# Service difficulty reports: N223NV, cancelled Mar 31, 2026

A list on [N223NV, cancelled Mar 31, 2026](https://openairdocs.org/deregistered/N223NV-2026-03-31.md).

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

- [SDR WX0A2025020332295](https://openairdocs.org/sdr/WX0A2025020332295.md): Hydraulic Line · leaking · Jan 31, 2025 · N223NV · Airbus A320214 · Smoke Detection
  > (AIRCRAFT GROUNDED) (EMERGENCY DECLARED) AIR RETURN FOR AFT CARGO SMOKE, RED LAND ASAP. CARGO SMOKE AFT AGENT DISCHARGED PER ECAM ALERT. REMOVED AND INSTALLED PANEL FIN 151LF IAW AMM 53-42-04. C/W THE INSTALLATION OF THE HYD LINE IAW AMM 20-23-11-300-001-A F
- [SDR EE4Y2023060917836](https://openairdocs.org/sdr/EE4Y2023060917836.md): Fence · corroded · Jun 9, 2023 · N223NV · Airbus A320214 · Standard Practices/Structures
  > DURING ALLEGIANT INSPECTION TASK ZL-500-02-1001 LEFT WING TIP FENCE INBOARD SURFACE HAS SPOT CORROSION AT FORWARD LOWER SECTION WAS FOUND. THE DAMAGE WAS REPAIRED IAW A320 SRM TASK 57-31-22-300-002 AND IS COVER WITH COOPESA JOB A1N113 ITEM 5-4.
- [SDR EE4Y2023100317405](https://openairdocs.org/sdr/EE4Y2023100317405.md): Unknown · unknown · Mar 10, 2023 · N223NV · Airbus A320214 · Fuselage Structure (General)
  > DURING THE ALLEGIANT EO # 53-120-003 ALLEGIANT EO INSTRUCTIONS ACCOMPLISHMENT WHICH IS RELATED WITH AD 2018-14-09 THERE WERE FOUND TWO (2 EA) FASTENER HOLES WITH CRACK INDICATION ON CROSSBEAM SPLICING AT FR 16 LHS (H8) AND AT FR 20 LHS (H26). WORK PERFORMED
- [SDR EE4Y2023100317404](https://openairdocs.org/sdr/EE4Y2023100317404.md): Unknown · unknown · Mar 10, 2023 · N223NV · Airbus A320214 · Fuselage Structure (General)
  > DURING THE ALLEGIANT EO # 53-120-003 ALLEGIANT EO INSTRUCTIONS ACCOMPLISHMENT WHICH IS RELATED WITH AD 2018-14-09 THERE WERE FOUND TWO (2 EA) FASTENER HOLES WITH CRACK INDICATION ON CROSSBEAM SPLICING AT FR 16 LHS (H8) AND AT FR 20 LHS (H26). WORK PERFORMED
- [SDR EE4Y2023031017406](https://openairdocs.org/sdr/EE4Y2023031017406.md): Skin Panel · corroded · Mar 10, 2023 · N223NV · Airbus A300* · Wing Structure
  > DURING THE STRUCTURAL INSPECTION PER ZL-500-03-1-002 CORROSION WAS FOUND AT LH WING REAR SPAR T/E OVERHANG AREA BETWEEN RIB 10 AND RIB 11+186MM ADDITIONAL CORROSION ON THE OVERHANG TOP SKIN LOWER SURFACE WAS NOTED AND A ZERO STRESS JACKING WITH SKIN SEPARATION
- [SDR WX0A2023021731732](https://openairdocs.org/sdr/WX0A2023021731732.md): Epsu · none · Feb 15, 2023 · N223NV · Airbus A320214 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS AND SIGNS INOP AT L1 AND R1 WHILE ON BATTERY POWER. / REMOVED AND REPLACED BATTS AND EPSU'S AT 10 WL &13WL REF AMM 33-51-38-000-001-A AND 33-51-38-400-001-A AND 33-51-38-000-002-A AND 33-51-38-400-002-A -BITE TEST OK REF AMM 33-51-00-710-
- [SDR WX0A1900010074058](https://openairdocs.org/sdr/WX0A1900010074058.md): Lubrication Unit · oil consumption · Apr 8, 2022 · N223NV · Airbus A320214 · Engine Oil Cooler
  > 1 WHILE REACHING 10,000 ' WE GOT A ENG # 2 ECAM ADVISORY OIL QUANTITY (3.5) WE FOLLOWED THE ADVISORY CHECK LIST AND INDICATION BECAME DOUBLE XX AMBER 2 ABOUT 3 MINUTES LATER WE GOT ENG # 2 ECAM ADVISORY PSI (DROP) 3 IT FOLLOWED BE AN ECAM ENG # 2 OIL LOW PRESS
- [SDR WX0A2021122773905](https://openairdocs.org/sdr/WX0A2021122773905.md): Dampener · low pressure · Dec 24, 2021 · N223NV · Airbus A320214 · Passenger/Crew Doors
  > L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. / SERVICED L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER FROM 1400PSI- 1700PSI."
- [SDR WX0A2021070573753](https://openairdocs.org/sdr/WX0A2021070573753.md): Battery Pack · not reported · Jul 3, 2021 · N223NV · Airbus A320214 · Emergency Lighting
  > ALL 4 EMERGENCY BATTERIES REQUIRE REPLACEMENT FOR 1A PHASE 1 CHECK / R/R ALL 4 EMERGENCY BATTERIES FOR 1A PHASE 1 CHECK REF AMM 33-51-38 PB 401 OPS CHECK GOOD"
- [SDR WX0A2020082173559](https://openairdocs.org/sdr/WX0A2020082173559.md): Damper · leaking · Aug 19, 2020 · N223NV · Airbus A320214 · Passenger/Crew Doors
  > L1 DOOR DAMPER AND EMERGENCY- OPERATION CYLINDER PRESSURE AND FOUND IT TO BE @ 1000 PSI. SUSPECT INTERNAL LEAK. / R&R'D L1 DOOR-DAMPER EMERGENCY OPERATION CYLINDER IAW AMM 52-11-14-000-001-B AND 52-11-14-400-001-B NO RIG/ADJUSTMENT PERFORMED. OPS CHECK GOOD."
- [SDR WX0A2020060863512](https://openairdocs.org/sdr/WX0A2020060863512.md): Megaphone · inoperative · Jun 6, 2020 · N223NV · Airbus A320214 · Emergency Equipment
  > MEGAPHONE IS INOP / REPLACED FWD MEGAPHONE"
- [SDR WX0A2020011373456](https://openairdocs.org/sdr/WX0A2020011373456.md): Light · unsecure · Jan 11, 2020 · N223NV · Airbus A320214 · Emergency Lighting
  > FA REPORTS ESCAPE PATH LIGHTING ON FLOOR MID A/C EXITS CAME OFF. RE-SECURED ESCAPE STRIP LIGHTING ON MID FLOOR A/C EXITS IAW AMM 25-60-00.
- [SDR WX0A2017011800001](https://openairdocs.org/sdr/WX0A2017011800001.md): Unknown · smoke · Jan 17, 2017 · N223NV · Airbus A320214 · Air Distribution System
  > HEAVY CABIN SMOKE STARTING FROM AFT CABIN NEAR LAV TO FLIGHT DECK. INSPECTED ENGINE WITH NO DEFECTS NOTED. RAN APU AND ENGINES AND COULD NOT DUPLICATE.
- [SDR WX0A2016112873204](https://openairdocs.org/sdr/WX0A2016112873204.md): Control System · failed · Nov 25, 2016 · N223NV · Airbus A320214 · Trailing Edge Flap Control System
  > F/CTL FLAPS LOCKED ECAM DURING RETRACTION FROM CONFIG 2 TO CONFIG 1. DUE TO F/CTL FLAP SYS 2 FAIL ON PFR R&R SFCC 2.
- [SDR WX0A2015090972855](https://openairdocs.org/sdr/WX0A2015090972855.md): Unknown · odor · Sep 6, 2015 · N223NV · Airbus A320214 · Passenger Compartment Equipment
  > AFTER ENG START & THROUGHOUT FLIGHT, AFT FLIGHT ATTENDANTS REPORTED ELEC BURNT RUBBER SMELL COMING FROM L2 DOOR, JUMP SEAT AREA. SEE PREVIOUS PAGE. DETERMINED SMELL COMING FROM A SEALED COMPARTMENT BY L2 DOOR, FLIGHT ATTENDANT JUMP SEAT, RUBBER FROM INSIDE O
- [SDR WX0A2015090972854](https://openairdocs.org/sdr/WX0A2015090972854.md): Unknown · odor · Sep 6, 2015 · N223NV · Airbus A320214 · Air Distribution System
  > AFTER TAKEOFF, AFT FLIGHT ATTENDANT NOTED A SMELL, ELEC OR LIKE A BURNT RUBBER SMELL. THE SMELL ONLY DETECTED FROM L2 JUMP SEAT. NOW COME BACK INTERMITTENTLY FOR ONE H & FULL DISSIPATED APPROX 30 MIN PRIOR TO TOUCHDOWN. CHECKED ALL LIGHTS, SOCKETS & CHECKED
- [SDR WX0A2015061572652](https://openairdocs.org/sdr/WX0A2015061572652.md): Acoustic Panel · damaged · Jun 9, 2015 · N223NV · Airbus A320214 · Turbine Engine Air Inlet Section
  > LEFT ENG HAS DAMAGE IN 1 PLACE TP FWD ACOUSTIC PANEL AT 12 O'CLOCK POSITION ON INTAKE. REPAIRED PANEL IAW EB-SR NO 001318971001 NR 11636. REINSTALLED PANELS IAW AMM 72-23-00. IAW EB-SR-NO, 00131897001 REQUIRES REINSPECTION WITHIN 50 FLIGHT HOURS & REPLACEMEN
- [SDR WX0A2015061072644](https://openairdocs.org/sdr/WX0A2015061072644.md): Warning System · false activation · Jun 6, 2015 · N223NV · Airbus A320214 · Windshield/Door Rain/Ice Removal
  > IN THE CLIMB, RECEIVED ANTI-ICE RT WINDSHIELD ECAM & MASTER CAUTION. REFERENCED AOM 18.2.30.1, NO FURTHER ACTION. PERFORMED TROUBLESHOOTING IAW TSM 30-42-00-810-804A & FOUND OHMS TO BE WITHIN RANGE UNDER ACFT PRESSURIZATION. OPERATIONS TESTED GOOD ON BOTH
- [SDR WX0A2015051172586](https://openairdocs.org/sdr/WX0A2015051172586.md): Warning System · false activation · May 8, 2015 · N223NV · Airbus A320214 · Door Warning System
  > ABORTED TAKEOFF AT 79KTS FOR MATER CAUTION WITH ECAM, DOOR LT AFT CABIN. DEFERRED IAW MEL 527001B CAT C.

## 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 = 'N223NV' AND deregistration_id = 'N223NV-2026-03-31'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N223NV-2026-03-31/reports

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