# Service difficulty reports: N497UA

A list on [N497UA](https://openairdocs.org/aircraft/N497UA.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 3 · 107 reports

- [SDR CALA2026021613779](https://openairdocs.org/sdr/CALA2026021613779.md): Lug · broken · Feb 12, 2026 · N497UA · Airbus A320232 · Elevator Structure
  > LEFT ELEVATOR OTBD SERVO HAS A MISSING LOCKING LUG. BROKEN LUG PER AAR LCQ N/R 9294030/38030 GEN BY V923643 ESFR COMPLETED REPAIRED L/H ELEVATOR O/B SERVO LOCKING LUG IAW SRM 55-26- 47-300-001-A. PERFORMED OPS CHECKED GOOD IAW 27-34-00-710-001-A.
- [SDR CALA2026020913632](https://openairdocs.org/sdr/CALA2026020913632.md): Hinge Fitting · gouged · Feb 5, 2026 · N497UA · Airbus A320232 · Nacelle/Pylon, Main Frame
  > NR 2 ENG OTBD FAN COWL NR 3 HINGE HAS GOUGE FWD SIDE OF FITTING FROM CONTACT WITH ANTI ICE DUCT V-BAND CLAMP IAW AAR LCQ NR 9294106/3 8106. REMOVED GOUGES ON NR 2 ENG OTBD FAN COWL NR 3 HINGE FITTING FWD SIDE IAW SRM 54-02-00 REPAIR 012 TO A SMOOTH CONTOUR FI
- [SDR CALA2026022013949](https://openairdocs.org/sdr/CALA2026022013949.md): Skin · dented · Feb 3, 2026 · N497UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > EXTERIOR FUSELAGE SKIN DENTED BETWEEN FR 27-28, S37-38L. EVALUATED DENT AT FR 27-28, S37L-38L IAW SRM 53-21-11-283 -020, FIG 2, SHEET 1 & 2. DENT IS TYPE 1 AS D/A IS LESS THAN 0.1 00IN. PERFORMED DVI WITH NO CRACKS OR DISCREPANCIES IAW NTM 51-9 0-00-007-A.
- [SDR CALA2025091108754](https://openairdocs.org/sdr/CALA2025091108754.md): Control Panel · malfunctioned · Sep 8, 2025 · N497UA · Airbus A320232 · Passenger Compartment Lighting
  > LIGHT ON PANEL 2L INOPERATIVE, CONFIRMED LT CONTROL PANEL AT L2 DOOR WOULD NOT COMMAND THE AFT ENTRY LIGHTS ON. RESET CONTROL PANEL. AFT ENTRY LTS NOW COMMAND NORMAL. IAW AMM 33-21-00-710-801
- [SDR CALA2025040703591](https://openairdocs.org/sdr/CALA2025040703591.md): Fuel Cap · missing · Apr 6, 2025 · N497UA · Airbus A320232 · Fuel Storage
  > FUEL CAP MISSING RT WING COMPLIED WITH CDL TERMS NO LEAKAGE NOTED. APPROVED COMPLIED WITH CDL TERMS NO LEAKAGE NOTED PART NIS ORD. NEED PART NUMBER 0727540 REPLACED MISSING FUEL CAP REF AMM 28-25-41.
- [SDR CALA2025021400355](https://openairdocs.org/sdr/CALA2025021400355.md): Seat Track · corroded · Feb 13, 2025 · N497UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > RH SEAT TRACK FWD INB AT FR 20 REQUIRES REPLACEMENT DUE TO CORROSION. REF STS NR W003716 N0074: REMOVED AND REPLACED SEAT TRACK Y-765 FWD INB AT FR 24 TO FR 12 IAW A320 SRM 51-72-11-911-001. SEE SFR 1038399
- [SDR CALA2024121001466](https://openairdocs.org/sdr/CALA2024121001466.md): Battery Pack · no test · Dec 9, 2024 · N497UA · Airbus A320232 · Emergency Lighting
  > EPSU BATTERY EMERGENCY L FAILED EMERGENCY TEST REMOVED AND REPLACED EPSU BATTERY L, REF AMM 33-51-38-000-002-A & 33-51-38-400-002-A OPS CHECK NORMAL OK TO CONTINUE.PARTS USED: 18-3351-3-0001, QTY:1
- [SDR CALA2024032800898](https://openairdocs.org/sdr/CALA2024032800898.md): Panel · broken · Mar 27, 2024 · N497UA · Airbus A320232 · Wing, Plate/Skin
  > WHISTLING NOISE REPORTED20A. PRESSURIZATION ANDOTHER INDICATIONS ALLNORMAL. PIC ADDED PANEL 191DT PANEL FASTENED AND TAPED. PICS ADDED APPROVED ACP INTERM REPAIR PER PART 1 OF ECRA 5330-07206. ACP PERMANENT REPAIR PER PART 3 WITHIN 1 FLT CYCLE. CARRY APPROVED
- [SDR CALA2024031500742](https://openairdocs.org/sdr/CALA2024031500742.md): Cable · broken · Feb 22, 2024 · N497UA · Airbus A320232 · Escape Slide
  > UPON REMOVAL FOR REPLACEMENT FOUND RT O/W SLIDE BOTTLE CABLE BAL L END BROKEN. PERFORMED BY AT HAECO LCQ PER NR 9296158 ( 36158). COMPLETED SDR FORM.
- [SDR CALA2023102703208](https://openairdocs.org/sdr/CALA2023102703208.md): Fuel Cap · missing · Oct 26, 2023 · N497UA · Airbus A320232 · Fuel Storage
  > FUEL CAP MISSING FUEL CAP FOUND MISSING UPON ARRIVAL AT DFW. REQUEST TO PLACE FUEL CAP ON CDL 28A. PLACED FUEL CAP ON CDL 28A. INSTALLED FUEL CAP OPS CK NORMALREF AMM 28-25-41.
- [SDR CALA2021100101746](https://openairdocs.org/sdr/CALA2021100101746.md): Epsu · none · Sep 30, 2021 · N497UA · Airbus A320232 · Lighting System
  > EPSU FAIL OPC EPSU 12WL REPLACED IAW AMM 33-51-38-400-002-A REV.113.
- [SDR CALA2021100101745](https://openairdocs.org/sdr/CALA2021100101745.md): Epsu · none · Sep 30, 2021 · N497UA · Airbus A320232 · Lighting System
  > EPSU FAIL OPC EPSU 11WL REPLACED IAW AMM 33-51-38-400-002-A REV.113
- [SDR CALA2021100101744](https://openairdocs.org/sdr/CALA2021100101744.md): Epsu · none · Sep 30, 2021 · N497UA · Airbus A320232 · Emergency Lighting
  > EPSU FAIL OPC EPSU 10WL REPLACED IAW AMM 33-51-38-400-002-A REV.113
- [SDR CALA2021092401678](https://openairdocs.org/sdr/CALA2021092401678.md): Connector · broken · Sep 24, 2021 · N497UA · Airbus A320232 · Emergency Lighting
  > CEILING EMER LIGHT DEFECT FOUND WITH THE CONECTOR BASE BROKEN PANEL 251FL. REPLACE OF THE CEILING 251FC EMERGENCY LIGHT (206 WL) IAW AMM: 33-51-11 REV 112 OPERATIONAL TEST OF THE CEILING EMERGENCY LIGHT IAW AMM 33-51-11-710-050-A REV.112
- [SDR CALA2021092401677](https://openairdocs.org/sdr/CALA2021092401677.md): Connector · damaged · Sep 24, 2021 · N497UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT CONECTOR BASE FOUND BROKEN. REPLACEMENT OF CEILING 251FC EMERGENCY LIGHT (206WL) PERFORMED IAW AMM 33-51-11 REV.112
- [SDR CALA2021092401676](https://openairdocs.org/sdr/CALA2021092401676.md): Connector · damaged · Sep 24, 2021 · N497UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT CONECTOR BASE FOUND BROKEN. REPLACEMENT OF CEILING 251FC EMERGENCY LIGHT (206WL) PERFORMED IAW AMM 33-51-11 REV.112
- [SDR CALA2021092401673](https://openairdocs.org/sdr/CALA2021092401673.md): Skin · cracked · Sep 23, 2021 · N497UA · Airbus A320232 · Fuselage Main, Frame
  > AFTER ULTRASOUND INSPECTION AS PER EA 5300-02254 REV B STEP 2.2 REF. (NTM 51-10-15-270-801-A-01) AT DOUBLER REPAIR FOUND INDICATION OF CRACK. EVALUATE ACCORDINGLY, AS NOTED ON LTPR NR# 5001090137-0010. ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2 OF LATEST R
- [SDR CALA2021092401671](https://openairdocs.org/sdr/CALA2021092401671.md): Connector · broken · Sep 23, 2021 · N497UA · Airbus A320232 · Emergency Lighting
  > CONNECTOR BACKSHELLS FOUND BROKEN 202 WL-A. REPLACED CONNECTOR BACKSHELLS 202 WL-A IAW ESPM 20-53-45-02 REV 41 AND AWM 33-51-02 PAGE 203 SHEET 1 AND 2 REV 114. PERFORMED OPC CONTINUITY CHECK IAW ESPM 20-52-21. REV 41 AND IAW AWM 33-51-02 SHEET 1 AND 2 REV 114.
- [SDR CALA2021092401670](https://openairdocs.org/sdr/CALA2021092401670.md): Connector · broken · Sep 23, 2021 · N497UA · Airbus A320232 · Emergency Lighting
  > CONNECTOR BACKSHELL 205WL-A NEEDS REPLACEMENT. REPLACEMENT OF CONNECTOR BACKSHELL 205 WL-A WAS PERFORMED IAW ESPM 20-53-45-02 REV 41. AND AWM 33-51-02 PAGE 203 SHEET 1 AND 2 REV 114. PERFORMED CONTINUITY CHECK IAW ESPM 20-52-21 REV 41 AND IAW AWM 33-51-02 SHEE
- [SDR CALA2021092401669](https://openairdocs.org/sdr/CALA2021092401669.md): Connector · broken · Sep 23, 2021 · N497UA · Airbus A320232 · Emergency Lighting
  > REPLACEMENT OF THE CONNECTOR BACKSHELL 203WL-A IS NEEDED. REPLACEMENT OF CONNECTOR BACKSHELL 203WL-A WAS PERFORMED IAW ESPN 20-53-45-02 REV 41 AND AWM 33-51-02 PAGE 203 SHEET 1 AND 2 REV 114. PERFORMED CONTINUTY CHECK IAW ESPM 20-52-21 REV 41. AND AWM 33-51-02
- [SDR CALA2021092401662](https://openairdocs.org/sdr/CALA2021092401662.md): Epsu · no test · Sep 23, 2021 · N497UA · Airbus A320232 · Emergency Lighting
  > FOR SCEPTRE TRACKING PURPOSE ONLY REMOVE AND REPLACE (A3NB-33-3- 6013) OPC EMERGENCY LIGHTING BATTERY CAPACITY WAS PERFORMED AND FAIL. THE TWO MESSAGES WERE EPSU UNIT FWD L AND EPSU BAT CAP AFT L. TROUBLE SHOOTING REQUIRED. FOR SCEPTRE TRACKING PURPOSE ONLY RE
- [SDR CALA2021092401663](https://openairdocs.org/sdr/CALA2021092401663.md): Epsu · no test · Sep 23, 2021 · N497UA · Airbus A320232 · Emergency Lighting
  > EPSU UNIT FAIL OPC/ REMOVAL OF THE EPSU 10WL IAW AMM 33-51-38- 000-001-A REV 113. INSTALLATION OF ESPU 10WL IAW AMM 33-51-38-400-001-A. REV 113 PERFORMED OF A BITE TEST IAW AMM 33-51-00-710-001 A REV 113.
- [SDR CALA2021092401661](https://openairdocs.org/sdr/CALA2021092401661.md): Fitting · corroded · Sep 22, 2021 · N497UA · Airbus A320232 · Emergency Equipment
  > CORROSION-R2 DOOR STILL BEAM GRT BAR FIT ZONE 261 SEQ 2282 A3NB-53-3-6222 AS NOTED ON LTPR NR# 5001085231-0130. REPAIR IS A CAT-A MAJOR AND PERMANENT REPAIR. NO FURTHER ACTION REQUIRED IAW EC/RA 5311-02643 WITH LHT-PR EO A320-53-10796-00-FINAL. NO RE-ISPECTION
- [SDR CALA2021092201648](https://openairdocs.org/sdr/CALA2021092201648.md): Stringer · corroded · Sep 21, 2021 · N497UA · Airbus A320232 · Fuselage Structure (General)
  > A3BN-05-3-6013 DURING INSPECTION OF THE FWD CARGO COMPARTMENT, FOUND CORRODED FLOOR RIVETS FROM STRINGER 38 L/H TO STRINGER 38 R/H FROM FRAME 24 TO FRAME 34, FURTHER EVALUATION REQUIRED. REMOVED AND REPLACED CLEATS ON FRAME 32 FROM STRINGER 41-42R PER AIRBUS
- [SDR CALA2021090101460](https://openairdocs.org/sdr/CALA2021090101460.md): Bracket · corroded · Aug 30, 2021 · N497UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > A3BN-05-3-6013 DURING INSPECTION OF THE FWD CARGO COMPARTMENT, FOUND CORRODED FLOOR RIVETS FROM STRINGER 38 L/H TO STRINGER 38 R/H FROM FRAME 24 TO FRAME 34, FURTHER EVALUATION REQUIRED.
- [SDR CALA2021081101314](https://openairdocs.org/sdr/CALA2021081101314.md): Floorbeam · corroded · Aug 10, 2021 · N497UA · Airbus A320232 · Fuselage Main, Floor Beam
  > AFT FLOOR ENTREANCE AREA CORR.FINDINGS. A3NB-53-3-6222 ORIG.18-5341-1-2710.
- [SDR CALA2020032000638](https://openairdocs.org/sdr/CALA2020032000638.md): Pressure Panel · damaged · Mar 12, 2020 · N497UA · Airbus A320232 · Fuselage Main, Structure
  > LH PRESSURE PANEL AND FR 36, HAVE HOLES 1,2,4,5,6,7,8,9,10,11,16,17,20,23,24,2,28 HAVE REJETABL INDICATIONS REPAIR BEFORE NEXT F LIGHT CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS PER HAECO LCQ NON ROUTINE 9298259 GENERATED ACCOMPLISHED INTERIM REPAIR ON LH PR
- [SDR CALA2020030900610](https://openairdocs.org/sdr/CALA2020030900610.md): Skin · dented · Mar 8, 2020 · N497UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > LH AFT FUSELAGE EXT SKIN HAS A DENT 6" FWD OF FR65 ST34L ON HAEC O LCQ REF 9298438 GENERATED BY N078625 UPON FURTHER EVALUATION FOUND DENT TO BE IN STIFFENED AREA AND R EQUIRES REPAIR IAW A320 SRM 53-41-11-283-059 FABRICATED AND INST ALLED REPAIR DOUBLER AND F
- [SDR CALA2019120302141](https://openairdocs.org/sdr/CALA2019120302141.md): Fuel Cap · missing · Dec 2, 2019 · N497UA · Airbus A320232 · Fuel Storage
  > FUEL CAP REPORTED MISSING UPON ARRIVAL PER MCIOO INVESTIGATE AND CONTACT TOMC UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V929091 MAC RELATED WORK ORDER 000000002260917 AND PRTR PDA 2 REPORTED REF LP 3970599. LOCAL F
- [SDR CALA2019032900482](https://openairdocs.org/sdr/CALA2019032900482.md): Pressure Switch · leaking · Mar 27, 2019 · N497UA · Airbus A320232 · Hydraulic Pressure Sensor
  > Y RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN. HYD LOW CONFIRMED ON SYS PAGE. FOUND NR 2 ENG YELLOW DRIVEN PUMP PRESS SWITCH LEAKING, REPLACED SWITCH PER AMM 29-13-17, ALSO INSPECTED AND REPLACED CASE DRAIN FILTER ELEMENT, NO METAL FOUND ON ELEMENT OR CASE BOWL
- [SDR CALA2019032500468](https://openairdocs.org/sdr/CALA2019032500468.md): Pressure Switch · leaking · Mar 25, 2019 · N497UA · Airbus A320232 · Hydraulic Pressure Sensor
  > ENG 2 PUMP LO PR DISPLAYED ON UPPER ECAM. DEFERRED PER MEL 2930GG. APPROVED MEL 2930GG FOR NR 2 ENGINE DRIVEN HYD PUMP LOW PRESSURE WARNING ERRONEOUSLY DISPLAYED. ASOCIATED SYSTEM PRESSURE INDICATION OPERATES NORMALY. ITEM DEFERRED PER 2930GG. OK TO CONTINUE.
- [SDR CALA2018021900686](https://openairdocs.org/sdr/CALA2018021900686.md): Epsu · unserviceable · Feb 19, 2018 · N497UA · Airbus A320232 · Emergency Lighting
  > REMOVE AND REPLACE FWD L EPSU. REMOVED AND REPLACED FWD L EPSU.
- [SDR CALA2018021900685](https://openairdocs.org/sdr/CALA2018021900685.md): Battery · no test · Feb 19, 2018 · N497UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY FAILED A CAPACITY TEST. REMOVED AND REPLACED THE BATTERY IAW AMM 33-51-38-000-00 2-A, AND 33-51-38-400-002-A. PERFORMED AN OPS TEST, NO FAULTS NOTED.
- [SDR CALA2018021600629](https://openairdocs.org/sdr/CALA2018021600629.md): Skin · chafed · Feb 16, 2018 · N497UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT FRAME 34, STRINGER 43L - 43R, CHAFE. REPAIRED IAW EA 5300-02120, OP 1, STEP 4.1.
- [SDR CALA2018010500033](https://openairdocs.org/sdr/CALA2018010500033.md): Eec · faulted · Jan 5, 2018 · N497UA · Airbus A320232 · Fuel Controlling System
  > NR 2 ENGINE KEPT ACCELERATING ON START. TRIED A RESTART. NO LUCK. SHUTDOWN THE ENGINE EACH TIME. REMOVED AND REPLACED THE NR 2 ENGINE EEC IAW AMM 73-22-34. FADEC OPS CHECKED NORMAL. ENGINE IDLE RUN NORMAL. NO DEFECTS NOTED. PERFORMED A NR 2 ENGINE START,
- [SDR CALA2017082102837](https://openairdocs.org/sdr/CALA2017082102837.md): Slide · no test · Aug 21, 2017 · N497UA · Airbus A320232 · Escape Slide
  > CABIN EMERGENCY LIGHT SYS TEST ON CIDS DISPLAYS MESSAGE, EPSU EXT LOAD FWD L. DURING 2 SERVICE OPS CHECKS IAW AMM 33-51-00-710-001-A. REPLACED THE NR 1 LEFT DOOR SLIDE ASSEMBLY IAW AMM 25-62-4 4-400-006-A.
- [SDR CALA2017062602004](https://openairdocs.org/sdr/CALA2017062602004.md): Slide · failed · Jun 26, 2017 · N497UA · Airbus A320232 · Escape Slide
  > CABIN EMERGENCY LIGHTS OP CK HAS MSG "EPSU EXT LOAD FWD L". CHANGED ESCAPE SLIDE REF AMM 25-62-44-000-802-A. OPS CHECKED CABIN EMER LIGHTS REF AMM 33-50-00-0001.
- [SDR CALA2017052601602](https://openairdocs.org/sdr/CALA2017052601602.md): Battery Pack · no test · May 26, 2017 · N497UA · Airbus A320232 · Emergency Lighting
  > AFT EMERGENCY LIGHT FAILED BATTERY CAPACITY TEST. REPLACED THE AFT POWER SUPPLY UNIT. OP CHECKED GOOD.
- [SDR CALA2017012300173](https://openairdocs.org/sdr/CALA2017012300173.md): Power Supply · faulted · Jan 23, 2017 · N497UA · Airbus A320232 · Emergency Lighting
  > EPSU UNIT AFT L MESSAGE AFTER EMERGENCY LIGHT TEST. PERFORMED A EPSU BITE TEST IAW AMM 33-51-38 SYTEM TESTED OK.
- [SDR CALA2017012300172](https://openairdocs.org/sdr/CALA2017012300172.md): Power Supply · faulted · Jan 23, 2017 · N497UA · Airbus A320232 · Emergency Lighting
  > EPSU UNIT EMERGENCY RT MESSAGE AFTER COMPLETION OF CABIN EMERGENCY LIGHT OPERATIONAL CHECK. REPLACED THE POWER SUPPLY IAW MM 33-51-38, OPS CHECKED GOOD.
- [SDR CALA2016122101142](https://openairdocs.org/sdr/CALA2016122101142.md): Power Supply · inoperative · Dec 21, 2016 · N497UA · Airbus A320232 · Emergency Lighting
  > THE PTP EMERGENCY LIGHT TEST FAILED FOR EPSU UNIT EMR R, AFT L. REPLACED FWD LT POWER SUPPLY UNIT AND BATTERY PN 31-3350-9-9001 PN 3214-54-10 SN 1373 RESET EMERG LIGHT CBS. SYSTEM CKS OK.
- [SDR CALA2016122101141](https://openairdocs.org/sdr/CALA2016122101141.md): Power Supply · inoperative · Dec 21, 2016 · N497UA · Airbus A320232 · Emergency Lighting
  > THE PTP EMERGENCY LIGHT TEST FAILED FOR EPSU EXT LOAD FWD L. REPLACED RT OVERWING EPSU AND BATTERY.
- [SDR CALA2016111800943](https://openairdocs.org/sdr/CALA2016111800943.md): Light · malfunctioned · Nov 18, 2016 · N497UA · Airbus A320232 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHTS ARE INOPERATIVE. LIGHTS STAY ILLUMINATED ENTIRE FLIGHT CYCLED GOUND POWER SWITCH, AFTER PUT BACK ON LINE THE EMERGENCY LIGHTS EXTINGUISHED, NO FAULTS WERE NOTED AT THIS TIME DURING OPERATIONAL CHECK.
- [SDR CALA2016101795815](https://openairdocs.org/sdr/CALA2016101795815.md): Power Supply · inoperative · Oct 15, 2016 · N497UA · Airbus A320232 · Emergency Lighting
  > PROXIMITY EMERGENCY AISLE LIGHTS AT ROWS 10 AND 11 INOP. REPLACED MID LEFT POWER SUPPLY AND BATTERY.
- [SDR CALA2016081195628](https://openairdocs.org/sdr/CALA2016081195628.md): Connector · loose · Jun 19, 2016 · N497UA · Airbus A320232 · Light System Wiring
  > EMERGENCY LIGHT TEST FAILED. MESSAGE EPSU EXT LOAD FWD L. RESEATED EPSU CONNECTOR, REPLACED BATTERY.
- [SDR CALA2016081195627](https://openairdocs.org/sdr/CALA2016081195627.md): Warning Message · false activation · Jun 5, 2016 · N497UA · Airbus A320232 · Emergency Lighting
  > CIDS EMERGENCY LIGHT TEST. MESSAGE EPSU BATTERY EMERGENCY LIGHT R. RESET, MESSAGE CLEARED, OPS CHECKED GOOD.
- [SDR CALA2015091694359](https://openairdocs.org/sdr/CALA2015091694359.md): Slide · defective · Sep 14, 2015 · N497UA · Airbus A320232 · Escape Slide
  > EMERGENCY LIGHT FAILED TEST, FAULT LT FWD EXT LIGHTS. REPLACED SLIDE PACK DOOR 1 LT IAW AMM 25-62-44. EMER LIGHT TESTED OK.
- [SDR CALA2015091494349](https://openairdocs.org/sdr/CALA2015091494349.md): Light · inoperative · Sep 14, 2015 · N497UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT FAILS TEST, FAULT LT FWD EXTERIOR LIGHTS. TROUBLE SHOT TO DOOR 1L SLIDE PACK. HAS OPEN IN ONE BULB, WILL NEED TO HAVE SLIDE PACK REPLACED.
- [SDR CALA2015091494348](https://openairdocs.org/sdr/CALA2015091494348.md): Battery · discharged · Sep 14, 2015 · N497UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHTS FAILED TEST IAW 2 SVC. REPLACED BATTERY IAW AMM 33-5 1-38. TESTED OK.
- [SDR CALA2014101692447](https://openairdocs.org/sdr/CALA2014101692447.md): Skin · gouged · Oct 10, 2014 · N497UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN GOUGE AT FRAME 32 BETWEEN STRINGER 38 -39R. DAMAGE REMOVED & DOUBLER REPAIR INSTALLED IAW SRM 53-00-11 FIG 240.

Next page: https://openairdocs.org/aircraft/N497UA/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 = 'N497UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N497UA/reports

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