N283UP

Part: PUMP — INOPERATIVE (NR 2 HYD SYSTEM) · airframe 78,282 hrs · 17,643 cycles

AIR TURNBACK, RECEIVED LEVEL 1 HYD 2 OFF ALERT ENG 2 HYD PUMPS INOP AUTO SYSTEM TURNED PUMPS OFF. REPLACED 2R HYD PUMP REF AMM 29-11-20. PERFORMED OPS & LEAK CHECK PER AMM 29-11-20-400-803. NO FAULTS. NO LEAKS NOTED. R/R ESR IAW IPC 29-11-10. R/R #2 ENG LH ENG DRIVEN HYD PUMP PER AMM 29-11-20-400-803. OPS & LEAK CK NORMAL PER IPC 29-11-10-10.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 78,257 hrs · 17,627 cycles

EMERGENCY LIGHTING BATTERY 1 LOW, DURING EMERGENCY LIGHT TEST. R & R EMERGENCY POWER SUPPLY BATTERY IAW AMM 33-50-01-401.

Part: BATTERY PACK — MISINSTALLED (EMERGENCY LIGHT) · airframe 78,043 hrs · 17,554 cycles

EMERGENCY LIGHTS INOP. REPLACED EMERGENCY LIGHT PWR SUPPLY BATTERY REVERSED DMP 33-50-04. OPS AND TEST GOOD IAW AMM 33-51-01.

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:CL/H I/B FLAP O/B AFT HINGE #6 LUG BORE HOLE AND I/B FACE HAS PITTINGREMOVED PITTING AND CORROSION FROM FLAP LUG BORE IAW CMM 57-52-03. PERFORMED DETAIL INSPECTION ,FPI, AND HFEC TO INSURE NO CRACKING OR FURTHER DAMAGE.FABBED AND INSTALLED BUSHINGS IAW CMM 57-52-03

Part: HINGE — CORRODED (RT WING TE FLAP) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:CR/H I/B FLAP O/B AFT HINGE #7 LUG BORE AND O/B FACE HAS PITTINGCORROSION REMOVED PER CMM 57-52-03. PERFORMED DETAILED, FPI, HFEC TO ENSURE NO CRACKING OR FURTHER DAMAGE PRESENT.INSTALLED BUSHINGS IAW CMM 57-52-03 REF. EO MD11-5740-80847-A AND EA 011-5740-01-A9191 REV. IR

Part: HINGE BRACKET — CORRODED (LT WING TE FLAPS) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CLT I/B FLAP FWD HINGE BRACKET CORRODED AT #3 LUG.REPAIRED CORRODED HINGE BRACKET IAW VT-SAA EA 011-5740-01-A91998 REV I/R AND UPS EO MD11-5740-80864-A (MINOR).

Part: TEE ANGLE — CRACKED (RT WING TE FLAP) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CRT WING O/B FLAP I/B AFT HINGE FAIRING FWD END TEE ANGLE IS CRACKED.REMOVED AND REPLACED CRACKED RT WING O/B FLAP I/B AFT HINGE FAIRING FWD END TEE ANGLE IAW SRM 51-33-01. (MINOR)

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CLT WING O/B FLAP O/B FWD HINGE #1 LUG BORE HOLE HAS PITTING.REPAIRED CORRODED LT WING O/B FLAP O/B FWD HINGE BRACKET LUG AT STA. XW 638.31 IAW VT-SAA EA 011-5740-01-A9190 REV. IR AND UPS EO MD11-5740-80794-A. (MINOR)

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CR/H WING O/B FLAP HINGE BRACKET ASSY ON A/C SIDE HAS CORROSION ON LUG BORE AND FACE.REPAIRED HINGE BRACKET ASSY IAW VT-SAA EA 011-5700-01-A9180 REV. I/R AND UPS EO MD11-5740-80834-A. (MINOR)

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CLH O/B FLAP O/B AFT HINGE #7 LUG HOLE HAS PITTING CORROSION.REPAIRED CORRODED LH O/B FLAP LUG HOLE IAW CMM 57-52-04 (MINOR)

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CLT O/B FLAP O/B FWD HINGE #2 LUG HOLE HAS PITTING CORROSION.REPAIRED CORRODED LT O/B FLAP HINGE IAW CMM 57-44-09 PG 602 (MINOR)

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CRT WING I/B FLAP O/B AFT HINGE BRACKET LUG BORES HAS PITTING CORROSION.REPAIRED CORRODED RT WING I/B FLAP O/B AFT HINGE BRACKET LUGS IAW VT-SAA EA 011-5740-01-A9191 REV. IR AND UPS EO MD11-5740-80847-A. (MINOR)

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CRT WING I/B FLAP O/B FWD HINGE BRACKET LUGS HAS PITTING CORROSION.REPAIRED CORRODED RT WING I/B FLAP O/B FWD HINGE BRACKET LUGS IAW VT-SAA EA 011-5740-01-A9192 REV. IR AND UPS EO MD11-5740-80879-A. (MINOR)

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CLT WING I/B FLAP O/B AFT HINGE BRACKET LUGS HAS CORROSION.REPAIRED CORRODED LT WING I/B FLAP O/B AFT HINGE BRACKET LUGS IAW VT-SAA EA 011-5740-01-A9196 REV. IR AND UPS EO MD11-5740-80863-A. (MINOR)

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CR/H WING O/B FLAP O/B HINGE BRACKET ASSY. O/B LUG ON A/C SIDE HAS CORROSION ON LUG BORE AND FACE.REPAIRED HINGE BRACKET ASSY. IAW VT-SAA EA 011-5700-01-A9180 REV. I/R AND UPS EO MD11-5740-80834-A. (MINOR)

Part: FRAME — DENTED (BS 740 L12R) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CMAIN CABIN FUSELAGE FRAME AT STA 740 & LONGERON 12R IS DENTED.REPAIRED DENTED MAIN CABIN FUSELAGE FRAME AT STA 740 & LONGERON 12R IAW VT-SAA EA 011-5310-01-A9184 REV. IR AND UPS EO MD11-5310-80867-A. REF. FAA FORM 9100-9 SIGNED BY: STEPHEN KANG (AR-605677) DATED 06/29/2021. (MAJOR)

Part: ANGLE — CRACKED (BS 1341 L15R) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CMAIN CABIN LONGERON 15 R/H T ANGLE IS CRACKED AT STA. 1341.REMOVED, FABRICATED AND REP[LACED T ANGLE IAW DWG. AEA7588 AND SRM 51-33-01. (MINOR)

Part: SUPPORT BRACKET — CRACKED (BS 1341 L15R) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:C3MAIN CABIN SUPPORT BRACKET CRACK AT STA.1341 LON 15R.REMOVED,FABRICATED AND REPLACED CRACKED SUPPORT BRACKET IAW SRM 51-33-01 AND 51-31-01 (MINOR).

Part: LONGERON SPLICE — CRACKED (BS 1531 L7R) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CMAIN CABIN CEILING AREA HAS A PRODUCTION SPLICE THAT IS CRACKED AT STA. 1531 ON LONG. 7 R/H.REMOVED, FABRICATED AND REPLACED SPLICE IAW DWG. AEA7633 AND SRM 51-33-01. (MINOR)

Part: CHANNEL — CRACKED (VERTICAL STAB) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CUPPER FUSELAGE SUPPORT ANGLE (CHANNEL) INSIDE VERTICAL STAB PANEL 364FR IS CRACKED.REMOVED AND REPLACED CRACKED SUPPORT ANGLE (CHANNEL) INSIDE VERTICAL STAB PANEL 364FR AT UPPER FUSELAGE IAW SRM 51-35-01. (MINOR)

Part: BEAM — CRACKED (L3 DOOR) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CMAIN CABIN L3 DOOR PLUG LOWER HORIZONTAL BEAM IS CRACKED AT FWD END.REMOVED AND REPLACED CRACKED MAIN CABIN L3 DOOR PLUG LOWER HORIZONTAL BEAM IAW SRM 51-31-01, 51-33-01 AND 51-35-01. (MINOR)

Part: SKIN — CORRODED (BS 2153-2163) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CL/H EXTERIOR FUSELAGE SKIN HAS CORROSION BETWEEN STA. 2153 TO 2163 AND BETWEEN L33L TO 35L.REPAIRED CORRODED FUSELAGE SKIN BETWEEN STA. 2153 TO 2163 AND BETWEEN L33L TO 35L IAW SRM 53-70-01 REPAIR 3 FIG. 201. (MAJOR)

Part: STRINGER — CRACKED (S52) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:2CCENTER WING UPPER AUX TANK STRINGER 52 CRACKED BETWEEN STA.XCW 35 TO XCW 59.75.REPAIRED CRACKED CENTER WING UPPER AUX TANK STRINGER 52 BETWEEN STA.XCW 35 TO XCW 59.75 IAW SRM 57-10-03 REPAIR 1 FIG 201 (MAJOR).

Part: INTERCOSTAL — CRACKED (FWD CARGO) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:C3FWD CARGO COMPARTMNET INTERCOSTAL CRACK AT RH STA.6-50 BETWEEN LON 42R-43R.REMOVED,FABRICATED AND REPLACED CRACKED INTERCOSTAL IAW SRM 51-35-01 AND 51-31-01 (MINOR).

Part: FRAME — GOUGED (MAIN CARGO DOOR) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CMAIN CARGO DOOR AFT FRAME IS GOUGED AT MID SECTION.REPAIRED GOUGED MAIN CARGO DOOR AFT PAN AT STA 765.375 BETWEEN Z= 30 AND Z= 40 IAW VT-SAA EA 011-5230-01-A9189 REV. IR AND UPS EO MD11-5230-80836-A. REF. FAA FORM 8100-9 SIGNED BY STEPHEN KANG (AR-605677) DATED 06/28/2021 (MAJOR).

Part: BEAM — CRACKED (L3 DOOR PLUG) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CL3 DOOR PLUG UPPER HORIZONTAL BEAM IS CRACK AT AFT END.REMOVED AND REPLACED CRACKED HORZ BEAM IAW SRM 51-35-01,51-33-01 AND 51-31-01 (MINOR).

Part: INTERCOSTAL — CRACKED (VERTICAL STAB) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CLOWER VERTICAL STABILIZER REAR CENTER SPAR INTERCOSTAL IS CRACKED AT STA. YID= 375, XID= 7.1 AND ZID= 65.REPAIRED CRACKED LOWER VERTICAL STABILIZER REAR CENTER SPAR INTERCOSTAL AT STA. YID= 375, XID= 7.1 AND ZID= 65 IAW VT-SAA EA 011-5530-01-A9171 REV. I/R AND UPS EO MD11-5530-80832-A. (MAJOR) REF. FAA FORM 8100-9 BY S.KANG (AR-605677) DATED 06/24/2021.

Part: TEE FITTING — CORRODED (WNG-BDY FAIRING) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CR/H AFT LOWER WING TO BODY FAIRING SUPPORT FRAME AT STA 1521 IS CORRODED.REPAIRED CORRODED R/H AFT LOWER WING TO BODY FAIRING SUPPORT FRAME TEE AT STA 1521 IAW VT-SAA EA 011-5314-01-A9182 REV. IR AND UPS EO MD11-5320-80808-A. (MINOR)

Part: BRACKET — RUSTED (RT WING TE FLAP) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CR/H WING O/B FLAP I/B FWD. HINGE O/B SIDE LOAD FITTING HAS RUST COMING OUT.REMOVED AND REPLACED SIDE LOAD FITTING/BRACKET IAW AMM 57-53-01-400-801. (MINOR)

Part: SEAT TRACK — CRACKED (BS 1421) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CMAIN CABIN SEAT TRACK IS CRACKED AT STA. 1421 AT X= 27.50.REAPIRED CRACKED SEAT TRACK BETWEEN STA. 1411 TO 1431 AT X= 27.50 IAW SRM 53-00-52 REPAIR 1 FIG. 201. (MAJOR)

Part: INTERCOSTAL — CRACKED (FWD CARGO LH) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:C3FWD CARGO COMPARTMENT INTERCOSTAL CRACK AT STA. 6-50 BETWEEN LON 42L-43L.REMOVED,FABRICATED AND REPLACED CRACKED INTERCOSTAL IAW SRM 51-35-01 AND 51-31-01 (MINOR).

Part: RUB STRIP — CRACKED (RT WING) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CRT WING #2 SLAT LOWER RUB STRIP CRACK AT O/B T/E STA.XIS 358.005.REPAIRED CRACKED RUB STRIP IAW VT-SAA EA 011-5754-01-A9197 REV I/R AND UPS EO MD11-5750-80874-A (MINOR).

Part: ATTACH ANGLE — CRACKED (BS 1361) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CR/H UPPER WING TO BODY FAIRING SUPPORT ATTACH ANGLE IS CRACKED AT STA. 1361.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. AEA0553 AND SRM 51-35-01. (MINOR)

Part: SUPPORT ANGLE — CRACKED (CENTER CARGO LH) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:C3CENTER CARGO COMPARTMENT FRAME SUPPORT ANGLE CRACK AT STA. 5-53 LON 41L.REMOVED,FABRICATED AND REPLACED CRACKED SUPPORT ANGLE IAW SRM 51-35-01 AND 51-33-01 (MINOR).

Part: ATTACH ANGLE — CRACKED (BS 1561) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:C3CENTER CARGO COMPARTMENT SLOPE PANEL SUPPORT ANGLE CRACK AT STA.1561 RH SIDE.REMOVED,FABRICATED AND REPLACED CRACKED SUPPORT ANGLE IAW SRM 51-33-01 AND 51-35-01 (MINOR).

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CAFT CARGO FLOOR BEAM SUPPORT AT STA. 1841 AND X= 46 IS CORRODED.REPAIRED CORRODED AFT CARGO FLOOR BEAM SUPPORT AT STA 1841 AND X= 46 IAW EA 011-5310-01-A9187 REV. IR AND EO MD11-5310-80841-A. REF. FAA FORM 8110-3. (MAJOR)

Part: SUPPORT — CRACKED (BS 1761 L41L) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CCENTER CARGO FRAME ANGLE/SUPPORT IS CRACKED AT STA. 1761 AND LONG. 41L.REMOVED, FABRICATED AND REPLACED SUPPORT IAW DWG ADA0130 AND SRM 51-35-01. (MINOR)

Part: ANGLE — CRACKED (FWD CARGO) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:C3FWD CARGO COMPARTMENT STRUT TO FLOOR BEAM TEE ANGLE CRACK AT STA. 6-75 RBL 58".REMOVED,FABRICATED AND REPLACED CRACKED TEE ANGLE IAW SRM 51-33-01 (MINOR).

Part: FRAME ANGLE — CRACKED (BS 1701 L41L) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:C3CENTER CARGO FRAME ANGLE CRACK AT STA.1701 LON 41L.REMOVED,FABRICATED AND REPLACED CRACKED FRAME ANGLE IAW SRM 51-31-01 AND 51-35-01 (MINOR).

Part: TRUSS — CRACKED (BS 1159 L27R) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CLONGERON 27R/H TRUSS FITTING IS CRACKED AT STA. 1159.REMOVED, FABRICATED AND REPLACED TRUSS FITTING IAW DWG. AFA7605 AND SRM 51-31-01. (MINOR)

Part: SKIN — GOUGED (RT WING) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CR/H WING FIXED L/E UPPER SKIN IS GOUGED BETWEEN STA. XOS. 1187 TO 1191 & 10" FWD FROM AFT EDGE.REPAIRED R/H WING FIXED L/E UPPER SKIN BETWEEN STA. XOS. 1187 TO 1191 & 10" FWD. FROM AFT EDGE IAW SRM 57-40-01 REPAIR 16. (MAJOR)

Part: SKIN — CORRODED (RT WING) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CRT WING UPPER SURFACE BETWEEN STA. XORS 372 - XORS 402 AT STRINGER 6 IS CORRODED.REPAIRED CORRODED RT WING UPPER SURFACE BETWEEN STA. XORS 372 - XORS 402 AT STRINGER 6 IAW VT-SAA EA 011-5730-01-A9178 REV. IR AND UPS EO MD11-5730-80772-A. (MINOR)

Part: SKIN — CORRODED (RT WING) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CRT WING UPPER SKIN BETWEEN XORS 97 TO XORS 130.40 AT STRINGER 15 IS CORRODED.REPAIRED CORRODED RT WING UPPER SKIN BETWEEN XORS 97 TO XORS 130.40 AT STRINGER 15 IAW VT-SAA EA 011-5730-01-A9179 REV. IR AND UPS EO MD11-5730-80823-A. REF. FAA FORM 8100-9 SIGNED BY STEPHEN KANG (AR-605677) DATED 06/24/2021 (MAJOR)

Part: SPAR CAP — CORRODED (LT WING) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CLT WING REAR SPAR LOWER CAP VERTICAL FLANGE BETWEEN STA XORS 724 AND XORS 730 IS CORRODED.REPAIRED CORRODED LT WING REAR SPAR LOWER CAP VERTICAL FLANGE BETWEEN STA XORS 724 AND XORS 730 IAW VT-SAA EA 011-5710-01-A9174 REV. IR AND UPS EO MD11-5710-80710-A. (MINOR)

Part: SPAR CAP — CORRODED (RT WING) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3C, RT WING UPPER T/E PANELS ARE BULGED AT REAR SPAR APPROX. XORS 980.REPAIRED CORRODED RT WING UPPER REAR SPAR CAP AFT FLANGE BETWEEN XORS 964 - XORS 989 IAW EA 011-5710-01-A9175 REV. IR AND UPS EO MD11-5710-80846-A. REF. FAA FORM 8100-9. (MAJOR)

Part: SUPPORT ANGLE — CRACKED (LT I/B T/E WING) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:C3LH I/B T/E WING ACCESS PANEL #541JB LWR SUPPORT ANGLE CRACK.REMOVED,FABRICATED AND REPLACED CRACK SUPPORT ANGLE IAW SRM 51-31-01 AND 51-33-01 (MINOR).

Part: SPAR CAP — CORRODED (RT WING) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CRT WING UPPER T/E PANEL IS BULGED AT REAR SPAR & APPROX. XORS 813.REPAIRED CORRODED RT WING REAR SPAR UPPER CAP AFT FLANGE BETWEEN XORS 769.25 AND XORS 826 IAW VT-SAA EA 011-5710-01-A9193 REV. IR AND UPS EO MD11-5710-80793-A. (MINOR)

Part: SPAR CAP — CORRODED (RT WING TE) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CRT WING UPPER T/E PANEL IS BULGED JUST FWD OF #5 SPOILER O/B HINGE.REPAIRED CORRODED RT WING REAR SPAR UPPER CAP AFT FLANGE BETWEEN XORS 769.25 - XORS 826 IAW VT-SAA EA 011-5710-01-A9193 REV. IR AND UPS EO MD11-5710-80793-A. (MINOR)

Part: SKIN — CORRODED (LT WING) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CL/H WING UPPER SKIN HAS CORROSION BETWEEN STA. XORS. 185 TO XORS. 196.5 AT STR. 11.REPAIRED CORRODED L/H WING UPPER SKIN BETWEEN STA. XORS. 185 TO XORS. 196.50 AT STR. 11 IAW VT-SAA EA 011-5720-01-A9181 REV. I/R AND UPS EO MD11-5730-80803-A, REF. FAA FORM 8100-9 SIGNED BY S. KANG (AR-605677) DATED 6/22/2021.

Part: STRINGER — CRACKED (LT WING) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:2CLT WING FIXED L/E STRINGER CRACKED BETWEEN STA. XOS 789.6 TO XOS 795.7.REPAIRED CRACKED LT WING FIXED L/E STRINGER BETWEEN STA. XOS 789.6 TO XOS 795.7 IAW SRM 57-40-03 REPAIR 2 FIG 201. (MAJOR)

Part: SKIN — CRACKED (LT WING) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CL/H WING L/E LOWER SKIN IS CRACKED AT STA. XOS.= 490.850.REPAIRED CRACKED L/H WING FIXED L/E LOWER SKIN AT STA. XOS.=490.850 IAW SRM 57-40-01 REPAIR 17 FIG. 201. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 661.71 TO 673.76.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 661.71 TO 673.76 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CL/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 698.1274 TO 703.5466.REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 698.1274 TO 703.5466 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 692.038 TO 698.127.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 692.038 TO 698.127 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:C3RH WING FIXED L/E SPLICE DOUBLER CRACK AT XOS STA.585.REMOVED,FABRICATED AND REPLACED CRACKED SPLICE DOUBLER IAW SRM 51-31-01 (MINOR).

Part: DOUBLER — CRACKED (RT WING) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED AT STA. XOS. 578.584.REPAIRED CRACKED R/H WIG FIXED L/E BEADED DOUBLER AT STA. XOS. 578.584 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CLT WING FIXED L/E SKIN SPLICE DOUBLER AT STA XOS 667 IS CRACKED.REMOVED AND REPLACED CRACKED LT WING FIXED L/E SKIN SPLICE DOUBLER AT STA XOS 667 IAW SRM 51-33-01. (MINOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED AT STA. XOS. 667.673.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER AT STA. XOS. 667.673 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CL/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 625.5 TO 629.6.REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 625.5 TO 629.6 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CLT WING FIXED L/E BEADED DOUBLER BETWEEN XOS 789.6 TO XOS 795.7 IS CRACKED.REPAIRED CRACKED LT WING FIXED L/E BEADED DOUBLER BETWEEN XOS 789.6 TO XOS 795.7 IAW SRM 57-40-02 REPAIR I5 FIG 205. (MAJOR).

Part: BRACKET — DAMAGED (NLG W/W) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3CNLG RETRACT ACTUATOR BRACKET L/H UPPER LUG IS DAMAGED.REPAIRED DAMAGED NLG RETRACT ACTUATOR BRACKET L/H UPPER LUG IAW VT-SAA EA 011-5310-01-A9168 REV. IR AND UPS EO MD11-5310-80877-A. (MINOR)

Part: DOOR — CRACKED (LT MLG) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:C3LT MLG DOOR EXTENSION FWD CORNER IS CRACKED.REMOVED AND REPLACED CRACKED DOOR CORNER IAW SRM 51-31-01 AND 51-35-01 (MINOR).

Part: STRUCTURE — CRACKED (THRUST REVERSER) · airframe 78,039 hrs · 17,551 cycles

INSPECTION TYPE:3C#1 ENGINE L/H T/R LOWER BIFURCATION ASSY STRUCTURE IS CRACKED.REPAIRED CRACKED 31 ENGINE L/H T/R LOWER BIFURCATION ASSY STRUCTURE IAW VT-SAA EA 011-7830-01-A9169 REV. IR AND UPS EO MD11-7830-80639-A. (MINOR)

Part: SKIN — CORRODED (LT WING) · airframe 78,035 hrs · 17,549 cycles

INSPECTION TYPE:3CLT WING UPPER SKIN BETWEEN STA XORS 97 - XORS 130.40 AND BETWEEN STRINGER 11 - STRINGER 15 IS CORRODED.REPAIRED CORRODED LT WING UPPER SKIN BETWEEN STA XORS 97 - XORS 130.40 AND BETWEEN STRINGER 11 - STRINGER 15 IAW VT-SAA EA 011-5730-01-A9188 REV. IR AND UPS EO MD11-5730-80786-A. (MINOR)

Part: ANGLE — CRACKED (NR 2 INLET) · airframe 77,508 hrs · 17,303 cycles

INSPECTION TYPE: S/V NR 2 ENGINE INLET LOWER VERTICAL STABILIZER REAR SPAR FIRE SEAL ZEE EXTRUSION IS CRACKED. REMOVED, FABRICATED AND REPLACED CRACKED NR 2 ENGINE INLET LOWER VERTICAL STABILIZER REAR SPAR FIRE SEAL ZEE EXTRUSION, IAW VT-SAA EA 011-5530-01-A8804 REV I/R AND UPS EO MD11-5530-79116-A. (MAJOR)

Part: SOLENOID — INOPERATIVE (LT DOORS) · airframe 77,398 hrs · 17,258 cycles

CREW DOOR LEFT SIDE ELECTRIC DOOR SWITCH INTERMITTENT BOTH IN CABIN AND EXTERIOR SWITCHES INTERMITTENT. DEFERRAL ISSUED, PER MD11 MEL 52-10-3-1-2-1-2 PLACARDS INSTALLED DMI LOG UPDATED. REPLACED L1 DOOR LOCK PIN RELEASE SOLENOID, PER MM 52-10-06, FUNCTIONAL TEST GOOD. THIS CLEARS M729452 IPC: 52-11-70-01-070K.

Part: DOOR — MALFUNCTIONED (L1) · airframe 77,252 hrs · 17,191 cycles

INSPECTION TYPE: N/A LEFT MAIN ENTRY DOOR ELEC OPERATION INOPERABLE. PERFORMED OPERATIONAL CHECK OF FWD ENTRY DOOR IN NORMAL MODE, REF MD11 AMM 52 10 01. DOOR OPERATES NORMAL NO FAULTS NOTED AT THIS TIME.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 77,083 hrs · 17,117 cycles

INSPECTION TYPE: NA EMERGENCY LIGHT BATTERY 1 LO FAULT. R & R EMERGENCY LIGHT BATTERY POWER SUPPLY, PER MM33-51-01-400-802.

Part: FILTER — LEAKING (NR 3 ENGINE) · airframe 76,821 hrs · 16,997 cycles

ATB - EMERGENCY DECLARED, APPROX 22,000 FT NR 3 OIL QTY SHOWED 1 IN AMBER BOX. AFTER RUNNING NON-ALERT CHECKLIST, NR 3 ENG PRESSURE STARTED TO DECREASE. LEVEL AT 26,000 FT RECEIVED LVL 2 ENG OIL PRESS LO. ENG 3 WAS THEN SHUT DOWN. FOUND NR NR 3 ENG OIL FILTER HOUSING MOUNT BOLT OUT OF CASE. REPLACING NR 3 ENG. FOUND THE NR 3 ENGINE MAIN OIL FILTER HOUSING STUDS LOOSE AND PULLED OUT. REMOVED MAIN OIL FILTER HOUSING IAW AMM 72-65-04-000-868. REPLACED ENGINE IAW WAN 3136145.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU DOOR) · airframe 76,767 hrs · 16,968 cycles

APU DOOR DIASG LVL 1 CAME ON AFTER TAKEOFF. MESSAGE WENT AWAY AFTER 10 MINS INFLIGHT. OPS TESTED APU INLET & EXHAUST DOORS IAW AMM 49-17-01. OPS TESTED GOOD.

Part: BRACKET — CHAFED (NR 2 ENGINE) · airframe 76,692 hrs · 16,937 cycles

INSPECTION TYPE:SV NR 2 ENGINE BRIDGE ASSY BOX RIB 2ND FROM O/B ON RT SIDE HAS A CHAFED BOLT HOLE. REMOVED AND REPLACED NR 2 ENGINE BRIDGE ASSY BOX RIB 2ND FROM O/B IAW SRM 51-33-01. (MINOR)

Part: SKIN — CHAFED (FAN COWLING) · airframe 76,692 hrs · 16,937 cycles

INSPECTION TYPE:SV NR 2 LT FAN COWL CLOSE OUT (DOOR JAMB) SKIN IS CHAFED THROUGH. REMOVED AND REPLACED CHAFED NR 2 LT FAN COWL CLOSE OUT (DOOR JAMB) SKIN IAW SRM 51-35-01. (MINOR)

Part: CHANNEL — DAMAGED (FAN COWLING) · airframe 76,692 hrs · 16,937 cycles

INSPECTION TYPE:SV NR 2 ENG LT FAN COWL SKIN PANEL LANDING HAT CHANNEL IS DAMAGED. REPAIRED HAT CHANNEL IAW SRM 54-00-00 FIG 208. (MINOR)

Part: CHANNEL — DAMAGED (NR 2 PYLON) · airframe 76,692 hrs · 16,937 cycles

INSPECTION TYPE:SV NR 2 ENG, PYLON FAN COWL LANDING HAT CHANNEL IS DAMAGED. REPAIRED NR 2 PYLON FAN COWL LANDING HAT CHANNEL IAW SRM 54-00-00 FIG 208. (MINOR)

Part: CHANNEL — DAMAGED (FAN COWLING) · airframe 76,692 hrs · 16,937 cycles

INSPECTION TYPE:SV LT FAN COWL LANGING FRAME IS DAMAGED(MID-SPAN). REPAIRED FAN COWL FRAME IAW SRM 54-00-00 FIG 208. (MINOR)

Part: CHANNEL — DAMAGED (FAN COWLING) · airframe 76,692 hrs · 16,937 cycles

INSPECTION TYPE:SV NR 2 PYLON RT FAN COWL LANDING HAT CHANNEL IS DAMAGED. REPAIRED DAMAGED HAT CHANNEL IAW SRM 54-00-00 FIG 208. (MINOR)

Part: SKIN — CHAFED (FAN COWLING) · airframe 76,692 hrs · 16,937 cycles

INSPECTION TYPE:SV NR 2 RT FAN COWL CLOSE OUT SKIN (DOOR JAMB) SKIN IS CHAFED THROUGH. REMOVED AND REPLACED CHAFED NR 2 RT FAN COWL CLOSE OUT (DOOR JAMB) SKIN IAW SRM 51-35-01. (MINOR)

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 76,689 hrs · 16,936 cycles

INSPECTION TYPE:SV LOWER VERTICAL STABILIZER REAR SPAR FIRE SEAL ANGLE CRACKS. REMOVED AND REPLACED CRACKED LOWER VERTICAL STABILIZER REAR SPAR FIRE SEAL IAW EA 011-5530-01-A8380 REV IR AND EO MD11-5530-77008-A. (MAJOR)

Part: MOUNT BRACKET — CRACKED (AFT FUSELAGE) · airframe 76,132 hrs · 16,675 cycles

INSPECTION TYPE:2CAFT FUSELAGE COMPARTMENT 316 HAS RT UPPER SURGE DUCT UPPER MOUNT BRACKET CLIP CRACKED.REMOVED AND REPLACED CRACKED AFT FUSELAGE COMPARTMENT 316 RT UPPER SURGE DUCT UPPERMOUNT BRACKET CLIP IAW MD-11 SRM 51-33-01. (MINOR)

Part: POWER SUPPLY — FAULTED (CABIN) · airframe 75,420 hrs · 16,352 cycles

INSPECTION TYPE:N/A **SUPPLEMENTAL SDR** EMER LT BAT 1 LO LEVEL ONE ALERT AFTER TEST. DEFERRED PER MEL 33-50-4 ASSIGNED M682153 PLACARD INSTALLED C/W DMP 33-50-4. REPLACED EMERGENCY LIGHTING BATTERY POWER SUPPLY IAW AMM 33-51-01-000-802/33-51-01-400-802. OPS CK GOOD. THIS CLEARS M6825153.

Part: UNKNOWN — MALFUNCTIONED (AILERON) · airframe 75,133 hrs · 16,224 cycles

INSPECTION TYPE:NA DIVERSION -- AFTER T/O FLAP/SLAT RETRACTION LEVEL 2 AIL DEFLECT DISAG AC FT VERY DIFFICULT TO CONTROL REQUIRING ALMOST FULL RT AILERON AT TIMES QRH CHECK LIST NO HELP DECLARED EMERGENCY AND DIVERTED TO KCVG. DEFERRED PER MEL 27-13-2-0-1 DMP 27-13-2-0-1 C/W. **SUPPLEMENTAL SDR**REF D674590 LOGPAGE 082589 IT 2. PERFORMED FUNCTIONAL TEST OF THE AILERON DEFLECTION CONTROL ACTUATOR OPS CHECK GOOD REF 27-16-00-700-801. PLACARD REMOVED REVERSED DMP CLEARED DMI LOG THIS CLEARS DEFERRAL M674589. AIRCRAFT OK FOR SERVICE.

Part: PAN — CRACKED (CARGO DOOR) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:3C, MCD CARGO DOOR FWD DOOR PAN IS CRACKED. ACCOMPLISHED REPAIR ON MAIN CARGO DOOR FWD PAN PER EA 011-5230-01-A7804 I/R, AND EO MD11-5230-72967-A PARA 6A. THIS IS A MAJOR REPAIR

Part: STIFFENER — CRACKED (MLG WW) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:2C, DURING INSTALLATION OF #3 SYSTEM HYDRAULIC RESERVOIR FOUND LOWER MOUNT INTERCOSTAL (STIFFENER) CRACKED.REMOVED AND REPLACED CRACKED #3 SYSTEM HYDRAULIC RESERVOIR LOWER MOUNT INTERCOSTAL (STIFFENER) IAW MD-11 SRM 51-31-01, 51-35-01 AND 51-33-01. (MINOR)

Part: DOUBLER — WORN (TAILCONE) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:3C, TAILCONE LH INTERNAL UPPER PRODUCTION DOUBLER HAS DEEP WEAR. ACCOMPLISHED REPAIR ON TAILCONE LH INTERNAL PRODUCTION DOUBLER PER UPS EO MD-11 5350-66790 APPENDIX A

Part: FUEL TANK — CORRODED (CENTER) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:3CCENTER WING BOX UPPER AFT SKIN CORRODED AT STGR 5 BETWEEN XCW -101 AND XCW -110ACCOMPLISHED BLEND OUT REPAIR ON CENTER WING TANK UPPER AFT SKIN AT STGR 5 BETWEEN XCW -101 AND XCW -110 PER VT SAA EA# 011-5730-01-A7784 REV I/R AND UPS EO MD-11 573--72835-A

Part: DOUBLER — WORN (TAILCONE) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:3C, TAILCONE RH INTERNAL UPPER PRODUCTION DOUBLER HAS DEEP WEAR, ACCOMPLISHED REPAIR ON TAILCONE RH UPPER INTERNAL DOUBLER PER UPS EO MD-11-5350-66790-A APPENDIX A

Part: STIFFENER — CRACKED (AFT CARGO) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:2CAFT CARGO AT STA. 1841 BL 0 BELOW FLOOR HAS A CRACKED VERTICAL STIFFENER.REMOVED AND REPLACED CRACKED VERTICAL STIFFENER AT STA. 1841 BL 0 BELOW AFT CARGO FLOOR IAW MD-11 SRM 51-33-01. (MINOR)

Part: LONGERON — CORRODED (BS 1541-1561) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:2CCENTER CARGO BILGE AREA HAS CORROSION ON LONGERON 48L SPLICE BETWEEN STA. 1541 - 1561.REPAIRED CORRODED CENTER CARGO LONGERON 48L SPLICE BETWEEN STA. 1541 - 1561 IAW MD-11 SRM 53-00-05 REPAIR 1 FIGURE 202. (MAJOR)

Part: STIFFENER — CRACKED (AFT CARGO) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:2C, AFT CARGO STA. 1841 LBL 30 BELOW FLOOR HAS A CRACKED VERTICAL STIFFENER.REMOVED AND REPLACED CRACKED VERTICAL STIFFENER AT STA. 1841 LBL 30 BELOW AFT CARGO FLOOR IAW MD-11 SRM 51-33-01. (MINOR)

Part: STIFFENER — CRACKED (BS 1841) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:2C, AFT CARGO AT STA.1841 RBL 30 HAS A CRACKED VERTICAL STIFFENER BELOW FLOOR.REMOVED AND REPLACED CRACKED AFT CARGO VERTICAL STIFFENER AT STA. 1841 RBL 30 BELOW FLOOR IAW MD-11 SRM 51-33-01. (MINOR)

Part: LONGERON — CORRODED (BS 1641-1661) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:2CCENTER CARGO BILGE AREA HAS CORROSION ON LONGERON 44R BETWEEN STA. 1641 - 1661. REPAIRED CORRODED CENTER CARGO LONGERON 44R BETWEEN STA. 1641 AND STA. 1681 IAW VT-SAA EA 011-5310-01-A7789 REV. IR AND UPS MD11-5310--72928-A. (MAJOR)

Part: LUG — GOUGED (THRUST REVERSER) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:2C#3 ENG. L/H T/R UPPER LUG IS GOUGED.REPAIRED GOUGED #3 L/H T/R UPPER BEAM AFT CASCADE RING LUG IAW VT-SAA EA 011-7830-01-A7793 REV. IR AND UPS EO MD11-7830-72915-A. (MINOR)

Part: FLOOR SUPPORT — CRACKED (BS 1751) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:2CCENTER CARGO AT STA. 1751 AND LONG. 41 L/H, FLOOR SUPPORT ANGLE IS CRACKED.REMOVED, FABRICATED AND REPLACED FLOOR SUPPORT ANGLE AT STA. 1751 AND LONG. 41 L/H IAW DWG. ADA0130 AND SRM 51-33-01. (MINOR)

Part: FLOOR SUPPORT — CRACKED (CENTER CARGO) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:2CCENTER CARGO AT STA. 1741 AND LONG. 41 L/H, FLOOR SUPPORT ANGLE IS CRACKED.REMOVED, FABRICATED AND REPLACED FLOOR SUPPORT ANGLE AT STA. 1741 AND LONG. 41 L/H IAW DWG. ADA0130 AND SRM 51-33-01. (MINOR)

Part: SKIN — CRACKED (LT WING) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:2CL/H WING LOWER SKIN AT ACCESS PANEL LANDING STA. XORS.= 683.4- 713.650 HAS 6 CRACKED FASTENER HOLES.REPAIRED CRACKED L/H WING LOWER SKIN AT ACCESS PANEL LANDING BETWEEM STA. XORS.= 683.4- 713.650 IAW SRM 57-20-02 REPAIR 5 FIG. 201. (MINOR)

Part: FLOOR SUPPORT — CRACKED (CENTER CARGO) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:2CCENTER CARGO AT STA. 1781 AND LONG. 41 L/H, FLOOR SUPPORT ANGLE IS CRACKED.REMOVED, FABRICATED AND REPLACED FLOOR SUPPORT ANGLE AT STA. 1781 AND LONG. 41 L/H IAW DWG. AFA7295 AND SRM 51-33-01. (MINOR)

Part: SKIN — CRACKED (RT WING) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:2CR/H WING LOWER SURFACE AT PANEL #636AB, PANEL LANDING HAS 13 CRACKS AT FASTENER HOLES ( STA. XORS.=683.4-713.65)REPAIRED CRACKED R/H WING LOWER SURFACE PANEL LANDING BETWEEN STA. XORS. 683.4- 713.65 IAW SRM 57-20-02 REPAIR 5 FIG. 201.(MINOR)

Part: BEAM — CRACKED (FWD CARGO) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:2C, FWD LOWER CARGO STA. 6-73 ABOVE LONGERON 43 L/H HORIZONTAL BEAM IS CRACKED AND CORRODED.REMOVED AND REPLACED CRACKED & CORRODED FWD LOWER CARGO HORIZONTAL BEAM AT STA. 6-73 ABOVE LONGERON 43L IAW MD-11 SRM 51-35-01 & 51-33-01. (MINOR)

Part: WEB — CRACKED (BS 1307) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:2CL-3 DOOR JAMB LOWER AFT WEB IS CRACKED AT STA. 1307 AND Z=-18.REPAIRED CRACKED L-3 DOOR JAMB LOWER AFT WEB AT STA. 1307 AND Z=-18 IAW SRM 53-40-15 REPAIR 3 FIG. 201. (MAJOR)

Part: BRACE — BROKEN (RT WING) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:2C, RT WING T/E VERTICAL SUPPORT (BRACE) JUST AFT OF MLG AT APPROX. XOS 247 IS BROKEN.REMOVED AND REPLACED RT WING T/E VERTICAL SUPPORT (BRACE) JUST AFT OF MLG AT APPROX. XOS 247 IAW MD-11 SRM 51-31-01 & 51-33-01. (MINOR)

Part: PANEL — GOUGED (RT WING) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:2CR/H WING LOWER L/E PANEL 615DB HAS TOOLING MARKS AROUND FASTENER HOLES.REPAIRED DAMAGED R/H WING L/E PANEL 615DB IAW VT-SAA EA 011-5730-01-A7798 REV. IR AND UPS EO MD11-5720-72921-A. (MINOR)

Part: VANE — DAMAGED (RT WING TE FLAP) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:2CR/H O/B FLAP VANE O/B LOWER EDGE IS DAMAGED.REPAIRED DAMAGED R/H O/B FLAP VANE O/B LOWER EDGE IAW MD-11 SRM 57-50-80, REPAIR 2, PARA. 2.A(2)(A)(5). (MAJOR)

Part: DOUBLER — CRACKED (LT WING LE) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:2CLT WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN XOS 633 - 636.REPAIRED CRACKED LT WING FIXED L/E BEADED DOUBLER BETWEEN XOS 633 - 636 IAW MD-11 SRM 57-40-02 REPAIR 15 FIGURE 205. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:3CL/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS.=648-653.REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS=648-653 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)

Part: SKIN — CRACKED (RT WING) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:2CR/H WING FIXED L/E SKIN IS CRACKED AT #9 SLAT TRACK CUTOUT.REPAIRED CRACKED R/H WING FIXED L/E SKIN AT XOS=610.8437 IAW MD-11 SRM 57-40-01 REPAIR 18, FIGURE 202. (MAJOR)

Part: CAP — CRACKED (RT WING) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:2C, R/H UNDER WING CANTED PANEL UPPER CAP IS CRACKED AT STA. 1236.8.REPAIRED CRACKED R/H UNDER WING CANTED PANEL UPPER CAP AT STA. 1236.8 IAW UPS EO MD11-5310-72747-A. (MAJOR)

Part: RIB — CRACKED (RT MLG WW) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:2CR/H MLG W/W O/B FWD. DOOR CUT-OUT WEB/RIB IS CRACKED.REMOVED, FABRICATED AND REPLACED WEB/RIB IAW DWG. ANB7180 AND SRM 51-35-01. (MINOR)

Part: ANGLE — CRACKED (RT MLG WW) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:2CR/H MLG W/W O/B FWD. WALL DOOR LANDING/CLIP IS CRACKED.REMOVED, FABRICATED AND REPLACED LANDING/CLIP IAW DWG.ANB7180 AND SRM 51-35-01.(MINOR)

Part: INTERCOSTAL — CRACKED (TAIL CONE) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:2CTAIL CONE R/H CENTER GUIDE PIN INTERCOSTAL IS CRACKED.REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG. AKC7520 AND SRM 51-35-01 & 51-33-01. (MINOR)

Part: ATTACH BRACKET — DAMAGED (NLG) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:2C, NLG OVERCENTER UPPER LINK UPPER ATTACH BOLT HAS ROTATED PAST ANTI-ROTATION TAB. REPAIRED DAMAGED NLG OVERCENTER UPPER LINK UPPER ATTACH BRACKET IAW VT-SAA EA 011-5300-01-A7785 REV IR AND UPS EO MD11-5310-72893-A. (MINOR)

Part: DOUBLER — CRACKED (CTR MLG WW) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:2CCENTER W/W L/G FWD. WALL AT PUSH ROD FEED THRU, THE DOUBLER IS CRACKED.REMOVED AND REPLACED DOUBLER IAW SRM 51-33-01. (MINOR)

Part: SUPPORT BRACKET — CRACKED (NR 1 PYLON) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:2C#1 ENG. PYLON DRIP PAN SUPPORT BRACKET ABOVE FUEL LINE DISCONNECT IS CRACKED.REPAIRED CRACKED #1 ENG. PYLON DRIP PAN SUPPORT BRACKET ABOVE FUEL LINE DISCONNECT IAW VT-SAA EA 011-5420-01-A7799 REV. IR AND UPS EO MD11-5420-72917-A. (MINOR)

Part: ATTACH FITTING — DAMAGED (NLG ACTUATOR) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE: 2C, NLG RETRACT ACTUATOR UPPER ATTACH PIN HAS ROTATED PAST ANTI-ROTATION TAB.REPAIRED DAMAGED NLG RETRACT ACTUATOR UPPER ATTACH LUG IAW VT-SAA EA 011-5300-01-A7785 REV. IR AND UPS EO MD11-5310-72893-A. (MINOR)

Part: SKIN — CHAFED (NR 1 FAN COWL) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:2C#1 ENGINE O/B FAN COWL FWD HINGE FITTING IS CHAFED.REPAIRED CHAFED #1 ENGINE O/B FAN COWL FWD HINGE FITTING IAW VT-SAA EA 011-7110-01-A7782 REV. IR AND UPS EO MD11-7110-72744-A. (MINOR)

Part: TRUNNION — CRACKED (NLG) · airframe 75,122 hrs · 16,216 cycles

INSPECTION TYPE:2CR/H NOSE GEAR TRUNNION FITTING IS CRACKED AT STA. 582.5, Z=-114 AND X=-24.REPAIRED CRACKED R/H NOSE GEAR TRUNNION FITTING AT STA. 582.5, Z=-114 AND X=-24 IAW SRM 53-10-14 REPAIR 2 FIG. 202. (MAJOR)

Part: SKIN — NOT REPORTED (TE FLAP) · airframe 74,773 hrs · 16,091 cycles

INSPECTION TYPE:N/A RIGHT WING OUTBOARD FLAP LOWER SKIN REPAIR AT XOF 547. REPAIRED IAW EO MD11-5750-71297-C.

Part: BEAM — CRACKED (FWD CARGO) · airframe 74,720 hrs · 16,077 cycles

INSPECTION TYPE:2C, FWD CARGO HORIZONTAL BEAM AT STA. 6-73 ABOVE LONGERON 43R IS CRACKED AND CORRODED.REMOVED AND REPLACED CRACKED AND CORRODED FWD CARGO HORIZONTAL BEAM AT STA. 6-73 ABOVE LONGERON 43R IAW MD-11 SRM 51-33-01 & 51-35-01. (MINOR)

Part: DOOR FRAME — CRACKED (MLG DOOR AREA) · airframe 74,700 hrs · 16,067 cycles

INSPECTION TYPE:2CCLG L/H DOOR FWD PAN (FRAME) IS CRACKED.REMOVED AND REPLACED CRACKED CLG L/H DOOR FWD PAN (FRAME) IAW MD-11 SRM 51-35-01 AND 51-35-02. (MINOR)

Part: SKIN — CORRODED (BS 1219-1239) · airframe 74,700 hrs · 16,067 cycles

INSPECTION TYPE: 2C, CENTER WING BOX AT STA. 1219 - 1239 AND X=-101 HAS HEAVY CORROSION AND EXTENDS UNDER CORD ANGLE.REPAIRED CENTER WING TANK UPPER CENTER SKIN BETWEEN S-14 & S-15 AND STA. XCW=-87.5 TO XCW -97 CORROSION IAW VT-SAA EA 011-5730-01-A7787 REV. IR AND UPS EO MD11-5730-72851-A. (MINOR)

Part: SOLENOID — INOPERATIVE (PAX DOOR) · airframe 74,695 hrs · 16,064 cycles

L1 ENTRY DOOR OPENING ELECT INTERMITTENT. DEFERRED L1 ENTRY DOOR PER MEL 52 10 1 2 0 1, ACCOMPLISHED DMP 52 10 1 2 0 1 . REPLACED L1 DOOR RELEASE SOLENOID PER 52-10-06.

Part: CHAIN — MISSING (L1 DOOR) · airframe 74,495 hrs · 16,010 cycles

INSPECTION TYPE:N/A REF DEFERRAL # M659408 L1 DOOR MAIN ENTRY DOOR INOP. PNEUMATIC MOTOR CHAIN MISSING. INSTALLED PNUMATIC MOTOR CHAIN. OPS CK GOOD. IAW AMM 52-11-08. THIS ACTION CLEARS DEFERRAL # M659408. NO DMP TO REVERCE. PLACARD REMOVED REF: 52-11-05-05 #555.

Part: LINK — DEFECTIVE (RT MLG DOOR) · airframe 74,459 hrs · 15,995 cycles

INSPECTION TYPE:N/A ATB - AFTER GEAR RETRACTION THE RIGHT MAIN GEAR INDICATION SHOWED GEAR IN THE DOWN POSITION BOTH ON THE PRIMARY AND SECONDARY INDICATION. RR RT MLG DOOR LINK ASSY REF AMM 32-34-05 OPS CHECKS GOOD PLACED AIRCRAFT ON JACKS PER AMM 7-11-00-582-801 AND PERFORMED GEAR RETRACTION AND EXTENSION TEST PER AMM 32-62-00-700-801 OPS CHECKS NORMAL OK FOR SVC.

Part: BATTERY — DISCHARGED (CABIN) · airframe 74,439 hrs · 15,990 cycles

INSPECTION TYPE:N/A EMERGENCY LIGHTS TEST FAILED EMER LT BATTERY 1 LOW. REMOVED AND INSTALLED NEW EMER LT BATTERY PER AMM 33-51-01-0401 OPS TEST PASSEDÏ¿½Ï¿½ESR: AIPC 33-51-10-01.

Part: SKIN — DENTED (TE FLAP) · airframe 74,111 hrs · 15,847 cycles

RT WING INBD AFT FLAP UPPER SURFACE HAS 3EA DENTS ALL WITHIN 4" CIRCLE. REPAIRED IAW EO 5750-70163-A.

Part: WARNING MESSAGE — FALSE ACTIVATION (EMERGENCY LIGHTS) · airframe 74,104 hrs · 15,842 cycles

EMERGENCY LIGHT BATTERY 1 LOW LEVEL 1 ALERT DURING AN EMERG LIGHT TEST. REVERSED DMP 33-50-4. COMPLIED WITH FIM 33-51-00-101, & AMM 33-51-00, EMERGENCY LIGHTS CHECKED GOOD.

Part: PACKING — LEAKING (FUEL FILTER BOWL) · airframe 74,066 hrs · 15,829 cycles

NR 1 ENGINE LEAKING FUEL FROM THE FUEL FILTER BOWL. REMOVED AND REPLACED THE PACKING ON THE FUEL FILTER BOWL COVER PLATE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 73,240 hrs · 15,546 cycles

DURING PDC, EMERGENCY LIGHT BATTERY LOW ALERT APPEARED ON THE EAD. .R & R THE BATTERY PACK IAW AMM 33-51-01, REV 90.07. OPS TEST PASSED.

Part: RELAY — INOPERATIVE · airframe 72,584 hrs · 15,349 cycles

INSPECTION TYPE:N/AATB - AT TOP OF CLIMB FIRST OSERVED LVL 1 "BUS DC 3 OFF" FOLLOWED BY LVL 2" FCC 2A DATA FAULT" AND LVL1 ENG3 FADEC FAULT AND A ICE SENSOR FAIL AND SEL LSAS RIBOFF. YAW DMP UPR B OFF, A/P SINGLER & R RELAY R2 51 53 AND RCEB B1- 894 IAW MD11 MM 24 50 01 24 08 02 ESR 24 61 01 01 & 24 67 53 01

Part: CONNECTOR — DAMAGED (R1 DOOR ACTUATOR) · airframe 71,958 hrs · 15,204 cycles

R1 DOOR ELECTRICAL ACTUATOR DAMAGED AT CONNECTOR SHROUD. R&R THE ACTUATOR IAW MM 52-11-01-401, THRU STEP F(1)(D) TH 0557558 9-11-17, AND AMM 52-11-01.

Part: CABLE — DISCONNECTED (R1 DOOR) · airframe 71,958 hrs · 15,204 cycles

R1 DOOR FOLLOW UP PANEL CABLE DISCONNECTED. CONNECTED THE CABLE AT CLEVIS.

Part: TORQUE TUBE — SCORED (R1 DOOR) · airframe 71,958 hrs · 15,204 cycles

R1 DOOR FWD DRIVE TORQUE TUBE FOUND SCORED, CIRCUMFRENTIALLY NEAR SPLINED END. REMOVED AND REPLACED THE TORQUE TUBE.

Part: CABLE — DAMAGED (R1 DOOR) · airframe 71,958 hrs · 15,204 cycles

R1 DOOR FWD UPPER CABLE, UPPER ROD ASSY DAMAGED. R & R THE ROD ASSY IAW AMM 32-11-03.

Part: GUARD — BROKEN (R1 DOOR) · airframe 71,958 hrs · 15,204 cycles

R1 DOOR AFT CABLE DRUM AND SUPPORT ASSY ROLLER CHAIN GUARD BRACKET BROKEN. R & R THE CHAIN GUARD ASSY IAW MM 20-50-02.

Part: DRIVE ASSY — FAILED (R1 DOOR) · airframe 71,958 hrs · 15,204 cycles

R1 DOOR INTERCOSTAL DAMAGED DUE TO DRIVE MECHANISM FAILURE. REPAIRED IAW EO MD11-5310-65637-A

Part: DRUM — BROKEN (R1 DOOR) · airframe 71,901 hrs · 15,182 cycles

R1 DOOR WILL NOT OPEN LOUD GRINDING NOISE. ACCOMPLISHED EO MD11-5210-65441-A THRU PARA 6 A (5) FINISHED REMAINING STEPS OF EO MD11-5210-65441-A. R&R BROKEN DOOR AFT CABLE DRUM AND SUPPORT ASSY ROLLER CHAIN GUARD BRACKET.

Part: THRUST REVERSER — CRACKED (NR 3) · airframe 71,394 hrs · 15,051 cycles

INSPECTION TYPE: 1C, NR 3 ENGINE LT THRUST REVERSER LOWER TRACK GUIDE IS CRACKED. REMOVED AND REPLACED THE THRUST REVERSER IAW AMM 78-13-01-400-868.

Part: TRUSS FITTING — GOUGED (NR 3 NACELLE) · airframe 71,394 hrs · 15,051 cycles

INSPECTION TYPE: 1C, RT WING NR 3 PYLON ENGINE MOUNT, LT TRUSS FITTING HAS TWO GOUGES. REPAIRED THE TRUSS FITTING IAW EA 011-5410-01-A6811 REV I/R, AND EO MD11-7120-64408-A.

Part: SKIN — CORRODED (LT WING) · airframe 71,394 hrs · 15,051 cycles

INSPECTION TYPE: 1C, LT WING UPPER SURFACE HAS CORROSION AT XORS 280 BETWEEN REAR SPAR AND AUX SPAR. REPAIRED SKIN IAW EA 011-5730-01-A6809 REV I/R, AND EO MD11-5730-64409-A.

Part: SKIN — CORRODED (LT WING) · airframe 71,394 hrs · 15,051 cycles

INSPECTION TYPE: 1C, LT WING UPPER FWD SKIN HAS CORROSION BETWEEN XORS. 99.5 AND XORS. 125.3 COMMON TO STRINGER 15. REPAIRED LT WING UPPER FWD SKIN IAW EA 011-5730-01-A6813, REV I/R AND EO MD11-5730-64422-A.

Part: SKIN — DAMAGED (RT WING SLAT) · airframe 71,394 hrs · 15,051 cycles

INSPECTION TYPE: 1C, RIGHT WING NR 5 SLAT LOWER SKIN GOUGED WITH OPEN HOLE BETWEEN XOS 712 - 717. REPAIRED THE SLAT IAW EA 011-5754-01-A6804, REV IR, AND EO MD11-5750-64373-A.

Part: SKIN — CRACKED (LT WING) · airframe 71,394 hrs · 15,051 cycles

INSPECTION TYPE: 1C, LT DROOPED L/E FORWARD OTBD SKIN CHAFED AND CRACKED. REPAIRED THE SKIN IAW SRM 57-40-01, REPAIR 15, FIG 202. MAJOR.

Part: DOUBLER — CRACKED (RT WING) · airframe 71,394 hrs · 15,051 cycles

INSPECTION TYPE: 1C, RT WING FIXED L/E BEADED DOUBLER IS CRACKED AT XOS 589. REPAIRED THE DOUBLER IAW SRM 57-40-05, REPAIR 15, FIG 205. MAJOR.

Part: PANEL — GOUGED (NR 3 PYLON) · airframe 71,394 hrs · 15,051 cycles

INSPECTION TYPE: 1C, NR 3 PYLON PANEL 487BL GOUGED AT VENT. REPAIRED THE PANEL IAW EA 011-5450-01-A6802, REV IR, AND EO MD11-5450-64348-A.

Part: HINGE — CHAFED (NR 3 NACELLE) · airframe 71,394 hrs · 15,051 cycles

INSPECTION TYPE: 1C, THE NR 3 ENGINE. INBD FAN COWL UPPER FWD HINGE IS CHAFED. REPAIRED THE HINGE IAW EA 011-7110-01-A6798, REV I/R, AND EO MD11-7110-64327-A.

Part: SKIN — GOUGED (BS 895) · airframe 71,392 hrs · 15,050 cycles

INSPECTION TYPE: 1C, FUSELAGE SKIN GOUGED AT FWD CARGO DOOR CUT-OUT AT BS 895, LONGERON 41R. REPAIRED THE SKIN IAW SRM 53-00-15, REPAIR 8, FIG. 202. MAJOR.

Part: FITTING — CRACKED (NR 10) · airframe 71,392 hrs · 15,050 cycles

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

Part: DOUBLER — CRACKED (LT WING LE) · airframe 71,392 hrs · 15,050 cycles

INSPECTION TYPE: 1C, LEFT WING FIXED L/E INNER BEADED DOUBLER IS CRACKED BETWEEN XORS. 673.3 AND 703.5. REPAIRED THE DOUBLER IAW EA 011-5740-01-A6805 REV I/R, AND EO MD11-5720-64411-A. MAJOR.

Part: PROXIMITY SENSOR — OUT OF ADJUST (LT MLG) · airframe 71,317 hrs · 15,017 cycles

LANDING GEAR UNSAFE INDICATION BOTH PRIMARY AND SECONDARY WITH GEAR HANDLE UP, MAXIMUM AIRSPEED 245 KNOTS. PERFORMED ADJUSTMENT CLEARANCE CHECK OF LEFT MLG PROXIMITY SENSOR IAW AMM 32-61-15-400-802. FOUND THE SENSOR CONDUIT INTERFERING WITH LINK ASSY B. ADJUSTED CONDUIT LOOP AND JACKED ACFT AND PERFORMED GEAR SWING IAW AMM 07-11-582-801. PRI & SEC GEAR INDICATIONS CHECKED GOOD.

Part: STRAP — MISSING (L1 DOOR) · airframe 71,039 hrs · 14,952 cycles

L1 DOOR RED SAFETY STRAP MISSING. INSTALLED NEW RED SAFETY STRAP IAW AMM 52-12-12.

Part: SKIN — DAMAGED (TE FLAP) · airframe 69,732 hrs · 14,658 cycles

INBD MAIN FLAP UPPER SKIN DAMAGE. REPAIRED IAW EO MD11-5750-61768-A.

Part: CIRCUIT BREAKER — TRIPPED · airframe 69,495 hrs · 14,584 cycles

BUSS LT EMERGENCY DC OFF. INSPECTION FOUND THE LT EMERGENCY DC BUSS FEED TR 1 C/B OUT. PERFORMED RESET OF C/B AND CARRIED OUT OPS CHECK OF THE DC TIE SWITCH LIGHTS IAW AMM TASK 24-08-02-700-803REV 86.00. OPS CHECKED OK. PERFORMED EPCU R-T-S PER AMM 24-08-01-741-801. OPS CHECKED OK. ACFT OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 68,984 hrs · 14,463 cycles

DURING AS-E FOUND EMERGENCY LIGHT BATTERY 1 LOW. R & R EMERGENCY LIGHTING BATTERY NR 1 IAW. AMM 33-51-01, PB 401, REV 85.01, EMERGENCY LIGHTS TEST PASSED.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 68,984 hrs · 14,463 cycles

DURING AS-E FOUND EMERGENCY LIGHT BATTERY 1 LOW. R & R EMERGENCY LIGHTING BATTERY IAW AMM 33-51-01, PB 401, REV 85.01, EMERGENCY LIGHTS TEST PASSED.

Part: PSEU — INOPERATIVE (SLATS) · airframe 68,866 hrs · 14,431 cycles

ON DEPARTURE, AT FLAP RETRACT RECEIVED A STICK SHAKER, MOMENTARY, SAW A MOMENTARY SLAT DISAGREE. AFTER RETRACTING THE SLATS RECEIVED A LEVEL 2 SLAT DISAGREE, SPEED 300 STAYED BELOW 280 KTS AND ACCOMPLISHED SLAT INSP SLAT MECHANICAL SYS, INSP OK SLAT POS IND SYS OPS TEST OK, REF MM 27-84-00-700-801, ACCOMPLISH FIM 31-71-07-00, BLKS 1, 2, 3, 4 AND BLKS 1, 2, 5, 6, 7, 14. BITE PSEU=PREVIOUS FLT FAULT TARGETS 21, 20, 13, 12, 06 AND 06 SENSOR. TESTED SENSOR D1-16 RESISTANCE=TO D1-15 NO SHORTS, IAW WDM 27-84-01, PG 5.1, SHT 2. R & R PSEU.

Part: SKIN PANEL — MISSING (LT WING) · airframe 67,237 hrs · 13,988 cycles

PANEL ABOVE LT OTBD AILERON, OTBD SECTION OF WING SKIN PANEL FOUND MISSING FROM AIRPLANE WHILE PERFORMING OTHER WORK. INSTALL AND FIT ROBBED PANEL ASSEMBLY.

Part: SKIN — DENTED (RIGHT WING) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE: 4C, RT INBD WING LOWER SKIN SURFACE HAS A DENT AT APPROXIMATELY XW BS 158, STRINGER 41. TRANSFERRED FROM 2015060889982, ACCOMPLISHED TIME LIMITED REPAIR PENDING DTA TO RT INBD LOWER WING SKIN AT XORS 130, STR 41R IAW EO 5730-57664A AND EA 011-5730-01-A5837, REV I/R 8100-9.

Part: LONGERON — CORRODED (BS 1741-1781) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE:4C, LONGERON 46R CORRODED STA 1741-1781. REPAIRED THE LONGERON SECTION IAW EA 011-5310-01-A5828, REV IR AND EO MD11-5310-57653-A.

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE:4C, CENTER MLG LT TRUNNION SUPPORT FITTING HAS CORROSION ON UPPER SURFACE ACCOMPLISHED BLEND REPAIR ON CENTER MLG LT TRUNNION FITTING IAW VT-SAA EA 011-5310-01-A5834 REV I/R AND EO 5340-57672-A.

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE: 4C, CENTER MLG RT TRUNNION SUPPORT FITTING HAS CORROSION ON UPPER SURFACE ACCOMPLISHED BLEND REPAIR ON CENTER MLG RT TRUNNION SUPPORT FITTING IAW VT-SAA EA 011-5310-01-A5833, REV I/R AND EO 5340-57671-A.

Part: FRAME — CORRODED (ACCESSORY BAY) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE:4C, TRANSVERSE FRAME IN CENTER ACCESSORY COMPARTMENT HAS CORROSION FS 6-90 BETWEEN L51L AND L51R. ACCOMPLISHED BLEND REPAIR ON TRANSVERSE FRAME IN CENTER ACCESSORY COMPARTMENT FS 6-90 BETWEEN L51L AND L51R IAW SRM 53-00-00 REPAIR GENERAL.

Part: STRINGER — CRACKED (RT WING) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE: 4C, RT WING UPPER STRINGER 16 CRACKED BETWEEN XORS 372 AND XORS 402. ACCOMPLISHED PERMANENT REPAIR ON RT WING UPPER STR 16, BS XORS 372 TO XORS 402 IAW EA 011-5710-01-A5829, REV I/R AND EO MD11-5710-57670-A.

Part: LONGERON — CORRODED (BS 806-824) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE:4C, DISCOVERED CORROSION ON FOWARD CARGO LONGERON 38L BETWEEN FS 806 AND 824. ACCOMPLISHED BLEND REPAIR ON FORWARD CARGO LONGERON 38L BETWEEN FS 806 AND 824 IAW SRM 53-00-00. REPAIR GENERAL FIG 205.

Part: LONGERON — CORRODED (BS 1421-1441) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE:4C, UPPER CARGO LONGERON 16R HAS CORROSION BS 1421 TO 1441. REMOVED, FABRICATED AND REPLACED UPPER CARGO INTERRUPTED LONGERON 16R BS 1421 TO 1441 IAW VT-SAA EA 011-5310-01-A5824 REV I/R AND EO MD11-5310-57506-A.

Part: SKIN — CORRODED (BS 2122-2163) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE: 4C, AFT FUSELAGE, RT SIDE SKIN PANEL CORRODED ALONG PANEL 347DF LOWER INTERFACE. REPAIRED RT TAIL SKIN BS 2122-2163 IAW SRM 53-70-01, REPAIR 3, FIG 201.

Part: SKIN — CRACKED (LT WING) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE: 4C, LT WING L/E EXTERNAL SKIN CRACKED AT XOS907. REPAIRED L/E SKIN XOS 905-909 IAW SRM 57-40-01, REPAIR 9, FIG 201.

Part: LONGERON — CORRODED · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE:4C, CORROSION ON FORWARD CARGO LONGERON 37R, STA 6-02 TO 6-25. ACCOMPLISHED PERMANENT SPLICE REPAIR ON FORWARD CARGO LONGERON 37R FROM STA 6-02 TO 6-25 IAW SRM 53-00-05, REPAIR 1 AND SREO MD11-5310-57161-A.

Part: FLOOR SUPPORT — CORRODED (BS 1900-1979) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE:4C, AFT CAGRO RT FLOOR SUPPORT HAS CORROSION IN MULTIPLE AREAS BS 1900-1979. REMOVED, FABRICATED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-31-01 AND SRM 51-35-01.

Part: CARGO TRACK — CORRODED (AFT CARGO) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE:4C, CARGO TRACK AT DOOR OPENING BS 1917-1947, LBL 31. R & R THE CARGO TRACK IAW SRM 51-31-01.

Part: LONGERON — CORRODED · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE: 4C, HEAVY CORROSION ON LONGERON 36R BS 6-02. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF THE LONGERON IAW DWG A6A7022, AND SRM 51-33-01.

Part: TRUNNION — CRACKED (NLG) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE:4C, NLG LT TRUNNION FITTING CRACKED, BS 587. REPAIRED LT NLG TRUNNION FITTING IAW SRM 53-10-14, REPAIR 2, FIG 202.

Part: LONGERON — CORRODED (MAIN CARGO) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE:4C, MAIN CARGO LONGERON 24R HAS CORROSION BETWEEN FS 6-50 TO 6-70. ACCOMPLISHED REPAIR ON MAIN CARGO LONGERON 24R BETWEEN FS 6-50 TO 6-70 IAW SRM 53-00-05, REPAIR 1, FIG 203.

Part: LONGERON — CORRODED (BS 1361-1381) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE: 4C, LONGERON 16R CORRODED AT BS 1361-1381 CORRODED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW EA 011-5310-01-A5822, REV IR AND EO MD11-5310-57507-A.

Part: LONGERON SPLICE — CRACKED · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE: 4C, LONGERON SPLICE 2L CRACKED AT STA 5-123. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON SPLICE IAW DWG A5A7111, SRM 51-33-01, AND 51-31-01.

Part: SKIN — CORRODED (BS 2007-2033) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE: 4C, AFT FUSLEAGE SKIN CORRODED ALONG LOWER EDGE OF PANEL 347AF INTERFACE, BS 2007 - 2033, L30R. REPAIRED THE SKIN PANEL IAW EA 011-5330-01-A5842, REV IR AND EO MD11-5330-57691-A.

Part: LONGERON — CORRODED (BS 1461-1481) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE:4C, UPPER CARGO LONGERON 16R HAS CORROSION BS 1461 TO 1481. REMOVED, FABRICATED AND REPLACED UPPER CARGO INTERRUPTED LONGERON 16R STA 1461 TO 1481 IAW VT-SAA EA 011-5310-01-A5820, REV I/R AND EO MD11-5310-57580-A.

Part: LONGERON — CORRODED (BS 1481-1501) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE:4C, DISCOVERED CORROSION ON LONGERON 12L IN UPPER CARGO BETWEEN BS 1481 AND 1501. ACCOMPLISHED BLEND REPAIR ON LONGERON IAW SRM 53-00-00.

Part: STRINGER — CRACKED (LT WING) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE:4C, LEFT WING STRINGER 31 CRACKED AT BS XORS 1042. REPAIRED THE STRINGER IAW EA 011-5710-01-A5827, REV IR AND EO MD11-5710-57647-A.

Part: LONGERON — CORRODED (BS 1401-1421) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE:4C, UPPER CARGO LONGERON 16R HAS CORROSION BS 1401 TO 1421. REMOVED, FABRICATED AND REPLACED UPPER CARGO INTERRUPTED LONGERON 16R IAW VT-SAA 011-5310-01-A5825 REV I/R AND EO MD11-5310-57505-A.

Part: LONGERON — CORRODED (BS 1461-1481) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE:4C, DISCOVERED CORROSION ON LONGERON 12L IN UPPER CARGO BETWEEN STA 1461 AND 1481. ACCOMPLISHED BLEND REPAIR ON LONGERON 12L UPPER CARGO BETWEEN 1461 AND 1481 IAW SRM 53-00-00. REPAIR GENERAL FIG 205, MINOR.

Part: LONGERON SPLICE — CRACKED (CARGO BAY) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE:4C, DISCOVERED MAIN CARGO LONGERON SPLICE FITTING CRACKED FS 5-123 L10L. REMOVED, FABRICATED AND REPLACED MAIN CARGO LONGERON SPLICE FITTING STA 5-113 TO 5-123 L10L IAW SRM 51-33-01.

Part: LONGERON SPLICE — CRACKED · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE: 4C, LONGERON SPLICE 44L CRACKED AT BS 5-113. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON SPLICE IAW DWG A5A7116, SRM 51-35-01, AND 51-33-01.

Part: LONGERON SPLICE — CORRODED (BS 1541) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE: 4C, LONGERON SPLICE 36R CORRODED AT BS 1541. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON SPLICE IAW DWG A5A7125, AND SRM 51-33-01.

Part: LONGERON SPLICE — CRACKED (BS 1695) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE:4C, LONGERON SPLICE 25R CRACKED AT BS 1695. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON SPLICE IAW DWG AFA7181, SRM 51-33-01, AND 51-31-01.

Part: LONGERON — CORRODED (BS 1159-1179) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE:4C, UPPER CARGO LONGERON 16R HAS CORROSION BS 1159 TO 1179. REMOVED, FABRICATED AND REPLACED UPPER CARGO. INTERRUPTED LONGERON 16R, BS 1159 TO 1179 IAW VT-SAA EA 011-5310-01-A5821 REV I/R AND EO 5310-57582-A.

Part: LONGERON — CORRODED (BS 1179-1199) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE:4C, UPPER CARGO LONGERON 16R HAS CORROSION STA 1179 TO 1199. REMOVED, FABRICATED AND REPLACED UPPER CARGO INTERRUPTED LONGERON 16R BS 1179 TO 1199 IAW VT-SAA EA 011-5310-01-A5823, REV I/R AND EO MD11-5310-57581-A.

Part: STRINGER — CRACKED (RT WING) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE:4C, RT WING STRINGER 14 CRACKED AT OTBD END. REPAIRED RT STR 14 BETWEEN XORS 506 - 538 IAW EA 011-5710-01-A5832 REV IR AND EO MD11-5710-57652-A.

Part: LONGERON — CRACKED (BS 1257-1305) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE:4C, UPPER CARGO R3 DOOR LONGERON 27R CRACKED ON AFT END. REMOVED, FABRICATED AND REPLACED R3 DOOR LONGERON 27R SRM 51-33-01 AND DWG AEA7127.

Part: LONGERON SPLICE — CRACKED (BS 1651 L13L) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE:4C, MAIN CARGO LONGERON SPLICE CRACKED STA 1651 L13LREMOVED, FABRICATED AND REPLACED MAIN CARGO LONGERON SPLICE IN MAIN CARGO BS 1651, L13L IAW SRM 51-33-01.

Part: SLIDE — NO TEST (L1 DOOR) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE:4C, L1 DOOR ESCAPE SLIDE FAILED TO FULLY DEPLOY DURING TC 4045. OPS CHECK L1 ESCAPE SLIDE ROUTINE REPLACEMENT COMPLIED WITH ON TC4045.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE:4C, RT INBD FLAP UPPER SKIN CRACKED AT XIFH171 AND 177, 10" ABOVE REAR SPAR. REPAIRED RT INBD FLAP UPPER SKIN IAW SRM 57-00-01, REPAIR 1, FIG. 201.

Part: STRINGER — CRACKED (LT WING) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE:4C, DISCOVERED CRACK ON STR 9 LT WING STA XORS 799.40. ACCOMPLISHED PERMANENT REPAIR ON LT WING, STR 9 BETWEEN STA XORS 799.4 AND 826.5 IAW SRM 57-00-03, REPAIR 4, FIG 201.

Part: HINGE BRACKET — CHAFED (RT WING TE FLAP) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE:4C, RT WING INBD FLAP, OTBD FORWARD HINGE BRACKET HAS CHAFE DAMAGE. ACCOMPLISHED BLEND REPAIR ON RT WING INBD FLAP, OTBD FORWARD HINGE BRACKET IAW VT-SAA EA 011-5753-01-A5838 REV I/R AND EO MD11-5740-57650-A, MINOR.

Part: DOUBLER — CORRODED (RT WING) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE:4C, RT WING LOWER MLG TRUNNION SUPPORT DOUBLER HAS CORROSION ON AFT END. ACCOMPLISHED BLEND REPAIR ON RT WING LOWER MLG TRUNNION SUPPORT DOUBLER IAW VT-SAA 011-5730-01-A5830, REV I/R AND EO 5720-57667-A.

Part: DOOR FRAME — CRACKED (BS 1250-1256) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE: 4C, R3 DOOR JAMB LOWER FORWARD LIGHTING HOLE CRACKED BS 1250 TO 1256. ACCOMPLISHED PERMANENT DOUBLER REPAIR TO R3 DOOR JAMB LOWER FORWARD LIGHTING HOLE BS 1250 TO 1256 IAW SRM 53-40-15, REPAIR 3, FIGURE 201.

Part: STRINGER — CRACKED (LT WING) · airframe 67,099 hrs · 13,960 cycles

INSPECTION TYPE: 4C, LT WING L/E PANEL LANDING STRINGER CRACKED AT STA XOS 909, REPLACES 2015052289342. ACCOMPLISHED PERMANENT DOUBLER REPAIR ON LT WING L/E PANEL LANDING STR AT STA XOS 909 IAW SRM 57-40-03, FIG 201, REPAIR 1, MAJOR.

Part: CONTROL UNIT — FAILED (COCKPIT) · airframe 66,658 hrs · 13,836 cycles

FUMES IN THE COCKPIT AT 380FL. DONNED O2 MASK. ALSO, HAD FUEL LEVEL ALERT 1 TANK 3 AND TANK3 FUEL QTY LOW. RECIEVED A ENG 2 START VALVE OPEN LIGHT ILLUMINTED. EMERGENCY DECLARED. PERFORMED GVI OF AVIONICS BAY EQUIPMENT RACKS & WIRING. ACFT FOUND NORMAL. FOUND ACU-2 FAILED SUSPECT CAUSE OF FUMES. R & R ACU IAW AMM 33-15-01-000 AND 400 DPS TESTS NORMAL IAW MM 33-15-01-700.

Part: UNKNOWN — ODOR (COCKPIT)

FUMES IN THE COCKPIT AT 380FL. DONNED OXYGEN MASK. FUEL LEVEL ALERT 1, TANK 3 AND TANK 3 FUEL QTY LOW. NR 2 ENGINE START VALVE OPEN LIGHT ILLUMINTED. EMERGENCY DECLARED.

Part: CONTROL UNIT — INOPERATIVE (NR 2) · airframe 66,658 hrs · 13,836 cycles

FUMES IN FLIGHT PRESENT OXYGEN MASKS WERE USED AT 100 PERCENT EMERGENCY WAS DECLARED AT CRUISE, FL380. DIVERT TO LIGHT PERFORMED GVI OF AVIONICS BAY EQUIPMENT RACKS & WIRING. ACFT FOUND NORMAL T/S ITEM 3 ON L/P 824502 FOUND ACU-2 FAILED SUSPECT ACU-2 CAUSE OF FUMES R & R ACU IAW 33-15-01-000 AND 400 TEST NORMAL.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,658 hrs · 13,836 cycles

EMERGENCY LIGHTING TEST FUNCTION INOPERATIVE. FOUND SWITCH 51-402 INOPERATIVE. REPLACED THE SWITCH IAW SWPM 20-20-03. SYSTEM TESTED IAW MM 33-51-01.

Part: ACTUATOR — INOPERATIVE (R1 DOOR)

R1 DOOR WILL NOT CLOSE. REPLACED PAX DOOR ACTUATOR IAW AMM 52-11-01-000-801. OPS CHECKED OK.

Part: CABLE — SHEARED (L1 DOOR)

L1 DOOR AFT CABLE SHEARED. R & R L1 DOOR AFT DRIVE CABLE, IAW AMM 52-11-03 AND ELECTRIC MOTOR IAW AMM 52-11-01. OPS CHECKED IAW AMM 52-10-01.

Part: WARNING MESSAGE — FALSE ACTIVATION (EMERGENCY LIGHTS)

EMERGENCY LIGHT BAY 1 LOW MESSAGE SHOWN DURING EMERGENCY LIGHT TEST. ACCOMPLISHED AMM 33-51-02-00, FIG 104 AND OPS TEST OF EMERGENCY LIGHTING BATTERY POWER SUPPLY IAW AMM 33-51-01-700-805. NO FAULTS FOUND, TEST PASS SHOWS OK FOR SERVICE.

Part: STRINGER — CRACKED · airframe 65,491 hrs · 13,525 cycles

INSPECTION 1C, STRINGER 51 CRACKED. REPAIRED STRINGER IAW EA 011-5710-01-A5492, REV.IR AND EO 5710-55061-A. MAJOR REPAIR.

Part: ANGLE — BROKEN (BS 1298) · airframe 65,491 hrs · 13,525 cycles

INSPECTION 1C, LOWER AUX TANK FRAME TIE ANGLE BROKEN LT SIDE BS 1298, R & R ANGLE IAW SRM 51-31-01 AND 51-33-01

Part: ANGLE — BROKEN (BS 1298) · airframe 65,491 hrs · 13,525 cycles

INSPECTION 1C, LOWER AUX TANK BAY FRAME TIE ANGLE BROKEN ON RT SIDE BS 1298. R & R ANGLE IAW SRM 51-31-01 AND 51-33-01.

Part: STRINGER — CRACKED · airframe 65,491 hrs · 13,525 cycles

INSPECTION 1C, STRINGER 48 FOUND CRACKED. INSTALLED TIME LIMITED REPAIR IAW EO 5710-55064-A AND EA 011-5710-01-A5488.

Part: STRINGER — CRACKED · airframe 65,491 hrs · 13,525 cycles

INSPECTION 1C, CRACK FOUND ON STRINGER 49. INSTALLED TIME LIMITED REPAIR IAW EO 5710-55066-A AND EA 011-5710-01-A5489.

Part: STRINGER — CRACKED · airframe 65,491 hrs · 15,299 cycles

INSPECTION 1C, STRINGER 47 FOUND CRACKED. REPAIRED IAW EA 011-5710-01-A5490 REV I/R, EO 5710-55065-A.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,491 hrs · 13,525 cycles

INSPECTION 1C, CRACK FOUND ON LOWER STRINGER 50. INSTALLED TIME LIMITED REPAIR IAW WITH EO 5710-55063-A AND EA 011-5710-01-A5487.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,491 hrs · 13,525 cycles

INSPECTION 1C, STRINGER 51 CRACKED AT XCW46.5. REPAIRED STRINGER IAW EA 011-5710-01-A5492 REV IR AND EO 5710-55061-A. MAJOR REPAIR.

Part: DOUBLER — CRACKED (LT WING) · airframe 65,491 hrs · 13,525 cycles

INSPECTION TYPE:1C, CRACKS MIGRATING FROM 3 EA RIVETS ON BEADED DOUBLER AT LT WING FIXED L/E XOS=701. ACCOMPLISHED TIME LIMITED REPAIR TO LT WING FIXED L/E BEADED DOUBLER XOS=673.7- XOS=703.5 IAW EO 5730-55062-A AND EA 011-5730-01-A5485.

Part: DOUBLER — CRACKED (LT WING) · airframe 65,491 hrs · 13,525 cycles

INSPECTION 1C, CRACKS ON BEADED DOUBLER AT LT WING FIXED L/E XOS=676. ACCOMPLISHED TIME LIMITED REPAIR TO LT WING FIXED L/E BEADED DOUBLER XOS=673.7-XOS 703.5 IAW EO 5730-55062-A AND EA 011-5730-01-A5485. MAJOR REPAIR.

Part: DOUBLER — GOUGED (BS 1002 L40-41R) · airframe 65,491 hrs · 13,525 cycles

INSPECTION 1C, FORWARD CARGO DOOR FRAME AFT LOWER EDGE REPAIR DOUBLER GOUGED BS 1002 BETWEEN L40-41R. REPAIRED IAW EA 011-5330-01-A5493, REV I/R AND EO-5330-54968-A (MINOR)

Part: CONTROL UNIT — INOPERATIVE (ANNUNCIATOR)

EMERGENCY POWER TEST FAILED, LT DOES NOT ILLUMINATE FOR 30 SECONDS. R & R NR 3 ANNUNCIATOR CONTROL UNIT IAW AMM 33-15-01-201. OPS CHECKED SYSTEM NORMAL.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS)

EMERGENCY LIGHT BATTERY LOW. R & R BATTERY IAW AMM 33-50-00-01. TEST PASSED IAW AMM 33-5 0-00-501.

Part: WEDGE — DENTED (LT WING TE FLAP) · airframe 63,168 hrs · 12,907 cycles

INSPECTION TYPE:2C, LT INBD FLAP SKIN DENTED (AT XIFH216). REPAIRED LT INBD FLAP, INBD WEDGE SKIN AT STA XIFH216 IAW STASA EA 011-5700 -01-A4636, REV IR AND EO MD11-5750-50859-A. (MAJOR)

Part: DOOR FRAME — CORRODED (BS 1954 L33-44L) · airframe 63,168 hrs · 12,907 cycles

INSPECTION TYPE:2C, AFT/BULK CARGO DOOR FRAME CORRODED, BS 1954, L33L - L44L. R & R AFT CARGO DOOR FRAME IAW SRM 51-31- 01, 51-33-01, 51-35-01. (MINOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 63,168 hrs · 12,907 cycles

INSPECTION TYPE:2C, RT WING L/E INNER BEADED DOUBLER CRACKED INBD OF NR 11 SLAT TRACK REPAIRED RT WING L/E INNER BEADED DOUBLER BETWEEN STA XOS 698-703 IAW EO MD11-5730-48222-A.

Part: SKIN — DENTED (FUSELAGE) · airframe 63,168 hrs · 12,907 cycles

INSPECTION TYPE:2C, 12 DENTS ON FUSELAGE EXTERIOR SKIN AFT OF BULK CARGO DOOR, BS 1958- 2007, L36L -L42L. REPAIRED FUSELAGE SKIN AT NOTED LOCATION IAW STASA EA 011-5330-01- A4630, REV IR AND EO MD11-5330-50829-A. FAA 8100-9 DATED 20 MAY 2013 (MINOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 63,168 hrs · 12,907 cycles

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

Part: LONGERON — CORRODED (BS 1541 L48L) · airframe 63,168 hrs · 12,907 cycles

INSPECTION TYPE:2C, LONGERON 48L CORRODED AT BS 1541. REMOVED FABRICATED AND INSTALLED REPLACEMENT SECTION OF LONGERON IAW DWG AFA7775, SRM 53-00-00, 53-00-05, 51-33-01.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS)

INSPECTION TYPE: ASE, EMERGENCY LT BAT 1 LO, LEVEL 1 ALERT DURING EMERGENCY LIGHT TEST. PERFORMED T/S IAW FIM 33-51-02-00. FOLLOW ITEMS 1, 2, 6, 7. FOUND EMER LIGHTING BATTERY POWER SUPPLY INOPERATIVE. BATTERY POWER SUPPLY R & R IAW AMM33-51-01-401 & TESTED AND FOUND STATISFACORY.

Part: ACCESS PANEL — DAMAGED (NR 2 NACELLE)

NR 2 ENGINE INLET ACCESS PANEL DAMAGED. REPAIRED IAW EO MD11-5530-48904-A.

Part: COMPUTER — INOPERATIVE (NR 1 FCC)

COULD NOT ENGAGE AP1, COULD NOT SWITCH TO NAV 1, CHECKED AND FOUND FCC 1 FAULT, R & R FCC1 THEN CHECKED NO CURRENT FAULT BUT WHILE PERFORM FCC1 CAT3B TEST FOUND PROBABLE CAUSE EL L/O VALVE-LIB SO R & R LIB ELEV ACTUATOR, REMOVED PN 205300-5005, SN AT408.

Part: LONGERON — CORRODED (BS 1129-1156) · airframe 60,840 hrs · 12,287 cycles

INSPECTION TYPE: 3C, LONGERON 46L CORRODED BEYOND ALLOWABLE LIMITS BS 1129-1156. REMOVED FABRICATED AND INSTALLED REPLACEMENT LONGERON 46L SECTION IAW DWG N6A6713, SRM 51-33-01, 51-35-01.

Part: SKIN — CORRODED (XORS428 AT S6) · airframe 60,840 hrs · 12,287 cycles

INSPECTION TYPE:3C, RT WING UPPER SKIN SURFACE HAS CORROSION AT APPROX STA XORS 428 ALONG S6. REPAIRED RT WING CORROSION ON UPPER SURFACE AT STA XORS 428 IAW EO 5730-46212-A AND STA SA EA 011-5730-01-A3707 REV IR.

Part: VANE — DELAMINATED (RT WING TE FLAP) · airframe 60,840 hrs · 12,287 cycles

INSPECTION TYPE:3C, DELAMINATION ON RT INBD FLAP VANE LOWER SURFACE AT XIFH252. REPAIRED RT INBD FLAP VANE LOWER SKIN DELAMINATION IAW SRM 57-50-80, REPAIR 2 WET LAY-UP BONDED REPAIR.

Part: DOUBLER — CRACKED (LWS 621-625) · airframe 60,840 hrs · 12,287 cycles

INSPECTION TYPE: 3C, LEFT WING FIXED L/E BEADED DOUBLER HAS MULTIPLE CRACKS ON OTBD SIDE OF INBD REFUEL PORT. REPAIRED DOUBLER BETWEEN XOS621-625 IAW EO MD11-5730-42916-C AND SRM 57-40-02, REPAIR 9 FIG 203.

Part: DOUBLER — CRACKED (LWS 610-616) · airframe 60,840 hrs · 12,287 cycles

INSPECTION TYPE: 3C, LEFT WING FIXED L/E BEADED DOUBLER CRACKED ABOVE INBD END OF INBD REFUEL PORT. REPAIRED DOUBLER BETWEEN XOS 610-616 IAW EO MD11-5730-42916-C AND SRM 57-40-02, REPAIR 9, FIG 203.

Part: DOUBLER — CRACKED (LWS 636-643) · airframe 60,840 hrs · 12,287 cycles

INSPECTION TYPE: 3C, LEFT WING FIXED L/E BEADED DOUBLER HAS MULTIPLE CRACKS ABOVE OTBD REFUEL PORT. REPAIRED DOUBLER BETWEEN XOS 636-643 IAW EO MD11-5730-42916-C AND SRM 57-40-02, REPAIR 9, FIG 203.

Part: DOUBLER — CRACKED (RWS 679-685) · airframe 60,840 hrs · 12,287 cycles

INSPECTION TYPE: 3C, RIGHT WING L/E BEADED DOUBLER CRACKED BETWEEN SLAT TRACKS 10 & 11. REPAIRED DOUBLER BETWEEN XOS 679-685 IAW EO MD11-5730-42916-C AND SRM 57-40-02, REPAIR 9, FIG 203.

Part: DOUBLER — CRACKED (LWS 536-547) · airframe 60,840 hrs · 12,287 cycles

INSPECTION TYPE: 3C, LEFT WING FIXED L/E BEADED DOUBLER CRACKED INBD OF SUPPORT RIB AT NR 8 SLAT TRACK. REPAIRED DOUBLER BETWEEN XOS 536-547 IAW EO MD11-5730-42916-C AND SRM 57-40-02, REPAIR 9, FIG 203.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHT)

EMERGENCY LIGHT TEST FAILED, BATTERY 1 LOW FAULT. REPLACED EMERERGENCY LIGHT BATTERY PACK REF MM 33-51-01-4. OPS CHECKED GOOD, NO FAULTS NOTED. LIGHT TEST PASS.

Part: LIGHT — MALFUNCTIONED (COCKPIT)

PERFORMED OPS CHECK OF EMERGENCY LIGHT SYS IAW AMM 33-50-00-5, REV 70. OPS CHECK SATISFACTORY, NO FAULTS NOTED. THIS CLOSES DMI.

Part: LONGERON SPLICE — CRACKED (BS 1631 L13R) · airframe 53,381 hrs · 11,717 cycles

INSPECTION TYPE:4C, LONGERON SPLICE FITTING CRACKED AT STA 1631, L13R. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SPLICE FITTING REF SRM 51-33-010, STA SA EA 011-5340-01-A2889, REV IR & EO MD11-5310-41619-A.

Part: LONGERON SPLICE — CRACKED (BS 1631 L14L) · airframe 53,381 hrs · 11,717 cycles

INSPECTION TYPE:4C, LONGERON SPLICE FITTING CRACKED AT STA 1631, L14L. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SPLICE FITTING REF SRM 51-33-01, STA SA EA 011-5340-01-A2889, REV IR & EO MD11-5310- 416198-A.

Part: LONGERON SPLICE — CRACKED (BS 1631 L12R) · airframe 53,381 hrs · 11,717 cycles

INSPECTION TYPE:4C, LONGERON SPLICE FITTING CRACKED AT STA 1631, L12R. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SPLICE FITTING REF SRM 51-33-01, STA SA EA 011-5340-01-A2889, REV IR AND EO MD11- 5310-41619-A.

Part: LONGERON SPLICE — CRACKED (BS 1631 L14R) · airframe 53,381 hrs · 11,717 cycles

INSPECTION TYPE:4C, LONGERON SPLICE FITTING CRACKED AT STA 1631 L14R. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SPLICE FITTING REF SRM 51-33-01, STA SA EA 011-5340-01-A2889, REV IR & EO MD11-5310-41619-A.

Part: LONGERON SPLICE — CRACKED (BS 1631 L12L) · airframe 53,381 hrs · 11,717 cycles

INSPECTION TYPE:4C, LONGERON SPLICE FITTING CRACKED AT STA 1361, L12L. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SPLICE FITTING REF SRM 51-33-01, STA SA EA 011-5340-01-A2889, REV IR & EO MD11-5310- 41619-A.

Part: LONGERON SPLICE — CRACKED (L15L) · airframe 53,381 hrs · 11,717 cycles

INSPECTION TYPE:4C, LONGERON SPLICE FITTING CRACKED IN MAIN CABIN AT STA 5-0, L15L. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SPLICE FITTING REF SRM 51-33-01 AND DWG AE A7654.

Part: INTERCOSTAL — CORRODED (STA.1521 L14L) · airframe 53,381 hrs · 11,717 cycles

INSP TYPE:4C, MAIN CARGO COMPT AT STA 1521, L24L INTERCOSTAL CORRODED JUST BELOW WINDOW PLUG. REMOVED FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL REF DWG AEA- 0146 AND SRM 51-33-01.

Part: STRINGER — CRACKED (LWS 562) · airframe 53,381 hrs · 11,717 cycles

INSPECTION TYPE:4C, POSSIBLE CRACK IN OTBD END OF STRINGER 43 BETWEEN LAST FASTENER HOLE AND E.O.P. IN LT WING NEAR STA XORS572. NDT VERIFIED CRACK. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SPLICE FITTING AT OTBD END OF LT WING STRINGER 43, BETWEEN XORS562-39 & XORS592.6 REF IAW SRM 51-33-01, 57-00-03, DAC DWG. ARB7401, STA SA EA 011-5710-01-A2890 REV A & EO MD11-5710-41629-B.

Part: SKIN — CRACKED (RT WING L/E) · airframe 53,381 hrs · 11,717 cycles

INSPECTION TYPE:4C, RT TELESCOPIC DUCT CUTOUT XOS 464-470 HAS CRACK ON OTBD UPPER CORNER. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-01, REPAIR 10, FIG 201.

Part: SKIN — CRACKED (LT WING L/E) · airframe 53,381 hrs · 11,717 cycles

INSPECTION TYPE:4C, LT WING ANTI-ICE TELESCOPIC DUCT UPPER DOOR CUTOUT CRACK AT OTBD CORNER. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-01, REPAIR 10, FIG 201.

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 53,381 hrs · 11,717 cycles

INSPECTION TYPE:4C, RT WING L/E INNER SKIN CRACKED AT 3 EA RIVETS, ABOUT THE SLAT CABLE PULLEY JUST INBD OF THE NR4 SLAT OTBD TRACK, APPROX STA XOS 645. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.

Part: DOUBLER — CRACKED (LT WING L/E) · airframe 53,381 hrs · 11,717 cycles

INSPECTION TYPE:4C, CRACK ON LT WING FIXED L/E COMPT BEADED DOUBLER AT APPROX STA XOS 692. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.

Part: SKIN — CRACKED (LT WING SLATS) · airframe 53,381 hrs · 11,717 cycles

INSPECTION TYPE:4C, LT WING NR 2 SLAT INNER SURFACE HAS A CRACK/PUNCTURE THROUGH SKIN AT OTBD AREA. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-01, REPAIR 3, FIG 203.

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 53,381 hrs · 11,717 cycles

INSPECTION TYPE:4C, RT WING L/E INNER SKIN CRACKED AT 2 EA RIVETS, ABOVE THE INBD REFUEL/DEFUEL RECEPTACLE, APPROX STA XOS 610. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 53,381 hrs · 11,717 cycles

INSPECTION TYPE:4C, RT WING L/E INNER SKIN CRACKED AT 2 EA RIVETS ABOUT THE OUTBD REFUEL/DEFUEL RECEPTACLE, APPROX STA XOS 635. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.

Part: DOUBLER — CRACKED (LT WING L/E) · airframe 53,381 hrs · 11,717 cycles

INSPECTION TYPE:4C, BEADED DOUBLER CRACK ON LT WING FIXED L/E COMPT AT APPROX STA XOS 647. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.

Part: DOUBLER — CRACKED (LT WING L/E) · airframe 53,381 hrs · 11,717 cycles

INSPECTION TYPE:4C, CRACK ON LT WING FIXED L/E BEADED DOUBLER AT STA XOS 673. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.

Part: DOUBLER — CRACKED (LT WING L/E) · airframe 53,381 hrs · 11,717 cycles

INSPECTION TYPE:4C, LT WING FIXED L/E BEADED DOUBLER CRACK RT ALONG SUPPORT STRAP AT STA XOS 669. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.

Part: DOUBLER — CRACKED (LT WING L/E) · airframe 53,381 hrs · 11,717 cycles

INSPECTION TYPE:4C, CRACK ON LT WING FIXED L/E COMPT. BEADED DOUBLER AT APPROX STA XOS 708. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.

Part: DOUBLER — CRACKED (LT WING L/E) · airframe 53,381 hrs · 11,717 cycles

INSPECTION TYPE:4C, BEADED DOUBLER CRACK AT LT WING FIXED L/E COMPT AT APPROX STA XOS 587. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 53,381 hrs · 11,717 cycles

INSPECTION TYPE:4C, RT WING L/E INNER SKIN CRACKED AT 2 EA RIVETS, APPROX. STA XOS 567 JUST OTBD OF SLAT OTBD TRACK. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.

Part: WEB — CRACKED (COCKPIT)

FLOOR BENEATH PSI OBSVR SEAT CRACKED. REMOVED RIVETS IN FLOOR WEB. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR AND HAS BEEN TRANSFERRED TO NRC 337600. NRC 337600 COMPLETED, REPAIR IS COMPLETED AND PERMANENT. NO FURTHER ACTION NEEDED.

Part: MEMBRANE — DAMAGED (COCKPIT)

COCKPIT FLOOR MEMBRANE WEB LIGHTNING HOLE DAMAGED AT FS360, RBL6. (BELOW RT OBSERVER'S SEAT) REMOVED DAMAGE AND REPAIRED IAW MD11-5310-41133-A ON NRC 337600.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS)

DURING EMERGENCY LIGHT TEST GOT EMERGENCY LIGHT BATTERY 1 LOW MESSAGE. R & R RECHARGEABLE BATTERY EMERGENCY LIGHTS POWER SUPPLY REF AMM 33-51-01-4. OPS CHECKS GOOD.

Part: LIGHT — FAILED (COCKPIT)

EMERGENCY LIGHTS FAIL TEST. EMER LTS BAT 1 LOW ALERT. PERFORMED POWER DOWN OF A/C AND BATT/BATT RELAY/EMER PWR LTS CB'S WERE CYCLED. RE-POWER A/C AND C/OUT EMER POWER LIGHTS TEST SEVERAL TIMES IAW MM 24-32-00-741-001. FOUND ALL GOOD AND NO FURTHER FAULTS/ALERTS NOTED. ACFT OK FOR CONT SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

EMERGENCY LIGHT TEST FAILS EMERGENCY LIGHT BATTERY 1 LO MESSAGE. D 426879 ASSIGNED IAW MEL 33-50-02. T/S IAW FRIM TREE 33-51-02-00 BLKS 1-3, OPS CHECK GOOD. THIS CLEARS M 426879.

Part: STRUCTURE — DAMAGED (WING) · airframe 55,549 hrs · 11,007 cycles

INSPECTION TYPE:1/C REPAIR SURVEY SEQ 283-W3-17 NEEDS VALIDATION FOR REPAIR. REPAIR CORRELATES TO MD11 SRM 57-40-01, REPAIR 6, PAGE 201-203 FIG 201, REV 41.

Part: STRUCTURE — DAMAGED (WING) · airframe 55,549 hrs · 11,007 cycles

INSPECTION TYPE:1/C REPAIR SURVEY SEQ 283-W4-07 NEEDS VALIDATION FOR REPAIR. REPAIR CORRELATES TO MD11 SRM 57-40-01, REPAIR 6 PAGE 201-203, FIG 20 1 REV 41.

Part: SKIN — DENTED (WING) · airframe 55,549 hrs · 11,007 cycles

INSPECTION TYPE:1/C REPAIR SURVEY SEQ. 283-W4-01, REPAIR DOUBLER IS DENTED REPAIRED AS PER UPS EO MD11-5730-35269-B, AND SAA EA 011-5730-01-A20 62, ISSUE B, REF RCD# 358207

Part: SKIN — MISREPAIRED (LT WING) · airframe 55,549 hrs · 11,007 cycles

INSPECTION TYPE:1/C REPAIR SURVEY SEQ. 283-W3-05 AT LT WING FIXED L/E EXISTING REPAIR AP PROX. BETWEEN XOS STA. 610 AND 621 DOES NOT CORRELATE TO SRM 57-1 0-00, FIG. 14, AND PAGE 40, VOL. 1, REV. 38 REPAIRED AS PER UPS EO MD11-5730-35339-A AND SAA EA 011-5730-01-A205 9, ISSUE A, REF. RCD329622

Part: SKIN — MISREPAIRED (LE SLAT) · airframe 55,549 hrs · 11,007 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQ 283-W3-02 LT NR 3 SLAT L/E BETWEEN STA W344-XDS408 EXISTING REPAIR NOT CORRELATED TO SRM 57-40-01 FIG 201 REPAIR 11. FASTENERS C/O BLINDS INSTALLED SOLIDS. REMOVED SKIN INSERT FOR INSPECTION REF MD11 SRM 51-35-01. FOUND REPAIR TO CORRELATE WITH MD11 SRM 57-40-01 FIG 201 REPAIR 11. INSTALLED SKIN INSERT REF MD11 57-40-01 FIG 201 REPAIR 11 AND SRM 51-35-01 PARA 8/ NOTE 8.

Part: SKIN — MISREPAIRED (BS 1959-1964) · airframe 55,549 hrs · 11,007 cycles

INSPECTION TYPE:1/C REPAIR SURVEY SEQ NR 283-F1-06 BETWEEN BS 1959-1964 L41L AND 45L, DO NOT CORRELATE WITH EFN NR 28320061034 AND SRM 53-50-00, VOL 1, FIG 16, REV 38. REPAIRED AS PER IPXA EO NR MD11-5330-35291-A AND SAA EA NR 011-5330-01-A2057, ISSUE A, REF RCD NR 358139.

Part: WEDGE — MISREPAIRED (LT AILERON) · airframe 55,549 hrs · 11,007 cycles

INSPECTION TYPE:1/C REPAIR SURVEY SEQ NR 283-W3-09 LT WING INBD AILERON OTBD T/E WEDGE PREVIOUS REPAIR NOT CORRELATED TO SRM. REPAIRED AS PER IPXA EO NR MD11-5750-35153-B AND SAA EA NR 011-5751-01-A205 1, ISSUE B REF RCD 358165.

Part: SKIN — DAMAGED (BS 1721-1741) · airframe 55,549 hrs · 11,007 cycles

INSPECTION TYPE:1/C REPAIR SURVEY SEQ. 283-F1-04 REQUIRES SRI DWG. 922881 TO VALIDATE REP AIR AT BS 1721 AND BS 1741, L51R AND 52 REPAIRED AS PER UPS EO MD11-5330-35335-A AND SAA EA# 011-5330-01-A206 1, ISSUE A, REF. RCD# 358167

Part: SKIN — MISREPAIRED (RT WING) · airframe 55,549 hrs · 11,007 cycles

INSPECTION TYPE:1/C RT WING FIXED LEADING EDGE REPAIR SURVEY SEQ NR 283-W4-06 DOES NOT CORRELATE WITH SRM. REMOVED, FABBED AND INSTALLED REPAIR DOUBLER IAW IPXA EO NR MD11-5730-35 228-A AND SAA EA NR 011-5730-01-A2064 ISSUE "A", REF IPXA RCD NR 358007.

Part: SKIN — MISREPAIRED (BS 1002-1019) · airframe 55,549 hrs · 11,007 cycles

INSPECTION TYPE:1/C REPAIR SURVEY SEQ NR 283-F1-03 BETWEEN STA 1002-1019, LONG 31R-33R NOT CORRELATED TO EFN NR 28320061033 DUE TO WRONG THICKNESS. FABRICATED AND INSTALLED REPAIR IAW SRM 53-00-15, REPAIR 8, FIG 202, SHEET 1-4, NOTE 14.B REF UPS RCD NR 358011.

Part: DOUBLER — CRACKED (LT WING) · airframe 55,549 hrs · 11,007 cycles

INSPECTION TYPE:1/C LT WING FIXED L/E INSIDE FUEL PANEL APPROX STA X0S631, BEADED DOUBLER HAS NUMEROUS CRACKS. REPAIRED AS PER MD11 SRM 57-40-02, REPAIR 9, FIG 203, SHEETS 1-4 REF IPXA RCD NR 358082.

Part: RESERVOIR — NO TEST (R-1 DOOR) · airframe 55,549 hrs · 11,007 cycles

INSPECTION TYPE:C1 R-1 DOOR EMERGENCY CONTROL SYSTEM PNEUMATIC RESERVIOR FAILED OPS CHECK. REMOVED AND REPLACED R-1 DOOR EMERGENCY CONTROL SYSTEM PNEUMATIC RESERVIOR PER MD-11 AMM 52-11-04-4.

Part: SKIN — CRACKED (RT WING L/E) · airframe 55,549 hrs · 11,007 cycles

INSPECTION TYPE:C1 RT WING L/E BEADED SKIN CRACKED IN 3 AREAS, JUST OTBD OF NR 10 SLAT TRACK (BOTH SIDES OF RIB). REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER MD-11 SRM 57-40-02 FIG 203 REPAIR 9.

Part: SKIN — CRACKED (RT WING LE) · airframe 55,549 hrs · 11,007 cycles

INSPECTION TYPE:C1 RT WING L/E UPPER SKIN IS CRACKED, JUST OTBD OF NR 12 SLAT TRACK. REMOVED DAMAGE, FABRICATED AND INSTALLED 1 DOUBLER, 1 FILLER AND 2 REPAIR ANGLES PER MD-11 SRM 57-40-02 REPAIR 9 FIG 203.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 55,549 hrs · 11,007 cycles

INSPECTION TYPE:1/C LIGHTNING STRIKE RT WING OTBD FLAP UPPER SURFACE AT 2 FT OTBD OF INBD END OF FLAP T/E. REPAIRED AS PER IPXA EO NR MD11-5750-35158-A, AND SAA EA NR 011-5753-01-A205 0 ISSUE A REF RCD NR 329554.

Part: SKIN — GOUGED (BS 999-1010) · airframe 55,549 hrs · 11,007 cycles

INSPECTION TYPE:1/C REPAIR SURVEY SEQ NR 283-F1-02 STA 999-1010, L39R-42R, HAS OUTER DOUBLER GOUGED. FABBED AND INSTALLED REPAIR DOUBLER IAW IPXA EO NR MD11-5330-35226-A AND SAA EA 011-5330-01-A2058, ISSUE A, REF RCD NR 329568.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 55,549 hrs · 11,007 cycles

INSPECTION TYPE:1/C REPAIR SURVEY SEQ 283-F1-05 BETWEEN STA 1781 AND 1787 LONG 39R AND 42R HAS OUTER DOUBLER GOUGED. FABBED AND INSTALLED REPAIR IAW MD11 SRM 53-00-15, REPAIR B, FIG 202 PAGE 1-4, REV 41, REF UPS RCD 329567.

Part: SKIN — DAMAGED (FUSELAGE)

INSPECTION TYPE:N/A SKIN DAMAGED 6 INCHES AFT OF STA 840.250 L35R. REPAIRED PER EO MD11-5330-34520-B.

Part: SKIN — DAMAGED (FUSELAGE)

INSPECTION TYPE:N/A LEFT STA 348 SKIN DAMAGED. REPAIRED PER EO MD11-5330-34614-A.

Part: WEDGE — DAMAGED (AILERON)

INSPECTION TYPE:N/A LT WING AILERON I/B TRAILING EDGE WEDGE DAMAGED AT O/B SECTION. REPAIRED AILERON AS PER EO MD11-2710-32103-B.

Part: WEDGE — CRACKED (TE FLAP)

INSPECTION TYPE:N/A LEFT I/B TRAILING EDGE FLAP WEDGE CRACKED 9.5 INCHES. REPAIRED PER EO MD11-5750-31369-B.

Part: SKIN — DENTED (NR 6 SLAT) · airframe 53,491 hrs · 10,475 cycles

INSPECTION TYPE:C LT WING NR 6 SLAT EXTERIOR SURFACE FOUND QTY 04EA DENTED AREA AT 20 TO 27 INCHES FROM B/B END AND 26 INCHES FROM T/E. DENTED AREAS MEASURED DEPTH: 0.039 INCH AND FOUND EXCEED LIMIT AS PER SRM 57-10-00 FIG 16 VOL I REV 40. DENTED AREA TRIMMED OFF PER EN1340-08 & HFEC INSP NO CRACK EVIDENT. REPAIR PARTS FABRICATED AND INSTALLED AS PER EN1340-08 AND SRM 51-31-01 VOL II REV 40.

Part: SKIN — DENTED (LT WING SLAT) · airframe 53,491 hrs · 10,475 cycles

INSPECTION TYPE:C LT WING NR 6 SLAT EXTERIOR SURFACE FOUND DENTED AT 40.5 INCHES FROM I/B END AND 30.5 FROM T/E. LT WING NR 6 SLAT EXTERIOR SURFACE DENTED AREA MEASURED DEPTH 0.037 INCH AND FOUND EXCEED LIMIT AS PER SRM 57-10-00 FIG 16 VOL I REV 40. DENT AREA TRIM-OFF, HFEC INSP & NO CRACK EVIDENT. REPAIR PARTS FABRICATED AND INSTALLED AS PER SRM 57-10-00 FIG 5 VOL I REV 40.

Part: STRAP — CRACKED (RT WING SLAT) · airframe 53,491 hrs · 10,475 cycles

INSPECTION TYPE:C RT WING L/E LOWER ACCESS AT 13 INCHES O/B OF SLAT NR 12 FOUND STRAP SUSPECT CRACK. HFEC CARRIED OUT IAW DAC NDT SPM REV 13 PART 06-10-01.001 AND CRACK CO CONFIRM APPROX 4.75 INCHES LONG. DAMAGE STRAP AND ATTACH FORMER REMOVED, STRAP FABRICATED AND INSTALLED AS PER SRM 51-31-01 VOL II REV 40.

Part: LONGERON — CORRODED (FUSELAGE)

INSPECTION TYPE:N/A CTR CARGO STA 1641 BILGE AREA LONGERON 48 RT FOUND CORROSION. CTR CARGO STA 1641 L48 RT LONGERON CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01. MATERIAL REMOVED 0.012" ORIGINAL THK 0.100" REMAINED THK 0.088" FOUND WITHIN LIMIT PER SRM 53-00-01.

Part: FRAME — CORRODED (FUSELAGE)

INSPECTION TYPE:N/A CTR CARGO FRAME AT STA 1841 BILGE AREA BETWEEN L50 - L52 RT FOUND CORROSION. FRAME CHANNEL CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 MATERIAL REMOVED 0.008" ORIGINAL THK 0.071" REMAINED THK 0.063" FOUND WITHIN LIMIT PER SRM 53-30-00.

Part: FITTING — CORRODED (CARGO BAY)

INSPECTION TYPE:N/A CTR CARGO FRAME SHEAR CLIP AT STATION 1681 BILGE AREA L52 FOUND CORROSION. FRAME SHEAR CLIP CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL II REV 40. MATERIAL REMOVED 0.008" ORIGINAL THK 0.071" REMAINED 0.068" FOUND WITHIN LIMITS PER SRM 53-00-01 FIG 2 VOL I REV 40.

Part: FRAME — CORRODED (FUSELAGE)

INSPECTION TYPE:N/A CTR CARGO FRAME AT STA 1741 BILGE AREA BETWEEN L51 - L52 LT FOUND CORROSION. FRAME SHEAR CLIP CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21- 01. MATERIAL REMOVED 0.009" ORIGINAL THK 0.071" REMAINED THK 0.062" FOUND WITHIN LIMIT PER SRM 53-00-01.

Part: FRAME — CORRODED (FUSELAGE)

INSPECTION TYPE:N/A CTR CARGO FRAME AT STA 1801 BILGE ARE L52 FOUND CORROSION. FRAME CHANNEL CORROSION REMOVED AND REPROTECTED PER SRM 51-21-01. MATERIAL REMOVED 0.006" ORIGINAL THK 0.071" REMAINED THK 0.065" FOUND WITHIN LIMIT PER SRM 53-30-00.

Part: FRAME — CORRODED (FUSELAGE)

INSPECTION TYPE:N/A CTR CARGO FRAME AT STA 1661 BILGE AREA BETWEEN L51 LT & RT FOUND CORROSION. FRAME SHEAR CLIP CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21- 01. MATERIAL REMOVED 0.005" ORIGINAL THK 0.071" REMAINED 0.066" FOUND WITHIN LIMIT PER SRM 53-00-01 FIG 2.

Part: LONGERON — CORRODED (BS 1561-1601) · airframe 53,491 hrs · 10,475 cycles

INSPECTION TYPE:C CTR CARGO STA 1561 TO 1601 BILGE AREA LONGERON 48 RT FOUND CORRODED. LONGERON CORR CLEANED, FOUND EXCEED LIMIT AT STA 1571-1591 L48R AS PER SRM 53-00-01 FIG 4 VOL I REV 40. THICKNESS REMAINED 0.034 INCH, ORIG THICKNESS 0.100", MATERIAL REMOVED 0.066". CORR LONG I BEAM SPLICE CUT AT STA 1571 & 1591 L48R & HFEC INSP NO CRACK EVIDENT. REPAIR PART FAB & INSTALLED PER SRM 53-10-00 FIG 2 VOL I REV 40.

Part: WEDGE — DELAMINATED (T/E FLAP)

INSPECTION TYPE:C LT WING O/B FLAP T/E DELAMINATION. REPAIRED LT WING O/B FLAP T/E WEDGE PANEL DELAMINATED AREA AS PER EN1339-08 AND UPS EO MD11-5750-30265A.

Part: SKIN PANEL — CORRODED (FUSELAGE)

INSPECTION TYPE:N/A CTR CARGO SKIN PANEL AT STA 1551 BILGE AREA L52 FOUND CORROSION. SKIN PANEL CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL II REV 40. MATERIAL REMOVED 0.004". ORIGINAL THK 0.068" REMAINED 0.064" FOUND WITHIN LIMITS PER SRM 53-00-01 FIG 2 VOL 1 REV 40.

Part: LONGERON — CORRODED (FUSELAGE)

INSPECTION TYPE:N/A CTR CARGO STA 1561 - 1601 BILGE AREA LONGERON 48 RT FOUND CORROSION. CTR CARGO STA 1561 - 1601 LONGERON RT REPAIRED AS PER SRM 53-10-00.

Part: FRAME — CORRODED (FUSELAGE)

INSPECTION TYPE:N/A CTR CARGO FRAME AT STA 1721 BILGE ARE L52 FOUND CORROSION. FRAME CHANNEL AND SHEAR CLIP CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01. MATERIAL REMOVED 0.007" ORIGINAL THK 0.071" REMAINED THK 0.064" FOUND WITHIN LIMITS PER SRM 53-30-00.

Part: RIB — CRACKED (LT WING) · airframe 53,491 hrs · 10,475 cycles

INSPECTION TYPE:C LT WING L/E CAVITY AT 15 INCHES I/B OF SLAT TRACK NR 9, RIB SUSPECT CRACK. HFEC CARRIED OUT IAW NDT SPM REV13 PART 06-10-01.001 AND CRACK CONFIRM APPROX 3.75 INCH LONG. DAMAGE RIB REMOVED, NEW RIB FABRICATED & REPLACED AS PER SRM 51-31-01 VOL II REV 40.

Part: DOOR FRAME — CRACKED (LT MLG) · airframe 53,491 hrs · 10,475 cycles

INSPECTION TYPE:C LT MLG DOOR AROUND CTR HINGE FOUND FRAME CRACKED. CRACKED FRAME REMOVED, REPAIR FRAME PART, FILLER & DOUBLER FABRICATED AND INSTALLED AS PER EN1338-08 AND SRM 51-31-011 VOL II REV 40.

Part: RIB — CRACKED (RT WING) · airframe 53,491 hrs · 10,475 cycles

INSPECTION TYPE:C RT WING LOWER WINGLET FWD RIB FOUND CRACKED AS MARKED. CRACKED RIB REMOVED PER SRM 51-31-01 V2 R40. NEW RIB FAB PER BOEING DRWG ARB7774 USING MATL 7075-0-0.040". RIB HEAT TREATED TO T6 PER DPS7.00-1 HARDNESS VALUE OBTAINED HRB80.1 PER DPS1.053. NEW RIB HOLES P/UP&NEW RIB PROTECTED PER SRM 51-21-01 V2 R40. NEW RIB INSTALLED PER SRM 51-31-01 V2 R40. PAINT TOUCH UP ON REPAIRED AREA PER SRM 51-21-02 V2 R40.

Part: RIB — CRACKED (LT WING) · airframe 53,491 hrs · 10,475 cycles

INSPECTION TYPE:C LT WING LOWER WINGLET FWD RIB FOUND CRACKED AS MARKED. CRACKED REMOVED PER SRM 51-31-01 V2 R40. NEW RIB FAB PER BOEING DRAWING ARB7774 USING MATL 7075-0-0.040". RIB HEAT TREATED TO T6 PER DPS7.001 HARDNESS HRB80.1 PER DPS1.053. NEW RIB HOLES P/UP&NEW RIB PROTECTED PER SRM51-21-01 V2 R40. NEW RIB INSTALLED PER SRM 51-31-01 V2 R40. PAINT TOUCH UP ON REPAIRED AREA PER SRM 51-21-02 V2 R40.

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT)

INSPECTION TYPE:N/A MULTIPLE CIRCUIT BREAKERS TRIPPED & WILL NOT RESET. WORK ACCOMPLISHED PER EO MD11-2400-29911-C. REPLACED DAMAGED WIRE BUNDLE AND RELATED COMPONENTS.

Part: WIRE — BURNED (E&E BAY) · airframe 51,825 hrs · 10,206 cycles

DURING TROUBLE SHOOTING OF C/B POPPING FOUND WIRE BUNDLES BURNED THROUGH, LOCATED IN E&E BAY RT SIDE. TRANSFERRED TO UPS NRC MD015501-REFER FOR DETAILS & SIGN OFF. SUMMARY INCLUDES 247 WIRES REPLACED END TO END, 3 WIRE SPLICE REPAIRED. ALL SYS AFFECTED OPS AND FUNCTIONAL CKD FOR UPS & BOEING ENG INSTRUCTIONS

Part: PUMP — FAILED (NR 2 ENGINE)

INSPECTION TYPE:N/A SYSTEM 2 HYD QTY LOSS IN FLIGHT, 50 MINUTES INTO FLIGHT HYD PUMP 2L OFF, 10 MINUTES LATER HYD 2R OFF. QTY 8.2 FOLLOWED BY HYD 2 OFF, 15 MINUTES LATER HYD 2 FIL QTY WAS 0.0. REMOVED AND REPLACED NR 2 ENG LT HYD PUMP PER 29-11-20-4. REQUIRES OPS CHECK. REMOVED AND REPLACED NR 2 ENG R/H HYD PUMP PER 29-11-20. PUMP REQUIRES LEAK AND OPS CHECK. LEAK AND OPS CHECKED PER MM 29-11-20-4-2.

Part: CONTROL SYSTEM — INOPERATIVE (AILERONS)

ATB - AILERON DEFLECT DISAGREE MESSAGE. TAKEOFF DEFLECTED AILERON SYSTEM INOP. ITEM TRANSFERRED TO DMI M336464 PER MEL 27-13-2-0-1. DMP 27-13-2 C/W. PLACARD INSTALLED. REMOVED AND REPLACED WIRES 24-18 BL & 24-18 RD PER AMM 20-30-09-2. CHECKS GOOD PER AMM 27-16-00-5 PLACARD REMOVED & DEFERRAL CLEARED.

Part: SHIELD — CHAFED (NR 1 ENGINE)

INTERMITTENT FIRE WARNING ON NR 1 ENGINE. THRUST LEVER WAS RETARDED TO IDLE, ALL "FIRE DET FAULT" AND FIRE ALERTS WENT AWAY. OPERATED REMAINDER OF FLIGHT WITH NR 1 AT IDLE. CHECKED A/B FIRE LOOP. ALL ELEMENTS, OK. CHECKED ALL BLEED DUCTS, SECURITY CHECK OK. MOTORIZED NR 1 ENGINE, NO DUCT LEAKS. REF FIM 26-11 -00-1 FIG 103. A/B FIRE DETECTOR LT CORE COWL THIRD CLAMP FROM TOP, BOTH WIRE CHAFED THRU SHIELDING. INSULATED/ISOLATED BOTH WIRES. PERFORMED CFDS FDCU MENU. A/B TEST OK, FIRE TEST OK NR 1 ENGINE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

FOUND EMERGENCY EXIT LIGHT INOP. TRANSFERRED TO DMI M335480 PER MEL 33-50-4. REPLACED EMERGENCY LIGHTS BATTERY IAW MM 33-51-01-4. TESTS GOOD M335480 CLEARED PLACARD REMOVED.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS)

INSPECTION TYPE: N/A EMERGENCY LT BAT 1 LOW MSG APPEARED DURING PREFLIGHT OPS.TRANSFERRED TO DMI M334273 IAW MEL 33-50-4. PLACARD INSTALLED. CARRY OUT TEST ON EMERGENCY LIGHT. PASS TEST WITH MESSAGE. NO FAULTS OBSERVED. THIS CLOSES DMI. PLACARD REMOVED.

Part: PIVOT ASSY — CORRODED (L/E SLAT) · airframe 47,013 hrs · 9,437 cycles

INSPECTION TYPE:SV OUTBOARD LEFT SLAT DRIVE MECHANISM PIVOT MOUNTING ASSEMBLY PIVOT FACE HAS PITTING. REWORKED LEFT WING OUTBOARD SLAT MECHANISM PIVOT SHAFT PER SAA EA 011-2783- 01-A0217.

Part: ANGLE — CRACKED (NR 2 SLAT) · airframe 46,984 hrs · 9,427 cycles

RT NR 2 SLAT O/B END RIB ATTACH ANGLE FOUND CRACKED AS MARKED. RHW NR 2 SLAT REMOVED. INNER SKIN OPENED FOR ACCESS. CRACKED ANGLE REMOVED NEW ATTACHMENT ANGLE FAB USING MAT'L 7075-0-0.050" PER DWG ARB1647. ANGLE HEAT TREATED. HOLES PICK-UP ON NEW ANGLE. NEW ANGLE REPROTECTED. NEW ANGLE PAINTED. NEW ANGLE INSTALLED ON RT NR 2 SLAT O/B END PER SRM 51-35-01 INNER SKIN REINSTALLED AND RHW NR 2SLAT INSTALLED AMM 27-80-20 REV 50.

Part: RIB — CRACKED (LT WING) · airframe 46,984 hrs · 9,427 cycles

LT WING L/E RIB FOUND CRACKED AT 24 INCHES O/B OF SLAT TRACK NR 11 AS MARKED. LHW L/E SLAT NR 5 EXTENDED CABLE DISCONNECTED. CRACKED RIB LHW L/E 24 INCHES O/B SLAT TRACK NR 11 REMOVED. LHW L/E RIB REMOVED. RIB FAB PER DWG ARB292 3,7075-0-0.040". RIB HEAT TREATED. PULLY BRACKET REMOVED. HOLES TRANSFERRED ON RIB. PRIMER APPLIED. RIB INSTALLED SRM 51-35-01. PULLY BRACKET INSTALLED LHW L/E SLAT CABLE NR 5 EXTEND RECONNECTED AMM20-20-05 REV 50.

Part: ANGLE — CRACKED (NR 2 SLAT) · airframe 46,984 hrs · 9,427 cycles

INSPECTION TYPE:C LT WING NR 2 SLAT O/B RIB ATTACHMENT ANGLE FOUND CRACKED 1 INCH LONG AS MARKED. LHW NR 2 SLAT REMOVED. INNER SKIN OPENED. CRACKED ANGLE NR 2 SLAT REMOVED. NEW ATTACHMENT ANGLE FAB, MAT'L 7075-0-0.050" AS PER DWG ARB1647 ANGLE HEAT TREATED. HOLES PICK UP ON NEW ANGLE AND REPROTECTED. NEW ANGLE PAINTED. NEW ANGLE INSTALLED ON LHW NR 2 SLAT O/B RIB PER SRM 51-35-01 VOL II. INNER SKIN REINSTALLED. LHW NR 2 SLAT INSTALLED IAW MD11 AMM27-80-20 REV 50.

Part: FLOORBEAM — CORRODED (BS 1841) · airframe 46,984 hrs · 9,427 cycles

AFT CARGO COMPT AT STA1841 X=-14 TO -28 FOUND LOWER FLOORBEAM UPPER CAP CORROSION AROUND THE FASTENER HOLES 2 PLCS AS MARKED. AFT CARGO COMPT STA1841 X=-14 TO -28 FLOORBEAM UPPER CAP CORROSION REMOVED AND FOUND OUT OF LIMIT SRM 51-21-01 VOLII. REMOVED FLOORBEAM UPPER CAP SRM51-31-01 VOLII. NEW FLOORBEAM UPPER CAP HOLES PICK-UP AND REWORKED SRM 51-31-01. NEW FLOORBEAM UPPER CAP PAINTED. NEW FLOORBEAM UPPER CAP INSTALLED STA 1841 X=-14 TO -28, SRM 51-33-01 AND 51-35-01 VOL II REV 38.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,984 hrs · 9,427 cycles

INSPECTION TYPE:C CABIN:RT SEAT TRACK X=-75.25 AT STA1305-1371, FOUND CORROSION ON BOTH TOP SURFACE AND BASE. RT SEAT TRACK X=-75.25 STA 1350 CORROSION REMOVED AND FOUND EXCEED LIMIT SRM 53-70-00 FIG3 VOL1 38, FASTENERS REMOVED, SEAT TRACK CUT AT STA 1265 AND STA 1391 SRM 53-70-00 FIG1 VOL 1 38, HFEC INSP CARRIED OUT AND NO CRACK EVIDENT, NEW SEAT TRACK HOLES PICK UP AND PROTECTED. SEAT TRACK SPLICE FAB AND PAINTED. NEW SEAT TRACK AND SPLICE INSTALLED SRM 53-70-00 FIG1 VOL1 REV 38.

Part: BUSHING — CORRODED (HORIZONTAL STAB) · airframe 46,984 hrs · 9,427 cycles

INSPECTION TYPE:C HORIZONTAL STABILIZER BARREL NUT HOLE NR 11L EXISTING REPAIR BUSHING FOUND CORRODED. CORRODED REPAIR SLEEVE BUSHING REMOVED. CORROSION AT BORE REMOVED, REMANING BLEND OUT AT BORE 0.050" DEEP, EXCEEDED LIMIT. VISUAL INSPECTION CARRIED OUT, NO CORROSION FOUND. BORE BOTTOM PERIPHERY RADIUSES, BLEND OUT AND SMOOTHENED. REPAIR SLEEVE BUSHING FAB AND PROTECTED. SEALANT AND PRIMER APPLIED. REPAIR CARRIED OUT AT BARREL NUT BORE NR 11L IS ACCEPTABLE EN1051-06.

Part: BUSHING — CORRODED (HORIZONTAL STAB) · airframe 46,984 hrs · 9,427 cycles

INSPECTION TYPE:C HORIZONTAL STABILIZER BARREL NUT HOLE NR 5L EXISTING REPAIR BUSHING FOUND CORRODED. CORRODED SLEEVE BUSHING REMOVED. CORROSION AT BORE REMOVED. SURFACE CLEANED, REMAINING BORE BLEND 0.020" EXCEEDED LIMIT. DVI CARRIED OUT NO CORROSION FOUND. BORE AND BOTTOM PERIPHERY RADUIS 0.12"R AND SMOOTHENED. FAB AND PROTECTED REPAIR SLEEVE. SEALANT APPLIED AND PRIMER PAINTED. REPAIR CARRIED OUT AT BARREL NUT BORE NR 5L IA ACCEPTABLE IAW EN1049-06.

Part: SKIN — DENTED (BS 1964 L41L) · airframe 46,984 hrs · 9,427 cycles

INSPECTION TYPE:C STA 1964 LONGERON 41L TO LONGERON 42L OF AFT CARGO DOOR AFT CUT-OUT FOUND WITH DENT MARKS. REMOVED FASTENER STA1964 LT LONG 41L TO 42L OF AFT CARGO AND TRIMMED OFF DENT MARK AREA, 2"X2(1/2)". HFEC CARRIED OUT AND FOUND NO CRACK. FABICATED 2 DOUBLERS AND 1 FILLER, MATL 2024T3-0.071" AND 2024T3-0.080" SRM 53-50-00 VOL I FIG 38 2EA REPAIR DOUBLER AND 1EA FILLER INSTALLED SRM 51-33-01 VOL II REV 38. PAINTED REWORKED AREA SRM 51-21-01 VOL II REV 38.

Part: SKIN — DAMAGED (BS 999) · airframe 46,984 hrs · 9,427 cycles

INSPECTION TYPE:C FUSELAGE: FWD LOWER CARGO DOOR AFT CUT-OUT AT STA 999 LONGERON 40R TO L ONGERON 42R ON EXTERIOR SKIN FOUND DAMAGED. FWD CGO DR AFT CUT-OUT STA999 LONG 40R TO LONG 42R EXISTING FASTENERS REMOVED SRM 51-21-01. TRIMMED-OFF EXTERIOR SKIN DAMAGED AREA SRM 53-50-00 TRIMMED AREA 2.5" X 7". HFEC CARRIED OUT AND NO CRACK EVIDENT. FAB 2 REPAIR DOUBLER, FILLER SRM 53-50-00, PICKED-UP HOLES AND REPROTECTED. INSTALLED 2 PCS NEW REPAIR DOUBLER AND 1EA FILLER SRM 51-33-01 VOL II REV 38.

Part: BUSHING — CORRODED (HORIZONTAL STAB) · airframe 46,984 hrs · 9,427 cycles

HORIZONTAL STABILIZER BARREL NUT HOLE NR 12R EXISTING REPAIR BUSHING CORRODED. CORRODED SLEEVE BUSHING REMOVED (1.067"DIA). CORROSION AT BORE REMOVED REMAINING BLEND OUT AT BOTTOM 0.035", SIDEWALL 0.130" DEEP EXCEEDED LIMIT. DVI CARRIED OUT NO CORROSION FOUND. BARREL NUT BORE AND BLEND SMOOTHENED AND PROTECTED. FAB AND PROTECTED REPAIR BUCKET BUSHING. SEALANT AND PAINTED PRIMER. REPAIR CARRIED OUT AT BORE NR 12R IS ACCEPTABLE IAW EN1053-06.

Part: BUSHING — CORRODED (HORIZONTAL STAB) · airframe 46,984 hrs · 9,427 cycles

HORIZONTAL STABILIZER BARREL NUT HOLE NR 6R EXISTING REPAIR BUSHING CORRODED. CORRODED BUCKET BUSHING REMOVED. CORROSION AT BORE REMOVED REMAINING BLENDOUT AT SIDEWALL 0.160"DEEP EXCEEDED LIMIT. DVI CARRIED OUT NO CORROSION FOUND. BARREL NUT BORE AND BLEND OUT SMOOTHENED AND PROTECTED. FAB AND PROTECTED REPAIR BUCKET BUSHING. SEALANT APPLIED AND PRIMER PAINTED. REPAIR CARRIED OUT AT BORE NR 6R IS ACCEPTABLE IAW EN1052-06.

Part: BUSHING — CORRODED (HORIZONTAL STAB) · airframe 46,984 hrs · 9,427 cycles

HORIZONTAL STABILIZER BARREL NUT HOLE 18R EXISTING REPAIR BUSHING CORRODED. CORRODED BUCKET BUSHING (1.089"DIA) REMOVED. CORROSION AT BORE REMOVED REMAINING SIDEWALL BLENDOUT 0.050" EXCEEDED. DVI CARRIED OUT AND NO CORROSION FOUND. BARREL NUT BORE AND BLEND OUT AREA SMOOTHENED. FAB AND PROTECTED REPAIR BUCKET BUSHING. SEALANT APPLIED AND PRIMER PAINTED. REPAIR CARRIED OUT AT BARREL NUT BORE NR 18R IS ACCOMPLISHED IAW 1059-06.

Part: BUSHING — CORRODED (HORIZONTAL STAB) · airframe 46,984 hrs · 9,427 cycles

HORIZONTAL STABILIZER BARREL NUT HOLE NR 2R EXISTING REPAIR BUSHING CORRODED. CORRODED BUCKET BUSHING REMOVED. CORROSION AT BORE REMOVED REMAINING BLEND OUT 0.080"DEEP EXCEEDED LIMIT. DVI CARRIED OUT NO CORROSION FOUND. BARREL NUT BORE AND BLEND OUT SMOOTHENED AND PROTECTED. FAB AND PROTECTED REPAIR BUCKET BUSHING. SEALANT APPLIED AND PAINTED PRIMER. REPAIR CARRIED OUT AT BORE NR 2R IS ACCEPTABLE IAW EN1054-06.

Part: BUSHING — CORRODED (HORIZONTAL STAB) · airframe 46,984 hrs · 9,427 cycles

INSPECTION TYPE:C HORIZONTAL STABILIZER BARREL NUT HOLE NR 8L EXISTING REPAIR BUSHING FOUND CORRODED. CORRODED REPAIR BUSHING REMOVED. CORROSION AT BORE REMOVED. BOTTOM SURFACE CLEANED, REMAINING BLEND OUT AT BORE 0.035"DEEP EXCEEDED LIMIT. DVI CARRIED OUT, NO CORROSION FOUND. BORE AND BOTTOM PERIPHERY RADIUSES 12R AND SMOOTHENED. FAB AND PROTECTED REPAIR SLEEVE BUSHING. SEALANT AND PRIMER APPLIED ED. REPAIR CARRIED OUT AT BORE NR 8L IS ACCEPTABLE IAW EN 1050-06.

Part: SKIN — DAMAGED (BS 999 L32R) · airframe 46,984 hrs · 9,427 cycles

FWD LOWER CARGO DOOR CUT-OUT AT STA 999 LONGERON 32R AT AFT T AREA FOUND DAMAGED ON EXTERIOR SKIN. FWD LOWER CARGO DOOR CUT-OUT STA 999 RT LONG 32R AFT AREA FASTENER REMOVED AND DAMAGED AREA TRIMMED OUT 1(1/2)"X2". HFEC INSP FOUND NO CRACK. FAB NEW TWO REPAIR DOUBLER AND FILLER, MATL 2024T3-0.080", 2024T3-0. 090" AND 2024T3-0.080". NEW REPAIR DOUBLER AND FILLER INSTALLED SRM 51-33-01 VOL II REV38. DOUBLER AND FILLER PAINTED SRM 51-21-01 VOL II REV 38.

Part: BUSHING — CORRODED (HORIZONTAL STAB) · airframe 46,984 hrs · 9,427 cycles

HORIZONTAL STABILIZER BARREL NUT HOLE NR 17L EXISTING REPAIR BUSHING CORRODED. CORRODED REPAIR BUSHING REMOVED. CORROSION AT BORE REMOVED REMAINING BLEND OUT AT SIDEWALL 0.050" DEEP, BOTTOM 0.015" DEEP EXCEEDED LIMIT. VISUAL INSP FOUND NO CORROSION. BORE SMOOTHENED. FAB AND PROTECTED REPAIR SLEEVE BUSHING. SEALANT APPLIED AND PRIMER TOUCH UP. REPAIR CARRIED OUT AT BARREL NUT BORE NR 17L IS ACCEPTABLE IAW EN1056-06.

Part: BUSHING — CORRODED (HORIZONTAL STAB) · airframe 46,984 hrs · 9,427 cycles

HORIZONTAL STABILIZER BARREL NUT HOLE NR 15R EXISTING REPAIR BUSHING CORRODED. CORRODED BUCKET BUSHING REMOVED. CORROSION AT BORE REMOVED REMAINING BLEND OUT AT SIDEWALL 0.040" DEEP EXCEEDED LIMIT. DVI CARRIED OUT NO CORROSION FOUND. BARREL NUT BORE AND BLEND OUT VOIDS SMOOTHENED AND PROTECTED. FAB AND PROTECTED REPAIR BUCKET BUSHING. SEALANT APPLIED AND PAINTED PRIMER. REPAIR CARRIED OUT AT BORE NR 15R IS ACCEPTABLE IAW EN1058-06.

Part: BUSHING — CORRODED (HORIZONTAL STAB) · airframe 46,984 hrs · 9,427 cycles

INSPECTION TYPE:C HORIZONTAL STABILIZER BARREL NUT HOLE NR 23L EXISTING REPAIR BUSHING CORRODED. CORRODED SLEEVE BUSHING (1.067"DIA) REMOVED. CORROSION AT BORE REMOVED, SIDEWALL REMAINING BLEND OUT 0.010" EXCEEDED LIMIT. VISUAL INSP FOUND NO CORROSION. BORE SMOOTHENED AND PROTECTED. REPAIR SLEEVE BUSHING FAB AND PROTECTED. SEALANT APPLIED AND PRIMER PAINTED. REPAIR CARRIED OUT AT BARREL NUT BORE NR 23L IS ACCEPTABLE IAW EN 1057-06.

Part: BUSHING — CORRODED (HORIZONTAL STAB) · airframe 46,984 hrs · 9,427 cycles

HORIZONTAL STABILIZER BARREL NUT HOLE NR 9R EXISTING REPAIR BUSHING CORRODED. CORRODED BUCKET BUSHING REMOVED. CORROSION AT BORE REMOVED REMAINING BLEND OUT 0.200" EXCEEDED LIMIT. BARREL NUT BORE CLEANED AND PROTECTED. DVI CARRIED OUT AND NO CORROSION FOUND. FAB AND PROTECTED REPAIR BUCKET BUSHING. SEALANT APPLIED AND PAINTED PRIMER. REPAIR CARRIED OUT AT BORE NR 9R IS A ACCEPTABLE IAW EN1055-06.

Part: BUSHING — CORRODED (HORIZONTAL STAB) · airframe 46,984 hrs · 9,427 cycles

HORIZONTAL STABILIZER BOLT HOLE 1R EXISTING REPAIR BUSHING FOUND WITH CORROSION. EXISTING REAPIR BUSHING REMOVED. CORROSION REMOVED, BOTTOM 0.100"DEEP B BEARING/SIDEWALL REMAINING BLENDOUT 0.170"DEEP EXCEEDED LIMIT. VISUAL INSP CARRIED OUT NO CORROSION FOUND. BARREL NUT BORE AND BLEND OUT SMOOTHENED AND PROTECTED. FAB REPAIR BUCKET BUSHING AND PROTECTED. SEALANT APPLIED AND PAINTED PRIMER. REPAIR CARRIED AT BORE NR 1R ACCEPTABLE IAW EN1047-06.

Part: BUSHING — CORRODED (HORIZONTAL STAB) · airframe 46,984 hrs · 9,427 cycles

INSPECTION TYPE:C HORIZONTAL STABILIZER BARREL NUT HOLE 36L EXISTING BUSHING FOUND WITH CORROSION. REPAIR SLEEVE BUSING REMOVED. CORROSION AT BORE REMOVED. BOTTOM BLEND OUT 0.075 DEEP, BEARING/SIDEWALL REMAINING 0.065" EXCEEDED LIMITS. DVI CARRIED OUT NO CORROSION FOUND. BORE SMOOTHENED. FAB AND PROTECTED REPAIR SLEEVE BUSHING. SEALANT APPLIED AND PRIMER PAINTED. REPAIR CARRIED OUT AT BARE NUT BORE NR 36L IS ACCEPTABLE IAW EN1048-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,984 hrs · 9,427 cycles

INSPECTION TYPE:C CABIN:RT SEAT TRACK X=-107.25 FOUND CORROSION AT STA1305~1361 AS MARKED. RT SEATRACK X=-107.25 STA1351 CORROSION REMOVED AND EXCEED LIMITS SRM 53- 70-00 FIG3 VOL1 38, SEATRACK FASTENERS REMOVED, SEAT TRACK CUT AT STA1229 AND 1371. HFEC INSP CARRIED OUT AND NO CRACK EVIDENT. NEW SEAT TRACK HOLES PICK UP AND PROTECTED. SEAT TRACK SPLICE FAB AND PAINTED. NEW SEAT TRACK AND SPLICE INSTALLED SRM 53-70-00 FIG1 VOL 1 REV 38.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,984 hrs · 9,427 cycles

INSPECTION TYPE:C CABIN: RT SEAT TRACK X=-107.25 FOUND CORROSION AT STA1381-1421 AS MARKED. RT SEAT TRACK X=-107.25 STA 1390 TO STA 1461 CORROSION. REMOVED AND EXCEED LIMIT SRM 53-70-00 FIG 3 VOL1 38. SEAT TRACK FASTENERS REMOVED AND SEAT TRACK CUT. HFEC INSP CARRIED AND NO CRACK EVIDENT. SEAT TRACK STA1371-14 91 HOLES PICK-UP AND PROTECTED. SEAT TRACK SPLICE FAB AND PAINTED. NEW SEAT TRACK AND SPLICE INSTALLED SRM 53-70-00 FIG1 VOL 1 REV 38.

Part: DOOR FRAME — DAMAGED (CARGO DOORWAY) · airframe 46,984 hrs · 9,427 cycles

INSPECTION TYPE: C, CENTER CARGO COMPARTMENT DOOR JAMB, AFT VERTICAL SIDE HAS 4" LONG BLEND OUT ON THE EDGE. CTR CARGO COMPT DR JAMB AFT VERT SIDE EDGE TRIM-OFF SRM53-50-00 FIG1 6,TRIMMED AREA 2" BY 6". HFEC CARRIED OUT AND NO CRACK EVIDENT. FAB TWO PC S REPAIR DOUBLER AND FILLER SRM 53-50-00, DOUBLER AND FILLER FASTENER HOLE PICK-UP AND REPROTECTED. NEW REPAIR DOUBLER 2PCS AND FILLER 1EA INSTALL SRM 51-31-01. PAINT TOUCHED UP ON REWORK AREA SRM 51-21-01 VOL II REV 38.

Part: DOUBLER — DAMAGED (CARGO DOOR) · airframe 46,984 hrs · 9,427 cycles

INSPECTION TYPE:C BULK CARGO COMPARTMENT DOOR HAS A VERTICAL DOUBLER ON THE FORWARD EDGE. BULK CARGO COMPT DR FWD EYE END ROD BOLT AND NUT REMOVED FOR SHEETMETAL ACCESS AMM20-50-02. DOUBLER REMOVED SRM 51-31-01. FAB NEW REAPIR DOUBLER SRM 52-10-00, HOLES PICK-UP SRM 51-31-01, REPROTECTED SRM 51-21-01. NEW DOUBLER PAINTED SRM 51-21-01. NEW DOUBLER INSTALLED SRM 51-35-01 AND SRM 51-33- 01. BULK CARGO COMPT DR FWD EYE END ROD BOLT AND NUT INSTALL AMM 20-50-02.