N219NV
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 = 'N219NV' 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.
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 = 'N219NV' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR WX0A2025120132651Power Supply · no test(AIRCRAFT NOT GROUNDED) DURING EPSU BITE TEST, EMERGENCY BATTERY 10WL FAILED. EMERGENCY BATTERY 10WL REPLACED AND TESTED SERVICEABLE PER AMM 33-51-38-400-002-A.SDR WX0A2025061632460Battery · no test(AIRCRAFT NOT GROUNDED) FA FLASHLIGHT WONT TURN ON / REMOVED AND REPLACED FA FLASHLIGHT BATTERY PER AMM 25-65-00 OPS CHECKS GOOD"SDR WX0A2025040732377Oxygen Mask · no test(AIRCRAFT NOT GROUNDED) CAP OXYGENMASK NOT TESTING PROPERLY / REMOVED AND REPLACED OB'S BOX/MASK IAW AMM 35-12-41-000-001-A AND 35-12-41-400-001-A OPS CHECK AND LEAK CHECK GOOD. INOP PLACARD REMOVED."SDR WX0A2024060332064Controller · faulted(EMERGENCY DECLARED)(AIRCRAFT GROUNDED) CAB PR SYS2 FAULT ECAM AFTER ENG SHUT DOWN. CABIN PR CONTROLLERS 1 AND 2 REMOVED AND REPLACED IAW AMM 21-31-34-000-001-A AND 21-31-34-400-001-A. OPS CHECK GOOD. CLEAN PFR ON ARRIVAL AT BQN.SDR EE4Y2024032219627Rib · corrodedDURING THE STRUCTURAL INSPECTION PER ALLEGIANT TASK CARD 572179-01-1-001 RELATED TO MPDTASK 572179-01, IT WAS FOUND AT LH WING REAR SPAR AREA THE RIBLET L WITH CORROSION. SINCE THAT THE MENTIONED RIBLETS HAVE DEEP CORROSION, THEY WILL BE REPLACED BY NEW ONES.DSDR EE4Y2024032219625Skin · corrodedDURING ACCOMPLISHMENT OF THE ALLEGIANT WORK CARD 572179-01-1-001 LH WING TRAILING EDGEBETWEEN RIB 15 AND RIB 16 OVERHANG AREA WITH CORROSION WAS FOUND.DAMAGE WAS REPORTED TOAIRBUS ASKING REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRUCTIONS AND OVERHANG ARESDR EE4Y2024032219567Skin Panel · corrodedDURING ACCOMPLISHMENT OF THE ALLEGIANT WORK CARD 572179-01-1-002 RH WING TRAILING EDGEBETWEEN RIB 13 AND RIB 16 OVERHANG AREA WITH CORROSION WAS FOUND.DAMAGE WAS REPORTED TO AIRBUS ASKING REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRUCTIONS AND OVERHANG ARSDR EE4Y2024032219622Rib · corrodedDURING THE STRUCTURAL INSPECTION PER ALLEGIANT TASK CARD 572179-01-1-002 RELATED TO MPD TASK 572179-01, IT WAS FOUND AT RH WING REAR SPAR AREA THE RIBLET J WITH CORROSION. SINCE THAT THE MENTIONED RIBLETS HAVE DEEP CORROSION, THEY WILL BE REPLACED BY NEW ONES.SDR EE4Y2024032219621Rib · corrodedDURING THE STRUCTURAL INSPECTION PER ALLEGIANT TASK CARD 572179-01-1-002 RELATED TO MPD TASK 572179-01, IT WAS FOUND AT RH WING REAR SPAR AREA THE RIBLET E WITH CORROSION. SINCE THAT THE MENTIONED RIBLETS HAVE DEEP CORROSION, THEY WILL BE REPLACED BY NEW ONES.SDR EE4Y2024032219719Plate · corrodedDURING ACCOMPLISHMENT OF ALLEGIANT WORK CARD ZL-471-01-1-002, RH WING LOWER SURFACE PYLON REINFORCING PLATE WITH CORROSION BETWEEN WING RIB 8 AND RIB 9 STRINGER 5 AND 6. AIRBUS WAS CONTATCED ASKING REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRUCTIONS AND DSDR EE4Y2024032219718Battery · inoperativeDURING ACCOMPLISHMENT OF THE EMERGENCY LIGHTING TEST IAW ALLEGIANT WORK CARD 335100-03-1-001 , FWD LH EPSU BATTERY WAS FOUND INOP. THE EPSU BATTERIES FWD 2H WAS REPLACED IAW A320 AMM TASK 33-51-38-000-002-A AND 33-51-38-400-002-A. AFTER NEW THE SYSTEM WAS FOUSDR EE4Y2024032119626Skin Panel · corrodedDURING ACCOMPLISHMENT OF THE ALLEGIANT WORK CARD 572179-01-1-001 LH WING TRAILING EDGE BETWEEN RIB 21 AND RIB 22 OVERHANG AREA WITH CORROSION WAS FOUND.DAMAGE WAS REPORTED TO AIRBUS ASKING REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRUCTIONS AND OVERHANG ASDR EE4Y2024032119682Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT WORK CARD 534135-01-4-001, UPPER FUSELAGE AFT PAX/CREW DOOR CUT OUT AT FR68 LEVEL STGR 8L FRAME VERTICAL INTERNAL RADIUS CRACK WAS FOUND. AIRBUS WAS CONTATCED TO REQUEST REPAIR INSTRUCTIONS. AIRBUS PROVIDE REPAIR INSTRUCTSDR EE4Y2024032119681Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT WORK CARD 534135-01-4-001 , UPPER FUSELAGE AFT PAX DOOR CUT OUT AT FR68 STGR 8RH FRAME VERTICAL INTERNAL RADIUS CRACK WAS FOUND. AIRBUS WAS CONTATCED TO REQUEST REPAIR INSTRUCTIONS. AIRBUS PROVIDED SRM REFERENCE TO PERFORSDR EE4Y2024032119680Frame · crackedDURING THE ACCOMPLISHMENT OF WORK ORDER 53-260-004 UPPER FUSELAGE AFT PASSENGER CREW DOOR CUTOUT AT FR 68 STRINGER 22 LH WEB HORIZONTAL LOWER FLANGE RADII CRACKED WAS FOUND.AIRBUS WAS CONTACTED ASKING REPAIRINSTRUCTIONS.AIRBUS PROVIDED REPAIR INSTRUCTIONS ANDSDR EE4Y2024031919618Frame · crackedDURING THE ACCOMPLISHMENT OF ALLEGIANT ENGINEERING ORDER E5331-0011 AT FR43 RH WITH OPEN HOLE CRACKED AT MILLED FRAME LAYER WAS FOUND.AIRBUS WAS CONTACTED ASKING REPAIR INSTRUCTIONS.AIRBUS PROVIDED REPAIR INSTRUCTIONS AND FR43 RHS FOOT COUPLING WITH HOLE CRACKSDR EE4Y2024031919679Frame · damagedDURING THE ACCOMPLISHMENT OF ALLEGIANT TASK 53-260-003 AT FR68 LH STOP FITTING # 7 WITH OUTBOARD HOLES ELONGATED WERE FOUND.AIRBUS WAS CONTACTED ASKING REPAIR INSTRUCTIONS.AIRBUS PROVIDED REPAIR INSTRUCTIONS AND FR68 LH HOLES WERE REPAIRED FOLLOW THE REPAIR INSDR EE4Y2024031819678Frame · damagedDURING THE ACCOMPLISHMENT OF ALLEGIANT TASK 53-260-003 AT FR68LH STOP FITTING # 5 WITH OUTBOARD HOLES ELONGATED WERE FOUND.AIRBUS WAS CONTACTED ASKING REPAIR INSTRUCTIONS.AIRBUS PROVIDED REPAIR INSTRUCTIONS AND FR68 LH HOLES WERE REPAIRED FOLLOW THE REPAIR INSSDR EE4Y2024031819677Frame · damagedDURING THE ACCOMPLISHMENT OF ALLEGIANT TASK 53-260-003 AT FR68LH STOP FITTING # 3 WITH OUTBOARD HOLES ELONGATED WERE FOUND.AIRBUS WAS CONTACTED ASKING REPAIR INSTRUCTIONS.AIRBUS PROVIDED REPAIR INSTRUCTIONS AND FR68 LH HOLES WERE REPAIRED FOLLOW THE REPAIR INSSDR EE4Y2024031819676Frame · crackedDURING THE ACCOMPLISHMENT OF ALLEGIANT TASK 53-260-003 AT FR68LH STOP FITTING # 2| INBOARD LOWER HOLE WITH CRACK WAS FOUND.AIRBUS WAS CONTACTED ASKING REPAIR INSTRUCTIONS.AIRBUSPROVIDED REPAIR INSTRUCTIONS AND FR68 LH HOLES WERE REPAIRED FOLLOW THE REPAIRINSTRSDR EE4Y2024031819675Frame · corrodedDURING THE ACCOMPLISHMENT OF ALLEGIANT TASK 53-260-003 AT FR68LH STOP FITTING # 1| WITH ALL HOLES CORRODED WERE FOUND.AIRBUS WAS CONTACTED ASKING REPAIR INSTRUCTIONS.AIRBUS PROVIDED REPAIR INSTRUCTIONS AND FR68 LH HOLES WERE REPAIRED FOLLOW THE REPAIR INSTRUCTSDR WX0A2024031831981Battery · inoperativeAFT MEGAPHONE BATTERY INOP / REMOVED AND REPLACED THE AFT MEGAPHONE IAW AMM 25-65-51-710-002-A, STEP 3B AND STEP 5A AND LOPA A2250001L03"SDR EE4Y2024031519620Frame · crackedDURING THE ACCOMPLISHMENT OF ALLEGIANT TASK 53-260-002 AT FR66LH STOP FITTING #6 WITHOUTBOARD HOLES ELONGATED WERE FOUND.AIRBUS WAS CONTACTED ASKING REPAIR INSTRUCTIONS.AIRBUS PROVIDED REPAIR INSTRUCTIONS AND FR66LH HOLES WERE REPAIRED FOLLOW THE REPAIRINSTRUCSDR WX0A2023091031839Unknown · unknownEXIT SIGN ABOVE R1 DOOR HAS MULTIPLE INOP BULBS / REPLACED SEVERAL BULBS ON EXIT SIGN ABOVE R1 DOOR PER AMM 33-51-00-710-001"SDR WX0A2023020131719Epsu · noneL2 AND R2 EMERGENCY LIGHTS AND SIGNS ARE INOP WHILE ON BATTERY POWER / REMOVED AND REPLACED AFT EPSU IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A. OPS CHECK GOOD"SDR WX0A2022090774237Epsu · noneEMERGENCY LIGHTS INOP AT L1,R1,BOTH OVERWINGS AND MOST CEILING LIGHTS. / REMOVED AND REPLACED EMERGENCY LIGHT BATTERYS AT FIN 10WL, 11WL, AND 12WL OPS CHECK GOOD PER AMM 33-51-38 AND TSM 33-51-00-810-812-A."SDR WX0A2022081274198Light · inoperativeDURING EMERGENCY LIGHTING CHECK FOUND LH OVERWING EXIT LIGHT INOP / FOUND ALL LAMPS TO BE BURNT OUT, RELAMPED THE LIGHT DISTRIBUTION ASSY FOR THE LEFT HAND OVERWING EXIT LIGHT IAW AMM 33-51-15. OPERATIONAL CHECKS GOOD NO FURTHER DISCREPANCIES NOTED."SDR WX0A2022071874161Megaphone · damagedFORWARD FA MEGAPHONE APPEARS TO GOTTEN WET FROM RAIN, IS INTERMITTENT. / R/R FWD FA MEGAPHONE PER LOPA."SDR WX0A2022011073921Light · false indicationFA REPORTS THAT NONE OF THE EMERGENCY EXIT LIGHTS TURNED OFF AFTER GEAR RETRACTION. EMER EXIT LT SWITCH VERIFIED IN ARM POSITION / PER TSM 33-51-00-810-881-A PERFORMED OPERATIONAL TEST OF CABIN LIGHTS REF AMM 33-51-00-710-004-A OPS TEST GOOD A/C OKAY FOR SERVSDR DU4R2021010400002Box Beam · crackedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FL, FOUND RT FR 43 SIDE BOX BEAM FLANGE HOLES NR 9, NR 20 AND NR 11 HAVE CRACK INDICATIONS IN THE AFT DIRECTION. S/O 193117 N/R 24166.SDR DU4R2021010400001Box Beam · crackedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FL, FOUND LT FR 43 SIDE BOX BEAM FLANGE HOLES NR 9 AND NR 10 HAVE A CRACK INDICATION IN THE AFT DIRECTION. S/O 193117 N/R 24165.SDR WX0A201801120001Plug · leakingODOR DETECTED DURING DESCENT, TIGHTENED & SECURED A LOOSE APU GENERATOR OIL DRAIN PLUG. R & R THE RECIRCULATION FILTERS.SDR WX0A2017053073254Valve · malfunctionedRECEIVED AN ECAM FOR THE MLG DOOR NOT CLOSED, EMERGENCY DECLARED, FOLLOWED BY MULTIPLE HYDRAULIC SYSTEM FAULTS. R & R NLG DOOR GROUND OPERATING VALVE.SDR WX0A073201Water Heater · failedPREVIOUS CREW REPORTED BURNING ODOR IN AFT RIGHT LAVATORY DURING FLIGHT. TROUBLESHOT AND FOUND RIGHT AFT LAV FAUCET WATER HEATER TO HAVE A BURNED ODOR. REMOVED AND REPLACED WATER HEATER.SDR WX0A073179Indicator · inoperativeDURING TAKE OFF ROLL ABORTED AT 100 KIAS DUE TO NO AIRSPEED INDICATION ON CAPT IAS. FO INDICATED 100 KIAS. AUTO BRAKES DEPLOYED MAXIMUM BOT BRAKES. PEAK TEMPERATURE 340C OAT 27C / PERFORMED LEAK TEST OF PITOT STATIC SYSTEM ON BOTH CAPT AND FO SIDES NOTICED AIRSDR WX0A2016041200131Slide · unwanted deployRIGHT OFF WING EMERGENCY SLIDE DEPLOYED. R & R RT WING SLIDE IAW AMM 25-62-42. R & R RT SLIGHT BOTTLE IAW AMM 25-62-46.SDR WX0A2016041273133Vhf Comm · malfunctionedLOST COMM, BOTH VHF & BOTH PILOTS, FOR 10 MIN DURING DESCENT. UNABLE TO HEAR CTR, BUT COULD HEAR OTHER ACFT CALLING CTR. FINALLY ABLE TO HEAR ANOTHER ACFT, GUARD TO US NEW FREQUENCIES. PERFORMED TROUBLESHOOTING IAW TSM 23-12-00, NO FAULTS FOUND.SDR WX0A2016030173095Circuit Breaker · pulled7000' ECAM AT BLW 100' COMPLY WITH ECAM ACTIONS. UNABLE TO RESTORE, SYS WENT TO MANUAL MODE & DID NOT WORK, PRESS WENT UP, CABIN ALT 5800'. TROUBLESHOOTING REVEALED A PULLED & COLLARED CB Y17, AVIONICS VENT MONITORING, & THE EXTRACT AIR VLV SWITCH IN THE OFFSDR WX0A2015081172782Light · inoperativeSEVERAL LIGHTS BURNED OUT AT L1, L2, R1 & R2 EMER EXIT SIGNS. RELAMPED L1, L2, R1 & R2 EMER EXIT SIGNS IAW MM 33-51-16. OPERATIONS CHECKED GOOD.SDR WX0A2015081172785Water Heater · overheatedELECTRIC BURNING SMELL COMING FROM AFT LAVATORY, ACFT RT. MEL 38-10-01A CAT C LAVATORY E HOT WATER DEACTIVATED. TROUBLE SHOT IAW TSM 05-50-00-810-831-A. FOUND LAVATORY E WATER HEATER OVERHEATING. PLACARD INSTALLED.SDR WX0A2015061572657Unknown · odorBACK RT LAVATORY, FLIGHT ATTENDANT REPORTS BURNING & ELEC SMELL. FLIGHT ATTENDANT REPORTED SMELL WHEN ACFT LANDED. INSPECTED RT AFT LAVATORY FOR ODORS, NONE FOUND AT THIS TIME. REPLACED RT AFT LAVATORY EXTRACT FAN FILTER PRECAUTIONARY IAW TSM 05-50-00 & AMMSDR WX0A2015033072495Blade · damagedENGINE NR 2 N1 VIBES READS 3.4 ON CLIMB OUT. ENG VIBES REACH 1.0 PASSING 200FL ON DESCENT 8000. ENG NR 2 VIBES SPIKED TO 8.8 THEN STABILIZED AT 4.0 FOR REMAINDER OF LANDING, COULD EASILY FEEL THE VIBE THROUGHOUT THE ACFT. INSPECTION OF ENG NR 2 INLET EVIDENSDR WX0A2015033072494Warning System · false activationLANDING GEAR SYS DISAGREE ON LANDING ROLLOUT. COMPUTE SYS RESET IAW MX CONTROL. BL 11695 FAULT CLEARED.SDR WX0A2015021672418Light · inoperativeSEVERAL EMER LIGHT LAMPS WILL NOT ILLUMINATE. REPLACED EMER LIGHT LAMPS IN CTR RT EXIT & RT FWD EXIT IAW AMM 33-51-00.SDR WX0A2014111872264Battery · dischargedAFT R2 FLIGHT ATTENDANT STATION FLASHLIGHT INOPERATIVE. R & R AFT FLIGHT ATTENDANT STATION FLASHLIGHT BATTERY IAW AMM 25-60-00. OPERATIONS CHECKED GOOD.SDR WX0A2014092572168Slide · deployedWHILE PERFORMING WORK CARD 25-831-002 DOOR ESCAPE SLIDE, L2 DOOR SLIDE ENGAGED & DEPLOYED. REMOVED L2 SLIDE IAW AMM 25-62-44-000-010-A. FOR SLIDE INSTALLATION REFERENCE WORK ORDER 00235140.
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