N828UA

Service difficulty reports · 94

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 = 'N828UA' 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 CALA2026062217220Battery Pack · failedPROCEDURE - EMERGENCY BATTERY FAILURE ON EMER EXIT ROW LH & RH, AFT LT TOO REPLACED BATTERIES IAW AMM 33-51-38-400-002-A & 33-51-38-000-002-A, GOOD FOR SVC.PARTS USED: 18-3351-3-0001, QTY :1Jun 20, 2026 · N828UA · Airbus A319131 · Emergency LightingSDR CALA2026040815208Door Frame · crackedR1 DOOR FRAME 16 STOP FITTING NO.7 HOLES 6 AND C CRACKED. ACCOMPLISHED IMPROVED INTERIM REPAIR ON R1 DOOR FR16 STOP FITTING #7 HOLE #6 IAW ECRA 5311-02464 REV A PART 1A-IMPROVED INTERIM REPAIR STEP 1. INITIAL AND REPEAT INSPECTIONS FROM ECRA 5311-02464 PART Apr 7, 2026 · N828UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2026040815204Door Frame · damagedL1 DOOR STOP NO.1 FRAME 16 FWD FLANGE HOLE 19 DOES NOT MATCH EC/ RA MEASUREMENTS. GENERATED BY V940370 ON AAR LCQ NR 9290180/2218 0. SFR DETAILS ENTERED ACCOMPLISHED REPAIR PER ECRA 5311-03445 AND REO-L25887 ACCOMPLIS H INITIAL INSPECTION OF THE L/H FR 16 LOWEApr 7, 2026 · N828UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2026031314541Unknown · odorPOSSIBLE FUME EVENTWET SOCKS SMELL COMING THROUGH THE VENTS WHILE DECENDING THROUGH 4000 RAN PACKS WITH NO NOTABLE SMELLS FLIGHT DECK OR CABIN. PERFORMED INSPECTION CHECK AS PER AMM TASK 05-51-10-200-801-C1, FORM 46.6020 WAS FILLED OUT BY THE FLIGHT CREW. THENMar 9, 2026 · N828UA · Airbus A319131 · Air Distribution SystemSDR CALA2026011212885Skin · dentedFOUND PREVIOUS DAMAGE ON RT OTBD FLAP TRAILING EDGE. REMOVED OLD BONDING MATERIAL. MAPPED DAMAGE DENT IS LOCATED BETWEEN RIBS 7 & 8 LOWER SURFACE APPROX. 3" AFT OF TE SPAR FASTENERS. DENT NOT IN ALLOWABLE LIMITS IAW SRM 57-53-00-283-092, FIG 1, SHEET 1. REFJan 10, 2026 · N828UA · Airbus A319131 · Trailing Edge FlapsSDR CALA2025111811326Bottle · low pressureR2 DOOR PRESURE BELOW LIMITS. SERVICED R2 CREW DOOR IAW AMM 52-10-00/301.Nov 16, 2025 · N828UA · Airbus A319131 · Service DoorsSDR CALA2025092309150Slide · no discrepancyDOOR 2L SLIDE GAUGE IN RED INSPECTED DOOR 2L SLIDE IAW AMM 25-62-00. DOOR 2L SLIDE IS WITHIN LIMITS AT THIS TIME, SHOWING IN GREEN BAND.Sep 19, 2025 · N828UA · Airbus A319131 · Escape SlideSDR CALA2025062706020Warning Message · false activationECAM IN FLIGHT-AVIONICS DOOR OPEN. AFT AVIONICS COMPT DOOR VERIFIED AFT RIGHT AVONICS DOOR CLOSED AND SECURE. COMPLIED WITH MEL 5270BY. VERIFIED ALL AVONICS ACCESS DOORS ARE SECURE CLOSED AND INSTALLED STICKER ON LOWER ECAM. PERFORMED TEST IAW FIM 52-41-00-Jun 24, 2025 · N828UA · Airbus A319131 · Door Warning SystemSDR CALA2024123003180Battery · dischargedEMERGENCY LIGHT BATTERY 12WL INOP REQUIRES REPLACEMENT. REMOVED AND REPLACED BATTERY PER REF AMM 33-51-38 OPS CHECK GOOD.Dec 28, 2024 · N828UA · Airbus A319131 · Emergency LightingSDR CALA2024122403152Fuel Cap · missingPDA 2 FUEL FILLER CAP NOT INSTALLED. CREW APPLIED STICKER NO LEAKS OR DAMAGE NOTED DISPATCH DESK: 38 NAME: JL DATE: 22-DEC-24- DEFERRED DIRECTLY BY TOMC PERFORMED TASK 28-25-41-400-005-A TO REPLACE MISSING FUEL CAP. CORRECT PART INSTALLED AND LOGGED. PARTS UDec 22, 2024 · N828UA · Airbus A319131 · Fuel StorageSDR CALA2024051501482Window Frame · damagedWINDOW FRAME CENTER POST HAS OUT OF ROUND HOLES REF. HAECO LCQ S.O. 375260 NR 30866. UPDATING MAJOR REPAIR AND SDR TO YES ACCOMPLISHED REPAIR ON WINDOW FRAME CENTER POST HOLES PER HAECO REO ? L25010 REV IR AND ECRA 5311-03174 REV A WITH NO DEVIATION. REF. LP 7May 13, 2024 · N828UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2024051501481Fitting · unknownLOWER NOSE SKIN AND CONTINUITY FITTINGS REQUIRES REMOVAL TO BE RESEALED AND REINSTALLED. REF HAECO LCQ S.O. 375260 NR 30850 ACCOMPLISHED REPAIR PER HAECO REO ? L25010 REV IR AND ECRA 5311-03174 WITH NO DEVIATION. REF. LP 7617185 AND 7617138 FOR DIP THRESHOLDS.May 13, 2024 · N828UA · Airbus A319131 · Fuselage Main, FrameSDR CALA2024041801122Frame · crackedR/H FRAME 20 DOUBLE JOGGLE HOLE #5 HAS A CRACK INDICATION AT 11 O''CLOCK IN FRAME LAYER.Apr 17, 2024 · N828UA · Airbus A319131 · Fuselage Main, FrameSDR CALA2024041201047Window Frame · crackedWINDSHIELD CENTER POST LOWER NODE HAS 2EA CRACK INDICATIONS ADJACENT TO UPPER BOLT ONE LH AND ONE RH BOTH AT UPPER AFT AREA OF BOLT HOLE PER HAECO LCQ N/R 9290616/30616.Apr 10, 2024 · N828UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2024041201046Fitting · crackedWINDSHIELD CONTINUITY FITTING HAS CRACK INDICATION LH AND RH SIDE TOP LEG APPROX .600" FROM CTR POST PER HAECO LCQ N/R 9290349/30349.Apr 10, 2024 · N828UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2024041601108Pad · gougedACFT LOWER TAIL CONE SAFETY STAY MOUNTING PAD CUT OUT INNER SURF ACE GOUGED PER HAECO LCQ N/R 9290786/30786 GEN BY V901665Apr 9, 2024 · N828UA · Airbus A319131 · Aerodynamic FairingsSDR CALA2024031400720Door Frame · crackedL/H EMERGENCY EXIT AFT FRAME CRACKED PER HAECO LCQ N/R 9290392/ 30392.Mar 12, 2024 · N828UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2024031400719Door Frame · crackedL/H EMERGENCY EXIT FWD FRAME CRACKED PER HAECO LCQ N/R 9290393/ 30393.Mar 12, 2024 · N828UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2024030800669Angle · corrodedL2 DOOR SILL CORRODED AT FR 68 PER HAECO LCQ N/R 9290375/30375 GEN BY V061642 PERFORMED REPAIR ON THE L2 DOOR SILL AT FR68 IAW A319 SRM 53-41- 14-300-001.Mar 7, 2024 · N828UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2024030700654Shear Web · crackedL/H AFT CABIN SHEAR WEB FR 68 TO FRAME 69 CRACKED. REMOVED AND REPLACED SHEAR WEB ON L/H AFT CABIN FR68 IAW A319 SRM 51-42-11.Mar 7, 2024 · N828UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2024022900602Door Frame · crackedR/H EMERGENCY EXIT AFT FRAME CRACKEDFeb 28, 2024 · N828UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2024022900600Door Frame · crackedR/H EMERGENCY EXIT FWD FRAME CRACKED.Feb 28, 2024 · N828UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2023030300604Fastener · missingPDA 3 1 FASTENER MISSING FROM EACH LOGPAGE 3778276 (PANEL414FR), 3778267 (PANEL482AR), 3778271 (PANEL414AR)AND 3778263 (PANEL192FB). ALL FASTENERS REPLACED ON THE RESPECTIVE PANELS. TOMC NOTIFIED.Mar 3, 2023 · N828UA · Airbus A319131 · Nacelle/Pylon StructureSDR CALA2022083102225None · noneHYD Y RSVR LOHYD Y RSRV OVHT INSP AC FOUND LEAK AT PRIORITY VALVE ON POWER TRANSFER UNIT MANIFOLD ON AFT WALL ABOVE KEEL BEEM. REMOVED AND REPLACED YELLOW HYDRAULIC PRIORITY VALVE REF AMM.29-11-33-000/400-0001-A. OPERATED YELLOW HYDRAULIC . NO LEAKS FOUND. ROAug 31, 2022 · N828UA · Airbus A300* · Hydraulic Pump, AuxiliarySDR CALA2022041801017Fuel Cap · missingPDA 3 OPS REPORTS FUEL CAP LANYARD MISSING CURRAN, MICHAEL (V921870)APPLIED CDL 28A. NO LEAKS NOTED. REMOVED REMAINING PORTION OF LANYARD. DISPATCH DESK: 31 NAME: AM DATE: 14-APR-22- DEFERRED DIRECTLY BY TOMC UPDATED MAA CODE FIX USING VENDApr 18, 2022 · N828UA · Airbus A319131 · Aircraft Fuel SystemSDR CALA2021033000401Indicator · failedLEFT BRAKE SHOWS 2000PSI ON GAUGE INFLIGHT R&R''D TRIPPLE INDICATOR AMM 32-44-21 PERFORMED BOTH OP''S CK''S ALL TESTS PASSED. PART ENTRY UPDATE. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1937450 SN OFF 3816 IPC REFERENCE # 32-44-08-01 ITEM 50Mar 30, 2021 · N828UA · Airbus A319131 · Landing Gear Brake SystemSDR CALA2019110501920Seal · crackedPDA 2 RIGHT ENG INBD T-R TO PYLON FLEX SEAL (SECOND FROM AFT) IS CRACKED AND MISSING SEGMENT. PARTS UPDATE IPC 54-57-22-07A REMOVED AND REPLACED FLEX SEAL - REF ECRA 5450-02357 REV-B.Nov 2, 2019 · N828UA · Airbus A319131 · Nacelle/Pylon Miscellaneous StructureSDR CALA2019071301186Proximity Sensor · defectiveFWD AVIONICS DISPLAYED ON UPPER ECAM SCREEN. - DOOR IINDICATION WAS RIGHT FORWARD DOOR. APPROVED FOR MEL 5270CB COMPLIED THE PROXIMITY SENSOR OF RH FWD AVIONICS DOOR WAS REPLACED IAW AMM 52-71-14-000-001-A REMOVAL, AMM 52-71-14-400-001-A INSTALLATION, OP TEST Jul 12, 2019 · N828UA · Airbus A319131 · Door Warning SystemSDR CALA2019051700770Battery · discharged(SUPPORT TASK) L-58 NO DOT; THE EMER LIGHT TEST FAILS WITH THE MESSAGE ''EPSU UNIT FWD L'' ATA 33-51-38. REMOVED AND FWD EPSU(10WL) AND FWD EPSU BATTERY IAW AMM 33- 51-38-000-002-A, 33-51-38-000-001-A, 33-51-38-400-001-A AND 33-5 1-38-400-002-A. OPS CHK GOOD IMay 13, 2019 · N828UA · Airbus A319131 · Emergency LightingSDR CALA2018101502125Skin · damagedRT AIRPHONE SYSTEM ANTENNA MOUNT SKIN HOLES HAVE ELEVEN HOLES THAT ARE DAMAGE/OUT OF ROUND/CORROSION AS MARKED ON EXTERIOR OF SKIN (SUPPORT TASK) AT REF. NR 9294752. REPAIRED RT AIRFONE SYSTEM ANTENNA MOUNT IAW EC/RA 5331-02272. DTA DIP LOG PAGE ACCOMPLISH A POct 15, 2018 · N828UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2018101302101Skin · corrodedRT AIRPHONE SYSTEM ANTENNA MOUNT SKIN HOLES HAVE ELEVEN HOLES THAT ARE DAMAGE/OUT OF ROUND/CORROSION AS MARKED ON EXTERIOR OF SKIN. REPAIRED RT AIRFONE SYSTEM ANTENNA MOUNT IAW EC/RA 5331-02272.Oct 12, 2018 · N828UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2018101302092Skin · corrodedLT AIRPHONE SYSTEM ANTENNA MOUNT SKIN HOLES HAVE SEVEN (7) HOLES THAT ARE DAMAGED /OUT OF ROUND/ CORROSION AS MARKED ON EXTERIOR OF SKIN. CUT OUT DAMAGE AT LT AIRPHONE ANTENNA MOUNT BETWEEN FR 63 AND 64 AND STR 42 LT AND 43 LT IAW SRM 53-00-11-300-002. CUTOUT Oct 9, 2018 · N828UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2018101302090Skin · dentedREAR AVIONICS COMPARTMENT ACCESS DOOR 824 HAS MULTIPLE DENTS. REWORKED DENTS & INSTALLED REPAIR DOUBLER AT REAR AVIONICS COMPT ACCESS DOOR 824 PER SRM 51-73-00 PARA 7(A) & SRM 52-41-00- 300-001 PG 4 STEP 3(R).Oct 9, 2018 · N828UA · Airbus A319131 · Electrical/Electronic Compartment DoorsSDR CALA2018100802056Intercostal · crackedAD RELATED 2017-22-03 A3NB-53-4-6304 ABHEC SCAN REAVEALED CRACK OF 2EA IB HOLES OF NR 7 STOP FITTING AT FR 16 OF R1 DOOR GENERATED BY V892444 UPON FURTHER EVALUATION FOUND CRACKS TO BE IN INTERCOSTAL ONLY REMOVED AND REPLACED INTERCOSTAL AT NR 7 STOP FITTING LOct 1, 2018 · N828UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2018092801996Stop Fitting · crackedL-1 DOOR CUTOUT FRAME 16 STOP FITTING LOCATION 7 HAS TWO CRACKED HOLES. UPPER INBOARD HOLE IN INTERCOSTAL AT 6:00 AND LOWER INB OARD HOLE IN WEB AT 4:00 A3NB-53-4-6304 GENERATED BY V061633 REMOVED AND REPLACED INTERCOSTAL AT FR16 STOP FITTING NO. 7 IAW A319 SSep 26, 2018 · N828UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2018091701934Nut Plate · brokenAFT CABIN L2 DOOR SILL AT FR68 HAS BROKEN NUT PLATE HOLE. REPAIRED AFT CABIN L2 DOOR SILL AT FR68 IAW SRM 53-41-14-30 0-001 FIG 20101 PRINCIPLE 5 REPAIR CATEGORY A.Sep 11, 2018 · N828UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2018011200171Battery · faultedDURING A SERVICE CHECK, FOUND EPSU FOR THE EMERGENCY LIGHT BATTERY LT FAULT MESSAGE ON CIDS DISPLAY. REPLACED THE EPSU BATTERY AND OP CHECKED GOOD IAW AMM 33-51-39.Jan 12, 2018 · N828UA · Airbus A319131 · Emergency LightingSDR CALA2017041400963Proximity Sensor · faultyL/G SHOCK ABSORBER FAULT. EMERGENCY DECLARED. CLEARED ITSELF DURING DESCENT AT 11000 FEET. WHILE SPEAKING TO THE PILOT IN FLIGHT HE ALSO OBSERVED THE FOLLOWING WARNINGS: AUTO FLT AP OFF AUTO FLT A/THR OFF ANTI ICE STBY PITOT L/G SHOCK ABSORBER FAULT L/G RETRAApr 14, 2017 · N828UA · Airbus A319131 · Landing Gear Position and WarningSDR CALA2017041000947Warning System · false activationAUTO FLT ''AP OFF'' AND ''A-THR OFF'' DISPLAYED ON UPPER ECAM SCREEN. EMERGENCY DECLARED. SUSPECTED LGCU 1 FAULT PERFORMED BITE TEST ON LGCU1 TEST OK MESSAGE CLEARED.Apr 10, 2017 · N828UA · Airbus A319131 · Autopilot SystemSDR CALA2017040700852Windshield · failedF/O FWD WINDSCREEN OUTER PANE SHATTERED. EMERGENCY DECLARED. REMOVED & REPLACED THE WINDSHIELD IAW MM 56-11-00 & 56-11-11.Apr 7, 2017 · N828UA · Airbus A319131 · Flight Compartment WindowsSDR CALA2017010900055Power Supply · faultyBATTERY EMERG POWER SUPPLY FOUND INOP AT FWD LT CABIN. REPLACED BATTERY EMERG POWER SUPPLY LT FWD IAW AMM 33-51-38-000- 002A AND 33-51-38-400-002A, OPS CK GOOD.Jan 9, 2017 · N828UA · Airbus A319131 · Emergency LightingSDR CALA2016081195613Cids · malfunctionedCIDS MESSAGE, EPSU BATTERY AFT LEFT. CYCLED CIDS, TESTED GOOD IAW AMM.Jun 24, 2016 · N828UA · Airbus A319131 · Emergency LightingSDR CALA2016081195612Cids · malfunctionedCIDS MESSAGE, EPSU BATTERY FORWARD LEFT. CYCLED CIDS, TESTED GOOD IAW AMM.Jun 24, 2016 · N828UA · Airbus A319131 · Emergency LightingSDR CALA2015082894254Battery Pack · dischargedFORWARD LT EPSU BATTERY INOPERATIVE. REPLACED BATTERY PACK FWD LT. OPERATIONS CHECKED GOOD IAW AMM 33-51-38-400-002.Aug 28, 2015 · N828UA · Airbus A319131 · Emergency LightingSDR CALA2015082894253Battery Pack · dischargedEPSU MID LT INOPERATIVE. REPLACED EPSU & BATTERY PACK OPERATION CHECKS GOOD IAW AMM 33-51-38-400-001 & 33-51-38-400-002.Aug 28, 2015 · N828UA · Airbus A319131 · Emergency LightingSDR CALA2014123092875Battery · failed11WL EPSU BATTERY FAILED. REPLACED BATTERY IAW AMM 33-51-38.Dec 23, 2014 · N828UA · Airbus A319131 · Emergency LightingSDR CALA2013112093111Control Unit · faultySDCU MESSAGES REPEAT LEVEL 1 CHRONIC SDCU NO DATA MESSAGES. PROBLEM STARTED AFTER THE LAST SDCU WAS INSTALLED, OCCURS ON ENG START. REPLACED THE SDCU PCN 565-9019 IPC 26-17-08-02-130E AMM 26-17-34-401, SYSTEM CHECKED OK.Nov 19, 2013 · N828UA · Airbus A319131 · Smoke DetectionSDR CALA2013102592389Cylinder · crackedONE RT MED DAMPER CYLINDER STRIKER ASSEMBLY IS CRACKED AT ATTACH FLANGE. GENERATED C-CHECK WU M7739I. REPLACED CYLINDER ON WU M7739I.Oct 24, 2013 · N828UA · Airbus A319131 · Passenger/Crew DoorsSDR CALA2013101592081Display · faultyCAPTS LT PFD SCREEN IS BLURRY, EVEN SWITCHING DISPLAY THE LT SCREEN IS FUZZY. R & R LOWER ECAM DU IAW TASK 31-63-22, OPERATIONS CHECKED GOOD. ALSO PERFORMED TASK 2 4-25-00-710-001-A ESS-GEN SWITCHING TESTED GOOD.Oct 15, 2013 · N828UA · Airbus A319131 · Central DisplaySDR CALA2013082290649Battery · dischargedDURING TWO SERVICE EMERGENCY LIGHT CHECK HAD EPSU EMERGENCY LIGHT MESSAGE. REPLACED EPSU IAW AMM 33- 51-38 & EPSU BATTERY IAW AMM 33-51-38. BITE TESTED GOOD ON EPSU & EMERGENCY LIGHT CHECKED GOOD AT DOOR 1L.Aug 14, 2013 · N828UA · Airbus A319131 · Emergency Lighting
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