N338NV

Service difficulty reports · 46

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 = 'N338NV' 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 WX0A2026071732894Engine · faulted(AIRCRAFT GROUNDED) (ENG SHUTDOWN EVENT) AT ABOUT 26000FT DURING A DECENT ENG 1 MADE A LOUD BANG AND SHUT ITSELF DOWN. UPON INSPECTION, DETERMINATION MADE FOR ENGINE REPLACEMENT. ASSIGNED W.O. 556297 FOR REPLACEMENT. REFER TO ALL NR'S ON WORK ORDER.Jul 17, 2026 · N338NV · Airbus A319112 · Engine (Turbine/Turboprop)SDR WX0A2026021332732Power Supply · no testAIRCRAFT NOT GROUNDED. 10WL FAILED EPSU BATTERY CAPACITY TEST AND 11WL FAILED EPSU BATTERY TEST. R & R 10WL EPSU IAW AMM 33-51-38-000-001-A AND AMM 33-51-38-400-002-A. R & R 11WL EPSU IAW AMM 33-51-38-000-001-A AND AMM 33-51-38-400-002-A.Feb 11, 2026 · N338NV · Airbus A319111 · Emergency LightingSDR WX0A2025092432579Lens · brokenAIRCRAFT NOT GROUNDED, EXIT LIGHT COVER FROM L1 BROKEN. INSTALLED EXIT LIGHT LENS AT L1 DOOR IAW AMM 33-51-13-400-001-A. A/C OK FOR SERVICE.Sep 22, 2025 · N338NV · Airbus A319111 · Emergency LightingSDR WX0A2025061332458Slide · faulted(AIRCRAFT NOT GROUNDED) LEFT OVERWING SLIDE NOT ARMED / REMOVED AND REINSTALLED LT OVER WING EXIT ROW DOOR TO RESET SLIDE IND. IAW AMM 52-21-11-04 CONF"Jun 12, 2025 · N338NV · Airbus A319111 · Escape SlideSDR WX0A2025061832466Cooling Fan · odor(AIRCRAFT NOT GROUNDED) AFTER LANDING AFT FA'S REPORTED ""DIRTY SOCKS"" SMELL FOR LAST 15 MIN OF FLIGHT ON DESCENT / PERFORMED TC A32X-21-000-001, BEFORE PERFORMING ENGINE RUNS REACTICATED PACK 2 IAW AMM 21-51-00-400-002-A. WHILE AT THE GATE WITH APU BLEED ANDJun 10, 2025 · N338NV · Airbus A319111 · Air Distribution FanSDR WX0A2025060632448Slide · inoperative(AIRCRAFT NOT GROUNDED) FA ADVISES L1 DOOR SLIDE WILL NOT ARM / PERFOMED OPS CHECK SEVERAL TIMES IAW AMM 25-42-44-400-006-A NO FAULTS FOUND. NORMAL OPERATION VERIFIED."Jun 5, 2025 · N338NV · Airbus A319111 · Escape SlideSDR EE4Y2025060422450Fitting · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT WORK CARD A32X-53-210-003, UPPER FUSELAGE COCKPIT WINDSHIELD CENTER POST LOWER ATTACHMENT AREA CONTINUITY FITTINGS WITH CRACK WERE FOUND. CONTINUITY FITTINGS WERE REPLACED PER ALLEGIANT EO # A32X-STR-53ERO-00285-R00.THIS Jun 4, 2025 · N338NV · Airbus A319112 · Fuselage Main, StructureSDR EE4Y2025060422449Door Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT INSPECTION PER WROK CARD A32X-53-260-002, UPPER FUSELAGE AFT PAX CABIN/CREW ENTRY DOOR FR 66 LHS DOOR STOP FITTING # 2 LOWER I/B HOLE WITH CRACK INDICATION. PERFORMED REPAIR STOP FITTING HOLES OF LH AFT DOOR FR 66 FREEZE Jun 4, 2025 · N338NV · Airbus A319112 · Fuselage Main, StructureSDR EE4Y2025060422448Door Frame · crackedDURING ALLEGIANT INSPECTION PER WORK CARD A32X-53-260-002, UPPER FUSELAGE AFT PAX CABIN/ENTRY DOOR FR66 LHS DOOR STOP FITTING # 1 LOWER I/B HOLE WITH CRACK INDICATION WAS FOUND.PERFORMED REPAIR STOP FITTING HOLES OF LHS AFT DOOR FR 66 - FREEZE PLUG AND OVERSIZJun 4, 2025 · N338NV · Airbus A319112 · Fuselage Main, StructureSDR EE4Y2025060422447Door Frame · crackedDURING ALLEGIANT INSPECTION PER WORK CARD A32X-53-260-002, UPPER FUSELAGE AFT PAX CABIN/CREW ENTRY DOOR FR66 RHS DOOR STOP FITTING # 1 LOWER I/B HOLE WITH CRACK INDICATION WAS FOUND.PERFORMED REPAIR STOP FITTING HOLES OF RHS AFT DOOR FR 66 FREEZE PLUG AND OVERJun 4, 2025 · N338NV · Airbus A319112 · Fuselage Main, StructureSDR EE4Y2025060422446Frame · crackedDURING ALLEGIANT INSPECTION PER EO # A32X-E5311-0018, UPPER FUSELAGE DOOR FR16 RH AT DOUBLE JOGGLE AREA IN THE OUTER FLANGE OF THE FRAME AFT ROW OF FASTENER TWO INCHES ABOVE OF THE STOP FITTING 7 FASTENER HOLE WITH CRACK INDICATION WAS FOUND.PERFORMED FASTENERJun 4, 2025 · N338NV · Airbus A319112 · Fuselage Main, FrameSDR WX0A2025032832369Oxygen Bottle · faulted(AIRCRAFT NOT GROUNDED) OXYGEN CONTAINER ROW 26ABC CAME DOWN AFTER TAKE OFF. / REMOVED AND REPLACED EMERGENCY O2 CONTAINER AT 26ABC IAW AMM 35-21-41-000/400-001-A. OPS CHECK GOOD. THIS CLEARS MEL 35-21-01A. MDDR# 209815. PLACARDS REMOVED."Mar 27, 2025 · N338NV · Airbus A319111 · Passenger Oxygen SystemSDR WX0A2025032432365Light · inoperative(AIRCRAFT NOT GROUNDED) EMERGENCY EXIT LIGHT ABOVE R1 DOOR INOP / REPLACED LIGHT ASSEMBLY, OPS CHECK GOOD IAW AMM 33-51-11-04 CONF 00"Mar 22, 2025 · N338NV · Airbus A319111 · Emergency LightingSDR WX0A2025012732287Stowage Box · no test(AIRCRAFT NOT GROUNDED) F/O OXYGEN MASK NOT TESTING PROPERLY / REMOVED & REPLACED F/O'S MASK AND BOX REF AMM 35-12-41-400-001-A OPS AND LEAK OK"Jan 26, 2025 · N338NV · Airbus A319111 · Crew Oxygen SystemSDR WX0A2024120432227Skin · dented(AIRCRAFT NOT GROUNDED) (DISCREPANCY NOTED DURING AIRCRAFT HEAVY MX VISIT) PERMANENT REPAIR PER EA 79-2024-184 NEED ACCOMPLISHED. DENT FWD FUSE AT FR21 +300MM, BELOW STR 23L / PERMANENT REPAIR PER EA 79-2024-184 ACCOMPLISHED. DENT FWD FUES AT FR21+300 MM BELONov 29, 2024 · N338NV · Airbus A319111 · Fuselage Main, FrameSDR WX0A2024022631967Epsu · no testDURING EPSU BATTERY CAPACITY TEST ALL FOUR BATTERIES FAILED. / REMOVED AND REPLACED EPSU BATTERIES (10WL, 11WL, 12WL, 13WL) REF AMM 33-51-38-000-002-A & 33-51-38-400-002-A. OPS TEST GOOD."Feb 22, 2024 · N338NV · Airbus A319111 · Emergency LightingSDR WX0A2023121131916Epsu · unknownEPSU 11WL FAILED WEEKLY BITE CHECK / TROUBLESHOT PER TSM 33-51-00-810-834-A. REMOVED AND REPLACED 11WL BATTERY PER AMM 33-51-38-000-001-A AND AMM 33-51-38-400-001-A. OPS CHECK GOOD"Dec 10, 2023 · N338NV · Airbus A319111 · Emergency LightingSDR WX0A2023100431858Epsu · unknownFOUND FWD EMERGANCY LIGHTS OUT / REPLACED EMER BATTERY PACK, FWD FIN 10WL, OPS CHECK GOOD REF AMM 33-51-38-400-002A"Oct 3, 2023 · N338NV · Airbus A319111 · Emergency LightingSDR WX0A2023083031826Epsu · unknownEPSU BATTERY 13WL AFT, FAILED CAP TEST PER T/C 335100-03-1 / REPLACED AFT EPSU BATTERY FIN 13WL IAW AMM 33-51-38-000-002A AND 33-51-38-400-002A. OPS CHECKS NORMAL."Aug 29, 2023 · N338NV · Airbus A319111 · Emergency LightingSDR EE4Y2023062717942Frame · unknownDURING THE STRUCTURAL INSPECTION AS PER ALLEGIANT TASK: 534124-01-2-001 AN EXISTNG REPAIR WHICH INTERFERES WITH THE INSPECTION AND WITH A DEVIATION WAS FOUND. ALL DETAILS ABOUT EXISTING REPAIR WERE SENT TO AIRBUS ASKING ABOUT FORM APPROVAL TO COVER THE DEVIATIJun 27, 2023 · N338NV · Airbus A319112 · Fuselage Structure (General)SDR EE4Y2023031017394Beam · corrodedDURING TH ESTRUCTURE INSPECTION WAS FOUND AT UPPER FUSELAGE FORWARD PAX CABIN AT FR 16, Y503.2 LONGITUDINAL BEAM WITH CORROSION. DUE TO THIS FACT LONGITUDINAL BEAM P/N: D5311282720200 FROM FR 12 TO FR 16 Y503.2 WAS REPLACED IAW A319 SRM 51-72-11-911-001. THE RMar 10, 2023 · N338NV · Airbus A319111 · Fuselage Structure (General)SDR EE4Y2023031017393None · corrodedDURING TH ESTRUCTURE INSPECTION WAS AT UPPER FUSELAGE AFT PASSENGER CREW DOOR CUTOUT BETWEEN FR 66 AND FR 68 AT STRG 23R SILL BEAM WITH CORROSION. DUE TO THIS FACT SILL BEAM P/N D5348004320701 WAS REPLACED IAW A319 SRM 51-72-11-911-001 PARAGRAPH 2B. THE REPLACMar 10, 2023 · N338NV · Airbus A319111 · Fuselage Structure (General)SDR EE4Y2023031017392Beam · corrodedDURING TH ESTRUCTURE INSPECTION WAS AT UPPER FUSELAGE AFT PAX CABIN AT FR 68+80MM Y160.5 LONGITUDINAL BEAM WITH CORROSION. DUE TO THIS FACT LONGITUDINAL BEAM FROM FR 68 TO FR 70 Y160.5 WAS REPLACED IAW A319 SRM 51-72-11-911-001. THE REPLACE WAS HANDLED UNDER CMar 10, 2023 · N338NV · Airbus A319111 · Fuselage Structure (General)SDR EE4Y2023031017391Beam · corrodedDURING TH ESTRUCTURE INSPECTION WAS FOUND IN THE UPPER FUSELAGE AFT PAX CABIN AT FR 68 Y765 LONGITUDINAL BEAM WITH CORROSION. DUE TO THIS FACT LONGITUDINAL BEAM P/N D5472192200000 WAS REPLACED IAW A319 SRM 51-72-11-911-001 PARAGRAPH 2 . THE REPAIR WAS HANDLED Mar 10, 2023 · N338NV · Airbus A319111 · Fuselage Structure (General)SDR EE4Y2023031017390Frame · noneDURING TH ESTRUCTURE INSPECTION WAS FOUND IN THECCKPIT WINSHIEL SIDE POST FR 4LH UPPER ATTACHMENT FITTING AND FRAME SECTION WITH DOUBLE HOLE. DUE TO THIS FACT FITTING P/N D5311086620200 AND FRAME P/N D53111068202200 WERE REPLACED. THE REPAIR WAS HANDLED UNDER Mar 10, 2023 · N338NV · Airbus A319111 · Fuselage Structure (General)SDR EE4Y2023100317401Skin Panel · dentedDESCRIPTION: DURING THE STRUCTURAL INSPECTION, IT WAS FOUND AT LH WING SLAT #1 FROM TRACK #2 100MM O/B AND 111MM FROM THE LOWER EDGE, EXTERNAL SKIN WITH DENT CORRECTIVE ACTION EVALUATED DENT AND IT WAS FOUND WITHIN LIMITS IAW A319 SRM 57-40-00-283-001 FIGURMar 10, 2023 · N338NV · Airbus A319111 · Wing StructureSDR EE4Y2023100317400Skin Panel · corrodedDESCRIPTION: DURING THE STRUCTURAL INSPECTION PER ALLEGIANT WORK CARD 200003-01-1-001_P1-OP-UP/0 PROCESS, COO FOUND AT EMPENNAGE, DORSAL FIN AREA WITH CORROSION BETWEEN THE SKIN AND CONNECTOR 7113VC. CORRECTIVE ACTION REPAIRED FUSELAGE SKIN SECTION FROM FMar 10, 2023 · N338NV · Airbus A319111 · Fuselage Structure (General)SDR EE4Y2023031017399Fitting · corrodedDESCRIPTION: DURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: 553006-01-2-001 MPD, IT WAS FOUND AT EMPENNAGE RUDDER HINGE ARM#7 WITH CORROSION. CORRECTIVE ACTION: REPLACED HINGE ARM BR7 IAW A319-SRM TASK 55-36-42-300-003. SEE COOPESA WORK ORDER A1M116 Mar 10, 2023 · N338NV · Airbus A319111 · Empennage StructureSDR EE4Y2023031017398Fitting · noneDESCRIPTION: DURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: 553006-01-2-001 MPD, IT WAS FOUND AT EMPENNAGE RUDDER HINGE #3 BEARING WITH PLAY. CORRECTIVE ACTION: REPLACED FORK AND END FITTING AT HINGE ARM BR3 IAW A319-SRM TASK 55-36-42-300-008. SEEMar 10, 2023 · N338NV · Airbus A319111 · Empennage StructureSDR EE4Y2023031017397Fitting · noneDESCRIPTION: DURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: 553006-01-2-001 MPD, IT WAS FOUND AT EMPENNAGE RUDDER HINGE #7 BEARING WITH PLAY. CORRECTIVE ACTION: REPLACED FORK AND END FITTING AT HINGE ARM BR7 IAW A319-SRM TASK 55-36-42-300-008. SEEMar 10, 2023 · N338NV · Airbus A319111 · Empennage StructureSDR EE4Y2023031017396Fitting · excess playDURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: 553006-01-2-001 MPD, IT WAS FOUND AT EMPENNAGE RUDDER HINGE#5 BEARING WITH PLAY. REPLACED FORK AND END FITTING AT HINGE ARM BR5 IAW A319-SRM TASK 55-36-42-300-008. SEE COOPESA WORK ORDER A1M116 3-16Mar 10, 2023 · N338NV · Airbus A319111 · Fuselage Main, StructureSDR EE4Y2023031017395Fitting · excess playDURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: 553006-01-2-001 MPD, IT WAS FOUND AT EMPENNAGE RUDDER HINGE#4 BEARING WITH PLAY. REPLACED FORK AND END FITTING AT HINGE ARM BR4 IAW A319-SRM TASK 55-36-42-300-008. SEE COOPESA WORK ORDER A1M116 3-15Mar 10, 2023 · N338NV · Airbus A319111 · Fuselage Main, StructureSDR WX0A2023010931694Megaphone · no testAFT MEGAPHONE FAILED PRE FLIGHT INSPECTION / REMOVED AND REPLACED MEGAPHONES PER LOPA ""A125000L03"" REV ""00"" AND PER AMM 25-65-51"Jan 8, 2023 · N338NV · Airbus A319111 · Emergency EquipmentSDR WX0A2023010931693Megaphone · noneFWD MEGAPHONE FAILED PRE FLIGHT INSPECTION / PERFORMED OPS CHECK ON MEGAPHONE ""FLASHING GREEN"" INDICATES GOOD BATTIERIES. OPS CHECK GOOD PER AMM 25-65-710-002"Jan 8, 2023 · N338NV · Airbus A319111 · Emergency EquipmentSDR WX0A2022091674250None · noneR2 DOOR SLIDE INADVERTENTLY DEPLOYED / REPLACED R2 SLIDE PER AMM 25-62-44-000-802-A. GOOD FOR SERVICE."Sep 14, 2022 · N338NV · Airbus A300* · Emergency Locator BeaconSDR WX0A2022090674232Epsu · noneEPSU BATTERY (10WL) FWD L FAILED WHEN PERFORMING TC CHECK BATTERY CAPACITY 335100-03-1-001. / R&R EPSU BATTERY (10WL) FWD L IAW TSM 33-51-00-810-822-A. OPS CHECK GOOD. NO DEFECTS NOTED."Sep 6, 2022 · N338NV · Airbus A319111 · Lighting SystemSDR WX0A2022080874195Megaphone · noneR2 MEGAPHONE INOP / R&R'D MEGAPHONE IN REF TO AMM 25-65-11. OPS CHECK GOOD."Aug 6, 2022 · N338NV · Airbus A319111 · Escape SlideSDR EE4Y2022063015861Frame · crackedDURING THE STRUCTURAL INSPECTION PER 531135-01-2-001 MPD, IT WAS FOUND LH WINDSHIELD SIDE POST UPPER ATTACHMENT AT FRAME 4 WITH A HOLE WITH CRACK INDICATION AND FITTING WITH A DOUBLE HOLE AND FRAME SECTION WITH TOOL MARK. . DUE TO THIS FACT DETAILS WERE SENT TJun 30, 2022 · N338NV · Airbus A319111 · Fuselage Structure (General)SDR WX0A2022012473935Cover · missingTHE R/H FWD EMERGENCY EXIT WALL MOUNTED LIGHT COVER MISSING / REPLACED MISSING LENS COVER ON THE R/H FWD EMERGENCY EXIT WALL MOUNTED LIGHT IAW AMM 33-51-13"Jan 23, 2022 · N338NV · Airbus A319111 · Emergency LightingSDR WX0A2021093073848Battery Pack · faultedWHEN POWER IS DISCONNECTED AND EMERGENCY LIGHTS ARE SUPPOSED TO TRIGGER ON, ONLY THE REAR CABIN EXIT SIGN AND OVERHEAD LIGHTS AT SEAT ROWS 19 AND 28 ILLUMINATE. ALL OTHER OVERHEAD LIGHTS ARE INOP, INCLUDING OVERWING EXIT SIGNS AND L1 & R1 EXIT SIGNS. / FOUND (Sep 27, 2021 · N338NV · Airbus A319111 · Emergency LightingSDR WX0A2021092773844Battery Pack · faultedWHEN POWER IS DISCONNECTED AND EMERGENCY LIGHTS ARE SUPPOSED TO TRIGGER ON, ONLY THE REAR CABIN EXIT SIGN AND OVERHEAD LIGHTS AT SEAT ROWS 19 AND 28 ILLUMINATE. FOUND (10WL , 11WL AND 12WL) EPSU BATTERY TO BE FAULTING REPLACED ALL 3 BATTERY IAW AMM 33-51-38 Sep 26, 2021 · N338NV · Airbus A319111 · Emergency LightingSDR WX0A2021051773717Battery Pack · no testR/H OVER WING EMERGENCY POWER PACK BATTERY FAILS TEST. / REPLACED R/H EMERGENCY POWER PACK BATTERY AND PERFORMED OPS TEST PER AMM 33-51-38 P/B 401. OK FOR SERVICE."May 15, 2021 · N338NV · Airbus A319112 · Emergency LightingSDR WX0A2020080373542Battery Pack · no testCABIN EMERGENCY BATTERY CLASS 1 FAULT AFT L (13WL) / REMOVED AND REPLACED AFT L EMERGENCY SUPPLY BATTERY UNIT IAW AMM 33-51-000-002-A AND 33-51-38-400-002-A. OPS CHECK GOOD"Jul 31, 2020 · N338NV · Airbus A319111 · Emergency LightingSDR WX0A2020072473532Controller · malfunctionedDESCENDING THROUGH APPROXIMATELY FL320 RECEIVED ECAM CAB PR EXCESS CAB ALT AND COMPLIED WITH THOSE PROCEDURE. CABIN PRESSURE GOT AS HIGH AS 12500 FT. MASK DID NOT DEPLOY. OTHER ECAM THAT FOLLOWED WERE CABPR LO DIFF PR, DOOR R AFT CABIN, AND CAB PR SAFETY VALVJul 23, 2020 · N338NV · Airbus A319111 · Cabin Pressure ControllerSDR WX0A2019120273441Battery Pack · inoperativeDURING EMERGENCY LIGHT TEST FOUND EMERGENCY BATTERY PACK 12WL INOP / "Dec 1, 2019 · N338NV · Airbus A319112 · Emergency LightingSDR WX0A2019120273440Battery Pack · inoperativeDURING EMERGENCY LIGHT TEST FOUND EMERGENCY LIGHT BATTERY PACK 11WL INOP. / "Nov 29, 2019 · N338NV · Airbus A319112 · Emergency Lighting
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