N272UP

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,363 hrs · 19,590 cycles

*** SUPPLEMENTAL SDR *** AT CRUISE 30 MINUTES INTO FLIGHT LEVEL 2 FUEL QTY FAULT WITH TANK 2 FUEL QTY "X"-ED. #2 FUEL QTY REGAINED ON FINAL APPROACH **OII 2** **DD 12/04** R/R #2 TANK L/H MJP REF AMM 28-41-40-401 OPS AND LEAK CHECK GOOD PLACARD REMOVED DMP REVERSED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,361 hrs · 19,589 cycles

*SDR FILED OPEN* AT CRUISE 30 MINUTES INTO FLIGHT LEVEL 2 FUEL QTY FAULT WITH TANK 2 FUEL QTY "X"-ED. #2 FUEL QTY REGAINED ON FINAL APPROACH

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 71,247 hrs · 19,522 cycles

EMER LTS BAT 1 LO MESSAGE DURING TEST REVERSED DMP. R&R'D EMER LIGHT BATTERY POWER SUPPLY PER AMM 33-51-01. OPS CHECK GOOD. DEFERRAL CLEARED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,244 hrs · 19,519 cycles

DAMAGE FOUND ON RH WING NO. 3 SLAT, STATION XOS 402. INADVERTENLY CLOSED. C/W EO-88327-REQ1. CHKS GOOD. OK TO CONT.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,244 hrs · 19,519 cycles

DAMAGE FOUND AT RH NO. 4 SLAT TRAILING EDGE, OUTBOARD, UPPER SURFACE. COMPLETED #4 SLAT INSTALLATION PER MM 27-80-30-400-802 ITEM IS CLOSED.

Part: PANEL — FUMES (CABIN) · airframe 71,076 hrs · 19,422 cycles

INSPECTION TYPE:NA*** EMERGENCY DECLARED *** ON DESCENT SDF HEARD ELECTRICAL ARC SOUND AND FLASH FROM ELECTRICAL PANEL BEHIND F.O. IMMEDIATELY SMELLED ELECTRICAL FUMES OVERHEAD PANEL LIGHTS WENT OUT.FOUND OVERHEAD/ OBSERVER STATION INSTRUMENT LIGHTING DIMMER SWITCH BURNED UP REMOVED AND REPLACED U1-130 (OVERHEAD INSTRUMENT LIGHTING DIMMER) OPS CHECKS GOOD REF AMM 33-11-03 FIM 33-11-22-00 FIG 116 ESR 33-11-10-01.

Part: BOTTLE — BLOWN (DOORS) · airframe 71,076 hrs · 19,422 cycles

INSPECTION TYPE:NAL1 DOOR BOTTLE BLOWN TO EXIT AC.RESERVICED L1 DOOR BOTTLE PER AMM 12-25-04.

Part: CABLE — BROKEN (DOORS) · airframe 70,946 hrs · 19,339 cycles

INSPECTION TYPE:NA *SDR FILED OPEN* L1 DOOR BOUNCES WHILE CLOSING UPPER AFT CABLE IS EXCESSIVELY LOOSE WHEN THE DOOR IS UP AND THE LOWER AFT CABLE IS EXCESSIVELY LOOSE WHEN THE DOOR IS DOWN. UPPER AFT CABLE HAS MULTI BROKEN STRANDS ALSO CABLE ORD ON REQ #450834, 450843. PLACED L1 DOOR ON MEL 52-10-3-1-2-1. NO DMP. R1 DOOR TO BE USED AS PRIMARY DOOR. PLACARD INSTALLED. R&R L1 DOOR UPPER AFT DRIVE CABLE IAW AMM 52-11-03-000-801 & AMM 52-11-03-400-801. L1 DOOR OPS CKS GOOD. THIS CLEARS M809218 PLACARD REMOVED. IPC: 51-11-05-05 ITEM 243

Part: SIGN — DETACHED (CABIN) · airframe 70,826 hrs · 19,259 cycles

INSPECTION TYPE:NAEXIT SIGN ON DOOR 1L FELL OFF WHILE DOOR WAS IN TRANSIT REPEAT WRITE FROM PAGE 295518.R&R L1 EXIT SIGN ASSY OPS GOOD PER MM 33-27-05 ESR IPC 33-27-01-05 #130K.

Part: SUPPORT BRACKET — CRACKED (BS 1139) · airframe 70,224 hrs · 18,951 cycles

INSPECTION TYPE:1CCAC AVI COMPARTMENT R/H SIDE AVI RACK HAS BRACKET SUPPORT THAT IS CRACKED AT STA 1139.REPLACED CRACKED SUPPORT IN THE CAC AVI COMPARTMENT AVI RACK IAW SRM 51-31-01 (MINOR)

Part: BRACKET — CORRODED (LT WING TE FLAP) · airframe 70,224 hrs · 18,951 cycles

INSPECTION TYPE:1CL/H WING I/B FLAP O/B FWD FITTING PANEL BRACKET I/B SIDE HAS CORROSION.REPLACED TEE BRACKET ON THE L/H WING I/B FLAP I/B SIDE IAW SRM 51-31-01 (MINOR)

Part: SKIN — GOUGED (FUSELAGE) · airframe 70,224 hrs · 18,951 cycles

INSPECTION TYPE:1CFWD CARGO DOOR AFT LWR SILL AREA EXISTING REPAIR HAS A GOUGE.REPAIRED FWD CARGO DOOR AFT LWR SILL AREA EXISTING REPAIR IAW VT-SAA EA 011-5330-01-A9740 REV I/R AND UPS EO MD11-5330-85131-A DATED 10/28/2022 (MINOR)

Part: BRACKET — CORRODED (LT WING TE FLAP) · airframe 70,224 hrs · 18,951 cycles

INSPECTION TYPE:1CL/H WING I/B FLAP O/B FWD FITTING PANEL BRACKET O/B SIDE HAS CORROSION.REPLACED TEE BRACKET ON THE L/H WING I/B FLAP O/B FWD FITTING O/B SIDE IAW SRM 51-33-01 (MINOR)

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 70,224 hrs · 18,951 cycles

INSPECTION TYPE:1C, LEFT WING I/B FLAP SURFACE HAS A DENT AT STA YIFH=70.5, XIFH=177.320.REPAIRED L/H WING I/B FLAP AT STA YIFH=70.5, XIFH=177.320 IAW EA 011-5753-01-A9741 REV I/R AND MD11-5750-85123-A AND FAA FORM 8100-9. MAJOR

Part: STIFFENER — CHAFED (AFT BULKHEAD) · airframe 70,224 hrs · 18,951 cycles

INSPECTION TYPE:1CAFT BODY STA 2163.685 BULKHEAD R/H SIDE STIFFENER HAS CHAFE DAMAGEDREPAIRED STIFFENER AT STA 2163.685 BULKHEAD R/H SIDE IAW SRM 53-00-00 (MINOR)

Part: FRAME — CRACKED (INSTRUMENT PANEL) · airframe 70,224 hrs · 18,951 cycles

INSPECTION TYPE:1CCAPT AND FIRST OFFICER LOWER INSTRUMENT PANEL FRAME IS CRACKED.REPAIRED CRACKED INSTRUMENT PANEL FRAME IAW UPS EO MD11-2510-82425-C DATED 10/27/2022. (MINOR)

Part: TRUNNION — CRACKED (NLG) · airframe 70,224 hrs · 18,951 cycles

INSPECTION TYPE:1CR/H NLG TRUNION FITTING APPEARS TO BE CRACKED FROM FASTENER TO FASTENER AT STA Y=582.5, Z=-114, X=-24.00.REPAIRED R/H NLG TRUNION FITTING AT STA Y=582.5, Z=-114, X=-24.00 IAW SRM 53-10-14 REPAIR 2 FIG 202 REV. 69.01. (MAJOR)

Part: DOOR — INOPERATIVE (DOOR) · airframe 69,821 hrs · 18,729 cycles

INSPECTION TYPE:NADOOR L1 "DOOR DISARMED" LIGHT HOUSING KEEPS FALLING OUT OF BULKHEADR&R DOOR DISARMED LIGHT INDICATOR PER AMM 20-50-00 AND WPM 52-11-01. OPS CHECKS GOOD PER AMM 52-11-02-010-801 STEP C. (1). ESR: IPC 52-11-70-01 ITEM 170

Part: NONE — NONE (POWERPLANT) · airframe 69,605 hrs · 18,618 cycles

INSPECTION TYPE:NA"ENG 1 FADEC MAINT" MSG 1:30 INTO FLIGHT AT FL390REMOVED & REPLACED #1 ENGINE CONTROL STATORALTERNATOR IAW MD11 AMM 73-21-21-401 CONFIG2. PERFORMED EEC IDLE TEST 06 NO FAULTS LOGGED.

Part: NONE — DAMAGED (DOOR) · airframe 69,039 hrs · 18,331 cycles

INSPECTION TYPE:N/AL1 DOOR PIN LANYARD FORWARD UPPER FOR SLIDE DAMAGEDREPLACED LANYARD REF AMM 52-11-02-000-801.

Part: NONE — NONE (DOORS) · airframe 69,039 hrs · 18,331 cycles

INSPECTION TYPE:NAL-1 UPPER DOOR COVER AFT SIDE PIN LANYARD BROKEN.R/R LANYARD REF AMM 52-11-02-000-801.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 67,951 hrs · 17,754 cycles

INSPECTION TYPE: NA CREW REPORTED EMERGENCY LIGHT BAT 1 LO. DEFERRED EMERGENCY LIGHT SYSTEM, IAW MEL 33-50-4. PLACARD INSTALLED C/W DMP 33-50-4 CBS OPENED OVERHEAD PANEL F24 E67 G23 LOWER MAIN ILLEG G13 F13 ILLEG M731047 ASSGNED. REPLACED EMERGENCY POWER SUPPLY. REPLACED RELAY R2-5700, NO HELP. FOUND 28 VDC MISSING P10-1756A, P/N 11. T/S PER WD 33-51-010. REPAIRED WIRING AT TB S3-692, PER SWPM 20-30-00. OPERATIONS CHECK OK. M731047 CLOSED.

Part: PAN — GOUGED (MAIN CARGO DOOR) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 4C UPPER CARGO DOOR FWD LOWER PAN IS GOUGED.REMOVED AND REPLACED GOUGED UPPER CARGO DOOR FWD LOWER PAN IAW MD-11 SRM 51-33-01 AND 51-35-01. (MINOR)

Part: BEAM — CRACKED (RT WING TE FLAP) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 2C RT OUTBOARD FLAP INBOARD HINGE FAIRING BEAM CRACK. REMOVED AND REPLACED CRACKED BEAM AT RT OUTBOARD FLAP INBOARD HINGE, IAW SRM 51-35-01,51-33-01 AND DWG ARC2151. (MINOR)

Part: FITTING — DAMAGED (LT AILERON) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 4C LT WING INBOARD AILERON ACTUATOR MOUNT FITTING INBOARD LUG ANTI-ROTATION TAB IS DAMAGED. REPAIRED DAMAGED LT WING INBOARD AILERON ACTUATOR MOUNT FITTING INBOARD LUG ANTI-ROTATION TAB, IAW VT-SAA EA 011-5751-01-A8719 REV IR AND UPS EO MD11-5750-78561-A. (MINOR)

Part: BRACKET — CORRODED (RT WING TE FLAP) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 2C RT WING OUTBOARD FLAP INBOARD HINGE LUG HOLES CORRODED. REPAIRED RT OUTBPARD FLAP INBOARD HINGE CORRODED LUG HOLES, IAW VT-SAA EA 011-5740-01-A8716 REV I/R AND UPS EO MD11-5750-78565-A. (MINOR).

Part: FITTING — MIGRATED (RT ELEVATOR) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 4C RT HORIZONTAL STABILIZER TRAILING EDGE NR 2 HINGE FITTING AT STA XE 108 INBOARD & OUTBOARD BUSHINGS ARE MIGRATED. REPAIRED MIGRATED RT HORIZONTAL STABILIZER TRAILING EDGE NR 2 HINGE FITTING AT STA XE 108 INBOARD & OUTBOARD BUSHINGS, IAW VT-SAA EA 011-5510-01-A8710 REV IR AND UPS EO MD11-5520-78540-A. (MINOR)

Part: FITTING — DAMAGED (RT AILERON) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 4C RT WING INBOARD AILERON ACTUATOR MOUNT FITTING INBOARD LUG ANTI-ROTATION TAB IS DAMAGED. REPAIRED DAMAGED RT WING INBOARD AILERON ACTUATOR MOUNT FITTING INBOARD LUG ANTI-ROTATION TAB, IAW VT-SAA EA 011-5751-01-A8720 REV IR AND UPS EO MD11-5750-78562-A. (MINOR)

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 2C RT OUTBOARD FLAP HAS A CRACKED FITTING INSIDE PANEL 657HT, HINGE ATTACH FITTING. REMOVED AND REPLACED RT OUTBOARD FLAP, IAW AMM27-50-30-400-802. (MINOR)

Part: LONGERON — CRACKED (MAIN CABIN) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 4C MAIN CABIN LONGERON 14R IS CRACKED AT STA 1219. REPAIRED CRACKED MAIN CABIN LONGERON 14R BETWEEN STA 1211-1226.5, IAW MD-11 SRM 53-00-05, REPAIR 1, FIGURE 201 & 202. (MAJOR)

Part: SPAR CAP — CORRODED (RT WING) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 4C RT WING AFT LOWER SPAR CAP HAS EXFOLIATION CORROSION INBOARD OF OUTBOARD FLAP OUTBOARD HINGE.REPAIRED CORRODED RT WING REAR SPAR LOWER CAP VERTICAL FLANGE AFT SURFACE, HORIZONTAL AFT FLANGE UPPER AND LOWER SURFACES/BETWEEN XORS 720 & XORS 732, IAW VT-SAA EA 011-5710-01-A8702 REV IR AND UPS EO MD11-5710-78524-A. (MINOR)

Part: SPAR CAP — CORRODED (LT WING) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 4C LT WING REAR SPAR LOWER CAP HAS CORROSION JUST BELOW NR 3 SPOILER. REPAIRED LT WING REAR SPAR LOWER CAP/VERTICAL FLANGE AFT SURFACE/BETWEEN XORS 582 & XORS 587, IAW VT-SAA EA 011-5710-01-A8708 REV. IR AND UPS EO MD11-5710-78522-A. (MINOR)

Part: STIFFENER — CRACKED (RT WING) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 2C RT WING UPPER LEADING EDGE PANEL 616ET 2 EA STIFFENER CRACK. REMOVED AND REPLACED CRACKED 2 EA STIFFENER AT RT WING LEADING EDGE, IAW SRM 51-31-01 AND SRM 51-35-01. (MINOR)

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 4C LT WING INBOARD FLAP UPPER SKIN HAS 2 EA LARGE DENTS 45" FROM TRAILING EDGE AND 77' FROM INBOARD END. REPAIRED DENTED LT WING INBOARD FLAP UPPER SKIN AT STA XIFH 203 AND XIFH 39, IAW MD-11 SRM 57-00-01, REPAIR 1, FIGURE 201. (MAJOR)

Part: SPAR CAP — CORRODED (LT WING) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 4C LT WING REAR SPAR UPPER CAP AFT FLANGE HAS CORROSION BETWEEN XORS 672.5 AND XORS 762. REPAIRED CORRODED LT WING REAR SPAR UPPER CAP AFT FLANGE BETWEEN XORS 672.5 AND XORS 762, IAW VT-SAA EA 011-5710-01-A8724 REV IR AND UPS EO MD11-5710-78556-A. (MINOR)

Part: SKIN — DENTED (TAILCONE) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 2C TAILCONE LT SKIN HAS A DENT AT 7 O'CLOCK POSITION STA 2184. REPAIRED DENT ON TAILCONE LT SKIN AT 7 O'CLOCK POSITION STA 2184, IAW SRM 53-00-00 REPAIR GENERAL FIG 204. (MINOR)

Part: SPAR CAP — CORRODED (RT WING) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 2C RT WING AFT LOWER SPAR CAP HAS CORROSION AT XORS STA 705. REPAIRED RT WING AFT LOWER SPAR CAP BETWEEN XORS STA 703-XORS STA 708, IAW SRM 57-00-10 FIG 101 ALLOWABLE DAMAGE 1. (MINOR).

Part: SKIN — CHAFED (RT WING DROOP) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 4C RT WING DROOP LEADING EDGE INBOARD LEADING EDGE SKIN REPAIR DOUBLER IS CHAFED. REPAIRED CHAFED RT WING DROOP LEADING EDGE INBOARD LEADING EDGE SKIN REPAIR AT STA XDLE 309.934, IAW MD-11 SRM 57-40-01, REPAIR 15, FIGURE 202. (MAJOR)

Part: RIVET — LOOSE (NR 2 INLET) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 4C NR 2 ENGINE INLET NOSE COWL LIP HAS NUMEROUS LOOSE AND WORKING RIVETS. REPAIRED NR 2 ENGINE INLET NOSE COWL LIP LOOSE AND WORKING RIVETS, IAW VT-SAA EA 011-7110-01-A8735 REV IR AND UPS EO MD11-7110-78559-A. (MINOR)

Part: INTERCOSTAL — CRACKED (RT A/C BAY) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 4C RT A/C BAY INTERCOSTAL BETWEEN STA 535-555 IS CRACKED. REMOVED AND REPLACED CRACKED RT A/C BAY INTERCOSTAL BETWEEN STA 535-555, IAW MD-11 SRM 51-35-01. (MINOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 4C RT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED BETWEEN STA XOS 783-XOS 789. REPAIRED CRACKED RT WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN STA XOS 783-789, IAW MD-11 SRM 57-40-02, REPAIR 15, FIGURE 205. (MAJOR)

Part: STIFFENER — CRACKED (AFT CARGO) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 4C AFT CARGO RT VERTICAL STIFFENER 31" FROM CENTER LINE AT STA 1841 IS CRACKED. REMOVED AND REPLACED CRACKED RT VERTICAL STIFFENER 31" FROM CENTER LINE AT STA 1841, IAW MD-11 SRM 51-33-01. (MINOR)

Part: FORMER — CRACKED (RT WING) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 2C RT WING FIXED LEADING EDGE FORMER CRACK AT XORS STA 993. REMOVED AND REPLACED CRACK FORMER AT RT WING FIXED LEADING EDGE XORS STA 993, IAW SRM 51-33-01 AND DWG ARB1164. (MINOR)

Part: TRUSS — CRACKED (MAIN CABIN) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 4C CENTER ACCESSORY COMPARTMENT LONGERON 27R TRUSS FITTING BETWEEN STA 1139-1159 IS CRACKED. REMOVED AND REPLACED CRACKED CENTER ACCESSORY COMPARTMENT LONGERON 27R TRUSS FITTING BETWEEN STA 1139-1159, IAW MD-11 SRM 51-33-01. (MINOR)

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 4C RT MLG WHEEL WELL AFT OUTBOARD WEB 4TH VERTICAL STIFFENER IS CRACKED. REMOVED AND REPLACED CRACKED RT MLG WHEEL WELL AFT OUTBOARD WEB 4TH VERTICAL STIFFENER, IAW MD-11 SRM 51-35-01. (MINOR)

Part: STIFFENER — CRACKED (LT WING) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 2C LT WING FIXED LEADING EDGE STIFFENER CRACK AT XOS STA 1026. REMOVED AND REPLACED CRACKED STIFFENER AT LT WING FIXED LEADING EDGE STA 1026, IAW SRM 51-35-01 AND SRM 51-33-01.

Part: STRAP — CRACKED (LT WING L/E) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 2C LT WING FIXED LEADING EDGE SPLICE STRAP CRACK XOS STA 906.5. REMOVED AND REPLACED CRACKED SPLICE STRAP AT LT WNG LEADING EDGE AT XOS STA 906.5, IAW SRM 51-33-01. (MINOR)

Part: STIFFENER — CRACKED (AFT CARGO) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 4C AFT CARGO RT VERTICAL STIFFENER 38" FROM CENTER LINE AT STA 1841 IS CRACKED. REMOVED AND REPLACED CRACKED AFT CARGO RT VERTICAL STIFFENER 38" FROM CENTER LINE AT STA 1841, IAW MD-11 SRM 51-33-01. (MINOR)

Part: STIFFENER — CRACKED (AFT CARGO) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 4C AFT CARGO RT VERTICAL STIFFENER 38" FROM CENTER LINE AT STA 1841 IS CRACKED. REMOVED AND REPLACED CRACKED AFT CARGO RT VERTICAL STIFFENER 38" FROM CENTER LINE AT STA 1841, IAW MD-11 SRM 51-33-01. (MINOR)

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 2C LT OUTBOARD FLAP INBOARD HINGE FITTING CRACK. REMOVED AND REPLACED LT OUTBOARD FLAP ASSEMBLY, IAW AMM 27-50-30-000-802 AND AMM 27-50-30-400-802. (MINOR)

Part: SKIN — GOUGED (RT WING) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 4C RT WING FIXED LEADING EDGE SKIN SHROUD OUTBOARD OF NR 8 SLAT IS GOUGED. REPAIRED GOUGED RT WING FIXED LEADING EDGE SKIN SHROUD BETWEEN XOS 1187-XOS 1191, IAW MD-11 SRM57-40-01, REPAIR 16, FIGURE 201. (MAJOR)

Part: FLOORBEAM — CRACKED (FWD CARGO) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 4C FWD CARGO FLOOR BEAM TEE ANGLE AT STA 6-70 ABOVE LONGERON 43R IS CRACKED. REMOVED AND REPLACED CRACKED FWD CARGO FLOOR BEAM TEE ANGLE AT STA 6-70 ABOVE LONGERON 43R, IAW MD-11 SRM 51-33-01. (MINOR)

Part: ANGLE — CRACKED (LT WING) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 4C LT WING FIXED LEADING EDGE TEE ANGLE SUPPORT FOR PANEL 515FB IS CRACKED. REMOVED AND REPLACED CRACKED LT WING FIXED LEADING EDGE TEE ANGLE SUPPORT FOR PANEL 515FB, IAW MD-11 SRM 51-35-01. (MINOR)

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 2C RT MLG WHEEL WELL 3RD VERTICAL STIFFENER AT AFT OUTBOARD END IS CRACKED. REMOVED, FABRICATED, AND REPLACED STIFFENER, IAW DWG ANB7203 AND SRM 51-35-01. (MINOR)

Part: DOUBLER — CRACKED (RT WING LE) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 4C RT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED BETWEEN XOS 637-XOS 643. REPAIRED CRACKED RT WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN XOS 637-XOS 643, IAW MD-11 SRM 57-40-02, REPAIR 15, FIGURE 205. (MAJOR)

Part: PAN — CRACKED (RT GEAR DOOR) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 2C RT MLG DOOR AFT LOWER PAN (CORNER) CRACK. REMOVED AND REPLACED CRACKED RT MLG DOOR PAN (CORNER) AT AFT LOWER END, IAW SRM 51-31-01,51-35-02,51-35-01 AND 51-41-01. (MINOR)

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 2C LT MLG WHEEL WELL 3RD VERTICAL STIFFNER AT OUTBOARD END IS CRACKED. REMOVED AND REPLACED STIFFNER, IAW SRM 51-35-01. (MINOR)

Part: FITTING — GOUGED (NR 3 FAN COWL) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 4C NR 3 ENGINE OUTBOARD FAN COWL FWD MOUNT FITTING IS GOUGED. REPAIRED GOUGED NR 3 ENGINE OUTBOARD FAN COWL FWD MOUNT FITTING, IAW VT-SAA EA 011-7110-01-A8699 REV IR AND UPS EO MD11-7110-78456-A. (MINOR)

Part: INTERCOSTAL — CRACKED (LT MLG WW) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 2C LT MLG KEEL BEAM BULKHEAD INTERCOSTAL IS CRACKED JUST FWD OF HYD SERVICING CONTAINER. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL, IAW DWG AEA7094 AND SRM 51-35-01. (MINOR)

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 4C VERTICAL STAB NR 2 PYLON WEB ANGLE IS CRACKED JUST AFT OF NR 4 BANJO FITTING INSIDE PANEL 457AL. REPLACED CRACKED VERTICAL STAB NR 2 PYLON WEB ANGLE JUST AFT OF NR 4 BANJO FITTING INSIDE PANEL 457AL, IAW MD-11 SRM 54-05-41. (MINOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 4C RT WING BEADED DOUBLER BETWEEN XOS 746-XOS 753 TEMPORARY REPAIR REQUIRES PERMANENT REPAIR. REPAIRED CRACKED RT WING BEADED DOUBLER BETWEEN XOS 746-XOS 753, IAW MD-11 SRM 57-40-02 REPAIR 15, FIGURE 205. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 2C RT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED BETWEEN STA XOS 698 TO 703. REPAIRED CRACKED RT WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN STA XOS 698 TO 703, IAW SRM 57-40-02 REPAIR 15 FIG 205. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 4C RT WING FIXED LEADING EDGE BEADED DOUBLER TEMPORARY REPAIR BETWEEN STA XOS 728-XOS 734 REQUIRES PERMANENT REPAIR. REPAIRED CRACKED RT WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN STA XOS 728-XOS 734, IAW MD-11 SRM 57-40-02, REPAIR 15, FIGURE 205. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 4C LT WING BEADED DOUBLER BETWEEN XOS 661-XOS 667 TEMPORARY REPAIR REQUIRES PERMANENT REPAIR.REPAIRED CRACKED LT WING BEADED DOUBLER BETWEEN XOS 661-XOS 667, IAW MD-1 SRM 57-40-02 REPAIR 15 FIGURE 205. (MAJOR)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 67,779 hrs · 17,675 cycles

INSPECTION TYPE: 4C FUSELAGE SKIN FWD LOWER CARGO DOOR CUTOUT AFT JAMB EXISTING REPAIR AT STA 1002 HAS EDGE DAMAGE. REPAIRED DAMAGED FUSELAGE SKIN FWD LOWER CARGO DOOR CUTOUT AFT JAMB EXISTING REPAIR AT STA 1002, IAW VT-SAA EA 011-5330-01-A8704 REV IR AND UPS EO MD11-5330-78482-A. (MINOR)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 67,558 hrs · 17,599 cycles

INSPECTION TYPE: NA EMERGENCY LT BAT 1 LOW. DEFERRED EMERGENCY LIGHTING SYSTEM, PER MEL 33-50-4 CW DMP 33-50-4. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY, PER MM 33-51-01-401. REVERSED DMP 33-50-4. OPERATIONS CHECKS GOOD. M721465 CLOSED. ESR 33-51-01-05-015.

Part: SEAL — DAMAGED (ANTI-ICE SYSTEM) · airframe 66,469 hrs · 17,131 cycles

INSPECTION TYPE:N/A*** DIVERTED*** APPROACHING TOP OF DESCENT FOR EWR, WITH ANTI-ICE SELECTEDON RCVD LEVEL 2 A-ICE DISAG. CONSULTED WITH FLIGHT CONTROL FOR DIVERT TO RDU.REPLACED DAMAGED SEAL ON LEFT OUTBD HORIZ STAB LEADING EDGE ANTI-ICE DUCT EXPANSION SLEEVE. OPS OK. NO LEAKS NOTED. REF MM 55-11-02-400-802 AND MM 30-12-00-700-802.

Part: TRANSMITTER — MALFUNCTIONED (ANTI ICE SYSTEM) · airframe 66,389 hrs · 17,100 cycles

DIVERSION - LVL 2 "TAIL A/I DISAG" AFTER T.O.D. DIVERT TO KSLC DUE TO ICING CONDITIONS AT DEN. AIRCRAFT REMAINED IN VMC CONDITIONS. TRANSFERRED TAIL ANTI-ICE DIFFERENTIAL PRESSURE SENSORS, M697697 ASSIGNED. SEE ITEM 3 FOR REQUIRED ADDITIONAL DEFERRAL M697701. DMP 30-12-2 ACCOMPLISHED.T/S PER FIM 30-12-00-101. R/R PRESS TRANSMITTER T2-1396 AND T2-1397 PER AMM 36-12-04/401. CKS OK. RTS CKS GOOD. THIS CLEARS M697697

Part: HINGE FITTING — CORRODED (RT WINGTE FLAP) · airframe 66,228 hrs · 17,025 cycles

INSPECTION TYPE:SVR/H O/B FLAP UPPER O/B ACTUATOR ATTACH LUG HAS PITTING CORROSION IN THE BORE.REPAIRED CORRODED R/H FLAP UPPER O/B ATTACH LUG IAW UPS EO MD11-5740-74906-B.

Part: ATTACH FITTING — CORRODED (RT FLAP ACTUATOR) · airframe 66,228 hrs · 17,025 cycles

INSPECTION TYPE:S/VR/H O/B FLAP UPPER I/B ACTUATOR ATTACH LUG HAS PITTING CORROSION IN THE BORE.REPAIRED CORRODED R/H O/B FLAP UPPER I/B ACTUATOR ATTACH LUG IAW UPS EO MD11-5740-74906-B.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 65,407 hrs · 16,710 cycles

DURING EMERGENCY LIGHTS TEST, OBSERVED LEVEL 1 EMERGENCY LIGHT BATTERY 1 LOW ILLUMINATED. REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY. OPS CHECK GOOD IAW AMM 33-51-01.

Part: SKIN — CRACKED (LT WING) · airframe 65,318 hrs · 16,671 cycles

DENT WITH CRACK LEFT WING LOWER SURFACE ARB7119-1REPAIRED IAW EO MD11-5730-72713-A.

Part: CONTROL HANDLE — OUT OF ADJUST (R1 DOOR) · airframe 65,288 hrs · 16,662 cycles

INSPECTION TYPE:N/A R-1 DOOR EMERGENCY/DOOR CONTROL MECHANISM PROTRUDING I/2 INCH OUT FROM FUSELAGE. FOUND FWD GIRT BAR ARM VIEWING WINDOW FLAPPER INTERFERRING WITH LOCK. ADJUSTED WINDOW & FLAPPER SLIDE ARMING CONTROL HANDLE OPS CHECKS GOOD PER AMM 52-11-02-501.

Part: VAPOR BARRIER — DEBONDED (FLT DECK) · airframe 65,119 hrs · 16,616 cycles

INSPECTION TYPE:NAVAPOR BARRIER BEHIND FWD BULKHEAD R/H SIDE LOWER PORTION DISBONDINGRESECURED VAPOR BARRIER AS REQUIRED. REF AMM 20 00 00

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,422 hrs · 16,401 cycles

CREW BERTH EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE LAMPS & OPS TESTED OK IAW AMM 33-52-01.

Part: FASTENER — SHEARED (BS 316.9-345.7) · airframe 64,120 hrs · 16,331 cycles

INSPECTION TYPE: 3C, FOUND A SHEARED FASTENER BETWEEN BS 316.9 - 345.7. REMOVED AND REPLACED THE FASTENER IAW EA 011-5730-01-A7537, REV IR, AND EO MD11-5730-70571-A. MINOR.

Part: STRINGER — CRACKED (LT WING) · airframe 64,120 hrs · 16,331 cycles

INSPECTION TYPE: 3C, LT WING STRINGER 32 WAS CRACKED BETWEEN XORS 896.070 & 917.200. REPAIRED THE STRINGER IAW EA 011-5710-01-A7515, REV I/R, AND EO MD11-5710-70579-A. MAJOR.

Part: LONGERON — CORRODED (BS 1300) · airframe 64,120 hrs · 16,331 cycles

INSPECTION TYPE: 3C, EXFOLIATED CORROSION ON EXTERNAL LONGERON 28L UNDER WING TO BODY FAIRING, BELOW THE L3 DOOR AT BS 1300. REPAIRED THE LONGERON IAW EA 011-5310-01-A7528, REV IR, AND EO MD11-5310-70581-A. MAJOR.

Part: MOUNT — DAMAGED (L1 DOOR SLIDE) · airframe 64,120 hrs · 16,331 cycles

L1 DOOR FWD SLIDE MOUNT FITTING WAS WORN AND CHAFED. REMOVED, FABRICATED, AND REPLACED THE MOUNT FITTING IAW DWG ABA8513, AND SRM 51-33-01. MINOR.

Part: STRINGER — CRACKED · airframe 64,120 hrs · 16,331 cycles

INSPECTION TYPE:3C, STRINGER 46 WAS CRACKED. REPAIRED STRINGER IAW EA 011-5710-01-A7529, REV I/R, AND EO MD11-5710-70582-A. MAJOR.

Part: SKIN — CRACKED (LT WING LOWER) · airframe 64,120 hrs · 16,331 cycles

LEFT LOWER WING SKIN ACCESS PANEL 536AB LANDING HAD TWO CRACKED FASTENER HOLES. REPAIRED THE ACCESS PANEL LANDING IAW SRM 57-20-02, REPAIR 5, FIG 201. MINOR.

Part: RIB — BROKEN (LT ELEVATOR) · airframe 64,120 hrs · 16,331 cycles

LEFT ELEVATOR L/E RIB UPPER AFT INBD FLANGE WAS BROKEN OFF INSIDE PANEL 335CT. REPAIRED THE RIB AT XE 125.8 IAW EA 011-5520-01-A7521, REV IR, AND EO MD11-5520-70541-A. MAJOR.

Part: FLOORBEAM — CORRODED (BS 1841) · airframe 64,120 hrs · 16,331 cycles

INSPECTION TYPE 3C, AFT CARGO COMPARTMENT FLOORBOARD FLOORBEAM WAS CORRODED AROUND THE NUT PLATES, BS 1841, LBL 7 - LBL 22. REPAIRED THE FLOORBEAM IAW EA 011-5310-A7527, REV IR, AND EO MD11-5310-70498-A. MAJOR.

Part: STRINGER — CRACKED · airframe 64,120 hrs · 16,331 cycles

STRINGER 47 WAS CRACKED. REPAIRED THE SRTINGER IAW SRM 57-10-03, REPAIR 1, FIG 201. MAJOR.

Part: STRINGER — CRACKED · airframe 64,120 hrs · 16,331 cycles

STRINGER 45 WAS CRACKED. REPAIRED THE STRINGER IAW SRM 57-10-03, REPAIR 1, FIG 201. MAJOR.

Part: SKIN — CRACKED (RT WING) · airframe 64,120 hrs · 16,331 cycles

RT WING LOWER SKIN ACCESS PANEL 636AB LANDING HAD CRACKS AT 2 FASTENER HOLES BETWEEN XORS. 683.4 - 713.650. REPAIRED RT WING LOWER SKIN LANDING IAW SRM 57-20-02, REPAIR 5, FIG 201.

Part: MOUNT — DAMAGED (L1 DOOR SLIDE) · airframe 64,120 hrs · 16,331 cycles

L1 DOOR AFT SLIDE MOUNT FITTING WAS WORN AND CHAFED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG ABA8513, AND SRM 51-33-01. MINOR.

Part: SUPPORT BRACKET — CRACKED (RT WING TE FLAP) · airframe 64,120 hrs · 16,331 cycles

RIGHT OTBD FLAP, INBD FWD HINGE FAIRING CENTER PANEL SUPPORT BRACKET WAS CRACKED. REMOVED, FABRICATED, AND REPLACED THE SUPPORT BRACKET IAW DWG ARC0504, AND SRM 51-33-01. MINOR.

Part: TEE FITTING — CRACKED (BS 1321) · airframe 64,120 hrs · 16,331 cycles

MAIN CABIN, BS 1321, LONGERON 15L TEE FITTING WAS CRACKED. REMOVED, FABRICATED, AND REPLACED THE LONGERON TEE FITTING IAW DWG AEA7568, AND SRM 51-33-01.

Part: WEB — CRACKED (BS 1372) · airframe 64,120 hrs · 16,331 cycles

RIGHT WW FUEL TANK UPPER AFT WEB WAS CRACKED AT AT BS 1372, RBL 80. REPAIRED THE WEB IAW EO MD11-5710-70319-A. MAJOR.

Part: BEAM — CHAFED (TAIL CONE) · airframe 64,120 hrs · 16,331 cycles

TAIL CONE HORIZONTAL BEAM HAD DEEP CHAFE DAMAGE ON THE RT SIDE. REPAIRED THE HORIZONTAL BEAM IAW DWG AKC7520, AND SRM 51-35-01. MINOR.

Part: TEE FITTING — CRACKED (BS 1321) · airframe 64,120 hrs · 16,331 cycles

MAIN CABIN, BS 1321, LONGERON 15R, TEE FITTING CRACKED. REMOVED, FABRICATED, AND REPLACED THE LONGERON TEE FITTING IAW DWG AEA7568, AND SRM 51-33-01.

Part: LONGERON — CRACKED (MAIN CABIN) · airframe 64,120 hrs · 16,331 cycles

LONGERON 27R WAS CRACKED UNDER THE R3 DOOR. REMOVED, FABRICATED, AND REPLACED THE LONGERON IAW DWG AEA7127, SRM 51-35-01, AND SRM 51-33-01.

Part: INTERCOSTAL — CRACKED (TAILCONE) · airframe 64,120 hrs · 16,331 cycles

TAILCONE LT UPPER BOX FITTING INTERCOSTAL WAS CRACKED. REMOVED, FABRICATED, AND REPLACED THE INTERCOSTAL IAW DWG AKC7520, AND SRM 51-31-01.

Part: DOOR FRAME — CRACKED (L3 DOOR) · airframe 64,120 hrs · 16,331 cycles

L3 DOOR FRAME LOWER WEB WAS CRACKED AT BS 1251, Z -15. REPAIRED THE DOOR FRAME IAW SRM 53-40-15, REPAIR 3, FIG 201. MAJOR.

Part: FUEL TANK — CORRODED · airframe 64,120 hrs · 16,331 cycles

CENTER WING TANK UPPER CENTER SKIN HAD CORROSION AT XCW=-17, AND BETWEEN STRINGERS 14 & 15. REPAIRED THE TANK IAW 011-5730-01-A7523, REV I/R AND EO MD11-5730-70469-A.

Part: TEE FITTING — CRACKED (FWD CARGO BAY) · airframe 64,120 hrs · 16,331 cycles

TEE FITTING WAS CRACKED AT STATION 6-70, LONGERON 43L. REMOVED, FABRICATED, AND REPLACED THE TEE FITTING IAW DWG A6A7092, AND SRM 51-33-01. MINOR.

Part: LANDING — CORRODED (RT WING) · airframe 64,120 hrs · 16,331 cycles

RIGHT WING UPPER T/E PANEL LANDING INSIDE PANEL 651AB HAD CORROSION AT THE NUTPLATES. REPAIRED T/E PANEL LANDING BETWEEN XOSP 467.342 & XOSP 494.342 IAW SRM 57-50-02, REPAIR 10, FIGURE 201, REV 65, AND SRM 51-38-01, PAR 6 D, REV 65. MAJOR.

Part: WEB — CRACKED (RT WING TE FLAP) · airframe 64,120 hrs · 16,331 cycles

RIGHT WING OTBD FLAP, INBD AFT HINGE FAIRING CENTER -A- FRAME WEB WAS CRACKED. REMOVED, FABRICATED, AND REPLACED THE WEB IAW DWG ARC2151, AND SRM 51-35-02. MINOR.

Part: SUPPORT ANGLE — CRACKED (RT WING TE FLAP) · airframe 64,120 hrs · 16,331 cycles

RIGHT WING OTBD FLAP, INBD HINGE FAIRING, OTBD AFT PANEL SUPPORT ANGLE WAS BROKEN. REMOVED, FABRICATED, AND REPLACED THE SUPPORT ANGLE IAW DWG ARC0745, AND SRM 51-33-01. MINOR.

Part: PAN — CHAFED (MAIN CARGO DOOR) · airframe 64,120 hrs · 16,331 cycles

MAIN CARGO DOOR FWD FRAME PAN HAD A DEEP CHAFE IN TWO PLACES. REMOVED, FABRICATED, AND REPLACED THE MAIN CARGO DOOR FRAME PAN IAW DWG ACA7301, SRM 51-35-01 AND SRM 51-33-01.

Part: FRAME — CRACKED (THRUST REVERSER) · airframe 64,120 hrs · 16,331 cycles

NR 2 ENGINE LT THRUST REVERSER COWL AT 12 O'CLOCK POS., THE FRAME WAS CRACKED. REMOVED AND REPLACED THE NR 2 ENG LT THRUST REVERSER FRAME IAW SRM 54-05-41.

Part: SPAR — CORRODED (RT WING) · airframe 64,120 hrs · 16,331 cycles

RIGHT WING UPPER SKIN HAD CORROSION AT THE AFT SPAR AND T/E PANEL FWD OF THE NR 2 & 3 SPOILERS, WAS BULGED. REPAIRED THE RT WING UPPER SKIN AND AFT SPAR UPPER AFT FLANGE IAW EA 011-5710-01-A7533, REV IR, AND EO MD11-571070578-A. MINOR.

Part: FRAME — CRACKED (LT WING) · airframe 64,120 hrs · 16,331 cycles

LEFT WING L/E COMPARTMENT FRAME AT XORS 630 WAS CRACKED. REMOVED AND REPLACED THE FRAME IAW SRM 51-31-01, 51-33-01, AND 51-35-01. MINOR.

Part: WEB — TORN (TAIL CONE) · airframe 64,120 hrs · 16,331 cycles

TAILCONE RT PATIO DOOR PLATFORM STRUCTURE WAS TORN. REMOVED, FABRICATED, AND REPLACED R/H PATIO DOOR WEB IAW DWG AKC7861 AND SRM 51-35-01.

Part: TAIL CONE — CHAFED (BS 2165) · airframe 64,120 hrs · 16,331 cycles

LEFT SIDE EXTENDED TAILCONE REPAIR FILLER WAS CHAFED BS 2165, BETWEEN Z=35 AND Z=61.5. REPAIRED THE TAIL CONE REPAIR FILLER IAW EO MD11-5350-70353-A.

Part: SKIN — CRACKED (THRUST REVERSER) · airframe 64,120 hrs · 16,331 cycles

NR 1 ENGINE, INBD THRUST REVERSER EXHAUST COWL UPPER AFT END, EXTERNAL SKIN WAS CRACKED AT A RIVET HOLE. REPAIRED IAW EA 011-7830-01-A7519-IR, AND EO MD11-7830-70490-A.

Part: VANE — CRACKED (PRECOOLER) · airframe 64,120 hrs · 16,331 cycles

NR 1 ENGINE OTBD THRUST REVERSER PRECOOLER VANE WAS CRACKED. REMOVED AND REPLACED THE PRECOOLER VAE IAW SRM 54-05-41.

Part: SKIN — CHAFED (RT WING DROOP) · airframe 64,120 hrs · 16,331 cycles

RIGHT WING DROOP L/E SKIN REPAIR DOUBLER WAS CHAFED AT XLDE 309.934. REPAIRED DROOP L/E SKIN IAW SRM 57-40-01, REPAIR 15, FIG 202. MAJOR.

Part: SKIN — CRACKED (THRUST REVERSER) · airframe 64,120 hrs · 16,331 cycles

NR 1 ENGINE, OTBD THRUST REVERSER EXHAUST COWL HAD A CRACK AT A RIVET HOLE ON THE UPPER AFT EXTERIOR SKIN. REPAIRED THE THRUST REVERSER UPPER AFT EXTERIOR SKIN IAW EA 011-7830-01-A7520-IR, AND EO MD11-7830-70491-A. MINOR.

Part: ACCESS DOOR — GOUGED (THRUST REVERSER) · airframe 64,120 hrs · 16,331 cycles

NR 3 ENGINE RT FAN REVERSER LATCH ACCESS AFT DOOR WAS GOUGED. REPAIRED ACCESS DOOR IAW EA 011-7830-01-A7532, REV I/R, AND EO MD11-7830-70508-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 64,120 hrs · 16,331 cycles

LEFT WING L/E BEADED DOUBLER WAS CRACKED BETWEEN XOS 667 - 673. REPAIRED THE CRACKED DOUBLER IAW SRM 57-40-05, REPAIR 15, FIG 205. MAJOR.

Part: CABLE ASSY — DAMAGED (L1 DOOR) · airframe 64,078 hrs · 16,303 cycles

L1 DOOR FWD DRIVE CABLE AND UPPER PULLEY COMPONENTS WERE DAMAGED. R & R THE L1 DOOR LOWER CABLE IAW 52-11-09. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 62,912 hrs · 15,960 cycles

L1 CABIN DOOR DISARMED LIGHT INOPERATIVE. INSTALLED A NEW LIGHT ASSY L2-1361 IAW WDM 52-11-01, OPS NORMAL.

Part: LIGHT — INOPERATIVE (INDICATOR) · airframe 62,776 hrs · 15,919 cycles

R1 EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST LIGHT INOPERATIVE. OPS CHECKED R1 THE SLIDE REMOTE PRESSURE TEST OPS TEST GOOD IAW MM 25-61-15.

Part: SWITCH — INOPERATIVE (R1 DOOR) · airframe 62,160 hrs · 15,720 cycles

R1 DOOR PRESS TO TEST LIGHT INOPERATIVE. INSTALLED NEW BATTERIES, INSTALLED NEW SWITCH ASSY. OPS CHECKED GOOD

Part: LIGHT — NO TEST (R1 DOOR SLIDE) · airframe 62,106 hrs · 15,707 cycles

R1 DOOR SLIDE WILL NOT TEST. R & R BOTH C CELL BATTERIES AND BULB, SYS OPS CHECKED GOOD IAW 25-61-04-710-801

Part: ROLLER — LACK OF LUBE (L1 DOOR) · airframe 61,840 hrs · 15,653 cycles

L1 DOOR DOES NOT OPERATE SMOOTHLY. OILED THE DOOR ROLLERS AND CHAINS. OPS CHECKED SMOOTH IAW AMM 12-25-05

Part: SKIN — CORRODED (BS 2139-2163) · airframe 61,547 hrs · 15,577 cycles

INSPECTION TYPE: PE, XTERIOR FUSELAGE SKIN HAS CORROSION AT BS 2139 - 2163, LONGERONS 33 - 35R. REPAIRED THE SKIN IAW EO MD11-5330-64948-A. MAJOR.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,278 hrs · 15,502 cycles

EMERGENCY LIGHT BATTERY 1 LOW. REMOVED AND REPLACED THE BATTERY POWER SUPPLY IAW AMM 33-51-01-400-802. OPS CHECKED GOOD IAW 33-51-10-01, ITEM 8.

Part: WARNING MESSAGE — ILLUMINATED (EMERGENCY LIGHT) · airframe 60,858 hrs · 15,398 cycles

EMERGENCY BATTERY 1 LOW. R & R R & R MSC IAW AMM 31-42-01 OPS CHECKED NORMAL.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE:2C, INTERCOSTAL CRACKED IN BILGE OF NR 1 A/C COMPARTMENT. REMOVED FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER DWG ACA3816 AND SRM 51-33-01. (MINOR)

Part: LUG — WORN (THRUST REVERSER) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, NR 2 ENGINE LEFT THRUST REVERSER LOWER TRACK LUG WORN. REPAIRED THE TRACK IAW EA 011-7830-01-A6579 REV IR AND EO MD11-7830-62988-A.

Part: HINGE FITTING — CHAFED (RT SPOILER) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE:2C RT WING NR 1 SPOILER IDLER HINGE FITTING CHAFE DAMAGE XISP 269. REPAIRED NOTED CHAFE DAMAGE PER EA 011-5755-01-A6574 REV IR AND EO MD11-5750-62937-A MINOR.

Part: FLOOR SUPPORT — CORRODED (BS 424-453) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, FLOOR SUPPORT CORRODED BS 424 - 453, RBL 65. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT FLOOR SUPPORT BETWEEN BS 380 - 450 IAW DWG ABA7341, AND SRM 51-31-01.

Part: ATTACH FITTING — GOUGED (FUSELAGE) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE:2C, RIGID CARGO BARRIER SIDE ATTACH FITTING 12 GOUGED. REPAIRED NOTED FITTING PER EA 011-5310-01-A6577 REV IR AND UPS EO MD11-5340-62953-A. (MINOR)

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, MAIN CABIN FLOOR PANEL WSP0821-47 CORRODED. REMOVED AND REPLACED THE FLOOR PANEL IAW DWG WSP0821.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE:2C, LAV AREA FLOOR SUPPORT PANEL CORRODED NEAR STA 421 AT X=-67. REMOVED FABRICATED AND INSTALLED REPLACEMENT PANEL PER DWG ABA7331 AND SRM 51-31-01. (MINOR)

Part: ATTACH FITTING — GOUGED (FUSELAGE) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE:2C, RIGID CARGO BARRIER SIDE ATTACH FITTING 16 GOUGED. REPAIRED NOTED FITTING PER EA 011-5310-01-A6576 REV IR AND EO MD11-5340-62954-A. (MINOR)

Part: ATTACH FITTING — GOUGED (FUSELAGE) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE:2C, RIGID CARGO BARRIER SIDE ATTACH FITTING 13 GOUGED. REPAIRED NOTED FITTING PER EA 011-5310-01-A6575 REV IR AND EO MD11-5340-62938-A. (MINOR)

Part: STRUCTURE — CHAFED (TAILCONE) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C,EXTENDED TAILCONE LT SIDE INTERNAL DOUBLER CHAFED. REPAIRED IAW EA 011-5350-01-A6570 REV. IR AND EO MD11-5350-62920-A.

Part: SEAT TRACK — CORRODED (BS 450) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, FWD CABIN SEAT TRACK CORRODED BS 450 RBL 36. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT SEAT TRACKBS 439 - 516 IAW DWG WSP0826, SRM 53-20-52 REPAIR 1, AND 51-31-01.

Part: FLOOR PANEL — CORRODED (BS 475-500) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, RCB AREA FLOOR PANEL WSP0785-501 CORRODED BS 475 - 500, RBL 8.5 TO 17. REPAIRED THE FLOOR PANEL IAW EA 011-5310-01-A6566 REV. IR AND EO MD11-5310-62914-A. (MINOR)

Part: STRUCTURE — CHAFED (TAILCONE) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, EXTENDED TAILCONE RT SIDE INTERNAL DOUBLER CHAFED . REPAIRED IAW EA 011-5320-01-A6571 REV. IR AND EO MD11-5350-62932-A.

Part: FITTING — CORRODED (FUSELAGE) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE:2C, RCB FLOOR FITTING CORRODED AT STA 489 X=-62. REPAIRED CORRODED FITTING PER EA 011-5310-01-A6565 REV IR AND EO MD11-5340-62916-A (MINOR).

Part: SKIN — CHAFED (DROOP LE) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE:2C, RT DROOP L/E OUTER SKIN CHAFED AND CRACKED AT XDLE309. REPAIRED DROP L/E SKIN PER SRM 57-40-01 REPAIR 15 FIG 202 (MAJOR).

Part: FITTING — CORRODED (FUSELAGE) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE:2C, RCB FLOOR FITTING CORRODED AT STA 489 X=8.5. REPAIRED CORRODED FLOOR FITTING PER EA 011-5310-01-A6565 REV IR AND EO MD11-5340-62916-A MINOR.

Part: FITTING — CORRODED (FUSELAGE) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE:2C, RCB FLOOR FITTING CORRODED AT STA 489 X=27.5. REPAIRED CORRODED FITTING PER EA 011-5310-01-A6565 REV IR AND EO MD11-5340-62916-A (MINOR).

Part: SUPPORT FRAME — CRACKED (BS 2122) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C SUPPORT FRAME ANGLE IS CRACKED INSIDE ACCESS 311AB IN COMPARTMENT ABOVE HORIZONTAL STABILIZER IN CEILING AREA BS 2133. REMOVED AND REPLACED SUPPORT FRAME ANGLE IAW DWG AJC7372 AND SRM 51-33-01 & 51-35-01.

Part: ANGLE — CRACKED (BS 2103) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, SUPPORT FRAME ANGLE IS CRACKED INSIDE ACCESS 311AB IN COMPARTMENT ABOVE HORIZONTAL STABAILIZER IN CEILING AREA BS 2103. REMOVED AND REPLACED SUPPORT FRAME ANGLE IAW DWG AJC7028 AND SRM 51-33-01.

Part: TRUNNION — CHAFED (LT MLG) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, LEFT MAIN LANDING GEAR FWD TRUNNION AFT LUG CHAFED. REPAIRED THE TRUNNION IAW EA 011-5740-01-A6559 REV IR, AND EO MD11-5740-62934-A.

Part: STANCHION — CORRODED (CARGO BAY) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, FWD CARGO BAY AFT BULKHEAD LT SUPPORT STANCHION CORRODED BS 6-70 LBL 57 Z=-94. REPAIRED THE STANCHION IAW EA 011-5310-01-A6556 REV. IR AND EO MD11-5310-63015-A. (MAJOR)

Part: SEAT TRACK — CORRODED (BS 475) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, RCB AREA SEAT TRACK CORRODED AT BS 475 LBL 8.5. REPLACED THE SEAT TRACK BETWEEN BS 440 - 605 IAW EA 011-5310-01-A6572 REV IR, AND EO MD11-5310-62968-A.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE:2C, RCB AREA FLOOR PANEL WSP0785-502 CORRODED STA 485 X=31. REMOVED AND REPLACED NOTED FLOOR PANEL PER SRM 53-20-50 REPAIR 1 AND AMM 53-21-10. (MINOR)

Part: FLOOR PANEL — CORRODED (BS 475-500) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 3C, RCB AREA FLOOR PANEL WSP0788-501 CORRODED STA. 475 - 500 X=36 TO X=47REPAIRED CORROSION PER VTSAA EA 011-5310-01-A6569 REV. IR AND UPS EO MD11-5310-62935-A (MINOR)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE:2C, RCB AREA SEAT TRACK CORRODED AT STA 487 X=-17. REMOVED AND REPLACED NOTED SEAT TRACK BETWEEN STA 439 - 515 PER SRM53-20-52 REPAIR 1, 51-31-01, AND DWG WSP0826. (MINOR)

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, RCB AREA FLOOR PANEL WSP0785-502 CORRODED BS 475 - 500 BL 0 TO RBL 8 CORRODED. THE FLOOR PANEL WAS REPAIRED IAW EA 011-5310-01-A6560 REV. IR, AND EO MD11-5310-62898-A.

Part: LONGERON — CORRODED (BS 1219-1401) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, LONGERON 28R CORRODED. REMOVED AND REPLACED THE LONGERON BETWEEN STA. 1219 - 1401 IAW SRM 51-33-01, AND 51-35-01. (MINOR)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE:2C, RCB AREA SEAT TRACK CORRODED STA 475 - 488 ALONG X=-27. REMOVED AND REPLACED NOTED SEAT TRACK BETWEEN STA 420 - 630 PER SRM 53-20-52 REPAIR 1, 51-31-01, AND DWG WSP0826 (MINOR)

Part: LONGERON SPLICE — CRACKED (BS 1531) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, CENTER CARGO BAY LONGERON 31L SPLICE FITTING IS CRACKED AT BS 1531. REMOVED AND REPLACED THE LONGERON SPLICE IAW DWG A5A7112 AND SRM 51-33-01.

Part: FLOOR PANEL — CORRODED (BS 475-500) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, RCB AREA FLOOR PANEL WSP0789-501 CORRODED BS 475 - 500 LBL 47 TO 75. REPAIRED THE FLOOR PANEL IAW EA 011-5310-01-A6569 REV. IR AND EO MD11-5310-62935-A. (MINOR)

Part: FLOOR PANEL — CORRODED (BS 475-500) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, RCB AREA FLOOR PANEL WSP0785-501 CORRODED BS 475 - 500, LBL 19 TO 27. REPAIRED THE FLOOR PANEL IAW EA 011-5310-01-A6562 REV. IR AND EO MD11-5310-62929-A.

Part: FLOOR PANEL — CORRODED (BS 482) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, RCB AREA FLOOR PANEL WSP0786-501 CORRODED BS 482, LBL 18. REMOVED AND REPLACED THE FLOOR PANEL IAW AMM 53-21-10-400, AND SRM 53-20-50 REPAIR 1.

Part: FLOOR PANEL — CORRODED (BS 485) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, RCB AREA FLOOR PANEL WSP0785-501 CORRODED BS 485 RBL 31. REMOVED AND REPLACED THE FLOOR PANEL IAW AMM 53-21-10-400 AND SRM 53-20-50 REPAIR 1.

Part: SEAT TRACK — CORRODED (BS 476-491) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, FORWARD FUSELAGE SEAT TRACK CORRODED, LBL 27.5 BETWEEN BS 476 - 491. REPAIRED IAW EA 011-5310-01-A6558 REV. IR AND EO MD11-5310-62885-A. (MINOR)

Part: FLOOR PANEL — CORRODED (BS 482) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE :2C, RCB AREA FLOOR PANEL WSP0785-501 CORRODED BS 482 LBL 4. REMOVED AND REPLACED THE FLOOR PANEL IAW AMM 53-21-10-400 AND SRM 53-20-50 REPAIR 1.

Part: SPAR — CORRODED (RT WING) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE:2C, RIGHT WING REAR SPAR LOWER CAP VERTICAL FLANGE CORRODED AT STA XORS 500. CORROSION REPAIRED PER EA 011-5710-01-A6568 REV IR AND EO MD11-5710-62926-A. (MINOR)

Part: INTERCOSTAL — CRACKED (RT MLG WW) · airframe 60,626 hrs · 15,339 cycles

RT MLG W/W INTERCOSTAL BELOW UPPER FWD ACCUMULATOR IS CRACKED. REPAIRED RT MLG W/W INTERCOSTAL BELOW UPPER FWD ACCUMULATOR IAW SRM 53-40-12 FIG 201 REPAIR 3.

Part: SPAR CAP — CORRODED (RT WING) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, RIGHT WING REAR SPAR UPPER CAP AFT FLANGE CORRODED BETWEEN XORS 774 - 826. REPAIRED THE SPAR CAP IAW EA 011-5710-01-A6567 REV. IR AND EO MD11-5710-62963-A.

Part: RIB — CHAFED (NR 1 SLAT) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, RT NR 1 SLAT INBOARD RIB CHAFED. REPAIRED THE RIB IAW EA 011-5754-01-A6578 REV. IR AND EO MD11-5750-63016-A. (MAJOR)

Part: LONGERON — CORRODED (BS 1256-1305) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, LONGERON 27R CORRODED BELOW R3 DOOR. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT LONGERON BETWEEN BS 1256 - 1305 IAW DWG AEA7127 AND SRM 51-33-01.

Part: DOUBLER — CRACKED (MLG WW) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, DOUBLER IS CRACKED INSIDE MLG WW AT LEFT WALL FWD PUSHROD FEED THROUGH. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-33-01.

Part: LUG — CHAFED (LE SLAT) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE:2C, RIGHT WING NUMBER 3 SLAT, NUMBER 6 TRACK LOWER LUG CHAFED AT XOS 429. REPAIRED NOTED CHAFE DAMAGE PER EA 011-5754-01-A6557 REV IR AND UPS EO MD11-5750-62892-A (MINOR)

Part: SPAR — CORRODED (RT WING) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE:2C, RIGHT WING REAR SPAR LOWER CAP VERTICAL FLANGE CORRODED AT STA XORS 760. REPAIRED NOTED CORROSION PER EA 011-5710-01-A6563 REV IR AND EO MD11-5710-62927-A (MINOR).

Part: TRUNNION — CRACKED (NLG) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, LEFT NLG TRUNNION FITTING IS CRACKED. REPAIRED THE TRUNNION FITTING IAW SRM 53-10-14 REPAIR 2 FIG. 202. (MAJOR)

Part: INTERCOSTAL — CRACKED (LT MLG WW) · airframe 60,626 hrs · 15,339 cycles

LT MLG W/W INTERCOSTAL BELOW UPPER FWD ACCUMULATOR IS CRACKED. REPAIRED LT MLG W/W INTERCOSTAL BELOW UPPER FWD ACCUMULATOR IAW SRM 53-40-12 FIG 201 REPAIR 3. (MAJOR)

Part: SKIN — DELAMINATED (TE FLAP VANE) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE:2C, RT OB FLAP VANE LARGE AREA OF DELAM ON LOWER SKIN. REMOVED AND REPLACED RT OB FLAP VANE PER SRM 27-50-32-400.

Part: DOUBLER — CRACKED (LT WING) · airframe 60,626 hrs · 15,339 cycles

LT WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN XOS 753 - 759. REPAIRED LT WING FIXED L/E BEADED DOUBLER BETWEEN XOS 753 - 759 IAW 57-40-02 REPAIR 15 FIG 203. (MAJOR)

Part: SKIN — CHAFED (LT WING) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE:2C, LT WING FIXED L/E LOWER EXTERIOR SKIN CHAFE DAMAGE XIS164. REPAIRED L/E CHAFE DAMAGE PER EA 011-5730-01-A6561 REV IR AND EO MD11-5730-62882-A. (MINOR)

Part: STRAP — CRACKED (LT WING) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, LEFT WING FIXED L/E SPLICE STRAP IS CRACKED AT XOS 789. REMOVED AND REPLACED THE SPLICE STRAP IAW DWG ARB3954 AND SRM 51-33-01.

Part: DOUBLER — CRACKED (LT WING) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, LEFT WING BEADED DOUBLER AT XOS. 629-633 IS CRACKED. REPAIRED IAW SRM 57-40-02 REPAIR 15 FIG. 203. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, LEFT WING BEADED DOUBLER AT XOS. 636-643 IS CRACKED. REPAIRED IAW SRM 57-40-02 REPAIR 15 FIG. 202. (MAJOR)

Part: DOUBLER — DAMAGED (LT WING) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, LT WING INNER BEADED DOUBLER AT XOS 734 - 740 DAMAGED. REPAIRED IAW SRM 57-40-02 REPAIR 15 FIG 203. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, LEFT WING BEADED DOUBLER AT XOS. 610-616 IS CRACKED. REPAIRED IAW SRM 57-40-02 REPAIR 15 FIG. 202. (MAJOR)

Part: DOUBLER — DAMAGED (LT WING) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, LEFT WING INNER BEADED DOUBLER AT XOS 698 - 703 DAMAGED. REPAIRED IAW SRM 57-40-02 REPAIR 15 FIG 203. (MAJOR)

Part: DOUBLER — CRACKED (LT WING) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE:2C, LT WING INNER BEADED DOUBLER AT STA XOS 692-698 IS CRACKED. REPAIRED CRACKED LT WING BEADED DOUBLER AT STA XOS 692-698 IAW SRM 57-40-02 REPAIR 15 FIG 202. (MAJOR)

Part: DOUBLER — DAMAGED (LT WING) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, LEFT WING INNER BEADED DOUBLER REPAIR AT XOS 621 - 625 DAMAGED. REPAIRED IAW SRM 57-40-02 REPAIR 15 FIG. 203. (MAJOR)

Part: DOUBLER — DAMAGED (LT WING) · airframe 60,626 hrs · 15,339 cycles

INSPECTION TYPE: 2C, LEFT WING INNER BEADED DOUBLER REPAIR AT XOS 679 - 685 DAMAGED. REPAIRED IAW SRM 57-40-02 REPAIR 15 FIG. 203. (MAJOR)

Part: MOUNT — WORN (ENGINE)

DURING ROUTINE MAINTENANCE AND INSPECTION, THE GUIDE AND SHEAR PIN HOLES OF THE SUBJECT AFT ENGINE MOUNT WERE FOUND TO BE ELONGATED BEYOND SERVICEABLE LIMITS IAW CMM 221-0260-501. REPAIRED IAW ERA.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 59,717 hrs · 15,130 cycles

BULK PIT DOOR DEFLECTED AT LOWER CORNER PAN DAMAGED OUTER SKIN REPAIRED IAW EO MD11-5230-60528-B.

Part: LIFE VEST — OPEN (PAX SEAT) · airframe 59,254 hrs · 15,021 cycles

FOUND PASSENGER SEAT LIFE VEST SEAL BROKEN. R&R THE LIFE VEST IAW AMM 25-64-01-2 REV 85.03.

Part: TIRE — FAILED (NR 2 MLG) · airframe 58,939 hrs · 14,953 cycles

EMERGENCY DECLARED, RECEIVED A LEVEL 2 ALERT FOR TIRE FAILURE. CONTINUED, FOUND TIRE BELOW 50 PSI. REPLACED NR2 MLG WHEEL ASSY IAW MM 32-41-01.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 58,521 hrs · 14,857 cycles

EMERGENCY LIGHTING SYS TEST BATTERY LOWER & REPLACED EMERGENCY LIGHTING BATTERY IAW AMM 33-51-01-401-00-802.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 58,218 hrs · 14,771 cycles

R1 DOOR ASSIST BOTTLE LOW PRESSURE SERVICED R1 DOOR BOTTLE PRESSURE IAW AMM 12-25-04. OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,148 hrs · 14,754 cycles

UPON BLOCK AT THE R1 DOOR, THE DISARMED LIGHTS INOPERATIVE. REPLACED THE LAMP AT THE R1 DOOR THE DISARM LIGHTS AND CHECKED GOOD IAW AMM 33-50-00.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,222 hrs · 14,499 cycles

INSPECTION TYPE: PS1, EMERGENCY LIGHT POWER LOW 1. . R & R EMERGENCY LIGHT POWER SUPPLY BATTERY. OPS CHECKED OK IAW MM 33-51-01-401 AND 33-51-01-501.

Part: ATTACH FITTING — CRACKED (RT WING) · airframe 56,915 hrs · 14,408 cycles

INSPECTION TYPE:3C, RT LOWER WINGLET AFT ATTACHED FITTING CRACKED. REPLACES 2015051989235. REMOVED FWD AND AFT ATTACHED FITTINGS, INSTALLED KIT SB11570063-5 IAW EO MD11-5720-27680-C, APPROXIMATELY E.

Part: HINGE — CORRODED (RT WING TE FLAP) · airframe 56,915 hrs · 14,408 cycles

INSPECTION TYPE:3C, RT OTBD FLAP INBD HINGE FITTING CORRODED. REPAIRED HINGE FITTING IAW VTSAA EA 011-5753-01-A5817, REV IR AND EO MD11-5710-57513-A.

Part: SKIN — CORRODED (RT WING TE FLAP) · airframe 56,915 hrs · 14,408 cycles

INSPECTION TYPE:3C, RT INBD FLAP HAS CORROSION ON UPPER SKIN AT RUBSTRIP FS XIFH 133.900 TO XIFH 140.600. REPAIRED THE FLAP UPPER SKIN IAW EA 011-5753-01-A5812, REV I/R AND EO MD11-5750-57528-A.

Part: SHEAR TIE — CRACKED (BS 2140) · airframe 56,915 hrs · 14,408 cycles

INSPECTION TYPE:3C, SUPPORT FRAME, SHEAR CLIP, CRACKED IN 316 COMPARTMENT CEILING, FS 2140. R & R SHEAR CLIP IAW SRM 51-33-01.

Part: SKIN — CHAFED (RT WING) · airframe 56,915 hrs · 14,408 cycles

INSPECTION TYPE: 3C, L/E WING SKIN CHAFED AT XIS 361.145 INBD OF PYLON. REPAIRED IAW EA 011-5710-01-A5818, REV I/R AND EO MD11-5730-57543-A.

Part: DOUBLER — CRACKED (RT WING) · airframe 56,915 hrs · 14,408 cycles

INSPECTION TYPE:3C, RT WING L/E INNER BEADED DOUBLER TEMP REPAIR CRACKED NEAR STA XOS 1005, ACTUAL 995, MINOR. REPAIRED RT WING BEADED DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 203, XOS 993-998.

Part: DOUBLER — CRACKED (RT WING) · airframe 56,915 hrs · 14,408 cycles

INSPECTION TYPE:3C, RT WING L/E INNER BEADED DOUBLER CRACKED AT XOS 753. REPAIRED RT WING BEADED DOUBLER XOS 746-753 IAW SRM 57-40-02, REPAIR 15, FIG 206.

Part: DOUBLER — CRACKED (RT WING) · airframe 56,915 hrs · 14,408 cycles

INSPECTION TYPE:3C, RT WING L/E INNER BEADED DOUBLER CRACKED AT XOS728. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 206.

Part: RIB — CRACKED (RT WING) · airframe 56,915 hrs · 14,408 cycles

INSPECTION TYPE:3C, RT WING L/E INTERNAL RIB CRACKED IN RADIUS, STA 855. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT RIB IAW DWG ARB2922 AND SRM 51-31-01.

Part: DOUBLER — CRACKED (RT WING) · airframe 56,915 hrs · 14,408 cycles

INSPECTION TYPE:3C, RIGHT WING L/E INNNER BEADED DOUBLER CRACKED, XOS700. REPAIRED RT WING BEADED DOUBLER XOS 698-703 IAW SRM 57-40-02, REPAIR 15 FIG 206, MAJOR.

Part: SHEAR TIE — CRACKED (BS 2122) · airframe 56,915 hrs · 14,408 cycles

INSPECTION TYPE:3C, SHEAR CLIP CRACKED IN EMPENNAGE INTERIOR COMPARTMENT ABOVE HORIZONTAL STABILIZER CENTER BOX, FS 2122, LT SIDE. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SHEAR CLIP IAW DWG. AJC7372 AND SRM 51-33-01, MINOR.

Part: BEAM — CRACKED (LT WING) · airframe 56,915 hrs · 14,408 cycles

INSPECTION TYPE: 3C, LEFT WING T/E BEAM LOWER CAP CRACKED AT STA XW=225 ACCOMPLISHED PERMANENT REPAIR ON LT WING T/E BEAM LOWER CAP AT XW=225 IAW EA 011-5710-01-A5813 REV A AND EO MD11-5720-57409-B.

Part: STRUCTURE — CORRODED (LT WING) · airframe 56,915 hrs · 14,408 cycles

INSPECTION TYPE:3C, LT WING UPPER SPOILER SILL HAS CORROSION AT FS XOS 509. ACCOMPLISHED REPAIR IAW SRM 57-50-02, REPAIR 10, MAJOR.

Part: SPAR CAP — CORRODED (LT WING) · airframe 56,915 hrs · 14,408 cycles

INSPECTION TYPE: 3C, LT WING REAR SPAR CAP AFT FLANGE CORRODED XORS 780-826. REPAIRED CORROSION IAW FS, SA, EA 011-5700-01-A5816, REV IR AND EO MD11-5710-57487-A.

Part: BEAM — CRACKED (LT WING) · airframe 56,915 hrs · 14,408 cycles

INSPECTION TYPE: 3C, LEFT WING INBD TE LOWER BEAM IS CRACKED AT XW-213.97. ACCOMPLISHED REPAIR IAW EA011-5710-01-A5313, REV I/R AND EO MD11-5720-57409-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 56,915 hrs · 14,408 cycles

INSPECTION TYPE:3C, LEFT WING L/E INNER BEADED DOUBLER CRACKED XOS 665. REPAIRED LT WING BEADED DOUBLER XOS 661-667 IAW SRM 57-40-02, REPAIR 15, FIG 206.

Part: FLOOR PANEL — PUNCTURED (MAIN CABIN) · airframe 56,915 hrs · 14,408 cycles

INSPECTION TYPE: 3C, MAIN CABIN FLOOR PANEL PUNCTURED AT L4 DOOR, REPAIRED FLOOR PANEL IAW SRM 53-00-50, REPAIR 2, PARA 4.A FIG 206.

Part: CURTAIN — DAMAGED (MAIN DECK) · airframe 56,879 hrs · 14,393 cycles

SMOKE CURTAIN HAS OPENING AT TOP. RESERVED MCD FORWARD SMOKE CURTAIN IAW AMM 25 59 15.

Part: SWITCH — LOOSE (EMERGENCY LIGHTS)

EMERGENCY LIGHT SWITCH LOOSE IN PANEL. SECURED SWITCH.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 54,986 hrs · 13,895 cycles

DURING A 1CINSPECTION , MAIN CABIN FLOOR PANEL 271DF DAMAGED. FABRICATED REPLACEMENT FLOOR PANEL IAW EO 5320-27386-C.

Part: STRINGER — CRACKED (LT WING) · airframe 54,986 hrs · 13,895 cycles

DURING A 1C INSPECTION, LT WING STRINGER 15 CRACKED NEAR XORS 433. REPAIRED STRINGER XORS 433-455 IAW SRM 57-20-03, REPAIR 3, FIG 201, EA 011-5710-01-A5305 REV IR AND EO 5710-54418-A.

Part: STRINGER — CRACKED (RT WING) · airframe 54,986 hrs · 13,895 cycles

DURING A 1C INSPECTION, RT WING STRINGER 22 CRACKED NEAR XORS 163. REPAIRED STRINGER XORS 163-197 IAW EA 011-5710-01-A5303, REV IR AND EO 5710-54416-A.

Part: STRINGER — CRACKED (STRINGER) · airframe 54,986 hrs · 11,249 cycles

DURING 1C INSPECTION, RT WING STRINGER 44 CRACKED . REPAIRED RT WING STRINGER XORS 298.500 IAW EA 011-5710-01-A5316 IR, EO 5710-5 4443-A AND 8100-9.

Part: STRINGER — CRACKED (RT WING) · airframe 54,986 hrs · 13,895 cycles

DURING 1C INSPECTION, RT WING STRINGER 15 CRACKED NEAR XORS 433. REPAIRED STRINGER XORS 433-455 IAW SRM 57-20-03, REPAIR 3, FIG 201, EA 011-5710-01-A5306, REV IR AND EO 5710-54419-A.

Part: STRINGER — CRACKED (RT WING) · airframe 54,986 hrs · 13,895 cycles

DURING 1C INSPECTION, RT WING LOWER STRINGER 35 CRACKED AT XORS 316.9. REPAIRED STRINGER IAW EA 011-5710-01-A5302, REV I/R AND EO MD11-5710-54417-A.

Part: STRINGER — CRACKED (LT WING) · airframe 54,986 hrs · 13,895 cycles

DURING 1C INSPECTION, LEFT WING LOWER STRINGER 32 CRACKED AT XORS 917.2. REPAIRED STRINGER IAW EA 011-5710-01-A5308, REV I/R AND EO MD11-5710- 54413-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 54,986 hrs · 11,249 cycles

DURING 1C INSPECTION, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 624. REPAIRED DOUBLER BETWEEN XOS 621-625 IAW SRM 57-40-02. REPAIR 15 FIG 206.

Part: DOUBLER — CRACKED (LT WING) · airframe 54,986 hrs · 13,895 cycles

INSPECTION TYPE:1C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR STA XOS701. INSTALLED REPAIR TO LT WING INNER BEADED DOUBLER BETWEEN XOS 698-703 IAW SRM 57-40-02. REPAIR 15, FIG 206.

Part: DOUBLER — CRACKED (LT WING) · airframe 57,986 hrs · 13,895 cycles

INSPECTION TYPE:1C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 631. REPAIRED LT WING INNER BEADED DOUBLER BETWEEN XOS629-633 IAW SRM 57-40-02, REPAIR 15 FIG 206.

Part: DOUBLER — CRACKED (LT WING) · airframe 57,986 hrs · 13,895 cycles

INSPECTION TYPE:1C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 640. REPAIRED LT WING INNER BEADED DOUBLER BETWEEN XOS 636-643 IAW SRM 57-40-02, REPAIR 15 FIG 206.

Part: DOUBLER — CRACKED (LT WING) · airframe 54,986 hrs · 11,249 cycles

DURING A 1C INSPECTION, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 684. REPAIRED DOUBLER BETWEEN XOS 679-685 IAW SRM 57-40-02, REPAIR 15, FIG. 206.

Part: DOUBLER — CRACKED (LT WING) · airframe 54,986 hrs · 13,895 cycles

DURING A 1C INSPECTION, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 733. REPAIRED DOUBLER BETWEEN XOS 728-734 IAW SRM 57-40-02, REPAIR 15 FIG 203.

Part: DOUBLER — CRACKED (LT WING) · airframe 54,986 hrs · 13,895 cycles

INSPECTION TYPE:1C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 738. REPAIRED LT WING INNER BEADED DOUBLER BETWEEN XOS 734-740 IAW SRM 57-40-02. REPAIR 15 FIG 206.

Part: DOUBLER — CRACKED (LT WING) · airframe 54,986 hrs · 13,895 cycles

INSPECTION TYPE:1C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 646. REPAIRED LT WING INNER BEADED DOUBLER BETWEEN XOS 643-648 IAW SRM 57-40-02, REPAIR 15, FIG 203.

Part: DOUBLER — CRACKED (LT WING) · airframe 54,986 hrs · 11,249 cycles

DURING A 1C INSPECTION, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEARS XOS 613 REPAIRED DOUBLER BETWEEN XOS 610-616 IAW SRM 57-40-02, REPAIR 15 FIG. 206.

Part: DOUBLER — CRACKED (LT WING) · airframe 57,986 hrs · 13,895 cycles

INSPECTION TYPE:1C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 669. REPAIRED LT WING INNER BEADED DOUBLER BETWEEN XOS667-673 IAW SRM 57-40-02, REPAIR 15 FIG. 206.

Part: SPAR CAP — CORRODED (LT WING) · airframe 54,986 hrs · 13,895 cycles

DURING A 1C INSPECTION, LT WING T/E UPPER FALSE SPAR CAP CORRODED, XW170- XW233. PERFORMED SPLICE REPAIR IAW EA 011-5720-01-A5300, REV IR AND EO 5720-54374-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 57,986 hrs · 13,895 cycles

INSPECTION TYPE:1C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 695. REPAIRED LT WING INNER BEADED DOUBLER BETWEEN XOS692-698 IAW SRM 57-40-02. REPAIR 15, FIG 206.

Part: DOUBLER — CRACKED (RT WING) · airframe 54,986 hrs · 11,249 cycles

DURING A 1C INSPECTION, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XORS 488 - 586. REPAIRED DOUBLER BETWEEN XOS 584-589 IAW SRM 57-40-02, REPAIR 15 FIG 206.

Part: DOUBLER — CRACKED (RT WING) · airframe 54,986 hrs · 11,249 cycles

DURING A 1C INSPECTION, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XORS 540 - 644. REPAIRED DOUBLER BETWEEN XOS 643-648 IAW SRM 57-40-02. REPAIR 15, FIG 206.

Part: FUEL SYS — MALFUNCTIONED (NR 1 TANK)

RECEIVED LEVEL 2 TANK WING OVERFILL WARNING INFLIGHT. SINCE NR 3 TANK QTY WAS INSP, HAD NO WAY OF VERIFYING IF FUEL WAS VENTING OVERBOARD. DECLARED EMERGENCY AND RETURNED TO DEPARTURE. FOUND 6 GALLONS FUEL IN RT VENT BOX. DRAINED OK. TROUBLESHOT IAW FIM 28-14-2-00, NO FAULT FOUND. REPLACED TANK-1 FILL VALVE CONTROLLER AS A PRECAUTION IAW AMM 28-21-02. ACFT OK FOR SERVICE.

Part: SKIN — DENTED (LT WING TE FLAP)

LT INBD FLAP DENT ON UPPER SURFACE 30" FWD OF T/E DAMAGED STA XIFH 188. REPAIRED REF EO MD11-5750-50011-A.

Part: SEAT TRACK — CORRODED (BS 475 RBL 61) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE: 4C, CABIN COURIER AREA GALLEY AFT MOUNT FITTING SEAT TRACK CORRODED. CUT OUT DAMAGE SECTION OF SEAT TRACK AT STA 475 AND RBL 61 AND INSTALLED SEAT TRACK PLUG REF SRM 53-00-52, REPAIR 4, FIG 201.

Part: SKIN — CORRODED (CENTER WING) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE:4C, CENTER WING UPPER SKIN CORRODED ALONG S10 BETWEEN XCW-101 & XCW-118. REPAIRED CORRODED SKIN IAW STASA EA 011-5730-01-A4428 REV IR AND EO MD11-5730-49658-A.

Part: SKIN — CORRODED (CENTER WING) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE:4C, CENTER WING UPPER SKIN CORRODED ALONG S15 BETWEEN STA XCW-81 & XCW-118. REPAIRED CORRODED CENTER WING UPPER SKIN IAW STASA EA 011-5730-01- A4427 REV.IR AND EO MD11-5730-49659-A.

Part: SKIN — CORRODED (CENTER WING) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE:4C, CENTER WING UPPER SKIN CORRODED ALONG S15 BETWEEN XCW17 AND XCW-17. REPAIRED CORRODED WING SKIN IAW STASA EA 011-5730-01-A4427, REV IR AND EO MD11-5730-49659.

Part: FITTING — CRACKED (FUEL CELL) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE: 4C, FITTING CRACKED ON CENTER, LOWER AUXILARY TANK AT 3:00 POS RT SIDE 4TH FRAME FROM REAR. FABRICATED AND REPLACED FITTING IAW SRM 51-33-01 PG 45, PARA 9 AND PG 30, PARA 8.

Part: STRINGER — CRACKED (RT WING) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE:4C, RT WING NR 13 STRINGER CRACKED BETWEEN XORS 562-593. REPAIRED NR13 RT WING STRINGER BETWEEN XORS 562-593 REF SRM 57-00- 03, REPAIR 5, FIG 201.

Part: WEB — CRACKED (R3 DOOR) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE:4C, R-3 DOOR FORWARD DOOR JAMB LIGHTNING HOLE CRACKED. REPAIRED R-3 DOOR FWD DOOR JAMB LIGHTNING HOLE REF SRM 53-40-15, REPAIR 3, FIG 201.

Part: STRINGER — CRACKED (RT WING) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE: 4C, RT WING NR 14 STRINGER IS CRACKED BETWEEN XORS 506-538. REPAIRED NR 14 RT WING STRINGER BETWEEN XORS 506-538 REF SRM 57-00- 03, REPAIR 5, FIG 201.

Part: LONGERON SPLICE — CRACKED (BS 1531 L9L) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE:4C, LONGERON 9L, SPLICE FITTING IS CRACKED AT STA 1531/5-123. REPLACED SPLICE FITTING LONGERON 9L AT STA 1531/5-123 REF SRM 51-33-01 PARA. 8, PAGE 30 AND SRM 51-31-01 PAGE 36, TABLE 13.

Part: STRINGER — CRACKED (RT WING) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE:4C, RT WING STRINGER NR 12 IS CRACKED BETWEEN XORS 623-653. REPAIRED NR 12 RT WING STRINGER BETWEEN XORS 623-653 REF SRM 57-00- 03, REPAIR 5, FIG 202.

Part: LONGERON SPLICE — CRACKED (BS 1531) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE:4C, LONGERON 6LT SPLICE FITTING CRACKED AT STA 1531/5-123. R & R SPLICE FITTING IAW SRM 51-31-01.

Part: STRINGER — CRACKED (LT WING) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE:4C, LT WING NR 11 STRINGER IS CRACKED BETWEEN XORS 683-714. REPAIRED LT WING NR 11 STRINGER BETWEEN XORS 683-714 REF SRM 57-00- 03, REPAIR 5, FIG 202.

Part: STRINGER — CRACKED (LT WING) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE: 4C LT WING STRINGER NR 9 CRACKED BETWEEN XORS 799-827. REPAIRED LT WING NR 9 STRINGER BETWEEN XORS799-827 REF SRM 57-00-03, REPAIR 5, FIG 202.

Part: STRINGER — CRACKED (RT WING) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE:4C, RT WING STRINGER NR 10 CRACKED BETWEEN XORS 738-772. REPAIRED NR 10 RT WING STRINGER BETWEEN XORS 738-772 REF SRM 57-00-0 3, REPAIR 5, FIG 202.

Part: PANEL — CRACKED (INLET) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE:4C, UPPER FWD CORNER OF INTERCOSTAL CRACKED AT 11:00 POSITION ON NR 2 ENGINE INLET DUCT BETWEEN VERT STAB LT REAR CTR SPAR AND REAR SPAR LOWER PANEL AT 363PL. REPAIRED UPPER FWD CORNER OF INTERCOSTAL AT 11:00 POSITION ON NR 2 ENGINE INLET DUCT BETWEEN VERT STAB LT REAR CTR SPAR AND REAR SPAR LOWER PANEL AT 363PL, REF STA SA EA 011-5530-01-A4398 REV I/R, EO MD11-5530-49694-A AND 8100-9.

Part: STRINGER — CRACKED (LT WING) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE:4C, LT WING NR 10 STRINGER IS CRACKED BETWEEN XORS 738-772. REPAIRED LT WING NR 10 STRINGER BETWEEN XORS 738-772 REF SRM 57-00- 03, REPAIR 5, FIG 202.

Part: STRINGER — CRACKED (RT WING) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE: 4C, RT WING NR 9 STRINGER CRACKED BETWEEN XORS 799-827. REPAIRED NR 9 RT WING STRINGER BETWEEN XORS 799-827 REF SRM 57-00-0 3, REPAIR 5, FIG 201.

Part: STRINGER — CRACKED (RT WING) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE:4C, RT WING NR 11 STRINGER CRACKED BETWEEN XORS 683-714. REPAIRED NR 11 RT WING STRINGER BETWEEN XORS 683-714 REF SRM 57-00- 03, REPAIR 5, FIG 202.

Part: BEAM — CORRODED (LT WING) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE:4C, LT WING TEE BEAM ASSY LWR CAP BETWEEN XW311 AND XW373 CORRODED. REPAIRED TEE BEAM ASSY LWR CAP BETWEEN XW311 AND XW373 REF STASA EA 011-5720-01-A4405 REV I/R, EO MD11-5720-49716-A AND 8110-3.

Part: BEAM — CORRODED (RT WING) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE:4C, RT WING TEE BEAM ASSY LOWER CAP BETWEEN XW311 AND XW373 CORRODED AT FASTENER HOLES. REPAIRED RT WING TEE BEAM ASSY LOWER CAP BETWEEN XW311 AND XW373 REF STASA EA 011-5720-01-A4404 REV I/R, EO MD11-5720-49715-A AND 8110-3.

Part: SKIN — CRACKED (LT WING) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE: 4C, LT WING FIXED L/E SKIN CRACKED AT NR 14 SLAT TRACK CUT OUT. REPAIRED IAW SRM 57-40-02, REPAIR 7, FIG 201.

Part: SKIN — CORRODED (LT WING) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE:4C, AREA OF CORROSION ON LT WING UPPER SKIN AT XORS315.9, STRINGER 15 AREA EXCEEDED ALLOWABLE SRM LIMITS AFTER CORROSION REMOVAL. REPAIRED LT WING UPPER SKIN CORROSION STA XORS 315.9 ABOVE S15 IAW STASA EA 011-5730-01-A4431, REV IR AND EO MD11-5730-49676-A.

Part: FORMER — CRACKED (LT WING) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE: 4C, LT WING FIXED L/E FORMER AT XFS 544.5 IS CRACKED OTBD OF PANEL 518FB. REPLACED LT WING FIXED L/E FORMER AT XFS 544.5 AT AFT END OF PANEL 518F B REF SRM 51-35-00 AND SRM 51-33-00.

Part: ANGLE — CRACKED (RT WING) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE:4C RT WING FIXED L/E SKIN SPLICE ANGLE IS CRACKED AT XFS 587. REMOVED, FABRICATED AND INSTALLED RT WING L/E SKIN SPLICE ANGLE AT XFS 587 REF 51-33-01 PG 4, 5, 30 AND 31, SRM 51-21-01, PG 41.

Part: STRINGER — CRACKED (RT WING) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE: 4C, RT WING FIXED L/E STRINGER/PANEL LANDING IS CRACKED AT XFS 996. REPAIRED RT WING FIXED L/E STRINGER/PANEL LANDING AT XFS 996 REF SRM 57-40-03, REPAIR 1, FIG 201.

Part: SKIN — CRACKED (RT WING) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE:4C, RT WING FIXED L/E SKIN IS CRACKED AT INBD FWD CORNER OF PANEL 619CB CUT OUT. REPAIRED RT WING FIXED L/E SKIN AT INBD FWD CORNER OF PANEL 619CB CUT OUT REF SRM 57-40-02, REPAIR 7, FIG 202.

Part: SKIN — CRACKED (RT WING) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE:4C, RT WING FIXED L/E SKIN SPLICE STRAP IS CRACKED AT XFS 669. REPLACED RT WING FIXED L/E SKIN SPLICE STRAP AT XFS 669 SRM 51-31-01, PARA 3 AND PAGE 1 AND 36, SRM 51-33-01 PARA 8, PAGE 30.

Part: SKIN — CRACKED (NR 8 SLAT) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE: 4C, RT WING FIXED L/E END CAP OTBD OF NR 8 SLAT IS CHAFED. REPAIRED RT WING FIXED L/E SKIN BETWEEN XOS 1185 AND XORS 1093 CANTED, 8.9' FWD OF FRONT SPAR AND 2.3' FROM INBD EDGE REF STASA EA 011-5730-0 1-A4419 REV I/R, EO MD11-5730-49687-A AND 8100-9.

Part: SKIN — CRACKED (RT WING) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE:4C, RT WING FIXED L/E SKIN CRACKED AT NR 14 SLAT TRACK CUT OUT. REPAIRED RT WING FIXED L/E SKIN AT NR 14 SLAT TRACK CUT OUT REF SRM 57-40-02, REPAIR 7, FIG 201.

Part: FORMER — CRACKED (RT WING) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE:4C RT WING FIXED L/E FORMER CRACKED NEAR XFS994. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FORMER IN RT WING L/E AT XFS994 IAW SRM51-33-01 AND DWG ARB1164.

Part: DOUBLER — CORRODED (RT WING) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE: 4C, RT WING FIXED L/E LOWER SACRIFICIAL DOUBLER AT XFS925 IS CORRODED. REPAIRED RT WING FIXED L/E LOWER SACRIFICIAL DOUBLER AT XFS925 REF STA SA EA 011-5710-01-A4423 REV I/R, EO MD11-5710-49721-A AND 8100-9.

Part: RIB — CRACKED (RT WING) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE:4C, RT WING FIXED L/E NR 16 SLAT TRACK INBD RIB AT XFS 1004 IS CRACKED IN 2 PLACES. REPLACED RIB IN RT WING FIXED L/E NR 16 SLAT TRACK AT XFS 1004 REF SRM 51-35-01, PG 38 AND SRM 51-33-01, PG 45.

Part: BULKHEAD WEB — DENTED (BS 2007) · airframe 52,250 hrs · 13,185 cycles

INSPECTION TYPE: 4C, BS 2007 AFT PRESSURE BULKHEAD DENTED JUST OTBD OF RBL 60 STIFFENER. REPAIRED APB DENT IAW STASA EA 011-5310-01-A4426 REV IR AND EO MD11-5310-49726-A.

Part: CHANNEL — CRACKED (FUEL TANK) · airframe 49,650 hrs · 12,452 cycles

INSPECTION TYPE:C3, FOUND CRACKED GANG CHANNEL AT THE NR 3 TANK FUEL ACCESS PANEL 639GB, OPENING. REPAIRED CRACKED GANG CHANNEL IAW A.011-5720-A3505, REV IR, AND EO MD11-5720-44640-A.

Part: SPAR — CORRODED (RT WING) · airframe 49,650 hrs · 12,452 cycles

3C CHECK, RT WING UPPER T/E FILLER STRIP BULGING BETWEEN XORS 548-559. REPAIRED CORROSION ON RT WING REAR SPAR UPPER AFT FLANGE BEWTEEN XORS 550-562 IAW STA SA EA 011-5710-01-A3495 & EO MD11-5710-44571-A.

Part: SPAR CAP — CORRODED (RT WING) · airframe 49,650 hrs · 12,452 cycles

INSPECTION TYPE:3C, INTERGRANULAR CORROSION ON RT WING AFT SPAR T-CAP STA XORS580. REPAIRED CORROSION ON RT WING REAR SPAR UPPER CAP VERTICAL LEG BETWEEN XORS 570-590 IAW STA SA EA 011-5710-01-A3490 REV IR & EO MD11-5710-44570-A.

Part: SPAR — CORRODED (RT WING) · airframe 49,650 hrs · 12,452 cycles

INSPECTION TYPE:3C RT WING UPPER T/E FILLER STRIP BULGING BETWEEN XORS646-657. REPAIRED CORROSION ON UPPER AFT FLANGE OF RT WING REAR SPAR BETWEEN XORS 634-657 IAW STA SA EA 011-5710-01-A3497 REV IR AND EO MD11- 5710-44585-A.

Part: DOUBLER — CRACKED (RT WING) · airframe 49,650 hrs · 12,452 cycles

INSPECTION TYPE:3C, RT WING L/E COMPT BEADED DOUBLER CRACKED AT XOS613. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS610-616 IAW SRM 57-40-02, REPAIR 9, FIG 203.

Part: SKIN — DENTED (BS 899 L40-41R) · airframe 49,650 hrs · 12,452 cycles

INSPECTION TYPE:3C, FWD CARGO DOOR FWD JAMB STA 899 DENTED ON EDGE OF SKIN BETWEEN L40-41R. REPAIRED FWD CARGO DOOR FWD JAMB STA 899 BETWEEN L40R/L41R IAW SRM 53-00-15, REPAIR 8.

Part: WIRE HARNESS — SHORTED (L1 DOOR SLIDE) · airframe 49,650 hrs · 12,452 cycles

INSPECTION TYPE:3C L1 DOOR ESCAPE SLIDE REMOTE PRESSURE INDICATOR LIGHT WIRING HARNESS SHORTED, WARNING LIGHT ALWAYS ON, BOTTLE PRESSURE GOOD. PROCURED AND INSTALLED REPLACEMENT L1 DOOR ESCAPE SLIDE ASSY.

Part: ANGLE — CORRODED · airframe 49,650 hrs · 12,452 cycles

INSPECTION TYPE:3C, IN COMPT THRU DOOR 311AB LT UPPER AREA NEAR CROWN AT APB 2ND FROM LT STIFFENER OTBD ANGLE EXFOLIATED AT LOWER END. R & R STIFFENER CLIP (ANGLE) IAW STA SA EA 011-5300-01-A3504, REV IR, EO MD11-5310-44638-A, SRM 51-31-01.

Part: ATTACH FITTING — CORRODED (NR 2 NACELLE) · airframe 49,650 hrs · 12,452 cycles

INSPECTION TYPE:3C, NR 2 ENGINE SUPPORT LINK ATTACH FITTING AT 6 O`CLOCK ON FAN CASE IS EXFOLIATED AT Y STA 2198. ACCOMPLISHED EO MD11-7110-44569-B.

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 49,650 hrs · 12,452 cycles

INSPECTION TYPE:3C, IN FWD AFT FUSELAGE THROUGH ACCESS 311AB, LT SIDE LOWER FUSELAGE LONGERON SPLICE IS CRACKED AT RADIUS, AT 4TH LONGERON FROM ENTRY ACCOMPLISHED STA-SA EA 0115310-01-A3485 I/R AND UPS EO MD11-5310-44562-A.

Part: DOOR FRAME — DAMAGED (BS 1781 L41R) · airframe 49,650 hrs · 12,452 cycles

INSPECTION TYPE:3C, CTR CARGO DOOR AFT JAMB GOUGED & CRACKED AT EXTERNAL REPAIR DOUBLER ADJACENT TO L41-42R STA 1781. DVI AND NDT VERIFIED NO CRACKS PRESENT AT DAMAGE SITE. REPAIRED CTR CARGO DOOR AFT JAMB, GOUGE DAMAGE STA 1781 IAW STA SA EA 011-5330-01- A3483 REV IR AND EO MD11-5330-44523-A.

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR)

R1 DOOR SLIDE DEPLOYED. INSTALLED SERVICEABLE EMERGENCY ESCAPE SLIDE IAW AMM 25-61-15-4. OPS CHECK NORMAL. THIS CLEARS M454747.

Part: ENGINE — POWER LOSS (NR 2)

REJECTED TAKEOFF AT 145 KTS FOR NR 2 ENGINE LOSS OF POWER. R & R NR2 ENG IAW TC-9103 & IAW AMM 71-00-03-42. ENG RUN TEST OK.

Part: VANE — DAMAGED (LT WING TE FLAP) · airframe 46,308 hrs · 11,793 cycles

INSPECTION TYPE:2C, LT WING INBD FLAP VANE T/E HAS A CHIP BETWEEN MIDDLE AND OTBD TRACKS. PERFORMED REPAIR IAW STA SA EA 011-5750-01-A2575, REV I/R AND AUTHORIZED BY EO MD11-5750-3900-A.

Part: VANE — DAMAGED (LT WING TE FLAP) · airframe 46,308 hrs · 11,793 cycles

INSPECTION TYPE:2C, LT WING OTBD FLAP VANE OTBD LOWER EDGE HAS WEAR DAMAGE AND MISSING MATERIAL. REMOVED DAMAGE, FILLED AREA AND BONDED REPAIR PLIES IAW STA-SA EA 011-5750-01-A2559 I/R AND EO MD11-5750-38951-A.

Part: SKIN — CRACKED (RT WING L/E) · airframe 46,308 hrs · 11,793 cycles

INSPECTION TYPE:2C, RT WING TELESCOPIC DUCT CUT-OUT CRACKED AT UPPER INBD AND OTBD CORNER. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLER IAW SRM 57-40-01, REPAIR 10, FIG 201, REV 43.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

LIGHT OVER RT EMERGENCY EXIT DOOR HANDLE IS INOP. REMOVED AND REPLACED LAMP AS REQUIRED. OK FOR CONTINUED SERVICE.

Part: SKIN — NONE (FUSELAGE) · airframe 44,667 hrs · 13,392 cycles

INSPECTION TYPE:SV DEFERRED ITEM: D-411587: CENTER CARGO DOOR CUTOUT REPAIR AT FS 1781 BETWEEN LONGERON 40R AND 41R REF WAN 1543617. REMOVED TEMP REPAIR, FABRICATED AND INSTALLED REPAIR IAW SAA EA 011-5330-01-A2094 ISSUE A AND IPXA EO MD11-5330-35504-B.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHTS INOP, DEFERRED PER MEL 33-50-4 ASSIGNED M404690. T/S PER FIM 33-52-00-1. CHECKED ALL WIRING ALL SATIS. ON T/S FOUND "EMER LT BAT 1 LO" MSG INTERMITTENTLY SHOWING. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW MM 33-51-01-4. MESSAGE GOES OFF. FOUND LOOSE CONNECT AT S3-735 BLOCK 28X. SECURED CONNECTION. SYSTEM CHECKS OK PER MM 33-50-00-5.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

PDC, EMERGENCY LIGHT TEST FAIL. ITEM TRANSFERRED TO M403264 PER MEL 33-50-4. PLACARD INSTALLED AND DI UPDATED. PER FIM, 33-51-02-00 CHANGE BATT.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 43,778 hrs · 11,140 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQUENCE F2-02 NOT FOUND ON MRCSSR AND IS NOT PER SRM. REMOVED, FABRICATED AND INSTALLED NEW REPAIR DOUBLER PER EO MD11-5330-33438-A AND EA 011-5330-01-A1766.

Part: SKIN — CRACKED (LT WING) · airframe 43,778 hrs · 12,130 cycles

INSPECTION TYPE:1C LT WING L/E SKIN CRACKED AT OPENING FOR SLAT DEICE TELESCOPE DUCT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW MD-11 SRM 57-10-00 FIG 43 SHT 1-5.

Part: SKIN — MISREPAIRED (BS 1159-1199) · airframe 43,778 hrs · 11,140 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQ NR 272-F1-03, EXISTING REPAIR DOUBLER ON RT CTR FUSELAGE BETWEEN STA 1159-1199 L26R-27R IS NOT ON MRCSSR REPORT AND NOT PER SRM. REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLER PER EO MD11-5330-3342 6-A.

Part: SKIN — CORRODED (BS 2140-2164) · airframe 43,778 hrs · 11,140 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQUENCE NR 272-F1-05, EXISTING REPAIR DOUBLER ON RT TAIL BETWEEN STA 2140 TO 2164 HAS CORROSION. REMOVED, FABRICATED AND INSTALLED NEW REPAIR DOUBLER PER EO MD11-5330- 33427-A AND EA 011-5330-01-A1756 REV A.

Part: SKIN — GOUGED (LT WING XW344) · airframe 43,778 hrs · 11,140 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQUENCE NR 272-W3-01, EXISTING REPAIR DOUBLER ON LT WING FIXED L/E LWR SKIN BETWEEN XDLE 330-XW344 NR 1 PYLON HAS GOUGED FASTENER HEADS, AS WELL CAN NOT CORRELATE TO THE SRM AND IS NOT ON MRCSSR REPORT. REMOVED DOUBLER ,TRIMMED OUT DAMAGE, FABRICATED AND INSTALLED NEW REPAIR DOUBLER PER EO MD11-5730-33428-A AND EA 011-5721-A1746.

Part: SKIN — GOUGED (FUSELAGE) · airframe 43,778 hrs · 12,130 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQ F1-02, FWD CARGO DOOR CUTOUT, AFT LWR COVER HAS AN EXISTING REPAIR THAT IS GOUGED BETWEEN FS 1002.3-1019 LONGERONS 40-41 RT. REMOVED DOUBLERS, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLERS IAW IPXA EO MD11-5330-33362-A.

Part: SKIN — MISREPAIRED (RT WING) · airframe 43,778 hrs · 11,140 cycles

INSPECTION TYPE:1C REPAIR SURVEY DWQ 272-W4-01, EXISTING REPAIR DOUBLER ON RT WING FIXED L/E LWR SKIN BETWEEN XOLE 330- XW 344 HAS SHEARED FASTENER HEADS AND GOUGED, AS WELL CAN NOT BE CORRELATED TO THE SRM AND IS NOT ON THE MRCSSR REPORT. REMOVED DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER IAW IPXA EO MD11-5750-33348-A.

Part: LENS — CRACKED (CABIN)

INSPECTION TYPE:N/A R1 DOOR AFT EMERGENCY LIGHT LENS CRACKED. REMOVED AND REPLACED R1 DOOR AFT EMERGENCY LIGHT LENS IAW MM 33-52. OK FOR SERVICE.

Part: DRIVE SHAFT — DAMAGED (L1 DOOR)

INSPECTION TYPE:N/A L1 DOOR INOP DEFERRED M396582. FOUND L1 DOOR DRIVE SHAFT ON FWD DRUM & SUPPORT ASSY DAMAGED. REMOVED AND REPLACED L1 DOOR FWD DRUM SUPPORT ASSY IAW AMM 52-11-08-4. ALSO REPLACED AIR MOTOR IAW AMM 52-11-05-4. P/N ON/OFF L30825-602, S/N ON 98265C005. OPS CHECK ELECTRICAL & PNEUMATICAL FUNCTION. FOUND SATISFACTORY. THIS CLEARS DMI.

Part: INDICATOR — UNKNOWN (EVAC SLIDE)

INSPECTION TYPE:N/A L1 DOOR REMOTE SLIDE PRESS INDICATOR. INSTALLED OVERHAULED ESCAPE SLIDE & EVAC SLIDE KIT IAW AMM 25-61-01- 4 & AMM 25-61-15-4. THIS CLEARS DMI 395653. SWITCH ASSY REPLACED IAW AMM 25-61-04-4.

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY DOME LIGHT INOP. RELAMPED EMERGENCY LIGHT, OPS CHECK GOOD.

Part: INDICATION SYS — INOPERATIVE (L1 SLIDE)

INSPECTION TYPE:N/A L1 DOOR SLIDE PTT IND LIGHT INOP. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PRESSURE IND KIT. SYS CHECKS OK M/M 25-61-04-5.

Part: FLOORBOARD — DAMAGED (AFT CARGO BAY)

INSPECTION TYPE:N/A AFT LWR PIT FLOOR AT DOOR HAS DAMAGE BEYOND REPAIR. STARTED FABRICATION OF NEW FLOORBOARD FROM AER98-5320-0004-1 SP 13580 77 IAW UPS EO MD115320-27386A. COMPLETED REPAIR REF UPS EO MD11-5320-2 7386-A.

Part: FITTING — DAMAGED (CARGO DOOR) · airframe 41,446 hrs · 10,611 cycles

INSPECTION TYPE:C REF: D368427 - MAIN CARGO DOOR ACTUATOR SUPPORT ASSY FITTING INTERIM REPAIR. REMOVED MAIN CARGO ACTUATOR AND LINK ASSY AS PER AMM 52-34-01-4/EO N MD11-5230-28549-A. TEMP INSTALLED MAIN CARGO DOOR ACTUATOR TO FOM. REMOVED MAIN CARGO DOOR ACTUATOR IAW AMM 52-34-01-4. REMOVED GOUGE FITTING BY REAMING HOLES 2EA UP TO .850" IAW EA11-523.

Part: SKIN — DAMAGED (BS 1119 S1) · airframe 41,446 hrs · 10,611 cycles

INSPECTION TYPE:C LIGHTNING STRIKE OUTER FUSE SKIN, FS 1119 STR 1. DISPLACED INSULATION FOR ACCESS IAW AMM 25-82-01-4 2. REMOVED DAMAGED FASTENERS IAW SRM 51-35-01, BURN AROUND COUNTER SINK & OUTER SKIN DIA OR LENGTH: .420" DEEP: .060"D, NORMAL DIA OF CSK IS .290"~.30" LOCATION: STA 6-91.5 STRINGER 1R. DAMAGE IS BEYOND LIGHTNING STRIKE DAMAGE REPAIR LIMIT IAW SRM 53-20-00.

Part: SKIN — CORRODED (AFT FUSELAGE)

CORROSION FOUND IN AFT FUSELAGE. REMOVED DAMAGED AND CORRODED SKIN. FABRICATED AND INSTALLED SKIN DOUBLER PER SRM 53-20-00. TRIMMED AND REPAIRED HORIZONTAL STAB AFT FAIRING SUPPORT ANGLE IAW EO 28738B.

Part: LIGHT — INOPERATIVE (R1 DOOR)

R1 DOOR LOWER EMERGENCY LIGHTS ARE INOP. PERFORMED FUNCTIONAL TEST PER TC 112. OPS CHECK NORMAL.

Part: RIB — CRACKED (L/E SLAT) · airframe 38,236 hrs · 10,094 cycles

INSPECTION TYPE:3C LEFT WING FIXED LEADING EDGE I/B SLAT TRACK FITTING BETWEEN NR 7 & 8 SLATS IS CRACKED. REMOVED AND REPLACED SLAT TRACK FITTING (RIB) BETWEEN NR 7 & 8 SLATS IAW MD-11 SRM 51-35-01.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,236 hrs · 10,094 cycles

INSPECTION TYPE:3C TRANSFERRED FROM LOG PAGE 699901 ITEM 2; DMI D344991 FUSELAGE SKIN DENT AT STA 1661, BETWEEN L32R & L33R. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR DOUBLERS IAW SAA EA 011-5330-01-A0795.

Part: PEDESTAL — FAILED (WEATHER RADAR)

INSPECTION TYPE: N/A ATB - WX RADAR FAILED IN ALL MODES IN SYSTEM 1&2. W/WX FAIL ON DISPLAY. SEVERE GRINDING NOISE IN ANTENNA. REPLACED WX RADAR ANTENNA PEDESTAL. SYSTEM OPS CKS OK REF MM 34-41-07-4.

Part: A/C PACK — ODOR (NR 1)

WITH THE NR 1 PACK ON, A NOXIOUS ODOR WAS ENTERING THE FLIGHT DECK THROUGH THE AIR CONDITIONING SYSTEM. SELECTING THE NR 1 PACK OFF ELIMINATED THE PROBLEM. OPERATED NR 1 PACK FULL HEAT, FULL COLD WITH NO ILL ODORS. ALL PACK TEMPS NML, OK FOR SERVICE.

Part: PIN — INSTALLED (MLG)

CENTER GEAR WOULD NOT RETRACT. ON POST FLIGHT INSPECTION FOUND CENTER GEAR PIN INSTALLED. REMOVED AND STOWED GEAR PIN. OK FOR SERVICE

Part: BRAKE ASSY — DISINTEGRATED (MLG)

BTB MECHANIC REPORTED NR 8 BRAKE ASSY DISINTEGRATING. REMOVED AND REPLACED NR 8 BRAKE ASSY IAW MM 32-43-01.

Part: INDICATOR — INOPERATIVE (FUEL QTY)

PILOT REPORT - LEVEL 2 FUEL QTY. FAULT EMERGENCY DECLARED FUEL QTY ALERT & FUEL SYSTEM MALFUNCTION DUE TO FUEL QTY ERROR W/PSC IN AUTO MODE. NO FAULTS STORED IN PSC-CURRENT FAULTS OR EXISTING FAULTS. T/S PERFMD IAW FIM 28-41-00. FUEL QTY BITE TEST PERFMD. PASSED. NIL FUEL ALERTS. FQBU INDICATES NO FAULTS/SYSTEM OK. PERFMD MANUAL STICK READING TO CONFIRM FUEL UPLIFT.

Part: LANDING GEAR — INOPERATIVE (ALL)

DURING GEAR EXTENSION, GEAR WOULD NOT ACHIEVE THE DOWN AND LOCKED POSITION (ALL 4). SECONDARY DISPLAY SHOWED UNSAFE ON ALL 4 GEARS. GEAR DOORS DID OPEN. GEAR CYCLED AND ACHIEVED A SAFE CONDITION, ALTHOUGH TOOK LONGER THAN NORMAL. T/S PER FIM 32-30-00 PSEU RTS AND SENSORS ALL OK. CLEANED AND LUBED LANDING GEAR CONT MECH PER MM 32-31-00-7. JACKED A/C & PERFORMED GEAR SWING SEVERAL TIMES PER MM 07-11-00-2 & 32-31-00-5. ALL FOUND NORMAL ALL EXTEND TIMES WITHIN MM LIMITS. REPLACED LANDING GEAR HANDLE POS SW PER MM.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

EMERGENCY BATTERY 1 LOW. BATTERY CHARGED UP AFTER 45 MIN OF CHARGING. EMERGENCY BATTERY TEST GO OD

Part: LANDING GEAR — DAMAGED (NOSE)

NOSE GEAR DAMAGED ON LANDING (FIRE).

Part: STRUCTURE — CRACKED (A/C PACK DOOR)

LT SIDE FUSELAGE FWD AIR CONDITION PACK ACCESS DOOR APPEARS CRACKED AT TOP OF DOOR. C/W HFEC AREA VERIFIED DOOR IS CRACKED APPROX 2.75 IN LENGTH MKD (QC0558905). REMOVED DOOR TO SM SHOP FOR REPAIR (0996300). REPLACED DOOR ASSY PER MM 52-42-01.

Part: SMOKE GOGGLES — CRACKED (COCKPIT)

CAPTS SMOKE GOGGLES ARE CRACKED. REMOVED AND REPLACED CAPTS SMOKE GOGGLES IAW MM11 AMM CH 35-13-03.

Part: MECHANISM — MALFUNCTIONED (PAX DOOR)

INSPECTION TYPE:N/A, LT ENTRY DOOR WILL NOT ARM ESCAPE SLIDE WHEN CLOSED. MANIPULATED EMERGENCY FLIPPER MECHAMISM WHILE MOVING EMERGENCY HANDLE FROM OUTSIDE. PERFORMED FUNCTIONAL CHECK OF ARMING DOOR PER MM 52-10-00, DOOR OPERATES AND ARMS NORMALLY.

Part: SLIDE — WILL NOT TEST (ENTRY DOOR)

LEFT CREW ENTRY DOOR SLIDE LIGHT WILL NOT TEST. DEFERRED PER MEL 25-61-2 M283588. INSTALLED CORRECT P/N BULBS IN REMOTE TEST SW PER WDM 25-61-01. OPS CHECKS GOOD. THIS CLEARS M283588.

Part: WEDGE — DELAMINATED (T/E FLAP)

INSPECTION TYPE:N/A LEFT O/B FLAP I/B TRAILING EDGE WEDGE HAS DELAMINATION (MRK). REMOVED AND REPLACED LEFT OUTBOARD FLAP INBOARD TRAILING EDGE WEDGE. THIS CLOSES DEFER RAL D272416 PER 57-50-03. REFERENCE LP33934.

Part: FLAP — DELAMINATED (RT WING)

INSPECTION TYPE:N/A RIGHT O/B FLAP HAS DELAMINATION AT I/B END (MRK).

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,303 hrs · 8,095 cycles

INSPECTION TYPE C :CABIN SEAT TRACK AT STA 1321 TO STA 1341 LBL 27.5 FOUND CORROSION. CORROSION REMOVED AT STA 1321 TO STA 1341 LBL 27.5 SEAT TRACK AT CAB IN FOUND EXCEED LIMIT IAW SRM 53-70-00 VOL I FIG 3 REV 32. CORRODED AREA TRIMMED OFF IAW SRM 53-70-00 VOL I REV 32 FIG 1. NEW SEAT TRACK REWORKED AND INSTALLED IAW SRM 53-70-00 VOL I FIG 1 REV 3 2

Part: SKIN — CORRODED (RT WING) · airframe 27,303 hrs · 8,095 cycles

INSPECTION TYPE: C, RT WING, UPPER SURFACE, FWD O/B FLAP FIXED PANEL STA XORS=799 FOUND CORROSION. CORROSION REMOVED AND PROTECTED AT REAR SPAR UPPER CAP AFT LEG FROM ST A XORS 780 TO STA 826 PER SRM 51-21-01 REV 32 VOL II. MATERIAL REMOVED 0.025 INCH, ORIGINAL THK 0.262 INCH, LEAVE THE BLENDOUT AREA 'AS IS' PER EN1014-03 AND UPS REPAIR/ALTERATION AUTH. ENGINEERING FILE NUMBER : MD11-57-20010. 2. HFEC INSP C/OUT ON REWORK AREA, NO CRACK FOUND.

Part: SPAR CAP — CORRODED (LT WING) · airframe 27,303 hrs · 8,095 cycles

INSPECTION TYPE:C LT WING REAR SPAR AT XORS 772.500 UPPER SURFACE FOUND CORROSION AS MARKED. CORR REMOVED AND REPROTECTED AT REAR SPAR UPP CAP AFT LEG FROM STA XORS 772 TO STA XORS 799 IAW SRM 51-21-01 REV 32 VOL II, MATERIAL REMOVED 0.009, ORG THK 0.266, LEAVE THE BLEND OUT AREA AS 'AS IS' PER EN1013-03 AND UPS REPAIR/ALTERNATION AUTO, ENGINEERING FILE NO. : MD11-57-20009. 2. HFEC INSP ON REWORK AREA FOUND NO CRACK EVIDENT.