N259UP

MCDONNELL DOUGLAS MD-11F Fatal injury Part 121 — UNITED PARCEL SERVICE CO. Not yet finalized — may be revised.

ATA 5313

CENTER CARGO BILGE AREA STA 5-11 TO 5-32 LONGERON 49R HAS CORROSION. PERFORMED A DVI CENTER CARGO AREA BETWEEN STA 5-11 & 5-32 NO DEFECTS NOTED IAW EA 0115310-01-B0566 STEP 6.

ATA 5313

CTR CARGO BILGE AREA STA 5-53 TO 5-73 LONGERON 48L HAS CORROSION. 74-049 ATA CODE 53 QC AUDIT C/W

ATA 5313

CENTER WING UPPER FUEL TANK LOWER STRINGER 41 CRACK AT XCW = -81 REQUIRES PERMANENT REPAIR PER EO 81811-REQ001 ATA 57-11 QC AUDIT C/W

ATA 5210

SLIDING PANEL ATTACHED TO L1 ENTRY DOOR INOP INSTALLED SPRING IAW AMM 25-23-23/401 AND IPC 25-23-04-15. OPS CHECK GOOD. SLIDING PANEL OPENS AND CLOSES WITH NORMAL DOOR OPERATION WITH NO ISSUES. THIS CLOSES DEFERRAL. PLACARD REMOVED.

ATA 5210

R1 DOOR ASSIST BOTTLE DEPLETED. REMOVED AND REPLACED R1 DOOR ASSIST BOTTLE CHARGE VALVE IAW AMM 52-11-04-400-801 (H)(J)(K). C/W SERVICING IAW 12-25-04-600-801

ATA 5753

ABSORB FOUND L/H WING I/B FLAP I/B ATTACHMENT MOUNT UPPER BOLT HOLE CUT-OUT IS GOUGED, DURING IN-PROCESS INSTALL VERIFIED STEP 1 AND 2

ATA 5753

INSPECTION TYPE:2CL/H WING A/C SIDE I/B FLAP O/B HINGE #3 LUG I/B FACE HAS CORROSION AT REF STA.XW=254,YW=495.961 AND ZW=-28.941REPAIR ACCOMPLISHED IAW VTSAA EA 011/5740-01-B0094 I/R DATED 09/25/2023, UPS EO. MD11-5740-88267-A DATED 09/26/2023 AND 8100-9 SIGNED BY STEPHEN KANG AR-605677 DATED SEP. 22,2023 (MINOR)

ATA 5753

INSPECTION TYPE:2CL/H WING A/C SIDE I/B FLAP O/B HINGE #3 LUG BORE HAS CORROSION AT REF STA. XW=254,YW=495.961 AND ZW=28.941ACCOMPLISHED REPAIR IAW VTSAA EA 011/5740-01-B0094 I/R DATED 09/25/2023, UPS EO MD11-5740-88267-A AND 8100-9

ATA 5753

INSPECTION TYPE:2CL/W A/C SIDE I/B FLAP O/B HINGE # 3 LUG O/B FACE HAS CORROSION AT REF STA. XW=254 , YW= 495.961 AND ZW=-28.941ACCOMPLISHED REPAIR IAW VTSAA EA 011/5740-01-B0094 I/R DATED 09/25/2023 , UPS EO MD11-5740-88267-A 8100-9 SIGNED BY STEPHEN KANG AR-605677 DATED SEP. 22 2023.(MINOR)

ATA 5320

INSPECTION TYPE:2CAFT CARGO COMP STA 1954 UNDER FLOOR PANEL 187HF ANGLE SUPPORT HAS CRACKREPLACED ANGLE SUPPORT IAW MD11-SRM 51-35-01-0G-01. (MINOR)

ATA 5350

INSPECTION TYPE:2CTAIL CONE FWD HORIZONTAL FRAME HAS A GOUGE R/H SIDEREPAIRED WITH DOUBLER IAW SRM 53-00-00-2R-1 FIG. 201 AND 53-80-02-01-1 . (MINOR)

ATA 5350

INSPECTION TYPE:2CTAIL CONE COMP RH PATIO DOOR FWD SIDE FRAME AND METAL PLATE HAS DEEP GOUGEDREPLACED SUPPORT ANGLE FRAME AT TAIL CONE COMP. R/H PATIO DOOR FWD SIDE FRAME AND METAL PLATE IN REF.MD11 SRM 51-35-01-0G-0 AND SRM 51-33-01-0G-0(MINOR)

ATA 5340

INSPECTION TYPE:2CUPPER CENTER TANK CRACKED BRACKET AT STA -81/STR52REPLACED BRACKET IAW MD11 SRM 51-31-01 AND SRM 51-33-01. MINOR

ATA 5753

L/H WING I/B FLAP IB ACTUATOR UPPER LUG IS WORN AT STA XIFH=116.850, YIFH=43.493. REPAIRED WORN LUG ATTACHMENT AT THE L/H WING I/B FLAP I/B ACTUATOR UPPER LUG AT STA XIFH=116.80, YIFH=43.493 IAW VTSAA EA 011-5700-01-B0104 I/R, UPS EO MD11-5740-88219-A DATED 09/29/23 (MINOR)

ATA 5753

R/H WING I/B FLAP SIDE O/B HINGE #14 LUG BORE HAS CORROSION AT STA XW=-254, YW=495.96. REPAIRED CORRODED HINGE BRACKET AT THE R/H WING I/B FLAP SIDE O/B HINGE AT STA XW=-254, YW=495.96 IAW VTSAA EA 011-5740-01-B0105 I/R, UPS EO MD11-5750-88271-A DATED 09/28/23 AND FAA FORM 8100-9 SIGNED BY J.TOM (AR-605565) DATED 09/28/23. (MINOR)

ATA 5753

INSPECTION TYPE:2CR/H WING O/B FLAP I/B HINGE #4 LUG BORE HAS CORROSION.REPLACED CORRODED HINGE-BRACKET AT THE R/H WING O/B FLAP I/B HINGE IAW AMM 57-53-01-400-801. (MINOR)

ATA 5753

INSPECTION TYPE:2CL/H WING O/B FLAP O/B HINGE-BRACKET #4 LUG BORE HAS CORROSION.REPLACED CORRODED HINGE-BRACKET AT THE L/H WING O/B FLAP O/B HINGE IAW AMM 57-53-01-400-801. (MINOR)

ATA 5753

INSPECTION TYPE:2CL/H WING I/B FLAP O/B HINGE #14 LUG BORE IS GOUGED AT STA XW=254, YW=495.96.REPAIRED L/H WING I/B FLAP O/B HINGE AT STA XW=254, YW=495.96 IAW VTSAA EA 011-5740-01-B0101 I/R, UPS EO MD11-5750-88274-A

ATA 5753

INSPECTION TYPE:2CR/H WING O/B FLAP O/B HINGE #13 LUG BORE HAS CORROSION AT STA XW=-638.305, YW=670.239.REPAIRED CORRODED HINGE BRACKET AT THE R/H WING O/B FLAP O/B HINGE AT STA XW=-638.305, YW=670.239 IAW EA 011-5740-01-B0106 I/R, UPS EO MD11-5750-88273-A.

ATA 5753

INSPECTION TYPE:2CR/H WING O/B FLAP I/B HINGE #13 LUG BORE HAS CORROISON AT STA XW=-486.403, YW=589.366.REPAIRED CORRODED HINGE-BRACKET AT THE R/H WING O/B FLAP I/B HINGE STA XW=-486.403, YW=589.366 IAW VTSAA EA 011-5740-01-B0100 I/R, UPS EO MD11-5750-88272-A.

ATA 5753

INSPECTION TYPE:2CL/H WING I/B FLAP O/B HINGE #14 LUG BORE HAS CORROSION AT STA XW=254, YW=495.96.REPAIRED CORRODED HINGE AT THE L/H WING I/B FLAP O/B HINGE AT STA XW=254, YW=495.96 IAW VTSAA EA 011-5740-01-B0101 I/R, UPS EO MD11-5750-88274-A

ATA 5753

R/H WING A/C SIDE I/B FLAP O/B HINGE #3 LUG I/B FACE HAS CORROSION AT STA XW= .254, YW= 495.961. REPAIRED CORRODED HINGE BRACKET AT R/H WING I/B FLAP O/B HINGE AT STA XW=.254, YW=495.961 IAW VTSAA EA 011-5740-01-B0095 IR, UPS EO MD11-5750-75959-J DATED 09/27/23 AND FAA FORM 8100-9 SIGNED BY S. KANG (AR-605677) DATED 09/27/23 (MINOR)

ATA 5753

R/H WING I/B FLAP SIDE O/B HINGE #13 LUG BORE HAS CORROSION AT STA XW=-254, YW=495.96. REPAIRED CORRODED HINGE-BRACKET AT THE R/H WING I/B FLAP SIDE O/B HINGE AT STA XW=-254, YW= 495.96 IAW VTSAA EA 011-5740-01-B0105 I/R, UPS EO MD11-5750-88271-A DATED 09/28/23 AND FAA FORM SIGNED BY J. TOM (AR-605565) DATED 09/28/23. (MINOR)

ATA 5753

INSPECTION TYPE:2CR/H WING A/C SIDE I/B FLAP O/B HINGE #3 LUG BORE HAS CORROISON AT STA XW=-254, YW=495.961.REPAIRED CORRODED HINGE-BRACKET AT THE R/H WING I/B FLAP O/B HINGE AT STA XW=-254, YW=495.961 IAW VTSAA EA 011-5740-01-B0095 I/R, UPS EO MD11-5740-88269-A DATED 09/29/23 AND FAA FORM 8100-9 SIGNED BY S. KANG (AR-605677) DATED 09/27/23 (MINOR)

ATA 5753

R/H WING A/C SIDE I/B FLAP O/B HINGE #3 LUG O/B FACE HAS CORROSION AT STA XW=-254, YW=495.961. REPAIRED CORRODED HINGE-BRACKET AT THE R/H WING A/C SIDE I/B FLAP O/B HINGE AT STA XW=-254, YW=495.961 VTSAA EA 011-5740-01-B0095 I/R, UPS EO MD11-5740-88269-A DATED 09/27/23 AND FAA FORM 8100-9 SIGNED BY S.KANG (AR-605677) DATED 09/27/23 (MINOR)

ATA 5320

INSPECTION TYPE:2CMAIN CABIN AT STA Y=1531, LONGERON 12L HAS A CRACKED PRODUCTION SPLICE.REPLACED CRACKED PRODUCTION SPLICE AT THE MAIN CABIN STA Y=1531, LONGERON 12L IAW SRM 51-33-01 AND DWG AEA7633. (MINOR)

ATA 5347

INSPECTION TYPE:2C*MAJOR REPAIR* MAIN CABIN R/H FLOOR SEAT TRACK AT STA Y=1541, X=-8.5 HAS CORROSION.REPAIRED CORRODED SEAT TRACK AT THE MAIN CABIN R/H FLOOR AREA STA Y=1541, X=-8.5 IAW SRM 53-00-52-2R-1 FIG. 201 REPAIR 1 (MAJOR)

ATA 5320

INSPECTION TYPE:2CMAIN CABIN AT STA Y=1531, LONGERON 11L HAS A CRACKED PRODUCTION SPLICE.REPLACED CRACKED PRODUCTION SPLICE AT THE MAIN CABIN STA Y=1531, LONGERON 11L IAW SRM 51-33-01 (MINOR)

ATA 5720

INSPECTION TYPE:2CL/H WING FIXED L/E BEADED DOUBLER AT STA XORS= 772 HAS A CRACKED.REPAIRED CRACKED BEADED DOUBLER AT THE L/H WING FIXED L/E AT STA XORS=772 IAW SRM 57-40-02 REPAIR 15 FIG 205 (MAJOR)

ATA 5350

INSPECTION TYPE:2CTAIL CONE R/H UPPER FWD PRODUCTION DOUBLER IS WORN AT STA Y=2165, X=36.5.REPAIRED PRODUCTION DOUBLER AT THE TAIL CONE R/H UPPER FWD AT STA Y=2165, X=36.5 IAW UPS EO MD11-5350-66790-B APPENDIX B. (MINOR)

ATA 5320

INSPECTION TYPE:2CR/H MLG WHEEL WELL AREA O/B AFT SIDE WALL STIFFENER HAS A CRACKED.REPLACED CRACKED STIFFENER AT THE R/H MLG WHEEL WELL AREA O/B AFT SIDE IAW SRM 51-35-01 (MINOR)

ATA 5753

INSPECTION TYPE:2CL/H WING OUT BOARD FLAP TRAILING EDGE UPPER SKIN WEDGE IS DAMAGED ATSTA XOF=498.367.REPLACED L/H WING O/B FLAP ASSY. IAW AMM 27-50-30-400-801 (MINOR)

ATA 5730

*MAJOR REPAIR* L/H WING OUTBD L/E SKIN GOUGED DAMAGED BETWEEN STA XOS=1113 AND XOS=1132.5. REPAIRED GOUGED SKIN AT THE L/H WING OUTBD L/E BETWEEN STA XOS=1113 AND XOS=1132.5 IAW VTSAA EA 011-5730-01-B0098 I/R, UPS EO MD11-5750-88290-A DATED 09/28/23 AND FAA FORM 8100-9 SIGNED BY P. LAU (AR-830967) DATED 09/27/23 (MAJOR)

ATA 2810

INSPECTION TYPE:2C*MAJOR REPAIR* CENTER WING UPPER FUEL TANK STRINGER #41 CENTER WING AT STA XCW=-81 HAS A CRACKED REPAIR.REPAIRED CRACKED STRINGER 41 AT THE CENTER WING UPPER FUEL TANK AT STA XCW=-81 IAW VTSAA EA 011-5710-01-B0087 I/R , UPS EO MD11-5710-81811-B DATED 09-06-23 AND FAA FORM 8100-9 SIGNED BY S.KANG (AR-605677) DATED 09/05/23. (MAJOR)

ATA 3240

INSPECTION TYPE:NA*A/C WAS TOWED* LEVEL 2 TIRE FAIL.BLOCK TURN BACK REJECTED TAKEOFF AROUND 110KTS FOR UNKOWN DECELERATION.LEFT CENTER GEAR TIRE IMMEDIATELY HEATED TO OVER 700 DEGREES.FUSE PLUG RELEASED. LEVEL 2 BRAKE OVERHEAT DUE TO REJECTED TAKEOFF ON #1 MAIN TIRE AND LEFT CENTER GEAR TIRE.PERFORMED HIGH ENERGY STOP INSP AMM.05-56-01-200-801 D.1-3. R&R # 1, 9 AND 10 BRAKE ASSY. 32-43-20-000/400-801 AND 32-43-20-000-802/400-802. PN OFF/ON 2609472-4(#1) SN OFF:B1249 SN ON:B0899(#9) SN OFF:B1681 SN ON:B0389(#10) SN OFF:B2125 SN ON:B0949. LEAK CHECK CW. OK FOR CONTINUE IN SERVICE IPC 32-43-01-01 ITEM#010J

ATA 3350

INSPECTION TYPE:NA*SDR FILED OPEN* EMER LT BAT 1 LO. DEFERRED PER MEL 33-50-4. DMP C/W AND PLACARD INSTALLED. R&R EMERGENCY LIGHTING BATTERY SUPPLY IAW 33 51 01 THS CLEARS DMI M807148 PLACARD REMOVED.

ATA 2120

DURING DESCENT PASSING TRHOUGH A SMOKY HAZY LAYER ON ODER ENTERED THE FLIGHT DECK. DISSIPATED AFTER 30 SEC. AFTER ENG SHUTDOWN W/APU RUNNING & AIR SELECTED ON THE SMELL/ODOR REOCCRRED. APPEARS TO BE EMANATING FROM THE REFRIG. VERIFIED SMELL IS CONCENTRATED AT REFRIG EXHAUST VENT. FAN RUN HOT. DEF, REFRIG IAW NEF 25-22-25-30-09REMOVED AND REPLACED REFRIGERATOR IAW AMM 25-37-57.

ATA 5753

INSPECTION TYPE:SV, LT WING O/B FLAP REAR SPAR AND T/E WEDGE DAMAGED AT STAXOF=498.367.REPAIRED LIH WING O/B FLAP REAR SPAR AND T/E WEDGE AT STAXOF=498.367 IAW VTSAA EA 011-575301-A9718-IR AND UPS EO MD11-5750-84886-A.

ATA 2530

INSPECTION TYPE:NA**SUPPLEMENTAL SDR** SMELLED FUMES COMING FROM THE GALLEY AREA THEN NOTICE A SLIGHT SMOKEY AIR, TURNED REFRIG SWITCH OFF, PULLED BOTH REFRIG AND HOT POT/OVEN BREAKERS, CALLED FLT CONTROL AND PER MAINT CONTROLL PULLED GALLEY BREAKER, PERFORMED QRH PROCEDURE NON-ALERT SMOKE/FIRE/FUMES CHECK LIST. WE BELIEVE IT WAS COMING FROM THE REFRIGR&R'D REFRIG W/REF TO MM 25-37-57. RESET C/B'S FOR GALLEY POWER & REFRIG PREVIOUSLY COLLARED. REFRIG OPS & TEMP OK PER MM 25-37-57. THIS CLEARS 776930.

ATA 3241

INSPECTION TYPE:N/A** EMERGENCY DECLARED** A/C TOWED OFF RUNWAY** FAA NOTIFIED**ON LANDING UNDER 60 KIAS, TIRE FAILURE. TAXIED OFF RUNWAY AND STOPPED. #10 TIRE PRESSURE 0.R&R #10 TIRE DUE TO TIRE BLOW OUT IAW MD11 AMM 32-41-01 PB 401. P/N ON & OFF MD11MN. S/N OFF H0508 S/N ON B0399.

ATA 2900

INSPECTION TYPE:3CAPPX. 250 MILES FROM SDF DURING DECENT AP1 DISCONNECTED AND WE RECEIVED A LEVEL 1 HYD. 2 OFF ALERT, HYD 2 QUANATY WAS 2.6 GALLONS, REDUCED TO 2.1 DURING APPROACH.REMOVED AND REPLACED HYD. PRESSURE LINE IN L/H W/W, LEAK CHECK IS GOOD REF. AMM 20-50-01-910-801, AND AMM 71-00-02-800-810.

ATA 5210

INSPECTION TYPE:N/A**SUPPLEMENTAL SDR OPEN** L-1 DOOR ALERT OPES'T SHOWS CLOSED ON SECONDARY DISPLAY. DEFERRED PER MEL 52-40-1-1-0-1 STICKER INSTALLED. TRANSFERRED TO NRC 458794CHK & INSPECT L-1 DOOR FOUND BROKEN SUPPORT BACKET ASSY, R & R SUPPORT BACKET ASSY ON L-1 DOOR SENSOR IN REF MD-11 SRM 51-33-01, PERFORMED OPERATIONAL CHK OPEN & CLOSE IN THE NORMAL MODE. NOW SHOW CLOSED ON SECONDARY DISPLAY IN REF MD11 AMM 52-10-01-700-801.

ATA 5530

INSPECTION TYPE:3CVERTICAL STABILIZER #4 BANJO FITTING R/H SIDE IS CRACKED.REPAIRED CRACKED VERTICAL STABILIZER #4 BANJO FITTING R/H SIDE IAW VT-SAA EA 011-5530-01-A9386 REV. I/R AND UPS EO MD11-5530-81955-A. (MAJOR) REF FAA FORM 8100-9 BY J. TOM (AR-605565) DATED 10/22/21.

ATA 5100

INSPECTION TYPE:3C#2 PYLON SPAR ANGLE IS CORRODED AT STA. YID= 380.310 & ZID= 54.5.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. AVB7510 AND SRM 51-33-01. (MINOR)

ATA 5310

INSPECTION TYPE:3CMAIN CABIN LONGERON 11L CRACK BETWEEN STA.1331 AND STA.1361.REPAIRED CRACKED LONGERON 11L BETWEEN STA.1331 AND STA. 1361 IAW VT-SAA EA 011-5310-01-A9397 REV I/R AND UPS EO MD11-5310-81923-A (MAJOR) REF. FAA FORM 8100-9 BY S.KANG (AR-605677) DATED 10/20/2021.

ATA 5710

INSPECTION TYPE:3CR/H WING REAR SPAR LWR CAP SUPPORT IS CORRORED AT STA-390.REMOVE, FABRICTED AND REPLACED CORRORED LWR CAP SUPPORT IAW DWG ARC3102 AND MD-11 SRM 51-33-01. (MINOR)

ATA 5710

INSPECTION TYPE:3CCENTER WING UPPER AUX TANK STRINGER 47 BETWEEN XCW 5.5 & XCW 28.5 IS CRACKED.REPAIRED CRACKED CENTER WING UPPER AUX TANK STRINGER 47 BETWEEN XCW 5.5 & XCW 28.5 IAW SRM 57-10-03, REPAIR 1, FIGURE 201. (MAJOR)

ATA 5710

INSPECTION TYPE:3CCENTER WIN TANK STRINGER #41 IS CRACKED AT SGTA. XCW= -81.REPAIRED CRACKED CENTER WING TANK STRINGER #41 BETWEEN STA. XCW= -69 TO XCW= -112 IAW VT-SAA EA 011-5710-01-A9389 REV. I/R AND UPS EO MD11-5710-81811-A. (MAJOR) REF FAA FORM 8100-9 BY P. LAU (AR-830967) DATED 10/22/2021.

ATA 5730

INSPECTION TYPE:3CR/H WING FIXED LE SKIN UPPER SURFACE FOUND MULTIPLE CHAFE DAMAGED BETWEEN STA XOS 832 TO STA XOS 889.REPAIRED CHAFE SKIN ON R/H FIXED L/E BETWEEN STA XOS 832 TO STA XOS 889 IAW VT-SAA EA 011-5730-01-A9394 REV I/R AND UPS EO MD11-5730-81868-A (MAJOR) REV FAA FORM 8100-9 BY S.KANG (AR-605677) DATED 10/19/2021.

ATA 5310

INSPECTION TYPE:3CCENTER UPPER AUX TANK STRINGER 42 HAS CRACKS BEWTEEN STA XCW=28.70 AND XCW=-57.REPAIRED CRACKED STRINGER 42 BEWTEEN STA XCW=28.70 AND XCW=-57 IAW DWG APB7471-1 AND MD-11 SRM 57-10-03 REPAIR 1 FIGURE201 REV 68. (MAJOR)

ATA 5320

INSPECTION TYPE:3CMAIN CABIN L/H CEILING AREA HAS A INTERCOSTAL WITH CORROSION BEWTEEN STA 1256-1239 AT LONGERON #1.REMOVED, FABRICATED, REPLACED CORRODED INTERCOSTAL IAW MD-11 SRM 51-35-01. (MINOR)

ATA 5330

INSPECTION TYPE:3CAFT RH FUSELAGE SKIN HAS CORROSION BETWEEN STA.2140.000-STA.2163.685 AND BETWEEN LONGERON 12R-13R.REPAIRED CORRODED RH AFT FUSELAGE SKIN BETWEEN STA.2140.000-STA.2163.685 AND BETWEEN LON 12R-13R IAW VT-SAA EA 011-5330-01-A9398 REV I/R AND UPS EO MD11-5330-81936-A (MAJOR)

ATA 5310

INSPECTION TYPE:3CMAIN CARGO DECK LH WALL HAS A PRODUCTION SPLICE WITH CORROSION AT LONGERON #11 BETWEEN STA Y=1321 AND Y=1341.REMOVE, FABRICATED AND REPLACED CORRORED PRODUCTION SPLICE IAW DWG AEA6700 AND MD11 SRM 51-33-01. (MINOR)

ATA 5330

INSPECTION TYPE:3CTAIL AFT BODY RH FUSELAGE SKIN HAS CORROSION BETWEEN STA 2138-STA 2163.685 AND BETWEEN LONGERON 33R-35R.REPAIRED CORRODED AFT FUSELAGE SKIN BETWEEN STA.2138-STA.2163.685 AND BETWEEN LON 33R-35R IAW VT-SAA EA 011-5330-01-A9385 REV I/R AND UPS EO MD11-5330-81825-A (MAJOR) REF.

ATA 5330

INSPECTION TYPE:3CMAIN CABIN CENTER FUSELAGE INTERNAL PRODUCTION DOUBLER HAS CORROSION BETWEEN STA 1219 - 1239 & BETWEEN LONGERONS 14L - 15L.REPAIRED CORRODED MAIN CABIN CENTER FUSELAGE INTERNAL PRODUCTION DOUBLER BETWEEN STA 1219 - 1239 & BETWEEN LONGERONS 14L - 15L IAW VT-SAA EA 011-5330-01-A9391 REV. IR AND UPS EO MD11-5330-81833-A. (MINOR)

ATA 5313

INSPECTION TYPE:3CMAIN CABIN LONGERON 13 R/H HAS CORROSION BETWEEN STA. 1219 TO 1239.REPAIRED CORRODED LONGERON 13 R/H BETWEEN STA 1209 TO 1239 IAW SRM 53-00-05 REPAIR 1 FIG. 201 & 202. (MAJOR)

ATA 5330

INSPECTION TYPE:3CMAIN CABIN INTERNAL PRODUCTION DOUBLER BETWEEN STA 1245 TO STA 1324 AND BETWEEN LONGERONS 11R TO 18R IS CORRODED IN 4 PLACES.REPAIRED CORRODED FUSELAGE INTERNAL PRODUCTION DOUBLER BETWEEN STA 1245 TO STA 1324 AND BETWEEN LONGERONS 11R TO 18R 4EA PLACES IAW VT-SAA EA 011-5330-01-A9388 REV. IR AND UPS EO MD11-5330-81858-A. (MAJOR)

ATA 5540

INSPECTION TYPE:3CUPPER RUDDER TEE ON L/E RIB AT ZFR 450.173 IS CORRODED.REMOVED AND REPLACED CORRODED UPPER RUDDER L/E RIB AT ZFR 450.173 IAW SRM 51-33-01 & 51-35-01. (MINOR)

ATA 5300

INSPECTION TYPE:3CR-3 DOOR PLUG TOP HORZ. BEAM IS CRACKED AT THE AFT END.REMOVED AND REPLACED BEAM IAW SRM 51-35-01 & 51-33-01. (MINOR)

ATA 5540

INSPECTION TYPE:3CUPPER FORWARD RUDDER L/E RIB HAS CORROSION AT STA ZFR=450.173.REMOVED AND REPLACED CORRODED RIB IAW MD11 SRM 51-35-01 PAGE 38 PARA.10 AND DWG. AMC7292 (MINOR).

ATA 5310

INSPECTION TYPE:3CCENTER WING BOX TANK UPPER FWD SKIN HAS CORROSION BETWEEN STA XCW=-73 AND XCW=-78.5 AND AT STRINGER 15.REMOVED,REPAIRED CORRODED SKIN SURFACE IAW VT-SAA EA 011-5730-01-A9377 I/R AND UPS EO MD11-5730-81783-A. (MINOR)

ATA 5730

INSPECTION TYPE:3CCENTER WING TANK UPPER SKIN BETWEEN XCW -103.84 TO XCW -118.2 AT STRINGERS 19 & 20 IS CORRODED.REPAIRED CORRODED CENTER WING TANK UPPER SKIN BETWEEN XCW -103.84 TO XCW -118.2 AT STRINGERS 19 & 20 IAW VT-SAA EA 011-5730-01-A9381 REV. IR AND UPS EO MD11-5730-81814-A. (MINOR)

ATA 5300

INSPECTION TYPE:3CL-3 DOOR PLUG TOP HORZ. BEAM IS CRACKED AT THE FWD. END.REMOVED AND REPLACED BEAM IAW SRM 51-35-01 & 51-33-01. (MINOR)

ATA 5320

INSPECTION TYPE:3CFWD CARGO L/H SLOPE PANEL SUPPORT ANGLE IS CRACKED AT STA 979.REMOVED,FABRICATED AND REPLACED ANGLE SUPPORT IAW MD-11 SRM 51-35-01. (MINOR)

ATA 5320

INSPECTION TYPE:3CFWD CARGO COMPARTMENT LH SLOPE PANEL SUPPORT ANGLE CRACK AT STA.919.REMOVED,FABRICATED AND REPLACED CRACKED SUPPORT ANGLE IAW MD-11 SRM 51-31-01 (MINOR).

ATA 5340

INSPECTION TYPE:3CR/H UNDER WING CANTED PANEL UPPER CAP IS CRACKED AT STA 1236.8.REPAIRED CRACKED R/H UNDER WING CANTED PANEL UPPER CAP AT STA 1236.8 IAW UPS EO MD11-5340-81713-A REF. FAA FORM 8110-3 SIGNED BY A. GALLAGHER (DERY-833013-CE) DATED 10/15/2021. (MAJOR)

ATA 5320

INSPECTION TYPE:3CFWD CARGO L/H SLOPE PANEL SUPPORT ANGLE IS CRACKED AT STA 959.REMOVED,FABRICATED AND REPLACED CRACKED ANGLE IAW MD-11 SRM 51-31-01. (MINOR)

ATA 5310

INSPECTION TYPE:3CL/H UNDER WING BARREL CANTED CAP FOUND CRACK ON THE VERTICAL FLANGE AT STA 1278.800 STRINGER 38 TRACE AND APPROX Z=-100.REPAIRED CRACKED CANTED CAP AT STA 1278.800 STRINGER 38 TRACE AND APPROX Z=-100. IAW VT-SAA EA 011-5310-01-A9375 REV I/R AND UPS EO MD11-5310-81934-A. (MAJOR) REV FAA FORM 8100-9 BY J.TOM (AR-605565) DATED 10/18/2021.

ATA 2500

INSPECTION TYPE:3CFORWARD CARGO COMPARTMENT ROLLER TRAY ASSY. BROKEN AT STA.X=0 AND STA.Y=810.25.REPAIRED BROKEN TRAY ASSY. IAW VT-SAA EA 011-5340-01-A9403 REV I/R AND UPS EO MD11-5320-81941-A (MINOR).

ATA 5315

INSPECTION TYPE:3C AFT CARGO HAS A FLOOR SUPPORT ANGLE FOUND WITH CORROSION AT STA Y=1841 BETWEEN X=-20 AND X=-57. REPAIRED CORRORED FLOOR SUPPORT ANGLE AT STA Y=1841 BETWEEN X-20 AND X=-57 IAW EA 011-5310-01-A9383 REV I/R AND UPS EO MD11-5310-81009-A (MAJOR) REF FAA FORM 8100-9 BY S.KANG (AR-605677) DATED 10/14/2021.

ATA 5710

INSPECTION TYPE:3C R/H WING T/E LOWER CAP AT STA BETWEEN XW=320 AND XW=372 HAS CORROSION.REPAIRED CORRORED R/H WING LOWER CAP AT STA XW=320 AND XW=372 IAW MD11 SRM 57-50-02, REPAIR 9,FIGURE 201,REV 68 (MAJOR)

ATA 5754

INSPECTION TYPE:3CLT WING O/B L/E SKIN GOUGE BETWEEN STA.XOS 1113 AND XOS 1132.5REPAIRED GOUGED LT WING L/E SKIN IAW VT-SAA EA 011-5730-01-A9396 REV I/R AND UPS EO MD11-5750-81869-A (MINOR).

ATA 5730

INSPECTION TYPE:3CRT WING REAR SPAR UPPER CAP HAS CORROSION BETWEEN STA. XORS=782 AND XORS=826.5.REPAIRED CORRODED RT WING UPPER CAP IAW VT-SAA EA 011-5700-01-A9378 REV I/R AND UPS EO MD11-5710-81838-A (MINOR).

ATA 5730

INSPECTION TYPE:3CLT WING REAR SPAR UPPER CAP HAS CORROSION BETWEEN STA. XORS=784-826.REPAIRED CORRODED LT WING UPPER CAP IAW VT-SAA EA 011-5710-01-A9384 REV I/R AND UPS EO MD11-5710-81777-A (MINOR).

ATA 5730

INSPECTION TYPE:3CLT WING FIXED L/E SKIN IS CRACKED AT XOS 611.REPAIRED CRACKED LT WING FIXED L/E SKIN AT XOS 611 IAW SRM 57-40-01, REPAIR 18, FIGURE 201. (MAJOR)

ATA 5730

INSPECTION TYPE:3CR/H WING UPPER SURFACE SKIN HAS CORROSION BETWEEN STA XORS 853 AND XORS 856 AND AT STRINGER 7.REMOVED,REPAIRED CORRODED SKIN SURFACE IAW VT-SAA EA 011-5700-01-A9380 I/R AND UPS EO MD11-5730-81779-A. (MINOR)

ATA 5740

INSPECTION TYPE:3CR/H WING FIXED L/E UPPER EXTERNAL REPAIR DOUBLER IS GOUGED AT STA. XIS= 247.028.REMOVED, FABRICATED AND REPLACED R/H WING FIXED L/E UPPER EXTERNAL REPAIR DOUBLER AT STA. XIS= 247.028 IAW SRM 57-40-02 REPAIR 8 FIG. 201. (MAJOR)

ATA 5754

INSPECTION TYPE:3CLT WING L/E SKIN CRACK AT LOWER SURFACE AT CUT OUT FOR SLAT TRACK #14 STA.XOS=891.REPAIRED CRACKED LT WING L/E SKIN LOWER SURFACE AT CUT OUT FOR SLAT TRACK #14 STA.XOS=891 IAW MD-11 SRM 57-40-02 REPAIR 7,FIG 201,REV 68 (MAJOR).

ATA 5730

INSPECTION TYPE:3CRT UPPER WING SURFACE SKIN HAS CORROSION BETWEEN STA. XORS 575 AND XORS 619.REPAIRED CORRODED RT WING UPPER SURFACE SKIN BETWEEN STA. XORS 575 AND XORS 619 IAW VT-SAA EA 011-5710-01-A9374 REV I/R AND UPS EO MD11-5730-81772-A (MINOR).

ATA 5711

INSPECTION TYPE:3CLT WING T/E LOWER FALSE SPAR CAP HAS CORROSION AROUND 2 FASTENER HOLES AT I/B FWD CORNER OF PANEL 541JB.REPAIRED CORRODED LT WING T/E FALSE SPAR LOWER CAP AT XW 332 IAW SRM 57-50-02, REPAIR 9, FIGURE 202. (MAJOR)

ATA 5340

INSPECTION TYPE:3CL/H NLG TRUNNION FITTING IS CRACKED PAST STOP DRILL.REPAIRED CRACKED L/H NLG TRUNNION FITTING AT Y= 582.5, Z= -114 & X= 24 IAW SRM 53-10-14, REPAIR 2, FIGURE 202. (MAJOR)

ATA 5340

INSPECTION TYPE:3CR/H NLG TRUNNION FITTING IS CRACKED PAST STOP DRILL.REPAIRED CRACKED R/H NLG TRUNNION FITTING AT Y= 582.5, Z= -114 & X= -24 IAW SRM 53-10-14, REPAIR 2, FIGURE 202. (MAJOR)

ATA 5210

INSPECTION TYPE:N/AARLEE OPENING L-1 DOOR MORE LOOSE DOOR CABLE EXPOSEDC/W DMP 52-10-2-2-1 REMOVED CABLE OK FOR SERVICE

ATA 5210

WHILE CLOSING THE L-1 ENTRY DOOR CABLE BROKE IN DOOR MEDHANISM. DEFERREED L1 DOOR PER 52-10-2-21. DMP 52-10-2-21 PLACARD INSTALLED. DI LOG UPDATEDINST SERVICEABLE CABLE ASSY ON L1 PASSENGER DOOR & PERFORM ADJ,OPS CK GOOD. REVERSING DMP 52-10-2-2-1 IN REF AMM 52-11-03-400-801 & AMM52-11-02-830-801. REMOVED PLACARD.

ATA 3350

INSPECTION TYPE:NAOPERATIONAL TEST EMERGENCY LIGHT BATTERY PACK FAILSR&R'D EMERGENCY LIGHTING POWER SUPPLY IAW AMM 33-51-01 PAGEBLOCK 401 IPC REF 33-51-10-01

ATA 2430

INSPECTION TYPE:N/A1.6 HOURS AFTER TAKEOFF LEVEL 1 "BUS DC3 OFF" WITH NUMEROUS CONSEQUENTIAL ALERTS (SEL LSAS RIB OFF), CAWS FAULT, AP2 DISCONNECT DUE TO F/O'S FD FAIL LEVEL 2 FCC 2A DATA FAULT, YAW DMP UPR B OFF, AUTOPILOT SINGLE, SINGLE LAND, AVNCS FAN OVRDT/S LVEL 1 "BUS DC3 OFF" MESSAGE PER MD11 FRM 24-30-01, REPLACED DC3 SENSING RELAY R2-5153. NO FAULTS NOTED AT THIS TIME, ALL OTHER FAULTS LISTED ARE NOT PRESENT ESR AIPC 24-61-01-01 ITEM 10

ATA 3350

INSPECTION TYPE:NAEMER LIGHT INOP.R&R EMER LIGHT BATTERY PACK PER MD11 AMM 33-51-01-401, SYSTEM CHECKS OKAY. IPC 33-51-01-05-015.

ATA 5330

INSPECTION TYPE:N/AFUSELAGE CRACKED NEAR #3 PACK DOOR AT UPPER AFT CORNERREPAIRED IAW UPS EO MD11-5330-79787-A

ATA 2560

INSPECTION TYPE: NA SDR FILED OPEN R1 PNEUMATIC PRESSURE BOTTLE IS AT 0 PSI. R1 PNEUMATIC DOOR MEL 52-10-3-1-2-1-1 DEFERRED. PLACARD INSTALLED.

ATA 3350

EMERG BATT 1 FAULTR & R EMERG BATTERY POWER SUPPLY PER MM33-51-01-400-802 OPS CHECKS GOOD

ATA 5210

FORWARD CABLE TO OPEN CREW ENTRY DOOR, LEFT SIDE IS OFF TRACK. REPLACED THE TENSIONER IAW MM 52-11-03. ADJUSTED AND TESTED IAW 52-11-02.

ATA 3260

INSPECTION TYPE:N/AATB - AFTER T/O GEAR RETRACTED GOT RED (RIGHT MAIN) GEAR NOT UP INDICATION ON GEAR HANDLE AND CONFIGURATION PG. RAN QRH CHECK LIST 6-56 "GEAR PRIMARY OR SECONDARY LTS ILLUMINATE WITH GEAR HANDLE UP" ATB REQUIREDR&R RH MAIN GEAR UP AND LATCHED PROXIMITY SENSOR PER AMM 32-61-15 RTS TEST GOOD IAW AMM 32-61-15-741-802 PERFORMED FULL LANDING GEAR SWING TO CONFIRM NO FAULTS EXISTED PER AMM 32-31-00-700-803 NO FAULTS NOTED DURING GEAR SWING A/C IS OK FOR CONTINUED SERVICE

ATA 5313

INSPECTION TYPE:2CLONGERON 4R SPLICE FITTING AT STA. 1129 IS CRACKED.REMOVED AND REPLACED CRACKED LONGERON 4R SPLICE FITTING AT STA. 1129 IAW MD-11 SRM 51-33-01. (MINOR)

ATA 5713

INSPECTION TYPE:2CLT WING FIXED L/E STRINGER IS CRACKED AT STA. XOS 667.REPAIRED CRACKED LT WING FIXED L/E STRINGER AT STA. XOS 667 IAW MD-11 SRM 57-40-03, REPAIR 2, FIGURE 202. (MAJOR)

ATA 5753

INSPECTION TYPE:2CL/H I/B FLAP O/B HINGE FITTING IS GOUGED AT STA. XIFH=261.REPAIRED GOUGED L/H I/B FLAP O/B HINGR FITTING AT STA. XIFH=261. IAW VT-SAA EA 011-5750-01-A7937 REV. I/R AND UPS EO MD11-5740-74451-A.

ATA 5313

INSPECTION TYPE:2CEXTERIOR FUSELAGE SKIN WAS TRIMMED OUT BETWEEN STA. 1641-1681 AND LONGERON'S 29R-30R TO ACCESS REPAIRS ON LONGERON'S 29R-30R.REPAIRED EXTERIOR FUSELAGE SKIN BETWEEN STA. 1641-1681 AND LONGERON'S 29R-30R IAW VT-SAA EA 011-5330-01-A7929 REV. I/R AND UPS EO MD11-5330-74414-A. (MAJOR)

ATA 5322

INSPECTION TYPE:2CUNDERWING BARREL (BLADDER AREA) FRAME TO BEAM SHEAR ANGLE IS CRACKED AT STA. Y=1278 R/H SIDE.REMOVED AND REPLACED ANGLE IAW SRM 51-33-01.(MINOR)

ATA 5320

INSPECTION TYPE:2CFWD. CARGO INTERCOSTAL IS CRACKED BETWEEN STA. 6-30 TO 6-50 AND ABOVE LONG. 43 R/H.REMOVED, FABRICATED AND REPLACED INTERCOSTAL BETWEEN STA. 6-30 TO 6-50 AND ABOVE LONG. 43 R/H IAW DWG. ACA7049 AND SRM 51-33-01. (MINOR)

ATA 2810

INSPECTION TYPE:2CCENTER WING TANK STRINGER #45 IS CRACKED AT STA. XCW=17 & XCW=46.5REPAIRED CRACKED CENTER WING TANK STRINGER # 45 BETWEEN STA. XCW= 4.5 TO XCW= 57.25 IAW SRM 57-10-03 REPAIR 1 FIG. 201. (MAJOR)

ATA 5313

INSPECTION TYPE:2CCENTER FUSELAGE LONGERON 28L BETWEEN STA Y=1266 - 1297 HAS CORROSION.REPAIRED CORRODED CENTER FUSELAGE LONGERON 28L BETWEEN STA Y=1266 - 1297 IAW VT-SAA EA 011-5310-01-A7933 REV. IR AND UPS EO MD11-5310-74408-A. (MINOR)

ATA 5755

INSPECTION TYPE:2CR/H WING T/E SPOILER PANEL SILL HAS CORROSION BETWEEN STA. XOFH=453.931 AND XOSP=544.75.REPAIRED CORRODED R/H WING SPOILER PANEL SILL BETWEEN STA. XOFH=453.931 TO XOSP=544.75 IAW SRM 57-50-02 REPAIR 10 FIG. 201. (MAJOR)

ATA 5313

INSPECTION TYPE:2CLONGERON 28 R/H SIDE IS CORRODED BETWEEN STA. 1288-1295.REPAIRED CORRODED LONGERON 28 R/H SIDE BETWEEN STA. 1288-1295 IAW VT-SAA EA 011-5310-01-A7935 REV. I/R AND UPS EO MD11-5310-74445-A. (MAJOR)

ATA 5313

INSPECTION TYPE:2CCENTER CARGO LONGERON 29R IS CRACKED BETWEEN STA. 1641-1651.REPAIRED CRACKED CENTER CARGO LONGERON 29R BETWEEN STA. 1641-1681 IAW SRM 53-00-05 REPAIR 1 FIG. 201 & 202. (MAJOR)

ATA 5710

INSPECTION TYPE:2CRT WING REFUEL ADAPTER FITTING IS GOUGED ON INSIDE.REPAIRED GOUGED RT WING REFUEL ADAPTER FITTING IAW VT-SAA EA 011-5720-01-A7931 REV. IR AND UPS EO MD11-5700-74425-A. (MINOR)

ATA 5730

INSPECTION TYPE:2CLT WING FIXED L/E BEADED DOUBLER CRACK REPAIR BETWEEN STA. XOS. 621 TO XOS. 636 REQUIRES PERMANENT REPAIR.ACCOMPLISHED PERMANENT REPAIR OF LT WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 621 - XOS. 636 IAW MD-11 SRM 57-40-02, REPAIR 15, FIGURE 205. (MAJOR)

ATA 5313

INSPECTION TYPE:2CCENTER CARGO LONGERON 30R SPLICE FITTING IS CRACKED BETWEEN STA. 1661-1681.REMOVED, FABRICATED AND REPLACED CENTER CARGO LONGERON 30R SPLICE FITTING IAW DWG. AFA7797 AND SRM 51-31-01. (MINOR)

ATA 5313

INSPECTION TYPE:2CCENTER CARGO LONGERON 29R SPLICE FITTING IS CRACKED BETWEEN STA. 1661-1681.REMOVED, FABRICATED AND REPLACED LONGERON 29R SPLICE FITTING BETWEEN STA. 1661-1681 IAW DWG. AFA7797 AND SRM 51-51-31-01. (MINOR)

ATA 5320

INSPECTION TYPE:2CAFT CARGO FLOORBOARD LANDING HAS CORROSION AT STA. 1887 L/H SIDE.REMOVED, FABRICATED AND REPLACED LANDING IAW DWG. AGA3857 AND SRM 51-35-01. (MINOR)

ATA 5320

INSPECTION TYPE:2CCENTER CARGO L/H SIDE FLOOR SUPPORT ANGLE IS CRACKED AT STA. 1781.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG.AFA7295 AND SRM 51-33-01. (MINOR)

ATA 5753

INSPECTION TYPE:2CLT WING I/B FLAP VANE L/E I/B END PREVIOUS REPAIR IS DAMAGED.REPAIRED DAMAGED LT WING I/B FLAP VANE L/E I/B END IAW MD-11 SRM 57-50-80, REPAIR 2, PAR. 2.A.(2).(A)(5), FIGURE 201. (MAJOR)

ATA 5310

INSPECTION TYPE:2CFWD. CARGO TRANVERSE BEAM IS CRACKED AT STA. 6-73 ABOVE LONG. 43 R/H.REMOVED, FABRICATED AND REPLACED TRANVERSE BEAM AT STA. 6-73 AND LONG. 43 R/H IAW DWG. ADA7667 AND SRM 51-35-01. (MINOR)

ATA 5320

INSPECTION TYPE:2CAFT CARGO FLOOR SUPPORT ANGLE IS CORRODED BETWEEN STA. 1902-16-967 R/H SIDE.REMOVED, FABRICATED AND REPLKACED SUPPORT ANGLE IAW DWG. AGA3857 AND SRM 51-35-01. (MINOR)

ATA 5340

INSPECTION TYPE:2CMAIN CABIN LONGERON 15L TEE ANGLE IS CRACKED AT STA. 1339.REMOVED AND REPLACED CRACKED MAIN CABIN LONGERON 15L TEE ANGLE IAW MD-11 SRM 51-35-01. (MINOR)

ATA 5340

INSPECTION TYPE:2CMAIN CABIN LONGERON 15R TEE ANGLE IS CRACKED AT STA. 1339.REMOVED AND REPLACED CRACKED MAIN CABIN LONGERON 15R TEE ANGLE AT STA. 1339 IAW MD-11 SRM 51-35-01. (MINOR)

ATA 5710

INSPECTION TYPE:2CR/H WING T/E AT PANEL # 641FB, THE PANEL LANDING IS CORRODED.REMOVED, FABRICATED AND REPLACED LANGING/TEE IAW DWG. ARC0307 AND SRM 51-33-01. (MINOR)

ATA 5320

INSPECTION TYPE:2CAFT CARGO R/H SIDE VERTICAL STIFFNER IS CRACKED AT STA. 1841.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. AGA7170 AND SRM 51-33-01. (MINOR)

ATA 5730

INSPECTION TYPE:2CRT WING FIXED L/E SKIN UPPER SURFACE O/B OF #8 SLAT IS GOUGED.REPAIRED GOUGED RT WING FIXED L/E SKIN UPPER SURFACE O/B OF #8 SLAT IAW MD-11 SRM 57-40-01, REPAIR 16, FIGURE 201. (MAJOR)

ATA 5730

INSPECTION TYPE:2CLT WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN XOS. 667.6 - XOS. 673.6.REPAIRED CRACKED LT WING FIXED L/E BEADED DOUBLER BETWEEN XOS. 667.6 - XOS. 673.6 IAW MD-11 SRM 57-40-02, REPAIR 15, FIGURE 205. (MAJOR)

ATA 5730

INSPECTION TYPE:2CR/H WING L/E LOWER SKIN IS CRACKED AT STA. XOS= 487.REPAIRED CRACKED R/H WING L/E LOWER SKIN BETWEEN STA. XOS=487.351 TO 490.850 IAW VT-SAA EA 011-5740-01-A7926 REV. I/R AD UPS EO MD11-5740-74435-A. (MAJOR)

ATA 5755

INSPECTION TYPE:2CL/H WING SPOILER PANEL SILL IS CORRODED BETWEEN STA. XOFH=453.931 TO XOSP=499.36.REPAIRED L/H WING SPOILER PANEL SILL BETWEEN STA. XOFH=453.931 TO XOSP=499.36 IAW SRM 57-50-02 REPAIR 10 FIG. 201. (MAJOR)

ATA 5530

INSPECTION TYPE:2CLOWER VERTICAL STABILIZER REAR CENTER SPAR TO REAR SPAR R/H INTERCOSTAL AFT END IS CRACKED BETWEEN STA. YID=375, XID=-7.1 AND ZID=65.REPAIRED CRACKED LOWER VERTICAL STABILIZER REAR CENTER SPAR TO REAR SPAR R/H INTERCOSTAL AFT END BETWEEN STA. YID=375, XID=-7.1 AND ZID=65 IAW VT-SAA EA 011-5530-01-A7925 REV. IR AND UPS EO MD11-5530-74444-A. (MAJOR)

ATA 5730

INSPECTION TYPE:2CL/H WING FIXED L/E SPLICE DOUBLER IS CRACKED AT STA. XOS.=799.REMOVED, FABRICATED AND REPLACED SPLICE DOUBLER ON L/H WING AT STA. XOS.=799 IAW DWG. ARB3954 AND SRM 51-33-01. (MINOR)

ATA 5730

INSPECTION TYPE:2CL/H WING L/E UPPER SKIN IS CRACKED AT STA. XOS.=464 TO 470.REPAIRED CRACKED L/H WING L/E UPPER SKIN BETWEEN STA XOS.=464-470 IAW SRM 57-40-01 REPAIR 10 FIG. 201. (MAJOR)

ATA 5730

INSPECTION TYPE:2CLT WING FIXED L/E O/B BULLNOSE (SKIN) UPPER SURFACE O/B OF #8 SLAT IS CHAFED.REPAIRED CHAFED LT WING FIXED L/E BULLNOSE (SKIN) UPPER SURFACE O/B OF #8 SLAT IAW MD-11 SRM 57-40-01, REPAIR 16, FIGURE 201. (MAJOR)

ATA 5740

INSPECTION TYPE:2CL/H WING L/E LOWER SKIN IS CRACKED AT STA. XOS.=717.REPAIRED CRACKED L/H WING L/E SKIN AT STA. XOS.=717 IAW SRM 57-40-02 REPAIR 7 FIG. 201. (MAJOR)

ATA 5730

INSPECTION TYPE:2CR/H WING L/E SKIN REPAIR DOUBLER IS DAMAGED AT STA. XOS.=734.7 TO 763.6.REMOVED AND REPLACED DOUBLER ON R/H WING L/E SKIN IAW SRM 57-40-02 REPAIR 5 FIG. 201.

ATA 5730

INSPECTION TYPE:2CRT WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN XOS. 661.71 - XOS. 667.67.REPAIRED CRACKED RT WING FIXED L/E BEADED DOUBLER BETWEEN XOS. 661.71 - XOS. 667.67 IAW MD-11 SRM 57-40-02, REPAIR 15, FIGURE 205. (MAJOR)

ATA 5320

INSPECTION TYPE:2CAFT ACCESSORY COMPARTMENT 316 UPPER R/H SUPPORT ANGLE FOR SURGE DUCT IS CRACKED.REMOVED AND REPLACED CRACKED AFT ACCESSORY COMPARTMENT 316 UPPER R/H SUPPORT ANGLE FOR SURGE DUCT IAW MD-11 SRM 51-33-01 AND 51-35-01. (MINOR)

ATA 5712

INSPECTION TYPE:2CRT WING O/B FIXED L/E RIB O/B OF #19 SLAT TRACK IS CRACKED.REMOVED AND REPLACED CRACKED RT WING O/B FIXED L/E RIB O/B OF #19 SLAT TRACK IAW MD-11 SRM 51-33-01. (MINOR)

ATA 5320

INSPECTION TYPE:2CCENTER ACCESSORY COMPARTMENT CEILING R/H O/B INTERCOSTAL FWD LOWER FLANGE IS CRACKED.REMOVED AND REPLACED CRACKED CENTER ACCESSORY COMPARTMENT CEILING R/H O/B INTERCOSTAL IAW MD-11 SRM 51-33-01 AND 51-35-01. (MINOR)

ATA 5330

INSPECTION TYPE:2CCENTER WING BOX UPPER SKIN HAS CORROSION AT F/S 1152, RBL=108 AND STRINGER 15.REPAIRED CORRODED CENTER WING BOX UPPER SKIN AT F/S 1152, RBL=108 AND STRINGER 15 IAW VT-SAA EA 011-5730-01-A7927 REV. IR AND UPS EO MD11-5730-74362-A. (MINOR)

ATA 5414

INSPECTION TYPE:2C#1 PYLON O/B SIDE SKIN ABOVE EXHAUST VENT IS CRACKED.REPAIRED #1 PYLON O/B SIDE SKIN IAW SRM 54-00-00 REPAIR GENERAL FIG. 204. (MINOR)

ATA 7830

INSPECTION TYPE:2C#1 ENG. I/B THRUST REVERSER BEAVER TAIL FAIRING HAS INCOMING OVERSIZE FASTENER HOLES EXCEEDING SRM LOIMITS.REPAIRED #1 ENG. I/B T/R BEAVER TAIL FAIRING IAW VT-SAA EA 011-7830-01-A7928 REV. I/R AND UPS EO MD11-7830-74334-A. (MINOR)

ATA 5730

INSPECTION TYPE:2CRT WING FIXED L/E BEADED DOUBLER IS CRACKED AT XOS. 610 - XOS. 616.REPAIRED CRACKED RT WING FIXED L/E BEADED DOUBLER BETWEEN XOS. 610 - XOS. 616 IAW MD-11 SRM 57-40-02, REPAIR 15, FIGURE 205. (MAJOR)

ATA 3350

INSPECTION TYPE:N/A EMER LT BAT 1 LO DURING PREFLIGHT WHEN TESTING EMERG LIGHTS. DEFERRED EMERGENCY LIGHTING SYSTEM PER MEL 33-50-4. COMPLETED DMP 33-50-4. PLACED PLACARD **SUPPLEMENTAL SDR** R/R BATTERY PACK P/N 60-4411-5. THIS CLEARS M677532.

ATA 5230

INSPECTION TYPE:N/A AFT BULK CARGO DOOR LWR CORNER DMG'ED AFT OF EXISTING PREVIOUS REPAIR. REPAIRED PER EO MD11-5230-71174-B.

ATA 5210

INSPECTION TYPE:N/A R1 DOOR ELECTRIC OPERATION INTERMITTENT FROM EITHER SWITCH. DEFERRED R1 DOOR ELECTRIC OPERATION INOP PER MEL 52-10-1-2-0-1 ON M668612. DMP C/W. **SUPPLEMENTAL SDR** REPLACED UP LIMIT SWITCH PER SWPM 20-30-00 ( 51-592) AND REPLACED ELECTRIC DOOR ACTUATOR M1-71 PER MM 52-11-01-401. DOOR OPS CKS GOOD PER MM 52-11-02-830-805 M668612. CLEARED ESR: IPC 52-11-70-01-080 AND 52-11-05-05-525.

ATA 5210

INSPECTION TYPE:NAL1 DOOR INTERMITTENT ON OPENINGREPLACED THE L1 SOLENOID AND R2-177 REF SWPM 20-40-01 AMM 52-10-06-40 OPS NORMAL. ESR: 52-11-70-01-070J

ATA 5240

R-1 DOOR DIFFICULT TO OPEN. OK TO CONTINUE PER MEL 52-10-3-1-2-1. R&R RELAY R2-176 IAW SWPM 20-20-03. DOOR OPS CHECK NORMAL.

ATA 5313

INSPECTION TYPE:2CCENTER CARGO LONGERON 30R IS CRACKED BETWEEN STA. 1641-1651.REPAIRED CRACKED CENTER CARGO LONGERON 30R BETWEEN STA. 1641-1681 IAW SRM 53-00-05 REPAIR 1 FIG. 201 & 202. (MAJOR)

ATA 3350

LEFT ENTRY DOOR EXIT SIGN BROKEN. R&R EXIT SIGN ASSY REF 33-27-01. OPS CHECK GOOD 33-27-01-05.

ATA 5210

L1 DOOR WILL NOT OPEN ELECTRICALLY BEYOND MID POSITION. REPLACED CONTACTOR R25-177 IAW SWPM 20-20-03 & WDM 52-11-01. L1 DOOR OPERATED NORMALLY IAW MM 52-11-02-2.

ATA 3350

FLIGHT CREW REPORTED EMERGENCY LIGHT COVER ON R1 DOOR FELL OFF. REINSTALLED R1 EMERGENCY LIGHT COVER W/R/T MD11-AM-M-33-27-05.

ATA 3244

AFTER FLYING FOR 2 HOURS, THE NOSE GEAR TIRE PRESSURE LOW MESSAGE ILLUMINATED. THE TIRE PRESSURES WERE LOW ON THE NOSE GEAR LEFT TIRE . THE PRESSURES WERE 131 AND 21. OUTSIDE TAT WW -19 C, REMOVED & REPLACED LEFT & RIGHT NOSE TIRE ASSEMBLY IAW AMM 32-42-01-000-801.

ATA 3244

DURING GEAR EXTENSION FOR LANDING, RECEIVED A LEVEL 2 ANTI -SKID R FAIL, EXECUTED A GO AROUND C/W QRH PROCEDURE. ON LANDING THE NR 7 TIRE FAILED. R & R THE ANTI-SKID CONTROL VALVE IAW AMM 32-45-21-401 REV 90.01. OPS TEST PERFORMED IAW AMM 32-45-00-700-801. TEST PASSED.

ATA 2561

CPT SEAT LIFE JACKET WILL NOT STAY IN HOLDER. SEC'D CAPT'S SEAT LIFE VEST HOLDER. OPS CHK NML.

ATA 3350

EXIT SIGN OVER THE L1 DOOR FELL OFF DURING LANDING. INSTALLED THE SIGN.

ATA 5312

INSPECTION TYPE: 1C, BS 2164 BULKHEAD LOWER HORIZONTAL STIFFNER IS CRACKED ON BOTH ENDS. REMOVED, FABRICATED, AND REPLACED THE STIFFNER IAW DWG AJC7001, AND SRM 51-31-01.

ATA 5410

INSPECTION TYPE: 1C, NR 3 PYLON ACCESS PANEL 488KL HAS A DAMAGED INTERNAL RIB. REMOVED AND REPLACED THE ACCESS PANEL RIB IAW SRM 54-01-42.

ATA 5320

INSPECTION TYPE: 1C, LT NOSE WW DOOR FRAME REINFORCEMENT HAS CORROSION AT BS 541, LBL 28, Z -110. REMOVED, FABRICATED, AND REPLACED THE REINFORCEMENT IAW DWG NCA6050-33, AND SRM 51-33-01.

ATA 5730

INSPECTION TYPE: 1C, LT WING L/E SKIN IS CHAFED BETWEEN XOS 1114.453 TO 1138.317. REPAIREDTHE LT WING L/E SKIN IAW EA 011-5730-01-A7016, REV I/R, AND EO MD11-5730-65908-A.

ATA 5311

INSPECTION TYPE: 1C, LT AC BAY FRAME BS 541 HAS CORROSION LBL 30, Z-110. REMOVED, FABRICATED, AND REPLACED THE FRAME IAW DWG ACA3348-3, AND SRM 51-35-01.

ATA 5754

INSPECTION TYPE: 1C, LT WING L/E NR 2 SLAT OTBD END HAS A CRACKED ANGLE. REMOVED, FABRICATED, AND REPLACED THE ANGLE IAW DWG ARB1647, AND SRM 51-35-01.

ATA 5753

INSPECTION TYPE: 3C, RT INBD FLAP DELAMINATED AT AT OTBD TRAILING EDGE. REPAIRED IAW SRM 57-50-02, REPAIR 2.

ATA 5711

INSPECTION TYPE: 1C, LEFT WING REAR SPAR UPPER CAP HAS CORROSION AT XORS. 897 TO 1042.3. REPAIRED THE SPAR UPPER CAP IAW EA 011-5710-01-A7015, REV I/R, AND EO MD11-5710-65911-A.

ATA 5710

INSPECTION TYPE: 1C, RIGHT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED AT XOS 786. REPAIRED THE DOUBLER IAW SRM 57-40-02, REPAIR 15, FIGURE 205. MAJOR.

ATA 5720

INSPECTION TYPE: 1C, RT WING INTERNAL L/E AT PANEL 616DB HAS A CRACKED STIFFNER. REMOVED, FABRICATED, AND REPLACED THE STIFFENER IAW DWG ARB0116, AND SRM 51-33-01.

ATA 3210

INSPECTION TYPE: 1C, RT MLG AFT BRAKE HYDRAULIC HOSE SUPPORT BRACKET ASSY HAS A CHAFE. REPAIRED SUPPORT BRACKET IAW EA 011-3210-01-A7003, REV I/R, AND EO MD11-3210-65809-A.

ATA 5320

INSPECTION TYPE: 1C, RT OVERWING UPPER FUEL TANK WEB IS CRACKED AT BS 1372, RBL 80 & Z-54. REPAIRED IAW EO MD11-5710-65670-A. MAJOR.

ATA 2565

INSPECTION TYPE:N/A RT DOOR SLIDE BLOWN. DEFERRED RT DOOR SLIDE REMOVED IAW MEL 52-10-3-1-2-1 PLACARD INSTALLED. **SUPPLEMENTAL SDR ** INSTALLED SLIDE RAFT INTO CONTAINER BOX IAW AMM 25-61-15-400-801; INSTALLED SLIDE AFT ASSY INTO R1 DOOR PER AMM 25-61-15-400-801; THIS CLEARS M607964

ATA 3350

EMERGENCY LIGHT BATTERY LOW MESSAGE. R & R THE BATTERY PACK IAW MM 33-51-01.

ATA 3350

L1 ENTRY DOOR EXIT LIGHT INOPERATIVE. REPAIRED CEILING PANEL EMERGENCY EXIT SIGN HOUSING.

ATA 3350

EXIT SIGN ABOVE L1 DOOR WILL NOT STAY SECURED. REPLACED THE COVER IAW 33-27-01-05, ITEM 130.

ATA 2611

CABIN SMOKE ALERT DURING CLIMB THROUGH 7000 FT. ALERT WAS MOMENTARY AND RETURNED AGAIN MOMENTARILY TROUBLESHOT IAW FIM 26-15-00-101 FIG 108. R & R IAW MM 31-42-01-741. OK TO CONTINUE.

ATA 3350

EMERGENCY LIGHT BATTERY 1 LOW MESSAGE DURING PREFLIGHT. R & R BATTERY EMERGENCY POWER SUPPLY. OPS TEST GOOD IAW AMM 33-51-01/401.

ATA 3350

DURING PDC CHECK, FOUND EMERGENCY LIGHT BATTERY VOLTAGE LOW. R & R THE POWER SUPPLY AND TESTED NORMAL IAW AMM 33-51-01/401,501.

ATA 5313

INSPECTION TYPE: 3C, LONGERON 11R CORRODED AT STA 1219. REPAIRED THE LONGERON BETWEEN BS 1209 - 1229 IAW EA 011-5310-01-A6102, REV IR AND EO MD11-5310-60129-A.

ATA 5313

INSPECTION TYPE:3C, MAIN CABIN AT BS 1401 TO 1421, LONGERON 16L HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT LONGERON SEGMENT BS 1401 TO 1421, L16L, REF SRM'S 51-31-01 AND 51-33-01.

ATA 5330

INSPECTION TYPE:C3, LT FUSELAGE FAIRING ATTACHMENT FASTENER HOLES AND ATTACH RIBS CORRODED AT BS 1941 TO 2033. ACCOMPLISHED BLEND REPAIR IAW SRM 51-21-01 AND 53-00-00.

ATA 5340

INSPECTION TYPE:C3, FWD ELECTRONIC EQUIPMENT BAY FLOORBEAM, BS 401 FWD SIDE RBL 14 ATTACH ANGLE CRACKED. R & R ATTACH ANGLE IAW SRM 51-33-01 AND 51-35-01.

ATA 5730

INSPECTION TYPE:3C, RT WING FIXED L/E COMP SPLICE STRAP CRACKED AT APPROXIMATELY XOS BS 789. R & R SPLICE STRAP IAW SRM 51-33-01.

ATA 5510

INSPECTION TYPE:C3, AREAS OF LIGHT SURFACE CORROSION ON FITTINGS INSIDE RT HORIZONTAL STABILIZER PANEL 344CB. REPAIRED IAW SRM 51-21-01, 55-00-00, PG 206 AND 51-31-01.

ATA 5520

INSPECTION TYPE:3C, RT DETACHABLE ELEVATOR INBD END MOUNT FLANGE CRACKED AT BS XE 53.5. REPAIRED CRACK TO RIB ALC8985-2 IAW EA 011-5520-01-A6130, REV IR AND EO MD11-5520-60072-A.

ATA 5320

INSPECTION TYPE:3C, AFT CARGO DOOR LOWR AFT JAMB SUPPORT STRUCTURE HAS CORROSION AROUND FASTENER HOLE. REPAIRED IAW SRM 53-00-00, FIG 202.

ATA 5320

INSPECTION TYPE:3C, SURFACE CORROSION ON FWD CARGO FLOORBOARD LANDING BS 6-70 LT SIDE. ACCOMPLISHED BLEND REPAIR IAW SRM 53-00-00, FIG 205.

ATA 5313

INSPECTION TYPE:3C, LONGERON 48L CORRODED AT BS 1019. REPAIRED L48L BETWEEN BS 999 - 1059 IAW SRM 53-00-05, REPAIR 1, FIG 201.

ATA 5553

INSPECTION TYPE: 3C, SURFACE CORROSION ON THE LOWER VERTICAL STAB UPPER MOUNTING FRAME FOR PANEL NR 361AL. REMOVED CORROSION IAW SRM 51-21-01. ORIGINAL MATERIAL THICKNESS .063 IAW DWG AJC7328, FOUND WITHIN LIMITS IAW SRM 55-00-00, PAGE 206. TREATED AND PRIMED AREA IAW SRM 51-21-01.

ATA 5313

INSPECTION TYPE:3C, LONGERON FITTING 18R CORRODED BETWEEN BS 1155-1175. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON FITTING IAW DWG AEA7530. SRM 51-33-01, 51-21-01.

ATA 5320

INSPECTION TYPE:3C, AREA OF LIGHT SURFACE CORROSION ON FLOOR PANEL SUPPORT IN MAIN CARGO AT BS 1361, RBL 114. ACCOMPLISHED BLEND REPAIR ON FLOOR PANEL SUPPORT IN MAIN CARGO BS 1361, RBL 114 IAW SRM 51-21-01 AND SRM 53-00-00.

ATA 5320

INSPECTION TYPE: 3C, WHILE INSPECTING CORROSION REMOVAL, FOUND VERTICAL STIFFENER BEAM WITH HEAVY CORROSION AT BS 6-70, ABOVE L43L. INSTALLED PERMANENT REPAIR BY REPLACEMENT OF STANCHION BS 6-70 X=57.00 IAW EA 011-5310-01-A6128, REV I/R AND EO MD11-5320-60055-A.

ATA 5420

INSPECTION TYPE:3C, NR 2 ENGINE RT FAN COWL DOOR JAMB AT BS 2166, X=14.25 HAS HAT CHANNEL CRACKED. ACCOMPLISHED PERMANENT CRACK REPAIR ON NR 2 ENGINE RT FAN COWL DOOR JAMB HAT CHANNEL BS 2166, X=14.25 IAW EA 011-5400-01-A6124, REV I/R AND EO MD11-5420-60048-A.

ATA 5310

INSPECTION TYPE:3C, AFT CARGO DOOR FWD JAMB SILL SUPPORT STRUCTURE CORRODED. REMOVED CORROSION IAW SRM 51-33-01, 51-21-01, AND 53-00-00, FIG 202.

ATA 5320

INSPECTION TYPE:3C, FRAME TO FLOORBEAM FITTING CORRODED STA 1129/6-70, LEFT SIDE REPAIRED CORRODED FLOORBEAM BETWEEN LBL29-46 IAW EA 011-5310-01-A6110, REV IR AND EO MD11-5310-60023-A.

ATA 5313

INSPECTION TYPE:3C, LONGERON 44L CORRODED AT BS 1129/6-100. REPAIRED L44L BETWEEN BS 1129/6-50 AND 1129/6-100 IAW EA 011-5310-01-A6111, REV IR AND EO MD11-5310-60046-A.

ATA 5313

INSPECTION TYPE:3C, LONGERON 51R CORRODED AT BS 6-80. REPAIRED CORRODED LONGERON BETWEEN BS 6-50 AND 6-90 IAW SRM 53-00-05, REPAIR 1, FIG 201/202

ATA 5320

INSPECTION TYPE: 3C, FORWARD CARGO SUPPORT ANGLE HAS CORROSION AT BS 919, BL 0 REMOVED, FABRICATED AND INSTALLED NEW SUPPORT ANGLE IN FORWARD CARGO BS 919, BL 0 IAW SRM 53-35-01 AND DWG ADA3623.

ATA 5313

INSPECTION TYPE:3C, LONGERON 40R CORRODED BETWEEN BS 859-879. REMOVED CORROSION IAW SRM 53-00-00, FIG 202 AND SRM 51-21-01.

ATA 5347

INSPECTION TYPE:3C, FORWARD CARGO TRACK CRACKED AT BS 6-70 ABOVE L43R. R & R THE CARGO TRACK IAW SRM 51-33-01 AND 51-33-01.

ATA 5320

INSPECTION TYPE:3CR,CB FLOOR FITTING NR 10, RT OTBD CRACKED. R & R RCB FLOOR FITTING IAW 51-31-01.

ATA 5313

INSPECTION TYPE:3C, LONGERON TIE FITTING CRACKED IN FWD CARGO COMPT BS 6-10, L42L. REMOVED FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DWG ACA7049, SRM 51-31-01, AND 51-33-01.

ATA 5313

INSPECTION TYPE:3C, REPAIR ANGLE CRACKED ON L36L AT BS 840. REPAIRED L36L IAW EA 011-5310-01-A6136, REV IR AND EO MD11-5310-60177-A.

ATA 5313

INSPECTION TYPE: 3C, LONGERON 43L CORRODED NEAR BS 1129 - 6-100. REPAIRED L43L BETWEEN STA 1129/6-50 AND 1129/6-100 IAW SRM 53-00-05, REPAIR 1, FIG 201, 202.

ATA 5313

INSPECTION TYPE:3C, LONGERON 47R CORRODED BS 1122. REPAIRED L47R BETWEEN BS 1099 AND 1129/6.00 IAW SRM 53-00-05, REPAIR 1 FIG 201, 202.

ATA 5313

INSPECTION TYPE:3C, LONGERON 47L CORRODED AT BS 1129/6-100. REPAIRED L47L BETWEEN BS 1129/6-70 AND 1129/6-100 IAW SRM 53-00-05, REPAIR 1 FIG 201, 202.

ATA 5313

INSPECTION TYPE:3C, LONGERON 38L CORRODED BETWEEN BS 6-50 AND 6-70. REMOVED CORROSION IAW SRM 53-00-00, FIG 205 AND 51-21-01.

ATA 5310

INSPECTION TYPE:3C, AFT CARGO DOOR LOWER FWD JAMB TORQUE BOX WEB CORRODED. REMOVED CORROSION IAW SRM 53-00-00, FIG 202 AND 51-21-01.

ATA 5313

INSPECTION TYPE:3C, LONGERON 38L CORRODED BETWEEN BS 6-50 AND 6-70. REMOVED CORROSION IAW SRM 53-00-00, FIG 205 AND 51-21-01.

ATA 5313

INSPECTION TYPE:3C, LONGERON 37R SPLICE FITTING CRACKED BETWEEN BS 1119 AND 6-10 REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SPLICE FITTING IAW DWG ADA8424 AND SRM 51-33-01.

ATA 5313

INSPECTION TYPE:3C, LONGERON 43R CORRODED NEAR BS 1129 - 6-100. INSTALLED REPLACEMENT SECTION OF THE LONGERON IAW SRM 53-00-05, REPAIR 1, TYPE 1, FIG 201, 202.

ATA 5511

INSPECTION TYPE:3C, VERTICAL STABILIZER LOWER MOUNTING FRAME FOR PANEL 361AL CORRODED. REPAIRED CORRODED FRAME IAW VTSAA EA 011-5530-01-A6105, REV IR AND EO MD11-5530-59958-A.

ATA 5313

INSPECTION TYPE:3C, MAIN CABIN LONGERON 17L FITTING BETWEEN F/S 1481-1501 HAS CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT L17L FITTING BS 1481-1501 REF SRM 51-31-01 AND SRM 51-33-01.

ATA 5313

INSPECTION TYPE: 3C, LONGERON 19R CORRODED AT BS 1217. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON BETWEEN BS 1199 -1219 IAW DWG AEA7503 SRM 51-33-01, 51-21-01, 53-00-00 FIG 205.

ATA 5313

INSPECTION TYPE: 3C, MAIN CABIN LONGERON 20R FITTING BETWEEN F/S 1461-1481 HAS CORROSION 2 PLACES. REMOVED, FABRICATED AND INSTALLED REPLACEMENT L20R FITTING BS 1461-1481, REF SRM'S 51-31-01 AND 51-33-01.

ATA 5313

INSPECTION TYPE:3C, LONGERON 19R CORRODED AT BS 1194. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON SECTION BETWEEN BS 1175-1195 IAW DWG AEA7605, AEA7530, SRM 51-31-01, 51-33-01.

ATA 5340

INSPECTION TYPE:3C, FORWARD FUSELAGE PRESSURE BULKHEAD UPPER LT ATTACH FITTING GOUGED BS 281.412, Z=10.125, X=33. ACCOMPLISHED BLEND REPAIR ON FORWARD FUSELAGE PRESSURE BULKHEAD UPPER LT ATTACH FITTING AT BS 281.412, Z=10.125, X=33 IAW VT-SAA, EA 011-5300-01-A6120, REV I/R AND EO MD11-5310-60063-A.

ATA 5313

INSPECTION TYPE:3C, LONGERON 20L CORRODED BETWEEN BS 1441-1461. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON BETWEEN BS 1441-1461 IAW DWG AEA0407 AND SRM 51-33-01.

ATA 5313

INSPECTION TYPE:3C, LONGERON FITTING 20L CORRODED BETWEEN BS 1179-BS 1199. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON FITTING IAW DWG AEA0163, SRM 51-38-01, 51-33-01, 51-21-01.

ATA 5347

INSPECTION TYPE:3C, MAIN CABIN SEAT TRACK SPLICE FITTING CORRODED AT BS 1256 LBL72. R & R SPLICE FITTING IAW DWG ACA7413, SRM 53-00-52, REPAIR 1, 51-33-01.

ATA 5330

INSPECTION TYPE:3C, MAIN CABIN CENTER WING BOX SKIN HAS CORROSION BS 1256 AT LBL87. ACCOMPLISHED BLEND REPAIR, MAIN CABIN CENTER WING BOX SKIN BS 1256 AT LBL 87 IAW SRM 57-10-01.

ATA 5347

INSPECTION TYPE:3C, MAIN CABIN SEAT TRACK CORRODED ON LOWER SURFACE, BS 1273 LBL72. REMOVED CORROSION IAW SRM 53-00-52, FIG 101 AND SRM 51-21-01.

ATA 5313

INSPECTION TYPE:3C, LONGERON FITTING 17L CORRODED BETWEEN BS 1401-1421. REPAIRED CORROSION IAW SRM 53-00-00, FIG 205 AND 51-21-01.

ATA 5313

INSPECTION TYPE: 3C, LONGERON 18L CORRODED BETWEEN BS 1199-1219. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW DWG AEA70656, SRM 53-00-00, FIG 205, 51-33-01, 51-21-01.

ATA 5313

INSPECTION TYPE:3C, LONGERON 19R CORRODED UNDER FLANGE BS 1140. REMOVED CORROSION ON LONGERON 19R AT BS 1140, REF SRM 53-00-00. MATERIAL REMOVED IS .008, REMAINING IS .092 AND WITHIN LIMITS OF SRM 53-00-00.

ATA 5313

INSPECTION TYPE:3C, LONGERON 20R CORRODED BETWEEN BS 1441-1461. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW DWG AEA0407, SRM 51-33-01, 51-21-01.

ATA 5313

INSPECTION TYPE:3C, LONGERON 23R CORRODED BETWEEN BS 1199-1219. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW DWG AEA0163, SRM 51-33-01, 51-21-01.

ATA 5313

INSPECTION TYPE:3C, LONGERON 23R CORRODED BETWEEN BS 1179 - 1199. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW DWG AEA0163, SRM 51-33-01, 51-21-01.

ATA 5313

INSPECTION TYPE:3CMAIN CABIN AT BS 1215 TO 1235, LONGERON 19L HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT L19L FITTING AT BS 1215 TO 1235 REF SRM'S 51-31-01 AND 51-33-01.

ATA 5313

INSPECTION TYPE:3C, MAIN CARGO LONGERON 20R AT BS 1199 - 1219 HAS CORROSION. ACCOMPLISHED BLEND REPAIR ON MAIN CARGO LONGERON 20R, BS 1199 TO 1219 IAW SRM 53-00-00, FIG 205.

ATA 5313

INSPECTION TYPE:3C, MAIN CARGO LONGERON 19L AT BS 1175 TO 1195 HAS CORROSION. ACCOMPLISHED BLEND REPAIR ON MAIN CARGO LONGERON 19L, BS 1175 TO 1195 IAW SRM 53-00-00, FIGURE 205.

ATA 5313

INSPECTION TYPE:3C, CORROSION ON LONGERON 17R BETWEEN BS 1159-1179. REMOVED CORROSION IAW SRM 53-00-00, FIG 205 AND 51-21-01.

ATA 5313

INSPECTION TYPE:3C, LONGERON 16L CORRODED BETWEEN BS 1421-1441. REMOVED CORROSION IAW SRM 53-00-00, FIG 205 AND 51-21-01.

ATA 5313

INSPECTION TYPE:3C, LONGERON 19R CORRODED BETWEEN BS1341-1361. REMOVED CORROSION IAW SRM 53-00-00, FIG 205 AND 51-21-01.

ATA 5313

INSPECTION TYPE:3C, CORROSION ON LONGERON 23L BETWEEN BS 1341-1361. REMOVED CORROSION IAW SRM 53-00-00, FIG 205 AND 51-21-01.

ATA 5313

INSPECTION TYPE:3C, CORROSION ON LONGERON 16R BETWEEN BS 1159-1179. REMOVED CORROSION IAW SRM 53-00-00, FIG 205 AND 51-21-01.

ATA 5313

INSPECTION TYPE:3C, MAIN CABIN LONGERON 18R FITTING BETWEEN F/S 1321-1341 HAS CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT L18R FITTING BS 1321-1341 REF SRM'S 51-31-01 AND 51-33-01.

ATA 5313

INSPECTION TYPE:3C, MAIN CARGO LONGERON 25R SPLICE FITTING CRACKED AT BS 6-0. REMOVED, FABRICATED AND REPLACED MAIN CARGO LONGERON 25R SPLICE FITTING AT BS 6-0 IAW SRM 51-31-01, DWG DAC ADA8435 AND SRM 51-33-01.

ATA 5313

INSPECTION TYPE:3C, CORROSION ON LONGERON 23R BETWEEN BS , 1159-1179. REMOVED CORROSION IAW SRM 53-00-00, FIG 205 AND 51-21-01.

ATA 5510

INSPECTION TYPE:3C, LT HORIZONTAL STABILIZER L/E FAIRING LOWER REAR SUPPORT AT XFS=86.31 CORRODED. ACCOMPLISHED PERMANENT REPAIR TO LT HORIZONTAL L/E FAIRING LOWER REAR SUPPORT AT XFS=86.31 IAW EA 011-5510-01-A6108, REV I/R AND EO MD11-5510-60045-A.

ATA 5510

INSPECTION TYPE:3C, LT HORIZONTAL STAB L/E FAIRING UPPER REAR SUPPORT AT XFS=86.31 CORRODED. ACCOMPLISHED PERMANENT REPAIR TO LT HORIZ STAB L/E FAIRING UPPER REAR SUPPORT AT XFS=86.31 IAW EA 011-5510-01-A6109, REV I/R AND EO MD11-5510-60044-A.

ATA 5510

INSPECTION TYPE:3C, LT HORIZONTAL STABILIZER L/E FAIRING UPPER FWD SUPPORT AT XFS=86.31 CORRODED. ACCOMPLISHED PERMANENT REPAIR TO LT L/E HORIZONTAL STABILIZER FAIRING UPPER FWD SUPPORT AT XFS=86.31 IAW EA 011-5510-01-A6138, REV I/R AND EO MD11-5510-60056-A.

ATA 5313

INSPECTION TYPE:3C, LONGERON 42L CRACKED JUST AFT OF BS 1531. REPAIRED L42L BETWEEN BS 1541-1561 IAW EA 011-5310-01-A6095, REV B AND EO MD11-5310-60174-C.

ATA 5510

INSPECTION TYPE:3C, LT HORIZONTAL L/E FAIRING FWD SUPPORT AT XFS=86.31 IS CORRODED. R & R LT HORIZ L/E FAIRING FWD SUPPORT AT XFS-86.31 IAW AMM 20-50-02-910-810, TABLE 203.

ATA 5510

INSPECTION TYPE:3C, LT HORIZONTAL STABILIZER RIB LOWER AFT CAP FITTING CORRODED AT BS XE122. REPAIRED NOTED CORROSION IAW EA 011-5510-01-A6114, REV IR AND EO MD11-5510-60082-A.

ATA 5510

INSPECTION TYPE: 3C, LT HORIZONTAL STABILIZER RIB LOWER AFT CAP FITTING CORRODED AT BS XE176. REPAIRED NOTED CORROSION IAW EA 011-5510-01-A6113, REV IR AND EO MD11-5510-60081-A.

ATA 5510

INSPECTION TYPE:3C, LT HORIZONTAL STABILIZER RIB LOWER AFT CAP FITTING CORRODED AT BS. XE198 REPAIRED NOTED CORROSION IAW EA 011-5510-01-A6112, REV IR AND EO MD11-5510-60080-A.

ATA 5510

INSPECTION TYPE:3C, LT HORIZONTAL STABILIZER RIB LOWER AFT CAP FITTING CORRODED AROUND FASTENER HOLES. REPAIRED CORRODED FITTING IAW EA 011-5510-01-A6132, REV IR AND EO MD11-5510-60083-A.

ATA 5313

INSPECTION TYPE:3C, LONGERON 48L CORRODED AT BS 807 REPAIRED CORROSION BETWEEN BS 791-24 IAW EA 011-5310-01-A6107, REV IR AND EO MD11-5310-59968-A.

ATA 5510

INSPECTION TYPE:3C, LEFT OTBD ELEVATOR, OTBD HINGE SUPPORT FITTING, CHAFE DAMAGE REPAIRED. NOTED CHAFE DAMAGE IAW EA 011-5510-01-A6101, REV IR AND EO MD11-5510-59940-A.

ATA 5511

INSPECTION TYPE:3C, LT HORIZONTAL STABILIZER REAR SPAR LOWER CAP CORRODED BETWEEN BS XE122-198. REPAIRED NOTED CORROSION IAW VTSAA EA 011-5510-01-A6134, REV IR AND EO MD11-5510-60141-A.

ATA 5330

INSPECTION TYPE:3C, FUSELAGE EXTERIOR SKIN CORRODED, LT SIDE, BS 2122-2160 FABRICATED AND INSTALLED REPAIR BETWEEN BS 2140- 2163, L33L-L35L IAW SRM 53-70-01, REPAIR 3, FIG 201.

ATA 5313

INSPECTION TYPE:3C, LONGERON FITTING 25R CORRODED BETWEEN BS 1321-1341. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON FITTING IAW DWG AEA0305, SRM 51-33-01, 51-21-01.

ATA 5313

INSPECTION TYPE:3C, MAIN CABIN LONGERON 20R FWD END FITTING AT F/S 1219 HAS CORROSION.REMOVED, FABRICATED AND INSTALLED REPLACEMENT FWD END FITTING AT L20R F/S 1219 IAW SRM 51-33-01.

ATA 5313

INSPECTION TYPE:3C, LONGERON FITTING 20R CORRODED BETWEEN BS 1381-1401 IAW IAW SAT THIS SDR REPLACES IPXA2016022399806 WHICH WAS SUBMITTED ON 2/29/16. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON FITTING IAW EA 011-5310-01-A6094, REV IR AND EO MD11-5310-60095-A.

ATA 5313

INSPECTION TYPE:3C, LONGERON FITTING 20R CORRODED BETWEEN STA 1481-1501. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON FITTING IAW DWG AEA0407, SRM 51-33-01, AND 51-21-01.

ATA 5313

INSPECTION TYPE:3C, LONGERON FITTING 20L CORRODED BETWEEN BS 1341-1361. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON FITTING IAW EA 011-5310-01-A6085, REV IR AND EO MD11-5310-60097-A.

ATA 5313

INSPECTION TYPE:3C, MAIN CABIN LONGERON 19R HAS CORROSION BS 1421 TO 1441. R & R MAIN CABIN LONGERON 19R BS 1421-BS 1441 IAW SRM 51-33-01 AND DWG AEA0220.

ATA 5313

INSPECTION TYPE:3C, MAIN CABIN LONGERON 20R FITTING BETWEEN F/S 1421-1441 HAS CORROSION 2 PLACES. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING L20R, BS 1421-1441 IAW EA 011-5310-01-A6090, REV I/R AND EO 5330-60074-A.

ATA 5313

INSPECTION TYPE:3C, MAIN CABIN LONGERON 20R FITTING BETWEEN F/S 1321-1341 HAS CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT L20R FITTING AT 1321 TO 1341 IAW EA 011-5310-01-A6083, REV I/R AND EO MD11-5310-60079-A.

ATA 5313

INSPECTION TYPE:3C, MAIN CABIN LONGERON 23L HAS CORROSION BS 1321 TO BS 1341. ACCOMPLISHED PERMANENT REPAIR ON MAIN CABIN LONGERON 23L, BS 1321 TO 1341 IAW EA 011-530-01-A6091, REV I/R AND EO MD11-5330-60075-A.

ATA 5313

INSPECTION TYPE: 3C, MAIN CABIN LONGERON 23R HAS CORROSION BETWEEN BS 1321-BS 1341. ACCOMPLISHED PERMANENT REPAIR ON MAIN CABIN LONGERON 23R, BS 1321 TO BS 1341 IAW EA 011-5310-01-A6084, REV I/R AND EO 5310-60084-A.

ATA 5313

INSPECTION TYPE:3C, LONGERON 23R FITTING CORRODED BETWEEN BS 1361 -BS 1381. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON FITTING BETWEEN BS 1361-BS 1381 IAW EA 011-5310-01-A6088, REV IR AND EO 5310-60029-A.

ATA 5313

INSPECTION TYPE:3C, LONGERON FITTING 23R CORRODED BETWEEN BS 1381-BS 1401. REPAIRED NOTED LONGERON FITTING IAW EA 011-5310-01-A6082, REV IR AND EO 5310-60078-A.

ATA 5313

INSPECTION TYPE:3C, LONGERON 20R CORRODED BETWEEN BS 1401-1421. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON FITTING IAW EA 011-5310-01-A6093, REV IR AND EO -5310-60077-A.

ATA 5313

INSPECTION TYPE:3C, LONGERON 20L CORRODED BETWEEN BS 1361-1381. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON FITTING IAW EA 011-5310-01-A6092, REV IR AND EO -5310-60076-A.

ATA 5313

INSPECTION TYPE:3C, LONGERON 23R CORRODED BETWEEN BS 1421-1441. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON FITTING IAW EA 011-5310-01-A6089, REV IR AND EO -5310-60031-A.

ATA 5313

INSPECTION TYPE: 3C, LONGERON 20R FITTING CORRODED BETWEEN BS 1361-1381. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON FITTING IAW EA 011-5310-01-A6087, REV IR AND EO MD11-5310-60028-A.

ATA 5313

INSPECTION TYPE:3C, LONGERON 23L CORRODED BETWEEN BS 1361-1381. REMOVED CORROSION FROM LONGERON FITTING BETWEEN BS 1361-1381 IAW SRM 53-00-00, FIG 205 AND 51-21-01.

ATA 5315

INSPECTION TYPE:3C, AFT CARGO FLOOR ANGLE HAS CORROSION BS 1966, RBL6 ACCOMPLISHED BLEND REPAIR ON AFT CARGO FLOOR ANGLE BS 1966, RBL 6 IAW SRM 53-00-00 AND SRM 53-60-08

ATA 5512

INSPECTION TYPE:3C, LT HOZONTAL L/E SKIN HAS CORROSION AT BS XFS103.300. ACCOMPLISHED BLEND REPAIR ON LT HORIZONTAL L/E SKIN BS XFS 103.300 IAW SRM 51-21-01 AND SRM 55-00-00.

ATA 5510

INSPECTION TYPE:3C, RT HORIZONTAL STABILIZER OTBD ELEVATOR HINGE SUPPORT FITTING HAS CHAFE DAMAGE AT STA XE=379.250. ACCOMPLISHED CHAFE REPAIR ON RT HORIZONTAL STABILIZER OTBD FITTING AT BS XE=379.250 IAW VT-SAA EA 011-5550-01-A6118, REV I/R AND EO 5520-60025-A.

ATA 5510

INSPECTION TYPE:3C, RT HORIZONTAL STABILIZER DETACHABLE ELEVATOR HINGE SUPPORT FITTING HAS CHAFE DAMAGE AT BS XE=51. ACCOMPLISHED CHAFE REPAIR ON RT HORIZONTAL STABILIZER ELEVATOR HINGE SUPPORT FITTING AT BS XE=51 IAW VT-SAA EA 011-5550-01-A6098, REV I/R AND EO MD11-5520-59984-A.

ATA 5313

INSPECTION TYPE: 3C, LONGERON 17R CRACKED BETWEEN BS 1239-1249. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON FITTING BETWEEN BS 1239-1256 IAW DWG AEA7064. SRM 51-31-01, 51-33-01.

ATA 5322

INSPECTION TYPE:3C, CENTER CARGO SHEAR TIE AT BS 5-53 BETWEEN L30R AND L35R HAS CORROSION. R & R CENTER CARGO SHEAR TIE BS 5-53 BETWEEN L30R AND L35R IAW SRM 51-35-01, SRM 53-00-06 AND DAC DWG A5A7056.

ATA 5313

INSPECTION TYPE:3C, LONGERON 17R CORRODED BETWEEN BS 1219-1239. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON BETWEEN BS 1219-1239 IAW DWG A, EA7530 AND SRM 51-33-01.

ATA 5313

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

ATA 5313

INSPECTION TYPE:3C, CORROSION ON L18R BETWEEN BS 1361-1381. REMOVED CORROSION IAW SRM 53-00-00, FIG 205 AND 51-21-01.

ATA 5313

INSPECTION TYPE:3C, CORROSION ON L25L BETWEEN BS 1321-1341. REMOVED CORROSION IAW SRM 53-00-00, FIG 205 AND 51-21-01.

ATA 5313

INSPECTION TYPE:3C, CORROSION ON LONGERON 20L BETWEEN BS 1321-1341. REMOVED CORROSION IAW SRM 53-00-00, FIG 205 AND 51-21-01.

ATA 5313

INSPECTION TYPE:3C, CORROSION ON LONGERON 16L BETWEEN BS 1441-1461. REMOVED CORROSION IAW SRM 53-00-00, FIG 205 AND 51-21-01.

ATA 5313

INSPECTION TYPE: 3C, AREAS OF CORROSION ON L25R BETWEEN BS 1179-1199. REMOVED CORROSION IAW SRM 51-21-01 AND 53-00-00, FIG 205.

ATA 5313

INSPECTION TYPE: 3C, LONGERON 19L CORRODED BETWEEN BS 1441-1461. REMOVED CORROSION IAW SRM 53-00-00, FIG 205 AND 51-21-01.

ATA 5313

INSPECTION TYPE: 3C, CORROSION ON L17R BETWEEN BS 1361-1381. REMOVED CORROSION IAW SRM 53-00-00, FIG 205 AND 51-21-01.

ATA 5313

INSPECTION TYPE: 3C, CORROSION ON L19R BETWEEN BS 1361-1381. REMOVED CORROSION IAW SRM 53-00-00, FIG 205 AND 51-21-01.

ATA 5313

INSPECTION TYPE: 3C, CORROSION ON L25R BETWEEN BS 1341-1361. REMOVED CORROSION IAW SRM 53-00-00, FIG 205 AND 51-21-01.

ATA 5313

INSPECTION TYPE:3C, CORROSION ON L23R BETWEEN BS 1341-1361. REMOVED CORROSION IAW SRM 53-00-00, FIG 205 AND 51-21-01.

ATA 5313

INSPECTION TYPE:3C, CORROSION ON L16L BETWEEN BS 1481-1501. REMOVED CORROSION IAW SRM 51-21-01 AND 53-00-00, FIG 205.

ATA 5313

INSPECTION TYPE: 3C, AREAS OF CORROSION ON L16L BETWEEN BS 1461-1481. REMOVED CORROSION IAW SRM 51-21-01 AND 53-00-00, FIG 205.

ATA 5313

INSPECTION TYPE: 3C, AREAS OF CORROSION ON LONGERON 20R BETWEEN BS 1179-1199. REMOVED CORROSION IAW SRM 51-21-01 AND 53-00-00, FIG 205.

ATA 5322

INSPECTION TYPE: 3C, SHEAR TIE CORRODED IN AFT CARGO COMPARTMENT BS 1853 AT L51L. REMOVED CORROSION IAW 51-00-00, 53-00-00, FIG 205, AND 51-21-01.

ATA 5313

INSPECTION TYPE: 3C, CORROSION ON L19L SECTION BETWEEN BS 1481-1501. REMOVED CORROSION IAW SRM 51-21-01 AND SRM 53-00-00, FIG 205.

ATA 5313

INSPECTION TYPE: 3C, CORROSION ON LONGERON 17R SECTION BETWEEN BS 1341-1361. REMOVED CORROSION IAW SRM 53-00-00, FIG 205 AND SRM 51-21-01.

ATA 5313

INSPECTION TYPE:3C, CORROSION ON LONGERON 20R SECTION BETWEEN BS 1219 - 1239. REMOVED CORROSION IAW SRM 53-00-00 FIG 205 AND 51-21-01.

ATA 5313

INSPECTION TYPE: 3C, MAIN CABIN LONGERON 20R FITTING BETWEEN FS 1159-1179 HAS CORROSION IN 2 PLACES. REMOVED CORROSION ON MAIN CABIN LONGERON 20R BETWEEN FS 1159-1179 REF SRM 53-00-00. MATERIAL LOSS IS .004 REMAINING IS .096. AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-00-00.

ATA 5313

INSPECTION TYPE:3C,MAIN CABIN LONGERON 23R FITTING BETWEEN F/S 1481-1501 HAS CORROSION IN 2 PLACES. REMOVED CORROSION LONGERON 23R BETWEEN F/S 1481-1501, REF SRM 53-00-00. MATERIAL LOSS IS .004, REMAINING IS .096. FOUND TO BE WITHIN LIMITS OF SRM 53-00-00.

ATA 5313

INSPECTION TYPE:3C, MAIN CABIN BS 1421-1441, LONGERON 19L HAS HEAVY CORROSION. REMOVED CORROSION FROM LONGERON 19L, BS 1421-1441, REF SRM 53-00-00. MATERIAL REMOVED IS .009, REMAINING IS .091 AND WITHIN LIMITS IAW SRM 53-00-00.

ATA 5313

INSPECTION TYPE:3C, LONGERON 20R CORRODED BETWEEN BS 1381-1401. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW DWG AEA0407 SRM 51-33-01, 51-21-01.

ATA 5313

INSPECTION TYPE:3C, LONGERON 23R CORRODED BETWEEN BS 1441-1461. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW DWG AEA0407, SRM 51-33-01, 51-21-01.

ATA 5313

INSPECTION TYPE: 3C, UPPER CARGO LONGERON 24R AT BS 1321 - 1341 HAS CORROSION. ACCOMPLISHED BLEND REPAIR IAW SRM 53-00-00, FIGURE 205.

ATA 5320

INSPECTION TYPE:3 C, UPPPER CARGO INTERCOSTAL BS 1341 - 1361 AT L20R HAS CORROSION. ACCOMPLISHED BLEND REPAIR IAW SRM 53-00-00, FIGURE 205.

ATA 5313

INSPECTION TYPE:3C, LONGERON 23R CORRODED BETWEEN BS 1461-1481. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW DWG AEA0407 SRM 51-33-01, 51-21-01.

ATA 5730

INSPECTION TYPE: 3C, LT WING LOWER SURFACE SKIN PANEL XORS 683-713, PANEL 536AB, 4 CRACKS AT PANEL LANDING FASTENER HOLES. REPAIRED NOTED CRACKS IAW SRM 57-20-02, REPAIR 5 FIG. 201.

ATA 5310

INSPECTION TYPE:3C, R3 DOOR JAMB AFT LOWER WEB CRACKED REPAIRED R3 DOOR JAMB WEB BETWEEN BS 1305-1315 IAW SRM 53-40-15, REPAIR 3, FIG 201.

ATA 5330

INSPECTION TYPE: 3C, FUSELAGE EXTERIOR SKIN CORRODED AT BS 1821 ALONG L27R. REMOVED CORROSION IAW SRM 53-00-00, FIG 202 AND SRM 51-21-01.

ATA 5730

INSPECTION TYPE:3C, RT WING LOWER SURFACE SKIN PANEL XORS 683-713, PANEL 636AB, 2 CRACKS AT PANEL LANDING FASTENER HOLES REPAIRED NOTED CRACKS IAW SRM 57-20-02, REPAIR 5, FIG. 201.

ATA 5310

INSPECTION TYPE:3C, L3 DOOR FORWARD FRAME WEB CRACKED AT LIGHTNING HOLE. REPAIRED L3 DOOR JAMB WEB BS 1250-1256, LBL 107, Z=-15 IAW EA 011-5310-01-A6096, REV IR AND EO MD11-5310-60127-A.

ATA 5720

INSPECTION TYPE:3C, LT WING LOWER T/E EXTERIOR SPACER CRACKED NEAR XW372. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SPACER IAW DWG ARC7016, SRM 51-33-01, AND 51-35-01.

ATA 5753

INSPECTION TYPE: 3C, RT WING INBD FLAP VANE HAS 2 EA AREAS OF DELAMINATION ON LOWER OTBD SURFACE ACCOMPLISHED PERMANENT REPAIR ON RT WING INBD FLAP VANE OTBD LOWER SURFACE, 40" TO 46" FROM OTBD EDGE, 13.5" TO 4.5" FROM T/E, 5.5" TO 8" WIDE IAW SRM 57-50-80, REPAIR 2.

ATA 5753

INSPECTION TYPE: 3C, RIGHT WING INBD FLAP VANE HAS 2 EA AREAS OF DELAMINATION ON LOWER INBD SKIN. ACCOMPLISHED PERMANENT REPAIR ON RT WING INBD FLAP VANE LOWER INBD SKIN 60.5" TO 65.5" FROM INBD EDGE, 8" TO 17.5" TO T/E, 5.5" TO 11" WIDE, IAW SRM 57-50-80, REPAIR 2.

ATA 5753

INSPECTION TYPE:3C, AREAS OF DELAMINATION ON LT INBD FLAP VANE LOWER SURFACE, MIDSPAN. REPAIRED NOTED DELAMINATED IAW SRM 57-50-80, REPAIR 2.

ATA 5753

INSPECTION TYPE:3C, AREAS OF DELAMINATION ON LT INBD FLAP VANE LOWER SURFACE AT OTBD END. REPAIRED NOTED DELAMINATED IAW SRM 57-50-80, REPAIR 2.

ATA 5321

INSPECTION TYPE:3CRCB, AREA FLOOR PANEL WSP 0791-501 CORRODED, BS 484, LBL 85. REPAIRED NOTED CORROSION IAW EA 011-5310-01-A6079, REV IR AND EO MD11-5310-59890-A.

ATA 5753

INSPECTION TYPE:3C, LT OTBD FLAP, OTBD TRACK WORN ALONG UPPER INBD SIDEREPAIRED FLAP TRACK IAW EA 011-5753-01-A6104, REV IR AND EO MD11-5310-60101-A.

ATA 5730

INSPECTION TYPE:3C, LEFT WING FIXED L/E INNER BEADED DOUBLER CRACKED BETWEEN XOS 621 - 636. REPAIR NOTED, BEADED DOUBLER IAW VTSAA EA 011-5730-01-A6086, REV IR AND EO MD11-5730-60126-A.

ATA 5730

INSPECTION TYPE:3C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED BETWEEN XOS 621 - 636. REPAIRED NOTED BEADED DOUBLER IAW EA 011-5730-01-A6086, REV IR AND EO MD11-5730-60126-A.

ATA 5730

INSPECTION TYPE:3C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED BETWEEN XOS 621 - 636. REPAIRED NOTED BEADED DOUBLER IAW EA 011-5730-01-A6086, REV IR AND EO MD11-5730-60126-A.

ATA 5730

INSPECTION TYPE:3C, LT WING LOWER L/E SKIN CRACKED AT NR 12 SLAT TRACK CUTOUT ACCOMPLISHED PERMANENT REPAIR ON LT WING L/E LOWER SKIN FROM BS XOS 768.2 TO XOS 783.2 IAW SRM 57-40-02, REPAIR 7, FIGURE 201.

ATA 5730

INSPECTION TYPE:3C, RT WING FIXED L/E SKIN INNER SPLICE STRAP CRACKED NEAR BS XOS 667. REMOVED FABRICATED AND INSTALLED REPLACEMENT SPLICE STRAP IAW DWG ARB3954 AND SRM 51-33-01.

ATA 5730

INSPECTION TYPE:3C, RT WING FIXED L/E EXTERIOR SKIN CHAFE DAMAGE ADJACENT TO NR 11 SLAT TRACK REPAIRED RT WING L/E EXTERIOR SKIN BETWEEN XOS 721-759 IAW SRM 57-40-02, REPAIR 3 FIG 201.

ATA 5710

INSPECTION TYPE:3C, LEFT WING L/E PANEL LANDING CHORD CRACKED AT BS XORS506. R & R LT WING CHORD IAW SRM 51-35-01, SRM 51-33-01, AND DAC DWG ARB2933.

ATA 5710

INSPECTION TYPE:3C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS789. REPAIRED BEADED DOUBLER BETWEEN BS 789-795 IAW SRM 57-40-02, REPAIR 15, FIG. 203.

ATA 5730

INSPECTION TYPE:3C, EXISTING TEMPORARY BEADED DOUBLER REPAIR LT WING FIXED L/E XOS 759 - 763. REQUIRES PERMANENT REPAIR PERFORMED PERMANENT REPAIR OF LT WING BEADED DOUBLER XOS 759-763 IAW SRM 57-40-02, REPAIR 15, FIG 203.

ATA 5730

INSPECTION TYPE:3C, RT WING FIXED L/E FORMER ANGLE CRACKED NEAR BS XOS 584 REMOVED, FABRICATED, AND INSTALLED REPLACEMENT ANGLE IAW DWG ARB2931 AND SRM 51-33-01.

ATA 5710

INSPECTION TYPE:3C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED XOS 698 -703. REPAIRED RT BEADED DOUBLER XOS 698-703 IAW SRM 57-40-02, REPAIR 15, FIG 203.

ATA 5710

INSPECTION TYPE:3C, REF D-511308 AND D-511309. LT WING L/E EDGE BEADED DOUBLER REPAIR AT BS 584-589, REQUIRES PERMANENT REPAIR. REMOVED EXISTING BEADED DOUBLER REPAIR LT WS XOS 584-589. ADDITIONAL CRACKS FOUND. ACCOMPLISHED PERMANENT REPAIR IAW SRM 57-40-02, REPAIR 15, FIG 203, REV 60.

ATA 5710

INSPECTION TYPE:3C, RT WING L/E BEADED DOUBLER REPAIR, XOS 610-616, REQUIRES REPLACEMENT DUE TO TIME LIMITED ACCOMPLISHED BEADED DOUBLER TEMP REPAIR ON RT WING L/E BS XOS 610-616 IAW SRM 57-40-02, REPAIR 15, FIGURE 206.

ATA 5320

INSPECTION TYPE:3C, LOWER CENTER CARGO DOOR JAMB SEAL RETAINER DAMAGED ALONG FWD JAMB FABRICATED AND INSTALLED REPLACEMENT RETAINER SECTION IAW SRM 53-00-15, REPAIR 10.

ATA 5710

INSPECTION TYPE:3C, LEFT WING L/E PANEL LANDING CHORD CRACKED AT BS XORS 506. R & R LT WING PANEL LANDING CHORD DOUBLER IAW SRM 51-35-01, SRM 51-33-01 AND DWG ARB2933.

ATA 5730

INSPECTION TYPE:3C, LT WING L/E SKIN CRACKED AT NR 10 SLAT TRACK TRACK CUTOUT BS XOS 661.7174. ACCOMPLISHED PERMANENT REPAIR ON LT WING FIXED L/E AT NR 10 SLAT TRACK CUTOUT, BS XOS 661.7174 IAW EA 011-5754-01-A6078, REV I/R AND EO MD11-5730-60183-A.

ATA 5710

INSPECTION TYPE:3C, RT WING L/E CRUISE PERFORMANCE FAIRING INBD WEB CRACKED. REPAIRED CRACKED WEB IAW EA 011-5754-01-A6100, REV. IR AND EO MD11-5720-60162-A.

ATA 5730

INSPECTION TYPE: 3C, RT WING FIXED L/E EXTERIOR SKIN CHAFE DAMAGE NEAR NR 11 SLAT TRACK. REPAIRED CHAFE DAMAGE TO RT WING L/E BETWEEN BS XOS 673-714 IAW EA 011-5730-01-A6097, REV IR AND EO MD11-5730-59919-A.

ATA 5710

INSPECTION TYPE:3C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED XOS 667-673. REPAIRED RT WING BEADED DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG. 203.

ATA 5320

INSPECTION TYPE:3C, RCB, WALL LT NR 1 FLOOR FITTING CRACKED. R & R RCB WALL LT NR 1 FLOOR FITTING IAW AMM 25-59-13-400-801 AND AMM 20-50-02-910-801, MINOR.

ATA 5711

INSPECTION TYPE:3C, LEFT WING LOWER T/E SPAR CAP SILL STRAP CRACKED NEAR XORS 433 REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SILL STRAP IAW DWG ARC7008, SRM 51-33-01, 51-21-01.

ATA 5240

R1 DOOR OUTER SKIN GOUGED. REPAIRED IAW EO MD11-5210-58495-B.

ATA 2565

L1 DOOR ESCAPE SLIDE CAME LOOSE FROM CONTAINER DURING REMOVAL. RESECURED L1 ESCAPE SLIDE IN CONTAINER IAW AMM 25-61-15.

ATA 2560

L1 DOOR SLIDE GIRT BAR FLAP LACING PIN & CABLE MISSING. INSTALLED NEW SLIDE/RAFT IN L1 DOOR SLIDE CORNER ASSY IAW AMM 25-61-15 EFF SOURCE.

ATA 5240

1 ENTRY DOOR OUTER SKIN DAMAGED, REF EO-MD11-5210-57709-B FOR REPAIR.

ATA 2565

L1 DOOR ESCAPE SLIDE/RAFT DAMAGED. REINSTALLED PANEL IAW AMM 25-61-01.

ATA 5532

CORROISON ON SKIN UNDER PANEL 364RR BOTTOM NEAR INTERCOSTAL. REMOVED DAMAGE IAW EO 5530-57772-A , FABRICATED DOUBLER AND FILLER IAW WITH EO 5530-57772-A AND INSTALL REPAIR IAW EO 5530-57772-A AND INSTALLED .

ATA 5414

SKIN CORROSION FOUND BETWEEN YIN111 AND YIN116 AND INTERCOSTAL AJC7157-1 RT SIDE OF NR 2 NACELLE. REPAIR ACCOMPLISHED IAW EO MD11-5530-57772-A TRANSFER FROM N/R 582751.

ATA 5210

L1 ENTRY DOOR UPPER OUTER SKIN BOND DAMAGED. REPAIRED DOOR DAMAGE IAW EO MD11-5210-56805B.

ATA 2620

NR 3 ENGINE, AGENT 1 WOULD NOT DISCHARGE FIRE BOTTLE, CONFIRMED FAULTY PRESSURE SWITCH. R & R BOTTLE ASSY IAW AMM.

ATA 2697

DURING INITIAL DESCENT, RECEIVED AN INTERMITTENT LEVEL 1 FIRE DETECTOR FAILURE, THEN RECEIVED A LEVEL 3 ENGINE FIRE INDICATION. EMERGENCY DECLARED SHUTDOWN ENGINE NR 3. REPAIRED THE TERMINAL AT UPPER LT LOOP A, DH4A AND DH4C IAW SWPM 20-30-11. REPLACED HARNESS BETWEEN LOOP B, UPPER LT AND RT AND UPPER RT TO LOWER IAW MM 20-30-01. OPS CHECKED GOOD IAW MM 26-11-02-700-801.

ATA 5730

INSPECTION 1C, RT WING FIXED L/E SKIN HAS CHAFE DAMAGE AT XDLE 330. REPAIRED IAW EA 011-5740-01-A5628, REV I/R AND EO 5720-5573-A.

ATA 5730

INSPECTION 1C, RT WING DROOP L/E OTBD END CHAFED AT AREA ABOVE SEAL. REPAIRED DROOP L/E END AT AREA ABOVE SEAL IAW SRM 57-40-01, REPAIR 15, FIG 202.

ATA 2910

HYDRAULIC QTY 3 LOW FAIL, REPLACED NR 3 SYS SPOILER SERVO AND ACTUATOR PACKING. PERFORMED HYD TEST NO MORE LEAK ALL SYS OK. PERFORMED NR 3 HYD SYS BLEEDING IAW 29 -03-00. ALL SYS OK.

ATA 3350

EMERGENCY LIGHTS TEST SHOWED BATTERY ONE LOW. R & R EMERGENCY BATTERY IAW MM 33-51-01-400-802. SYS OPS CHECKED OK.

ATA 3397

INSPECTION TYPE: 2C, EMERGENCY LIGHTS ARE ILLUMINATED WHILE SWITCH IS IN THE ARM POSITION. REPAIRED BROKEN WIRE AT TERMINAL BLOCK UNDER PANEL 227CC IAW WDM 33-51-01 AND SWPM 20-20-02. SYS CHECKED GOOD IAW AMM 33-50-00-700-802.

ATA 5330

INSPECTION TYPE:2C, MAIN CABIN CORROSION ON SKIN BS 1249, LBL75. REPAIRED IAW EA 011-5730-01-A4848 REV IR AND EO MD11-5730-51834-A.

ATA 5320

INSPECTION TYPE:1C, CENTER CARGO BAY TRANSCEIVERS, FRAME, SHEAR TIE AND J CHANNEL HAS CORROSION IN 2EA AREAS AT BS 1781 BETWEEN LONGERON 50R AND 51R. REMOVED, FABRICATED AND INSTALLED FILLER AND CHANNEL IAW EA 011-5310=0 1-A4847, REV I/R AND EO MD11-5310-51842-A.

ATA 5322

INSPECTION TYPE:2C CENTER CARGO COMPT FRAME SHEAR TIE 2EA HAS CORROSION BETWEEN L49-51L. R & R SHEAR TIE IAW SRM 53-00-06, REPAIR 1, FIG 202.

ATA 5713

INSPECTION TYPE:1C, CRACKED ON STRINGER 38 RT WING INSIDE FUEL ACCESS HOLE 638CB BETWEEN STA 855.3 TO 855.4. CUT OUT DAMAGED STRINGER. FABRICATED AND INSTALLED DOUBLER AND SPLICE IAW EA 011-5710-01-A4836, REV I/R AND EO MD11-5710-51835-A.

ATA 5730

INSPECTION TYPE:1C, LT WING L/E INNER SKIN BEADED DOUBLER REPAIR STA XOS 75 9-763, REQUIRES REPAIR. PREVIOUS REPAIR INSTALLED IAW EO MD11-5730-47 906-A. REMOVED, FABRICATED AND INSTALLED NEW DOUBLER IAW EA 011-5730-01-A48-39, REV I/R AND EO MD11-5730-47906-C.

ATA 5530

INSPECTION TYPE:2C, APPROX 1 INCH LONG CRACK, ALONG AFT EDGE OF INTERCOSTAL, AT VERTICAL STAB REAR SPAR RELIEF CUTOUT, AS SHOWN IN SRM 55-30-02, REPAIR 7, FIG 203. INSTALLED REPAIR AT VERTICAL STAB REAR SPAR INTERCOSTAL AFT EDGE AT RELIEF CUTOUT IAW SRM 55-30-02, REPAIR 7, FIG 203.

ATA 5730

INSPECTION TYPE:1C, REF D-484950, LT WING L/E INNER SHIM BEADED DOUBLER REQUIRES REPAIR STA XOS 625-629. PREVIOUS REPAIR INSTALLED IAW EO MD11-5730-47903-A. REMOVED, FABRICATED AND REPLACED BEADED DOUBLER AND FILLER IAW EA 01 1-5730-01-A4846, REV I/R AND EO MD11-5730-47903-C.

ATA 5730

INSPECTION TYPE:1C, LT WING L/E INNER SKIN DOUBLER STA 584-589 REQUIRES REP AIR. PREVIOUS REPAIR INSTALLED IAW EO MD11-5730-47904-A. REMOVED DAMAGED DOUBLER, FABRICATED AND INSTALLED DOUBLER IAW EA 011-5730-01-A4840, REV I/R AND EO MD11-5730-47904-C.

ATA 3350

DURING EMERGENCY LIGHT TEST THE EMERGENCY LT BATT 1 LOW MESSAGE ILLUMINATED, COMPLIED WITH FIM 33-51-02-00. REPLACED EMERGENCY LIGHT BATTERY IAW AM AMM 33-51-01-00/400-802. OPS CHECKED GOOD.

ATA 3211

AFTER GEAR RETRACTION, PRIMARY & SECONDARY IND GEAR INDICATES LT MAIN GEAR WAS UNSAFE. AIR TURNBACK DUE TO GEAR UNSAFE CONDITION AFTER TAKEOFF. R & R LT MLG SENSOR SUPPORT IAW AMM 32-34-03.

ATA 3350

DURING PDC, FOUND EMERGENCY LIGHT INOPERATIVE. R & R BATTERY POWER SUPPLY IAW MM 33-51-01-401. TEST SATISFACTORY.

ATA 3350

EMERGENCY LIGHTS DO NOT PASS TEST MESSAGE, EMERGENCY BATTERY 1 LOW, TROUBLESHOT IAW FIM 33-51-00-101, FIG 104. EMERGENCY LIGHT TEST PASSED. PERFORMED OPS TEST IAW MM 33-51-01-700-802.

ATA 5730

INSPECTION TYPE: 3C, BEADED DOUBLER CRACKED INSIDE RT WING L/E AT XORS593 (XOS698-703). REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS698-703 IAW STASA EA 011-5730-01-A4098, REV IR & EO MD11-5730-47973-A, FAA 8100-9.

ATA 5730

INSPECTION TYPE: 3C, RT WING FIXED L/E COMPT BEADED DOUBLER CRACKED NEAR XFS587 (XOS610- 616). REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS610-616 IAW EA 011-5730-01-A4097, REV IR, EO MD11-5730-47991-A.

ATA 5730

INSPECTION TYPE: 3C, LT WING FIXED L/E COMPT BEADED DOUBLER CRACKED NEAR XORS 656 (XOS759- 763). REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS759-763 IAW STASA EA 011-5730-01-A4099, REV IR & EO MD11-5730-47906-A, FAA 8100-9.

ATA 5712

INSPECTION TYPE: 3C, LEFT WING FIXED L/E COMPT RIB (FORMER) CRACKED NEAR XORS832. REMOVED FABRICATED & INSTALLED REPLACEMENT FORMER IAW DWG ARB1292, SRM 51-33-01 & 51-35-01.

ATA 5730

INSPECTION TYPE: 3C, LT WING FIXED L/E COMPT BEADED DOUBLER CRACKED NEAR XORS 482 (XOS584- 588). REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS584-588 IAW STASA EA 011-5730-01-A4096 REV IR & EO MD11-5730-47904-A, FAA 8100-9.

ATA 5730

INSPECTION TYPE: 3C, RT OUTER WING FIXED L/E COMPT BEADED DOUBLER CRACKED NEAR XFS669 (XOS 667-673). REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS 667-673 IAW EA 011-5730-01-A4098 REV IR & EO MD11-5730-47973-A FAA8100-9.

ATA 5730

INSPECTION TYPE:3C, LT WING FIXED L/E COMPT BEADED DOUBLER CRACKED NEAR XORS.524 (XOS625- 629). REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS625-629 IAW EA 011-5730-01-A4095 REV IR & EO MD11-5730-47903-A.

ATA 3497

DURING CLIMBOUT, PASSING 10000 FT RECEIVED AVNCS EXH FLO OFF LEVEL 2 MESSAGE. FOUND PINS A&C TO BE DEFECTIVE ON CONNECTOR P1-138. RETERMINATED PINS R & R WITH SERVICEABLE ESC REF 21-08-01-4. PERFORMED TEST OF AVIONICS VENTURI S/O VALVE REF 21-26-08-700-801 AND OPS TEST OF ESC 21-08-01-700-801. ALL TESTS GOOD

ATA 5542

INSPECTION TYPE:C4, LOWER LT FWD CORNER OF UPPER AFT RUDDER LAMINATED SKIN DISBONDED. REPAIRED LOWER LT FWD CORNER OF UPPER AFT RUDDER LAMINATED SKIN IAW STA-SA EA 011-5540-01-A-3289-I/R AND UPS EO MD11-5540-43566-A.

ATA 5540

INSPECTION TYPE:4C, RT SIDE OF LOWER FORWARD RUDDER AFT SEAL LANDING BELOW PANEL 375AR HAS CORROSION. REMOVED, FABRICATED AND INSTALLED RT SIDE OF LOWER FWD RUDDER AFT SEAL LANDING TEE REF STA, SA, EA 011-5540-01-A3265 AND EO MD11-5540-43492-A.

ATA 5540

INSPECTION TYPE:4C RT SIDE OF FWD UPPER RUDDER AFT SEAL LANDING BELOW PANEL 376CR IS CORRODED. REMOVED AFT SEAL LANDING TEE FROM RT SIDE OF FWD UPPER RUDDER. FABRICATED REPLACEMENT T-ANGLE AND INSTALLED REF STA, SA, EA 011-5540- 01-A3264 REV I/R AND EO MD11-5540-43491-A.

ATA 5313

INSPECTION TYPE:4C, AFTER REMOVAL OF SPICE FITTING ON LONGERON 51L FOUND CORROSION STA 1129. R & R LONGERON AND SPLICE FITTING REF SRM 51-33-01 PG. 45, 30.

ATA 5313

INSPECTION TYPE:4C, AFTER REMOVAL OF SPLICE FITTING ON LONGERON 52 AT FS 1129/6-73.5 FOUND 2EA CRACKS ON SPLICE FITTING. R & R SPLICED FITTING ON L52 AT FS1129/6-73.5 REF. SRM 51-33-01 PG 30 AND 45.

ATA 5330

INSPECTION TYPE:4C, MODERATE TO HEAVY CORROSION AROUND FASTENER HOLES FOR HORZ STAB FAIRING ON RT TAIL SKIN STA 2127-2163 UNDER MYLAR TAPE. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED ON RT TAIL SKIN AT STA 2140-2163 AND L33R TO L35R REF SRM 53-70-01, REPAIR 3, FIG 3.

ATA 5321

INSPECTION TYPE:4C MAIN CABIN FLOORBOARD 263AF HAS PUNCTURE AND DELAM ON UPPER SIDE. FABRICATED MAIN DECK FLOORBOARD 263AF REF EO MD11 5320-27386-C.

ATA 5713

INSPECTION TYPE:4C, LT WING NR 1 TANK THROUGH ACCESS 538CB FORWARD AREA LOWER STRINGER IS CRACKED AS MARKED. CUT OUT DAMAGE AT NR 1 TANK ACCESS 538CB STRINGER 38L FROM XORS855 TO AG XORS885. FABRICATED AND INSTALLED REPAIR PARTS REF SRM 57-00-03 03, REPAIR 4, FIG 201 AND 202, REV 46.1.

ATA 5713

INSPECTION TYPE:4C, LT WING TANK STRINGER IS CRACKED AT FASTENER AT XORS570 APPX, THROUGH ACCESS 535AT. TRIMMED DAMAGE FROM LT WING LOWER STRINGER 43 AT XORS570. FABRICATED SPLICE FITTING AND SPLICE DOUBLER AND INSTALLED REF STA, SA, EA 011- 5530-01-A3254 REV. I/R AND EO MD11-5710-43537-A.

ATA 5321

INSPECTION TYPE:4C, MAIN CABIN FLOOR PANEL 263RF HAS 2EA EDGE DAMAGE. FABRICATED MAIN DECK FLOOR PANEL 263RF REF EO MD11-5320-27386, APPX A/B.

ATA 5321

INSPECTION TYPE:4C, MAIN CABIN FLOORBOARD 261JF HAS A PUNCTURE ON LOWER SIDE. FABRICATED MAIN DECK FLOORBOARD 261JF REF EO MD11-5320-27386-C.

ATA 5321

INSPECTION TYPE:4C, MAIN CABIN FLOORBOARD 261KF HAS EDGE DAMAGE. FABRICATED CABIN FLOORBOARD 261KF REF EO MD11-5320-27386-C APPX A/B.

ATA 5321

INSPECTION TYPE:4C, MAIN CABIN FLOORBOARD 262AF HAS MULTIPLE PUNCTURES ON UPPER SIDE. FABRICATED FLOORBOARD 262AF REF. EO MD11-5320-27386-C APPX B.

ATA 5321

INSPECTION TYPE:4C, MAIN CABIN FLOORBOARD 263NF HAS 3EA EDGE DAMAGE. FABRICATED MAIN CABIN FLOOR PANEL 263NF IAW EO MD11-5320-27386-C APPX. B.

ATA 5313

INSPECTION TYPE:4C CORROSION ON LONGERON 52 AT FS 1129. R & R LONGERON REF SRM 51-33-01, PG 45 AND 30.

ATA 5313

INSPECTION TYPE:4C, CORROSION ON LONGERON 51L AT FS 1129/73.5. R & R LONGERON 51L AT FS 1129/73.5 REF SRM 51-33- 01 PG 45 AND 30.

ATA 5322

INSPECTION TYPE:4C, CENTER CARGO FRAME SHEAR TIE HAS EXFOLIATION CORROSSION AT STA 1721 AND RBL6 AND LBL3. REMOVED DAMAGE AREA, AND SPLICED NEW SECTION OF SHEAR TIE WITH FABRICATED DOUBLERS REF SRM 53-00-06, REPAIR 1, FIG 202 REV 46.

ATA 5313

INSPECTION TYPE:4C, CENTER CARGO COMPT L-30R SPLICE FITTING CRACKED AT STA 1671. REMOVED, FABRICATED AND INSTALLED L-30R SPLICE FITTING AT STA 1671 REF AFA7830-501 AND SRM 51-33-01.

ATA 5313

INSPECTION TYPE:4C CENTER CARGO COMPT L-29R SPLICE FITTING CRACKED AT STA 1671. REMOVED, FABRICATED AND INSTALLED L29R SPLICE FITTING AT STA 1671 REF AFA7830 AND SRM 51-33-01.

ATA 5313

INSPECTION TYPE:4C, CENTER CARGO COMPT L-45L SPLICE FITTING IS CRACKED ON BOTH FWD AND AFT RADIUS AT STA 1551. REMOVED, FABRICATED AND INSTALLED LONGERON SPLICE FITTING L-45L AT STA 1551, REF SRM 53-00-05 AND SRM 51-33-01.

ATA 5313

INSPECTION TYPE:4C, CTR CARGO COMPT L-45L SPLICE FITTING IS CRACKED ON FWD RADIUS AT STA 1591. REMOVED, FABRICATED AND INSTALLED L-45L SPLICE FITTINGAT STA 1591 REF SRM 53-00-05 AND SRM 51-33-01.

ATA 5330

INSPECTION TYPE:4C SURFACE CORROSION IN AFT FUSELAGE EXTERIOR SKIN BELOW LT HORZ STAB AT STA 2140-2164. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED AT AFT FUS SKIN BELOW LT HORZ STAB AT STA 2140-2164 REF 53-70-01, REPAIR 3, FIG 201.

ATA 5313

INSPECTION TYPE:4C, CENTER CARGO COMPT L-41L SPLICE FITTING CRACKED AT STA 1531/5-123 ON FWD END PAST FASTENER HOLE. REMOVED, FABRICATED AND INSTALLED L-41L SPLICE FITTING AT STA 1531/5-1 23 REF A5A7115 AND SRM 51-33-01.

ATA 5313

INSPECTION TYPE:4C, CENTER CARGO COMPT L-31R SPLICE FITTING IS CRACKED 2EA AT STA 1531/5-0. REMOVED, FABRICATED AND INSTALLED LONGERON AT STA 1531/5-0 REF DWG AEA7642 AND SRM 51-31-01.

ATA 5320

INSPECTION TYPE:4C, CORROSION ON FINGER DOUBLER AND STIFFENERS LOCATED BELOW MAIN DECK FLOOR AT FS 1381, BETWEEN SEAT TRACKS 2 AND 3. REMOVED 1EA FINGER DOUBLER AND 2EA STIFFENERS BELOW MAIN CABIN FLOOR S TA 1381 CTR WING STRUCTURE OVER WING FUEL TANK. FABRICATED REPLACEM ENT PARTS AND INSTALLED REF STA, SA, EA 011-5110-01-A3245 AND EO MD11-5710-43415-A.

ATA 5313

INSPECTION TYPE:4C, CENTER CARGO COMPT L-43R SPLICE FITTING IS CRACKED AT CENTER ROW OF FASTENER HOLES STA 1531/5-123. REMOVED, FABRICATED AND INSTALLED L-43R SPLICE FITTING AT STA 1531/ 5-123 REF DWG A5A7114 AND SRM 51-33-01.

ATA 5313

INSPECTION TYPE:4C, CENTER CARGO COMPT L-51L SPLICE FITTING IS CRACKED AT AFT RADIUS STA 1 531/5-123. REMOVED, FABRICATED AND INSTALLED L-51L SPLICE FITTING AT STA 1531/5-1 23 REF A5A7114 AND SRM 51-33-01.

ATA 5313

INSPECTION TYPE:4C CENTER CARGO COMPT L-38L SPLICE FITTING IS CRACKED AT STA 1531/5- 123. REMOVED, FABRICATED AND INSTALLED L-38L SPLICE FITTING AT STA 1531/5-1 23 REF DWG A5A7114 AND SRM 51-33-01.

ATA 5313

INSPECTION TYPE:4C CENTER CARGO COMPT L-42L SPLICE FITTING IS CRACKED AT FWD FASTENER HOLE OF CENTER ROW STA 1531/5-123. REMOVED, FABRICATED AND INSTALLED L-42L SPLICE FITTING AT STA 1531/5- 123 REF DWG A5A7115-503 AND SRM 51-31-01.

ATA 5313

INSPECTION TYPE:4C, FS1219, LONGERON 27R ANGLE CRACKED. REMOVED, FABRICATED AND INSTALLED LONGERON FITTING AT FS 1219 AND AND L27R REF STA, SA EA 011-5340-01-A3236 REV I/R AND EO MD11- 5310-43444-A.

ATA 5310

INSPECTION TYPE:4C, R3 DOOR FWD JAMB LOWER LIGHTENING HOLE AFT LOWER CORNER STA 1256 IS CRACKED AS VEIWED FROM BACKSIDE WITH MIRROR. REPAIRED R-3 DOOR FORWARD JAMB LIGHTENING HOLE BY CRACK TERMINATION, FABRICATION AND INSTALLATION OF REPAIR DOUBLER REF SRM 53-40-15 FIG 201, REPAIR 3, REV 46.

ATA 5313

INSP TYPE:4C, FS1139 LONGERON 16R END FITTING CRACKED. REMOVED, FABRICATED AND INSTALLED SHOVEL END FITTING AT FS 1139 AND LONG 16R REF STA, SA EA 011-5340-01-A3236 AND EO MD11-5310-43444-A .

ATA 5313

INSPECTION TYPE:4C, FS 1139 AND LONGERON 18L END FITTING CRACKED. REMOVED DAMAGED FITTING, FABRICATED AND INSTALLED NEW REPLACEMENT FITTING REF STA, SA, EA 011-5340-01-A3232 REV I/R AND EO MD11-5310-43443-A.

ATA 5522

INSPECTION TYPE:4C, LT INBD ELEVATOR IS DELAMINATED AT OTBD SIDE FWD EDGE. REPAIRED LT INBD ELEVATOR DELAMINATION AT OTBD SIDE FWD EDGE REF STA, SA , EA 011-5530-01-A3254 REV. I/R AND EO MD11-5520-43478-A.

ATA 5230

INSPECTION TYPE:4C, LOWER AFT CARGO DOOR HAS A BLENDED DENT AT LOWER EDGE MID AREA. CUT OUT DAMAGE IN LOWER EDGE OF LOWER AFT CARGO DOOR AT YABCD=0.0 FABRICATED REPAIR PARTS AND INSTALLED REF STA, SA, EA 011-5231-01-A324 2 AND EO MD11-52-30-43469-A.

ATA 5753

INSPECTION TYPE:4C, LT WING INBD FLAP UPPER SURFACE T/E NEAR CENTER HAS 2EA DENTS. CUT OUT DAMAGED AREA, FABRICATED A REPAIR DOUBLER AND INSTALLED REF SRM 57-00-01, REPAIR 1.

ATA 5320

INSPECTION TYPE:4C, AVIONICS COMPT CABIN FLOOR STRUCTURE CRACKED ABOVE FLOORBEAM AT FS 421 AND LBL 42. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED FLOOR STRUCTURE REPAIR AT FS 421 AND LBL 42 REF STA, SA, EA 011-5320-01-A3230 I/R AND EO MD11-5320-43394-A.

ATA 5210

INSPECTION TYPE:4C, DURING OPS CHECK OF L-1 DOOR SLIDE DEPLOYMENT, LOWER DRIVE CHAIN BROKE AT MASTER LINK. R & R PNUEMATIC MOTOR DRIVE CHAIN IAW DWG ABA7941. OPS CHECK GOOD IAW AMM 52-11-02-2.

ATA 5730

INSPECTION TYPE:4C, LT WING L/E COMPT AT XOS630 CEILING DOUBLER IS CRACKED AT SEVERAL FASTENERS. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED AT LT WING LE/ XOS630 REF SRM 57-40-02, REPAIR 9, FIG 203.

ATA 5730

INSPECTION TYPE:4C LT WING LE COMPT. AT XOS654 APPX CEILING BEADED DOUBLER IS CRACKED AT 2EA. FASTENERS. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED REPAIR AT LT WING L/E XOS654 REF SRM 57-40-02, REPAIR 9, FIG 203.

ATA 5730

INSPECTION TYPE:4C LT WING L/E COMPT AT XOS619 APPX,CEILING BEADED DOUBLER IS CRACKED AT 2 EA FASTENERS. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED AT LT WING STA XOS619 REF SRM 57-40-02, REPAIR 9, FIG 203.

ATA 5730

INSPECTION TYPE:4C, LT WING L/E COMPT AT XOS 646 APPX CEILING BEADED DOUBLER IS CRACKED AT SEVERAL FASTENERS. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED AT LT WING L/E COMPT STA XOS646 REF SRM 57-40-02, REPAIR 9, FIG 203.

ATA 5730

INSPECTION TYPE:4C, LT WING L/E COMPT AT XOS742 APPX CEILING BEADED DOUBLER IS CRACKED AT FASTENER. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALL ON LT L/E COMPT XOS 733 REF 1 SRM 57-40-02, REPAIR 9, FIG 203.

ATA 5730

INSPECTION TYPE:4C, LT WING L/E COMPT AT XOS665 CEILING BEADED DOUBLER IS CRACKED AT SEVERAL FASTENERS LOCATED ABOVE PULLEY. REMOVED DAMAGE, FABRICATED PARTS AND INSTALLED AT LT WING L/E XOS665 REF SRM 57-40-02, REPAIR 9, FIG 203.

ATA 5730

INSPECTION TYPE:4C, LT WING L/E COMPT AT XOS638 APPX CEILING BEADED DOUBLER HAS CRACKS AT SEVERAL FASTENERS. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED REF SRM 57 -40-02, REPAIR 9, FIG 203.

ATA 5730

INSPECTION TYPE:4C, RT WING FIXED L/E SKIN IS CRACKED AT XOS774, NR 12 SLAT TRACK CUT-OUT. REPAIRED RT WING FIXED L/E REF SRM 57-40-02, REPAIR 7, FIG 201.

ATA 5330

INSPECTION TYPE:4C, REF D-454178 DENT AT LT STA 1823 BETWEEN L39L AND L40L REQUIRES PERMINENT REPAIR. CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED REF STA, SA, EA 011-5330-01-A3240 AND EO MD11-5330-43496-A.

ATA 5713

INSPECTION TYPE:4C, RT WING L/E STRINGER AT XOS 1100 HAS DRILL START. REPAIRED DRILL START ON RT WING L/E STRINGER AT XOS1100 REF STA, SA, EA 011-5710-01-A3216 REV I/R AND EO MD11-5710-43397-A.

ATA 5713

INSPECTION TYPE:4C, RT WING FIXED L/E STRINGER AT XOS 646 IS CRACKED. REMOVED, FABRICATED AND INSTALLED STRINGER DOUBLER AT XOS 646 REF DWG ARB2933, SRM 51-21-01 AND 51-35-01.

ATA 5753

DENT IN LOWER SKIN OF LT INBD FLAP 3.20 X 2.8 X .055 DEEP. APPLIED REPAIR DOUBLER IAW EO MD11-5750-41042.

ATA 2697

FIRE DET FAULT ON STATUS PAGE/MAINT INTERMITTENT ON/OFF THROUGHOUT FLIGHT. PERFORMED FDCU-2 FAULT REVIEW, SHOWED SEVERAL FLT LEGS "UPRIGHT FIRE DET ASSY A" AND "LOOP A FAULT". R & R HARNESS ASSY PER MM 71-50-04 AND TERMINAL BLOCK. NR 2 ENG FIRE DETECTION SYSTEM OPS CK NML PER MM 26-11-02. REQUIRED. M427874 ASSIGNED. PLACARD INSTALLED.

ATA 5245

RT AIR COND BAY DOOR HAS A HOLE APROX 2 INCH BY 1,5 INCH D427388. C/O TIME LIMITED REPAIR IAW EO MD11-5240-31630-B, APPENDIX A. ITEM DEF ERRED IAW EO MD11-5240-31630-B. DMI OPENED.

ATA 5245

INSP RT AIR COND BAY DOOR HAS A HOLE APPROX 2 INCH X 1.5 INCH D427388. DMI OPENED. C/O TIME LIMITED REPAIR IAW EO MD11-5240-31630-B APPENDIX A. ITEM DEF ERRED IAW EO MD11-5240-31630-B. PERMANENT REPAIR (IAW SRM VOL 1 52-10-00, FIG 1) OR REPLACEMENT AT OR ON BEFORE NEXT C CHECK.

ATA 5730

INSPECTION TYPE:1C, RT WING FIXED L/E SKIN PUNCTURED BETWEEN STA XOS437 & XOS443. FABRICATED & INSTALLED REPAIR REF SRM 57-40-02 FIG 201 REPAIR 4 SHEET 4.

ATA 5753

INSPECTION TYPE:1C, RT WING AT OTBD FLAP, FLAP VANE OTBD LOWER EDGE IS DAMAGED, HAS CHUNK OF MATERIAL BROKEN OFF. REMOVED DAMAGE AT RT OTBD FLAP VANE OTBD LOWER EDGE AND REPAIRED REF SRM 59-50-80 REPAIR 2 AND UPS RCD 395085.

ATA 5710

INSPECTION TYPE:1C, RT WING FIXED L/E COMPT UPPER SKIN WEB IS CRACKED AS MARKED BEHIND WHEEL CABLE XOS 652 TO STA XOS657 THRU ACCESS PANEL 619DB. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, AND ANGLES IAW SRM 57-40-02, REPAIR 9, FIG 203

ATA 5710

INSPECTION TYPE:1C, RT WING FIXED LE COMPT UPPER SKIN WEB IS CRACKED AS MARKED BET STA XOS 643 TO STA XOS 647 THRU ACCESS PANEL 619DB. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, AND ANGLES IAW MD-11 57-40-02 REPAIR 9, FIG. 203

ATA 5730

INSPECTION TYPE:1C, RT WING FIXED L/E COMPT UPPER SKIN WEB IS CRACKED AS MARKED BET. STA XOS637 TO STA XOS 643 THRU ACCESS PANEL 619CB. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, AND ANGLES IAW SRM 57-40-02, REPAIR 9, FIG. 203.

ATA 5710

INSPECTION TYPE:1C, RT WING FIXED L/E COMPT UPPER SKIN WEB IS CRACKED AS MARKED BET STA XOS 550 TO STA XOS 587 THRU ACCESS PANEL 618GB. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, AND ANGLES IAW SRM 57-40-02, REPAIR 9, FIG. 203

ATA 3240

AUTOBRAKES SYS INOP SHORTLY AFTER TOUCHDOWN. DEFERRED M419422. T/S IAW FRIM 32-40-10-00 BLOCKS 1,4, &3. ALL TESTS OK. PERFORMED RTS IAW FRIM 32-40-00-810-821 FIG 102 SHEETS 17-22. ALL TESTS OK. THIS CLEARS M419422. PLACARD REMOVED.

ATA 2841

TAIL L PUMP LO LEVEL 2 ALERT AT FL 300 2300LBS IN TAIL TANK -28'C. TAIL PUMPS LLO LEVEL 2 ALERT AT 150 200LBS FUEL IN TAIL -27'C. RAN CHECKLIST & ENG 2 FLAMED OUT. OPS TEST OF PUMP LOW PX SWITCHES PERFORMED IAW AMM TASK 28-44-01-700- 801. BOTH TAIL TANK TRANSFER PUMPS WORK NORMAL, NO LOW PX LIGHTS, MANIFOLD PX 28PSI. R&R TAIL TANK DENSITOMETER IAW MM 28-41-83-4.

ATA 2560

INSPECTION TYPE:N/A L1 DOOR SLIDE COVER HITS SIDE PANEL AND EMERGENCY HANDLE WHEN OPENING. RE-SECURED DOOR LINING. OK FOR SERVICE.

ATA 5311

INSPECTION TYPE:C REFERENCE TO NRC MD037457, TO CARRY OUT FRAME TRIM OFF TO FACILITATE REMOVAL OF CORRODED LONGERONS 52 AT STA 959-979. FRAME AT STA 1039 TRIM-OUT BETWEEN L52-L51R. HFEC INSPECTION C/O ON TRIM-OUT AREA, FOUND NO CRACK EVDNT. REPAIR LOWER FRAME DOUBLERS FABRICATED. REPAIR DOUBLER HEAT TREATED. REPAIR PARTS REPROTECTED AND PRIMER APPLIED. REPAIR DOUBLER AND FRAME INSTALLED. ITEM TRANSFERRED TO MPI CONTROL NUMBER P20503.

ATA 5313

INSPECTION TYPE:C LOWER FWD CARGO COMPT BILGE AREA AT STA 939, LONG 52, WHILE DOING AFT SIDE LONGERON REPAIR FOUND ANOTHER CORROSION. CORRODED LONG TRIM OFF. HFEC INSPECTION C/O ON TRIM OFF AREA, FOUND NO CRACK EVIDENT. REPAIR LONGERON AND LONGERON SPLICE FABRICATED. FPI C/O ON BOTH, FOUND NO CRACK EVIDENT. REPAIR LONGERON AND SPLICE REPROTECTED, PAINTED AND INSTALLED AS PER SRM 53-10-00 FIG 1, VOL I, REV 40. ITEM TRANSFERRED TO MPI CONTROL NR P20506.

ATA 5524

INSPECTION TYPE:C REPAIR SURVEY SEQUENCE NR 259-S2-001 RT HORZ STAB O/B ELEVATOR AFT O/B EDGE NEEDS REPAIRS VALIDATION. BASE UPON EO MD11-5100-30530-B SEQ 259-S2-001, REPAIR DOES NOT CORRELATE WITH MD11 SRM 51-61-01 VOL II, REV 40 & NO. MRCSSR ISSUED. EARN RAISED. EXISTING REPAIR DOUBLER REMOVED. RT HORZ STAB O/B ELEVATOR AFT O/B EDGE REPAIRED IAW EARN: N259UP-0021. HOLES PICKED-UP & FASTENERS INSTALLED. PAINT TOUCHED UP ON REWORKED AREA PER SRM 51-21-02 VI, R40.

ATA 5313

INSPECTION TYPE:C LOWER CTR CARGO COMPT BILGE AREA BETWEEN STA 5-11 AND STA 5-32, LONGERON 49R, LONGERON SPLICE FITTING FOUND WITH CRACKED AS MARKED. EXISTING REPAIR CRACKED SPLICE REMOVED. NEW SPLICE FITTING FABRICATED. FPI C/O ON NEW SPLICE FITTING, FOUND NO CRACK EVIDENT. NEW SPLICE REWORKED, WITH HOLES PICK-UP, REPROTECTED AND PAINTED. NEW SPLICE INSTALLED LONGERON ITEM TRANSFERRED TO MPI CONTROL NO: P20505.

ATA 5313

INSPECTION TYPE:C FWD CARGO LT LONGERON 48 AT STA 1119 - 6-10 FOUND SPLICE AND LONGERON CORRODED AS MARKED. SPLICE AND LONGERON FASTENERS REMOVED, BETWEEN STA 1099 TO 1119 LONGERON 48L TRIMMED OFF REMOVED. HFEC INSPECTION C/O ON TRIM OUT LONGERON, FOUND NO CRACK EVIDENT. REPAIR LONGERON AND SPLICE FABRICATED. FPI C/O ON FABRICATED PARTS (9EA) AND FOUND NO CRACK EVIDENT. REPAIR LONGERON INSTALLED. NEW SPLICE SUPPORT REWORKED WITH FPI C/O, FOUND NO CRACK EVIDENT. NEW SPLICE INSTALLED.

ATA 5313

INSPECTION TYPE:C LOWER CTR CARGO COMPT BILGE AREA BETWEEN STA 5-113 AND STA 1541, LONGER ON 50R, LONGERON SPLICE FITTING FOUND WITH CRACKED AS MARKED. EXISTING CRACKED SPLICE REMOVED, 1 EA NEW SPLICE P/N A5A7114-515 HOLES PICK-UP. NEW HOLES ON SPLICE REPROTECTED. NEW SPLICE PAINTED & INSTALLED AS PER DRAWING N5A6774 AND EN 1175-09.

ATA 5313

INSPECTION TYPE:C LOWER CTR CARGO COMPT BILGE AREA BETWEEN STA 5-113 AND STA 1541, LONGERON 49R, LONGERON SPLICE FITTING FOUND WITH CRACKED AS MARKED. EXISTING CRACKED SPLICE REMOVED. NEW SPLICE FABRICATED. FPI C/O ON NEW SPLICE & FOUND NO CRACK EVDNT. NEW SPLICE REWORKED WITH HOLES PICK-UP. NEW SPLICE REPROTECTED & PAINTED. NEW SPLICE INSTALLED AS PER DRAWING N5A6774.

ATA 5730

INSPECTION TYPE:C RT WING FIXED L/E AT STA XORS 1170 FOUND CHAFING MARK. CHAFE MARK REMOVED & REPROTECTED, FOUND OUT OF LIMIT. ORG MATL 0.060 INCH, REMOVED 0.022 INCH, REMAIN 0.038 INCH. FIXED L/E SKIN ON RT WING REMOVED. AFFECTED AREA TRIMMED OUT. REPAIR SKIN FAB PER EN1167-09. HEAT TREATMENT C/O ON REPAIR PART. WELDING C/O ON RT WING FIXED L/E SKIN WITH FPI C/O - NO CRACK EVDNT ON WELDED AREA. RT WING FIXED L/E SKIN INSTALLED PER EN1167-09.

ATA 5730

INSPECTION TYPE:C REPAIR SEQUENCE NUMBER 259-W4-005 NEEDS VALIDATION FOR REPAIR. REPAIR DOUBLER REMOVED AT RT WING I/B FIXED L/E TOP SURFACE AT STA XORS 130 REMOVED AS PER MD11 SRM. AS BASED ON COLLECTED INFO IN EO MD11-5100- 30530 DOES NOT CORRELATE WITH SRM 57-10-00 VOL I, FIG 24, REV 40. RT WING I/B FIXED L/E SURFACE, REPAIR SEQUENCE 259-W4-005 REPAIR DOUBLER REMOVED PER EN1151-09. REPAIR ANGLES 3EA FAB & HEAT-TREATED. CRACK AREA AT DOUBLER (INNER) TRIM OUT AS PER EN1151-09 AT RT WING STA XORS 130. HFEC INSP C/O, FOUND NO CRACK EVDNT. REPAIR FILLER, DOUBLER & EXT REPAIR DOUBLER FAB. REPAIR PARTS INSTALLED PER EN 1151-09.

ATA 5754

INSPECTION TYPE:C REPAIR SURVEY SEQUENCE 259-W3-001 LT WING NR 8 SLAT XOS 1179-1186 OUTER SKIN SURFACE. DOUBLER REPAIR NEEDS VALIDATION DUE TO NO SRM REPAIR. REPAIR DOUBLER REMOVED PER EN1158-09. HFEC C/O ON EXISTING TRIM OUT AREA, FOUND NO CRACK EVDNT, 10X INSP. C/O PER EN1158-09, SATIS, 1 EA REPAIR SKIN, 2 EA FILLERS, 2 EA SPLICES AND 1 EA STRAP FABRICATED PER EN1158-09. REPAIR PARTS HOLES PICKED UP, REPROTECTED & PAINTED PER EN1158-09. REPAIR PARTS INSTALLED PER EN1158-09.

ATA 5754

INSPECTION TYPE:C REPAIR SURVEY SEQUENCE NR 259-W3-003 LHW NR 3 SLAT INBD EDGE STA XOS 397-406 OUTER SKIN SURFACE. DOUBLER REPAIR NEEDS VALIDATION. REPAIR DOUBLER AT AFFECTED AREA REMOVED. HFEC C/O ON TRIMMED OUT AREA AND FOUND NO CRACK EVIDENT. 10X INSP C/O, FOUND SATISFACTORY NEW CLIP ANGLE, REPAIR FILLER (2EA), CUT-OUT FILLER, REPAIR DOUBLER AND TAPER GAP FILLER FABRICATED. HOLES PICK-UP, REPROTECTION AND PAINTING C/O ON REPAIR PARTS. REPAIR PARTS INSTALLED AS PER EN1156-09.

ATA 5730

INSPECTION TYPE:C REPAIR SEQUENCE NUMBER 259-W4-008 NEEDS VALIDATION FOR REPAIR. BASED UPON COLLECTED INFO IN EO MD11-5100-30530-B REPAIR SEQUENCE NUMBER 259-W4-008 DOES NOT CORRELATE WITH SRM 57-10-00 VOL I, FIG 21, R40. REPAIR DOUBLER AT RT WING NR 14 SLAT TRACK XOS 890 REMOVED. HFEC C/O ON EXISTING TRIM-OUT AREA, FOUND NO CRACK EVDNT, 10X INSP C/O, SATIS. REPAIR DOUBLER & FILLER FABRICATED & INSTALLED PER EN1155-09.

ATA 5754

INSPECTION TYPE:C REPAIR SURVEY SEQUENCE NR 259-W3-002 LHW NR 7 SLAT STA XOS 953-963 OUTER SKIN SURFACE DOUBLER REPAIR NEEDS VALIDATION. REPAIR DOUBLER AT AFFECTED AREA REMOVED. HFEC C/O ON TRIM OUT AREA AND FOUND NO CRACK EVIDENT 10X INSP C/O AND FOUND SATISFACTORY. EXTERNAL DOUBLER, BAFFLES AND 2 INTERNAL DOUBLERS FABRICATED. HOLES PICK-UP, REPAIR PARTS REPROTECTED AND PAINTED. REPAIR PARTS INSTALLED PER EN1157-09.

ATA 5313

INSPECTION TYPE:C FWD CARGO, LONGERON 52 AT STA 959-979 6 O'CLOCK POSITION FOUND CORROSION AND CRACKED AS MARKED. ATTACH CORROSION LONG FASTENERS AND AREA PARTS REMOVED STA 949 AND STA 10 29 LONG TRIM REMOVED. HFEC C/O ON TRIM OFF AREA, FOUND NO CRACK EVIDENT. REPAIR LONGERON AND 2 LONGERON SPLICE FAB AND FPI C/O ON BOTH. FOUND NO CRACK EVIDENT. REPAIR LONGERON AND 2 SPLICE INSTALLED PER SRM 53-10-00 FIG 1, VOL I, REV 40. ITEM TRANSFERRED TO MPI CONTROL NR P20504.

ATA 5330

INSPECTION TYPE:C LWR FX: ALONG BS 1531/5-123, ALONG LONGERON 47R, LOWER BELLY SKIN AREA BULGE OUT. CTR CARGO FLOOR PANELS 183BF & 183AB REMOVED. EXISTING LONGERON SPLICE FROM STA 5-113R TO 1541R (L46 & L47) REMOVED FOR ACCESS. DETAILED VISUAL INSP C/O WITH NO CORROSION FOUND. EXISTING LONGERON SPLICE AT L46RT & L47RT INSTALLED PER DRAWING N5A6774 & EN 1175-09.

ATA 5730

INSPECTION TYPE:C REPAIR SEQUENCE NUMBER 259-W4-007 NEEDS VALIDATION FOR REPAIR. REPAIR SEQ 25--W4-007 DOES NOT CORRELATE WITH MD11-SRM 57-43-01, FIG 1,VOL I, REV 40. REPAIR DOUBLER REMOVED PER EN1153-09 AT RT WING NR 1 SLAT TRACK AREA. HFEC C/O ON EXISTING TRIM OUT AREA, FOUND NO CRACK EVDNT. L 10X INSP C/O AT RT WING NR 1 SLAT TRACK DOOR AREA PER EN1153-09, 'SATIS'. REPAIR DOUBLER & FILLER FAB & INSTALLED PER EN1153-09.

ATA 5230

INSPECTION TYPE:C AFT CARGO DOOR, TOP FWD DOOR SURFACE FOUND EXISTING REPAIR DOES NOT CORRELATE WITH SRM. EXISTING REPAIR DOUBLER ON AFT CARGO DOOR EXTERIOR SKIN REMOVED. DISCREPANT DOOR SKIN TRIM OUT & REPROTECTED PER SRM 51-21-01 VIIR40. HFEC INSP C/O ON TRIM OUT AREA, NO CRACK EVDNT. REPAIR DOUBLER & FILLER FABRICATED, HOLES PICKED-UP & REPROTECTED. REPAIR DOUBLER & FILLER INSTALLED PER SRM 52-10-00,FIG 17, VI, R40.

ATA 5330

INSPECTION TYPE:C LT UPPER FUSELAGE AT STA 475-495, LONGERON 26L-27L FOUND EXISTING REPAIR DOES NOT CORRELATE SRM. EXISTING REPAIR DOUBLER REMOVED. HFEC C/O ON TRIM OUT AREA, FOUND NO CRACK EVIDENT TWO REPAIR DOUBLERS AND FINGER DOUBLER FAB, HOLE PICK-UP, REPROTECTED AND PAINTED. REPAIR PARTS INSTALLED AS PER SRM 53-20-00, FIG 2, VOL I, REV 40.

ATA 5330

INSPECTION TYPE:C CENTER WING TANK UPPER SKIN EXT SURFACE LT SIDE STA 1226.5 STRINGER 15 XCW +100 FOUND EXISTING REPAIR DOES NOT CORRELATE WITH SRM. EXISTING DOUBLER AT AFFECTED AREA REMOVED AND FPI C/O, FOUND NO CRACK AND NO CORROSION EVIDENT. OPEN HOLE HFEC INSP C/O ON REMOVED FASTENER HOLES AND FOUND NO CRACK EVIDENT. TWO ON-EDGE-MARGIN HOLES AT AFFECTED AREA TRIM OFF AND HFEC INSP C/O, FOUND NO CRACK EVIDENT. REPAIR DOUBLER AND FILLER FAB AND INSTALLED PER EN1144-09.

ATA 2810

INSPECTION TYPE:C CENTER WING TANK UPPER SKIN EXT SURFACE LT SIDE STA 1226.5 STRINGER 15 XCW +78 FOUND FUEL SEEPING UNDER DOUBLER. EXISTING DOUBLER REMOVED, 1 EA HOLE REAMED TO 0.309 INCH PER EN1144-09. FPI C/O AFFECTED AREA, FOUND NO CRACK EVDNT. OPEN HOLE HFEC INSP C/O ON REMOVED FASTENER HOLES & FOUND NO CRACK EVDNT.0.309 INCH HOLE TRIM OFF HFEC INSP C/O ON TRIM OFF AREA, FOUND NO CRACK EVDNT. REPAIR DOUBLER & FILLER FABRICATED. REPAIR PARTS INSTALLED AS PER EN1144-09.

ATA 5330

INSPECTION TYPE:C TRANSFERRED DEFECT FROM LOG PG NR 213837-1, REFER TO D382204. FUSELAGE SKIN DAMAGE ALONG AFT EDGE OF CTR CARGO DOOR OPENING, LOWER AFT DOOR. EXISTING REPAIR DOUBLER FROM STA 1781-1791 RT (L40-L42) REMOVED. DAMAGED SKIN TRIM-OUT AND REPROTECTED. HFEC C/O ON TRIM-OUT AREA, FOUND NO CRACK EVIDENT. REPAIR DOUBLER AND FILLER FABRICATED, WITH HOLES PICK-UP, REPROTECTION AND PAINTING C/O. REPAIR WASHERS FABRICATED AND INSTALLED TWO REPAIR DOUBLERS, TWO FILLERS INSTALLED. TRAP SHIM FAB AND INSTALLED.

ATA 5297

R1 DOOR INOP ELEC AND PNEUMATIC. DEFERRED IAW MEL 391975. REF WDM 52-11-01 FOUND UP LIMIT SWITCH 51-588 TO HAVE INTERMITTENT HIGH RESISTANCE FROM PINS E TO D. REPLACED 51-588. DOOR CHECKS GOOD.

ATA 5730

INSPECTION TYPE:N/A LT WINGLET UPPER T/E FAIRING DAMAGED. REPAIRED IAW EO MD11-5730-90798-B.

ATA 3350

INSPECTION TYPE:N/A EMERGENCY LIGHTS TEST INOP. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY RECHARGEABLE BATTERY PER MM 33-51-01-04, PERFORMED EMERGENCY LIGHTS TEST & OPS CHECK. FOUND SATIS PER MM 33-51-01-5. THIS CLOSES DMI & STICKER REMOVED.

ATA 2565

INSPECTION TYPE:N/A L1 DOOR EMERGENCY ESCAPE SLIDE COVER NOT SECURED FLUSH AND RUBBING WHEN DOOR OPENED. RESECURED L1 DOOR SLIDE COVER IAW MM 25-23-07-4-1.

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 33 LT BARREL NUT BORE HOLE, UPPER. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.164 BORE I.D. 1.162.

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 4 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M. BUSHING O.D. .946 BORE I.D. .944.

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 4 LT BARREL NUT BORE HOLE, (UPPER). REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER MD11-5510-19409-M. BUSHING O.D. .946 BORE I.D. .944.

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 31 LT BARREL NUT BORE HOLE, UPPER. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.132 BORE I.D. 1.130.

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 31 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.180 BORE I.D. 1.178.

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 28 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M. BUSHING O.D. 1.132 BORE I.D. 1.130.

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 28 LT BARREL NUT BORE HOLE, UPPER. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.164 BORE I.D. 1.162.

ATA 5512

INSPECTION TYPE:3C CORROSION FOUND ON NR 7 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M, BUSHING O.D. .976 BORE I.D. .974.

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 3 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. .976 BORE I.D. .974.

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 22 LEFT BARREL NUT BORE HOLE, UPPER HORIZ STAB. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M. BUSHING O.D. 1.069 BORE I.D. 1.067

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 19 LEFT BARREL NUT BORE HOLE, UPPER HORIZ STAB. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.069 BORE I.D. 1.067

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 16 LEFT BARREL NUT BORE HOLE, UPPER HORIZ STAB. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M, BUSHING O.D. 1.069 BORE I.D. 1.067

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 25 LEFT BARREL NUT BORE HOLE, UPPER. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.069 BORE I.D. 1.067

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 7 LEFT BARREL NUT BORE HOLE, UPPER HORIZ STAB. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. .946 BORE I.D. .944

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 3 LEFT BARREL NUT BORE HOLE, UPPER. REMOVED CORROSION, FABRICATED, AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M. BUSHING OD .946 BORE ID .944.

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 22 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M. BUSHING O.D. 1.037 BORE I.D. 1.035.

ATA 5512

INSPECTION TYPE:3C CORROSION FOUND ON NR 36 LT BARREL NUT BORE HOLE, UPPER. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 2.243 BORE I.D. 2.442.

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 35 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.132 BORE I.D. 1.130

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 1 RT BARREL NUT BORE HOLE, UPPER. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.505 BORE I.D. 1.503.

ATA 5512

INSPECTION TYPE:3C CORROSION FOUND ON NR 21 LEFT BARREL NUT BORE HOLE, UPPER HORIZ STAB. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.037 BORE I.D. 1.035.

ATA 5512

INSPECTION TYPE:3C CORROSION FOUND ON NR 15 LEFT BARREL NUT BORE HOLE, UPPER HORIZ STAB. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M, BUSHING O.D. 1.037 BORE I.D. 1.035.

ATA 5512

INSPECTION TYPE:3C CORROSION FOUND ON NR 15 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.037 BORE I.D. 1.035.

ATA 5512

INSPECTION TYPE:3C CORROSION FOUND ON NR 30 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M. BUSHING O.D. 1.132 BORE I.D. 1.130.

ATA 5512

INSPECTION TYPE:3C CORROSION FOUND ON NR 30 LT BARREL NUT BORE HOLE, UPPER. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.132 BORE I.D. 1.130.

ATA 5512

INSPECTION TYPE:3C CORROSION FOUND ON NR 24 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.037 BORE I.D. 1.035.

ATA 5512

INSPECTION TYPE:3C CORROSION FOUND ON NR 2 LEFT BARREL NUT BORE HOLE, (UPPER). REMOVED CORROSION, FABRICATED, AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M, BUSHING OD 1.069 BORE I.D. 1.035.

ATA 5512

INSPECTION TYPE:3C CORROSION FOUND ON NR 18 LEFT BARREL NUT BORE HOLE, UPPER HORIZ STAB. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M, BUSHING O.D. 1.037 BORE I.D. 1.035.

ATA 5512

INSPECTION TYPE:3C CORROSION FOUND ON NR 6 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. .946 BORE I.D. .944.

ATA 5512

INSPECTION TYPE:3C CORROSION FOUND ON NR 12 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. .946 BORE I.D. .944.

ATA 5512

INSPECTION TYPE:3C CORROSION FOUND ON NR 24 LEFT BARREL NUT BORE HOLE, UPPER. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.037 BORE I.D. 1.035.

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 27 RT (UPPER) BARREL NUT BORE HOLE AND BOTTOM SURFACE CORRODED THRU. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M. BUSHING O.D. 1.164 BORE I.D. 1.162.

ATA 5512

INSPECTION TYPE:3C CORROSION FOUND ON NR 12 LEFT BARREL NUT BORE HOLE, UPPER HORIZ STAB. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M, BUSHING O.D. .946 BORE I.D. .944.

ATA 5512

INSPECTION TYPE:3C CORROSION FOUND ON NR 18 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.037 BORE I.D. 1.035.

ATA 5512

INSPECTION TYPE:3C CORROSION FOUND ON NR 9 LEFT BARREL NUT BORE HOLE, UPPER HORIZ STAB. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M. BUSHING O.D. .945 I.D. .944

ATA 5512

INSPECTION TYPE:3C CORROSION FOUND ON NR 21 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M. BUSHING O.D. 1.037 BORE I.D. 1.035.

ATA 5512

INSPECTION TYPE:3C CORROSION FOUND ON NR 9 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. .946 BORE I.D. .944.

ATA 5512

INSPECTION TYPE:3C CORROSION FOUND ON NR 6 LEFT BARREL NUT BORE HOLE, UPPER. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. .946 BORE I.D. .944.

ATA 5512

INSPECTION TYPE:3C CORROSION FOUND ON NR 35 LT BARREL NUT BORE HOLE, UPPER. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.180 BORE I.D. 1.178.

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 20 LT BARREL NUT BORE HOLE, UPPER HORIZ STAB. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.037 BORE I.D. 1.035.

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 32 LT BARREL NUT BORE HOLE, UPPER. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.132 BORE I.D. 1.130.

ATA 5512

INSPECTION TYPE:3C CORROSION FOUND ON NR 26 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.037 BORE I.D. 1.035.

ATA 5512

INSPECTION TYPE:3C CORROSION FOUND ON NR 23 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M BUSHING O.D. 1.037 BORE I.D. 1.035

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 11 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M. BUSHING O.D. .946 BORE I.D. .944.

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 8 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. .946 BORE I.D. .944.

ATA 5512

INSPECTION TYPE:3C CORROSION FOUND ON NR 11 LEFT BARREL NUT BORE HOLE, UPPER HORIZ STAB. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M, BUSHING O.D. .946 BORE I.D. .944

ATA 5512

INSPECTION TYPE:3C CORROSION FOUND ON NR 8 LEFT BARREL NUT BORE HOLE, UPPER HORIZ STAB. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M, BUSHING O.D. .946 BORE I.D. .944.

ATA 5512

INSPECTION TYPE:3C CORROSION FOUND IN NR 14 RT (UPPER) BARREL NUT BORE HOLE AND ON BOTTOM SURFACE OF RADIUS. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5110-19409-M, BUSHING O.D. .976 BORE I.D. .974.

ATA 5512

INSPECTION TYPE:3C CORROSION FOUND IN NR 5 LEFT BARREL NUT BORE HOLE, UPPER. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M. BUSHING O.D. .990 BORE I.D. .988.

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 17 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.069 BORE I.D. 1.067.

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 32 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M. BUSHING O.D. 1.132 BORE I.D. 1.130

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 36 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M. BUSHING O.D. 2.5735 BORE I.D. 2.572.

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 5 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M, BUSHING O.D .946 BORE I.D. .944.

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 20 RT (UPPER) BARREL NUT HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.037 BORE I.D. 1.035.

ATA 5512

INSPECTION TYPE:3C CORROSION ON NR 14 LEFT BARREL NUT BORE HOLE, UPPER HORIZ STAB. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M, BUSHING O.D. .9755 BORE I.D. .974.

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 29 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M. BUSHING O.D. 1.164 BORE I.D. 1.162.

ATA 5512

INSPECTION TYPE:3C FOUND CORROSION ON NR 2 RT BARREL NUT BORE HOLE, UPPER. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.077 BORE I.D. 1.075.

ATA 5720

INSPECTION TYPE:1C LEFT WING L/E COMPARTMENT XORS 683 HAS STRAP CRACKED. REMOVED STRAP, FABRICATED AND INSTALLED REPLACEMENT STRAP IAW DWG ARB3954 & SRM 51-33-01.

ATA 5720

INSPECTION TYPE:1C LEFT WING LE COMPARTMENT XORS 580 HAS STRAP CRACKED. REMOVED, FABRICATED, AND INSTALLED STRAP IAW MD-11 SRM 51-33-01, MD-11 SRM 51-21-01, AND DWG: ARB3954.

ATA 5730

INSPECTION TYPE:1C RIGHT LE NR 14 SLAT TRACK CUT OUT CRACKED ON LWR O/B CORNER, CUTOUT DAMAGE. FABRICATED DOUBLER AND INSTALLED DOUBLER IAW MD-11 SRM 57-10-00 FIG 21.

ATA 5754

INSPECTION TYPE:1C RT WING TELESCOPING DUCT CUT CRACK IN UPPER CORNERS. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER & FILLERS IAW MD-11 SRM 57-10-00.

ATA 5754

INSPECTION TYPE:1C RIGHT WING L/E NR 1 SLAT TRACK CUTOUT HAS DOUBLER CHAFED. REMOVED REPAIR DOUBLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER IAW MD-11 SRM 57-10-00, 51-21-01, 51-33-01 AND 51-35-01.

ATA 5720

INSPECTION TYPE:1C RIGHT L/E ACCESS PNL MATING SURFACE AFT OF NR 9 SLAT TRACK CRACKED. REMOVED CRACKED SUPPORT ANGLE, FABRICATED AND INSTALLED REPLACEMENT SUPPORT ANGLE IAW MD-11 SRM 51-10-00, 51-21-01, 51-35-01 AND DPS 1.05-3.

ATA 5720

INSPECTION TYPE:1C LEFT WING ACCESS PNL LANDING XORS 540 CRACKED. REMOVED SUPPORT ANGLE, FABRICATED AND INSTALLED REPLACEMENT SUPPORT ANGLE IAW DWG ARB2933 AND MD-11 SRM 51-33-01 & 51-35-01.

ATA 5751

INSPECTION TYPE:3C RT WING IB AILERON UPPER SURFACE AT OB VERY LE HAS 5 INCH LONG DEEP GOUGE RUNNING THRU REPAIR DOUBLER. REMOVED PREVIOUS REPAIR DOUBLER AND FILLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER PER MD-11 SRM 57-00-01 AND 51-35-01.

ATA 5511

INSPECTION TYPE:1C CORROSION FOUND IN HORIZONTAL STAB LT UPPER FWD SPAR CAP BARREL NUT HOLE NR 1. REMOVED CORROSION FROM ABOVE AREA AND REPAIRED PER EA 011-5510-01 -A1297.

ATA 2565

INSPECTION TYPE:N/A CREW PREFLIGHT - RIGHT (R1) DOOR SLIDE LOW PRESSURE. REMOVED AND REPLACED R1 DOOR SLIDE. REF MM 25-61-15-4.

ATA 5610

CAPTAIN'S WINDOW WILL NOT OPEN ALL THE WAY. SUNSHADE INTERFERES. RESECURED VISOR. WINDOW OPS CK OK.

ATA 2432

INSPECTION TYPE:N/A DIVERSION - BATTERY CHARGER LIGHT ILLUMINATED IN FLIGHT. T/S PER FIM 24-30-00 FIG 118. REPLACED BATTERIES PER MM 24-30-02 AND BATTERY CHARGER PER MM 24-34-03. EMERGENCY POWER TEST OK PER MM 24-24-00-5, NO MSG NOTED.

ATA 5313

INSPECTION TYPE:CK-C FWD CARGO STA 6-70 LONGERON R49 FOUND WITH CORROSION DURING CARRY OUT WORK ON ADJACENT AREA. CORRODED LONGERON R49 STA 6-70 REPAIRED AS PER SRM 53-10-00 FIG 2 VOL I REV 38.

ATA 5753

INSPECTION TYPE:C RIGHT WING O/B FLAP I/B HINGE (FLAP SIDE) I/B PIVOT PIN ATTACHMENT HOLE SPOT FACE FOUND CORRODED. RIGHT WING AFT O/B FLAP I/B HINGE PIVOT I/B BORE BUSHING & SPOTFACE CORROSION REMOVED & FOUND EXCESS LIMIT AS PER CMM 57-52-04 PG 621-22 REV.57. FPI CARRIED OUT IAW DAC NDT 8PM R.13 PART 8 REWORKED AREA & FOUND NO CRACK & CORROSION EVIDENT. MPI CARRIED OUT PER DPS4.704 REV. AN ON FAB BUSHING NO CRACK EVIDENT. BUSHING INSTALLED AS PER EN 1208-07.

ATA 5313

INSPECTION TYPE:C FWD CARGO BILGE AREA STA 1119 LONGERON 52 FOUND WITH CORROSION. FWD CARGO LONG 52 STA 1119 AREA SPLICE REMOVED & LONG 52 STA 1109 TO STA 6-0 6 AREA FASTENERS REMOVED. FWD CARGO LONG 52 DAMAGED AREA TRIMMED. HFEC INSP CARRIED OUT, NO CRACK EVIDENT. LONG REPAIR SECTION & SPLICE FAB. FPI CARRIED ON FAB LONG & SPLICE NO CRACK EVIDENT. REPAIR SECTION & SPLICE PAINTED. LONG REPAIR SECTION & SPLICE INSTALLED PER SRM 51-31-01 VOL II REV 38.

ATA 5313

INSPECTION TYPE:CK-C FWD CARGO BILGE AREA STA 6-06 LONGERON L41 FOUND WITH CORROSION AS MARKED. FWD CARGO BILGE AREA STA 6-06 LONGERON L41 DAMAGED AREA REPAIRED AS PER SRM 53-10-00 FIG 2 VOL I REV 38.

ATA 5313

INSPECTION TYPE:C FWD CARGO BILGE AREA LONGERON L48 FOUND WITH CORROSION AS MARKED. FWD CARGO STA 815 LONG L48 REMOVE AND FOUND OVER LIMITS PER SRM 53-00-01 FIG 3 V.I R.38. HFEC CARRIED OUT PER DAC NDTSPM R.13 PART6 06-10-01.001/011. FOUND NO CORROSION CRACK. REPAIR ANGLES FAB PER EN1146-07. FPI CARRIED OUT PER DPS 4.707 REV AW AND FOUND NO CRACK EVIDENT. REP ANGLES AND SHIM AT FWD CARGO STA 815 LONG L48. INSTALLED PER SRM 51-31-01 V.II R.38.

ATA 5313

INSPECTION TYPE:C AFT CARGO STA 1967 LONGERON R40 FOUND WITH CORROSION AS MARKED. AFT CARGO LONGERON R40 STA 1958-1980 DAMAGED AREA CUT & REMOVED. HFEC INSP CARRIED OUT & NO CRACK EVIDENT. LONGERON & SPLICE FAB. FPI CARRIED ON FAB LONGERON & SPLICE, FOUND NO CRACK. LONGERON & SPLICE FASTENER HOLE PICK UP. NEW LONGERON & SP SPLICE REPROTECTED. NEW LONGERON, SPLICE, FRAME & SHEAR CLIP INSTALLED PER SRM 53-10-00 FIG 1&2 VOL I REV 38 & SRM 51-31-01 VOL II REV 38.

ATA 5313

INSPECTION TYPE:C CTR CARGO STA 5-113, LONGERON L40 FOUND WITH CORROSION AS MARKED. CTR CARGO STA 5-113 LONG L40 SPLICE & CORROSION LONGERON CUT OFF PER SRM 51-33-01 V2 R38. REP LONG & SPLICE FAB PER SRM 53-10-00 FIG 2 V1 R38. FPI CUT OUT PER DPS 4.707 ON FAB LONG & SPLICE FOUND NO CRACK EVIDENT ALL REPAIR PARTS REPROTECTED PER SRM 51-21-01 V2 R 38. OK TO INSTALL. REPAIR LONG & SPLICE INSTALLED PER SRM 53-10-00 V1 R38.

ATA 5313

INSPECTION TYPE:C CTR CARGO, STA 1540 LONGERON L45 FOUND WITH CORROSION AS MARKED. THE A/M LONGERON L45 STA 1540 AREA OPENED UP FOR REPAIR PER SRM 51-31-0 1 V2 R38. S/BUSHING REMOVED PER EN 1148-07 FOR EXISTING REPAIR ON L45. LONGERON & SPLICE FAB PER SRM 53-10-00 V1 F2 R38. FPI CUT OUT ON FAB LONGERON & SPLICE FOUND NO CRACK EVIDENT. S/BUSHING FAB PER EN1148-07. OK TO INSTALL. REPAIRED S/BUSHING INSTALLED PER EN1148-07, FOUND SATIS.

ATA 5313

INSPECTION TYPE:C CTR CARGO LT TUNNEL AREA, STA 5-118 THRU STA 5-73 FOUND CORROSION ON LONGERON L38 AS MARKED. LT LONG L38 STA 5-73 THRU 5-118 SKIN REMOVED FOR ACCESS PER SRM 51-31- 01 VOL II. REPAIR LONG SECTION & REPAIR SPLICE FAB PER DOUGLAS DWG A5A 7046 & SRM 53-10-00 V2 R38. FPI CUT OUT PER DPS4.707 FOUND NO CRACK EVIDENT. REP LONG & SPLICE REPROTECTED PER SRM 51-21-01 V2 R38. OK TO INSTALL. REP LONG & SPLICE INSTALLED PER SRM 51-31-01 V2 R38.

ATA 5313

INSPECTION TYPE:C CTR CRGO, RT TUNNEL AREA, STA 5-53 THROUGH STA 1541 LONGERON R37 FOUND WITH CORROSION AT SEVERAL LOCATIONS AS MARKED. CTR CARGO RT STA 5-53-5-113 SKIN AND LONGERON R37 REMOVED PER SRM51-31-01 V.II R.38. LONGERON REWORKED PER DOUGLAS DWG A5A7022. FPI CARRIED OUT PER DPS 4.707 REV AW FOUND NO CRACK EVIDENT. LONGERON R37 FASTENER HOLES PICKED UP PER SRM 51-31-01 V.II R.38.CTR CGO RT STA 5-53 TO 5-113 SKIN AND NEW LONGERON R37. INSTALLED PER SRM 51-31-01 V.II R.38.

ATA 5753

INSPECTION TYPE:C RIGHT OUTBOARD FLAP, FLAP VANE SUPPORT FITTINGS FOUND WITH CORROSION AT INTERIOR OF LIGHTENING HOLES AS MARKED. RIGHT O/B FLAP VANE REMOVED AS PER AMM 27-50-32 R.55. SEND TO SHOP FOR REPAIR. RIGHT O/B FLAP INSTALLED PER AMM 27-50-32 R 55. OPERATIONAL CHECK CARRIED OUT AS PER AMM 27-50-00 R 55.

ATA 5753

INSPECTION TYPE:C LEFT OUTBOARD FLAP, FLAP VANE SUPPORT FITTINGS FOUND WITH CORROSION AT INTERIOR OF LIGHTENING HOLES AS MARKED. LEFT O/B FLAP VANE REMOVED AS PER AMM 27-50-32 R 55. SEND TO SHOP FOR REPAIR. LEFT O/B FLAP VANE INSTALLED AS PER AMM 27-50-32 R55. OPERATIONAL AND TEST CARRIED OUT AS PER AMM 27-50-00 REV 55.

ATA 5347

INSPECTION TYPE:C CABIN: LEFT SEAT TRACK AT STA 1961, X=107.25 FOUND CORRODED AS MARKED. FASTENERS AT CABIN SEAT TRACK REMOVED SRM 51-31-01 VOL II. DAMAGED AREA TRIMMED OFF SRM 53-70-00 FIG 1 VOL I. HFEC INSP CARRIED OUT & NO CRACK EVIDENT. HOLES ON NEW SEAT TRACK PICKED UP SRM 51-31-01 VOL II. SPLICE PARTS FAB, HOLES ON SPLICE PARTS PICKED UP, SPLICE PARTS PROTECTED & PAINTED. SPLICE PARTS & SEAT TRACK INSTALLED SRM 51-31-01 VOL II REV 38.

ATA 5753

INSPECTION TYPE:C RIGHT WING O/B FLAP MID STOP FITTING FOUND WITH CRACK AS MARKED. RIGHT WING O/B FLAP I/B & O/B HINGE ASSY, SIDE CARRIAGE & FLAP VANE TRACK REMOVED AS PER CMM 57-52-04 R.57. SEND OUT FOR REPAIR. RIGHT WING O/B FLAP VANE TRACK, SIDE CARRIAGE & I/B & O/B HINGE ASSY INSTALLED AS PER CMM 57-52-04 R.57. I/B & O/B HINGE FAIRING SUPPORTS INSTALLED AS PER SRM 51-31-01 V.II R.38. ADJUSTMENT & TEST CARRIED OUT PER AMM 27-50-00 R.55.

ATA 5753

INSPECTION TYPE:C LT WING O/B FLAP MID STOP FITTING FOUND WITH CRACK AS MARKED. LHW O/B FLAP I/B AND O/B HINGE ASSY, CARRIAGE, VANE TRACK AND HINGE FAIRING SUPPORT REMOVED PER CMM 57-52-04 R.57 AND SRM 51-31-01 V.II R.38 SEND OUT FOR REPAIR. LHW OB FLAP IB AND OB HINGE ASSY, VANE TRACK AND HINGE FAIRING SUPPORT INSTALLED PER CMM 57-52-04 R.57 AND SRM 51-31-01 V.II R. FUNCTIONAL CHK AND RIGGING CARRIED OUT PER AMM 27-50-00 R.55.