N895UA

Part: WIRE — BROKEN (ZONE 200) · airframe 50,074 hrs · 26,536 cycles

EMERGENCY LIGHT AT ROW 35CBA INOP. FOUND BROKEN WIRE, REPAIRED WIRE PER AIRBUS 319/320 ESPM 20-43-11-01. OPS CHECK GOOD

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 49,101 hrs · 26,046 cycles

EXIT LIGHT ABOVE L1 DOOR INOP. RE LAMPED L1 DOOR EXIT LIGHT IAW A319 AMM 33-51-00-710-001-A V073952 RESEATED CONNECTOR 2671VC IAW A319 ESPM 20-44-10-02 PERFORMED OP CHECK GOOD IAW A319 AMM 33-51-00-710-001-A

Part: BATTERY — NO TEST (ZONE 200) · airframe 48,855 hrs · 25,909 cycles

OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - PTP SHOWS FAULT: "EPSU EMER AFT L". CORRECTION: SHOWS " EPSU BATTERY AFT L". REMOVED AND REPLACED AFT L EPSU BATTERY 13WL REF AMM 33-51-38-000-002-A AND TASK 33-51-38-400-002-A. OPS CK GOOD. NO FAULTS. OK FOR SERVICE.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 48,738 hrs · 25,843 cycles

CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - FWD LH EMERGENCY BATTERY DID NOT PASS TEST. INSTALLED NEW EMERGENCY BATTER AT FWD LH POSITION. OPS CHECK GOOD. REF AMM TASK 33-51-38-000-002-A.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 48,738 hrs · 25,843 cycles

CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - AFT LH EMERGENCY BATTERY DID NOT PASS TEST. REPLACED AFT LH EMERGENCY BATTERY. OPS CHECK GOOD. REF AMM 33-51-38-000-002-A. PARTS USED: 18-3351-3-0001, QTY :1

Part: UNKNOWN — ODOR (ZONE 200) · airframe 48,485 hrs · 25,714 cycles

ACRID SMELL AFTER T/O IN FLIGHT DECK. UPDATING WITH SMOKE ODOR FORM PERFORMED CONDITIONAL INSPECTION PER AMM 05-51-10-200-801-C1. NO ODOR SMOKE OR FUMES FOUND. PER TOMC REQUEST RAN ENGINE WITH PACKS AND CROSSBLEED. COULD NOT DUPLICATE FAULT. NO HISTORY AND CAPTAIN WAS THE ONLY ONE WHO NOTICED IT BRIEFLY. BELIEVE TO BE MIS IDENTIFIED BY PILOT. OK TO CONTINUE

Part: FUEL CAP — MISSING (WING) · airframe 48,268 hrs · 25,599 cycles

PDA 2 RAMP REPORT FUEL CAP MISSING. INSP'D AREA, NO DAMAGE FOUND. CHAIN LANYARD MISSING WITH CAP. INSTALLED MISSING FUELING CAP, AND CHAIN LANYARD.PARTS USED: 1356545,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1356545 SN OFF 2121 CAP, COUPLING R OFF 31-2825-9-0001 2121 ON 31-2825-9-0001 2934

Part: UNKNOWN — ODOR (ZONE 200) · airframe 48,104 hrs · 25,527 cycles

UNABLE TO OPERATE DUE TO LOGPAGE NUMBER 9672781 PILOT IN COMMAND: UNKNOWN.REFERENCE LOG PAGE: 9672781 DATE AND TIME: 25OCT24 19:46 (26OCT24 02:46Z) AIRCRAFT: 4895 FLIGHT: 1787FROM: DEN TO: OMA PILOT COMMENTS: DEN-OMA. GLUE FUME SMELL NO FURTHER MAINTENANCE ACTION NEEDED

Part: UNKNOWN — FUMES (CABIN) · airframe 46,448 hrs · 24,689 cycles

STRONG ELECT ODOR IN AFT CABIN EMERGENCY DECLARED.... CONTAMINATED AT LEVEL C AIR DUCT AND ECS AT LEVEL C. LOCAL FIRE DEPARTMENT PERFOMED A IINFERED TEST FOR HEAT AND CARBON MONOXIDE TEST. BOTH WERE NORMAL. CONTACT TOMC 847-700-9980. PERFORM AMM INSPECTION 05-51-10-200-801-C1, ONCE SMOKE FORM IS REF TSM 05-50-00-810-831-A RAN BOTH ENGINES ONE AT A TIME . AND INSPECTED APU AREA AND FOUND APU INLET DOOR AREA WITH APPEARANCE OPERATED PACKS WITH APU AND FUMES STILL PRESENT IN CABIN AIR. FILLED OUT BY CREW SEND A COPY TO TOMC BOTH PACKS ONE AT A TIME . NO SMOKE WAS NOTED BUT A FUME THAT OF HYDRAULIC FLUID FROM ACTUATOR. MAY BE A SOURCE OF GRP. . BURNT MY EYES . THE FUME WAS STRONGER COMING OUT OF THE LEFT CONTAMINATION. REQUIRES MORE T/S TO VERIFY. PACK 1 WITH EITHER ENGINE RUNNING .SUSPECT BLEED DUCTS ENGINE RUN FOR BURN OUT. CONTAMINATION FOUND. REF. LP 7537423 FOR INSPECTION AND CLEANING OF APU AREA. VISUAL RAN ENGINES AT VARIOUS POWER SETTINGS WITH BLEEDS ISOLATED, AS PER TSM TASK 05-50-00-810-831-A OPENED BOTH LEFT AND RIGHT INSPECTED L/H PACK BAY AREA NO EVIDENCE OF LEAKS. PERFORMED IDLE PACKS ON, COULD NOT DUPLICATE , NO ODORS OR FUMES NOTED, C/W A/C BAY PANELS AND INSPECTED FOR ANY LEAKS OR FLUID AND FOR ANY RUN ON BOTH ENGINES WITH DIFFERENT PACKS SCENERIOS NO ODOR OR INSP 05-50-00-810-831-A, OPERATED ALL GALLEY OVENS AND COFFEE SIGNS OF CONTAMINATION, NONE FOUND. PANELS ARE REINSTALLED. ALSO FUMES NOTED IN AIRCRAFT CABIN.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,877 hrs · 24,379 cycles

AFT CARGO DOOR OPEN INDICATION ON TAKE OFF, NO LOSE OF CABIN PRESSURIZATION... ADJUSTED AFT CARGO DOOR BOTTOM SENSOR TARGET PER AMM 52-71-12--400 34WV OPS CHECK DOOR. NO FAULTS FOUND. NO LIGHT ON OPS CHECK PER 52-71-00-710-001.

Part: LENS — WRONG PART (FWD CABIN) · airframe 45,662 hrs · 24,271 cycles

F/A SAYS EMER EXIT SIGN OVER ROW 1 - DOES NOTHAVE REQUIRED ARROW S REMOVED AND REPLACED CABIN ROW 1 OVERHEAD EXIT LENS .REF ASM 33-51-01-15G. INSPECTED LIGHT SHADE, CK''D INSTALLATION AND SECURITY REF GMM 09-10-05.

Part: STRINGER — CORRODED (STR43L/FR62-63) · airframe 43,932 hrs · 23,357 cycles

AFT CARGO CORROSION FOUND ON UNDERFLOOR BAY STRINGER 43L IN BETW EEN FRAME 62-63. PERFORMED REPAIR AT AFT CARGO UNDER FLOOR BAY STR 43L BETWEEN FR AME 62-63 IAW A319 SRM 53-41-13-300-010.

Part: FITTING — CRACKED (LH FR 16 #7 DR) · airframe 43,932 hrs · 23,357 cycles

LH FRAME 16 #7 DOOR STOP, IB UPPER AND LOWER HOLES HAVE CRACK IND ICATIONS IN INTERCOSTAL LAYERS IN 6 OCLOCK DIRECTION AD2022-02-1 1 PER HAECO LCQ NR9294490/30490 GENERATED BY V892444 REMOVED AND REPLACED DISCREPANT L/H FR16 STOP #7 INTERCOSTAL IAW A319 EA 5311-02164-001 PER MECH V061616 INSP V079881

Part: INTERCOSTAL — CRACKED (FR 16 RH #7) · airframe 43,932 hrs · 23,357 cycles

FR 16 RH #7 DOOR STOP, IB UPPER AND LOWER HOLES HAVE CRACK INDIC ATIONS IN INTERCOSTAL LAYERS. 9 OCLOCK IB DIRECTION AD 2022-02-1 1 PER HAECO LCQ NR 9294489/30489 GENERATED BY V892444 REMOVED AND REPLACED DISCREPANT R/H FR16 STOP #7 INTERCOSTAL IAW A319 EA 5811-02164-002 PER MECH V061616 INSP V079881

Part: ACCESS PANEL — MISSING (RT WING) · airframe 38,800 hrs · 20,709 cycles

UPON ARRIVAL TO FLL RIGHT WING ACCESS PANEL FOR SPOILER ACUATOR NUMBER 675GB IS MISSING.PANEL OUTBOAD OF WING UNDERSIDE REF IPC 57-51-05-25K. ITEM NUMBER 40 MFG PART NUMBER D5754600900900A. FOR INFO. FURTHER DETAILS AWAITED.

Part: ACCELEROMETER — INOPERATIVE (FLIGHT CONTROL) · airframe 34,766 hrs · 18,763 cycles

AIRCRAFT CLIMBS UNLESS FORWARD PRESSURE IS KEPT ON STICK. NOT NORMAL SEE TSM TASK 27-30-00-810-853-A, PFR SHOWS ACCLRM 4 12CE4 FAILED. TOMC RECOMENDS REPLACING 12CE3 AND 12CE4 REMOVED #3 AND #4 FLIGHT CONTROL ACCELEROMETER 27-92-16 REPLACED BOTH FLT CONT ACCELEROMETERS ACCLRM 3 AND 4, IAW AMM 27-92-16-400-001-A OPS. CHK. GOOD. REMOVED AND REPLACED ELAC 2 REF AMM 27-93-34-400-001-A. PERFORMED OPERATIONAL TEST AND LAND VERIFY TEST. NO DEFECTS NOTED. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1249384 SN OFF 0596 COMPUTER, DO NO OFF 31-2793-9-0001 0596 ON 31-2793-9-0031 8037.

Part: SHEAR PLATE — CORRODED (FRAMES 69-70) · airframe 34,576 hrs · 18,669 cycles

AFT SHEAR PLATE CORRODED BETWEEN FRAMES 69 - 70, STRINGER 23L. REMOVED & REPLACED THE AFT SHEAR PLATE IAW A31 9 51-42-11-001 P6 & 51-72-11-911-001 P 1-3.

Part: SHEAR PLATE — CORRODED (FRAMES 69-70) · airframe 34,576 hrs · 18,669 cycles

RIGHT AFT SHEAR PLATE CORRODED BETWEEN FRAMES 69 - 70, STRINGER 23R. REMOVED & REPLACED THE SHEAR PLATE IAW SRM 51-42-11-001 P.6 & 51-72-11-911-001 P1-3.

Part: FITTING — CORRODED (DOOR SILL) · airframe 28,942 hrs · 15,779 cycles

AFT CARGO DOOR SILL SUPPORT FITTTING BETWEEN FRAMES 56 - 57 HAS CORROSION AROUND FASTENER HOLES. REMOVED AND REPLACED THE DOOR SILL FITTING IAW SRM 51-42-11-001, PARAGRAPH E, AND F.

Part: PANEL — CORRODED (FRAMES 56-58) · airframe 28,942 hrs · 15,779 cycles

AFT CARGO BAY CORROSION HAS PREVIOUS GRINDED OUT IN SEVERAL AREAS FROM FRAME 58R TO 56R (COVER S HEET). REMOVED AND REPLACED AFT CARGO COMPARTMENT COVER SHEET FROM FRAME 55 TO FRAME 59 IAW A319 SRM 51-42-11-001 PARAGRAPH E AND F.