N323UP

Part: STRAP — CRACKED (ZONE 100) · airframe 68,977 hrs · 22,983 cycles

CRACKED BULKHEAD OUTER CHORD STRAP AT BS 1725 S-7R. (REPAIR). COMPLETED REPAIR I.A.W EGAT WORK SHEET NO.40938 STEP D.5 AND D.6 AND D.8 AND D.10 AND D.11 AND D.13~D.19. ACCOMPLISHED UPS EO NO. EO-24301-JIC003 REV. 4 AND EGAT WORK SHEET NO. 40938.

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 69,007 hrs · 22,994 cycles

FOUND M/D FLOOR PNL NO. 241DFF BROKEN AT STA 731 TO STA 834 LBL-65, P/N : 145T5876-63.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 68,977 hrs · 22,983 cycles

FOUND M/D FLOOR PNL NO.241GFF DENT AT STA 834 TO STA 933 LBL-22, P/N: 145T5876-59. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.

Part: SKIN — DAMAGED (ZONE 500 SLAT) · airframe 68,977 hrs · 22,983 cycles

BIRD STRIKE - SKIN, UPPER FACE OF L/H WING NO.4 SLAT T/E SKIN, OSS 545.75.JOB COMPLETED AND CONDITION CHECK NORMAL AND ATTACHMENT ARE UPLOADED. I.A.W AMM 27-81-02-424-099 REV.143 STEP 3A TO H (16) INSTALLED NO.4 SLAT OF THE LH WING.

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 68,977 hrs · 22,983 cycles

FOUND M/D FLOOR PNL NO.241CFF DENT AND INSERT DAMAGE AT STA 731 TO STA 834 LBL-45, P/N:145T5876-65. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 68,977 hrs · 22,983 cycles

FOUND M/D FLOOR PNL NO.241EFF DENT AT STA 746 TO STA 876 LBL 80, P/N:145T5876-1.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 68,977 hrs · 22,983 cycles

FOUND M/D FLOOR PNL DENT AND INSERT DAMAGE AT STA 988 TO STA 1114 LBL 65 PNL NO.241ZFF, P/N:145T5876-77.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 69,007 hrs · 22,994 cycles

FOUND M/D FLOOR PNL DENT AND BROKEN AT STA 1040 TO STA 1114 LBL-45, P/N: 145T5876-43, PANEL NO 241BGF. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.

Part: FLOOR PANEL — DEBONDED (ZONE 200) · airframe 68,977 hrs · 22,983 cycles

FOUND M/D FLOOR PNL NO.241BFF DISBOND AT STA 731 TO STA 834 LBL-22, P/N:145T5876-70. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 68,977 hrs · 22,983 cycles

BROKEN - FOUND M/D FLOOR PNL BROKEN AT STA933 TO STA980 RBL-80 P/N: 145T5876-84 , PANEL NO.242MFF. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 68,977 hrs · 22,983 cycles

FOUND M/D FLOOR PNL DISBOND AND DENT AT STA 746 TO STA 876 RBL -80 PNL NO.242DFF, P/N: 145T5876-7. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 68,977 hrs · 22,983 cycles

FOUND M/D FLOOR PNL NO.241WFF DENT AT STA 980 TO STA-1114 LBL11, P/N: 145T5876-73. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 68,977 hrs · 22,983 cycles

DENT - FOUND M/D FLOOR PNL NO.242FFF AT STA 834 TO STA 933 RBL -45, P/N: 145T5876-61.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.

Part: FLOOR PANEL — DENTED (ZOEN 200) · airframe 68,977 hrs · 22,983 cycles

FOUND FLOOR PNL NO.241QFF DENT AT STA 933 TO STA 980 LBL-80, P/N: 145T5876-78. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.

Part: SPLINE — BROKEN (ZONE 800) · airframe 68,977 hrs · 22,983 cycles

FOUND MAIN ENTRY DOOR DOORWAY SPLINE TRIM BROKEN. (REPLACE) OK TO WORK.

Part: SKIN — CORRODED (ZONE 100) · airframe 68,977 hrs · 22,983 cycles

CORROSION , FUSELAGE SKIN STA 1410 BETWEEN S-38R AND S-39R. ACCOMPLISH REPAIR PER EO-91974-REQ1 AND EGAT EI F2024A53M-2800, REV. 0 AND 1.

Part: TRIM PANEL — BROKEN (MAIN DOOR) · airframe 69,018 hrs · 22,998 cycles

FOUND MAIN ENTRY DOOR DOORWAY SPLINE TRIM BROKEN. REPLACED SPLINE TRIM I.A.W AMM 52-12-02-004-001 REV.143 AND AMM 52-12-02-404-025 REV.143.

Part: ADAPTER — CRACKED (ZONE 200) · airframe 68,977 hrs · 22,983 cycles

FOUND THE MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING WITH CRACK DAMAGE AT STA 1109 BL 0.REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 90.INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 90. AND BOEING DWG NO. 457T4000 SH. 11 REV. B

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 68,977 hrs · 22,983 cycles

FOUND THE MAIN DECK CARGO FLOOR PANEL DENT , P/N: 146T5869-135. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 68,977 hrs · 22,983 cycles

FOUND THE MAIN DECK CARGO FLOOR PANEL DENT , P/N: 146T5869-134. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.

Part: NONE — NONE (NONE) · airframe 68,977 hrs · 22,983 cycles

FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. REVIEW COMPLETED PER EO-82173-J1C001.CONDITION CHECK OK

Part: FIRE SEAL — DAMAGED (ZONE 400) · airframe 68,827 hrs · 22,921 cycles

#2 ENG OUTBD ACCESS PANEL FOR ENG MOUNT BOLTS HAS A DAMAGED FIRE SEAL REMOVED AND REPLACED SEAL ON #2 ENG OUTBD ACCESS PANEL REF. SRM 51-40-02 AND IPC 54-52-01-19.

Part: FIRE SEAL — DAMAGED (NR 2 NACELLE) · airframe 68,829 hrs · 22,923 cycles

*SUPPLEMENTAL SDR* #2 ENG OUTBD ACCESS PANEL FOR ENG MOUNT BOLTS HAS A DAMAGED FIRE SEAL REMOVED AND REPLACED SEAL ON #2 ENG OUTBD ACCESS PANEL REF. SRM 51-40-02 AND IPC 54-52-01-19. RE-INSTALLED PANEL PER SRM 51-40-02.

Part: SLAT TRACK — DAMAGED (RT NR 7) · airframe 68,186 hrs · 22,659 cycles

R/H WING #7 SLAT TRACK LEADING EDGE PANEL DAMAGED. REMOVE AND REPLACED LEADING EDGE SUPPORT LINK DOOR R/H INB AS PER 57-41-59 404-009, OPS CHKS GOOD-

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 67,086 hrs · 22,288 cycles

CREW ENTRY DOOR ARMING LEVER HINGED COVER SPRING BROKEN DEFERRED CREW ENTRY DOOR HINGED COVER IAW MEL 52-11-2, PLACARDS INSTALLED. OPEN

Part: SPRING — BROKEN (CREW DOOR) · airframe 67,129 hrs · 22,308 cycles

*** SUPPLEMENTAL SDR *** CREW ENTRY DOOR ARMING LEVER HINGED COVER SPRING BROKEN REPLACED CREW ENTRY DOOR ARMING HINGE COVER REF MM 52-12-02 OPS CK GOOD THIS CLEARS DEFERRAL

Part: SLAT — INOPERATIVE (FUSELAGE) · airframe 65,156 hrs · 21,549 cycles

INSPECTION TYPE:NA*EMERGENCY DECLARED* LEADING EDGE SLATS DISAGREE RAN CHECKLIST AND CONFIGURED SUCCESFULLYBITE CARRIED OUT IAW FIM 27-51-00-815-809 FLAPS/SLATS EXTENDED/RETRACTED WITH NO FAULTS

Part: SKIN — MISREPAIRED (BS 676) · airframe 64,471 hrs · 21,273 cycles

TEMP BLIND FASTENER INSTALLED FUSELAGE 8" FWD OR STA 676 - 1 INCH O/B OF S39LREPAIRED IAW E.O. B767-5330-85085-B ON NRC 684229

Part: SKIN — MISINSTALLED (BS 676) · airframe 64,471 hrs · 21,273 cycles

INSPECTION TYPE:N/ATEMP BLIND FASTENER INSTALLED FUSELAGE 8 INCH FWD OR STA 676 - 1 INCH O/B OF S39LFABRICATED REPAIR DOUBLER IAW UPS E.O.B767-5330-85085-A ON NRC 684228

Part: THRUST REVERSER — INOPERATIVE (LEFT) · airframe 62,994 hrs · 20,758 cycles

INSPECTION TYPE:**ETOPS FILED OPEN** ON LANDING, L THRUST REV WOULD NOT DEPLOY. DEFERRED LEFT ENG T/R PER MEL 78-31-1 C/W DMP 78-31-

Part: ENGINE — SURGES (LEFT) · airframe 61,696 hrs · 20,295 cycles

IFSD, ATB, EMERGENCY DECLARED, AIRCRAFT OOS, APPROXIMATELY 200' AFTER TAKE OFF, ENG STARTED TO SURGE. DURING THE CLIMB THE L ENG HAD NO RESPONSE FROM THE L THRUST LEVER. RAN APPROPRIATE CHECKLIST AND SHUTDOWN L ENG. A/C AWAITING LEFT ENG CHANGE.R/R #1 ENGINE PER AMM 71-00-02, SN OFF- 704418, SN ON- 702140 PER UPS TC 6001 & TC 6002. COMPLED WITH REVISION OF UPS EO E-7900-62890, APPX B. ENGINE TEST & LEAK CHECK GOOD.

Part: PANEL — DAMAGED (CARGO FLOOR) · airframe 60,351 hrs · 19,775 cycles

INSPECTION TYPE: C12 DAMAGE ON MD CARGO FLOOR PANEL BETWEEN STA 510 - 620, LBL 11 - RBL 11. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NR B767-5320-9693-I.

Part: FLOORBEAM — CORRODED (MAIN DECK FLOOR) · airframe 60,351 hrs · 19,775 cycles

INSPECTION TYPE: C12 CORROSION WAS FOUND ON FLOOR BEAM PN 146T5144-11 OF MAIN DECK FLOOR STRUCTURE AT STA 1540, RBL 60 - RBL 80. REPAIR IAW BOEING SR 3-4942408700 AND UPS EO B767-5310-79230-A.

Part: FLOORBEAM — CORRODED (MAIN DECK FLOOR) · airframe 60,351 hrs · 19,775 cycles

INSPECTION TYPE: C12 CORROSION WAS FOUND ON FLOOR BEAM PN 146T5144-11 OF MAIN DECK FLOOR STRUCTURE AT STA 1540, LBL 60 - LBL 80. REPAIR IAW BOEING SR 3-4942408700 AND UPS EO B767-5310-79230-A.

Part: FLOORBEAM — CORRODED (MAIN DECK) · airframe 60,351 hrs · 19,775 cycles

INSPECTION TYPE:C12CORROSION WAS FOUND ON FLOOR BEAM (P/N : 146T5143-5) OF MAIN DECK FLOOR STRUCTURE AT STA 1518 , RBL 70 - RBL 90REPAIR I.A.W BOEING SR 3-4942597086 AND UPS EO B767-5310-79232-A

Part: STIFFENER — CRACKED (FUEL TANK) · airframe 60,351 hrs · 19,775 cycles

INSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER (P/N : 111T2011-5) ON STA 785.9 , LBL 55REAPIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.79.01 AND UPS EO B767-5740-58151-C

Part: STIFFENER — CRACKED (FUEL TANK) · airframe 60,351 hrs · 19,775 cycles

INSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER (P/N : 111T2008-11) ON STA 785.9 , LBL 33REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.79.01 AND UPS EO B767-5740-58151-C

Part: ACTUATOR — LEAKING (RUDDER RATIO) · airframe 60,290 hrs · 19,760 cycles

INSPECTION TYPE: NA, ATB, NO EMERGENCY DECLARED & NO EQUIPMENT USED. T/O & 38 MINS GOT L HYD QUANTITY EICAS LT QUANTITY L HYD PRIM PUMP. EICAS LIGHT CAME ON WHEN USING SPEEDBRAKES. ARRIVED WITH ZERO FLUID IN LT SYS. NEVER LOST SYSTEM PRESSURE FOUND ELECTRO-HYD SERVO VALVE ON RUDDER RATION CHGR ACT LEAKING FROM PLUG ON SIDE OF VALVE, REF AMM 27-21-15. R & R RRCA SOLENOID VALVE, AS PER AMM 27-21-15-201. OPERATIONS CHECK OK, PER AMM 27-21-15-422-024. NO LEAK NOTED AT THIS TIME.

Part: MODULE — MALFUNCTIONED (WARNING BELL) · airframe 59,460 hrs · 19,433 cycles

INSPECTION TYPE: N/A ATB- EMERGENCY DECLARED. RECEIVED FIRE WARNING BELL ON TAKE OFF ROTATION COULD NOT EXTINGUISH. R & R M1000 BELL CHIME MODULE BOARD, PER MM 31-51-04-004-133/404-014. TEST PER AMM 31-51-04-724-154. PN ON AND OFF 285T0385-5. SN OFF 01860 ON D01475. IPC REF 31-51-04-05C ITM 145.

Part: STIFFENER — CRACKED (BS 287) · airframe 55,748 hrs · 18,069 cycles

INSPECTION TYPE:C11CRACK ON VERTICAL STIFFENER AT WHEEL WELL BULKHEAD AT STA 287,RBL 25, WL 159.REPAIR I.A.W UPS EO B767-5310-20118-F AND 767-300F SRM 51-70-12 GENERAL, FIGURE 1 , REV 73.01

Part: SHUTOFF VALVE — FAULTY (AC BAY) · airframe 55,513 hrs · 17,991 cycles

INSPECTION TYPE:N/A ATB - DUE TO CABIN ALTITUDE. AFTER ACCOMPLISHING THE QRH PROC CABIN REMAINED UNCONTROLLABLE. PERFORMED PRESSURE CONTROLLER BITE PROCEDURE FOUND NR 2 LOW IN FLOW FAULT FIM 21-31-00-815-803/REF TS-B767-2150-00007 FOUND LEFT PACK "LO" FLOW 25% LESS THAN RIGHT PACK. REMOVED & REPLACED LEFT PACK FLOW CONTROL AND S.O. VALVE REF AMM 21-51-01-401. AFTER REPLACEMENT.

Part: CONTROLLER — MALFUNCTIONED (CABIN TEMP) · airframe 55,209 hrs · 17,874 cycles

EICAS MESSAGE FOR THE AFT CABIN TEMP INOPERATIVE. OPEN

Part: BLADE — DAMAGED (1ST STAGE HPT) · airframe 54,979 hrs · 17,789 cycles

PERFORMED A BORESCOPE INSPECTION ON THE NR 2 ENGINE IAW PMC 6. FOUND 1ST STAGE HPT BLADE MISSING MATERIAL ON THE LEADING EDGE, MEASURING DIMENSION GREATER THAN 5 EDGE HOLES IAW MM 72-00-00-206-363-H00, TABLE 680 FOR MAX SERVICABLE LIMITS.

Part: BLADE — MISSING (HP TURBINE) · airframe 54,979 hrs · 17,789 cycles

INSPECTION TYPE:N/A**SUPPLEMENTAL SDR** PERFORMED BORESCOPE INSPECTION #2 ENG PER PMC 6. FOUND 1ST STAGE HPT BLADE MISSING MATERIAL ON LEADING EDGE MEASURING DIMENSION GREATER THAN 5 EDGE HOLES. REFER TO AMM 72-00-00-206-363-H00 TABLE 680 FOR MAX SVCABLE LIMIT PICS EMAIL TO ENGINE.TRANSFERRED TO NON ROUTINE CARD 513828, DMI CLEARED. REMOVED ESN 704761 AND INSTALLED ESN 707222 PER UPS TC 6001 AND 6002. COMPLY WITH CURRENT REVISION OF UPS EO E-7900-62890 APPENDIX B.

Part: PUMP — MALFUNCTIONED (FUEL SYSTEM) · airframe 54,783 hrs · 17,725 cycles

ENGINE FUEL FEED SYSTEM L, FWD FUEL PUMP EICAS MSG SHOWS AND L FWD PUMP PRESS LIGHT IS ON WITH SWITCH ON. REPLACED L FWD FUEL PUMP GFI, RELAY REF FIM 28-22-00 FIG 114 & WDM 28-22-11, RELAY K10703 [TJQ 0558733 9-4-18] SYSTEM OPS CHECKS OK. REF FIM FIG 114, 28-22-00. IPC 28-22-03-410, ITEM 010.

Part: MODULE — FAULTED (RUDDER RATIO) · airframe 53,742 hrs · 17,368 cycles

AIR TURNBACK. AFTER TAKEOFF, THE RUDDER RATIO EICAS ILLUMINATED. FOUND THE RIGHT RUDDER RATIO CHANGER MODULE FAULTED. R & R THE MODULE IAW MM 27-09-00. OPS CHECKED GOOD IAW MM 27-21-00.

Part: BRACKET — DAMAGED (EMERGENCY LIGHT) · airframe 53,059 hrs · 17,128 cycles

L1 DOOR INTERIOR EMERGENCY EXIT LIGHT DAMAGED. R & R THE SIGN IAW MM 33-51-01-962-028. REPAIRED THE MOUNTING BRACKET IAW EO 5210 67082 B, PARAGRAPH 6.

Part: FUEL CONTROL — MALFUNCTIONED (APU) · airframe 52,510 hrs · 16,924 cycles

APU GEN OFF LIGHT, NO RESET INFIGHT TURNBACK, ONE ELECT POWER SOURCE. AHM SHOWS AT 370' APU COULDN'T MAINTAIN 95%. R & R THE APU FUEL CONTROL IAW MM 49-31-01, OPS AND LEAK CHECKED GOOD.

Part: STIFFENER — CRACKED (BS 785) · airframe 51,179 hrs · 16,445 cycles

INSPECTION TYPE: C10, CRACK ON STIFFENER UPPER SIDE AT BS 785.9, RBL 33. REPAIR IAW SRM 57-10-10-2R-2, REPAIR 2, REV.67 AND EO B767-5740-58151-A

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 51,179 hrs · 16,445 cycles

INSPECTION TYPE: C10, CRACK ON INBD SIDE SKIN AND DOUBLER OF THE NR 2 PYLON. REPAIRED THE PYLON IAW SR 3-3822893601 AND EO B767-5430-63695-A.

Part: LIFE VEST — UNSERVICEABLE · airframe 49,570 hrs · 15,887 cycles

FOUND DURING PS1 CHECK, LIFE VEST OF LT SUPERNUMERARY SEAT UNSERVICEABLE. REMOVED AND REPLACED THE LIFE VEST IAW AMM 25-62-00 REV. 118.02.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 49,570 hrs · 15,887 cycles

FOUND DURING PS1 CHECK, LIFE VEST OF F/O SEAT UNSERVICEABLE. R & R THE LIFE VEST IAW AMM 25-62-00 REV. 118.02.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 47,424 hrs · 15,075 cycles

AFTER RESTORING THE CAPTAIN`S OXYGEN MASK INFLIGHT, THE MASK DOES NOT TEST CORRECTLY WHEN THE RED EMERGENCY BUTTON IS PUSHED. REPACKED CAPTS OXYGEN MASK. PERFORMED AMM TASK 35-11-00-715-224. MASK CHECKS NORMAL.

Part: STRINGER — CRACKED (BS 1550) · airframe 46,684 hrs · 14,812 cycles

INSPECTION TYPE:C9, A THREE INCH CRACK WAS FOUND ON STRINGER 20R AT BS 1550, REPAIR IAW SR 4-2882995662 AND EO B767-5310-57269-A.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 46,684 hrs · 14,812 cycles

INSPECTION TYPE:C9, FOUND CRACK ON M/D CARGO FLOOR PANEL, 242GFF AT FS 850, RBL 54.75 - RBL 74.25, FABRICATE THE REPLACEMENT FLOOR PANEL IAW EO NR B767-5320-9693-H.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 46,684 hrs · 14,812 cycles

INSPECTION TYPE: C9, FOUND CRACK ON M/D CARGO FLOOR PANEL, 232GFF AT BS 533-654+22, RBL 33-55, FABRICATE THE REPLACEMENT FLOOR PANEL IAW EO NR B767-5320-9693-H.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 46,684 hrs · 14,812 cycles

INSPECTION TYPE:C9, FOUND CRACK ON M/D CARGO FLOOR PANEL, 232FFF, AT BS 620, RBL 11- 33 FABRICATE THE REPLACEMENT FLOOR PANEL IAW EO NR B767-5320-9693-H.

Part: SKIN — PUNCTURED (BS 1630) · airframe 46,684 hrs · 14,812 cycles

INSPECTION TYPE:C9, PUNCTURE HOLE DAMAGE, LENGTH=0.67", WIDTH=0.5", WAS FOUND ON SKIN OF TAIL FUSELAGE SECTION 48 AT STA 1630, BETWEEN S-36R AND S-38R. REPAIR IAW SR 3-3223765412 WITH APPROVED 8100-9 FORM DATED:22APR2015 AND EO B767-5310-57268-A.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

MAIN CARGO DECK FLOOR PANEL DAMAGED. FABRICATE A NEW FLOOR PANEL IAW EO 5320-9693-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

FLOOR PANEL DAMAGED. REPAIRED IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

FLOOR PANEL DAMAGED. REPAIRED IAW -5320-9693-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

FLOOR PANEL DAMAGED. REPAIRED IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (BS 726)

HOLE IN MCD FLOOR PANEL POS 4L AT BS 726. REPAIRED HOLE IAW SRM 53-00-2R-4B.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

MAIN CARGO FLOOR PANEL DAMAGED. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-H AND DWG 141T5856.

Part: SKIN — DELAMINATED (VERTICAL STAB)

VERTICAL STABILIZER LT SIDE LOWER PANEL DELAMINATED.. TRANSFERRED TO NRC 529065 FOR PANEL REPLACEMENT. COMPLETED PANEL REPLACEMENT IAW EO B7U67-5530-55201-A. MAJOR REPAIR

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHTS INTERMITTENT. WILL NOT STAY ON. R & R BATTERY PACK IAW MM 33-51-07-33-51-07-32. OPS CHECKED GOOD.

Part: OVERHEAT SENSOR — INOPERATIVE

AIR TURNBACK, DURING CLIMBOUT, RT BLEED DUCT LEAK EICAS AND OVERHEAD LIGHT DISPLAYED. RAN QRH CHECKLIST. R & R RT WING/BODY DETECTOR ELEMENTS IAW MM 26-18-01-024-001-001, PERFORMED DUCT LEAK CHECK AND ELMENT SYSTEM TEST. ALL CHECKS GOOD.

Part: SKIN — PUNCTURED (RT ELEVATOR)

RIGHT ELEVATOR LOWER SKIN PUNCTURED. REPAIRED IAW EO 5520-54318-A.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMPS EMERGENCY EXTERIOR LIGHT IAW AMM 33-51-16. OPS CHECKED GOOD.

Part: FAILSAFE — DAMAGED (FUSELAGE) · airframe 426,281 hrs · 13,213 cycles

INSPECTION TYPE:C08, DURING WORK OF SB 53-0116 & REQUIREMENT OF SB 53A0100, FOUND CORROSION DAMAGE TO SKIN COMMON TO FAILSAFE STRAP INTERFACING SURFACE FROM S-20R TO OVERWING LONGERON. CORROSION DAMAGE TO REAR SPAR SIDE FRAME FITTING COMMON TO INTERFACING SURFACE W/REAR SPAR WEB CORROSION DAMAGE TO REAR SPAR WEB COMMON TO INTERACING SURFACE W/REAR SPAR SIDE FRAME FITTING. REPAIR CORROSION IAW EO B767-5330-50717-A. B767-5310-50720-A AND B767-5710-50716-A. REPLACE THE FAILSAFE STRAP IAW EO B767-5350-50409-A, B767-5330-50723-A.

Part: FLOOR PANEL — DENTED (BS 1520) · airframe 42,628 hrs · 13,213 cycles

INSPECTION TYPE:C08, CARGO FLOOR PANEL DENTED BETWEEN BS 1520, LBL 55. REPAIRED IAW EO NO B767-5320-9693-H.

Part: FLOOR PANEL — DENTED (BS 1215 - 1294) · airframe 42,628 hrs · 13,213 cycles

INSPECTION TYPE:C08, FOUND CARGO FLOOR PANEL DENTED BETWEEN BS 1215 AND 1294, LBL 23-31. REPAIRED IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DELAMINATED (BS 1480) · airframe 42,628 hrs · 13,213 cycles

INSPECTION TYPE:C08, CARGO FLOOR PANEL DELAMINATED BS 1480, RBL 11. REPAIRED IAW EO NR B767-5320-9693-H.

Part: FLOOR PANEL — DENTED (BS 1197) · airframe 42,628 hrs · 13,213 cycles

INSPECTION TYPE:C08, MAIN DECK CARGO FLOOR PANEL DENTED BETWEEN BS 1197+25 AND 1197 +45, LBL 8 - RBL 8. REPAIRED IAW EO NO B767-5320-9693-H.

Part: FLOOR PANEL — DENTED (BS 1480) · airframe 42,628 hrs · 13,213 cycles

INSPECTION TYPE:C08, MAIN DECK CARGO FLOOR PANEL DENTED BS 1480, RBL 54. REPAIRED IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DENTED (BS 998-1003) · airframe 42,628 hrs · 13,213 cycles

INSPECTION TYPE:C08, FOUND CARGO FLOOR PANEL BETWEEN BS 998 AND 1003,BL 0 -LBL 5 DENTED. REPAIRED IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DENTED (BS 988 - 1004) · airframe 42,628 hrs · 13,213 cycles

INSPECTION TYPE:C08. CARGO FLOOR PANEL DENTED BS 988 - 1004, LBL 82. REPAIRED IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DENTED (BS 1410 - 1473) · airframe 42,628 hrs · 13,213 cycles

INSPECTION TYPE:C08, FOUND CARGO FLOOR PANEL DENTED BETWEEN BS 1410 AND 1473, LBL 35 - 54. REPAIRED IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DENTED (BS 1120 - 1180) · airframe 42,628 hrs · 13,213 cycles

INSPECTION TYPE:C08, CARGO FLOOR PANEL DENTED BETWEEN BS 1120 AND 1180, LBL 34 - RBL 45. REPAIRED IAW EO B767-5320-9693-H.

Part: STRINGER — CRACKED (BS 1502-1518) · airframe 42,628 hrs · 13,213 cycles

INSPECTION TYPE:C08, CRACK 1.1 INCHES, WAS FOUND ON STRINGER 20L BETWEEN BS 1502 AND 1518. REPAIR IAW SR 1-2419267958.

Part: BULKHEAD — CRACKED (BS 1809.5) · airframe 42,628 hrs · 13,213 cycles

INSPECTION TYPE:C08, CRACK (0.65") WAS FOUND ON LT HORIZONTAL INNER CHORD OF STA 1809.5 BULKHEAD AT APPROX WL 257 AND LBL 28. THE CRACK WAS EXTENDED FROM THE FASTENER HOLE THRU THE EDGE OF INNER CHORD. REPAIR IAW SRM 53-80-08, REPAIR 10, REV 56.

Part: FLOORBOARD — PUNCTURED (MAIN CARGO)

MAIN CARGO DECK FLOOR PANEL POSITION 2L HAS .5" DIA PUNCTURE. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO B767-5320-969.

Part: PANEL — CRACKED (HORIZONTAL STAB) · airframe 38,311 hrs · 11,610 cycles

INSPECTION TYPE:C, HORZ STAB RT LOWER AIRGATE FAIRING CUTOUT FWD SKIN PANELS FOUND CRACKED. HORZ STAB RT LOWER AIRGATE FAIRING CUTOUT FWD SKIN PANEL REPAIRED IAW SRM 53-80-01-2R3, REPAIR 3, FIG 201, REV49. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR.

Part: FAIRING — DELAMINATED (RT WING TE FLAP) · airframe 383,111 hrs · 11,610 cycles

INSPECTION TYPE:7C, RT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A(1) FIG 5, REV 49.

Part: FAIRING — DELAMINATED (LT WING TE FLAP) · airframe 383,111 hrs · 11,610 cycles

INSPECTION TYPE:7C, LT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A (1) FIG 5, REV 49.

Part: FLOOR PANEL — DENTED (BS 833-930) · airframe 38,311 hrs · 11,610 cycles

INSPECTION TYPE:C, MCD FLOOR PANEL FOUND 8 DENTS AND 7 PUNCTURES AT STA 833 TO 930 LBL 55 TO LBL 77. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-06.

Part: FLOOR PANEL — GOUGED (CARGO DECK) · airframe 38,311 hrs · 11,610 cycles

INSPECTION TYPE:C, MCD FLOOR PANEL FOUND DEEP GOUGE RUN THROUGH TOGETHER WITH 5 DENTS MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-06.

Part: STIFFENER — CRACKED (WING CTR TANK) · airframe 38,311 hrs · 11,610 cycles

INSPECTION TYPE:C, FX - WING CTR TANK FRONT SPAR VERTICAL STIFFENER UPPER AREA FOUND CRACK JUST AT STA 785.9, RBL 10.94. STIFFENER REPAIR IAW HX RS R57-10-37013, REV A & EO B767-5710-42201-A AT STA 785.9 RBL 10.94, ORG MAT;L BAC1518-749-2024T3511, CRK LENGTH IS 1" CUT OFF LENGTH IS 19.5", THIS CLASSIFIED AS MAJOR REPAIR WITH MAT'L BAC1518-749-2024T3511 STIFFENER REPLACE SECT, 2024T351-0250IN & 2024T3-0100IN STRAP & 7075T651BARE0250IN CLEVIS PLATE, TOTAL L 24"

Part: FLOOR PANEL — DENTED (CARGO DECK) · airframe 38,311 hrs · 11,610 cycles

INSPECTION TYPE:C, DMI D449761 - MAIN CARGO POSITION 6R OTBD FLOOR PANEL INTERIM REPAIR. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-06.

Part: STIFFENER — CRACKED (BS 246) · airframe 38,311 hrs · 11,610 cycles

INSPECTION TYPE:C, MAIN EQUIPMENT CTR STA 246, LBL 40 FLOORBEAM VERTICAL STIFFENER FOUND CRACK. STIFFENER REPAIRED IAW SRM 53-10-51-2R4 REPAIR 4, FIG 201, REV 49. ORG MATL BAC1490-2793-7075T62 CRK LENGTH 1.1" REPAIR CLASSIFIED AS MAJOR REPAIR REPEAT INSP AT 3000 FLT CYCLES OR 24 MONTHS WHICH EVER OCCUR FIRST IS REQUIRED IAW SRM 53-10-51-2R4. REPAIR 4, FIG 201, REV 49 REPAIR LENGTH IS 14.6".

Part: FLOORBOARD — DAMAGED (CARGO BAY)

INSPECTION TYPE:N/A FLOORBOARD DAMAGED POS 2R. FABRICATED NEW PANEL IAW EO B767-5320-9693-F.

Part: FLOOR PANEL — DAMAGED (CARGO BAY)

INSPECTION TYPE:N/A D-403978 MAIN CARGO DECK POS 2R FLOOR PANEL INTERIM REPAIR. REPLACED PANEL PER EO767-5320-9693-F.

Part: CYLINDER — DAMAGED (RT MLG) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:6C OUTER CYLINDER INNER WALL FOUND SEVERAL AREA CHIPPED. RT MLG OUTER CYLINDER INNER WALL NICK MARKS REPAIR CUTOUT AS PER HX RS R32-11-36300 AND IPXA EO C-3210-33050-A.

Part: SKIN PANEL — DELAMINATED (VERTICAL STAB) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C EMP - VERTICAL STAB LT LWR EXTERIOR SURFACE AREA DELAMINATION. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10 REPAIR 4 FIG 201 REV 43.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C MEC- BS 246 CABIN FLOORBEAM FWD FACE L/G ALTERNATE DRIVE MOTOR SUPPORT ANGLE CRACKED AT LBL 25. (CRACK 1 INCH LENGTH). MEC- BS 246 CABIN FLOORBEAM FWD FACE L/G ALTERNATE DRIVE MOTOR SUPPORT ANGLE REPLACED AS PER SRM 51-10-02 AND SRM 51-40-02 REV 43 JUST AT LBL 25.

Part: WEB — BENT (CARGO BAY) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C BULK CARGO STA 1480 LBL 14 FLOOR WEB FWD SIDE ATTACH STIFFENER BENT. BULK CARGO STA 1480 LBL 14 FLOOR WEB FWD SIDE ATTACH STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.

Part: FAIRING — CHAFED (AILERON) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C LT WING - I/B AILERON FWD UPPER L/E FAIRING CHAFE DAMAGED. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PARA 4G FIG 18.

Part: STIFFENER — BENT (CARGO BAY) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C BULK CARGO STA 1461 LBL 9 FLOOR WEB FWD SIDE ATTACH STIFFENER BENT. BULK CARGO STA 1461 LBL 9 FLOOR WEB FWD SIDE ATTACH STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.

Part: STIFFENER — BENT (CARGO BAY) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C BULK CARGO STA 1439 RBL 9 FLOOR WEB FWD SIDE ATTACH STIFFENER BENT. BULK CARGO STA 1439 RBL 9 FLOOR WEB FWD SIDE ATTACH STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.

Part: STIFFENER — BENT (CARGO BAY) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C BULK CARGO STA 1480 LBL 9 FLOOR WEB FWD SIDE ATT STIFFENER BENT. BULK CARGO STA 1480 LBL 9 FLOOR WEB FWD SIDE ATT STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.

Part: STIFFENER — DAMAGED (STA 1518)

BULK CARGO STA 1518 LBL 14 INCHES FLR WEB FWD SIDE ATT STIFFENER BENT. BULK CARGO STA 1518 LBL 14 INCHES FLOOR WEB FWD SIDE ATT STIFFENER REPLACED PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.

Part: SKIN — MISREPAIRED (CARGO DOOR) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C FUSELAGE SURVEY SEQ 323-F1-04 BETWEEN BS 1427 TO BS 1435.25 AND STA 24L - 26L. AT BULK CARGO DOOR AREA PATCH FOUND. (REPAIR CURRENTLY WITH SURVEY SEQ 323-F1-05). SURVEY SEQ 323-F1-05 AT BULK CARGO DOOR SKIN REPAIRED CURRENTLY WITH SURVEY SEQ 323-F1-04 AT BETWEEN BS 1427 TO BS 1444 AND STR 24L - 26L AREA AS PER HX RS R52-36-36298, THIS REPAIR CLASSIFIED AS MAJOR REPAIR WITH MATERIAL 2024T3 . 080" & REPAIR SIZE 14.2" X 16.5" , REFER HX NRC 50798 FOR WORKING DETAIL.

Part: STIFFENER — BENT (CARGO BAY) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C BULK CARGO STA 1439 LBL 22 FLOOR WEB FWD SIDE ATTACH STIFFENER BENT. BULK CARGO STA 1439 LBL 22 FLOOR WEB FWD SIDE ATTACH STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.

Part: SKIN — ACTIVATED (CARGO DOOR) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C FUSELAGE SURVEY SEQ 323-F1-05 BETWEEN BS 1436.55 TO BS 1443.55 STR 24L TO 26L AT BULK CARGO DOOR SKIN AREA PATCH FOUND, NOT CORRELATED TO SRM. SURVEY SEQ 323-F1-05 AT BULK CARGO DOOR SKIN REPAIRED AT BETWEEN BS 1427 TO BS 1444 AND STR 24L - 26L AREA AS PER HX RS R52-36-36298. THIS REPAIR CLASSIFIED AS MAJOR REPAIR WITH MATERIAL 2024T3.080" & REPAIR SIZE 14.2" X 16.5".

Part: STIFFENER — BENT (CARGO BAY) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C BULK CARGO STA 1518 RBL 9 FLOOR WEB FWD SIDE ATT STIFFENER BENT. BULK CARGO STA 1518 RBL 9 FLOOR WEB FWD SIDE ATT STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.

Part: STIFFENER — BENT (CARGO BAY) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C BULK CARGO STA 1439 LBL 9 FLOOR WEB FWD SIDE ATTACH STIFFENER BENT. BULK CARGO STA 1439 LBL 9 FLOOR WEB FWD SIDE ATTACH STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.

Part: STIFFENER — BENT (CARGO BAY) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C BULK CARGO STA 1439 LBL 16 FLOOR WEB FWD SIDE ATT STIFFENER BENT. BULK CARGO STA 1439 LBL 16 FLOOR WEB FWD SIDE ATT STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.

Part: SPOILER — DELAMINATED (LT WING) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:6C LT WING - NR 5 SPOILER PANEL FWD O/B CORNER DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-04 PARA 5G FIG 9 REV 43.

Part: STIFFENER — BENT (CARGO BAY) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C BULK CARGO STA 1502 RBL 14 FLOOR WEB FWD SIDE ATTACH STIFFENER BENT. BULK CARGO STA 1502 RBL 14 FLOOR WEB FWD SIDE ATTACH STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.

Part: STIFFENER — BENT (CARGO BAY) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C BULK CARGO STA 1502 LBL 20 FLOOR WEB FWD SIDE ATTACH STIFFENER BENT. BULK CARGO STA 1502 LBL 20 FLOOR WEB FWD SIDE ATTACH STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.

Part: STIFFENER — BENT (CARGO BAY) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C BULK CARGO STA 1502 RBL 9 FLOOR WEB FWD SIDE ATTACH STIFFENER BENT. BULK CARGO STA 1502 RBL 9 FLOOR WEB FWD SIDE ATTACH STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C CTR TANK FRONT SPAR STIFFENER UPPER END AT LBL 10 FOUND CRACK (CRACK 2.125 INCH LENGTH). FWD CARGO COMPT WING CTR TANK FRONT STIFFENER AT LBL 10 WL 178.96, APPROX REPAIRED AS PER HX RS R57-11-36294 REV A. THIS REPAIR CLASSIFIED AS A MAJOR REPAIR WITH REPAIR STRAP 202473 .250" & .100" WITH REPAIR LENGTH 19.25" IPXA EO B767-5710-33014-A.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 32,923 hrs · 9,911 cycles

1 HOLE 5TH FLOOR PANEL FROM LT SIDE POS 6R. FLOOR PANEL REPLACED AND INSTALLED AS PER EO B767-5320-9693-E.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C RT WING - O/B FLAP I/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PARA 4A FIG 10 REV 43.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C DMI D396282 - 1 HOLE FOUND AT 5TH FLOOR PANEL FROM LT SIDE POS 8R ZONE 2 (PUNCTURE .5 INCH DIA). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:6C MAIN DECK FLOOR SUPPORT ATT ANGLE FOUND CRACKED JUST AT STA 1575 LBL 75-76. MAIN DECK FLOOR SUPPORT ATT ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43 JUST AT STA 1575 LBL 75-76.

Part: HINGE FITTING — CRACKED (TE FLAP) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C LT WING I/B MAIN FLAP I/B AFT FLAP HINGE FTG FLANGE FOUND CRACKED (CRACK I/B FLANGE 1.125 INCH AND O/B FLANGE 1 INCH). LT WING I/B MAIN FLAP I/B AFT FLAP HINGE FTG REPAIRED AS PER SRM 57-53-02-2R1 FIG 201 REV 43. THIS IS CLASSIFIED AS A MAJOR REPAIR WITH MATERIAL AND 10134-2007-7075T6511, REPAIR SIZE 2 X 2 INCHES.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C DMI D396290 - 1 HOLE FOUND AT 8TH FLOOR PANEL FROM LT SIDE POS 12R ZONE 2 (PUNCTURE 1 INCH DIA.) FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 32,923 hrs · 9,911 cycles

1 HOLE 1ST PANEL FROM LT SIDE POS 2L ZONE 1. FLOOR PANEL REPLACED AND INSTALLED AS PER EO B747-5320-9693-E.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C DMI D396291 - 1 HOLE FOUND AT 1ST FLOOR PANEL FROM LT SIDE POS 13 ZONE 2 (PUNCTURE .75 INCH DIA). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.

Part: ANTENNA — MISLOCATED (GPS) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:N/A FX - THE UPPER GPS ANTENNA NOT INSTALLED AT THE CORRECT LOCATION. FUSELAGE THE UPPER GPS ANTENNA EXISTING CUTOUT REPAIRED AT BS 654+33 BL 0 AS PER RS R53-00-36295 REV A. REPEAT INSPECTION IS REQUIRED AS PER HX RS R53-00-36295 REV A SHEET 2. THIS REPAIR CLASSIFIED AS A MAJOR REPAIR WITH .125 INCH DOUBLER REPAIR SIZE 6.5" X 11.5", REF IPXA EO B767-5330-33047-A.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C DIM D396283 - 1 HOLE FOUND AT 8TH FLOOR PANEL FROM LT SIDE POS 8R ZONE 2 (PUNCTURE 1 INCH DIA). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C D396293 - 1 HOLE FOUND AT 3RD FLOOR PANEL FROM LT SIDE POS 2L ZONE 2 (PUNCTURE .5 INCH DIA). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C DMI D396295 - 3 HOLES FOUND AT 3RD FLOOR PANEL FROM LT SIDE POS 4L ZONE 2 (ALL PUNCTURE .5 INCH DIA). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 32,923 hrs · 9,911 cycles

1 HOLE 5TH FLOOR PANEL FROM LT SIDE POS 4L ZONE 2. FLOOR PANEL REPLACED AND INSTALLED AS PER EO B767-5320-9693-E.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C MAIN DECK FLOOR SUPPORT ATT ANGLE FOUND CRACKED JUST AT STA 1575 RBL 75-76 (CRACK 1.5 INCH LENGTH). MAIN DECK FLOOR SUPPORT ATT ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C DMI D396285 - 1 HOLE FOUND AT 1ST FLOOR PANEL FROM LT SIDE POS 12L ZONE 1 (PUNCTURE 1 INCH DIA). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:6C SURVEY SEQUENCE 323-F1-03 BETWEEN BS 1197+110 TO BS 1197+130 AND STR 24R-26R AREA SKIN REPAIR IS NOT CORRELATED TO SRM. SKIN REPAIRED AS PER HX RS 53-60-36299 REV A. REPEAT INSP IS REQUIRED AS PER HX RS 53-60-36299 REV A. THIS REPAIR CLASSIFIED AS A MAJOR REPAIR WITH DOUBLER 2024T3.125" AND STRUCTURAL FILLER 2024T3.100", REPAIR SIZE 22.75" X 26.5" AND REFER EO B767-5330- 33048-A.

Part: SKIN — DENTED (FUSELAGE) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:6C FX - SURVEY SEQUENCE 323-F1-02 A PROTRUDING HEAD FASTENER AREA DENT AND 2 LOC. DENT CLOSE TO THE EXISTING FLUSH REPAIR FOUND. SURVEY SEQUENCE 323-F1-02 LOCATION A FASTENER REMOVED AND REPLACED AS PER HX RS R53-31-36297 REV A. EXTERNAL AND INTERNAL DETAIL VISUAL INSPECTION AND HFEC INSPECTION CARRIED OUT AS PER HX RS R53-31-36297 REV A. NIL DEFECT FOUND CRACK FREE. THIS REPAIR CLASSIFIED AS A CATEGORY A REPAIR. REF IPXA EO B767-5330-33045-A.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C D396288 - 1 HOLE FOUND AT 5TH FLOOR PANEL FROM LT SIDE POS 12R ZONE 1 (PUNCTURE .5 INCH DIA). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 32,923 hrs · 9,911 cycles

1 HOLE 5TH FLOOR PANEL FROM LT SIDE POS 5R ZONE 2. FLOOR PANEL REPLACED AND INSTALLED AS PER EO B767-5320-9693-E.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C DMI D396287 - 1 HOLE FOUND AT 5TH FLOOR PANEL FROM LT SIDE POS 12R ZONE 1 (PUNCTURE .75 INCH DIA). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:N/A D396289 - 1 HOLE FOUND AT 7TH FLOOR PANEL FROM LT POS 12R ZONE 2 (PUNCTURE .75 INCH DIA). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C DMI D396292 - 1 HOLE AT 5TH FLOOR PANEL FROM LT SIDE POS 2R ZONE 2 (PUNCTURE 1 INCH DIA). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C DMI D396284 - 1 HOLE FOUND AT 7TH FLOOR PANEL LT SIDE POS 9R ZONE 1 (PUNCTURE .75 INCH DIA). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C DMI D396280 - 1 HOLE FOUND AT 7TH FLOOR PANEL FROM LT SIDE POS 6R ZONE 2 (PUNCTURE .5 INCH DIA). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.

Part: FLOOR PANEL — DENTED (FUSELAGE) · airframe 32,923 hrs · 9,911 cycles

POS 8R FLOOR PANEL HAS 6 DENTS. FLOOR PANEL REPLACED AND INSTALLED AS PER EO B767-5320-9693-E.

Part: MOUNT — CRACKED (CARGO BAY) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:C AFT CARGO DOOR MANUAL DRIVE SYS CHK FOUND FWD PDU EXCESSIVE MOVEMENT CAUSED THE PDU MOUNTING UPR STRUCTURE CRACKED. (CRACK 1.25 INCH LENGTH). AFT CARGO DOOR PDU MOUNTING UPPER WEB AND DOUBLER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43. (WEB P/N: 143T6312-502).

Part: SEAT TRACK — DAMAGED (FUSELAGE)

INSPECTION TYPE:N/A SEAT TRACK DAMAGED AT STA 1518 RBL 33. REPAIRED PER EO B767-5310-32616-B.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 32,923 hrs · 9,911 cycles

INSPECTION TYPE:6C DMI NR D395403, MAIN CARGO AFTER CENTER OF POS 4 HAS 2 EACH 2 INCH CRACK IN FL FLOOR PANEL. FLOOR PANEL REPLACED AND INSTALLED AS PER EO B767-5320-9693-E.

Part: FLOORBOARD — DAMAGED (MAIN CARGO BAY)

INSPECTION TYPE:N/A MAIN CARGO DOOR FLOORBOARD PANEL DAMAGED AT POS 13 REF D 392745. REMOVED FLOOR PANEL FOR REPAIR/REPLACEMENT. REMOVED AND REPLACED POS 13 FLOOR PANEL PER EO B767-5330-9693 APPX B. THIS CLEARS D 392745.

Part: FLOOR PANEL — DAMAGED (CABIN)

REF LOG PAGE 842810ITEM 3 DI 392745 MC FLOOR PANEL AT POS 13 DAMAGED. FABRICATED NEW FLOOR PANEL PER EO B767-5320-9693E

Part: FLOOR PANEL — CRACKED (MAIN CARGO BAY)

INSPECTION TYPE:N/A CENTERLINE FLOOR PANEL CRACKED AT POSITION 8. REMOVED PANEL AND ROUTED TO SHEET METAL FOR REPAIR. INSTALLED CENTERLINE FLOORBOARD PANEL AT POS NR 8 ON MCD PER EO B767-5320-9693E.

Part: FLAP — DENTED (RT WING)

INSPECTION TYPE:N/A RIGHT I/B MAIN FLAP DENTED OUT OF SRM LIMITS. REPAIRED PER EO B767-5750-30895-A.

Part: BRAKE — FIRE (NR 1)

INSPECTION TYPE:N/A, NR 1 BRAKE FIRE ON ARRIVAL, FUSE PLUGS MELTED. CFR WAS CALLED DUE TO FIRE.

Part: BRACKET — LOOSE (L1 DOOR)

INSPECTION TYPE:N/A L1 DOOR EMERGENCY EXIT LIGHT HOLDING BRACKET NEEDS RE-SECURED. RE-SECURED LIGHT ASSY USING STANDARD MX PRACTICES, CHAP 20.

Part: IDG — LOW (NR 1 GENERATOR)

INSPECTION TYPE:ETOP ATB - EICAS MSG R GEN DRIVE DISPL, GEN DRIVE LIGHT ILLUMINATED, GEN DRIVE DISCONNECTED. SERVICED OIL TO PROPER LEVEL, RECONNECTED NR 2, IDG RAN ENGINE. OPS CHECKS GOOD.

Part: SWITCH — DEFECTIVE (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY LIGHTS SWITCH ON OVERHEAD PANEL DOES NOT WORK PROPERLY. OPS CHECK EMERGENCY LIGHT SWITCH IAW MM 33-51-00, OPS CHECK GOOD.

Part: SEAT BELT — INOPERATIVE (SEAT)

LEFT SUPERNUMARY SEAT INTERTIAL RESTRAINT INOP. REMOVED AND REPLACED RESTRAINT IAW MM 25-11-00-6. OPS CK NORMAL.

Part: FRAME — CRACKED (AILERON)

INSPECTION TYPE:N/A LEFT WING I/B AILERON I/B HINGE SUPPORT FRAME CRACKED BETWEEN UPPER TWO FASTENER HOLES AND OUT TO THE LOWER FASTENER EDGE. REPAIRED LEFT WING INBOARD AILERON INBOARD HINGE SUPPORT FRAME PER EO B767-5740-27949-A.

Part: BLEED AIR SYS — INOPERATIVE (APU)

INSPECTION TYPE:ETOP NO APU BLEED AIR. BTB FOR EXTERNAL AIR CART. C/O OPERATIONAL TEST OF APU BLEED AIR IAW AMM 49-52-00-00. FOUND SATISFACTORY.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 27,281 hrs · 8,152 cycles

INSPECTION TYPE:C SEAT TRACK FLANGES GOUGED AT BS 632-654+20 RBL 54 WL 200. REMOVED AND REPLACED SEAT TRACK SECTION BS 621-654+55 RBL 54 IAW ER 07 07-1909 AND SRM 53-00-52-2R 9 FIG 201.

Part: TIRE — OUT OF ROUND (NLG)

INSPECTION TYPE:ETOP ON TAKEOFF ROLL OUT OF CGN AIRCRAFT A SLIGHT ODOR OF RUBBER AND VIBRATION IN THE NOSE WHEEL THAT STARTED SLIGHT AND BECAME MODERATE TO S EVERE. CREW REQUEST EMERGENCY SUPPORT UPON LANDING IN EWR FOR SUSPECTED BLOWN NOSE TIRE. AIRCRAFT LANDED WITHOUT INCIDENT IN EWR. MX FOUND LT AND RT NOSE TIRE PROPERLY INSTALLED AND SERVICED. HOWEVER BOTH TIRES WHERE SEVERLY OUT OF ROUND. REMOVED AND REPLACED BOTH TIRE ASSY. AIRCRAFT DEPARTED AND LANDED IN SDF WITH NO FURTHER REPORT.

Part: RIB — CRACKED (RT WING) · airframe 15,595 hrs · 4,927 cycles

INSPECTION TYPE:C3 NR 9 SLAT OB DRIVE ARM OB RIB AT OFSS 651 IS CRACKED ON FORWARD FLANGE. REPAIRED NR 9 SLAT OB DRIVE ARM OB RIB AT OFSS 651 IAW GOODRICH ER NR 03-3162

Part: SKIN — BUCKLED (FUSELAGE)

INSPECTION TYPE:PFLT SKIN BUCKLED AT NOSE JACK POINT STA 287. REMOVED FASTENERS THROUGH SKIN IN DENTED AREA IAW SRM 51-40-02. INSTALLED 90 PERCENT OF FASTNERS THAT WERE REMOVED AT BX 287 NOSE JACK POINT IN DENTED AREA IAW SRM 51-40-02. REMAINING FASTENERS FOUND TO BE COMMON TO FRAME REPAIR AT BS 287.

Part: AILERON — BINDING (WINGS)

WHEN CHECKING FLIGHT CONTROLS BEFORE ENGINE START, THE RIGHT OUTBOARD AILERON STUCK IN THE FULL UP POSITION WITH CONTROL YOKE IN NEUTRAL. ORDERED RIGHT AILERON (OUTBOARD) INBD PCA. EMP 25110 ACCOMPLISHED FIM B-767 27-11-00 NO PROBLEMS FOUND PCU OPERATE NORMALLY. LUBRICATED AILERON HINGES FOR PRECAUTIONARY SYSTEM 1 CHECKS NORMAL A/C OK FOR SERVICE (NO EICAS MESSAGES FOUND)

Part: ACTUATOR — LEAKING (SPOILER)

CENTER HYDRAULIC QTY DECREASED TO 0.07. SYSTEM DEPRESSURIZED AND LEAK CONTINUED. ***MRR FILED AS OPEN*** AWAITING LOG PAGE CORRECTIVE ACTION ENTRIES FOUND SPOILER ACTUTATOR LEAKING AT PLUG BELOW SERVO VALVE ON ACTUATOR JUST OUTBOARD OF INBOARD AILERON. REPLACED O-RINGS & SERVICED CENTER HYD SYSTEM. OP''S CHK''S OK. - NO LEAKS.