N817UA

Service difficulty reports · 128

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 = 'N817UA' 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 CALA2026101320358Power Supply · faultedTEST OF THE EMERGENCY LIGHTS FAILS WITH EPSU INT LOAD EMER R, EPSU BATTERY AFT L AND EPSU UNIT EMER L MESSAGES. R&R RIGHT OVER WING EPSU REF AMM 33-51-400-001-A. R&R AFT BATTERY OF EPSU REF AMM 33-51-38-000-002-A. OPS CHECK GOOD. NO FAULTS NOTED AT THIS TIME.Oct 12, 2026 · N817UA · Airbus A319131 · Emergency LightingSDR CALA2026090719266Unknown · odorNOTICED UNUSUAL BURNT PLASTIC/ELEC ODOR AS WE STARTED DESCENT. ALSO NOTICED IN AFT CABIN. PERFORMED ODOR MM 05-50-00.Sep 4, 2026 · N817UA · Airbus A319131 · Air Distribution SystemSDR CALA2026082118800Power Supply · no testEPSU BATTERY EMERGENCY LIGHT MESSAGE, DURING OPS CHECK . R & R EPSU 11WL. OPS CHKD GOOD IAW AMM 33-51-38.Aug 21, 2026 · N817UA · Airbus A319131 · Emergency LightingSDR CALA2026062217259Idg · faultedELEC IDG 1 OIL LO PR -AIR RETURN TO IAD PER FLIGHT CREW. VARGAS TOMC CREW PERFORMED ELEC IDG 1 DISCONNECTED, UNCOMFORTABLE CONTINUING TO RDU. VARGAS TOMC LOCKED FOR POSITIVE FIX IMAGES ADDED OF POST FLIGHT REPORT, AND POPPED #1 ENG IDG DPI. UNLOCKED LOG. REF LJun 19, 2026 · N817UA · Airbus A319131 · AC Generator-AlternatorSDR CALA2026042015540Check Valve · faultedTEST FLIGHT DISCREPANCY, NR 1 ENG FIRE HANDLE DID NOT SHUT DOWN THE ENGINE. REMOVED AND REPLACED NR 1 ENG FUEL RECIRCULATION CHECK VALVE IAW AMM 28-16-42-400-001-A. OPS CHECK GOOD, NO LEAKS NOTED. PERFORMED POST FLIGHT PF-6 ENGINE FIRE SHUTDOWN OPERATION CApr 17, 2026 · N817UA · Airbus A319131 · Aircraft Fuel Distribution SystemSDR CALA2025100609618Pin · installedINSTALLED SAFTEY PIN IN RH OFF WING SLIDE INFLATION CYLINDER REMOVED AND STOWED RH OFF WING SLIDE INFLATION BOTTLE SAFTEY PIN REF AMM 52-21-11 ACCOMPLISHED RII APPLICABLE STEPS PER GMM 09-25-05.Oct 3, 2025 · N817UA · Airbus A319131 · Standard Practices/StructuresSDR CALA2025080707414Proximity Sensor · out of adjustR FWD DOOR ECAM AFTERT/O TWICE SPORADICALLY.PRESS NORMAL. ADJUSTMENT OF THE FWD PAX/CREW DOOR.AMM TASK 52-71-00-820-002-A: ADJUSTMENT OF THE PROXIMITY SWITCHES LOCKED FOR FIX..WAS A DIVERSION INTO TPA YESTERDAY FOR THE SAME ISSUE. HAS HISTORY.CONTACT TOMC ONCAug 4, 2025 · N817UA · Airbus A319131 · Door Warning SystemSDR CALA2025080507339Door · false indicationECAM DOOR RT FWD CABIN ON DEPARTURE. FA REPORTS ORANGE LIGHT FLASHING. ACCOMPLISHED VISUAL INSPECTION OF DOOR, DOOR SEAL, STOP PADS, GUIDE ROLLERS, DOOR CLOSED & OPEN POSITIONS, ARMED AND UNARMED. NO DEFECTS SEEN. MEL 5270AX. CLEANED SENSOR IAW AMM 52-00-0Aug 3, 2025 · N817UA · Airbus A319131 · Door Warning SystemSDR CALA2025080407254Elec Connector · dirtyEPSU BATTERY EMERGENCY LIGHT RT. CLEANED CONNECTOR AND EMERGENCY LIGHT SYSTEM OP CHECKED GOOD.Jul 31, 2025 · N817UA · Airbus A319131 · Light System WiringSDR CALA2025073007084Warning Message · false activationDURING CLIMBOUT 2 INTERMITTENT ECAM DOOR RT FWD CABIN. CABIN PRESSURE NORMAL. FAULT WAS NOT ACTIVE AND THERE IS NO HISTORY OF THIS FAULT IN 90 DAYS. REF TSM 52-11-00-810-803-A. FWD RIGHT CREW/PASS DOOR INDICATIONS OP CHECK GOOD. OK FOR SERVICE.Jul 27, 2025 · N817UA · Airbus A319131 · Door Warning SystemSDR CALA2024030100615Target · distortedDOOR R EMER EXIT AT FL320. NO ABN V/S SPOKE WITH CREW, NO PRESSURIZATION PROBLEMS. NO AIR LEAKS NOTED AT EMERGENCY EXIT. PERFORMED VISUAL CHECK OF RT OVERWING EMERGENCY EXIT I.A.W. AMM 52-70-00-040-010-A MEL 5270BK TECH SUPPORT WILL TROUBLESHOOT. T/SING FOUNDFeb 28, 2024 · N817UA · Airbus A319131 · Door Warning SystemSDR CALA2023112703475Skin · crackedMAIN CABIN R2 DOOR OUTER SKIN HAS CRACK AT UPPER FWD CORNER PANEL. GEN BY V919150 ON HAECO LCQ NR 9294410/38410 PLATE COVER ASSY (SKIN) REPLACED ON UPPER CORNER R2 DOOR IAW A31 9 SRM 51-72-11-911-001. ACMP BY MECH V945145 INSP BY V921755Nov 22, 2023 · N817UA · Airbus A319131 · Service DoorsSDR CALA2023112003442Fitting · damagedLH WINDSHIELD SIDE POST UPPER ATTACHMENT HAS 3 FASTENER HOLES WITH CRACK INDICATIONS HOLE A FWD OTBD HOLE B FWD INBD HOLE C AFT INBD MARKED WITH DOTS RESPECTIVELY. REPAIRED HOLE A FWD OTBD, HOLE B FWD INBD, HOLE C AFT INBD AT L/ NO CRACKS FOUND. FINAL HOLE SINov 9, 2023 · N817UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2023112003440Fitting · out of roundLH FR4 SIDE POST UPPER ATTACHMENT CONNECTION FITTING REQUIRES REMOVAL TO FOM SEPERATION OF LAYERS FOR NDT INSPECTION. REINSTALLED LH FR4 SIDE POST UPPER ATTACHMENT CONNECTION FITTING IAW SRM 51-42-11-001 AND 51-72-11-911-001. NO FURTHER ACTION REQUIRED.Nov 9, 2023 · N817UA · Airbus A319131 · Fuselage Main, Attach FittingsSDR CALA2023112003428Skin · shearedAD 2015-02-14 RMLG DOOR ACTUATOR FITTING FWD LUG FWD OTBD FASTENER COMMON TO LOWER EXTERNAL SKIN IS SHEARED (BROEKN HEAD) (EA533 0-04821) GENERATED AT HAECO LCQ PER NR 9294537 LATEST REVISION OF ECRA 5330-07150 ON OR BEFORE 02-NOV-24. P REVISION OF ECRA 5330-Nov 8, 2023 · N817UA · Airbus A319131 · Landing Gear DoorsSDR CALA2023112003426Frame · crackedFRAME 35 STR 30 RH HOLE #2 HAS CRACK INDICATION IN FRAME LAYER 7 O''CLOCK POSITION 30% SCREEN HEIGHT. REPAIRED HOLE #2 AT RH FR35 STR30 IAW ECRA 5331-03064. CREATED CORRECT TO READ: PERFORMED INTERIM REPAIR RH FR35 STR30 HOLE #2 DIP FOR PERMANENT REPAIR TO BNov 8, 2023 · N817UA · Airbus A319131 · Fuselage Main, FrameSDR CALA2023111503384Crossbeam · crackedFRAME 16 LH CROSSBEAM HOLES H1, H2 AND H8 HAVE CRACK INDICATIONS IN LAYER (AD RELATED SUPPORT TASK) (AD 2018-14-09) GENERATED AT HAECO LCQ PER NR 9294461. ON OR BEFORE THE AIRCRAFT REACHES 81,622 TOTAL AIRCRAFT FLIGHT CYCLES ACCOMPLISH INITIAL INSPECTION OF LNov 8, 2023 · N817UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2023110803305Stringer · corrodedAFT CARGO, UNDERFLOOR COMPARTMENT, AFT FR.65 R/H STR. 25, EXFOLIATION CORROSION. PER HAECO LCQ NR 9294659/38659 REMOVED AND REPLACED STR 25R AT FR 64-67 IAW A319 SRM 53-41-13-3 00-004.Nov 4, 2023 · N817UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2023102503182Angle · crackedL/H WING RIB 15 L/E WEB SUPPORT ANGLE CRACKED. PER HAECO LCQ NR 9294242/38242 REMOVED AND REPLACED WEB SUPPORT ANGLE ON LH WING RIB 15 L/E IAW A319 SRM 51-42-11Oct 24, 2023 · N817UA · Airbus A319131 · Wing Miscellaneous StructureSDR CALA2023102303152Floor Support · corrodedMAIN CABIN R/H FR20, Y-254 FLOOR SUPPORT BEAM HAS CORROSION ON U PPER SUFACE A3NB-53-3-6038 PER HAECO LCQ NON ROUTINE 9294357/383 57 GENERATED BY V919150Oct 22, 2023 · N817UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2023102503177Seat Track · chafedMAIN CABIN SEAT TRACK Y-1292 HAS CHAFE MARKS IN TRACK @ FR 54,59 GEN BY V926223 ON HAECO LCQ NR 9294371/38371 REMOVED AND REPLACED -Y 1292 FR 47/51-66 SEAT TRACK IAW SRM 51-7 2-11-911-001.Oct 20, 2023 · N817UA · Airbus A319131 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2023102303162Door Sill · corrodedMAIN CABIN L/H DOOR SILL FR 68 IAW A319 SRM 53-41-14-300-001. REPAIRED MAIN CABIN LH DOOR SILL AT FR68 IAW A319 SRM 53-41-14-3 00-001.Oct 20, 2023 · N817UA · Airbus A319131 · Fuselage Main, Attach FittingsSDR CALA2023102303159Floor Support · wornFLOOR BEAM -Y254 FRAME 68-70 HAS OUT OF ROUND HOLES AT SPLICE AREA. PER HAECO LCQ NR 9294677/38677 REPLACED BEAM AT -Y 254 FR 68-70 I.A.W. A319 SRM 51-72-11-911-0 01.Oct 19, 2023 · N817UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2023102303147Beam · corrodedMAIN CABIN BEAM -Y 254 HAS CORROSION AT FR 66. PER HAECO LCQ NR 9294349/38349 REPLACED BEAMS AND SPLICES AT -Y254 & FR 64 - 68 I.A.W. A319 SRM 51-72-11-911-001.Oct 19, 2023 · N817UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2023102303143Seat Track · corrodedMAIN CABIN R/H FR20, Y-1292 FLOOR SEAT TRACK BEAM HAS CORROSION ON UPPER SURFACE. PER HAECO LCQ NR 9294356/38356 TRACK BEAM DAMAGE WAS REMOVED, NEW TRACK BEAM WAS INSTALLED IAW A319 SRM TASK 51-72-11-911-001Oct 19, 2023 · N817UA · Airbus A319131 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2023080402430Door · warning messageR FRD DOOR OPEN ECAMON T/O VISUALLY CHECKED DOOR THAT IT IS CLOSED AND LOCK. . VERIFY WHITE DOOR IS CLOSED AND LOCKED AND SLIDE ARMED. SLIDE ARMED LIGHT ON INSTALLED INOPERATIVE STICKER ADJACENT TO LOWER ECAM DISPLAY "SLIDE ARMED" LIGHT(S) ON THE DOOR DOES NOTAug 2, 2023 · N817UA · Airbus A319131 · Door Warning SystemSDR CALA2022081602090Skin · damagedFUSELAGE SKIN DAMAGED AT FR26 BETWEEN STR 38-39 LEFT. GENERATED BY V913126 ON HAECO LCQ NR 9298041/28041 X=.900 AND Y=.200. ACCOMPLISHED A DOUBLER REPAIR IAW SRM 53-21- 703 FR24 THRU FR35 ZONE A THE INSPECTION THRESHOLD FROM TIME OF INSPECTION UNTIL 60,000 FC Aug 12, 2022 · N817UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2022081602089Skin · dentedFUSELAGE SKIN DENTED AT FR26 JUST BELOW STR 29 LEFT. GENERATED B Y V913126 ON HAECO LCQ NR 9298042/28042 X=.900, AND Y=.900. ACCOMPLISHED A DOUBLER REPAIR IAW SRM 53-21- 073 FR24 THRU FR35 ZONE A INSPECTION THRESHOLD FROM TIME OF ADL/ UNTIL 60,000FC/120,000FH Aug 12, 2022 · N817UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2022081602088Skin · dentedFUSELAGE SKIN DENTED AT FR 19 RH BETWEEN STR 37-38R. GENERATED B Y V913126 ON HAECO LCQ NR 9298043/28043 =.150, Y=.800. ACCOMPLISHED A DOUBLER REPAIR IAW SRM 53-11-11- FR1 THRU FR24 ZONE F INSPECTION THRESHOLD FROM TIME OF REPAIR 60,000 FC/ 120,000 FH AT INTERAug 12, 2022 · N817UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2021101401884Wheel · damagedREJECTED TAKEOFF AT APPROX 80 KNOTS DO TO HAIL. ACCOMPLISHED REJECTED TAKEOFF / EMERGENCY BRAKE APPLICATION REF. AMM 05-51-16-200-001-A. REMOVED AND REPLACED BOTH #1 & #2 MAIN TIRE ASSY''SOct 14, 2021 · N817UA · Airbus A319131 · Landing Gear SystemSDR CALA2021072101152Fuel Cap · missingPDA 3 FUEL CAP REPORTED MISSING REF LOG 6689310 FOR FUEL CAP REPLACEMENTJul 20, 2021 · N817UA · Airbus A319131 · Fuel StorageSDR CALA2021032200362Brake · overheatedHOT L/INBD BRAKE AFTERT/O..DROPPED GEAR TO COOL..COULD NOT RETRA CT #2 MLG BRAKE READING APROX. 430 DEG. COMPAIRED TO THE OTHER 3 BRAKES READING APROX. 220 WHEN ARRIVED AT GATE. REPLACED WHEEL ASSEMBLY PER AMM 32-41-11. CHECKS GOOD. ROTABLE PARTS CHANGE WAS INMar 22, 2021 · N817UA · Airbus A319131 · Landing Gear Brake SystemSDR CALA2020100701155Battery · no test13WL FAILS BATTERY CAPACITY CHECK - SUPPORT TASK. REMOVED AND INSTALLED SERVICEABLE EPSU BATTERY (13WL) IAW A319 A MM 33-51-38-000-002-A / 400-002-A. OPERATIONAL BITE CHECK GOOD I AW A319 AMM 33-51-00-710-001-A.Sep 30, 2020 · N817UA · Airbus A319131 · Emergency LightingSDR CALA2020091801124Feeder Cable · looseEMERGENCY LIGHTS AT SEAT ROWS 23L; 24L ARE INOP. A3NB-33-3-6015 PER HAECO LCQ NON ROUTINE 9294339 GENERATED BY V061674.Sep 17, 2020 · N817UA · Airbus A319131 · Light System WiringSDR CALA2019042900671Cap · missingFUEL CAP FOUND MISSING ON LOG PAGE 3093282 ADDING SDR FOR PDA 2 PDA COMPLIED WITH PER GMM 023095Apr 29, 2019 · N817UA · Airbus A319131 · Fuel StorageSDR CALA2018120202458Strut · lack of lubeGEAR NOT UPLOCKED DISPLAYED ON UPPER ECAM SCREEN - L-G ON TAKEOFF GEAR WOULD NOT RETRACT SHOCK ABSORBER FAULT. ACP FULL NLG STRUT SVC AND LUBE OF ALL NLG ZERK FITTINGS JACKED AIRCRAFT AND CKED DIMENSIONS OF NLG STRUT EXTEND SWITCHES 24 & 25 GA ACP A FULL GEAR Nov 29, 2018 · N817UA · Airbus A319131 · Nose/Tail Landing Gear Strut/AxleSDR CALA2018102702183Fitting · corrodedRT MLG SIDESTAY ATTACHMENT LUGS TO REAR SPAR HAVE CORROSION IN BORES. BOTH LUGS HAD CORROSION REMOVED AND WERE OVERSIZED PER SRM 57-26-13-300-023. FINISHING CUTS WERE MADE AND OVERSIZED BUSHINGS INSTALLED PER EA 5700-03259 OP 2 PER SRM 57-26-13-300-023 PARA 1DOct 23, 2018 · N817UA · Airbus A319131 · Wing, Landing Gear Attach FittingsSDR CALA2018101302086Power Supply · defectiveEPSU 11WL DEFECTIVE, MULTIPLE SEAT ROWS WILL NOT LIGHT. REMOVED EPSU 11WL IAW AMM 33-51-38-000-001-A, REMOVED BATTERY FORM EPSU 11WL IAW AMM 33-51-000-002-A, INSTALLED BATTERY ON REPLACEMENT ESPU 11WL IAW AMM 33-51-38-400-002-A AMD INSTALLED EPSU 11WL IAW AMM Oct 9, 2018 · N817UA · Airbus A319131 · Emergency LightingSDR CALA2017050101223Lamp · inoperativeMESSAGE EPSU EMERGENCY LOAD RT APPEARED. REPLACED TWO LAMPS. OP CHECKED GOOD IAW AMM 33-51-15. AND AMM 33-51-00.May 1, 2017 · N817UA · Airbus A319131 · Emergency LightingSDR CALA2017031700645Circuit Breaker · malfunctionedSLIDE ARMED LIGHT STAYS ILLUMINATED WITH SLIDE IN THE DISARM POSITION . CYCLED THE CIRCUIT BREAKER 121-P10, TESTED OK IAW MM 52-73-00-710-001-AMar 17, 2017 · N817UA · Airbus A319131 · Escape SlideSDR CALA2017031300598Warning System · false activationDOOR 2R SLIDE ARMED LIGHT ILLUMINATED IN FLIGHT. CYCLED DOOR. DOOR ARMED AND DISARMED. NO DEFECTS FOUND WHILE ARMED. OPS CHECK GOOD REF AMM 52-13-00.Mar 13, 2017 · N817UA · Airbus A319131 · Door Warning SystemSDR CALA2017081402644Shear Tie · corrodedFWD CARGO UNDER FLOOR AREA SHEAR TIE, FRAME 30, STRINGERS 43 - 44R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-42-11.Feb 20, 2017 · N817UA · Airbus A319131 · Fuselage Internal Mounting StructureSDR CALA2017081402643Plate · chafedNR 1 ENGINE LOWER PLATE IS CHAFED. INSTALLED NEW PLATE IAW SRM 54-51-12 FIG 202.Feb 18, 2017 · N817UA · Airbus A319131 · Nacelle/Pylon Miscellaneous StructureSDR CALA2017022000429Plate · chafedNR 2 NACELLE LOWER CHAFE PLATE HAS A CHAFE. REMOVED AND REPLACED THE CHAFE PLATE IAW SRM 54-51-12, F 202, PAR 5B.Feb 18, 2017 · N817UA · Airbus A319131 · Nacelle/Pylon Miscellaneous StructureSDR CALA2017022000428Stringer · corrodedFWD CARGO STRINGER 43L HAS SURFACE CORROSION FRAMES 30 - 31. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-11, PARA 7.Feb 18, 2017 · N817UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2017021700405Tee Fitting · corrodedLEFT EMERGENCY EXIT DOOR LOWER CUTOUT AFT AND FWD SKIN CORRODED ON INNER SKIN AT ATTACH POINTS. REMOVED AND REPLACED THE TEE FITTINGS IAW SRM 51-42-11.Feb 16, 2017 · N817UA · Airbus A319131 · Fuselage Main, Attach FittingsSDR CALA2017021700404Cleat · corrodedFWD CARGO UNDER FLOOR AREA CLEAT ON FR29 STR43R HAS SURFACE CORROSION. REMOVED AND REPLACED THE CLEAT IAW SRM 51-42-11, PAR 7.Feb 16, 2017 · N817UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2017081402641Doubler · corrodedFWD CARGO UNDER FLOOR AREA INNER SKIN HAS SURFACE CORROSION ON DOUBLER FWD OF FRAME 31 AND STRINGERS 43 - 44R. REMOVED AND REPLACED THE DOUBLER.Feb 13, 2017 · N817UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2017081402640Shear Tie · corrodedC2, FWD CARGO UNDER FLOOR AREA SHEAR TIE ON FRAME 28, STRINGERS 42R - 43R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 5 1-92-11.Feb 13, 2017 · N817UA · Airbus A319131 · Fuselage Structure (General)SDR CALA2017081402639Shear Tie · corrodedC2, FWD CARGO UNDER FLOOR AREA SHEAR TIE ON FRAME 29 AND STRINGER 43L HAS SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-42-11, FIG 8.Feb 13, 2017 · N817UA · Airbus A319131 · Fuselage Internal Mounting Structure
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