N845UA

Service difficulty reports · 99

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N845UA' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CALA2026091419382Unknown · smokeTAXIING OUT W BOTH ENG RUNNING. 2 MIN AFTER ENG START FA CALLED TO REPORT LIGHT SMOKE IN CABIN.Sep 2, 2026 · N845UA · Airbus A319131 · Air Distribution SystemSDR CALA2026082018752Oxygen Mask · kinkedLEFT CLASS DIVIDER UPPER PORTABLE O2 MASK IS KINKED & PINCHED AT FITTING. REPLACED THE OXYGEN MASK IAW AMM 35-32-42.Aug 18, 2026 · N845UA · Airbus A319131 · Portable Oxygen SystemSDR CALA2026062917377Battery · abnormalPROCEDURE - EPSU L EMER BATTERY FAILED. REMOVED AND REPLACED EPSU L EMER BATTERY IN REF AMM 33-51-38-000/400-002, OPS TEST OKAY.Jun 26, 2026 · N845UA · Airbus A319131 · Emergency LightingSDR CALA2026062417311Battery Pack · no testRIGHT OVERWING EXT DOOR FAILED EMERGENCY LIGHT TEST. REMOVED AND REPLACED THE RT EPSU BATTERY PACK IAW AMM-33-51-38. INSTALLATION TEST PASSED AND NO FAULTS PRESENT.Jun 23, 2026 · N845UA · Airbus A319131 · Emergency LightingSDR CALA2025122412420Fuel Cap · missingFUEL CAP MISSING ON ARRIVAL AT DFW. NOTIFIED TOMC PER GMM 06-35-10.Dec 20, 2025 · N845UA · Airbus A319131 · Fuel StorageSDR CALA2025122312352Battery · no testEMERGENCY LIGHTS TEST FAILED. EPSU BATTERY FWD LT, REPLACED EPSU BATTERY AT 10WL. RESET BREAKERS & PERFORMED AN OPS CHECK FROM PTP PANEL BUT THE TEST WAS ABORTED WITH A COMMUNICATION FAULT. NEED FURTHER T/S IAW AMM 33-51-38-000-002-A, & 33-51-38-400-002-A. Dec 19, 2025 · N845UA · Airbus A319131 · Emergency LightingSDR CALA2025101410038Proximity Switch · out of adjustDOOR FWD CARGO ECAM ON L DG ROLL. CLEARED AFTER 5 SECONDS. ADJUSTED THE FWD CARGO DOOR PROXIMITY SWITCH. PERFORMED OPERATIONAL CHECK OF DOOR WARNING SYSTEM REF. AMM 52-71-00-710-001-A. THE FAULT HAS BEEN CLEARED, AND THE AIRCRAFT HAS BEEN RESTORED TO ITS NOROct 9, 2025 · N845UA · Airbus A319131 · Door Warning SystemSDR CALA2025091208838Warning Message · false activationWHILE BRAKING TO CLEAR R/W GOT FWD CARGO DOOR OPEN INDICATION FOR 2 SECS. FLT 632. SUSPECT PROX SWITCH REQUIRES ADJUSTMENT. REF TSM 52-31-00-810-801-A CHECKED FWD CARGO DOOR FOR SECURED LATCH CLOSED GREEN INDICATOR AS REQUIRED. CHECK IS GOODSep 7, 2025 · N845UA · Airbus A319131 · Door Warning SystemSDR CALA2025080807483Slide · not reportedDOOR L-2 SLIDE PACK ASSY REQ R & R. REMOVED AND REPLACED L-2 SLIDE PACK ASSY IAW AMM TASK 25-62-44-400-006-A. COMPLIED WITH RII STEPS FOR INSTALLATION OF L2 SLIDE PACK.Aug 8, 2025 · N845UA · Airbus A319131 · Escape SlideSDR CALA2025021302310Door Seal · damagedETREMELY LOUD NOISE COMMING FROM DOOR 1L INFLIGHT AIR RETURN DEBRIEFED CREW WAS LOUD AT ALL ALTITUDES AND AT ANY DIIFERENTIAL PRESS. NOISE LOUDEST AT LOWER AFT CORNER OF L-1 DOOR. RAGS AND BLANKETS NO HELP. DOOR SEAL HAS A HOLE IN THE LOWER AFT CORNER. REFeb 12, 2025 · N845UA · Airbus A319131 · Passenger/Crew DoorsSDR CALA2025010301772Girt Bar · fodINFORMATION ONLY REPORT . F/A REPORTS DOOR 2L IS DIFFICULT TO ARM - ARMING LEVER VERY STIF F DOOR DOES ARM PROPERLY CLEANED AND REMOVED FOD FROM GRIT BAR ATTACH POINTS. SLIDE ARMIMG BAR OPERATES NORMALLY. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.Dec 31, 2024 · N845UA · Airbus A319131 · Emergency EquipmentSDR CALA2024110601028Light · inoperativeRT EMERG EXIT SIDE LIGHTING INOP PROBLEM LIGHT WAS NOT AN EMERGENCY LIGHT. WAS INSTEAD A SIDEWALL LIGHT AND OPS CHECK GOOD OF SIDEWALL LIGHTING GOOD AT THIS TIMENov 3, 2024 · N845UA · Airbus A319131 · Passenger Compartment LightingSDR CALA2024100900791Switch · intermittentEMERG EXIT LIGHTS CAME ON DURING LANDING AND STAYED ON RECYCLE EMERGENCY SW, LIGHTS BACK TO NORMAL.Oct 7, 2024 · N845UA · Airbus A319131 · Emergency LightingSDR CALA2024082000454Oxygen Mask · unwanted deployO2 MASK DROPPED ROW 30 D E F PACKED MASKS PER MM 35-21-43-550-801-A, REQUIRES OPS CHECK PER 35-23-00-710-001-A BEFORE THREE DAYS. OK TO DIP PER 35-21-43-550-801-A FOR 3 DAYS TOMC-APPROVAL FROM SC1ELBYC COMMENT QC CONTROL #:SOURCE DOCUMENT: 35-21-43-550. DURIAug 19, 2024 · N845UA · Airbus A319131 · Passenger Oxygen SystemSDR CALA2024081202190Fitting · crackedR/H AND L/H CONTINUITY FITTING CRACKEDPER HAECO LCQ N/R 9298153 /20153 GEN BY V934190 RMVD AND RPLD RH/LH CONTINUITY FITTINGS PER UNITED EC/RA 5311- 03248 AND AIRBUS DWG R53112919 ISSUE J BY MECH V075077 INSP BY V892442Aug 8, 2024 · N845UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2024072902125Skin · contaminatedR/H ELEVATOR TOP SIDE HAS LIQUID INGRESS AT 100 1/2 INCHES FROM INBOARD END 18 INCHES FROM TRAILING EDGE WITH A DIAMETEROF 1 1/2 INCHES PER HAECO LCQ N/R 9298339/20339. REPAIRED R/ ELEVATOR UPPER SKIN 100.5 IN FROM I/B,18IN FROM T/E 2IN DIA ZONE A IAW A319 SJul 26, 2024 · N845UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2024072202082Floorbeam · crackedFLOOR BEAM FR 66 AT L2 DOOR HAS POSSIBLE CRACK PER HAECO LCQ N/R 9298306/20306 GEN BY.Jul 20, 2024 · N845UA · Airbus A319131 · Fuselage Main, Floor BeamSDR CALA2024071802064Angle · crackedRH AFT TI ANGLE IS CRACKED . REMOVED AND REPLACED RH AFT TI-ANGLE AT FR42 IAW A319 EA 5331-01 718 REV.D AND A319 SRM 51-42-11/001, A319 SRM 51-47-00/001, A319 SRM 51-43-00/001.Jul 15, 2024 · N845UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2022093002580Fastener · missingPDA 3 REF LOG PAGE 9639140 CREW REPORTED MISSING FASTENER, REF ORIGINAL LOG PAGE 9639140 MISSING FASTENER REPLACED.Sep 30, 2022 · N845UA · Airbus A300* · Fuselage Structure (General)SDR CALA2022031400665Flap · overspeedFLAP OVERSPEED AT FLAPS3. GUST RAISED AIRSPEEDFROM 170 TO ABOUT 200.INTO RED SPEED TAPE. PERFORMED INSPECTION AFTER FLAP SLAT EXTENSION AT MORE THAN THE FOUND. INSPECTED THE FLAP SYSTEM PHASE 1, NO DEFECTS FOUND. OF FLIGHT CONTROL SURFACES PHASE 1. OPS CK''D GMar 14, 2022 · N845UA · Airbus A319131 · Standard Practices/StructuresSDR CALA2022010500032Fuel Cap · missingPDA 2 FUEL CAP MISSING UPON ARRIVAL AT PHX. FUEL CAP PLACED ON CDL.Jan 5, 2022 · N845UA · Airbus A300* · Aircraft Fuel SystemSDR CALA2021030300254Latch · malfunctionedFROM TEST FLIGHT - TEST FLT AT 7.5 AP. THE TOP STRIKER LATCH WOU LD NOT REST. GENERATED ON HAECO LCQ N/R 9296979 (38979) BY MECH V892443. ACCOMPLISHED ADJUSTMENT OF FLT DOOR STRIKER LATCH IAW A319 AMM 5 2-51-00-820-051-A. ADJUSTED CHECK GOOD. PERFORMED BY MECHMar 3, 2021 · N845UA · Airbus A319131 · Fixed Inner DoorsSDR CALA2021022200207Plate · deformedCOMPLIES WITH AN AD: R2 DOOR FRAME 66 AT GUSSET PLATE STRINGER 12 HOLE 3,4 AND 5 ARE OUT OF ROUND A3NB-53-4-6355 GENERATED BY AT HAECO LCQ REF 9296328. REPAIRED IAW ECRA 5311-02500, DIP REQ''D TO ACCOMPLISH PERMANENT REPAIR OF RT FR66 STRINGER 12 HOLES PER PAFeb 20, 2021 · N845UA · Airbus A319131 · Fuselage Main, FrameSDR CALA2021022200192Skin · corrodedAFT CARGO DOOR SILL WEB UPPER SKIN SURFACE FRAME HAS CORROSION (4EA CORROSION/1EA TOOL MARKING) PER HAECO LCQ NON -ROUTINE. REMOVED AND REPLACED AFT CARGO DOOR SILL WEB UPPER SKIN WITH NEW SILL WEB PN D5347715400490 PO 1090652.1 PER A319 SRM 51-72-11-9 11-001Feb 19, 2021 · N845UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2021021900188Power Supply · no testDURING CHECK OF THE EMERGENCY POWER SUPPLY UNITS BITE CHECK FAILED FOR 10WL (ATA 33-51-38 EPSU UNIT FWD L) PER HAECO LCQ NON-ROU TINE 9296935/38935. REMOVED AND REPLACED EPSU OWR SUPPLY UNIT 10WL IAW A319/A320 AMM 33-51-38 OPS TEST GOOD IAW A319/A320 AMM 33-5Feb 18, 2021 · N845UA · Airbus A319131 · Emergency LightingSDR CALA2021021900186Power Supply · no test11WL AND 12WL EMER LIGHT BATTERIES FAIL CAPACITY TEST - A3NB-33- 3-6013 - NR 9296049(38049). PARTS TRANSACTION ONLY. ROTABLE PARTS CHANGE WAS INDICATED - TT NR 1248387 SN OFF 8051 TT NR 1211725 SN OFF 1749 IPC REFERENCE NR 3350-01431A POWER SUPPLY, C OFF 3Feb 18, 2021 · N845UA · Airbus A319131 · Emergency LightingSDR CALA2021021500169Intercostal · crackedR1 DOOR FRAME 20 STOP #7 INBD UPPER HOLE IS CRACKED IN THE INTER COSTAL FITTING AT 7: REPAIR BEFORE NEXT FLIGHT CONTACT ENGINEERI NG FOR REPAIR INSTRUCTIONS AD2019-20-10 GEN BY V061633 PER NR 92 96145/HAECO NR38145. REMOVED AND REPLACED CRACKED INTERCOSTAL FITFeb 12, 2021 · N845UA · Airbus A319131 · Service DoorsSDR CALA2021021200168Intercostal · crackedR1 DOOR FRAME 16 STOP #7 INBOARD UPPER AND LOWER HOLES ARE CRACK ED IN THE INTERCOSTAL FITTING AT 4:00. REPAIR BEFORE NEXT FLIGHT CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS PER NR 9296144 HAEC O NR 38144 GEN BY V061633Feb 11, 2021 · N845UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2021021200167Intercostal · crackedL1 DOOR FRAME 16 STOP #1 INBOARD LOWER HOLE IS CFRACKED IN THE W EB AND IN THE INTERCOSTAL FITTING AT 6:00. REPAIR BEFORE NEXT FL IGHT CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS PER NR 9296143 HAECO OPS 38143 AD 2019-20-10 GEN BY V061633 RMVD AND RPLD INTERCOFeb 11, 2021 · N845UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2021021000148Stringer · corrodedSTRINGER 41R BETWEEN FRAMES 61 AND 63 IS CORRODED. CORRODED STRINGER REMOVED AND NEW SPLICED IN PER SRM 53-00-13-300-001 FIG 1 SHEET 2. PER SRI 53-00-13-205-001 TABLE 006 NEED TO ACCOMPLISH INSPECTION AT 60,000 CYCLES OR 120,000 HOURS WHICHEVER IS ACHIEVED FIRFeb 8, 2021 · N845UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2021020800147Stringer · corrodedSTRINGER 41R BETWEEN FRAMES 61 AND 63 IS CORRODED. CORRODED STRINGER REMOVED AND NEW SPLICED IN PER SRM 53-00-13-300-001 FIG 1 SHEET 2. PER SRI 53-00-13-205-001 TABLE 006 NEED TO ACCOMPLISH INSPECTION AT 60,000 CYCLES OR 120,000 HOURS WHICHEVER IS ACHIEVED FIRFeb 8, 2021 · N845UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2021011800053Support Angle · corrodedAFT CABIN LT SHEAR WEB SUPPORT ANGLE HAS CORROSION ON BOTTOM SIDE (A3NB-53-3-6187), PER NR 9296615. GENERATED BY N078625 AT HAECO LCQ. REMOVED AND REPLACED AFT CABIN LT SHEAR WEB SUPPORT ANGLE, IAW A 319 SRM 51-72-11, FR 69 TO FR 70.Jan 17, 2021 · N845UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2021011800052Web · corrodedAFT CABIN LT SHEAR WEB AT FR 69-70 HAS CORROSION. SUPPORT TASK, PER NR 9296245.Jan 17, 2021 · N845UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2021011800049Door Sill · corrodedCORROSION ON R2 DOOR SILL FR 66 & FR 68, PER NR92963 72 HAECO OPS 38372. REMOVED AND REPLACED R2 DOOR SILL, IAW A319 SRM 51-72-11-911-002 AND SRM 51-42-11-801, PN D5348004320701, PO 1074080.8.Jan 15, 2021 · N845UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2021011800048Door Sill · corrodedCORROSION ON L2 DOOR SILL FR 68 DOT B105 A3NB-3-6187, PER NR929636 7 HAECO. OPERATIONS 38367 GEN BY V061680. REMOVED AND REPLACED L2 DOOR SILL FR 68-66 PN D5348004320601, PO 1080678.3,IAW A319 SRM 51-72-11-911-001 AND SRM 51-42-11-801.Jan 15, 2021 · N845UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2021010700020Frame Splice · crackedLT CABIN FLOOR OUTBOARD FRAME 68 SPLICER HAS A CRACK ON UPPER FLANGE SUPPORT TASK. REMOVED AND REPLACED LT CABIN FLOOR OUTBOARD FR 68 SPLICE, IAW A319 SRM 51-42-11 PG 21, 22, 25 AND 26 CAT "A".Jan 7, 2021 · N845UA · Airbus A319131 · Fuselage Main, FrameSDR CALA2018082701856Slide · faultyAN EMERGENCY LIGHT TEST FAILED WITH ASSOCIATED MESSAGE, EPSU EXT LOAD FWD L. ACCOMPLISHED TSM 33-51-00-810-808-A, FOUND THE L1 DOOR SLIDE FAULTY. REMOVED AND REPLACED THE SLIDE IAW AMM 25-62-44-4 00-006-A. OPS CHECKED NORMAL. EMERGENCY LIGHT TEST PASSED. Aug 27, 2018 · N845UA · Airbus A319131 · Escape SlideSDR CALA2018012200294Guide · lack of lubeAFT LEFT CABIN DOOR WILL NOT ARM. LUBRICATED SAFTEY PIN GUIDE FITTING AND DOOR ARMING & DISARMING MECHANISM IAW AMM 12-22-52-640-014A. DOOR OPS NORMAL IAW 52-73-00.Jan 22, 2018 · N845UA · Airbus A319131 · Passenger/Crew DoorsSDR CALA2017080802535Light · no testEPSU EXT LOAD FWD L MESSAGE SHOWN ON FA CIDS PANEL. TROUBLESHOT IAW TSM 33-51-00-810-808A. COMPLETED STEPS 2 A TO G, ALL WIRING CHECKED GOOD. CHECKED RESISTANCE IN LT SLIDE LIGHTS FOUND 10.9 OHMS RESISTANCE, RT SLIDE LIGHTS 296 OMS RESISTANCE. L1 AND R1 DOOAug 8, 2017 · N845UA · Airbus A319131 · Emergency LightingSDR CALA2017052801633Power Supply · no testEMERGENCY LIGHT TEST FAILED AT PTP OPS TEST. FOUND THE FWD LT EPSU INTERMITENT LOAD MESSAGES, REPLACED EPSU 10WL IAW AMM 33-51-38 PB401. OK FOR SERVICE.May 28, 2017 · N845UA · Airbus A319131 · Emergency LightingSDR CALA2017020300259Battery · faultyEMERGENCY LIGHTS TEST FAIL AT PTP PANEL. REPLACED THE BATTERIES AT EPSU UNITS 10WL AND 13WL IAW AMM 33-51-38 PB401. OK FOR SERVICEFeb 3, 2017 · N845UA · Airbus A319131 · Emergency LightingSDR CALA2015070694046Power Supply · inoperativeEMERGENCY LIGHTS IN AFT CABIN SEATS INOPERATIVE. R & R AFT CABIN EMER POWER SUPPLY & BATTERY IAW MM 33-51-38.Jul 5, 2015 · N845UA · Airbus A319131 · Emergency LightingSDR CALA2014101392396Flap · dentedDENT IN RT INBD FLAP NEAR FUSELAGE. DAMAGE WITHIN ALLOWABLE LIMITS IAW SRM 57-52-00 PAR 8. AREA FREE FROM CRACKS IAW NDT IAW NT M51-10-08.Oct 9, 2014 · N845UA · Airbus A319131 · Trailing Edge FlapsSDR CALA2014080691738Slide · faultedEPSU EXT LOAD FWD L FAULT WHEN EMER LIGHTS TEST PERFORMED. REPLACED SLIDE ASSEMBLY DUE TO EXTERNAL LOAD FAULT DOOR 1R IAW 25-62-44.Aug 3, 2014 · N845UA · Airbus A319131 · Escape SlideSDR CALA2014041490810Stringer Splice · corrodedSTRINGER SPLICES HAVE CORROSION AT FRAME 27 - FRAME 28 & STRINGER 39L - STRINGER 42L. UPON FURTHER EVALUATION CORROSION WAS FOUND TO BE OUT OF LIMITS IAW SRM 51-73-11. R & R 4 EACH SPLICES AT ABOVE LOCATIONS IAW SRM 51-42-11 PARA 7.Apr 11, 2014 · N845UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2014041490809Stringer · corrodedFWD CARGO COMPARTMENT STRINGERS HAVE CORROSION ON UPPER & LOWER SURFACES OF CROWN AT FRAME 26 - FRAME 27 & STRINGER 39L - STRINGER 42L. BLENDED CORROSION ON STRINGER & FOUND THE BLENDED AREAS TO BE OUT OF LIMITS SRM 53-21-13 FIG 101. FABRICATED NEW STRINGERSApr 11, 2014 · N845UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2014041490808Doubler · corrodedPREVIOUSLY INSTALLED DOUBLER IN FWD CARGO HAS CORROSION AT SKIN CUT OUT FRAME 26 - FRAME 27 & STRINGER 44R - STRINGER 41R. UPON FURTHER EVALUATION FOUND THE DOUBLER EXFOLIATED. REPLACED DOUBLER & FILLER IAW SRM 53-00-11 FIG 239 SH 2.Apr 11, 2014 · N845UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2014040390749Skin · saturatedRIGHT ELEVATOR UPPER SKIN PANEL HAS A TRAPPED WATER INDICATION 53.5 FROM INBD, 5 FROM TE, 2 DIAMETER. CUT OUT & SANDED AREA. REMOVED WATER, APPLIED REPAIR & RESTORED FINISH IAW UAL TC 4R5517310 PARA 3 5 & 3 6 & SRM 55-21-11 REPAIR 5A PG 215-217, 51-75-12 PARApr 3, 2014 · N845UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2014033190723Stringer · corrodedCORROSION IN AFT PIT IN BILGE AREA ON STRINGER 43L BETWEEN FRAME 55 - FRAME 56. R & R STRINGER 43L FROM FRAME 53 - FRAME 60 IAW SRM 51-42-11.Mar 31, 2014 · N845UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2014033190722Stringer · corrodedCORROSION IN AFT PIT BILGE AREA ON STRINGERS & FASTENERS DOUBLER CUT OUTS FROM FRAME 63 - FRAME 64. R & R STRINGER 41RT FROM FRAME 58 - FRAME 64 IAW SRM 51-42-11, PG 7 E.Mar 31, 2014 · N845UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
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