB PER EN1036-06.REPAIR BUSHING & DOUBLER INSTALLED PER EN1036-06, FOUND REPAIR ACCOMPLISHED WITH SATIS.

Part: SKIN — CORRODED (SPOILER) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C RT WING TOP SIDE FIXED T/E PANEL XORS 683.4 FWD OF NR 4 SPOILER FOUND CORROSION UNDERNEATH PNL. CORROSION REMOVAL C/OUT FOUND MAT REMOVED EXCEEDED LIMIT. HFEC C/OUT FOUND NO EVIDENT OF CRACK. FLAP PEENING C/OUT ON REWORK AREA PER EN1039-0 6. REPAIR FILLER FAB USING MAT 7075T6-0.090" PER EN1039-06. UPPER SKIN APP STA XORS 670 TO 697 HI-LOK INSTALLED PER SRM51-33-01,V2.R.38. FIXED T/E UPPER PNL INSTALLED PER SRM 51-33-.01.V2.R.38, FOUND SATIS.

Part: FUEL TANK — CORRODED (CENTER) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C CABIN, CORROSION ON UPPER SURFACE OF CENTER FUEL TANK BETWEEN STA 1159- 1239 X=-75.0 TO 107.0. FASTENERS AT UPPER SURFACE CTR F/TANK REMOVED FOR ACCESS. CORROSION REMOVAL C/OUT PER SRM 51-33-01 V.2.R38, FOUND EXCEEDED LIMIT. C/OUT MAGNIFIED V/INSP AND FPI FOUND SATIS. FLAP PEENING C/OUT ON REWORKED AREAS PER CMM2 0-11-01.R51, IAW EN1008-06. FAB DOUBLER PER SRM51-31-01.V2.R38. REPAIR AC ACCOMPLISHED AND INSTALLATION COMPLETED PER EN 1008-06 FOUND SATIS.

Part: SEAT TRACK — CORRODED (BS 1961) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C AFT CABIN-CORROSION ON SEAT TRACK FLANGE AT STA 1961 X=-107. NR 4 DR RT SILL PLATE REPLACED FOR SEAT TRACK REPAIR REPLACE PER AMM20-50-0 2R.50.SEAT TRACK AT STA 1961 X=-107. REMOVED PER SRM 51-21-01V.2R.37. FOUND OUT OF LIMIT .ORI THK 0.08 INCH AND MAT REMOVED 0.046 INCH. SEAT TRACK REMOVED PER SRM 51-31-01V.2R.37. HEFC INSP AND NDT PER SPM REV 12 C/OUT. FOUND NO CRACK EVIDENT. NEW SEAT/T INSTALLED PER SRM 53-70-00 V.1 REV.38-SATIS.

Part: SEAT TRACK — CORRODED (BS 1961) · airframe 55,014 hrs · 8,680 cycles

INSPECTION TYPE:C AFT CABIN, CORROSION ON SEAT TRACK AT STA 1961 X=107. NR 4 DR LT SILL PLATE REMOVED FOR SEAT REMOVED FOR REPAIR AND REPLACEMENT OF SEAT TRACK PER AMM20-50-02 R.50. CORROSION FOUND OUT OF LIMIT PER SRM 51- 21-01V.2.37. MAT REMOVED 0.043" AND ORI THK 0.145".SEAT TRACK REMOVED PER SRM 51-31-01V2R37. HFEC INSP AND NDT SPM C/OUT FOUND NO EVIDENT OF CRACK. NEW SEAT TRACK INSTALLED PER SRM 53-70-00 F.7.V1.7.R.38, FOUND SATIS.