N840UA

Service difficulty reports · 102

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 = 'N840UA' 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 CALA2026061917188Apu · odorMUSTY SOCK SMELL FROM PACKS W APU BLEED RUNNING OILY MUSTY SMELL WITH PACKS RUNNING ON APU. PLACED APU ON MEL MEL 4910B REJECTED NEED TO ADDRESS THE ODOR IN THE CABIN ACP INITIAL TROUBLE SHOOTING PER FIM TASK 05-50-00-810-831-A , CONFIRMED ORDER STRONG WHEN Jun 14, 2026 · N840UA · Airbus A319131 · Airborne Auxiliary Power Unit (APU) SystemSDR CALA2026060916954Light · inoperativeEMERGENCY LIGHT OUT AT ROW 31CBA, 32CBA REMOVED AND REPLACED SEAT/WALL MOUNT EMERGENCY LIGHT PER AMM 33-51-18. OPS CHECK GOODJun 8, 2026 · N840UA · Airbus A319131 · Emergency LightingSDR CALA2026041015259Fuel Cap · missingFUELER REPORTED FUEL CAP MISSING AFTER T-2272 ON ARRIVAL IN MSP FROM SFO.Apr 6, 2026 · N840UA · Airbus A319131 · Fuel StorageSDR CALA2026032314733Apu · faultedSMOKE FUME EVENT DURING ENGINE 1 START AFT CABIN WAS BAD FLT DEC K HAD FUMES TOO. INSPECTED APU IAW TASK 49-00-00-200-816-A, FOUND SMOKE AND OIL RESIDUE IN THE COMPARTMENT. REMOVED HEAT SHIELD AROUND THE AFT TURBINE SECTION FOUND UPPER & LOWER LUBRICATION LIMar 19, 2026 · N840UA · Airbus A319131 · APU Core EngineSDR CALA2025120211670Battery Pack · no testEPSU BATTERY EMER L, FAULT MESSAGE FROM CIDS WHILE CONDUCTING EMER LIGHT SYSTEM TEST. REMOVED AND REPLACED EPSU BATTERY 11WL, IAW AMM 33-51-38-000-002-A, 33-51-38-400-002-A. OPS CHECKED GOOD, NO FAULT MESSAGES OR DEFECTS NOTED.Nov 29, 2025 · N840UA · Airbus A319131 · Emergency LightingSDR CALA2025102910677Filter · cloggedFUMES REPORTED IN AFT GALLEY, ACFT DIVERTED TO RIC. LOCAL FBO TO FOLLOW AMM 05-51-10-200-801-C-1. REMOVED AND REPLACED CABIN RECIRCULATION FILTERS IAW MM 21-21-00, NO ABNORMAL FINDINGS, OK.Oct 27, 2025 · N840UA · Airbus A319131 · Air Distribution SystemSDR CALA2025072206829Stringer · corrodedAFT PIT STR 31R CORRODED AT FR 65. RMVD AND RPLD STRINGER 31R FROM FR 64-67 IAW A319 SRM 51-72-11- 911-001.Jul 19, 2025 · N840UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2025070706273Fitting · crackedWINDSHIELD LOWER NODE AREA, LEFT CONTINUITY FITTING CRACKED AT HORIZONTAL FLANGE, AFT EDGE. REMOVED/REPLACED LH AND RH CONTINUITY FITTINGS AS DIRECTED BY EA 5310-07675 AND IAW A319 SRM 51-42-14/001 AND AIRBUS REPAIR DRAW INGS R5311-2919 AND R 53113426.Jul 6, 2025 · N840UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2025071106461Door Frame · crackedLH O/W HATCH AFT FRAME SEGMENT IS CRACKED. REMOVED AND REPLACED AFT FRAME SEGMENT ON LH O/W HATCH IAW SRM 51-72-11-911-001, SRM 51-42-11-001, SRM 51-75-12-911-002.Jul 3, 2025 · N840UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2025071106460Door Frame · crackedLH O/W HATCH FWD FRAME SEGMENT IS CRACKED. REMOVED AND REPLACED FWD FRAME SEGMENT ON LH O/W HATCH IAW SRM 51-72-11-911-001, SRM 51-42-11-001, SRM 51-75-12-911-002.Jul 3, 2025 · N840UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2025071106459Door Frame · crackedRH O/W HATCH AFT FRAME SEGMENT IS CRACKED. REMOVED AND REPLACED 1EA FRAME DEGMENT (AFT) AT R/H O/W HATCH IAW SRM 51-42-11-001, SRM 51-72-11-911-001, AND SRM 51-75-12- 911-002.Jul 3, 2025 · N840UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2025071106458Door Frame · crackedRH O/W HATCH FWD FRAME SEGMENT IS CRACKED. REMOVED AND REPLACED 1EA FRAME SEGMENT (FWD) AT R/H O/W HATCH IAW SRM 51-42-11-001, SRM 51-72-11-911-001, AND SRM 51-75-12- 911-002.Jul 3, 2025 · N840UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2025062705994Floor Support · corrodedAFT FLOOR SUPPORT Y 765 AT FR 64-65 HAS CORROSION AT HARD POINT. REMOVED AND REPLACED 1EA FLOOR BEAM (Y765) AT AFT FUSELAGE L/H S IDE IAW A319 SRM 51-47-11/001 AND A319 SRM 51-72-11-911-001.Jun 25, 2025 · N840UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2025062705992Floor Support · corrodedAFT FLOOR SUPPORT Y 1292 AT FR 64-65 HAS CORROSION AT HARD POINT. REMOVED AND REPLACED 1EA FLOOR BEAM *Y1292) AT AFT FUSELAGE L/H SIDE IAW A319 SRM 51-42-11/001 AND A319 SRM 51-72-11-911-001.Jun 25, 2025 · N840UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2025051904829Cap · missingPDA 2 FUEL CAP MISSING AS FOUND ON SERVICE CHECK WALKAROUND. NOTIFIED TOMC NEWMAN REF AMM TASK 28-25-41. REPLACED MISSING FUEL CAP AND LANYARD. NO LEAKS OR DAMAGE NOTED. PARTS USED: 31-2825-9-0001,QTY :1 ROTABLE PARTS CHG SN OFF 4040 PN OFF 31-2825-9-0001 IPMay 16, 2025 · N840UA · Airbus A319131 · Fuel StorageSDR CALA2025040703576Slide · noneFORWARD DOOR ESCAPE SLIDE REMOVE {A3NB-25-3-0020} - SCHEDULED PARTS CHANGE OF L1 DOOR, REMOVED SLIDE PACK. R&R L1 ESCAPE SLIDE. AS PER AMM 25-62-44 C.W RII INSP REQUIREMENTS FOR L1 DOOR REF GMM 09-25-05Apr 2, 2025 · N840UA · Airbus A319131 · Escape SlideSDR CALA2025040703575Slide · not reportedFORWARD DOOR ESCAPE SLIDE PACK ASSEMBLY INSTALL {A3NB-25-3-0020} - SLIDE DOOR SAFETY ARMING PIN INSTALLED. REMOVED SLIDE DOOR SAFETY ARMING PIN AS PER 25-62-44 AFTER SCHEDULED PARTS CHANGE OF L1 SLIDE C.W WITH IDT INSP REQUIREMENT FOR SLIDE DOOF SAFETY ARMING Apr 2, 2025 · N840UA · Airbus A319131 · Escape SlideSDR CALA2024112502947Bolt · missing#1 MLG TIRE MISSING A WHEEL TIRE BOLT.... UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED. PERFORM A GVI MAC RELATED WORK ORDER 000000003123069 AND PRTR OF THE ARE FOR MISSING BOLT. REMOVE AND REPLACE THE MLG TIRE. REMOVED AND REPLACED THE Nov 24, 2024 · N840UA · Airbus A319131 · Wheel/Ski/FloatSDR CALA2024083000518Vent · unknownVENT SKIN VALVE FAULT ACCOMPLISHED RESET PROCEDURE AND AVEC TEST, REF TSM 21-26-00-810-803-A. TEST OK.Aug 28, 2024 · N840UA · Airbus A319131 · Pressure Regulator/Outflow ValveSDR CALA2024080700380Spoiler Sys · faultedF/CTL SPOILER FAULT MESSAGE ON ECAM. (L SPLR4 SERVO VLV 31CE7 OR OUTPUT FROM SEC 1)... TOMC SMITH REQUEST MEL, DEACTIVTED LH SPLR 4 REF MEL 2764W DISPATCH DESK: 34 NAME: CO DATE: 03-AUG-24-OK TO APPLY MEL 2764W FOR SPOILER #4 PAIR INOP PLACED ON MEL. *DM* SUAug 3, 2024 · N840UA · Airbus A319131 · Drag Control SystemSDR CALA2024072602106Skin · contaminatedLH ELEVATOR HAS INDICATION OF WATER INGRESS, VISIBLE AREA 2 INCH ES DIA, 71 INCHES FROM IB EDGE, 13 INCHES FROM AFT EDGE, EXTENDI NG UNDER LIGHTENING STRIP, GEN BY MECH V892444 REPAIRED L/H ELEVATOR UPPER SKIN 71 IN FROM I/B 13IN FROM T/E ZO NE A 2 IN DIS IAW Jul 21, 2024 · N840UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2024072302089Skin · contaminatedRH ELEVATOR UPPER SURFACE HAS EVIDENCE OF WATER INGRESS 29 INCHE S FROM IB EDGE, 22 INCHES FROM AFT .75 IN DIA., GEN BY MECH V892 444 DRILLED WITNESS HOLES ON R/H ELEVATOR UPPER SKIN 29 IN FROM I/B INSP BY V078632 22IN FROM T/E ZONE A 1.5 IN DIA IAW A319 AMM 5Jul 21, 2024 · N840UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2024072302090Skin · contaminatedLH ELEVATOR HAS INDICATION OF WATER INGRESS, 2 INCHES DIA, 117 I NCHES FORM IB EDGE, 13 INCHES FROM AFT EDGE. GEN BY MECH V892444 REPAIRED L/H ELEVATOR UPPER SKIN 77IN FROM I/B EDGE, 12IN FROM T /E ZONE A, 2IN DIA IAW A319 SRM 55-21-11-300-005 PAR 2A CATEGORY Jul 21, 2024 · N840UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2024072302087Skin · contaminatedRH ELEVATOR UPPER SURFACE HAS EVIDENCE OF WATER INGRESS 29 INCHES FROM IB EDGE, 18.5 INCHES FROM AFT EDGE, 1.75 INCH DIA., DRILLED WITNESS HOLES ON R/H ELEVATOR UPPER SURFACE 29IN FROM I/ 75, B 18.5 FROM T/E ZONE A 1.5IN DIA. FOUND NO LIQUID IAW A319 AMM 55-Jul 21, 2024 · N840UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2024011900142Fuel Cap · missingREPORTED BY FUELER FUEL CAP MISSING FUEL CAP MISSING WOULD LIKE TO APPLY CDL 28A CAP AND LANYARD MISSING PLACED ON CDL DISPATCH DESK: 37 NAME: MA. DATE: 17-JAN-24- OK TO DEFER FUEL CAP MISSING.Jan 17, 2024 · N840UA · Airbus A319131 · Fuel StorageSDR CALA2023022400545Valve · failedUPON ACFT ARRIVAL GATE RETURN VERBALLY ADVICED BY FLIGHT CREW FLAP SYST 2 FAULT . PFR SHOWING FLP2 PCU VALVE BLOCK 24CV VALVE SENSOR. SEE TSM PICTURE OF PFR 27-51-00-810-852-A. 27-54-53-000-001-A VERIFIED VALVE BLOCK OF THE POWER CONTROL UNIT (FLAP) WAS REMOVFeb 24, 2023 · N840UA · Airbus A319131 · Trailing Edge Flap Control SystemSDR CALA2022112803243Oxygen Mask · leakingCREW SYSTEM LOW CREW OXYGEN SYSTEM-LOW... RECORD PRESSURE PRIOR TO SERVICING 820PSI AFTER TAKEOFF PRESSURE WAS 870 ON GROUND MARTIN, ERIC (V907926) TROUBLESHOT PER TSM 35-10-00-810-813A. FO UND LARGE LEAK COMING FROM LH OBSERVERS MASK. REMOVED OBSERVER MASK ANNov 28, 2022 · N840UA · Airbus A319131 · Crew Oxygen SystemSDR CALA2022091402357Intercostal · noneAD RELATED SUPPORT TASK (AD 2022-02-11): RH FR16 STOP #7 HOLE #3 (IB LOWER) HAS CRACK INDICATION IN INTERCOSTAL @10 O''CLOCK. AT HAECO LCQ NON ROUTINE 9294266/24266 GENERATED BY V892444. REMOVED DAMAGED INTERCOSTAL & REPLACED WITH A NEW INTERCOSTAL @ R/H FR16 Sep 12, 2022 · N840UA · Airbus A300* · Fuselage Main, FrameSDR CALA2022082602187Fitting · noneRH WINDSHIELD SIDE POST UPPER ATTACHMENT, HOLE ON VERTICAL POST HAS CRACK INDICATION: AD RELATEDE SUPPORT TASK (A3NB-53-4-0068) GENERATED BY V892444 AT HAECO LCQ PER NR 9294532 (24532) PERFORMED CUT OUT OF CRACK AND REPLACED UPPER ATTACHMENT FITTING ON THE RH Aug 25, 2022 · N840UA · Airbus A300* · Fuselage Main, FrameSDR CALA2019012100129Fastener · shearedMAIN CABIN FLOOR FR68 R2 DOOR SILL AFT GIRT BAR SUPPORT HAS SHEARED FASTNER A3NB-53-3-6222 ON LCQ NR 9298248 REMOVED AND REPLACED R2 DOOR SILL BETWEEN FR66-FR68 IAW SRM 51-72-11-911-001.Jan 19, 2019 · N840UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2019012100128Support Angle · corrodedMAIN CABIN FR68 L2 DOOR SILL SUPPORT ANGLE HAS CORROSION SPOTS ON UPPER SURFACE A3NB-53-3-6222 ON LCQ NR 9298263 INSTALLED REPAIR ANGLE AND FILLER IAW SRM 53-41-14. ALODINE AND PRIMED IAW SRM 51-21-11-001. INSTALLED GIRT BAY ASSY IAW IPC 53-46-04-81 AND AMM 52Jan 19, 2019 · N840UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2017120304301Director · malfunctionedEMERG EXIT LIGHTS ON. RESEAT CIDS DIRECTOR SYST OP OKDec 3, 2017 · N840UA · Airbus A319131 · Lighting SystemSDR CALA2017052601598Battery · faultedDURING AN EMERGENCY LIGHTS TEST, MESSAGE FOR THE EPSU BATTERY AFT LT. REPLACED THE BATTERY. OPS CHECKED GOOD.May 26, 2017 · N840UA · Airbus A319131 · Emergency LightingSDR CALA2017051201363Interface Unit · faultedCONSTANT/MULTIPLE FALSE ECAM ALERTS. FADEC/DUAL ENG FAIL/NAV.. EMERGENCY DECLARED. REPLACED CFDIU IAW AMM 31-32-34-400-001-A.AND NR 2 FWC IAW AMM 31- 53-34 OPS CHECK OK . PERFORMED LAND VERIFY IAW AMM 22-97-00 LAND TEST OK . AIRCRAFT REMAINS FULL AUTOLAND STATMay 12, 2017 · N840UA · Airbus A319131 · Central DisplaySDR CALA2017031700609Arm · gougedLEFT HORIZONTAL STABILIZER NR 4 HINGE ARM GOUGED UNDER LOCK FASTENER COLLAR AT FWD OTBD UPPER ATTACH FLANGE. REMOVED AND REPLACED THE ARM IAW SRM 51-72-11, PG. 12.Mar 16, 2017 · N840UA · Airbus A319131 · Horizontal Stabilizer StructureSDR CALA2016101000736Check Valve · inoperativeACFT LOST GREEN HYD QTY OK FOR SERVICE, HYDRAULIC RESERVOIR DID NOT EMPTY, SERVICED TO FULL AFTER LEAK FIXEDOct 7, 2016 · N840UA · Airbus A319131 · Hydraulic System, MainSDR CALA2016100700731Check Valve · leakingLOST GREEN HYD FLUID, FOUND CHECK VALVE PTU MANIFOLD LEAKING. REMOVED AND REPLACED THE CHECK VALVE AND O-RING. LEAK CHECKED, NO LEAKS FOUND.Oct 7, 2016 · N840UA · Airbus A319131 · Hydraulic System, MainSDR CALA2016092095754Selector Valve · malfunctionedAIRCRAFT EXCURSION FROM TAXIWAY. CREW REPORTED LOSS OF BRAKES AND STEERING. PFR SHOWS BRAKE SELECTOR VALVE 23GG FAULT ALONG WITH MLG HYDRAULIC PIPE MESSAGE. TEST RUN ON BSCU CHANNEL 1 & 2. BSCU CHAN 1 LAST LEG REPORT - "BRK SELECTOR VALVE (23GG)/L G HYDRAULISep 18, 2016 · N840UA · Airbus A319131 · Landing Gear Brake SystemSDR CALA2016060795438Pump · leakingAIR RETURN DUE TO YELLOW HYD SYS QTY LOSS. REPLACED MAIN YELLOW SYS ENG PUMP. INSPECTED FILTERS & DPI'S, FOUND NO CONTAMINANTS. SERVICED SYS, PRESS & LEAK CHECKED GOOD.Jun 6, 2016 · N840UA · Airbus A319131 · Hydraulic Pump (Electric/Engine), MainSDR CALA2016060195421Skin · punctured.75 INCH PUNCTURE ON FIXED LE SKIN ABOVE FUEL DOOR UNDER RT NR 3 LE SLAT. ACCOMPLISHED REPAIR IAW SRM 57-41-11-2015A.May 28, 2016 · N840UA · Airbus A319131 · Wing, Plate/SkinSDR CALA2016052095377Battery Pack · defectiveEMERGENCY POWER SUPPLY UNIT FWD LT, FAULT MSG DISPLAYED ON EMER LIGHT SYS TEST. REPLACED BATTERY PACK AT FWD EPSU POSITION 10WL.May 20, 2016 · N840UA · Airbus A319131 · Emergency LightingSDR CALA2015121494878Power Supply · inoperativeEMERGENCY LIGHT TEST FAILED ON 2 SERVICE. REPLACED EMER LIGHT POWER SUPPLY & BATTERY IAW AMM 33-51-38 AT OVERWING EXIT LT SIDE, OPERATIONS CHECKED GOOD.Dec 9, 2015 · N840UA · Airbus A319131 · Emergency LightingSDR CALA2014122392857Fan · faultyFLIGHT ATTENDANT`S REPORTED SMOKE & BURNING SMELL. ACCOMPLISHED AMM TASK 05- 51-10-S00-801C1. DETERMINED THAT NR 2 CABIN RECIRC FAN 14HG IS AT FAULT IAW SEQ 1032003 FOR PART CHANGE.Dec 18, 2014 · N840UA · Airbus A319131 · Air Distribution FanSDR CALA2013122393906Door · brokenFIRST OFFICER`S OXY MASK DOOR BROKEN. IAW GMM 05-30-06 REPLACED FIRST OFFICER`S OXY MASK DOOR.Dec 23, 2013 · N840UA · Airbus A319131 · Crew Oxygen SystemSDR CALA2013120293373Microphone · defectiveUNABLE TO TRANSMIT FIRST OFFICER`S SIDE, RADIO HANDSET & MIC. TROUBLE SHOT TO A BAD MIC FIRST OFFICER`S POSITION. R & R MIC, PERFORMED ADJUSTMENT TEST IAW MM, OPERATIONS CHECKED GOOD.Nov 27, 2013 · N840UA · Airbus A319131 · Audio Integrating SystemSDR CALA2013111892981Power Supply · faultyEPSU INTERNAL LOAD EMERGENCY RT & EPSU UNIT EMERGENCY LIGHT FAULTS WHEN PERFORMING EMERGENCY LIGHTS CHECK IAW 2SV. REPLACED BATTERY PWR SUPPLY 12L RT SIDE, OPERATIONS CHECKED SYSTEM & OPERATIONS CHECKED NORMAL.Nov 15, 2013 · N840UA · Airbus A319131 · Emergency LightingSDR CALA2013111392888Tire · damagedCHUNK OF RUBBER MISSING FROM LT NOSE WHEEL, CORD SHOWING. REPLACED TIRE IAW AMM.Nov 13, 2013 · N840UA · Airbus A319131 · TireSDR CALA2013102892413Rudder · dentedRT SIDE OF RUDDER HAS DENT-DELAMINATION 47" FROM THE BOTTOM & 20.5" FROM THE TE. CUTOUT DENTED & DELAMINATION AREA, REMOVED HONEYCOMB CORE FULL DEPTH, PREPPED, CLEANED, BONDED HONEYCOMB. APPLIED REPAIR & RESTORED FINISH IAW SRM 51-77-11, AIRBUS TD-G2-S2-0055Oct 25, 2013 · N840UA · Airbus A319131 · Rudder StructureSDR CALA2013102892412Sill · corrodedR2 DOOR SILL CORRODED AT FR 68. RII INSP ACP.Oct 25, 2013 · N840UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2013101692094Skin · corrodedRIGHT FUEL TANK LANDING HAS CORROSION 640BB BETWEEN RIBS 6 & 7. REMOVED CORROSION & BLENDED AREA. FOUND WITHIN LIMITS IAW SRM 57-21-11 PG 106-110, STEP 4-H.Oct 15, 2013 · N840UA · Airbus A319131 · Wing, Plate/Skin
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