N884UA

Part: TIRE — DAMAGED (ZONE 700) · airframe 52,162 hrs · 26,475 cycles

AFTER AIRCRAFT DEPARTURE FROM SAT. TOMC MADE LOGPAGE 7254182 "DFW REPORTS FINDING A WHEEL TIEBOLT ON RAMP AT SAT AFTER FLIGHT 1282 LEFT". CONFIRM TIEBOLT MISSING ON #4 MAIN WHEEL ASSY. REF L/P 725 4364 FOR REPAIR. MLG TIRE FOUND BEYOND AMM LIMITS. TIEBOLT MISSING FROM NR 4 MLG WHEEL ASSY. REMOVED AND REPLACED NR 4 MLG TIRE ASSY REF AMM 32-41-11.

Part: LAMP — BURNED OUT (ZONE 200) · airframe 52,104 hrs · 26,436 cycles

FOUND CIDS FAULT, EPSU EXT LOAD EMER R. DURING EMERGENCY LIGHT TEST. RELAMPED RT OVERWING LIGHT LAMP IAW AMM 33-51-15. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED.

Part: SLIDE — NO DISCREPANCY (ZONE 800) · airframe 51,680 hrs · 26,201 cycles

OVERWING EXIT HATCHES , BOTH RESEVOIRS PINNED , LEFT & RIGHT SIDES . REMOVED PINS FROM BOTH INFLATION RESERVOIRS (LH AND RH SIDE) FOR OVERWING EMERGENCY HATCHES REF AMM TASK 25-62-00-081-001-A.

Part: DRAIN LINE — CLOGGED (APU FUEL) · airframe 51,643 hrs · 26,179 cycles

FUEL ODOR IN CABIN WITH APU DEBRIEFED CREW, FUEL ODOR DURING APU BLEED ON. SMELLED ODOR IN FLIGHT DECK FOR A FEW MINS. PARAMETER WERE NORMAL. TALKED TO FA, FA DID NOT SMELL ANY ODOR. .INSPECTED APU COMPARTMENT. FOUND FUEL BACKED UP IN AFT DRAIN LINE. SUSPECTED CLOGGED AT AFT DRAIN MAST, CLEARED DRAIN MASK AND LEAKED CHECK. NO LEAKS NOTED. APU OPS TEST NORMAL, NO SMELL. REF TSM 05-50-00-810-831-A AND AMM 49-17-00-200-805-A.

Part: UNKNOWN — ODOR (CABIN) · airframe 51,105 hrs · 25,876 cycles

FA REPORTED FUEL SMELL IN CABIN UPON ARRIVAL AT GATE PERFORMED INSPECTION, CHECK OF AIRCRAFT EXTERIOR WITH NO EVIDENCE OF FUEL LEAKS. RAN APU, BLEED AND PACKS WITH NO ODORS. F/A'S REPORTED ODOR DISIPATED UPON GATE ARRIVAL. AMM REF 05-51-10-200-801-C-1. ACFT OK TO CONTINUE..

Part: NONE — NONE (NONE) · airframe 50,862 hrs · 25,729 cycles

PASSENGER AT SEAT 34A COMPUTER STARTED ON FIRE WHILE CHARGING. INSPECTED SEAT 34A AND SURROUNDING AREA NO DAMAGE FOUND NO BURN MARKS.

Part: BATTERY — NO TEST (ZONE 200) · airframe 50,579 hrs · 25,582 cycles

OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - DID NOT PASS TEST, FAULT ON FWD PESU BATTERY. DID NOT PASS EMERGENCY LIGHT TEST, FAULT ON FWD LEFT EPSU BATTERY. REMOVED AND REPLACED NEW BATTERY IAW AMM 33-51-38, OPS CHECK OKAY.

Part: OXYGEN BOX — LEAKING (ZONE 200) · airframe 50,216 hrs · 25,380 cycles

CRW REPORTED POSSIBLE O2 LEAK, DOWN TO 280 PSI. PERFORMED LEAK CHECK, FOUND FIRST OFFICERS FWD OXYGEN MASK STOWAGE BOX (10RN2) TO BE LEAKING TO THE MASK CONTINUOUSLY AFTER PUSHING PRESS TO TEST BUTTON. REMOVED AND REPLACED IN REF TO AMM 35-12-41-400-001-A, PERFORMED LEAK CHECK AFTER CHANGING PART & NO LEAKS DETECTED. SERVICED OXYGEN SYSTEM IAW AMM 12-14-35-600-001-A.

Part: FUEL CAP — MISSING (WING) · airframe 49,619 hrs · 25,073 cycles

FUELER REPORTS ACFT CAME IN WITH NO SINGLE POINT REFUELING CAP. PENDING TOMC APPROVAL TO DEF PER A319/320 CDL 28A. SDR ADDED DISPATCH DESK: 29 NAME: T.B. DATE: 17-OCT-24-TOMC APPROVES CDL 28A. TOMC APPROVED TO DEF PER A319/320 CDL 28A. SDR ACCOMPLISHED. PLACARD INSTALLED FUEL CAP IAW 28-25-41-400-007-A.PARTS USED: 31-2825-9-0001,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1356554 SN OFF 2809 CAP, COUPLING R OFF 31-2825-9-0001 2809 ON 31-2825-9-0001 0424

Part: BOLT — MISSING (MLG WHEEL) · airframe 48,613 hrs · 24,572 cycles

PDA #3 MLG TIE BOLT MISSING SEE LOG PAGE 8032456. MAIN TIRE NUMBER 3 IS MISSING A BOLT UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. REPLACE #3 MLG TIRE MAC METER INITIATED FOR WITH VENDOR ID V912362 MAC RELATED WORK ORDER 000000003105476 AND PRTR PHAM, JIMMY (V912362) REPLACED #3 MLG TIRE AND WHEEL ASSY PER AMM 32-41-11 PHAM, JIMMY (V912362) REPLACED #3 MLG TIRE AND WHEEL ASSY PER AMM 32-41-11.

Part: OUTFLOW VALVE — OUT OF POSITION (CABIN PRESSURE) · airframe 47,701 hrs · 24,107 cycles

VENT AVNCS SYS FAULTON STATUS UNABLE TO RESET. AEVC TEST SHOWS SKIN AIR OUTLET. PLACED ON MEL 2126C. COMPLIED WITH DDPG AND MM 21-26-00-040-002-A. AEVC TEST COMPLIED WITH. COMPLIED WITH DDPG. OK TO MEL. VALVE, SKIN AIR OFF 31-2125-9-0001 2792 ON 31-2125-9-0001 0282 VALVE, SKIN AIR OFF 31-2125-9-0001 2792 ON 0000 REMOVED AND REPLACED SKIN AIR OUTLET VALVE IAW AMM 21-26-53. OPS CK GOOD. NO FURTHER DEFECTS NOTED. VENT AVNX SYS MESSAGE NO LONGER ACTIVE. PARTS USED: 31-2125-9-0001,QTY :1 18-2126-3-0092,QTY :1 40-0595-3-4206,QTY :1 40-0608-3-0272,QTY :1 40-0597-3-0713,QTY :1 1865638,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1865638 SN OFF 0746 IPC REFERENCE # 21-26-03.

Part: FUEL CAP — MISSING (REFUEL COUPLING) · airframe 46,896 hrs · 23,687 cycles

PDA 2 FUEL CAP MISSING REPORTED BY OPS....REPORTED BY CREW TOMC SMITH REPORTED TO TOMC> REF GMM 02-30-95. FUEL CAP AND LANYARD MISSING CAP, COUPLING R OFF 0000 ON 31-2825-9-0001 7046 REPLACED MISSING FUEL CAP PARTS USED: 1404819,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1404819 SN OFF 0001 IPC REFERENCE # OLD CAP MISSING.

Part: SENSOR — WARNING LIGHT (BRAKES/WHEELS) · airframe 45,989 hrs · 23,185 cycles

CREW REPORTS REJECTED TAKEOFF AT 80 KNTS, BRAKE TEMPS 385 UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V936162 PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. INSPECT PER AMM PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. INSPECT PER AMM MAC RELATED WORK ORDER 000000003078173 AND PRTR 05-51-16, INSPECT WHEELS FOR FLAT SPOTS 05-51-16, INSPECT WHEELS FOR FLAT SPOTS SCHOENFELDER, HAYDEN (V936162)INSPECETED WHEELS PER AMM 05-51-16, NO DEFECTS NOTED SCHOENFELDER, HAYDEN (V936162) INSPECETED WHEELS PER AMM 05-51-16, NO DEFECTS NOTED

Part: LIGHT — INOPERATIVE (RH WING EXT) · airframe 45,560 hrs · 22,955 cycles

CABIN EMERGENCY LIGHTS OPERATIONAL CHECK: {A3NB-33-3-6012} - EPSU EXT LOAD EMER R CIDS FAULT RELAMPED RH OVERWING EXIT LIGHTS REF AMM 33-51-15. OPC NORMAL. INSPECTED RT OVERWING EXIT LIGHT OPS CHECK GOOD. RELAMPED RH OVERWING EXIT LIGHTS REF AMM 33-51-15. OPC NORMAL.

Part: COMPUTER — INOPERATIVE (FWC #2) · airframe 45,429 hrs · 22,899 cycles

RUDDER TRAVEL LIMITER INOP - F-CTL ECAM CAME ON MULTIPLTIMES BELOW 80 KTS AFTER THRUST LEVERS SET I N FLXMCT DETENT ON TAKEOFF. PEFORMED AFS GROUND SCANN PER AMM 22-91-00, PERFORMED EFS 1 AND NORMAL AT THIS TIME. PARTS USED: 31-3152-9-0001,QTY :1 2 GROUND SCAN NO FAULTS NOTED PER AMM 27-96-00, PERFORMED RUDDER 1157644,QTY :1 TRAVEL LIMITING FUNCTION TEST PER 22-61-00-710-001-A NO FAULTS ROTABLE PARTS CHANGE WAS INDICATED - TT # 1157644 SN OFF 8031 NOTED. REPLACED FWC 2 PER AMM 31-53-34-400-001-A STSTEM OPS CKS ADD EMP:371731 COMPUTER, FLIGH OFF 31-3152-9-0001 8031 ON 31-3152-9-0001 1858

Part: NONE — MISSING (LH LDG LT ASSY) · airframe 45,138 hrs · 22,756 cycles

LFT LDG LT MISSING2 WIRES HANGING REPLACED LEFT LANDING LIGHT ASSY REF AMM 33-42-11 TESTS PASS PARTS USED: 31-3341-9-9001,QTY :1 ADD EMP:U102066 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1779896 SN OFF 1729 IPC REFERENCE # 33-42-05-01 LIGHT, RETRACTA OFF 31-3341-9-9001 8729 ON 31-3341-9-9001 5399

Part: FRAME — CORRODED (FR59STR39R) · airframe 44,583 hrs · 22,470 cycles

RH FRAME 59 AT STGR39R HAS CORROSION AT 4 EACH FASTENER HOLES PE R NR9292816/42816 GEN BY V925324 FOLLOWS: "FOR THE INTERIM REPAIR ACCOMPLISHED ON FR59 LATEST REVISION OF ECRA 5340-02066 ON OR BEFORE MAY 16,2023." STR36RH-42RH, ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF THE MECH: V080280 INSP: LC-99, LC98, LC30. PERFORMED INTERIM REPAIR ON FR59 STR39R TO STR42R IAW ECRA 5340-02066. PER PART 1.2 OF ERA GENERATE A DIP LP TO READ AS

Part: TORQUE BOX — CORRODED (AFT CARGO) · airframe 44,583 hrs · 22,470 cycles

AFT CARGO TORSION BOX COVER HAS MULTIPLE ELONGATED HOLES AND COR ROSION PER HAECO LCQ N/R 9292840/42840 GEN BY V080280 REMOVED AND REPLACED AFT CARGO DOOR TORSION BOX COVER SHEET P/N D5347715400490 IAW A319 SRM 51-44-11 BY MECH V061673 INSP BY V07 7960

Part: DOOR SILL — CORRODED (R2) · airframe 44,583 hrs · 22,470 cycles

MAIN CABIN R-2 DOOR SILL HAS SPOTS OF CORROSION. (A3NB-53-3-6185 ), GENERATED BY V919150 AT HAECO LCQ PER NR 9292549 (42549) REMOVED AND REPLACED DOOR SILL AT R-2 FR 66-68 STR 23R IAW A319 SRM 51-42-11 AND SRM 51-44-11, PN D5348004320701. PERFORMED BY V 061673 AND INSP BY V061629.

Part: FITTING — CORRODED (L2 DOOR SILL) · airframe 44,583 hrs · 22,470 cycles

L-2 DOOR SILL AFT CORNER FITTING HAS EXFOLIATING CORROSION, REQU IRES REPLACEMENT PER NR9292874/42874. EVALUATED L-2 DOOR CUT OUT AFT CORNER FITTING FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED CORNER FITTING IAW SRM 51-72-1 1.

Part: FITTING — CORRODED (R-2 DOOR SILL) · airframe 44,583 hrs · 22,470 cycles

MAIN CABIN R-2 DOOR SILL AFT CORNER FITTINGS HAS SPOTS OF CORROSION GENERATED AT HAECO LCQ PER NR 9292552 (42552) BY {A3NB-53-3-6185} REMOVED AND REPLACED AFT CORNER FITTING ON R-2 DOOR SILL IAW SRM 51-42-11/001. ACP BY V061673 INSP BY

Part: FITTING — CORRODED (R-2 DOOR SILL) · airframe 44,583 hrs · 22,470 cycles

MAIN CAIBN R-2 DOOR SILL FWD CORNER FITTINGS HAS SPOTS OF CORROSION. GENERATED AT HAECO LCQ PER NR 9292511 (42551) BY {A3NB-53-3-6185} REMOVED AND REPLACED FWD CORNER FITTING ON R2 DOOR SILL IAW A319 SRM 51-42-11/001. ACP BY V061673 INSP BY

Part: ANCHOR FITTING — CORRODED (LH MLG ANCHOR) · airframe 44,583 hrs · 22,470 cycles

REMOVE LH MLG ANCHORAGE FITTING TO FOM CORRODED. GENERATED AT HA ECO LCQ PER NR 9292728 (42728) BY V061757. {SUPPORT TASK}

Part: INTERCOSTAL — CRACKED (L/H FR16 DR) · airframe 44,583 hrs · 22,470 cycles

L/H FR16 DOOR STOP #7 HOLES 1&3 HAVE CRACK INDICATIONS IN INTERC OSTAL AND FRAME AT 3 O CLOCK "REPAIR BEFORE NEXT FLIGHT" SUPPORT TASK AD RELATED (AD 2022-02-11) GENERATED AT HAECO LCQ PER NR 9 292408 (42408) BY V061632 REMOVED AND REPLACED INTERCOSTAL AND REAMED HOLE 3 (FR LAYER) PE R R53113118, A319 SRM 51-72-11/001, 51-44-11/001. ACP BY V080280 INSP BY V077960.