# Service difficulty reports: N271NV

A list on [N271NV](https://openairdocs.org/aircraft/N271NV.md).

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

- [SDR WX0A2026061532847](https://openairdocs.org/sdr/WX0A2026061532847.md): Pin · installed · Jun 15, 2026 · N271NV · Airbus A320214 · Landing Gear Retraction/Extension System
  > (AIRCRAFT NOT GROUNDED) (EMERGENCY DECLARED) LDG GEAR AND DOORS NOT CLOSED ON TAKEOFF. PREFORMED GVI OF NLG IAW AMM 32-21-00-200-002A. FOUND SAFTEY LOCK STILL INSTALLED IN NLG LOCK STAY. REMOVED SAFTY LOCK FROM NLG LOCK STAY IAW AMM 32-00-00-081-002A. NO OT
- [SDR WX0A2026051832817](https://openairdocs.org/sdr/WX0A2026051832817.md): Epsu · no test · May 16, 2026 · N271NV · Airbus A320214 · Emergency Lighting
  > (AIRCRAFT NOT GROUNDED) DURING WEEKLY FOUND EPSU BATTERY 10WL FAILED / REMOVED AND REPLACED 10WL EPSU BATTERY WITH REPAIRED BATTERY IAW AMM 33-51-38-000/400-002-A."
- [SDR WX0A2025122932684](https://openairdocs.org/sdr/WX0A2025122932684.md): Megaphone · broken · Dec 29, 2025 · N271NV · Airbus A320214 · Emergency Equipment
  > (AIRCRAFT NOT GROUNDED) FWD MEGAPHONE BROKEN / FOUND REPLACEMENT FWD MEGA PHONE. REMOVED AND REPLACED FWD MEGA PHONE IAW AMM 25-65-21. OPS CHECK GOOD"
- [SDR WX0A2025092432578](https://openairdocs.org/sdr/WX0A2025092432578.md): Cover · detached · Sep 23, 2025 · N271NV · Airbus A320214 · Emergency Lighting
  > AIRCRAFT NOT GROUNDED, R2 DOOR EXIT COVER FELL OFF. INSTALLED EXIT COVER AT DOOR R2 PER AMM 33-51-17-400-001A. A/C OK FOR SERVICE.
- [SDR WX0A2025082732551](https://openairdocs.org/sdr/WX0A2025082732551.md): Unknown · odor · Aug 25, 2025 · N271NV · Airbus A320214 · Air Distribution System
  > (AIRCRAFT NOT GROUNDED) DIRTY SOCK SMELL IN CABIN AND FLIGHT DECK ON DESCENT / PERFORMED AMM 21-00-00-615-803-B REMOVAL OF THE CONTAMINATION OF THE ECS, NO FAULTS NOTED AND NO SMELL DETECTED. THIS CLEARS MEL 21-52-01-G, CAT C, MDDR#218679 'M' PROCEDURE REVERSE
- [SDR WX0A2025070732484](https://openairdocs.org/sdr/WX0A2025070732484.md): Plenum · contaminated · Jul 3, 2025 · N271NV · Airbus A320214 · APU Core Engine
  > (AIRCRAFT NOT GROUNDED) DIRTY SOCK SMELL OBSERVED DECENDING BELOW 10'000' SMELLED BY CA AND FO / CLEANED APU AIR INTAKE & PLENUM IAW 49-16-00-100-005-A. OPERATED APU & PACKS 1 & 2 - PRECONDITIONED BLEED SYSTEM. OP CK GOOD. NO ODORS DETECTED. C/W THE LEVEL
- [SDR WX0A2025012132275](https://openairdocs.org/sdr/WX0A2025012132275.md): Controller · faulted · Jan 19, 2025 · N271NV · Airbus A320214 · Cabin Pressure Controller
  > (AIRCRAFT GROUNDED) (EMERGENCY DECLARED) EXCESSIVE CABIN ALTITUDE ECAM / REMOVED AND REPLACED CABIN PRESSURE CONTROLLER CPC 1 AND CPC 2 IAW AMM 21-31-34-000-001-A AND 21-31-34-400-001-A. OP TEST CHECKED GOOD. REMOVED AND REPLACED BOTH AFT GALLEY SAFETY VALVE R
- [SDR WX0A2025012132274](https://openairdocs.org/sdr/WX0A2025012132274.md): Battery · inoperative · Jan 18, 2025 · N271NV · Airbus A320214 · Emergency Lighting
  > (AIRCRAFT GROUNDED) EPSU BATTERY INOP. EPSU BATTERY (11WL) EMER L REQUIRED A REMOVAL AND REPLACE. / (RESOLVED ON W/O: 511713 TASKCARD: NR-00001) REMOVED AND REPLACED (11WL) EMER L EPSU BATTERY. IAW AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A. OPS CHECK
- [SDR EE4Y2024122321462](https://openairdocs.org/sdr/EE4Y2024122321462.md): Frame · cracked · Dec 23, 2024 · N271NV · Airbus A320214 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT OF THE WORK CARD A32X-53-260-002 UPPER FUSELAGE FR66 LH SIDE DOOR STOP FITTING # 1 AT UPPER AND LOWER I/B HOLES WITH CRACK INDICATION WAS FOUND.AIRBUS WAS CONTACTED FOR REPAIR INSTRUCTIONS. PERFORMED PERMANENT REPAIR ON SECTION 18 AT FR6
- [SDR EE4Y2024122321461](https://openairdocs.org/sdr/EE4Y2024122321461.md): Frame · cracked · Dec 23, 2024 · N271NV · Airbus A320214 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT OF THE WORK CARD A32X-53-260-003 UPPER FUSELAGE FR68 RH SIDE DOOR STOP FITTING # 1 AT LOWER I/B HOLE WITH CRACK INDICATION WAS FOUND.AIRBUS WAS CONTACTED FOR REPAIR INSTRUCTIONS. PERFORMED PERMANENT REPAIR ON SECTION 18 AT FR68 LH STOP F
- [SDR EE4Y2024122321460](https://openairdocs.org/sdr/EE4Y2024122321460.md): Frame · cracked · Dec 23, 2024 · N271NV · Airbus A320214 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT OF THE WORK CARD A32X-53-260-003 UPPER FUSELAGE FR68 LH SIDE DOOR STOP FITTING # 1 AT LOWER I/B HOLE WITH CRACK INDICATION WAS FOUND.AIRBUS WAS CONTACTED FOR REPAIR INSTRUCTIONS. PERFORMED PERMANENT REPAIR ON SECTION 18 AT FR68 LH STOP F
- [SDR WX0A2024060532066](https://openairdocs.org/sdr/WX0A2024060532066.md): Megaphone · inoperative · Jun 3, 2024 · N271NV · Airbus A320214 · Emergency Equipment
  > FA AFT MEGAPHONE INOP. / REPLACED FA AFT MEGA PHONE IAW ALLEGIANT N271NV LOPA"
- [SDR WX0A1900010031697](https://openairdocs.org/sdr/WX0A1900010031697.md): Skin · corroded · Nov 28, 2022 · N271NV · Airbus A320214 · Ailerons
  > NRC 5000-0013: 1711-57 ON L/H WING, CORROSION SUSPECTED UNDER TRAILING EDGE SEAL PLATE AT INBORD HINGE SPOILER #2. / L/H WING, TRAILING EDGE OVERHANG SKIN PANEL #2 AT INBD HINGE OF SPOILER #2 (BTW RIBS 9-11) UPPER AND LOWER SURFACE PERMANENTLY REPAIRED PER AIR
- [SDR WX0A1900010031696](https://openairdocs.org/sdr/WX0A1900010031696.md): Skin · corroded · Nov 28, 2022 · N271NV · Airbus A320214 · Ailerons
  > NRC 5000-0012: 1711-51 ON L/H WING, CORROSION SUSPECTED UNDER TRAIING EDGE SEAL PLATE OUTBORD MAIN HINGE SPOILER #1. / L/H WING TRAILING EDGE OVERHANG EXTENDING FWD OF THE REAR FALSE SPAR, UPPER SKIN PANEL #2 LOWER SURFACE OUTBD OF OUTBD MAIN HINGE SPOILER #1
- [SDR WX0A2022102474290](https://openairdocs.org/sdr/WX0A2022102474290.md): Megaphone · inoperative · Oct 22, 2022 · N271NV · Airbus A320214 · Emergency Equipment
  > FWD MEGAPHONE IS NOT WORKING / REMOVED AND REPLACED FWD MEGAPHONE IAW ALLEGIANT LOPA DRAWING A2250011L03"
- [SDR WX0A2022070574135](https://openairdocs.org/sdr/WX0A2022070574135.md): Megaphone · none · Jul 4, 2022 · N271NV · Airbus A320214 · Emergency Locator Beacon
  > AFT CABIN MEGAPHONE INOP / REMOVED AND REPLACED AFT CABIN MEGAPHONE PER LOPA A2250011L03"
- [SDR WX0A2021122073902](https://openairdocs.org/sdr/WX0A2021122073902.md): Epsu · failed insp · Dec 19, 2021 · N271NV · Airbus A320214 · Emergency Lighting
  > FA STATED EXIT LIGHTS STAYED ON AFTER FOUR CHIMES MIDCENTER AFTCENTER. A/C LEFT OVER WING EXIT. / PERFORMED EPSU BITE TEST.TEST FAILED FOR BATTERY 10WL AND 11WL IAW AMM 33-51-00. REMOVED AND REPLACED BOTH 10WL AND 11WL BATTERIES IAW AMM 33-51-38. OPS-CHECK GOO
- [SDR WX0A1900010073983](https://openairdocs.org/sdr/WX0A1900010073983.md): Skin · corroded · Dec 3, 2021 · N271NV · Airbus A320214 · Wing, Plate/Skin
  > NRC 5000-0015: 1237-19. LH WING, UPPER SKIN PANEL, CORROSION FOUND BTW REAR SPAR AND FALSE SPAR AT RIB 6 AREA. / LH WING, UPPER SKIN PANEL CORROSION BETWEEN REAR SPAR AND FALSE SPAR AT RIB 6 AREA REPAIRED AS PER AIRBUS DOSSIER 80990965 AND REPAIR DRAWING R572
- [SDR WX0A1900010073982](https://openairdocs.org/sdr/WX0A1900010073982.md): Skin · corroded · Dec 3, 2021 · N271NV · Airbus A320214 · Wing, Plate/Skin
  > NRC 5000-0013: 1237-17. LH WING, UPPER SKIN PANEL SEVERAL CORROSION SPOTS (3X) FOUND AT REAR SPAR AREA BTW RIB 14-15. / LH WING, UPPER SKIN PANEL CORROSION SPOTS AT REAR SPAR AREA BETWEEN RIB 14-15 REPAIRED AS PER AIRBUS DOSSIER 80990965 AND REPAIR DRAWING R5
- [SDR WX0A1900010073981](https://openairdocs.org/sdr/WX0A1900010073981.md): Skin · corroded · Dec 3, 2021 · N271NV · Airbus A320214 · Wing, Plate/Skin
  > NRC 5000-0012: 1237-16. LH WING, UPPER SKIN PANEL, CORROSION FOUND AT REAR SPAR AND RIB 17 AREA. / LH WING, UPPER SKIN PANEL CORROSION AT REAR SPAR AREA AND RIB 17 REPAIRED AS PER AIRBUS DOSSIER 80990965 AND REPAIR DRAWING R572-58616 ISSUE K PARA. D AND COMPL
- [SDR WX0A1900010073980](https://openairdocs.org/sdr/WX0A1900010073980.md): Skin · corroded · Dec 3, 2021 · N271NV · Airbus A320214 · Wing, Plate/Skin
  > NRC 5000-0010: 1237-14. LH WING, UPPER SKIN PANEL, CORROSION FOUND AROUND BONDING SPIGOT HOLE (FRONT SPAR INBD OF RIB 20 AREA) / LH WING, UPPER SKIN PANEL CORROSION AROUNF BONDING SPIGOT HOLE (FRONT SPAR INBD OF RIB 20 AREA) REPAIRED IAW AIRBUS DOSSIER 80990
- [SDR WX0A1900010073979](https://openairdocs.org/sdr/WX0A1900010073979.md): Skin · corroded · Dec 3, 2021 · N271NV · Airbus A320214 · Wing, Plate/Skin
  > NRC 5000-0011: 1237-15. LH WING, UPPER SKIN PANEL, SEVERAL CORROSION SPOTS (5X) FOUND AT REAR SPAR AREA BTW RIB 18-20. / LH WING, UPPER SKIN PANEL CORROSION SPOTS (5X) AT REAR SPAR AREA BTW RIB 18-20 REPAIRED AS PER AIRBUS DOSSIER 80990965 AND REPAIR DRAWING
- [SDR WX0A1900010073978](https://openairdocs.org/sdr/WX0A1900010073978.md): Skin · corroded · Dec 3, 2021 · N271NV · Airbus A320214 · Wing, Plate/Skin
  > NRC 5000-0014:1237-18. LH WING, UPPER SKIN PANEL, SEVERAL CORROSION SPOTS (7X) FOUND BTW REAR SPAR AND FALSE SPAR AND RIB 7-9. / LH WING, UPPER SKIN PANEL CORROSION SPOTS (7X) BTW REAR SPAR AND FALSE SPAR AND BTW RIB 7-9 REPAIRED AS PER AIRBUS DOSSIER 80990965
- [SDR WX0A1900010073977](https://openairdocs.org/sdr/WX0A1900010073977.md): Skin · corroded · Dec 3, 2021 · N271NV · Airbus A320214 · Wing, Plate/Skin
  > NRC 5000-0008: 1237-12. LH WING, UPPER SKIN PANEL SEVERAL CORROSION SPOTS (4X) FOUND AT REAR SPAR AREA BTW RIB 25-26. / LH WING, UPPER SKIN PANEL CORROSION SPOTS (4X) AT REAR SPAR BTW RIB 25-26 REPAIRED AS PER AIRBUS DOSSIER 80990965 AND REPAIR DRAWING R572-58
- [SDR WX0A1900010073976](https://openairdocs.org/sdr/WX0A1900010073976.md): None · none · Dec 3, 2021 · N271NV · Airbus A320214 · Fuselage Main, Structure
  > NRC 1000-0005: CRACKS FOUND AT LH SIDEBOX BEAM FLANGE AT S15, FR43, UPPER AND MID FASTENER HOLES / AT LH SIDE BOX BEAM FLANGE LOCATION AT S15 FR43 UPPER AND MID FASTENER HOLE CRACKED ON PRESSURE PLATE ONLY AND REPAIRED AS PER AIRBUS TRM 80991084/001/010/017, R
- [SDR WX0A2021110873866](https://openairdocs.org/sdr/WX0A2021110873866.md): Battery · discharged · Nov 8, 2021 · N271NV · Airbus A320214 · Emergency Equipment
  > FWD OUTBOARD EMERGENCY FLASHLIGHT BATTERY LOW. / REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT BATTERY IAW CMM 25-60-02. OPS CHECK GOOD."
- [SDR WX0A2021062173744](https://openairdocs.org/sdr/WX0A2021062173744.md): Computer · faulted · Jun 20, 2021 · N271NV · Airbus A320214 · Leading Edge Slat Control System
  > (EMERGENCY DECLARED) F/CTL SLAT SYS 2 FAULT AFTER LANDING IN ONTARIO / SFCS 2 SLAT PCU VALVE BLOCK PLACED ON MEL 27-84-02A, CAT B, DMI #82402. WTB TEST ACCOMPLISHED IAW AMM 27-81-00-040-001-A - TEST OK. DEACTIVATION OF FSCC 2 ACCOMPLISHED IAW AMM 27-51-00-040-
- [SDR WX0A2021053173726](https://openairdocs.org/sdr/WX0A2021053173726.md): Battery Pack · not reported · May 28, 2021 · N271NV · Airbus A320214 · Emergency Lighting
  > REF T/C 335100-03-1-001,33-51-00-710-003-A, MANAGEMENT REQUESTS ALL FOUR BATTERIES BE REPLACED / R+R EPSU BATTERY 10WL, 11WL, 12WL,13WL REF AMM 33-51-38PB401, OPS CHECK GOOD"
- [SDR WX0A2021030873657](https://openairdocs.org/sdr/WX0A2021030873657.md): Epsu · inoperative · Mar 6, 2021 · N271NV · Airbus A320214 · Emergency Lighting
  > MID RIGHT EPSU BATT INOP / REMOVED AND REPLACED MID RIGHT EPSU BATT IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A. OPS CK GOOD AT THIS TIME.
- [SDR WX0A2021030873656](https://openairdocs.org/sdr/WX0A2021030873656.md): Epsu · inoperative · Mar 6, 2021 · N271NV · Airbus A320214 · Emergency Lighting
  > FWD EPSU BATT INOP / REMOVED AND REPLACED FWD EPSU BATT IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A. OPS CK GOOD AT THIS TIME.
- [SDR WX0A2021030873655](https://openairdocs.org/sdr/WX0A2021030873655.md): Epsu · inoperative · Mar 6, 2021 · N271NV · Airbus A320214 · Emergency Lighting
  > AFT EPSU BATT INOP / REMOVED AND REPLACED AFT EPSU BATT IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A. OPS CK GOOD AT THIS TIME.
- [SDR WX0A2021030873654](https://openairdocs.org/sdr/WX0A2021030873654.md): Epsu · inoperative · Mar 6, 2021 · N271NV · Airbus A320214 · Emergency Lighting
  > MID LEFT EPSU BATT INOP / REMOVED AND REPLACED MID LEFT EPSU BATT IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A. OPS CK GOOD AT THIS TIME.
- [SDR WX0A2020101473589](https://openairdocs.org/sdr/WX0A2020101473589.md): Control Unit · failed · Oct 12, 2020 · N271NV · Airbus A320214 · Leading Edge Slat Control System
  > DURING SLAT EXTENSION WE HAD THE ECAM SLAT FAIL MESSAGE. SLATS LOCKED AT 0 (DEGREES). REPLACED SLAT PCU, REF AMM 27-84-51 PB 401. LEAK AND OPERATIONS CHECK GOOD. NO FURTHER DEFECTS.
- [SDR WX0A2020091873577](https://openairdocs.org/sdr/WX0A2020091873577.md): Bulb · missing · Sep 17, 2020 · N271NV · Airbus A320214 · Central Warning
  > CREW REPORTS CAPT MASTER CAUTION LIGHT (AMBER) HAS MISSING BULBS. REPLACED MASTER WARNING SWITCH, IAW ESPM 20-45-11. OPS CHECK GOOD.

## 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 = 'N271NV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N271NV/reports

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