# Service difficulty reports: N235NV

A list on [N235NV](https://openairdocs.org/aircraft/N235NV.md).

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

- [SDR WX0A2026081232919](https://openairdocs.org/sdr/WX0A2026081232919.md): Flashlight · inoperative · Aug 9, 2026 · N235NV · Airbus A320214 · Emergency Equipment
  > (AIRCRAFT NOT GROUNDED) FWD FA FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FWD FA FLASHLIGHT P2-07-003-001, IAW CMM 25-60-02. THIS WILL LCEAR MEL PLACARD REMOVED OK FOR SERVICE. MDDR 236279.
- [SDR WX0A2026071332891](https://openairdocs.org/sdr/WX0A2026071332891.md): Light · inoperative · Jul 10, 2026 · N235NV · Airbus A320214 · Emergency Lighting
  > (AIRCRAFT NOT GROUNDED) ON EMERGENCY EQUIPMENT CHECK ON WEEKLY, FOUND L1, R1 DOOR LOWER EXIT LIGHTS INOP. REPLACEMENT REQUIRED / PER TSM 33-51-00-810-814-A STEP 4.A.(3) REMOVED AND REPLACED PSU (110WL1) REF AMM 33-51-39-000-001-A AND 33-51-39-400-001-A. OPS T
- [SDR WX0A2026032732767](https://openairdocs.org/sdr/WX0A2026032732767.md): Light · inoperative · Mar 25, 2026 · N235NV · Airbus A320214 · Emergency Lighting
  > (AIRCRAFT NOT GROUNDED) ON CABIN WALK THROUGH, FOUND R1 DOOR SIDE-WALL LOWER EXIT LIGHT DOES NOT ILLUMINATE DURING EMERGENCY LIGHT TEST. (FIN 90WL2) / REMOVED AND REPLACED R1 OOR LOWER EXIT LIGHT REF AMM 33-51-13-000-001A & 33-51-13-400-001A. OPS CK GOOD AT T
- [SDR WX0A2026022332737](https://openairdocs.org/sdr/WX0A2026022332737.md): Control Unit · intermittent · Feb 20, 2026 · N235NV · Airbus A320214 · Power Lever
  > (EMERGENCY DECLARED) (AIRCRAFT NOT GROUNDED) ENG 1 THRUST LEVER DISAGREE ECAM TRANSIENT INITIALLY, STAYED ON AFTER MULTIPLE FAILURES. / PER TSM 76-11-00-810-813-A RMEOVED AND REPLACED CTL UNIT-THROTTLE, ENG 1 (8KS1) PER AMM 76-11-19-000-042A, AND AMM 76-11-19-
- [SDR WX0A2026012832717](https://openairdocs.org/sdr/WX0A2026012832717.md): Bulb · inoperative · Jan 26, 2026 · N235NV · Airbus A320214 · Emergency Lighting
  > (AIRCRAFT NOT GROUNDED) RIGHT OVERWING EXIT SIGN HAS INTERNAL BULB INOP / REMOVED EXIT SIGN, REPLACED LIGHT BULB AND INSTALLED EXIT SIGN IAW AMM 33-5-17-000-001-A AND AMM 33-51-17-400-001-A"
- [SDR EE4Y2026150123774](https://openairdocs.org/sdr/EE4Y2026150123774.md): Frame · cracked · Jan 15, 2026 · N235NV · Airbus A320214 · Fuselage Main, Structure
  > DURING THE ALLEGIANT TASK CARD A32X-53-260-004 INSPECTION, CRACK WAS FOUND ON FR 68, STOP NR1 FRAME INBD LOWER FASTENER HOLE. THIS DISCREPANCIE WAS REPORTED TO AIB AND REPAIRED UNDER AIRBUS DOCUMENT 81709985/036 AND PER COOPESA EO COO-EO-2025-23646-R02. JOB A1
- [SDR EE4Y2026150123773](https://openairdocs.org/sdr/EE4Y2026150123773.md): Frame · cracked · Jan 15, 2026 · N235NV · Airbus A320214 · Fuselage Main, Frame
  > DURING THE ALLEGIANT TASK CARD A32X-53-260-004 INSPECTION, CRACK WAS FOUND ON FR68, STRINGER 22L FRAME WEB HORIZONTAL FLANGE RADII. THIS DISCREPANCIE WAS REPORTED TO AIB AND REPAIRED UNDER AIRBUS DOCUMENT 81709985/036 AND PER COOPESA EO COO-EO-2025-23646-R02.
- [SDR EE4Y2026150123772](https://openairdocs.org/sdr/EE4Y2026150123772.md): Frame · cracked · Jan 15, 2026 · N235NV · Airbus A320214 · Fuselage Main, Frame
  > DURING THE ALLEGIANT TASK CARD A32X-53-260-005 / TASK CARD A32X-53-260-003 INSPECTION RELATED TO AD 2022-15-05 AND A320-53-1491 REV 01 IN THE UPPER FUSELAGE PASSENGER CABIN AREA, CRACK WAS FOUND AT FR68 / STOP FITTING #1. (INBD LOWER HOLE) LOCATION AND WAS REP
- [SDR EE4Y2026120123745](https://openairdocs.org/sdr/EE4Y2026120123745.md): Frame · cracked · Jan 12, 2026 · N235NV · Airbus A320214 · Fuselage Main, Frame
  > DURING THE ALLEGIANT TASK CARD A32X-53-260-005 / TASK CARD A32X-53-260-003 INSPECTION RELATED TO AD 2022-15-05 AND A320-53-1491 REV 01 IN THE UPPER FUSELAGE PAX CABIN AREA, TOW CRACKS FOUND AT FR68, S22R (FASTENER HOLE NR1 ON STOP FITTING 1 AND HORIZONTAL FLAN
- [SDR EE4Y2026090123724](https://openairdocs.org/sdr/EE4Y2026090123724.md): Door Frame · cracked · Jan 9, 2026 · N235NV · Airbus A320214 · Fuselage Main, Structure
  > DURING THE ACCOMPLISHMENT OF ALLEGIANT TASK A32X-E5316-0002 RELATED TO AD 2022-02-11 / SB53-1330/SB53-1339, IT WAS FOUND AT FR16/20 LH DOOR STOP FITTING FASTENER HOLES AREA WITH CRACK INDICATION AND FR16 RH DOOR STOP FITTING FASTENER HOLE AREA WITH CRACK INDIC
- [SDR EE4Y2026090123723](https://openairdocs.org/sdr/EE4Y2026090123723.md): Fitting · cracked · Jan 9, 2026 · N235NV · Airbus A320214 · Fuselage Main, Structure
  > DURING THE ALLEGIANT TASK A32X-53-210-003 INSTRUCTIONS RELATED TO AD 2020-17-03 / SB A320-53-1331 LT CONTINUITY FITTING WITH CRACK WAS FOUND. THIS CONDITION WAS REPORTED TO AIB AND THE PART WAS REPLACED IAW AIB MESSAGE 81706551/003 AND PER SB 53-1331.
- [SDR EE4Y2026080123722](https://openairdocs.org/sdr/EE4Y2026080123722.md): Frame · cracked · Jan 8, 2026 · N235NV · Airbus A320214 · Fuselage Main, Frame
  > DURING THE REF. B, ACCOMPLISHMENT RELATED TO REF. C, & D; HOLES AT LH FR20, HOLE 7 AND A UPPER CORNER WERE FOUND WITH CRACKS INDICATIONS. THIS CONDITION MUST BE REPORTED IAW SB 53-1379 REV. 00 TO AIRBUS. DUE TO IT, PERMANENT REPAIR PER ERO A32X-STR-53ERO-00470
- [SDR WX0A2025111432633](https://openairdocs.org/sdr/WX0A2025111432633.md): Lens · cracked · Nov 13, 2025 · N235NV · Airbus A320214 · Emergency Lighting
  > (AIRCRAFT NOT GROUNDED) DURING EMERGENCY EQUIPMENT CHECK, FOUND R2 DOOR FLOOR EMERGENCY EXIT LIGHT LENSE CRACKED. / REPLACED EXIT MARKER AT R2 DOOR IAW AMM 33-51-13-000-001-A AND 33-51-13-400-001-A. OPS CHECK GOOD.
- [SDR WX0A2025092232572](https://openairdocs.org/sdr/WX0A2025092232572.md): Light · inoperative · Sep 20, 2025 · N235NV · Airbus A320214 · Emergency Lighting
  > (AIRCRAFT NOT GROUNDED) L2 AND R2 LOWER WALL MOUNTED EXIT MARKING SIGN INOP, REF TSM 33-51-00-810-814-A, PERFORMED AN OPERATIONAL TEST OF CABIN EMERGENCY LIGHTS AND SIGNS IAW MM 33-51-00-710-009-A. BOTH LOWER DOORS L2 AND R2 WALL MOUNTED EXIT SIGNS DID NOT CO
- [SDR WX0A1900010032396](https://openairdocs.org/sdr/WX0A1900010032396.md): Oil System · leaking · Apr 19, 2025 · N235NV · Airbus A320214 · APU Oil System
  > (AIRCRAFT NOT GROUNDED) FA'S STATE ""DIRTY SOCK SMELL"" FROM TAXI UNTIL APPROX 10,000FT / PERFORMED TC 21-00-002. NO DISCREPENCIES FOUND. PER TC 21-00-002 THIS CLEARS MEL 49-10-01-A MDDR# 211203. INOP PLACARDS REMOVED. NO 'M' PROCEDURES. M313 BEING GENERATED F
- [SDR WX0A2024110632211](https://openairdocs.org/sdr/WX0A2024110632211.md): Bellows · failed · Nov 4, 2024 · N235NV · Airbus A320214 · Air Distribution System
  > (AIRCRAFT NOT GROUNDED) AFT FLIGHT ATTENDENT REPORTED A DIRTY SOCK ODER DURING DESCENT THROUGH 9000 FEET. MID CABIN THROUGH AFT GALLEY / LH OZONE FILTER REMOVED, RH OZONE FILTER REMOVED, REPLACED SLEEVE (BELLOWS) ON CONDENSER W/REF AMM 21-52-32-400-001-A. (RE
- [SDR WX0A2023102031870](https://openairdocs.org/sdr/WX0A2023102031870.md): Unknown · unknown · Oct 18, 2023 · N235NV · Airbus A320214 · Emergency Lighting
  > ALL EMERGENCY LIGHT EXIT LOCATION SIGNS HAVE MULTIPLE LIGHTS INOP. / REMOVED AND REPLACED ALL INOP LAMPS IN CABIN EMERGENCY EXIT LOCATION SIGNS REF AMM 33-51-17-000-001-A AND 33-51-17-400-001-A"
- [SDR WX0A2023082131818](https://openairdocs.org/sdr/WX0A2023082131818.md): Epsu · unknown · Aug 20, 2023 · N235NV · Airbus A320214 · Emergency Lighting
  > FOUND LOWER EMERGENCY EXIT LIGHTS ON BOTH SIDES OF CABIN INTERIOR WOULD NOT ILLUMINATE. / REMOVED AND REPLACED L/H CABIN EPSU BATTERY 11WL0 IAW AMM 33-51-38-000-002-A & AMM 33-51-38-400-002-A. EMERGENCY EXIT LIGHT CHECK GOOD."
- [SDR WX0A2023080931812](https://openairdocs.org/sdr/WX0A2023080931812.md): Epsu · unknown · Aug 9, 2023 · N235NV · Airbus A320214 · Emergency Lighting
  > FWD & RH CABIN EMERGENCY LIGHTING BATTERY FAILED CABIN EMERGENCY LIGHTING TEST. / REMOVED AND REPLACED FWD & RH CABIN EMERGENCY LIGHTING BATTERY IAW AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A. OPS CHECK SATISFACTORY."
- [SDR WX0A1900010031755](https://openairdocs.org/sdr/WX0A1900010031755.md): Unknown · unknown · Apr 21, 2023 · N235NV · Airbus A320214 · Trailing Edge Flap Control System
  > (EMERGENCY DECLARED) F/CTL FLAPS FAULT ECAM WHEN SELECTING FLAPS 2 ON BASE. ECAM AND CHECKLIST WERE ACCOMPLISHED.LANDING AND ROLL OUT WAS NORMAL, BRAKES GOT TO 500 DEG C AFTER LANDING, NO ISSUES DURING COOLING // PERFORMED A BITE TEST OF SFCC1/2 IAW AMM 27-51-
- [SDR WX0A2021073073800](https://openairdocs.org/sdr/WX0A2021073073800.md): Controller · faulted · Aug 1, 2021 · N235NV · Airbus A320214 · Cabin Pressure Controller
  > CAB PR2 FAULT, ECAM PROC FOLLOWED. / R & R #2 CABIN PRESSURE CONTROLLER & OP TEST OK W/REF TSM 21-31-00-810-827A."
- [SDR WX0A2021061473738](https://openairdocs.org/sdr/WX0A2021061473738.md): Battery Pack · no test · Jun 13, 2021 · N235NV · Airbus A320214 · Emergency Lighting
  > EMERG BATT FIN 10WL FAILED CAP TEST / REMOVED AND REPLACED EMERG BATTER FIN 10WL IAW A320 AMM 33-51-38 OPS CHECK GOOD"
- [SDR WX0A2021061473737](https://openairdocs.org/sdr/WX0A2021061473737.md): Battery Pack · no test · Jun 13, 2021 · N235NV · Airbus A320214 · Emergency Lighting
  > EMERG BATT FIN 12WL FAILED CAP TEST / REMOVED AND REPLACED EMERG BATT, OPS CHECK GOOD IAW AMM 33-51-38 PB 401"
- [SDR WX0A2021061473736](https://openairdocs.org/sdr/WX0A2021061473736.md): Battery Pack · no test · Jun 13, 2021 · N235NV · Airbus A320214 · Emergency Lighting
  > EMERG BATT FIN 11WL FAILED CAP TEST / REMOVED AND REPLACED EMERG BATT FIN 11WL IAW A320 33-51-38 OPS CHECK GOOD"
- [SDR WX0A1900010073963](https://openairdocs.org/sdr/WX0A1900010073963.md): None · none · May 18, 2021 · N235NV · Airbus A320214 · Wing Main, Frame Structure
  > NRC 5000-0042: 1237-31. LH MAIN LANDING GEAR RETRACTION ACTUATOR ATTACHEMENT FITTING FOUND CORRODED ON LOWER SURFACE ARROUND THE BUSHING. / LH MLG RETRACTION, JACK ANCHORAGE FITTING REPAIRED IAW SRM 57-26-13-300-008. SEE AWS FOR REPAIR DETAILS. REPAIR CATEGORY
- [SDR WX0A1900010073962](https://openairdocs.org/sdr/WX0A1900010073962.md): None · none · May 18, 2021 · N235NV · Airbus A320214 · Wing, Plate/Skin
  > NRC 6000-0004: 211-2 R/H WING, HYDRAULIC PRESSURE LINE FEED THROUGH THE LOWER WING SKIN AT RIB 8 FWD OF FALSE SPAR HAS ELONGATED HOLE ELONGATED / R/H WING, PYLON MOUNTING PLATE BTW RIBS 7 AND 8 FWD OF FALSE SPAR PERMANENTLY REPAIRED IAW SRM 57-21-11-300-005. R
- [SDR WX0A1900010073961](https://openairdocs.org/sdr/WX0A1900010073961.md): None · none · May 18, 2021 · N235NV · Airbus A320214 · Fuselage Main, Plate/Skin
  > NRC 2000-0001: (274-2) JUST FWD OF R/H WINDSHIELD, BTWN FR3-4, DENT FOUND. / JUST FWD OF R/H WINDSHIELD BTW FR 3-4, DENT FOUND WITHIN LIMITS IAW SRM 53-00-11-283-005. REPAIR CATEGORY B, SEE SRI 53-00-11-205-050 FOR INSPECTION REQUIREMENTS. INSPECTION THRESHOLD
- [SDR WX0A1900010073960](https://openairdocs.org/sdr/WX0A1900010073960.md): None · none · May 18, 2021 · N235NV · Airbus A320214 · Fuselage, Wing Attach Fittings
  > NRC 1000-0110: 633-19 BULK CARGO DOOR CUTOUT LOWER SILL BEAM FR61 AND 62, NUT PLATE AREAS, CORROSION FOUND. / BULK CARGO DOOR CUTOUT LOWER SILL BEAM BTW FR 61 AND FR 62 AT NUT PLATES AREAS (QTY.2) PERMANENTLY REPAIRED IAW SRM 53-41-49-300-003. REPAIR CATEG
- [SDR WX0A2021050573704](https://openairdocs.org/sdr/WX0A2021050573704.md): Dummy Rail · corroded · Apr 23, 2021 · N235NV · Airbus A320214 · Fuselage, Seat/Cargo Attach Fittings
  > DURING THE S1 CHECK OF PASSENGER CABIN FLOOR STRUCTURE, CORROSION FOUND ON TRACK HARD POINT AT FR 16 AND Y503.2. / REPLACED PASSENGER CABIN FLOOR STRUCTURE DUMMY RAIL BEAM FR12- 16, Y503.2 PER IAW SRM 51-72-11-911-001."
- [SDR WX0A2021050573703](https://openairdocs.org/sdr/WX0A2021050573703.md): Door Sill · corroded · Apr 23, 2021 · N235NV · Airbus A320214 · Fuselage Miscellaneous Structure
  > DURING THE S1 CHECK OF FWD LH PASSENGER/CREW DOOR CUTOUT LOWER SILL, CORROSION FOUND ON BRACKET BTW FR 19-20 / REPLACED BRACKET BTW FR 19-20 ON FWD LH PASSENGER/CREW DOOR CUTOUT LOWER SILL PER SRM 51-42-11."
- [SDR WX0A2021050373694](https://openairdocs.org/sdr/WX0A2021050373694.md): Floor Support · corroded · Apr 20, 2021 · N235NV · Airbus A320214 · Fuselage Miscellaneous Structure
  > DURING THE S1 CHECK OF PASSENGER CABIN FLOOR STRUCTURE, FOUND CORROSION LOCATED ON LONGITUDINAL BEAM Y122 AT FR 66 AREA / REPLACED LONGITUDINAL BEAM BTW FR 64 - 66 AND Y122 PER SRM 51-72-11."
- [SDR WX0A2021021973648](https://openairdocs.org/sdr/WX0A2021021973648.md): Epsu · no test · Feb 17, 2021 · N235NV · Airbus A320214 · Emergency Lighting
  > CABIN EMERGENCY LIGHTING EPSU SYS TEST 10WL,11WL,12WL AND 13WL FAILED TEST /REMOVED AND REPLACED EMERGENY BATTERY PACK 10WL,11WL,12WL AND 13WL W/REF TO AMM 33-51-38 PB 401 OPS CHECK NORMAL.
- [SDR WX0A2020061273513](https://openairdocs.org/sdr/WX0A2020061273513.md): Light · inoperative · Jun 10, 2020 · N235NV · Airbus A320214 · Emergency Lighting
  > LT OVER WING EMERGENCY EXIT LIGHT INOP. REPLACED OVER WING EMERGENCY EXIT LIGHT.
- [SDR WX0A2020031373486](https://openairdocs.org/sdr/WX0A2020031373486.md): Controller · malfunctioned · Mar 11, 2020 · N235NV · Airbus A320214 · Cabin Pressure Controller
  > (EMERGENCY DECLARED) CAB PR SYS 1 FAULT AT CRUISE / REPLACED CABIN PRESS CONTROL UNIT "
- [SDR WX0A2020031373485](https://openairdocs.org/sdr/WX0A2020031373485.md): Controller · malfunctioned · Mar 11, 2020 · N235NV · Airbus A320214 · Cabin Pressure Controller
  > (EMERGENCY DECLARED) CAB PR SYS 1 FAULT AT CRUISE / REPLACED CABIN PRESS CONTROL UNIT "
- [SDR WX0A2020022473481](https://openairdocs.org/sdr/WX0A2020022473481.md): Computer · malfunctioned · Feb 22, 2020 · N235NV · Airbus A320214 · Trailing Edge Flap Control System
  > (EMERGENCY DECLARED) FLAP/CTL FLAPS FAULT ECAM MESSAGE FLAPS FAILED TO EXTEND /REPLACED SFCC #1. OPS CHECK GOOD."
- [SDR WX0A201906073396](https://openairdocs.org/sdr/WX0A201906073396.md): Regulator · malfunctioned · Jun 5, 2019 · N235NV · Airbus A320214 · Crew Oxygen System
  > (EMERGENCY DECLARED) IN CRUISE RECEIVED UNCOMMANDED O2 FLOW FROM FIRST OFFICERS MASK AT EXCESSIVE RATE. BLINKER LIGHTS ACTIVATED ON ALL OTHER MASKS O2 DEPLETED / REMOVED AND REPLACED PRESSURE REGULATOR"

## 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 = 'N235NV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N235NV/reports

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