N492UA

Service difficulty reports · 75

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 = 'N492UA' 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 CALA2025102210406Door · leakingEMERGENCY EXIT DOOR BY SEAT 21F HAS HIGH PITCH SQUEAL ABOVE FL25 0. CAB ALT/VS NORMAL. APPLIED SPEED TAPE TO WTB SEALS 192DT IAW MT 53-004, TAPE RECHECK DAILY, REPLACE SEALS WITHIN 1000 FH, REQUEST CREW COMMENT TO DETERMINE IF VIBRATION ELIMINATED. OK TO DIP TOct 22, 2025 · N492UA · Airbus A320232 · Emergency ExitsSDR CALA2025090508495Cids · faultedEMER EXIT SIGN ON OVER WING AND OVER MCD STAYS ILLUMINATED ALL OTHER LTS REMAIN EXTIGUISHED TURNED OFF EMEGENCY LIGHT SWITCH AND PERFORMED FULL CIDS SYSTEM RESET. EMERGENCY LIGHTS EXTINGUISHED. CYCLED SWITCH IN ALL POSITIONS 3 TIMES. ALL EMERGENCY LIGHTS NOW OSep 4, 2025 · N492UA · Airbus A320232 · Lighting SystemSDR CALA2025090308428Plug · deterioratedLEFT MLG DOOR AFT PROX SENSOR SWITCH (35GA)HAS DETERIORATED PLUG RUBBER. REPLACED LT MLG AFT PROX SENSOR SWITCH (35GA) AND ADJUSTED GAP REF AMM 32-12-11-820-059-A UP TO STEP 3K(G). . MLG DOOR OPERATIONAL CHECK WILL BE ACCOMPLISHED ON LOG ITEM 606683.Aug 31, 2025 · N492UA · Airbus A320232 · Landing Gear Position and WarningSDR CALA2025081107573Battery Pack · inoperativeDURING TEST FOUND ERROR MSG "EPSU BATTERY EMER L" ATA 33-51-38 SEE PIC REMOVED AND REPLACED LEFT OVERWING EMERGECNY EXIT LIGHT POWER SUPPLY BATTERY REF AMM 33-51-38/401. OPS CHECK GOOD, BITE TEST PASSES WITH A GREEN SYS OK LIGHT AND NO FAULTS.Aug 9, 2025 · N492UA · Airbus A320232 · Emergency LightingSDR CALA2025081107572Battery Pack · inoperativeWHILE PERFORMING BITE OF EPSU SYSTEM REF AMM 33-51-00-710-001-A RECIEVED AN EPSU BATTERY AFT L MESSAGE REMOVED AND REPLACED THE AFT LEFT EPSU BATTERY REF AMM 33-51-38/401. OPS CHECK GOOD, FAULT IS NO LONGER PRESENT AND THE BITE TEST PASSES.Aug 9, 2025 · N492UA · Airbus A320232 · Emergency LightingSDR CALA2025060405256Battery · no testEPSU BATT FWD L FAULT MESSAGE ON EMERGENCY LIGHT TEST. REPLACED FWD L EPSU BATTERY REF AMM 33-51-38/401. OPS CHECK GOOD. PARTS USED: 18-3351-3-0001, QTY :1Jun 3, 2025 · N492UA · Airbus A320232 · Emergency LightingSDR CALA2025040903651Proximity Switch · faultedAFT CARGO ECAM INDICATION REF LP 4404361 DEFERRED IAW MEL 5270D NOC DESK: 320 NAME: ATE: 05-APR-25. APPROVED DEFERRED *DM* SEE TSM 52-32-00-810-801-A & ASM 31-54-05 FOR T/S ASSIST. ADDED PROX SWITCHES (32WV, 34WV) IF NEEDED. PARTS UPDATED. REPLACED AFT CARGO SApr 5, 2025 · N492UA · Airbus A320232 · Door Warning SystemSDR CALA2024122701681Battery · inoperativeDURING OPERATIONAL CHECK OF EPSU BATTERIES, MESSAGES "EPSU BATTERY EMER R" AND "EPSU BATTERY AFT L" PRESENT. REMOVED AND REPLACED RIGHT EPSU BATTERY AND AFT LEFT EPSU BATTERY REF 33-51-38. OPS CHECK GOOD, MESSAGES DID NOT RETURN.Dec 25, 2024 · N492UA · Airbus A320232 · Emergency LightingSDR CALA2024091700647Fuel Cap · missingPDA 2 FUEL CAP FOUND MISSING. ITEM PUT ON CDL 28A. REF LP# 9273271.FUEL CAP MISSING.REQUESTING CDL 28A CDL 28A APPLIED DISPATCH DESK: 14 NAME: BB DATE: 16-SEP-24 28A APPROVED.LOCATED MISSING REFUEL COUPLING CAP IN DEN. REINSTALLED REFUEL COUPLING CAP REF IPC Sep 16, 2024 · N492UA · Airbus A320232 · Fuel StorageSDR CALA2024062400087Actuator · faultedREVERSER FAULT DISPLAYED ON UPPER ECAM SCREEN. - ENG 2 ENG 2 REVERSER FAULT ON ARRIVAL ENG NO 2 REV FAULTED BOTH CH A AND CH B ON REV LVDT /HC/EEC2 FIN . IF NEEDED ACTUATOR M&E NUMBER IS 31-7832-9-0002. *DM* AVIATAR CONFIRMS FAULT "REV LVDT CHB / HC / EEC2" REJun 20, 2024 · N492UA · Airbus A320232 · Engine Thrust ReverserSDR CALA2024032600867Fuel Cap · missingPDA 2 FUEL CAP MISSING ON ARRIVAL. FUEL CAP MISSING, VERIFIED NO LEAKS. INSTALLED FUEL CAP AND LANYARD IN REF TO AMM 28-25-41-400-005-A. FUEL CAP SECURE.Mar 22, 2024 · N492UA · Airbus A320232 · Fuel StorageSDR CALA2024012300204Accumulator · leakingBLUE SYSTEM LOST HYD FLUID IN FLIGHT BOTTOM OF AIRCRAFT WET WITH HYD FLUID. ACCUMULATOR, HY OFF 31-2912-9-9001 7440 ON 0000 ACCUMULATOR, HY OFF 31-2912-9-9001 7440 ON 31-2912-9-9001 7098 REPLACED BLUE SYSTEM ACCUMULATOR REF 29-12-00,OP CHECKS GOOD NO LEAKS FOUJan 16, 2024 · N492UA · Airbus A320232 · Hydraulic Power Accumulator, MainSDR CALA2024010500035Accumulator · leakingECAM CAUTION MESSAGE - B RSVR LO LVL MESSAGE INOP - HYD FOUND HYDRAULIC FLUID LEAKING SCHRADER AT TOP OF BLUE SYSTEM ACCUMULATOR. ORDERED ACCUMULATOR , SCHRADER VALVE ,PRESSURE GAUGE , AND O-RINGS.. PLACED PARTS IN GALLEY. LOGPAGE FLAGGED FOR SDR REPORTING ROTJan 3, 2024 · N492UA · Airbus A320232 · Hydraulic Indicating SystemSDR CALA2022102802980Stringer · corrodedAFT CARGO PIT R/H BETWEEN FR63-64 STRINGER 41R HAS CORROSION DOT M026. PER HAECO LCQ NR 9296400/20400 REMOVED AND REPLACED STRINGER 41RT IN AFT CARGO PIT FR 58-64 IAW A320 SRM 51-72-11-911-001Oct 27, 2022 · N492UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2022102702965Fitting · crackedLEFT AND RIGHT CONTINUITY FITTINGS HAVE CRACK INDICATIONS AT AFT EDGE OF HORIZONTAL LEG 15/16 INCHES OTBD OF WINDOW FRAME INBD ED GE (CENTER POST LINE) PER HAECO LCQ N/R 9296249/20249 GEN BY V06 1671 REMOVED AND REPLACED 2EA L/H AND R/H CONTINUITY FITTINGS IAWOct 26, 2022 · N492UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022102402909None · crackedREV B (AD 2022-02-11) L/H FR20 DOOR STOP FITTING #7 UPPER INBD H OLE (H1) FOUND CRACKED AFTER HFEC ROTO INSPECTION. CRACK APPEARS IN INTERCOASTAL LAYER AT APPROXIMATELY 4 O''CLOCK "REPAIR BEFORE NEXT FLIGHT" REMOVED AND REPLACED CRACKED INTERCOASTAL AT FR20 LHOct 21, 2022 · N492UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2022101402799None · corrodedFWD CARGO FRAME 25 STRINGER 41RT-42RT CLEAT HAS CORROSION PER HA ECO LCQ N/R 9296371/20371 GEN BY V052030Oct 13, 2022 · N492UA · Airbus A300* · Standard Practices/StructuresSDR CALA2022101202766Stringer · corrodedAFT CARGO PIT L/H BETWEEN FR58-59 STRINGER 42L HAS CORROSION DOT M015 A3NB-53-4-6179 GENERATED BY V929150 AT HAECO LCQ PER NR 929 6396 (20396) REMOVED AND REPLACED AFT CARGO L/H FR58-59 STRINGER42L PER A320 SRM 51-72-11-911-002 AND SRM 51-42-11/001 PERFORMED BOct 11, 2022 · N492UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2020120901349Skin · damagedUPON ARRIVAL ORD, GOUGE WAS BLENDED, PER SRM 53-11-11-283-001 AND HFEC ACCOMPLISHED PER NTM 51-10-08 WITH NO CRACKS FOUND. ULTRA SOUND WAS ACCOMPLISHED, PER NTM PT4-00-04-02 AND MEASURMENTS ISSUED ON MATRIX. BLEND IS LOCATED APPROXIMATELY 11.5" AFT OF STATIC Dec 7, 2020 · N492UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2020011900157Fitting · corrodedUPON REMOVAL OF R2 DOOR SILL, FOUND FR68 CORNER FITTING CORRODED -SUPPORT TASK. REMOVED AND REPLACED CORNER FITTING AT FR68 AT R2 DOOR SILL IAW SRM 51-72-11-911-001 WORK ACCOMPLISHED, INSPECTED.Jan 15, 2020 · N492UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2020011900159Door Sill · corrodedAFT CABIN R2 DOOR SILL IS CORRODED AT FR68 SUPPORT TASK PER NR 9296179 GENERATED. REMOVED AND REPLACED DOOR SILL AT R2 DOOR IAW SRM 51-72-11- 911-002 WORK ACCOMPLISHED, INSPECTED.Jan 15, 2020 · N492UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2020011300133Shear Plate · corrodedAFT MAIN CABIN R/H SHEER PLATE FR69-70 HAS CORROSION-(SUPPORT TA SK) AT HAECO LCQ REF. NO. 9296137, GENERATED. REMOVED AND REPLACED 1EA CORRODED SHEAR WEB IN THE AFT MAIN CABI N FR 69-70 IAW AIRBUS A320 SRM 51-72-11-911-001 REMOVED DOT G9 W ORK ACCOMPLISHED INJan 12, 2020 · N492UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2020011300130Shear Web · corrodedAFT CABIN SHEAR WEB FR 69-70 IS CORRODED - (SUPPORT TASK), AT HA ECO LCQ REF. NO. 9296176, GENERATED. REMOVED AND REPLACED SHEAR WEB P/N D5347112420200 INSTALL NEW SH EAR AT L/H SIDE FR 69-70 APPLIED TOP COAT AND CIC IAW A320 UAL S RM 51-72-11-911-001 AND 51-2Jan 11, 2020 · N492UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2019032500470Fmu · faultyCREW REPORTS: AFTER A NORMAL FLEX T/O 800 FT IN CLIMB CREW THROTTLED BACK ENG 1 DID NOT RESPOND TO THE THROTTLE MOVEMENT STAYED AT T/O EPR. NEXT A ECAM WARNING TO SHUT DOWN ENGINE APPEARED & CREW ACP A NORMAL SHUT DOWN. THEY ALSO STATED THERE WAS NO VIBRATION,Mar 25, 2019 · N492UA · Airbus A320232 · Fuel Control/Turbine EnginesSDR CALA2018012700357Unknown · odorSMELL OF BURNT TOAST AFT GALLEY REPORTED BY F/A VERIFIED BY CAPT INSPECTED ENTIRE AFT SECTION OF A/C AND FOUND NO OBVIOUS ODOR OF ELECTRICAL SMELL OR SMOKE INSPECTED LAV, COFFEE MAKERS WARMERS, OVENS ECT. ALSO RAN PACKS AND STILL NO OBVIOUS SMELLS NOTED AT THJan 27, 2018 · N492UA · Airbus A320232 · Air Distribution SystemSDR CALA2017092203302Battery · dischargedEMERGENCY LIGHT TEST FAILED AT PTP PANEL. REPLACED BATTERY AT EPSU 12WL NOW OK TEST OK FOR SERVICE REF AMM 33-51-38 PB401.Sep 22, 2017 · N492UA · Airbus A320232 · Emergency LightingSDR CALA2015100594565Apu · malfunctionedPACKS ON WITH APU, CABIN FILLED WITH SMOKE & APU AUTO SHUTDOWN. REPLACED APU IAW AMM 49-11-98-890-001-A.Oct 2, 2015 · N492UA · Airbus A320232 · APU Core EngineSDR CALA2014101392397Spar · mechanic errorNUMBER 2 PYLON LOWER SPAR WEB MIS DRILLED DURING ACCOMPLISHMENT OF SRM 54-51-12. ACCOMPLISHED INSPECTION REQUIREMENTS IAW RDAS, SPAR HAS INTERIM REPAIR ACCOMPLISHED IAW ECRA 5450-02258. REPAIR HAS BEEN APPROVED AS INTERIM FOR 1 MONTH IAW RDAS 80003171-003-20Oct 10, 2014 · N492UA · Airbus A320232 · Nacelle/Pylon, Frame/Spar/RibSDR CALA2014111092671Spar · mechanic errorNUMBER 2 PYLON LOWER SPAR WEB MIS-DRILLED DURING ACCOMPLISHMENT OF SRM 54-51-12. INTERIM REPAIR ACCOMPLISHED IAW ECRA 5450-02258. REPAIR HAS BEEN APPROVED AS INTERIM FOR 1 MONTH IAW RDAS 80003171-003-2014 DATED 9-10-14. A NEW RDAS THAT PROVIDES THE INSPECTSep 15, 2014 · N492UA · Airbus A320232 · Nacelle/Pylon, Frame/Spar/RibSDR CALA2014091892227Spar · mechanic errorNUMBER 2 PYLON LOWER SPAR WEB MIS-DRILLED DURING ACCOMPLISHMENT OF SRM 54-51-12. INTERIM REPAIR ACCOMPLISHED IAW ECRA 5450-02258. REPAIR APPROVED FOR 1 MONTH IAW RDAS 80003171-003-2014 DATED 9-10-14. A NEW RDAS THAT PROVIDES THE INSPECTION & THRESHOLD MUSTSep 13, 2014 · N492UA · Airbus A320232 · Nacelle/Pylon, Frame/Spar/RibSDR CALA2014090992097Skin · damagedLEFT ELEVATOR UPPER SURFACE HAD A 2.0 INCH BY 1.5 INCH AREA OF WATER INGRESS, 30 INCHES FROM THE OTBD END OF THE ELEVATOR & 13 INCHES FWD OF THE TE, ZONE 1. DAMAGE WAS R & R ACP IAW SRM 55-21-11 PARA 5 E FIG 205 CONFIG 1. REPAIR REQUIRES INSPECTION IAW SRI55Sep 6, 2014 · N492UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2014090392057Threshold · corrodedR2 DOOR THRESHOLD BEAM CORRODED AT FRAME 68 IN AFT CABIN. MATERIAL LOSS WAS 100% AT FRAME 68 NUTPLATE. OUT OF LIMITS IAW SRM 53-41-14 FIG 101. FABRICATED REPAIR ANGLE & FILLER & INSTALLED IAW SRM 53- 41-14 FIG 201 & MT.Aug 31, 2014 · N492UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014091892239Stringer · corrodedSTRINGER 41L IS CORRODED BETWEEN FRAME 63 - 64 IN AFT CARGO PIT. REMOVED DAMAGED SECTION. FABRICATED & INSTALLED STRINGER & REPAIR SPLICE IAW SRM 53-00-13 FIG 201. REPAIR REQUIRES SRI INSPECTIONS IAW SRI 53-00-13-2-001-00 TABLE 205. 1ST INSPECTION DUE AT 6Aug 30, 2014 · N492UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2014090392056Stringer · corrodedSTRINGER 41L IS CORRODED BETWEEN FRAME 63 - 64 IN AFT CARGO PIT. REMOVED DAMAGED SECTION. FABRICATED & INSTALLED STRINGER & REPAIR SPLICE IAW SRM 53-00-13 FIG 201. REPAIR REQUIRES SRI INSPECTIONS IAW SRI 53-00-13-2-001-00 TABLE 205. 1ST INSPECTION DUE AT 6Aug 30, 2014 · N492UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2014090392055Stringer · corrodedSTRINGER 42L IS CORRODED BETWEEN FRAME 63 - 64 IN AFT CARGO PIT. REMOVED DAMAGED PART. FABRICATED & INSTALLED NEW STRINGER & REPAIR SPLICE IAW SRM 53-00-13 FIG 201.Aug 30, 2014 · N492UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2014090392054Threshold · corrodedL2 DOOR THRESHOLD BEAM CORRODED AT FRAME 68 IN AFT CABIN. CORROSION AROUND 2 NUTPLATES WAS EXFOLIATED. CUT OUT DAMAGED PART & INSTALLED REPAIR PARTS IAW SRM 53-11-14 PG 203 PARA 5 FIG 201.Aug 30, 2014 · N492UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2013102992494Handset · intermittentINTERPHONE IS INTERMITTENT AT DOOR 1L. CABIN INTERPHONE INTERMITTENT THROUGHOUT CABIN & FROM CABIN TO COCKPIT. REPLACED FWD HANDSET, OPERATIONS CHECKED OKAY.Oct 28, 2013 · N492UA · Airbus A320232 · Interphone/Passenger Announcement (PA) SystemSDR CALA2013102892419Valve · inoperativeRT WING TANK REFUEL VLV INOPERATIVE.Oct 27, 2013 · N492UA · Airbus A320232 · Fuel StorageSDR CALA2013102992460Hydraulic Line · leakingEVIDENCE OF FLUID LEAK FROM VICINITY OF HYD SERVICE PANEL TO TAIL OF AIRCRAFT. BOTH LINES TO BRAKE VLV ON WW CEILING CENTERLINE LEAKING. TIGHTENED BOTH LINES NO LEAKS NOTED.Oct 26, 2013 · N492UA · Airbus A320232 · Hydraulic System, MainSDR CALA2013092791535Microphone · intermittentFIRST OFFICER`S OXYGEN MASK COMMUNICATION IS INTERMITTENT. REPLACED MASK, OPERATIONS OKAY.Sep 27, 2013 · N492UA · Airbus A320232 · Communications SystemSDR CALA2013090991118Selector Valve · leakingOI-HYDRAULIC STREAMING FROM GEAR DOORS TO TAIL, RIGHTSIDE MOSTLY. LEAKING RT WW AFT WALL, AT INBD END OF VALVE NEAR ALLEN BOLTS MATING SURFACE. REPLACED AUTOMATIC SELECTOR 2576GM. PRESSURIZED SYSTEM LEAK CHECKED OK.Sep 8, 2013 · N492UA · Airbus A320232 · Landing Gear SelectorSDR CALA2013082690739Switch · looseFIRST OFFICER`S SIDESTICK COMMUNICATIONS TRIGGER VERY LOOSE. RESECURED FIRST OFFICER`S PUSH TO TALK, OPERATIONS GOOD.Aug 23, 2013 · N492UA · Airbus A320232 · Audio Integrating SystemSDR CALA2013081990506Sensor · dirtyCOCKPIT TEMP CONTROL INOP COCKPIT TEMP AT 84 WITH ALL 3 SELECTORS AT FULL COLD. CLEANED COCKPIT TEMP SENSOR. GROUND AND SYS MCDU TEST OK.Aug 16, 2013 · N492UA · Airbus A320232 · Cabin Temperature Control SystemSDR UALA2013071805036Container · openOXYGEN PANEL OVER SEATS 21 ABC OPEN. SECURED EMERGENCY OXYGEN CONTAINER.Jul 17, 2013 · N492UA · Airbus A320232 · Passenger Oxygen SystemSDR UALA2013061904238Line · leakingRIGHT MLG HYD LEAK. FOUND THE PRESSURE LINE LEAKING JUST ABOVE THE BRAKE SERVO VALVE. REPLACED LINE, LEAK CHECKED GOOD.Jun 19, 2013 · N492UA · Airbus A320232 · Hydraulic System, MainSDR UALA2013032902027Switch · faultyF/O SIDE STICK PTT TRIGGER SENSATIVE TO LATERAL MOVEMENT. INCONSISTENT HOT MICS. REMOVED AND REPLACED F/O'S PTT SWITCH & OPS CHECK AS PER MM, OK FOR SERVICE.Mar 28, 2013 · N492UA · Airbus A320232 · Audio Integrating SystemSDR UALA2012112006701Starter · faultyCREW REPORT: DURING ENGINE 2 START USING APU PNEU DUCT PRESSURE DROPPED BELOW 10PS AND WOULD NOT START. CREW TRIED A CROSSBLEED START WITH THE SAME RESULT DUCT PRESS DROPPED BELOW 10 PSI DURING START ATTEMPT. REPLACED STARTER PER MM, OPS CHECKED GOOD.Nov 19, 2012 · N492UA · Airbus A320232 · Engine StarterSDR UALA2012112006700Igniter · faultyAPU WILL NOT CRANK ON START - APU. STARTED APU, OPS OK. MCDU REPORTS, APU FAULT CONDITION: IGNITION UNIT (8030KM) AND FUEL CONTROL UNIT.(8022KM) NO PARTS SFO. APU SYSTEM SELF TEST FAULTS SPEED SNSR1 (8060KM1) NOT IN STOCK. SPEED SENSOR ATA: 49-71-13 AND IGNov 19, 2012 · N492UA · Airbus A320232 · APU Start/Ignition SystemSDR UALA2012102606151Life Vest · unserviceableNEED 8 TOTAL ADULT LIFE VESTS FOR THE MISSING DATE STICKER ON THE PULL STRAP. SIX ARE IN THE SPARE POUCH AND TWO AT SEATS 27D AND 27E. LIFE VESTS ARE NOT OUT OF DATE. REPLACED ALL 8 LIFE VESTS.Oct 26, 2012 · N492UA · Airbus A320232 · Life JacketSDR UALA2012100905726Engine · leakingNR 1 ENGINE OIL LEAK AT TOWERSHAFT. MAINTENANCE REPORTS OIL LEAK UNDER NR 1 ENG, OPENED FAN COWLS AN DID VISUAL CHECK, APPEARS TO BE COMING FROM ACOC DRAIN PORT ON DRAIN MAST. THERE IS CURRENTLY NO RELIEF FOR LEAKS AT TOWER SHAFT AREA. REFERENCE MT71-017 FOOct 9, 2012 · N492UA · Airbus A320232 · Engine (Turbine/Turboprop)
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