# Service difficulty reports: N498UA

A list on [N498UA](https://openairdocs.org/aircraft/N498UA.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 85 reports

- [SDR CALA2026010212579](https://openairdocs.org/sdr/CALA2026010212579.md): Battery · faulted · Dec 31, 2025 · N498UA · Airbus A320232 · Emergency Lighting
  > DURING CABIN EMERG LIGHT TEST MESSAGE, EPSU BATTERY EMER RT, DISPLAYED ON CIDS SCREEN. PERFORMED BATTERY TEST AT BATTERY REF MM 33-51-00. CONFIRMED BATTERY FAULT. REMOVED EPSU BATTERY AT RT EMERGENCY EXIT ROW REF MM 33-51-38. NEW BATTERY ORDERED, COMING FROM O
- [SDR CALA2025122412421](https://openairdocs.org/sdr/CALA2025122412421.md): Selector Valve · faulted · Dec 21, 2025 · N498UA · Airbus A320232 · Landing Gear Retraction/Extension System
  > MAIN GEAR NOT DOWNLOCKED FOR FERRY, UNLOCKING COMPLETED AMM 32-30-00-867-001-A UP TO AND INCLUDING STEP 3.C. IAW AMM GROUND POWER CART HYD IS REQUIRED TO COMPLETE GEAR SWING. REF TSM 32-31-00-810-808-A, PERFORMED A FUNCTIONAL CHECK OF THE MLG. GEAR DOORS OP
- [SDR CALA2025112511449](https://openairdocs.org/sdr/CALA2025112511449.md): Power Supply · faulted · Nov 23, 2025 · N498UA · Airbus A320232 · Emergency Lighting
  > EPSU INT LOAD FWD LEFT MSG WHILE RUNNING OPS CHECK OF EPSUS REF AMM 33-51-00-710-001-A. R&R FWD EPSU (10WL) REF AMM 33-51-38-000-001-A. RE-ACCOMPLISHED OPS CHECK OF EPSUS BY BITE-CHECK REF AMM 33-51-00-710-001-A AND OPS CHECK PASSED AT THIS TIME. SEE PICS. OK
- [SDR CALA2024123101730](https://openairdocs.org/sdr/CALA2024123101730.md): Duct · leaking · Dec 28, 2024 · N498UA · Airbus A320232 · Airfoil Anti/De-ice System
  > ECAM AIR R WING LEAK LOCKED FOR DISCUSSING WITH TOMC CONTROLLER CORRECTIVE ACTION. ITEM LOCKED TO CONFIRM FIX. CHECKED BMC2 HAD PREVIOUS FLT LEAK DETECTION LOOP B RIGHT WING AND R WING LEAK FAULT ECAM FAULT. T/S PER TSM HAD NO FAULTS WITH LOOP WIRING CHECKS ME
- [SDR CALA2024122401640](https://openairdocs.org/sdr/CALA2024122401640.md): Computer · faulty · Dec 22, 2024 · N498UA · Airbus A320232 · Engine Anti-Icing System
  > AIR ENG 2 BLEED LEAK POST FLIGHT LAST LEG REPORT BMC BITE CHECK RESULTS AT GATE. CREW DEBRIEF: CREW GOT AIRBLEED ECAM AND AIR R WING LEAK ECAM AN D FOLLOWED THEIR CHECKLIST. NO APU BLEED WAS BEING USED. THEY TU RNED OF THE CROSS BLEED VALVE AND RIGHT ENGINE BL
- [SDR CALA2024120601417](https://openairdocs.org/sdr/CALA2024120601417.md): Fuel Cap · missing · Dec 3, 2024 · N498UA · Airbus A320232 · Fuel Storage
  > PDA 2 REF LOG 3083416, FUEL CAP DEPARTED AIRCRAFT. FUEL CAP MISSING. REPLACED MISSING FUEL CAP PER AMM 28-11-43-400-001A.
- [SDR CALA2024112202922](https://openairdocs.org/sdr/CALA2024112202922.md): Relay · faulted · Nov 20, 2024 · N498UA · Airbus A320232 · Landing Gear System
  > LDG GEAR DID NOT COME DN FOLLOWED ECAM AND MANUALLY EXTENDED GEA R TOWED TO GATE NW STR OF NOSE WHEEL STEERING REF AMM 32-51-00-720-004.MOMENTARILLY HA D NWS MESSAGE ON UPPER ECAM BEFORE RESETTING LGCIU.LGCIU AND BSC U TEST OK EXCEPT BSCU CH1 FAULT 6GC.REF TSM
- [SDR CALA2024080802178](https://openairdocs.org/sdr/CALA2024080802178.md): Angle · cracked · Aug 4, 2024 · N498UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > RH AFT TI-ANGLE CRACKED REPAIR PER EA 5331-01718 OF 08 BEFORE NEXT FLIGHT. REMOVED AND REPLACED RH AFT TI-ANGLE AS DIRECTED BY EA 5331-0171 8 AND IAW A320 SRM 51-42-11-001.
- [SDR CALA2024073102145](https://openairdocs.org/sdr/CALA2024073102145.md): Angle · cracked · Jul 30, 2024 · N498UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > L/H FWD TI-ANGLE CRACKED ON HAECO LCQ NR 92 90110/32110 REMOVED AND REPLACED 1EA TI-ANGLE CA L/H FWD KEELBEEM IAW A320 E A 5331-0718 OPS 05 AND A320 SRM 51-42-11/001.
- [SDR CALA2024051701490](https://openairdocs.org/sdr/CALA2024051701490.md): Fuel Cap · missing · May 16, 2024 · N498UA · Airbus A320232 · Fuel Storage
  > PDA 2 FUEL CAP REPORTED MISSING PLACED ON CDL REF LP 7974881 SDR REPORT # 1036203 CREATED. FUEL CAP REPORTED MISSING COMPLIED WITH MEL 28A. REQUESTING MEL VERIFIED COUPLING SEAL INTEGRITY. NO LEAKING. / MISSING FUEL CAP, REQ CDL 28A.
- [SDR CALA2024051601486](https://openairdocs.org/sdr/CALA2024051601486.md): Fuel Cap · unknown · May 15, 2024 · N498UA · Airbus A320232 · Fuel Storage
  > FUEL CAP REPORTED MISSING MISSING FUEL CAP, REQ CDL 28A FUEL CAP PLACED ON CDL 28A. COMPLIED WITH MEL 28A. REQUESTING MEL VERIFIED COUPLING SEAL INTEGRITY. NO LEAKING.
- [SDR CALA2024022800594](https://openairdocs.org/sdr/CALA2024022800594.md): Actuator · faulted · Feb 25, 2024 · N498UA · Airbus A320232 · Leading Edge Slat Actuator
  > SLAT SYS FAULT. WARNINGS & CORRELATED FAULTS F/CTL SLATS FAULT 27-00 06 19:39:00 SLT 1 SYSTEM JAMCHECK SLT MECH DRIVE 27-80-00 SFCC 1 06 19:39:00 SLT 2 SYSTEM JAMCHECK SLT MECH DRIVE 27-80-00 SFCC 2 06 19:40:00. IN REF TO TSM 27-81-00-810-810-A. INSECTED TO
- [SDR CALA2023102303139](https://openairdocs.org/sdr/CALA2023102303139.md): Battery Pack · failed · Oct 20, 2023 · N498UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS NOT ILLUMINATING IN AFT SECTION OF ACFT GE N BY V907039 ON HAECO LCQ NR 9296010/34010 REMOVED AND REPLACED EPSU BATTERY 13WL IAW A320 AMM 33-51-38-000 -002-A AND 33-51-38-400-002-A. OPS CHECK GOOD IAW A320 AMM 33-51 -00-710-001-A
- [SDR CALA2023040301014](https://openairdocs.org/sdr/CALA2023040301014.md): Fuel Cap · missing · Apr 3, 2023 · N498UA · Airbus A320232 · Aircraft Fuel System
  > FUEL CAP MISSING. PDA REPORT. PN 457-825. IPC 28-11-05-25, CAT 3 COMPLIED WITH PDA REPORT GENERATION
- [SDR CALA2022112803239](https://openairdocs.org/sdr/CALA2022112803239.md): Cap · missing · Nov 28, 2022 · N498UA · Airbus A320232 · Main Landing Gear Attach Section
  > PDA 3 FOUND ON WALK AROUND: RIGHT MAIN LANDING GEAR DAMPER IS MISSING DUST CAP. INSTALLED NEW DUST CAP AT MLG DAMPER PARTS USED: 18-3211-3-0037,QTY:1
- [SDR CALA2022112803238](https://openairdocs.org/sdr/CALA2022112803238.md): Cap · missing · Nov 28, 2022 · N498UA · Airbus A320232 · Main Landing Gear Attach Section
  > PDA 3 FOUND ON WALK AROUND: LEFT MAIN LANDING GEAR DAMPER IS MISSING DUST CAP. INSTALLED NEW DUST CAP AT MLG DAMPER.PARTS USED: 18-3211-3-0037,QTY:1
- [SDR CALA2022022800521](https://openairdocs.org/sdr/CALA2022022800521.md): Vent · faulted · Feb 28, 2022 · N498UA · Airbus A320232 · Air Conditioning System
  > *EMERGENCY DECLARED* VENT AVIONICS SYS FAULT PLACING ON MEL 2126AD. ALL DDP COMPLIED WITH. PLACED ON MEL 2126C. DDP COMPLIED WITH. OPS CHECK NORMAL. 2126C APPROVED. LEG REPORT OF AEVC AND READ ALL CLASS 3 FAULTS OF AEVC. RECORD THROUGH THE APPLICABLE TSM AS TI
- [SDR CALA2022022100466](https://openairdocs.org/sdr/CALA2022022100466.md): Control Rod · stiff · Feb 21, 2022 · N498UA · Airbus A320232 · Nose/Tail Landing Gear Strut/Axle
  > *EMERGENCY ON APPROACH* NOSE LG CONT SOUNDS TO CYCLE UP MAKING A LOUD THUMP FOUND RIGHT NOSE GEAR DOOR ADJUSTABLE ROD ASSY VERY STIFF REF REPLACE LT NOSE GEAR DOOR ROD ASSY AS PRECAUTION REF IPC IPC 32-31-01-12 ITEM 50 32-31-01-12 ITEM 50 LH & RH NLG DOOR RODS
- [SDR CALA2022021800428](https://openairdocs.org/sdr/CALA2022021800428.md): Landing Gear · noise · Feb 17, 2022 · N498UA · Airbus A320232 · Landing Gear Door Retract Section
  > NOISE AND SHAKING AFTERGEAR UP/ 250KTSNOISE WAS INTERMITTENT OCURRING AS PER L/P 8006234, PERFORMED FUNCTIONAL TEST OF NOSE LANDING EXTENSION ANDRETRACTION PER AMM 32-31-00-720-003-A ALL CHECKS NORMAL.SUSPECT NLG SHOCK STRUT SEVICEING.PERFORMED NLG SHOCK ABSO
- [SDR CALA2018032300988](https://openairdocs.org/sdr/CALA2018032300988.md): Stringer · corroded · Mar 23, 2018 · N498UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > STRINGER 31R, FRAME 65 BELOW THE OUTFLOW VALVE CORROSION ON THE STRINGER AND FRAME. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE STRINGER IAW A320 AMM 51-42-11 SDR, UAL CIR BY MECH V919086 INSP BY LC-126
- [SDR CALA2018032300987](https://openairdocs.org/sdr/CALA2018032300987.md): Door Sill · corroded · Mar 23, 2018 · N498UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL HAD TWO AREAS OF CORROSION AT FRAME 68. REPAIRED IAW SRM 53-41-14-300-001.
- [SDR CALA2018032200972](https://openairdocs.org/sdr/CALA2018032200972.md): Stringer · corroded · Mar 21, 2018 · N498UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT FR55-5 6 STRINGER 41L & SPLICE ARE CORRODED. INSTALLED REPAIR FR 53TO FR56+7 IAW SRM 53-00-13-300-001.
- [SDR CALA2018032200971](https://openairdocs.org/sdr/CALA2018032200971.md): Stringer · corroded · Mar 21, 2018 · N498UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO, STRINGER 43L, FRAMES 64 TO 70 CORRODED. INSTALLED A REPAIR IAW SRM 53-00-1 3-300-001.
- [SDR CALA2018032200970](https://openairdocs.org/sdr/CALA2018032200970.md): Stringer · corroded · Mar 21, 2018 · N498UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BAY, STRINGER 43L, FRAME 56 TO 58 CORRODED. INSTALLED A REPAIR IAW SRM 53-00-13-3 00-001.
- [SDR CALA2018031900932](https://openairdocs.org/sdr/CALA2018031900932.md): Shear Tie · gouged · Mar 18, 2018 · N498UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FRAME TO STR CLEAT AT FRAMES 62 FROM STRINGERS 40L-41L GOUGED ON VERTICAL UPPER EDGE. REMOVED AND REPLACED THE CLEAT IAW SRM 51-42 -11-001, PARA 2.
- [SDR CALA2018031900935](https://openairdocs.org/sdr/CALA2018031900935.md): Stringer · corroded · Mar 18, 2018 · N498UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO STRINGER 43L CORRODED AT FRAME 63. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-11-001, PARA 2.
- [SDR CALA2018031900934](https://openairdocs.org/sdr/CALA2018031900934.md): Stringer · corroded · Mar 18, 2018 · N498UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO STRINGER 41L, FRAMES 63 TO 64 CORRODED. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-11-001, PARA 2.
- [SDR CALA2018031900933](https://openairdocs.org/sdr/CALA2018031900933.md): Stringer · corroded · Mar 18, 2018 · N498UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO STRINGER 42L, FRAMES 60 TO 64 HAS CORRODED AFT OF FRAME 63. REMOVED AND REPLACED THE STRINGER BETWEEN FRAMES 60-64 IAW SRM 51-42-11-001, PARA 2.
- [SDR CALA2017111704129](https://openairdocs.org/sdr/CALA2017111704129.md): Battery · faulted · Nov 17, 2017 · N498UA · Airbus A320232 · Emergency Lighting
  > DURING AN EMERGENCY LIGHTS TEST, HAD AN EPSU BATTERY MESSAGE. REPLACED THE BATTERY PACK IAW MM 33-51-38. OPS CHECKED GOOD.
- [SDR CALA2017031700619](https://openairdocs.org/sdr/CALA2017031700619.md): Altimeter · faulty · Mar 17, 2017 · N498UA · Airbus A320232 · Altimeter, Barometric/Encoder
  > STANDBY ALTIMETER INDICATION ERRONEOUS, SHOWS 300 FEET HIGH AT FL350, DISPLAYS 35300 WITH STD SET. REMOVED AND REPLACED THE STANDBY ALTIMETER IAW MM 34-21-22-00-001A
- [SDR CALA2016081195629](https://openairdocs.org/sdr/CALA2016081195629.md): Light · malfunctioned · Jun 4, 2016 · N498UA · Airbus A320232 · Emergency Lighting
  > DURING TAXI, EMERGENCY CALL LIGHTS AND CHIMES WENT OFF THREE TIMES. UNABLE TO DUPLICATE FAULT, RESET CIDS AS PRECAUTION
- [SDR CALA2016032895234](https://openairdocs.org/sdr/CALA2016032895234.md): Power Supply · faulted · Mar 24, 2016 · N498UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY POWER SUPPLY UNIT AFT LT, FAULT MSG WHEN PERFORMING EMER LIGHTS TEST. REPLACED EMER POWER SUPPLY UNIT 13WL AFT LT IAW AMM 33-51-38. UNIT FAILED BITE.
- [SDR CALA2014120592795](https://openairdocs.org/sdr/CALA2014120592795.md): Skin · damaged · Dec 3, 2014 · N498UA · Airbus A320232 · Wing, Plate/Skin
  > MAJOR REPAIR & SDR. LT WING FUEL TANK ACCESS DOOR CUT OUT 540MB HAS 1 EACH ELONGATED HOLE. REPAIRED HOLE B IAW SRM 57-27-11 & SRM 57-21-11 PAGES 210 - 220 PARA 5B.
- [SDR CALA2014120592794](https://openairdocs.org/sdr/CALA2014120592794.md): Skin · damaged · Dec 3, 2014 · N498UA · Airbus A320232 · Wing, Plate/Skin
  > MAJOR REPAIR & SDR. RT WING FUEL TANK PLATE 640JB LANDING HAS 1 EACH OUT OF ROUND FASTENER HOLE. REPAIRED HOLE IAW SRM 57-27-11 & SRM 57-21-11 PARA 5B.
- [SDR CALA2014120292761](https://openairdocs.org/sdr/CALA2014120292761.md): Skin · damaged · Nov 30, 2014 · N498UA · Airbus A320232 · Wing, Plate/Skin
  > LEFT WING FUEL TANK ACCESS DOOR CUT OUT 540 LB HAS 5 OVERSIZED HOLES. REWORKED HOLES P, Q & R IAW SRM 57-21-11 PARA B & THE OTHER TWO HOLES L & K WORK IAW ECRA 5720-02620. ALL HOLES REAMED & HFEC ROTARY SCANNED IAW NTM 51-10-01 & NO DEFECT NOTED. COLD WORKE
- [SDR CALA2014112892746](https://openairdocs.org/sdr/CALA2014112892746.md): Skin Panel · damaged · Nov 17, 2014 · N498UA · Airbus A320232 · Elevator, Plate/Skin
  > LEFT ELEVATOR UPPER SKIN PANEL HAS WATER INGRESS INDICATION AT 11.5 INCHES FROM INBD END, 5.0 INCHES FROM TE, 3.5 INCHES IN DIAMETER & AT 28 INCHES FROM INBD END 8 INCHES FROM TE & 3 INCHES IN DIAMETER. CUT OUT TRAPPER WATER INDICATION IN BOTH AREAS APPLIED R
- [SDR CALA2014112492738](https://openairdocs.org/sdr/CALA2014112492738.md): Skin Panel · damaged · Nov 17, 2014 · N498UA · Airbus A320232 · Elevator, Plate/Skin
  > LEFT ELEVATOR UPPER SKIN PANEL HAS WATER INGRESS INDICATION AT 11.5 INCHES FROM INBD END, 5.0 INCHES FROM TE, 3.5 INCHES IN DIAMETER & AT 28 INCHES FROM INBD END, 8 INCHES FROM TE, 3 INCHES IN DIAMETER. CUT OUT TRAPPED WATER INDICATION IN BOTH AREAS APPLIED R
- [SDR CALA2014112492734](https://openairdocs.org/sdr/CALA2014112492734.md): Door Sill · corroded · Nov 17, 2014 · N498UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > R2 LOWER DOOR SILL CORRODED BEYOND LIMITS IAW SRM 5 3-41-14. REMOVED DOOR SILL & INSTALLED NEW DOOR SILL IAW SRM 51-42-11.
- [SDR CALA2014112492732](https://openairdocs.org/sdr/CALA2014112492732.md): Stringer · corroded · Nov 17, 2014 · N498UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT AT FRAME 56, STRINGER 4L CORRODED. SPLICED IN NEW STRINGER SECTION IAW SRM 53-00-13 FIG 201.
- [SDR CALA2013122693931](https://openairdocs.org/sdr/CALA2013122693931.md): Ignition Unit · faulty · Dec 24, 2013 · N498UA · Airbus A320232 · APU Start/Ignition System
  > ECAM MESSAGE APU AUTO SHUTDOWN DISPLAYED ON UPPER ECAM SCREEN. AUTO SHUTDOWN TWICE. R & R APU IGNITION UNIT, OPERATIONS CHECKED GOOD.
- [SDR CALA2013110192554](https://openairdocs.org/sdr/CALA2013110192554.md): Transceiver · faulty · Oct 31, 2013 · N498UA · Airbus A320232 · Weather Radar System
  > IAW LOG 1, TROUBLESHOOT WX RADAR TILT PROBLEM. PERFORMED ANTENNA CONTROL TEST IAW AMM 34.41.00.730.001.A & DURING THE TEST THE ANTENNA DID NOT TURN IN ELEVATION (+10, -10) PAGE 8 OF 10. REPLACED WX TRANSCEIVER, ON MR43123-1054, OFF 1128. WX CONTROL PANEL ON
- [SDR CALA2013102992475](https://openairdocs.org/sdr/CALA2013102992475.md): Seal · torn · Oct 27, 2013 · N498UA · Airbus A320232 · Ailerons
  > LT AILERON INBD UPPER & LOWER EDGE TO WING SEAL TORN. NEED PCN 110-2815 INBD & 110-2816 OTBD RJF. AILERON INBD UPPER & LOWER SEALS REMOVED. REPLACED UPPER & LOWER INBD AILERON SEAL ON LT AILERON. OKAYED FOR SERVICE.
- [SDR CALA2013102892402](https://openairdocs.org/sdr/CALA2013102892402.md): Fastener · missing · Oct 23, 2013 · N498UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > THREE MISSING FASTENERS ON PANEL LT FUSELAGE JUST 3FT AFT OF LT WING TE. REPLACED MISSING FASTENERS.
- [SDR CALA2013092591430](https://openairdocs.org/sdr/CALA2013092591430.md): Fdu · faulty · Sep 24, 2013 · N498UA · Airbus A320232 · Fire Detection
  > ENGINE 1 FIRE TEST NO RED LIGHT OR BELL. REPLACED FDU IAW MM. ACP, APU, FDU BITE & FIRE TEST, CHECKED OKAY.
- [SDR CALA2013073090075](https://openairdocs.org/sdr/CALA2013073090075.md): Transceiver · faulty · Jul 29, 2013 · N498UA · Airbus A320232 · Weather Radar System
  > RADAR ERRATIC & UNRELIABLE, SHOWS DIFFERENT ECHOES WITH EACH SWEEP, FALSE ECHOES. REPLACED WEATHER TRANSCEIVER IAW AMM.
- [SDR CALA2013080290110](https://openairdocs.org/sdr/CALA2013080290110.md): Engine · overheated · Jul 28, 2013 · N498UA · Airbus A320232 · Engine (Turbine/Turboprop)
  > ECAM ENG 2 EGT OVER LIMIT DURING APPROACH ABOUT 1500 FT.
- [SDR CALA2013072990041](https://openairdocs.org/sdr/CALA2013072990041.md): Indicator · leaking · Jul 26, 2013 · N498UA · Airbus A320232 · Fuel Quantity Indicator
  > DRIPLESS STICK L5 LEAKS WHEN EXTENDED. TO REPLACE ROD 482-0114 PULL ALL THE WAY OUT, SLIDE IN NEW ROD IAW AMM 28-43-22. VERIFIED NO LEAKS WHEN STOWED. DEFERRED IAW MEL, INSTALLED DEFERRED STICKER ADJ TO LOWER ECAM.
- [SDR UALA2013070804735](https://openairdocs.org/sdr/UALA2013070804735.md): Connector · leaking · Jul 6, 2013 · N498UA · Airbus A320232 · Hydraulic System, Main
  > NR 4 BRAKE LEAKING HYDRAULIC FLUID AT LINE CONNECTOR. SECURED NR 4 MLG BRAKE QUICK DISCONNECT FITTING AND RESAFTIED, NO LEAKS NOTED WITH BRAKES AND HYD PRESSURE ON.
- [SDR UALA2013053003785](https://openairdocs.org/sdr/UALA2013053003785.md): Amu · failed · May 27, 2013 · N498UA · Airbus A320232 · Audio Integrating System
  > F/O O2 MASK AUDIO DOES NOT TEST CORRECTLY. R & R AMU IAW AMM. PERFORMED BITE TEST IAW MM, OPS CHECKED GOOD, OK TO CONTINUE.
- [SDR UALA2013050703175](https://openairdocs.org/sdr/UALA2013050703175.md): Panel · dislodged · May 4, 2013 · N498UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > CEILING PANEL FELL DOWN SEAT POSITION 37 DEF. SECURED PANEL IAW ECRA 2523-01105 FOR 2D.

Next page: https://openairdocs.org/aircraft/N498UA/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'N498UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N498UA/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.