# Service difficulty reports: N493UA

A list on [N493UA](https://openairdocs.org/aircraft/N493UA.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 · 84 reports

- [SDR CALA2026082618936](https://openairdocs.org/sdr/CALA2026082618936.md): Fuel Cap · missing · Aug 25, 2026 · N493UA · Airbus A320232 · Fuel Storage
  > FUEL CAP REPORTED MISSING BY FUELER. NO LEAKS NOTED AT COUPLING. UNABLE TO FIND FUEL CAP LOCALLY. REMOVED FUEL CAP AND REPLACED WITH SERVICABLE PART IAW AMM 28-25-41/401, CONFIG 00. NO DEFECTS NOTED.
- [SDR CALA2026062317289](https://openairdocs.org/sdr/CALA2026062317289.md): Light · inoperative · Jun 22, 2026 · N493UA · Airbus A320232 · Emergency Lighting
  > PRE DEPARTURE CHECK, SEAT 8-A EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT AT SEAT ROW 8A IAW AMM 33-51-19 AND REMOVED TASK 33-51-19-19-000-002-A AND REPLACED AND TESTED PER 33-51-19-400-002-A. SEAT ROW 8-A AND ALL EMERGENCY ESCAPE PATH
- [SDR CALA2026051916385](https://openairdocs.org/sdr/CALA2026051916385.md): Unknown · odor · May 17, 2026 · N493UA · Airbus A320232 · Air Distribution System
  > FA REPORTS STRONG SEWAGE ODOR COMING FROM AFT LAVS INFLIGHT. CLEAN THE VACUUM WASTE LINES WITH THE CHEMICAL CLEANING AGENT AND CRUSHED ICE IAW AMM 38-11-00. NO STRONG SEWAGE ODOR FROM BOTH AFT LAVS AT THIS TIME.
- [SDR CALA2026042315644](https://openairdocs.org/sdr/CALA2026042315644.md): Duct · cracked · Apr 22, 2026 · N493UA · Airbus A320232 · Engine Thrust Reverser
  > NR 2 ENG RT T/R C-DUCT HAS CRACKED AT L/E UPPER AIR PATH SKIN. REMOVED NR 2 ENG RT T/R IAW AMM 78-32-03-000-010-A. REMOVED AND REPLACED L/E AIR PATH SKIN IAW SRM 51-42-11/001. REINSTALLED NR 2 ENG RT T/R IAW AMM 78-32-03-400-010-A. RIG AND OPS CHECKED GOOD.
- [SDR CALA2026021813859](https://openairdocs.org/sdr/CALA2026021813859.md): Cover · missing · Feb 17, 2026 · N493UA · Airbus A320232 · Wing, Plate/Skin
  > DURING WALK AROUND FOUND PANEL COVER MISSING FROM RT WING LEADING EDGE. OTBD OF RT ENGINE. OPEN.
- [SDR CALA2026012813400](https://openairdocs.org/sdr/CALA2026012813400.md): Vent · leaking · Jan 25, 2026 · N493UA · Airbus A320232 · Turbine Engine Oil System
  > AIRCRAFT HAD A LINGERING OIL ODOR. NOTICED ON GROUND. CAME BAC K IN DESCENT. WORKING THROUGH TSM 71-00-00-810-801-A, FOUND NR 2 ENG DE OILER OVERBOARD VENT HAVING EXCESSIVE OIL LEAKAGE. REF LP 7722927, SUBSEQUENT LEAK CHECK. OIL ODOR NOT ABLE TO BE DUPLICAT
- [SDR CALA2025101410040](https://openairdocs.org/sdr/CALA2025101410040.md): Bracket · damaged · Oct 11, 2025 · N493UA · Airbus A320232 · Escape Slide
  > L/H OVERWING EMERGENCY ESCAPE SLIDE VERTICAL AFT MOUNTING BRACKET HAS DAMAGE AT UPPER BOLT HOLE. PICS ATTACHED. PICTURES WITH SCALE FOR REFERENCE NEED MATERIAL VERIFICATION FOR AFT FAIRING STRUCTURE OUTER FLANGE RUN OUT REPAIR REF. SRM 53-45-12-300-010. MATERI
- [SDR CALA2025060305224](https://openairdocs.org/sdr/CALA2025060305224.md): None · none · Jun 1, 2025 · N493UA · Airbus A320232 · Standard Practices/Structures
  > SEVERE TURB ON APPCH TO CYYC REF AMM 05-51-17. ACCOMPLISHED SEVERE TURBULENCE INSPECTION UP TO AND INCLUDING STEP F AND ALSO INCLUDING STEP J IN REFERENCE TO AMM 05-51-17-200-001-A NEED TO ACCOMPLISH STEP G,H, AND K. NO FAULTS FOUND. PER TASK 05-51-17-200-0
- [SDR CALA2025021002248](https://openairdocs.org/sdr/CALA2025021002248.md): Bellows · ruptured · Feb 8, 2025 · N493UA · Airbus A320232 · Air Conditioning System
  > REF LP# 3803036 PRESSURATION AT 19000 WAS 8900 FEET CABIN PRES S. LEVELED OFF AT 20000 CABIN PRESS UP TO 9800 ORIGINAL LP 3803036 CLOSED IN ERROR. CPC 1 AND 2 NO FAULTS. AEVC TEST PERFORMED, NO FAULTS. MANUALLY CLOSED AND OPENED OUTFLOW VALVE, NO FAULTS NOTED.
- [SDR CALA2024110401000](https://openairdocs.org/sdr/CALA2024110401000.md): Light · no discrepancy · Nov 2, 2024 · N493UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ON BOTH AFT DOORS COMES ON AND OFF DURING LNG FOLLOWED TSM TASK 33-51-00-810-819-A (EMERGENCY EXIT LIGHTING FLICKER FAULT). CARRIED OUT OPERATIONAL CHECK OF THE EMERGENCY POWER UNITS BY BITE CHECK PER AMM TASK 33-51-00-710-001-A. RESULTS
- [SDR CALA2024052901604](https://openairdocs.org/sdr/CALA2024052901604.md): Skin · corroded · May 26, 2024 · N493UA · Airbus A320232 · Wing, Plate/Skin
  > LEFT WING TOP AFT PLATE AT RIB 11 FWD OF LH SPOILER #2 HAS EXFOLIATION CORROSION. WING TOP SKIN PANEL 2 COVERED BY THE REPAIR PLATE AND AROUND THE R PART 2A OF THE LATEST REVISION OF ECRA 5721-01495 ON OR BEFORE 447 TOTAL AIRCRAFT FLT HOURS. REPAIR PLATE & A
- [SDR CALA2024052401580](https://openairdocs.org/sdr/CALA2024052401580.md): Frame · cracked · May 21, 2024 · N493UA · Airbus A320232 · Fuselage Main, Frame
  > RH FR 16 UPPER DOUBLE JOGGLE AREA HOLE 4 HAS CRACK INDICATION IN FRAME LAYER 5 OCLOCK DIRECTION (VIEWED FROM OUTSIDE) 100% S.H PER HAECO LCQ NR 9292345 / 26345 IN THE RH FR16 UPPER DOUBLE JOGGLE HOLES NR 5, 6, 7, 8, A & # ORE THE AIRCRAFT REACHES 35,638 TOTAL
- [SDR CALA2022101802857](https://openairdocs.org/sdr/CALA2022101802857.md): Fuel Cap · missing · Oct 18, 2022 · N493UA · Airbus A320232 · Fuel Storage
  > PDA 3 FUEL CAP MISSING ON ARRIVAL ITEM PLACED ON CDL REF L/P 9767699
- [SDR CALA2022100602724](https://openairdocs.org/sdr/CALA2022100602724.md): Spring Assy · missing · Oct 5, 2022 · N493UA · Airbus A320232 · Steering Unit
  > PDA 3 NLG TOWING BOX LEVER HAS BOTH SPRING CLIPS MISSING -- SEE PHOTO PHOTO ADDED INSTALLED BOTH NEW SPRING CLIPS ON NLG TOWING BOX LEVER.. REF IPC 32-51-12-01E
- [SDR CALA2022071501760](https://openairdocs.org/sdr/CALA2022071501760.md): None · noisy · Jul 15, 2022 · N493UA · Airbus A320232 · Fuselage Structure (General)
  > EXCESSIVE VIBRATION ANDNOISE COMING FROM BENEATH THE CABIN CENTE REDIN THE AISLE AT ROW 3 ISSUES AND PACK OPERATIONS WERE NORMAL. SUSPECT A POSSIBLE DUCT ISSUE. THIS LOG PAGE INFO ADDED TO LP 9054089. THIS LOG PAGE CAN BE INSPECTED LOWER FUSELAGE AND FOUND SPE
- [SDR CALA2021080601263](https://openairdocs.org/sdr/CALA2021080601263.md): Stringer · corroded · Aug 4, 2021 · N493UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FWD CARGO BAY STR 43R HAS CORROSION APPROX. 4" AFT FR34 GENERATE D BY V077960 ON HAECO LCQ NR 9296354/36354 REMOVED AND REPLACED STRINGER 43RT FR31-34 IAW A320 SRM 51-72-11 ACCOMPLISHED BY MECH V052030 INSP BY V061334
- [SDR CALA2021080601262](https://openairdocs.org/sdr/CALA2021080601262.md): Skin · corroded · Aug 4, 2021 · N493UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > UPPER FUSELAGE SKIN AT FR69-70 HAS CORROSION AROUND BONDING POIN TS AT STR2L AND 2R BS 69-BS70, STR 2L - STR 2R - A3NB-53-3-6208 - NR 9296419 (36419) GENERATED BY V077960 AT HAECO LCQ. ACCOMPLISHED INTERIM REPAIR AT FR 69-70 STR 1L - 2R IAW ECRA 534 1-01257 PA
- [SDR CALA2021080401253](https://openairdocs.org/sdr/CALA2021080401253.md): Fitting · cracked · Aug 3, 2021 · N493UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > RH WINDSHIELD SIDE POST FRAME 4 UPPER ATTACHMENT FASTENER HOLE I N POST IS CRACKED IN THE FRAME LAYER - A3NB-53-4-6051, AD 2019-2 3-01 - NR 9296473 (36473) GENERATED BY V061633 AT HAECO LCQ. ACCOMPLISHED INTERIM REPAIR IAW PART 1 STEP 1 OF ECRA 5311-02617 NEED
- [SDR CALA2021080401252](https://openairdocs.org/sdr/CALA2021080401252.md): Stringer · corroded · Aug 3, 2021 · N493UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FWD CARGO BETWEEN FRAMES 31-33 RT STRINGER HAS CORROSION GENERAT ED BY V052030 ON HAECO LCQ NR 9296591/36591 REMOVED AND REPLACED STRINGER 41RT FR 31-33 IAW A320 SRM 51-72-1 1 ACCOMPLISHED BY MECH V052030 INSP BY V061334
- [SDR CALA2021080401251](https://openairdocs.org/sdr/CALA2021080401251.md): Frame · corroded · Aug 3, 2021 · N493UA · Airbus A320232 · Fuselage Main, Frame
  > AFT CARGO FRAME BAY 63, 64 STGR 42R, 41R SKIN REPAIR CORRODED. REMOVED AND REPLACED DISCREPANT SKIN REPAIR AT FR63-64 STR 41R-4 2R IAW A320 DWG 60N00001 AND 13N00001 AND A320 SRM 51-44-11-801.
- [SDR CALA2021072601188](https://openairdocs.org/sdr/CALA2021072601188.md): Stringer · corroded · Jul 25, 2021 · N493UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO PIT AT FRAME 63-64 PREVIOUSLY REPAIRED STRINGER HAS CORROSION. REMOVED AND REPLACED STRINGER 42 RIGHT FR 63-64 IAW A320 SRM 51- 72-11.
- [SDR CALA2021072601174](https://openairdocs.org/sdr/CALA2021072601174.md): Stringer Splice · corroded · Jul 23, 2021 · N493UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FWD CARGO STRINGER 42 RIGHT SPLICE FR 27-28 HAS CORROSION. REMOVED AND REPLACED SPLICE IN FWD CARGO ON STRINGER 42 RIGHT IA W A320 SRM 51-72-11.
- [SDR CALA2021072601173](https://openairdocs.org/sdr/CALA2021072601173.md): Stringer Splice · corroded · Jul 23, 2021 · N493UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FWD CARGO PIT STRINGER 41RT SPLICE HAS CORROSION. REMOVED AND REPLACED SPLICE IN FWD CARGO ON STRINGER 41 RIGHT IA W A320 SRM 51-72-11.
- [SDR CALA2021072301159](https://openairdocs.org/sdr/CALA2021072301159.md): Cover · corroded · Jul 21, 2021 · N493UA · Airbus A320232 · Fuselage Main, Structure
  > AFT CARGO LOWER DOOR FRAME AREA TORSION BOX COVER WITH CORROSION - A3NB-53-4-61-6179 - NR 9296328 (36328) GENERATED BY V898117 AT HAECO LCQ. REMOVED AND REPLACED AFT CARGO PIT TORSION BOX COVER SHEET FR 52 -FR 56 IAW A320 SRM 51-75-11. ACCCOMPLISHED BY V052030
- [SDR CALA2021072301158](https://openairdocs.org/sdr/CALA2021072301158.md): Cover · corroded · Jul 21, 2021 · N493UA · Airbus A320232 · Fuselage Main, Structure
  > FORWARD CARGO BAY TORSION BOX COVER HAS CORROSION AROUND TIE DOW NS AT FR 26 & 27 - A3NB-05-3-6013 - NR 9296345 (36345) GENERATED BY V077960 AT HAECO LCQ. REMOVED AND REPLACED FWD CARGO TORSION BOX COVER SHEET FR 24-28R T IAW A320 SRM 51-62-11. DOT REMOVED. AC
- [SDR CALA2021072301157](https://openairdocs.org/sdr/CALA2021072301157.md): Fitting · corroded · Jul 21, 2021 · N493UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FORWARD CARGO BAY FR 29 STR 43R-42R SHEAR TIE HAS CORROSION - A3 NB-05-3-6013 - NR 9296352 (36352) GENERATED BY V077960 AT HAECO LCQ. REMOVED AND REPLACED SHEAR TIE IN FWD CARGO PIT AT FR 29RT BETWE EN STRINGERS 42R-43R IAW A320 SRM 51-72-11. ACCOMPLISHED BY V
- [SDR CALA2021072301156](https://openairdocs.org/sdr/CALA2021072301156.md): Door Sill · corroded · Jul 21, 2021 · N493UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FORWARD CARGO BAY DOOR SILL HAS CORROSION AROUND 2 FASTENER HOLE S AT FR 28 - A3NB-05-3-6013 - NR 9296346 (36346) GENERATED BY V0 77960 AT HAECO LCQ. REMOVED AND REPLACED AFT FORWARD CARGO SILL AT FR 28RT IAW A320 SRM 51-42-11. DOT REMOVED. ACCOMPLISHED BY V05
- [SDR CALA2021071201062](https://openairdocs.org/sdr/CALA2021071201062.md): Door Sill · corroded · Jul 9, 2021 · N493UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > L-2 DOOR SILL HAS CORROSION SPOTS AT FR-68 (A3NB-53-3-6222). GEN ERATED BY V919150 AT HAECO LCQ PER NR 9296272 (36272). REMOVED AND REPLACED DOOR SILL AT L-2 DOOR FR-66-FR68 IAW A320 SRM 51-42-11. PERFORMED BY V061737 AND INSP BY N078570.
- [SDR CALA2021071201061](https://openairdocs.org/sdr/CALA2021071201061.md): Door Sill · corroded · Jul 9, 2021 · N493UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > R-2 DOOR SILL HAS CORROSION SPOTS AT UPPER FORWARD AND REAR SURF ACES (A3NB-53-3-6222). GENERATED BY V919150 AT HAECO LCQ PER NR 9296260 (36260). REMOVED AND REPLACED R-2 DOOR SILL FR66-68 IAW A320 SRM 51-42-11 PERFORMED BY V061737 AND INSP BY N078570.
- [SDR CALA2021071201060](https://openairdocs.org/sdr/CALA2021071201060.md): Fitting · corroded · Jul 9, 2021 · N493UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > L2 DOOR CUTOUT SILL ASSY FWD ADN AFT CORNER FITTINGS HAVE CORROS ION A3NB-53-3-6222 PER HAECO LCQ N/R 9296488/36488 GENERATED BY N078592. REMOVED FWD & AFT FITTING FROM L2 DOOR FOM IAW A320 SRM 51-42-11. REMOVED CORR FROM FWD & AFT FITTING IAW A320 SRM 51-74-
- [SDR CALA2021071201059](https://openairdocs.org/sdr/CALA2021071201059.md): Shear Plate · cracked · Jul 9, 2021 · N493UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > MAIN CABIN AFT L/H BETWEEN FR-69/70 STRINGER 23L UNDER FLOOR HAS CRACK SHEAR PLATE A3NB-53-3-6222 PER HAECO LCQ N/R 9296275/3627 5 GENERATED BY V919150. REMOVED SHEAT PLATE IAW A320 SRM 51-42-11-001 PROC 4A-E REC''D PR OPER REPLACEMENT PART, LOCATED, DRILLED &
- [SDR CALA2021070701038](https://openairdocs.org/sdr/CALA2021070701038.md): Stringer · corroded · Jul 6, 2021 · N493UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO PIT AT FR63-64 STRINGER 41C LEFT PREVIOUSLY REPAIRED S TRINGER HAS CORROSION A3NB-05-3-6022 PER HAECO LCQ N/R 9296479/3 6479 GENERATED BY V052030.
- [SDR CALA2021070501023](https://openairdocs.org/sdr/CALA2021070501023.md): Shear Tie · corroded · Jul 3, 2021 · N493UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FORWARD CARGO BAY FR 33 STR 44-43R SHEAR TIE HAS CORROSION A3NB- 05-3-6013 PER HAECO LCQ N/R 9296353/36353 GENERATED BY V077960. REMOVED & REPLACED CLEAT AT FR33 BETWEEN STRINGER 44-43RT IAW A3 20 SRM 51-42-11 AT HAECO LCQ ON HANGAR NR 9296353/36353 PERFORME D
- [SDR CALA2021070501022](https://openairdocs.org/sdr/CALA2021070501022.md): Stringer Splice · corroded · Jul 3, 2021 · N493UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > STR SPLICES AT FR BAY 63-64 HAS CORROSION 3 EA 42LT ON HAECO LCQ REF 9296368/36368 A3NB-05-3-6022. NR GENERATED BY V892442 REMOVED & REPLACED STR 42LT FRAME 60-64 IAW A320 SRM 51-72-11 AT HAECO LCQ ON HANGAR NR 9296368/36368
- [SDR CALA2018022300767](https://openairdocs.org/sdr/CALA2018022300767.md): Slide · damaged · Feb 23, 2018 · N493UA · Airbus A320232 · Escape Slide
  > LEFT FORWARD DOOR ESCAPE SLIDE DAMAGED. REPLACED THE SLIDE.
- [SDR CALA2017091003123](https://openairdocs.org/sdr/CALA2017091003123.md): Battery · discharged · Sep 10, 2017 · N493UA · Airbus A320232 · Emergency Equipment
  > AFT FA EMERG FLASHLIGHT NOT FLASHING RED ON PREFLIGHT. REPLACED FLASHLIGHT BATTERY, FLASHING RED LIGHT OPS CHK NORMAL.
- [SDR CALA2016111400920](https://openairdocs.org/sdr/CALA2016111400920.md): Battery · discharged · Nov 14, 2016 · N493UA · Airbus A320232 · Emergency Lighting
  > EMER LIGHT TEST FAILS, EMER BATTERY L AND EMER BATTERY R. REPLACED BATTERIES IAW AMM 33-51-38. OPS TEST GOOD.
- [SDR CALA2016060695432](https://openairdocs.org/sdr/CALA2016060695432.md): Stringer · corroded · Jun 4, 2016 · N493UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT PIT BULK STRINGER 31R, BELOW OUTFLOW VLV CORRODED. R & R THE AFT PIT BULK STRINGER 31R IAW SRM 51-72-11.
- [SDR CALA2015020393064](https://openairdocs.org/sdr/CALA2015020393064.md): Eec · malfunctioned · Feb 1, 2015 · N493UA · Airbus A320232 · Fuel Control/Turbine Engines
  > CREW REPORT ENG 2 SENSOR FAULT & ENG 2 STALL MSG ON ECAM. HELD AT FL 160 & PERFORMED QRH PROCEDURES, NO STALL OBSERVED. CREW ELECTED TO RETURN. R & R NR 2 EEC IAW AMM 73-22-34-400-010-A13. COMPLIED WITH STEPS 3 THRU 5D.
- [SDR CALA2014043090933](https://openairdocs.org/sdr/CALA2014043090933.md): Control Panel · defective · Apr 29, 2014 · N493UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHTS STUCK ON, WILL NOT TURN OFF WHEN ACFT IS UNPOWERED. REPLACED AFT FLIGHT ATTENDANT ANT PANEL IAW MM23-73-13-000-001-A, OPERATIONS CHECKED GOOD.
- [SDR CALA2014043090909](https://openairdocs.org/sdr/CALA2014043090909.md): Control Panel · defective · Apr 26, 2014 · N493UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHTS WILL NOT TURN OFF WITH POWER OF ACFT. WHILE TEST OF PTP PANEL SHOWING EPSU COM FWD LT. TESTED EMERGENCY LIGHTS. REPLACED AFT ATTENDANT PANEL & FWD LT POWER SUPPLY 10WL. EMERGENCY LIGHTS TESTED OK.
- [SDR CALA2013123194076](https://openairdocs.org/sdr/CALA2013123194076.md): Bleed Valve · faulty · Dec 30, 2013 · N493UA · Airbus A320232 · Compressor Bleed Valve
  > ENG 2 HP VLV FAULT DISPLAYED ON UPPER ECAM SCREEN. BLEED VLV SECURED CLOSED IAW MEL. DURING TROUBLE SHOOTING FOUND CONNECTOR BACK SHELL DAMAGED PCN 565-0756 IAW AWM 7 1-51-03 PG1 RDF-T. REMOVED BACK SHELL, ALL WIRE INSULATION CHECKED GOOD, INSTALLED NEW BAC
- [SDR CALA2013123194065](https://openairdocs.org/sdr/CALA2013123194065.md): Boot · unsecure · Dec 30, 2013 · N493UA · Airbus A320232 · Control Column Section
  > CAPTAIN'S SIDE STICK BOOT IS MISSING SECURING STRING ELASTIC STRAP. SECURED CAPTAIN'S SIDE STICK BOOT WITH STRING.
- [SDR CALA2013122793969](https://openairdocs.org/sdr/CALA2013122793969.md): Flt Controls · vibration · Dec 27, 2013 · N493UA · Airbus A320232 · Flight Control System
  > CREW REPORT HIGH SPEED AIRFRAME VIBRATION, IAW TO LOG01 AIRCRAFT VIBRATION. BEGAN TROUBLESHOOTING IAW FELT ON RUDDER PEDALS & REPORTED AS MODERATE IN AFT CABIN. 320 IAW AMM 27-24-00 PG 3 OF 12 UP TO ITEM B, NEED CONT FROM HERE THRU TO END.
- [SDR CALA2013121693748](https://openairdocs.org/sdr/CALA2013121693748.md): Starter · sparks · Dec 15, 2013 · N493UA · Airbus A320232 · Engine Starter
  > DURING ENG 1 START SPARKS OBSERVED COMING OUT OF THE ENG. REPLACED NR 1 ENG START IAW AMM.
- [SDR CALA2013111292838](https://openairdocs.org/sdr/CALA2013111292838.md): Sensor · faulty · Nov 11, 2013 · N493UA · Airbus A320232 · Landing Gear Position and Warning
  > LGCIU 1 FAULT, FLIGHT DIVERTED. PFR SHOWS 27GA DOOR SENSOR FAULT. REPLACED SENSOR MM32-31-73-400-001-A. OPERATIONS CHECKED NORMAL.
- [SDR CALA2013102992461](https://openairdocs.org/sdr/CALA2013102992461.md): Threshold · damaged · Oct 26, 2013 · N493UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT BAG PIT THRESHOLD DAMAGED. REPLACED SILL PLATE IAW ECRA 5322-01050 PERMANENT REPAIR.
- [SDR CALA2013090991102](https://openairdocs.org/sdr/CALA2013090991102.md): Contactor · faulty · Sep 6, 2013 · N493UA · Airbus A320232 · DC Generating System
  > AFTER T-S LOG1 WRITE UP FOUND 6PB1 CONTACTOR INOPERATIVE. SWAPPED 6PB1 & 6PB2 TO VERIFY! BAD NON STOCK SEA, PN NEEDED IS 565-0010. REPLACED 6PB1 CONTACTOR IAW MM. DISCONNECTED & RECONNECTED MAIN BATTERIES IAW MM. OPERATIONS CHECKED GOOD.
- [SDR CALA2013090290943](https://openairdocs.org/sdr/CALA2013090290943.md): Harness · defective · Sep 1, 2013 · N493UA · Airbus A320232 · Crew Oxygen System
  > CAPTAIN'S OXYGEN HARNESS FAILS TO INFLATE. SWAPPED WITH 2ND OBSERVERS SEAT, CAPTAIN'S WORKS.
- [SDR CALA2013082690767](https://openairdocs.org/sdr/CALA2013082690767.md): Screw · missing · Aug 25, 2013 · N493UA · Airbus A320232 · Audio Integrating System
  > CAPTAINS HAND MIC HAS TWO SCREWS MISSING BOTTOM FALLS OUT. RESECURED &TIGHTENED SCREWS ON CAPTAIN`S MICROPHONE OKAY.

Next page: https://openairdocs.org/aircraft/N493UA/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 = 'N493UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N493UA/reports

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