# Service difficulty reports: N326NV

A list on [N326NV](https://openairdocs.org/aircraft/N326NV.md).

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

- [SDR WX0A2026082432928](https://openairdocs.org/sdr/WX0A2026082432928.md): Megaphone · damaged · Aug 23, 2026 · N326NV · Airbus A319111 · Emergency Equipment
  > (AIRCRAFT NOT GROUNDED) FED MEGAPHONE HANDLE PARTIALLY DETACHED. REMOVED AND REPLACED FWD MEGAPHONE IAW AMM 25-65-51-710-002-A.
- [SDR WX0A2025110332624](https://openairdocs.org/sdr/WX0A2025110332624.md): Power Supply · no test · Nov 3, 2025 · N326NV · Airbus A319111 · Emergency Lighting
  > (AIRCRAFT NOT GROUNDED) FAILED TEST/EPSU / REMOVED AND REPLACED EPSU REF WO535169"
- [SDR WX0A2025081332541](https://openairdocs.org/sdr/WX0A2025081332541.md): Light · missing · Aug 11, 2025 · N326NV · Airbus A319111 · Emergency Lighting
  > AIRCRAFT NOT GROUNDED, FA DISCOVERED L2 FLOOR LEVEL EMERGENCY LIGHT MISSING IN FLIGHT. INSTALLED NEW EXIT LIGHT COVER ON L2 EXIT DOOR IAW AMM 33-51-11-400-001-A.
- [SDR WX0A2025072532513](https://openairdocs.org/sdr/WX0A2025072532513.md): Battery · no test · Jul 23, 2025 · N326NV · Airbus A319111 · Lighting System
  > (AIRCRAFT NOT GROUNDED) BATTERY FAULT INDICATION DURING EPSU BITE TEST / REMOVED AND REPLACED EPSU BATTERIES, REF WO519197"
- [SDR WX0A2025050732420](https://openairdocs.org/sdr/WX0A2025050732420.md): Power Supply · no test · May 7, 2025 · N326NV · Airbus A319111 · Emergency Lighting
  > (AIRCRAFT NOT GROUNDED) EPSU FAILED DURING TC #335100-03-1-001 / REMOVED AND REPLACED AFT EPSU/BATTERY 13WL IAW AMM 33-51-38-400-001-A, OPS CHECK GOOD"
- [SDR WX0A2024020731958](https://openairdocs.org/sdr/WX0A2024020731958.md): Megaphone · expired · Feb 5, 2024 · N326NV · Airbus A319111 · Emergency Equipment
  > FWD MEGAPHONE EXPIRATION DATE PAST DUE. / REMOVED AND REPLACED FWD GALLEY MEGAPHONE IAW AMM 25-65-51-920-001-A, 25-65-51-410-050-A."
- [SDR WX0A2024020531954](https://openairdocs.org/sdr/WX0A2024020531954.md): Megaphone · expired · Feb 5, 2024 · N326NV · Airbus A319111 · Emergency Equipment
  > FWD MEGAPHONE EXPIRATION DATE PAST DUE. / REMOVED AND REPLACED FWD GALLEY MEGAPHONE IAW AMM 25-65-51-920-001-A, 25-65-51-410-050-A."
- [SDR WX0A2023122931931](https://openairdocs.org/sdr/WX0A2023122931931.md): Epsu · unknown · Dec 27, 2023 · N326NV · Airbus A319111 · Emergency Lighting
  > WHILE PEFORMING EMERGENCY LIGHT TEST, FAULT (ESCAPE SLIDE LT/ EPSU (12WL) EMER R) APPEARED. / T/S PER TSM 25-62-00-810-814-A. FOUND CANNON PLUG DISCONNECTED ON OWS 7505MM. RESECURED CANNON PLUG PER AMM 25-62-42-400-001-A. REPERFORMED BITE CHECK PER AMM 33-51-0
- [SDR WX0A2023112031896](https://openairdocs.org/sdr/WX0A2023112031896.md): Epsu · unknown · Nov 18, 2023 · N326NV · Airbus A319111 · Emergency Lighting
  > ALL EPSU BATTERIES FAILED BATTERY CAPACITY CHECK DURING TC 335100-03-1-001 / REPLACED ALL 4 EPSU BATTERIES IAW AMM 33-51-38-400-002-A. OPS CHECK GOOD."
- [SDR EE4Y2023080218154](https://openairdocs.org/sdr/EE4Y2023080218154.md): Fitting · cracked · Aug 2, 2023 · N326NV · Airbus A319111 · Fuselage Main, Structure
  > DURING THE ALLEGIANT TASK 53-210-003_P1-OP-UP-NDT/00 WORK CARD INSTRUCTIONS ACCOMPLISHMENT RELATED TO AD 2020-17-03, WAS FOUND THE LH/RH CONTINUITY FITTING WITH CRACK. AIRBUS WAS CONTACTED TO REQUEST THE KITS P/N FOR REPLACEMENT. AIRBUS PROVIDED THE INFORMATIO
- [SDR EE4Y2023080218155](https://openairdocs.org/sdr/EE4Y2023080218155.md): Window Frame · cracked · Aug 2, 2023 · N326NV · Airbus A319111 · Fuselage Main, Structure
  > DURING THE ALLEGIANT TASK 53-210-003 WORK CARD INSTRUCTIONS ACCOMPLISHMENT RELATED TO AD 2020-17-03, WAS FOUND THE WINDSHIELD FRAME WITH CRACK. AIRBUS WAS CONTACTED TO REQUEST REPAIR INSTRUCTIONS. AIRBUS PROVIDED THE INFORMATION WITH DOSSIER 81242975 AND TH
- [SDR EE4Y2023080218153](https://openairdocs.org/sdr/EE4Y2023080218153.md): Window Frame · cracked · Aug 2, 2023 · N326NV · Airbus A319111 · Fuselage Main, Structure
  > DURING THE ALLEGIANT TASK 53-210-003 WORK CARD INSTRUCTIONS ACCOMPLISHMENT RELATED TO AD 2020-17-03, WAS FOUND THE WINDSHIELD FRAME WITH CRACK. AIRBUS WAS CONTACTED TO REQUEST REPAIR INSTRUCTIONS. AIRBUS PROVIDED THE INFORMATION WITH DOSSIER 81242975 AND TH
- [SDR EE4Y2023080218152](https://openairdocs.org/sdr/EE4Y2023080218152.md): Skin Panel · corroded · Aug 2, 2023 · N326NV · Airbus A319111 · Wing, Plate/Skin
  > DURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: ZL-575-01-1-001, IT WAS FOUND AT LHWING, TOP SKIN LOWER SURFACE AT RIB 8 OVERHANG AREA WITH CORROSION. DUE THE DAMAGE IS BEYOND SRM LIMITS AIRBUS WAS CONTACTED REQUESTING REPAIR INSTRUCTIONS AND FINAL APPROVAL
- [SDR EE4Y2023080218151](https://openairdocs.org/sdr/EE4Y2023080218151.md): Skin Panel · corroded · Aug 2, 2023 · N326NV · Airbus A319111 · Wing, Plate/Skin
  > DURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: ZL-575-01-1-001, IT WAS FOUND AT LH WING, TOP SKIN LOWER SURFACE AT RIB 17 OVERHANG AREA WITH CORROSION. DUE THE DAMAGE IS BEYOND SRM LIMITS AIRBUS WAS CONTACTED REQUESTING REPAIR INSTRUCTIONS AND FINAL APPROV
- [SDR EE4Y2023080118150](https://openairdocs.org/sdr/EE4Y2023080118150.md): Frame · cracked · Aug 1, 2023 · N326NV · Airbus A319111 · Fuselage Main, Structure
  > DURING ALLEGIANT TASK INSPECTION 53-260-002 REAR FUSELAGE AFT PASS DOOR RH SIDE FR66 DOOR STOP FITTING # 7 AREA I/B UPPER FASTENER HOLE WITH CRACK WAS FOUND. COOPESA PERFORMED REPAIR IN ACCORDANCE A319 SRM TASK 53-41-12-300-010. THIS REPAIR IS COVERED WITH COO
- [SDR WX0A1900010074286](https://openairdocs.org/sdr/WX0A1900010074286.md): Servo Valve · faulty · Oct 17, 2022 · N326NV · Airbus A319111 · Master Cylinder/Brake Valve
  > (EMERGENCY DECLARED) AFTER SELECTING GEAR DOWN RECEIVED BRAKES ALTN R RELEASED, ECAM MESSAGE ""ALTN R BRK"" WAS DISPLAYED ON STATUS PAGE./ R&R BRK ALTN SERVOVALVE,R&R PRESS XDCR-BRK,YELLOW R (100GG) IAW AMM 32-44-29,R&R PRESS XDCR 100GG CONNECTOR (100GGA) IAW
- [SDR WX0A1900010031775](https://openairdocs.org/sdr/WX0A1900010031775.md): Unknown · unknown · Sep 30, 2022 · N326NV · Airbus A319111 · Standard Practices/Structures
  > REF: NRI 3-2 - APU EXHAUST ACCESS FAIRING 317AL FRAME WITH CORROSION./REPLACED FRAME PART NUMBER D524853820200 IAW A319 SRM 51-72-11-911-001 ATTACHED WITH SOLID RIVETS IAW A319 SRM 51-42-11 PARAG 2E(4) AND 51-42-11 PARAG 2E(2) REV.142 DATED:08-01-2022 AND IPC
- [SDR WX0A2022030274016](https://openairdocs.org/sdr/WX0A2022030274016.md): Epsu · dirty · Mar 2, 2022 · N326NV · Airbus A319111 · Emergency Lighting
  > EPSU TEST FAILS 12WL. / CLEANED CONNECTOR AT 12 WL CANON PLUG, BITE TESTED OK & OPS CHECK GOOD I/A/W AMM 33-51-38-400-001.AND ESPM 2055-30."
- [SDR WX0A2021121773898](https://openairdocs.org/sdr/WX0A2021121773898.md): Epsu · failed insp · Dec 10, 2021 · N326NV · Airbus A319111 · Emergency Lighting
  > BATTERY CAP TEST FAILED 12WL. / BITE CHECK 12WL CONFIRM BATTERY FAULT, REMOVED AND REPLACED BATTERY AT 12WL, BITE CHECK GOOD, EPSU TEST OK. REF AMM 33-51-38 PB 401."
- [SDR WX0A2021120873887](https://openairdocs.org/sdr/WX0A2021120873887.md): Epsu · faulty · Dec 6, 2021 · N326NV · Airbus A319111 · Emergency Lighting
  > DURING EPSU SYSTEM TEST FOUND FAULTY EPSU AT 10WL / REMOVED AND REPLACED FRONT EPSU 10WL IAW A319 AMM 33-51-31 PB401 OPS CHECK GOOD."
- [SDR WX0A1900010073975](https://openairdocs.org/sdr/WX0A1900010073975.md): None · none · Nov 18, 2021 · N326NV · Airbus A319111 · Fuselage, Wing Attach Fittings
  > NRC 1000-0129: AFT CARGO DOOR STRUCTURE, CORROSION LOCATED ON UPPER SURFACE OF FR 55A AT FASTENERS HOLE BTW STR 39RH-38RH / AFT CARGO DOOR SURROUND STRUCTURE ON UPPER SURFACE OF FR55A AT FASTENERS HOLES (QTY.2) BTW STR38RH-39RH SHEET ASSY REPAIRED AS PER AIRBU
- [SDR WX0A1900010073974](https://openairdocs.org/sdr/WX0A1900010073974.md): None · none · Nov 18, 2021 · N326NV · Airbus A319111 · Fuselage, Wing Attach Fittings
  > NRC 1000-0095: 31594-12 FLOOR LEVEL, ON CARGO DOOR ENTRANCE BTW FRAMES 59 TO 55A, SURFACE CORROSION ON TOP AND UNDER THE FLOOR FRAME STRG 38RH TO 37RH / AT AFT CARGO DOOR ENTRANCE UNDER FLOOR LEVEL BTW FR55A-FR59 AND STR37-38RH AREA, DOORSILL BEAM REPLACED AS
- [SDR WX0A1900010073973](https://openairdocs.org/sdr/WX0A1900010073973.md): Fitting · corroded · Nov 18, 2021 · N326NV · Airbus A319111 · Emergency Equipment
  > NRC 2000-0075: (823-12) CORROSION FOUND UNDER R1 DOOR FWD GIRT BAR FITTING,AROUND HI-LOCK. / ON FWD CREW DOOR CUTOUT LOWER MAIN SILL BEAM AREA UNDER GIRT BAR FITTING HOLE LOCATION, PERMANANTLY REPAIRED PERFOMED IAW SRM 53-11-14-283-005. FIG 001 SHEET 5, MAJOR
- [SDR WX0A1900010073972](https://openairdocs.org/sdr/WX0A1900010073972.md): Skin · corroded · Nov 18, 2021 · N326NV · Airbus A319111 · Wing, Plate/Skin
  > NRC 5000-0042: 33284-34 LH WING, UPPER SURFACE, CORROSION FOUND ON AREA FWD OF SPOILER #3 (BETWEEN RIB 13 AND 14) / LH WING UPPER SURFACE SKIN, FWD OF SPOILER #3 BTW RIB 13-14, UPPER SKIN REPAIRED AND FOUND STRUCTURALLY ACCEPTABLE IAW AIRBUS DOSSIER # 80969544
- [SDR WX0A1900010073971](https://openairdocs.org/sdr/WX0A1900010073971.md): Skin · corroded · Nov 18, 2021 · N326NV · Airbus A319111 · Wing, Plate/Skin
  > NRC 5000-0044: 33284-36 LH WING, AREA FWD OF SPOILER #2 (BETWEEN RIB 10 AND 11) SUSPECTED CORROSION (02 RIVET DAMAGED AND PRC MISSING) / AFTER INVESTIGATION, CORROSION FOUND AT LH WING UPPER SKIN AREA FWD OF SPOILER #2 AND RIB 10 AREA. LH WING UPPER SKIN FWD O
- [SDR WX0A1900010073970](https://openairdocs.org/sdr/WX0A1900010073970.md): None · none · Nov 18, 2021 · N326NV · Airbus A319111 · Fuselage Main, Structure
  > NRC 2000-0048: 031-9 AFT PASSENGER CABIN FLOOR STRUCTURE, CORROSION FOUND AT LH THRESHOLD BEAM LOWER MAIN SILL AREA BTW FRAME 66-68. / AFT PASSENGER CABIN FLOOR STRUCTURE, LOWER MAIN SILL AREA BTW FRAME 66-68, LH THRESHOLD BEAM PERMANENTLY REPAIRED AS PER SR
- [SDR WX0A1900010073969](https://openairdocs.org/sdr/WX0A1900010073969.md): Skin · corroded · Nov 18, 2021 · N326NV · Airbus A319111 · Wing, Plate/Skin
  > NRC 6000-0048: 1237-66. RH WING, CORROSION FOUND ON BOTTOM SKIN PANEL #3 UPPER SURFACE, BETWEEN REAR SPAR AND FASLE SPAR AREA, INBD OF RIB #6. / RH WING BOTTOM SKIN PANEL #3 UPPER SURFACE BTW REAR SPAR AND FALSE REAR SPAR AREA INBOARD OF RIB #6, CORROSION REMO
- [SDR WX0A1900010073966](https://openairdocs.org/sdr/WX0A1900010073966.md): None · none · Nov 18, 2021 · N326NV · Airbus A319111 · Wing Structure
  > NRC 5000-0027: 1237-20 LH WING REAR SPAR, MLG RETRACTION ACTUATOR JACK ANCHORAGE FITTING, CORROSION FOUND AROUND BUSHING ON UPPER AND LOWER FACE. / LH MLG RETRACTION,JACK ANCHORAGE FITTING REPAIRED AS PER SRM 57-26-13-300-025. SEE AWS FOR DETAILS.REPAIR CATEGO
- [SDR WX0A1900010073965](https://openairdocs.org/sdr/WX0A1900010073965.md): None · none · Nov 18, 2021 · N326NV · Airbus A319111 · Fuselage Main, Structure
  > NRC 2000-0049: 031-11 AFT PASSENGER CABIN FLOOR STRUCTURE, CORROSION FOUND AT RH THRESHOLD BEAM LOWER MAIN SILL AREA BTW FRAME 66-68. / AFT PASSENGER CABIN FLOOR STRUCTURE LOWER MAIN SILL AREA BTW FRAME 66-68, PERMANENTLY REPAIRED PERFORMED AT THRESHOLD BEA
- [SDR WX0A2021040273676](https://openairdocs.org/sdr/WX0A2021040273676.md): Power Supply · no test · Mar 31, 2021 · N326NV · Airbus A319111 · Emergency Lighting
  > CIDS EPSU SYS TEST FAULTING EPSUC (12WL) / REPLACED EPSU-POWER SUPPLY UNIT, OPS CHECK GOOD, REF AMM 33-51-38"
- [SDR WX0A2021031273660](https://openairdocs.org/sdr/WX0A2021031273660.md): Light · faulted · Mar 10, 2021 · N326NV · Airbus A319111 · Emergency Lighting
  > NOTICED LH EXIT ROW EMERG LIGHTS REMAIN ILLUMINATED-BITE CK EPSU SYS TEST WITH FAULTS 11WL/DEUB. / "
- [SDR WX0A2020112773609](https://openairdocs.org/sdr/WX0A2020112773609.md): Connector · disconnected · Nov 26, 2020 · N326NV · Airbus A319111 · Light System Wiring
  > EPSU TEST FAILS 13WL AFT LT EMERGENCY SLIDE LT. PERFORMED TSM 25-62-00-810-819-A REMOVED AND REPLACED 13WL ESPU AND FAILS EXTERIOR LIGHTS. CONTINUED TROUBLESHOOTING AND FOUND CONNECTER UNDER SLIDE COVER AT L2 DOOR SLIDE DISCONNECTED. RECONNECTED SLIDE WIRE
- [SDR WX0A2020082673562](https://openairdocs.org/sdr/WX0A2020082673562.md): Battery Pack · no test · Aug 25, 2020 · N326NV · Airbus A319111 · Emergency Lighting
  > DURING WEEKLY EPSU TEST BATTERY 11WL FLAGGED DURING TEST. REMOVED AND REPLACED EPSU BATTERY 11WL REF A319 AMM 33-51-38 PB 401. OPS CHECK GOOD.
- [SDR WX0A2020022073474](https://openairdocs.org/sdr/WX0A2020022073474.md): Epsu · no test · Feb 18, 2020 · N326NV · Airbus A319111 · Emergency Lighting
  > WHILE PERFORMING EMERGENCY LIGHT TEST GOT A BAT/ EPSU 13WL AFT L MSG. / REPLACED EPSU BATTERY ON EPSU"
- [SDR WX0A20200219475](https://openairdocs.org/sdr/WX0A20200219475.md): Power Supply · no test · Feb 18, 2020 · N326NV · Airbus A319111 · Emergency Lighting
  > WHILE PERFORMING EMERGENCY LIGHT TEST GOT A BAT/ EPSU 13WL AFT L MSG. / REMOVED AND REPLACED EPSU BATTERY ON EPSU 13WL REF A319 AMM 33-51-58 PB401. OPS CHECK GOOD."
- [SDR WX0A2016010473060](https://openairdocs.org/sdr/WX0A2016010473060.md): Warning System · activated · Jan 1, 2016 · N326NV · Airbus A319111 · Landing Gear Position and Warning
  > AFTER TAKEOFF FROM NLG INDICATOR DISPLAYED, UNLK, ACCOMPANIED WITH ECAM MSG, LG DOORS NOT CLOSED, & LG NOT LOCKED. THE CONDITION WAS OBVIOUS, CONFIRMED, DUE TO EXCESSIVE GEAR NOISE. PERFORMED ECAM PROCEDURE WHICH CORRECTED THE ISSUE. PERFORMED INSPECTION OF

## 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 = 'N326NV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N326NV/reports

---
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