N280UP

Part: SUPPORT — CRACKED (RT WING TE FLAP) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:3CR/H O/B FLAP I/B HINGE STOP SUPPORT ASSEMBLY IS CRACKED.REPLACED R/H O/B FLAP I/B HINGE STOP SUPPORT ASSEMBLY IAW VT-SAA EA 011-5700-01-A8938 REV. I/R AND UPS EO MD11-5750-79660-A. (MAJOR)

Part: SUPPORT FRAME — GOUGED (TAILCONE) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:CGOUGE ON L/H CENTER MAIN SUPPORT FRAME FOR TAIL CONEREMOVED DAMAGE AND INSTALLED REPAIR IAW MD11 SRM 53-00-00 FIG. 210 AND MD11 SRM 51-31-01

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:CR/H MLG W/W THIRD VERTICAL STIFFNER IS CRACKED AT LWR END ON OB AFT WEBRMOVED AND REPLACED IAW MD11 SRM 51-31-01 AND DRAWING AN87203

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:3CRH MLG W/W 3RD VERTICAL STIFFNER IS CRACKED AT LWR ENF ON OB AFT WEBREMOVED AND REPLACED

Part: STRUCTURE — CORRODED (RT ELEVATOR) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:3CR/H O/B ELEVATOR HAS A CORRODED RIB AT POS. 3.REMOVED AND REPLACED R/H O/B ELEVATOR IAW EO MD11-2700-74700-D. (MINOR)

Part: FLOOR SUPPORT — CORRODED (FWD CABIN) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:C3MAIN CABIN FLOOR SUPPORT AFT FLANGE CORRODED AT STA,435 LBL 45.REMOVED AND REPLACED CORRODED FLOOR SUPPORT IAW SRM 51-33-01 AND 51-31-01 (MINOR).

Part: FITTING — CRACKED (LOWER AUX TANK) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:3CCENTER LOWER AUX TANK R/H FRAME FITTING AT Y=1278 IS CRACKED.REMOVED AND REPLACED CRACKED CENTER LOWER AUX TANK R/H FRAME FITTING AT Y=1278 IAW MD-11 SRM 51-33-01. (MINOR)

Part: RIB — CRACKED (RT WING SLAT) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:3CR/H WING #8 SLAT RIB IS CRACKED AT STA. XOS. 1050.REMOVED, FABRICATED AND REPLACED RIB IAW DWG. ARB1926 AND SRM 51-31-01. (MINOR)

Part: FLOOR PANEL — CORRODED (FWD CABIN) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:INFWD CABIN COURIER AREA FLOOR PANEL CORRODED AT STA. X=8.5-X-8.5 TO Y=501-Y535.REMOVED,FABRICATED AND REPLACED CORRODED FLOOR PANEL IAW SRM 51-31-01 AND DWG# WSP0820 (MINOR).

Part: STRINGER — CRACKED (#1 TANK) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:3CLEFT WING LOWER STRINGER # 33 IS CRACKED AT STA. XORS. 1070.REPAIRED CRACKED LEFT WING STRINGER #33 AT STA. XORS. 1070 IAW VT-SAA EA 011-5720-01-A8903 REV. I/R AND UPS EO MD11-5710-79624-A. (MAJOR)

Part: STRINGER — CRACKED (FUEL TANK) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:3CCENTER WING TANK STRINGER #45 IS CRACKED AT STA. XCW= -17.0.REPAIRED CRACKED CENTER WING TANK STRINGER #45 BETWEENSTA. XCW=0 TO XCW= -33.4 IAW SRM 57-10-03 REPAIR 1 FIG. 201. (MAJOR)

Part: STRINGER — CRACKED (CENTER TANK) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:3CCENTER WING TANK STRINGER #47 IS CRACKED BETWEEN STA. XCW= 32 AND XCW= -32.REPAIRED CRACKED CENTER WING TANK STRINGER #47 BETWEEN STA. XCW= 32, 0.00 AND -32 IAW VT-SAA EA 011-5710-01-A8929REV. I/R AND UPS EO MD11-5710-57361-C. (MAJOR)

Part: STRINGER — CRACKED (CENTER TANK) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:3CCENTER WING TANK STRINGER #47 IS CRACKED BETWEEN STA. XCW= 32 AND XCW= -32.REPAIRED CRACKED CENTER WING TANK STRINGER #47 BETWEEN STA. XCW= 32, 0.00 AND -32 IAW VT-SAA EA 011-5710-01-A8929REV. I/R AND UPS EO MD11-5710-57361-C. (MAJOR)

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:3CCABIN FLOOR PANEL WSP0785-501 IS CORRODED.REMOVED AND REPLACED FLOOR PANEL IAW DWG. WSP0785 AND SRM 51-31-01. (MINOR)

Part: FLOOR PANEL — CORRODED (FWD CABIN) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:C3FWD CABIN COURIER FLOOR PANEL CORRODED BETWEEN STA. Y=501- Y=575 AND X=8.5- X=27.5.REMOVED,FABRICATED AND REPLACED CORRODED FLOOR PANEL IAW SRM 51-31-01 AND DWG WSP0820 REV N (MINOR).

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:3CCABIN FLOOR PANEL WSP0789-501 IS CORRODED.REMOVED AND REPLACED FLOOR PANEL IAW DWG. WSP0789 AND SRM 51-31-01. (MINOR)

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:3CCOURIER FLOOR PANEL WSP0785-502 IS CORRODED.REMOVED AND REPLACED FLOOR PANEL IAW DWG. WSP 07856 AND SRM 51-31-01. (MINOR)

Part: STIFFENER — CRACKED (AFT CARGO) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:3CAFT CARGO AT STA. 1841 AND RBL 31, VERTICAL STIFFNER IS CRACKED.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. AGA7170 AND SRM 51-33-01. (MINOR)

Part: FLOOR PANEL — CORRODED (FWD CABIN) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:C3MAIN CABIN COURIER FLOOR PANEL WSP0820-77 HAS HEAVY CORROSION.REMOVED,FABRICATED AND REPLACED CORRODED FLOOR PANEL IAW SRM 51-31-01 AND DWG WSP0820 (MINOR).

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:3CFLOOR SUPPORT IS CORRODED BETWEEN STA. Y=392 TO 440, & X= -8.5 TO - 27.5.REMOVED, FABRICATED AND REPLACED FLOOR SUPPORT IAW DWG. WSP0668 AND SRM 51-31-01. (MINOR)

Part: STIFFENER — CRACKED (AFT CARGO) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:3CAFT CARGO VERTICAL STIFFNER IS CRACKED AT STA. 1841 AND RBL 25.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. AGA7170 AND SRM 51-33-01. (MINOR)

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:3CCABIN FLOOR PANEL WSP0785-501 IS CORRODED.REMOVED AND REPLACED FLOOR PANEL IAW DWG. WSP0785 AND SRM 51-30-01. (MINOR)

Part: FLOOR PANEL — CORRODED (FWD CABIN) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:C3FWD CABIN COURIER FLOOR PANEL WSP0785-502 HAS CORROSION.REPAIRED CORRODED FWD CABIN FLOOR PANEL IAW VT-SAA EA011-5320-01-A8924 REV I/R AND UPS EO MD11-5320-79598-A (MINOR).

Part: LONGERON — CORRODED (ZONE 100) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:3CCENTER CARGO LONGERON 44 R/H END SPLICE IS CORRODED AT STA. 1811.REMOVED, FABRIVCATED AND REPLACED LONGERON 44 R/H END SPLICE AT STA. 1811 IAW VT-SAA EA 011-5320-01-A8917 REV. I/R AND UPS EO MD11-5310-79653-A. (MAJOR)

Part: STIFFENER — CRACKED (AFT CARGO) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:3CAFTR CARGO VERTICAL STIFFNER IS CRACKED AT STA. 1841 AND LBL31.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. AGA7170 AND SRM 51-33-01. (MINOR)

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:3CCABIN FLOOR PANEL WSP0788-501 IS CORRODED.REMOVED AND REPLACED FLOOR PANEL IAW DWG. WSP0788 AND SRM 51-31-01. (MINOR)

Part: SKIN — CRACKED (RT WING) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:C3RT WING LWR SKIN CRACK AT 636AB ACCESS PANEL OPENING.REPAIRED CRACKED RT LWR WING SKIN IAW SRM 57-20-02 REPAIR 5 (MINOR).

Part: SKIN — CRACKED (LT WING) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:C3LT LWR WING SKIN CRACK AT ACCESS PANEL 536AB OPENING.REPAIRED CRACKED LT LWR WING SKIN IAW SRM 57-20-02 REPAIR 5 (MINOR).

Part: ATTACH ANGLE — CRACKED (RH KEEL BEAM) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:C3RH KEEL BEAM ATTACH ANGLE CRACK AT STA.1370.REMOVED ,FABRICATED AND REPLACED CRACKED ATTACH ANGLE IAW SRM 51-35-01 AND 51-21-01 (MINOR).

Part: BARRIER — CRACKED (CABIN) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:3CRIGID CARGO BARRIER WALL IS CRACKED AT STA. 488.81 AND X= -27.5.REPAIRED CRACKED RIGID CARGO BARRIER WALL AT STA. 488.81 AND X= -27.5 IAW SRM 53-20-53 REPAIR 1 FIG. 201. (MAJOR)

Part: FITTING — CHAFED (MAIN CARGO) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:3C, RIDGED CARGO BARRIER SIDE FITTING #3 HAS DEEP WEAR/CHAFE DAMAGE.REPAIRED CHAFED RIDGED CARGO BARRIER SIDE FITTING #3 IAW VT-SAA EA 011-2550-01-A8931 REV. IR AND UPS EO MD11-5310-79580-A. (MINOR)

Part: BARRIER — CRACKED (CABIN) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:3CRIGID CARGO BARRIER WALL IS CRACKED AT STA. 488.81 AND X= -53.REPAIRED CRACKED RIGID CARGO BARRIER WALL AT STA. 488.81 AND X= -53 IAW SRM 53-20-53 REPAIR 1 FIG. 201. (MAJOR).

Part: SPAR CAP — CORRODED (RT WING) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:3CR/H WING REAR SPAR UPPER CAP AFT FLANGE IS CORRODED BETWEEN STA. XORS. 787.5 & 827.0.REPAIRED CORRODED R/H WING REAR SPAR UPPER CAP AFT FLANGE BETWEEN STA. XORS. 787.5 & 827 IAW VT-SAA EA 011-5720-01-A8895 REV. I/R AND UPS EO MD11-5710-79608-A. (MAJOR)

Part: SPLICE — CRACKED (MAIN CABIN) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:C3MAIN CABIN SPLICE(WEB SUPPORT) CRACK AT STA.1841 LON 19R.REMOVED,FABRICATED AND REPLACED CRACKED SPLICE IAW SRM 51-35-01 AND DWG AFA7798 (MINOR).

Part: FORMER — CRACKED (LT WING L/E) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:C3LH WING L/E COMPARTMENT HAS A CRACK FORMER AT XOS STA.1038.REMOVED,FABRICATED AND REPLACED CRACKED FORMER IAW SRAM 57-35-01 AND 51-33-01 (MNOR).

Part: SUPPORT — CRACKED (MAIN CABIN) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:C3MAIN CABIN WEB SUPPORT CRACK AT STA.1841 LON 19L.REMOVED,FABRICATED AND REPLACED CRACKED WEB SUPPORT IAW SRM 51-36-01 AND 51-35-01 (MINOR).

Part: DOUBLER — CRACKED (RT WING) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:3CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA.XOSA. 692.0 TO 698.127.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 692.0 TO 698.127 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: SKIN — CRACKED (RT WING SLAT) · airframe 66,507 hrs · 13,155 cycles

INSPECTION TYPE:3CR/H WING #8 SLAT INNER SKIN IS CRACKED BETWEEN STA. XOS. 1042.5 TO 1073.0.REPAIRED CRACKED R/H WING #8 SLAT INNER SKIN BETWEEN STA. XOS. 1042.5 TO 1073.0 IAW SRM 57-40-01 REPAIR 3 FIG. 201. (MAJOR)

Part: SOLENOID — MALFUNCTIONED (L1 DOOR) · airframe 66,488 hrs · 13,147 cycles

L1 DOOR WILL NOT CLOSE ELECTRONICLLY WITH EITHER INDOOR OR OUTDOOR SWITCHES. R/R'D L1 DOOR SOLENOID S2-730 IAW BOEING MD SWPM 20-00-09 AND MD11 WDM 52-11-01 IN REF TO UPS M734971. PERFORMED SATIS OPS CHECK OF DOOR REF MD11 AMM 52-11-02-010-802 & 52-11-02-410-802.

Part: DOOR — MALFUNCTIONED (L1) · airframe 66,214 hrs · 13,004 cycles

L1 DOOR STOPPED HALF WAY OPEN WILL NOT 60 UP OR DOWN ELECTRICALLY. HAD 115VAC AT A2 B2 C2 PUT SWITCH TO DOWN AND HAD NO POWER TO A1 B1 OR C 1 ON R2-177. R & R RELAY R2477, REF WDM 52-11-01, NO HELP. DEFERRED L1 DOOR, REF MEL 52-10-3-1-2-1-2. PERFORMED OPERATIONS TEST OF L1 ENTRY DOOR, IAW NORMAL MODE. DOOR OPERATE NORMALLY, IAW AMM 52-10-01. M728464 CLOSED.

Part: SWITCH — INOPERATIVE (MAIN CABIN DOOR) · airframe 66,126 hrs · 12,959 cycles

INSPECTION TYPE: N/A MAIN CABIN DOOR WILL NOT CLOSE. NO POWER TO SWITCH. CYCLED POWER TO MAIN CABIN DOOR, IAW MM 52-11-02. OPERATIONS CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 65,899 hrs · 12,863 cycles

INSPECTION TYPE: NA DURING PER FLT FOUND EMERGENCY LIGHT BAT 1 LOW MESSAGE. REMOVED AND REPLACED EMERGENCY BATTERY POWER SUPPLY BATTERY, PER AMM 33-51-01. OPERATIONS TEST GOOD

Part: TRANSCEIVER — INOPERATIVE (VHF COMMS) · airframe 65,578 hrs · 12,715 cycles

INSPECTION TYPE:N/AAFTER T.O. WE COULD NOT TRANSMIT ON VHF 1. WE TRIED BOTH CAPT & F.O. SIDE WITH BOOM AND HAND MIKE. WE ARE ABLE TO HEAR TRANSMISSIONS.SWAPPED NR 1 & 3 R/T UNITS IAW MM 23-12-01. VHF 1 OPS CHECKED GOOD IAW MM 23-12-01.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 65,174 hrs · 12,546 cycles

INSPECTION TYPE:N/A*** ATB *** AT FL230 ANTI ICE ON WHEN DESELECTING ANTI ICE L SW L WINDSHEILD POPPED AND SHATTERED CRACKS ACROSS ENTIRE WINDSHEILD.R/R WINDOW ASSY PER MM 56-11-01 ALL OPS CHECK GOOD TORQUED TERMINAL BLOCKS PER SWPM 20-20-03. ESR: IPC 56-11-05-01-005.

Part: ANTI-ICE VALVE — FAULTED (NR 2 ENGINE) · airframe 64,505 hrs · 12,288 cycles

INSPECTION TYPE:N/ADIVERSION - ON DESCENT IN CAE, SELECTED ANTI ICE ON LVL 1 ALERT ENG 2 A-ICE OFF WITH ENG 2 ANTI ICE SELECTED ON, DISAGREE IN SWITCHWRAPPED #2 NOSE COWL ANTI ICE DUCT WITH FOIL AND RAN ENG FOR LEAK CHECK. NO LEAKS NOTED TRENT DERUDDER 0558900 12-13-19/// R&R ANTI ICE SHUTOFF VALVE FOR #2 ENG IAW AMM 30-22-04. ALSO, REPLACED # 2 ENG ANTI ICE PRESSURE SWITCH IAW AMM 30-22-02. OPS AND LEAK CHECK GOOD. FOIL REMOVED FROM #2 ENG AN

Part: CHANNEL — DAMAGED (BS 1009) · airframe 64,298 hrs · 12,179 cycles

INSPECTION TYPE:N/ADAMAGE TO FORWARD PIT CEILING POSITION #4.REPAIRED IAW EO MD11-5310-74417-A. REMOVED DAMAGE HAT CHANEL 50.0 INCH LENGTH STA 1009 X - 30.78 REF SRM 51-25-01 0558918 10-22-19 THIS IS A MAJOR REPAIR TRANSFERRED TO NRC 656793 5501132 10-23-19 ACCOMP. PERM REPAIR (MAJOR) TO CEILING REF NR 656793 THIS COMPLETES THE REPAIR.

Part: GIRT BAR — BROKEN (L1 DOOR) · airframe 63,568 hrs · 11,855 cycles

INSPECTION TYPE:SDR ON PREFLIGHT L1 EVAC SLIDE BROKEN. REATTACHED GIRT BAR INTO LOCKING CLIP. AIRCRAFT OK FOR SERVICE.

Part: HINGE — CHAFED (NR 1 COWLING) · airframe 63,393 hrs · 11,794 cycles

INSPECTION TYPE:2C NR 1 ENG OTBD FAN COWL FWD HINGE IS CHAFED. ACCOMPLISHED REPAIR ON NR 1 ENG OTBD FAN COWL FWD HINGE PER EA# 011-7110-01-A7658 I/R AND EO MD-11-7110-72001-A.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,393 hrs · 11,794 cycles

INSPECTION TYPE:2C STEP UP BETWEEN CENTER AND AFT CARGO HAS CRACKED VERTICAL STIFFENER AT STA. 1841 & RBL 18. REMOVED AND REPLACED CRACKED VERTICAL STIFFENER AT STA. 1841 & RBL 18 IAW SRM 51-33-01. (MINOR)

Part: SPLICE — CHAFED (TAIL CONE) · airframe 63,393 hrs · 11,794 cycles

INSPECTION TYPE:2C TAIL CONE LOWER INTERNAL SPLICE SKIN HAS CHAFE DAMAGE. REMOVED, FABRICATED AND REPLACED INTERNAL SPLICE SKIN IAW DWG AKC7541 AND SRM 51-31-01. (MINOR)

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,393 hrs · 11,794 cycles

INSPECTION TYPE:2C STEP UP BETWEEN CENTER AND AFT CARGO STA. 1841 HAS 2 VERTICAL STIFFENERS CRACKED AT LBL 18 & LBL 24. REMOVED AND REPLACED 2 CRACK VERTICAL STIFFENERS AT STA. 1841 AND LBL 18 & LBL 24 IAW SRM 51-33-00. (MINOR)

Part: FRAME — CRACKED (THRUST REVERSER) · airframe 63,393 hrs · 11,794 cycles

INSPECTION TYPE:2C NR 2 ENG. LT T/R FIXED COWL CASCADE VANE FWD ATTACH FRAME IS CRACKED AT LOWER END. REPAIRED CRACKED NR 2 ENG. LT T/R FIXED COWL CASCADE VANE FWD ATTACH FRAME AT LOWER END IAW CMM 78-32-35 REPAIR 34. (MINOR)

Part: PAN — CHAFED (FUSELAGE) · airframe 63,393 hrs · 11,794 cycles

INSPECTION TYPE:2C MAIN CARGO DOOR FWD LOWER PAN HAS CHAFE DAMAGE IN 2 PLACES. REMOVED AND REPLACED CHAFED MAIN CARGO DOOR FWD LOWER PAN IAW SRM 51-33-01 AND 51-35-01. (MINOR)

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,393 hrs · 11,794 cycles

INSPECTION TYPE:2C FLOORBEAM IS CRACKED AT STA. 6-70, X=-57.5 AND Z=-98. REPAIRED CRACKED FLOORBEAM AT STA. 6-70, X=-57.5 AND Z=-98 IAW SRM 53-40-51 REPAIR 1 FIG. 202. (MAJOR)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,393 hrs · 11,794 cycles

INSPECTION TYPE:2C MAIN CABIN AT STA. 1341, LONGERON 15L "T" ANGLE IS CRACKED. REMOVED, FABRICATED AND REPLACED "T" ANGLE AT STA. 1341 AND LONG. 15L IAW DWG. AEA7568 AND SRM 51-33-01. (MINOR)

Part: DOUBLER — CHAFED (TAIL CONE) · airframe 63,393 hrs · 11,794 cycles

INSPECTION TYPE:2C TAIL CONE INTERNAL DOUBLER IS CHAFED AT STA. 5162 AND X=-36. REPAIRED CHAFED TAIL CONE INTERNAL DOUBLER AT STA. 2165 AND X=-36 IAW EO MD11-5350-66790-A APPX. A. (MINOR)

Part: INTERCOSTAL — CRACKED (TAIL CONE) · airframe 63,393 hrs · 11,794 cycles

INSPECTION TYPE:2C TAIL CONE RT CENTER GUIDE PIN INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG AKC7520 AND SRM 51-35-01. (MINOR)

Part: SKIN — CRACKED (THRUST REVERSER) · airframe 63,393 hrs · 11,794 cycles

INSPECTION TYPE:2C NR 2 ENG. LT T/R AFT FIXED INNER BARREL SKIN IS CRACKED. REPAIRED CRACKED NR 2 ENG. LT T/R IAW EA 011-7830-01-A7657 REV. I/R AND EO MD11-7830-71920-A. (MINOR)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,393 hrs · 11,794 cycles

INSPECTION TYPE:2CSTA. 6-100 SPLICE AT LONG. 3L HAS PULLING FASTENERS AND IS DENTED.REPAIRED DENTED EXTERIOR FUSELAGE SKIN AT STA. 6-100 AND LONG. 3L IAW VT-SAA EA 011-5330-01-A7676 REV. I/R AND UPS EO MD11-5330-72077-A. (MAJOR)

Part: SKIN — CHAFED (RT WING) · airframe 63,393 hrs · 11,794 cycles

INSPECTION TYPE:2C RT WING FIXED L/E SKIN HAS CHAFE DAMAGE BETWEEN STA. XORS. 854-874. REPAIRED CHAFED RT WING FIXED L/E SKIN BETWEEN STA. XORS. 854-874 IAW EA 011-5730-01-A7678 REV. I/R AND EO MD11-5730-72501-A. (MINOR)

Part: SKIN — CHAFED (DROOP LE) · airframe 63,393 hrs · 11,794 cycles

INSPECTION TYPE:2C LT WING DROOP L/E SKIN IS CHAFED AT STA. XDLE=329.774. REPAIRED CHAFED LT WING DROOP L/E SKIN AT STA. XDLE=329.774 IAW SRM 57-40-01 REPAIR 15 FIG. 202 AND 51-31-04 GEN. (MAJOR)

Part: SKIN — CORRODED (FUEL TANK) · airframe 63,393 hrs · 11,794 cycles

INSPECTION TYPE:2C CENTER WIN BOX UPPER SKIN HAS CORROSION AT STA. XCW=-17.0 AND BETWEEN STR. 14 & 15. REPAIRED CORRODED CENTER WING BOX UPPER SKIN AT STA. XCW=-17.0 AND BETWEEN STR. 14 & 15 IAW EA 011-5730-01-A7664 REV. I/R AND EO MD11-5730-72026-A. (MINOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 63,393 hrs · 11,794 cycles

INSPECTION TYPE:2C LT WING FIXED L/E SKIN SPLICE DOUBLER IS CRACKED AT STA.XOS.906. REMOVED, FABRICATED AND REPLACED DOUBLER AT LT WING L/E STA. XOS. 906 IAW DWG. ARB3954 AND SRM 51-33-01. (MINOR)

Part: STIFFENER — CRACKED (RT MLG W/W) · airframe 63,393 hrs · 11,794 cycles

INSPECTION TYPE:2CRT MLG WW O/B AFT WALL 2ND VERTICAL STIFFENER IS CRACKED. REMOVED AND REPLACED CRACKED RT MLG WW O/B AFT WALL VERTICAL STIFFENER IAW SRM 51-33-01. (MINOR)

Part: SKIN — DAMAGED (THRUST REVERSER) · airframe 63,393 hrs · 11,794 cycles

INSPECTION TYPE:2C NR 1 ENG. RT T/R AFT FIXED INNER BARREL LOWER SKIN AT 6 O'CLOCK POS. HAS PULLED RIVETS. REPAIRED DAMAGED NR 1 ENG. RT T/R IAW EA 011-7830-01-A7659 REV. I/R AND EO MD11-7830-71939-A. (MINOR)

Part: INTERCOSTAL — CRACKED (RT MLG WW) · airframe 63,393 hrs · 11,794 cycles

INSPECTION TYPE:2C RT MLG WW INTERCOSTAL BELOW AFT BRAKE ACCUMULATOR IS CRACKED. REPAIRED RT MLG WW INTERCOSTAL CRACK BELOW AFT BRAKE ACCUMULATOR IAW SRM 53-40-12 REPAIR 3, FIGURE 201. (MAJOR)

Part: INTERCOSTAL — CRACKED (LT MLG WW) · airframe 63,393 hrs · 11,794 cycles

INSPECTION TYPE:2C LT MLG WW INTERCOSTAL BELOW FWD BRAKE ACCUMULATOR IS CRACKED. REPAIRED CRACKED LT MLG WW INTERCOSTAL BELOW FWD BRAKE ACCUMULATOR IAW SRM 53-40-12 REPAIR 3, FIGURE 201. (MAJOR)

Part: TRUNNION — CRACKED (NLG WW) · airframe 63,393 hrs · 11,794 cycles

INSPECTION TYPE:2C LT NLG TRUNNION FITTING IS CRACKED AT STA. 582.5, Z=-114 AND X=24. REPAIRED CRACKED NLG TRUNNION AT STA. 582.5, Z=-114 AND X=24 IAW SRM 53-10-14 REPAIR 2 FIG. 202. (MAJOR)

Part: DRIVE CHAIN — BROKEN (L1 DOOR ASSIST) · airframe 62,620 hrs · 11,502 cycles

L1 DOOR EMERGENCY ASSIST BOTTLE DRIVE CHAIN WAS BROKEN. INSTALLED THE DRIVE CHAIN IAW CMM 52-11-09. OPS CHECKED GOOD,

Part: DRIVE CHAIN — BROKEN (L1 DOOR ASSIST) · airframe 62,620 hrs · 11,502 cycles

L1 DOOR EMERGENCY ASSIST BOTTLE DRIVE CHAIN WAS BROKEN. INSTALLED A DRIVE CHAIN IAW CMM 52-11-09. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 62,516 hrs · 11,470 cycles

EMERGENCY LIGHT BAT 1 LOW ALERT. R&R EMERGENCY LIGHT BATTERY RE MM 33 51 01 ESR 33 51 01 01.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,217 hrs · 11,125 cycles

EMERGENCY LIGHTS FAILED TO TEST. R & R THE POWER SUPPLY IAW MM 33-51-01. PERFORMED AN OPS CHECK PER MM 33-51-01-700-802. SYSTEM WORKS NORMALLY.

Part: LIMIT SWITCH — INOPERATIVE (DOOR ASSIST) · airframe 60,924 hrs · 11,020 cycles

INSPECTION TYPE:N/AREF DEFERRAL M 622633 L1 DOOR -- PASS DOOR ELECTRIC ACTUATORS- CGO CONFIG- L1 & R1 ONLY PERM REPAIR. BEARING BUSHING SEIZED ON INPUT SHAFT TO UPPER LIMIT SWITCH. INSTALLED L1 AND R1 DOOR OPEN LIMIT SWITCH ADJUSTMENT. OPS CK GOOD. REF AMM 52-11-02-830-805. DMP REVERSED. PLACARD REMOVED. CLEARED DMI LOG. THIS CLEARS DEF M622633. EFF SOURCE REF MM 52-11-20.

Part: BAR — LOOSE (SLIDE) · airframe 60,577 hrs · 10,931 cycles

LEFT ESCAPE SLIDE MANUAL LIFT BAR LOOSE. SECURED THE SLIDE LIFT BAR. OK FOR SERVICE.

Part: LIMIT SWITCH — INOPERATIVE (L1 DOOR) · airframe 59,335 hrs · 10,655 cycles

L1 DOOR ELECTRIC FUNCTION INOPERATIVE, WILL NOT OPEN OR CLOSE, MANUAL OK. R & R THE UP LIMIT SWITCH AND CIRCUIT BREAKER IAW MM 52-10-01.

Part: BEAM — CRACKED (FWD CARGO) · airframe 59,312 hrs · 10,650 cycles

INSPECTION TYPE: 1C, CRACKED BEAM IN FWD CARGO BAY FLOOR, ABOVE LONGERON 43L AT BS 6-73. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT BEAM IAW DWG ADA7667, AND SRM 51-33-01.

Part: FITTING — CORRODED (MAIN CABIN) · airframe 59,312 hrs · 10,650 cycles

INSPECTION TYPE: 1C, RIGID CARGO BARRIER FLOOR FITTING 10 IS CRACKED. REMOVED AND REPLACED THE FITTING IAW EO MD11-2520-58701-D.

Part: LONGERON — CORRODED (BS 1262-1268) · airframe 59,312 hrs · 10,650 cycles

INSPECTION TYPE: 1C, LONGERON 28L HAS CORROSION AT BS 1262 - 1268. REPAIRED THE LONGERON IAW EA 011-5310-01-A6729, REV I/R, AND EO MD11-5310-63744-A.

Part: FITTING — CORRODED (MAIN CABIN) · airframe 59,312 hrs · 10,650 cycles

INSPECTION TYPE: 1C, RIGID CARGO BARRIER FLOOR FITTING NR 4 IS CORRODED. REMOVED AND REPLACED THE FITTING IAW EO MD11-2520-58701-D.

Part: FITTING — CORRODED (MAIN CABIN) · airframe 59,312 hrs · 10,650 cycles

INSPECTION TYPE: 1C, RIGID CARGO BARRIER FLOOR FITTING NR 6 IS CORRODED. REMOVED AND REPLACED THE FITTING IAW EO MD11-2520-58701-D.

Part: SUPPORT RIB — CRACKED (LT WING) · airframe 59,312 hrs · 10,650 cycles

INSPECTION TYPE: 1C, LEFT WING FIXED L/E COMPARTMENT SUPPORT RIB IS CRACKED AT THE OTBD END OF THE NR 8 SLAT. REMOVED, FABRICATED, AND REPLACED THE SUPPORT RIB IAW DWG ARB2904, AND SRM 51-35-01.

Part: DOUBLER — CRACKED (LT WING) · airframe 59,312 hrs · 10,650 cycles

INSPECTION TYPE: 1C, LEFT WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN XOS 625.5 - 633.4. REPAIRED THE DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 203. MAJOR.

Part: FORMER — CRACKED (RT WING LE) · airframe 59,312 hrs · 10,650 cycles

INSPECTION TYPE: 1C, RT WING FIXED L/E INTERNAL FORMER CRACKED NEAR XORS 653. REMOVED FABRICATED AND INSTALLED A REPLACEMENT FORMER IAW DWG ARB2922 AND SRM 51-35-01.

Part: DOUBLER — CRACKED (LT WING) · airframe 59,312 hrs · 10,650 cycles

INSPECTION TYPE: 1C, LEFT WING FIXED L/E COMPARTMENT. PANEL LANDING IS CRACKED AT XORS 546. REMOVED, FABRICATED, AND REPLACED IAW DWG.ARB2933 AND SRM 51-31-01.

Part: SKIN — CORRODED (LT WING) · airframe 59,312 hrs · 10,650 cycles

INSPECTION TYPE: 1C, LEFT WING UPPER SKIN HAS CORROSION BETWEEN XORS 751 - 779, STRINGER 1 & REAR SPAR. REPAIRED THE SKIN IAW EA 011-5730-01-A6728, REV I/R, AND EO MD11-5730-63733-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 59,311 hrs · 10,649 cycles

INSPECTION TYPE: 1C, LEFT WING FIXED L/E BEADED DOUBLER IS CRACKED AT XOS. 667 - 673. REPAIRED THE DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG. 205. MAJOR.

Part: DOUBLER — CRACKED (RT WING) · airframe 59,311 hrs · 10,649 cycles

INSPECTION TYPE: 1C, RIGHT WING FIXED L/E BEADED DOUBLER AT XOS 627.6502 IS CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 205. MAJOR.

Part: DOUBLER — CRACKED (RT WING) · airframe 59,311 hrs · 10,649 cycles

INSPECTION TYPE: 1C, RIGHT WING FIXED L/E BEADED DOUBLER AT XOS 561.0878 IS CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 205. MAJOR.

Part: DOUBLER — CRACKED (RT WING) · airframe 59,311 hrs · 10,649 cycles

INSPECTION TYPE: 1C, RIGHT WING FIXED L/E BEADED DOUBLER AT XOS 613.6502 IS CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 205. MAJOR.

Part: COMPRESSOR — STALLED (NR 2 ENGINE) · airframe 59,297 hrs · 10,644 cycles

EMERGENCY DECLARED DUE TO THE NR 2 ENGINE COMPRESSOR STALLED. CREW SHUTDOWN THE ENGINE. REPLACED THE NR 2 ENGINE.

Part: CONTROL MODULE — LEAKING (HYD SYSTEM) · airframe 59,076 hrs · 10,584 cycles

HYD 3 ELEVATOR OFF LEVEL 1 MESSAGE OCCURED SHORTLY AFTER TAKEOFF, NOTICED HYDRAULIC FLUID IN NR 3 DECREASING RAPIDLY FROM 7.8 GAL TO 2.5 GAL IN APPROX 5 MIN. EMERGENCY DECLARED. FOUND PRIMARY STAB TRIM CTRL MODULE (UPPER) LEAK AT CRACK ON MODULE BODY, DEACTIVATED PRIMARY TRIM CONROL VALVE, IAW MM 27-43-40-000-801, STARTED REMOVAL OF PRI-TRIM CONTROL VALVE IAW MM 27-43-40-000-801 UP TO STEP 1A) (1A) .

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 57,895 hrs · 10,330 cycles

LEVEL 1 EMERGENCY LIGHT BATTERY LOW, REPAIRED IAW 33-51-01 OPS OK.

Part: BRACKET — DAMAGED (GIRT BAR) · airframe 57,438 hrs · 10,219 cycles

DURING PRE FLIGHT, FOUND L1 DOOR GIRT BAR BRACKET HAS COME APART. REINSTALLED L1 DOOR ESCAPE SLIDE GIRT BAR AS REQ'D

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 57,022 hrs · 10,112 cycles

EMERGENCY LIGHT BATTERY 1 LO, ALERT, WHEN EMERGENCY LIGHT TEST BUTTON WAS PUSHED PRE-FLIGHT, R & R EMERGENCY BATTERY POWER SUPPLY IAW AMM 33-51-01-000-802, 33-51-01-400-802. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 57,010 hrs · 10,109 cycles

NR 1 LT EMERGENCY BATTERY LOW PERFORMED EMERGENCY LIGHT TEST, TEST PASSED, ALL EMERGENCY LIGHTS WORKING FINE.

Part: CONTAINER — DAMAGED (LIFE VEST) · airframe 56,095 hrs · 9,881 cycles

LIFE VEST 4TH CREW MEMBER SEAT VACUUM PACKAGE DAMAGED. AFFECTED LIFE VEST REPLACED IAW AMM 25-64-01, PB 201, REV 84.01, DATED 11-19-15. PN OFF-ON: P01074-201C, SN OFF: 15071900049, SN ON: 14031350278. EFF REF IPC: 25-64-01-08, ITEM -010B, REV 149.01, DATED 12-08-15.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 55,323 hrs · 9,721 cycles

"EMERGENCY LT BATTERY 1 LO" R & R EMERGENCY BATTERY PACK IAW AMM 33-51-01. OPS CHECKED IAW 33-51-01-700-802.

Part: FLOOR SUPPORT — CORRODED (BS 410) · airframe 54,574 hrs · 9,562 cycles

INSPECTION TYPE:4C, DISCOVERED SUPPORT WITH CORROSION UNDER FLOOR PANEL AT R1 DOOR STA 410, L27L. R & R SUPPORT UNDER FLOOR PANEL AT R1 DOOR STA 410 L27L IAW SRM 51-31-01.

Part: DOUBLER — CRACKED (LT WING) · airframe 54,574 hrs · 9,562 cycles

INSPECTION TYPE:4C, LT WING L/E INTERNAL SPLICE DOUBLER STRAP CRACKED AT XOS 789. R & R SPLICE DOUBLER STRAP IAW SRM 51-33-01.

Part: SKIN — CORRODED (BS 2163-2122) · airframe 54,574 hrs · 9,562 cycles

INSPECTION TYPE:4C, RT AFT FUSELAGE SKIN HAS CORROSION BS 2163 TO 2122 BETWEEN L32R AND L35R. ACCOMPLISHED SKIN REPAIR IAW EA 011-5310-01-A5802, REV I/R AND EO MD11-5330-57372-A.

Part: FRAME — CORRODED (BS 555) · airframe 54,574 hrs · 9,562 cycles

INSPECTION TYPE:4C, LEFT NR 2 A/C BAY BILGE LONGERON SUPPORT AND FRAME SUPPORT HAS LIGHT CORROSION. ACCOMPLISHED BLEND REPAIR ON LT NR 2 A/C BAY BILGE LONGERON SUPPORT AND FRAME SUPPORT IAW SRM 53-00-00, REPAIR GENERAL.

Part: STRINGER — CRACKED (RT WING) · airframe 54,574 hrs · 9,562 cycles

INSPECTION TYPE:4C, RT WING LOWER STRINGER 33 CRACKED AT STA XORS 1070. ACCOMPLISHED REPAIR ON RT WING LOWER STRINGER 33 AT STA XORS 1070 IAW VT-SAA EA 011-5710-01-A5793, REV I/R AND EO MD11-5710-57370-A.

Part: STRINGER — CRACKED (BS 1305) · airframe 54,574 hrs · 9,562 cycles

INSPECTION TYPE:4C, LONGERON 27R FITTING CRACKED BS 1305. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT L27R FITTING IAW DWG AEA7127, SRM 51-33-01, 51-31-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,574 hrs · 9,562 cycles

INSPECTION TYPE:4CR3, DOOR FORWARD JAMB HAS CRACK IN SKIN AT LOWER LIGHTING HOLE ACCOMPLISHED REPAIR ON R3 FORWARD JAMB AT LOWER LIGHTING HOLE STA 1250 TO 1256 IAW SRM 53-40-15, FIG 201, REPAIR 3.

Part: SKIN — CORRODED (FUSELAGE) · airframe 54,574 hrs · 9,562 cycles

INSPECTION TYPE:4C, DISCOVERED CORROSION ON CENTER WING TANK UPPER SKIN PANEL ON STRINGER 15 BETWEEN XCW =-78 AND XCW =-118. ACCOMPLISHED BLEND REPAIR ON CENTER WING TANK UPPER SKIN PANEL ON STRINGER 15 BETWEEN XCW=-78 AND XCW=-118 IAW VT-SAA EA 011-5730-01-A5798, REV I/R AND EO MD11-5730-57366-A.

Part: SKIN — CRACKED (LT WING) · airframe 54,574 hrs · 9,562 cycles

INSPECTION TYPE:4C, LEFT WING FIXED L/E EXTERIOR SKIN CRACKED ADJACENT TO NR 14 SLAT TRACK DOOR. REPAIRED LT WING L/E SKIN FS XOS 886-891 IAW SRM 57-40-02, REPAIR 7, FIG 201.

Part: SKIN — CORRODED (BS 1273) · airframe 54,574 hrs · 9,562 cycles

INSPECTION TYPE:4C, DISCOVERED CORROSION ON CENTER WING UPPER SKIN PANEL STA 1273 ON STRINGER 9 BETWEEN XCW =-101.85 AND XCW =-118.20. ACCOMPLISHED BLEND REPAIR ON CENTER WING UPPER SKIN PANEL STA 1273 ON STR 9 BETWEEN XCW=-101.85 AND -118.20 IAW VT-SAA EA 011-5730-01-A5799, REV I/R AND EO MD11-5730-57367-A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,574 hrs · 9,562 cycles

INSPECTION TYPE:4CL3, DOOR FORWARD JAMB HAS CRACK IN SKIN AT LOWER LIGHTING HOLE ACCOMPLISHED REPAIR ON L3 FORWARD JAMB AT LOWER LIGHTING HOLE FS 1250 TO 1256 IAW SRM 53-40-15, FIG 201, REPAIR 3.

Part: STRINGER — CRACKED · airframe 54,574 hrs · 9,562 cycles

INSPECTION TYPE: 4C, CENTER WING TANK LOWER LOWER STRINGER 47 CRACKED AT XCW =17 AND XCW =-17. ACCOMPLISHED SPLICE REPAIR ON CENTER WING TANK LOWER STRINGER 47 FROM XCW=32 TO XCW =-32 IAW VT-SAA EA 011-5710-01-A5791, REV I/R AND EO 5710-57361-A.

Part: SPAR CAP — CORRODED (RT WING) · airframe 54,574 hrs · 9,562 cycles

INSPECTION TYPE:4C, RIGHT WING REAR SPAR UPPER CAP HAS CORROSION BETWEEN STA XORS 1012 TO XORS 1051. ACCOMPLISHED BLEND REPAIR ON RT WING REAR SPAR UPPER CAP AFT HORIZONTAL FLANGE BETWEEN STA XORS 1012 TO 1051 IAW VT-SAA, EA 011-5710-01-A5796, REV I/R AND EO MD11-5710-57360-A.

Part: BATTERY PACK — INOPERATIVE (FLIGHT DECK)

DURING PREFLIGHT THE LEVEL 1 ALERT FOR EMERGENCY LIGHT BATTERY ONE LOW ILLUMINATED. R & R POWER SUPPLY EMERGENCY LIGHTING BATTERY AND TESTED NORMAL IAW AMM 33-51-01-401. ACFT OK FOR SERVICE, REF IPC 33-51-10-01.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 51,953 hrs · 8,926 cycles

1C INSPECTION, LT INBD FLAP LOWER SKIN CHAFE DAMAGE. SKINNED LT INBD FLAP OTBD WEDGE LOWER SURFACE BETWEEN XIFH 237-276 IAW SRM 57-50-01, REPAIR 1, FIG 201.

Part: SPAR CAP — CORRODED (LT WING) · airframe 51,953 hrs · 8,926 cycles

INSPECTION TYPE:1C, LT WING REAR SPAR UPPER CAP AFT FLANGE CORRODED XORS 779-800 REPAIRED LT WING REAR SPAR UPPER CAP AFT FLANGE IAW EA 011-5710- 01-A5121 REV IR AND EO MD11-5710-53624-A.

Part: SKIN — CORRODED (BS 1227) · airframe 51,953 hrs · 8,926 cycles

1C INSPECTION, CENTER WING UPPER SKIN CORRODED NEAR BS 1227, RBL 36 ABOVE STRINGER 15. REPAIRED SKIN PANEL IAW EA 011-5730-01-AS111 IR AND EO 730-53574-A.

Part: STRINGER — CRACKED (LT WING) · airframe 51,953 hrs · 8,926 cycles

1C INSPECTION, CRACK ON LT WING STRINGER 31L AT XORS 948.85. REPAIRED BETWEEN XORS 933 AND XORS 964 IAW EA 011-5710-01-A5112 IR AND EO MD11-571053622-A.

Part: STRINGER — CRACKED (RT WING) · airframe 51,953 hrs · 8,926 cycles

1C INSPECTION, CRACK ON RT WING STRINGER 31 AT XORS 980.8. REPAIRED BETWEEN XORS 965 .55 AND XORS 997.43 IAW EA 011-5710-01-A5113 IR AND EO 5710-53621-A.

Part: STRINGER — CRACKED (RWS 697) · airframe 51,953 hrs · 8,926 cycles

1C INSPECTION, RT WING STRINGER 11 CRACKED NEAR XORS 697. REPAIRED STRINGER 11R BETWEEN XORS 683-713 IAW SRM 57-00 -03, REPAIR 5, FIG 202.

Part: LIGHT — INOPERATIVE (COCKPIT)

EMERGENCY LIGHT INOPERATIVE. OPEN.

Part: WIRE — LOOSE (EMERGENCY LIGHT)

EMERGENCY LIGHT INOPERATIVE. FOUND WIRE B203-1187-20 PULLED OUT OF CONTACT AT R5-5700 TERMINAL 3A, REF SWPM 20-31-06 AND WDM 33-51-01. EMERGENCY LIGHTING SYS OPS CHECKED NORMAL. REF AMM 33-50-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHT BATTERY 1 LOW. R & R POWER SUPPLY BATTERY.

Part: DOUBLER — CRACKED (RT WING) · airframe 49,857 hrs · 8,321 cycles

INSPECTION TYPE: 2C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 561. REPAIRED RT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS559-565 IAW EO MD11-5730-48222-A. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 49,857 hrs · 8,321 cycles

INSPECTION TYPE:2C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 627. REPAIRED RT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS625-629 IAW EO MD11-5730-48222-A. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 49,857 hrs · 8,321 cycles

INSPECTION TYPE: 2C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 613. REPAIRED RT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS610-616 IAW EO MD11-5730-48222-A. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 49,857 hrs · 8,321 cycles

INSPECTION TYPE:2C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 638. REPAIRED RT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS636-648 IAW SRM 57-40-02, REPAIR 15, FIG 203. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 49,857 hrs · 8,321 cycles

INSPECTION TYPE:2C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 700. REPAIRED RT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS 698-708 IAW SRM 57-40-02, REPAIR 15, FIG 203. (MAJOR).

Part: DOUBLER — CRACKED (LT WING) · airframe 49,857 hrs · 8,321 cycles

INSPECTION TYPE: 2C, LT WING L/E INNER BEADED DOUBLER CRACKED NEAR XOS 770. REMOVED EXISTING REPAIR DOUBLER BETWEEN XOS 763-768. INSTALLED NEW REPAIR TO INCORPORATE INTERNAL BEADED DOUBLER DAMAGES BETWEEN XOS 763- 772 IAW SRM 57-40-02, REPAIR 15, FIG 203.

Part: DOUBLER — CRACKED (LT WING) · airframe 49,857 hrs · 8,321 cycles

INSPECTION TYPE: 2C, LEFT WING BEADED DOUBLER CRACKED NEAR XOS 645. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS 643-648 IAW SRM 57-40-02, REPAIR 15, FIG 203. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 49,857 hrs · 8,321 cycles

INSPECTION TYPE: 2C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 670. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS 667-673 IAW SRM 57-40-02, REPAIR 15, FIG. 202. (MAJOR).

Part: LIGHT — MALFUNCTIONED (COCKPIT)

FOUND EMERGENCY LIGHT SYS TEST FAIL DUE TO BATTERY LOW, INTERMITTENT. PERFORMED OPS TEST OF EMERGENCY LIGHTING IAW MM 33-51-01-700-802. OPS CHECKED GOOD.

Part: SKIN — CRACKED (LT AILERON) · airframe 47,033 hrs · 7,573 cycles

INSPECTION TYPE: C3, LEFT OTBD AILERON HAS A CRACK AT XOA 1021. MX INITIATED ON NRC 480980. IDENTIFIED AREA OF DAMAGE. TRIMMED OUT DAMAGED AREA. INSPECTED AND IAW FORMED TAP TEST OF DAMAGED AREA IAW SRM 51-61-01. REPAIRED DAMAGED AREA WITH COMPOSITE MATERIAL IAW SRM 57-60-80, REPAIR 1. ACCOMPLISHED IAW EA 011-5750-01-A3445, REV IR. AND EO-5750-44299A.

Part: SKIN — CRACKED (LT AILERON) · airframe 47,033 hrs · 7,573 cycles

INSPECTION TYPE:C3, LT OTBD AILERON HAS A CRACK AT XOA991.5. MX INITIATED NRC 4 80980. IDENTIFIES DAMAGED AREA. TRIMMED OUT DAMAGE. PERFORMED INSP AND TAP TEST IAW SRM 51-61-01. REPAIRED DAMAGED AREA WITH COMPOSITE MATERIAL IAW SRM 57-60-80, REPAIR 1. ACCOMPLISHED EA 011-5750-A3445 REV IR A ND EO 5750-44299A.

Part: SKIN — GOUGED (LT AILERON) · airframe 47,033 hrs · 7,573 cycles

INSPECTION TYPE:C3, LT OTBD AILERON INBD UPPER COVER ASSY GOUGED IN 3EA AREAS. IDENTIFIED AREAS OF DAMAGE. TRIMED OUT DAMAGED AREAS. INSPECTED AND PERFORMED TAP TEST OF DAMAGED AREAS IAW SRM 51-61-01. REPAIRED DAMAGED AREAS WITH COMPOSITE MATERIAL AND PROCCESS IAW SRM 57-60-80. ACCOMPLISHED EA 011-5750-01-A3445, REV IR AND EO MD11-5750-44299A.

Part: SPAR — CORRODED (RT WING) · airframe 47,033 hrs · 7,573 cycles

INSPECTION TYPE:3C, BULGING SKIN ABOVE RT WING REAR SPAR UPPER SURFACE BETWEEN XORS786-830. REPAIRED CORROSION ON RT WING REAR SPAR UPPER CAP AFT FLANGE BETWEEN XORS 786-830 IAW SRM 51-21-01, STA EA 011-5710-01-A3438 REV IR AND EO MD11-5710-44282-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 47,033 hrs · 7,573 cycles

INSPECTION TYPE:3C, LT WING L/E COMPT, JUST ABOVE INBD FUEL RECEPTACLE, BEADED DOUBLER CRACKED. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS610-616 IAW SRM 57-40-02, REPAIR 9, FIG 203 & EO MD11-5730-42916-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 47,033 hrs · 7,573 cycles

INSPECTION TYPE:3C, LT WING FIXED L/E COMPT, INBD SIDE OF SLAT TRACK NR 8, BEADED DOUBLER CRACKED. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS542-547 IAW SRM 57-40-02, REPAIR 9, FIG 203 & EO MD11-5730-42916-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 47,033 hrs · 7,573 cycles

INSPECTION TYPE:3C, LT WING L/E COMPT OTBD OF SLAT TRACK NR 11 BEADED DOUBLER CRACKED. REPAIRED LT WING FIXED L/E INTERIOR BEADED DOUBLER BETWEEN XOS726-734 IAW SRM 57-40-02, REPAIR 9, FIG 203 AND EO MD11-5730-42916-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 47,033 hrs · 7,573 cycles

INSPECTION TYPE:3C, LT WING L/E COMPT, INBD OF SLAT TRACK NR 12, BEADED DOUBLER CRACKED. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BEWTEEN XOS763-768 IAW SRM 57-40-02, REPAIR 9, FIG 203 & EO MD11-5730-42916-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 47,033 hrs · 7,573 cycles

INSPECTION TYPE:3C, LT WING L/E COMPT INBD OF SLAT TRACK NR 11 BEADED DOUBLER CRACKED. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BEWTEEN XOS698-703 IAW SRM 57-40-02, REPAIR 9 FIG 203 & EO MD11-5730-42916-A.

Part: STIFFENER — CRACKED (LT WING) · airframe 47,033 hrs · 7,573 cycles

INSPECTION TYPE:3C, LT WING L/E COMPT, OTBD OF SLAT TRACK NR 10 L/E STIFFENER FOUND CRACKED. REPAIRED STIFFENER (STRINGER) IN LT WING L/E COMPT AT STA XOS667 IAW SRM 57-40-03, REPAIR 2 & DWG ARB2932.

Part: SKIN — CRACKED (LT AILERON) · airframe 47,033 hrs · 7,573 cycles

INSPECTION TYPE:3C, LT OTBD AILERON UPPER L/E EDGE PANEL IS CRACKED AT 3EA OTBD HINGES STRICKERS. IDENTIFIED DAMAGED AREAS. PERFORMED TAP TESTS FOR DELAMINATION. CUTOUT DAMAGED AREAS. REPAIRED DAMAGED AREAS WITH COMPOSITE MATERIAL IAW SRM 57-60-80, REPAIR 1. ACCOMPLISHED WEIGHT AND BALANCE IAW SRM 51-91-07. ACCOMPLISHED EA 011-5750-01-A3445, REV IR AND EO MD11-5750-44299A.

Part: SLAT — DAMAGED (LT WING)

LT WING DROOPED L/E DAMAGED. REPAIRED IAW EO MD11-5750-43663A.

Part: WEB — CRACKED (FUSELAGE)

FLOOR LIGHTING HOLE TORN AND CRACKED UNDERNEATH OBSERVER SEAT REF MD11-5310-41900. DAMAGE REMOVED 18.58" X 17.34" INSTALLED NEW WEB 7075-T6 0.032" DOUBLER INSTALLED 7075-T6 0.050" REPAIR ACCOMPLISHED IAW EO MD11-5310-49100.

Part: MANIFOLD — FAILED (ANTI ICE SYSTEM)

DURING CLIMBOUT, ENGINE ANTI ICE SELECTED ON AND ENG 2 ANTI ICE DISAGREE LIGHT REMAINED ILLUMINATED ON OVERHEAD SWITCH. ENG 2 ANTIICE OFF EAD MSG DISPLAYED. DIVERTED, TROUBLESHOT NR 2 ENG ANTI ICE MANIFOLD DETECTION SYS INOP REF FR FIM 30-22-07-00, FIG 107. R & R NR 2 ENGINE COWL ANTI ICE MANIFOLD FAILURE SENSING ELEMENT D1-91 REF AMM 30-22-11-4. R & R NR 2 ENGINE ANTI ICE DUCT BURST DETECTION UNIT REF AMM 30-22-10- 4. PERFORMED OPS CHECK OF NR2 ENGINE COWL ANTI ICEMNFLD FAILURE SENSING, CHECKS GOOD REF AMM 30-22-11-5.

Part: SENSOR — INOPERATIVE (NR 2 ANTI ICE)

ON DESCENT THROUGH 14000, ENCOUNTERED MODERATE ICING. SELECTED A/I ON AND REC'D A LEVEL 1 ENG 2 A-ICE OFF ALERT. DIVERTED. REPLACED DUCT BURST SENSOR. REPLACED NR 2 ENG COWL A-ICE MAN FAIL SENSORS IAW 30-22-11-4. FOLLOWED FIM 30-22-07. RAN ENG AND TEST INSP FOR LEAKS OR BLOWN DUCTS. NR 2 ENG ANTI ICE OPS NORMAL AT THIS TIME.

Part: VANE — GOUGED (RT WING TE FLAP) · airframe 44,124 hrs · 6,909 cycles

INSPECTION TYPE:4C, RT OTBD FLAP VANE HAS GOUGES ON OTBD SIDE. REMOVED DAMAGED GRAPHITE PLIES ON RT OTBD FLAP VANE OTBD LWR SKIN AND REPAIRED REF SRM 57-50-80, REPAIR 2, PARA 2 AND PARA 4 AND MM 51-52-0 1 PARA 8.0.

Part: VANE — GOUGED (RT WING TE FLAP) · airframe 44,124 hrs · 6,909 cycles

INSPECTION TYPE:4C, RT OTBD FLAP VANE HAS GOUGE IN INBD SIDE. REMOVED DAMAGE GRAPHITE PLIES ON RT OTBD FLAP VANE INBD SIDE AND REPAIRED REF SRM 57-50-80, REPAIR 2, FIG 201 AND SRM 51-62-01.

Part: SPLICE — CRACKED (STA 1129 L3L) · airframe 44,124 hrs · 6,909 cycles

INSPECTION TYPE:4C, MAIN CABIN LONGITUDINAL SPLICE CRACKED AT STA 1129/6-100 AND L3L. REMOVED LONGITUDINAL SPLICE FITTING AT STA 1129/6-100 AND L3L. FABICATED SPLICE FITTING AND INSTALLED REF DWG A6A7112 AND SRM 51-33-01, PG 30 PARA 5.

Part: SPLICE — CRACKED (STA 1531 L5R) · airframe 44,124 hrs · 6,909 cycles

INSPECTION TYPE:4C, MAIN CABIN LONGERON SPLICE FITTING IS CRACKED AT STA 1531/5-0 L5R. R & R LONGERON SPLICE FITTING AT STA 1531/ 5-0 AND L5R REF SRM 51-31-01 PG 1 AND SRM 51-33-01, PG 30, PARA 8.

Part: LONGERON SPLICE — CRACKED (STA 1531 L24R) · airframe 44,124 hrs · 6,909 cycles

INSPECTION TYPE:4C, MAIN CABIN LONGERON SPLICE FITTING IS CRACKED AT STA 1531/5-123 AND L24R. REMOVED LONGERON SPLICE FITTING AT STA 1531/5-123 AND L24R. FABRICATED AND INSTALLED SPICE FITTING REF DWG A6A7112 AND SRM 51-33-01, PG 36, TABLE 13.

Part: LONGERON SPLICE — CRACKED (STA 1531 L43R) · airframe 44,124 hrs · 6,909 cycles

INSPECTION TYPE:4C, CTR CARGO COMPT LONGERON SPLICE FITTING CRACKED AT L43R STA 1531/5-123. REMOVED LONG SPLICE FITTING IN CTR CARGO COMPT AT L43R STA 1531/5-123. FABRICATED AND INSTALLED REPLACEMENT FITTING REF DWG A5A7114 AND SRM 51-31-01, PG 1 AND SRM 51-33-01, PG 30.

Part: LONGERON SPLICE — CRACKED (BS 1531 L37R) · airframe 44,124 hrs · 6,909 cycles

INSPECTION TYPE:4C, CTR CARGO COMPT LONGERON SPICE FITTING CRACKED AT L37R STA 1531/5-1 23. REMOVED LONGERON SPICE FITTING IN CTR CARGO COMPT AT L37R AND STA 1531 /5-123. FABBED AND INSTALLED REPLACEMENT LONGERON SPICE FITTING REF DWG A5A7114, MD11 SRM 51-31-01 PG1, MD11 SRM 51-33-01 PG 30-31.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 44,124 hrs · 6,909 cycles

INSPECTION TYPE:4C, RT INBD FLAP LOWER OTBD SKIN CHAFED ALL THE WAY AROUND THE AFT FAIRING. BLENDED RT INBD FLAP LOWER OTBD SKIN AT XIFH 269. REPAIRED IAW EO MD11 5750-38704 AND EA 011-5700-01-A2518.

Part: VANE — DELAMINATED (RT TE FLAP) · airframe 44,124 hrs · 6,909 cycles

INSPECTION TYPE:4C, RT INBD FLAP VANE DELAMINATED ON LWR SURFACE AND 65 INCH FROM IB END, CUT OUT DAMAGE ON RT INBD FLAP VANE LWR SURFACE. PREPPED AND BONDED DISC REPAINT AREA REF SRM 51-50-80 REPAIR 2 PARA 4D.

Part: FLOOR PANEL — CORRODED (BS 480 RBL 78) · airframe 44,124 hrs · 6,909 cycles

INSPECTION TYPE:4C, COURIER COMPT FLOOR PANEL CORRODED AT GALLEY WATER DRAIN CONNECTIONS, STA 480 RBL 78. REMOVED CORROSSION FROM RCB FLOORBOARD PNL AROUND WATER DRAIN AT STA 480 RBL 78. TREATED, PRIMED AND TOP COATED REF EA 011-5320-01-A2483 AND EO MD11-5310-38330-A.

Part: STRUCTURE — ERODED (RT ELEVATOR) · airframe 44,124 hrs · 6,909 cycles

INSPECTION TYPE:4C, RT OTBD ELEVATOR HAS SEVERAL AREAS OF AERO DYNAMIC FILLER BUBBLED AND PEELING FROM WIND EROSION. REMOVED DAMAGED AREA OF ASTROSTRIKE ON RT OTBD ELEVATOR PREPPED AND BONDED REPLACEMENT ASTROSTRIKE CURING 70 MIN AT 160 TO 180 DEGREES F. PREPPED AND PAINTED REPAIR AREA IAW SRM 51-21-05, PARA 4C.

Part: TORQUE BOX — CRACKED (FUSELAGE)

3/8 INCH CRACK IN CORNER OF CUTOUT IN UPPER TORQUE BOX FOUND DURING TAIL TANK TRANSFER PIPE INSPECTION EO MD11-2820-14180-K MAJOR REPAIR - REPAIRED PER EO MD11-5310-35352-A

Part: SKIN — CRACKED (LT WING) · airframe 41,698 hrs · 6,312 cycles

INSPECTION TYPE-C LT WING L/E LOWER ACCESS COMPT. NR519CB, FOUND EXISTING REPAIR ON BEADED DOUBLER AS MARKED. EXISTING REPAIR AT ABOVE-MENTIONED AREA, 02 EA RIB AND REPAIR AREA FASTENER REMOVED. CRACK AREA AT EXISTING REPAIR DOUBLER REMOVE AREA TRIM OFF. REPAIR ANGLES FOR BEADED DOUBLER FABRICATED AND HEAT-TREATED. HFEC C/O ON TRIMMED EDGE AND FOUND NO CRACK EVIDENT. REPAIR FILLER AND DOUBLER FABRICATED. REPAIR PARTS INSTALLED IAW SRM 57-10-00, FIG27, VOLI, REV40.

Part: SKIN — DAMAGED (TE FLAP) · airframe 41,698 hrs · 6,312 cycles

INSPECTION TYPE-C REPAIR SEQUENCE NBR 280-W4-007, RT INBD FLAPS OUTER SKIN SURFACE STA XIFH 153.3 23 INCH AWAY FROM FLAPS L/E. REPAIR NEEDS VALIDATION. EXISTING REPAIR DOUBLER REMOVED. 10X VISUAL INSP C/O, FOUND NO CRACK OR CORROSION. HFEC INSP C/O ON EXISTING TRIMMED OUT AREA, FOUND NO CRACK EVIDENT. REPAIR DOUBLER AND FILLER FABRICATED IAW EN 1247-09. REPAIR PARTS HOLES PICKED-UP, PROTECTED, PAINTED AND BONDED. REPAIR PARTS INSTALLED IAW EN 1247-09.

Part: SKIN — DAMAGED (LE SLAT) · airframe 41,698 hrs · 6,312 cycles

INSPECTION TYPE-C REPAIR SEQUENCE NR 280-W3-009, LT NR5 SLAT INNER SKIN SURFACE STA XOS 773 REPAIR NEEDS VALIDATION. EXISTING DOUBLER REMOVED. HFEC AND 10X VISUAL INSP C/O ON EXISTING DOUBLER REMOVE AREA, FOUND NO CRACK OR CORROSION EVIDENT. REFER TO NRC: MD038229 FOR REPAIR WORK DETAILS.

Part: SKIN — MISREPAIRED (NR 5 SLAT) · airframe 41,698 hrs · 6,312 cycles

INSPECTION TYPE-C REPAIR SEQUENCE NBR 280-W3-008, LT NR 5 SLAT INNER SKIN SURFACE STA XOS 770 REPAIR NEEDS VALIDATION. EXISTING REPAIR REMOVED. HFEC AND 10X VISUAL INSP C/O ON DOUBLER REMOVED AREA, FOUND NO CRACK OR CORROSION EVIDENT. 02 EA FILLERS AND 01 EA REPAIR DOUBLER FABRICATED IAW EN 1246-09. IDENTIFICATION PLATE MS27253-1 REMOVED AND RELOCATED TO NEW POSITION IAW EN 1246-09. REPAIR PARTS INSTALLED IAW EN 1246-09.

Part: SKIN — DAMAGED (LE SLAT) · airframe 41,698 hrs · 6,312 cycles

INSPECTION TYPE-C REPAIR SEQUENCE NR 280-W3-002, LTW NR 3 SLAT NR3 INNER SKIN STA XOS 451-459 REPAIR NEEDS. EXISTING REPAIR AT LTW NR 3 SLAT REMOVED IAW EN 1242-09. HFEC INSP C/O ON EXISTING TRIM EDGE,FOUND NO CRACK EVDNT. 10X VISUAL INSP C/O ON DOUBLER REMOVED AREA FOUND NO CRACK AND NO CORROSION EVIDENT. REPAIR DOUBLER AND RING DOUBLER FABRICATED IAW EN 1242-09. REPAIR PARTS HOLES PICKED-UP, PROTECTED, PAINTED AND INSTALLED IAW EN 1242-09.

Part: DOUBLER — CHAFED (LT WING) · airframe 41,698 hrs · 6,312 cycles

INSP TYPE-C REPAIR SEQUENCE NBR 280-W3-001, LT FIXED LEADING EDGE STA XORS 372 BETWEEN ANTI ICE TELESCOPIC DUCT REPAIR NEEDS VALIDATION. FOUND CHAFED MARKED ON DOUBLER AS MARKED. CHAFE MARK ON DOUBLER REMOVED. ORG THK 0.063INCH, MATL REMOVED 0.023 INCH, MATL REMAIN 0.040 INCH AND FOUND EXCEED LIMITS. DAMAGED DOUBLER REMOVED. HFEC INSP C/O ON EXISTING CUT OUT AREA, FOUND NO CRACK EVIDENT. 10X VISUAL INSP C/O ON DOUBLER REMOVE AREA, FOUND NO CRACK OR CORROSION. REPAIR DOUBLER AND FILLER FAB AND INSTALLED IAW EN 1253-09.

Part: STRUCTURE — CRACKED (LT WING) · airframe 39,283 hrs · 7,983 cycles

INSPECTION TYPE:2C LT WING OUTBOARD L/E FIXED PANEL, SLAT ANTI-ICE DUCT ACCESS CUTOUT AREA FOUND UPPER CORNER CRACKED. CUT OUT TWO EACH AREAS, FABRICATED 2 EA DOUBLERS AND FILLERS, AND INSTALLED IAW MD11 SRM 57-10-00, 51-35-01, 51-21-01, AND 51-21-02.

Part: STRAP — CRACKED (RT WING) · airframe 39,283 hrs · 7,983 cycles

INSPECTION TYPE:2C RIGHT WING L/E SPLICE STRAP XFS 669 CRACKED. REMOVED, FABRICATED, AND INSTALLED SPLICE STRAP IAW MD11 SRM 51-21-01, 51-33-01, AND DWG ARB3954.

Part: STRINGER — CRACKED (LT WING) · airframe 39,283 hrs · 7,983 cycles

INSPECTION TYPE:2C LT WING L/E FIXED PANEL SUPPORT LOWER STRINGER FOUND CRACKED AT WING STA YORS AS MARKED, JUST O/B OF SLAT DRIVE MECHANISM. FABRICATED AND INSTALLED DOUBLER IAW MD11 SRM 57-10-00 FIG 18, 51-31-01, AND 51-21-01.

Part: SKIN — CRACKED (RT WING) · airframe 39,283 hrs · 7,983 cycles

INSPECTION TYPE:2C RIGHT WING OUTER ACCESS PNL LANDING HAS CRACK. CRACK BETWEEN UPPER AND LOWER HINGE. VIEWED WITH MIRROR. FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD11 SRM 57-10-00 FIG 18.

Part: FITTING — CRACKED (RH WINGLET) · airframe 39,283 hrs · 7,983 cycles

INSPECTION TYPE:2C RT WING LWR WINGLET FWD ATTACH FITTING ANGLED CLIP CRACKED AND AFT ATTACH FITTING CRACKED. REMOVED AND REPLACED FWD ATTACH FITTING ANGLED CLIP AND AFT ATTACH FITTING IAW UPS EO MD11-5720-27680-A APPENDIX E.

Part: FITTING — CRACKED (RH WINGLET) · airframe 39,283 hrs · 7,983 cycles

INSPECTION TYPE:2C FOUND CRACK AROUND SMALL HOLE ON RT WING LWR WINGLET. REMOVED CRACKED WEB (BOX FITTING) AND REPLACED IAW MD-11 SRM 51-31-01.

Part: ANTI-ICE VALVE — STUCK (NR 2 ENGINE)

ATB - NR 2 ENG ANTI-ICE LVL 1 ENG 2 ANTI-ICE OFF ALERT APPEARED. COULD NOT GET ENG 2 ANTI-ICE HEAT TO COWL. ACCOMPLISHED FIM 30-22-007 AND 30-22-04, FOUND NR 2 ENG ANTI-ICE VALVE NOT RESPONDING AND STUCK IN MID POS. REMOVED AND REPLACED VALVE PER AMM 30-22-04. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)

INSPECTION TYPE:N/A EMERGENCY BATTERY LOW. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PER 33-51-01-4. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:P-3 EMERGENCY LIGHT INOP AT L1 FWD LOWER DOOR FRAME. RELAMPED, OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY LIGHT BATTERY 1 LO EMERGENCY LIGHT TEST FAIL. DEFERRED PER MEL 33-50-02. VERIFIED OPER OF EMERGENCY LIGHTING PERFORMED PER DMP 33-50-2 PLACARD INSTALLED D327548.

Part: SEAT TRACK — CORRODED (BS 855-890) · airframe 31,257 hrs · 4,456 cycles

MAIN DECK MID ENTRY AREA, SEAT TRACK ALONG 8.5 RBL, BETWEEN STA 855 AND STA 890, CORROSION FOUND ON BASE. SEAT TRACK BET STA 855 AND 890 CORROSION ON BASE. REMOVED 53-70-00, SEAT TRACK FASTENERS REMOVED, SPLICE CUT AT STA 832 TO 949. REPAIR SPLICE AND SPLICE PLATE FAB 53-70-00. HFEC INSP SATISFACTORY. REPAIR SEAT TRACK REWORKED, HOLE TRANSFERRED TO REPAIR PART, REPROTECTED AND PAINTED. SEAT TRACK EXT REPAIR SPLICE HATS AND SPLICE INSTALLED BET STA 832 TO 949, SRM 51-31-01, 53-70-00.

Part: SEAT TRACK — CORRODED (BS 855-875) · airframe 31,257 hrs · 4,456 cycles

INSPECTION TYPE:C, MAIN DECK MID-ENTRY AREA, SEAT TRACK ALONG LBL 8.5, CORROSION FOUND ON BASE, BETWEEN STA 855 AND STA 875. M/D MID ENTRY AREA CORROSION REMOVED FROM STA 855 TO STA 875. SEAT TRACK FASTENERS REMOVED & SPLICE CUT AT STA 832 TO STA 949, SRM 53-70-00 FIG 1 VOL 1 REV 37. HFEC CARRIED OUT & FOUND NO CRACK EVIDENT. REPAIR SPLICE FAB AS PER SRM 51-31-01 VOL II REV 37, REWORKED AREA REPROTECTED AND PAINTED. NEW SEAT TRACK EXT INSTALLED PER SRM 51-31-01 VOL II, 53-70-00 VOL I REV 37.

Part: SEAT TRACK — CORRODED (BS 865-887) · airframe 31,257 hrs · 4,456 cycles

MAIN DECK MID-ENTRY AREA, SEAT TRACK ALONG RBL 27.5, CORROSION FOUND ON CROWN, BETWEEN STA 865 AND STA 887. MID ENTRY SEAT TRACK BET STA 865 AND 887 CROWN REMOVED SRM5 3-70-00 FIG 3 VOL I REV 37, MAT THK 0.145 INCH AND MAT REMOVED 0.035" EXCEED LIMIT 53-70-00. SEAT TRACK FASTENERS REMOVED AND SPLICE CUT BET STA 832 AND 909. HFEC INSP SATISFACTORY. REPAIR SPLICE PLATE FAB SRM 53-70-00, HOLES PICK-UP, REPROTECTED AND PAINTED. SEAT TRACK EXTRUSION INSTALLED BETWEEN STA 832 TO 909, SRM 51-31-01.