# Service difficulty reports: N219NV

A list on [N219NV](https://openairdocs.org/aircraft/N219NV.md).

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

- [SDR WX0A2025120132651](https://openairdocs.org/sdr/WX0A2025120132651.md): Power Supply · no test · Nov 29, 2025 · N219NV · Airbus A320214 · Emergency Lighting
  > (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 WX0A2025061632460](https://openairdocs.org/sdr/WX0A2025061632460.md): Battery · no test · Jun 13, 2025 · N219NV · Airbus A320214 · Emergency Equipment
  > (AIRCRAFT NOT GROUNDED) FA FLASHLIGHT WONT TURN ON / REMOVED AND REPLACED FA FLASHLIGHT BATTERY PER AMM 25-65-00 OPS CHECKS GOOD"
- [SDR WX0A2025040732377](https://openairdocs.org/sdr/WX0A2025040732377.md): Oxygen Mask · no test · Apr 5, 2025 · N219NV · Airbus A320214 · Flight Compartment Equipment
  > (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 WX0A2024060332064](https://openairdocs.org/sdr/WX0A2024060332064.md): Controller · faulted · Jun 1, 2024 · N219NV · Airbus A320214 · Cabin Pressure Controller
  > (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 EE4Y2024032219627](https://openairdocs.org/sdr/EE4Y2024032219627.md): Rib · corroded · Mar 22, 2024 · N219NV · Airbus A320214 · Wing, Rib/Bulkhead
  > DURING 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.D
- [SDR EE4Y2024032219625](https://openairdocs.org/sdr/EE4Y2024032219625.md): Skin · corroded · Mar 22, 2024 · N219NV · Airbus A320214 · Wing, Plate/Skin
  > DURING 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 ARE
- [SDR EE4Y2024032219567](https://openairdocs.org/sdr/EE4Y2024032219567.md): Skin Panel · corroded · Mar 22, 2024 · N219NV · Airbus A320214 · Wing, Plate/Skin
  > DURING 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 AR
- [SDR EE4Y2024032219622](https://openairdocs.org/sdr/EE4Y2024032219622.md): Rib · corroded · Mar 22, 2024 · N219NV · Airbus A320214 · Wing, Rib/Bulkhead
  > DURING 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 EE4Y2024032219621](https://openairdocs.org/sdr/EE4Y2024032219621.md): Rib · corroded · Mar 22, 2024 · N219NV · Airbus A320214 · Wing, Rib/Bulkhead
  > DURING 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 EE4Y2024032219719](https://openairdocs.org/sdr/EE4Y2024032219719.md): Plate · corroded · Mar 22, 2024 · N219NV · Airbus A320214 · Wing, Plate/Skin
  > DURING 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 D
- [SDR EE4Y2024032219718](https://openairdocs.org/sdr/EE4Y2024032219718.md): Battery · inoperative · Mar 22, 2024 · N219NV · Airbus A320214 · Emergency Lighting
  > DURING 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 FOU
- [SDR EE4Y2024032119626](https://openairdocs.org/sdr/EE4Y2024032119626.md): Skin Panel · corroded · Mar 21, 2024 · N219NV · Airbus A320214 · Wing, Plate/Skin
  > DURING 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 A
- [SDR EE4Y2024032119682](https://openairdocs.org/sdr/EE4Y2024032119682.md): Frame · cracked · Mar 21, 2024 · N219NV · Airbus A320214 · Fuselage Main, Frame
  > DURING 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 INSTRUCT
- [SDR EE4Y2024032119681](https://openairdocs.org/sdr/EE4Y2024032119681.md): Frame · cracked · Mar 21, 2024 · N219NV · Airbus A320214 · Fuselage Main, Frame
  > DURING 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 PERFOR
- [SDR EE4Y2024032119680](https://openairdocs.org/sdr/EE4Y2024032119680.md): Frame · cracked · Mar 21, 2024 · N219NV · Airbus A320214 · Fuselage Main, Frame
  > DURING 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 AND
- [SDR EE4Y2024031919618](https://openairdocs.org/sdr/EE4Y2024031919618.md): Frame · cracked · Mar 19, 2024 · N219NV · Airbus A320214 · Fuselage Main, Frame
  > DURING 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 CRACK
- [SDR EE4Y2024031919679](https://openairdocs.org/sdr/EE4Y2024031919679.md): Frame · damaged · Mar 19, 2024 · N219NV · Airbus A320214 · Fuselage Main, Frame
  > DURING 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 IN
- [SDR EE4Y2024031819678](https://openairdocs.org/sdr/EE4Y2024031819678.md): Frame · damaged · Mar 18, 2024 · N219NV · Airbus A320214 · Fuselage Main, Frame
  > DURING 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 INS
- [SDR EE4Y2024031819677](https://openairdocs.org/sdr/EE4Y2024031819677.md): Frame · damaged · Mar 18, 2024 · N219NV · Airbus A320214 · Fuselage Main, Frame
  > DURING 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 INS
- [SDR EE4Y2024031819676](https://openairdocs.org/sdr/EE4Y2024031819676.md): Frame · cracked · Mar 18, 2024 · N219NV · Airbus A320214 · Fuselage Main, Frame
  > DURING 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 REPAIRINSTR
- [SDR EE4Y2024031819675](https://openairdocs.org/sdr/EE4Y2024031819675.md): Frame · corroded · Mar 18, 2024 · N219NV · Airbus A320214 · Fuselage Main, Frame
  > DURING 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 INSTRUCT
- [SDR WX0A2024031831981](https://openairdocs.org/sdr/WX0A2024031831981.md): Battery · inoperative · Mar 17, 2024 · N219NV · Airbus A320214 · Emergency Equipment
  > AFT 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 EE4Y2024031519620](https://openairdocs.org/sdr/EE4Y2024031519620.md): Frame · cracked · Mar 15, 2024 · N219NV · Airbus A320214 · Fuselage Main, Frame
  > DURING 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 REPAIRINSTRUC
- [SDR WX0A2023091031839](https://openairdocs.org/sdr/WX0A2023091031839.md): Unknown · unknown · Sep 8, 2023 · N219NV · Airbus A320214 · Emergency Lighting
  > EXIT 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 WX0A2023020131719](https://openairdocs.org/sdr/WX0A2023020131719.md): Epsu · none · Jan 30, 2023 · N219NV · Airbus A320214 · Emergency Lighting
  > L2 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 WX0A2022090774237](https://openairdocs.org/sdr/WX0A2022090774237.md): Epsu · none · Sep 6, 2022 · N219NV · Airbus A320214 · Lighting System
  > EMERGENCY 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 WX0A2022081274198](https://openairdocs.org/sdr/WX0A2022081274198.md): Light · inoperative · Aug 11, 2022 · N219NV · Airbus A320214 · Flight Compartment Lighting
  > DURING 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 WX0A2022071874161](https://openairdocs.org/sdr/WX0A2022071874161.md): Megaphone · damaged · Jul 15, 2022 · N219NV · Airbus A320214 · Escape Slide
  > FORWARD FA MEGAPHONE APPEARS TO GOTTEN WET FROM RAIN, IS INTERMITTENT. / R/R FWD FA MEGAPHONE PER LOPA."
- [SDR WX0A2022011073921](https://openairdocs.org/sdr/WX0A2022011073921.md): Light · false indication · Jan 7, 2022 · N219NV · Airbus A320214 · Emergency Lighting
  > FA 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 SERV
- [SDR DU4R2021010400002](https://openairdocs.org/sdr/DU4R2021010400002.md): Box Beam · cracked · Dec 30, 2020 · N219NV · Airbus A320214 · Fuselage Main, Structure
  > DURING 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 DU4R2021010400001](https://openairdocs.org/sdr/DU4R2021010400001.md): Box Beam · cracked · Dec 30, 2020 · N219NV · Airbus A320214 · Fuselage Main, Structure
  > DURING 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 WX0A201801120001](https://openairdocs.org/sdr/WX0A201801120001.md): Plug · leaking · Jan 11, 2018 · N219NV · Airbus A320214 · Electrical Power System
  > ODOR DETECTED DURING DESCENT, TIGHTENED & SECURED A LOOSE APU GENERATOR OIL DRAIN PLUG. R & R THE RECIRCULATION FILTERS.
- [SDR WX0A2017053073254](https://openairdocs.org/sdr/WX0A2017053073254.md): Valve · malfunctioned · May 23, 2017 · N219NV · Airbus A320214 · Landing Gear Door Retract Section
  > RECEIVED AN ECAM FOR THE MLG DOOR NOT CLOSED, EMERGENCY DECLARED, FOLLOWED BY MULTIPLE HYDRAULIC SYSTEM FAULTS. R & R NLG DOOR GROUND OPERATING VALVE.
- [SDR WX0A073201](https://openairdocs.org/sdr/WX0A073201.md): Water Heater · failed · Oct 31, 2016 · N219NV · Airbus A320214 · Humidity Control System
  > PREVIOUS 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 WX0A073179](https://openairdocs.org/sdr/WX0A073179.md): Indicator · inoperative · Jul 21, 2016 · N219NV · Airbus A320214 · Airspeed/Mach Indicator
  > DURING 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 AIR
- [SDR WX0A2016041200131](https://openairdocs.org/sdr/WX0A2016041200131.md): Slide · unwanted deploy · Apr 11, 2016 · N219NV · Airbus A320214 · Escape Slide
  > RIGHT 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 WX0A2016041273133](https://openairdocs.org/sdr/WX0A2016041273133.md): Vhf Comm · malfunctioned · Apr 9, 2016 · N219NV · Airbus A320214 · VHF Communications System
  > LOST 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 WX0A2016030173095](https://openairdocs.org/sdr/WX0A2016030173095.md): Circuit Breaker · pulled · Feb 27, 2016 · N219NV · Airbus A320214 · Cabin Pressure Control System
  > 7000' 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 OFF
- [SDR WX0A2015081172782](https://openairdocs.org/sdr/WX0A2015081172782.md): Light · inoperative · Aug 7, 2015 · N219NV · Airbus A320214 · Emergency Lighting
  > SEVERAL 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 WX0A2015081172785](https://openairdocs.org/sdr/WX0A2015081172785.md): Water Heater · overheated · Aug 5, 2015 · N219NV · Airbus A320214 · Potable Water System
  > ELECTRIC 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 WX0A2015061572657](https://openairdocs.org/sdr/WX0A2015061572657.md): Unknown · odor · Jun 11, 2015 · N219NV · Airbus A320214 · Air Distribution System
  > BACK 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 & AMM
- [SDR WX0A2015033072495](https://openairdocs.org/sdr/WX0A2015033072495.md): Blade · damaged · Mar 26, 2015 · N219NV · Airbus A320214 · Turbine Engine Compressor Section
  > ENGINE 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 EVIDEN
- [SDR WX0A2015033072494](https://openairdocs.org/sdr/WX0A2015033072494.md): Warning System · false activation · Mar 26, 2015 · N219NV · Airbus A320214 · Landing Gear Position and Warning
  > LANDING GEAR SYS DISAGREE ON LANDING ROLLOUT. COMPUTE SYS RESET IAW MX CONTROL. BL 11695 FAULT CLEARED.
- [SDR WX0A2015021672418](https://openairdocs.org/sdr/WX0A2015021672418.md): Light · inoperative · Feb 10, 2015 · N219NV · Airbus A320214 · Emergency Lighting
  > SEVERAL EMER LIGHT LAMPS WILL NOT ILLUMINATE. REPLACED EMER LIGHT LAMPS IN CTR RT EXIT & RT FWD EXIT IAW AMM 33-51-00.
- [SDR WX0A2014111872264](https://openairdocs.org/sdr/WX0A2014111872264.md): Battery · discharged · Nov 11, 2014 · N219NV · Airbus A320214 · Emergency Equipment
  > AFT R2 FLIGHT ATTENDANT STATION FLASHLIGHT INOPERATIVE. R & R AFT FLIGHT ATTENDANT STATION FLASHLIGHT BATTERY IAW AMM 25-60-00. OPERATIONS CHECKED GOOD.
- [SDR WX0A2014092572168](https://openairdocs.org/sdr/WX0A2014092572168.md): Slide · deployed · Sep 23, 2014 · N219NV · Airbus A320214 · Escape Slide
  > WHILE 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.

## 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 = 'N219NV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N219NV/reports

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