# Service difficulty reports: N285NV

A list on [N285NV](https://openairdocs.org/aircraft/N285NV.md).

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

- [SDR WX0A2025110332621](https://openairdocs.org/sdr/WX0A2025110332621.md): Megaphone · inoperative · Oct 31, 2025 · N285NV · Airbus A320214 · Emergency Equipment
  > (AIRCRAFT NOT GROUNDED) AFT MEGAPHONE INOP. REMOVED AND REPLACED AFT MEGAPHONE IAW AMM 25-65-51-710-002-A, OPS CHECK GOOD."
- [SDR WX0A2025071832503](https://openairdocs.org/sdr/WX0A2025071832503.md): Slide · out of adjust · Jul 16, 2025 · N285NV · Airbus A320214 · Escape Slide
  > (AIRCRAFT NOT GROUNDED) R1 DOOR NOT SHOWING SLIDE ARMED IN FLIGHT /CRUISE DURING CHECK. / ADJUSTED FWD R/H DOOR ESCAPE SLIDE ASSEMBLY IAW AMM 25-62-44-400-803-A. OPS CHECK GOOD. DOOR ESCAPE SLIDE SHOWS ARMED WHEN STOWED."
- [SDR WX0A2025071132497](https://openairdocs.org/sdr/WX0A2025071132497.md): Megaphone · inoperative · Jul 9, 2025 · N285NV · Airbus A320214 · Emergency Equipment
  > (AIRCRAFT NOT GROUNDED) FWD MEGAPHONE INOP. R&R FWD MEGAPHONE AND OPS CHECK GOOD IAW AMM 25-65-51"
- [SDR WX0A2025050732418](https://openairdocs.org/sdr/WX0A2025050732418.md): Window · cracked · May 5, 2025 · N285NV · Airbus A320214 · Flight Compartment Windows
  > (AIRCRAFT GROUNDED) (EMERGENCY DECLARED) RIGHT HAND FIXED WINDOW CRACKED / REMOVED AND REPLACED RH FIXED WINDOW PER AMM 56-11-12-400-003-A OPS TEST OK A/C OK FOR SERVICE "
- [SDR WX0A2025050732416](https://openairdocs.org/sdr/WX0A2025050732416.md): Oxygen Box · no test · May 4, 2025 · N285NV · Airbus A320214 · Crew Oxygen System
  > (AIRCRAFT GROUNDED) FO OXYGEN MASK YELLOW BLINKER NOT DISPLAYED DURING TEST. / REMOVED AND REPLACED FO OXYGEN MASK BOX IAW AMM 35-12-41-000-001-A AND 35-12-41-400-01-A. OPS + LEAK CHECK OK."
- [SDR WX0A2025031432354](https://openairdocs.org/sdr/WX0A2025031432354.md): Latch · not closed · Mar 12, 2025 · N285NV · Airbus A320214 · Emergency Exits
  > (AIRCRAFT NOT GROUNDED) LEFT O/W EXIT ARMED INDICATION MISSING ON ECAM / C/W TSM 33-51-00-810-809-A. FOUND LEFT HAND FOWARD OVERWING SLIDE DOOR LATCH PIN NOT FULLY ENGAGED. CORRECTED AND INDICATIONS CLEARED. NO ADDITIONAL FAULTS FOUND AT THIS TIME"
- [SDR WX0A2024050632031](https://openairdocs.org/sdr/WX0A2024050632031.md): Cover · out of adjust · May 3, 2024 · N285NV · Airbus A320214 · Passenger/Crew Doors
  > ON BASE LEG AT 5000': ECAM DOOR R AFT EMER EXIT (OVERWING) REPEATED 6 TIMES TILL LANDING. REMAIN ON INTO THE PARKING GATE. / ADJUSTED COVER FLAP OF BOTH RH OVER WING EXIT DOOR COVER FLAPS AS PER A320 AMM 25-23-47-400-001-A. OPS CHECKED NORMAL AT THIS TIME. NO
- [SDR EE4Y2024042820002](https://openairdocs.org/sdr/EE4Y2024042820002.md): Rib · corroded · Apr 28, 2024 · N285NV · Airbus A320214 · Wing, Rib/Bulkhead
  > DURING THE STRUCTURAL INSPECTION PER ALLEGIANT TASK CARD 572112-01-1, IT WAS FOUND AT LH WING REAR SPAR AREA THE RIBLET J WITH CORROSION.SINCE THAT THE MENTIONED RIBLET HAVE DEEPCORROSION, IT WILL BE REPLACED BY NEW ONE.DUE TO FLIGHT BY WIRE CABLES PASSING THR
- [SDR EE4Y2024042820001](https://openairdocs.org/sdr/EE4Y2024042820001.md): Rib · corroded · Apr 28, 2024 · N285NV · Airbus A320214 · Wing, Rib/Bulkhead
  > DURING THE STRUCTURAL INSPECTION PER ALLEGIANT TASK CARD 572112-01-1, IT WAS FOUND AT LH WING REAR SPAR AREA THE RIBLET E WITH CORROSION.SINCE THAT THE MENTIONED RIBLET HAVE DEEPCORROSION, IT WILL BE REPLACED BY NEW ONE.DUE TO FLIGHT BY WIRE CABLES PASSING THR
- [SDR EE4Y2024042820000](https://openairdocs.org/sdr/EE4Y2024042820000.md): Rib · corroded · Apr 28, 2024 · N285NV · Airbus A320214 · Wing, Rib/Bulkhead
  > DURING THE STRUCTURAL INSPECTION PER ALLEGIANT TASK CARD 572112-01-1, IT WAS FOUND AT LH WING REAR SPAR AREA THE RIBLET L WITH CORROSION.SINCE THAT THE MENTIONED RIBLET HAVE DEEP CORROSION, THEY WILL BE REPLACED BY NEWONES.DUE TO FLIGHT BY WIRE CABLES PASSING
- [SDR EE4Y2024042820032](https://openairdocs.org/sdr/EE4Y2024042820032.md): Skin Panel · corroded · Apr 28, 2024 · N285NV · Airbus A320214 · Wing, Plate/Skin
  > DURING THE ACCOMPLISHMENT OF ALLEGIANT TASK 572112-01-1, LH WING TEOH AREA BETWEEN RIB 14 AND 15 CORROSION WAS FOUND. AIRBUS WAS CONTACTED TO REQUEST REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRUCTIONS AND REPAIR WAS ´PERFORMED IAW COOPESA ENGINEERING OR
- [SDR EE4Y2024042820005](https://openairdocs.org/sdr/EE4Y2024042820005.md): Frame · cracked · Apr 28, 2024 · N285NV · Airbus A320214 · Fuselage Main, Frame
  > DURING ALLEGIANT TASK INSPECTION 53-260-002 REAR FUSELAGE AFT PASS DOOR RH 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 REPAIR ACCOMP
- [SDR EE4Y2024042820003](https://openairdocs.org/sdr/EE4Y2024042820003.md): Rib · corroded · Apr 28, 2024 · N285NV · Airbus A320214 · Wing, Rib/Bulkhead
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 572112-01-1-002, RIGHT WING SPAR RIBLET WITH CORROSION WAS FOUND.DUE TO FLIGHT BY WIRE CABLES PASSING THROUGH THE RIBLETS E AND THE AMOUNT OF WORK TO REMOVE THEM AIRBUS WAS CONTACTED TO USE ALTERNATIVE METHOD OF INST
- [SDR EE4Y2024042720024](https://openairdocs.org/sdr/EE4Y2024042720024.md): Strap · corroded · Apr 27, 2024 · N285NV · Airbus A320214 · Fuselage Miscellaneous Structure
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK ZL-161-03-2-001 LOWER FUSELAGE BULK CARGO COMPARMENT FR64 BETWEEN STGR 43LH AND STGR 40RH, STRAP CORROSION AT SEVERAL PLACES. DUE A DEVIATION OF SRM REPAIR AIRBUS WAS CONTACTED TO OBTAIN REPAIR INSTRUCTIONS TO REPLAC
- [SDR WX0A1900010031734](https://openairdocs.org/sdr/WX0A1900010031734.md): None · none · Jan 31, 2023 · N285NV · Airbus A320214 · Fuselage Main, Attach Fittings
  > NRC 2000-0119: 32779-05 AT L2 DOOR SILL PLATE BETWEEN FR 67-68 STRG 23L CORROSION FOUND AROUND FASTENER HOLES. / L2 DOOR SILL BEAM BETWEEN FR 67-68 AND STRG 23LH, SILL BEAM CORROSION REPAIRED AS PER SRM TASK 53-41-14-300-001 REV 143, REPAIR PRINCIPLE 7. REPAI
- [SDR WX0A1900010031733](https://openairdocs.org/sdr/WX0A1900010031733.md): None · none · Jan 30, 2023 · N285NV · Airbus A320214 · Fuselage Main, Attach Fittings
  > NRC 2000-0115: 32779-02 ON R2 DOOR SILL BEAM BETWEEN FR 67-68 AND STRG 23 RH CORROSION FOUND. / R2 DOOR SILL BEAM BETWEEN FR 67-68 AND STRG 23RH, SILL BEAM CORROSION REPAIRED AS PER SRM TASK 53-41-14-300-001 REV 143, REPAIR PRINCIPLE 7. REPAIR CATEGORY A, NO
- [SDR WX0A2022091674246](https://openairdocs.org/sdr/WX0A2022091674246.md): Epsu · none · Sep 15, 2022 · N285NV · Airbus A320214 · Lighting System
  > DURING EMERGENCY EQUIPMENT CHECK L2 AND R2 DOOR EMERGENCY EXITS SIGN LIGHTS FOUND INOP / REMOVED AND REPLACED THE BATTERY OF THE AFT EPSU IAW A320 AMM 33-51-38-000-002-A REMOVAL AND 33-51-38-400-002-A INSTALL, OPS CHECKED GOOD"
- [SDR WX0A2022091674245](https://openairdocs.org/sdr/WX0A2022091674245.md): Epsu · none · Sep 15, 2022 · N285NV · Airbus A320214 · Lighting System
  > DURING EMERGENCY EQUIPMENT CHECK L1 AND R1 DOOR EMERGENCY EXIT SIGN LIGHTS FOUND INOP / REMOVED AND REPLACED THE BATTERY OF THE FWD EPSU IAW A320 AMM 33-51-38-000-002-A REMOVAL AND 33-51-38-400-002-A INSTALL, OPS CHECKED GOOD"
- [SDR WX0A2022081274203](https://openairdocs.org/sdr/WX0A2022081274203.md): Light · inoperative · Aug 11, 2022 · N285NV · Airbus A320214 · Emergency Lighting
  > EMERGENCY LIGHT SWITCH SYSTEM IS INOP / REPLACED EPSU 10WL AND EPSU BETT 13WL IAW AMM 33-51-38-000-001-A AND 33-51-38-400-001-A, NO FIX. REPLACED EMERGENCY LIGHT C/B 2WL PER AMM 20-16-00 AND ESPM 20-40-610. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED."
- [SDR WX0A2022080574182](https://openairdocs.org/sdr/WX0A2022080574182.md): Epsu · none · Aug 5, 2022 · N285NV · Airbus A320214 · Lighting System
  > CA REPORTS AFT EMERGENCY LIGHTS STAY ON W/ SWITCH IN ARMED POSITION. / ACCOMPLISHED EPSU BITE TEST IAW AMM 33-51-00-710-001, TEST FAULTED SWITCH 4 WL, R + R SWITCH 4WL IAW ESPM 20-30-00, OPS CHECK FAILED FAULTED 11WL BAT AND 13WL BAT. R + R EPSU BATTERIES 11WL
- [SDR WX0A2022070574136](https://openairdocs.org/sdr/WX0A2022070574136.md): None · none · Jul 5, 2022 · N285NV · Airbus A320214 · Emergency Locator Beacon
  > EPSU SYS TEST FAILED/REMOVED AND REPLACED RH AFT SLIDE IAW AMM 25-62-44 OPS CHECK GOOD EPSU BITE TEST GOOD IAW AMM 33-51-00-710-001-A NO FAULT NOTED"
- [SDR WX0A2022070674139](https://openairdocs.org/sdr/WX0A2022070674139.md): None · none · Jul 3, 2022 · N285NV · Airbus A320214 · Lighting System
  > CABIN EMERGENCY CEILING LIGHT 205WL, 206WL, 207WL REQUIRE REMOVAL / REMOVED CABIN EMERGENCY CEILING LIGHT 205WL, 206WL, 207WL IAW AMM 33-51-11"
- [SDR WX0A1900010074259](https://openairdocs.org/sdr/WX0A1900010074259.md): None · none · Sep 18, 2021 · N285NV · Airbus A320214 · Emergency Lighting
  > EXIT SIGN LIGHTS DO NOT ILLUMINATE WHEN LANDING GEAR IS DOWN OR ON GROUND/PERFORMED TSM 33-51-00-810-819-A. REMOVED AND REPLACED RELAY 8WL PER ESPM 20-46-50. OPS CHECK GOOD NO FAULTS AT THIS TIME."
- [SDR WX0A2021082373817](https://openairdocs.org/sdr/WX0A2021082373817.md): Switch · faulted · Aug 21, 2021 · N285NV · Airbus A320214 · Emergency Lighting
  > FA'S REPORT EMERGENCY EXIT LIGHTS STAY ON WHEN ARMED EVEN AFTER RESETTING THE COCKPIT EMER EXIT LT SWITCH TO OFF AND ARM / REPLACED COCKPIT EMER LIGHT SWITCH IAW WDM 33-51-01, OPS CHECK GOOD."
- [SDR WX0A2021020173637](https://openairdocs.org/sdr/WX0A2021020173637.md): Cids · intermittent · Jan 30, 2021 · N285NV · Airbus A320214 · Emergency Lighting
  > CABIN EMERGENCY LIGHTS BLINKING. R & R CIDS 1 IAW AMM 23-73-34. OP'S CHECK GOOD. REF CT00732224 TROUBLE SHOOTING PERFORMED.

## 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 = 'N285NV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N285NV/reports

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