N832UA

Service difficulty reports · 81

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 = 'N832UA' 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 CALA2026031014477Fuel Cap · missingON ARRIVAL FOUND REFUEL/DEFUEL COUPLING CAP MISSING FROM THE AIRCRAFT. INSTALLED NEW FUEL CAP.Mar 9, 2026 · N832UA · Airbus A319131 · Fuel StorageSDR CALA2026022514057Power Supply · no testEPSU BATTERY MESSAGE DURING EMERGENCY LIGHT TEST. R & R RT EPSU IAW AMM 33-51-38-000-001-A AND 33-51-38-400-001-A. PASSED EMERGENCY LIGHT TEST.Feb 23, 2026 · N832UA · Airbus A319131 · Emergency LightingSDR CALA2026021113699Battery · shortedFWD LEFT EPSU UNIT INOPERATIVE. REPLACED EPSU BATTERY AT DOOR 1L PER AMM 33-51-38-000-002-A, BATTERY FAULT & UNIT FAULT CLEARED. FOUND BATTERY SHORTED & FAULTED UNIT.Feb 10, 2026 · N832UA · Airbus A319131 · Emergency LightingSDR CALA2025102110335Skin · corrodedEXTERNAL FUSELAGE SKIN FR34 STR 43 IS CHAFFED. PERFORMED INTERNAL & EXTERNAL DOUBLER REPAIR PER HAECO REO L2558 5 / ECRA 5321-02170. GENERATE DIP ACCOMPLISH A PERMANENT REPAIR AT FR34 STGR 41LH - 41RH FUSELAGE SKIN PANEL PER PART 3 OF THE L ATEST REVISION OF EOct 17, 2025 · N832UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2025101510118Stringer · corrodedAFT CARGO STR 33R HAS CORROSION, FRS 59-61. REMOVED AND REPLACED STRINGER 33R BETWEEN FRS 59-61 IAW SRM 51-72-11 -911-001.Oct 6, 2025 · N832UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2025100309584Brace · gougedFR 1 BULKHEAD CENTER SUPPORT STRUT HAS A GOUGE. REMOVED AND REPLACED RH CENTER POST AT FR 1 BULKHEAD IAW A319 S RM 51-42-11/001 AND SRM 51-72-11-911-002.Sep 30, 2025 · N832UA · Airbus A319131 · Fuselage Main, BulkheadSDR CALA2025103010760Window Frame · crackedFLIGHT DECK, WINDSHIELD FRAME LT SIDE HAS A CRACK INDICATION I N LOWER HORIZONTAL FLANGE AT CONTINUITY FITTING INBD HOLE. ACCOMPLISHED INTERIM REPAIR PER HAECO REO-L25587 REV IR WITH NO DEVIATIONS IAW ECRA 5311-03394 PART 1 INTERIM REPAIR STEP 1.Sep 26, 2025 · N832UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2025092609292Fitting · crackedFLIGHT DECK RT CONTINUITY FITTING HAS CRACK INDICATION APPROX .400 INCH FROM CTR POST. REPLACED CONTINUITY FITTING IAW EA 5310-07675 004.Sep 23, 2025 · N832UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2025101510111Skin · corrodedFR 34 AREA I STRG 42L HAS CORROSION. REPAIRED STR 42L BETWEEN FR34-29 IAW SRM 53-21-13-300-018.Sep 22, 2025 · N832UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2025101410055Stringer · corrodedAFT PIT S37R HAS CORROSION FROM FR 59-61. REMOVED AND REPLACED STRINGER SECTION 37RH FROM FR 59-FR61 IAW SRM 51-72-11. SEE CONTINUATION SHEET ATTACHED FOR ADDITIONAL WORK ACCOMPLISHED. REF LP 6206878. REMOVED AND REPLACED STRINGER SECTION STR 37RH FROM FR59-Sep 22, 2025 · N832UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2025103010761Door Frame · corrodedCABIN R-2 DOOR CORROSION AT FR 68 BETWEEN STR 22 AND STR 23. EVALUATED CORROSION AT R2 DOOR FR68 RT BETWEEN STR 22 AND 23 IAW SRM 53-41-12-283-001, CORROSION FOUND TO BE OUT OF LIMITS, MAXI MUM REWORK ALLOWED .02 IN, FOUND DAMAGE TO BE .025 IN. IAW SRM 5 3-41Sep 15, 2025 · N832UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2025092409209Rib · crackedPOSSIBLE CRACK AT TWO PLACES ON INNER FWD RIB ON RT EMERGENCY EXIT HATCH. REMOVED AND REPLACED INNER FWD RIB ON R/H EMERGENCY EXIT IAW A31 9 SRM 51-72-11-911-001Sep 15, 2025 · N832UA · Airbus A319131 · Emergency ExitsSDR CALA2025092409207Skin · corrodedUPPER FUSELAGE, VERT STABILIZER FUSE CORRODED FWD OF VERT STAB AT FR 69 BETWEEN STR AD STR 2R. PERFORMED DOUBLER REPAIR IAW SRM 53-41-11-300-037.Sep 8, 2025 · N832UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2025092409206Support Beam · corrodedAFT CABIN WET AREA R/H AFT LATERAL SHEAR PLATE SUPPORT BEAM BETWEEN FR69-70 HAS CORROSION ON LOWER SURFACE. REMOVED AND REPLACED R/H FR 69-70 SHEAR PLATE SUPPORT BEAM AND REINSTALLED SHEAR PLATE RE APPLIED SURFACE PROTECTION IAW SRM 51-42-11 AND 51-75-12.Sep 3, 2025 · N832UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2025090208359Seat Track · corrodedSEAT TRACK -Y1292 FR 41-47 IS OUT OF LIMITS. REPLACED SEAT TRACK REMOVED AND REPLACED SEAT TRACK -Y1292 ON FR41-47 IAW A319 SRM 5 1-72-11.Aug 28, 2025 · N832UA · Airbus A319131 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2025090208358Seat Track · corrodedFWD CABIN FLOOR BEAM Y765 CORRODED AT FR 16. REMOVED AND REPLACED SEAT TRACK Y765 FROM FR12 TO FR24 MAIN CAB IN IAW A319 SRM 51-42-11 AND SRM 51-72-11-911-001.Aug 28, 2025 · N832UA · Airbus A319131 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2025090208357Seat Track · corrodedFWD CABIN SEAT TRACK -Y765 CORRODED AT FR 20. REMOVED AND REPLACED SEAT TRACK Y-765 AT BETWEEN FR12-FR24 IAW A 320 SRM 51-72-11-911-001.Aug 28, 2025 · N832UA · Airbus A319131 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2025090208356Floor Support · corrodedAFT CABIN WET AREA FLOOR SUPPORT Y -765 HAS SPOTS OF CORROSION & SCRIBE MARKS AT FR67 AND 68. REMOVED AND REPLACED AFT CABIN WET AREA FLOOR SUPPORT -Y765 FR67 AN D 68 IAW SRM 53-41-14-03-A AND SRM 51-42-11/001.Aug 28, 2025 · N832UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2025082908262Dummy Rail · corrodedFWD CABIN CTR DUMMY BEAM CORRODED AT FR21. REMOVED AND REPLACED NEW CTR DUMMY BEAM FROM FR 20 TO FR 24 IAW A319 SRM 51-42-11-001.Aug 27, 2025 · N832UA · Airbus A319131 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2025082908261Seat Track · corrodedFWD CABIN SEAT TRACK -Y1292 CORRODED AT FR20. REMOVED AND REPLACED SEAT TRACK Y-1292 FROM FR 12 TO FR 24 AT MA IN CABIN IAW SRM 51-42-11 AND SRM 51-72-11-911-001.Aug 27, 2025 · N832UA · Airbus A319131 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2025082908260Seat Track · corroded-Y1292 FR 35-36 IS OUT OF LIMITS. REPLACED SEAT TRACK -Y1292 BTW FR 35 TO 36 IAW A319 SRM 51-72-11 AND SRM 51-42-11. SFR #1698.Aug 27, 2025 · N832UA · Airbus A319131 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2025082108015Floor Support · damagedAFT CABIN WET AREA FLOOR SUPPORT Y 765 HAD SCRIBE MARKS AT FR66. R & R THE FLOOR SUPPORT IAW SRM 51-72-1 1.Aug 20, 2025 · N832UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2025030702628Indication Sys · faultedRIGHT OVERWING EXIT "SLIDE" DOES NOT INDICATE ARMED. INSTALL THE LOCK PIN ASSY ON THE INFLATION RESERVOIR IN THE AFT CARGO COMPARTMENT AS PER AMM 52-21-11-000-001-A STEP 3 A. ECAM PAGE INDICATION SHOWS RT HAND OVERWING DOOR CLOSED AND LATCHED BUT DOES NOT SHOWMar 4, 2025 · N832UA · Airbus A319131 · Door Warning SystemSDR CALA2024112901348Chiller · malfunctionedAFT CHILLER OR CHILLERS MOTORS PULSATE ON/OFF. FA SMELLED ELECTR ICAL FA SMELL ELECTRIC BURN. OPERATED BOTH AFT GALLEY CHILLERS AND OPERATED NORMALLY. FOUND NO EVIDENCE OF ANY ELECTRICAL BURNING OR ODORS. ONLY SOURCE OF SMELL WAS A SMALL AMOUNT OF COFFEE ON A Nov 27, 2024 · N832UA · Airbus A319131 · Buffet/GalleysSDR CALA2024092700698Fan · faultyWHILE PERFORMING SMOKE AND ODOR INSPECTION FOUND RT HAND RECERCULATION FAN C/B POPPED. UNABLE TO RESET. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE APPLY MEL # 2121B, CONTACT TOMC ONCE AT AIRCRAFT FOR DDP PROCEDURE.. UPDATED MAA CODE FIX USING VENDOR MSep 27, 2024 · N832UA · Airbus A319131 · Air Distribution FanSDR CALA2023111703412Lens · wrong partLEFT OVERWING EXIT DOOR LIGHTED SIGN LENS POINTING THE WRONG WAY REQ DEFER NEF 2522MP REJECTED MEL 2522MP-..LEGIBILTY OF SIGN IS CONSIDERED IMPAIRED DUE TO EXIT ARROW FACING THE WRONG DIRECTION. SINCE ITS EMERGENCY EXIT LIGHTING IT MUST BE FIXED. RPL LENS WITHNov 16, 2023 · N832UA · Airbus A319131 · Emergency LightingSDR CALA2023090402691Stringer · damagedLH FR35 STGR28-31 HAS REJECTABLE DAMAGE INDICATIONS AT BULKHEAD HOLES AND AT LH STR31 AT FR35. "FR35 STGR 28LH-31LH BULKHEAD HOLES & LH STGR 31 AT FR35 WERE SOLUTION WITH INSP REQUIREMENTS. ACCOMPLISH A PERMANENT OR BEFORE 22-FEB-2024." REPAIRED AT BFM. REPAIRSep 2, 2023 · N832UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2019083001458Cylinder · leakingR2 PASSENGER CREW DOOR DAMPER EMERGENCY OPERATION CYCLINDER FOUND LEAKING. REMOVED AND REPLACED R2 DOOR EMERGENCY OPERATION CYLINDER DIAPHR AM IAW AMM 52-10-00-610-001-A.Aug 29, 2019 · N832UA · Airbus A319131 · Emergency EquipmentSDR CALA2019083001447Skin · crackedDURING HMV-3/C-4 CHECK AT AAR DLH "REF NON-ROUTINE 9026654" ROTO PROBE INSP SHOWS CRACK INDICATION @ FR35 (HOLE#2) STRINGER 30RH SIDE @ 8 O''CLOCK. ACCOMPLISHED ITERIM REPAIR PER PART 1 OF ECRA 5331-02439.Aug 26, 2019 · N832UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2019082301410Door Frame · crackedAD 2018-03-12 EA 5340-01724 REV A OP 002 A-20 NO DOT ROTO PROBE INSP SHOWS CRACK INDICATION @ FR68 RH SIDE DOOR STOP #1 (BOTTOM DOOR STOP) LOWER I/B HOLE REPAIR BEFORE NEXT FLIGHT. ACCOMPLISHED FREEZE PLUG REPAIR TO FR68 RH SIDE DOOR STOP #1 LOWER I/B HOLE IAWAug 21, 2019 · N832UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2019082301409Skin · dentedDENT IN SKIN BETWEEN FR25-FR26 STR L/H 39-40 DENT IN FUSELAGE SKIN BETWEEN FR 25 AND FR 26 STR 39L AND 40L WA S OUT OF LIMITS. PERFROMED DUOBLER REPAIR IAW A319 SRM 53-00-11- 300-029. SIR INSPECTION THERSHOLD FROM THE TIME OF ADD EMP:V918695 ADL/REPAIR EMBODIMAug 21, 2019 · N832UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2019082301408Bulkhead · crackedL/H SIDE PRESSURE PANEL BTW FR 35-36 FASTNER HOLES OUTSIDE THE C UTOUT AREA #18, #19, #20, #24 AND #26 HAVE CRACK INDICATIONS. REPAIRED HOLES 18,19,20,24 AND 26 L/H SIDE PRESSURE PANEL BETW EEN FR35-36 IAW ECRA 5331-02433.Aug 21, 2019 · N832UA · Airbus A319131 · Fuselage Main, BulkheadSDR CALA2019080401305Door Sill · corrodedAAR NR 9027023, SPEC NO. A3NB-53-3-6222 DOTNO. A3-009 CORROSION ON L2 DOOR SILL BETWEEN AFT GIRTBAR FITTING LOWER PLATE AND FRA ME 68 REPLACED L2 DOOR SILL IAW A319 SRM 51-72-11 TREATED, PRIMED AND PAINTED IAW SRM 51-75-12.Aug 2, 2019 · N832UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2019080401304Door Sill · corrodedSPEC NO.A3NB-53-3-6222 DOTNO.A3-012 CORROSION ON R2 DOOR SILL TWO MOST INBOARD FASTENER HOLES NEXT AFT GIRT BAR LOWER ATTACH FIT TING AAR NR 9027032 REPLACED R2 DOOR SILL IAW SRM A319 51-72-11. TREATED, PRIMED AND PAINT IAW A319 SRM 51-75-12.Aug 2, 2019 · N832UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2017100903570Switch · stuckEMERGENCY LIGHTS STUCK IN THE ON POSITION. CYCLED NSFSB SWITCH. EMERGENCY LIGHTS OPS NORMAL.Oct 9, 2017 · N832UA · Airbus A319131 · Light System WiringSDR CALA2017091103151Power Supply · inoperativeEMERGENCY LIGHTS TEST TO FAILED. REPLACED THE EPSU AND BATTERY 12WL IAW AMM 33-51-38, PB401.OK FOR SERVICESep 11, 2017 · N832UA · Airbus A319131 · Emergency LightingSDR CALA2017071002179Switch · malfunctionedEMERGENCY EXIT LIGHTS STAY ON WITH SWITCH IN ARMED OR OFF POSITION. RESET NSFSB SWITCH - OPS CHECKS GOOD.Jul 10, 2017 · N832UA · Airbus A319131 · Emergency LightingSDR CALA2017061101791Socket · looseFA REPORTED ELECTRICAL BURNING ODOR AT ROWS 8-10. ODOR DISIPATED MINUTES LATER. ISOLATED TO ROWS 8-10. F/O WENT TO THE AREA OF ODOR & DID NOT DETECT ANYTHING. ODOR SEEMED TO BE ELECTRICAL IN NATURE. INSPECTED THE AREA FOR OBVIOUS ELECTRICAL PROBLEMS, FOUNJun 11, 2017 · N832UA · Airbus A319131 · Electrical Power SystemSDR CALA2016121901124Pcu · faultedCABIN EMERGENCY LIGHT TEST FAILS. MESSAGE IS AFT L PSCU IS AT FAULT. REPLACED EMERGENCY POWER CONTROL UNIT IAW 33-51-39.Dec 19, 2016 · N832UA · Airbus A319131 · Emergency LightingSDR CALA2016081295639Connector · unsecureEMERGENCY LIGHT POWER SUPPLY WARNING LIGHT APPEARED DURING CIDS TEST. SECURED CONNECTOR AT THE POWER SUPPLY, OPS CHECKED GOOD.Aug 9, 2016 · N832UA · Airbus A319131 · Light System WiringSDR CALA2013122793995Battery · faultedIAW NR 2 SVC ITEM R EMERGENCY LIGHT TEST FAULTS BATTERY EMERGENCY LIGHT 33-51-38. RESET LT EMERGENCY BATTERY AMM 24-50-00.Dec 27, 2013 · N832UA · Airbus A319131 · Emergency LightingSDR CALA2013121693714Nut · damagedFASTENER ABOVE LT WING ESCAPE SLIDE PANEL ONE OUT. REPLACED CAPTION NUT & FASTENER.Dec 13, 2013 · N832UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2013111492937Liner · damagedENG 1 INLET LINER HAS APPROXIMATELY 1-2 IN HANGING DOWN LOOSE AT 12 O'CLOCK POSITION.Nov 13, 2013 · N832UA · Airbus A319131 · Turbine Engine Air Inlet SectionSDR CALA2013081990543Sdac · unknownGREEN & YELLOW SYS LOW PRESSURE DISPLAYED ON UPPER ECAM SCREEN. REPLACED SDAC 1 IAW AMM, ALL INDICATIONS NORMAL.Aug 18, 2013 · N832UA · Airbus A319131 · Hydraulic Indicating SystemSDR UALA2013052303580Switch · looseCAPTAIN`S MICROPHONE TRIGGER ON SIDE STICK IS LOOSE. REPLACED IAW AMM AND ACCOMPLISHED OP TEST OF SIDE STICK ASSY, OPS NORMAL.May 22, 2013 · N832UA · Airbus A319131 · Audio Integrating SystemSDR UALA2013050203081Floor Panel · delaminatedAFT CARGO PIT FLOOR PANEL 151ZG IS DELAMINATED 24 INCH BY 22 INCH, 7.5 INCH FROM FWD EDGE AND 4 INCH FROM DOOR EDGE. IPC REF 53-42-04-22X ITEM 90, P/N BF530014-103. SRM REF 53-02-00 PG 120. REMOVED AFT CARGO PIT FLOOR PANEL IAW IPC 53-42-04-22X FLOOR PNL 110May 1, 2013 · N832UA · Airbus A319131 · Fuselage Floor PanelSDR UALA2013042602935Oxygen Mask · brokenFIRST OFFICER`S OXYGEN MASK BROKEN. REPLACED OXYGEN MASK PER MM, OPS CHECKED OKAY.Apr 26, 2013 · N832UA · Airbus A319131 · Crew Oxygen SystemSDR UALA2013042202773Position Sensor · out of adjustREF LOG 3 AUTO PILOT TRIMS A-C 2 UNITS LEFT RUDDER AND RIGHT 3 DEGREES BANK. -PER TSM 27-20-00-810-804- A ITEM 4A(1) ACP ADJ OF RUDDER POSITION INDICATING TO ITEM 4A 2 (A). CONTINUE WITH ITEM 4A2(C). ACP'D AFS TEST, AMM TASK 22-96-00 -710-001-A & EFCS-1, EApr 21, 2013 · N832UA · Airbus A319131 · Rudder Control SystemSDR UALA2013042202774Servo · faultedDURING FLIGHT CONTROL CHECK, RIGHT AILERON DOES NOT SHOW FULL DOWN TRAVEL INICATOR DOES NOT ENTER. REPLACED SERVO 33CE2 RIGHT GREEN SERVO ACTUATOR PER AMM. RIGGED AND OPS & LEAK CHECKED GOOD.Apr 19, 2013 · N832UA · Airbus A319131 · Aileron Control SystemSDR UALA2013041502580Panel · damagedNR 2 ENGINE OUTBOARD PYLON PANEL 482AR HAS WRINKLING DISTORTION ON THE LOWER EDGE BETWEEN THE FIRST TWO FASTENERS AND 1.5 INCHES AFT OF THE LEADING EDGE. REPLACED NR 2 OTBD PYLON PANEL UNDER WING LEADING EDGE.Apr 14, 2013 · N832UA · Airbus A319131 · Nacelle/Pylon, Plate/Skin
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