N281UP

Part: ACCUMULATOR — DISCHARGED (L1 DOOR) · airframe 71,302 hrs · 16,625 cycles

L1 DOOR PNEUMATICALLY OPENED BY CREW, DOOR RESERT AND DOOR ACCUMULATOR SERVICED PER MD11 AMM 52-10-01-201 AND 12-25-04-600-801.

Part: CABLE — BROKEN (R1 DOOR) · airframe 71,283 hrs · 16,612 cycles

R 1 DOOR FWD CABLE BROKEN/OFF OF DRUM. R1 DOOR. R/R R1 FWD LOWERING CABLE PER AMM 52-11-03. OPS CHECK GOOD PER AMM 52-11-02.

Part: SOLENOID — INOPERATIVE (R1 DOOR) · airframe 71,052 hrs · 16,491 cycles

R1 DOOR INOP. R/R PASS DOOR LOCK PIN RELEASE SOLENOID REF AMM 52-10-06 PB 401. R/R R1 CLOSE-LIMIT SWITCH REF AMM 52-11-02 PB 501 830-805. DOOR OPERATES NORMALLY.

Part: LONGERON — CORRODED (CENTER CARGO) · airframe 70,712 hrs · 16,298 cycles

INSPECTION TYPE:1CCENTER CARGO COMPARTMENT AFT INTERMEDIATE FUSELASE LON 51L CORRODED BETWEEN STA. 1701 AND STA, 1721.REPAIRED CORRODED LONGERON 51L BETWEEN STA. 1701 AND STA. 1721 IAW VT-SAA EA 011-5310-01-A9542 REV I/R AND UPS EO MD11-5310-83450-A BY P.LAU (AR-830967) DATED 04-22-2022 (MAJOR).

Part: SPLICE — CRACKED (CTR CARGO) · airframe 70,712 hrs · 16,298 cycles

INSPECTION TYPE:4CFOUND LONGERON 49R PRODUCTION SPLICE FITTING CRACKED BETWEEN STA 5-113 AND 1541.REPLACED PRODUCTION SPLICE P/N A5A7114-511 IAW MD11 SRM 51-31-01. (MINOR)

Part: LONGERON — CORRODED (FUSELAGE) · airframe 70,712 hrs · 16,298 cycles

INSPECTION TYPE:4CEXTERIOR FUSELAGE LONGERON 28R P/N AEA7545-2 HAS CORROSION BETWEEN STA Y=1207 - Y=1305.5.REPAIRED CORRODED LONGERON 28R P/N AEA7545-2 IAW EA 011-5300-01-A9541 REV I/R AND UPS EO MD11-5310-83430-A (MINOR)

Part: BEAM — CRACKED (R-3 DOOR) · airframe 70,712 hrs · 16,298 cycles

INSPECTION TYPE:2CR-3 DOOR PLUG UPPER HORZ. BEAM IS CRACKED AT THE FWD. END.REMOVED AND REPLACED BEAM IAW SRM 51-31-01 & 51-35-01. (MINOR)

Part: LONGERON — CORRODED (CENTER CARGO) · airframe 70,712 hrs · 16,298 cycles

INSPECTION TYPE:2CCENTER CARGO LONGERON 49R HAS CORROSION AT STA. 5-93/1541.REPAIRED CORRODED CENTER CARGO LONGERON 49R BETWEEN STA. 5-103 TO 5-123 IAW VT-SAA EA 011-5310-01-A9540 REV. I/R AND UPS EO MD11-5310-83411-A. (MAJOR) REF FAA FORM 8100-9 BY. S. KANG (AR-605677) DATED 4/22/2022.

Part: STIFFENER — CRACKED (AFT CARGO) · airframe 70,712 hrs · 16,298 cycles

INSPECTION TYPE:4CAFT CARGO STEP UP HAS A STIFFENER P/N AGA7170-11 HAS A CRACK AT STA 1841.REMOVED, FAB AND REPAIRED THE CRACKED STIFFENER P/N AGA7170-11 IAW MD11 51-31-01 AND 51-35-01 (MINOR)

Part: STIFFENER — CRACKED (AFT CARGO) · airframe 70,712 hrs · 16,298 cycles

INSPECTION TYPE:1CAFT CARGO COMPARTMENT STEP UP BULKHEAD STIFFENER CRACK AT STA.1841 LON 49R.REMOVED,FABRICATED AND REPLACED CRACKED STIFFENER IAW MD-11 SRM 51-33-01 AND 51-35-01 (MINOR).

Part: STIFFENER — CRACKED (WING TO BODY) · airframe 70,712 hrs · 16,298 cycles

INSPECTION TYPE:4CLOWER FUSELAGE R/H WING TO BODY HAS A STIFFENER P/N AYB7104-526 WITH A CRACK AT STA 1298.REMOVED,FAB AND REPLACED THE CRACK STIFFENER P/N AYB7104-526 IAW DWG AYB7104 AND MD11 SRM 51-33-01. (MINOR)

Part: LONGERON — CORRODED (FUSELAGE) · airframe 70,712 hrs · 16,298 cycles

INSPECTION TYPE:4CEXTERIOR FUSELAGE , LONGERON 28L P/N AEA7545-1 HAS CORROSION BETWEEN STA 1304-1309.REPAIRED CORRODED LONGERON 28L P/N AEA7545-1 IAW EA 011-5300-01-A9539 I/R AND UPS EO MD11-5310-83429-A (MINOR)

Part: STIFFENER — CRACKED (AFT CARGO) · airframe 70,712 hrs · 16,298 cycles

INSPECTION TYPE:4CAFT CARGO STEP UP HAS A STIFFENER P/N AGA7170-9 THAT IS CRACKED AT STA 1841.REMOVED,FAB AND REPLACED THE CRACKED STIFFENER P/N AGA7170-9 IAW MD11 SRM 51-31-01 AND 51-35-01 (MINOR)

Part: STRINGER — CRACKED (R/H WING L/E) · airframe 70,712 hrs · 16,298 cycles

INSPECTION TYPE:4CR/H WING FIXED L/E LOWER STRINGER EXISTING REPAIR DOUBLER IS CRACKED AT STA XOS=906.5607.REMOVED, FAB AND REPLACED CRACK REPAIR DOUBLER AT STA XOS=906.5607 IAW MD11 SRM 57-40-03 FIG 201 REPAIR 1 (MAJOR)

Part: NONE — CRACKED (R/H I/B FLAP) · airframe 70,712 hrs · 16,298 cycles

INSPECTION TYPE:4CR/H I/B FLAP I/B TRACK THE 2ND FITTING FROM THE BOTTOM IS CRACKED.REMOVED, REPLACED R/H I/B FLAP ASSY P/N NRC6055-508 IAW MD11 AMM 27-50-20-400-801 (MINOR)

Part: WEB — CRACKED (R3 DOOR JAMB) · airframe 70,712 hrs · 16,298 cycles

INSPECTION TYPE:4CMAIN CARGO R3 DOOR TORQUE BOX LWR AFT WEB IS CRACKED AT STA Y=1313 AND Z=-16.REMOVED, FAB AND REPAIRED CRACKED AFT WEB P/N AEA0112-2 AT STA Y=1313 AND Z=-16 IAW MD11 SRM 53-40-15 FIG 201 REPAIR 3 (MAJOR)

Part: FLOOR PANEL — CORRODED (COURIER AREA) · airframe 70,712 hrs · 16,298 cycles

INSPECTION TYPE:C4FWD CABIN FLOOR PANEL P/N WSP0788-502 AT STA Y=475.0 - Y=503.175 AND X=-36.000 - X=-47.500 HAS HEAVY CORROSION.REMOVED, REPLACED FLOOR PANEL WSP0788-502 IAW DWG WSP0788 AND DWG SP11530078, SRM 51-31-01 (MINOR)

Part: DOUBLER — CRACKED (R/H WING L/E) · airframe 70,712 hrs · 16,298 cycles

INSPECTION TYPE:C4R/H O/B WING FIXED LEADING EGDE BEADED DOUBLER IS CRACKED AT STA XOS=661.7 -XOS=667.62 .REMOVED, FAB AND REPAIRED THE CRACK BEADED DOUBLER AT STA XOS=661.7 - XOS=667.62 IAW DWG ARB2893-2 AND MD11 SRM 57-40-02 REPAIR 15, FIG 205 REV 68.01 (MAJOR)

Part: BRACE — CRACKED (L/H REAR SPAR) · airframe 70,712 hrs · 16,298 cycles

INSPECTION TYPE:4CL/H WING T/E REAR SPAR HAS A BRACE THAT IS CRACKED.REMOVED,FAB REPLACED THE CRACKED BRACE IAW MD11 DWG ARC0295 AND SRM 51-31-01. (MINOR)

Part: SKIN — DAMAGED (LOWER FUSELAGE) · airframe 70,712 hrs · 16,298 cycles

INSPECTION TYPE:4CCENTER FUSELAGE LOWER SKIN PANEL HAS EXISTING CHAFED DAMAGED AT STA 1153 AND LONGERON 44L .REMOVED, REPAIRED EXISTING CHAFED DAMAGED AT STA 1153 AND LONGERON 44L IAW VTSAA EA 011-5340-01-A9535 REV I/R AND UPS EO MD11-5330-83452-A FAA FORM 8100-9 SIGNED BY JEFFREY . TOM (AR-605565) DATED 04/19/22

Part: STIFFENER — CRACKED (R/H W/W) · airframe 70,712 hrs · 16,298 cycles

INSPECTION TYPE:2CR/H MLG W/W 3RD STIFFNER AT O/B WEB IS CRACKED.REMOVED AND REPLACED STIFFNER IAW SRM 51-35-01. (MINOR)

Part: FLOOR PANEL — CORRODED (COURIER AREA) · airframe 70,712 hrs · 16,298 cycles

INSPECTION TYPE:C4FWD CABIN FLOOR PANEL P/N WSP0786-501 AT STA Y=475.0 -Y=503.175 AND X=-17.000 - X=-27.500 HAS HEAVY CORROSION.REMOVED, REPLACED FLOOR PANEL IAW DWG WSP0786 AND DWG SP11530078, SRM 51-31-01 (MINOR)

Part: STATUS MESSAGE — ILLUMINATED (BATTERY PACK) · airframe 69,932 hrs · 15,899 cycles

INSPECTION TYPE:N/ALEVEL 1 EMER LT BAT 1 LO MESSAGE DISPLAYEDR&R #1 EMER LT BAT IAW MD 11 AMM 33-51-01. PERFORMED OPS CHECK IAW AMM 33-51-01-700-802. BATTERY TEST PASSED

Part: ACTUATOR — INOPERATIVE (L1 DOOR) · airframe 69,839 hrs · 15,860 cycles

INSPECTION TYPE:N/AWHILE RIGGING L1 DOOR ELEC. DOOR ACT BRAKE NOT HOLDING DOOR IN CUTOUT.R&R L1 DOOR ELEC ACTUATOR PER MM 52-11-01-400-801, L1 DOOR OPS CK GOOD.

Part: INDICATION SYS — INOPERATIVE (L1 DOOR) · airframe 69,063 hrs · 15,492 cycles

L1 DOOR ALERT SYSTEM INOP. NEEDS BRACKET REPLACED TO SWITCH. EAD DOOR OPEN ALERT SYSTEM DEFERRED REF MD11 MEL 52-40-1-1-0-1 ITEM PLACARDED.REPLACED CLOSED SENSOR TARGET. OPS TEST GOOD REF 52-70-04. M732653 CLEARED. PLACARD REMOVED.

Part: CABLE — DETACHED (L1 DOOR) · airframe 69,063 hrs · 15,492 cycles

L DOOR, CABLE CAME OFF TRACK. DEFERRED L1 DOOR. INSTALLED L/H AFD TOP CABLES PER 52-11-03. OPS TES GOOD.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 69,075 hrs · 15,503 cycles

INSPECTION TYPE: NA ATB EMERGENCY DECLARED, NO EQUIP USED- LANDING UNEVENTFUL. DURING CLIMB OUT ZTIME GOT LEVEL 1 CABIN RATE MESSAGE APPROXIMATELY 12000' MESSAGE NOTICED CAB ALT 8000 FT CLIMBING REQUIRED LEVEL OFF AT 17500 FT CAB ALT ABOVE 1000 MAX CABIN ALT WAS 12000 FT WENT TO MANUAL & VERIFIED OUTFLOW VALVE CLOSED, NO EFFECT. REMOVED AND REPLACED CABIN PRESSURE OUTFLOW VALVE MOTOR, IAW AMM 21-31-21. FUNCTIONAL TEST GOOD.

Part: CONTROL SWITCH — FAILED (EMERGENCY LIGHTS) · airframe 68,999 hrs · 15,458 cycles

INSPECTION TYPE: N/A, SUPPLEMENTAL SDR, EMERGENCY LIGHTS WILL NOT ILLUMINATE. DEFERRED EMERGENCY LIGHT SYSTEM, IAW MEL 33-50-4. REPLACED BATTERY SUPPLY FOR T/S PURPOSES, NO HELP, SUSPECT FAULTY SWITCH. PLACARD INSTALLED. DMP C/W. REPLACED RELAY R2-5700 EMERGENCY LIGHTS BATT PACK TEST AND REPLACED S1-346 EMERGENCY LIGHTS CONTROL SWITCH, IAW WDM 33-51-01. OPERATIONS CHECK OK, IAW AMM 33-50-00. REVERSED DMP. IPC: 33-51-05-01.

Part: SIGN — LOOSE (R1 DOOR) · airframe 68,809 hrs · 15,370 cycles

INSPECTION TYPE: N/A 1R EXIT DOOR SIGN LOOSE. INSTALLED 1R EMERGENCY EXIT IDENTIFIER SIGN, IAW AMM 33 52 05. OPERATIONS CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (FCC 2) · airframe 68,642 hrs · 15,309 cycles

INSPECTION TYPE: N/A ATB, NO EMERGENCY DECLARED. LANDED UNEVENTFUL. AT LEVEL 2 FCC 2B DATA FAULT AT CRUISE FL 360 LEVEL SEL YAW UPR AA OFF LEVEL 1 LSAS LOB OFF. R & R FCC 2, PER AMM 22-01-03. PERFORMED AUTO FLIGHT SYSTEM CATT111B FCC-2 RTS, REF AMM 22-00-00-700-801 P/B 501, RTS PASSED. A/C REMAINS CATIII QUALIFIED.

Part: FITTING — WORN (RT ELEVATOR) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3CR/H DETACHABLE ELEVATOR O/B CAM FITTING IS WORN.REMOVED,REPAIRED AND INSTALLED RH DETACHABLE ELEVATOR O/B CAM FITTING IAW EA #011-5520-01A8384 I/R AND UPS EO #MD11-5520-77027-A. (MINOR)

Part: FITTING — WORN (LT ELEVATOR) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3CLH I/B ELEVATOR O/B CAM FITTING IS WORN. REMOVED,REPAIRED AND INSTALLED LH I/B ELEVATOR O/B CAM FITTING IAW EA #011-5520-01-A8384 I/R AND UPS EO # MD11-5520-77027-A. (MINOR)

Part: FITTING — WORN (RT ELEVATOR) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3CR/H I/B ELEVATOR O/B CAM FITTING IS WORNREMOVED,REPAIRED AND INSTALLED WORN RH I/B ELEV O/B CAM FITTING IAW VT SAA EA # 011-5520-01-A8384 I/R AND UPS EO MD11-5520-77027-A. (MINOR)

Part: FITTING — WORN (LT ELEVATOR) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3CLH O/B ELEVATOR CAM FITTING I/B OF #7 BEARING IS WORN.REMOVED,REPAIRED AND INSTALLED LH O/B ELEVATOR CAM FITTING I/B OF #7 BEARING IAW VT SAA EA #011-5520-01-A8384 I/R AND UPS EO #MD11-5520-77027-A. (MINOR)

Part: SKIN — CORRODED (LT WING) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3C. LT WING UPPER CENTER SKIN CORRODED BETWEEN STA. XORS 514 TO XORS 521 ABOVE STRINGER 10.REPAIRED CORRODED LH WING UPPER CENTER SKIN BET. STA. XORS 514 TO XORS 521 ABOVE STRINGER 10 IAW VT SAA EA #011-5730-01-A8397 I/R AND UPS EO #MD11-5730-77092-A. (MINOR)

Part: FITTING — WORN (LT ELEVATOR) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3CL/H DETACHABLE ELEV I/B CAM FITTING IS WORN.REMOVED,REPAIRED AND INSTALLED LH DETACHABLE ELEV I/B CAM FITTING IAW EA #011-5520-01-A8384 I/R AND UPS EO # MD11-5520-77027-A. (MINOR)

Part: SKIN PANEL — CRACKED (LT WING) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3C LT WING SKIN FUEL ACCESS PANEL 536AB 9EA FASTENER HOLES CRACK. REPAIRED LT WING SKIN FUEL ACCESS PANEL 536AB 9EA FASTENER HOLES IAW SRM 57-20-02 REPAIR 5 (MINOR).

Part: SKIN PANEL — CRACKED (RT WING) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3C RT WING SKIN FUEL ACCESS PANEL 636AB 9EA FASTENER HOLES CRACKED. REPAIRED CRACKED RT WING SKIN ACCESS PANEL 636AB 9EA FASTENER HOLES IAW SRM 57-20-02 REPAIR 5. (MINOR)

Part: LONGERON SPLICE — CRACKED (MAIN CABIN) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3C, MAIN CABIN LONGERON 6R SPLICE AT BS 1531/5-123 IS CRACKED.REMOVED AND REPLACED MAIN CABIN CRACKED LONGERON 6R SPLICE AT BS 1531/5-123 IAW SRM 51-33-01. (MINOR)

Part: HINGE FITTING — WORN (RT WING TE FLAP) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3CRT WING O/B FLAP O/B FWD HINGE UPPER ACTUATOR I/B LUG BUSHING IS LOOSE.REPAIRED RT WING O/B FLAP O/B FWD HINGE UPPER ACTUATOR I/B LUG WORN BUSHING BORE IAW VT-SAA EA 011-5740-01-A8394 REV. IR AND UPS EO MD11-5740-77054-A. (MINOR)

Part: ANGLE — CRACKED (RT WING) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3C RT WING T/E ABOVE PANEL 641JB, VERTICAL STIFFNER ANGLE IS CRACKED. REMOVED, FABRICATED AND REPLACED TEE ANGLE IAW DWG ARC0472 AND SRM 51-33-01. (MINOR)

Part: SUPPORT BRACKET — CRACKED (NR 1 PYLON) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3C **SUPPLEMENTAL SDR** NR 1 PYLON "V" RIB SUPPORT BRACKET IS CRACKED. REMOVED, FABRICATED AND REPLACED SUPPORT BRACKET IAW DWG AUB7517 AND SRM 51-31-01. (MINOR)

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3C EXTERIOR FUSELAGE SKIN HAS CORROSION BETWEEN STA 2154.0 TO 2163.8 AND BETWEEN L33L TO 35L. REPAIRED CORRODED EXTERIOR FUSELAGE SKIN BETWEEN STA 2154.0 TO 2163.8 AND BETWEEN L33L TO 35L IAW SRM 53-70-01 REPAIR 3 FIG 201. (MAJOR)

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3C EXTERIOR FUSELAGE HAS CORROSION BETWEEN STA 2150.0 TO 2163.8 AND BETWEEN L33R TO 35R. REPAIRED CORRODED EXTERIOR FUSELAGE SKIN BETWEEN STA 2150.0 TO 2163.8 AND BETWEEN L33R TO 35R IAW SRM 53-70-01 REPAIR 3 FIG 201. (MAJOR)

Part: STRINGER — CRACKED (WING) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3C CENTER WING TANK STRINGER 52 IS CRACKED AT STA XCW=46.5. REPAIRED CRACKED CENTER WING TANK STRINGER 52 BETWEEN STA XCW= 36 TO XCW= 58 IAW SRM 57-10-03 REPAIR 1 FIG 201. (MAJOR)

Part: STRINGER — CRACKED (LT WING) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3C LT WING STRINGER 5 IS CRACKED BETWEEN STA XORS= 683.4 TO 700.0 AND BETWEEN STA XORS= 713.65 TO 737.55. REPAIRED CRACKED LT WING STRINGER 5 BETWEEN STA XORS= 669 TO 700 AND BETWEEN STA XORS= 726 TO 757 IAW SRM 57-00-00 REPAIR 3 FIG 201. (MAJOR)

Part: SKIN — CORRODED (STRINGER 15) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3CCENTER WING BOX UPPER SKIN HAS CORROSION AT STA. XCW= -87.7 ABOVE STR. 15.REPAIRED CORRODED CENTER WING BOX UPPER SKIN AT STA. XCW= -87.7 ABOVE STR. 15 IAW VT-SAA EA 011-5730-01-A8388 REV. I/R AND UPS EO MD11-5730-77106-A. (MINOR)

Part: SUPPORT — CHAFED (HORIZONTAL STAB) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3CL/H AFT FUSELAGE TO HORZ. STAB FAIRING SUPPORT FOR PANEL 337BF IS CHAFED.REPAIRED FAIRING SUPPORT IAW SRM SRM 55-00-00 PARA. 4 FIG. 208. (MINOR)

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3C LT AFT FUSELAGE TO HORIZ STAB FAIRING SUPPORT CHANNEL IS CORRODED. REMOVED, FABRICATED AND REPLACED CHANNEL IAW DWG AJC7898 AND SRM 51-31-00. (MINOR)

Part: STRINGER — CRACKED (LT WING) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3C, LEFT WING NR 1 MAIN FUEL TANK UPPER STRINGER 6 AT XORS 316.9 WAS CRACKED. REPAIRED THE LT WING FUEL TANK UPPER STRINGER 6 IAW 011-5710-01-A8398, REV IR AND EO MD11-5710-77236-A. (MAJOR)

Part: FUEL TANK — CORRODED (CENTER) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3CCENTER WING TANK UPPER SKIN HAS CORROSION ABOVE STRINGER 15 AT XCW=108.REPAIRED CENTER WING TANK UPPER SKIN CORROSION ABOVE STRINGER 15 AT XCW=108 IAW VT-SAA EA 011-5730-01-A8396 REV. IR AND UPS EO MD11-5730-77067-A. (MINOR)

Part: SKIN — CORRODED (STRINGER 12) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3C, CENTER WING BOX UPPER SKIN HAS CORROSION AT STA. XCW= -111 AT STR. 12.REPAIRED CENTER WING BOX UPPER SKIN AT STA. XCW= -111 AT STR. 12 IAW EA 011-5710-01-A8390 REV. I/R AND EO MD11-5730-770859-A. (MINOR)

Part: SKIN — CORRODED (STRINGER 15) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3C, CENTER WING BOX UPPER SKIN HAS CORROSION AT STA. XCW= 55.5 AT STR. 15.REPAIRED CORRODED CENTER WING BOX UPPER SKIN AT STA. XCW= 55.5 AT STR. 15 IAW VT-SAA EA 011-5730-01-A8393 REV. I/R AND UPS EO MD11-5730-77095-A. (MINOR)

Part: LONGERON — CORRODED (BS 1821-1841) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE: 3C, CENTER CARGO LONGERON 43L WAS CORRODED BETWEEN BS 1821 - 1841. REPAIRED THE LONGERON IAW EA 011-5310-01-A8387, REV I/R AND EO MD11-5310-77194-A. MAJOR.

Part: FUEL TANK — CORRODED (CENTER) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3CCENTER WING TANK UPPER SKIN HAS CORROSION ABOVE STRINGER 16 AT XCW=-101.REPAIRED CENTER WING TANK UPPER SKIN CORROSION ABOVE STRINGER 16 AT XCW=-101 IAW VT-SAA EA 011-5730-01-A8395 REV. IR AND UPS EO MD11-5730-77104-A. (MINOR)

Part: SKIN — CORRODED (STRINGER 15) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3C, CENTER WING BOX UPPER SKIN HAS CORROSION AT STA. XCW= -11 ABOVE STR. 15.REPAIRED CORRODED CENTER WING BOX UPPER SKIN AT STA. XCW= -11 ABOVE STR. 15 IAW VT-SAA EA 011-5730-01-A8391 REV I/R, AND EO MD11-5730-77097-A. (MINOR)

Part: SKIN — CORRODED (STRINGER 15) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3C, CENTER WING BOX UPPER SKIN HAS CORROSION AT STA. XCW= 47 AND STR. 15.REPAIRED CORRODED CENTER WING BOX UPPER SKIN AT STA. XCW= 47 AND STR. 15 IAW VT-SAA EA 011-5730-01-A8386 REV. I/R AND UPS EO MD11-5730-77099-A. (MINOR)

Part: SKIN — CORRODED (STRINGER 15) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3C, CENTER WING BOX UPPER SKIN HAS CORROSION AT STA. XCW= 2 AND STR. 15.REPAIRED CORRODED CENTER WING BOX UPPER SKIN AT STA. XCW= 2 AND STR. 15 IAW VT-SAA EA 011-5710-01-A8392 REV. I/R AND UPS EO MD11-5730-77090-A. (MINOR)

Part: STRUCTURE — CORRODED (LT WING SPOILER) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3C, LEFT WING SPOILER SILL IS CORRODED BETWEEN STA. XOSP= 494.50 TO XOSP= 566.75.REPAIRED CORRODED L/H WING SPOILER SILL BETWEEN STA. XOSP= 494.50 TO XOSP= 566.75 IAW SRM 57-50-02 REPAIR 10 FIG. 201. (MAJOR)

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3C EXTERIOR FUSELAGE SKIN HAS CORROSION BETWEEN STA 2153.0 TO 2163.8 AND BETWEEN L12R TO 13R. REPAIRED CORRODED EXTERIOR FUSELAGE SKIN BETWEEN STA 2153.0 TO 2163.8 AND BETWEEN L12R TO 13R IAW SRM 53-70-01 REPAIR 3 FIG 201. (MAJOR)

Part: FILLER — CHAFED (TAILCONE) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3C TAIL CONE RT PRODUCTION FILLER IS CHAFED. REMOVED, FABRICATED AND REPLACED FILLERS IAW EO MD11-5350-66790-A. (MINOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3C LT WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA XOS 572.1 TO 578.5. REPAIRED CRACKED LT WING FIXED L/E BEADED DOUBLER BETWEEN STA XOS 572.1 TO 578.5 IAW SRM 57-40-02 REPAIR 15 FIG 205. (MAJOR)

Part: PAN — CHAFED (RT MLG DOOR) · airframe 68,206 hrs · 15,122 cycles

INSPECTION TYPE:3C RT MLG DOOR CENTER AFT PAN IS CHAFED. REMOVED AND REPLACED CORNER/PAN IAW SRM 51-35-02. (MINOR)

Part: PUMP — CRACKED (HYD SYSTEM) · airframe 67,815 hrs · 14,923 cycles

INSPECTION TYPE:N/AATB - A/C TAKEN OOS. ON UPWIND AT 1509 MSL LVL 2 HYD 3 FAIL EMERGENCY DECLARED AIR TURN BACK TO SDF COMPLIED WITH QRH PROCEDURESSTOWED BOTH ALT GEAR EXT HANDLES 32-32-00. R/R CRCKED #3 ENG L EDP AMM 29-11-20-400. R/R #3 ENG L & R EDP OIL SEAL ASSY AMM 72-65-06-1401 (REAR) & 72-65-07-1401 (FRONT). R/R RT SIDE AFT PUMP AMM 29-11-20-401-2. R/R FILTERS AT ENG #3 HYD SYS MANFLD AMM 29-12-41-201. PERF. #3 ENG HYD SYS MANFLD FLTR LK CK & REINSTALL. COVER AMM 29-12-41. NO LKS NOTED

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 66,606 hrs · 14,400 cycles

INSPECTION TYPE:N/A "EMER LIGHTS BAT 1 LO" L1 MSG ON PREFLIGHT TEST OF EMER LIGHTS QRH PROCEDURES FOLLOWED. EMERG LT BAT 1 LO DEFERRED PER MEL 33-50-4, CNTRL # M 671464 ASSIGNED DMP 33-50-4 C/W PLACARD INSTALLED. REMOVED AND REPLACED EMERGENCY POWER SUPPLY REF AMM 33-51-01-401. DMP REVERSERED PLACARD REMOVED.

Part: MSC — DEFECTIVE (COCKPIT) · airframe 66,605 hrs · 14,399 cycles

INSPECTION TYPE:N/A DURING PREFLIGHT, EMER LIGHT TEST, EMER LT BAT 1 LO ALERT. DEFERED PER MEL 33-50-2, DMP CW, PLARARD INSTALLED. **SUPPLEMENTAL SDR** T/S REF FIM 33-51-00-101 FIG 104. REPLACED MSC NO FAULTS NOTED REF MM 31-42-01. DEFERRAL CLEARED. IPC 31-42-01-01-020K.

Part: RESERVOIR — LOW PRESSURE (L1 DOOR) · airframe 65,955 hrs · 14,171 cycles

INSPECTION TYPE:N/A L1 DOOR EMERGENCY BOTTLE PRESSURE LOW. DEFERRAL ISSUED PER MEL 52-10-3-1-2-1 AUTH M659003 ASSIGNED PLACARD INSTALLED DMI LOG UPDATED. **SUPPLEMENTAL SDR** SERVICED L1 DOOR PNEUMATIC RES REF AMM 12-25-04-301.

Part: SKIN — DAMAGED (TE FLAP) · airframe 65,895 hrs · 14,153 cycles

INSPECTION TYPE:N/A RT INBD FLAP LOWER SKIN DAMAGED REPAIRED IAW EO MD11-5750-70846-C.

Part: SKIN — DAMAGED (TE FLAP) · airframe 65,895 hrs · 14,153 cycles

INSPECTION TYPE:N/A D655519 ITERM REPAIR TO RT INBRD FLAP LWR SKIN REMOVED DAMAGE 1.0 DIM HOLE (ILLEG 0986314 12-28-18) / THIS IS A MAJOR REPAIR TRANSFERRED TO MRC 590056 (ILLEG 0986314 12-28-18) / ACCOMPLISHED REPAIR IAW APPENDIX A OF EO MD11-5750-70846-C. THIS CLOSES DEFERRAL D655519.

Part: INDICATOR — DAMAGED (L1 DOOR SLIDE) · airframe 65,829 hrs · 14,118 cycles

L1 ENTRY DOOR SLIDE DISARM LIGHT DAMAGED. REMOVED AND REPLACED L1 ENTRY DOOR SLIDE DISARM LIGHT INDICATION ASSY IAW SWPM 20-20-01, AND AMM 25-61-15. OPS CHECKED AND FUNCITONAL CHECKED GOOD.

Part: DOOR — STUCK (R1) · airframe 65,628 hrs · 14,050 cycles

R1 DOOR WILL NOT OPEN. COMPLIED WITH AN OPS CHECK OF THE DOOR. CHECKED GOOD IAW AMM 52-10-01.

Part: RIB — GOUGED (LT WING) · airframe 64,974 hrs · 13,818 cycles

LEFT WING DROOP LEADING RIB WAS GOUGED AT XDLE309 AND YW275. REPAIRED THE RIB IAW EA 011-5754-01-A7308, REV IR, AND EO MD11-5750-69036-A. MAJOR.

Part: SKIN — CHAFED (THRUST REVERSER) · airframe 64,974 hrs · 13,818 cycles

NR 2 ENGINE, LT THRUST REVERSER AFT FIXED INNER BARREL ,OUTER SKIN IS CHAFED THROUGH. REPAIRED THE THRUST REVERSER SKIN IAW EA 011-7830-01-A7303, REV I/R, AND EO MD11-7830-68965-A.

Part: SKIN — CHAFED (THRUST REVERSER) · airframe 64,974 hrs · 13,818 cycles

NR 2 ENGINE, RT THRUST REVERSER AFT FIXED INNER BARREL OUTER SKIN WAS CHAFED. REPAIRED THE THRUST REVERSER IAW EA 011-7830-01-A7306, REV IR, AND EO MD11-7830-68966-A.

Part: TEE FITTING — CRACKED (BS 1340) · airframe 64,974 hrs · 13,818 cycles

MAIN CABIN LONGERON 15L TEE FITTING WAS CRACKED AT BS 1340. REMOVED AND REPLACED THE TEE FITTING IAW SRM 51-33-01, 51-35-01, AND DWG AEA 7568.

Part: INTERCOSTAL — CRACKED (DOOR) · airframe 64,974 hrs · 13,818 cycles

INSPECTION TYPE:2C, UPPER INTERCOSTAL BROKEN INSIDE LT FWD A/C DOOR 113AL. REMOVED FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER DWG ACA3820 AND SRM 51-33-01. (MINOR)

Part: FRAME — CRACKED (NR 2 PYLON) · airframe 64,974 hrs · 13,818 cycles

INTERNAL FRAME CRACKED INSIDE THE NR 2 PYLON LOWER AFT FAIRING. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT FRAME IAW DWG AVB7599, AND SRM 54-01-42.

Part: INTERCOSTAL — CRACKED (LONGERON 43L) · airframe 64,974 hrs · 13,818 cycles

INTERCOSTAL CRACKED ALONG LONGERON 43L BETWEEN 1129/6-30 AND 1129/6-50. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT INTERCOSTAL IAW DWG ACA7049, AND SRM 51-33-01.

Part: INTERCOSTAL — CRACKED (LONGERON 43L) · airframe 64,974 hrs · 13,818 cycles

INTERCOSTAL CRACKED ALONG LONGERON 43L. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT INTERCOSTAL IAW DWG ACA7049, AND SRM 51-33-01.

Part: CAP — CRACKED (BS 1236) · airframe 64,974 hrs · 13,818 cycles

LT UNDERWING BARREL CANTED PANEL CAP WAS CRACKED AT BS 1236.8, AND Z=-100. REPAIRED THE PANEL CAP IAW EO MD11-5310-68793-A. MAJOR.

Part: BRACE — CRACKED (FUSELAGE) · airframe 64,974 hrs · 13,818 cycles

INSPECTION TYPE:2C, FLOORBEAM SUPPORT BRACE IS CRACKED IN FWD CARGO COMPARTMENT CENTER CEILING AREA BETWEEN STA 6-10 TO 6-30. REMOVED AND REPLACED FLOORBEAM SUPPORT BRACE IN FWD CARGO COMPARTMENT CENTER CEILING AREA BETWEEN STA 6-10 - 6-30 IAW SRM 51-33-01.

Part: INTERCOSTAL — CRACKED (BS 1129) · airframe 64,974 hrs · 13,818 cycles

INTERCOSTAL CRACKED ALONG LONGERON 43R AT BS 1129. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT INTERCOSTAL IAW DWG ACA7049, AND SRM 51-33-01.

Part: CAP — CRACKED (BS 1236) · airframe 64,974 hrs · 13,818 cycles

RT UNDERWING BARREL CANTED PANEL CAP IS CRACKED AT BS 1236.8 AND Z=-100. REPAIRED THE CANTED PANEL CAP IAW EO MD11-5310-68794-A. MAJOR

Part: FLOORBEAM — CRACKED (FWD CARGO) · airframe 64,974 hrs · 13,818 cycles

LOWER FWD CARGO FLOORBEAM IS CRACKED AT STA. Y=6-70, X=57.5 AND Z=-98. REPAIRED THE FLOORBEAM IAW SRM 53-40-51 REPAIR 1, FIG 201. MAJOR

Part: TEE FITTING — CRACKED (BS 1129) · airframe 64,974 hrs · 13,818 cycles

FRAME TEE FITTING CRACKED ALONG LONGERON 42R, BS 1129. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT TEE FITTING IAW DWG ADA3645, AND SRM 51-33-01.

Part: VERTICAL SUPPORT — CRACKED (RT WING TE) · airframe 64,974 hrs · 13,818 cycles

RIGHT WING T/E VERTICAL SUPPORT WAS CRACKED JUST FWD OF THE NR 1 SPOILER, INBD HINGE. REMOVED, FABRICATED, AND REPLACED THE SUPPORT IAW DWG ARC0297, AND SRM 51-33-01.

Part: THRUST REVERSER — CRACKED (NR 2 ENGINE) · airframe 64,974 hrs · 13,818 cycles

NR 2 ENGINE, RT THRUST REVERSER AFT FIXED INNER BARREL UPPER SKIN IS CRACKED. REPAIRED THE THRUST REVERSER FIXED INNER BARREL UPPER SKIN IAW EA 011-7830-01-A7297, REV I/R, AND EO MD11-7830-68788-A.

Part: TAIL CONE — CHAFED (BS 2163-2165) · airframe 64,974 hrs · 13,818 cycles

TAILCONE RT UPPER INTERNAL DOUBLER HAD SEVERAL WORN AREAS BETWEEN BS 2163.685 AND 2165.061, RBL 36.5, APPROXIMATELY BETWEEN WL 40 AND 61.5. REPAIRED THE TAILCONE IAW EA 011-5320-01-A7300, REV I/R, AND EO MD11-5350-68853-A.

Part: INTERCOSTAL — CRACKED (TAIL CONE) · airframe 64,974 hrs · 13,818 cycles

INSPECTION TYPE:2C, TAIL CONE LT CENTER GUIDE PIN ATTACH INTERCOSTAL IS CRACKED. REMOVED AND REPLACED TAIL CONE LT CENTER GUIDE PIN INTERCOSTAL IAW DWG AKC7520 AND SRM 51-31-01, 51-33-01 AND 51-35-01.

Part: SKIN — CHAFED (NR 1 FAN COWL) · airframe 64,974 hrs · 13,818 cycles

NR 1 ENGINE. OTBD FAN COWL UPPER FWD DOOR HINGE FITTING WAS CHAFED. REPAIRED THE SKIN IAW EA 011-7110-01-A7299, REV I/R, AND EO MD11-7110-68797-A.

Part: LATCH — GOUGED (THRUST REVERSER) · airframe 64,974 hrs · 13,818 cycles

NR 1 ENGINE OTBD THRUST REVERSER LATCH DOOR WAS GOUGED. REPAIRED LATCH DOOR IAW EA 011-7110-01-A7302, REV I/R, AND EO MD11-7830-68843-A.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 64,974 hrs · 13,818 cycles

INSPECTION TYPE:2C, INBD SUPPORT BRACKET BROKEN AT FUELING CONTROL PANEL IN RT WING L/E. REMOVED FABRICATED AND INSTALLED REPLACEMENT BRACKET PER DWG ARB2382 AND SRM 51-35-01. (MINOR)

Part: SKIN — CHAFED (BS 1153) · airframe 64,974 hrs · 13,818 cycles

EXTERIOR FUSELAGE SKIN HAD CHAFE DAMAGE AT BS 1153, LONGERON 44L. REPAIRED THE SKIN IAW EA 011-5330-01-A7301, REV I/R, AND EO MD11-5330-68946-A.

Part: INLET — CRACKED (NR 2 ENGINE) · airframe 64,970 hrs · 13,816 cycles

INSPECTION TYPE:2C, NR 2 ENG INLET L/E SKIN IS CRACKED AT THE 6 O'CLOCK POSITION. STOP DRILLED CRACK AND WELD REPAIRED PER SRM 54-10-01 REPAIR 4 /DPS10.301. (MINOR)

Part: SKIN — BENT (R2 DOOR) · airframe 64,970 hrs · 13,816 cycles

R2 DOOR EXTERNAL SKIN WAS BENT IN THREE PLACES. REPAIRED THE R2 DOOR EXTERIOR SKIN IAW EA 011-5210-01-A7304, REV I/R, AND EO MD11-5210-68944-A.

Part: STOWAGE BOX — CRACKED (LIFE VEST) · airframe 64,564 hrs · 13,680 cycles

SUPERNUMERARY SEAT, RT SIDE LIFE VEST STORAGE COMPARTMENT DOOR, LOWER HINGE MISSING AND PLASTIC HOUSING CRACKED. R & R THE STORAGE COMPARTMENT ASSY AMM 25-60-00.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 64,564 hrs · 13,680 cycles

EMERGENCY LIGHTS TEST SHOWED THE NR 1 BATERY LOW. OPS CHECKED THE EMERGENCY LIGHTING BATTERY POWER SUPPLY IAW AMM 33-51-01 CHECKED OK

Part: CABLE — BROKEN (L1 DOOR) · airframe 64,521 hrs · 13,667 cycles

WIRE CABLE FOR THE L1 DOOR FOUND BROKEN AND HANGING OUT OF CEILING. CABLE REMOVED. L1 DOOR UPPER DRIVE CABLE ASSY REPLACED IAW AMM 52-11-03, REV 90.05.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 64,337 hrs · 13,628 cycles

INSPECTION TYPE: PDC, FOUND DURING PDC EMERGENCY BATTERY POWER SUPPLY, NR 1 LOW. THE BATTERY WAS REPLACED IAW AMM 33-51-01-401, REV 90.04. TESTED SATISFACTORY.

Part: PULLEY — FAILED (L1 DOOR) · airframe 64,191 hrs · 13,598 cycles

L1 DOOR FWD DRIVE CABLE PULLEY HAS COME APART IN CEILING. R & R THE L1 DOOR FWD DRIVE CABLE PULLEY IAW AMM 52-11-05. OPS CHECKED GOOD.

Part: ANTI-ICE VALVE — FAILED (LT WING) · airframe 64,013 hrs · 13,554 cycles

DURING TAKEOFF, A LEVEL 2 WING ANTI-ICE DISAGREE, LT SIDE DEPARTED ICING CONDITIONS DUMPED 118,000LBS FUEL AND DIVERTED. REPLACED THE LT WING ANTI-ICE VALVE IAW MM 30-11-01-401, AND SECURED THE DIFFERENTIAL PRESSURE SENSOR IAW MM 30-11-02-401, OPS TESTED THE WING ANTI-ICE IAW MM 30-11-00-501, TEST PASSED, ESC RTS PASSED IAW MM 30-11-00-501, PSC 1 & 2 RTS PASSED IAW MM 36-10-02-501.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 63,834 hrs · 13,502 cycles

INSPECTION TYPE:N/AEMERGENCY LIGHT LEFT BTRY 1 LOW MSG ON DURING TESTREPLACED BTRY PACK NO HELP ALL LIGHTS WORK PLACE TEST FUNCTION INOP PER MEL 33-50-2. C/W DMP 33-50-2. MM33-51-01-4.

Part: SMOKE BARRIER — LOOSE (MCD) · airframe 63,587 hrs · 13,436 cycles

MCD FWD WALL LEFT SIDE SMOKE BARRIER CURTAIN LOOSE. SECURED MCD FWD WALL LEFT SIDE SMOKE BARRIER CURTAIN AS REQUIRED.

Part: DUMP VALVE — WARNING LIGHT (NR 2) · airframe 63,129 hrs · 13,300 cycles

NR 2 DUMP VALVE LIGHT DISAGREE ILLUMINATED. CHECKLIST COMPLIED WITH.

Part: WARNING MESSAGE — FALSE ACTIVATION (EMERGENCY LIGHTS) · airframe 62,846 hrs · 13,205 cycles

FOUND EMERGENCY LIGHT BATTERY 1 LOW ALERT DISPLAYED DURING TEST. TESTED IAW AMM 33-51-01-000.

Part: CABLE — FAILED (PAX DOOR) · airframe 61,224 hrs · 12,808 cycles

L1 DOOR INOPERATIVE. REPLACED THE DRIVE CABLE AND SUPPORT ASSEMBLY. OPS OK. IAW MM 52-11-09-000-801.

Part: DRIVE SYSTEM — STUCK (L1 DOOR) · airframe 61,219 hrs · 12,805 cycles

L1 DOOR WILL NOT OPEN. REPLACED DRIVE CABLE AND SUPPORT ASSY. OPS CHECKED GOOD IAW MM 52-11-09-000-801.

Part: STRUCTURE — WORN (THRUST REVERSER) · airframe 60,655 hrs · 12,611 cycles

INSPECTION TYPE: 1C, LOWER CASCADE SUPPORT RING BEARING LUG BORE WORN BEYOND REPAIRABLE LIMITS. R & R NR 1 THRUST REVERSER IAW AMM 78-13-01-000-868 AND -400-868.

Part: RUB STRIP — DAMAGED (NR 2 NACELLE) · airframe 60,655 hrs · 12,611 cycles

INSPECTION TYPE: 1C, NR 2 ENGINE LT FAN COWL, T/E RUBSTRIP CHAFE DAMAGE. REPAIRED IAW EA 011-7110-01-A6298, REV. IR AND EO MD11-5420-60987-A.

Part: SKIN — GOUGED (LT WING) · airframe 60,655 hrs · 12,611 cycles

INSPECTION TYPE: 1C, LT WING FIXED L/E UPPER SURFACE IS GOUGED BETWEEN XOS 1185 AND 1191. REPAIRED LT WING FIXED L/E UPPER SKIN BETWEEN XOS 1185 AND XOS 1191 IAW EA 011-5730-01-A6296-IR, DATED 06/10/2016 AND UPS EO 5730-61025-A, DATED 06/10/2016.

Part: TRUNNION — CRACKED (NLG) · airframe 60,655 hrs · 12,611 cycles

INSPECTION TYPE:1C, NLG LT TRUNION FITTING CRACKED ADJACENT TO TRUNION PIN BOSS, BS 582, Z=-114, X=24, REPAIRED CRACKED TRUNION FITTING IAW SRM 53-10-14, REPAIR 2, FIG 202.

Part: SHEAR TIE — CRACKED (BS 2084) · airframe 60,655 hrs · 12,611 cycles

INSPECTION TYPE:1C, SHEAR TIE CRACKED IN 311 COMPARTMENT CEILING, BS 2084. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SHEAR CLIP IAW DWG AJC7029, SRM 51-33-01, 51-35-01.

Part: INTERCOSTAL — CRACKED (MLG WHEEL WELL) · airframe 60,655 hrs · 12,611 cycles

INSPECTION TYPE:1C, UPPER INTERCOSTAL CRACKED IN LT MAIN WHEEL WELL. REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW DWG AEA0218, SRM 51-33-01, 51-35-01.

Part: INTERCOSTAL — CRACKED (RH WHEEL WELL) · airframe 60,655 hrs · 12,611 cycles

INSPECTION TYPE:1C, UPPER INTERCOSTAL CRACKED IN RT WHEEL WELL. REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW DWG AEA0218, SRM 51-33-01, 51-35-01.

Part: DOUBLER — CHAFED (RT WING) · airframe 60,655 hrs · 12,611 cycles

INSPECTION TYPE: 1C, RT WING FIXED LEADING EDGE EXTERNAL DOUBLER HAS CHAFE DAMAGE BS XOS 442-467 ACCOMPLISHED BLEND REPAIR ON RT WING FIXED L/E EXTERNAL DOUBLER IAW EA 011-5700-01-A6289, REV I/R AND EO MD11-5700-60939-A.

Part: DOUBLER — CRACKED (RT WING) · airframe 60,655 hrs · 12,611 cycles

INSPECTION TYPE: 1C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED XOS 758-763. REPAIRED NOTED BEADED DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 203.

Part: SKIN — CRACKED (RT WING) · airframe 60,655 hrs · 12,611 cycles

INSPECTION TYPE:1C, RT WING FIXED L/E SKIN CRACKED ON LOWER SURFACE NEAR BS XOS 720. REPAIRED L/E SKIN IAW SRM 57-40-02. REPAIR 7, FIG 201.

Part: STRINGER — CRACKED (RT WING) · airframe 60,655 hrs · 12,611 cycles

INSPECTION TYPE:1C, PREVIOUSLY INSTALLED REPAIR AT RT WING L/E STRINGER FOUND CRACKED AT BS XOS.906. R & R REPAIR DOUBLER IN RT WING L/E SRM 57-40-03, REPAIR 1, FIG 201.

Part: SKIN — CRACKED (LT WING) · airframe 60,655 hrs · 12,611 cycles

INSPECTION TYPE:1C, LT WING FIXED L/E EXTERIOR SKIN CRACKED AT NR 12 SLAT TRACK CUTOUT BS XOS776. REPAIRED LT WING SKIN BS XOS.776 IAW SRM 57-40-02, REPAIR 7, FIG 201.

Part: SKIN — CRACKED (LT WING) · airframe 60,655 hrs · 12,611 cycles

INSPECTION TYPE:1C, LT WING FIXED L/E EXTERIOR SKIN CRACKED AT INBD END OF REFUELING DOOR CUTOUT, BS XOS611. REPAIRED NOTED CRACK IAW SRM 57-40-02, REPAIR 18, FIG 201.

Part: SKIN — DENTED (THRUST REVERSER) · airframe 60,655 hrs · 12,611 cycles

INSPECTION TYPE:1C, REF EO MD11-7830-60613-A NR 2 LT REV INNER BARREL EXTERIOR SKIN. REQUIRES PERMANENT REPAIR. REPAIR NR 2 LT REV SKIN IAW EA 011-7830-01-A6279, REV. IR AND EO MD11-7830-60928-A.

Part: STRINGER — CRACKED (LT WING) · airframe 60,655 hrs · 12,611 cycles

INSPECTION TYPE:1C, LT WING FIXED L/E INNER STRINGER CRACKED NEAR BS XOS906. REPAIRED CRACKED STRINGER IAW SRM 57-40-03, REPAIR 1, FIG 201.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 60,437 hrs · 12,559 cycles

EMERGENCY LIGHT BATTERY 1 LOW LEVEL 1 ALERT DURING EMERGENCY LIGHT TEST. R & R EMERGENCY LIGHTING BATTERY POWER SUPPLY IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 58,782 hrs · 12,131 cycles

HOLE IN FUSELAGE APPROXIMATELY 3 FT FWD OF FWD LOWER CARGO DOOR. REPAIRED IAW EO 533-58286A. MAJOR REPAIR.

Part: SKIN — PUNCTURED (BS 850) · airframe 58,782 hrs · 12,131 cycles

PUNCTURE IN FUSELAGE AT BS 850 BETWEEN STRINGERS 34 & 35R. REPAIRED IAW EO MD11-5330-58286-A & SRM 53-00-01, REPAIR 8.

Part: CONTAINER — BROKEN (COCKPIT) · airframe 58,668 hrs · 12,116 cycles

F/O SEAT IS HITTING EVAS CONTAINER WHEN SEAT IS FULL. AFT CONTAINER TOP BROKEN WITH REF TO AMM 25-69-00. CHECKED AND INS EVAS CLOSED TOP, VELCRO FLAPS, MOVED SEAT SEVERAL TIMES FULL FWD OF AFT POSITIONS NOT STRIKING EVAS CONTAINER TOP NOT BROKEN VELCO FLAPS WERE UNDER RESTORED TO ORGINAL SERVICABLE CONDITION.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 58,166 hrs · 11,987 cycles

EMERGENCY LIGHTS INOPERATIVE T/S IAW FIM 33-52-01-00, BLOCKS 1-15. FOUND WIRE B362-154-20 SHORTED TO GROUND, REF WDM 33-52-01. REPAIRED WIRE IAW SWPM 20-10-03, EMERGENCY LIGHTS OPS NORMAL. PRIOR TO REPAIRING WIRE, REPLACED POWER SUPPLY IAW MM 33-51-01, NO HELP. IPC REF 33-51-01-05-015.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,131 hrs · 11,968 cycles

EMERGENCY LIGHTS INOPERATIVE. R & R EMERGENCY LIGHT SWITCH. S1-346 AND RELAY R2-5700 IAW WDM 33-51-01, PAGE 6. OPS TEST OF EMERGENCY SYSTEM IAW MM 33-50-00-700-802 OK.

Part: RELAY — FAILED (EMERGENCY LIGHTS) · airframe 58,026 hrs · 11,939 cycles

EMERGENCY LIGHTS INOPERATIVE, PERFORMED FIM PROCEDURE 33-52-00. R & R RELAY R2-5700 IAW WDM 33-51-01. OPS CHECK GOOD, EFF REF: IPC 24-51-17-06, 145.

Part: WIRE — BURNED (RT WING) · airframe 58,004 hrs · 11,932 cycles

NR 3 FWD MAIN TANK PUMP INOPERATIVE, AUTO MODE. T/S FOUND T/B S3-377 WITH BURNED, CHARRED, LOOSE WIRES ON TERMINALS. R & R TB S3-377 IAW SWPM 20-20-03 & WDM 28-22-03 SCH 4, PG 3.1. ALSO, REPLACED RCCB B1-677, L/P 805137 I-2 & CFD U1-75B, LP 805137 I-3 AS PRECAUTION FSC RTS PASSENGER IAW 28-08-01-501, REVIEWED MEL 28-22-1-4-1, DMP REVERSED SYS NORMAL M5.

Part: RELAY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,913 hrs · 11,906 cycles

EMERGENCY LIGHTS INOPERATIVE. R & R RELAY, OPS CHECKED GOOD IAW 33-50-00.

Part: STRUCTURE — GOUGED (LT WING) · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE:4C, LT WING FIXED L/E OTBD END CAP HAS MULTIPLE WEAR DAMAGE/GOUGE AT UPPER SURFACE. ACCOMPLISHED REPAIR ON LT WING FIXED L/E OTBD END CAP REF SRM 57-40-01 REPAIR 16 PARA 7. MAJOR REPAIR.

Part: SKIN — WORN (RT WING) · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE:4C, RT OTBD WING FIXED L/E REPAIR DOUBLER HAS WEAR DAMAGE JUST INBD OF TELESCOPIC DUCT CUT OUT. REPAIRED RT OTBD WING FIXED L/E IAW EA 011-5730-01-A5757, REV I/R AND EO MD11-5730-56866-A. MAJOR REPAIR.

Part: LONGERON — CORRODED (BS 1541) · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE:4C, LONGERON 38R CORRODED AT STA 1541. ACCOMPLISHED REPAIR TO LONGERON 38R, STA 1541 IAW EA 011-5310-01-A5747 AND EO MD11-5310-56840-A. MAJOR REPAIR.

Part: LONGERON — CORRODED · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE:4C, CENTER CARGO LONGERON 39R HAS CORROSION AT STA 5-113 ACCOPLISHED PERMANENT REPAIR ON CENTER CARGO LONGERON 39R FROM STA 5-93 TO 5-123 IAW SRM 53-00-05 REPAIR 1, FIG 202.

Part: LONGERON SPLICE — CRACKED · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE:4C, DISCOVERED CENTER CARGO LONGERON SPLICE CRACKED STA 5-123, L37R. R & R CENTER CARGO LONGERON SPLICE STA 5-123, L37R IAW SRM 51-33-01.

Part: FRAME — MECHANIC ERROR (BS 1712) · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE:4C, HOLE DRILLED THROUGH EDGE OF FRAME AND INTERCOSTAL AT STA 1712 L49R. REPAIRED FRAME AND INTERCOSTAL IAW EA 011-5310-01-A5753, REV IR AND EO MD11-5310-56881-A.

Part: LONGERON — CORRODED · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE:4C, LONGERON 46L CORRODED AT STA. 5-113. REPAIRED L46L BETWEEN STA. 5-103-5-123 IAW EA 011-5310-01-5746A REV IR AND EO MD11-5310-56885-A.

Part: LONGERON — CORRODED · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE:4C, LONGERON 45RT CORRODED AT STA 5-113 REPAIRED L45R BETWEEN STA 5-103 AND 5-123 IAW EA 011-5310-01-A5748 REV IR AND EO MD11-5310-56883-A.

Part: LONGERON SPLICE — CORRODED (CARGO BAY) · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE:4C, LONGERON SPLICE STRAP IN CENTER CARGO BILGE HAS CORROSION, STA 5-73 TO 5-53 L48L. R & R CENTER CARGO LONGERON SPLICE STRAP STA 5-73 TO 5-53 L48L IAW SRM 51-33-01.

Part: LONGERON — CORRODED (BS 1601) · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE:4C, LONGERON 48LT CORRODED AT STA 1601. REMOVED, FABRICATED AND INSTALLED REPLACEMENT LONGERON 48LT BETWEEN STA 1534-1706 IAW EA 011-5310-01-A5736, REV IR AND EO MD11-5310-56745- A.

Part: TORQUE TUBE — CHAFED (R1 DOOR) · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE:4CR1 DOOR LOWER TORQUE TUBE HAS CHAFE DAMAGE AT STA Y=434. ACCOMPLISHED PERMANENT REPAIR ON R1 DOOR LOWER TORQUE TUBE IAW EA 011-5210-01-A5754 REV I/R AND EO MD11-5210-56821-A.

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE:4C, DISCOVERED CORROSSION ON MAIN CARGO CENTER WING TANK UPPER SKIN AT STRINGER 15 XCW =-24. ACCOMPLISHED REPAIR ON MAIN CARGO CENTER WING TANK UPPER SKIN AT STRINGER 15 XCW = -24 IAW EA 011-5730-01-A5751, REV I/R AND EO MD11-5310-56853-A.

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE:4C, DISCOVERED CORROSION ON MAIN CARGO CENTER WING TANK UPPER SKIN AT STRINGER 15 XCW=21, ACCOMPLISHED REPAIR ON MAIN CARGO CENTER WING TANK UPPER SKIN AT STRINGER 15 XCW =21 IAW EA 011-5730-01-A5751, REV I/R AND EO MD11-5730-56853-A.

Part: LONGERON — CRACKED (BS 1305) · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE:4C, MAIN CARGO LONGERON 27R CRACKED AT BS 1305. ACCOMPLISHED PERMANENT REPAIR ON LONGERON 27 AT STA 1305 IAW 011-5310-01-A5752 AND EO MD11-5310-56845-A.

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE:4C, DISCOVERED CORROSION ON MAIN CARGO CENTER WING TANK UPPER SKIN STRINGER 22 XCW = - 109ACCOMPLISHED REPAIR ON MAIN CARGO CENTER WING TANK UPPER SKIN AT STRINGER 22 XCW = -109 IAW EA 011-5730-01-A5751, REV I/R AND EO MD11-5730-56853-A.

Part: LONGERON — CORRODED (BS 1641-1661) · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE:4C, CENTER CARGO LONGERON 36R HAS CORROSION BETWEEN STA 1641 TO 1661. R & R CENTER CARGO LONGERON 36R FROM STA 5-113 TO 1661 IAW EA 011-5310-01-A5737, REV I/R AND EO MD11-5310-56746-A.

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE:4C, DISCOVERED CORROSION ON MAIN CARGO CENTER WING TANK UPPER SKIN AT STRINGER 15 XCW =-75 ACCOMPLISHED REPAIR ON MAIN CARGO CENTER WING TANK UPPER SKIN AT STRINGER 15 XCW =-75 IAW EA 011-5730-01-A5751, REV I/R AND EO MD115730-56853-A.

Part: LONGERON — CORRODED (CARGO BAY) · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE:4C, DISCOVERED CORROSION ON CENTER CARGO LONGERON STA 5-53 L35R ACCOMPLISHED SPLICE REPAIR ON CENTER CARGO LONGERON STA 5-32 TO 5-73 L35R IAW SRM 53-00-05, REPAIR 1, FIG 202.

Part: SKIN — CRACKED (BS 1309) · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE: 4C, MAIN CARGO R3 DOOR JAMB LOWER FWD SKIN CRACKED STA 1309 TO 1315. ACCOMPLISHED PERMANENT REPAIR ON R3 DOOR JAMB LOWER FWD SKIN STA 1309 TO 1315 IAW SRM 53-40-15, REPAIR 3, FIGURE 201.

Part: SEAT TRACK — DAMAGED (BS 495) · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE:4C, MAIN CARGO SEAT TRACK BENT AND CRACKED AT STA 495, LBL 27. ACCOMPLISHED PERMANENT REPAIR ON MAIN CARGO SEAT TRACK FROM STA 467 TO STA 525 IAW EA 011-5310-01-A5749, REV I/R AND EO MD11-5310-56842-A.

Part: SKIN — CRACKED (BS 1256) · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE: 4C, MAIN CARGO L3 DOOR JAMB LOWER FORWARD SKIN CRACKED STA 1256.75. ACCOMPLISHED PERMANENT REPAIR ON L3 DOOR JAMB LOWER FORWARD SKIN AT STA 1256.75 IAW SRM 53-40-15, REPAIR 3, FIGURE 201.

Part: STRINGER — CRACKED · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE:4C, CTR WING TANK STRINGER 51 CRACKED NEAR XCW-46. REPAIRED STRINGER 51 BETWEEN XCW-32 AND XCW-62 IAW EA 011-5710-01-A5725, REV IR AND EO 5710-56806-A.

Part: STRINGER — CRACKED (RT WING) · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE:4C, DISCOVERED CRACK IN RT WING UPPER STRINGER 13 BETWEEN STA XORS 562 ABD XORS 592. ACCOMPLISHED PERMANENT SPLICE REPAIR ON RT WING UPPER STRINGER 13 BETWEEN STA XORS 562 AND 592 IAW EA 011-5710-01-A5739, REV I/R AND EO MD11-5710-56841-A.

Part: STRINGER — CRACKED · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE:4C, CENTER WING TANK LOWER STRINGER 47 CRACKED AT XCW = 17, -17 AND -46.5. ACCOMPLISHED TIME LIMITED SPLICE REPAIR ON CENTER WING TANK LOWER STRINGER 47 AT XCW =17, -17 AND -46.5 IAW VT-SAA EA 011-5710-01-A5726, REV I/R AND EO MD11-5710-56851-A.

Part: STRINGER — CRACKED (LT WING) · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE:4C, LT WING STRINGER 43 CRACKED OTBD OF XORS 562. REPAIRED STRINGER 43 LT OTBD OF XORS 562 IAW EA 011-5710-01-A5738, REV. IR AND EO MD11-5710-56882-A, MAJOR.

Part: STRINGER — CRACKED (RT WING) · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE:4C, RT WING STRINGER 10 CRACKED STA XORS 737 TO 772 ACCOMPLISHED PERMANENT REPAIR ON RT WING STRINGER 10 STA XORS 737 TO 772 IAW SRM 57-00-03, REPAIR 5, FIGURE 202.

Part: SKIN — CRACKED (RWS 683-713) · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE:4C, DISCOVERED 2 EA CRACKS ON RT WING SKIN LOWER FUEL ACCESS DOOR LANDING HOLES STA XORS 683.40 TO XORS 713.65. ACCOMPLISHED 2 EA BUSHING REPAIRS TO RT WING SKIN LOWER FUEL ACCESS DOOR LANDING HOLES STA XORS 683.40 TO XORS 713.65 IAW SRM 57-20-02, REPAIR 5, FIGURE 201.

Part: STRINGER — CRACKED (RT WING) · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE:4C, DISCOVERED RT WING UPPER STR 15 CRACKED BETWEEN STA XORS 433-455. ACCOMPLISHED PERMANENT REPAIR ON RT WING UPPER STR 15 BETWEEN XORS 433 AND XORS 455 IAW EA 011-5710-01-A5745, REV I/R AND EO MD11-5710-56843-A.

Part: LONGERON SPLICE — CRACKED · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE:4C, LONGERON 10RT SPLICE FITTING CRACKED AT STA 5-123. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SPLICE FITTING IAW DWG A5A7112 AND SRM 51-33-01.

Part: FLOOR PANEL — PUNCTURED (MAIN CABIN) · airframe 57,913 hrs · 11,906 cycles

INSPECTION TYPE: 4C, MAIN CABIN FLOOR PANEL 261FF PUNCTURED REPAIRED PANEL 261FF IAW SRM 53-00-50, PARA 4, FIG 6.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHTS STAY ON WITH LIGHT SWITCH OFF. R & R EMERGENCY LIGHTING BATTERY POWER SUPPLY IAW MM 33-51-01. OPS CK GOOD. REF IPC 33-51-10-01, ITEM 35-40.

Part: CONTROL UNIT — INOPERATIVE (FUEL QTY)

DURING CLIMB, RECEIVED LEVEL 2 FUEL OFF SCHEDULE. DURING CRUISE, RECEIVED 4 MORE LEVEL 2 ALERTS FUEL OFF SCHEDULE. ACFT DIVERTED. R & R FUEL QTY DATA CONTROL UNIT IAW AMM 28-41-91-4. R & R SEM IAW 28-41-92-4.

Part: CHARGER — INOPERATIVE (ELECTRICAL)

EMERGENCY POWER TEST FAIL. R & R BATTERY CHARGER IAW AMM 24-34-03, IPC 24-34-03-01-001J, IPC 243 4-02-01-270. EMERGENCY POWER TEST PASS.

Part: SKIN — GOUGED (LT WING) · airframe 55,580 hrs · 11,339 cycles

INSPECTION TYPE:1C, LT WING FIXED L/E EXTERIOR SKIN GOUGED UNDER OTBD END OF NR 8 SLAT NEAR XOS 1186. REPAIRED LT WING L/E EXTERIOR SKIN AT NOTED LOCATION IAW EA 011- 5730-01-A5069, REV IR AND EO MD11-5730-53350-A.

Part: FLOOR PANEL — CRACKED (BS 474 LBL 58) · airframe 55,580 hrs · 11,339 cycles

INSPECTION 1C, RCB AREA COMPOSITE FLOOR PANEL BROKEN AT CORNER, BS 474, LBL 58. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FLOOR PANEL IAW EO MD11-5320-27386-C AND M-5320-38342-B.

Part: FLOOR PANEL — CORRODED (BS 480) · airframe 55,580 hrs · 11,339 cycles

INSPECTION 1C, RCB AREA FLOOR PANEL WSP0790-501 CORRODED AT BS 480. R & R FLOOR PANEL IAW AMM 53-21-01 AND SRM 51-30-00.

Part: SEAT TRACK — CORRODED (BS 478) · airframe 55,580 hrs · 11,339 cycles

INSPECTION 1C MAIN CABIN SEAT TRACK CORRODED AROUND GALLEY ANCHOR FITTING BS 478 RBL 75.25. REPAIRED SEAT TRACK BETWEEN BS 475-485 IAW SRM 53-00-52, REPAIR 4, FIG. 201.

Part: FLOOR PANEL — CORRODED (BS 483) · airframe 55,580 hrs · 11,339 cycles

INSPECTION 1C, RCB AREA FLOOR PANEL CORRODED BS 483, RBL 52. R & R FLOOR PANEL IAW AMM 53-21-10 & SRM 51-30-00.

Part: SEAT TRACK — CORRODED (BS 470) · airframe 55,580 hrs · 11,339 cycles

INSPECTION 1C, MAIN CABIN SEAT TRACK CORRODED BS 470, LBL 9. REMOVED FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK IAW DWG SP10530218, SRM 51-31-01 AND SRM 51-33-01.

Part: FLOOR PANEL — CORRODED (BS 475-484) · airframe 55,580 hrs · 11,339 cycles

INSPECTION 1C, RCB AREA FLOOR PANEL CORRODED BS 475-484, LBL 58. R & R FLOOR PANEL AMM 53-21-10 & SRM 51-30-00.

Part: FLOOR PANEL — CORRODED (BS 475-484) · airframe 55,580 hrs · 11,339 cycles

INSPECTION 1C, RCB FLOOR PANEL CORRODED BS 475-484, LBL 26. R & R FLOOR PANEL IAW AMM 53-21-10 AND SRM 51-30-00.

Part: FLOOR PANEL — CORRODED (BS .475-484) · airframe 55,580 hrs · 11,339 cycles

INSPECTION 1C, RCB AREA FLOOR PANEL CORRODED BS 475-484, RBL 34. R & R FLOOR PANEL IAW AMM 53-21-10 & SRM 51-30-00.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 55,580 hrs · 11,339 cycles

1C INSPECTION, CORRODED FLOOR PANEL AT BS 425 BETWEEN X=27.5 AND 80.5. REPAIRED FLOOR PANEL IAW EA 011-5300-01-A5056, REV I/R, EO MD11-5310-53383-A AND 8100-9.

Part: FLOOR PANEL — CORRODED (BS 470) · airframe 55,580 hrs · 11,339 cycles

INSPECTION 1C, RCB AREA FLOOR PANEL CORRODED BS 470, LBL 19. R & R FLOOR PANEL IAW AMM 53-21-10 & SRM 51-30-00.

Part: SEAT TRACK — CORRODED (BS 470) · airframe 55,580 hrs · 11,339 cycles

INSPECTION 1C, MAIN CABIN SEAT TRACK CORRODED BS 470, RBL 36. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK BS 439-516 IAW DWG WSP0826 AND SRM 51-31-01.

Part: SEAT TRACK — CORRODED (BS 470) · airframe 55,580 hrs · 11,339 cycles

INSPECTION 1C, MAIN CABIN SEAT TRACK CORRODED BS 470, RBL 17. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK BS 439 - 516 IAW DWG WSP0826 AND SRM 51-31-01.

Part: FLOOR PANEL — CORRODED (BS 470) · airframe 55,580 hrs · 11,339 cycles

INSPECTION 1C, RCB AREA FLOOR PANEL CORRODED, BS 470, BL 0. R & R FLOOR PANEL IAW AMM 53-21-10 & SRM 51-30-00.

Part: DOUBLER — CRACKED (RT WING) · airframe 55,580 hrs · 11,339 cycles

INSPECTION 1C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED XOS 584-594. REPAIRED RT WING BEADED DOUBLER IAW SRM 57-40 -02, REPAIR 15, FIG.203.

Part: STRINGER — CRACKED (LT WING) · airframe 55,580 hrs · 11,339 cycles

INSPECTION 1C, LEFT WING STRINGER 11 CRACKED NEAR XORS 690. REPAIRED STRINGER IAW SRM 57-00 -03, REPAIR 5, FIG 202.

Part: STRINGER — CRACKED (LT WING) · airframe 55,580 hrs · 11,339 cycles

INSPECTION TYPE:1C, LEFT WING STRINGER 5 CRACKED AT XORS713. REPAIRED LT WING STRINGER 5 BETWEEN XORS 700-727 IAW EA 011- 5710-01-A5046, REV IR AND EO 5710-53371-A.

Part: WIRE — DAMAGED (ELECTRICAL)

AT ROTATION, MULTIPLE CIRCUIT BREAKERS COULD BE HEARD TRIPPING, LOST PFD DATA AND NUMEROUS OTHER INDICATIONS OF LOST EQUIP DECLARED EMERGENCY LANDED UNEVENTFULLY. FOUND MULTIPLE WIRES DAMAGED. WIRES REPAIRED.

Part: SKIN — DAMAGED (NR 7 SLAT)

RT WING NR 7 L/E SLAT SKIN DAMAGED. REPAIRED IAW EO-MD11-5750-57872-A.

Part: SLIDE — DEPLOYED (R1 DOOR)

R2 DOOR SLIDE BLOWN.

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR)

DURING BLOCK-IN, R1 DOOR SLIDE IS ACCIDENTALLY DEPLOYED, AIR BOTTLE IS ALSO DISCHARGED. SLIDE REMOVED. REPLACED SLIDE IAW AMM 25-61-400-801.

Part: GAUGE — OUT OF POSITION (R1 DOOR SLIDE)

NR 1 DOOR SLIDE PRESSURE INDICATOR NOT READABLE. APPEARS SLIDE PACK HAS SHIFTED DOWN AND PRESSURE GAUGE IS NOT READABLE. REPOSITIONED AS MUSH AS POSSIBLE TO ALIGN PRESS GAUGE WITH INSPECTION. GAUGE IS NOW VIEWABLE THROUGH WINDOW REF AMM 25-23-07-401, 25-61-01- 401, 25-61-06-601.

Part: CABLE — BROKEN (L1 DOOR)

L1 DOOR HAS A BROKEN MANUAL CRANK CABLE. OPEN

Part: CABLE — BROKEN (L1 MAIN ENTRY)

L1 MAIN ENTRY DOOR HAS A BROKEN MANUAL CRANK CABLE DEFERRED L1 DOOR IAW MEL 52-10-3-2. SYS PLACARDED ASSIGNED CONTROL M496809. R & R L1 DOOR AFT LOWER DRIVE CABLE ASSY - REF AMM 52-11-03, ADJUSTED CABLES REF AMM 52-11-02. THIS CLEARS M496809. PLACARD REMOVED IPC REF 52-11-05-05.

Part: B-NUT — LOOSE (OIL LINE)

DIVERSION - NR 1 ENGINE OIL QUANTITY DECREASED AT APPROX 1 QT IAW 30 MINUTES FOUND LOOSE B-NUT ON OIL PRESSURE TRANSMITTER. RETORQUED AND LEAK CHECKED OK.

Part: FORMER — CRACKED (LT WING) · airframe 52,891 hrs · 10,676 cycles

INSPECTION TYPE: 2C, LT WING FIXED L/E COMPT FORMER CRACKED NEAR STA XOS1025.5. REMOVED FABRICATED AND INSTALLED REPLACEMENT FORMER IN LT WING L/E IAW DWG ARB2920 AND SRM 51-31-01, 51-33-01.

Part: DOUBLER — CRACKED (RH XOS.768-772) · airframe 52,891 hrs · 10,676 cycles

INSPECTION TYPE:2C, RT WING FIXED L/E COMPT BEADED DOUBLER CRACKED NEAR XOS.769. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS.768-772 IAW SRM 57-40-02. REPAIR 15, FIG 203. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 52,891 hrs · 10,676 cycles

INSPECTION TYPE: 2C, RT WING FIXED L/E BEADED DOUBLER CRACKED NEAR XOS 626. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS 625-629 IAW EA 011-5730-01-A5359 REV IR AND EO MD11-5730-49013-A FAA 8100-9. MAJOR

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 52,891 hrs · 10,676 cycles

INSPECTION TYPE: 2C, RT INBD FLAP UPPER SKIN CRACKED AT XIFH 171.5 APPROX 7.25" FWD OF REAP SPAR PLANE. REPAIRED SKIN IAW SRM 57-00-01, REPAIR 1, FIG 201. (MAJOR)

Part: DOUBLER — CRACKED (RH XOS610-616) · airframe 52,891 hrs · 10,676 cycles

INSPECTION TYPE:2C, RT WING FIXED L/E COMPT INNER BEADED DOUBLER CRACKED NEAR XOS.613. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS.610-616 IAW SRM 57-40-02, REPAIR 15, FIG 202. (MAJOR)

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 52,891 hrs · 10,676 cycles

INSPECTION TYPE:2C, ONE INCH DENTED ON UPPER SURFACE OF RT INBD FLAP FIVE INCHES AFT OF REAR SPAR NEAR STA. XIFH195.3 REPAIRED DENT IAW SRM 57-00-01, REPAIR 1, FIG 201. (MAJOR)

Part: STRINGER — CRACKED (RT XOS.906) · airframe 52,891 hrs · 10,676 cycles

INSPECTION TYPE:2C, PREVIOUSLY INSTALLED REPAIR DOUBLER AT RT WING L/E PANEL 626DB ATTACH FLANGE CRACKED NEAR STA XOS 906 STRINGER. REMOVED FABRICATED AND INSTALLED REPLACEMENT DOUBLER AT RT WING L/E STA.906 IAW SRM 57-40-03, REPAIR 1 FIG 201. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 52,891 hrs · 10,676 cycles

INSPECTION TYPE: 2C, RT WING FIXED L/E COMPT BEADED DOUBLER CRACKED NEAR STA XOS 701. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS 698 - 703 IAW SRM 57-40-02, REPAIR 15, FIG 203. (MAJOR)

Part: SKIN — CRACKED (RT WING) · airframe 52,891 hrs · 10,676 cycles

INSPECTION TYPE:2C, REPAIR DOUBLER CHAFED AT RT WING SLAT DE-ICE DUCT CUT-OUT. R & R REPAIR DOUBLER AT RT WING L/E EXTERIOR BETWEEN XOS 443 - 464 IAW SRM 57-40-02. REPAIR 5, FIG 201.

Part: DOUBLER — CRACKED (RT WING) · airframe 52,891 hrs · 10,676 cycles

INSPECTION TYPE:2C, RT WING FIXED L/E COMPT BEADED DOUBLER CRACKED NEAR XOS 639. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS 636-648 IAW SRM 57-40-02, REPAIR 15, FIG 203.

Part: DOUBLER — CRACKED (LT WING) · airframe 52,891 hrs · 10,676 cycles

INSPECTION TYPE: 2C, LT WING FIXED L/E BEADED DOUBLER CRACKED NEAR XOS 627. REPAIRED BETWEEN XOS 625-629 IAW SRM 57-40-02, REPAIR 15, FIG 203. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 50,219 hrs · 10,004 cycles

INSPECTION TYPE:3C, LT WING FIXED L/E COMPT BEADED DOUBLER CRACKED IN 3 AREAS AT XOS 733. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS728-734 IAW SRM 57-40-02, REPAIR 9, FIG 203.

Part: SKIN — CHAFED (RT WING) · airframe 50,219 hrs · 10,004 cycles

INSPECTION TYPE:3C, DEEP CHAFING DAMAGE ON RT WING L/E FROM XOS431-465. REPAIRED RT WING L/E EXTERIOR SKIN BETWEEN STA XOS431-465 IAW SRM 57-40-02, REPAIR 5, FIG 201.

Part: DOUBLER — CRACKED (LT WING) · airframe 50,219 hrs · 10,004 cycles

INSPECTION TYPE:3C, LT WING FIXED L/E COMPT BEADED DOUBLER CRACKED IN 2 AREAS ST STA XOS646. REPAIRED LT WING FIXED L/E INTERNAL BEADED BETWEEN STA XOS643-648 IAW SRM 57-40-02, REPAIR 9, FIG 203 & EO MD11-5730-42916-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 50,219 hrs · 10,004 cycles

INSPECTION TYPE:3C, LT WING FIXED L/E COMPT BEADED DOUBLER CRACKED IN 3 AREAS AT XOS701. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS698-703 IAW SRM 57-40-03, REPAIR 9, FIG 203 AND EO MD11-5730-42916-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 50,219 hrs · 10,004 cycles

INSPECTION TYPE:3C, LT WING FIXED L/E COMPT BEADED DOUBLER CRACKED AT AFT END JUST ABOVE SLAT CABLE DRUM AT XOS 499. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BEWTEEN XOS494-500 IAW SRM 57-40-02, REPAIR 9, FIG 203 & EO MD11-5730-42916-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 50,219 hrs · 10,004 cycles

INSPECTION TYPE:3C, LT WING FIXED L/E COMPT BEADED DOUBLER CRACKED IN 2 BAYS AT STA XOS672 & XOS676. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS661-673 IAW SRM 57-40-02, REPAIR 9, FIG 203 AND EO MD11-5730-42916-A.

Part: DOUBLER — CRACKED (RT WING) · airframe 50,219 hrs · 10,004 cycles

INSPECTION TYPE:3C, CRACKED BEADED DOUBLER IN RT WING AT STA XOS670. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS667-673 IAW SRM 57-40-02, REPAIR 9, FIG 203 & EO MD11-5730-42916-A.

Part: RIB — CRACKED (LT WING) · airframe 50,219 hrs · 10,004 cycles

INSPECTION TYPE:3C, LT WING FIXED L/E COMPT RIB SUPPORT BRACKET CRACKED AT AFT END, JUST OTBD OF NR 2 SLAT TRACK. FABRICATED AND INSTALLED REPLACEMENT RIB IN LT WING FIXED L/E INTERIOR OTBD OF NR 2 SLAT TRACK.

Part: STRINGER CLIP — CRACKED (STA.2141 L1R) · airframe 50,219 hrs · 10,004 cycles

INSPECTION TYPE:3C, FRAME STA 2141, LONGERON 1L-TO-SKIN CLIP CRACKED. REPAIRED SHEAR TIE CLIP IN MAIN CABIN CEILING STA 2141, L1R IAW SRM 53-70-07, REPAIR 1, FIG 201.

Part: PUMP — INOPERATIVE (NR 2 ENG FUEL)

ON DESCENT, GOT LEVEL 0 ENGINE RPM LO, ATTEMPTED RESTART IN FLIGHT, UNSUCCESSFUL. EMERGENCY DECLARED. R & R ENGINE DRIVEN NR 2 ENGINE FUEL PUMP IAW MM 73-12-12-01-4. ENGINE STATS & RUNS NORMAL IAW MM 71-02-03. 5 MINUTE MINIMUM IDLE POWER.

Part: FLOORBOARD — DAMAGED (CARGO BAY)

BULK PIT 3 EA HOLES IN FLOOR. DAMAGE FOUND TO EXCEED LIMITS IN EO MD11-5320-17899-H. FABRICATED 3 NEW FLOORBOARD IAW MD11-5320-34874-B. PANEL CURED, REPAIR COMPLETE REF MD11-5320-34874-B.

Part: TANK — LEAKING (LAVATORY)

LAV TANK LEAKED INTO E&E COMPARTMENT CAUSING WIRES TO SHORT AND DAMAGE TO SEVERAL COMPONENTS. R & R WASTE TANK ASSY REF MM CHAP 38-31-02-4 THROUGH 3E(1)(D) XFER TO LMECA 020807. REF L/P 423363/3 FOR C/A. R & R THE FOLLOWING: AUX IRU, NR2 ADF RECEIVER, NR2 FCC, NR2 & 3 VHF, NR1 DMU, WIRE BUNDLES NR2 IRU, NR1 EEC B CHANNEL, ANCILLARY FUEL SYS CONTROLLER, INSULATION BLANKETS, UPPER EDGE CARGO DOOR JAMB SEAL.

Part: WIRE HARNESS — BURNED (E&E COMPARTMENT)

WIRE BUNDLE BURNED IN E & E COMPARTMENT - SUSPECT LAV LEAK. (OPEN)

Part: SWITCH — INTERMITTENT (DOOR OPEN)

LT ENTRY DOOR ELECT OPEN SWITCH INTERMITTENT.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHT BATTERY LOW LEVEL 1 WARNING RECEIVED DURING EMERGENCY LT TEST. R & R LIGHTS POWER SUPPLY REF MM 33-51-01-4. OPS CKS GOOD REFER MM 33-51-01-5.

Part: CRANK ASSY — CRACKED (FWD CARGO DOOR) · airframe 48,216 hrs · 9,520 cycles

INSPECTION TYPE:4C, LWR FWD CARGO DOOR, ACTUATION CTR DRIVE LINK/ARM FOUND CRACKED AS MARKED. REMOVED ARM AND INSTALLED NEW ARM IAW CMM 52-31-08, PGS 701-703.

Part: SKIN — CRACKED (NR 3 PYLON) · airframe 48,216 hrs · 9,520 cycles

INSPECTION TYPE:4C, NR 3 PYLON FAIRING 488EL OTBD SIDE SKIN HAS CRACK AT RIVET AT MARKED. REMOVED EXISTING DOUBLER, CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER AND FILLER AT NR 3 PYLON FAIRING 488EL OTBD SIDE SKIN REF DWG AUB7562 , SRM 51-38-01, SRM 54-00-00 FIG 204, SRM 54-05-41 PARA 5.

Part: ANGLE — CRACKED (HORIZONTAL STAB) · airframe 48,216 hrs · 9,520 cycles

INSPECTION TYPE:4C, RT HORZ STAB STA 323 RIB TO FRONT SPAR VERTICAL ATTACH ANGLE UPPER END HAS 3" LONG CRACK IN RADIUS. REMOVED ATTACH ANGLE AT RT HORZ STAB STA 323 RIB TO FRONT SPAR. FABRICATED AND INSTALLED ATTACH ANGLE REF DWG ALC8120 AND SRM 51-31-01 PARA 3 PG 1 AND SRM 51-33-01, PARA 8 TABLE 12, PG 30/31.

Part: LONGERON SPLICE — CRACKED (L39R) · airframe 48,216 hrs · 9,520 cycles

INSPECTION TYPE:4C, LOWER CTR CARGO LONGERON SPLICE FITTING HAS A CRACK AT STA 5-123 RH L- 39. REMOVED SPLICE FITTING AT 5-123 AND L39R. FABRICATED AND INSTALLED SPLICE FITTING, REF DWG A5A7114 AND SRM 51-33-01, PG 30/31, TABLE 12.

Part: VANE — DELAMINATED (RT WING TE FLAP) · airframe 48,216 hrs · 9,520 cycles

INSPECTION TYPE:4C, RT INBD FLAP VANE DELAMINATED, SEPARATION AT T/E AND DISTORTED AT OTBD UPPER SURFACE. R & R RT INBD FLAP VANE WITH SERVICABLE UNIT.

Part: VANE — DAMAGED (RT WING TE FLAP) · airframe 48,216 hrs · 9,520 cycles

INSPECTION TYPE:4C, RT OTBD FLAP VANE HAS EDGE DAMAGE AT LWR OTBD END REMOVED DAMAGE, PERFORMED WET LAY-UP REPAIR IAW STA-SA EA011-5750-01-A2616, REV A AND EO MD11-5750-39209-B.

Part: LONGERON — CORRODED (L38L) · airframe 48,216 hrs · 9,520 cycles

INSPECTION TYPE:4C, LOWER CTR CARGO LONGERON 38L HAS EXFOLIATED CORROSSION AT 5-113. REMOVED SPLICE AND CUT OUT DAMAGED AREA OF L38L AT STA 5-113. FABRICATED AND INSTALLED LONGERON SECTION AT L38L AND INSTALLED EXISTING PRODUCTION SPLICE REF SRM 53-00-05, REPAIR 1, TYPE 1 AND DWG A5A7046.

Part: LONGERON — CORRODED (L38R) · airframe 48,216 hrs · 9,520 cycles

INSPECTION TYPE:4C, LOWER CTR CARGO RT LONGERON 38 HAS CORROSSION AT STA 5-90. REMOVED DAMAGED LONGERON SEGMENT AT L38R AND STA 5-113. FABRICATED AND INSTALLED LONGERON REPAIR SEGMENT REF SRM 53-00-05, REPAIR 1, FIG 202.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 48,216 hrs · 9,520 cycles

INSPECTION TYPE:4C, LOWER CTR CARGO LONGERON HAS CORROSION FROM STA 5-81 TO 5-113 RT L36. REMOVED L36R SPLICE FITTING AND L36R FROM STA 5-5 TO 5-113. FABRICATED AND INSTALLED LONGERON SECTION FROM STA 5-5 TO 5-113 AND INSTALLED SPLICE FITTING REF DWG A5A7021 AND SRM 51-33-01, PG 30.

Part: LONGERON SPLICE — CRACKED (L35R) · airframe 48,216 hrs · 9,520 cycles

INSPECTION TYPE:4C, LOWER CTR CARGO LONGERON SPLICE FITTING AT STA 5-123 RT LONGERON 35 IS CRACKED. REMOVED SPLICE FITTING AT STA 5-123 AND L35R. FABRICATED AND INSTALLED REPLACEMENT SPLICE FITTING REF DWG A5A7114 AND SRM 51-33-01, PG 30 /31.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 48,216 hrs · 9,520 cycles

INSPECTION TYPE:4C, LOWER CTR CARGO RT LONGERON 35 HAS CORROSION AT 5-113. REMOVED DAMAGED SECTION OF LONGERON AT L35R FROM STA 5-103 TO STA 5-123. FABRICATED & INSTALLED LONGERON SECTION REPLACEMENT & SPLICE PLATE REF DWG A5A7020 AND SRM 53-00-05, REP 1.

Part: SKIN — DENTED (BS 1868 L3R) · airframe 48,216 hrs · 9,520 cycles

INSPECTION TYPE:4C, DEFERED ITEM D-429361 RT FUS DENT AT STA 1868 AND L3R. REMOVED DAMAGE AT STA 1868 AND L3R. FABRICATED AND INSTALLED REPAIR REF SRM 53-00-01, REPAIR 1, FIG 201, CLASS 1 AND RCD 388368.

Part: MEMBRANE — CRACKED (COCKPIT FLOOR) · airframe 48,216 hrs · 9,520 cycles

INSPECTION TYPE:4C, INSIDE AVIONICS COMPT 1ST OBSERVERS SEAT BOTTOM THROUGH HOLE ON FLOOR DAMAGE. BLENDED MEMBRANE BELOW 1ST OBSERVERS SEAT OUT OF LIMITS. FABRICATED AN D INSTALLED REPAIR RING DOUBLER REF EA 011-5310-01-A2580 AND EO MD11-5310-39127A.

Part: STRUCTURE — CRACKED (NR 1 SLAT)

DIVERSION - ENG VIBRATION EVM (NR 1) 1.0 (NR 2) .6 (NR 3) .8 MACH .831 FL 370 ENG NOISE & VIBRATION FELT THROUGH THE AIRFRAME. REDUCED POWER OF NR 1 ENG TO MACH .82 EVM .9 .4 .5 MACH .81 EVM .9 .5 .8. LT WING FILLET ASSY REPLACEMENT FOUND FILLET ATTACH POINT TO NR 1 SLAT CRACKED. REF LP 412451.

Part: SKIN — MISREPAIRED (BS 1139-1159) · airframe 46,216 hrs · 9,046 cycles

INSPECTION TYPE:SVDO GAIN ACCESS TO REPAIR AT STA 1139 TO 1159 BETWEEN LONGERON 3R TO 5R INTERNAL FUSELAGE SKIN AND VERIFY REPAIR DOUBLER MATERIAL F1-12. VERIFIED MATERIAL AND THICKNESS IS NOT PER SRM. REMOVED, FABRICATED AND INSTALLED NEW INTERNAL REPAIR DOUBLER PER SAA EA 011-5330- 01-A2067 AND IPXA EO MD11-5330-34301-B.

Part: DOUBLER — DAMAGED (SPOILER) · airframe 45,780 hrs · 8,929 cycles

INSPECTION TYPE:1C NEED TO ACCOMPLISH REPAIR ON LT NR 1 SPOILER. REPAIRED DAMAGED AREA AT XISP 216 REF EO MD11-5750-34295-B AND EA 011-5755-01-A1908.

Part: SLAT — MISREPAIRED (LT WING) · airframe 45,780 hrs · 8,929 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQ 281-W3-01 LT WING NR 1 SLAT BETWEEN STA XIS204 TO XIS211 DOES NOT CORRELATE WITH EFN2812005118 FIG 3 EN1642-05 CALL OUT ON DOUBLER 17 ROWS FASTENERS, INSTALLED 16 ROWS ONLY. REMOVED EXISTING REPAIR AT LT WING NR 1 SLAT LOWER SKIN AT XIS207.844 FABRICATED AND INSTALLED REPLACEMENT REPAIR REF EO MD11-5750-34286-A AND EA 011-5754-01-A1914.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 45,780 hrs · 8,929 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQ 281-F1-01 EXTERNAL REPAIR DOUBLER ON RT FORWARD FUSELAGE SKIN BETWEEN STA 485-515 BETWEEN L27R-30R NOT CORRELATE TO SRM REPAIR. REMOVED EXISTING REPAIR ON RT FORWARD FUSELAGE SKIN AT STA 485-515 BETWEEN L27R AND L30R. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF EO MD11-5330-34285-A AND EA 011-5330-01-A1917.

Part: SKIN — MISREPAIRED (BS 1139-1159) · airframe 45,780 hrs · 8,929 cycles

INSPECTION TYPE: 1C REPAIR SURVEY SEQUENCE NR 281-F1-12 UPPER RT CTR FUSELAGE SKIN REPAIR STA 1139-1159, L-3R - L5R NO EFN, NOT IAW SRM. ACCOMPLISHED EA 011-5330-01-A1911 AND EO MD11-5330-34301-A.

Part: SKIN — MISREPAIRED (CTR WING BOX) · airframe 45,780 hrs · 8,929 cycles

INSPECTION TYPE: 1C REPAIR SURVEY SEQ W11-01 REPAIR DOUBLER ON RT CTR WING BOX UPPER SURFACE BETWEEN RBL 96-112 AND STRS 16-19 REQUIRES VALIDATION. FOUND NOT PER SRM. REMOVED DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER IAW EA 011-5730-01-A1913 AND UPS EO MD11-5730-34298-A.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 45,780 hrs · 8,929 cycles

INSPECTION TYPE: 1C REPAIR SURVEYSEQUENCE NR 281-F1-11 RT EXTENDED FUSELAGE SKIN REPAIR STA 5-32 BETWEEN L13R AND L14R NO EFN NOT IAW SRM. ACCOMPLISHED EA 011-5330-A1918 AND UPS EO MD11-5330-34255-A.

Part: SKIN — MISREPAIRED (BS 1821-1853) · airframe 45,780 hrs · 8,929 cycles

INSPECTION TYPE: 1C REPAIR SURVEY SEQ NR 281-F1-08 LT AFT FUS. EXTERNAL LR SKIN REPAIR SAT 1821-1853.950, L45L-L46L DOES NOT CORRELATE WITH SRM. REMOVED EXISTING FUS, SKIN REPAIR FROM BETWEEN STA 1821-1853, L45L-L46 L. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF EO MD11-5330-34309 -B AND EA 011-5330-01-A1923.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 45,780 hrs · 8,929 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQUENCE 281-F1-13 LT FWD INTERMEDIATE FUSELAGE SKIN REPAIR STA 979 AND 999 L5L AND L6L NO EFN NOT PER SRM. REMOVED DOUBLER, REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLERS, FINGER DOUBLERS IAW MD-11 SRM 53-20-00 FIG 2 SHT 4, 5, 6.

Part: WEDGE — MISREPAIRED (LT WING TE FLAP) · airframe 45,780 hrs · 8,929 cycles

INSPECTION TYPE :1C REPAIR SURVEY SEQUENCE NR 281-W3-03, LT WING INBD FLAP T/E WEDGE BTWN STA XIFH 133.900 TO XIFH 177.300. DOES NOT CORRELATE TO SRM. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR ZEE ANGLE IAW MD-11 SRM 57-20-00 PARA (4) AND FIG. 3.

Part: DOUBLER — MISREPAIRED (LT WING) · airframe 45,780 hrs · 8,929 cycles

INSPECTION TYPE: 1C REPAIR SURVEY SEQUENCE NR 281-W3-06 LT WING UPPER WINGLET L/E REPAIR DOUBLER DOES NOT CORRELATE TO SRM. REMOVED, FABRICATED, AND INSTALLED NEW REPAIR DOUBLER IAW EO MD11-5730-34297-A.

Part: SKIN — MISREPAIRED (TE FLAP) · airframe 45,780 hrs · 8,929 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQUENCE NUMBER 281-W3-04 LT WING INBOARD FLAP UPPER SKIN BETWEEN STA XIFH 213.050 TO XIFH 225.140 REPAIR DOUBLER NOT CORRELATED TO SRM 57-10-00 FIG 38. REMOVED DOUBLER, REMOVED DAMAGE, FABRICATED, & INSTALLED DOUBLER IAW MD-11 SRM 57-10-00 FIG 38 SHT 2, UPS EO MD11-5750-34267-A, AND SAA EA 011-5730-01-A1906.

Part: SKIN — MISREPAIRED (CARGO DOOR) · airframe 45,780 hrs · 8,929 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQ 281-F1-07 AFT CARGO DOOR EXTERNAL SKIN REPAIR DOUBLER DOES NOT CORRELATE WITH EFN/SRM. REMOVED EXISTING REPAIR FROM AFT BULK CARGO DOOR UPPER FORWARD CORNER OF DOOR SKIN AT STA 1927. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF MD11-5230-34291-A AND EA 011-5230-01-A1905.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 45,780 hrs · 8,928 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQ 281-F1-03 EXTERNAL REPAIR DOUBLER ON RT EXTENDED FUSELAGE SKIN SECTION 6 BETWEEN STA 6-50-STA 6-70 AND BETWEEN L29R AND L30R NOT CORRELATED WITH SRM REPAIR. REMOVED EXISTING REPAIR AT STA 6-50 BETWEEN L29R AND L30R. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF EO MD11-5330-34338-A AND EA 01153 -5330-01-A1920.

Part: PRESSURE PANEL — MISREPAIRED (FUSELAGE) · airframe 45,780 hrs · 8,929 cycles

INSP TYPE: 1C REPAIR SURVEY SEQUENCE NR 281-F2-03, REPAIR DOUBLER IN LT FWD AC BAY STA 475-495 LBL 46 TO LBL 55. HORIZONTAL PRESSURE PNL DOES NOT CORRELATE TO SRM. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER IAW EA 011-5330-01-A1912 AND UPS EO MD11-5330-34303-A.

Part: SKIN — DAMAGED (RT AILERON) · airframe 45,780 hrs · 8,929 cycles

INSPECTION TYPE: 1C REPAIR SURVEY SEQ NR 281-W4-03 RT INBD AILERON LWR SKIN EXTERNAL DOUBLER BETWEEN STA XIH329.911 TO XIH335.767, 2 EA FASTENER HEADS PULLED. REMOVED EXISTING REPAIR FROM RT WING INBD AILERON LWR SKIN BETWEEN STA XIH 329.911 TO XIH 335.767. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF SRM VOL 1 57-10-00 FIG 38 SHEET 2.

Part: SKIN — DAMAGED (BS 1626 L42L) · airframe 45,780 hrs · 8,929 cycles

INSPECTION TYPE: 1C DRILL START IN FUSELAGE SKIN AT FUS STA 1626, ONE INCH ABOVE LONG 42L. REAMED HOLE, FABRICATED AND INSTALLED FREEZE PLUG, FABRICATED AND INSTALLED REPAIR DOUBLER IAW EA 011-5330-A1903 AND UPS EO MD11-5330-34312-A

Part: SKIN — MISREPAIRED (LT WING) · airframe 45,780 hrs · 8,929 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQ 281-W3-02 LT WING L/E TELESCOPIC REPAIR DOUBLER DOES NOT CORRELATE TO SRM AND DAMAGED INBOARD UPPER CORNER STA ZOS 4 61-XOS 473. REMOVED EXISTING REPAIR FROM LT WING L/E TELESCOPIC DUCT CUTOUT AT XOS 464 AND XOS 470. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF EO MD11-5730-34288-A AND EA 011-5730-01-A1897.

Part: SKIN — GOUGED (FUSELAGE) · airframe 45,780 hrs · 8,929 cycles

INSPECTION TYPE: 1C SURVEY SEQ NR281-F1-04 REPAIR DOUBLER ON LWR AFT CORNER OF CTR CARGO DOOR CUTOUT EXTERNAL SKIN HAS DEEP GOUGE. REMOVED EXISTING REPAIR AT LWR AFT CORNER OF CTR CARGO DOOR CUTOUT. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF SRM VOL1 53-50 -00, FIG. 17 VIEW B INCORPERATING SRM VOL 1 53-50-00 FIG 17 VIEW C SHT. 1 NOTE 2 OF VIEW B AND NOTE 14A OF VIEW B.

Part: SOLENOID — INOPERATIVE (L1 DOOR)

L1 DOOR INOP. SUSPECTED SOLENOID 52-730 FAULTY. REMOVED AND REPLACED SOLENOID DOOR LOCK PIN RELEASE ON L1 DOOR REF MD11 AMM 52-10-06-4. PERFORMED OPS CHECK OF THE L1 DOOR. OPS CHECK GOOD. REF MD11 AMM 52-11-02-2. NO ADJUSTMENT REQUIRED. RE42858 SAA019 SAA043 SAAP55 SJA.

Part: WIRE — DAMAGED (LT MLG WW)

INSPECTION TYPE:N/A LEFT W/W WIRE BUNDLE DAMAGED.

Part: WIRE HARNESS — DAMAGED (LT MLG WW)

INSPECTION TYPE:N/A DURING NR 1 ENG RUN TO T/S EPR PROBLEM SMOKE AND SPARKS APPEARED AT THE LT WHEEL WELL AREA. FOUND BEHIND LT WING TRAILING EDGE ACCESS PANELS WIRE BUNDLE BURNED. ALL AFFECTED WIRED TO BE REPLACED, REFER TO NRC 268256.

Part: RADOME — DAMAGED (FUSELAGE)

INSPECTION TYPE:N/A AT 1500 TO 2000 MSL A/C PASSED THROUGH LARGE FLOCK OF BIRDS. TOOK MULTIPLE HITS, NO IMMEDIATE DAMAGE NOTED. A/C RETURNED TO AIRPORT NORMALLY. NO EMERGENCY. PERFORMED BIRD STRIKE INSPECTION PER AMM 72-00-02-6. NOSE RADOME DAMAGE FROM BIRD STRIKE. FOUND EVIDENCE OF BIRD INGESTION INTO CORE AREA OF NR 1 AND NR 3 ENGINES. REMOVED AND REPLACED RADOME. NO DAMAGE NOTED IN EITHER HPC, LPC OR EXTERNAL SERVICES OF ENGINE. REF LP 204474.

Part: PAN — CRACKED (NLG) · airframe 44,340 hrs · 8,584 cycles

INSPECTION TYPE:SPV DURING SPECIAL VISIT- SAA, FOR MLG CHANGE, NLG DOOR JAMB AFT LT WAS FOUND TO BE BENT AND CRACKED. TRIMMED OUT DAMAGED AREA 3 INCHES, REPAIRED PERFORMED PER EO -MD11- 5320-31154-A AND PER INSTRUCTIONS IN EA 011-5320-01-A1555.

Part: SUPPORT FITTING — GOUGED (CLG TRUNNION) · airframe 44,340 hrs · 8,584 cycles

INSPECTION TYPE:SPV DURING SPECIAL VISIT FOR GEAR CHANGE AT SAA, CORROSION WAS FOUND ON THE CLG TRUNNION SUPPORT FITTING, RT SIDE. WHILE PERFORMING MACHINING TO SUPPORT FITTING FAYING SURFACE, PER SRM 53-40-00 FIG 16, THE SET SCREWS FOR THE CUTTER TOOL CAME LOOSE AND THE RADIUS WAS DAMAGED. BLENDED AREA REPAIRED PER EO MD11-5310-31226 AND PERFORMED ON EA SAA-011-5310-01-A1558. REPEAT INSPECTIONS EVERY CLG REMOVAL, NOT TO EXCEED 7,500 CYCLES. METHOD- HFEC.

Part: RIB — CRACKED (LEFT WING LE) · airframe 43,994 hrs · 8,475 cycles

INSPECTION TYPE:2C LEFT WING FIXED L/E RIB XFS 1024 CRACKED ON AFT SIDE BETWEEN FASTENERS. REMOVED, FABRICATED, AND INSTALLED RIB IAW MD-11 SRM 51-33-01 AND DWG ARB2920.

Part: STRUCTURE — CRACKED (LT WING) · airframe 43,994 hrs · 8,475 cycles

INSPECTION TYPE:2C LT WING FIXED L/E TELESCOPIC DOOR CUTOUT FOUND CRACKED ON ONE SIDE. REMOVED CRACK, FABRICATED, AND INSTALLED FILLER AND DOUBLER IAW MD-11 SRM 57-10-00 FIG 43, 51-21-01, 51-35-01, 51-33-01.

Part: SKIN — CRACKED (LT WING) · airframe 43,944 hrs · 8,475 cycles

INSPECTION TYPE:2C LEFT WING L/E SKIN SPLICE STRAP XFS 669 CRACKED. REMOVED SKIN SPLICE STRAP, REPLACED SKIN SPLICE STRAP IAW MD-11 SRM 51-33-01.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 43,944 hrs · 8,475 cycles

INSPECTION TYPE:2C RCB FLOOR PANEL PART NUMBER WSPO785-501 HAS AREAS OF CORROSION. REMOVED AND REPLACED FLOOR PANEL IAW UPS EO MD11-5330-27218-C.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 43,994 hrs · 8,475 cycles

INSPECTION TYPE:2C, LT WING FIXED L/E ANGLE SUPPORT AT STA XORS 346 FOUND CRACKED. REMOVED, FABRICATED AND INSTALLED ANGLE IAW MD-11 SRM 51-33-01 DWG ARB2918 AND SRM 51-21-01.

Part: SKIN PANEL — CHAFED (RT WING LE) · airframe 43,944 hrs · 8,475 cycles

INSPECTION TYPE:2C RT WING I/B FIXED L/E SKIN PANEL FOUND WITH CHAFE ON O/B EDGE CORNER JUST FWD OF PANEL 616HB. REMOVED, FABRICATED AND INSTALLED RT WING I/B FIXED L/E SKIN PANEL IAW DWG ARB2434 AND MD-11 SRM 51-33-01 & 51-35-01.

Part: SKIN — CRACKED (RT WING LE) · airframe 43,944 hrs · 8,475 cycles

INSPECTION TYPE:2C RT WING L/E SKIN SPLICE AT XFS669 IS CRACKED. REMOVED CRACKED SPLICE, FABRICATED AND INSTALLED REPLACEMENT IAW DWG ARB3954 AND MD-11 SRM 51-33-01.

Part: CONNECTOR — SHORTED (NR 2 START VALVE)

NR 2 ENGINE START VALVE LIGHT ILLUMINATED IN FLIGHT. DURING T/S, FOUND PIN "D" ON SOCKET R5-8235 SHORTED. REQUESTED P/N;DC60-28M15SX AND DC63-28K15PX. REPAIRED AT CONNECTOR P1-8235, REF STANDARD WIRING PRACTICES MANUAL CHAPTER 20. NR 2 ENG START VALVE AND LIGHT OPS CHECKED NORMAL ON IDLE ENG ENG RUN IAW 71-02-01.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY LIGHT BATTERY LOW ALERT ILLUMINATED DURING EMERGENCY LIGHT TEST. DEF NR 353905. T/S C/O IAW FIM 33-51-01-00. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY IAW MM 33-51-01-4. OPS CHECKED SATISFACTORY. THIS CLOSES DMI.

Part: PAINT — MISSING (LT WING)

INSPECTION TYPE:N/A LEFT WING UPPER TRAILING EDGE SKIN HAS SEVERAL AREAS OF PAINT MISSING JUST INBD OF WINGLET. LEFT WING INBD SIDE OF WINGLET SKIN HAS SEVERAL AREAS OF PAINT MISSING COMPOSITE PANELS & T/E IS DELAMINATED. ITEM DEFERRED D344293. *S/D* REMOVED PAINT, INSPECTED PANEL. THE DELAMINATION APPEARANCE WAS FROM A PREVIOUS REPAIR. THE GRITTINESS OF PANEL IS OK PER DRAWING ARB7793. UPPER PANEL ASSY, T/E WING EXT OK FOR SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (AILERONS)

ATB - LEVEL 2 "AILERON DEFLECT DISAGREE" UPON CLEAN UP AFTER T/O. FOLLOWED CHECKLIST PROCEDURES AND WHEN COMPLETED, THE LEVEL 2 ALERT RETURNED. FUEL WAS DUMPED AND A/C RETURNED TO ANC. DEFERRED PER MEL 27-13-2-01-1, PLACARD INSTALLED, M335539. DMP 27-13-2 C/W. A/C OK FOR SERVICE. COMPLIED WITH ADJUSTMENT/TEST PER MM 27-16-00-5. ALSO R&R BOTH LT DEFLECTION ACTUATOR PER MM 27-16-01 & 27-16-02. REF TARGET ALERT H134380

Part: COFFEEMAKER — OVERHEATED (GALLEY)

HOT CUP OVERHEAT DUE TO DEFAULT OF TIMER AND SUBSEQUENT MELT-DOWN OF 3 PIN CONNECTIONS W/ACRID FUMES IN COCKPIT AND EXCESSIVE HEAT AROUND OVEN AREA. REPLACED HOT CUP JUG AND PERFORMED OPS TEST OF HOT CUP TIMER AND FOUND NORMAL IAW 25-32-14-2. TIMER OPERATION NORMAL, SEVERAL TIMES UNABLE TO FAULT. A/C OK FOR SERVICE.

Part: FIRE WARNING — INTERMITTENT (NR 1)

FIRE DET 1 FAULT MESSAGE DISPLAYED AFTER ENG START (INTERMITTENT) PERFORMED FCDU RTS, ALL SYSTEMS PASSED. OK FOR SERVICE.

Part: SEAT TRACK — CORRODED (BS 1381) · airframe 36,457 hrs · 7,228 cycles

INSPECTION TYPE:C CABIN AT STA 1381 RT RBL 107.25 SEAT TRACK CROWN FOUND WITH CORROSION. CORROSION REMOVED PER SRM 51-2101 REV 31 VOL II AT SEAT TRACK & MAT REMOVED 0.038 INCH ORIG THK 0.100 INCH & FOUND EXCEED LIMIT PER SRM 53-70-00 VOL I REV 37 FIG 3. NEW SEAT TRACK EXTRUSION REPAIR SPLICE HATS & SPLICE PLATES BETWEEN STA 1351 TO STA 1411 RBL 107.25 INSTALLED PER SRM 51-31-01 VOL II REV 37 & SRM 53-7 0-00 FIG 1 VOL I REV 37.

Part: SEAT TRACK — CORRODED (STA1321 LBL27.5) · airframe 36,457 hrs · 7,228 cycles

INSPECTION TYPE:C CABIN AT STA 1321 LBL 27.5 SEAT TRACK CROWN FOUND CORRODED. CABIN STA 1321 LBL 27.5 SEAT TRACK CROWN CORROSION REMOVED PER SRM 53-70-00 FIG 3 VOL I REV 37 MAT ORIG THK 0.145: & MAT REMOVED 0.035 FOUND EXCEED LIMIT PER SRM 53-70-00 FIG 3 VOL 3 VOL I REV 37. NEW SEAT TRACK EXTRUSION, REPAIR SPLICE HATS & SPLICE PLATES BETWEEN STA 1209 TO STA 1351 LBL 27.5. INSTALLED PER SRM 51-31-01 VOL II REV 37 & SRM 53-70-00 FIG1 VOL I REV 37.

Part: SEAT TRACK — CORRODED (BS 1964,) · airframe 36,457 hrs · 7,228 cycles

INSPECTION TYPE:C RT CURVED SEAT TRACK STN 1964, RBL 107.25 EXFOLIATION CORROSION, RT CURVED S/TRACK ST1964 RBL 107.25 EXFOLIATION CORROSION REMOVED PER SRM 53-7 0-00 FIG 3 VOL I REV37 MAT ORIG THK 0.145" AND MAT REMOVED 0.075" FOUND EXCEED LIMIT, NEW S/TRACK REPAIR SPLICE HAT AND SPLICE PLATE BET STA1831-2 007 RBL107.25 INSTALLED PER SRM 51-31-01 VOL II REV37 AND SRM 53-70-00 FIG 1 VOL I REV 37.

Part: SEAT TRACK — CORRODED (BS 1964) · airframe 36,457 hrs · 7,228 cycles

INSPECTION TYPE:C LT CURVED SEAT TRACK ST 1964 LBL 107.25 EXFOLIATION CORROSION. LT CURVED S/TRACK STA1964 LBL107.25 EXFOLIATION CORROSION REMOVED PER SRM53-70 -00 FIG3 VOL I REV 37 MAT ORIG THK 0.145" AND MAT REMOVED 0.070" FOUND EXCEED LIMIT PER SRM 53-70-00 FIG3 VLO I REV37. NEW S/TRACK REPAIR SPLICE HAT AND SPLICE BET ST1831-2007 LBL107.25, INSTALLED PER SRM51-31-01 VOL II REV37 AND SRM53-70-00 FIG 1 VOL I REV 37.