# Service difficulty reports: N496UA

A list on [N496UA](https://openairdocs.org/aircraft/N496UA.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 · 94 reports

- [SDR CALA2026082418859](https://openairdocs.org/sdr/CALA2026082418859.md): Adiru · faulted · Aug 21, 2026 · N496UA · Airbus A320232 · Outside Air Temperature Indicator/Sensor
  > REPEAT GRIPE OF IR-1 AFTER TAKEOFF. DEBRIEFED PILOT, AFTER TAKEOFF, IR-1 FAULTED. CAPT FOLLOWED QRH AND SWITCHED TO CAPT 3 FOR THE IR BACKUP BUT NO HELP. CAPTAIN`S HAD RED X EVEN AFTER SWITCHING TO CAPT 3. REPLACED NR 1 ADIRU IAW AMM 34-12-34. OPS CHKD GOOD.
- [SDR CALA2026072317962](https://openairdocs.org/sdr/CALA2026072317962.md): Bleed Valve · faulted · Jul 20, 2026 · N496UA · Airbus A320232 · Compressor Bleed Valve
  > NUMBER 1 ENG DID NOT SPOOL UP APPROPRIATELY ON TAKE OFF. REJECTED TAKE OFF, CREW STATES: FLEX TAKEOFF BEING PERFORMED. TECHS PERFORMED ACCEL & DECEL CHK OF ENG 1 IAW AMM 71-00-00-700-011-B. ENG 1 FAILED TO REACH TARGET EPR BY 1 SEC. TIME TARGET EPR IS 6.2 SECS
- [SDR CALA2026020113462](https://openairdocs.org/sdr/CALA2026020113462.md): Power Supply · no test · Jan 31, 2026 · N496UA · Airbus A320232 · Emergency Lighting
  > EPSU UNIT FWD L FAULT DISPLAYED AFTER TESTING OF THE EMERGENCY LIGHTS. R & R EPSU IAW AMM 33-51-38/401, CONFIG 00. OPS CHECKED GOOD.
- [SDR CALA2025081307688](https://openairdocs.org/sdr/CALA2025081307688.md): Cap · missing · Aug 9, 2025 · N496UA · Airbus A320232 · Fuel Storage
  > PDA 2 PDA CREATED FOR FUEL CAP MISSING LP#5856941 REFERENCE LP# 5856941 FOR CLEARING OF LOGPGE.
- [SDR CALA2025061805654](https://openairdocs.org/sdr/CALA2025061805654.md): Unknown · odor · Jun 16, 2025 · N496UA · Airbus A320232 · Air Distribution System
  > POSSIBLE FUME EVENT AFT GALLEY FA REPORTED AFT GALLEY BURNT POPCORN SMELL AFTER ENGINE START APU SHUT DOWN, FOR A FEW MINUTES, A/C UNDER ITS POWER RETURNED TO GATE, SMELL DISSAPATED BEFORE ARRIVAL AT GATE AND ENGINE SHUT DOWN. CHECKED AFT LAVS AN UNDER VANITY
- [SDR CALA2025051904766](https://openairdocs.org/sdr/CALA2025051904766.md): Slide · unknown · May 15, 2025 · N496UA · Airbus A320232 · Escape Slide
  > O/B FA REPORT: R1 DOOR SLIDE MATERIAL HANGING LOW. INSPECTION OF THE R1 DOOR SLIDE CHECK GOOD REF AMM TASK 25-62-44-000-803-A, OPS CHECK GOOD.
- [SDR CALA2025042804277](https://openairdocs.org/sdr/CALA2025042804277.md): Frame · cracked · Apr 24, 2025 · N496UA · Airbus A320232 · Fuselage Main, Frame
  > RH FR 16 DOUBLE JOGGLE HOLE 7 HAS 2EA CRACK INDICATIONS IN FRAME LAYER ONLY 80% S.H.
- [SDR CALA2025042804276](https://openairdocs.org/sdr/CALA2025042804276.md): Frame · corroded · Apr 24, 2025 · N496UA · Airbus A320232 · Fuselage Main, Frame
  > FUSELAGE UNDERFLOOR AFT FACE OF FR 67 HAS CORROSION B/W LSTR42 A ND RSTR42.
- [SDR CALA2025041803986](https://openairdocs.org/sdr/CALA2025041803986.md): Angle · cracked · Apr 17, 2025 · N496UA · Airbus A320232 · Wing Miscellaneous Structure
  > LEFT WING FIXED L/E INNER BOTTOM ANGLE HAS CRACK AT FR 15. RMVD AND RPLD L/W FIXED L/E INNER BOTTOM ANGLE AT FR15 IAW A320 SRM 51-72-11-911-002.
- [SDR CALA2022072901922](https://openairdocs.org/sdr/CALA2022072901922.md): Stringer · corroded · Jul 27, 2022 · N496UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > RH STRINGER 31R AT FR65 HAS CORROSION PER HAECO LCQ N/R 9294637/ 40637 GEN BY N078625 RMVD AND RPLD STINGER AT R/H STR 31 AT FR65-66 PER A320 SRM 51-7 2-11 AFT CARGO BAY BY MECH V061737 INSP BY N078625
- [SDR CALA2022072901921](https://openairdocs.org/sdr/CALA2022072901921.md): Frame · cracked · Jul 27, 2022 · N496UA · Airbus A320232 · Fuselage Main, Frame
  > R/H FR16 DOUBLE JOGGLE UPPER HOLE #1 AND #5 HAS A CRACK INDICATI ON PER HAECO LCQ N/R 9294348/40348 GEN BY V061632 LP USED FOR SDR REPORTING ONLY, REF LP 9072984 FOR REPAIR DETAIL & DIP REQUIREMENTS.
- [SDR CALA2022071801801](https://openairdocs.org/sdr/CALA2022071801801.md): Door Sill · corroded · Jul 17, 2022 · N496UA · Airbus A320232 · Fuselage Main, Structure
  > AFT WET AREA FR66 DOOR SILL -Y1732 CORRODED. GENERATED AT HAECO LCQ PER NR 9294473 (40473) BY V061629 {A3NB-53-3-686} REMOVED AND REPLACED R-2 DOOR SILL AFT WET AREA PER A320 51-42-1 1/001. PERFORMED BY V061737 INSP BY V919150.
- [SDR CALA2022071801785](https://openairdocs.org/sdr/CALA2022071801785.md): Stringer · corroded · Jul 16, 2022 · N496UA · Airbus A320232 · Fuselage Main, Structure
  > MAIN CABIN R2 DOOR CUTOUT FR 68 FORWARD FACE AND FASTENER HOLE A T STRG 23R HAS CORROSION. GENERATED BY V917055 ON HAECO LCQ NR 9 294582/40582.098" MAXIMUM ALLOWED =.02". REMOVED =.035" W=.700" L=.500". 50% OF NOMINAL. INSTALLED REPAIR PART IAW SRM 53-41-1
- [SDR CALA2022071801791](https://openairdocs.org/sdr/CALA2022071801791.md): Stringer · cracked · Jul 16, 2022 · N496UA · Airbus A320232 · Fuselage Main, Structure
  > FR 35 STR30 RH HOLE #2 HAS OUT OF ROUND CONDITION UNABLE TO INSP FOR CRACKS REQUIRES ROTO SCAN AFTER HOLE BECOMING ROUND AND TRUE A3NB-53-3-6315 PER HAECO LCQ N/R 9294111/40111 GEN BY V892444 ER. STEP REAMED HOLE TO 0.3710IN AND VERIFIED THE HOLE IS ROUND. 15I
- [SDR CALA2022071801790](https://openairdocs.org/sdr/CALA2022071801790.md): Frame · cracked · Jul 16, 2022 · N496UA · Airbus A320232 · Fuselage Main, Frame
  > R/H FR16 DOUBLE JOGGLE UPPER HOLE #1 AND #5 HAS A CRACK INDICATI ON A3NB-53-4-0024 PER HAECO LCQ N/R 9294348/40348 GEN BY V061632
- [SDR CALA2022071801789](https://openairdocs.org/sdr/CALA2022071801789.md): None · cracked · Jul 16, 2022 · N496UA · Airbus A320232 · Fuselage Structure (General)
  > LH FR16 UPPER DOUBLE JOGGLE HOLE #1 HAS A CRACK INDICATION REPAIR NEXT FLIGHT PER A3NB-53-4-0002 AD RELATED AD 2020-20-05 PER NR 9294350/40350 ACCOMPLISHED REPAIR INSTRUCTIONS PER HAECO REO L23956 REV IR WIT H NO DEVIATIONS ON DUCTED BY EC/RA 5311-02846 CAT A
- [SDR CALA2022071801788](https://openairdocs.org/sdr/CALA2022071801788.md): None · cracked · Jul 16, 2022 · N496UA · Airbus A320232 · Fuselage Main, Frame
  > R/H FR16 DOUBLE JOGGLE LOWER HOLE #11 AND #19 HAS A CRACK INDICATION A3NB-53-4-00249(AD 2020-20-05) PER HAECO LCQ N/R 9294349/40 349 GEN BY V061632
- [SDR CALA2022071801787](https://openairdocs.org/sdr/CALA2022071801787.md): None · cracked · Jul 16, 2022 · N496UA · Airbus A320232 · Fuselage Structure (General)
  > LH FR16 LOWER DOUBLE JOGGLE HOLE #11 AND #19 HAS A CRACK INDICATION A3NB-53-4-0002 AD RELATED AD2020-20-05 PER NR9294351/40351 G EN BY V061632 ACP REPAIR INSTRUCTIONS PER HAECO REO L23956 REV IR WITH NO DEVI AITONS AS DUNCTED BY ECRA 5311-02846 CAT A REPAIR BY
- [SDR CALA2022071501742](https://openairdocs.org/sdr/CALA2022071501742.md): Intercostal · cracked · Jul 13, 2022 · N496UA · Airbus A320232 · Fuselage Main, Frame
  > R1 DOOR FR16 DOOR STOP HAS CRACK INDICATION IN I/B UPPER HOLE AT THE 6 O''CLOCK POSITION IN THE INTERCOSTAL AND THE I/B LOWER HOL E AT THE 7 O''CLOCK POSITION IN THE INTERCOSTAL. AD 2022-02-11. G NERATED BY V061632 AT HAECO LCQ PER NR 9294284 (40284). REPLACED
- [SDR CALA2022071501741](https://openairdocs.org/sdr/CALA2022071501741.md): Intercostal · cracked · Jul 13, 2022 · N496UA · Airbus A320232 · Fuselage Main, Frame
  > L1 DOOR FR16 DOOR STEP #7 HAS CRACK INDICATIONS IN I/B UPPER HOL E AT THE 3 O''CLOCK POSITION IN THE INTERCOSTAL AND I/B LOWER HOL E AT THE 5 O''CLOCK POSITION IN THE INTERCOSTAL. GENERATED BY V06 1632, AT HAECO LCQ PER NR 9294283(40283) REPLACED INTERCOSTAL I
- [SDR CALA2022071101694](https://openairdocs.org/sdr/CALA2022071101694.md): Angle · corroded · Jul 8, 2022 · N496UA · Airbus A320232 · Fuselage Main, Structure
  > AFT WET AREA LH FR68 DOOR SILL 3EA FASTENER HOLES/NUTPLATES CORR ODED A3NB-53-3-6186 GENERATED BY V061629 AT HAECO LCQ PER NR 929 4481 (40481) CUT OUT CORRODED AREA FABRICATED REPAIR ANGLE SHIM AND INSTALLED REPAIR ANGLE AND SHINE AT FR68 LEFT HAND IAW A320 SM
- [SDR CALA2022071101695](https://openairdocs.org/sdr/CALA2022071101695.md): Shear Plate · corroded · Jul 8, 2022 · N496UA · Airbus A320232 · Fuselage Main, Structure
  > AFT WET AREA RH FR68-FR69 SHEAR PLATE CORRODED CORRODED - A3NB-5 3-3-6186 GENERATED BY V061629 AT HAECO LCQ PER NR 9294474 (40474) REMOVED AND REPLACED SHEAR PLATE AT FR68-69 IAW A320 SRM 51-42-1 1 DOT REMOVED PERFORMED BY V061765 INSP BY V917055
- [SDR CALA2022070601653](https://openairdocs.org/sdr/CALA2022070601653.md): Fitting · worn · Jul 4, 2022 · N496UA · Airbus A300* · Standard Practices/Structures
  > #2 RUDDER HINGE BUSHING IS WORN BEARING FALLS THRU. GENERATED AT HAECO LCQ PER NR 9294395 (40395) BY N078625. {A3NB-55-3-6022} REMOVED AND REPLACED RUDDER HINGE FITTING #2 IAW A320 SRM 51-42- 11-001, SRM 51-72-11-911-002, SRM 51-49-001/001. PERFORMED BY V9 319
- [SDR CALA2020032000634](https://openairdocs.org/sdr/CALA2020032000634.md): Bushing · migrated · Mar 11, 2020 · N496UA · Airbus A320232 · Landing Gear Actuator
  > L/H & R/H MLG ACTUATOR FITTINGS HAVE MIGRATED BUSHINGS, SUPPORT TASK, AS PER HAECO LCQ NR 9294134 (34134), GENERATED BY MECH V07 1330 RMVD & RPLCD L/H MLG ACTUATOR BUSHING & R/H MLG UPPER FWD FITTIN G IAW A320 SRM 51-42-11-801 & REPAIR INSTRUCTION R533-70501E,
- [SDR CALA2020032000633](https://openairdocs.org/sdr/CALA2020032000633.md): Battery · failed · Mar 11, 2020 · N496UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHTING FAILS FOR 13WL UNIT FAULT. (A3NB-33-3-6012) O N HAECO LCQ NR 9294362 GENERATED BY V894373. REMOVED AND REPLACED BWL EPSU AND EPSU BETTERY IAW A320 AMM 33-5 1-38-000-001-A, 33-51-38-400-001-A, 33-51-38-000-002-A, 33-51-38 -400-002-A. OPS CHEC
- [SDR CALA2020032000620](https://openairdocs.org/sdr/CALA2020032000620.md): Bulkhead · cracked · Mar 10, 2020 · N496UA · Airbus A320232 · Fuselage Main, Bulkhead
  > R/H SIDE PRESSURE PANEL FRAME 35-36 HAS CRACKED/REJECTABLE HOLES IN PROFILE PANEL #3, 4, 5, 6, 7, 9, 10 HOLES IN BEAM #37, 49, 5 8, 61, 62, 63, 64, 67 - SUPPORT TASK: AD RELATED (AD 2018-06-04) - ON HAECO LCQ NR 9294218 GENERATED. ACCOMPLISH A PERMANENT REPAIR
- [SDR CALA2019082301428](https://openairdocs.org/sdr/CALA2019082301428.md): Solenoid · failed · Aug 23, 2019 · N496UA · Airbus A320232 · Compressor Bleed Control
  > NR 2 ENGINE COMPRESSOR STALLED. CLEARED WITHOUT THROTTLE MOVEMENT. ACP TSM 71-00-00-810-809 WITH THE EXCEPTION OF LUBE/INSP 2.5 BLEED SYSTEM (ITEM4D8) AND POWER ASSURANCE TEST (4D10). FOUND 7B BLEED SOLENOID WEAK AND REPLACED. ALL OTHER INSPECTIONS PASSED W
- [SDR CALA20190821401](https://openairdocs.org/sdr/CALA20190821401.md): Eec · unknown · Aug 20, 2019 · N496UA · Airbus A320232 · Engine Fuel and Control
  > NR 2 EEC INCORECT REPORTING OF STALL. PB SENSE LINE WAS PRESSURE CHECKED FOR LEAKS, NO LEAKS NOTED, LINE HELD PRESSURE FOR 15 MINUTES.
- [SDR CALA2018021100603](https://openairdocs.org/sdr/CALA2018021100603.md): Slide · delaminated · Feb 11, 2018 · N496UA · Airbus A320232 · Escape Slide
  > LT OW SLIDE ASSY OUTER PANEL DELAMMED. REPLACED OW LT SLIDE ASSY PER AMM 53-35-11-400-001-A.
- [SDR CALA2017120204290](https://openairdocs.org/sdr/CALA2017120204290.md): Sdac · leaking · Dec 2, 2017 · N496UA · Airbus A320232 · Hydraulic System, Main
  > ECAM WARNING "G RSVR LO LVL". EMERGENCY DECLARED. REF TSM 29-11-00-810-803, POSSIBLE SDAC ISSUE. RMVD AND RPLD SDAC 1 (1WV1) PER AMM 31-55-34-000-001-A AND 400- 001-A. OPS CHKD OK PER AMM 31-50-00-710-001-A.
- [SDR CALA2017111004018](https://openairdocs.org/sdr/CALA2017111004018.md): Wire Harness · faulty · Nov 10, 2017 · N496UA · Airbus A320232 · Light System Wiring
  > EMERGENCY LIGHT INOPERATIVE. REPLACED THE EMERGENCY LIGHT AT SEAT 23C, WIRE HARNESS. OPS CHECKED GOOD.
- [SDR CALA2017081102626](https://openairdocs.org/sdr/CALA2017081102626.md): Power Supply · no test · Aug 11, 2017 · N496UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAILED ON 2 SERVICE CHECK. REPLACED THE ESPU AND BATTERY, OP CHECKED NORMAL.
- [SDR CALA2017052601601](https://openairdocs.org/sdr/CALA2017052601601.md): Controller · no test · May 26, 2017 · N496UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT FAILED A TEST. R & R THE BATTERY CONTROLER AND BATTERY PACK IAW AMM 33-51-38. TESTED OK
- [SDR CALA2017052201536](https://openairdocs.org/sdr/CALA2017052201536.md): Slide · cracked · May 22, 2017 · N496UA · Airbus A320232 · Escape Slide
  > RAMP REPORTS CRACKS AROUND ALL UPPER ATTACHMENT FASTENERS FOR RT OVERWING ESCAPE SLIDE. REMOVED AND REPLACED RT OVER WING SLIDE REF AMM25-62-42-400-001-A AND AMM 25-62-42-000-001-A.
- [SDR CALA2017050501262](https://openairdocs.org/sdr/CALA2017050501262.md): Connector · loose · May 5, 2017 · N496UA · Airbus A320232 · Equipment/Furnishings Wiring
  > REAR OVEN CB R41 POPPED F/A SMELLED ELECTRICAL SMELL. NO VISIBLE SMOKE. T/S IAW AWM 25-33-01 AND AWM 25-33-04. FOUND CONNECTOR 9003ML4 LOOSE AND RESECURED. ALSO CHANGED CB 9008ML4 AS PRECAUTIONARY FOR OVEN R41 IAW ESPM 20-46-00/10 AND WDM 25-33-04. OPS CHECK O
- [SDR CALA2017040400806](https://openairdocs.org/sdr/CALA2017040400806.md): Oven · inoperative · Apr 4, 2017 · N496UA · Airbus A320232 · Buffet/Galleys
  > GALLEY OVEN INOP AT R42 OVEN R42 IN AFT GALLEY TRIPPED BREAKER R42. PLASTIC BURN SMELL ASSOC BUT DISSIPATED. REPLACED R42 GALLEY OVEN, OPS CHK GOOD.
- [SDR CALA2017010600021](https://openairdocs.org/sdr/CALA2017010600021.md): Fan · faulty · Jan 6, 2017 · N496UA · Airbus A320232 · Air Distribution Fan
  > AVIONICS VENT EXHAUST FAN CB TRIPPED. SMOKE IN COCKPIT, FAN 18HQ FAULT CB POPPED COMPLIED WITH MEL CARD 2126AB. OK TO MEL FAN REPLACED AV EXHAUST FAN REF MM 21-26-51. TESTS GOOD.
- [SDR CALA2016123001188](https://openairdocs.org/sdr/CALA2016123001188.md): Outflow Valve · faulty · Dec 30, 2016 · N496UA · Airbus A320232 · Pressure Regulator/Outflow Valve
  > EXCESS CABIN ALTITUDE DISPLAYED ON UPPER ECAM SCREEN.. EMERGENCY DECLARED. REPLACED OUTFLOW VALVE AND #1 CABIM PRESSURE CONTROLER REF AMM 2 1-31-51 AND AMM 21-31-34 OPS CHECK GOOD REF AMM 21-31-51,21-31- 00,TASK 05-53-00,AMM 21-31-00-710-0032-A
- [SDR CALA2015102094599](https://openairdocs.org/sdr/CALA2015102094599.md): Pressure Switch · faulty · Oct 17, 2015 · N496UA · Airbus A320232 · APU Oil System
  > APU AUTO SHUTDOWN EN-ROUTE, RESTART NO GOOD. REPLACED OIL PRESS SWITCH & CONFIRMED OIL QTY SERVICED TO FULL.
- [SDR CALA2015041393523](https://openairdocs.org/sdr/CALA2015041393523.md): Valve · faulted · Apr 12, 2015 · N496UA · Airbus A320232 · Pressure Regulator/Outflow Valve
  > RETURNING TO FIELD DUE TO UNABLE TO PRESSURIZE. SKIN VLV FAULT. ALSO REF DF96 SKIN EXCH INLET BYPASS VLV CURRENTLY ON MEL. PFR SHOWS SEVERAL FAULTS VENT AVNCS SYS FAULT, VENT SKIN VLV FAULT & VENT BLOWER FAULT. CFDS MSGS, INLET BYPASS V16HQ, SKIN AIR OUTLE
- [SDR CALA2015033093489](https://openairdocs.org/sdr/CALA2015033093489.md): Battery · failed · Mar 23, 2015 · N496UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY CAP TEST FAILS. REPLACED 10WL & 12WL IAW AMM 33-51-38-000-002-A & 33-51-38-400-002-A. CAPACITY TEST OK IAW AMM 33-51-00-710-003.
- [SDR CALA2014112492729](https://openairdocs.org/sdr/CALA2014112492729.md): Threshold · corroded · Nov 18, 2014 · N496UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CARGO DOORWAY THRESHOLD CORRODED FRAME 52 - 56 AT STRINGER 38R. REPLACED AFT CARGO THRESHOLD FROM FRAME 52 - 56 IAW SRM 51-42-11.
- [SDR CALA2014112492736](https://openairdocs.org/sdr/CALA2014112492736.md): Stringer · corroded · Nov 17, 2014 · N496UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FORWARD CARGO INNER AFT BILGE AREA HAS CORROSION ON STRINGER AROUND RIVET HOLES AS MARKED 1 TO 6 INCHES FWD OF FRAME 34. R & R STRINGER 44 FROM FRAME 30 & 31 TO END FITTING AT FRAME 35 IAW SRM 5 1-42-11.
- [SDR CALA2014112492735](https://openairdocs.org/sdr/CALA2014112492735.md): Stringer · corroded · Nov 17, 2014 · N496UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FORWARD CARGO INNER AFT BILGE AREA HAS CORROSION ON STRINGER 43R AROUND RIVET HOLES AS MARKED 1 TO 4 INCHES FWD OF FRAME 34. R & R WITH NEW STRINGER FROM FRAME 30 TO 35 IAW SRM 51-42-11.
- [SDR CALA2014112492733](https://openairdocs.org/sdr/CALA2014112492733.md): Stringer · corroded · Nov 17, 2014 · N496UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FORWARD CARGO INNER AFT BILGE AREA HAS CORROSION ON STRINGER 43L AROUND RIVET HOLE AS MARKED 1 TO 4 INCHES FWD OF FRAME 34. R & R WITH NEW STRINGER FROM FRAME 31 - 35 IAW SRM 51-42-11.
- [SDR CALA2014111492705](https://openairdocs.org/sdr/CALA2014111492705.md): Stringer · corroded · Nov 13, 2014 · N496UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FORWARD CARGO INNER AFT BILGE AREA HAS CORROSION ON STRINGER 24L AROUND RIVETS HOLES AS MARKED 4 TO 8 INCHES FWD OF FRAME 34. R & R WITH NEW FACTORY STRINGER 24 LT FROM FRAME 30 TO 34 IAW SRM 51-42-11.
- [SDR CALA2014111492704](https://openairdocs.org/sdr/CALA2014111492704.md): Stringer · corroded · Nov 13, 2014 · N496UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO FLOOR LT SIDE AT FRAME 63 TO 64 STRINGER 41 LT HAS CORROSION. R & R WITH NEW FACTORY STRINGER 41 LT FROM FRAME 60 TO 64 IAW SRM 51- 42-11.
- [SDR CALA2014111492703](https://openairdocs.org/sdr/CALA2014111492703.md): Stringer · corroded · Nov 13, 2014 · N496UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO FLOOR RT SIDE AT FRAME 63 TO 64 STRINGER 42 RT HAS CORROSION. R & R WITH NEW FACTORY STRINGER 42 RT FROM FRAME 60 TO 64 IAW SRM 51- 42-11.
- [SDR CALA2014111092678](https://openairdocs.org/sdr/CALA2014111092678.md): Door Sill · corroded · Nov 9, 2014 · N496UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > L2 DOORSILL CORRODED AT GIRT BAR ATTACH HOLES. L2 DOORSILL REPLACED IAW SRM 51-42-11.
- [SDR CALA2014111092677](https://openairdocs.org/sdr/CALA2014111092677.md): Stringer · corroded · Nov 9, 2014 · N496UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT PIT STRINGER 42L CORRODED BETWEEN FRAME 63 & 64. STRINGER 42L REPLACED BETWEEN FACTORY SPLICES AT FRAME 60 & 64 IAW SRM 51-42-11.

Next page: https://openairdocs.org/aircraft/N496UA/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 = 'N496UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N496UA/reports

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