# Service difficulty reports: N287NV

A list on [N287NV](https://openairdocs.org/aircraft/N287NV.md).

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

- [SDR WX0A2026082832936](https://openairdocs.org/sdr/WX0A2026082832936.md): Battery · inoperative · Aug 27, 2026 · N287NV · Airbus A320214 · Emergency Equipment
  > (AIRCRAFT NOT GROUNDED) FWD FA MEGAPHONE INOPERATIVE. REPLACED BATTERIES IN FWD FA MEGAPHONE IAW AMM 25-65-51-920-001-A. OPS CHECKED GOOD. ACFT GOOD FOR SERVICE.
- [SDR WX0A2026032732769](https://openairdocs.org/sdr/WX0A2026032732769.md): Plug · contaminated · Mar 27, 2026 · N287NV · Airbus A320214 · Air Distribution System
  > (AIRCRAFT NOT GROUNDED) FA'S REPORT DIRTY SOCK SMELL ON DESCENT AFTER 18000 FOR APPROXIMATLEY 10 MINUTES. / REF LP 2129855 & 2129856, NO SMELLS NOTED FROM BOTH PACKS USING BOTH ENGINES. T/C A32X-21-000-001 WAS PREVIOUSLY PERFORMED AND COMPLIED WITH TASK CARD A
- [SDR WX0A2026030232744](https://openairdocs.org/sdr/WX0A2026030232744.md): Unknown · odor · Mar 1, 2026 · N287NV · Airbus A320214 · Air Distribution System
  > (AIRCRAFT NOT GROUNDED) DESCENDING THROUGH 8,000 TO 4,000 FEET STRONG DIRTY SOCK SMELL NOTED IN FLIGHT DECK, FWD CABIN, AND AFT CABIN. PERFORMED TC A32X-21-000-001 (W/O: 545051, TASKCARD: NR-00001). TASK CARD 21-000-002 COMPLIED (W/O: 544173, TASKCARD: NR-00
- [SDR WX0A2026010732694](https://openairdocs.org/sdr/WX0A2026010732694.md): Unknown · odor · Jan 6, 2026 · N287NV · Airbus A320214 · Air Distribution System
  > (AIRCRAFT NOT GROUNDED) DIRTY SOCK SMELL FILLED CABIN DURING IDLE DESCENT. ODOR REPORTED BY ALL FLIGHT ATTENDANTS AND SOME PASSENGERS. COMPLIED WITH T/C 21-000-002. THIS ACTION CLEARS MDDR 224997. REF LP 2163487 FOR COMPLETION REQUIREMENTS OF T/C 21-000-002.
- [SDR WX0A2025121032661](https://openairdocs.org/sdr/WX0A2025121032661.md): Seal · damaged · Dec 8, 2025 · N287NV · Airbus A320214 · Emergency Exits
  > (AIRCRAFT NOT GROUNDED) FA'S REPORT LOUD SQUEALING/BUZZING NOISE COMING FROM EMERGENCY EXIT DOOR AT 14A. INSPECTED & NOTED DAMAGE TO HATCH SEAL AT 14ABC. REMOVED DAMAGED SEAL & INSTALLED NEW SEAL IAW AMM 52-21-18-960-003-A.
- [SDR WX0A2025082532547](https://openairdocs.org/sdr/WX0A2025082532547.md): Light · detached · Aug 23, 2025 · N287NV · Airbus A320214 · Emergency Lighting
  > FA REPORTS COVER OF LOWER EMERGENCY EXIT LIGHT AT ROW 12 ABC HAS POPPED OFF. FIN 90WL3. REMOVED AND REPLACED LOWER EMERGENCY EXIT LIGHT AT ROW 12 ABC IAW AMM 33-51-11-000-001-A AND 33-51-11-400-001-A.
- [SDR WX0A2025080832531](https://openairdocs.org/sdr/WX0A2025080832531.md): Power Supply · inoperative · Aug 2, 2025 · N287NV · Airbus A320214 · Emergency Lighting
  > (AIRCRAFT NOT GROUNDED) EPSU FAILURE. REMOVED AND REPLACED EPSU.
- [SDR WX0A2025012432280](https://openairdocs.org/sdr/WX0A2025012432280.md): Latch Pin · not seated · Jan 23, 2025 · N287NV · Airbus A320214 · Escape Slide
  > (AIRCRAFT NOT GROUNDED) RIGHT OVERWING SLIDE DOES NOT SHOW ARMED / PERFORMED TSM 52-21-00-810-809-A. RESEATED ARMING LATCH PIN & OPS CHECK GOOD"
- [SDR WX0A2025010232251](https://openairdocs.org/sdr/WX0A2025010232251.md): Epsu · no test · Dec 31, 2024 · N287NV · Airbus A320214 · Emergency Lighting
  > (AIRCRAFT NOT GROUNDED) BAT/EPSU (13WL) AFT L FAILURE / R/R EPSU REF WO510570"
- [SDR WX0A2024121132231](https://openairdocs.org/sdr/WX0A2024121132231.md): Light · inoperative · Dec 10, 2024 · N287NV · Airbus A320214 · Emergency Locator Beacon
  > (AIRCRAFT NOT GROUNDED) L1 ESCAPE SLIDE EMERGENCY LIGHT INOP / FAILED EPSU TEST: ""ESCAPE SLIDE LT/EPSU (10WL) FWD LT IAW AMM 33-51-00-710-001-A. REMOVED AND REPLACED FORWARD LEFTHAND SLIDE IN ACCORDANCE WITH AMM 25-62-44-000-012-A, AND 25-62-44-400-007-A. EPS
- [SDR WX0A2024032031982](https://openairdocs.org/sdr/WX0A2024032031982.md): Battery · failed · Mar 19, 2024 · N287NV · Airbus A320214 · Emergency Lighting
  > EPSU BATTERY AT 12WL FAILED / REMOVED AND REPLACED EPSU BATTERY AT 12WL IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A, OPS CHECK GOOD"
- [SDR EE4Y2023121118969](https://openairdocs.org/sdr/EE4Y2023121118969.md): Unknown · unknown · Dec 10, 2023 · N287NV · Airbus A320214 · Emergency Lighting
  > DURING INSPECTION IAW ALLEGIANT TASK 335100-03-1-001 UPPER FUSELAGE PAX CABIN EPSU BATTERY FAILED AT FOLLOWING POSITIONS FWD LH,EMER LH AND AFT LH. DUE THIS CONDITION WAS REPLACED 3 EA EPSU BATTERY ON POSITIONS FWD LH,EMER LH AND AFT LH IAW A320 AMMTASK 33-5
- [SDR EE4Y2023120618938](https://openairdocs.org/sdr/EE4Y2023120618938.md): Frame · cracked · Dec 6, 2023 · N287NV · Airbus A320214 · Fuselage Main, Frame
  > DURING THE INSPECTION PROCESS AS PER ALLEGIANT ENGINEERING ORDER E5316-0003 REV. 01RELATED TO SB 53-1330 REV. 00, IT WAS FOUND THE FWD FUSELAGE - FR16 - DOOR STOP FITTING LOCATION #7 WITH CRACK INDICATION. THE DETAILS WERE SENT TO AIRBUS ASKING FOR REPLACEMENT
- [SDR EE4Y2023120618939](https://openairdocs.org/sdr/EE4Y2023120618939.md): Intercostal · cracked · Dec 6, 2023 · N287NV · Airbus A320214 · Fuselage Miscellaneous Structure
  > DURING THE INSPECTION PROCESS AS PER ALLEGIANT ENGINEERING ORDER E5316-0003 REV. 01RELATED TO SB 53-1330 REV. 00, IT WAS FOUND THE FWD FUSELAGE - INTERCOSTAL WITH ELONGATED HOLES. THE DETAILS WERE SENT TO AIRBUS ASKING FOR REPLACEMENT INSTRUCTIONS AND FINAL AP
- [SDR EE4Y2023120618941](https://openairdocs.org/sdr/EE4Y2023120618941.md): Door Frame · damaged · Dec 6, 2023 · N287NV · Airbus A320214 · Fuselage Main, Structure
  > DURING THE INSPECTION PROCESS AS PER ALLEGIANT ENGINEERING ORDER E5316-0003 REV. 01RELATED TO SB 53-1330 REV. 00, IT WAS FOUND THE FWD FUSELAGE - FR16 RHS- DOOR STOP FITTING LOCATION #1 WITH ELONGATED HOLES. THE DETAILS WERE SENT TO AIRBUS ASKING FOR REPLACEME
- [SDR EE4Y2023120618940](https://openairdocs.org/sdr/EE4Y2023120618940.md): Door Frame · damaged · Dec 6, 2023 · N287NV · Airbus A320214 · Fuselage Main, Structure
  > DURING THE INSPECTION PROCESS AS PER ALLEGIANT ENGINEERING ORDER E5316-0003 REV. 01 RELATED TO SB 53-1330 REV. 00, IT WAS FOUND THE FWD FUSELAGE - FR16 - DOOR STOP FITTING LOCATION #1 WITH ELONGATED HOLES. THE DETAILS WERE SENT TO AIRBUS ASKING FOR REPLACEMENT
- [SDR EE4Y2023120618942](https://openairdocs.org/sdr/EE4Y2023120618942.md): Door Frame · cracked · Dec 6, 2023 · N287NV · Airbus A320214 · Fuselage Main, Structure
  > DURING ALLEGIANT TASK INSPECTION 53-260-002 REAR FUSELAGE AFT PASS DOOR LH SIDE FR66 DOORSTOP FITTING # 6 AREA I/B UPPER FASTENER HOLE WITH CRACK WAS FOUND. COOPESA PERFORMED REPAIR IN ACCORDANCE WITH A320 SRM TASK 53-41-12-300-009. THIS REPAIR IS COVERED WITH
- [SDR EE4Y2023120618937](https://openairdocs.org/sdr/EE4Y2023120618937.md): Door Frame · cracked · Dec 6, 2023 · N287NV · Airbus A320214 · Fuselage Main, Structure
  > DURING ALLEGIANT TASK INSPECTION 53-260-003 REAR FUSELAGE AFT PASS DOOR LH SIDE FR68 DOORSTOP FITTING # 4 AREA I/B LOWER FASTENER HOLE WITH CRACK WAS FOUND. COOPESA PERFORMED REPAIR IN ACCORDANCE A320 SRM TASK 53-41-12-300-010. THIS REPAIR IS COVERED WITH COOP
- [SDR EE4Y2023120618936](https://openairdocs.org/sdr/EE4Y2023120618936.md): Stop Fitting · cracked · Dec 6, 2023 · N287NV · Airbus A320214 · Fuselage Main, Structure
  > DURING ALLEGIANT TASK INSPECTION 53-260-002 REAR FUSELAGE AFT PASS DOOR LH SIDE FR68DOORSTOP FITTING # 1 AREA I/B LOWER FASTENER HOLE WITH CRACK WAS FOUND. COOPESA PERFORMEDREPAIR IN ACCORDANCE A320 SRM TASK 53-41-12-300-011. DUE DEVIATION DURING REPAIRACCOMPL
- [SDR EE4Y2023120618935](https://openairdocs.org/sdr/EE4Y2023120618935.md): Frame · cracked · Dec 6, 2023 · N287NV · Airbus A320214 · Fuselage Main, Structure
  > DURING ALLEGIANT TASK INSPECTION 53-260-002 REAR FUSELAGE AFT PASS DOOR RH SIDE FR68 DOORSTOP FITTING # 1 AREA I/B LOWER FASTENER HOLE WITH CRACK WAS FOUND. COOPESA PERFORMED REPAIR IN ACCORDANCE A320 SRM TASK 53-41-12-300-011. DUE DEVIATION DURING REPAIR ACCO
- [SDR WX0A1900010031794](https://openairdocs.org/sdr/WX0A1900010031794.md): Heater · unknown · Jul 12, 2023 · N287NV · Airbus A320214 · Water and Waste System
  > (EMERGENCY DECLARED) AT CRUISE AFT FA NOTED LAV G WAS VERY HOT INSIDE SINK AREA WAS VERY HOT TO TOUCH. CABINET BELOW SINK WAS OPENED AND VERY STRONG ELEC BURN SMELL OCUED + CONTINUED ALL THE WAY UNTIL LANDING. FA TOUCHED THE WATER HEATER AND WAS EXTREMELY HOT
- [SDR WX0A2021122273903](https://openairdocs.org/sdr/WX0A2021122273903.md): Light · false indication · Dec 21, 2021 · N287NV · Airbus A320214 · Emergency Lighting
  > BOTH OVERWING EMERGENCY EXIT LIGHTS (EXTERIOR) DO NOT WORK. / ACCOMPLISHED TESTING OF BOTH OVERWING EMERGENCY EXITS LIGHTS (EXTERIOR) I/A/W AMM 33-51-15-70-053-A. LIGHTS TEST ALL 4EA (EXTERIOR) CHECK GOOD. ACFT OK FOR CONTINUE SERVICE."
- [SDR WX0A2021122273904](https://openairdocs.org/sdr/WX0A2021122273904.md): Lens · damaged · Dec 20, 2021 · N287NV · Airbus A320214 · Emergency Lighting
  > EMERGENCY EXIT LIGHT LENS IS DAMAGED ON AC RH SIDE ABOVE WING / PERFORMED TEMP REPAIR OF THE AFT EMERGENCY EXIT LIGHT LENS COVER ON AIRCRAFT RIGHT PER STS EA 79-2021-277. THE ONE FLIGHT CYCLE INSPECTION IS TRACKING ON M313 05330001/1.THE PERMENANT REPAIR IS DU
- [SDR WX0A2021120673885](https://openairdocs.org/sdr/WX0A2021120673885.md): Epsu · failed · Dec 6, 2021 · N287NV · Airbus A320214 · Emergency Lighting
  > EPSU FAIL DURING TEST. / R&R A/C LH EPSU IAW A320 AMM 33-51-38 AND 33-51-00-865-050-A OPS CHECK GOOD."
- [SDR WX0A2021081173807](https://openairdocs.org/sdr/WX0A2021081173807.md): Battery · no test · Aug 10, 2021 · N287NV · Airbus A320214 · Emergency Lighting
  > EPSU BITE TEST FAILS AND DISPLAYS 13WL AFT L. / REMOVED AND REPLACED 13WL BATTERY AND BITE TEST OK REF AMM 33-51-38 PB 401."

## 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 = 'N287NV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N287NV/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
