N285UP

Part: BOOT — MISSING (DOOR SWITCH) · airframe 104,920 hrs · 20,693 cycles

INSPECTION TYPE:NAL1 ENTRY DOOR SWITCH ENVIROMENTAL BOOT MISSINGINSTLLED ENVIROMENT SWITCH BOOT REF AMM 20-50-02

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 104,896 hrs · 20,673 cycles

EMERGENCY LIGHT TEST WILL NOT TEST PASS. R & R EMERGENCY POWER SUPPLY BATTERY IAW AMM 33-51-01. REV DMP 33-50-04. OPS CHECK NORMAL. ORIG SUB DATE: 11/1/2022

Part: SOLENOID — INOPERATIVE (L1 DOOR) · airframe 104,781 hrs · 20,622 cycles

L1 ENTRY DOOR ELECTRICALLY INOP INTERMITTENTLY. STOPS APPROXIMATELY ONE FOOT FROM FULL OPEN POSITION WILL NOT OPEN OR CLOSE ELECTRONICALLY FROM THERE. R&R L1 DOOR SOLENOID IAW AMM 52-10-06. OPS CHECKS GOOD. ORIGINAL SUBMISSION DATE: 10/7/2022

Part: CONNECTOR — LOOSE (L1 DOOR) · airframe 104,752 hrs · 20,601 cycles

L1 DOOR INOPERATIVE. FOUND LOOSE CONNECTION TO LOCK PIN RELEASE SOLENOID. RESECURED CONNECTION. OPERATED L1 DOOR SEVERAL TIMES NO FAULTS. REF AMM 52-10-06. THIS CLEARS M791806. PLACARD REMOVED. ORIG SUB DATE: 9/26/2022

Part: PANEL — CRACKED (COURIER AREA) · airframe 104,278 hrs · 20,341 cycles

INSPECTION TYPE:3CRCB WALL P/N WSP0798-505 HAS A CRACK INSIDE AT POSITION 4.REPLACED THE RCB WALL P/N WSP0798-505 IAW MD11 AMM 25-59-13-400-801 (MINOR)

Part: FLOOR PANEL — CORRODED (RCB FLOOR PANEL) · airframe 104,278 hrs · 20,341 cycles

INSPECTION TYPE:3CRCB FLOOR PANEL P/N WSP0786-501 HAS CORROSION AT BETWEEN STA Y=475.0 - Y=503.175 AND X=-17.500 - X=-27.500.REMOVED, REPLACED CORRODED FLOOR PANEL P/N WSP0786-501 IAW DWG WSP0786 AND MD11 SRM 51-31-01. (MINOR)

Part: CHANNEL — CRACKED (VERT. STAB) · airframe 104,278 hrs · 20,341 cycles

INSPECTION TYPE:3CLOWER VERTICAL STAB UNDER PICKLE BARREL SUPPORT ANGLE IS CRACKED AT BOTH END.REMOVED, FABRICATED AND REPLACED ANGLE/CHANNEL IAW DWG. AJC7372 AND SRM 51-35-01. (MINOR)

Part: RUDDER — CORRODED (UPPER RUDDER) · airframe 104,278 hrs · 20,341 cycles

INSPECTION TYPE:3CUPPER AFT RUDDER P/N NMC6019-505 EXTERNAL L/H SKIN HAS CORROSION.REPLACED UPPER AFT RUDDER P/N NMC6019-505 IAW MD11 AMM 27-20-30-400-801 (MINOR)

Part: NONE — CRACKED (MAIN CABIN) · airframe 104,278 hrs · 20,341 cycles

INSPECTION TYPE:3CLONG. 27R TRUSS FITTING IS CRACKED AT STA. 1159.REMOVED, FABRICATED AND REPLACED FITTING IAW DWG. AFA7605 AND SRM 51-33-01. (MINOR)

Part: DOUBLER — CRACKED (L/H WING L/E) · airframe 104,278 hrs · 20,341 cycles

INSPECTION TYPE:3CL/H WING FIXED L/E HAS A BEADED DOUBLER P/N ARB2894-1 THAT IS CRACK AT STA XOS=768 - XOS=772.REMOVED,FAB,REPLACED THE CRACKED BEADED DOUBLER P/N ARB2894-1 ON THE L/H WING FIXED L/E AT STA XOS=768 - XOS=772. IAW DWG ARB2894 AND MD11 SRM 57-40-02 REPAIR 15 FIGURE 205 REV.68.01 (MAJOR)

Part: NONE — CRACKED (AFT CARGO) · airframe 104,278 hrs · 20,341 cycles

INSPECTION TYPE:3CAFT CARGO VERTICAL STIFFNER IS CRACKED AT STA. 1841 AND LONG. 49R.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. AGA7170 AND SRM 51-31-01. (MINOR)

Part: NONE — CRACKED (AFT CARGO) · airframe 104,278 hrs · 20,341 cycles

INSPECTION TYPE:3CAFT CARGO VERTICAL STIFFNER IS CRACKED AT STA. 1841 AND LONG. 46R.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. 7170 AND SRM 51-33-01. (MINOR)

Part: BEAM — CRACKED (MAIN CABIN) · airframe 104,278 hrs · 20,341 cycles

INSPECTION TYPE:1CMAIN CABIN R-3 DOOR PLUG HORIZONTAL BEAM CRACK.REPAIRED R-3 DOOR HORIZONTAL BEAM IAW VT-SAA EA 011-5210-01-A9537 REV I/R AND UPS EO MD11-5210-83427-A BY P.LAU (AR-830967) DATED 04/19/2022 (MAJOR).

Part: STIFFENER — CRACKED (AFT CARGO) · airframe 104,278 hrs · 20,341 cycles

INSPECTION TYPE:3CAFT CARGO AT STA 1841 FLOOR BEAM HAS A VERTICAL STIFFENER THAT IS CRACKED.REMOVED, FAB AND REPLACED THE CRACKED STIFFENER IAW DWG AGA7170 AND MD11 SRM 51-31-01, SRM 51-33-01 (MINOR)

Part: BEAM — CRACKED (L3 DOOR) · airframe 104,278 hrs · 20,341 cycles

INSPECTION TYPE:3CL3 DOOR PLUG HAS A BEAM THAT IS CRACKED AT STA Y=838 X=-116.095 AND Z=9.702.REMOVED, REPLACED CRACKED BEAM IAW SRM 51-33-01 AND 51-35-01, (MINOR)

Part: TEE FITTING — CRACKED (CENTER TANK) · airframe 104,278 hrs · 20,341 cycles

INSPECTION TYPE:3CCENTER AUX TANK FWD. SPAR FITTING BETWEEN STA. X=46 & X=81 IS CRACKED.REMOVED, FABRICATED AND REPLACED FITTING IAW DWG. APB7351 AND SRM 51-31-01. (MINOR)

Part: SLAT TRACK — CRACKED (LT WING L/E) · airframe 104,278 hrs · 20,341 cycles

INSPECTION TYPE:1CLT WING FRONT SPAR CAN ASSY. CRACK AT STA. XOS 717/SLAT #5 SLAT TRACK #11.REPAIRED CRACKED CAN ASSY. IAW VT-SAA EA 011-5720-01-A9547 REV I/R AND UPS EO MD11-5720-83528-A (MINOR).

Part: NONE — CRACKED (AFT CARGO) · airframe 104,278 hrs · 20,341 cycles

INSPECTION TYPE:3CAFT CARGO VERTICAL STIFFNER IS CRACKED AT STA. 1841 AND LONG. 48R.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. 7170 AND SRM 51-33-01. (MINOR)

Part: NONE — CRACKED (AFT CARGO) · airframe 104,278 hrs · 20,341 cycles

INSPECTION TYPE:3CAFT CARGO VERTICAL STIFFNER IS CRACKED AT STA. 1841 AND LONG. 49L.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. 7170 AND SRM 51-33-01. (MINOR)

Part: FRAME — GOUGED (CENTER GEAR DOOR) · airframe 104,278 hrs · 20,341 cycles

INSPECTION TYPE:1CCENTER LANDING RH FWD DOOR GOUGE AT FWD FRAME(PAN).REMOVED AND REPLACED GOUGED FRAME IAW SRM 51-31-01 AND 51-33-01 (MINOR).

Part: STIFFENER — CRACKED (L/H WHEEL WELL) · airframe 104,278 hrs · 20,341 cycles

INSPECTION TYPE:3CL/H MLG WHEEL WELL HAS A STIFFENER THAT IS CRACK AT AFT O/B WEB.REMOVED, FAB, AND REPLACED THE CRACK STIFFENER IAW DWG ANB7203, MD11 SRM 51-31-01 AND 51-35-01. (MINOR)

Part: FLOOR PANEL — CORRODED (RCB FLOOR PANEL) · airframe 104,278 hrs · 20,341 cycles

INSPECTION TYPE:3CMAIN CABIN FLOOR PANEL WSP0785-501 HAS CORROSION BETWEEN STA Y=475.000 - Y=503.175 AND X=-27.500 - X=-36.000.REMOVED, REPLACED THE CORRODED FLOOR PANEL P/N WSP0785-501 IAW DWG WSP0785 AND MD11 SRM 51-31-01. (MINOR)

Part: WARNING MESSAGE — VIBRATION (NR 2 ENGINE) · airframe 104,107 hrs · 20,248 cycles

INSPECTION TYPE:NA**ATB** **EMERGENCY DECLARED** AFTER T/O RECIEVED ENG 2 VIBRATION HI, REVERSER UNLOCK MESSAGE AND SIGNIFICANT FEEDBACK VIBRATION IN THE RUDDER PEDALS ENG 2 VIBRATION WAS OBSERVED TO BE AT LEAST 4.32 EMERGENCY DECLARED RETURNED TO LOUISVILLE, LANDED WITHOUT INCIDENTINSPECTED ENGINE PER MM 72 00 05 200 869 AND FOUND NO DEFECTS REPLACED FAN CASE ACCELEROMETER AND HARNESS PER MM 77 32 03 401 PERFORMED ENGINE VIBRATION SURVEY PER MM 71 02 08 700 875 AND VIBRATION WELL WITHIN LIMITS PER MM 71 00 00 800 820.

Part: ENGINE — VIBRATION (NR 2) · airframe 104,106 hrs · 20,247 cycles

INSPECTION TYPE:N/A*ATB SDR FILED OPEN*EMERG DECL'D* A/C LANDED W/OUT INCIDENT* A/C OOS* T/O REC'D ENG 2 VIBRATION HI, REVERSER UNLOCK MSG, & SIGNIFICANT FEEDBACK VIBRATION IN THE RUDDER PEDALS. ENG 2 VIBRATION WAS OBSERVED TO BE AT 4.2. EMERGENCY DECLARED, RETURNED TO LOUISVILLE, LANDED WITHOUT INCIDENT. INSPECTED ENGINE PER MM 72-11-05-200-869 & FOUND NO DEFECTS REPLACED FAN CASE ACCELERROMETER & HARNESS PER MM 77-32-03-401. PERFORMED ENGINE VIBRATION SURVEY PER MM 71-02-08-700-875 & VIBRATION WELL WITHIN LIMITS PER MM 71-00-00-800-820.

Part: SWITCH — INOPERATIVE (L1 DOOR) · airframe 103,300 hrs · 19,855 cycles

L1 ENTRY DOOR INTERIOR & EXTERIOR SWITCHES INOP. L1 DOOR INOP IAW 52-10-3-1-2-1 PLACARDS INSTALLED.R/R'D L1 SOLENOID PER AMM 52-10-06-401. OPS CHECK NML. NO DEFECTS NOTED. M749325 CLEARED. PLACARD REMOVED.

Part: DOOR — STUCK (FWD LEFT) · airframe 103,272 hrs · 19,845 cycles

INSPECTION TYPE:NAFORWARD CABIN DOOR (L) STUCK IN HALF OPEN POSITIONCYCLED CIRCUIT BREAKERS AND PERFROMED OPS CHECK PER AMM 52 10 01 700 801 OPS CHECK GOOD

Part: SWITCH — BROKEN (L1 DOOR) · airframe 103,232 hrs · 19,825 cycles

L1 DOOR BROKEN SWITCH INOP. CLOSED L1 DOOR MANUALY IAW MD11 AMM 52-11-02-410-806, VERIFIED DOOR FULLY DOWN,CLOSED,SLIDE/RAIL IS ARMED AND OUTSIDE HANDLE IS FLUSH.PLACED L1 DOOR ON MET #52-10-1-2-0-1, PLACED INOP DO NOT USE PLACARD ON OUTSIDE HANDLE AND INSIDE SWITCH.DMP 52-10-1-2-0-1 COMPLIED WITH.REPLACED L-1 PAX DOOR CONTROL RELAY (R2-177) IAW MD11 WM 52-11-01. OPS CK PER AMM 52-11-00. M747828 CLEARED, DMP REVERSED, PLACARD REMOVED IPC: 52-34-01-05-855.

Part: SHUTOFF VALVE — OUT OF TOLERANCE (STAB TRIM) · airframe 103,174 hrs · 19,805 cycles

INSPECTION TYPE:NA**ATB-NO EMERG DECL'D-NO EQUIP USED-LANDED UNEVENTFULLY**STAB OUT OF TRIM LEVEL 2 ALERT UPON AUTOPILOT ENGAGEMENT. RAN CHECKLIST AND CAUTION REMAINED. A/P 2 WILL STAY ENGAGED. ATTEMPTED AP 1 ENGAGEMENT WHICH RESULTS IN IMMEDIATE DISCONNECT WITH PITCH UP MOMENT.C/O T/S IAW FIM 22-00-00-810-801 AND T-17427, FOUND LIB ELEV ACT S/O VLV (S2-729) OUT OF RANGE. R/R SAME IAW AMM 27-30-00-830-801. ADDITIONALLY FOUND LOB ELEV IND 1 UNIT TOO HIGH. RIGGED IAW AMM 27-30-00-830-801, OPS CHK SATIS. C/O AFS LAND IAW AMM 22-00-02-700-801 ON BOTH FCC'S. ALL TEST PASS.

Part: AOA — FAULTED (NR 2 RIGHT) · airframe 103,163 hrs · 19,802 cycles

ATB-NO EMERG DECL'D/NO EQUIP USED-LANDED UNEVENTFULLY. STAB OUT OF TRIM LEVEL 2 UPON AUTOPILOT ENGAGEMENT PASSING 1000FT, RAN LEVEL 2 CHECKLIST WITH NORMAL MANUAL TRIM MOVEMENTS. HOWEVER LIGHT RETURNED WITH EITHER AUTOPILOT ENGAGED. LEFT OUTER STAB SHOWED IN UP POSITIONT/S IAW FIM 22-00-00-810-801, FCC 1 SHOWS AOA SENS 2, CURRENT FAULTS AND AOA SENS 2 RTS FAILE. R/R #2 AOA SENSOR IAW AMM 27-35-02-400-801 ALL TESTS PASSED P/N ON-OOF: 2568A-13 S/N ON: 1269 S/N OFF: GST 02157 IPC REF: 27-35-01-01

Part: SWITCH — INOPERATIVE (L1 DOOR) · airframe 103,139 hrs · 19,785 cycles

L1 CABIN DOOR SWITCHES ( INSIDE AND OUTSIDE) DONT WORK. THEY WORK WHEN WE ENTERED THE AIRCRAFT THEN STOPPED WORKING. DEFERRED PER MEL 52-10-3-1-2-1 PLACARD INST LOG UPDATEDPERFORMED INSP, CHECK & OPS CHECK OF L1 DOOR. OPS CHKS GOOD BOTH OUTSIDE AND INSIDE SWITCHES NUMEROUS TIMES IAW MD11 AMM 52-11-02. DMP REVERESED. M745301 CLOSED. PLACARD REMOVED.

Part: RIB — CRACKED (LT WING TE FLAP) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2CL/H WING I/B FLAP ELEPHANT EAR 4TH RIB FROM FWD. END IS CRACKED.REMOVED, FABRICATED AND REPLACED RIB IAW DWG. ARC2784 AND SRM 51-33-01. (MINOR).

Part: INTERCOSTAL — CRACKED (AFT CARGO) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C, AFT(CENTER) CARGO INTERCOSTAL DOUBLER CRACKED UNDER FLOOR STA.5-11. FABRICATED AND INSTALLED AFT (CENTER) CARGO INTERCOSTAL REPAIR DOUBLER AT STA 5-11 IAW SRM 53-00-00 FIG 204. (MINOR).

Part: RIB — CORRODED (RT ELEVATOR) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2CRT O/B ELEVATOR L/E RIB AT STA. XE=215.120 HAS CORROSION.REMOVED AND REPLACED CORRODED RT O/B ELEVATOR L/E RIB AT STA. XE=215.120 IAW MD-11 SRM 51-33-01. (MINOR)

Part: FITTING — WORN (RT ELEVATOR) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C, RIGHT OTBD ELEVATOR CAM FITTING IS WORN AT THE #6 RIB. REPAIRED CAM FITTING IAW EA 011-5520-01-A8472 REV. I/R, AND EO MD11-5520-77483-A. (MINOR)

Part: INTERCOSTAL — CRACKED (VERTICAL STAB) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C LOWER VERTICAL STABILIZER REAR CENTER SPAR TO REAR SPAR INTERCOSTAL RT SIDE IS CRACKED. REPAIRED CRACKED LOWER VERTICAL STABILIZER REAR CENTER SPAR TO REAR SPAR INTERCOSTAL RT SIDE IAW EA 011-5530-01-A8485 REV. I/R AND EO MD11-5530-77665-A (MAJOR).

Part: FITTING — WORN (LT ELEVATOR) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C, LEFT INBD ELEVATOR O/B CAM FITTING IS WORN.REPAIRED CAM FITTING IAW EA 011-5520-01-A8472 REV. I/R AND EO MD11-5520-77483-A. (MINOR)

Part: ANGLE — CRACKED (BS 1341) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2CUPPER CARGO COMPT. T-ANGLE CRACK AT LON 15R STA.1341. REMOVED AND INSTALLED CRACKED T-ANGLE AT LON 15R STA.1341 IAW SRM 51-33-01 AND 51-35-01. (MINOR)

Part: BUSHING — MIGRATED (RT WING AILERON) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C RT WING I/B AILERON ACTUATOR MOUNT FITTING I/B BUSHING IS MIGRATED.REPAIRED RT WING I/B AILERON ACTUATOR MOUNT FITTING I/B MIGRATED BUSHING IAW VT-SAA EA 011-5750-01-A8493 REV. IR AND UPS EO MD11-5750-77629-A (MINOR).

Part: AILERON — DAMAGED (RT WING) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C RT WING I/B AILERON ACTUATOR MOUNT FITTING O/B BUSHING IS MIGRATED. REPAIRED RT WING I/B AILERON ACTUATOR MOUNT FITTING O/B MIGRATED BUSHING IAW VT-SAA EA 011-5750-01-A8493 REV. IR AND UPS EO MD11-5750-77629-A(MINOR).

Part: ANGLE — CRACKED (BS 1341) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C, UPPER CARGO BAY TEE ANGLE CRACKED AT END OF LONGERON 15L, BS 1341. REMOVED AND INSTALLED A NEW ANGLE IAW SRM 51-35-01, AND 51-33-01. (MINOR)

Part: FITTING — WORN (LT ELEVATOR) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C, LEFT OTBD ELEVATOR CAM FITTING IS WORN JUST O/B OF THE #7 BEARING.REPAIRED CAM FITTING IAW EA 011-5520-01-A8472 REV. I/R, AND EO MD11-5520-77483-A. (MINOR)

Part: FITTING — WORN (LT ELEVATOR) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C, LEFT OTBD ELEVATOR CAM FITTING IS WORN JUST I/B OF THE #9 BEARING.REPAIRED CAM FITTING IAW EA 011-5520-01-A8472 REV. I/R AND EO MD11-5520-77483-A. (MINOR)

Part: INTERCOSTAL — CRACKED (FWD CARGO.) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C, LOWER FWD. CARGO INTERCOSTAL IS CRACKED AT STA. 6-30 AND LONG. 41 R/H. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG. ACA7049 AND SRM 51-33-01. (MINOR)

Part: SUPPORT — CRACKED (RT WINGLET) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C, RT LOWER WINGLET WEB SUPPORT IS CRACKED. REMOVED, FABRICATED AND REPLACED WEB IAW DWG. ARB7774 AND SRM 51-33-01. (MINOR)

Part: LONGERON — CRACKED (BS 1813) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C CENTER CARGO LONGERON 46 RT IS CRACKED ATSTA. 1813. REPAIRED CRACKED CENTER CARGO LONGERON 46 RT BETWEEN STA. 1821 TO 1841 IAW VT-SAA EA 011-5310-01-A8478 REV. I/R AND UPS EO MD11-5310-77624-A (MAJOR).

Part: STRINGER — CRACKED (RT WING) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE: 2C RT WING STRINGER # 38 IS CRACKED BETWEEN STA. XORS. 855.3 AND 885.4. REPAIRED CRACKED RT WING STRINGER #38 BETWEEN STA. XORS. 855.3 AND 885.4 IAW VT-SAA EA 011-5710-01-A8482 REV. I/R AND UPS EO MD11-5710-77666-A (MAJOR).

Part: STRINGER — CRACKED (FUSELAGE) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C, CENTER WING TANK STRINGER #51 IS CRACKED AT STA. XCW= -46.5.REPAIRED CRACKED CENTER WING TANK STRINGER #51 BETWEEN STA. XCW= -34.0 TO XCW= -58.0 IAW SRM 57-10-03 REPAIR 1 FIG. 201. (MAJOR)

Part: SUPPORT ANGLE — CORRODED (BS 1841) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2CAFT CARGO BILGE SUPPORT ANGLE AT STA 1841 HAS CORROSION.REMOVED AND REPLACED CORRODED AFT CARGO BILGE SUPPORT ANGLE AT STA 1841 IAW MD-11 SRM 51-33-01 & 51-35-01. (MINOR)

Part: SUPPORT ANGLE — CRACKED (BS 1701) · airframe 101,932 hrs · 19,267 cycles

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

Part: STIFFENER — CRACKED (AFT CARGO) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2CAFT CARGO BILGE VERTICAL STIFFNED IS CRACKED AT AT STA. 1841 L/H.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. AGA7170 AND SRMN 51-31-01. (MINOR)

Part: STRINGER — CRACKED (FUSELAGE) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C, CENTER WING TANK STRINGER # 47 IS CRACKED AT STA. XCW= 17.0. REPAIRED CRACKED CENTER WING TANK STRINGER # 47 BETWEEN STA. XCW= 5.5 TO XCW= 28.5 IAW SRM 57-10-03 REPAIR 1 FIG. 201. (MAJOR)

Part: STRINGER — CRACKED (FUSELAGE) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2CCENTER WING TANK STRINGER #48 IS CRACKED AT STA. XCW= -17.0REPAIRED CRACKED CENTER WING TANK STRINGER # 48 BETWEEN STA. XCW= -4.75 TO XCW= -33.0 IAW SRM 57-10-03 REPAIR 1 FIG. 201. (MAJOR)

Part: BULKHEAD — CRACKED (LT WING) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C LT WING UPPER BULKHEAD CAP IS CRACKED AT STA. XORS. 402 AND BETWEEN STRINGER # 13 & 14. REPAIRED CRACKED LT WING UPPER BULKHEAD CAP AT STA. XORS. 402 AND BETWEEN STRINGER 13 & 14 IAW VT-SAA EA 011-5710-01-A8473 REV. I/R AND UPS EO MD11-5710-77655-A (MAJOR).

Part: TEE FITTING — CRACKED (TANK TO BULKHEAD) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C, UPPER AUX TANK TEE TO BULKHEAD FITTING IS CRACKED AT STA. X= -46. REMOVED, FABRICATED AND REPLACXED TEE FITTING IAW DWG. APB7351 AND SRM 51-33-01. (MINOR)

Part: VANE — PUNCTURED (LT WING TE FLAP) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C, LEFT I/B FLAP VANE HAS PUNCTURE DAMAGE ON LOWER SURFACE BETWEEN STA. XIFH 197.6 TO 196.1 & 14" FROM T/EREPAIRED PUNCTURED L/H I/B FLAP VANELOWER SURFACE BETWEEN STA. XIFH 197.6 TO 196.1 AND 14" FROM T/E IAW SRM 51-71-00 REPAIR GENERAL PARA. 19 B. (MAJOR)

Part: SKIN — CRACKED (RT WING) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2CRT WING LOWER SKIN PANEL ACCESS DOOR 636AB HAS 17 CRACKED FASTENER HOLES.REPAIRED CRACKED RT WING LOWER SKIN PANEL ACCESS DOOR 636AB 17 EA FASTENER HOLES IAW MD-11 SRM 57-20-02 REPAIR 5. (MINOR)

Part: SKIN — CRACKED (LT WING) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2CRT WING LOWER SKIN ACCESS DOOR 536AB CUT OUT HAS 17 CRACKED FASTENER HOLES.REPAIRED CRACKED RT WING LOWER SKIN ACCESS DOOR 536AB CUT OUT FASTENER HOLES IAW MD-11 SRM 57-20-02 REPAIR 5. (MINOR)

Part: VANE — DELAMINATED (RT WING TE FLAP) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C RT WING I/B FLAP VANE LOWER SKIN IS DELAMINATED. REMOVED AND REPLACED RT WING I/B FLAP VANE IAW AMM 27-50-22-400-801 (MINOR).

Part: BRACKET — CRACKED (FWD CARGO) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C, FWD CARGO L/H STA 6-70 FLOOR BEAM ANGLE BRACKET CRACKED. REMOVED, FABBED AND INSTALLED FLOOR BEAM ANGLE BRACKET IAW SRM51-31-01 AND DRAWING ADA3645

Part: DOUBLER — CRACKED (LT WING) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C, L/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 673.7 TO 679.8. REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 673.7 TO 679.8 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: SKIN — CORRODED (RT WING) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C, RT WING UPPER SKIN HAS CORROSION BETWEEN XORS. 429-581 AT REAR SPAR.REPAIRED CORRODED R/H WING UPPER SKIN AT NOTED LOCATIONS IAW EA 011-5730-01-A8479 REV. I/R, AND EO MD11-5730-77584-A. (MINOR)

Part: SKIN — CORRODED (RT WING) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C, RT WING UPPER SKIN HAS CORROSION BETWEEN STA. XORS. 429 TO XORS. 581 AT AFT SPAR.REPAIRED CORRODED R/H WING UPPER SKIN BETWEEN STA. XORS. 429 TO XORS. 581 AT AFT SPAR IAW EA 011-5730-01-A8479 REV. I/R AND EO MD11-5730-77584-A.

Part: SKIN — CORRODED (RT WING) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE: 2C RT WING UPPER SKIN HAS CORROSION AT STA. XORS.= 197.2 AND STRINGER 6. REPAIRED CORRODED RT WING UPPER SKIN AT STA. XORS.= 197.2 AND STRINGER 6 IAW VT-SAA EA 011-5730-01-A8480 REV. I/R AND UPS EO MD11-5730-77670-A (MAJOR).

Part: FORMER — CRACKED (RT WING) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C, RT WING FIXED L/E FORMER IS CRACKED AT XOS 584. REMOVED AND REPLACED CRACKED RT WING FIXED L/E FORMER AT XOS 584 IAW MD-11 SRM 51-33-01. (MINOR)

Part: INTERCOSTAL — CRACKED (FWD CARGO) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C, FWD CARGO AT BS 6-70 AND LONGERON 43R, TEE-INTERCOSTAL IS CRACKED.REMOVED, FABRICATED AND REPLACED TEE- INTERCOSTAL IAW DWG. ADA3645 AND SRM 51-33-01. (MINOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C, LT WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN XOS. 584.89 TO 589.88. REPAIRED THE LT WING FIXED L/E BEADED DOUBLER IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR).

Part: RIB — CRACKED (LT WING LE) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2CL/H O/B WING L/E I/B OG #9 SLAT TRACK HAS CRACKED RIBREMOVED , FABBED, AND REINSTALLED RIB ON L/H WING L/E IAW SRM 51-31-01 AND DWG ARB2931-3 (MINOR)

Part: SKIN — CRACKED (RT WING) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2CR/H WING L/E LOWER SKIN IS CRACKED AT STA. XOS.490.850. REPAIRED CRACKED R/H WING L/E LOWER SKIN IAW SRM 57-40-01 REPAIR 17 FIG. 201. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C, LEFT WING FIXED L/E BEADED DOUBLER WAS CRACKED BETWEEN XOS. 633.4 TO 636.8. REPAIRED THE LT WING FIXED L/E BEADED DOUBLER IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C, LT WING FIXED L/E BEADED DOUBLER WAS CRACKED BETWEEN XOS. 759.1 TO 763.6. REPAIRED CRACKED LT WING FIXED L/E BEADED DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 205. MAJOR.

Part: WEB — CRACKED (BS 1307) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE: 2C, R-3 DOOR JAMB LOWER WEB IS CRACKED AT STA. 1307 AND Z= -17.5. REPAIRED CRACKED R-3 DOOR JAMB LOWER WEB AY STA. 1307 AND Z= -17.5 IAW SRM 53-40-15 REPAIR 3 FIG. 201. (MAJOR)

Part: BEAM — CRACKED (R-3 DOORWAY) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C, R-3 DOOR PLUG UPPER BEAM IS CRACKED AT THE FWD. END. REMOVED AND REPLACED DOOR BEAM IAW SRM 51-33-01 & 51-35-01. (MINOR).

Part: DOOR FRAME — CRACKED (MLG) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2CCENTER LANDING L/H GEAR DOOR FWD. FRAME IS CRACKED.REMOVED AND REPLACED FRAME IAW SRM 51-35-01. (MINOR)

Part: BEAM — CRACKED (L-3 DOORWAY) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C, L-3 DOOR PLUG LOWER BEAM IS CRACKED AT THE FWD END. REMOVED AND REPLACED DOOR BEAM IAW SRM 51-33-01 & 51-35-01. (MINOR)

Part: SKIN — CORRODED (FUSELAGE) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C, CENTER WING BOX UPPER SKIN HAS CORROSION O/B OF STA. XCW. 101 ABOVE STR. 10 & 13.REPAIRED CORRODED CENTER WING BOX UPPER SKIN AT NOTED LOCATIONS IAW VT-SAA EA 011-5710-01-A8476 REV. I/R AND UPS EO MD11-5730-77578-A. (MINOR)

Part: SKIN — CORRODED (FUSELAGE) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C, CENTER WING BOX UPPER SKIN HAS CORROSION BETWEEN STA. XCW= 101 ABOVE STR. 10 AND 13.REPAIRED CORRODED CENTER WING BOX UPPEWR SKIN AT NOTED LOCATIONS IAW VT-SAA EA 011-5710-01-A8476 REV. I/R AND UPS EO MD11-5730-77578-A. (MINOR)

Part: DOUBLER — CRACKED (LEFT WING) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2C, LT WING FIXED L/E BEADED DOUBLER WAS CRACKED BETWEEN XOS. 653 TO 657.7. REPAIRED THE DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 205. MAJOR.

Part: DOUBLER — CRACKED (LT WING) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2CL/H WING FIXED L/E BEADED DOUBLER IS CRACKED AT STA. XOS. 738.REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 734.7 TO 740.8 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: DOOR FRAME — CRACKED (MLG DOOR) · airframe 101,932 hrs · 19,267 cycles

INSPECTION TYPE:2CCENTER LANDING GEAR R/H DOOR FWD. FRAME IS CRACKED.REMOVED AND REPLACED FRAME IAW SRM 51-35-01. (MINOR)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 101,858 hrs · 19,227 cycles

EMRGENCY BATTERY PACK INOPERATIVE. R & R EMERGENCY POWER SUPPLY AMM 33-51-01-000-802, 33-51-01-400-802 AND 33-51-01-700-802.

Part: HINGE — EXCESS PLAY (RT WING) · airframe 101,746 hrs · 19,181 cycles

INSPECTION TYPE:SV RT O/B FLAP O/B HINGE BEARING HAS AXIAL PLAY. REPAIRED R/T O/B FLAP O/B HINGE BEARING LUG BORE IAW CMM 57-44-09. (MINOR)

Part: BUSHING — MIGRATED (TE FLAP) · airframe 101,746 hrs · 19,181 cycles

INSPECTION TYPE:SV RT O/B FLAP I/B HINGE O/B BUSHING IS MIGRATED. REPAIRED RT O/B FLAP I/B HINGE O/B BUSHING LUG BORE IAW CMM 57-52-04. (MINOR)

Part: BUSHING — MIGRATED (TE FLAP) · airframe 101,746 hrs · 19,181 cycles

INSPECTION TYPE:SV RT O/B FLAP O/B HINGE I/B BUSHING IS MIGRATED. REPAIRED RT O/B FLAP O/B HINGE I/B BUSHING LUG BORE IAW CMM 57-52-04. (MINOR)

Part: BUSHING — MIGRATED (TE FLAP) · airframe 101,746 hrs · 19,181 cycles

INSPECTION TYPE:SV RT O/B FLAP O/B HINGE O/B BUSHING IS MIGRATED. REPAIRED RT O/B FLAP O/B HINGE O/B BUSHING LUG BORE IAW CMM 57-52-04. (MINOR)

Part: BEARING — MIGRATED (RT WING) · airframe 101,744 hrs · 19,180 cycles

INSPECTION TYPE:SV RT O/B FLAP I/B HINGE BEARING IS MIGRATED. REPAIRED RT O/B FLAP I/B HINGE BEARING LUG BORE IAW CMM 57-44-08. (MINOR)

Part: CONTROL UNIT — FAILED (NR 2 ENGINE) · airframe 101,405 hrs · 19,067 cycles

INSPECTION TYPE:N/A#2 FIRE ALERT DISPLAYED ALONG WITH LIGHTS.R&R #2 ENGINE FDCU IAW AMM 26-11-02 IPC 26-11-01-01-005

Part: SOLENOID — FAILED (L1 DOOR LOCK) · airframe 100,369 hrs · 18,626 cycles

L1 DOOR SOLENOID CLICKING EXCESSIVELY. REPLACED THE L1 FWD PASSENGER DOOR LOCK PIN RELEASE SOLENOID IAW AMM 52-10-06. OPS TEST NORMAL.

Part: POWER SUPPLY — FAULTED (COCKPIT) · airframe 99,958 hrs · 18,451 cycles

INSPECTION TYPE:NA EMERG BATT & LO MSG DURING TEST. REPLACED EMERG BATT POWER SUPPLY PER MM 33-51-01. OPS CHK GOOD PER TASK 33-51-01. OPS CHK GOOD PER TASK 33-51-01-700-802. IPC 33-51-01-05.

Part: LANDING — CRACKED (LT WING) · airframe 98,206 hrs · 17,942 cycles

INSPECTION TYPE:4C, LT OUTER WING ACCESS DOOR CUT-OUT PANEL LANDING HAS 3 CRACKS BETWEEN STA XORS 683.4 TO XORS 713.6. REPAIRED CRACKED LT OUTER WING ACCESS DOOR CUT-OUT PANEL LANDING BETWEEN STA XORS 683.4 TO XORS 713.6 IAW SRM 57-20-02 REPAIR 5.

Part: LANDING — CRACKED (RT WING) · airframe 98,206 hrs · 17,942 cycles

INSPECTION TYPE:4C, RT OUTER WING ACCESS DOOR CUT-OUT PANEL LANDING HAS 3 CRACKS BETWEEN STA XORS 683.4 TO XORS 713.6. REPAIRED CRACKED RT OUTER WING ACCESS DOOR CUT-OUT PANEL LANDING BETWEEN STA XORS 683.4 TO XORS 713.6 IAW SRM 57-20-02 REPAIR 5. (MINOR)

Part: SPAR CAP — CORRODED (RT WING) · airframe 98,206 hrs · 17,942 cycles

INSPECTION TYPE:4C, RT WING UPPER T/E PANEL IS BULGED UP JUST FWD OF NR 5 SPOILER O/B END. REPAIRED RT WING REAR SPAR UPPER CAP AFT FLANGE BETWEEN XORS 771.5 - XORS 826 IAW EA 011-58710-01-A7348 REV IR AND EO MD11-5710-69280-A. (MAJOR)

Part: SKIN — BROKEN (RT WING) · airframe 98,206 hrs · 17,942 cycles

INSPECTION TYPE:4C, RT WING FIXED L/E EXTERIOR SKIN AT NR 8 SLAT TRACK CUT-OUT, STA XOS551, SMALL PIECE OF SKIN BROKEN AWAY. REPAIR RT WING L/E SKIN PER EO MD11-5710-69196-A AND EA 011-5730-01-A7343 REV IR (MINOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 98,206 hrs · 17,942 cycles

INSPECTION TYPE:4C, LT WING L/E BEADED DOUBLER IS CRACKED BETWEEN XOS 616 - XOS 621. REPAIRED LT WING L/E BEADED DOUBLER BETWEEN XOS 616 - XOS 621 IAW SRM 57-40-02 REPAIR 15 FIGURE 205 REV 64. (MAJOR)

Part: SKIN — DENTED (FUSELAGE) · airframe 98,206 hrs · 17,942 cycles

INSPECTION TYPE:4C, FUSELAGE EXTERIOR SKIN DENTED AT STA 5-46 BETWEN L46R AND L47R. DENT REPAIRED PER EO MD11-5330-69249-A AND EA 011-5300-01-A7349 REV IR (MINOR)

Part: LONGERON — CORRODED (FUSELAGE) · airframe 98,206 hrs · 17,942 cycles

INSPECTION TYPE:4C, AGING AIRCRAFT FINDING. EXTERIOR FUSELAGE SKIN AT STA 1129 AND LONGERON 45L HAS 5 FASTENERS PULLING THROUGH SKIN AND SKIN IS BULGED. FOUND LONGERON 45L WITH EXFOLIATION CORROSION BETWEEN STA 6-30 TO 1129. REPAIRED LONGERON 45L BETWEEN STA 6-30 TO 1129 IAW SRM 53-00-05, REPAIR 1, FIGURE 201 (TYPE 1), REV 64. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 98,206 hrs · 17,942 cycles

INSPECTION TYPE:4C, RT WING L/E BEADED DOBLER IS CRACKED BETWEEN STA XOS 783.2-789.6. REPAIRED CRACKED RT WING FIXED L/E BEADED DOUBLER AT STA XOS 783.2-789.6 IAW SRM 57-40-02 REPAIR 15 FIG 205.

Part: SKIN — CORRODED (FUSELAGE) · airframe 98,206 hrs · 17,942 cycles

INSPECTION TYPE:4C, UPPER AFT NUT PLATE HAS EXFOLIATION CORROSION AROUND IT ON SKIN INSIDE ACCESS 316AB RT SIDE APPROX STA 2160. REPAIRED AFT FUSELAGE UPPER AFT SKIN AT APPROX STA Y=2160 BETWEEN LONGERON 12R AND LONGERON 13R IAW EA 011-5370-01-A7362 REV IR AND EO MD11-533-69255-A. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 98,206 hrs · 17,942 cycles

INSPECTION TYPE:4C, LT WING L/E PANEL LANDING DOUBLER IS CRACKED AT XORS 885. REPAIRED LT WING L/E PANEL LANDING DOUBLER BETWEEN XOS 993 - XOS 1003 IAW SRM 57-40-03 REPAIR 1, FIGURE 201 REV 64. (MAJOR)

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 98,206 hrs · 17,942 cycles

INSPECTION TYPE:4C, CRACKED CABIN FLOOR SEAT TRACK AT STA 919 AND RBL 45. REPAIRED MAIN CABIN SEAT TRACK BETWEEN STA Y=909 - Y=929 AT X=-47.5 IAW SRM 53-00-52 REPAIR 1, FIGURE 201, REV 64. (MAJOR)

Part: DOUBLER — CHAFED (TAILCONE) · airframe 98,206 hrs · 17,942 cycles

INSPECTION TYPE:4C, TAIL CONE INNER DOUBLER AND LONGERON BEAM HAVE CHAFE DAMAGE AT STA CANT STA Y=2163.685 AND Y=2165.061 AT RBL X=-36.5 REPAIRED TAIL CONE INNER DOUBLER AND LONGERON BEAM IAW EA 011-5350-01-A7337 REV I/R AND EO MD11-5350-69240-A. (MINOR)

Part: LONGERON — CHAFED (TAILCONE) · airframe 98,206 hrs · 17,942 cycles

INSPECTION TYPE:4C, TAIL CONE INNER DOUBLER AND LONGERON BEAM HAVE CHAFE DAMAGE BETWEEN CANT STA 2163.685 AND 2165.061 AT LBL X=36 AND BETWEEN WL Z=45 & Z=60.1. REPAIRED TAIL CONE INNER DOUBLER AND LONGERON BEAM AT SAID LOCATION IAW EA 011-5350-01-A7336 REV I/R AND EO MD11-5350-69239-A. (MINOR)

Part: HINGE FITTING — GOUGED (NR 3 FAN COWL) · airframe 98,206 hrs · 17,942 cycles

INSPECTION TYPE:4C, NR 3 ENGINE I/B FAN COWL FWD HINGE FITTING IS GOUGED. REPAIRED NR 3 ENGINE I/B FAN COWL FWD HINGE FITTING IAW EA 011-7110-01-A7344 REV IR AND EO MD11-7110-69182-A. (MINOR)

Part: HINGE FITTING — GOUGED (NR 3 COWLING) · airframe 98,206 hrs · 17,942 cycles

INSPECTION TYPE:4C, NR 3 ENG O/B FAN COWL FWD HINGE FITTING IS GOUGED. REPAIRED NR 3 ENG O/B FAN COWL FWD HINGE FITTING IAW EA 011-7110-01-A7346 REV IR AND EO MD11-7110-69181-A. (MINOR)

Part: RAIL — CRACKED (MAIN CARGO BAY) · airframe 98,206 hrs · 17,942 cycles

INSPECTION TYPE:4C, MAIN CARGO COMP RT OVERHEAD STOWAGE SIDE RAIL BETWEEN STA 1715 TO 1841 IS CRACKED. REPAIRED CRACKED MAIN CARGO RT OVERHEAD SIDERAIL BETWEEN STA 1715 TO 1841 IAW EA 011-2511-01-A7351 REV I/R AND EO MD11-2550-69227-A. (MINOR)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 97,798 hrs · 17,806 cycles

EMERGENCY LIGHT BATTERY DISCHARGED. REPLACED THE BATTERY IAW MM 33-51-01.

Part: SMOKE DETECTOR — FAULTY (MAIN CARGO) · airframe 97,557 hrs · 17,767 cycles

FOUND A CABIN SMOKE WARNING MESSAGE ON THE DISPLAY UNIT. PERFORMED A CARGO SMOKE TEST AND VERIFIED ONE SMOKE DETECTOR IN THE MAIN CARGO BS 1541 FAULTY. REPLACED THE SMOKE DETECTOR IAW AMM 26-15-08-000-801, REV 90.05. PERFORMED AN OPS TEST, TESTED GOOD.

Part: ADC — MALFUNCTIONED · airframe 97,234 hrs · 17,666 cycles

AIR TURNBACK DUE TO INCORRECT INFO ON PDF CONTRADICTORY FROM SIDE TO SIDE. R & R THE NR 1 ADC IAW AMM 34-16-01-000-801/400-801, REV 01/08/18. COMPLIED WITH AN OPS TEST IAW AMM 34-16-01-700-801, REV. COMPLIED WITH ADC IEIS INTERFACE TEST IAW AMM 34-16-01-700-804, ALL TESTS PASSED, NO FURTHER FAULTS DISPLAYED.

Part: FLOOR PANEL — PUNCTURED (AFT CARGO) · airframe 96,456 hrs · 17,500 cycles

AFT CARGO BAY FLOOR PANEL HAS A PUNCTURE ON THE LEFT SIDE.

Part: DRIVE ASSY — CORRODED (L1 DOOR) · airframe 96,404 hrs · 17,488 cycles

FWD CABIN L1 DOOR POWER DRIVE MECHANISM ASSY CORRODED. REMOVED AND REPLACED THE ASSEMBLY IAW AMM 52-11-09. OPS CHECKED GOOD3

Part: CABLE — MISSING (L1 DOOR) · airframe 96,384 hrs · 17,479 cycles

L1 DOOR AFT FOLLOW UP CABLE MISSING. R & R THE PULLEY ON AFT TRUCK ON L1 DOOR IAW MM 20-50-02. OPS CHECKED GOOD.

Part: SWITCH — INOPERATIVE (L1 DOOR) · airframe 95,883 hrs · 17,354 cycles

L1 DOOR AFT DOWN CABLE BROKEN, DOOR ELECTRICAL FUNCTION INOPERATIVE. REPLACED LEFT ENTRY DOOR OUTSIDE SWITCH 51-1013 IAW WD 5211-01. OPS CHECKED OK.

Part: SWITCH — MALFUNCTIONED (L1 DOOR) · airframe 95,883 hrs · 17,354 cycles

L1 DOOR OPENED ON IT`S OWN WHEN THE ARM LEVER WAS DEACTIVATED. REPLACED SWITCH 51-1013 IAW WD 52-11-01. OPS CHECKED OK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 95,783 hrs · 17,329 cycles

EMERGENCY LIGHT BATTERY POWER SUPPLY INOPERATIVE. R & R THE POWER SUPPLY REF 33 51 01

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 94,932 hrs · 17,133 cycles

EMERGENCY LIGHT BATTERY 1 LOW. R & R THE POWER SUPPLY IAW AMM 33-51-01-4 REV 87. OPS TESTED GOOD.

Part: ACTUATOR — INOPERATIVE (RT AILERON) · airframe 94,073 hrs · 16,917 cycles

RECEIVED A LEVEL 2 AILERON DEFLECT DISAGREE. RAN CHECKLIST, NO HELP. REPLACED THE RT WING AILERON DEFLECTION ACTUATOR IAW AMM 27-16-01-401 REV 86.02. OPS TESTED IAW AMM 27-16-00-700-801 REV 86.02. TESTED GOOD. O

Part: SEAT TRACK — DAMAGED (BS 889) · airframe 93,970 hrs · 16,901 cycles

SEAT TRACK DAMAGED AT BS 889, LBL 27.5. REPAIRED IAW EO MD11-5310-62059-A.

Part: SKIN — CRACKED (NR 5 SPOILER) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, LT NR 5 SPOILER UPPER SKIN DENTED WITH CRACKED. REPAIRED THE DENT IAW SRM 51-71-00 REPAIR GENERAL, PARA. 19.B. MAJOR REPAIR.

Part: DOOR FRAME — CORRODED (AFT CARGO BAY) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, AFT CARGO DOOR FRAME HAS CORROSION AT BS 1959 BETWEEN X 30 TO 40 AND Z 80. REPAIRED THE DOOR FRAME IAW EA 011-5310-A6351 REV. I/R AND EO MD11-5310-61221-A. (MINOR)

Part: THRUST REVERSER — CRACKED (NR 3 ENGINE) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C. NR 3 ENG. O/B THRUST REVERSER CASCADE FRAME LOWER LUG BORE IS CRACKED. REMOVED AND REPLACED THE THRUST REVERSER HALF IAW AMM 71-13-01-000-868 AND 71-13-01-400-868.

Part: FITTING — CORRODED (MAIN CABIN) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, RIGID CARGO BARRIER FLOOR FITTING NR 6 HAS CORROSION. REPAIRED CORRODED RCB FLOOR FITTING NR 6 IAW EA 011-5340-01-A6346 REV. I/R AND EO MD11-5340-61193-A. (MINOR)

Part: FITTING — CORRODED (MAIN CABIN) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, RIGID CARGO BARRIER FLOOR FITTING NR 7 HAS CORROSION. REPAIRED THE FLOOR FITTING IAW EA 011-5340-01-A6346 REV. I/R AND EO MD11-5340-61193-A. (MINOR)

Part: FITTING — CRACKED (FUSELAGE) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE:3C, RIGID CARGO BARRIER FLOOR FITTING NR 10 IS CRACKED. R & R RCB FLOOR FITTING IAW EO MD11-2520-58701-C.

Part: FRAME — CRACKED (BS 469) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, FUSELAGE FRAME CRACKED AT BS 469 NEAR X=60. REPAIRED IAW EA 011-5310-01-A6348 REV. IR AND EO MD11-5310-61274-A. MAJOR REPAIR.

Part: DRIP TRAY — CHAFED (E/E BAY) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, AFT SIDE OF MAIN AVIONICS RACK DRIP SHIELD IS CHAFED. REMOVED, FABRICATED AND REPLACED THE DRIP SHIELD IAW DWG SP11251227 AND SRM 53-00-00.

Part: FRAME — CRACKED (BS 469) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, FUSELAGE FRAME CRACKED AT BS 469 NEAR X 30. REPAIRED IAW EA 011-5310-01-A6348 REV. IR AND EO MD11-5310-61274-A. MAJOR REPAIR.

Part: INTERCOSTAL — CRACKED (FWD. CARGO) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, FWD. CARGO BAY BETWEEN BS 6-39 TO 6-59 AND LONGERON 42-43L, INTERCOSTAL IS CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-33-01. (MINOR)

Part: LONGERON SPLICE — CRACKED (CENTER CARGO) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, CENTER CARGO LONGERON SPLICE 33L IS CRACKED AT BS 5-123. REMOVED, FABRICATED AND REPLACED THE LONGERON SPLICE IAW DWG A5A7112 AND SRM 51-33-01. (MINOR)

Part: LONGERON SPLICE — CRACKED (FWD CARGO) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, FWD CARGO LONGERON SPLICE 45L AT BS 685 IS CRACKED. REMOVED AND REPLACED THE LONGERON SPLICE IAW SRM 51-33-01. (MINOR)

Part: SKIN — CORRODED (BS 2120-2163) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, AFT FUSELAGE EXTERIOR SKIN CORRODED BS 2120 - 2163 L33 - 35L. REPAIRED IAW EA 011-5330-01-A6341 REV. IR AND EO MD11-5330-61287-A. MAJOR REPAIR.

Part: LONGERON — CRACKED (BS 1219 -1239) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE:3C, LONGERON 27L CRACKED BS 1219 - 1239. REPLACED THE LONGERON IAW EA 011-5310-01-A6343 REV. IR AND EO MD11-5310-61257-A. MAJOR REPAIR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, CENTER WING UPPER SKIN CORRODED ABOVE STRINGER 15 BETWEEN XCW -5 AND -20. REPAIRED IAW EA 011-5730-01-A6357 REV. IR AND EO MD11-5730-61284-A.

Part: SKIN — CORRODED (FUSELAGE) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, CENTER WING UPPER SKIN CORRODED ABOVE STRINGER 15 NEAR XCW102. REPAIRED NOTED CORROSION IAW EA 011-5730-01-A6357 REV. IR AND EO MD11-5730-61284-A.

Part: STRINGER — CRACKED (CENTER TANK) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, CENTER TANK STRINGER 48 HAS AN 8 INCH CRACK AT XCW=32.00. REPAIRED THE STRINGER IAW SRM 57-10-03 REPAIR 1 FIG. 201. (MAJOR)

Part: LONGERON — CRACKED (BS 1179-1199) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, MAIN CABIN AT BS 1179-1199, LONGERON 27 LT IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE LONGERON IAW EA 011-5310-01-A6344 REV. I/R AND EO MD11-5310-61228-A. MAJOR REPAIR.

Part: SKIN — CORRODED (BS 2150-2164) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE:3CAFT FUSELAGE EXTERIOR SKIN CORRODEDSTA. 2140 - 2164 L33 - 35L. REPAIRED IAW EA 011-5330-01-A6341 REV. IR AND EO MD11-5330-61287-A. MAJOR REPAIR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, CENTER WING UPPER SKIN PANEL CORRODED ABOVE S15 BETWEEN XCW -32 AND -45. REPAIRED IAW EA 011-5730-01-A6357 REV. IR AND EO MD11-5730-61284-A.

Part: FUEL TANK — CORRODED (CENTER) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, MAIN CABIN UNDER FLOOR CENTER TANK UPPER SKIN HAS CORROSION AT XCW=-50 AT STR. 15.REPAIRED CORRODED CTR. WING SKIN AT STA. XCW=-50 IAW EA 011-5730-01-A6345 REV. I/R AND EO MD11-5730-61283-A. MAJOR REPAIR.

Part: FRAME — DENTED (BS 775) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, MAIN CABIN FRAME IS DENTED AT BS 775 LONGERON 12R. REPAIRED THE FRAME IAW EA 011-5310-01-A6352 REV. I/R AND EO MD11 5310-61255-A. MAJOR REPAIR.

Part: LONGERON — CRACKED (BS 1219-1239) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, MAIN CABIN LONGERON 27R IS CRACKED BETWEEN BS 1219-1239. REPAIRED THE LONGERON IAW EA 011-5310-01-A6355 REV. I/R AND EO MD11-5310-61227-A. MAJOR REPAIR.

Part: FRAME — DENTED (BS 675) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, MAIN CABIN FRAME IS DENTED AT BS 675, LONGERON 12R. REPAIRED THE FRAME IAW EA 011-5310-01-A6349 REV. I/R AND EO MD11-5310-61250-A. MAJOR REPAIR.

Part: LONGERON SPLICE — CRACKED (L12L) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE:3CMAIN CABIN LONGERON 12 L SPLICE FITTING IS CRACKED AT STA 5-123. REMOVED, FABRICATED AND REPLACED THE LONGERON SPLICE IAW DWG A5A7112 AND SRM 51-33-01. (MINOR)

Part: LONGERON — CHAFED (FUSELAGE) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE:3C, MAIN CABIN LONGERON 12 LT IS CHAFED BETWEEN STA 1781-1801. REPAIRED CHAFED LONGERON 12 LT BETWEEN STA 1781-1801 IAW EA 011-5310-01-A6353, REV I/R AND EO MD11-5310-61225-A.

Part: LONGERON SPLICE — CRACKED (MAIN CABIN) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE:3CMAIN CABIN LONGERON 10L SPLICE FITTING IS CRACKED AT STA. 5-123.REMOVED, FABRICATED AND REPLACED LONG. 10 L/H SPLICE FITTING AT STA. 5-123 IAW DAC DWG. A5A7112 AND SRM 51-33-01.(MINOR)

Part: LONGERON SPLICE — CRACKED (MAIN CABIN) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE:3C, MAIN CABIN LONGERON 8L SPLICE FITTING IS CRACKED AT STA. 5-123.REMOVED , FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DAC DWG.A5A7112 AND SRM 51-33-01. (MINOR)

Part: FRAME — DENTED (BS 715) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE:3C, MAIN CABIN FRAME IS DENTED AT BS 715, LONGERON 12R. REPAIRED THE FRAME IAW EA 011-5310-01-A6350 REV. I/R AND EO MD11-5310-61254-A. MAJOR REPAIR.

Part: TUBE — KINKED (RT WING FUEL) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, RT WING FUEL TRANSFER PIPE HAS A LARGE DENT AT XOS 703.6. REPAIRED THE TRANSFER PIPE IAW EA 011-2820-A6336 REV. I/R AND EO MD11-2820-61199-A. (MINOR)

Part: DOOR FRAME — CRACKED (R3 DOOR) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE:3CMAIN CABIN R-3 DOOR JAMB FWD. LOWER WEB IS CRACKED.REPAIRED CRACKED R-3 DOOR JAMB LOWER WEB IAW MD11 SRM 53-40-15 REPAIR 3 FIG. 201.(MAJOR)

Part: SUPPORT — CRACKED (WING TO BODY) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, LEFT WING TO BODY FAIRING SUPPORT STRUCTURE BRACKET IS CRACKED AT BS 1661. REMOVED, FABRICATED AND REPLACED THE SUPPORT BRACKET IAW DWG. AFA7769 AND SRM 51-33-01. (MINOR)

Part: SKIN — CRACKED (LT WING) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, LEFT WING T/E REAR SPAR LOWER PANEL LANDINGL IS CRACKED AT XORS 344. REMOVED, FABRICATED AND REPLACED IAW DWG ARC7008 AND SRM 51-33-01. (MINOR)

Part: DOOR FRAME — CRACKED (R3 DOORWAY) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, MAIN CABIN R3 DOOR FRAME FWD UPPER WEB IS CRACKED. REPAIRED THE DOOR FRAME WEB IAW EA 011-5310-01-A6355 REV. I/R AND EO MD11-5310-61151-A. (MAJOR)

Part: SKIN — DELAMINATED (NR 5 SPOILER) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, RT NR 5 SPOILER LOWER SKIN DELAMINATED. SPOILER REPAIRED IAW EA 011-5750-01-A6354 REV. IR AND EO MD11-5755-61215-A. MAJOR REPAIR.

Part: RIB — CRACKED (RT WING SLAT) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, RIGHT WING NR 1 SLAT RIB AT XIS=151.2578 IS CRACKED. REPAIRED THE SLAT RIB IAW EA 011-5750-01-A6347 REV. I/R AND EO MD11-5750-61271-A. MAJOR REPAIR.

Part: STRINGER — CRACKED (LT WING) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, LEFT WING FIXED L/E COMPARTMENT STRINGER AT XOS.789-795 IS CRACKED. REPAIRED CRACKED STRINGER IAW SRM 57-40-03 REPAIR 2 FIG. 201. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, LT WING FIXED L/E BEADED DOUBLER IS CRACKED AT XOS. 678. REPAIRED THE DOUBLER IAW EA 011-5710-A6326 REV. I/R AND EO 5730-61201-A. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, RT WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN XOS.789-795. REPAIRED THE DOUBLER IAW SRM 57-40-02 REPAIR 15 FIG. 203 (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, RT WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN XOS 789-795. REPAIRED THE DOUBLER IAW SRM 57-40-02 REPAIR 15, FIG 203.(MAJOR)

Part: ANGLE — CRACKED (RT WING) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, RT WING FIXED L/E SPLICE ANGLE IS CRACKED AT XOS. 584. REMOVED, FABRICATED AND REPLACED THE ANGLE IAW DWG ARB2931 AND SRM 51-33-01. (MINOR)

Part: RIB — CRACKED (RT WING) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, RT WING FIXED LOWER RIB AT XOS 1025 IS CRACKED. REMOVED, FABRICATED AND REPLACED THE RIB IAW DWG ARB 2920 AND SRM 51-33-01. (MINOR)

Part: WEDGE — DELAMINATED (RT WING AILERON) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, RIGHT WING O/B AILERON T/E WEDGE I/B END IS DELAMINATED. REMOVED AND REPLACED THE AILERON WEDGE IAW DWG.NRC6741 AND SRM57-60-80 REPAIR 1.

Part: DOUBLER — CRACKED (LT WING) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED XOS 654. REPAIRED THE DOUBLER IAW SRM 57-40-02 REPAIR 15 FIG. 206. MAJOR REPAIR.

Part: SKIN — CRACKED (RT WING) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, RT WING FIXED L/E SKIN IS CRACKED AT XOS. 611 I/B FWD CORNER OF ACCESS DOOR CUT-OUT. REPAIRED THE SKIN IAW SRM 57-40-01 FIG.201 REPAIR 18. (MAJOR)

Part: SKIN — CRACKED (RT WING) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE:3C, RT WING FIXED L/E SKIN IS CRACKED AT NR 11 SLAT TRACK CUTOUT STA XOS 720.18. REPAIRED CRACKED RT WING L/E SKIN AT STA XOS 720.18. SLAT TRACK CUTOUT IAW SRM 57-40-02, REPAIR 7, FIG 201.

Part: DOUBLER — CRACKED (LT WING) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, LEFT WING FIXED L/E SKIN INNER SPLICE STRAP DOUBLER CRACKED NEAR XOS 789. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW DWG ARB3954 AND SRM 51-33-01. (MINOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE: 3C, RT WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN XOS 906-911.5. REPAIRED THE DOUBLER IAW SRM 57-40-02 REPAIR 15 FIG.203.(MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE:3C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED XOS738. REPAIRED LT WING BEADED DOUBLER XOS 734-740 IAW SRM 57-40-02, REPAIR 15, FIG 206.

Part: SKIN — CRACKED (LT WING) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE:3C, LEFT WING L/E SKIN AT CORNER OF REFUELING ACCESS DOOR AT STA XOS.611 IS CRACKED. REPAIRED CRACKED LT WING SKIN AT STA XOS 611 IAW SRM 57-40-01 REPAIR 18, FIG 201.

Part: DOOR FRAME — CRACKED (R3 DOOR) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE : 3C, MAIN CABIN R3 DOOR FRAME FWD. LOWER WEB IS CRACKED. REPAIRED THE DOOR FRAME IAW SRM 53-40-15 REPAIR 3 FIG.201. (MAJOR)

Part: FITTING — CRACKED (FUSELAGE) · airframe 93,473 hrs · 16,788 cycles

INSPECTION TYPE:3C, RIGID CARGO BARRIER FLOOR FITTING NR 1 IS CRACKED. R & R RCB FLOOR FITTING NR 1 IAW EO MD11-2520-58701-C.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 93,348 hrs · 16,753 cycles

EMERGENCY LIGHT BATTERY LOW, 1 DISPLAYED DURING EMERGENCY LIGHT TEST. R & R EMERGENCY LIGHTING POWER SUPPLY IAW AMM 33-51-01-700-802. OPS CK GOOD IAW AMM 33-51-01-700-802.

Part: BATTERY — DISCHARGED (MASTER) · airframe 92,870 hrs · 16,627 cycles

DURING CRUISE FLIGHT THE LEVEL 1 ALERT "BATTERY LOW" ILLUMINATED, RETURNED TO DEPARTURE AIRPORT, CHECK LIST COMPLETED, FUEL DUMP WAS COMPLETED, CHECK LIST COMPLETED, FLIGHT CONTINUE AND LANDED UNEVENTFULLY, ON TAXI IN THE BATTERY WAS R & R MAIN BATTERY AND BATTERY CHARGER, OPS TEST OF BATTERY, ALL NORMAL IAW AMM 24-34-02-400 AND 24-34-03-400, CHARGER PN OFF & ON: 3S2060PM169A3, SN OFF: 87D2542M1R, SN OFF: GOS00043R, BATTERY, PN OFF AND ON: AD43B050LB01, SN OFF: 503538, SN ON: 504195CR51, IPC REF: 24-34-02-01-273, 24-34-03-01-001.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 92,452 hrs · 16,530 cycles

ENTRY DOOR L1 PNEUMATIC BOTTLE LOW. SERVICED L1 DOOR PNEUMATIC SYSTEM IAW MM 12-25-04-600-801.

Part: SIGHT GLASS — DAMAGED (PAX DOOR) · airframe 92,424 hrs · 16,525 cycles

THE BOTTOM LT SIDE MODE VERIFICATION INDICATOR, SIGHT WINDOW ON CABIN DOOR 1L , BROKE OFF. L1 MAIN ENTRY DOOR INOPERATIVE, INSTALLED NEW SERVICEABLE LOWER DOOR COVER ON L1 DOOR IAW MM 25-23-07-400-802AKK, DOOR OPS CHECKS NORMAL THIS CLEARS M568236, PLACARD REMOVED 52-11-14-05.

Part: CONTROL SYSTEM — OUT OF ADJUST (SPOILERS) · airframe 91,550 hrs · 16,280 cycles

WHEN SPEED BRAKE DEPLOYED FULLY DURING FLIGHT, ACFT ENTERED 3 DEGREE RT BANK. ADJUSTED LATERAL SPOILER CONTROLS IAW MM 27-61-00-830-801, THROUGH STEP G. (21).

Part: WINDSHIELD — CRACKED (L1) · airframe 91,473 hrs · 16,265 cycles

INSPECTION TYPE: MX, CAPTAIN'S LEFT OUTER PANE CRACKED. REMOVED AND REPLACED THE L1 WINDSHIELD IAW MM 56-11-01-401, AND MM 56-11-01-400.

Part: TRUNNION — CORRODED (LEFT) · airframe 90,637 hrs · 16,073 cycles

INSPECTION TYPE:1C, CLG LT TRUNION FITTING CENTER ALIGNMENT PIN HOLE FOR PILLOW BLOCK CORRODED. REPAIRED CLG LT TRUNION FITTING IAW SRM 53-40-14, REPAIR 1.

Part: TRUNNION — CORRODED (RT MLG) · airframe 90,637 hrs · 16,073 cycles

INSPECTION TYPE:1CCLG, RT TRUNION FWD PILLOW BLOCK BOLT HOLE ID CORRODED REPAIRED BOLT HOLE ID IAW EA 011-5340-01-A5761 REV IR AND EO MD11-5340-56869-A.

Part: LENS — CRACKED (EMERGENCY LIGHT)

L1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. WILL NOT INSTALL. R & R L1 DOOR EMERGENCY EXIT LIGHT LENS IAW AMM 33-37-05.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS)

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

Part: UNKNOWN — VIBRATION (FUSELAGE)

FOUR HOURS INTO FLT AT FL340, A LOUD BANG WAS HEARD WITH A DEFINATE SHUDDER. CONFIGURATION PAGE SHOWED NO LT NOSE GEAR PRESSURE. NORMAL LANDING AND TAXI. CHECKED ACFT FOR DAMAGE OR MISSING PARTS. NO FAULTS FOUND. "TP CHANNEL NL" SHOWN IN CURRENT FAULTS. R & R BTM/TPI COMPUTER, NO HELP. R & R PRESSURE TRANSDUCER, NO HELP. REPLACED INBD REFUELING ADAPTER FLANGE.

Part: HOUSING — CRACKED (EMERGENCY LIGHT)

L1 DOOR FWD DOOR HANDLE EMERGENCY LIGHT HOUSING CRACKED. R & R LIGHT ASSY IAW AMM 33-52-02-00-80.

Part: SIGN — DISLODGED (COCKPIT)

EMERGENCY SIGN OVER GALLEY FELL OFF. R & R R1 DOOR HANDLE EMERGENCY LIGHT ASSY IAW AMM 33-52-02 AND WDM 33-52-01. OPS TESTED GOOD.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 88,173 hrs · 15,457 cycles

INSPECTION 2C, LEFT WING INBD FLAP UPPER SURFACE DENTED 12 INCHES FWD OF T/E AT CENTER OF FLAP. INSTALLED REPAIR IAW SRM 57-0 0-01, REPAIR 1, FIG 201. MAJOR REPAIR.

Part: SUPPORT CHANNEL — CRACKED (BS 2014) · airframe 88,173 hrs · 15,457 cycles

INSPECTION 2C, SUPPORT CRACKED AT BS 2014.982 L2R. R & R SUPPORT CHANNEL IAW SRM 51-35-01 AND SRM 51-33-01 PARA 10. MINOR.

Part: LONGERON SPLICE — CRACKED (CARGO BAY) · airframe 88,173 hrs · 15,457 cycles

INSPECTION 2C, CENTER CARGO LONGERON SPLICE CRACKED AT STA 5-123, LONGERON 51R. R & R LONGERON SPLICE IAW SRM 51-33-01, PARA 8 AND SRM 51-31-01, TABLE 12, PG 35.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 88,173 hrs · 15,457 cycles

INSPECTION 2C, RIGHT WING REAR SPAR SUPPORT FITTING, CRACKED AT APPROX STA XORS 564, OTBD SIDE OF INBD FLAP ACTUATOR SUPPORT. R & R RT WING REAR SPAR SUPPORT FITTING IAW SRM 51-33-01.

Part: STRINGER — CRACKED (LT WING) · airframe 88,173 hrs · 15,457 cycles

INSPECTION 2C, LT WING STRINGER 12 CRACKED AT XORS 637.5. REPAIRED AND R & R ARROW HEAD FITTING IAW SRM 57-00-03, REP 5. MAJOR REPAIR.

Part: LONGERON CLIP — CRACKED (BS 2092) · airframe 88,173 hrs · 15,457 cycles

INSPECTION 2C, AFT BODY FRAME, BS 2092 LONGERON 2R CLIP CRACKED. R & R IAW SRM 51-35-01 AND SRM 51-33-01, PARA 10 MINOR.

Part: STRINGER — CRACKED (RT WING) · airframe 88,173 hrs · 15,457 cycles

INSPECTION 1C, RT WING STRINGER 16 CRACKED BETWEEN XORS 372-402. REPAIRED STRINGER IAW EA 011-5710-01-A5024, REV IR AND EO MD11 5710-53248-A, FAA 8100-9.

Part: STRINGER — CRACKED (RT WING) · airframe 88,173 hrs · 15,457 cycles

INSPECTION 1C, RT WING STRINGER 14 CRACKED AT XORS 506. REPAIRED STRINGER IAW EA 011-5710-01-A5023 REV IR AND EO 5710-53250-A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 86,898 hrs · 15,177 cycles

INSPECTION TYPE:3C, STA 1239, LONGERON 27, LT FLOORBEAM END FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FLOORBEAM END FITTING AT STA 1239, LONGERON 27 LT IAW DWG AEA7357 AND SRM 51-33-01.

Part: CONNECTOR — LOOSE (TIRE PRESSURE)

EMERGENCY DECLARED, DURING DESCENT LEVEL 1 ALERT, TIRE PRESSURE LOW - NR 9 TIRE, PRESSURE INDICATION CONFIG PAGE BLANK. FOUND LOOSE PIN RECEPTICAL AT P1-3676 AT NR 9 POS. SECURED AND PERFORMED SYST TEST OF BTMTP IAW MM 32-46-00-700. SYS TESTS GOOD.

Part: SKIN — DENTED (R1 DOOR) · airframe 85,137 hrs · 14,728 cycles

INSPECTION TYPE:3C, R1 DOOR EXTERIOR SKIN DENTED AT UPPER AFT CORNER. REPAIRED R1 DOOR SKIN AT UPPER AFT CORNER BETWEEN STA YNPD 17.3-5.5 IAW SRM 52-01-01, REPAIR 3, FIG 201.

Part: TRUNNION — CRACKED (NLG) · airframe 85,137 hrs · 14,728 cycles

INSPECTION TYPE: 3C, NLG RT TRUNION FITTING CRACKED. REPAIRED NLG RT TRUNION IAW EA 011-5310-01-A4305 REV.IR AND UPS EO 5310-48760-A. MAJOR.

Part: DOUBLER — CRACKED (LT WING) · airframe 85,137 hrs · 14,728 cycles

INSPECTION TYPE: 3C, LEFT WING FIXED L/E BEADED DOUBLER CRACKED NEAR STA XOS 541. REPAIRED IAW SRM 57-40-02, REPAIR 15 FIG 203. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 85,137 hrs · 14,728 cycles

INSPECTION TYPE: 3C LT WING FIXED L/E BEADED DOUBLER CRACKED NEAR XOS 693. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLERS BETWEEN XOS679-708 IAW STASA EA-011-5730-01-A4303 REV IR AND EO 5730-48823-A, FAA 8100-9. MAJOR.

Part: DOUBLER — CRACKED (LT WING) · airframe 85,137 hrs · 14,728 cycles

INSPECTION TYPE:3C LT WING FIXED L/E BEADED DOUBLER CRACKED NEARS XOS628. REPAIRED IAW SRM 57-40-02, REPAIR 15, FIG 203. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 85,137 hrs · 14,728 cycles

INSPECTION TYPE: 3C, LT WING FIXED L/E COMPT BEADED DOUBLER CRACKED NEAR XOS613. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS 610-616 IAW SRM 57-40-02. REPAIR 15, FIG 203 (MAJOR).

Part: DOUBLER — CRACKED (LT WING) · airframe 85,137 hrs · 14,728 cycles

INSPECTION TYPE: 3C, PREVIOUSLY INSTALLED REPAIR DOUBLER CRACKED IN LT WING FIXED L/E ON STRINGER, NEAR XOS906. REPLACED REPAIR DOUBLER IN LT WING FIXED L/E NEAR XOS906 IAW SRM 57-40-03, REPAIR 1, FIG 201. (MAJOR)

Part: SKIN — CRACKED (LT WING) · airframe 85,137 hrs · 14,728 cycles

INSPECTION TYPE:3C, LT WING FIXED L/E INTERNAL SKIN SPLICE DOUBLER CRACKED NEAR XOS584. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FORMER IAW DWG ARB2931 AND ARM 51-33-01 (MINOR).

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING PRE-FLIGHT EMERGENCY LIGHT TEST, WARNING MESSAGE EMERGENCY LIGHT BATTERY 1 LOW ILLUMINATED. REPLACED EMER LT BATTERY POWER SUPPLY. OPS TESTED OK.

Part: SPRING — BROKEN (L1 DOOR)

MANUAL LIFT BAR ON LT CREW ENTRANCE DOOR IS BROKEN. R & R L1 ENTRY DOOR MANUAL LIFT HANDLE SPRING IAW AMM 20 50 02 2. THIS CLEARS M471384.

Part: DOUBLER — CRACKED (LT WING) · airframe 85,137 hrs · 14,728 cycles

INSPECTION TYPE: 3C, LEFT WING FIXED L/E BEADED DOUBLER CRACKED NEAR XOS 651. REPAIRED IAW SRM 57-40-02, REPAIR 15, FIG 203. (MAJOR)

Part: FLOOR PANEL — DAMAGED · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, FLOOR PANEL 226CF IN COURIER IS DAMAGED IN CORNER. FABRICATED FLOOR PANEL 226CF REF EO MD11-5320-27386-C, APPX A/B.

Part: FLOOR PANEL — CHIPPED (MAIN CABIN) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, MAIN CABIN FLOOR PANEL 261KF CHIPPED ON LOWER SURFACE AT AFT INBD CORNER. FABRICATED FLOOR PANEL 261KF REF EO MD11 5320-27386-C APPX A/B.

Part: FLOOR PANEL — CHIPPED (MAIN CABIN) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, MAIN CABIN FLOOR PANEL 261CF CHIPPED ON LOWER SURFACE AT FWD INBD CORNER. FABRICATED MAIN CABIN FLOOR PANEL 261CF REF EO MD11-5320-27386-C, APPROX A/B.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, RT AFT FUSELAGE HORZ STAB AREA LOWER SKIN HAS CORROSION PANEL AREA 347DF STA2164. REPAIRED RT FUSELAGE UNDER PANEL 347DF AT STA2164 REF SRM 53-70-0 -01, REPAIR 3, FIG 201, REV 47.

Part: SHEAR TIE — CORRODED (BS 1741 L51L-R) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, CENTER CARGO SHEAR TIE HAS CORROSION BETWEEN L-51L TO L51R, STA 1741 ON LOWER AN UPPER FACE OF SHEAR TIE. REPAIRED SHEAR TIE BY FABRICATION AND INSTALLATION OF REPLACEMENT PART REF SRM 53-00-06, REPAIR 1, FIG 202.

Part: LONGERON — CORRODED (BS 1887 L33R) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, AFT CARGO L-33R HAS CORROSION AT STA 1887. REPAIRED LONGERON 33R AT STA 1887 REF STA, SA, EA 011-5310-01-A3367 RE REV I/R AND EO MD11-5310-44048-A.

Part: LONGERON SPLICE — CRACKED (LONGERON 47R) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, CENTER CARGO L47R SPLICE FITTING IS CRACKED AT STA 5-123. REMOVED, FABRICATED AND INSTALLED CENTER CARGO L45R SPLICE FITTING REF SRM 51-33-01 AND DWG A5A7116.

Part: FRAME SPLICE — CRACKED (BS 5-123 L51L) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, CENTER CARGO L51L SPLICE FITTING IS CRACKED AT STA 5-123. REMOVED, FABRICATED AND INSTALLED CENTER CARGO L51L SPLICE FITTING AT STA 5-123 REF 51-33-01 AND DWG A5A7114.

Part: LONGERON SPLICE — CRACKED (LONGERON 45R) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, CENTER CARGO L45R SPLICE FITTING IS CRACKED AND HAS CORROSION. REMOVED, FABRICATED AND INSTALLED CENTER CARGO L45R SPLICE FITTING REF IAW SRM 51-33-01 AND DWG A5A7116.

Part: FRAME SPLICE — CRACKED (BS 5-123 L38R) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, CENTER CARGO LONGERON 38R STA 5-123 SPLICE FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED L38R SPLICE FITTING AT STA 5-123 REF DWG A5A7114 AND SRM 51-33-01.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, LT WING INBD FLAP LOWER SURFACE HAS A CREASE 13" INBD OF SPRING CARTRIDGE. REPAIRED LT WING INBD FLAP LOWER SURFACE CREASE, 13" INBD OF SPRING CARTRIDGE REF STA, SA, EA 011-5730-01-A3341 REV I/R AND EO MD11-5750-43966.-A

Part: DOUBLER — CRACKED (LT WING LE) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, LT WING L/E COMPT BEADED DOUBLER IS CRACKED AT 4EA FASTENERS AT XOS 671 APPROX. REPAIRED LT WING L/E COMPT BEADED DOUBLER AT XOS671 REF EO MD11- 5730-42916-A.

Part: FRAME SPLICE — CORRODED (BS 1865 L48R) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, BULK PIT LOWER BILGE STA 1865 AND L48R SPLICE FITTING HAS CORROSION. R & R 2EA SPLICE FITTINGS AT STA 1865 AND L48R REF DWG NGA6314 REV J AND SRM 51-33-01.

Part: WEB — CRACKED (DOOR FRAME) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C TORQUE BOX WEB CRACKED AT LIGHTNING HOLE AT LOWER AFT CORNER OF L-3 DOOR JAMB. REPAIRED TORQUE BOX WEB AT LIGHTNING HOLE AT LOWER AFT CORNER OF L-3 DOOR JAMB REF STA, SA, EA 011-5330-01-A3316 REV I/R AND EO10-43806-A.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, STA 5-93 AREA LONGERON 30R HAS CORROSION. REPAIRED LONGERON 30R FROM STA 5-73 TO 5-113 REF STA, SA, EA 011- 5310-01-A3334 REV I/R AND EO MD11-5310-44017-A.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, LT WING L/E COMPT CEILING DOUBLER IS CRACKED AT 4EA FASTENERS AT XOS 700. REPAIRED LT WING L/E COMPT BEADED DOUBLER AT XOS700 REF EO MD11- 5730-42916-A.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 825,591 hrs · 4,082 cycles

INSPECTION TYPE:4C, LT WING L/E COMPT CEILING BEADED DOUBLER IS CRACKED AT 2EA FASTENERS AT XOS639 APPROX. REPAIRED LT WING L/E COMPT BEADED DOUUBLER AT XOS639 REF EO MD11- 5730-42916-A.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, LT WING L/E COMPT CEILING BEADED DOUBLER IS CRACKED AT 2EA FASTENERS AT APPX XOS754. REPAIRED LT WING L/E COMPT BEADED DOUBLER AT XOS754 REF EO MD11-5730-42916-A.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, LT WING L/E COMPT BEADED DOUBLER IS CRACKED AT 5 EA FASTENERS AT XOS 732 APPROX. REPAIRED LT WING L/E COMPT BEADED DOUBLER AT XOS732 REF EO MD11- 5730-42916-A.

Part: WEB — CRACKED (DOOR FRAME) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, TORQUE BOX WEB CRACKED AT LIGHTNING HOLE LOCATED AT LOWER FWD CORNER OF L-3 DOOR JAMB. REPAIRED TORQUE BOX LIGHTNING HOLE WEB AT LOWER FWD CORNER OF L-3 DOOR JAMB REF SRM 53-40-15, REPAIR 3, FIG 201, REV 46.

Part: LONGERON SPLICE — CRACKED (BS 1119 L33R) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, FWD CARGO COMPT RT TUNNEL AREA BETWEEN STA 1119 TO STA 6-10 AT L33R LONGERON SPLICE FOUND CRACKED. REMOVED FABRICATED AND INSTALLED FWD LOWER CARGO RT TUNNEL SPLICE FITTING AT STA 1119 TO 6-10 AND L33R REF DWG ARB8426 AND SRM 51-33-01.

Part: DOUBLER — CRACKED (LT WING) · airframe 825,591 hrs · 4,082 cycles

INSPECTION TYPE:4C, LT WING L/E COMPT CEILING BEADED DOUBLER IS CRACKED AT 2EA FASTENERS AT XOS682 APPROX. REPAIRED LT WING L/E COMPT BEADED DOUBLER AT XOS682 REF EO MD11- 5730-42916-A.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 825,591 hrs · 4,082 cycles

INSPECTION TYPE:4C, LT WING L/E COMPT CEILING BEADED DOUBLER IS CRACKED AT 1EA FASTENER AT XOS 664. REPAIRED LT WING L/E COMPT BEADED DOUBLER AT XOS664 REF EO MD11-5730-42916-A.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, LT WING L/E COMPT CEILING BEADED DOUBLER IS CRACKED AT 3EA FASTENERS AT XOS880 APPROX. REPAIRED LT WING L/E COMPT BEADED DOUBLER AT STA XOS880 REF EO MD11-5730-42916-A.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 825,591 hrs · 4,082 cycles

INSPECTION TYPE:4C, LT WING L/E COMPT CEILING BEADED DOUBLER HAS CRACKS AT SEVERAL FASTENERS AT XOS445 APPROX. REPAIRED LT WING L/E COMPT BEADED DOUBLER AT XOS445 REF EO MD11- 5730-42916-A.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, LT WING L/E COMPT CEILING BEADED DOUBLER IS CRACKED AT 3EA FASTENERS AT XOS 689. REPAIRED LT WING L/E COMPT BEADED DOUBLER AT XOS689 REF EO MD11-57 5730-42916-A.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, LT WING L/E COMPT BEADED DOUBLER IS CRACKED AT 4EA FASTENERS AT XOS 646 APPROX. REPAIRED LT WING L/E COMPT BEADED DOUBLER AT XOS646 REF EO MD11-5730-42916-A.

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, RT WING L/E COMPT THROUGH ACCESS 619EB AREA ABOVE SLAT CABLE PULLEY, BEADED DOUBLER FOUND CRACKED. REPAIRED RT WING L/E COMPT BEADED DOUBLER AT ACCESS 619EB ABOVE SLAT CABLE PULLEY REF EO MD11-5730-42916-A.

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, RT WING L/E COMPT THROUGH ACCESS 619EB CEILING AREA FOUND BEADED DOUBLER CRACKED. REPAIRED RT WING L/E COMPT BEADED DOUBLER AT ACCESS 619EB REF EO MD11-5730-42916-A.

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, RT WING L/E COMPT INBD OF SLAT TRACK NR11, BEADED DOUBLER FOUND CRACKED. REPAIRED RT WING L/E COMPT BEADED DOUBLER INBD OF SLAT TRACK NR 11 REF EO MD11-5730-42916-A.

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, RT WING L/E COMPT THROUGH ACCESS 619CB AREA ABOVE INBD FUEL RECEPTICAL FOUND BEADED DOUBLER CRACKED. REPAIRED RT WING L/E BEADED DOUBLER AT ACCESS 619CB REF EO MD11-573 0-42916-A.

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, RT WING L/E COMPT INBD OF SLAT TRACK NR 12 BEADED DOUBLER FOUND CRACKED. REPAIRED RT WING L/E BEADED DOUBLER INBD OF SLAT TRACK NR 12 REF EO MD11-5730-42916-A.

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, RT WING L/E INBD OF SLAT TRACK NR16 BEADED DOUBLER FOUND WITH CRACKS. REPAIRED RT WING L/E BEADED DOUBLER OTBD OF SLAT TRACK 16 REF EO MD11-5730-42916-A.

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, RT WING L/E COMPT THROUGH ACCESS 619CB AREA ABOVE OTBD FUEL RECEPTICAL FOUND BEADED DOUBLER CRACKED. REPAIRED RT L/E BEADED DOUBLER AT ACCESS 619CB REF EO MD11-5730-42916-A.

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 82,559 hrs · 14,082 cycles

INSPECTION TYPE:4C, RT WING L/E COMPT OTBD OF SLAT TRACK NR 10 BEADED DOUBLER FOUND CRACKED. REPAIRED RT WING L/E BEADED DOUBLER OTBD OF SLAT TRACK NR 10 REF EO MD11-5730-42916-A.

Part: COVER — BROKEN (L1 DOOR)

LT ENTRY DOOR WILL NOT DISARM M455727. R & R L1 DOOR LWR COVER IAW MM 25-23-07-4 1.

Part: SKIN — CRACKED (FUSELAGE)

RT SIDE (3) ACFT BAY DOOR FRAME UPPER AFT CORNER FUSELAGE SKIN CRACKED. CRACK IS APPROX 1.5" IN LENGTH AND TRAVELS THROUGH ONE FASTENER HOLE. REMOVED DAMAGE AND REPAIRED IAW EO MD11-5330-41314.

Part: STRUCTURE — DAMAGED (LT WING TE FLAP)

LT INBD FLAP DAMAGED. REPAIRED IAW EO MD11-5750-40990-B.

Part: COVER — CRACKED (EMERGENCY LIGHT)

L1 EMERGENCY EXIT LIGHT BROKEN. R & R L1 EXIT (EMERGENCY) LENS COVER ASSY IAW AMM 33-2 7-05-04.

Part: SIGN — DISLODGED (EMERGENCY LIGHTS)

EMERGENCY EXIT SIGN ABOVE L1 DOOR FELL OFF AFTER LANDING. SECURED THE EXIT SIGN AND CHECK OK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

EMERGENCY LIGHT BATT ONE LOW ALERT (LEVEL ONE) DEF IAW MEL 33-50-4. PLACARD INSTALLED OK TO CONTINUE. T/S IAW FIM 33-51-02-00, FIG 104, BLOCK 1,2,6 FOUND MSG EMERGENCY LIGHT BATTERY 1 LOW. R & R EMERGENCY LIGHTS POWER SUPPLY. OPS CHECK SATIS. THIS CLOSES DMI.

Part: SKIN — PUNCTURED (LT WING) · airframe 80,158 hrs · 13,494 cycles

INSPECTION TYPE:1C, PANEL ARC0583 ON LT WING T/E UPPER SURFACE HAS HOLE ACCOMPLISHED REPAIR ON LT WING T/E UPPER SURFACE SKIN PANEL ARC0583 IAW SRM 57-00-01, FIG 201, SHEETS 1&2.

Part: SKIN — CRACKED (LT WING) · airframe 80,158 hrs · 13,494 cycles

INSPECTION TYPE:1C, LT WING TELESCOPIC DUCT CUTOUT CRACKED UPPER INBD AND OTBD CORNER. REMOVED DAMAGE, FABRICATE, AND INSTALLED REPAIR FILLERS AND DOUBLER IAW STA SA EA 011-5730-01-A2490 I/R AND EO MD11-5730-38326-A.

Part: SKIN — CRACKED (RT WING L/E) · airframe 44,124 hrs · 6,909 cycles

INSPECTION TYPE:1C, RT WING TELESCOPIC DUCT CUTOUT UPPER IB CORNER CRACKED. TRIMMED OUT DAMAGE ON RT WING FIXED L/E TELESCOPIC DUCT CUTOUT INBD AND OTBD CORNERS BETWEEN STA XOS 464-470. FABRICATED AND INSTALLED REPAIR REF EA 011-5730-01-A2491 AND EO MD11-5730-38327-A.

Part: SKIN — DENTED (L1 DOOR) · airframe 80,158 hrs · 13,494 cycles

INSPECTION TYPE:1C, DEFERRED ITEM D 421851: L-1 CREW ENTRY DOOR SKIN UPPER EDGE REPAIR. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 52-10-01, REPAIR 3, FIG. 201.

Part: STRUCTURE — DAMAGED (L1 DOOR)

DOOR DAMAGED AT FWD UPPER CORNER AT L1 DOOR. COMPLIED WITH L1 CREW DOOR REPAIR IAW EO MD11-5210-37125-A.

Part: WEDGE — DAMAGED (LT WING TE FLAP)

LEFT WING I/B TRAILING EDGE FLAP T/E WEDGE ASSY DAMAGED. REPAIRED PER EO MD11-5750-35554-A.

Part: SKIN — CRACKED (RT WING) · airframe 78,142 hrs · 12,925 cycles

INSPECTION TYPE:C RT WING FIXED L/E UPPER SKIN FOUND CRACKED DURING BEADED DOUBLER REPAIR AT STA XORS 571, SLAT TRACK NR 10 VICINITY. CRACK AT AFFECTED AREA TRIMMED OFF PER EN 1234-09. HFEC AND 10X VISUAL INSP C/O ON TRIMMED EDGE, FOUND NO CRACK OR CORROSION. EXT REPAIR DOUBLERS AND FILLER FAB PER EN 1234-09. REPAIR PARTS INSTALLED AS PER EN1234-09.

Part: STIFFENER — CRACKED (BS 571) · airframe 78,142 hrs · 12,925 cycles

INSPECTION TYPE:C RT WING FIXED L/E LOWER COMPT STIFFENER FOUND CRACKED DURING BEADED DOUBLER REPAIR AT APPROX STA 571, SLAT TRACK NR 10 VICINITY. RT WING FIXED L/E LWR COMPT AT APPROX STA 571, SLAT TRACK NR 10 CRACKED STIFFENER REMOVED AND TRIMMED OFF. HFEC AND 10X VISUAL INSP C/O FOUND NO CRACK OR CORROSION. REPAIR STRAP, FILLER, EXT DOUBLER, STRINGER SPLICE FABRICATED. REPAIR PARTS INSTALLED AS PER EN 1234-09.

Part: SKIN — DAMAGED (AFT CARGO DOOR) · airframe 78,142 hrs · 12,925 cycles

INSPECTION TYPE:C AFT CARGO DOOR, UPON REMOVAL OF DOOR SKIN, 3 INCHES BELOW PLANE NR 2 FOUND EXISTING HOLE FALL ON THE RADIUS OF THE FRAME. REFER TO IPXA EO MD11-5230-33479-A AND SCO EN 1201-09 FOR DISPOSITION. NOTE: REFER TO SASCO EARN: N285UP-0001 (ON NRC: MD040061) FOR DETAILS.

Part: SKIN — DAMAGED (AFT CARGO DOOR) · airframe 78,142 hrs · 12,925 cycles

INSPECTION TYPE:C AFT CARGO DOOR, UPON REMOVAL OF DOOR SKIN, 4 INCHES BELOW PLANE NR 2 FOUND EXISTING HOLE FALL ON THE RADIUS OF THE FRAME. REFER TO EO MD11-5230-33479-A AND EN 1201-09 FOR DISPOSITION.

Part: SKIN — DAMAGED (AFT CARGO DOOR) · airframe 78,142 hrs · 12,925 cycles

INSPECTION TYPE:C AFT CARGO AT STA 1947, UPON REMOVAL OF AFT CARGO DOOR SKIN FOUND FRAME WITH ELONGATED HOLE AS MARKED. REFER TO IPXA EO MD11-5230-33479-A AND SCO EN 1201-09 FOR DISPOSITION. NOTE: REFER TO SASCO EARN N285UP-001 (NRC: MD040061) FOR DETAILS.

Part: LONGERON — CORRODED (BS 1641 L51R) · airframe 78,142 hrs · 12,925 cycles

INSPECTION TYPE:C CTR CARGO COMPT RT L51 AT STA 1641 FOUND CORROSION AS MARKED. CORROSION ON LONGERON 51 RT STA 1641. REMOVED AND REPLACED AND FOUND EXCEED LIMIT PER SRM 53-20-00, FIG 4, VOL I, REV 40. DAMAGED LONG TRIM-OUT FROM STA 1631-1651RH (L51). HFEC INSPECTION C/O ON TRIM OUT AREA, FOUND NO CRACK EVIDENT. NEW LONG AND 2 REPAIR SPLICE FABRICATED. FPI C/O ON FABRICATED LONG AND REPAIR SPLICE, FOUND NO CRACK EVIDENT. NEW LONG AND REPAIR SPLICE INSTALLED.

Part: SKIN — MISREPAIRED (RT WING) · airframe 78,142 hrs · 12,925 cycles

INSPECTION TYPE:C REPAIR SEQUENCE NBR 285-W4-016, RT WING, FIXED L/E ACCESS PANEL NR 615DB, NEEDS VALIDATION FOR REPAIR. BASE ON INFO COLLECTED IN EO MD11-5100-30530-B, REPAIR SEQ NBR 285-W4 -016 DOES NOT CORRELATE WITH SRM REPAIR. EXISTING REPAIR AT ACCESS PANEL 615DB REMOVED PER EN1229-09. 10X VISUAL AND HFEC INSP C/O FOUND NO CRACK OR CORROSION. NEW REPAIR DOUBLER AND FILLER FAB AND INSTALLED PER EN1229-09.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 78,142 hrs · 12,925 cycles

INSPECTION TYPE:C LT WING L/E LOWER ACCESS NR 519CB COMPT FOUND BEADED DOUBLER CRACKED AS MARKED, STA XORS 528 APPROX. DAMAGED AREA AT BEADED DOUBLER TRIM OFF AS PER SRM 57-10-00, FIG 27, VOLI, REV40. HFEC INSP C/O ON TRIM OUT EDGE AND FOUND NO CRACK EVIDENT. REPAIR ANGLES, REPAIR FILLER AND REPAIR DOUBLER FABRICATED AND INSTALLED AS PER SRM 57-10-00, FIG 27, VOL I, REV 40.

Part: DOUBLER — CRACKED (RT WING) · airframe 78,142 hrs · 12,925 cycles

INSPECTION TYPE:C RT WING L/E LOWER ACCESS NR 619DB COMPT FOUND BEADED DOUBLER CRACKED AS MARKED, STA XORS 573 APPROX OTBD OF SLAT TRACK NR 10. DAMAGE AREA AT BEADED DOUBLER TRIM OFF PER SRM 57-10-00, FIG 27, VOL I REV40. HFEC INSPECTION C/O ON TRIMMED EDGE AND FOUND NO CRACK EVIDENT. REPAIR ANGLES, REPAIR FILLER AND REPAIR DOUBLER FABRICATED. REPAIR PARTS HOLES PICKED UP, PROTECTED AND PAINTED. REPAIR PARTS INSTALLED PER SRM 57-10- 00, FIG 27, VOL I, REV 40.

Part: DOUBLER — CRACKED (XORS 536) · airframe 78,142 hrs · 12,925 cycles

INSPECTION TYPE:C LT WING L/E LOWER ACCESS NR 519CB COMPT FOUND BEADED DOUBLER CRACKED AS MARKED, STA XORS 536 APPROX. DAMAGE AREA AT BEADED DOUBLER TRIM OFF PER SRM 57-10-00, FIG 27, VOL I, REV 40. HFEC INSP C/O ON TRIMMED OUT EDGE AND FOUND NO CRACK EVIDENT. REPAIR ANGLES, REPAIR FILLER AND REPAIR DOUBLER FABRICATED PER SRM 57-10-00 FIG 27, VOL I, REV 40. REPAIR PARTS HOLES PICKED-UP, PROTECTED AND PAINTED. REPAIR PARTS INSTALLED PER SRM 57-10-00 FIG 27, VOL I, REV 40.

Part: SKIN — MISREPAIRED (TE FLAP FAIRING) · airframe 78,142 hrs · 12,925 cycles

INSPECTION TYPE:C REPAIR SEQUENCE NBR 285-W3-013 LHW INBD FLAP INBD FAIRING INNER LWR SKIN FLUSH REPAIR SPLICE SECTION ON SCREW HOLE. REPAIR NEEDS VALIDATION. BASED UPON COLLECTED INFO, REPAIR SEQ NBR 285-W3-013 DOES NOT CORRELATE TO ANY SRM REPAIR. LHW INBD FLAP INBD FAIRING SKIN REMOVED PER EN 1223-09. 10X VISUAL AND HFEC INSPECTION C/O ON DISCREPANT AREA AND TRIM EDGE, FOUND NO CRACK AND CORROSION. NEW SKIN, SPLICE DOUBLER, REPAIR DOUBLER FABRICATED AND INSTALLED PER EN 1223-09.

Part: WEDGE — MISREPAIRED (RT WING TE FLAP) · airframe 78,142 hrs · 12,925 cycles

INSPECTION TYPE:C REPAIR SEQUENCE NUMBER 285-W4-012, RT WING, INBD FLAP, INBD T/E, NEEDS VALIDATION FOR REPAIR. BASED UPON COLLECTED INFO, REPAIR SEQ NBR 285-W4-012 DOES NOT CORRELATE TO SRM 57-20-00, FIG 3, VOL I, REV 40. EXISTING REPAIR REMOVED PER SRM 51-31-01 VOL II, REV 40. NEW WEDGE AND CLIP FABRICATED. REPAIR PARTS INSTALLED PER SRM 57-20-00, FIG 3, VOL I, REV 40.

Part: SKIN — MISREPAIRED (RT WING TE FLAP) · airframe 78,142 hrs · 12,925 cycles

INSPECTION TYPE:C REPAIR SEQUENCE NUMBER 285-W4-010, RT WING, INBD FLAP TOP SURFACE AT XIFH 145, NEEDS VALIDATION FOR REPAIR. BASED UPON COLLECTED INFO, REPAIR SEQ NBR 285-W4-010 DOES NOT CORRELATE TO SRM 57-10-00, FIG 38, VOLI, REV40. EXISTING REPAIR DOUBLER REMOVED PER SRM 51-31-01, VOLII, REV40. 10X VISUAL AND HFEC INSP C/O ON DISCREPANT AREA, FOUND NO CRACK AND CORROSION. NEW REPAIR DOUBLER FAB AND INSTALLED PER EN 1218-09.

Part: SKIN — MISREPAIRED (LT WING LE) · airframe 78,142 hrs · 12,925 cycles

INSPECTION TYPE:C REPAIR SEQUENCE NBR 285-W3-004 LHW FIXED LEADING EDGE TOP SURFACE STA 247 REPAIR DOUBLER NEEDS VALIDATION. BASED UPON COLLECTED INFO, REPAIR SEQ NBR 285-W3-004 DOES NOT CORRELATE TO SRM 57-10-00 FIG 24, VOLI, REV40. EXISTING REPAIR REMOVED. 10X VISUAL INSPECTION AND HFEC INSP C/O, FOUND NO CRACK AND CORROSION. FAB NEW REPAIR DOUBLER PER EN1210-09, WITH HOLES PICK-UP AND PAINTED. NEW REPAIR PARTS INSTALLED AS PER EN 1210-09.

Part: WEDGE — MISREPAIRED (LT WING AILERON) · airframe 78,142 hrs · 12,925 cycles

INSPECTION TYPE:C REPAIR SEQUENCE NBR 285-W3-007 LHW INBD AILERON TRAILING WEDGE STA XIA 312.342 SECTION REPAIR NEED VALIDATION. BASED UPON COLLECTED INFO, REPAIR SEQ NBR 285-W3-007 DOES NOT CORRELATE TO SRM 57-20-00, FIG3, VOLI, REV40. EXISTING REPAIR WEDGE REMOVED PER SRM 51-31-01, VOL II, REV 40. TRAILING EDGE WEDGE TRIM OFF. NEW WEDGE AND 02 EA CLIPS FABRICATED AND INSTALLED PER SRM 57-10-00 FIG3, VOL I, REV 40.

Part: SKIN — MISREPAIRED (LT WINGLET) · airframe 78,142 hrs · 12,925 cycles

INSPECTION TYPE:C REPAIR SEQUENCE NBR 285-W3-001 LHW UPPER WINGLET LEADING EDGE TOP END REPAIR DOUBLER NEEDS VALIDATION. BASE ON EO MD11-5100-30530-B, REPAIR SEQ NR 285-W3-001 DOES NOT CORRELATE TO ANY SRM REPAIR. EXISTING REPAIR AT LHW UPPER WINGLET L/E REMOVED PER EN 1211-09. HOLE WITH SHORT EDGE TRIM OFF WITH 0.5 RADIUS 10X VISUAL INSP AND HFEC C/O ON DISCREPANT AREA AND FOUND NO CRACK OR CORROSION. NEW REPAIR DOUBLER AND FILLER FABRICATED AND INSTALLED PER EN 1211-09.

Part: SKIN — MISREPAIRED (RT WING TE FLAP) · airframe 78,142 hrs · 12,925 cycles

INSPECTION TYPE:C REPAIR SEQUENCE NUMBER 285-W4-011, RT WING, INBD FLAP TOP SURFACE AT XIFH 228, NEEDS VALIDATION FOR REPAIR. BASED UPON COLLECTED INFO, REPAIR SEQ NBR 285-W4-011 DOES NOT CORRELATE TO SRM 57-10-00 FIG 38, VOLI, REV40. RHW INBD FLAP TOP SURFACE AT XIFH 228 EXISTING REPAIR DOUBLER REMOVED. 10X VISUAL AND HFEC INSP C/O, FOUND NO CRACK AND CORROSION. NEW REPAIR DOUBLER FAB AND INSTALLED PER EN 1218-09.

Part: SKIN — MISREPAIRED (RT WING LE) · airframe 78,142 hrs · 12,925 cycles

INSPECTION TYPE:C REPAIR SEQUENCE NUMBER 285-W4-007, RT WING, INBD TOP FIXED L/E AT XFS 231, NEEDS VALIDATION FOR REPAIR. BASED UPON COLLECTED INFO, REPAIR SEQ NBR 285-W4-007 DOES NOT CORRELATE TO SRM 57-10-00, FIG 24, VOL I, REV 40. EXISTING REPAIR AT DISCREPANT AREA. REMOVED PER EN 1217-09. 10X VISUAL AND HFEC INSPECTION C/O ON CUT OUT AREA, FOUND NO CRACK OR CORROSION. NEW REPAIR DOUBLER FABRICATED AND INSTALLED PER EN 1217-09.

Part: WEDGE — MISREPAIRED (RT WING AILERON) · airframe 78,142 hrs · 12,925 cycles

INSPECTION TYPE:C REPAIR SEQUENCE NBR 285-W4-015, RT WING, INBD AILERON INBD T/E, NEEDS VALIDATION FOR REPAIR. BASED UPON COLLECTED INFO, REPAIR SEQ NBR 285-W4-015 DOES NOT CORRELATE TO SRM 57-20-00, FIG3, VOLI, REV40. EXISTING REPAIR WEDGE REMOVED PER SRM 51-31-01, VOLII, REV40. TRAILING EDGE WEDGE TRIM OFF. NEW WEDGE AND NEW CLIP FABRICATED. REPAIR PARTS INSTALLED PER SRM 57-20-00 FIG 3 VOL I, REV 40.

Part: DOUBLER — MISREPAIRED (STA XORS 402-433) · airframe 78,142 hrs · 12,925 cycles

INSPECTION TYPE:C REPAIR SEQUENCE NBR 285-W3-011 LWH REPAIR DOUBLER AT FIXED LEADING EDGE STA XORS 402-433 NEEDS VALIDATION. BASED UPON COLLECTED INFO, REPAIR SEQ NBR 285-W3-011 DOES NOT CORRELATE TO ANY SRM REPAIR. EXISTING REPAIR AT LHW FIXED L/E REMOVED. 10X INSPECTION C/O AND FOUND NO CRACK EVIDENT. NEW REPAIR SKIN, 2 EA EXT STRAPS, 3 INT SPLICES, 2 SPLICE DOUBLERS AND 1 EA FILLER FAB AND INSTALLED PER EN1222-09.

Part: SKIN — MISREPAIRED (BS 374) · airframe 78,142 hrs · 12,925 cycles

INSPECTION TYPE:C REPAIR SEQUENCE NUMBER 285-F1-013, FWD LWR FUSELAGE SKIN STA 374 (AFT OF FAC DR), NEEDS VALIDATION FOR REPAIR. BASED UPON INFO COLLECTED, REPAIR SEQ NBR 285-F1-013 DOES NOT CORRELATE TO ANY SRM REPAIR. EXISTING DOUBLER AT STA 374-383 REMOVED PER SRM 51-33-01 VOL II, REV 40. HFEC INSPECTION AND 10X VISUAL INSPECTION C/O, FOUND NO CRACK OR CORROSION. 02 EA REPAIR DOUBLERS, FILLER AND CONICAL WASHERS FAB AND INSTALLED PER SRM 53-20-00, FIG 2, VOL I, REV 40.

Part: SKIN — MISREPAIRED (AFT CARGO DOOR) · airframe 78,142 hrs · 12,925 cycles

INSPECTION TYPE:C REPAIR SEQUENCE NUMBER 285-F1-003, AFT CARGO DR, LWR FWD DR SKIN SURFACE, NEEDS VALIDATION FOR REPAIR. BASE UPON COLLECTED INFO, REPAIR SEQ NR 285-F1-003 DOES NOT CORRELATE TO ANY SRM REPAIR. EXISTING DOUBLER AT AFT CARGO DR, LWR FWD DOOR EXT SKIN REMOVED. DISCREPANT DR LWR SKIN TRIM-OUT. REPAIR SKIN, DOUBLER AND INTERNAL DOUBLER FABRICATED, DISCREPANT HOLES ON SUPPORTS AND PAN REAMED TO REQ DIA PER EN1201-09. BUSHING, SKIN AND SPLICE DOUBLER FABRICATED AND INSTALLED.

Part: SKIN — MISREPAIRED (BS 1195) · airframe 78,142 hrs · 12,925 cycles

INSPECTION TYPE:C REPAIR SEQUENCE NUMBER 285-F1-011 RT LWR FUSELAGE SKIN STA 1195 LONGERON 50R NEEDS VALIDATION FOR REPAIR. BASED UPON COLLECTED INFO, REPAIR SEQ NBR 285-F1-011 DOES NOT CORRELATE TO ANY SRM REPAIR. EXISTING REPAIR DOUBLER REMOVED PER SRM 51-33-01, VOL II, REV 40. HFEC AND 10X VISUAL INSP C/O ON DOUBLER REMOVED AREA, FOUND NO CRACK OR CORROSION. REPAIR DOUBLER AND CONICAL WASHERS FAB AND INSTALLED PER EN 1206-09.

Part: SKIN — MISREPAIRED (BS 1761 - 1801) · airframe 78,142 hrs · 12,925 cycles

INSPECTION TYPE:C REPAIR SEQUENCE NUMBER 285-F1-004, LT LWR FUSELAGE SKIN STA 1761 - 1801 LONGERON 37L - 41L. NEEDS VALIDATION FOR REPAIR. BASED UPON COLLECTED INFO, REPAIR SEQ NR 285-F1-004 DOES NOT CORRELATE TO ANY SRM REPAIR. EXISTING REPAIR DOUBLER REMOVED. HFEC AND 10X VISUAL INSP C/O ON REMOVE AREA FOUND NO CRACK OR CORROSION. 02 REPAIR DOUBLERS, 06 EA FINGER DOUBLERS FAB AND CONICAL WASHERS FABRICATED AND INSTALLED PER EN 1203-09.

Part: SKIN — MISREPAIRED (BS 1129) · airframe 78,142 hrs · 12,925 cycles

INSPECTION TYPE:C REPAIR SEQUENCE NR 285-F1-012. LT LWR FUSELAGE SKIN STA 1129 LONGERON 46L-44L NEEDS VALIDATION FOR REPAIR. BASED UPON COLLECTED INFO, REPAIR SEQ NBR 285-F1-012 DOES NOT CORRELATE TO ANY SRM REPAIR. EXISTING REPAIR DOUBLER REMOVED. HFEC AND 10X VISUAL INSP C/O FOUND NO CRACK OR CORROSION. EXISTING TRIM-OUT AREA REWORKED WITH A DIMENSION CUT-OUT 11-3/8 INCH BY 12 INCH AND 1 INCH MIN RADIUS. REPAIR DOUBLER, FINGER DOUBLERS AND FILLERS FAB AND INSTALLED.

Part: SKIN — MISREPAIRED (BS 1278) · airframe 78,142 hrs · 12,925 cycles

INSPECTION TYPE:C REPAIR SEQUENCE NUMBER 285-F1-010 LWR FUSELAGE STA 1278 BETWEEN LONG 47L TO 46L NEEDS VALIDATION REPAIR. BASED UPON COLLECTED INFO, REPAIR SEQ NBR 285-F1-010 DOES NOT CORRELATE TO ANY SRM REPAIR. EXISTING REPAIR DOUBLER REMOVED WITH HFEC AND 10X VISUAL INSPECTION C/O, FOUND NO CRACK OR CORROSION. REPAIR DOUBLER AND CONICAL WASHERS FABRICATED AND INSTALLED PER EN1205-09.

Part: SMOKE DETECTOR — INTERMITTENT (CABIN)

INSPECTION TYPE:N/A ATB - CABIN SMOKE DETECTOR WARNING WAS INTERMITTENT AFTER LEVEL OFF. NO SMOKE INDICATION VISUALLY NOTED. INDICATION DID NOT OCCUR DURING LAST HALF HOUR OF FLIGHT. BRIEF WITH FLT CREW - NR 1 SMOKE DETECTOR MAIN DECK WARNING INTERMITTENT. NR 1 SMOKE DETECTOR REPLACED PER MM 26-15-01, TEST OK.

Part: DOOR — STUCK

L1 CREW ENTRY DOOR WILL NOT OPEN. DEFERRED PER MEL M374808 ASSIGNED. FOUND CONNECTOR BROKEN OFF OF UPLIMIT SWITCH. REPLACED SWITCH. OPS CHECK GOOD, REF MM 52-11-02. THIS CLEARS M374808. PLACARD PULLED.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,183 hrs · 12,288 cycles

INSPECTION TYPE:C CENTER ACCESSORY COMP STR 45L CORRODED AT FRAME FWD OF DOOR 131AB F/S1129/6-90. REPAIRED STRINGER 45L IAW MAINTENANCE MANUAL 52-31-00-02 PARA 2 TASK 52-31-00-00-801.

Part: INDICATOR — ERRATIC (AIRSPEED)

ATB - PASSING THRU 10000 FT (FL100) NOTED ALT COMPARATORS ON BOTH PFD, THEN A/S COMPARATOR ALTIMETERS WERE IN ERROR OF UP TO 150-180 FT. FCP PANEL FUNCTIONS WENT TO DASHES. PERFORMED AIRSPEED, LOST, SUSPECT ERRATIC. REMOVED AND REPLACED ADC NR 2 IAW AMM 34-16-01-4. SEE P/N S/N OFF BELOW. REMOVED AND REPLACED FO'S PITOT TUBE IAW AMM 34-11-01-2, P/N OFF: 851DK, S/N OFF: 246454. REMOVED AND REPLACED RT AOA SENSOR IAW AMM 27-35-02-4, P/N OFF: 2568A13, S/N OFF: 038-2A.

Part: SLIDE — UNWANTED DEPLOY (L1 DOOR)

L1 DOOR SLIDE BLOWN. REMOVED AND REPLACED SLIDE PER AMM 25-61-15-4. SERVICE PAX DOOR PNEU BOTTLE PER AMM 12-25-04-3. OPERATIONAL CHECK OF L1 DOOR PER AMM 52-11-02-2. FOUND OK. ARM/DISARM LEVER CHECKED NORMAL.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS)

EMERGENCY LIGHTING SYS 1 FAILED. DEFERRED PER MEL M348451. [SUP 4-20-07] REPAIRED WIRE TO CONNECTOR P1-328 BATTERY LOWER CHANGE. EMERGENCY EXIT LIGHTS TEST PASS. DEFERRAL CLOSED.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS)

PREFLIGHT - WHEN TESTING EMERGENCY LIGHT SYSTEM, MESSAGE SAYS -NO 1 BAT LO-. REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPPLY PER AMM 33-51-01-4. FOLLOWED FIM 33-51-02-00. REMOVED AND REPLACED MSC PRECAUTIONARY AS PER AMM 31-42-01-4. EMERGENCY LIGHTS AND MSC TEST GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)

INSPECTION TYPE:N/A EMERGENCY LIGHT BATTERY 1 LOW WARNING (LVL 1) PRESENT DURING EMERGENCY LIGHT TEST (PREFLIGHT). T/S AS PER FIM 33-51-02-00, FOUND POWER SUPPLY FAULTY. REMOVED AND REPLACED FAULTED BATTERY, EMERGENCY LIGHT OPS CHECKED SATISFACTORY PER MM 33-51-01-4.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

ON AS-N FOUND EMERGENCY LIGHT BATTERY LOW WARNING DURING EMERGENCY LIGHT TEST. REMOVED AND REPLACED EMERGENCY BATTERY POWER SUPPLY IAW MM 33-52-01. OPS CHECK NORMAL.

Part: UNKNOWN — UNKNOWN (EMERGENCY LIGHTS)

INSPECTION TYPE:N/A EMERGENCY LIGHT BATTERY LOW ALERT DISPLAYED. EMERGENCY LIGHTING SYSTEM DEFERRED PER MEL 33-50-4, PLACARD INSTALLED M343837.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

EMERGENCY LIGHT "BAT 1 LOW LVL 1" WARNING ILLUMINATED. DEFERRAL NR M341506. PER WDM 33-51-01 WIRE CONTINUITY CK FOR EMER LT CONTROL SYSTEM CONDITION NML. REPLACED EMERG LT BATTERY POWER SUPPLY RELAYS PER AMM 33-51-01-4. REPLACE EMERG LT POWER SUPPLY AND RECHARGEABLE BATTERY PER AMM 33-51-01-5. EMERGENCY LT TEST PASS.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

EMERGENCY LIGHT BATTERY LOW DURING EMERGENCY TEST. DEFERRED EMERGENCY LIGHT SYSTEM IAW MEL 33-50-4. PLACARD INSTALLED, D339480. REPLACED BATTERY PER MM 33-50-01-4.

Part: LIGHT — NO TEST (CABIN)

INSPECTION TYPE:C EMERGENCY LIGHTS WILL NOT TEST. MSC R5-1114B PIN 13K FOUND PUSH BACK. PIN 13K REWORKED AS PER SWPM 20 -20-2 REV 15, SATIS. EMERG LIGHTING TEST CARRIED OUT AS PER AMM 33-50-00 REV 55 SATIS.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT)

INSPECTION TYPE:N/A EMERGENCY LIGHTS WILL NOT TEST. *S/D* PIN 13K FOUND PUSHED BACK. PIN 13K REWORKED AS PER SWP 20-20-02 REV 15 SATISFACTORY. EMERGENCY LIGHT TEST CUTOUT AS PER AMM 33-50-00 RE 55 SATISFACTORY.

Part: SKIN — DENTED (BS 380) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C FWD FUSELAGE BOTTOM AREA AT STA 380 APPROX (AFT SIDE OF FAC CUTOUT) FOUND DENT AS MARKED, STA 380 LWR BOTTOM DENT AREA FASTENERS. REMOVED AS PER SRM 53-20-00 FIG 2 V.I AND SRM 51-31-01 V.II R.38.BOTTOM MATERIAL TRIMMED OFF AS PER SRM 53 -20-00 FIG 2 V.I R.38. HFEC INSP C/O PER DAC NDTSPM R.12 06-10-01.001 ON TRIMMED OUT AREA FOUND NO CRACK EVIDENT. FAB DOUBLER AND FILLER INSTALLED AS PER SRM 53-20-00 FIG 2 VOL.I REV 38.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C CTR CGO AFT CUT-OUT CENTER AREA FOUND WITH BLEND OUT. CUSTOMER REQUEST TO INSTALL DOUBLER PER SRM. SKIN BLEND OUT MAT`L TRIM OFF PER SRM 53-50-00 FIG 16 V.I R.38. HFEC C/O IAW DAC NDT SPM R.12 PART 06-10-01.001 ON TRIMMED EDGE AND FOUND NO CRACK EVIDENT. REPAIR FILLER AND DOUBLERS FAB AND FASTENERS HOLES PICKED UP PER SRM 53-50-00 FIG 16 VI R38 AND SRM 51-31-01 V.II R.38. REPAIR DOUBLER AND AREA FASTENERS PER SRM 53-50-00 FIG 16 V.I R.38/51-33-01 V.II R.38.

Part: STRUT — CORRODED (FUSELAGE) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C FWD CARGO, DURING CARRY-OUT OF WORK AT AFT BULKHEAD, AFTER REMOVAL OF ANCHOR NUT, FOUND CORROSION AT STRUT AT STA 6-72, X=18.25 LT AT FLOOR LEVEL AS MARKED FWD CARGO STA 6-72,X=18.25 LT FLOOR LEVEL CORROSION STRUT ATTACH PARTS REMOVED PER SRM 51-31-01 V.II R.38. BADLY CORRODED STRUT TRIMMED OFF PER SRM 53-00-01 FIG 7 V.II R.38. REPAIR FILLER, STRAP ANGLE FAB PER SRM 53-00 01 FIG 7 V.II R.38. REPAIR PARTS INSTALLED PER SRM 53-00-01 FIG 7 V.I R. 38 AND ATTACH PARTS REINSTALLED PER SRM 51-33-01 V.II R.38.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C RT HORIZ STAB FOUND NR 27 BARREL NUT BORE CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOL II R38. BORE REAMED TO 1.178 DIA REMAINING BLEND OUT 0.070 DEEP, BOTTOM SURF CLEANED FOUND EXCEED EO LIMITS. B/N BORE BLEND OUT AND BOTTOM PERI RADIUS SMOOTHEN AND PROTECTED PER EO F IG 5. REPAIR BUSHING FAB, PROTECTED AND INSTALLED PER EO FIG 5. REPAIR C/O AT B/N BORE NR 27 RT ACCEPTABLE IAW EN1338-06.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C RT HORIZ STAB FOUND NR 30 BARREL NUT BORE CORRODED CORROSION AT B/N BORE REMOVED PER SRM51-21-01 V.II R.38. BORE REAMED TO 1.178"DIA. REMAINING BLEND OUT FOUND EXCEEDED LIMITS PER EO MD11-551 -19409K. REPAIR SLEEVE BUSHING FAB AND PROTECTED PER EO MD11-5510-19409 K. REPAIR SLEEVE BUSHING INSTALLED PER EO MD11-5510-19409K. REPAIR C/O AT BARREL NUT BORE NR 30 RT IS ACCEPTABLE PER EN 1337-06.

Part: SHEAR TIE — CORRODED (BS 1721 L49L-49R) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C CTR CARGO, STA 1721, LONGERON L49-R49 FRAME SHEAR TIE CORROSION AS MARKED CTR CARGO STA 1721 LONGERON L-49-R49 FRAME CORROSION SHEAR TIE ATTACH SUPPORT AND FASTENERS REMOVED PER SRM 51-31-01 V.II R.38.CORROSION SHEAR TIE REMOVED PER SRM 51-31-01 V.II R.38. NEW SHEAR TIE P/N ADA0112-23 FAB PER DWG ADA0112. NEW SHEAR TIE INSTALLED AND ATTACHED PARTS REINSTALLED PER SRM 51-31-01 V.II R.38 AND DWG ADA0112.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C LT HORIZ STAB FOUND NR 28 BARREL NUT BORE CORRODED CORROSION REMOVED AT B/N BORE AS PER SRM 51-21-01 V.II R.38. BORE REAMED TO 1.178" DIA REMAINING BLEND OUT 0.015" DEEP, BOTTOM SURFACE CLEANED, REMAINING BLEND OUT 0.045" DIA DEEP FOUND EXCEEDED LIMIT PER EO MD11-5510- 19409K. REPAIR SLEEVE BUSHING FAB PER B/N EO FIG 5. REPAIR SLEEVE BUSHING INSTALLED PER B/N EO. REPAIR AT B/N BORE NR 28 LT IS ACCEPT PER EN 1318-06.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C RT HORIZ STAB FOUND NR 28 BARREL NUT BORE CORRODED CORROSION AT B/N BORE REMOVED PER SRM51-21-01 V.II R.38. BORE REAMED TO 1.178" DIA REMAINING BLEND OUT 0.050" DEEP BOTTOM THRU, EXCEEDED PER B/N EO 5510-19409K. REPAIR BUCKET BUSHING FAB AND PROTECT PER EO MD11-5510-19 409K FIG 5, PR1422 B1/2 SEALANT APPLIED AND REPAIR BUCKET BUSHING INSTALLED PER B/N EO. REPAIR C/O AT B/N BORE NR 28 RT IS ACCEPTABLE PER EN 1319-06.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C RT HORIZ STAB FOUND NR 34 BARREL NUT BORE CORRODED. CORROSION AT B/N BORE REMOVED PER SRM 51-21-01VOL IIR 38. BORE REAMED TO 1.178D IA REMAINING BLEND OUT 0.040 BOTTOM SURFACE CLN AND REMAINING BLEND OUT 0.035 DEEP EXCEED EO LIMITS. B/N BORE BLEND OUT, BOTTOM PERI RADIUS SMOOTHEN AND PROTECTED PER EO. REPAIR SLEEVE BUSHING FAB, PROTECTED AND INSTALLED PER EO FIG 5. REPAIR C/O AT B/N BORE NR 34 RT IAW EN1320-06.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C RT HORIZ STAB FOUND NR 22 BARREL NUT BORE CORRODED CORROSION AT B/N BORE REMOVED PER SRM 51-21-01 V.II R.38. BORE REAMED TO 1.067" DIA, REMAINING BLEND OUT 0.055"DEEP FOUND EXCEEDED LIMITS PER EO MD11-5510-19409K. B/N BORE REWORKED TO 1.105"DIA PER EN 1317-06. REPAIR SLEEVE BUSHING FAB AND PROTECTED PER B/N EO. REPAIR SLEEVE BUSHING INSTALLED PER B/N EO. REPAIR C/O AT B/N BORE NR 22 RT IS ACCEPT PER EN1317-06.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C RT HORIZ STAB FOUND NR 15 BARREL NUT BORE CORRODED CORROSION AT B/N BORE REMOVED PER SRM 51-21-01 V.II R.38. BORE REAMED TO 1.067" DIA REMAINING BLEND OUT 0.050" BOTTOM SURFACE CLEANED REMAINING BLEND OUT 0.030" DEEP EXCEEDED LIMITS PER B/N EO. REPAIR SLEEVE BUSHING FAB PER B/N EO. REPAIR SLEEVE BUSHING INSTL PER B/N EO FIG 5. REPAIR CARRIED OUT AT B/N BORE NR 15 LT IS ACCEPTABLE PER EN 1305-06.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C LT HORIZ STAB FOUND NR 35 BARREL NUT BORE CORRODED CORROSION AT B/N BORE REMOVED PER SRM 51-21-01 V.II R.38. BORE REAMED TO TO 1.178" DIA, REMAING BLEND OUT 0.050" EXCEEDED LIMITS PER EO MD11-5510 -19409K. REPAIR BUCKET BUSHING FAB AND PROTECTED PER EO MD11-5510-19409 K. REPAIR BUCKET BUSHING INSTALLED PER EO MD11-5510-19409K FIG 5. REPAIR C/O AT B/N BORE NR 35 LT IS ACCEPTABLE PER EN 1312-06.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C RT HORIZ STAB FOUND NR 18 BARREL NUT BORE CORRODED CORROSION AT B/N BORE REMOVED PER SRM 51-21-01 VII R.38. BORE REAMED TO 1.067" DIA BOTTOM BORED THRU, REMAINING SIDEWALL BLEND OUT IS 0.040" DEEP , EXCEEDED LIMITS PER B/N EO. REPAIR BUCKET BUSHING FAB PER B/N EO. REPAIR BUCKET BUSHING INSTALLED PER B/N EO. REPAIR CARRIED OUT AT B/N BORE NR 18 RT IS ACCEPTABLE PER EN 1306-06.

Part: COVER PLATE — CORRODED (BS 1959 L39-40R) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C AFT CGO, STA 1959, LONGERON R39-R40, FOUND COVER PLATE INTERFACE MOUNT AREA WITH SURFACE CORROSION AS MARKED. LONGERON FASTENERS REMOVED PER SRM51-31-01 V.II R.38 AT STA 1953 TO 19 64 L-39 AND L-40. CORROSION EXIT DOUBLER REMOVED PER SRM 51-35-01 V.II R.3 8. FAB DOUBLER P/N:AGA8013-1 PER DOUGLAS DWG AGA8013. NEW DOUBLER INSTALLED PER DWG AGA8013 AND SRM51-35-01 V.II R.38. REINSTALLED LONGERON FASTENERS PER SRM 51-35-01 V.II R.38.

Part: FITTING — GOUGED (LT TRUNNION) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C LT TRUNNION SUPPORT FITTING FWD HOLE FOUND SEVERAL GOUGE MARKS. REFER TO NRC 956648. HOLE REAMED TO 1.385 DIA PER SRM 53-40-00 VOL II R38 2. LOCAL BLEND AREA PER EN1336-06. FPI INSP C/O PER DACNDTSPM PART 08 R12 FOUND NO CRACK AND CORRODED. REPAIR SLEEVE BUSHING FAB PER SRM 53-40-00 FIG 15 VOL I R38 (MATL USED AMS4640X1.5DIA). FAB BUSHING CAD PLATED PER SRM 53-40-00 FI G15 VOLI. FAB BUSHING INSTALLED PER SRM 53-40-00 FIG 15 VOL I IAW EN1336-06.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C RT HORIZ STAB, FOUND NR 35 BARREL NUT BORE CORRODED CORROSION AT B/N BORE REMOVED PER SRM 51-21-01 V.II R.38. BORE REAMED TO 1.178" DIA, REMAINING BLEND OUT 0.050" BOTTOM, 0.040" DEEP FOUND EXCEEDED LIMITS PER EO MD11-5510-19409K. REPAIR SLEEVE BUSHING FAB AND PROTECTED PER B/N EO FIG 5. REPAIR SLEEVE BUSHING INSTALLED PER EO MD11-5510-19409K. REPAIR C/O AT B/N BORE NR 35 RT IS ACCEPTABLE PER EN 1304-06.

Part: SUPPORT FITTING — CRACKED (BS 1278 S38R) · airframe 71,564 hrs · 11,685 cycles

BLADDER CELL COMPT AT STA 1278.00 S-38R FOUND WEB SUPPORT FITTING CRACKED. REMOVED ATTACHED SUPPORT AND FASTENER ON FITTING PER SRM 51-31-01 V.II R .35.ANGLE P/N:AYB7035-12 M/F EXTRUDED 'T' P/N:S1362783 IAW DOUGLAS DWG AYB7035.FPI C/O PER DPS4.707 R.AW ON FAB ANGLE FOUND NO CRACK EVIDENT. ITEM INSPECTED,OK TO INSTALL. NEW ANGLE INSTALLED PER DWG AYB7035 AND SRM 51-3 1-01 V.II R.38. REINSTALLED REWORK AREA PARTS PER SRM 51-31-01 V.II R.38.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 715,641 hrs · 11,685 cycles

INSPECTION TYPE:C EMP-AFT ACC COMPT AFT BULKHEAD TOP OF LATCH HOUSING ASSY FOUND INTERCOSTAL CLIP CRACKED. CRACKED INTERCOSTAL CLIP REMOVED PER SRM 51-33-01 V.II R.38. NEW INTERCOSTAL CLIP P/N:AJC7345-2 MACHINED USING 7075T6511 STOCK IAW DOUGLAS DWG AJC7345. NEW INTERCOSTAL HOLE PICKUP PER SRM 51-31-01 V.II R.38. NEW INTERCOSTAL CLIP REPROTECTED PER SRM 51-21-01 V.II R.38. NEW INTERCOSTAL CLIP INSTALLED PER SRM 51-31-01 V.II R.38.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C RT HORIZ STAB FOUND NR 36 BARREL NUT BORE CORRODED. CORRODED REMOVED PER SRM 51-21-01 VOL II R38. BORE REAMED TO 2.538 DIA REMAINING BLEND OUT 0.050 DEEP BOTTOM SURF CLN AND BLEND OUT 0.020 DEEP FOUND EXCEED EO LIMITS. B/N BLEND OUT AND BORE BOTTOM PERI RADIUS SMOOTHEN AND PROTECTED. REPAIR BUSHING FAB, PROTECTED AND INSTALLED PER EO FIG 5. REPAIR DOUBLER AND FILLERS FAB AND INSTALLED PER EO FIG 6. REPAIR NR 36 RT C/O IAW EN1396-06.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C RT HORIZ STAB, FOUND NR 29 BARREL NUT BORE CORRODED CORROSION AT B/N BORE, REMOVED PER SRM 51-21-01 V.II R.38. BORE REAMED TO 1.178" DIA, REMAINING BLEND OUT FOUND EXCEEDED LIMITS PER EO MD11-551 0-19409K. B/N BORE REWORKED TO 1.219"DIA PER EN 1307-06. REPAIR SLEEVE BUSHING FAB AND PROTECTED PER B/N EO. REPAIR SLEEVE BUSHING INSTALLED PER B/N EO. REPAIR C/O AT B/N BORE NR 29 RT IS ACCEPTABLE PER EN 1307-06.

Part: SUPPORT FITTING — CRACKED (WING TO BODY) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C FX-RT WING TO FX FAIRING CUT-OUT LOWER SIDE AT Y=1216.200 FOUND SUPPORT FITTING CRACKED. CRACKED FITTING ON FX-RHW TO FX FAIRING CUTOUT LOWER SIDE AT Y=1216.20 0 AND ATTACHED INTERNAL FITTING REMOVED PER SRM 51-31-01 V.II R.38. HOLE S PICK-UP ON NEW FITTING PER SRM 51-35-01 V.II R.38. REWORKED AREA CLEANED UP PER SRM 51-21-01 V.II R.38. STIFFENERS INSTALLED PER SRM 51-31-01 V.II R.38 AND DWG AYB7104 AND INTERNAL FTG REINSTALLED PER SRM 51-31-01 V.II R.38

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C RT HORIZ STAB, FOUND NR 17 BARREL NUT BORE CORRODED CORROSION AT B/N BORE REMOVED PER SRM 51-21-01 V.II R.38. BORE REAMED TO TO 1.067" DIA. REMAINING BLEND OUT 0.025" DEEP, FOUND EXCEEDED LIMITS PER EO MD 11-5510-19409K. REPAIR SLEEVE BUSHING FAB AND PROTECTED PER EO MD1 1-5510-19409K. REPAIR SLEEVE BUSHING INSTALLED PER EO MD11-5510-19409K. REPAIR C/O AT B/N BORE NR 17 RT IS ACCEPTABLE PER EN 1298-06.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C RT HORIZ STAB, FOUND NR 32 BARREL NUT BORE CORRODED. CORRODED REMOVED BORE REAMED TO 1.178 DIA BOTTOM BORED THRU REMAINING BLEND OUT 0.060 DEEP LIMIT EXCEEDED. 10X MAG DVI C/O FOUND NO CORROSION. BORE REWORKED TO 1.203 DIA. BLEND OUT, SMOOTHENED AND PROTECTED. FRAME PRIMER TOUCH UP. REPAIR BUSHING FAB AND PROTECTED. RII INSP C/O OK. SEALANT APPLIED BUSHING INSTALLED, C/O PAINT. REPAIR C/O IAW EN1308-06.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C LT HORIZ STAB, FOUND NR 23 BARREL NUT BORE CORRODED. CORROSION AT B/N BORE REMOVED PER SRM 51-21-01 V.II R.38. BORE REAMED TO 1.067"DIA,REMAINING BLEND OUT AT SIDEWALL IS 0.035"DIA FOUND EXCEEDED LIMITS PER EO MD11-5510-19409K. REPAIR SLEEVE BUSHING FAB AND PROTECTED PER EO MD11-5510-19409K FIG 5. REPAIR SLEEVE BUSHING INSTALLED PER EO M D11-5510-19409K. REPAIR C/O AT B/N BORE NR 23 LT IS ACCEPT PER EN1290-06.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C LT HORIZ STAB, FOUND NR 14 BARREL NUT BORE CORRODED. B/N BORE REAMED TO 0.988 DIA REMAINING BLEND OUT 0.010 BOTTOM SURFACE CLEAN AND REMAINING BLEND OUT 0.015 DEEP FOUND EXCEED EO LIMIT. BORE RWK TO 1.016 DIA PER EN12994-06. BOTTOM PERIPHERY RADIUS SMOOTHEN AND PROTECTED PER EO. REPAIR SLEEVE BUSHING FAB AND PROTECTED PER EO FIG 5. REPAIR BUSHING INSTALLED PER EO FIG 5. REPAIR C/O AT BORE NR 14 LT IAW EN1299-06.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C LT HORIZ STAB, FOUND NR 26 BARREL NUT BORE CORRODED B/N BORE AT SPLICE FITTING REAMED TO 1.067" DIA, REMAINING BLEND OUT 0.0 65" DIA DEEP, BOTTOM SURFACE CLEANED AND REMAINING BLEND OUT 0.040" DEEP. FOUND EXCEEDED LIMITS PER B/N EO. B/N BORE REWORKED TO 1.121"DIA PER EN 1300-06. REPAIR SLEEVE BUSHING FAB PER B/N EO FIG 5. REPAIR SLEEVE BUSHING INSTALLED PER B/N EO. REPAIR AT B/N BORE NR 26 LT IS ACCEPT PER EN1300-06.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C RT HORIZ STAB, FOUND NR 26 BARREL NUT BORE CORRODED, BARREL NUT BORE AT SPLICE FITTING REAMED TO 1.067"DIA. REMAINING BLEND OUT 0.108" DEEP, BOTTOM BLEND OUT 0.066" DEEP, EXCEEDED LIMITS PER EO MD11 -5510-19409K. BARREL NUT BORE AND FASTENERS HOLES TRANSFERED ONTO NEW FITTING PER DOUGLAS DWG ALC8100. NEW SPLICE FITTING INSTALLED PER SRM 51-38 -01 V.II R.38 AND SRM 51-33-01 V.II R.38.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C LT HORIZ STAB, FOUND NR 17 BARREL NUT BORE CORRODED CORROSION AT B/N BORE REMOVED PER SRM 51-21-01 V.I R.38. BORE REAMED TO 1.067" DIA BOTTOM, REMAINING BLEND OUT AT BEARING SURFACE IS 0.050"DIA FOUND EXCEEDED B/N EO. B/N BORE RERWORKED TO 1.105" DIA PER EN1289-06. REPAIR SLEEVE BUSHING FAB PER B/N EO FIG 5. REPAIR SLEEVE BUSHING INSTALLED PER B/N EO. REPAIR C/O AT B/N BORE NR 17 LT IS ACCEPTABLE PER EN 1289-06.

Part: STIFFENER — CRACKED (WING TO BODY) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C FX-RT WING TO FX FAIRING CUT-OUT LOWER SIDE AT Y=1236.800 FOUND SUPPORT FITTING CRACKED. CRACKED STIFFENER INTERNAL SUPPORT AND CRACKED STIFFENER REMOVED PER SRM 51-31-01 VII R.38. NEW STIFFENER FASTENER HOLES PICK-UP PER DWG AYB7104 AND SRM 51-31-01 V.II R.38. OK TO INSTALL STIFFENER. STIFFENER INSTALLED PER SRM 51-31-01 V.II R.38 AND DWF AYB7104 AND INNER SUPPORT REINSTALLED PER SRM 51-31-01 V.II R.38.

Part: STRUT — DAMAGED · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C FWD CARGO,AT STA 6.30 LT, X=16.5 FOUND STRUT DAMAGED FWD CARGO AT STA 6.30 LH, X=16.5 DAMAGED STRUT REMOVED AND NEW STRUT INSTALLED AS PER DRAWING ADA0033 AND SRM 51-31-01 VOL II REV 38.

Part: LONGERON — CRACKED (BS 535-547 L33L) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C LT AIRCON BAY, FOUND LONGERON CRACKED AT STA 535-547,L-33 LT A/C BAY STA 535-547 L-33 LT CRACK LONGERON REMOVED AND NEW LONGERON INSTALLED AS PER DWG ACA 3849 AND SRM 51-35-01 V.2 R.38 LT AIRCON BAY STA 535-547 L-33 LT LONGERON PAINT TOUCHED UP PER SRM 51-21-01 VOL I I REV 38.

Part: STIFFENER — CRACKED (BULKHEAD) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C EMP-AFT FX COMPT FWD BULKHEAD RT SIDE OF LADDER ASSY FOUND VERTICAL STIFFENER SUSPECTED CRACK ON MOST TOP AS MARKED. HFEC INSP C/O PER DAC NDTSPM R.12 06-10-01.001 ON CRACK SUSPECTED AREA AND FOUND CRACKED APPROX 1/2 INCH LONG AS MARKED. VERTICAL STIFFENER CRACKED AREA CUT OFF PER SRM 53-00-01 V.I R.38 AND REMOVED PER SRM 51-31-01 V.II R.38. REPAIR ANGLES AND FILLERS FAB PER SRM 53-00-01 V.I R.38. NEW CAP STIFF. FAB PER DWG AJC7050-70. REPAIR PARTS INSTALLED PER SRM 53-00-01 R.38.

Part: SEAT TRACK — CORRODED (BS 865-869) · airframe 71,559 hrs · 11,684 cycles

INSPECTION TYPE-C MAIN DECK:X=8 (LT SIDE), BETWEEN STA 865 AND STA 869, SEAT TRACK CROWN AREAS CORRODED STA 849-919 X=8 CORROSION SEAT TRACK REMOVED IAW SRM 51-31-01 V.2 R.38, CORROSION OUT OF LIMIT TO REPAIR. REPAIR SEAT TRACK FAB IAW SRM 53-70-00 FIG 1 V.1 R.38. REPAIR SEAT TRACK REPROTECTED IAW SRM 51-21-01 V.2 R.38. REPAIRED SEAT TRACK PAINT TOUCHED UP IAW SRM 51-21-01 V.2 R.38. REPAIRED SEAT TRACK INSTALLED IAW SRM 53-70-00 FIG 1 V.2 R.38.

Part: SEAT TRACK — CORRODED (BS 865-869) · airframe 71,559 hrs · 11,684 cycles

INSPECTION TYPE-C MAIN DECK:ALONG X=-8 (RT SIDE), BETWEEN STA 865 AND STA 869, SEAT TRACK CROWN AREAS CORRODED STA 849-919 X=-8 CORROSION SEAT TRACK REMOVED IAW SRM 51-31-01 V.2 R.38, CORROSION OUT OF LIMIT TO REPAIR. REPAIR SEAT TRACK FAB IAW SRM 53-70-0 0 FIG 1 V.1 R.38. REPAIR SEAT TRACK REPROTECTED IAW SRM 51-21-01 V.1 R.3 8. REPAIRED SEAT TRACK PAINT TOUCHED UP IAW SRM 51-21-01 V.2 R.38. REPAIR SEAT TRACK INSTALLED IAW SRM 53-70-00 FIG 1 V.1 R.38.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C CABIN:STA 1179 TO STA 1199 AT S-14L FOUND STIFFENER CRACKED. ATTACH STIFFENER AREA PARTS AND CRACK SPLICE REMOVED PER SRM 51-31-01 V 2 R.38. MACHINE FAB SPLICE PER DOUGLAS DWG AEA 7600. FPI C/O PER DAC NDT SPM R.2 PT.8 ON FAB SPLICE. NO CRACK EVIDENT. NEW SPLICE INSTALLED AS PER DWG AEA7600 AND SRM51-33-01 R.38 V.2. ATTACH STIFFENER PARTS REINSTALLED AS PER SRM 51-31-01 V.2 R.38.

Part: SEAT TRACK — CORRODED (BS 1331-1381) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C MAIN DECK:ALONG X=-75, STA 1331 TO STA 1381, SEAT TRACK CROWN AND FLANGE AREAS FOUND CORRODED. STA 1256.25 TO 1381 X=-75 OUT OF LIMIT CORROSION. TRACK ATTACH PARTS AND FASTENERS REMOVED PER SRM 51-31-01 V.II R.38 STA 1265 & 1391 X=-75 SEAT TRACK CUTOFF FOR NDT INSPECT AND REPAIR PER SRM 53-70-00 FIG 1 V.I R.38 AND EN NR1285-06. REPAIR SEAT TRACK AND SPLICES FAB PER SRM 53-70-00 FIG 1 V.1 R.38 AND EN NR1285-06.

Part: SEAT TRACK — CORRODED (BS 1911-2007) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE-C MAIN DECK: FROM STA 1911 TO STA 2007, RT MOST OB SEAT TRACK FLANGE AREAS AND SEAT TRACK CROWN AREAS FOUND CORRODED. CORRODED SEAT TRACK AT STA 1831 TO 2007 RBL 107.25 ATTACH PARTS AND TRACK REMOVED IAW SRM51-31-01 V.II R.38. NEW SEAT TRACK FASTENER HOLES P/U IAW SRM51-31-01 V.II R.38. NEW SEAT TRACK SPLICE AND PLATE FAB IAW SRM 53-70-00 FIG 1 V.II. REPAIR SEAT TRACK INSTL IAW SRM53-70-00 V.II R.38. REPAIR S/TRACK AREA PTS. AND FASTENERS REINSTL IAW SRM51-31-01 V.II R.38

Part: SKIN — CRACKED (RT WING) · airframe 71,559 hrs · 11,684 cycles

INSPECTION TYPE:C RT WING FIXED L/E LOWER SURFACE NR 16 SLAT TRACK CUTOUT SKIN FOUND CRACKED. RHW FIXED L/E LOWER SURFACE NR 16 SLAT TRACK CUTOUT AREA FASTENERS REMOVED PER SRM 51-31-01 V.2 R.38. REPAIR DOUBLER FABRICATED, FASTENERS HOLES PICK UP AS PER SRM 57-10-00 FIG 21 V.1 R.38 AND REPROTECTED PER SRM 51-21- 01 V.2 R.38. REPAIR DOUBLER INSTALLED PER SRM 57-10-00 FIG 21 V.1 R.38.

Part: FITTING — CRACKED (NLG TRUNNION) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C NLG W/W, NLG LT FITTING FOUND CRACK WITH STOP DRILL. MAJOR REPAIR TO CRACK AND STOP DRILL HOLE ON NLG LT TRUNNION FITTING. CARRIED OUT AS PER ENGINEERING FILE NR MD11-53-20073 AND EN 1278-06.

Part: SKIN — CRACKED (RWS 402) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C RT L/E COMPARTMENT AT STA XORS 402 APPROX FOUND UPPER SKIN DOUBLER CRACKED. HFEC C/OUT CRACKED AREA AND CONFIRMED CRACKED END APPROX 1". CRACKED END STOP DRILLED IAW SRM57-10-00 FIG 25 VOLI REV38. HFEC INSP C/OUT AROUND STOP DRILLED HOLE. FOUND CRACK CONTAIN. REPAIR PART FAB USING GAL-4V 0.020" TITANIUM IAW SRM 57-10-00 FIG 25 VOL I REV38. REPAIR PART PRIMER. REPAIR PART INSTALLED IAW SRM 57-10-00 FIG 25 VOL I REV38.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C MAIN DECK FROM STA 1911 TO STA 2007, LT MOST O/B SEAT TRACK FLANGE AREAS AND SEAT TRACK CROWN AREAS FOUND CORRODED SEAT TRACK AT STA 1831 - 2007 LBL107.25 ATTACH PARTS AND TRACK REMOVED PER SRM 51-31-01 V.II R.38. NEW SEAT TRACK FASTENER HOLES PICKED UP PER SRM 51-31-01 V.II R.38. NEW SEAT TRACK INSTALLED PER SRM 51-31-0 1 R.38 AND DWG AFA7789. ATTACHED SEAT TRACK PARTS REINSTALLED AS PER SRM 51 -31-01 VOL II REV 38.

Part: BEAM — CHAFED (LT MLG WW) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C LT MLG WW, STRUT DOOR CUT-OUT AFT JAMB FOUND CHAFING MARK AT LWR CHORD AS MARKED. MAJOR REPAIR TO DEEP CHAFING ON LEFT WING INNER TRAILING EDGE AFT BEAM LOWER CAP CARRIED OUT PER ENGINEERING FILE NR MD11-57-20068 AND EN1302-06.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 71,559 hrs · 11,684 cycles

INSPECTION TYPE:C MAIN DECK:ALONG STA 1964, ALONG LONGERON 27L, FRAME SHEAR TIE WEB FOUND CORRODED. CORROSION WEB REMOVED PER SRM 51-35-01 V.2. NEW WEB P/N:AGA7145-4. FAB PER DWG AGA7145 AND HEAT TREAT TO T62 PER DPS7.00-1. NEW WEB FASTENER HOLES PICKED UP PER DWG AGA7145 AND SRM 51-31-01 V.2 R38 ON WEB P/N:7145-4. NEW WEB PROTECTED PER SRM 51-21-01 V.2 R.38. NEW WEB INSTALLED PER DWG AGA71 45 AND SRM 51-31-01 V.2 R.38.

Part: SKIN — CRACKED (RT WING) · airframe 71,559 hrs · 11,684 cycles

RT WING LOWER SURFACE FIXED L/E NR 14 SLAT TRACK CUTOUT SKIN CRACKED. RT WING LOWER SURFACE L/E NR 14 SLAT TRACK CUTOUT AREA FASTENERS REMOVED PER SRM 51-31-01 V2 R38. REPAIR DOUBLER FABRICATED, FASTENERS HOLE PICK UP PER SRM 57-10-00 FIG 21 V.1 R.38 AND REPROTECTED PER SRM 51-21-01 V.2 R.38 REPAIR DOUBLER INSTALLED PER SRM 57-10-00 FIG 21 V.1 R.38.

Part: INTERCOSTAL — CRACKED (BS 1621-1641) · airframe 71,559 hrs · 11,684 cycles

INSPECTION TYPE-C CABIN:1 INTERCOSTAL BETWEEN STA 1621-1641 AT RT LONG 7 HEIGHT, FOUND CRACKED. CRACK INTERCOSTAL REMOVED IAW SRM 51-35-01 V.2. CRACKED MATERIAL REMOVED 0 .063 INCH FOUND WITHIN LIMIT IAW SRM 53-00-01 FIG1A V.1 R.38.HFEC C/O IAW D AC NDT SPM R.12 PT06-10-01.001. ON CRACK SUSPECTED AREA AND CRACK CONFIRM APPROX .3750 INCH. NEW INTERCOSTAL FAB IAW DWG AFA7761-17 AND INSTALLED IAW DWG AFA7761 AND SRM 51-31-01 V.2 R.38.

Part: SKIN — CRACKED (LT WING) · airframe 71,559 hrs · 11,684 cycles

LT WING FIXED L/E LOWER SURFACE AT NR 14 SLAT TRACK CUTOUT FOUND SKIN CRACKED. LHW L/E LOWER SURFACE AT NR 14 SLAT TRACK CUTOUT FASTENERS REMOVED PER SRM 51-31-01 V.2 R.38. REPAIR DOUBLER FABRICATED, FASTENERS HOLES PICK UP PER SRM 57-10-00 FIG 21 V.1R.38 AND REPROTECTED PER SRM 51-21-01 V.2 R.3 8. REPAIR DOUBLER INSTALLED PER SRM 57-10-01 FIG 21 V.1 R.38.

Part: SLAT TRACK — CRACKED (NR 12) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE-C LT WING LOWER SURFACE FIXED L/E AT NR 12 SLAT TRACK CUTOUT FOUND SKIN CRACKED. LT LWR SURFACE L/E SLAT TRACK CUTOUT NR 12 FASTENERS AREA REMOVED IAW SR SRM51-31-01 VOLII REV38. REPAIR DOUBLER FAB FASTENER HOLES PICKUP AND REPROTECTED IAW SRM51-21-01 VOLII REV38 AND SRM57-10-00 FIG21 VOLI REV 38. REPAIR DOUBLER INSTALLED IAW SRM51-10-00 FIG21 VOL1 REV38.

Part: SKIN — DAMAGED (ZONE 120) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C FX-FWD CARGO DOOR CUT-OUT FWD JAMB FOUND EDGE DAMAGED ALONG S-40R TO S -42R AS MARKED FWD CARGO DOOR JAMB LWR FWD SCUFF PLATE RMVD AS PER AMM53-10-05 R.50 DAMAGED SKIN AREA FASTENERS REMOVED AS PER SRM 51-31-01 V.2 R.38. REMOVED DAMAGED SKIN MAT PER SRM53-50-00 FIG 6 V.1 R.38. REPAIR DOUBLERS FAB AND INSTALLED PER SRM 53-50-00 FIG 16 V.1 SHT.5 ITEM 14(A) R.38 FWD CARGO DOOR JAMB LWR FWD SCUFF PLATE INSTL PER AMM53-10-05 R.50

Part: SKIN — DAMAGED (FUSELAGE) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C FX-AFT CARGO DOOR CUT-OUT FWD JAMB ALONG ABOVE LWR FWD SCUFF PLATE TO S-43L FOUND EDGE DAMAGED (2 LOCATION) AS MARKED AFT CARGO DOOR JAMB SEAL REMOVED PER AMM 20-50-02 R.50. EDGE DAMAGED (2 LOC) AT S43L ABOVE LWR FWD SCUFF PLATE OF FX-AFT CARGO DOOR CUT-OUT FWD JAMB, TRIMMED OUT AND SMOOTHED, (0.85") PER SRM 53-50-00 FIG 16 V.I R. 38. REPAIR DOUBLERS FAB PER SRM 53-50-00 FIG 16 V.I R.38. REPAIR DOUBLER INSTALLED PER SRM 53-30-00 FIG 16 V.I R.38 AND SRM 51-31-01 V.II R.38.

Part: SCUFF PLATE — DAMAGED (CARGO DOOR) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE-C FX AFT CARGO DOOR CUT-OUT AFT JAMB ALONG ABOVE LWR AFT SCUFF PLATE TO S-43L FOUND EDGE DAMAGED AS MARKED. EDGE DAMAGE AT S-43L ABOVE LWR AFT SCUFF PLATE OF FX AFT CGO DR CUT- OUT AFT JAMB TRIMMED OUT/SMOOTHENED IAW SRM53-50-00 FIG6 VOLI REV38. REWORKED AREA REPROTECT IAW SRM51-21-01 VOLII REV38. CARRY OUT HFEC INSP. REPAIR DOUBLERS FAB IAW SRM53-50-00 FIG6 VOLI REV38. REPAIR DOUBLERS INSTALLED IAW SRM53-50-00 FIG16 VOLI REV38 AND SRM51-31-01.

Part: SKIN — DENTED (RT TE FLAP) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE-C RT IB FLAP OB SEGMENT LOWER SURFACE FOUND NUMEROUS DENTS. RT IB FLAP OB SEGMENT RMVD IAW CMM57-57-03 REV54. SEGMENT LWR SURFACE DMG SKIN REMOVED IAW SRM51-31-01 VOLII REV38.SEGMENT LWR SKIN FAB USING 2024-T3 0.040 INCH IAW DWG ARC2444. NEW FAB SKIN FASTENER HOLE PICKUP IAW SRM51-35-01 VOLII REV38.NEW FAB SKIN ALODINE AND PRIME. NEW SKIN INSTALLED IAW SRM51-35-01 VOLII REV38.

Part: SKIN — DENTED (T/E FLAP) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C RT I/B FLAP I/B SEGMENT LOWER SURFACE FOUND NUMEROUS DENTS RT I/B FLAP I/B SEGMENT LWR SURFACE SKIN DAMAGED REMOVED PER SRM51-31- 01 V.II R.38. RT I/B FLAP I/B SEGMENT LWR SKIN FAB USING 2024-T3 0.040" IAW DWG ARC 2736. NEW FAB SKIN ALODINE AND PRIME IAW SRM 51-21-01 V.II R.3. NEW SKIN INSTALLED IAW SRM51-35-01 V.II R.38. RT I/B FLAP OPS CHK C/O FOUND SATISFACTORY AS PER MM27-50.00 REV.35

Part: SKIN — WORN (LT TE FLAP) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE-C LT IB FLAP OB SEGMENT LOWER SURFACE OB SIDE EDGE WORN. LT IB FLAP OB SEGMENT LWR OB SIDE SKIN REMOVED IAW SRM51-35-01 VOLII REV38. NEW SKIN FAB USING 2024-T3 0.040 INCH IAW DWG ARC3098. NEW SKIN ALODINE AND PRIME IAW SRM51-21-01 VOLII REV38. OK TO INSTALL. NEW SKIN INSTALLED IAW SRM51-35-01 VOLII REV38.

Part: SKIN — DENTED (T/E FLAP) · airframe 71,564 hrs · 11,685 cycles

INSPECTION TYPE:C LT I/B FLAP I/B SEGMENT LOWER SURFACE FOUND NUMEROUS DENTS LT I/B FLAP I/B SEGMENT LWR SURFACE DAMAGED SKIN REMOVED PER SRM 51-31- 01 V.II R.38. LT I/B FLAP I/B SEGMENT LWR SKIN FAB PER DWG ARC 2736 USING 2024T3-0.040". NEW FAB SKIN ALODINE AND PRIME IAW SRM 51-21-01 V.II R.3 8. NEW SKIN INSTALLED PER SRM51-35-01 V.II R.38. LT I/B FLAP OPERATION CHECK C/O FOUND SATISFACTORY PER SRM 27-50-00 REV 55.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 71,564 hrs · 11,685 cycles

LT I/B FLAP O/B SEGMENT LOWER SURFACE FOUND NUMEROUS DENTS. LT IB FLAP OB SEGMENT REMOVED PER CMM57-52-03 REV54. LT I/B FLAP O/B SEGMENT LWR SURFACE SKIN DAMAGED REMOVED PER SRM 51-51-01 VOL II REV 38. SEGMENT LWR SKIN FAB USING 2024-T3 0.040" IAW DWG ARC2444. SEGEMNT FAB SKIN FASTENER HOLE P/U IAW SRM 51-35-01 VOLII REV38. NEW FAB SKIN ALODINE AND PRIME. NEW SKIN INSTALLED IAW SRM51-35-01 VOL II REV38.