N614UP

Part: FIRE LOOP — FALSE ACTIVATION (ZONE 100) · airframe 24,969 hrs · 3,653 cycles

WHEEL WELL FIRE INDICATION AT GEAR DOWN. REMOVED AND REPLACED THE LEFT BODY GEAR WHEEL WELL FIRE LOOPS M691 AND M694 IN REF TO THE AMM 26-17-02-000-801 ALL OPS CHECKS ARE GOOD AT THIS TIME . ALSO REMOVED AND REPLACED THE DUCT LEAK WHEEL WELL CTL CARD ASSY IN REF TO AMM 26-10-01 OPS CHECKS ARE GOOD.

Part: FIRE WARNING — ILLUMINATED (MLG WW) · airframe 24,796 hrs · 3,628 cycles

WHEEL WELL FIRE INDICATION AT GEAR DOWN. DEFERRED WHEEL WELL FIRE DETECTION SYSTEM IAW MEL 26-17-1A.

Part: FIRE WARNING — FALSE ACTIVATION (ZONE 100) · airframe 24,688 hrs · 3,614 cycles

FIRE WHEEL WELL WARNING DISPLAYED AND SOUNDED BFOR ABOUT ONE SECOND WHEN LANDING GEAR SERLECTED DOWN AT 3000 FEET. R & R MASTER MONITOR A CARD IAW AMM 31-51-02, OPS CHECK GOOD. NO DEFECTS NOTED.

Part: FIRE WARNING — ILLUMINATED (ZONE 100) · airframe 24,434 hrs · 3,579 cycles

FIRE WHEEL WELL WARNING DISPLAYED AND SOUNDED BFOR ABOUT ONE SECOND WHEN LANDING GEAR SERLECTED DOWN AT 3000 FEET. DEFERRED PER MEL 26-17-1A

Part: SKIN — DAMAGED (ZONE 100) · airframe 24,059 hrs · 3,525 cycles

**SDR FILED OPEN** POSSIBLE CRACK IN SKIN DAMAGE ADJACENT TO TAIL BALL. DEFERRED IAW E0-93768-REQ1

Part: FLAP SYSTEM — WARNING MESSAGE · airframe 23,186 hrs · 3,401 cycles

**EMERGENCY DECLARED**ON DESCENT FOR APPROACH FLAPS DRIVE EICAS ALERT AS PER CREW BRIEFING €˜EMERGENCY LANDING€™DECLARED BY CREW.FCU L,C,R C/OUT IAW AMM 27-51-00-745-028 REV 46.TEST PASSED.DMP PROCEDURE AS PER MEL 27-81-1 C/OUT VERIFIED ALL SATIS.FLAP OPS C/OUT FOUND SATIS IAW AMM 27-51-00/201 REV 46.

Part: NONE — NONE (NONE) · airframe 22,828 hrs · 3,354 cycles

RH OUTBOARD ELEVATOR FRONT SPAR AND RIB REINFORCEMENT

Part: NONE — NONE (NONE) · airframe 22,828 hrs · 3,354 cycles

LH OUTBOARD ELEVATOR FRONT SPAR AND RIB REINFORCEMENT. ACCOMPLISHED EO-85445-JIC. ACCOMPLISHED SDER

Part: NONE — NONE (NONE) · airframe 22,860 hrs · 3,359 cycles

RH OUTBOARD ELEVATOR FRONT SPAR AND RIB REINFORCEMENT. ACCOMPLISHED EO-85445-JIC2. ACCOMPLISHED SDR

Part: SPRING — DEFORMED (ZONE 800) · airframe 22,828 hrs · 3,354 cycles

FOUND MAIN ENTRY DOOR STOP PIN RETAINER SPRING DEFORM 1 EA. (REPLACE) OK TO WORK. OPEN

Part: SPRING — DEFORMED (STOP FITTING) · airframe 22,828 hrs · 3,354 cycles

FOUND MAIN ENTRY DOOR STOP PIN RETAINER SPRING DEFORM 1 EA.INSTALLED AND ADJUSTED F/O #2 SLIDING WINDOW PER AMM 56-11-02/401 AND 56-11-02/501. LEAK CHK PERFORMED PER 05-51-24/201.

Part: ESCAPE REEL — OPEN (ZONE 200) · airframe 22,828 hrs · 3,354 cycles

**SDR FILED OPEN** FAULT - FOUND COCKPIT DESCENT DEVICE TAMPER PROOF SEAL BROKEN, TOTAL: 4EA, LOCATION AT L7~L10 (REPLACE)

Part: SEAL — BROKEN (ESCAPE REEL) · airframe 22,853 hrs · 3,358 cycles

**SUPPLEMENTAL SDR** FAULT - FOUND COCKPIT DESCENT DEVICE TAMPER PROOF SEAL BROKEN, TOTAL: 4EA, LOCATION AT L7~L10 (REPLACE). I.A.W. AMM 25-61-01-000-801 REV.46 AND AMM 25-61-01-400-801 REV.46, TO REPLACE COCKPIT DESCENT DEVICE TOTAL:4EA, AT POSITION 7~10. REVIEW COMPLETED

Part: SKIN — DENTED (ZONE 500 K FLAP) · airframe 23,427 hrs · 3,434 cycles

MAJOR REPAIR, DURING WALKAROUND FOUND DENT ON LH WING #13 KRUEGER FLAP PANEL NEAR LEFT LOWER CORNER OK TO INSTALL LEADING EDGE FLAP INSTALLED #13 KRUEGER FLAP REF AMM 27-81-01 UP TO AND INCLUDING STEP E(3)(F) OPEN

Part: FAIRING — DAMAGED (ZONE100) · airframe 21,415 hrs · 3,140 cycles

LH BODY FAIRING PANELS DAMAGED FOLLOWING PANELS FOUND DAMAGED. 193GL WITH A DELAMINATION AT 3" TO 13" FROM FWD EDGE AND 26" TO 28" FROM INBD CORNER<BR><BR>193FL WITH A DELAMINATION AT 22,5" TO 29" FROM OUTBD EDGE AND 8" TO 19" FROM AFT EDGE AND A SECOND DELAMINATION AT 35,5" TO 37" FROM OUTBD EDGE AND 17,5" TO 20,5" FROM AFT EDGE.

Part: FAIRING — DAMAGED (LEFT BODY) · airframe 21,516 hrs · 3,154 cycles

LH BODY FAIRING PANELS DAMAGED OPEN SEPARATE ITEM FOR PANEL 193BL UNDER TASK [T3F18E0054ZFR], PANEL 193CL UNDER TASK [T3F18E0054ZFZ], PANEL 193DL UNDER TASK [T3F18E0054ZG1], PANEL 193FL UNDER TASK [T3F18E0054ZG2] AND PANEL 193GL UNDER TASK [T3F18E0054ZG3] NO FURTHER MEASUREMENTS REQUIRED AND INSPECTION REQUIRED IAW AMM 57-05-03-201 REV.45.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 19,432 hrs · 2,869 cycles

*MAJOR REPAIR* FUSELAGE SKIN DAMAGE / RIGHT SIDE, AFT OF FWD LOWER CARGO DOOR C/W

Part: SKIN — DAMAGED (RT FUSELAGE) · airframe 19,432 hrs · 2,869 cycles

FUSELAGE SKIN DAMAGE / RIGHT SIDE, AFT OF FWD LOWER CARGO DOOR C/W

Part: SKIN — UNKNOWN (UNKNOWN) · airframe 16,871 hrs · 2,488 cycles

*** SDR FILED OPEN *** PUNCTURE TO FUSELAGE SKIN BY CARGO VEHICLE FWD OF AFT LOWER CARGO DOOR OPENING, ABOVE CARGO DOOR CONTROL PANEL.***SM EVAL REQ*** DEFERRED PER EO 87620- REQ. 1

Part: SKIN — GROUND DAMAGE (ZONE 100) · airframe 22,848 hrs · 3,357 cycles

PUNCTURE TO FUSELAGE SKIN BY CARGO VEHICLE FWD OF AFT LOWER CARGO DOOR OPENING, ABOVE CARGO DOOR CONTROL PANEL. ACCOMPLISHED REPAIR I.A.W UPS EO-87620-REQ3 REV.1 REVIEW COMPLETED

Part: FLAP — DAMAGED (LE) · airframe 16,482 hrs · 2,436 cycles

#15 LEADING EDGE FLAP DENT***SM40/LMX20*** ALL STEPS COMPLIED WITH IAW EO-87340-REQ1. REFERENCE T3F18E001ZAFL.

Part: UNKNOWN — CRACKED · airframe 15,887 hrs · 2,353 cycles

DURING ACCOMPLISHMENT OF EO #86006-REQ1 STEPS 1,2,AND 3 FOUND TOP CHORD AFT END OF R/H STAB TIP CRACKED INSTALLED NEW NUT PLATES AND INSTALLED NEW T CHORD PER SRM 51-40-02

Part: SPRING — BROKEN (L1 DOOR) · airframe 15,238 hrs · 2,252 cycles

FAULT - FOUND L1 ENTRY DOOR AFT SIDE SPRING - PIN BROKEN. TOTAL: 1EA (REPLACE) ALL PAPERWORK C/W

Part: STATUS MESSAGE — FALSE ACTIVATION (FIRE LOOP) · airframe 10,349 hrs · 1,479 cycles

INSPECTION TYPE:N/AENG 2 FIRE LP 1 STATUS MESSAGE.T/S PERFORMED IAW FIM 26-11-00-810-819 REV. 2021-09-15. 03.01. FOUND NO EXISTING FAULT. OPC SATIS IAW AMM 26-11-03-501 REV. 36.02.

Part: PROXIMITY SENSOR — FAULTED (MLG TRUCK TILT) · airframe 10,251 hrs · 1,462 cycles

INSPECTION TYPE:N/A**AIR TURN BACK** EMERGENCY DECLARED** REQUIRED DUE TO GEAR TILT MESSAGE. 22:57 Z ON 9/14/2021.T/S PERFORMED IAW FIM TASK 32-31-00-810-822, REV 08-11-21. FOUND MAINT MSG 32724, R/H BODY GEAR TRUCK TILT LEVER LOCK PROX SENSOR S2654. REPLACED IAW AMM 32-553-11-201 REV. 36-02 BODY GEAR TRUCK TILT SENSOR TEST PERF IAW AMM 32-61-12-722-05J REV 36.02. IPC 32-61-02-21 ITEM 055

Part: PROXIMITY SENSOR — FAULTED (MLG TRUCK TILT) · airframe 10,251 hrs · 1,462 cycles

INSPECTION TYPE:N/A**ATB ** - **EMERGENCY DECLARED. FLIGHT LANDED WITHOUT INCIDENT.**GEAR TILT MESSAGE DISPLAYED AFTER TAKEOFF.T/S PERFOMRED IAW IFIM TASK 32-31-00-810-822 REV. 08-11-21. FOUND MAINT MSG 32724, RH BODY GEAR TRUCK TILT LEVER LOCK PROX SENSOR S2654. REPLACED IAW AMM 32-53-11-201 REV. 36.02. BODY GEAR TRUCK TILT SENSOR TEST PERFORMED IAW AMM 32-61-12-722-05J REV. 36.02,

Part: WARNING MESSAGE — FALSE ACTIVATION (LANDING GEAR) · airframe 9,345 hrs · 1,331 cycles

INSPECTION TYPE:NAAFTER GEAR RETRACTION, "GEAR DISAGREE" EICAS MESSAGE WITH INDICATION THAT RIGHT BODY GEAR WAS NOT UP. APPROX 3MIN. LATER, ALL INDICATIONS NORMAL (STATUS MSGS "GEAR MONITOR AND GEAR DISAGREE" REMAIN)PERF. FIM 32-61-00-810-878, 32-30-00-810-803, NO EXISTING FAULTS FOUND, NO FAULT PREVIOUS HISTORY, INTERMITANT FAULT. OK FOR CONT. SERVICE.

Part: DRIVE ASSY — MALFUNCTIONED (FLAP SYSTEM) · airframe 7,879 hrs · 1,135 cycles

INSPECTION TYPE:N/A** ATB ** NO EMERGENCY DECLARED ** FLIGHT ARRIVED WITHOUT INCIDENT ** CREW RECVD FLAP DRIVE EICAS MESSAGE. FRM CODE 27500400 RAN CHECKLIST. APPROX 190. LBS OF FUEL WAS DUMPED TO ARRIVE BELOW LANDING WEIGHT.1CHECK CMC MSG 27770 T/S CHECK FOUND R/H INBD T/E FLAP POS TRANSMITTER INOP AS PER FIM 27-51-00-810-886 .2.REPLACED R/H INBD T/E FLAP POS TRANSMITTER AND ADJUSTED R/H INBD T/E FLAP POS TRANSMITTER AND OPERATION TEST FLAP ALL COND NML. 3.PERFORMED CMC GND TEST FOR FCU L/C/R ALL PASSED AND NO FAULT

Part: PANEL — CORRODED (NR 4 NACELLE) · airframe 7,879 hrs · 1,135 cycles

INSPECTION TYPE:C1DISCOLORATION AND CORROSION ON THE INBD LWR PANEL (P/N: 323U8740-1) OF PYLON #4.REPAIR I.A.W. BOEING SRID: 3-4953205556 AND UPS EO B747-5430-79275-A.

Part: PANEL — CORRODED (NR 3 NACELLE) · airframe 7,879 hrs · 1,135 cycles

INSPECTION TYPE:C1DISCOLORATION AND CORROSION ON THE INBD LWR PANEL (P/N: 313U8740-1) OF PYLON #3.REPAIR I.A.W. BOEING SRID: 3-4953124628 AND UPS EO B747-5430-79272-A.

Part: PANEL — CORRODED (NR 2 NACELLE) · airframe 7,879 hrs · 1,135 cycles

INSPECTION TYPE:C1DISCOLORATION AND CORROSION ON THE INBD LWR PANEL (P/N: 313U8740-2) OF PYLON #2.REPAIR I.A.W. BOEING SRID: 3-4953124306 AND UPS EO B747-5430-79269-A.

Part: PANEL — CORRODED (NR 1 NACELLE) · airframe 7,879 hrs · 1,135 cycles

INSPECTION TYPE:C1DISCOLORATION AND CORROSION ON THE INBD LWR PANEL (P/N: 323U8740-2) OF PYLON #1.REPAIR I.A.W. BOEING SRID: 3-4955139309 AND UPS EO B747-5430-79277-A.

Part: WARNING MESSAGE — FALSE ACTIVATION (LANDING GEAR) · airframe 6,519 hrs · 935 cycles

INSPECTION TYPE: NA ON DEPARTURE GEAR DISAGREE EICAS DISPLAYED. PERFORMED NON NORMAL CHECKLIST MESSAGE CLEARED. GEAR DOOR, GEAR MONITOR, GEAR DISAGREE STATUS MESSAGE REMAIN. ACCOMPLISHED FIM 32-61-00/ 810-878 AND FIM 32-61-00-810-888. CMC GROUND TEST PASSED. FAULT MESSAGE CLEARED. A/C GOOD FOR OPERATIONS.

Part: STATUS MESSAGE — ACTIVATED (PSEU) · airframe 2,695 hrs · 385 cycles

INSPECTION TYPE:N/AIN FLIGHT GOT "GEAR MONITOR" STATUS MESSAGE.PSEU GND TEST I.A.W. AMM 32-61-00 REV. 30.10 "PASS", NEVERTHELESS CLEANED R/H WING GEAR UPLOCK SENSORS. A/C O.K. FOR FLIGHT.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 2,101 hrs · 302 cycles

INSPECTION TYPE:N/A ENG 2 FIRE LP A STATUS MSG OCCURED DURING CRUISE (INTERMITTENTLY). NO ACTIVE FAULT ON GROUND. PERFORMED ENGINE FIRE AND OVERHEAT OPERATIONAL TEST IAW AMM 26-11-00/501 TEST PASSED. NO FURTHER FAULTS.

Part: CONTROL PANEL — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 1,025 hrs · 153 cycles

EMERGENCY LIGHTS STAY ON WITH SWITCH OFF. R & R THE PANEL ASSY IAW AMM 26-10-02-401 OPS CHECKED GOOD.