N308NV

Service difficulty reports · 42

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR WX0A2026090232940Megaphone · expired(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 A125001L03Aug 30, 2026 · N308NV · Airbus A319112 · Emergency EquipmentSDR WX0A2026080332909Battery · inoperative(AIRCRAFT NOT GROUNDED) FWD FA MEAGPHONE INOP / REMOVED AND REPLACED BATTERIES IAW AMM 25-65-51-02. OPS CHECK GOOD. "Aug 2, 2026 · N308NV · Airbus A319112 · Emergency EquipmentSDR WX0A2026040832781Epsu · inoperative(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."Apr 7, 2026 · N308NV · Airbus A319112 · Emergency LightingSDR EE4Y2025090823081Window Frame · crackedDURING 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 AISep 8, 2025 · N308NV · Airbus A319112 · Fuselage Main, StructureSDR EE4Y2025090823080Fitting · crackedDURING 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-SSep 8, 2025 · N308NV · Airbus A319112 · Fuselage Main, StructureSDR EE4Y2025090823079Frame · crackedDURING 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 REPSep 8, 2025 · N308NV · Airbus A319112 · Fuselage Main, FrameSDR EE4Y2025090823078Door Frame · crackedDURING 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 REPSep 8, 2025 · N308NV · Airbus A319111 · Fuselage Main, StructureSDR WX0A2025021932322Seal · broken(AIRCRAFT NOT GROUNDED) AFT PBE SEAL BROKEN / INSTALLED SERVICABLE AFT PBE SEAL IAW ALLEGIANT PROCEDURES"Feb 16, 2025 · N308NV · Airbus A319112 · Emergency EquipmentSDR EE4Y2024092620905Glowstrip · damagedDURING 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 WASSep 26, 2024 · N308NV · Airbus A319112 · Emergency EquipmentSDR EE4Y2024091820893Frame · crackedDURING 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 Sep 18, 2024 · N308NV · Airbus A319112 · Fuselage Main, FrameSDR EE4Y2024091820892Frame · crackedDURING 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 ENGINEERINSep 18, 2024 · N308NV · Airbus A319112 · Fuselage Main, FrameSDR EE4Y2024091820890Skin Panel · corrodedDURING 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 ENGINEERISep 18, 2024 · N308NV · Airbus A319112 · Wing, Plate/SkinSDR EE4Y2024091820889Hinge Arm · corrodedDURING 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 VERTICSep 18, 2024 · N308NV · Airbus A319112 · Vertical StabilizerSDR EE4Y2024091820906Skin Panel · damagedDURING 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. PESep 18, 2024 · N308NV · Airbus A319112 · Fuselage Main, Plate/SkinSDR EE4Y2024091720891Skin Panel · crackedDURING 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-R02Sep 17, 2024 · N308NV · Airbus A319112 · Fuselage Main, Plate/SkinSDR EE4Y2024091620904Frame · crackedDURING 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 81452785/004/2Sep 16, 2024 · N308NV · Airbus A319112 · Fuselage Main, FrameSDR EE4Y2024091620895Door Frame · crackedDURING 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 INSSep 16, 2024 · N308NV · Airbus A319112 · Fuselage Main, StructureSDR WX0A2024081232151Mechanism · malfunctioned(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 MECAug 7, 2024 · N308NV · Airbus A319112 · Escape SlideSDR WX0A2024081232150Mechanism · faulted(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 MAug 7, 2024 · N308NV · Airbus A319112 · Escape SlideSDR WX0A2024072232119Megaphone · no test(AIRCRAFT NOT GROUNDED) FWD CABIN MEGAPHONE INOP. / REMOVED AND REPLACED FWD CABIN MEGAPHONE IAW AMM 25-65-51-920-001-A."Jul 18, 2024 · N308NV · Airbus A319112 · Emergency EquipmentSDR WX0A2023102731876Epsu · unknownEPSU 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"Oct 25, 2023 · N308NV · Airbus A319112 · Emergency LightingSDR WX0A2023091431841Megaphone · unknownFWD MEGA PHONE MISSING VOLUME KNOB. / REMOVED AND REPLACED FWD MEGA PHONE IAW LOPA."Sep 12, 2023 · N308NV · Airbus A319112 · Emergency EquipmentSDR WX0A2023091031837Epsu · unknownDURING 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"Sep 4, 2023 · N308NV · Airbus A319112 · Emergency LightingSDR WX0A2023090631831Epsu · unknownDURING 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"Sep 4, 2023 · N308NV · Airbus A319112 · Emergency LightingSDR WX0A1900010031851Unknown · unknownREINSPECT 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 ELEVATSep 2, 2023 · N308NV · Airbus A319112 · Elevator, Plate/SkinSDR WX0A2023073131806Unknown · unknown(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 RESPOJul 31, 2023 · N308NV · Airbus A319112 · Cabin Pressure ControllerSDR WX0A2023050331763Epsu · unknownBATTERY 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."May 2, 2023 · N308NV · Airbus A319112 · Emergency LightingSDR EE4Y2023031017364Fitting · crackedDURING 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 Mar 10, 2023 · N308NV · Airbus A319112 · Fuselage Main, StructureSDR WX0A2022082674220Megaphone · inoperativeFA REPORTED FWD CABIN MEGAPHONE WEAK / REMOVED AND REPLACED MEGAPHONE PER AIRBUS A320 LOPA A1250001L03, OPS CHECK GOOD"Aug 26, 2022 · N308NV · Airbus A319112 · Escape SlideSDR WX0A2021111773872Epsu · failedAFTER 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."Nov 16, 2021 · N308NV · Airbus A319112 · Emergency LightingSDR EE4Y2021092513904Fitting · crackedPER 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.Sep 26, 2021 · N308NV · Airbus A319112 · Fuselage Structure (General)SDR WX0A2021052473722Battery Pack · no testR/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."May 22, 2021 · N308NV · Airbus A319112 · Emergency LightingSDR WX0A2021052473721Battery Pack · no testFWD 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."May 22, 2021 · N308NV · Airbus A319112 · Emergency LightingSDR WX0A2021030373652Cover · brokenRH 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 # 05330001Mar 2, 2021 · N308NV · Airbus A319112 · Emergency LightingSDR WX0A2020091473572Epsu · no testEPSU 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.Sep 11, 2020 · N308NV · Airbus A319112 · Emergency LightingSDR WX0A2020070373521Battery · failedEMERGENCY LIGHT BATTERY FIN 11WL FAILED CAPACITY CHECK. REPLACED EMERGENCY LIGHT BATTERY FIN 11WL IAW AMM 33-51-38. OPS CHECK GOOD.Jul 2, 2020 · N308NV · Airbus A319112 · Emergency LightingSDR WX0A2020041573499Battery · dischargedEPSU BATTERY FIN# 13WL FAILED EPSU BAT CAP TEST / REPLACED EPSU BATTERY"Apr 13, 2020 · N308NV · Airbus A319112 · Emergency LightingSDR WX0A2019031173386Blower · odorELECTRICAL ODOR FROM VENTILATION SYSTEM. R&R BLOWER FAN".Mar 10, 2019 · N308NV · Airbus A319112 · Air Distribution FanSDR WX0A2018072173356Not Reported · leakingSTRONG 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.Jul 16, 2018 · N308NV · Airbus A319112 · Hydraulic System, MainSDR 2017FA0000302Control Unit · failedDURING 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,32-31-73-2Jul 27, 2017 · N308NV · Airasc J2AIRASC · Landing Gear Retraction/Extension SystemSDR WX0A2017073100282Proximity Sensor · failedDUAL LGCIU FAILURE. EMERGENCY DECLARED. R & R THE NLG FLIGHT GROUND SENSING MECHANISM, PROXIMITY SENSOR, AND TARGETS.Jul 22, 2017 · N308NV · Airbus A319112 · Landing Gear Position and WarningSDR WX0A2017072673282Interface Unit · failedEMERGENCY DECLARED, DUAL LGCIU FAILURE. CORRECTIVE ACTION PENDING-AC AOG.Jul 22, 2017 · N308NV · Airbus A319112 · Landing Gear Position and Warning
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