N290UP

Part: UNKNOWN — NO TEST (FUSELAGE) · airframe 107,893 hrs · 21,468 cycles

INSPECTION TYPE:NA*SDR FILED OPEN* LEVEL 1 EMERGENCY POWER TEST FAIL

Part: LIGHT — INOPERATIVE (CABIN) · airframe 107,826 hrs · 21,428 cycles

INSPECTION TYPE:NAL1 DOOR EMERGENCY EXIT LIGHT AND PANEL FELL OFF WHEN CREW OPENED DOOR ON ARRIVALREPAIRED L1 SLIDING CEILING PANE PER EO MD11 2520 70609-D SECTOIN 6.B.

Part: DOOR — INOPERATIVE (L1) · airframe 107,826 hrs · 21,428 cycles

L1 SLIDING CEILING PANEL EXTENSION SPRING BROKE. DEFERRED L1 DOOR AIW MEL 52 10 3 1 2 1 2 PALCARD INSTALLED CONT # M 812779R&R L1 DOOR TENSION SPRING IAW MD11 AMM 25-23-23 OPS CHECKS OK THIS CLEARS MEL 52-10-3-1-2-1-2 M812179

Part: UNKNOWN — UNKNOWN (POWERPLANT) · airframe 107,802 hrs · 21,414 cycles

INSPECTION TYPE:NAX-FEED FROM TNK3 TO ENG 1 AT 2300LB IMBALANCE RECONFIGURED PER MEL AT 100LB AND IMBALANCE GREW AGAIN. TURNED #1 XFEED OFF AT 700LB IMBALANCE. NO LEAK SUSPECTED BASED ON FUEL USED AND FLIGHT PLAN FUELS. NO SIGNIFICANT CHANGE REST OF FLT.REMOVED REPLACED #3 FUEL FILL SHUTOFF VALVE & CONTROLLER PER AMM 28-21-02-401 & 28-21-09-401 & OPS CK GOOD. WORK PERFORMED ON FFC RO 5230248 PAK 2553 PERFORMED OPERERNATIONAL AND FUNCTIONAL TEST OF #3 OFF VALVE AND CONTROLLER PER AMM 28-21-02 TEST PASSED AND NO LEAKS NOTED FUEL STILL MIGRATING.

Part: SLIDE — INOPERATIVE (DOORS) · airframe 107,775 hrs · 21,395 cycles

INSPECTION TYPE:NAL1 DOOR SLIDE UNZIPPED.REPLACED L1 DOOR SLIDE PER AMM 25-61-15 OPS TEST GOOD 25-01-05-01.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 107,478 hrs · 21,253 cycles

INSPECTION TYPE:NA*SDR FILED OPEN* ON PREFLIGHT EMERG LIGHT BAT 1 LOW DISPLAYED. OK TO CONTINUE PER MEL 33-50-4. DMP 33-50-4 C/W. REMOVED & REPLACED EMERGENCY LIGHT BATTERY PER AMM 33 51 01, THIS CLEARS DEFERRAL M809063. CB'S RESTORED TO NORMAL. OPS CHECK GOOD.

Part: GIRT BAR — FOD (L1 DOOR) · airframe 106,993 hrs · 21,003 cycles

L1 DOOR SLIDE WONT ARM. GIRT BAR AREA CLEANED OF DEBRIS, SUSPECT MOISTURE & ICE. OPS CHECKED L1 DOOR ARMING/DISARMING IAW AMM 52-10-01-700-801. NO FAULTS FOUND.

Part: LONGERON — CORRODED (CENTER CARGO) · airframe 106,432 hrs · 20,716 cycles

INSPECTION TYPE:3CCENTER CARGO LONGERON HAS CORROSION BETWEEN STA. 1752 TO 1811.REPAIRED CORRODED LONGERON 47 R/H BETWEEN STA. 1611 TO 1811 IAW VT-SAA EA 011-5350-01-A9638 REV. I/R AND UPS EO MD11-5310-84327-A. (MAJOR) REF. FAA FORM 8100-9 BY JEFFREY TOM (AR-605565) DATED 8/01/2022.

Part: STIFFENER — CRACKED (AFT CARGO) · airframe 106,432 hrs · 20,716 cycles

INSPECTION TYPE:3CAFT CARGO AT STA 1841 AND RBL 36 VERTICAL STIFFENER IS CRACKED.REMOVED,FABRICATED, REPLACED VERTICAL STIFFENER IAW SRM 51-31-01 AND 51-33-01 (MINOR)

Part: SUPPORT ANGLE — CRACKED (FWD CARGO) · airframe 106,432 hrs · 20,716 cycles

INSPECTION TYPE:3CFWD CARGO COMPARTMENT SIDEWALL SUPPORT ANGLE CRACK AT LH SIDE STA.919.REMOVED,FABRICATED AND REPLACED CRACK SUPPORT ANGLE IAW SRM 51-35-01 AND 51-31-01 (MINOR).

Part: STIFFENER — CRACKED (AFT CARGO) · airframe 106,432 hrs · 20,716 cycles

INSPECTION TYPE:3CAFT CARGO UNDER FLOOR PANEL 187AF AT STA 1841 AND LBL26 HAS A STIFFENER THAT IS CRACKED.REMOVED, FABRICATED, REPLACED THE STIFFENER IAW SRM 51-33-01 AND 51-31-01 (MINOR)

Part: RETAINER — CRACKED (CTR CARGO) · airframe 106,432 hrs · 20,716 cycles

INSPECTION TYPE:3CCTR CARGO FLOOR SUPPORT ANGLE (RETAINER) IS CRACKED AT STA 1521 AND LBL10 TO RBL 10.REMOVED, FABRICATED, REPLACED RETAINER IAW SRM 51-31-01 (MINOR)

Part: FLAG — CRACKED (L/H I/B FLAP) · airframe 106,432 hrs · 20,716 cycles

INSPECTION TYPE:3CL/H WING I/B FLAP UPPER SKIN IS CRACKED AT STA XIFH = 171.300 AND ABOVE STA YIFH 34.530 SPAR DOUBLER REPAIR.REMOVED, REPAIRED THE CRACKED ON THE L/H WING I/B FLAP UPPER SKIN AT STA XIFH = 171.300 AND ABOVE STA YIFH = 34.530 SPAR IAW VTSAA EA 011-5730-01-A9633 I/R AND UPS EO MD11-5750-84131-A FAA 8100-9 SIGNED BY J.TOM (AR-605565) DATED 07/12/22 (MAJOR)

Part: SPAR CAP — CORRODED (R/H WING) · airframe 106,432 hrs · 20,716 cycles

INSPECTION TYPE:3CR/H WING REAR SPAR UPPER CAP IS CORRODED BETWEEN STA. XORS. 743.52 TO 756.82.REPAIRED CORRODED R/H WING REAR SPAR UPPER CAP IAW VT-SAA EA 011-5710-01-A9632 REV. I/R AND UPS EO MD11-5710-84161-A. (MINOR)

Part: STIFFENER — CRACKED (RT WING T/E) · airframe 106,432 hrs · 20,716 cycles

INSPECTION TYPE:3CRH I/B WING T/E REAR SPAR VERTICAL STIFFENER CRACK FWD OF I/B AILERON.REMOVED AND REPLACED CRACKED STIFFENER IAW SRM 51-33-01 AND 51-31-01 (MINOR)

Part: FORMER — CRACKED (R/H WING) · airframe 106,432 hrs · 20,716 cycles

INSPECTION TYPE:3CR/H WING FIXED L/E FORMER IS CRACKED AT STA. XOS. 584.0.REPAIRED CRACKED R/H WING FIXED L/E FORMER AT STA. XOS. 584.0 IAW SRM 57-00-00 REPAIR GENERAL FIG. 204. (MAJOR)

Part: DOUBLER — CRACKED (RT WING L/E COMP) · airframe 106,432 hrs · 20,716 cycles

INSPECTION TYPE:3CRT O/B WING FIXED L/E BEADED DOUBLER CRACK AT STA. XOS 789.6 TO XOS 795.7.REPAIRED CRACKED BEADED DOUBLER AT STA.XOS 789.6 TO XOS 795.7 IAW MD-11 SRM 57-40-02 REPAIR 15,FIG 205 REV 68.01 (MAJOR).

Part: WEB — CRACKED (R/H A/C BAY) · airframe 106,432 hrs · 20,716 cycles

INSPECTION TYPE:3CR/H A/C BAY HAS A INTERCOSTAL (WEB) AFT OF DOOR CUTOUT AT L34 IS CRACKED.REMOVED, FABRICATED, REPLACED THE WEB IAW SRM 51-33-01 AND 51-31-01. (MINOR)

Part: SKIN — CORRODED (CENTER WING BOX) · airframe 106,432 hrs · 20,716 cycles

INSPECTION TYPE:3CCENTER WING BOX UPPER SKIN HAS CORROSION BETWEEN STA. XCW= 81 TO XCW= 118.2 AT STR. 15.REPAIRED CORRODED CENTER WING BOX UPPER SKIN BETWEEN STA. XCW= 81 TO XCW= 118.2 AT STR. 15 IAW VT-SAA EA 011-5730-01-A9629 REV. I/R AND UPS EO MD11-5730-84189-A, (MAJOR) REF. FAA FORM 8100-9 BY S. KANG (AR-605677) DATED 07/13/2022.

Part: STIFFENER — CRACKED (RH MLG W/W) · airframe 106,432 hrs · 20,716 cycles

INSPECTION TYPE:3CRH MLG W/W AFT O/B WEB 3RD STIFFENER CRACK AT LWR END.REMOVED AND REPALCED CRACKED STIFFENER IAW SRM 51-35-01 AND 51-31-01 (MINOR).

Part: SKIN — CORRODED (CTR WING BOX) · airframe 106,432 hrs · 20,716 cycles

INSPECTION TYPE:3CCENTER WING TANK UPPER FWD AND CENTER SKIN AND AT S-15 BETWEEN XCW=13 AND XCW=-86 HAS CORROSION.REMOVED, REPAIRED CTR WING TANK SKIN IAW VT-SAA EA 011-5730-01-A9625 REV I/R AND UPS EO MD11-5730-84125-A. (MINOR)

Part: ACTUATOR — GOUGED (CTR CARGO DOOR) · airframe 106,432 hrs · 20,716 cycles

INSPECTION TYPE:3CCENTER CARGO DOOR AFT ACTUATING ARM IS GOUGED.REPAIRED THE AFT ACTUATING ARM IAW VT-SAA EA-011-5230-01-A9628 REV I/R AND UPS EO MD11-5230-84126-A (MINOR)

Part: ACTUATOR — GOUGED (CTR CARGO DOOR) · airframe 106,432 hrs · 20,716 cycles

INSPECTION TYPE:3CCENTER CARGO DOOR FWD ACTUATING ARM IS GOUGED.REPAIRED THE FWD ACTUATING ARM IAW VT-SAA EA-011-5230-01-A9628 REV I/R AND UPS EO MD11-5230-84126-A. (MINOR)

Part: TRANSMITTER — FAULTED (LT WING TE FLAP) · airframe 105,841 hrs · 20,405 cycles

ATB, NO EMERG DECLARED, LANDED WITHOUT INCIDENT, A/C OOS. AFTER RAISING LANDING GEAR ON TAKEOFF, LANDING GEAR AURAL WARNING HORN WENT OFF CONTINUOUSLY. WE CYCLED THE GEAR DOWN AND THEN UP, ONCE BACK UP THE AURAL WARNING CONTINUED UNTIL WE PUT THE LANDING GEAR DOWN FOR LANDING. ALL INDICATIONS WEREPERFORMED TEST 5 ON CAWS UNIT, TEST FAILED. R&R UNIT IAW 31-51-01 NO HELP. TRIED ANOTHER CAWS UNIT, NO HELP. REINSTALLED ORIGINAL CAWS, TEST 5 PASSES INTERMITTENTLY. .R&R CAWC & L/H IB FLAP POS. TRANSMITTER. OPS CHECK GOOD PER AMM 31-51-01. EFF SOURCE REF: I

Part: PSEU — FAULTED (SLAT SYSTEM) · airframe 105,463 hrs · 20,221 cycles

INSPECTION TYPE:N/A**EMERGENCY DECLARED ** T/O PLUS 2 HRS LVL 2 SLAT DISAG FL360 .83MT/S PER MD-11 FIM 31.71.00.101 FOUND PSEU FAULT. REMOVED & REPLACED PSEU IAW M.M.31.71.01.000.801 OPS CKS NORMAL

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 104,880 hrs · 19,937 cycles

INSPECTION TYPE:NA**SUPPLEMENTAL SDR** DURING PRE-FLIGHT EMER LT 8AT1LO ALERT CAME ON DURING THE EMERGENCY LIGHT TEST. DEFERRED PER MEL 33-50-4. C/W DMP 33-50-4. M742774 ASSIGNEDREPLACED BATT. EMERGENCY POWER SUPPLY REF AMM 33 51 01 401. OPS NORMAL.

Part: SWITCH — INTERMITTENT (L1 DOOR) · airframe 104,661 hrs · 19,824 cycles

INSPECTION TYPE:NA**SUPPLEMENTAL SDR** LEFT ENTRY DOOR SWITCH INTERMITTENT YOU CAN HEAR THE RELAYS CLICKING BUT IT TAKES A FEW TRIES. L1 ENTRY DEFFERED PER MEL 52-10-1-2-0-1 VERIFIED PNEUMATIC BOTTLE CHARGE O.K DMP 52-10-1-2-0-1 ASSIGNED CONTROL NO M735553. PLACARD INSTALLED REQ 341919.REPLACED RELAY R2-177 PER SWPM 20-00-09, OPS CK FAILED. REPLACED LOCKPIN SOLEMOID PER AMM 52-10-06, OPS CK GOOD. DMP 52-10-1-2-0-1 REVERSED, PLACARD REMOVED DEFERRAL CLEARED.

Part: SKIN — CRACKED (A/C DOOR) · airframe 104,653 hrs · 19,818 cycles

INSPECTION TYPE:N/ARH AIR CONDITIONING DOOR JAMB CORNER SKIN CRACK REPAIRREPAIRED PER EO MD11-5330-78847-C.

Part: CHILLER — ODOR (GALLEY) · airframe 104,651 hrs · 19,817 cycles

INSPECTION TYPE:NASTRONG CHEMICAL ODOR IN COCKPIT.DID NOT NOTICE A CHEMICAL SMELL BUT DID NOTICE A STRONG ELECTRICAL SMELL AROUND COURIER SEATS AND GALLEY AREA. HAS HISTORY OF REFRIGERATOR NOT WORKING AND GIVING OFF A BURNING SMELL. R&R REFRIGERATOR IAW AMM 25-37-57. OPS CHECK GOOD. SMELL NO LONGER NOTICED. EFF SOURCE REF: AIPC 25-31-05-10

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 104,328 hrs · 19,655 cycles

INSPECTION TYPE: NA ATB, NO EMERGENCY DECLARED. CABIN INFLOW LOW LEVEL 1 ALERT ON DURING CLIMBOUT. FOLLOWED CABIN ALTITUDE CHECKLIST AND MONITORED ILLEG CONTINUED TO CLIMB OUTFLOW VALVE WAS FULL CLOSED. CABIN ALTITUDE COULD NOT BE MAINTAINED. RETURNED TO SDF. RECEIVED AVIONICS FLO OVERIDE 101 ADJUSTED CABIN PRESSURE OUTFLOW VALVE ACTUATOR PUSH ROB ASSEMBLY, IAW MM 21-31-20-400-801. PERFORMED FUNCTIONAL TEST OF CABIN PRESS CONTROL SYSTEM, IAW MM 21-31-00-700-801, ALL OPERATIONS NROMAL.

Part: BRACE — CRACKED (RT WING T/E) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C RT WING T/E FALSE SPAR VERTICAL BRACE NR 2 POS IS CRACKED. REMOVED AND REPLACED BRACE, IAW SRM 51-*33-01, MINOR.

Part: HINGE FITTING — WORN (LT WING TE FLAP) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C LT OUTBOARD FLAP INBOARD FLAP ACTUATOR UPPER MOUNT INBOARD BUSHING IS MIGRATED. REPAIRED LT OUTBOARD FLAP INBOARD ACTUATOR HINGE LUG, IAW VT-SAA EA NR 011-5740-01-A8524 I/R AND UPS EO NR MD11-5740-77852-A (MINOR).

Part: RIB — CORRODED (RT ELEVATOR) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C RT OUTBOARD ELEVATOR INBOARD RIB HAS CORROSION. REMOVED AND REPLACED RT OUTBOARD ELEVATOR ASSY, IAW AMM 27-30-30-401 AND UPS EO NR MD11-2700-74700-C (MINOR).

Part: RIB — CORRODED (LT ELEVATOR) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C LT DETACHABLE ELEVATOR HAS A CORRODED RIB. REMOVED AND REPLACED LT DETACHABLE ELEVATOR ASSY, IAW AMM 27-30-10-401 AND UPS EO NR MD11-2700-74700-C (MINOR).

Part: FITTING — CHAFED (CABIN) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C RCB WALL SIDE FITTING NR 6 IS CHAFED. REPAIRED RCB WALL SIDE FITTING NR 6, IAW VT-SAA EA NR 011-5310-01-A8522 I/R AND UPS EO NR MD11-5340-77713-A (MINOR).

Part: FITTING — CHAFED (CABIN) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C RCB WALL SIDE FITTING NR 7 IS CHAFED. REPAIRED RCB WALL SIDE FITTING NR 7, IAW VT-SAA EA NR 011-5310-01-A8523 I/R AND UPS EO NR MD11-5340-77712-A (MINOR).

Part: SKIN — CORRODED (LT WING TE) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C LT OUTBOARD WING UPPER SURFACE TRAILING EDGE HAS AREAS OF CORROSION FWD OF NR 2 SPOILER. REPAIRED LT WING UPPER CAP, IAW VT-SAA EA NR 011-5710-01-A8537 I/R AND UPS EO NR MD11-5750-48560-B (MINOR).

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C MAIN CABIN FLOOR PANEL NR WSP0789-502 HAS CORROSION. REPAIRED MAIN CABIN FLOOR PANEL NR WSP0789-502, IAW VT-SAA EA NR 011-5320-01-A8542 I/R AND UPS EO NR MD11-5320-77841-A (MINOR).

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C MAIN CABIN FLOOR PANEL NR WSP0786-501 HAS CORROSION. REPAIRED MAIN CABIN FLOOR PANEL NR WSP0786-501, IAW VT-SAA EA NR 011-5320-01-A8533 I/R AND UPS EO NR MD11-5320-77834-A (MINOR).

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C MAIN CABIN FLOOR PANEL NR WSP0788-501 HAS CORROSION. REPAIRED MAIN CABIN FLOOR PANEL NR WSP0788-501, IAW VT-SAA EA NR 011-5320-01-A8543 I/R AND UPS EO NR MD11-5320-77836-A (MINOR).

Part: FITTING — CHAFED · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: IN RCB SIDE FITTING NR 16 HAS CHAFE DAMAGE. REPAIRED RCB SIDE FITTNG NR 16, IAW VT -SAA EA 011-5310-01-A8530 I/R AND UPS EO MD11-5310-48610-B (MINOR).

Part: HEAT SHIELD — DENTED (APU EXHAUST) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C LOWER FUSELAGE APU EXHAUST HEAT SHIELD HAS 2EA DENTS. REPAIRED APU EXHAUST HEAT SHIELD, IAW VT-SAA EA NR 011-5350-01-A8541 I/R AND UPS EO NR MD11-5350-77839-A (MINOR).

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C MAIN CABIN FLOOR PANEL NR WSP0785-501 HAS CORROSION. REPAIRED MAIN CABIN FLOOR PANEL NR WSP0785-501, IAW VT-SAA EA 011-5320-01-A8534 I/R AND EO NR MD11-5320-77824-A (MINOR).

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C MAIN CABIN SEAT TRACK AT STA.X=19.0 HAS CORROSION. REPAIRED CORRODED MAIN CABIN SEAT TRACK AT STA.X=19.0, IAW SRM 51-31-01 (MINOR).

Part: SKIN — CRACKED (LT WING FAIRING) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C LT INBOARD WING T/E BLISTER FAIRING CRACKED AFT OF LT MLG. REPAIRED LT INBOARD WING T/E CRACKED BLISTER FAIRING, IAW SRM 51-31-01 AND 51-35-01 (MINOR).

Part: TEE FITTING — CRACKED (BS 1341) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C MAIN CABIN LONGERON 15R TEE ANGLE CRACKED AT STA. 1341. FABRICATED AND INSTALLED MAIN CABIN LONGERON 15R TEE ANGLE AT STA.1341 IAW SRM 51-31-01 AND 51-33-01. (MINOR).

Part: TEE FITTING — CRACKED (BS 1219) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE:2C MAIN CABIN LONGERON 15R TEE ANGLE IS CRACKED AT STA. 1219. FABRICATED AND INSTALLED MAIN CABIN TEE ANGLE AT LONGERON 15R STA.1219 IAW SRM 51-33-01 AND 51-31-01. (MINOR)

Part: TEE FITTING — CRACKED (BS 1341) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C MAIN CABIN LONGERON 15L TEE ANGLE CRACKED AT STA.1341. FABRICATED AND INSTALLED MAIN CABIN LONGERON 15L TEE ANGLE AT STA. 1341 IAW SRM 51-31-01 AND 51-33-01. (MINOR)

Part: FORMER — CRACKED (LT O/B FLAP) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C LT OUTBOARD FLAP INBOARD HINGE FRAME, FORMER IS CRACKED. REMOVED, FABRICATED, AND REPLACED FORMER, IAW DWG ARC 0547 AND SRM 51-31-01 (MINOR).

Part: SKIN — CRACKED (RT WING) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE:2C RT WING ACCESS DOOR 636AB LOWER SKIN CUT-OUT FASTENER HOLE HAS 5 EA CRACKS. REPAIRED RT WING ACCESS DOOR 636AB SKIN CUT-OUT FASTENER HOLES IAW SRM 57-20-02 REPAIR 5 (MINOR).

Part: SKIN — CRACKED (LT WING) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE:2C LT WING LOWER SKIN ACCESS DOOR 536AB CUT-OUT 1 EA FASTENER HOLE CRACK.REPAIRED LT WING CRACKED LOWER SKIN ACCESS DOOR 536AB CUT-OUT IEA FASTENER HOLE IAW SRM 57-20-02 REPAIR 5 (MINOR).

Part: SKIN — CORRODED (BS 2154-2163) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C EXTERIOR FUSELAGE SKIN HAS CORROSION BETWEEN STA 2154-2163.8 AND L12R TO 13R. REPAIRED CORRODED EXTERIOR FUSELAGE SKIN BETWEEN STA 2154-2163.8 AND L12R TO 13R, IAW SRM 53-70-01 REPAIR 3 FIG. 201 (MAJOR).

Part: INTERCOSTAL — CRACKED (FWD CARGO) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C LOWER FWD CARGO INTERCOSTAL IS CRACKED AT STA 6-50 AT L43R. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL, IAW DWG ACA7049 AND SRM 51-35-01 (MINOR).

Part: FLOORBEAM — CRACKED (FWD CARGO) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C LOWER FWD CARGO FLOOR BEAM IS CRACKED AT STA 6-70 AND X=57.50. REPAIRED CRACKED FLOOR BEAM AT STA 6-70 AND X=57.50, IAW VT-SAA EA 011-5340-01-A8529 REV. I/R AND UPS EO MD11-5340-77877-A (MAJOR).

Part: BEAM — CRACKED (FWD CARGO) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C LOWER FWD CARGO HORIZ BEAM IS CRACKED AT STA 6-73 ABOVE L43R. REMOVED, FABRICATED, AND REPLACED BEAM, IAW DWG ADA 7667 AND SRM 51-33-01 (MINOR).

Part: SKIN — CORRODED (BS 2148-2155) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE:2C EXTERIOR FUSELAGE SKIN HAS CORRROSION BETWEEN STA 2148-2155 AND L33R TO 35R. REPAIRED CORRODED EXTERIOR FUSELAGE SKIN BETWEEN STA 2148-2155 AND L33R TO 35R, IAW SRM 53-70-01 REPAIR 3 FIG. 201 (MAJOR).

Part: LONGERON — CORRODED (50 LEFT) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE:2CLONGERON 50 L/H IS CORRODED BETWEEN STA. 6-70 TO 6-80.REPAIRED CORRODED LONGERON 50 L/H BETWEEN STA. 6-40 TO 6-80 IAW VT-SAA EA 011-5340-01-A8525 REV. I/R AND UPS EO MD11-5340-77874-A. (MAJOR)

Part: SEAT TRACK — CORRODED (BS 459-485) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C MAIN CABIN SEAT TRACK IS CORRODED BETWEEN STA 459.227 TO 485.227 AND X=50 TO X=63. REPAIRED CORRODED MAIN CABIN SEAT TRACK BETWEEN STA 459.227 TO 485.227 AND X=50 TO X=63, IAW VT-SAA EA 011-5310-01-A8521 REV I/R AND UPS EO MD11-5310-77862-A (MAJOR).

Part: STRINGER — CRACKED (STRINGER 45) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C CENTER WING TANK STRINGER NR 45 IS CRACKED AT STA XCW= -17.0. REPAIRED CRACKED CENTER WING TANK STRINGER NR 45 BETWEEN STA XCW= -4.250 TO XCW= -29.5, IAW SRM 57-10-03 REPAIR 1 FIG. 201 (MAJOR).

Part: STIFFENER — CRACKED (BS 1841) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C VERTICAL STIFFNER IS CRACKED AT STA 1841 AND LBL=20. REMOVED, FABRICATED, AND REPLACED STIFFNER IAW DWG. AGA7170 AND SRM 51-33-01 (MINOR).

Part: STRINGER — CRACKED (47) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C CENTER WING TANK STRINGER NR 47 IS CRACKED IN 3 PLACES, CXW=17, XCW= 46.5, AND XCW= -17.0. REPAIRED CRACKED CENTER WING TANK STRINGER NR 47 BETWEEN STA XCW= -34.0 TO XCW= 58.5, IAW SRM 57-10-03 REPAIR 1 FIG 201 (MAJOR).

Part: SKIN — GOUGED (LEFT WING) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE:2C LT WING FIXED LEADING EDGE UPPER SKIN IS GOUGED AT STA XOS 1185.65. REPAIRED GOUGED LT WING FIXED LEADING EDGE SKIN AT STA XOS 1185.65, IAW SRM 57-40-01 REPAIR 16 FIG 201 (MAJOR).

Part: SEAT TRACK — CORRODED (BS 440-515) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C MAIN CABIN SEAT TRACK IS CORRODED BETWEEN STA 440-515 AND X= -36. REMOVED AND REPLACED SEAT TRACK BETWEEN STA 440-515 AND X= -36, IAW DWG WSP0826 AND SRM 51-31-01 (MINOR).

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C MAIN CABIN FLOOR PANEL NR WSP 0709-501 HAS CORROSION. REPAIRED CORRODED FLOOR PANEL, IAW VT-SAA EA 011-5320-01-A8535 REV I/R AND UPS EO MD11-5320-77799-A (MINOR).

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C MAIN CABIN FLOOR PANEL IS CORRODED BETWEEN STA X= -8.5 TO -27.5 AND Y=392-440. REMOVED, FABRICATED, AND REPLACED FLOOR PANEL IAW DWG WSP0668 AND SRM 51-33-01 (MINOR).

Part: SKIN — CRACKED (RT WING) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C RT WING FIXED LEADING EDGE LOWER SKIN IS CRACKED AT STA XOS 490.850. REPAIRED CRACKED RT WING FIXED LEADING EDGE LOWER SKIN AT STA XOS 490.850, IAW SRM 57-40-01 REPAIR 17 FIG. 201 (MAJOR).

Part: DOUBLER — CRACKED (LT WING) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C LT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED BETWEEN STA XOS 667.6 TO 673.7. REPAIRED CRACKED LT WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN STA XOS 667.6 TO 673.7, IAW SRM 57-40-02 REPAIR 15 FIG 201 (MAJOR).

Part: DOUBLER — CRACKED (LT WING) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C LT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED BETWEEN STA XOS 753.1 TO 759.1. REPAIRED CRACKED LT WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN STA XOS 753.1 TO 759.1, IAW SRM 57-40-02 REPAIR 15 FIG 205 (MAJOR).

Part: CAP — DAMAGED (LT WING) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C LT WING LOWER T/E CAP HAS GOUGES ON HORZ FLANGE BETWEEN STA XW=120.630 TO XW=146.618. REPAIRED DAMAGED LT WING LOWER T/E CAP HORZ FLANGE BETWEEN SGTA XW=120.630 TO XW=146.618, IAW EA 011-5710-01-A8546 REV I/R AND EO MD11-5710-77871-A (MAJOR).

Part: HINGE — CHAFED (NR 1 NAC DOOR) · airframe 104,154 hrs · 19,575 cycles

INSPECTION TYPE: 2C NR 1 ENG OUTBOARD FAN COWL FWD HINGE IS CHAFED. REPAIRED NR 1 ENG OUTBOARD FAN COWL FWD HINGE, IAW VT-SAA EA 011-7110-01-A8528 REV I/R AND UPS EO MD11-7110-77740-A (MINOR).

Part: PANEL — DENTED (VERTICAL STAB) · airframe 103,432 hrs · 19,249 cycles

INSPECTION TYPE:N/ALWR VERT STAB PANEL 364CRDENTEDREPAIRED PER EO MD11-5430-75682-A COMPOSITE DOUBLER REPAIR

Part: SHUTOFF VALVE — INOPERATIVE (WING ANTI-ICE) · airframe 103,013 hrs · 19,071 cycles

INSPECTION TYPE:N/ADIVERSION - OUT OF 10,000 FT ON CLIMBOUT WE ENCOUNTERED ICING CONDITIONS. WE SELECTED THE R WING A ICE SWITCH TO OFF PER QRH. GOT LEVEL 2 RT WING ANTI ICE DISAS MSG.R/R RT WING ANTI-ICE SHUTOFF VALVE IAW AMM 30-11-01-400-801. OPS TEST OK FOR BORROWED PART INSTALLED.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 102,424 hrs · 18,832 cycles

INSPECTION TYPE:N/A LVL 1 EMERGENCY BAT 1 LO WHEN TESTING THE EMER LIGHTS. DEF EMERGENCY BAT 1 LO PER MEL 33-50-4, DMP 33-50-4 C/W. PLACARD INSTALLED. R/R EMERGENCY LIGHT POWER SUPPLY REF MM 33-51-10-01. OPS TEST GOOD. THIS CLEARS M676778.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 101,246 hrs · 18,437 cycles

L1 DOOR EMERGENCY EXIT LENS HOUSING WAS DAMAGED. ACCOMPLISHED EO MD11-02520-70732-A SECTION 6.A.

Part: DOOR — OUT OF ADJUST (L1) · airframe 101,246 hrs · 18,437 cycles

L1 DOOR OUT OF ADJUSTMENT. REMOVED FWD LT L1 DOOR SLIDING CEILING PANEL IAW AMM 25-23-23. PERFORMED AN ADJUSTMENT OF THE DOOR.

Part: BOTTLE — LOW PRESSURE (CREW DOOR) · airframe 100,994 hrs · 18,385 cycles

LEFT CREW DOOR PNEUMATIC STORAGE PRESSURE WAS LOW. SERVICED THE BOTTLE IAW AMM 12-25-04. ACFT OK FOR SERVICE.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHTS) · airframe 100,854 hrs · 18,329 cycles

DURING AN EMERGENCY LIGHT TEST, LEVEL 1, EMERGENCY LIGHT BATTERY 1 LOW. TROUBLESHOT IAW FIM 33-51-00-101. REMOVE AND REPLACED THE EMERGENCY LIGHTING BATTERY POWER SUPPLY IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: DOOR — INOPERATIVE (CABIN) · airframe 100,845 hrs · 18,323 cycles

L1 DOOR EMERGENCY. SERVICED PAX DOOR SYSTEM TO PROPER LEVEL IAW AMM 12-25-04-600-801.

Part: FLOOR SUPPORT — CRACKED (AFT CARGO) · airframe 100,752 hrs · 18,285 cycles

AFT CARGO FLOOR SUPPORT WAS CRACKED AT BS 1842, RBL 20. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-33-01.

Part: LANDING — CRACKED (LT WING) · airframe 100,752 hrs · 18,285 cycles

LEFT WING OTBD FLAP, INBD HINGE, OTBD LOWER LANDING WAS CRACKED AROUND A RIVET. REMOVED AND REPLACED THE LANDING IAW SRM 51-31-01, AND 51-35-01.

Part: ATTACH FITTING — CRACKED (RT WINGLET) · airframe 100,752 hrs · 18,285 cycles

RIGHT LOWER WINGLET, AFT ATTACH FITING WAS CRACKED. REPLACED THE ATTACH FITTING IAW EO MD11-5720-27680-C, APPX E. MAJOR.

Part: SHEAR TIE — CORRODED (BS 1531) · airframe 100,752 hrs · 18,285 cycles

CENTER CARGO BAY SHEAR TIE WAS CORRODED AT BS 1531, LONGERON 48R. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT SHEAR TIE IAW DWG A5A7058, AND SRM 51-33-01.

Part: STIFFENER — CRACKED (BS 1841) · airframe 100,752 hrs · 18,285 cycles

AFT CARGO FLOOR SUPPORT HAD A CRACKED STIFFENER, BS 1841, RBL 20. REMOVED AND REPLACED STIFFENER IAW SRM 51-31-01, AND 51-33-01.

Part: DOUBLER — DAMAGED (TAILCONE) · airframe 100,752 hrs · 18,285 cycles

TAILCONE RT INTERNAL PRODUCTION DOUBLER HAD DEEP WEAR AT THE TOP. REPAIRED THE TAILCONE IAW EA 011-5350-01-A7397, REV IR, AND EO MD11-5350-69448-A.

Part: ANGLE — CRACKED (LT WING) · airframe 100,752 hrs · 18,285 cycles

LT WING FIXED L/E AT XIS 290 HAD A CRACKED ANGLE, INSIDE PANEL 516DB. REPAIRED THE ANGLE IAW EA 011-5720-01-A7411, REV IR, AND EO MD11-5740-69544-A. MAJOR.

Part: LANDING — CRACKED (LT WING`) · airframe 100,752 hrs · 18,285 cycles

LEFT OTBD FLAP INBD HINGE, INBD FAIRING PANEL LANDING BEAM WAS CRACKED AT THE LOWER FASTENER. REMOVED AND REPLACED FAIRING PANEL LANDING IAW SRM 51-31-01, 51-33-01, AND 51-35-01.

Part: DOUBLER — DAMAGED (TAIL CONE) · airframe 100,752 hrs · 18,285 cycles

TAILCONE LT INTERNAL PRODUCTION DOUBLER HAD DEEP WEAR AT THE TOP. REPAIRED IAW EA 011-5350-01-A7396, REV IR, AND EO MD11-5350-69447-A.

Part: SUPPORT ANGLE — CRACKED (LEFT WING) · airframe 100,752 hrs · 18,285 cycles

LEFT WING FIXED L/E SUPPORT ANGLE WAS CRACKED AT XOS 325. REMOVED, FABRICATED, AND REPLACED THE LT WING FIXED L/E SUPPORT BRACKET IAW DWG ARB0116, AND SRM 51-33-01.

Part: DOOR FRAME — CHAFED (NR 2 NACELLE) · airframe 100,752 hrs · 18,285 cycles

NR 2 ENGINE RT FAN COWL DOOR FRAME HAD A WIDE SPREAD, DEEP CHAFE TO THE RUBSTRIP FROM TOP TO BOTTOM WITH DAMAGE TO UNDERLYING SKIN. REMOVED, FABRICATED AND INSTALLED THE RT FAN COWL DOOR FRAME AND RUBSTRIP IAW SREO MD11-5420-42847-A.

Part: SKIN — CRACKED (LT WING LOWER) · airframe 100,752 hrs · 18,285 cycles

THE LEFT WING FIXED L/E LOWER SKIN WAS CRACKED AT XOS 776. REPAIRED THE SKIN IAW SRM 57-40-02, REPAIR 7, FIG 201. MAJOR.

Part: SKIN — CRACKED (RT WING LOWER) · airframe 100,752 hrs · 18,285 cycles

RIGHT WING FIXED L/E LOWER SKIN WAS CRACKED AT XOS. 891. REPAIRED THE RT WING SKIN IAW SRM 57-40-02, REPAIR 7, FIG 201. MAJOR.

Part: WEB — CRACKED (BS 1372) · airframe 100,752 hrs · 18,285 cycles

LEFT OVERWING UPPER FUEL TANK AFT WEB WAS CRACKED AT BS 1372, LBL 80. REPAIRED THE WEB IAW EO MD11-5710-69413-A. MAJOR.

Part: SHEAR TIE — CRACKED (BS 2033) · airframe 100,752 hrs · 18,285 cycles

SHEAR TIE CRACKED, BS 2033. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT SHEAR TIE IAW DWG AJC7372, AND SRM 51-33-01.

Part: SKIN — CRACKED (RT WING LOWER) · airframe 100,752 hrs · 18,285 cycles

RIGHT WING, FIXED L/E LOWER SKIN WAS CRACKED AT XOS 720. REPAIRED THE WING LOWER SKIN IAW SRM 57-40-02, REPAIR 7, FIG 201. MAJOR.

Part: WEB — CRACKED (FLAP FAIRING) · airframe 100,752 hrs · 18,285 cycles

LEFT OTBD FLAP FAIRING LOWER FWD WEB WAS CRACKED. REMOVED, FABRICATED AND REPLACED THE FLAP FAIRING WEB IAW DWG ARC2152, AND SRM 51-31-01.

Part: WEB — CRACKED (BS 1372) · airframe 100,752 hrs · 18,285 cycles

RT OVERWING UPPER FUEL TANK AFT WEB WAS CRACKED, BS 1372, RBL 80. REPAIRED THE WEB IAW EO MD11-5710-69412-A. MAJOR.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 100,752 hrs · 18,285 cycles

LOWER STIFFENER IN THE RT MLG WW, BEHIND THE NR 3 HYDRAULIC RESERVOIR WAS CRACKED. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-31-01, AND SRM 51-33-01.

Part: DOOR FRAME — CRACKED (CENTER MLG DOOR) · airframe 80,180 hrs · 12,872 cycles

CENTER LANDING GEAR DOOR LOWER FWD CORNER WAS CRACKED. REMOVED AND REPLACED CENTER GEAR DOOR FWD LOWER FRAME IAW SRM 51-35-02.

Part: COVER — DAMAGED (RT ELEVATOR) · airframe 100,752 hrs · 18,285 cycles

RIGHT INBD ELEVATOR INBD UPPER L/E COVER PANEL DAMAGED. REPAIRED THE ELEVATOR COVER PANEL IAW EA 011-5520-01-A7405, REV IR, AND EO MD11-5520-69534-A.

Part: BRACKET — CRACKED (NR 1 PYLON) · airframe 100,705 hrs · 18,269 cycles

NR 1 UPPER PYLON OTBD WEB BRACKET, FWD OF PRECOOLER WAS CRACKED. REMOVED AND REPLACED THE BRACKET IAW SRM 51-31-01, AND 54-05-41.

Part: FLAP — OUT OF POSITION (L1 DOOR) · airframe 100,597 hrs · 18,229 cycles

R1 DOOR SLIDE INDICATOR NOT VIEWABLE IN INSPECTION WINDOW. SLIDE NEEDS ADJUSTED NEEDLE IN GREEN BAND DEFERRED PER MEL 52-10-3-1-2-1 M-641003 ASSIGNED. REPOSITIONED FLAP COVERING SLIDE GAUGE. PRESSURE WITHIN LIMITS.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 100,536 hrs · 18,216 cycles

RIGHT INBOARD ELEVATOR RIB PANEL ATTACHMENT TAB REPAIR AT XE = 125.8, DAMGED FLANGE. REPAIRED IAW PRELIMINARY EO 5520-68929-A.

Part: PANEL — LOOSE (L1 DOOR) · airframe 99,030 hrs · 17,817 cycles

PANEL ON THE L1 DOOR IS COMING OFF. SEATED THE PANEL ON THE L1 DOOR. OPS CHECKED OK.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 98,956 hrs · 17,805 cycles

L1 DOOR NITROGEN BOTTLE HAD LOW PRESSURE. SERVICED THE L1 DOOR NITROGEN BOTTLE IAW AMM 12-25-04-600-801, REV 89.01.

Part: MFC — FAULTED · airframe 98,910 hrs · 17,795 cycles

AT FL 310, CLIMBING TO FL 330, A LEVEL 2 ALERT FOR AIR SYS 2 OFF DISPLAYED. ALSO ON OVERHEAD PANEL NR 2 MAN FAIL LIGHT ILLUMINATED. SHORTLY THEREAFTER AIR SYS MANUAL ALERT DISPLAYED. RAN CHECKLIST. THE LEVEL 3 ALERT ENG 2 ANTI ICE DUCT. TROUBLESHOT IAW FIM 36-23-01, FOUND MFC FAULTING RAM FAILURE ON RTS. R & R THE MFC IAW AMM 36-23-01-400-801, OPS CHECKED NORMAL. RAN THE NR 2 ENGINE, NO FAULTS NOTED.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 97,954 hrs · 17,591 cycles

EMERGENCY LIGHT TEST FAILED. REMOVED & REPLACED THE POWER SUPPLY IAW AMM 33-51-01, OPS CHECKED NORMAL.

Part: SEALANT — SEPARATED (FUSELAGE) · airframe 97,506 hrs · 17,465 cycles

SEPARATION OF SHEET METAL ON FUSELAGE AFT OF L1 DOOR. PRESSURE CHECK FUSELAGE REF AMM 21-00-00 AND SMALL SEALANT LEAK. REAPPLIED SEALANT RE SREO M-5100-19877-H. LEAK CHECK OK. BS 515, 6" BELOW FLOOR LINE.

Part: THRUST REVERSER — CRACKED (NR 2 ENGINE) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, NR 2 ENGINE LT THRUST REVERSER ASSY. HAS TWO CRACKS COMMON TO THE FAN COWL LANDING. REPAIRED THE THRUST REVERSER ASSY IAW EA 011-7110-01-A6452 REV. I/R AND EO MD11-7830-61936-A.

Part: LONGERON SPLICE — CRACKED (49R) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, BS 6-100, LONGERON 49R SPLICE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED THE LONGERON SPLICE IAW EA 011-5310-01-A6445 REV. I/R AND EO MD11-5310-61950-A (MAJOR).

Part: FITTING — CORRODED (FUSELAGE) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE:3C, RIGID CARGO BARRIER FLOOR FITTING AT STA 488.812 BETWEEN X=19 TO X=27.5 HAS CORROSION. REPAIRED CORRODED RCB FLOOR FITTING AT STA 488.812, X=12 TO X=27.5 IAW EA 011-5310-01-A6436, REV I/R AND EO MD11-5320-61843-A, MINOR.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE:3CR, CB AREA FLOOR PANEL WSP0789-501 CORRODED X=-47-X=-75. REPAIRED FLOOR PANEL IAW EA 011-5310-01-A6437 REV IR AND EO MD11-5320-61842-A, MINOR.

Part: SKIN — CRACKED (TAILCONE) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, EXTERIOR SKIN CRACKED AT FWD TAILCONE RT UPPER AFT SIDE. REPAIRED IAW SRM 53-00-00 PG 213 FIG 204.

Part: LONGERON — CORRODED · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, CENTER ACCESSORY COMPARTMENT AT BS 6-73.5 LONGERON 49R AND SPLICE FITTING ARE CORRODED. REMOVED, FABRICATED AND REPLACED THE LONGERON AND SPLICE FITTING IAW DWG A6A7026 AND SRM 51-33-01.

Part: STRINGER — CRACKED (47) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, CENTER FUEL TANK STRINGER 47 IS CRACKED AT X-46. REPAIRED STRINGER 47 IAW SRM 57-10-03 REPAIR 1 FIG. 201. (MAJOR)

Part: SPAR CAP — CORRODED (LT WING) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, LEFT WING REAR SPAR UPPER CAP HAS CORROSION AT XORS. 1037-1044. REPAIRED THE SPAR CAP IAW EA 011-5710-01-A6434 REV I/R AND EO MD11-5710-61841-A.

Part: SKIN — CORRODED (BS 1942-1986) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, AFT EXTERIOR SKIN BETWEEN BS 1942-1986, LONGERON 26AL HAS AREAS OF CORROSION. REPAIRED THE SKIN IAW EA 011-5330-01-A6450 REV. I/R AND EO MD11-5330-61890-A.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE:3C, MAIN CABIN FLOOR PANEL NR 263DF HAS PUNCTURE AND EDGE DAMAGE. FABRICATED REPLACEMENT FLOOR PANEL 263DF IAW EO MD11-5320-27386-C, MAJOR.

Part: LONGERON — CRACKED (BS 1239-1250) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, MAIN CARGO LONGERON 17L IS CRACKED BETWEEN BS 1239 - 1250. REPLACED THE LONGERON IAW SRM 51-33-01 PG17.

Part: LONGERON — CRACKED (BS 1481-1501) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, LONGERON 25R CRACKED BS 1481 - 1501. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW DWG AEA0303 AND SRM 51-33-01.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE:3C, MAIN CABIN FLOOR PANEL 273DF HAS A PUNCTURE AND EDGE DAMAGE. FABRICATED REPLACEMENT FLOOR PANEL 273DF IAW EO MD11-5320-27386-C, MAJOR.

Part: SKIN — CORRODED (BS 2022-2055) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, EXTERIOR AFT SKIN PANEL LEFT SIDE AT BS 2022 TO 2055 HAS CORROSION. REPAIRED THE SKI IAW EA 011-5310-01-A6443 REV I/R AND EO MD11-5330-61884-A.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE:3C, L13L SPLICE FITTING CRACKED AT STA 1651. REMOVED FABRICATED AND INSTALLED REPLACEMENT SPLICE FITTING IAW DWG AFA7181 AND SRM 51-33-01, MINOR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE:3C, AFT LT FUSELAGE SKIN HAS CORROSION BETWEEN STA 2153-2163 AND L33L TO 35L. REPAIRED CORRODED FUSELAGE SKIN BETWEEN STA 2153-2163 AND L33L TO 35L IAW SRM 53-70-01, REPAIR 3, FIG 201, MAJOR.

Part: FAIRING — DAMAGED (STAB TO BODY) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE:3CL/H HORZ. STAB. WING TO BODY FAIRING ATTACH HOLE AT STA. Y=2007 AND LONG. 29TR IS ELONGATED.REPAIRED BODY ATTACH FAIRING SKIN HOLE AT SAID LOCATION IAW VT-SAA EA 011-5330-01-A6435 REV. I/R AND UPS EO MD11-5330-61929-A. (MAJOR)

Part: LONGERON — CHAFED (FUSELAGE) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE:3C, STA 1902-1921, LONGERON 42 RT IS CHAFED. REPAIRED CHAFED LONGERON 42 RT AT STA 1902-1921 IAW SRM 53-00-05, REPAIR 1, FIG 203, MAJOR.

Part: PAN — GOUGED (CARGO DOOR) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, MCD FWD PAN GOUGED AND DENTED BS 624 Z=35. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FWD PAN PER DWG ACA7301, SRM 51-33-01, AND 51-35-01.

Part: LONGERON SPLICE — CORRODED (FUSELAGE) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE:3C, CENTER CARGO LONGERON 47 RT SPLICE FITTING IS CORRODED AT STA 1811. R & R SPLICE FITTING AT STA 1811, LONGERON 47 RT IAW SRM 51-33-01, MINOR.

Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, LEFT INBD FLAP VANE LOWER SURFACE IS DELAMINATED. REMOVED AND REPLACED THE FLAP VANE IAW AMM 27-50-22-400-801.

Part: LONGERON — CORRODED (BS 1139) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, CENTER ACCESSORY BAY, LONGERON 51R IS CORRODED AT BS 1139. REMOVED AND REPLACED THE LONGERON IAW DWG AAA7086 AND SRM 51-33-01.

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE:3C CENTER CARGO LONGERON 40. RIGHT SPLICE FITTING IS CRACKED AT STA 5-123. REMOVED, FABRICATED AND REPLACED LONGERON 40 RT SPLICE FITTING AT STA 5-123 IAW DWG A5A7114 AND SRM 51-33-01, MINOR.

Part: LONGERON SPLICE — CORRODED (FUSELAGE) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE:3C, CENTER CARGO AT STA 1601-1621, LONGERON 46 RT SPLICE FITTING IS CORRODED. REMOVED, FABRICATED AND REPLACED LONGERON 46 RT SPLICE FITTING IAW AGA 3188 AND SRM 51-33-01, MINOR.

Part: VANE — CORRODED (LT WING TE FLAP) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, LEFT WING OTBD FLAP VANE NR 1 TRACK HAS CORROSION AT WEB INSIDE ACCESS HOLE. REMOVED AND REPLACED THE FLAP VANE IAW AMM 27-50-32-400-801.

Part: LONGERON SPLICE — CORRODED (FUSELAGE) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE:3C, CENTER CARGO AT STA 1601-1621, LONGERON 47 RT SPLICE FITTING IS CORRODED. REMOVED, FABRICATED AND REPLACED LONGERON 47 RT SPLICE FITTING AT STA 1601-1621 IAW DWG AGA3188 AND SRM 51-33-01, MINOR.

Part: SPAR CAP — CORRODED (LT WING) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, LEFT WING REAR SPAR UPPER CAP HAS CORROSION AT XORS 780 - 827. REPAIRED THE SPAR CAP IAW EA 011-5710-01-A6430 REV. I/R AND EO MD11-5710-61899-A.

Part: LONGERON SPLICE — CRACKED · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, LONGERON SPLICE 31L CRACKED STA 5-123. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT SPLICE IAW DWG A5A7112 AND SRM 51-33-01.

Part: LONGERON SPLICE — CORRODED (BS 1701-1721) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, CENTER CARGO BAY LONGERON 52 SPLICE FITTING IS CORRODED BETWEEN BS 1701 - 1721. REMOVED, FABRICATED AND REPLACED THE LONGERON SPLICE IAW DWG AFA7102 AND SRM 51-33-01.

Part: LONGERON — CORRODED (BS 1661) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, CENTER CARGO BAY LONGERON 52 AT BS 1661 IS CORRODED. REMOVED, FABRICATED AND REPLACED THE LONGERON IAW EA 011-5310-01-A6428 REV. I/R AND EO MD11-5310-61934-A (MAJOR).

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE:3C, CENTER CARGO LONGERON 39 RT SPLICE FITTING IS CRACKED AT STA 5-123. REMOVED, FABRICATED AND REPLACED LONGERON 39 RT SPLICE FITTING AT STA 5-123 IAW DWG A5A7114 AND SRM 51-33-01, MINOR.

Part: TORQUE TUBE — CHAFED (CABIN DOOR) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, L4 DOOR LOWER TORQUE TUBE CHAFED. REPAIRED THE TORQUE TUBE IAW EA 011-5210-01-A6432 REV. I/R AND EO MD11-5210-61827-A.

Part: SPAR CAP — CORRODED (RT WING) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, RT WING REAR SPAR CAP HAS CORROSION BETWEEN XORS 480 - 506. REPAIRED THE SPAR CAP IAW EA 011-5710-01-A6451 REV. I/R AND EO MD11-5710-61904-A.

Part: FRAME — CORRODED (BS 1841) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, AFT CARGO FRAME AT BS 1841, LONGERON 43R HAS CORROSION. REPAIRED THE FRAME IAW EA 011-5310-01-A6441 REV. I/R AND EO MD11-5310-61961-A. (MAJOR).

Part: BEAM — CRACKED (LT WING TE) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, LEFT WING T/E VERTICAL SUPPORT BEAM CRACKED NEAR XW 371. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT BEAM IAW DWG ARC0472 AND SRM 51-33-01.

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE:3C, CENTER CARGO LONGERON SPLICE 37 RT IS CRACKED AT STA 5-123. REMOVED, FABRICATED AND REPLACED LONGERON 37 RT SPLICE FITTING IAW DWG A5A7114 AND SRM 51-33-01, MINOR.

Part: FRAME — CRACKED (THRUST REVERSER) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE:3C, NR 2 ENGINE RT THRUST REVERSER FWD CASCADE ATTACH FRAME IS CRACKED AT THE NR 4 POSITION. REPAIRED IAW EA 011-7830-01-A6446 REV. I/R AND EO MD11-7830-61952-A. (MINOR).

Part: FRAME — CRACKED (TAIL CONE) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, FWD TAIL CONE FRAME IS CRACKED AT UPPER TAIL CONE LATCH. REPAIRED THE FRAME IAW DWG AKC7539 AND SRM 53-80-07 REPAIR 4.

Part: FRAME — CRACKED (THRUST REVERSER) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE:3C, NR 2 ENGINE LT T/R CASCADE ATTACH FRAME IS CRACKED AT POSITION 15. REPAIRED CRACKED NR 2 ENGINE LT T/R CASCADE ATTACH FRAME IAW CMM 7832-35, REPAIR 34, MINOR.

Part: SKIN — CHAFED (RT WING) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, RIGHT WING FIXED L/E SKIN IS CHAFED AT XIS. 717.66 TO 178. REPAIRED THE RT WING L/E SKIN IAW EA 011-5730-01-A6429. (MAJOR)

Part: STRINGER — CRACKED (LT WING) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, LT WING FIXED L/E UPPER STRINGER IS CRACKED AT XOS 666. REPAIRED THE STRINGER IAW SRM 57-40-03 REPAIR 2, FIG. 202. MAJOR REPAIR.

Part: SUPPORT — CRACKED (RT WING) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, RIGHT WING T/E SUPPORT TEE CRACKED NEAR WS XW247. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT SUPPORT TEE IAW DWG ARC3111 AND SRM 51-31-01.

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, UPPER FWD RUDDER MIDDLE BALANCE WEIGHT HAS CORROSION AND MISSING PRIMER. REPAIRED IAW EA 011-5440-01-A6448 REV. I/R AND EO MD11-5540-61857-A (MINOR).

Part: DOUBLER — CRACKED (LT WING) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, LT WING FIXED L/E BEADED DOUBLER IS CRACKED AT XOS 629 - 633. REPAIRED THE DOUBLER IAW SRM 57-40-02 REPAIR 15 FIG. 203. MAJOR REPAIR.

Part: INTERCOSTAL — CRACKED (LT MLG WW) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE:3C, LEFT MLG W/W AT BS 1441 - 1461 X 31.5, Z -56 CYCLINDER SUPPORT INTERCOSTAL IS CRACKED. REPAIRED IAW SRM 53-40-12 REPAIR 3 FIG. 201. (MAJOR).

Part: SKIN — CHAFED (RT WING AILERON) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, RT WING I/B AILERON LOWER SKIN L/E IS GOUGED. REMOVED AND REPLACED SECTION OF SKIN IAW DWG ARC1250 AND SRM 51-31-01.

Part: TRUNNION — CRACKED (BS 583) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, NLG RIGHT TRUNNION FITTTING CRACKED ADJACENT TO TRUNNION PIN BOSS. TRUNNION REPAIRED IAW SRM 53-10-14 REPAIR 2 FIG. 202. (MAJOR)

Part: DOOR — GOUGED (THRUST REVERSER) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, NR 3 OTBD THRUST REVERSER LOWER AFT ACCESS DOOR GOUGED. DOOR REPAIRED IAW EA 011-7110-01-A6439 REV. IR AND EO MD11-7830-61835-A.

Part: ACCESS DOOR — GOUGED (THRUST REVERSER) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, NR 2 ENGINE RT THRUST REVERSER ASSY HAS A GOUGED LOWER AFT ACCESS DOOR. REPAIRED IAW EA 011-7110-01-A6442 REV. I/R AND EO MD11 7830-61931-A.

Part: FITTING — CHAFED (RT WING) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE:3CR/H WING PYLON ENGINE MOUNT TRUSS FITTING HAS CHAFED. REPAIRED IAW EA 011-5440-01-A6427 REV. I/R AND EO MD11-5440-61796-A.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, RIGHT WING REFUELING PANEL IB SUPPORT BRACKET CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT PANEL SUPPORT BRACKET IAW DWG ARB2382 AND SRM 51-31-01.

Part: TRUSS FITTING — CHAFED (RT WING PYLON) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, RIGHT WING PYLON ENGINE MOUNT TRUSS FITTING CHAFED AT YWN 200.2. REPAIRED THE TRUSS FITTING IAW EA 011-5440-01-A6431 REV. I/R AND EO MD11-5440-61822-A.

Part: STRUCTURE — CHAFED (NR 3) · airframe 96,673 hrs · 17,230 cycles

INSPECTION TYPE: 3C, NR 3 ENGINE OB FAN COWL FWD HINGE ARM CHAFED. REPAIRED PER EA 011-7110-01-A6426 REV. IR AND EO MD11-7110-61774-A.

Part: DOUBLER — CRACKED (RT WING) · airframe 96,669 hrs · 17,227 cycles

INSPECTION TYPE: 3C, RT WING FIXED L/E BEADED DOUBLER IS CRACKED AT XOS 542 - 547. REPAIRED THE DOUBLER IAW SRM 57-40-02 REPAIR 15 FIG. 203. MAJOR REPAIR.

Part: DOUBLER — CRACKED (RT WING) · airframe 96,669 hrs · 17,227 cycles

INSPECTION TYPE: 3C, RIGHT WING FIXED L/E BEADED DOUBLER IS CRACKED AT XOS 610 - 616. REPAIRED THE DOUBLER IAW SRM 57-40-02 REPAIR 15 FIG. 203. (MAJOR)

Part: SKIN — DAMAGED (RT WING) · airframe 96,472 hrs · 17,169 cycles

RIGHT WING FIXED LE SKIN DAMAEGD AT XIS 207.844. COMPLETED TEMP REPAIR PER EO MD11-5720-59485-B

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 96,178 hrs · 17,108 cycles

EMERGENCY LIGHT BATTERY 1 LOW. R & R EMERGENCY LIGHT BATTERY IAW MM 133-51-01 TESTS GOOD EFF SOURCE 33511001.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 95,773 hrs · 17,021 cycles

EMERGENCY LIGHT BATTERY LO ALERT WHEN EMERGENCY LIGHTS TESTED. R & R EMERGENCY LIGHT BATTERY POWER SUPPLY UNIT. OPS CHECK GOOD IAW AMM 33 51 01 EFF SOURCE IPC 33-51-10-01-003.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHTS) · airframe 95,759 hrs · 17,019 cycles

FOUND EMERGENCY LIGHT TEST SWITCH INOPERATIVE. R & R TEST SWITCH IAW WDM 33-51-01, REV 86.00, 03-23-16. OPS-CHECK SATISFACTORY.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 95,660 hrs · 16,999 cycles

DURING COCKPIT PREFLIGHT TEST OF EMERGENCY LIGHT SYS, DISPLAYED "EMERGENCY LIGHT BATTERY 1 LOW, LEVEL 1 ALERT. PERFORMD OPS CK OK IAW MM 33-51-01, P 501.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 95,409 hrs · 16,947 cycles

IN PASSENGER AREA LT SIDE AFT LENS FOR AFT L/E EMERGENCY LIGHT HAS FALLEN OFF, REF MM 33-52-02-000-801. RESECURED LENS AND REINSTALLED COVER.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 95,388 hrs · 16,938 cycles

PNEUMATIC BOTTLE FOR L1 DOOR IS BELOW GREEN PRESSURE BAND, SERVICED L1 DOOR PNEUMATIC STORAGE SYS REF AMM 12-25-04.

Part: SKIN — CRACKED (RT WING) · airframe 95,086 hrs · 16,873 cycles

CRACK IN LOWER RT WING L/E AT BS X15 204.094 6.6" IN LENGTH. CUTOUT MEASURES 7.1 X 6.6" PERFORM FILLER-DOUBLER REPAIR IAW EO MD11-5720-59485-A.

Part: LIFE RAFT — LOOSE (L1 DOOR) · airframe 95,002 hrs · 16,838 cycles

RAFT PACK AT THE L1 DOOR LOOSE. REPOSITIONED RAFT PACK COVER IAW AMM 25-61-01.

Part: SLIDE — LOOSE (PAX DOOR) · airframe 94,726 hrs · 16,776 cycles

SLIDE PACK HOUSING ON LT MAIN ENTRY DOOR IS LOOSE AT TOP FORWARD SIDE. REPOSITIONED LT ENTRY DOOR SLIDE PACK COVER, OPS CK NORMAL.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 93,819 hrs · 16,541 cycles

EMERGENCY EXIT LIGHT TEST FAIL, "BATTERY 1 LOW" MESSAGE DISPLAYED. EMERGENCY LIGHTS BATTERY POWER SUPPLY REPLACED IAW AMM 33-51-01-000-802. NIL HELP. DEFERRED IAW MEL 33-50-4. DEI LOG UPDATED, PLACARDS INSTALLED. DMP PROCEDURES C/OUT. PN ON, OFF 60-4411-5, SN ON 0095, SN OFF 1018.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 93,322 hrs · 16,386 cycles

R1 ENTRY DOOR EMERGENCY ACCUMMULATOR BOTTLE LOW PRESSURE SERVICED R1 ENTRY DOOR PNEUMATIC BOTTLE AS REQUIRED IAW AMM 12-25-04.

Part: LIGHT — INOPERATIVE (CABIN)

L1 DOOR EMERGENCY EXIT LIGHT LENS WILL NOT STAY SECURED. R & R EMERGENCY EXIT LIGHT ASSEMBLY IAW 33-27-05. OPS CHECKED GOOD.

Part: CYLINDER — OUT OF ADJUST (MLG)

AFTER TAKE OFF, GEAR HANDLE WOULD NOT MOVE TO UP POSITION. ACCOMPLISHED CHECKLIST. GEAR RETRACTED. GROUND SENSOR SWITCHED TO FLIGHT MODE. FOUND LANDING GEAR CONTROL MECHANISM ANTI-RETRACT, CABLE OUT OF ADJUSTMENT. ACCOMPLISHED ADJUSTMENT. REF AMM 32-50-00. R & R TRIM INTERLOCK CYCLINDER, PRECAUTIONARY REF AMM 32-31-04. ACCOMPLISHED LANDING GEAR, OPERATION REF AMM 32-31-00. ALL INDICATIONS NORMAL.

Part: DOUBLER — CRACKED (RT WING STRINGER) · airframe 92,756 hrs · 16,211 cycles

INSPECTION 3C, REPAIR DOUBLER CRACKED ON RT WING FIXED L/E LOWER STRINGER DOUBLER NEAR XOS 906, INSTALLED NEW REPAIR AT RT WING FIXED L/E STRINGER DOUBLER IAW SRM 57-40-03, REPAIR 1, FIG 201.

Part: STRAP — CRACKED (RT WING) · airframe 92,756 hrs · 16,211 cycles

INSPECTION 3C, RT WING L/E SKIN SPLICE STRAP CRACKED AT XOS 906. FABRICATED AND INSTALLED RT WING L/E SKIN SPLICE STRAP IAW DWG ARB3954 AND SRM 51-33-01.

Part: TRUNNION — CORRODED (MLG) · airframe 92,756 hrs · 16,211 cycles

INSPECTION 3C, CENTER LANDING GEAR LEFT TRUNNION FITTING SHEAR PIN HOLE PITTED. ACCOMPLISHED REPAIR ON CENTER LANDING GEAR LT TRUNNION FITTING SHEAR PIN HOLE IAW EA 011-5340-01-A5634, REV I/R AND EO 5340-55874-A.

Part: SUPPORT FITTING — GOUGED (ELEVATOR) · airframe 92,756 hrs · 16,211 cycles

INSPECTION 3C, LEFT HORIZONTAL STABILIZER INBD ELEVATOR HINGE SUPPORT FITTING HAS GOUGE DAMAGE ACCOMPLISHES PERMANENT BLEND REPAIR ON LT HORIZONTAL STABILIZER INBD ELEVATOR HINGE SUPPORT FITTING IAW EA 011-5510-01-A5643, REV I/R AND EO 5550-55888-A.

Part: TRUNNION — CORRODED (NLG) · airframe 92,756 hrs · 16,211 cycles

INSPECTION 3C, RT NLG TRUNNION SUPPORT FITTING HOLE HAS CORROSION ACCOMPLISHED PERMANENT REPAIR ON RT NLG SUPPORT FITTING HOLE IAW VT-SAA EA-011-5310-01-A5642, REV I/R AND EO 5310-55872-A.

Part: LONGERON — CORRODED (BS 1541) · airframe 92,756 hrs · 16,211 cycles

INSPECTION 3C, LONGERON 48L CORRODED BEYOND LIMITS BS 1541. REPLACED SECTION OF LONGERON 48L BETWEEN BS 1541-1556 IAW SRM 53-00-05, REPAIR 1, FIG 202.

Part: SPAR CAP — CORRODED (RT WING) · airframe 92,756 hrs · 16,211 cycles

INSPECTION 3C, RIGHT WING REAR SPAR UPPER CAP AFT HORIZONTAL FLANGE HAS CORROSION BETWEEN STA XORS 799 TO 830. ACCOMPLISHED PERMANENT REPAIR ON RT WING REAR SPAR UPPER CAP AFT HORIZONTAL FLANGE STA XORS 799 TO 830 IAW EA 011-5710-01-A5639 REV I/R AND EO 5710-55881-A.

Part: FRAME — CRACKED (BS 2092) · airframe 92,756 hrs · 16,211 cycles

INSPECTION 3, ACFT BODY FRAME ANGLE CRACKED. REPAIRED IAW SRM 53-70-07, REPAIR 1, FIGURE 201.

Part: SPAR CAP — CORRODED (LT WING) · airframe 92,756 hrs · 16,211 cycles

INSPECTION 3C, LT WING REAR SPAR UPPER CAP AFT HORIZONTAL FLANGE HAS CORROSION BETWEEN XORS 480 TO 510. ACCOMPLISHED PERMANENT REPAIR ON LT WING REAR SPAR UPPER CAP AFT HORIZONTAL FLANGE STA XORS 480 TO 510 IAW EA 011-5710-01-A5640, REV I/R AND 5710-55878-A.

Part: STRINGER — CRACKED (RT WING) · airframe 92,756 hrs · 16,211 cycles

INSPECTION 3C, CRACKED STRINGER INSIDE RT WING FIXED L/E AT XOS 665. REPAIRED THE STRINGER IAW SRM 57-40-03, REPAIR 2, FIG 202.

Part: DOUBLER — CRACKED (RT WING) · airframe 92,756 hrs · 16,211 cycles

INSPECTION TYPE:3C, BEADED DOUBLER CRACKED IN RT WING FIXED L/E AT XOS 665, REPAIRED THE DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 203.

Part: SKIN — CHAFED (LT WING) · airframe 92,756 hrs · 16,211 cycles

INSPECTION 3C, CHAFE DAMAGE ON REPAIR DOUBLER ON LT WING L/E EXTERIOR SKIN ANTI-ICE DUCT SLOT. REMOVED DOUBLER AND INSTALLED NEW REPAIR IAW SRM 57-40-01 REPAIR 10 FIG 201.

Part: SUPPORT STRAP — CRACKED (LT WING) · airframe 92,756 hrs · 16,211 cycles

INSPECTION 3C, LEFT WING OTBD FLAP INBD HINGE TENSION STRAP SUPPORT CRACKED STA XW 486.403. R & R LT WING OTBD FLAP INBD HINGE TENSION STRAP SUPPORT IAW EA 011-5710-01-A5632 AND EO 5710-55875-A.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 92,756 hrs · 16,211 cycles

INSPECTION 3C, RIGID CARGO BARRIER SUPPORT FLOOR PANEL HAS CORROSION AT STA Y=480, X=-27.500. ACCOMPLISHED PERMANENT REPAIR ON RIGID CARGO BARRIER SUPPORT FLOOR PANEL STA Y=480, X=-27.500 IAW EA 011-5310-01-A5629, REV I/R AND EO 5320-55788-A.

Part: SEAT TRACK — CORRODED (BS 466-473) · airframe 92,756 hrs · 16,211 cycles

INSPECTION 3C, COURIER AREA SEAT TRACK CORRODED BS 466-473, LBL 9. REPAIRED THE SEAT TRACK IAW EA 011-5310-01-A5630, REV IR AND EO 5310-55907-B.

Part: PITOT TUBE — DIRTY (CAPTAIN'S SIDE)

AT APPROX 110 KTS, CAPTAIN`S SIDE, UNREALIABLE AIRSPEED, RAN CHECKLIST AND LANDED NORMALLY ON CAD C2. PURGED CAPT PITOT TUBE IN REF TO MM 34-11-00. FOUND VERY LITTLE DEBRIS IAW TECH. R & R CAPT PITOT TUBE DUE TO SUSPECTED DISTORTION. OPS CHECK AND LEAK CHECK GOOD. REF MM 34-11-01 & 34-11-00.

Part: STRINGER — CRACKED (LT WING) · airframe 90,689 hrs · 15,602 cycles

INSPECTION TYPE:1C, STRINGER 15 CRACKED IN LT WING NEAR PANEL 534AT XORS433 -435. REPAIRED STRINGER IAW EA 011- 5700-01-A4825, REV IR AND EO MD11-5710-51771-A.

Part: STRINGER — CRACKED (LT WING) · airframe 90,689 hrs · 15,602 cycles

INSPECTION TYPE:1C, STRINGER 11 CRACKED AT FUEL ACCESS 536AB INBD OF NR 1 TANK LT WING. REPAIRED LT WING UPPER STRINGER S-11 FROM XORS 683 TO 713 IAW EA 011-5710-01-A4822 REV I/R, EO MD11-5710-51785-A.

Part: STRINGER — CRACKED (RT WING) · airframe 90,689 hrs · 15,602 cycles

INSPECTION TYPE: 1C, RT WING STRINGER 11 CRACKED NEAR ACCESS PANEL 636AB BETWEEN XOS 683 -713. REPAIRED RT WING STRINGER 11 BETWEEN XOS 683 - 713 IAW STASA EA 011- 5700-01-A4826 REV IR AND EO MD11-5710-51644-A.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 90,689 hrs · 15,602 cycles

INSPECTION TYPE: 1C, LT WING FIXED L/E SUPPORT BRACKET CRACKED AT AFT END JUST OTBD OF NR 7 SLAT TRACK XOS 559. REMOVED FABRICATED AND INSTALLED REPLACEMENT SUPPORT BRACKET IAW DWG ARB1162, SRM 51-31-01 AND 51-33-01. (MINOR)

Part: STRINGER — CRACKED (RT WING) · airframe 90,689 hrs · 15,602 cycles

INSPECTION TYPE:1C, RT WING STRINGER 15 CRACKED NEAR XORS 433. REPAIRED RT WING STRINGER 15 AT XORS433 IAW STASA EA 011-5710-01- A4828 REV IR AND IPXA EO MD11-5710-51790-A FAA 8100-9.

Part: DOUBLER — CRACKED (RT WING) · airframe 90,689 hrs · 15,602 cycles

INSPECTION TYPE: 1C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 613 REPAIRED RT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS 610 -616 IAW SRM 57-40-02 REPAIR 15 FIG 206. (MAJOR)

Part: WEB — CRACKED (COCKPIT) · airframe 90,689 hrs · 15,602 cycles

INSPECTION TYPE:1C, COCKPIT FLOOR WEB CRACKED AT OBSERVERS SEAT POSITION. REPAIRED IAW SRM 53-10-51, REPAIR 1, FIG 202. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 90,689 hrs · 15,602 cycles

INSPECTION TYPE :1C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 544 REPAIRED RT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS542 -547 IAW SRM 57-40-02. REPAIR 15 FIG 206. (MAJOR)

Part: SKIN — CHAFED (RT WING) · airframe 90,689 hrs · 15,602 cycles

INSPECTION TYPE:1C, RT WING FIXED L/E SKIN REPAIR DOUBLER FOUND CHAFED FROM XOS 839 TO XOS 867. REPAIRED RT WING FIXED L/E CHAFED REPAIR DOUBLER WITH REPLACEMENT REPAIR FROM XOS 839 TO XOS 867 REF STASA EA 011-5730-01-A4830 REV I/R, EO MD11-5730-51806-A AND 8100-9.

Part: STRINGER — CRACKED (RT WING) · airframe 90,689 hrs · 15,602 cycles

INSPECTION TYPE:1C, RT WING FIXED L/E COMPT PANEL 626FB STRINGER LANDING AND PREVIOUS REPAIR FILLER CRACKED AT XOS 906.5807. REPAIRED IAW SRM 57-40-03, REPAIR. 1, FIG 201. (MAJOR REPAIR)

Part: TRUNNION — CRACKED (NLG) · airframe 90,689 hrs · 15,602 cycles

INSPECTION TYPE:1C, NLG LEFT TRUNION FITTING CRACKED. REPAIRED NLG LT TRUNION FITTING IAW STASA EA 011-5310-01-A4818, REV IR AND EO MD11-5310-51773-A.

Part: DOUBLER — CRACKED (RT WING) · airframe 90,689 hrs · 15,602 cycles

INSPECTION TYPE: 1C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 554. REPAIRED RT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS 551-555 IAW SRM 57-40-02 REPAIR 15, FIG 206. (MAJOR)

Part: DOUBLER — CRACKED (RT WING) · airframe 90,689 hrs · 15,602 cycles

INSPECTION TYPE: 1C, RT WING FIXED L/E BEADED DOUBLER CRACKED AT XOS 653.7174. REPAIRED IAW SRM 57-40-02, REPAIR 15, FIG 203.

Part: DOUBLER — CRACKED (RT WING) · airframe 90,689 hrs · 15,602 cycles

INSPECTION TYPE:1C, RT WING FIXED L/E BEADED DOUBLER CRACKED AT XOS 880.7835. REPAIRED IAW SRM 57-40-02, REPAIR 15, FIG 203. MAJOR REPAIR.

Part: FITTING — DAMAGED (NLG) · airframe 90,689 hrs · 15,602 cycles

INSPECTION TYPE: 1C, WHILE REPAIRING CRACKED NLG LT TRUNION FITTING FOUND BUSHING IN LT SIDE LOAD FITTING FASTENER HOLE COMMON TO LT TRUNION FITTING. REPAIRED BUSHED FASTENER HOLE IAW STASA EA 011-5310-01-A4818, REV IR AND EO MD11-5310-51773-A.

Part: DOUBLER — CRACKED (RT WING) · airframe 90,689 hrs · 15,602 cycles

INSPECTION TYPE: 1C, RT WING FIXED L/E COMPT BEADED DOUBLER CRACKED AT XOS 711.7851. REPAIRED IAW SRM 57-40-02, REPAIR 15, FIG 203.

Part: LANDING GEAR — UNKNOWN (CENTER)

CENTER GEAR FAILED TO EXTEND MANUALLY. PERFORMED OPS TEST LANDING GEAR ALTERNATE RELEASE SYS IAW MM 32-32-00-710-803. ALL TESTS PASS OK FOR SVC.

Part: LANDING GEAR — INOPERATIVE (CENTER)

CENTER GEAR FAILED TO EXTEND MANUALLY. OPEN

Part: LONGERON — CORRODED (BS 1701 L51R) · airframe 87,883 hrs · 14,941 cycles

INSPECTION TYPE: 4C, CORROSION ON LONGERON 51R UNDER TRANSVERSE FRAME STA 1701. REPAIRED LONGERON IAW EA 011-5310-01-A3920 REV I/R AND EO MD11-5310-47526-A.

Part: LONGERON SPLICE — CORRODED (BS 1848 L48L) · airframe 87,883 hrs · 14,941 cycles

INSPECTION TYPE: 4C, CORROSION ON SPLICE OF LONGERON 48L BETWEEN TRANSVERSE FRAME STA 1848 AND 1853. REPAIRED LONGERON 48 BETWEEN TRANSVERSE FRAME STA 1841-1853 BY PART REPLACEMENT REF SRM 51-33-01, PARA 8, PG 30 AND DWGS NGA6314 AND AGA7438.

Part: SUPPORT ANGLE — CORRODED (BS 1761 L51L/R) · airframe 87,883 hrs · 14,941 cycles

INSPECTION TYPE:4C, CORROSION TRANSVERSE FRAME SUPPORT ANGLE AT FR STA 1761 BETWEEN LONGERON 51L AND 51R. ACCOMPLISHED REPAIR IAW SRM 53-00-06, REPAIR 1, FIG 202.

Part: LONGERON — CORRODED (BS 1701-1721) · airframe 87,883 hrs · 14,941 cycles

INSPECTION TYPE: 4C, CORROSION ON LONGERON 48R UNDER TRANSVERSE BS 1680 AND 1701 TO 1721. ACCOMPLISHED EA 011-5300-01-A3910 I/R.

Part: LONGERON — CORRODED (BS 1541 L43L) · airframe 87,883 hrs · 14,941 cycles

INSPECTION TYPE: 4C, CENTER CARGO BAY LONGERON 43L EXFOLIATED BETWEEN FR STA 5-113 TO 1541. REPAIRED CENTER CARGO COMPT LONGERON 43L BETWEEN FR STA 5-113 TO 1541 REF STA, SA, EA 011-5310-01-A3916 REV I/R AND EO MD11-5310- 01-A3916.

Part: LONGERON SPLICE — CRACKED (BS 1531 L7L) · airframe 87,883 hrs · 14,941 cycles

INSPECTION TYPE: 4C, LONGERON 7L, SPLICE AT FS 1531 CRACKED. REMOVED FABRICATED AND INSTALLED LONGERON SPLICE AT FS 1531 IAW DWG A5A7112 AND 51-33-01, PG 45, 30, 31.

Part: BULKHEAD — CRACKED (RT WING) · airframe 87,883 hrs · 14,941 cycles

INSPECTION TYPE: 4C, RIGHT WING FUEL TANK BULKHEAD WEB LIGHTENING HOLE LIP CRACKED TWO PLACES AT STA XORS 433. REPAIRED IAW EA 011-5710-01-A3906 REV I/R AND EO MD11- 5710-47471-A.

Part: LONGERON SPLICE — CORRODED (FS 1541 L48R) · airframe 87,883 hrs · 14,941 cycles

INSPECTION TYPE:4C, CENTER CARGO COMPT BILGE AREA, EXFOLIATED CORROSION AT LONGERON 48R BETWEEN STA 1531/5-113 AND STA 1541. REPLACED LONGERON 48R SPLICE BY FABRICATION AND INSTALLATION REF DWG N5A677A AND A5A7125.

Part: LONGERON — CORRODED (BS 1461) · airframe 87,883 hrs · 14,941 cycles

INSPECTION TYPE: 4C, LONGERON 16R BETWEEN FS1461-1481 HAS EXFOLIATION CORROSION. REPAIRED LONGERON 16R BETWEEN FS1461-1481 REF EA 011-5310-01- A3896 AND EO MD11-5310-47319-A.

Part: FRAME — CORRODED (BS 1801 L26L) · airframe 87,883 hrs · 14,941 cycles

INSPECTION TYPE: 4C, FUSELAGE FRAME AT FS 1801 AND LONGERON 26L HAS EXFOLIATION CORROSION. REPAIRED IAW EA 011-5310-01-A3905 REV I/R AND EO MD11-5310-47487-A.

Part: DRIVE CHAIN — BROKEN (L1 DOOR) · airframe 87,883 hrs · 14,941 cycles

INSPECTION TYPE: 4C L-1 DOOR INNER EMERGENCY DRIVE CHAIN FOUND BROKEN. R & R L-1 DOOR EMERGENCY DRIVE CHAIN REF MFG DWG NBA6258 AND AMM 52-11-02-5.

Part: INTERCOSTAL — CRACKED (NR 2 INLET DUCT) · airframe 87,883 hrs · 14,941 cycles

INSPECTION TYPE:4C, VERTICAL WEB CRACKED AT 12:00 POS ON RT SIDE OF NR 2 ENGINE INLET DUCT AT FWD FACE OF LOWER VERT STAB REAR SPAR INSIDE PNL 364RR. REPAIRED INTERCOSTAL ON RT SIDE OF NR 2 ENGINE INLET DUCT AT FWD FACE OF LOWER VERT STAB REAR SPAR AT PNL 364RR ACCESS.

Part: WEB — CRACKED (R3 DOOR FRAME) · airframe 87,883 hrs · 14,941 cycles

INSP TYPE: 4C, R3 DOOR JAMB FWD LOWER LIGHTNING HOLE IS CRACKED. REPAIRED R3 DOOR JAMB FWD LOWER LIGHTNING HOLE REF SRM 53-40-15, REPAIR 3, FIG 201.

Part: WEB — CRACKED (R3 DOOR FRAME) · airframe 87,883 hrs · 14,941 cycles

INSPECTION TYPE: 4C, R3 DOOR JAMB AFT LOWER LIGHTNING HOLE IS CRACKED. REPAIRED R3 DOOR JAMB AFT LOWER LIGHTNING HOLE REF SRM 53-40-15, REPAIR3, FIG 201.

Part: FITTING — CRACKED (LH WING TIP) · airframe 87,883 hrs · 14,941 cycles

INSPECTION TYPE: 4C, LT LOWER WINGLET FWD MOUNT FITTING CRACKED. R & R LT LOWER WINGLET FWD AND AFT MOUNT FITTINGS REF EO MD11-5720-27680-C, APPX D.

Part: WEB — CRACKED (L3 DOOR FRAME) · airframe 87,883 hrs · 14,941 cycles

INSPECTION TYPE:4C, L3 DOOR FWD JAMB LOWER LIGHTNING HOLE IS CRACKED. REPAIRED L3 DOOR FWD JAMB LOWER LIGHTNING HOLE REF SRM 53-40- 15, REPAIR 3, FIG 201.

Part: WEB — CRACKED (L3 DOOR FRAME) · airframe 87,883 hrs · 14,941 cycles

INSPECTION TYPE: 4C, L3 DOOR JAMB AFT LOWER LIGHTNING HOLE IS CRACKED. REPAIRED L3 DOOR JAMB AFT LOWER LIGHTNING REF SRM 53-40-15, REPAIR 3, FIG 201.

Part: DOUBLER — CRACKED (LT WING) · airframe 87,883 hrs · 14,941 cycles

INSPECTION TYPE: 4C, LT WING FIXED L/E BEADED DOUBLER CRACKED BETWEEN XFS 730-736. REPAIRED LT WING FIXED L/E BEADED DOUBLER BETWEEN XFS 730-736 REF EO MD11-5730-42916-D.

Part: SPLICE — CRACKED (LT WING L/E) · airframe 87,883 hrs · 14,941 cycles

INSPECTION TYPE: 4C, LT WING FIXED L/E SKIN SPLICE STRAP AT XFS907 IS CRACKED. REPLACED LT WING FIXED L/E SKIN SPLICE STRAP AT XFS907 REF SRM 51- 33-01.

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 87,883 hrs · 14,941 cycles

INSPECTION TYPE: 4C, RT WING FIXED L/E BEADED DOUBLER CRACKED BETWEEN XFS669-675. REPAIRED RT WING FIXED L/E COMPT BEADED DOUBLER BETWEEN CRACKED BETWEEN XFS669-675 REF EO MD11-5730-42916-D.

Part: DOUBLER — CRACKED (LT WING L/E) · airframe 87,883 hrs · 14,941 cycles

INSPECTION TYPE: 4C, LT WING FIXED L/E COMPT BEADED DOUBLER CRACKED BETWEEN XOS 537-2676 TO 542. REPAIRED LT WING FIXED L/E COMPT BEADED DOUBLER BETWEEN XOS537-2676 TO XOS542 REF EO MD11-5730-42916-D.

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 87,883 hrs · 14,941 cycles

INSPECTION TYPE: 4C, RT WING FIXED L/E BEADED DOUBLER CRACKED BETWEEN XFS760-765. REPAIRED RT WING FIXED L/E COMPT BEADED DOUBLER BETWEEN XFS760-765 REF MD11-5730-42916-D.

Part: RIB — CRACKED (LT WING L/E) · airframe 87,883 hrs · 14,941 cycles

INSPECTION TYPE:4C, LH WING FIXED LE COMPT RIB CRACKED AT STA XOS801.840. REPAIRED LT WING FIXED L/E COMPT RIB AT STA XOS801.840 REF STA, SA, EA 011-5700-01-A3909 AND EO MD11-5720-47459-A.

Part: FITTING — WORN (VERTICAL STAB) · airframe 87,883 hrs · 14,941 cycles

INSPECTION TYPE: 4C, ONE SHEARED FASTENER ON FWD SIDE LOWER FASTENER OF THE NR 4 BANJO FITTING LT SIDE. REPAIRED VERT STAB AFT SPAR NR 4 BANJO FITTING LT SIDE REF EO MD11-5530-46641-A APPX C AND E.

Part: DOUBLER — CRACKED (LT WING L/E) · airframe 87,883 hrs · 14,941 cycles

INSPECTION TYPE: 4C, LT WING FIXED L/E COMPT BEADED DOUBLER CRACKED BETWEEN XOS 896.878- 901-770. REPAIRED L/E WING FIXED L/E COMPT BEADED DOUBLER BETWEEN XOS896.878- XOS901-770 REF EO MD11-5730-42916-D.

Part: FITTING — WORN (VERTICAL STAB) · airframe 87,883 hrs · 14,941 cycles

INSPECTION TYPE: 4C, ONE LOOSE FASTENER ON FWD SIDE LOWER FASTENER OF THE NR 4 BANJO FITTING RT SIDE. REPAIRED VERTICAL STAB AFT SPAR NR 4 BANJO FITTING RT SIDE, REF EO MD11-5530-46641-A APPX B AND D.

Part: DOUBLER — CRACKED (LT WING L/E) · airframe 87,883 hrs · 14,941 cycles

INSPECTION TYPE: 4C, LT WING FIXED L/E BEADED DOUBLER CRACKED BETWEEN XOS643.5904 AND XOS 648.2294. REPAIRED LT WING FIXED L/E BEADED DOUBLER BETWEEN XOS 643.5904 AND XOS 648.2294 REF EO 5730-42916-D.

Part: RIB — CRACKED (LT WING L/E) · airframe 87,883 hrs · 14,941 cycles

INSPECTION TYPE:4C, LT WING FIXED L/E COMPT RIB CRACKED AT STA XOS795.743. REPAIRED LT WING FIXED L/E COMPT RIB AT XOS795.743 REF STA, SA, EA 011 -5700-01-A3908 REV I/R AND EO MD11-5730-47450-A.

Part: DOUBLER — CRACKED (RT WING L/E) · airframe 87,883 hrs · 14,941 cycles

INSPECTION TYPE: 4C, RT WING FIXED L/E BEADED DOUBLER CRACKED BETWEEN XFS 730-736. REPAIRED RT WING FIXED L/E COMPT BETWEEN XFS730-736 REF EO MD11- 5730-42916-D.

Part: LIGHT — MALFUNCTIONED (COCKPIT)

ON PREFLIGHT, LEVEL 1 EMERGENCY LIGHT BATTERY 1 LOW. PERFORMED EMERGENCY LIGHT TEST IAW MM 33-51-00. OPS CHECKED GOOD. THIS CLEARS M462036.

Part: LIGHT — INOPERATIVE (L1 DOOR)

L1 DOOR HANDLE EMERGENCY LIGHT ASSY INOPERATIVE. R & R L1 DOOR EMERGENCY DOOR HANDLE LIGHT ASSY IAW MM 33-52-02-2.

Part: CONTROLLER — FAILED (EMERGENCY LIGHTS)

EMERGENCY BATTERY LIGHT, LOW ALERT. R & R MSC IAW AMM 21-42-01, PERFORMED MSC R-T-R TEST, ALL PASSED. PERFORMED EMERGENCY LIGHT SYS OPS TEST IAW AMM 33-51-01, ALL PASSED. THIS CLOSED DMI, STICKER REMOVED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHT BATTERY 1 LOW ALERT. R & R EMERGENCY LIGHT BATTERY IAW AMM 33-51-01-4. OPS CK NORMAL.

Part: CONNECTOR — DAMAGED (PAX DOOR)

L1 MAIN ENTRY DOOR WILL NOT OPEN. DURING T/S FOUND WIRES RIPPED OUT OF DR1884 AT LT FOD DOOR UP LIFT SWITCH. R & R CONNECTOR PLUG IAW SWPM 20-31-15 AND WDM 52-11-01 AND WDM 33-22-01. OPERATED DOOR ELECTRICALLY, DOOR OPS NORMAL.

Part: DOUBLER — CRACKED (LT WING L/E) · airframe 850,781 hrs · 4,249 cycles

INSPECTION TYPE:3C, IN LT WING L/E COMPARTMENT AT XOS 631 APPX, CEILING DOUBLER IS CRACKED AT 2 EA LOCATION. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG. 203.

Part: ANGLE — CRACKED (LT WING LE) · airframe 85,078 hrs · 14,249 cycles

INSPECTION TYPE:3C, IN LT WING L/E COMPARTMENTAT XOS 792, FWD AREA, ANGLE IS CRACKED. FABRICATED AND INSTALLED REPAIR AT XOS792 LT WING L/E REF EO MD11-5720-41805-A AND STA, SA, EA 011-5720-01-A2942.

Part: DOUBLER — CRACKED (LT WING L/E) · airframe 850,781 hrs · 4,249 cycles

INSPECTION TYPE:3C, IN LT WING L/E COMPARTMENT AT XOS 544 APPRX, CEILING DOUBLER IS CRACKED AT 3 EA FASTNERS. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.

Part: DOUBLER — CRACKED (LT WING L/E) · airframe 850,781 hrs · 4,249 cycles

INSPECTION TYPE:3C, IN LT WING L/E COMPARTMENT AT XOS 638, CEILING DOUBLER IS CRACKED AT 1 EA LOCATION. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW REPAIR 9, FIG 203.

Part: BEAM — CHAFED (LT WING T/E) · airframe 850,781 hrs · 4,249 cycles

INSPECTION TYPE:3C, LT WING T/E INBD BEAM CAP FWD FLANGE CHAFING INTERM REPAIR TRANSFERRED FROM LOG PAGE 615637. DEF 438237 ACCOMPLISHED REPAIR IAW EO MD11-5720-40406-D.

Part: WEDGE — DAMAGED (LT WING TE FLAP)

LT WING OTBD FLAP T/E WEDGE DENTED. REMOVED DAMAGE AND REPAIRED FLAP IAW EO B767-5750-38892-B.

Part: SKIN — GOUGED (BS 1811 L13-14R)

FUSELAGE SKIN GOUGE AT STA Y=1811, LONGERON 13R AND 14R. DOUBLER REPAIR IAW EO MD11-5330-38106-B.

Part: SKIN — DAMAGED (BS 1811 S13-14L)

FUSELAGE SKIN DAMAGED, STA 1811 STR 13/14L. REPAIRED IAW EO MD11-5330-38106-A.

Part: SKIN — MISREPAIRED (SLAT) · airframe 82,818 hrs · 13,605 cycles

INSPECTION TYPE:2C REPAIR SURVEY SEQ NR 290-W3-01 PREVIOUS REPAIR DOUBLER INSTALLED SOLID R IVETS IN LIEU OF BLIND RIVETS APPROX BETWEEN STA XIS 151- 180 REF SRM 57-40-01 FIG 201 REPAIR 7. REMOVED EXISTING REPAIR ON LT INBD SLAT, SLAT SKIN BETWEEN XIS 151 AND XIS 180. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF EO MD11-5750-36304-A AND EA 011-5730-01-A2121.

Part: SKIN — MISREPAIRED (LT WING L/E) · airframe 82,818 hrs · 13,605 cycles

INSPECTION TYPE:2C, REPAIR SURVEY SEQUENCE NR 290-W3-03 LT WING FIXED L/E PREVIOUS REPAIR DOUBLER DOES NOT CORRELATE TO SRM 57-40-01 REPAIR 5, FIG. 201 DUE TO FASTNER PATTERN. REMOVED DOUBLER, FABRICATED AND INSTALLED NEW REPAIR DOUBLER AND SHIMS IAW SRM 57-40-02 REPAIR 5, FIG 201.

Part: FUEL TANK — MISREPAIRED (CENTER WING) · airframe 82,818 hrs · 13,605 cycles

INSPECTION TYPE:2C REPAIR SURVEY SEQ NR 290-W11-01 WING CTR TANK RT UPPER SKIN PREVIOUS REPAIR DOUBLER BETWEEN STA XCW-110 TO XCW-118. NOT IN SRM. REMOVED EXISTING REPAIR FROM CTR TANK UPPER SKIN AT STGR 19 TO 17 AND XCW-110 TO XCW-118. FABRICATED REPLACEMENT REPAIR AND INSTALLED REF EO MD11-5730-36359A AND EA 011-5730-A2119.

Part: SKIN — MISREPAIRED (NR 2 SLAT) · airframe 82,818 hrs · 13,605 cycles

INSP TYPE: 2C REPAIR SURVEY SEQ NR 290-W4-06 PREVIOUS REPAIR NOT IAW SRM 57-40-01, FIG 201 REPAIR 3 FASTENERS INSTALLED BUTTON HEAD SHOULD BE FLUSH HEAD. REMOVED EXISTING REPAIR ON NR 2 RT SLAT ASSY, INCREASED CUTOUT ON LOWER SKIN, FABRICATED AND INSTALLED REPLACEMENT REPAIR REF EO MD11-5750--36 366A AND EA 011-5730-01-A2125.

Part: SKIN — CANNING (RT WING TE FLAP) · airframe 82,818 hrs · 13,605 cycles

INSPECTION TYPE:2C, REPAIR SURVEY SEQ NR 290-W4-02 RT WING INBD FLAP UPPER SKIN APPROX BETW EEN STA XIFH 165 TO 177 REPAIR DOUBLER HAS OILCANNING CONDITION. REMOVED EXISTING REPAIR 290-W4-02 RT WING INBD FLAP UPPER SKIN BETWEEN XIFH 165 TO 177. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF SRM 57-00-01 FIG 201 REPAIR 1.

Part: SKIN — CANNING (RT WING TE FLAP) · airframe 82,818 hrs · 13,605 cycles

INSPECTION TYPE:2C, REPAIR SURVEY SEQ NR 290-W4-01 RT INBD. FLAP UPPER PREVIOUS REPAIR DOUBLER OIL CANNING CONDITION APPROX BETWEEN STA XIFH 133-153. REMOVED EXISTING REPAIR ON RT INBD. FLAP BETWEEN STA XIFH 133-153. CUT OUT DAMAGE SKIN, FABRICATED AND INSTALLED REPLACEMENT REPAIR REF SRM 57-00-01, FIG 201 REPAIR 2.

Part: WEB — MISREPAIRED (BS 475) · airframe 82,818 hrs · 13,605 cycles

INSP TYPE: 2C REPAIR SURVEY SEQ NR 290-F2-01 BETWEEN STA 475 AND 495, X=0 AND X=24, REPAIR DOUBLER IS NOT IN SRM. REMOVED EXISTING REPAIR BETWEEN STA 475 AND 495, BETWEEN X=0.00 AND X= 24. ON WEB. FABRICATED AND INSTALLLED REPLACEMENT REPAIR REF EO MD11-5330-36353-A AND EA 011-5330-01-A2112.

Part: SKIN — DAMAGED (RT WING) · airframe 82,818 hrs · 13,605 cycles

INSPECTION TYPE:2C, REPAIR SURVEY SEQUENCE NR 290-W4-10 RT WING FIXED L/E LWR SURFACE PREVIOUS REPAIR DOUBLER GOUGED, TOOLMARK, OVER COUTERSUNK. APPROX BTWN STA XOS836-867. REMOVED DOUBLER, REMOVED DAMAGE, AND FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLER IAW SRM 57-40-02 REPAIR 5, FIG 201.

Part: SKIN — DAMAGED (BS 1959-1975) · airframe 82,818 hrs · 13,605 cycles

INSPECTION TYPE:2C, REPAIR SURVEY SEQUENCE NR 290-F1-06, BETWEEN STA 1959 AND 1975, L40L AND L45L SRM 53-50-00, FIG. 16, VOL 1, REV 38 REQUIRES INNER DOUBLER TO BE .068 AND OUTER TO BE .080, ACTUAL INNER DOUBLER IS .080 AND OUTER DOUBER IS .100. REMOVED DOUBLER AND INNER DOUBLER, REMOVED DAMAGE, FABRICATED AND INSTALLED NEW REPAIR DOUBLERS AND FILLERS IAW SRM 53-00-15 REPAIR 8, FIG. 202

Part: SKIN — CRACKED (LT WING) · airframe 82,818 hrs · 13,605 cycles

INSPECTION TYPE:2C, LT L/E TELESCOPIC DUCT CUTOUT UPPER INBD AND OTBD CORNER CRACKED. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLERS AND DOUBLER IAW SRM 57-40-01 REPAIR 10 FIG 201.

Part: SKIN — MISREPAIRED (R4 DOOR) · airframe 82,818 hrs · 13,605 cycles

INSP TYPE:2C REPAIR SURVEY SEQUENCE NR 290-F1-05, BETWEEN STA 1853 AND 1887, LONGERON 16R AND 18R, AT R4 DOOR, REPAIR IS NOT IN SRM. REMOVED DOUBLER, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SAA EA 011-5210-01-A211 ISSUE A AND UPS EO MD11-5210-36361-A.

Part: REPAIR — INADEQUATE (L3 DOOR) · airframe 82,818 hrs · 13,605 cycles

INSPECTION TYPE:2C, REPAIR SURVEY SEQ NR290-F1-08 BETWEEN STA 1273 AND 1305 AND BETWEEN Z=32.837 TOZ=9.702 AT L3 DOOR IS NOT IAW SRM. REMOVED EXISTING REPAIR ON L3 DOOR SKIN BETWEEN STA 1273 AND 1305 BELO W Z=32.837. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF EO MD11- 5210-36350-A AND EA 011-5240-01-A2114.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 82,818 hrs · 13,605 cycles

INSPECTION TYPE:2C, POSSIBLE CRACKS AROUND BUCKED RIVETS IN BEADED DOUBLER RT WING L/E INTERIOR THRU PANEL 619DB. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, AND ANGLES IAW SRM 57-40-02 REPAIR 9, FIG 203.

Part: SKIN — CRACKED (LT WING L/E) · airframe 82,818 hrs · 13,605 cycles

INSPECTION TYPE: 2C, LT WING SLAT TRACK CUT OUT NR 14 CRACKED ON LWR OTBD CORNER, REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 57-40-02 REPAIR 7, FIG 201.

Part: DOUBLER — CRACKED (LT WING) · airframe 82,818 hrs · 13,605 cycles

INSPECTION TYPE: 2C, LT L/E SKIN BEADED DOUBLER AT XFS 667 CRACKED IN 4 SPOTS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, AND ANGLES IAW SRM 57-40-02 REPAIR 9, FIG. 203 SHT. 1-3.

Part: SKIN — CRACKED (RT WING) · airframe 82,818 hrs · 13,605 cycles

INSPECTION TYPE: 2C RT WING L/E SKIN CRACKED AT BOTH CORNERS OF SLOT FOR ANTI-ICE DUCT CUT OUT DAMAGE. FABRICATED & INSTALLED FILLERS AND DOUBLER REF SRM 57-40-01 REPAIR 10 FIG 201.

Part: SKIN — CRACKED (LT WING) · airframe 82,818 hrs · 13,605 cycles

INSPECTION TYPE:2C, LT WING L/E SLAT TRACK CUTOUT NR 12 CRACK ON LWR OTBD CORNER. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 57-40-02 REPAIR 7, FIG. 201.

Part: SKIN — MISREPAIRED (R3 DOOR) · airframe 82,818 hrs · 13,605 cycles

INSPECTION TYPE:2C, REPAIR SURVEY SEQ 290-F1-04 AT R3 DOOR BETWEEN STA 256 AND 1289 AND BETWEEN Z22 TO Z58 APPROX REPAIR DOUBLER HAS 37" BLENDOUT. REMOVED EXISTING REPAIR BETWEEN STA 1256 TO 1289 AND Z22 TO Z58. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF EO MD11-5210-36369-A AND EA 011-52-01-A2109.

Part: SKIN — MISREPAIRED (BS 1002 L39R) · airframe 82,818 hrs · 13,605 cycles

INSPECTION TYPE:2C, REPAIR SURVEY SEQ NR 290-F1-03 AT RT FUSELAGE BETWEEN STA 1002 AND 1019 AND L39R AND 42R APPROX HAS INNER AND OUTER REPAIR. DOUBLER GOUGED AND THICKNESS OF NR 1 AND NR 2 DOUBLERS DO NOT MATCH IAW SRM 53-50-00 FIG 16, VOL 1, REV 38. REMOVED EXISTING REPAIRS (REPAIR SURVEY) 290-F1-02 AND 290-F1-03 BETWEEN STA 1002-1019 AND L39R TO L42R. CUT OUT DAMAGED AREA, FABRICAT ED AND INSTALLED INCORPORATED REPLACEMENT REPAIR 290-F1-03 REF SRM 53-00-15, FIG 202, REPAIR 8.

Part: SKIN — CRACKED (LT WING TE FLAP)

LH IB FLAP UPPER SKIN CRACK 1.75 INCH. LONG AT STA XIFH 171.300 REPAIRED REF EO MD11-5750-35282-C

Part: WEB — MISSING (LT WING TE FLAP)

INSPECTION TYPE:PS-1 LEFT INBOARD FLAP OUTBOARD CLOSURE RIB WEB IS MISSING A SECTION MEASURING 5.00 INCH BY 4.5 INCH AREA 500 ZONE 544. ACCOMPLISHED DOUBLER REPAIR PER EO MD-11-5750-35271 APPENDIX A.

Part: GUARD — DAMAGED (ENTRY DOOR)

INSPECTION TYPE:N/A MAIN ENTRY DOOR EMERGENCY DOOR HANDLE GUARD REPAIR. REPLACED MAIN ENTRY DOOR EMERGENCY DOOR HANDLE GUARD PER 25-60-00-0. THIS CLEARS D402710.

Part: SLIDE — INOPERATIVE (L1 DOOR)

INSPECTION TYPE:N/A L1 DOOR SLIDE INOP. REMOVED AND REPLACED L1 SLIDE/RAFT PER MM 25-61-15-4. OPS CHECK PER MM 25-61-15-720- 002. OPS GOOD FOR SERVICE, THIS CLEARS M402658.

Part: RELAY — FAILED (L1 DOOR)

INSPECTION TYPE:N/A DURING PREFLIGHT CHECK L1 DOOR HAS NO ELECTRICAL POWER TO OPEN/CLOSE (OPERATE) DOOR. REPLACED RELAY R2-177. REF WDM 52-11-01. OPS CHECK OF L1 DOOR GOOD PER MM 52-10-01-2.

Part: COVER — UNSECURE (EVAC SLIDE)

INSPECTION TYPE:N/A L1 DOOR SLIDE COVER NOT STOWED PROPERLY/UNSECURED. RE-SECURED L1 DOOR SLIDE COVER PER MM 25-23-07-4-1. ALL OPS NORMAL.

Part: GAUGE — UNSERVICEABLE (EVAC SLIDE)

INSPECTION TYPE:N/A ESCAPE SLIDE GAUGE ON LEFT ENTRANCE DOOR IS UNREADABLE. DEFERRED L1 DOOR, IAW MEL 52-10-3-3. PLACARD INSTALLED. ***SDR FILED OPEN***

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYSTEM)

INSPECTION TYPE:N/A NR 2 HYD QTY LOSS IN FLIGHT. CK LWR RUD ACTUATOR, NO SIGN OF LK FOUND. TAIL TANK FUEL VENT BOX DRAIN CK NO HYD FLUID FOUND. NR 2 HYD RESERVOIR OVERFLOW BOTTLE EMPTY NR 2 ENG RUN UP FOR EDPS LEAKAGE CK NO LEAK FOUND. INSP LT & RT WING FLT CTRL HYD LINES FOUND EVIDENCE OF HYD LEAK AT LT IB AIL. TIGHTEN HYD LINE CONNECT AT ACT & CLEANED. LEAK CK PER AMM 29-00-00-6. NO LEAKS

Part: FLUID — LEAKING (HYDRAULIC SYS)

INSPECTION TYPE:N/A LOST HYDRAULIC FLUID SYSTEM DURING FLIGHT. *SDR FILED OPEN*

Part: HYDRAULIC SYSTEM — LOW (NR 2)

INSPECTION TYPE:N/A LOST HYDRAULIC FLUID SYSTEM - DURING FLIGHT. SERVICED NR 2 HYDRAULIC SYSTEM IAW AMM 12-13-02-3. CYCLED ALL FLT CONTROLS SEVERAL TIMES WITH ELECTRIC HYD PUMPS ON. NO LEAKS FOUND. C/O NR 2 ENG MOTORING AND VERIFIED NO LEAKS ON EDP'S. ALL THE TIME NO HYD QTY IND DROP. C/O MOTORING AND CYCLED T/R & FLT CONTROLS. NO LEAKS FOUND. FOUND AT AFT FIREWALL B-NUT.

Part: SKIN — DENTED (NR 2 SLAT) · airframe 80,415 hrs · 12,914 cycles

INSPECTION TYPE:C RT WING NR 2 SLAT LEADING EDGE DENT. DENT SKIN REMOVED PER SRM 57-10-00 FIG 37 VIR 40 & CUT OUT PROTECTED PER SRM 51-21-01 VII R40. HFEC INSP C/OUT PER NDTSPM R.13 06-10-01.001 FOUND NO CRACK ON TRIMMED OUT AREA. REP FILLER & DOUBLER FABRICATED PER SRM 57-10-00 FIG 37 V1. R40. ALL REPAIR PARTS REPROTECTED PER SRM 51-21-0 1 VII R40. OK TO INSTALL REPAIR PARTS.

Part: SLIDE — MALFUNCTIONED (L1 DOOR)

SLIDE REMOVED DUE TO NOT ABLE TO DISARM SLIDE WITH INSIDE OR OUTSIDE ARMING HANDLE. FOUND AFT ARMING LATCHING CATCHING ON INSPECTION VIEWING WINDOW AT BOTTOM OF LWR COVER. ADJUSTED VIEWING WINDOW AND REINSTALLED L1 SLIDE ASSY IAW AMM 25-61-15-4. OK FOR SERVICE CLEARS M382494. VERIFIED SAFETY PIN AND STOWED PRESSURE AND DATE GOOD.

Part: OIL SYSTEM — OVERTEMP (NR 2 ENGINE)

ATB - NR 2 ENGINE OIL TEMP WENT TO 175C AFTER TAKEOFF. RAN CHECKLIST WITH NR 2 ENGINE AT IDLE, OIL TEMP WAS 122C (ENG OIL TEMP HI MSG). OIL TEMP WAS IN CAUTION ZONE FOR APPROXIMATELY 3 MINUTES. REFER FIM 79-00-03-02 FIG 105 NO FAULT MSG FOUND. OIL TEMP PEAK AT 175 DEG FOR 3 MINS. NO MAINTENANCE ACTION REQ, PER MM 72-00-04-280- 357 OIL QTY INDICATED 24 QTS ON ARRIVAL. SAME AS OTHER ENGINE. INSP OIL CAP CHK NO OVER SERVICE, NO FUEL SMELL, RPL MGB OIL TEMP PROBE PER MM 79-32-01. ENG RUN CHK, OIL TEMP OK PER MM 71-02-03-700-870.

Part: CONNECTOR — BURNED (FUEL PUMP)

AFTER REFUELING MESSAGE "AUX LWR L PUMP OFF" APPEARED. DEFERRED AUX LWR L PUMP IAW MEL 28-22-6-1-1 M367263. DMP 28-22-6-1 ACCOMPLISHED. REMOVED AUX LWR L PUMP. FOUND BURNT CONNECTOR IN HOUSING AND ON PUMP. REMOVED OLD HARNESS AND INSTALLED NEW HARNESS THRU CONDUIT REF MM 20-22-10-8. COMPLETED HARNESS INSTALLATION IAW MM 28-22-10 AND INSTALLED NEW PUMP IAW 28-22-01.

Part: STRUCTURE — CORRODED (TE FLAP) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C RIGHT WING: DURING O/B FLAP I/B FWD HINGE PIVOT BEARING REPLACEMENT FOUND PIVOT BORE CORRODED AS MARKED. RIGHT O/B FLAP I/B FWD HINGE REMOVED PER AMM 57-53-01 R.50. RIGHT FWD O/B FLAP I/B HINGE PIVOT BORE CORROSION REMOVED & FOUND EXCEED LIMIT PER CMM5 7-44-08. FPI C/O PER DAC NDT SPM R.13 PT 08, NO CORROSION FOUND ON BORE SURFACE. CADIUM PLATING C/O ON REWORK AREA PER BSOPM20-10-01 R.58. BUSHING FAB AND INSTALLED AS PER EN 1667-07.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C CABIN - SEAT TRACK AT STA 842 - 909, X=8.5 AFTER CLEANING FOUND CORROSION AS MARKED. CORROSION ON SEAT TRACK AT STA 842 - 909 X=8.5 RMVED FOUND EXCEEDS LIMITS. CORRODED SEAT TRACK AT STA 850 - 909 REMOVED. REPAIR SEAT TRACK REWORKED AS PER SRM 53-70-00 VOL I FIG 1A REV 38. REPAIR SEAT TRACK FASTENER HOLES PICKED UP, PROTECTED & PAINTED. REPAIR SEAT TRACK INSTALLED AS PER SRM 51-31-01 VOL II REV 38.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C CABIN - SEAT TRACK AT STA 775 - 909, X=8.5 AFTER CLEANING FOUND CORROSION AS MARKED. SEAT TRACK CORROSION AT STA 775 - 909 X=8.5 REMOVED FOUND EXCEEDED LIMITS. CORRODED SEAT TRACK AT STA 785 - 909 REMOVED. REPAIR SEAT TRACK REWORKED PER SRM 53-70-00 VOL I FIG 1A REV 38. REPAIR SEAT TRACK FASTENER HOLES PICKED UP, PROTECTED & PAINTED. REPAIR SEAT TRACK INSTALLED AT REWORKED AREA AS PER SRM 51-31-01 VOL II REV 38.

Part: INTERCOSTAL — CRACKED (BS 1761-1781) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C CTR CARGO INTERCOSTAL AT LT 42, LT 43 STA 1761 - 1781 FOUND CRACKED. CTR CARGO STA 1761-1781 LONGERON 42-43 LT CRACKED INTERCOSTAL REMOVED. INTERCOSTAL FABRICATED FROM MAT'L 7075-0 CONDITION AS PER DWG AC A7049. INTERCOSTAL HEAT TREATED PER DPS 7.00-1 & HARDNESS VALUES HRB 86.9 AS PER DPS 1.05-3. INTERCOSTAL HOLES PICKED UP, REPROTECTED & PAINTED. INTERCOSTAL INSTALLED AT CTR CARGO STA 1761 - 1781 LT 42-43.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C EMP - RT HORZ STAB NR 7 BARREL NUT BORE FOUND CORROSION. CORROSION AT BARREL NUT BORE REMOVED, BORE REAM & REMAINING BLEND OUT FOUND EXCEEDS LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE. REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APP.

Part: LONGERON — CRACKED (BS 6-100 S6R) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C CRACK INDICATION FOUND APPROX 0.3 INCH IN LENGTH DURING HFEC INSPECTION AT STA 6-100 FWD SECTION LONGERON EDGE OF STR 6R AS MARKED. STA 6-100 FWD SECTION LONGERON ATTACHED SPLICE REMOVED. CRACKED LONGERON TRIMMED OFF AT STA 6-80 & REMOVED. TRIMMED OFF AREA REPROTECTED. HFEC INSP C/OUT ON TRIMMED OFF AREA FOUND NO CRACK. LONGERON & REPAIR SPLICE FAB PER SRM 53-10-00 FIG 1 VOL I REV 38. NEW FAB LONGERON & REPAIR SPLICE FASTENER HOLES PICKED UP, PROTECTED, PAINTED & INSTALLED.

Part: LONGERON SPLICE — CRACKED (BS 6-100 S1R) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C X-RAY C/OUT FOUND CRACK INDICATING AT STA 6-100, STR 1 (1EA) AT RT LONGERON SPLICE AS MARKED. STA 6-100 STR 1 RT CRACKED LONGERON SPLICE REMOVED. CRACKED LONGERON TRIMMED OFF & REMOVED. TRIMMED OFF AREA REPROTECTED. HFEC INSP C/OUT ON TRIMMED OFF AREA FOUND NO CRACK. LONGERON & REPAIR SPLICE FAB PER SRM 53-10-00 FIG 1 VOL 1 REV 38. LONGERON & REPAIR SPLICE FASTENERS PICKED UP. FAB LONGERON & REPAIR SPLICE PROTECTED.

Part: LONGERON SPLICE — CRACKED (BS 6-100 S6R) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C X-RAY C/OUT FOUND CRACK INDICATION AT STA 6-100, STR 6 (1EA) RT AT LONGERON SPLICE AS MARKED. STA 6-100 STR 6 RT CRACKED LONGERON ATTACHED SPLICE REMOVED. CRACKED LONGERON TRIMMED OFF AT STA 1149 & REMOVED. TRIMMED OFF AREA PROTECTED. HFEC INSP C/OUT ON TRIMMED OFF AREA FOUND NO CRACK. LONGERON & REPAIR SPLICE FAB PER SRM 53-10-00 FIG 1 VOL I REV 38. FAB LONGERON & REPAIR SPLICE FASTENERS PICKED UP. FAB LONGERON & REPAIR SPLICE PROTECTED.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C EMP - RT HORZ STAB NR 28 BARREL NUT BORE FOUND CORROSION. CORROSION AT BARREL NUT BORE REMOVED, BORE REAM & REMAINING BLEND OUT EXCEEDS LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APPLIED.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C EMP - RT HORZ STAB NR 25 BARREL NUT BORE FOUND CORROSION. CORROSION AT BARREL NUT BORE REMOVED, BORE REAM & REMAINING BLEND OUT FOUND EXCEEDS LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE. REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APP.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C EMPENNAGE RT HORIZONTAL STABILIZER BARREL NUT NR 19 FOUND BORE WITH CORROSION. CORROSION AT BARREL NUT BORE REMOVED, BORE REAM & REMAINING BLEND OUT FOUND EXCEEDS LIMIT. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE. REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APP.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C EMP - LT HORZ STAB NR 11 BARREL NUT BORE FOUND CORROSIONS. CORROSION AT BARREL NUT BORE REMOVED, BORE REAM & REMAINING BLEND OUT FOUND EXCEEDING LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE. REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APP.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C EMP - RT HORZ STAB NR 27 BARREL NUT BORE FOUND CORROSION. CORROSION AT BARREL NUT BORE REMOVED. BORE REAM & REMAINING BLEND OUT FOUND EXCEEDING LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS, BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE. REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APP.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C EMP - RT HORZ STAB NR 24 BARREL NUT BORE FOUND CORROSION. CORROSION AT BARREL NUT BORE REMOVED, BORE REAM & REMAINING BLEND OUT FOUND EXCEEDING LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE. REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APP.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C EMP - LT HORZ STAB NR 20 BARREL NUT BORE FOUND CORROSION. CORROSION AT BARREL NUT BORE REMOVED, BORE REAM & REMAINING BLEND OUT FOUND EXCEEDS LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE. REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APP.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C EMP - RT HORZ STAB NR 18 BARREL NUT BORE FOUND CORROSION. CORROSION AT BARREL NUT BORE REMOVED, BORE REAM & REMAINING BLEND OUT FOUND EXCEEDS LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE. REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APP.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C EMPENNAGE LT HORIZONTAL STABILIZER BARREL NUT NR 16 FOUND BORE WITH CORROSION. CORROSION AT BARREL NUT BORE REMOVED, FOUND EXCEEDS LIMIT. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE. REPAIR SLEEVE BUSHING FAB & PROTECTED PER EO MD11-5510-19409-L FIG 5. PR 1422 B1/2 SEALANT APP.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C EMP - LT HORZ STAB NR 31 BARREL NUT BORE FOUND CORROSION. CORROSION AT BARREL NUT BORE REMOVED, BORE REAM & REMAINING BLEND OUT FOUND EXCEEDS LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP. REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APPLIED AT BLEND OUT.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C EMP - LT HORZ STAB NR 36 BARREL NUT BORE FOUND CORROSIONS. TORQUE BOX WEB CUT FOR ACCESS. CORROSION AT BARREL NUT BORE REMOVED. BORE REAM & REMAINING BLEND OUT FOUND EXCEEDS LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS & BOTTOM PERIPHERY RADIUS SMOOTHENED & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE. REPAIR SLEEVE BUSHING.

Part: TANK — CORRODED (BS 1245) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C RT SIDE CENTER AUX TANK STA 1245.0, X=-103.0 FOUND CORROSION AROUND FASTENER. RT SIDE CENTER AUX TANK STA 1245.0 X=-103.0 FASTENER AS MARK REMOVED. RT SIDE CENTER AUX TANK STA 1245 X=-103 CORROSION REMOVED. REWORKED AREAS PROTECTED. FPI & HFEC INSP C/OUT ON REWORKED AREA FOUND NO CRACK & NO CORROSION. REWORKED AREAS UPP SKIN MAT'L REMOVED & REMAINED FOUND EXCEED LIMITS. FLAP PEENING C/OUT ON REWORKED AREA PER EN1642-0.

Part: TANK — CORRODED (BS 1239-1255) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C LEFT SIDE CENTER AUX TANK STA 1239.0 - 1255.0, X=103.0 FOUND CORROSION A ROUND FASTENERS AS MARKED. LEFT SIDE CTR AUX TANK STA 1239.0-1255.0 X=103.0 FASTENER AS MARK REMOVED. CORROSION ON UPPER SKIN REMOVED & REWORKED AREA PROTECTED. HFEC OPEN HOLE & FPI C/OUT ON REWORKED AREA FOUND NO CRACK & NO CORROSION. REWORKED AREA UPP SKIN MAT'L REMOVED & REMAINED ALL FOUND EXCEED LIMITS. FLAP PEENING C/OUT ON REWORKED AREA PER EN1638-07. REWORKED AREA.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C EMP - RT HORIZ STAB NR 6 BARREL NUT BORE FOUND CORROSION. CORROSION AT BARREL BORE REMOVED, BORE REAM & REMAINING BLEND OUT EXCEEDS LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APPL.

Part: ACCESS PANEL — CRACKED (LWS 536AB) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C LEFT WING ACCESS PANEL 536AB CUTOUT AREA FOUND CRACK INDICATION DURING NDT INSPECTION. HOLES REAMED FOR LEFT WING ACCESS PANEL 536AB CUTOUT AREA AS PER EN1639-07. HFEC OPEN HOLE INSPEC C/OUT ON REWORKED HOLE FOUND NO CRACK. BUSHINGS 17EA FA AS PER EN1639-07. NEW FAB BUSHINGS 17EA & REWORKED AREA REPROTECTED AS PER SRM 51-21-01 VOL II REV 38 IAW EN1639-07. BUSHINGS 17EA INSTALLED AS PER EN1639-07.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C EMP - LT HORZ STAB NR 27 BARREL NUT BORE FOUND CORROSIONS. CORROSION AT BARREL NUT BORE REMOVED, BORE REAM & REMAINING BLEND OUT FOUND EXCEEDING LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS, BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE. REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT AP.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C EMP - LT HORZ STAB NR 30 BARREL NUT BORE FOUND CORROSIONS. CORROSION AT BARREL NUT BORE REMOVED, BORE REAM & REMAINING BLEND OUT FOUND EXCEEDING LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID, BOTTOM PERIPHERY RADIUS SMOOTHEN/PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APP.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C EMP - LEFT HORZ STAB NR 24 BARREL NUT BORE FOUND CORROSION. CORROSION AT BARREL NUT BORE REMOVED, BORE REAM & REMAINING BLEND OUT FOUND EXCEEDING LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE. REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APP.

Part: STRUCTURE — CRACKED (LT WING) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C LEFT WING LOWER SURFACE L/E ACCESS PANEL CUTOUT STRUCTURE AT STA XORS 51 0 APPROX FOUND CRACK AS MARKED. LEFT WING LOWER SURFACE L/E APPROX XORS 510 DOUBLER REMOVED. NEW DOUBLER FABRICATED USING MAT'L 7075-T6-0.090" PER DOUGLAS DWG ARB2933. NEW DOUBLER FASTENER HOLES PICKED UP, REPROTECTED & PAINTED. NEW DOUBLER INSTALLED AS PER SRM 51-31-01 VOL II REV 38.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C EMP - LEFT HORZ STAB NR 18 BARREL NUT BORE FOUND CORROSION. CORROSION AT BARREL NUT BORE REMOVED, BORE REAM & REMAINING BLEND OUT FOUND EXCEEDING LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT & NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE. REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT BUSHING.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C EMP - LT HORZ STAB NR 12 BARREL NUT BORE FOUND CORROSION. CORROSION AT BARREL NUT BORE REMOVED. BORE REAM & REMAINING BLEND OUT FOUND EXCEEDING LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE. REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APP.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C EMP - RIGHT HORZ STAB NR 17 BARREL NUT BORE FOUND CORROSION. CORROSION AT BARREL NUT BORE REMOVED, BORE REAM & REMAINING BLEND OUT FOUND EXCEEDING LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE REAM FURTHER PER EN1574-07. BARREL NUT BORE B/OUT VOIDS, BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE. REPAIR SLEEVE BUSHING.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C EMP - RIGHT HORZ STAB NR 23 BARREL NUT BORE FOUND CORROSION. CORROSION AT BARREL NUT BORE REMOVED, BORE REAM & REMAINING BLEND OUT FOUND EXCEEDING LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE. REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APP.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C RIGHT HORIZONTAL STABILIZER BARREL NUT HOLE 8R HAS CORROSION IN BORE. CORROSION AT BARREL NUT BORE REMOVED & BORE BOTTOM SURFACE CLEANED, BORE REAM & REMAINING BLEND OUT FOUND EXCEEDS LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID & BOTTOM PERIPHERY RADIUS SMOOTHEN/PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE. FAB REP SLEEVE BUSHING & PROTECT.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C LEFT HORIZONTAL STABILIZER BARREL NUT HOLE 1L HAS CORROSION IN HOLE. CORROSION AT BARREL NUT BORE REMOVED, BORE REAM & REMAINING BLEND OUT FOUND EXCEEDING LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE. REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APPLIED.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C RIGHT HORIZONTAL STABILIZER BARREL NUT HOLE 36R HAS CORROSION IN BORE. TORQUE BOX WEB CUT FOR ACCESS. BARREL NUT BORE CORROSION REMOVED & BORE REAM & REMAINING BLEND OUT FOUND EXCEEDING LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE REAM FURTHER & BORE BOTTOM MACHINE DOWN DEEPER. BARREL NUT BORE BLEND OUT & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. CUT OUT FR PRIMER.

Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C CTR CABIN - SEAT TRACK FROM STA 1273 - STA 1381, +X27.5 SEVERAL SCRATCH MARKS FOUND ON CROWN & CHANNEL SURFACE AS MARKED. CABIN SEAT TRACK STA 1273 - 1381 X=27.5 SCRATCH MARK AT CROWN & CHANNEL SURFACE REMOVED FOUND EXCEEDS LIMIT. SEAT TRACK WITH SCRATCH MARKS TRIMMED OFF AT STA 1247 & 1391. HFEC INSP CUTOUT ON TRIMMED OFF FOUND NO CRACK. NEW SEAT TRACK, SPLICE HAT & PLATE FAB, HOLES PICK UP, REPROTECTED, PAINTED & INSTALLED.

Part: STRINGER — CRACKED (RT WING) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C RT WING UNDERSIDE IN NR 3 FUEL TANK ACCESS CUTOUT 638AB FOUND UPPER STRINGER NR 9 XORS 819.0 SUSPECT CRACK. HFEC INSP C/OUT FOUND CRACK APPROX 6.5 INCHES. STRINGER NR 9 XORS 819 FASTENER & SPLICE REMOVED. REPAIR DOUBLERS FAB & HEAT TREATED. SLOT OPENED ON STR 9 XORS 819 & REPROTECTED. HFEC INSP C/OUT ON SLOTTED OUT AREA, FOUND NO CRACK. FUEL LINES IN NR 3 FUEL TANK ACCESS CUTOUT 638AB, NR 3 FUEL TANK FILL S/O VLV CONTROLLER & SHUTOFF VALVE BODY REMOVED.

Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C CTR CABIN - SEAT TRACK FROM STA 1273 - STA 1381 -X27.5 SEVERAL SCRATCH MARKS FOUND ON CROWN & CHANNEL SURFACE AS MARKED. CTR CABIN SEAT TRACK FROM STA 1273-1381 X=-27.5 RT SCRATCH MARKS ON CROWN & CHANNEL REMOVED FOUND EXCEEDS LIMIT. SCRATCH MARK SEAT TRACK TRIMMED OFF AT STA 1284 & 1391 REMOVE. HFEC INSP CUTOUT ON TRIMMED AREAS FOUND NO CRACK. NEW SEAT TRACK, SPLICE HAT & PLATE FAB, HOLES PICK UP, REPROTECTED, PAINTED & INSTALLED.

Part: SEAT TRACK — DAMAGED (BS 1273-1381) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C CTR CABIN - SEAT TRACK FROM STA 1273 - STA 1381, -X27.5 SEVERAL SCRATCH MARKS FOUND ON CROWN & CHANNEL SURFACE AS MARKED. CTR CABIN SEAT TRACK FR STA 1273-1381 X=-27.5 RT SCRATCH MARKS ON CROWN & CHANNEL REMOVED FOUND EXCEED LIMIT. SCRATCH MARK SEAT TRACK TRI TRIMMED OFF AT STA 1284 & 1391. HFEC INSP CUTOUT ON TRIMMED OFF AREAS FOUND NO CRACK. NEW SEAT TRACK, SPLICE HAT & SPLICE PLATE FAB, HOLES PICKED UP, PROTECTED, PAINT TOUCHED UP & INSTALLED.

Part: FLOOR SUPPORT — CORRODED (BS 1841) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C CENTER CARGO COMPT AT STATION 1841,X-56 TO X+56 FOUND FLOOR SUPPORT W WITH SURFACE CORROSION. CENTER CARGO COMPT STA 1841 X=56 LT-56 RT FLOOR SUPPORT CORROSION REMOVED FOUND EXCEED LIMIT PER SRM 53-00-01 FIG 1A VI R38. FPI C/O PER DACNDTS PM R.13 PT 08 ON REWORK AREA FOUND NO CORROSION EVIDENT. REPAIR ANGLE QTY 03EA FAB PER EN 1659-07. FLOOR SUPPORT RWK AREA & REPAIR ANGLE 3EA REPROTECT PER SRM 51-21-01 VII. REPAIR ANGLES 3EA INSTL PER EN 1659-07.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C CABIN - C-ZONE STA 1941 - 1951 INTERCOSTAL FOUND CRACK AT L2 RIGHT AS MARKED. CABIN C-ZONE STA 1941-1951 INTERCOSTAL FOUND CRACK AT L2 RIGHT REMOVED NEW INTERCOSTAL FABRICATED, HEAT TREATED & HARDNESS VALUES HRB 8 6.2 PER DPS 1.05-3. NEW INTERCOSTAL FASTENER HOLES PICKED UP. NEW INTERCOSTAL ALODINE CARRIED OUT, PAINTED & INSTALLED.

Part: SHEAR TIE — CORRODED (BS 1974 S51L/R) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C AFT WASTE AREA AT STATION 1974 IN BETWEEN LONGERON 51R TO 51L FOUND SHEAR CLIP WITH SURFACE CORROSION. AFT WASTE AREA STA 1974 IN BETWEEN LONGERON 51R - 51L SHEAR CLIP AREA FASTENERS AS PER SRM 51-33-01 VII R38. SHEAR CLIP CORROSION REMOVED FOUND EXCEEDED LIMIT. CORRODED SHEAR TEE REMOVED AT STA 1974 LONGERON 49 LT - 49 RT PER SRM 51-33-01 VII R38. SHEAR TEE REWORK PER DWG AGA8002. SHEAR TEE INSTL AT AFT WASTE AREA STA 1974 L49LT - 49RT PER SRM 51-33-01VII R38.

Part: SEAT TRACK — CORRODED (BS 1921) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C CABIN - RIGHT STA 1921 Y=-107.25 SEAT TRACK FOUND CORROSION AS MARKED. CABIN RIGHT STA 1921 X=-107.25 CORROSION ON SEAT TRACK REMOVED FOUND EXCEEDS LIMITS. RIGHT NR 4 DOOR SILL PLATE REMOVED. CORRODED SEAT TRACK TRIMMED OFF & AREA REPROTECTED. NEW SEAT TRACK REWORKED, FASTENER HOLES P/U & REPROTECTED. HFEC INSP CUTOUT ON TRIMMED OFF AREA, FOUND NO CRACK SEAT TRACK SPLICE HAT, SPLICE PLATE FAB, HOLES PICK UP, PROTECT.

Part: SEAT TRACK — CORRODED (BS 1921) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C CABIN - LT STA 1921, Y=107.25 SEAT TRACK FOUND CORROSION AS MARKED. CABIN LT STA 1921 Y=107.25 CORROSION ON SEAT TRACK REMOVED FOUND EXCEED LIMIT. CORRODED SEAT TRACK TRIMMED OFF AT STA 1831 & PROTECTED. HFEC INSP C/OUT ON TRIMMED OFF AREA FOUND NO CRACK. SEAT TRACK SPLICE & SPLICE PLATE FAB PER SRM 53-70-00 FIG 1A VOLI REV38. FAB PARTS FASTENER HOLES PICK UP, PROTECTED & PAINTED. NEW SEAT TRACK FASTENER HOLES.

Part: TANK — CORRODED (BS 1258) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C LT SIDE CENTER WING BOX TOPSIDE STA 1258.0 X=108.0 FOUND CORROSION ON TANK SKIN AS MARKED. LEFT SIDE CENTER WING BOX TOPSIDE STA 1258.0 X=108.0 FUEL TANK FASTENER AS MARK REMOVED. CORROSION ON UPP SKIN REMOVED & REWORKED AREAS PROTECTED. FPI & HFEC OPEN HOLE INSP C/OUT ON REWORKED AREA FOUND NO CRACK & NO CORROSION. REWORKED AREA UPP SKIN MAT'L REMOVED & REMAINED FOUND EXCEED LIMITS. FLAP PEENING C/OUT ON REWORKED AREA PER EN1638-07.

Part: TANK — CORRODED (BS 1210) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C CTR CABIN - UNDER FLOOR AREA FUEL TANK TOP SURFACE AT STA 1210, -X103 01EA CORROSION FOUND NEAR FASTENER. CTR CABIN UNDER FLOOR AREA FUEL TANK TOP SURFACE AT STA 1210 -X103 FUEL TANK SCREW AS MARK REMOVED FOR S/M ACCESS. CORROSION ON FUEL TANK TOP SURFACE REMOVED FOUND EXCEEDED LIMIT. FPI & HFEC OPEN HOLE INSP C/OUT ON REWORKED AREA FOUND NO CRACK & NO CORROSION. FLAP PEENING C/ OUT ON REWORKED AREA PER EN1642-07. REWORKED AREA REPROTECTED, PAINT.

Part: LONGERON — CORRODED (BS 1954 L51L) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C AFT CARGO COMPT AT STA 1954 BILGE AREA LONGERON 51 LEFT FOUND SURFACE CORROSION. AFT CARGO COMPT STA 1954 BILGE AREA LONGERON 51 LEFT FASTENERS REMOVED FRAME SHEAR CLIP AREA CORROSION RMVD FOUND EXCEEDS LIMIT. CORRODED SHEAR CLIP REMOVED AT STA 1954 LONG 49RT-50LT AFT CARGO AREA. SHEAR CLIP FAB FORM MAT'L 7075-0-0.071" PER DWG AGA7133. FAB SHEAR CLIP HOLES PICKED UP, REPROTECTED, PAINTED & INSTALLED AT AFT CARGO COMPT.

Part: DOUBLER — CRACKED (RWS 548) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C RIGHT WING: L/E COMPARTMENT AT STA XORS 548 APPROX FOUND UPPER DOUBLER CRACKED AS MARKED. REPAIR ANGLE FAB PER EN 1538-07 & SRM 57-10-00 FIG 28 R.TR 57-5. CRACKED AREA AT RT WING L/E COMPARTMENT AT STA XORS 548 TRIMMED OUT PER EN 15 38-07. HFEC INSP C/O ON TRIMMED OUT FOUND NO CRACK EVIDENT. REPAIR FAB PER EN 1538-07 AND INSTALLED AS PER SRM 51-31-01 VOL II AND EN 153-8-07.

Part: SKIN — CRACKED (RT WING) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C RIGHT WING LOWER SURFACE FIXED L/E SKIN AT I/B FWD CORNER OF REFUELING PANEL FOUND CRACK AS MARKED. FASTENERS AT RIGHT WING REFUELING PANEL CRACKED AREA REMOVED. DAMAGED AREA TRIMMED OFF. HFEC INSP C/OUT ON TRIMMED OFF AREA FOUND NO CRACK. REPAIR DOUBLER & FILLER FABRICATED, HOLES PICKED UP, PROTECTED & PAINTED. REPAIR DOUBLER & FILLER INSTALLED AS PER SRM 51-31-01 VOL II & SRM 57-10-00 FIG 21 VOL I REV 38.

Part: STIFFENER — CRACKED (RWS 714) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C RIGHT WING L/E COMPARTMENT AT STA XORS 714 APPROX FOUND UPPER STIFFENER CRACKED AS MARKED. CRACKED STIFFENER REMOVED. NEW STIFFENER FABRICATED USING MAT'L 707 5-0-0.071" AS PER DOUGLAS DWG ARB3954. STIFFENER HEAT TREATED PER DPS 7.00-1 & HARDNESS VALUES HRB 88.7. RIGHT WING L/E COMPT AT STA XORS 714 STIFFENER HOLES PICKED UP & REPROTECTED. NEW STIFFENER PAINT TOUCH UP & INSTALLED.

Part: SKIN — CRACKED (RWS 510) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C RIGHT WING LOWER SURFACE L/E ACCESS PANEL CUTOUT STRUCTURE AT STA XORS 51 0 APPROX FOUND CRACK AS MARKED. HFEC INSP C/OUT & CRACK FOUND AS MARKED. CRACKED DOUBLER REMOVED. RIGHT WING LOWER SURFACE APPROX XORS 510 DOUBLER FABBED USING MAT'L 7075T6-0.090" PER DOUGLAS DWG ARB2933. NEW DOUBLER FASTENER HOLES PICKED UP, REPROTECTED & PAINTED. NEW DOUBLER INSTALLED AS PER SRM 51-31-01 VOL II REV 38.

Part: DOUBLER — CRACKED (RT WING) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C RIGHT WING L/E COMPARTMENT AT STA XORS 538 APPROX FOUND UPPER DOUBLER CRACKED AS MARKED. FRAMES REMOVED FOR ACCESS. CRACKED AREA TRIMMED OFF. HFEC INSP C/O ON TRIMMED OFF FOUND NO CRACK. REPAIR ANGLES FABRICATED, HEAT TREATED & HARDNESS VALUES HRB84.2 PER DPS 1.05-3. REPAIR FILLER & DOUBLER FABRICTAED, REPROTECTED, PRIMER TOUCH UP & INSTALLED.

Part: DOUBLER — CRACKED (RT WING) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C RIGHT WING L/E COMPARTMENT AT STA XORS 710 APPROX FOUND UPPER DOUBLER CRACKED AS MARKED. RIBS REMOVED FOR ACCESS. CRACKED AREA TRIMMED OFF. HFEC INSP C/OUT ON TRIMMED OFF AREA FOUND NO CRACK. REPAIR ANGLES FABRICATED, HEAT TREATED & HARDNESS VALUES HRB 84.3 PER DPS 1.05-3. REPAIR FILLER & DOUBLER FABRICATED, REPROTECTED, PRIMER TOUCHED UP & INSTALLED.

Part: STRUCTURE — CORRODED (BS 1239- 189) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C LEFT SIDE CENTER WING BOX TOPSIDE AT STA 1239.0 - 1189.0 X=108.0 FOUND CORROSION AROUND FASTENERS AS MARKED. LEFT SIDE CENTER WING BOX TOPSIDE AT STA 1239.0-1189.0 X=108.0 FASTENER AS MARK & CORRODED AREAS REMOVED. CORROSION ON UPP SKIN REMOVED. REWORKED AREAS PROTECTED. FPI & HFEC OPEN HOLE INSP C/OUT ON REWORKED AREA FOUND NO CRACK & NO CORROSION. REWORKED AREAS SKIN P/N APB7441-1 MAT'L REMOVED & REMAINED, ALL FOUND EXCEED LIMITS. FLAP PEENING C/OUT.

Part: STIFFENER — CRACKED (RWS 568) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C RIGHT WING L/E COMPARTMENT AT STA XORS 568 APPROX FOUND UPPER STIFFENER CRACKED AS MARKED. CRACKED STIFFENER & ATTACH PARTS REMOVED. NEW STIFFENER FABBED USING MAT'L 7075-0-0.071" PER DOUGLAS DWG ARB3954. STIFFENER HEAT TREATED PER DPS 7.00-1 & HARDNESS VALUES HRB 84.0 PER DPS 1.02-3. NEW STIFFENER HOLES P/UP, REPROTECTED & PAINTED. NEW STIFFENER INSTALLED AS PER SRM 51-33-01 VOL II REV 38 & SRM 51-35-01 VOL II REV 38.

Part: BRACKET — CRACKED (BS 495 S27R) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C FWD CABIN - RIGHT SIDEWALL AREA 01EA L-ANGLE BRACKET AT STA 495, S-27R FOUND CRACK NEAR FASTENER AS MARKED. FWD CABIN - RIGHT AT STA 495 S-27R CRACK AREA TRIMMED OFF. TRIMMED OFF AREA PROTECTED. HFEC INSP C/OUT ON TRIMMED OFF, FOUND NO CRACK EVIDENT 01EA FILLER FAB FROM MAT'L 7075T6-0.080" & REPAIR ANGLE FAB FROM ET MAT'L S2929486 PER EARN EN1536-07.5. NEW FAB PARTS FASTENER HOLES PICKED UP, PROTECTED, PAINTED & INSTALLED.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C CENTER CARGO COMPT AT STATION 1841 IN BETWEEN LONGERON 51 LT TO 51 RT FOUND CORROSION AS MARKED. CTR CARGO COMPT STA 1841 BETWEEN L51 LT - L51 RT CORROSION REMOVED FOUND EXCEEDED LIMITS. REPAIR CHANNEL FAB FROM MAT'L 7075-0 0.080". CHANNEL HEAT TREATED & HARNESS VALUES HRB 82.2 AS PER DPS 1.05-3. REPAIR CHANNEL REPROTECTED. REPAIR CHANNEL PAINTED. REPAIR CHANNEL INSTALLED. PAINT TOUCHED UP ON REWORK AREA.

Part: RIB — CRACKED (LT WING) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C LEFT WING LEADING EDGE HAS NOSE RIB CRACKED BETWEEN SLAT TRACKS 12 AND 13 STICKER 7058. CRACKED RIB REMOVED. NEW RIB FABBED USING MAT'L 7075-0-0.040" PER DWG ARB2922. RIB HEAT TREATED AS PER DPS 7.00-1 & HARDNESS VALUES HRB 83.1 AS PER DPS 1.05-3. NEW RIB HOLES PICKED UP AND PROTECTED. NEW RIB PAINTED & INSTALLED.

Part: SKIN — CHAFED (LT WING) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C LT WING LEADING EDGE SKIN CHAFED AT SLAT TRACK NR 2 AREA STICKER 5712. LT WING L/E SKIN CHAFED AT SLAT TRACK NR 2 AREA CHAFED MARK REMOVED FOUND W/N LIMIT & REPROTECTED. HFEC INSP C/OUT FOUND CRACK APPROX .75 INCH LONG WING L/E ACCESS PANEL 515BT & NR 2 SLAT TRACK DOOR REMOVED. REPAIR DOUBLER & FILLER FAB PER EN1621-07. REPAIR DOUBLER & FILLER HOLES, PICKED UP PAINTED & INSTALLED. NR 2 SLAT TRACK DOOR PNL 515BT INSTALLED.

Part: BRACKET — CRACKED (TAIL CONE) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C EMP - FWD TAIL CONE, RIGHT UPPER ALIGNMENT PIN MOUNTING BRACKET CRACKED. EMP FWD TAIL CONE AFT FUSE FIXED FAIRING 317AR REMOVED PER AMM20-50-02 R.50. EMP FWD TAIL CONE RIGHT UPPER ALIGNMENT PIN MOUNTING CRACKED AREA CUT OFF PER EN 1600-07. HFEC INSP C/O PER DACNDTSPM R.13 PT 06-10-01-001 ON CUTOFF AREA FOUND NO CRACK EVIDENT. FAB NEW CLIP, REPAIR DOUBLER & FRAME DOUBLER PER EN 1600-07. INSTALL NEW CLIP & DOUBLERS PER EN1600-07.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C CENTER CARGO COMPT AT STATION 1841 X-48 AFT FRAME FOUND CRACKED. CENTER CARGO COMPT STA 1841 X=0 -48RT CRACK FRAME WEB REMOVED. FRAME WEB FAB FROM MAT'L 7075T6-0.050" AS PER DWG AGA7170. FRAME WEB HOLES PICKED UP & REPROTECTED. FRAME WEB PAINTED. FRAME WEB INSTALLED AT CTR CARGO COMPT STA 1841 X=0 -48RT AS PER SRM 51-31-01 VOL II REV 38.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C CENTER CARGO COMPT AT STATION 1841 X+50 AFT FRAME FOUND CRACKED. CNTR CARGO COMPT STA 1841 X=0 -50LT CRACK FRAME WEB REMOVED. FRAME WEB FAB FROM MAT'L 7075T6-0.050" AS PER DWG AGA7170. FRAME WEB HOLES PICKED UP & REPROTECTED. FRAME WEB PAINTED. FRAME WEB INSTALLED AT CNTR CARGO COMPT STA 1841 X=0 -50LH AS PER SRM 51-31-01 VOL II REV 38.

Part: LONGERON SPLICE — CORRODED (FUSELAGE) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C CTR CARGO COMPT AT STATION 1809 LONGERON 46 RIGHT FOUND CORRODED DOUBLER AS MARKED. CTR CARGO COMPT STA 1809 LONGERON 46 RIGHT CORRODED SPLICE DOUBLER RMVD LONGERON SPLICE MACHINED FROM S2641454-12000 HAT SECTION PER DOUGLAS DWG AFA7103. FPI C/OUT ON FABRICATED SPLICE FOUND NO CRACK. FABBED LONGERON SPLICE HOLES PICKED UP, REPROTECTED, PAINTED & INSTALLED.

Part: DOUBLER — CRACKED (BS 5-125 L43R) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C CTR CARGO COMPT AT STATION 5-125 LONGERON 43 RIGHT FOUND SUSPECTED CRACKED ON DOUBLER. HFEC INSP C/OUT FOUND CRACK APPROX 1 INCH AS MARKED. CRACKED LONGERON DOUBLER REMOVED AT STA 5-125 LONGERON 43 RIGHT. SPLICE MACHINE FROM 1D1104- 7150-T61511 PER DOUGLAS DWG A5A7114. FPI C/OUT ON FAB SPLICE FOUND NO CRACK. FAB SPLICE HOLES PICKED UP, REPROTECTED & PAINTED. LONGERON SPLICE INSTALLED AT CTR CARGO COMPT STA 5-125 LONGERON 43 RIGHT.

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C CTR CARGO COMPT AT STATION 5-120 LONGERON 44 LEFT FOUND SUSPECTED CRACKED ON DOUBLER. HFEC INSP C/OUT FOUND CRACK APPROX 1 INCH AS MARKED. CRACKED LONGERON SPLICE RMV'D AT CTR CARGO COMPT STA 5-120 LONG 44 LT. LONGERON SPLICE MACHINE FROM 1D1104-7150-T61511 EXTRUSION PER DOUGLAS DWG A5A7116. FPI C/OUT ON FAB SPLICE FOUND NO CRACK. FAB LONGERON SPLICE HOLES PICKED UP, REPROTECTED, PAINTED & INSTALLED.

Part: BRACKET — CRACKED (BS 1236) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C LEFT UNDERSIDE CANTED PANEL AREA AT STA 1236.0 FOUND CANTED PANEL BRACKET CRACKED AS MARKED. REMOVED LWR AUX BLADDER CELL DECKING PANEL LEFT AT STA 1236.0 FOR S/M ACCESS. FTG AT STA 1236 FRAME TO CANT PANEL REMOVED FOR ACCESS. EXISTING CRACKED BRACKET REMOVED. NEW BRACKET FASTENER HOLES PICKED UP & INSTALL. FTG AT STA 1236 FRAME TO CANT PANEL REINSTALLED. LOWER AUX BLADDER CELL DECKING PANEL LINER AT LEFT STA 1236 REINSTALLED.

Part: BRACKET — CRACKED (BS 1216) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C LEFT UNDERSIDE CANTED PANEL AREA AT STA 1216.0 FOUND CANTED PANEL BRACKET CRACKED AS MARKED. REMOVED LWR AUX BLADDER CELL DECKING PNL LEFT AT STA 1216.0 FOR S/M ACCESS. FITTING AT STA 1216 FRAME TO CANT PANEL REMOVED. CRACKED BRACKET REMOVED. NEW BRACKET FASTENER HOLES PICKED UP. NEW BRACKET INSTALLED. FITTING AT STA 1216 FRAME TO CANT PANEL REINSTALLED. LOWER AUX BLADDER CELL DECKING PANEL LINER AT LEFT STA 1216.0 INSTALL.

Part: RIB — CRACKED (RT WING SLAT) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C RIGHT WING NR 16 SLAT TRACK I/B RIB FITTING SUSPECTED CRACK AS MARKED. HFEC INSP C/OUT FOUND CRACK AS MARKED. RIGHT WING NR 8 EXT & RET CABLES DISCONNECTED. RIGHT WING NR 16 SLAT TRACK DOOR, ATTACHED HARDWARES & ROLLERS & SLAT TRACK REMOVED. RIGHT WING NR 16 SLAT WIRING, CLAMPS & RIB REMOVED. NEW HOLES TRANSFERED ONTO NEW RIB PER DOUGLAS DWG ARB2873. DAMAGE AREA AT WING SKIN & DOUBLER TRIM OFF. HFEC INSP C/OUT ON TRIMMED OFF AREA FOUND.

Part: SUPPORT — DEFORMED (BS 1039) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C FWD CARGO COMPT AT STATION 1039 X=16.5 FOUND SUPPORT STRUT DEFORMED DAMAGED. FWD CARGO COMPT STA 1039 X=16.5 LT DEFORMED DAMAGED SUPPORT STRUT REMOVED PER SRM 51-33-01 VOL II REV 38. NEW SUPPORT STRUT ADA0033-2 HOLES P/UP PER SRM 51-33-01 VOL II REV 38. NEW SUPPORT STRUT ADA0033-2 INSTALLED AT FWD CARGO COMPT STA1039 X=16.5 LT PER SRM 51-33-01 VOL II REV 38. PAINT TOUCHED UP ON REWORK AREA PER SRM 51-21-01 VOL II REV 38.

Part: SUPPORT — DEFORMED (BS 1059) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C FWD CARGO COMPT AT STATION 1059 X=16.5 FOUND SUPPORT STRUT DEFORMED DAMAGED. FWD CARGO COMPT STA 1059 X=16.5 LT DEFORMED DAMAGED SUPPORT STRUT REMOVED AS PER SRM 51-33-01 VOL II REV 38. NEW SUPPORT STRUT AFA0043-6 HOLES P/UP PER SRM 51-33-01 VOL II REV 38. NEW SUPPORT STRUT AFA0043-6 INSTALLED AT FWD CARGO COMPT STA 1059 X=16.5 LT PER SRM 51-33-01 VOL II REV 38. PAINT TOUCHED UP ON REWORK AREA PER SRM 51-21-01 VOL II REV 38.

Part: SUPPORT — DAMAGED (BS 1039) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C FWD CARGO COMPT AT STATION 1039 X-16.5 FOUND SUPPORT STRUT DEFORMED/DAMAGED. FWD CARGO COMPT STA 1039 X-16.5 RT DEFORMED DMG SUPPORT STRUT REMOVED. NEW SUPPORT STRUT ADA0033-1 HOLES P/UP. NEW SUPPORT STRUT ADA0033-1 INSTALLED AT FWD CARGO COMPT STA 1039 X-16.5 RT. PAINT TOUCHED UP ON REWORK AREA.

Part: SKIN — DAMAGED (AFT CARGO DOOR) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C AFT CARGO DOOR CUTOUT LWR AFT EDGE FOUND PREVIOUS BLEND OUT AS MARKED. AFT CARGO DOOR CUTOUT LWR AFT EXT SKIN PREVIOUS BLEND OUT AREA FASTENERS REMOVED. PREVIOUS BLEND OUT EXT SKIN & INNER DOUBLER TRIMMED OUT HFEC INSP C/OUT ON REWORKED AREA FOUND NO CRACK. REPAIR DOUBLERS 2 EA & FILLERS 2EA FAB, REPROTECTED, PAINTED & INSTALLED. REPAIR DOUBLER RS 2EA & FILLERS 2EA INSTALLED AT AFT CARGO DOOR CUTOUT LWR AFT.

Part: SKIN — DENTED (NR 5 SLAT) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C RIGHT NR 5 SLAT L/E 6 DENTS IN A ROW. RIGHT WING NR 5 SLAT L/E DENTS MEASURED FOUND OUT OF LIMIT. DAMAGE AREA TRIM OFF AS PER EN1663-07. HFEC INSP C/OUT ON TRIM OFF AREA FOUND NO CRACK. REPAIR PARTS FAB PER SRM 57-10-00 FIG 5 VOL I REV 38 & EN1663-07. REPAIR PARTS HOLES PICKED UP, PROTECTED & PAINTED. RIGHT NR 5 SLAT REPAIR PARTS INSTALLED AS PER EN1663-07.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 78,001 hrs · 12,487 cycles

INSPECTION TYPE:C LEFT WING INBOARD FLAP UPPER SURFACE SKIN DENT. LEFT WING I/B FLAP UPPER SURFACE SKIN DENT AREA TRIMMED OUT. HFEC INSP C/OUT ON TRIMMED OUT FOUND NO CRACK. REPAIR DOUBLER FABRICATED USING MAT'L 2024T3-0.040" & HOLES PICKED UP. REPAIR PARTS REPROTECTED & PAINTED. REPAIR PARTS INSTALLED AS PER SRM 57-10-00 VOL I REV 38 FIG 34.