# Service difficulty reports: N288NV

A list on [N288NV](https://openairdocs.org/aircraft/N288NV.md).

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

- [SDR WX0A2025110332623](https://openairdocs.org/sdr/WX0A2025110332623.md): Power Supply · no test · Nov 3, 2025 · N288NV · Airbus A320214 · Emergency Lighting
  > (AIRCRAFT NOT GROUNDED) FAILED EPSU BITE CHECK / REMOVED AND REPLACED EPSU REF WO535097"
- [SDR WX0A2025102032605](https://openairdocs.org/sdr/WX0A2025102032605.md): Unknown · odor · Oct 20, 2025 · N288NV · Airbus A320214 · Air Distribution System
  > (AIRCRAFT NOT GROUNDED) FAS REPORTED EARTHY & MUSKY SMELL DURING CLIMB IN AFT 4 ROWS AND GALLEY THEN AFTER LANDING DESCRIBED SMELL WORSENED IN DESCENT AND DESCRIBED AS DIRTY SOCK SMELL. CLEANING AND DECONIMATION FO DIRTY SOCK /LOCKER ROOM/MUSTY SMELL REPORT RE
- [SDR WX0A2025062332471](https://openairdocs.org/sdr/WX0A2025062332471.md): Fan · failed · Jun 21, 2025 · N288NV · Airbus A320214 · Air Distribution Fan
  > (AIRCRAFT NOT GROUNDED) FA REPORTED BURNING HAIR / ELECTRICAL SMELL FROM AFT GALLEY AREA DURING CRUISE. REMOVED AND REPLACED LAV/GALLEY EXTRACT FAN IAW AMM 21-23-51-400-001-A AND AMM 21-23-51-000-001-A. OPS TEST GOOD AND NO DEFECTS NOTED. THIS CLEARS MEL 21-23
- [SDR WX0A2025021932321](https://openairdocs.org/sdr/WX0A2025021932321.md): Unknown · odor · Feb 17, 2025 · N288NV · Airbus A320214 · Air Distribution System
  > (AIRCRAFT GROUNDED) LEAD FA REPORTED IN CRUISE DIRTY SOCK ODOR IN FWD GALLEY AREA. 2 TIMES FOR A FEW MINUTES EACH. DISSIPATED ON ITS OWN. 36000 FEET. / COMPLETED TC 21-000-002 OIL PHASE TASK CARD, NO DEFECTS NOTED.
- [SDR WX0A2025020732308](https://openairdocs.org/sdr/WX0A2025020732308.md): Girt Bar · misinstalled · Feb 6, 2025 · N288NV · Airbus A320214 · Emergency Equipment
  > (AIRCRAFT NOT GROUNDED) SLIDE INDICATOR FRO R2 DOOR ON ECAM INTERMITTENT. / FOUND GIRT BAR ASSEMBLY IMPROPERLY FOLDED AND DRAGGING ON FLOOR. RE-SECURED GIRT BAR FOLD PER AMM 25-62-44-400-803-A. R2 DOOR ECAM ARMED/DISRAMED INDICATIONS OK PER AMM 52-10-00-410-00
- [SDR WX0A2025012732283](https://openairdocs.org/sdr/WX0A2025012732283.md): Indication Sys · malfunctioned · Jan 26, 2025 · N288NV · Airbus A320214 · Door Warning System
  > (AIRCRAFT GROUNDED) R2 DOOR SLIDE INDICATION WENT AWAY IN FLIGHT / PERFORMED OPS CHECK ON R2 DOOR INDICATION IAW 52-71-00-710-001-A, OPS CK GOOD. NO DEFECTS NOTED. A/C OK FOR SERVICE"
- [SDR WX0A2024030131968](https://openairdocs.org/sdr/WX0A2024030131968.md): Megaphone · expired · Mar 1, 2024 · N288NV · Airbus A320214 · Emergency Equipment
  > MEGAPHONE FOUND TO BE EXPIRED / REPLACED MEGAPHONE BATTERIES IAW AMM 25-61-51-920-001-A"
- [SDR EE4Y2024011719221](https://openairdocs.org/sdr/EE4Y2024011719221.md): Skin · corroded · Jan 17, 2024 · N288NV · Airbus A320214 · Wing, Plate/Skin
  > DURING ACCMPLISHMENT OF THE ALLEGIANT TASK ZL-574-01-1-002 TEOH SKIN LOWER SURFACE WASFOUND WITH CORROSION BETWEEN RIBS 7-8.DUE THE REWORKED AREAS ARE BEYOND SRM LIMITS AIRBUS WAS CONTACTED FOR FURTHER INSTRUCTIONS.AIRBUS PROVIDED STRESS JACKING ANDREPAIR INST
- [SDR EE4Y2024011619220](https://openairdocs.org/sdr/EE4Y2024011619220.md): Skin · corroded · Jan 16, 2024 · N288NV · Airbus A320214 · Wing, Plate/Skin
  > DURING ACCMPLISHMENT OF THE ALLEGIANT TASK 572112-01-01-1-002 TEOH SKIN LOWER SURFACE WAS FOUND WITH CORROSION BETWEEN RIBS 7-8 AND 14-15.DUE THE REWORKED AREAS ARE BEYOND SRM LIMITS AIRBUS WAS CONTACTED FOR FURTHER INSTRUCTIONS.AIRBUS PROVIDED STRESS JACKING
- [SDR EE4Y2024011619219](https://openairdocs.org/sdr/EE4Y2024011619219.md): Rib · corroded · Jan 16, 2024 · N288NV · Airbus A320214 · Wing, Rib/Bulkhead
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 572112-01-1-001 LH WING RIBLET E CORRODED WAS FOUND. DUE TO FLIGHT BY WIRE CABLES PASSING THROUGH THE RIBLET E AND THE AMOUNT OF WORK TO REMOVE THEM, AIRBUS WAS CONTACTED FR ALTERNATIVE METHOD OF INSTALLATION. AIRBUS
- [SDR EE4Y2024011619218](https://openairdocs.org/sdr/EE4Y2024011619218.md): Battery · unknown · Jan 16, 2024 · N288NV · Airbus A320214 · Emergency Lighting
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 335100-03-1-001 CABIN EMERGENCY LIGHTING TEST FOUND BATTERY OF THE FWD LH AND EMERGENCYT RIGHT THE BATTERIES WERE REPLACED IAWA319 AMM TASK 33-51-38-000-002-A AND 33-51-38-400-002-A, AFTERTEST WAS FOUND IN SATISFAC
- [SDR EE4Y2024011619217](https://openairdocs.org/sdr/EE4Y2024011619217.md): Frame · cracked · Jan 16, 2024 · N288NV · Airbus A320214 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT OF THE ALLEGIAN ENGINEERING ORDER E5316-0003 FR20 LH DOOR STOP # 1FRAME WEB I/B UPPER HOLE SCRATCHES WERE FOUND.AIRBUS WAS CONTACTED FOR REPAIRINSTRUCTIONS, THEY PROVIDE REPAIR INSTRUCTIONS UNDER DOSSIER 81330428.THIS REPAIR IS COVERED BY
- [SDR EE4Y2024011619215](https://openairdocs.org/sdr/EE4Y2024011619215.md): Frame · scratched · Jan 16, 2024 · N288NV · Airbus A320214 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT OF THE ALLEGIAN ENGINEERING ORDER E5316-0003 FR16 LH DOOR STOP # 1 FRAME WEB I/B UPPER HOLE SCRATCHES WERE FOUND.AIRBUS WAS CONTACTED FOR REPAIR INSTRUCTIONS, THEY PROVIDE REPAIR INSTRUCTIONS UNDER DOSSIER 813304281.THIS REPAIR IS COVERED
- [SDR EE4Y2024011619212](https://openairdocs.org/sdr/EE4Y2024011619212.md): Frame · cracked · Jan 16, 2024 · N288NV · Airbus A320214 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 53-260-002 FR68 RH DOOR STOP # 4 UPPER I/B ONWEB AREA CRACK WAS FOUND. THE FRAME WAS REPAIRED FOLLO REPAIR INSTRUCTIONS IAW A320 SRM53-41-12-300-008 AND 53-41-12-300-010 PARAG 2A FIG 01 AND FIG 002 REV 146 DATED08-01
- [SDR EE4Y2024011619211](https://openairdocs.org/sdr/EE4Y2024011619211.md): Frame · cracked · Jan 16, 2024 · N288NV · Airbus A320214 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 53-260-002 FR68 LH DOOR STOP # 3 UPPER I/B ONWEB AREA CRACK WAS FOUND. THE FRAME WAS REPAIRED FOLLO REPAIR INSTRUCTIONS IAW A320 SRM53-41-12-300-008 AND 53-41-12-300-010 PARAG 2A FIG 001 AND FIG 002 REV 146 DATED08-0
- [SDR EE4Y2024011619210](https://openairdocs.org/sdr/EE4Y2024011619210.md): Frame · cracked · Jan 16, 2024 · N288NV · Airbus A320214 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 53-260-003 FR68 LH DOOR STOP # 2 LOWER I/B ON WEB AREA CRACK WAS FOUND. THE FRAME WAS REPAIRED FOLLO REPAIR INSTRUCTIONS IAW A320 SRM 53-41-12-300-008 AND 53-41-12-300-010 PARAG 2A FIG 01 AND FIG 002 REV 146 DATED 08
- [SDR WX0A2023071231791](https://openairdocs.org/sdr/WX0A2023071231791.md): Epsu · unknown · Jul 11, 2023 · N288NV · Airbus A320214 · Emergency Lighting
  > WHILE PERFORMING EPSU BATTERY CAPACITY TEST, TEST FAULTED 11WL AND 13WL BATTERY. / REMOVED AND REPLACED EPSU BATTERY AT FIN LOCATION 11WL AND 13WL IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A."
- [SDR WX0A1900010074132](https://openairdocs.org/sdr/WX0A1900010074132.md): None · none · Jun 27, 2022 · N288NV · Airbus A320214 · Hydraulic Pump (Electric/Engine), Main
  > ECAM. Y RSVR LO LVL CAUSING TOTAL Y HYD FAILURE./REPLACMENT OF #2 ENG DRIVEN PUMP,REMOVED AND REPLACED UNION FITTING. REF AMM 29-13-43.REMOVED AND REPLACED CHECK VALVE. REF AMM 29-13-37.REMOVED THE TOP CASE DRAIN HOSE/ TUBE ASSEMBLY REF 39-13-49-400-003-A."
- [SDR WX0A2022013173948](https://openairdocs.org/sdr/WX0A2022013173948.md): Epsu · failed insp · Jan 30, 2022 · N288NV · Airbus A320214 · Emergency Lighting
  > BATTERY FAILED TEST / REMOVED AND REPLACED BATTERY IAW 33-51-38-400-002A. NO DEFECTS NOTED"
- [SDR WX0A2022013173947](https://openairdocs.org/sdr/WX0A2022013173947.md): Epsu · failed insp · Jan 30, 2022 · N288NV · Airbus A320214 · Emergency Lighting
  > BATTERY FAILED TEST / REMOVED AND REPLACED BATTERY IAW 33-51-38-400-002A. NO DEFECTS NOTED"
- [SDR WX0A2022013173946](https://openairdocs.org/sdr/WX0A2022013173946.md): Epsu · failed insp · Jan 30, 2022 · N288NV · Airbus A320214 · Emergency Lighting
  > BATTERY FAILED TEST / REMOVED AND REPLACED EPSU IAW 33-51-38-400-002A. NO DEFECTS NOTED"
- [SDR WX0A2022013173945](https://openairdocs.org/sdr/WX0A2022013173945.md): Epsu · failed insp · Jan 30, 2022 · N288NV · Airbus A320214 · Emergency Lighting
  > BATTERY TEST FAIL / REMOVED AND REPLACED EPSU IAW 33-51-38-400-002A. NO DEFECTS NOTED"
- [SDR EE4Y2023031017357](https://openairdocs.org/sdr/EE4Y2023031017357.md): Skin · nicked · Mar 27, 2021 · N288NV · Airbus A320214 · Fuselage Structure (General)
  > DURING THE VISUAL INSPECTION PER TASK CARD CR 20-3_P1-VISUAL INSP/011, MULTIPLE NICKS WERE FOUND COMMON TO LOWER REAR FUSELAGE SKIN BETWEEN FR55 AND FR56 AND BETWEEN STR 39R AND STR 40R. CORRECTIVE ACTION: PERMANENT REPAIR WAS PERFORMED AS PER AIRBUS DOSSIER#

## 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 = 'N288NV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N288NV/reports

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