N314UP

Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 72,818 hrs · 24,640 cycles

DURING PDC FOUND EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-07. OPS CHECK GOOD. A/C OK FOR SVC

Part: UNKNOWN — ODOR (ZONE 200) · airframe 72,493 hrs · 24,520 cycles

AFTER AIR CART CONNECTED & PACKS TURNED ON STRONG FUMES ENTERED THE COCKPIT, FUMES REMAINED UNTIL PACKS WERE SELECTED OFF. ACCOMPLISHED REMOVAL OF OIL CONTAMINATION FROM THE AIR CONDITIONING AND PNEUMATIC SYSTEMS PER AMM 21-00-21, NO OIL FUMES OR SMELL ARE PRESENT.

Part: SKIN — CORRODED (ZONE 100) · airframe 72,025 hrs · 24,332 cycles

CORROSION-SKIN, AFT CGO COMPT FWD BULKHEAD LWR STRINGER AREA, NEAR STA 1083, S-39L.I.A.W AMM 53-66-01-004-002 REV.145 REMOVED FAIRING PANEL NO.197AL AND 197JL.REMOVED THE AFFECTED FASTENERS I.A.W SRM 51-40-02-0G REV. 92.BLENDED OUT THE DAMAGE AREA I.A.W SRM 51-10-02-0G-0 REV. 92.COMPLETED INSTALL OF REPAIR PARTS I.A.W EI NO: F2025A53M-1102 SEQUENCE B PART 4 STEP 11 REV. 1.ACCOMPLISHED INSTALL OF PANEL NO.197AL AND 197JL INSP CHECK NORMAL.ACCOMPLISHED REPAIR I.A.W EO-94032-REQ1 REV1 AND BOEING DWG NO. 140T0130 SH 16 REV.C; 140T0130 SH 7 REV.C; 140T0833 SH 1 REV.B; 145T2620 SH 4 REV.H; 145T2620 SH 10 REV.H; 146T1201 SH 1 REV.H, 146T3220 SH 1 REV.D AND 146T3261 SH 3

Part: STRAP — CORRODED (ZONE 100) · airframe 72,023 hrs · 24,331 cycles

CORROSION-U CHANNEL, FORWARD CARGO COMPARTMENT AROUND CEILING PANEL NUTPLATES AREA BETWEEN STA 566 AND STA 610, RBL 40.(REPLACE) 1. JOB COMPLETED.

Part: SKIN — CORRODED (ZONE 600 FLAP) · airframe 72,023 hrs · 24,331 cycles

RIGHT WING INBOARD MAIN FLAP TE LOWER SKIN INSIDE SUSPECT CORROSION, IFS 105.75. ACCOMPLETED REPAIR IAW EO-94005-REQ1 REV1.

Part: ANGLE — CRACKED (ZONE 100) · airframe 72,023 hrs · 24,331 cycles

CRACKED ANGLE, L/H LOWER WING TO BODY AREA, STA 785. (AGING A/C INSPECTION).REMOVED DAMAGE ANGLE I.A. W SRM 51-40-02-0G REV. 92. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV.92, BOEING DWG NO.140T0705 SHEET 2 REV.- AND BOEING DWG NO.149T7340 SHEET 1 REV.D

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 72,023 hrs · 24,331 cycles

FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 146T5869-134 PANEL NO: 252UFF. (REPAIR) I.A.W AMM 25-57-05-004-001, AMM 25-57-02-004-029, AMM 25-58-01-004-001 AND AMM 25-58-04-004-010 REV.145 REMOVED MAIN DECK CARGO HANDLING AND G.V.I CHECK NORMAL.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 72,023 hrs · 24,331 cycles

FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 146T5869-89 PANEL NO: 251XFF. (REPAIR) I.A.W AMM 25-57-05-004-001, AMM 25-57-02-004-029, AMM 25-58-01-004-001 AND AMM 25-58-04-004-010 REV.145 REMOVED MAIN DECK CARGO HANDLING AND G.V.I CHECK NORMAL.

Part: SATCOM — FAULTED · airframe 71,485 hrs · 24,103 cycles

**ATB**BOTH HF UNABLE TRANSMIT. OPS CHECK OK ON GND, SATCOM INOP ALSO. RESULTED IN ATB. DEFERRED BOTH HF COMMUNICATION SYSTEMS REF MEL 23-11-1-2A-2, PLACARD INSTALLED, NO DMP REQUIRED SEE BARCODE T3F18E0064Q4L FOR SATCOM DEFERRAL. OPEN

Part: TRANSCEIVER — FAULTED (HF COMMS) · airframe 71,559 hrs · 24,136 cycles

BOTH HF UNABLE TRANSMIT. OPS CHECK OK ON GND, SATCOM INOP ALSO. RESULTED IN ATB. ++ C/W FIM T/S 23-11-00. R&R HF TRANSCEIVER REF AMM 23-11-03-424-005. BOTH HFS OPS CK GOOD.

Part: DOOR — OBSTRUCTED (ZONE 800) · airframe 71,234 hrs · 23,986 cycles

CREW ENTRY DOOR IS NOT CLOSING CORRECTLY FROM THE INSIDE UPON FURTHER INSP FOUND SMALL PIECE OF RUBBER TRIM WEDGED IN INSIDE HANDLE AREA, REMOVED TRIM PIECE ,OPS CHK GOOD IAW MM52-12-00-862-027-001

Part: SKIN — DAMAGED (ZONE 500) · airframe 71,181 hrs · 23,957 cycles

L WING PANEL 561GB LEADING EDGE HAS SEPARATION WITH RIVETS PULLED THROUGH. MARKED WITH TAPE. REPLACED DAMAGED WIGGLE PLATES WITH 113T1663Y1013, 113T1663-1037 AND 113T1663Y1009 IAW BOEING SRM 51-40-02.

Part: TORQUE TUBE — BENT (ZONE 600 FLAP) · airframe 71,110 hrs · 23,920 cycles

*** SDR FILED OPEN *** R/H AFT INBOARD FLAP TORQUE TUBE SLOT DOOR BENT/ DAMAGED WILL REQUIRE SM TO DRILL NEW PARTS AND FASTENER INSTALLATION 12 HOURS. MAINTENANCE NEEDED TO ACCESS AREA AND RETURN TO ORIGINAL CONFIGURATION 8 HRS.PARTS ORDERED.

Part: TORQUE TUBE — BENT (ZONE 300) · airframe 71,563 hrs · 24,140 cycles

R/H AFT INBOARD FLAP TORQUE TUBE SLOT DOOR BENT/ DAMAGED INSTALLED NEW UPPER TORQUE TUBE / AFT SLOT DOOR ASSY IAW AMM 27-51-07. WILL REQUIRE ADJUSTMENTS AFTER THE LOWER TORQUE TUBE / CENTER SLOT DOOR ASSY IS INSTALLED. ADJUSTED NEW UPPER TORQUE TUBE ATTACH-SUPPORT RODS IAW AMM 27-51-07. ALL WORK PERFORMED BY ALLCAT AND ETOPS QUALIFIED AMT. THIS CLEARS DEFERRAL. PLACARD REMOVED. NO DMP.

Part: IRU — OUT OF ALIGNMENT (UNKNOWN) · airframe 68,696 hrs · 22,940 cycles

*** SUPPLEMENTAL SDR *** COULD NOT ALIGN IRU'S ATTEMPTED TWICE. FMC MESSAGE IRS MOTION. (CENTER NOT ALIGNING) **OII 2** R&R RIGHT IRU PER MM 34-21-01, OPS CHECK GOOD DMP REVERSED PLACED REMOVED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 68,690 hrs · 22,938 cycles

*SDR FILED OPEN* *DIV* COULD NOT ALIGN IRU'S ATTEMPTED TWICE. FMC MESSAGE IRS MOTION. (CENTER NOT ALIGNING) **OII 2** SWAPPED CENTER IRU(PART NUMBER HG1050AE15, SN 98062901) WITH RIGHT IRU (PN HG1050AD15 SN 2815) PER AMM 34-21-01. OPS CHECK OF CENTER AND LEFT IRU GOOD.

Part: HANDLE — UNKNOWN (UNKNOWN) · airframe 68,440 hrs · 22,834 cycles

*** SUPPLEMENTAL SDR *** FAULT - WORN - PAWL, CREW ENTRY DOOR HANDLE MECHANISM. (REPLACE) REVIEW COMPLETE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 68,417 hrs · 22,826 cycles

*SDR FILED OPEN* FAULT - WORN - PAWL, CREW ENTRY DOOR HANDLE MECHANISM. (REPLACE) OK TO WORK

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 68,417 hrs · 22,826 cycles

*SDR FILED OPEN* FAULT - FOUND MAIN DECK CARGO ZONE TEMP SENSOR COVER CRACK AT STA 654+33 RIGHT SIDE (REPLACE) OK TO WORK

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 68,417 hrs · 22,826 cycles

*SDR FILED OPEN* FAULT - FOUND MAIN DECK CARGO ZONE TEMP SENSOR COVER CRACK AT STA 1164 RIGHT SIDE (REPLACE) OK TO WORK

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 68,440 hrs · 22,834 cycles

*** SUPPLEMENTAL SDR *** FAULT - FOUND MAIN DECK CARGO ZONE TEMP SENSOR COVER CRACK AT STA 1164 RIGHT SIDE (REPLACE) REVIEW COMPLETE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 68,440 hrs · 22,834 cycles

*** SUPPLEMENTAL SDR *** FAULT - FOUND MAIN DECK CARGO ZONE TEMP SENSOR COVER CRACK AT STA 654+33 RIGHT SIDE (REPLACE) REVIEW COMPLETE

Part: FITTING — BROKEN (UNKNOWN) · airframe 68,417 hrs · 22,826 cycles

FAULT - FOUND MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING BROKEN AT STA ( 870 & 890 ) RBL47.5 & STA890 BL0 & STA ( 999 & 1087 & 1131 ) LBL47.5 TTL: 6EA(REPLACE) I.A.W AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 REV.139 RESTORED MAIN DECK CARGO HANDLING<BR>JOB COMPLETED AND CONDITION CHECK NORMAL. FOUND MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING BROKEN AT STA ( 870 & 890 ) RBL47.5 & STA890 BL0 & STA ( 999 & 1087 & 1131 ) LBL47.5 TTL: 6EA(REPLACE) REVIEW COMPLETE

Part: STIFFENER — CRACKED (UNKNOWN) · airframe 68,417 hrs · 22,826 cycles

MAJOR REPAIR, FAULT - CRACK CENTER WING FRONT SPAR CRACK IS STIFFENERS AT STA 785.9 LBL 33 (REPAIR) THE CENTER WING FRONT SPAR IS CLASSIFIED AS PRIMARY STRUCTURE PER SRM 51-00-04-0G. THIS REPAIR IS AS REINFORCING REPAIR AND CLASSIFIED AS MAJOR PER GMM 05.04.01.02 CLASSIFICATION OF REPAIRS. CRACK CENTER WING FRONT SPAR CRACK IS STIFFENERS AT STA 785.9 LBL 33 (REPAIR) REVIEW COMPLETE

Part: STIFFENER — CRACKED (UNKNOWN) · airframe 68,417 hrs · 22,826 cycles

*SDR FILED OPEN* *MAJOR REPAIR* FAULT - CRACK CENTER WING FRONT SPAR CRACK IS STIFFENERS AT STA 785.9 RBL 55 (REPAIR) THE CENTER WING FRONT SPAR IS CLASSIFIED AS PRIMARY STRUCTURE PER SRM 51-00-04-0G. THIS REPAIR IS AS REINFORCING REPAIR AND CLASSIFIED AS MAJOR PER GMM 05.04.01.02 CLASSIFICATION OF REPAIRS.

Part: FLOOR PANEL — UNKNOWN (UNKNOWN) · airframe 68,350 hrs · 22,798 cycles

FLOOR PANEL IN POS 12L AND 12R HAS DAMAGE NEAR FASTENER. LABOR ROW NOT REQUIRED.

Part: SENSOR — NONE (RTMLG) · airframe 67,239 hrs · 22,432 cycles

INSPECTION TYPE:N/A**ATB** ON TAKEOFF, CREW HAD TO USE OVERRIDE SWITCH TO BRING UP GEAR . A/C NEVER RECOGNISED T/OFOUND RMLG TILT SENSOR BRACKET IMPROPERLY INSTALLED. R&R BRACKET CORRECTLY , IAW AMM 32-11-18-4.PERFORMED ADJ/TEST AND OPS CKS. GEAR SWINGS AND GAP CKS GOOD.IAW AMM32-09-07-02 AND 32-32-00-5

Part: FLOORBOARD — DAMAGED (MAIN DECK CARGO) · airframe 66,762 hrs · 22,274 cycles

DAMAGE ON FLOORBOARD ON MCD CENTER 9R/9L.FABRICATED NEW FLOOR BOARD PER EO B767-5320-9693-I.

Part: EICAS — INOPERATIVE (CABIN) · airframe 66,148 hrs · 22,026 cycles

INSPECTION TYPE:NA** ATB**SDR FILED OPEN**NO EMERG ACTION** A/C LANDED WITHOUT INCIDENT**DURING START L AOA PROBE EICAS DISPLAYED. LEFT ANGLE OF ATTACK SENOSR HEATER SYS ICING MEL / CDL 30 32 1 DMP ACCOMPLISHED BY 1833951 AUTHORIZED BY 1833951 AUTORIZED BY 0557551 REQ'D WNTRY PLACARD INSTALLED DI LOG UPDATED

Part: SKIN — DENTED (BS 1417-1439) · airframe 63,864 hrs · 21,169 cycles

INSPECTION TYPE:C13, DENT ON FUSELAGE SKIN (PN:146T3241-15) BETWEEN STA 1417 AND 1439, S-36L TO S-37L.REPAIR IAW SRM 53-00-01-2R-12, REV 20.03. REPAIRED I.A.W 767-300F SRM 53-00-01-2R-12, REV 20.03.

Part: WARNING MESSAGE — FALSE INDICATION (MLG) · airframe 63,738 hrs · 21,137 cycles

INSPECTION TYPE:N/A** ATB **LANDED UNEVENTFULLY** GEAR DISAGREE WITH GEAR DOORS LIGHT ILLUMINATED AFTER TAKE OFF.VISUALLY INSPECTED ALL LANDING GEARS & GEAR DOORS, FOUND #6 BRAKE ROD WAS DISCONNECTED WITH BRAKE. PERFORMED PSEU BITE CHECK AS PER AMM32-09-03-001 & CHECKED LANDING GEAR HYD FUSE AS PER AMM 32-32-19-725-001. NO FAULT NOTED. INSTALL #6 BRAKE ASSY MM 32-41-08-401, TEST GOOD. REPLACED BRAKE HOSE MM 32-41-16-401 INSTALL TEST OK. IPC: 32-41-06-01D-200.

Part: SKIN — DAMAGED (BS 637) · airframe 59,258 hrs · 19,552 cycles

SKIN PUNCTURE AT FS 637 JUST AFT AND BELOW MAIN CARGO DOOR. DUE TO A1 CAN BEING BLOWN INTO FUSELAGE DURING WIND STORM. THIS IS A MAJOR REPAIR. CUTOUT DAMAGED SKIN 18.5 F&AX 11.2. SKIN IS 063202473 CLAD CUTOUT DAMAGE TEAR STRAP .071 6.5/4", REF SRM 51-40-02 SE 0807902 08/22/19. PERFORMED HFEC, IAW NTM 51-00-19 & ROTO SCAN DAMAGE WAS REPAIRED, IAW B767-5330-73738-B.

Part: STRINGER — DAMAGED (BS 637) · airframe 59,258 hrs · 19,552 cycles

STRINGER 31L DAMAGED AT BS 637. STRINGER SHEARED AT TEAR STRAP LOCATION. REPAIRED IAW EO B767-73734-A AND SRM 53-30-03-01.

Part: SKIN — DAMAGED (BS 637) · airframe 59,258 hrs · 19,552 cycles

FUSELAGE SKIN PUNCTURED AT BS 637, STRINGER 31L. TEAR STRAP DAMAGED. REPAIRED IAW EO B767-5330-73738-A AND SRM 53-00-01-2R.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 59,022 hrs · 19,459 cycles

INSPECTION TYPE:C12 CRACK ON CENTER WING TANK STIFFENER(P/N:111T2008-12) ON STA 785.9,RBL33. REPAIR IAW SRM 57-10-10-2R-2 REPAIR 2 REV.74.00, EO B767-5740-58151-B, SRID :4-4530245710 AND EO B767-5710-73154-A.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 59,022 hrs · 19,459 cycles

INSPECTION TYPE:C12 CRACK ON VERTICAL STIFFENER AT WHEEL WELL BULKHEAD AT STA 287, LBL 25. REPAIR IAW EO B767-5310-20118-F AND SRM 51-70-12 GENERAL , FIGURE 1 ,REV 74.00.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 56,639 hrs · 18,629 cycles

MAIN CARGO SMOKE DETECT 2 MESSAGE. AFTER ARRIVAL FOUND SMOKE DETECTOR 2 EA FAULT LIGHT ILLUMINATED. REMOVED AND REPLACED SMOKE DETECTOR FOR MAIN CARGO IN POSITION 2 EA OPS CHECKS GOOD AT THIS TIME. IAW AMM 26 14 01 IPC 26 16 01 54 / 190K.

Part: ESCAPE REEL — UNSERVICEABLE (COCKPIT) · airframe 56,158 hrs · 18,472 cycles

DECENT DEVICE S/N 14877 FOUND TO BE UNSERVICEABLE. REF PART REQ 228947A MOST FORWARD POSITION, EXP DATE JULY 6, 2020. REMOVED & REPLACED FWD DECENT DEVICE PER AMM 25-61-03 REF: 25-61-02-04.

Part: LIFE VEST — OPEN (FIRST OFFICER'S) · airframe 55,203 hrs · 18,136 cycles

FIRST OFFICEER`S LIFE VEST OPENED. INSTALLED A NEW LIFE VEST.

Part: CONNECTOR — DIRTY (START VALVE) · airframe 55,007 hrs · 17,981 cycles

DURING START, THE LEFT ENGINE START VALVE DID NOT OPEN. CLEANED THE CONNECTOR ON LT ENGINE STARTER MOTOR AND PERFORMED AN OPS CHECK 3 TIMES ON GROUND. ALL CHECKED OK IAW AMM 81-10-00.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 54,795 hrs · 17,894 cycles

RT AFT FLIGHT DECK EMERGENCY EXIT LIGHT INOP. RELAMPED IN REFERENCE TO AMM 33-51-11, OPS NORMAL.

Part: WARNING MESSAGE — ILLUMINATED (WX RADAR SYS) · airframe 54,411 hrs · 17,779 cycles

STATUS MESSAGE FOR WEATHER RADAR SYS. OPEN

Part: SENSOR — OUT OF LIMITS (PAX DOOR) · airframe 54,138 hrs · 17,693 cycles

CLEARANCE OF ENTRY DOOR CLOSER SENSOR IS NOT WITHIN LIMITS IAW TC 52-000-100. ADJUSTED ENTRY DOOR CLOSED SENSOR IAW TC 52-000-100 AND AMM 52-12-00

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,045 hrs · 17,660 cycles

INSPECTION TYPE: C11, FOUND EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED EXTERIOR EMERGENCY LIGHT LAMP IAW AMM 33-51-16-962-001, REV 121. PERFORMED TEST OF THE LAMP IAW AMM 33-51-16-962-001, REV 121.

Part: FLOOR PANEL — WORN (CABIN) · airframe 53,964 hrs · 17,634 cycles

FLOOR PANEL WORN THROUGH BY BALL MAT ROLLER HOUSINGS. FABRICATE A NEW FLOOR PANEL IAWEO B767-5320-9693-1

Part: FLOORBOARD — DAMAGED (FLIGHT DECK) · airframe 53,964 hrs · 17,634 cycles

FLOORBOARD AT POS 2/3 LBL 49 DAMAGED. REMOVED THE FLOORBOARD. MAJOR REPAIR. FABRICATED A NEW FLOORBOARD.

Part: FLOOR PANEL — WORN (MAIN CABIN) · airframe 53,964 hrs · 17,634 cycles

MAIN CABIN FLOOR PANEL WORN BY BALL MAT ROLLER HOUSING. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-I.

Part: FLOOR PANEL — PUNCTURED (MAIN CARGO) · airframe 53,964 hrs · 17,634 cycles

MAIN CARGO DECK FLOOR PANEL POSITION 3L PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-I.

Part: FLOORBOARD — DAMAGED (MAIN CARGO) · airframe 53,964 hrs · 17,634 cycles

MAIN CARGO DECK FLOORBOARD POSITION 3L HAS MULTIPLE AREAS OF DAMAGE. MANUFACTURED A NEW FLOORBOARD IAW EO B767-5320-9693-I, APPX B.

Part: FLOORBOARD — DENTED (MAIN CARGO) · airframe 53,964 hrs · 17,634 cycles

MAIN CAGRO DECK FLOORBOARD, POSITION 3L HAS MULTIPLE DENTS. MANUFACTURED A NEW FLOORBOARD IAW EO B767-5320-9693-I, APPX B.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 53,658 hrs · 17,507 cycles

FLOOR PANEL IS DAMAGED. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-I.

Part: WARNING LIGHT — FALSE ACTIVATION (THRUST REVERSER) · airframe 52,988 hrs · 17,266 cycles

NO LANDING RECEIVED A RT THRUST REVERSER ISOLATION VALVE EICAS MESSAGE. TROUBLESHOT IAW FIM 78-34-00-990-813. NO FAULTS FOUND. SYSTEM TESTED IAW AMM 78-31-00 FOUND OPS NORMAL.

Part: TRANSCEIVER — MALFUNCTIONED (HF SYSTEM) · airframe 52,211 hrs · 16,945 cycles

RIGHT HF WOULD NOT RECEIVE. PERFORMED AN AIR TURNBACK BEFORE ETOPS ENTRY POINT. RERACKED THE RT HF TRANSCEIVER IAW MM 23-11-03-401. OPS TEST PASSED IAW MM 23-11-00-501-2.

Part: SKIN — CRACKED (RT WING) · airframe 50,119 hrs · 16,178 cycles

INSPECTION TYPE:C10, CRACK INDICATION WAS FOUND ON RT WING LOWER SKIN, FASTENER HOLE AT STR L-9.5, NEAR WING STA 995. REPAIR IAW SR 3-3334851482 AND EO B767-5730-58408-A.

Part: FLOOR PANEL — CRACKED (CARGO) · airframe 50,119 hrs · 16,178 cycles

INSPECTION TYPE:C10, FOUND CRACK ON CARGO FLOOR PANEL, 242VFF AT BS 985-BS 1087, RBL 78-RBL 88. FABRICATED THE REPLACEMENT FLOOR PANEL IAW EO NR B767-5320-9693-H.

Part: STIFFENER — CRACKED (BS 785) · airframe 50,119 hrs · 16,178 cycles

INSPECTION TYPE:C10, CRACK ON THE CENTER WING FRONT SPAR STIFFENER UPPER SIDE AT BS 785.9, RBL 11. REPAIR IAW SRM 57-10-10, REPAIR 2, REV.63 , SRID:3-3334935982 AND EO: B767-5710-58407-A.

Part: STIFFENER — CRACKED (BS 785) · airframe 50,119 hrs · 16,178 cycles

INSPECTION TYPE:C10, CRACK ON CENTER WING FRONT SPAR STIFFENER UPPER SIDE AT BS 785.9 , LBL 11. REPAIR IAW SRM 57-10-10, REPAIR 2, REV 63 , SRID:3-3334935982 AND EO: B767-5710-58407-A.

Part: LIGHT — CRACKED (CABIN) · airframe 49,926 hrs · 16,110 cycles

EMERGENCY EXIT LIGHT CASE NEAR ENTRY DOOR CAME OUT OF WALL MOUNT. EMERGENCY EXIT LIGHT WORKS. REPAIRED IAW EO B767-2510-58066-A.

Part: UNKNOWN — ODOR (COCKPIT)

DURING CLIMBOUT, ODOR LIKE BURNED FOOD. SUSPECT RT ENGINE BIRDSTRIKE SINCE ONLY HAD ODOR IF RIGHT PACK WAS ON AND ONLY FOR A FEW MINUTES. RT FAN VIBRATION WAS 3.5 IN CLIMB. ALL OTHER INDICATIONS NORMAL. INSPECTON IAW FIM 71-05-00-815-872-H01 SHOWS ENGINE OK TO CONTINUE IN SERVICE. IAW AMM 71-00-00-501 TEST NR.6. NOTE, VIBRATION LEVEL IS ACCEPTABLE. INSPECTION IAW AMM 05-51-18-201, SHOWS NO EVIDENCE OF BIRDSTRIKE ON THE ACFT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHTS INADVERTANTLY IN THE ARMED WITH SHIPS POWER. R & R EMERGENCY BATTERY IAW AMM 33-51-07-022-001 AND 33-51-07-422-012. OPS CK GOOD.

Part: RADOME — DAMAGED (NOSE)

NOSE RADOME DAMAGED DUE TO BIRD STRIKE DURING LANDING. R & R RADOME IAW AMM 53-12-01-902-038 AND AMM 53-12-01-402-059.

Part: SWITCH — FAILED (EMERGENCY LIGHTS)

EMERGENCY LIGHTS FAILED TEST, FOUND SWITCH BAD. R & R EMERGENCY CONTROL PANEL IAW AMM 33-51-08-401. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (COCKPIT)

INSPECTION TYPE:ETOP ELECTRICAL BURNING ODOR NOTED IN FLIGHT. BOTH PACKS RUNNING. ODOR DISSIPATED THEN NOTICED MORE STRONGLY UPON BLOCK IN. AFTER BLOCK IN, ODOR WAS STRONGER IN AFT RT TUNNEL OF E/E BAY. COULD NOT PIN POINT SOURCE. RAN BOTH ENGINES, PACKS. APU OPENED AND CHECKED ALL ELECTRICAL CABINETS AND CHECKED. CLOSED ALL CABINETS FOUND NO EVIDENCE OF BURNING OR SMOKE. C/W TASK 21-00-21-102-030-767.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

MAIN CARGO DECK FLOOR PANEL AT POS NR 6L HAS 1" HOLE. REPAIRED IAW SRM 53-00-50-2R.

Part: SKIN — PUNCTURED (BS 1919)

LT FUSELAGE SKIN PUNCTURE AT STA 1919 TOP OF FUSELAGE LBL 4. HOLE IS . 95". REPAIRED IAW EO B767-5330-46446-B.

Part: SKIN — DAMAGED (FUSELAGE)

FUSELAGE CROWN IS DAMAGED JUST FORWARD OF APU EXHAUST. REPAIRED IAW EO B767-5330-46446-A.

Part: FAILSAFE — UNKNOWN (BS 955) · airframe 41,596 hrs · 13,053 cycles

INSPECTION TYPE:8C INSTALLED A PROTECTIVE SHIM BETWEEN THE SKIN AND THE FAILSAFE STRAP ON RT SIDE IAW EO B767-5350-17922-J APPENDIX 'D' FIG 6, REPAIR IS CLASSIFIED AS A MAJOR.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,596 hrs · 13,053 cycles

INSPECTION TYPE:8C, EMERGENCY LIGHTS DID NOT STAY FOR 15 MINUTES. EMERGENCY LIGHTS BATTERY PACK REPLACED AND OPS TEST CARRIED OUT NORMAL. REF AMM 33-51-07.

Part: TEE FITTING — CORRODED (BS 955) · airframe 41,596 hrs · 13,053 cycles

INSPECTION TYPE:8C, FRETTING FOUND AT TEE FITTING FWD LOWER HOLE MATING SURFACE AREA, TEE FITTING REPLACED IAW EO B767-5350-17922-J, APPENDIX 'D' FIG 6. REPAIR IS CLASSIFIED AS A MAJOR.

Part: FLOORBEAM — CORRODED (MAIN DECK) · airframe 41,596 hrs · 13,053 cycles

INSPECTION TYPE:8C, M/D STA 1518 LBL 80.75, FLOORBEAM AFT FACE UPPER TEE FOUND CORRODED. REPAIRED IAW HX RS NR R53-65-37241 REV A & EO B767-5310-44765-A, ORIGINAL THICKNESS AT FWD FLANGE IS 0.150" & AFT FLANGE IS 0.180", CORROSION BLENDED OUT AREA AT FWD FLANGE IS DEPTH 0.044" X WIDTH 1" X LENGTH 2.5" & AFT FLANGE IS 0.079" X WIDTH 2" X LENGTH 5.

Part: WEDGE — DELAMINATED (LT WING TE FLAP) · airframe 41,596 hrs · 13,053 cycles

INSPECTION TYPE: 8C, LT WING OTBD T/E FLAP, T/E WEDGE MID AREA LWR SURFACE DELAMINATION. FIBERGLASS PREPERG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR5 A (1), FIG 9, REV 50.

Part: FLOOR PANEL — DAMAGED (BS 1540-1598) · airframe 41,596 hrs · 13,053 cycles

INSPECTION TYPE:C, MCD FLOOR PANEL FOUND 2 DAMAGED AND 8 DENTS AT STA 1540 TO STA 1598 LBL 55 TO LBL 80. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-06.

Part: FLOORBEAM — CORRODED (MAIN DECK) · airframe 41,596 hrs · 13,053 cycles

INSPECTION TYPE: C, MAIN DECK BS 1540 RBL 71.25" FLOORBEAM FWD FACE UPPER CHORD FOUND CORROSION. FLOORBEAM REPAIRED IAW RS R53-65-37244, REV A & EO B767-5310-44764-A, ORG MATERIAL IS BAC1506-4177-7075T6511 EXTRUSION, ORG THICKNESS 0.150" CORROSION BLEND OUT AREA DEPTH 0.072" X WIDTH 2" X LENGTH 5" REPAIR CLASSIFIED AS MAJOR REPAIR WITH MAT'L AND10134-2007-7075T6511 AS A REPAIR ANGLE, TOTAL REPAIR SIZE IS 10.5" X 1.25" X 1".

Part: FLOORBEAM — CORRODED (MAIN DECK) · airframe 41,596 hrs · 13,053 cycles

INSPECTION TYPE:8C, M/D STA 1540 LBL 75.25" TO LBL 78" FLOORBEAM FWD FACE UPPER CHORD FOUND CORROSION. REPAIRED IAW HX RS NR R-53-65-37243 REV A & EO B767-5310-44767-A, ORIGINAL THICKNESS IS 0.150", CORROSION BLENDED OUT AREA IS DEPTH 0.084" X WIDTH 2" X LENGTH 8", CLASSIFIED AS A MAJOR REPAIR.

Part: TEE FITTING — CRACKED (BS 955) · airframe 41,596 hrs · 13,053 cycles

INSPECTION TYPE:8C, FUSELAGE BS 955 LT REAR SPAR BULKHEAD FITTING AREA WAS FOUND 1 EA FASTENER HOLE CRACKED ON 6 O/C POSITION AT TEE FITTING APPROX .1250" IN LENGTH. TEE FITTING REPLACED IAW EO NR B767-5350-17922-J APPENDIX 'C', FIG 6, CRACK APPROX .1250" IN LENGTH, REPAIR IS CLASSIFIED AS A MAJOR.

Part: FAILSAFE — CRACKED (BS 955) · airframe 41,596 hrs · 13,053 cycles

INSPECTION TYPE:8C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FITTING WAS FOUND 1EA FASTENER HOLE CRACKED AT FAILSAFE STRAP ON 2 O/C AND 4 O/C POSITION THROUGH THICKNESS AND .1250" IN LENGTH. REPAIRED IAW EO B767-5350-17922-J APPENDIX 'C', REPAIR IS CLASSIFIED AS A MAJOR.

Part: FAILSAFE — CRACKED (BS 955) · airframe 41,596 hrs · 13,053 cycles

INSPECTION TYPE:8C, FUSELAGE RT BS 955 FAILSAFE STRAP FOUND CRACKED. REPAIRED IAW EO B767-5350-17922-J APPENDIX 'D'. REPAIR IS CLASSIFIED AS A MAJOR.

Part: FAILSAFE — CRACKED (BS 955) · airframe 41,596 hrs · 13,053 cycles

INSPECTION TYPE:8C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD FITTING FAILSAFE STRAP AREA, CRACK FOUND, REMOVE FASTENER FOR NDT CONFIRMATION. REMOVED AND REINSTALLED IAW EO NR B767-5350-17922-J APPENDIX 'C' FIG 6. REPAIR IS CLASSIFIED AS A MAJOR.

Part: FAILSAFE — CRACKED (BS 955) · airframe 41,596 hrs · 13,053 cycles

INSPECTION TYPE:8C, FUSELAGE RT BS 955 REAR SPAR BULKHEAD FITTING FAILSAFE STRAP AREA CRACK FOUND, REMOVE FASTENER FOR NDT CONFIRMATION. R & R IAW EO B767-5350-17922-J APPENDIX 'D' FIG 6. REPAIR IS CLASSIFIED AS A MAJOR.

Part: FLOORBOARD — DAMAGED (MAIN DECK)

FLOORBOARD DAMAGED FED OF MAIN CARGO DOOR. FABRICATED IAW EO B767-5320-9693-H.

Part: FLOORBOARD — DAMAGED (MAIN DECK)

FLOORBOARD DAMAGED AFT OF MAIN CARGO DOOR LT SIDE. FABRICATED IAW EO.

Part: FLOOR PANEL — DAMAGED (CARGO BAY)

NUMEROUS HOLES IN MAIN CARGO FLOOR PANEL, POS 2L, JUST FWD OF MAIN CARGO DOOR OPENING. FABRICATED NEW PANEL IAW EO B767-5320-9693-H.

Part: COMPRESSOR — STALLED (RT ENGINE)

INSPECTION TYPE:ETOP, RT ENGINE HAD 4 COMPRESSOR STALLS AT 200 FT, NO HIGH EGT OR ENGINE EXCEEDENCE. CHECKLIST WAS ACCOMPLISHED, TRIED ONE MORE RECOVERY, HOWEVER ENGINE STALLED AGAIN. ENGINE WAS SHUTDOWN, LANDING WEIGHT WAS 320.00. R & R ENGINE.

Part: PRESSURE SWITCH — INOPERATIVE (LT ENGINE)

E-TOP DIVERSION LT ENGINE ANTI-ICE DISPLAYED AND ENGINE ANTI ICE VALVE REMAINED ILLUMINATED WITH SWITCH ON. REPLACED LT ENG ANTI ICE VALVE IAW MM 30-21-03-4 AND THERM A/I PRESS SWITCH IAW MM 30-21-04-4. OPS CHECK NORMAL.

Part: FLOOR PANEL — DAMAGED (CARGO BAY)

D424528 MAIN CARGO POS 4 L FLOOR PANEL 2ND FR PM OTBD HAS .5" HOLE. REMOVED AND MFG NEW FLOOR PANEL IAW B767-5320-9693G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY)

D424529 MAIN CARGO POS 5 L FLOOR PANEL 2ND FROM OTBD HAS .5" HOLE. REMOVED AND MFG NEW FLOOR PANEL IAW B767-5320-9693G.

Part: SKIN — MISREPAIRED (BULK CARGO DOOR) · airframe 37,233 hrs · 11,558 cycles

SURVEY SEQUENCE NR 314-F1-06 BULK CARGO DOOR FWD LWR STA1423.5 TO 1431 THE EXISTING REPAIR DOES NOT CORRELATED TO A SRM DUE NO CUTOUT FOUND. FX SURVEY SEQUENCE NR 314-F1-06 BULK CARGO DOOR FWD LWR EDGE AT STA 1423.5 TO 1431 AREA SKIN REPAIRED IAW RS R52-36-36580 ORG MATL & THICKNESS ARE CLAD2024T3 0.071" CHEM-MILLED SKIN. NEW CUTOUT IS 2.15" X 1.75". THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR. REPAIR SIZE 10" X 4.75". FOLLOW UP ACTION IS REQUIRED REF EO B767-5230-36207.

Part: FLOOR SUPPORT — CRACKED (BS 246) · airframe 37,233 hrs · 11,558 cycles

STA 246 CABIN FLOOR STRUCTURE ATT CLIP FOUND CRACKED JUST AT RBL10". AV COMPT STA 246 CABIN FLOOR STRUCTURE ATTACH CLIP AT RBL10" REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 45.

Part: SKIN — MISREPAIRED (BS 382-398) · airframe 37,233 hrs · 11,558 cycles

FX - SURVEY SEQUENCE NR 314-F1-04 STA382 TO 398 BETWEEN STR33L TO 35L THE EXISTING REPAIR NOT CORRELATE TO SRM DUE TOO CLOSE OF 314-F1-03 EXISTING REPAIR DOUBLER. FX SURVEY SEQUENCE NR 314-F1-04 STA382 TO 398 BTN STR33L-35L SKIN REPAIRED IAW RS R53-11-36575 ORG MATL & THICNESS ARE CLAD2024T3 CHEM-MILLED SKIN 0.056" AT EXISTING CUTOUT WITH SIZE 1" X 3.75" THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR. REPAIR SIZE IS 14" X 8" FOLLOW UP ACTION IS REQUIRED REFER EO B767-5330-36226-A.

Part: SKIN — MISREPAIRED (BS 362-374) · airframe 37,233 hrs · 11,558 cycles

SURVEY SEQUENCE NR 314-F1-03 STA 362 TO 374 BETWEEN STR31L AND 33L EXISTING REPAIR NOT CORRELATED TO SRM DUE TOO CLOSE OF 314-F1-04 EXISTING REPAIR DOUBLER. FX SURVEY SEQUENCE NR 314-F1-03 STA362 TO 374 BTN STR31L-33L SKIN REPAIRED IAW RS R53-11-36575 ORG MATL AND THICKNESS ARE CLAD2024T3 CHEM-MILLED SKIN 0.056" AT EXISTING CUTOUT WITH SIZE 1" X 1.75". THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR. REPAIR SIZE IS 12" X 8 1/4" FOLLOW UP ACTION IS REQUIRED REFER EO B767-5330-36226-A.

Part: SPAR — CRACKED (RT WING) · airframe 37,233 hrs · 11,558 cycles

RT WING L/E LES675 FIXED FAIRING SUPPORT RIB AFT FRONT SPAR ANGLE FOUND CRACKED. RT WING L/E LES675 FIXED FAIRING SUPPORT RIB AFT FRONT SPAR ANGLE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02, REV 45.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 37,233 hrs · 11,558 cycles

INSPECTION TYPE:SPV-RT WING INBD AFT FLAP LOWER SURFACE INBD T/E FOUND DELAMINATED ON THE EXISTING REPAIR PATCH OTBD EDGE. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10 REPAIR 4, FIG 202, SHEET 1 REV 45.

Part: SUPPORT FITTING — CRACKED (RT WING TE FLAP) · airframe 37,233 hrs · 11,558 cycles

INSPECTION TYPE:SPV-RT WING INBD MAIN FLAP, INBD AFT FLAP SUPPORT FITTING FOUND CRACKED. RT INBD MAIN FLAP AFT FLAP SUPPORT FITTING REPAIRED IAW SRM 57-53-02-2R1 FIG201, REV45. INBD FLANGE CRACK LENGTH 1.25". OTBD FLANGE CRACK LENGTH 1.5" BOTH INBD & OTBD CUTOUT SIZE 1.5" X 0.75" THIS REPAIR IS CLASSIFIED AS A MAJOR.

Part: SKIN — CRACKED (NR 4 SLAT) · airframe 37,233 hrs · 11,558 cycles

INSPECTION TYPE:SPV-LT WING NR 4 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT INBD AREA AT OSS573.25 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG201 REV 45. CRACK LENGTH IS 0.25" DAMAGED CUTOUT IS 8.875" X 7.25" THIS REPAIR IS CLASSIFIED AS A MAJOR.

Part: SKIN — CRACKED (NR 3 SLAT) · airframe 37,233 hrs · 11,558 cycles

INSP TYPE:SPV-LT WING NR 3 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 3 SLAT INBD AREA AT OSS724.61 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG201 REV45. CRACK LENGTH IS 0.125" DAMAGED CUTOUT IS 8.875" X 7.125" THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: SKIN — CRACKED (NR 4 SLAT) · airframe 37,233 hrs · 11,558 cycles

INSPECTION TYPE:SPV-LT WING NR 4 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT OTBD AREA AT OSS641.5 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG201, REV 45. CRACK LENGTH IS 0.125" DAMAGED CUTOUT IS 8.875" X 7.5" THIS REPAIR IS CLASSIFIED AS A MAJOR.

Part: ATTACH FITTING — CRACKED (BS 1087) · airframe 37,233 hrs · 11,558 cycles

INSPECTION TYPE:C-AFT CARGO STA 1087 FWD PARTITION BELOW FLOOR LBL 25 CLIP FOUND CRACKED. AFT CARGO STA 1087 LBL 25 FWD PARTITION BELOW FLOOR ATTACH CLIP REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV45.

Part: SKIN — CRACKED (NR 9 SLAT) · airframe 37,233 hrs · 11,558 cycles

INSPECTION TYPE:C-RT WING NR 9 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED RT WING NR 9 SLAT INBD AREA AT OSS573.125 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG201, REV45. CRACK LENGTH IS 0.125" DAMAGED CUTOUT IS 9" X 7.125" THIS REPAIR IS CLASSIFIED AS A MAJOR.

Part: SKIN — CRACKED (NR 9 SLAT) · airframe 37,233 hrs · 11,558 cycles

INSP TYPE:SPV- RT WING NR 9 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 9 SLAT OTBD AREA AT OSS641.6 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG201 REV 45. CRACK LENGTH IS 0.160" DAMAGED CUTOUT IS 8.875" X 7.25" THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: SKIN — CRACKED (NR 10 SLAT) · airframe 37,233 hrs · 11,558 cycles

INSPECTION TYPE:SPV-RT WING NR 10 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 10 SLAT OTBD AREA AT OSS792.1 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG201, REV45. CRACK LENGTH IS 0.100" DAMAGED CUTOUT IS 8.875" X 7.25" THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: ATTACH FITTING — CRACKED (BS 1087) · airframe 37,233 hrs · 11,558 cycles

INSPECTION TYPE:SPV AFT CARGO STA 1087 FWD PARTITION BELOW FLOOR RBL 25 CLIP FOUND CRACKED. AFT CARGO STA 1087 RBL 25 FWD PARTITION BELOW FLOOR ATTACH CLIP REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV45.

Part: SKIN — CRACKED (NR 3 SLAT) · airframe 37,233 hrs · 11,558 cycles

INSPECTION TYPE:SPV-LT WING NR 3 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 3 SLAT O/B AREA AT OSS792.1 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201, REV 45. CRACK LENGTH IS 0.090" DAMAGED CUTOUT IS 8.875" X 7.25" THIS REPAIR IS CLASSIFIED AS A MAJOR.

Part: SKIN — CRACKED (NR 10 SLAT) · airframe 37,233 hrs · 11,558 cycles

INSPECTION TYPE:C - RT WING NR 10 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED RT NR 10 SLAT INBD AREA AT OSS724.35 NOSE SKIN REPAIRED AS IAW SRM 57-43-01-2R2 FIG201 REV45 ORG MATL IS CLAD7075T6-0.063" CRACK LENGTH IS 0.125" DAMAGED CUTOUT IS 8.875" X 7.125". THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR

Part: FLOOR PANEL — DAMAGED (BS 873-932) · airframe 37,233 hrs · 11,558 cycles

INSPECTION TYPE:7C MCD FLOOR PANEL AT STN 873-932 R77 TO R88 FOUND DAMAGED. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 37,233 hrs · 11,558 cycles

INSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGED AT STN 1197+22 - 1207, R55 TO R77. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.

Part: FLOOR PANEL — DAMAGED (BS 1480-1598) · airframe 37,233 hrs · 11,558 cycles

INSPECTION TYPE:7C MCD FLOOR PANEL AT STN 1480-1598 L33 TO L55 FOUND DAMAGED. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.

Part: FLOOR PANEL — DAMAGED (BS 1480-1598) · airframe 37,233 hrs · 11,558 cycles

INSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STN 1480-1598 R33 TO R55. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.

Part: FLOOR PANEL — DAMAGED (BS 412-540) · airframe 37,233 hrs · 11,558 cycles

INSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STN 412-540 L11 TO R11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 37,233 hrs · 11,558 cycles

INSPECTION TYPE: 7C, MCD FLOOR PANEL FOUND DAMAGE AT STN 1197+22 - 1207 L55 TO L77. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 37,233 hrs · 11,558 cycles

INSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGED AT STN 1114 TO 1197+22 R55 TO R77. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.

Part: FLOOR PANEL — DAMAGED (BS 1370-1480) · airframe 37,233 hrs · 11,558 cycles

INSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STN 1370-1480 R33 TO R55. FLOOR PANEL FABRICATED EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.

Part: FLOOR PANEL — DAMAGED (BS 1480-1598) · airframe 37,233 hrs · 11,558 cycles

INSPECTION TYPE:7C MCD FLOOR PANEL AT STN 1480-1598 L11 TO R11 FOUND DAMAGED. FLOOR PANEL FABRICATED, EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.

Part: FLOOR PANEL — PUNCTURED (CARGO DECK) · airframe 37,233 hrs · 11,558 cycles

INSPECTION TYPE:7C DMI NR D415072 POSITION 11R MCD FLOOR HAS A 3/16" HOLE. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.

Part: FLOORBOARD — PUNCTURED (CARGO DECK) · airframe 37,233 hrs · 11,558 cycles

INSPECTION TYPE:7C DMI NR D415075 POSITION 5 HAS A 1/2" HOLE IN THE CENTER FLOORBOARD. FLOORBOARD FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.

Part: FLOOR PANEL — PUNCTURED (CARGO DECK) · airframe 37,233 hrs · 11,558 cycles

INSPECTION TYPE:7C DMI NR D415073 POSITION 7R MCD HAS 2 HOLES, ONE 3/16" AND THE OTHER 1/2". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.

Part: CONTROL PANEL — DEFECTIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REMOVED & REPLACED OVERHEAD EMERGENCY LIGHT CONTROL PANEL. OPS CHECKED GOOD PER MM 33-54-08-4.

Part: LIGHT — INOPERATIVE (COCKPIT)

EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE WHEN IN THE OFF POSITION. PERFORMED TEST OF EMERGENCY LIGHTS REF AMM 33-51-00-5. OPS CHECK NORMAL.

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

INSPECTION TYPE:N/A FLOOR PANEL DAMAGED FS 486 AND 491 LBL 84. REPAIRED PER EO B767-5320-32227-A.

Part: FLOORBOARD — DAMAGED (MAIN CARGO BAY)

INSPECTION TYPE:N/A FLOORBOARD DAMAGED FS 1096. REPAIRED PER SRM 53-00-50-2R.

Part: FLOORBOARD — DAMAGED (MAIN CARGO BAY)

INSPECTION TYPE:N/A FLOORBOARD DAMAGED FS 694. REPAIRED PER SRM 53-00-50-2R.

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

INSPECTION TYPE:N/A FLOOR PANEL DAMAGED FS 964 RBL 4. REPAIRED PER EO B767-5320-32226-A.

Part: MODULE — MALFUNCTIONED (RUDDER TRIM)

RUDDER TRIM STUCK AT 4 UNITS. T/S IAW FIM 27-21-00 FIG 106 FOUND RUDDER TRIM CONTROL PANEL FAULT. R/R AILERON AND RUDDER TRIM CONTROL MODULE IAW MM 27-21-23-2. OPS GOOD.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 32,240 hrs · 9,974 cycles

INSPECTION TYPE:C FX- MEC STA 246 LBL 40 CABIN FLOORBEAM STIFFENER FOUND CRACK (CRACK LENGTH 2"). FX MEC STA 246 LBL 40" CABIN FLOORBEAM STIFFENER REPAIRED AS PER SRM 53-10-51-2R4 FIG 201, REF UPS MPI P19656.

Part: SKIN — PUNCTURED (LT MLG DOOR) · airframe 32,240 hrs · 9,974 cycles

INSPECTION TYPE:C LEFT MLG DOOR INNER SURFACE FOUND PUNCH HOLE AT O/B AREA AS MARKED. COMPOSITE REPAIR CARRIED OUT AS PER HX RS#R-52-80-35973A AND UPS ENGINEERING FILE 767-32-20012 THE REPAIR PROCEDURE REFER SRM 51-70-05 PAR 5A (1) AND HX PROCESS CARD CONTROL SEQ AWC504651-1.

Part: ENGINE — BIRD INGESTION (NR 1)

INSPECTION TYPE: ETOP FOD - BIRD STRIKE NR 1 ENGINE. EMERGENCY DECLARED. ON SHORT FINAL CREW REPORTED BIRD INGESTION IN NR 1 ENGINE. ENGINE VIBRATION REACHED 3.8 AND WAS REDUCED TO IDLE. A/C IS OOS. FOUND DAMAGE BLADES 24,25,26,27 BEYOND REPAIR. INSTALLED BLD INGT POS 7-178310 & INT IN POS 26, INST NEW 177208IN POS 6, INST NEW 178246 IN POS 7, INST NEW 177486 IN POS 27, ALL AS PER AMM 72-31-02-4.

Part: APU — MALFUNCTIONED

INSPECTION TYPE:ETOP APU INOP, WILL NOT START DEFERRED PER MEL 49-11-1-0-2. INSTALLED NEW ECU, NO HELP. PLACARD INSTALLED. D356179 *SUPPLEMENTAL SDR* APU OPS CHECK IAW AMM 49-11-00 SATISFACTORY. DMI 356179 NOW CLOSED.

Part: CONNECTOR — DAMAGED (LT ENGINE)

INSPECTION TYPE:ETOP LT ENGINE PRSOV INOP. FOUND CONNECTOR D17066P RUBBER DETERIORATED AND PIN 1 LOCK BROKEN. REMOVED AND REPLACED CONNECTOR PER WEM 36-11-62 & CHECKED PER MM 36-11-005 & ALL CHECKS NORMAL. ALL VALVES RETURNED TO NORMAL CONFIGURATION.

Part: SMOKE GOGGLES — CRACKED (CABIN)

LEFT SUPERNUMERARY SMOKE GOGGLES CRACKED. REMOVED AND REPLACED SMOKE GOGGLES.

Part: STRUT — FAILED (NLG DOOR)

AIR TURN BACK DUE TO NOSE GEAR DOOR UPLATCH BROKE DURING GEAR RETRACTION WITH VIBRATION. FOUND RT NOSE GEAR DOOR STRUT ASSY FAILED INTERNALLY.

Part: PANEL — CRACKED (L/E SLAT)

INSPECTION TYPE:IN L-SHAPED CRACK IN NR 6 L/E SLAT LOWER SIDE, FWD OF INBOARD TRACK. REPAIRED SLAT CLOSE OUT PANEL AS PER SRM 51-70-07.

Part: STRINGER — CRACKED (FUSELAGE)

CRACK FOUND DURING HFEC INSP OF GOUGE AT STA 460 STR 31R REMOVED FASTNERS IN AREA COMMON TO REPAIR REINSTALLED FASTNERS IAW BOEING 767 SRM 51-40-00 INTERIM REPAIR HAS BEEN RECLASSIFIED AS PERMANENT REPAIR PER BOEING AND UPS EO B767 5330-14262