# Service difficulty reports: N308NV

A list on [N308NV](https://openairdocs.org/aircraft/N308NV.md).

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

- [SDR WX0A2026090232940](https://openairdocs.org/sdr/WX0A2026090232940.md): Megaphone · expired · Aug 30, 2026 · N308NV · Airbus A319112 · Emergency Equipment
  > (AIRCRAFT NOT GROUNDED) FWD AND AFT CABIN MEGAPHONE EXPIRING REQUIRES REMOVAL AND REPLACEMENT. REMOVED AND REPLACED BOTH MEGAPHONES IAW LOPA. EMERGENCY EQUIPMENT LAYOUT REV L, DRAWING A125001L03
- [SDR WX0A2026080332909](https://openairdocs.org/sdr/WX0A2026080332909.md): Battery · inoperative · Aug 2, 2026 · N308NV · Airbus A319112 · Emergency Equipment
  > (AIRCRAFT NOT GROUNDED) FWD FA MEAGPHONE INOP / REMOVED AND REPLACED BATTERIES IAW AMM 25-65-51-02. OPS CHECK GOOD. "
- [SDR WX0A2026040832781](https://openairdocs.org/sdr/WX0A2026040832781.md): Epsu · inoperative · Apr 7, 2026 · N308NV · Airbus A319112 · Emergency Lighting
  > (AIRCRAFT NOT GROUNDED) EPSU BATTERIES 11WL AND 12WL FAULTED DURING EPSU BAT CAP TEST, REQUIRES REPLACEMENT / REMOVED AND REPLACED EPSU BATTERIES 11WL AND 12WL IAW AMM 33-51-38-000-002-A AND AMM 33-51-38-400-001-A OPS CHECK GOOD."
- [SDR EE4Y2025090823081](https://openairdocs.org/sdr/EE4Y2025090823081.md): Window Frame · cracked · Sep 8, 2025 · N308NV · Airbus A319112 · Fuselage Main, Structure
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT A32X-53-210-003-WINDSHIELD, UPPER FUSELAGE COCKPIT LH WINDSHIELD CENTER POST LOWER HORIZONTAL FLANGE OPEN FASTENER HOLE WITH CRACK DETECTED DURING ROTOTEST INSPECTION OF THE CONTINUITY FITTINGS REPLACE PROCEDURE AS PER AI
- [SDR EE4Y2025090823080](https://openairdocs.org/sdr/EE4Y2025090823080.md): Fitting · cracked · Sep 8, 2025 · N308NV · Airbus A319112 · Fuselage Main, Structure
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-210-003-WINDSHIELD, UPPER FUSELAGE COCKPIT WINDSHIELD CENTER POST LOWER ATTACHMENT ARE CONTINUITY FITTINGS LH AND RH WITH CRACK. THE BOTH FITTINGS WERE REPLACED FOLLOW THE ALLEGIANT ENGINEERING ORDER # A32X-S
- [SDR EE4Y2025090823079](https://openairdocs.org/sdr/EE4Y2025090823079.md): Frame · cracked · Sep 8, 2025 · N308NV · Airbus A319112 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-534123-01-2-001, UPPER FUSELAGE FR68 RH AT DOORSTOP 6 LEVEL FRAME INNER CAP JOINT TO GUSSET PLATE FASTENER HOLE WITH CRACK INDICATION DUE MISSED HOLE.PERFORMED GUSSET PLATE ATTACHMENT HOLES REPAIR AND GUSSET REP
- [SDR EE4Y2025090823078](https://openairdocs.org/sdr/EE4Y2025090823078.md): Door Frame · cracked · Sep 8, 2025 · N308NV · Airbus A319111 · Fuselage Main, Structure
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-534123-01-2-001, UPPER FUSELAGE FR66 RH AT DOORSTOP 4 LEVEL FRAME INNER CAP JOINT TO GUSSET PLATE FASTENER HOLE WITH CRACK INDICATION DUE MISSED HOLE.PERFORMED GUSSET PLATE ATTACHMENT HOLES REPAIR AND GUSSET REP
- [SDR WX0A2025021932322](https://openairdocs.org/sdr/WX0A2025021932322.md): Seal · broken · Feb 16, 2025 · N308NV · Airbus A319112 · Emergency Equipment
  > (AIRCRAFT NOT GROUNDED) AFT PBE SEAL BROKEN / INSTALLED SERVICABLE AFT PBE SEAL IAW ALLEGIANT PROCEDURES"
- [SDR EE4Y2024092620905](https://openairdocs.org/sdr/EE4Y2024092620905.md): Glowstrip · damaged · Sep 26, 2024 · N308NV · Airbus A319112 · Emergency Equipment
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 533187-01-1-001, UPPER FUSELAGE PAX CABIN CENTER SECTION EVACUATION PHOTOLUMINESCENSE STRIPS 2 EA DAMAGED.THE DAMAGE STRIP WERE REPLACED IAW A319 AMM TASK 33-51-21-000-001A AND TASK 33-51-21-400-001A. THIS REPAIR WAS
- [SDR EE4Y2024091820893](https://openairdocs.org/sdr/EE4Y2024091820893.md): Frame · cracked · Sep 18, 2024 · N308NV · Airbus A319112 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT OF THE WORK CARD 53-260-003, UPPER FUSELAGE AFT PASSENGER CREW DOOR FR68RHS DOOR STOP FITTING HOLES AT STOP FITTING # 1 INBOARD AND OUTBOARD LOWER HOLES WITH CRACK WERE FOUND. PERFORMED PERMANENT REPAIR AT RH REAR FUSELAGE FR68 DOOR STOP
- [SDR EE4Y2024091820892](https://openairdocs.org/sdr/EE4Y2024091820892.md): Frame · cracked · Sep 18, 2024 · N308NV · Airbus A319112 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT OF THE WORK CARD 53-260-003, UPPER FUSELAGE AFT PASSENGER CREW DOOR FR68 LHS DOOR STOP FITTING HOLES AT STOP FITTING # 1 INBOARD LOWER HOLE WITH CRACK WAS FOUND. PERFORMED PERMANENT REPAIR AT FR 68 LH DOOR STOP FITTING # 1 IAW ENGINEERIN
- [SDR EE4Y2024091820890](https://openairdocs.org/sdr/EE4Y2024091820890.md): Skin Panel · corroded · Sep 18, 2024 · N308NV · Airbus A319112 · Wing, Plate/Skin
  > DURING ACCOMPLISHMENT OF THE WORK CARD ZL-500-03-1-002 RH WING AT FRONT SPAR AREA BETWEEN RIB 1/2 TOP SKIN PANEL WITH CORROSION WAS FOUND, PERFORMED PERMANENT REPAIR AT RH WING TOP SKIN PANEL 1 UPPER SURFACE RIBS 1 AND 2 FRONT SPAR L.E OVERHANG IAW ENGINEERI
- [SDR EE4Y2024091820889](https://openairdocs.org/sdr/EE4Y2024091820889.md): Hinge Arm · corroded · Sep 18, 2024 · N308NV · Airbus A319112 · Vertical Stabilizer
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT WORK CARD ZL325-01-1-001, EMPENNAGE VERTICAL STABILIZER TRAILING EDGE CORROSION WAS FOUND COMMON TO ATTACHMENT HOLES AT THE TRAILING EDGE PANEL ATTACHMENT FLANGES OF THE HINGE ARM 6 LH /RH SIDE. PERFORMED REPAIR AT VERTIC
- [SDR EE4Y2024091820906](https://openairdocs.org/sdr/EE4Y2024091820906.md): Skin Panel · damaged · Sep 18, 2024 · N308NV · Airbus A319112 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT ENGINEERING ORDER E5311-0019, UPPER FUSELAGE FR16 LHS DOUBLE JOGGLE AREA AT LEVEL OF DOOR STOP # 1 HOLES #10,#12,#14;#15,#17 THRU #19 WERE FOUND GREATER THAN THE STARTING HOLE DIAMETER FOR COLD WORK PROCESS WERE FOUND. PE
- [SDR EE4Y2024091720891](https://openairdocs.org/sdr/EE4Y2024091720891.md): Skin Panel · cracked · Sep 17, 2024 · N308NV · Airbus A319112 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF THE ENGINEERING ORDER E5311-0019, UPPER FUSELAGE FR 16 LHS LOWER DOUBLE JOGGLE AREA HOLE # 14 WITH SKIN CRACKED WAS FOUND.PERFORMED PERMANENT REPAIR AT UPPER FUSELAGE FR16 LH DOUBLE JOGGLE IAW ENGINEERING ORDER COO-EO-2024-20736-R02
- [SDR EE4Y2024091620904](https://openairdocs.org/sdr/EE4Y2024091620904.md): Frame · cracked · Sep 16, 2024 · N308NV · Airbus A319112 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT ENGINEERING ORDER E5311-0119, UPPER FUSELAGE FR 16 LHS UPPER DOUBLE JOGGLE AREA HOLE # 7 WITH CRACK WAS FOUND. PERFORMED PERMANENT REPAIR AT UPPER FUSELAGE FR16LH DOUBLE JOGGLE AREA IAW EO COO-EO-2024-20736-R02 AND RDAF REF 81452785/004/2
- [SDR EE4Y2024091620895](https://openairdocs.org/sdr/EE4Y2024091620895.md): Door Frame · cracked · Sep 16, 2024 · N308NV · Airbus A319112 · Fuselage Main, Structure
  > DURING ACCOMPLISHMENT WORK CARD 53-260-003, UPPER FUSELAGE AFT PASSENGER/CREW DOOR FR 68RH SIDE DOOR STOP FITTING HOLES AT STOP FITTING # 6 INBOARD LOWER HOLE WITH CRACK WAS FOUND.PERMANENT REPAIR AT FR68 RHS STOP FITTING # 6 (FREEZE PLUG AND OVERSIZE BOLT INS
- [SDR WX0A2024081232151](https://openairdocs.org/sdr/WX0A2024081232151.md): Mechanism · malfunctioned · Aug 7, 2024 · N308NV · Airbus A319112 · Escape Slide
  > (AIRCRAFT NOT GROUNDED) REF: NRI 2-11 - DURING FUNCTIONAL TEST OF THE RELEASE MECHANISM OF THE EMERGENCY ESCAPE SLIDE, FOUND AFT RH DOOR EMERGENCY CONTROL HANDLE OUT OF LIMITS. / PERFORMED LUBRICATION OF SAFETY PIN GUIDE FITTING AND DOOR ARMING / DISARMING MEC
- [SDR WX0A2024081232150](https://openairdocs.org/sdr/WX0A2024081232150.md): Mechanism · faulted · Aug 7, 2024 · N308NV · Airbus A319112 · Escape Slide
  > (AIRCRAFT NOT GROUNDED) REF: NRI 2-12 - DURING FUNCTIONAL TEST OF THE RELEASE MECHANISM OF THE EMERGENCY ESCAPE SLIDE, FOUND AFT LEFT DOOR EMERGENCY CONTROL HANDLE OUT OF LIMITS. / PERFORMED LUBRICATION OF SAFETY PIN GUIDE FITTING AND DOOR ARMING / DISARMING M
- [SDR WX0A2024072232119](https://openairdocs.org/sdr/WX0A2024072232119.md): Megaphone · no test · Jul 18, 2024 · N308NV · Airbus A319112 · Emergency Equipment
  > (AIRCRAFT NOT GROUNDED) FWD CABIN MEGAPHONE INOP. / REMOVED AND REPLACED FWD CABIN MEGAPHONE IAW AMM 25-65-51-920-001-A."
- [SDR WX0A2023102731876](https://openairdocs.org/sdr/WX0A2023102731876.md): Epsu · unknown · Oct 25, 2023 · N308NV · Airbus A319112 · Emergency Lighting
  > EPSU 13WL FAILED CABIN EMERGENCY LIGHTING TEST / REMOVED AND REPLACED EPSU 13WL IAW AMM 33-51-38-000-001-A AND 33-51-38-400-001-A"
- [SDR WX0A2023091431841](https://openairdocs.org/sdr/WX0A2023091431841.md): Megaphone · unknown · Sep 12, 2023 · N308NV · Airbus A319112 · Emergency Equipment
  > FWD MEGA PHONE MISSING VOLUME KNOB. / REMOVED AND REPLACED FWD MEGA PHONE IAW LOPA."
- [SDR WX0A2023091031837](https://openairdocs.org/sdr/WX0A2023091031837.md): Epsu · unknown · Sep 4, 2023 · N308NV · Airbus A319112 · Emergency Lighting
  > DURING EMERGENCY LIGHT BITE TEST, FAILURE MESSAGE ''BAT/EPSU(13WL)AFT L''. / EPSU 13WL BATTERY REPLACED AND TESTED SERVICEABLE IAW AMM 33-51-38-400-002A"
- [SDR WX0A2023090631831](https://openairdocs.org/sdr/WX0A2023090631831.md): Epsu · unknown · Sep 4, 2023 · N308NV · Airbus A319112 · Emergency Lighting
  > DURING EMERGENCY LIGHT BITE TEST, FAILURE MESSAGE ''BAT/EPSU(13WL)AFT L''. / EPSU 13WL BATTERY REPLACED AND TESTED SERVICEABLE IAW AMM 33-51-38-400-002A"
- [SDR WX0A1900010031851](https://openairdocs.org/sdr/WX0A1900010031851.md): Unknown · unknown · Sep 2, 2023 · N308NV · Airbus A319112 · Elevator, Plate/Skin
  > REINSPECT TEMP REPAIR AT EVERY SERVICE CHECK, FOUND LH ELEVATOR UPPER SKIN WITH COMPOSITE DAMAGE 74'' FROM OUTBOARD EDGE, 134'' FROM INBOARD EDGE, 6'' FROM LEADING EDGE AND 17'' FROM TRAILLING EDGE. MEASUREMENTS L=2.5'' W=2'' MAX D 0.244'' INSPECTED LH ELEVAT
- [SDR WX0A2023073131806](https://openairdocs.org/sdr/WX0A2023073131806.md): Unknown · unknown · Jul 31, 2023 · N308NV · Airbus A319112 · Cabin Pressure Controller
  > (EMERGENCY DECLARED) CAB PR SYS 1 FAULT IN FLIGHT, EXCESSIVE CABIN ALT MASTER WARNS SHORTLY AFTER, OUTFLOW VALVE SHOWED 1/4 OPEN ON SYSTEM PAGE. CABIN ALTTUDE EXCEEDED 25000, O2 MASK DROPPED. SYSTEM WAS IN AUTO ECAMS COMPLIED WITH. / CPC1 (11HL) WAS NOT RESPO
- [SDR WX0A2023050331763](https://openairdocs.org/sdr/WX0A2023050331763.md): Epsu · unknown · May 2, 2023 · N308NV · Airbus A319112 · Emergency Lighting
  > BATTERY CAPACITY CHECK FAULTED 10WL, 11WL, 12WL BATTERY. / R & R'D LEFT EMERGENCY EXIT EPSU 10WL,11WL,12WL BATTERY IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A."
- [SDR EE4Y2023031017364](https://openairdocs.org/sdr/EE4Y2023031017364.md): Fitting · cracked · Mar 10, 2023 · N308NV · Airbus A319112 · Fuselage Main, Structure
  > DURING THE STRUCTURE INSPECTION WE FOUND AT COCKPIT WINDSHIELD AREA, INNER SIDE OF THE UPPER ATTACHMENT OF THE SIDE POST AT FR4, T FITTING AT LH SIDE, INNER HOLE WITH CRACK INDICATION. CORRECTIVE ACTION: THE FITTING WAS REPAIRED AS PER AIRBUS INSTRUCTIONS AST
- [SDR WX0A2022082674220](https://openairdocs.org/sdr/WX0A2022082674220.md): Megaphone · inoperative · Aug 26, 2022 · N308NV · Airbus A319112 · Escape Slide
  > FA REPORTED FWD CABIN MEGAPHONE WEAK / REMOVED AND REPLACED MEGAPHONE PER AIRBUS A320 LOPA A1250001L03, OPS CHECK GOOD"
- [SDR WX0A2021111773872](https://openairdocs.org/sdr/WX0A2021111773872.md): Epsu · failed · Nov 16, 2021 · N308NV · Airbus A319112 · Emergency Lighting
  > AFTER STARTING EPSU BAT CAP TEST, FAILURE ""BAT/EPSU(13WL)AFT L"" APPEARED. / REF. TSM 33-51-00-810-857, R & R'D EPSU BATTERY (13WL) AFT L IAW AMM 33-51-38."
- [SDR EE4Y2021092513904](https://openairdocs.org/sdr/EE4Y2021092513904.md): Fitting · cracked · Sep 26, 2021 · N308NV · Airbus A319112 · Fuselage Structure (General)
  > PER CUSTOMER INSPECTION TASK, IT WAS FOUND ON LH AND RH WINDSHIELD SIDE POST UPPER ATTACHMENT FITTING - 2 EA HOLES WITH CRACK INDICATION. DUE TO THIS FACT DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL.
- [SDR WX0A2021052473722](https://openairdocs.org/sdr/WX0A2021052473722.md): Battery Pack · no test · May 22, 2021 · N308NV · Airbus A319112 · Emergency Lighting
  > R/H (12WL) EMERGENCY LIGHT BATTERY PACK DISPLAYS FAILED ON EMERGENCY LIGHT TEST / REMOVED AND REPLACED R/H (12WL) EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-38-000-002-A AND 33-51-38-400-002-A."
- [SDR WX0A2021052473721](https://openairdocs.org/sdr/WX0A2021052473721.md): Battery Pack · no test · May 22, 2021 · N308NV · Airbus A319112 · Emergency Lighting
  > FWD L/H (10WL) EMERGENCY LIGHT BATTERY PACK DISPLAYS FAILED ON EMERGENCY LIGHT TEST / REMOVED AND REPLACED FWD L/H (10WL) EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-38-000-002-A AND 33-51-38-400-002-A OPS CHECK GOOD."
- [SDR WX0A2021030373652](https://openairdocs.org/sdr/WX0A2021030373652.md): Cover · broken · Mar 2, 2021 · N308NV · Airbus A319112 · Emergency Lighting
  > RH WALL LIGHT EMERGENCY SIGN COVER BOTTOM LEFT & RIGHT COVER TABS BROKEN / REMOVED AND REPLACED RH BOTTOM LEFT & RIGHT WALL LIGHT EMERGENCY SIGN COVER IAW AMM 33-51-13-000-001-A & 33-51-13-400-001-A. THIS CLEARS M313 CONTROL # 05330001
- [SDR WX0A2020091473572](https://openairdocs.org/sdr/WX0A2020091473572.md): Epsu · no test · Sep 11, 2020 · N308NV · Airbus A319112 · Emergency Lighting
  > EPSU 11WL FAULT DURING WEEKLY CHECK. C/W TSM 33-51-00-810-855-A. REMOVED AND REPLACED 11WL EPSU BATTERY, AS PER A319 AMM 33-51-38 PB401. OPS CHECKS GOOD, FAULT CLEARED.
- [SDR WX0A2020070373521](https://openairdocs.org/sdr/WX0A2020070373521.md): Battery · failed · Jul 2, 2020 · N308NV · Airbus A319112 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY FIN 11WL FAILED CAPACITY CHECK. REPLACED EMERGENCY LIGHT BATTERY FIN 11WL IAW AMM 33-51-38. OPS CHECK GOOD.
- [SDR WX0A2020041573499](https://openairdocs.org/sdr/WX0A2020041573499.md): Battery · discharged · Apr 13, 2020 · N308NV · Airbus A319112 · Emergency Lighting
  > EPSU BATTERY FIN# 13WL FAILED EPSU BAT CAP TEST / REPLACED EPSU BATTERY"
- [SDR WX0A2019031173386](https://openairdocs.org/sdr/WX0A2019031173386.md): Blower · odor · Mar 10, 2019 · N308NV · Airbus A319112 · Air Distribution Fan
  > ELECTRICAL ODOR FROM VENTILATION SYSTEM. R&R BLOWER FAN".
- [SDR WX0A2018072173356](https://openairdocs.org/sdr/WX0A2018072173356.md): Not Reported · leaking · Jul 16, 2018 · N308NV · Airbus A319112 · Hydraulic System, Main
  > STRONG DIRTY SOCK SMELL NOTICED DURING DESCENT, HYDRAULIC LEAK FOUND AT SERVICING BAY. R&R CHECK VALVE, RECIRC FILTERS, WATER INJECTORS, OZONE FILTERS AND PERFORMED DECONTAMINATION OF ECS.
- [SDR 2017FA0000302](https://openairdocs.org/sdr/2017FA0000302.md): Control Unit · failed · Jul 27, 2017 · N308NV · Airasc J2AIRASC · Landing Gear Retraction/Extension System
  > DURING LANDING GEAR EXTENSION, ECAM DISPLAYED L/G LGCU 1&2 FAULT. ECAM PROCEDURE COMPLETED AND LANDING GRAVITY EXTENSION PROCEDURE COMPLETED. REMOVED AND REPLACE NLG SENSING MECHANISM AND PROX SENSOR 24GA & 25GA AND TARGETS PER MM 32-21-45-400-801A,32-31-73-2
- [SDR WX0A2017073100282](https://openairdocs.org/sdr/WX0A2017073100282.md): Proximity Sensor · failed · Jul 22, 2017 · N308NV · Airbus A319112 · Landing Gear Position and Warning
  > DUAL LGCIU FAILURE. EMERGENCY DECLARED. R & R THE NLG FLIGHT GROUND SENSING MECHANISM, PROXIMITY SENSOR, AND TARGETS.
- [SDR WX0A2017072673282](https://openairdocs.org/sdr/WX0A2017072673282.md): Interface Unit · failed · Jul 22, 2017 · N308NV · Airbus A319112 · Landing Gear Position and Warning
  > EMERGENCY DECLARED, DUAL LGCIU FAILURE. CORRECTIVE ACTION PENDING-AC AOG.

## 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 = 'N308NV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N308NV/reports

---
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