N224NV

Service difficulty reports · 33

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 = 'N224NV' 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 WX0A2025021432314Oxygen Mask · unwanted deploy(AIRCRAFT NOT GROUNDED) ROW 14ABC O2 MASK FELL DOWN -AGAIN / R&R ROW 14ABC EMERGENCY OXYGEN GENERATOR IN REF. TO AMM 35-21-41-020-050-A & AMM 35-21-41-420-050-A. OK FOR SERVICE."Feb 12, 2025 · N224NV · Airbus A320214 · Passenger Oxygen SystemSDR EE4Y2025021221719Frame · corrodedFWD FUSELAGE AT FR16 RH SIDE LANYARD HOOK HOLES WITH CORROSION, PERFORMED TEMPORARY REPAIR IAW COOPESA EO# COO-EO-2025-21556-R02 DATED 01/27/2025 AND AIRBUS RDAF 80873219/054/2025#A DATED 01/28/2025, UNDER COOPESA JOB: A1Q002 NRI 7-80Feb 12, 2025 · N224NV · Airbus A320214 · Fuselage Main, FrameSDR EE4Y2025021421709Hinge Fitting · damagedEMPENNAGE RH ELEVATOR O/B HINGE LUG FITTING DAMAGED. REPAIRE IAW A320 SRM 55-26-47-300-001 PARAG. 2A FIG 001. DOCUMENTED UNDER COOPESA JOB: A1P002 NRI 3-29Feb 10, 2025 · N224NV · Airbus A320214 · Elevator StructureSDR EE4Y2025021421708Door Frame · corrodedUPPER FUSELAGE CABIN/CREW DOOR FR68 BETWEEN STRG 22L AND 23L WEB WITH CORROSION.. / PERFORMED PERMANENT REPAIR IAW COOPESA EO# COO-EO-2025-21559-R01 AND RDAF 81526989/005/2025#A. JOB PERFORMED UNDER COOPESA JOB: A1P002 NRI 2-46Feb 10, 2025 · N224NV · Airbus A320214 · Fuselage Main, StructureSDR EE4Y2025021421707Door Frame · crackedUPPER FUSELAGE CABIN/CREW DOOR FR68L DOOR STOP FITING #1 CRACKED. / PERFORMED PERMANENT REPAIR IAW COOPESA EO# COO-EO-2025-21559-R01 AND RDAF 81526989/005/2025#AFeb 10, 2025 · N224NV · Airbus A320214 · Fuselage Main, StructureSDR EE4Y2025021021706Skin · corrodedREAR FUSELAGE BETWEEN FR69 AND FR70, SATRG 31R AND STRG 32R SKIN WITH CORROSION. / REPAIRED IAW A320 SRM TASK 53-41-11-300-004 PARAG. 2A FIG 001 / DOCUMENTED UNDER COOPESA JOB A1P002 NRI 1-35Feb 10, 2025 · N224NV · Airbus A320214 · Fuselage Main, Plate/SkinSDR WX0A1900010031764Idg · unknown(EMERGENCY DECLARED) GEN 2 FAULT FOLLOWED BY AC BUS 2 FAULT FOLLOWED BY CASCADING FAILURES PERFORMED OVERWEIGHT LANDING/PERFORMED T/SHOOTING IAW A320 TSM 24-20-00-810-814-A. REMOVED AND REPLACED IDG #2 IAW A 320 AMM 24-21-51-000/400/-040-A AND PERFORMED T/SHOMay 6, 2023 · N224NV · Airbus A320214 · AC Generator-AlternatorSDR EE4Y2023013017052Skin · corrodedDURING THE STRUCTURAL INSPECTION PER ALLEGIANT WORK CARD Nº: ZL-575-01-001 MPD, CORROSIONON LH WING TOP SKIN PANEL 2 LOWER SURFACE, RS AND TEOH AT RIBS 17 WAS FOUND. DUE THECORROSION RUNNING OVER REAR SPAR DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIRINSTRUCTIJan 30, 2023 · N224NV · Airbus A320214 · Wing, Plate/SkinSDR EE4Y2023013017051Skin · corrodedDURING THE STRUCTURAL INSPECTION PER ALLEGIANT WORK CARD Nº: ZL-575-01-001 MPD, CORROSIONON LH WING TOP SKIN PANEL 2 LOWER SURFACE, RS AND TEOH AT RIB 10 WAS FOUND. DUE THECORROSION RUNNING OVER REAR SPAR DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIJan 30, 2023 · N224NV · Airbus A320214 · Wing, Plate/SkinSDR EE4Y2023013017050Skin · corrodedDURING THE STRUCTURAL INSPECTION PER ALLEGIANT WORK CARD Nº: ZL-575-01-001 MPD, CORROSIONON LH WING TOP SKIN PANEL 2 LOWER SURFACE, RS AND TEOH RIBS 14-15 WAS FOUND. DUE THECORROSION RUNNING OVER REAR SPAR DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIRINSTRUCTIJan 30, 2023 · N224NV · Airbus A320214 · Wing, Plate/SkinSDR EE4Y2023013017049Skin · corrodedDURING THE STRUCTURAL INSPECTION PER ALLEGIANT WORK CARD Nº: ZL-575-01-001 MPD, CORROSIONON LH WING TOP SKIN PANEL 2 LOWER SURFACE, RS AND TEOH RIBS 14-15 WAS FOUND. DUE THECORROSION RUNNING OVER REAR SPAR DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIRINSTRUCTIJan 30, 2023 · N224NV · Airbus A320214 · Wing, Plate/SkinSDR EE4Y2023013017044Skin · corrodedDURING THE STRUCTURAL INSPECTION PER ALLEGIANT WORK CARD Nº: ZL-575-01-001 MPD, CORROSION ON LH WING TOP SKIN PANEL 2 LOWER SURFACE, RS AND TEOH RIBS 14-15 WAS FOUND. DUE THE CORROSION RUNNING OVER REAR SPAR DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUJan 30, 2023 · N224NV · Airbus A320214 · Wing, Plate/SkinSDR WX0A2022110774310Epsu · noneWHILE PERFORMING TASK CARD 33-51-00-710-003-A FWD EPSU BATTERY FIN (10WL) AND AFT EPSU BATTERY FIN (13WL) FAILED BATTERY CAPACITY TEST. / REMOVED AND REPLACED FWD AND AFT EPSU BATTERIES IAW AMM 33-51-38-000-002-A. PERFORMED BITE CHECK OF THE EPSU'S IAW AMM 33-Nov 4, 2022 · N224NV · Airbus A320214 · Lighting SystemSDR WX0A2022110274306Epsu · noneMID R BATTERY FAIL ON EMERGENCY LIGHT TEST / REMOVED AND REPLACED MID RIGHT BATTERY IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A, OPS CHECK GOOD."Nov 1, 2022 · N224NV · Airbus A320214 · Lighting SystemSDR WX0A2022110274305Epsu · noneMID L UNIT FAIL ON EMERGENCY LIGHT TEST / REMOVED AND REPLACED MID LEFT POWER SUPLY UNIT IAW AMM 33-51-38-000-001-A AND 33-51-38-400-001-A. OPS CHECK GOOD."Nov 1, 2022 · N224NV · Airbus A320214 · Lighting SystemSDR WX0A1900010074276None · none(EMERGENCY DECLARED) #1 ELEC GEN FAULT INFLIGHT FOLLOWED ECAM PROCEDURE RESET GEN 1 FAULT CLEARED AFTER 1 TO 2 MIN, GEN 1 FAULT RETURNED ON ECAM PROCEDURES- NO ELECTRICAL BURN SMELL OR VISUAL INDICATORS / INSTALLED NEW APU STARTER LEADS IAW ESPM 20-48-19.REMOOct 7, 2022 · N224NV · Airbus A320214 · AC Generation SystemSDR WX0A2022100374269Megaphone · noneFWD MEGAPHONE INOP / REMOVED AND REPLACED FWD MEGAPHONE, OPS CHECKS GOOD, W/REF TO A/C LOPA DRAWING A2250001L03"Oct 2, 2022 · N224NV · Airbus A320214 · Escape SlideSDR WX0A2022070174134None · noneR2 EXIT LIGHT INOP. / FOUND BROKEN WIRE AT EMERGENCY EXIT SIGN (44WL) AND REPAIRED IT IAW ESPM - AIRBUS 20-43-00 AND AMM 33-51-16 PB 401. OPS CHECK GOOD."Jun 29, 2022 · N224NV · Airbus A320214 · Lighting SystemSDR WX0A1900010074119Skin · corrodedNRC 6000-0030: (744-1) CORROSION FOUND ON RH WING, TOP SKIN UPPER SURFACE AT REAR SPAR AREA, 5 INCHES INBD FROM RIB 13./RH WING TOP SKIN TRAILING EDGE OVERHANG AT RIB 13 DATUM (AREA #6) PERMANENTLY REPAIRED AS PER AIRBUS DOSSIER #80871570 AND ERO #R5721-0105 RJun 2, 2022 · N224NV · Airbus A320214 · Wing, Plate/SkinSDR WX0A2022062274124Skin · corrodedNRC 6000-0024: AT R/H WING TOP SKIN, CORROSION FOUND AT TRAILING EDGE OVERHANG AT RIB 12 DATUM, STATION WMRX 3355.516. / RH WING TOP SKIN TRAILING EDGE OVERHANG AT RIB 12 DATUM, APPROX STA WMRX 3355.516 (AREAS #4 - #5) PERMANENTLY REPAIRED AS PER AIRBUS DOSSIEMay 31, 2022 · N224NV · Airbus A320214 · Wing, Plate/SkinSDR WX0A2022062274123Skin · corrodedNRC 6000-0027: AT R/H WING TOP SKIN, CORROSION FOUND AT TRAILING EDGE OVERHANG BTW STATION WMRX 5626.98 AND WMRX 6173.91 (APPROX. RIB 16 TO 17). / RH WING TOP SKIN TRAILING EDGE OVERHANG BETWEEN STA WMRX 5626.98 AND WMRX 6173.91 (AREAS #10 - #11) PERMANENTLY RMay 31, 2022 · N224NV · Airbus A320214 · Wing, Plate/SkinSDR WX0A2022062274122Skin · corrodedNRC 6000-0025: AT R/H WING TOP SKIN, CORROSION FOUND AT TRAILING EDGE OVERHANG BTW STATION WMRX 4037.38 AND WMRX 5261.977 (APPROX. RIB 13 TO 15). / RH WING TOP SKIN TRAILING EDGE OVERHANG BETWEEN WMRX 4037.38 AND WMRX 5261.977 (AREAS #7, #8, #9), PERMANENTLY RMay 31, 2022 · N224NV · Airbus A320214 · Wing, Plate/SkinSDR WX0A2022062274121Skin · corrodedNRC 6000-0023: AT R/H WING TOP SKIN, CORROSION FOUND AT TRAILING EDGE OVERHANG BTW STATION WX 3494.5 AND WX 4490.52 (APPROX. RIB 7 TO 8). / RH WING TOP SKIN TRAILING EDGE OVERHANG BETWEEN WX 3494.5 AND WX 4490.52 (AREAS #1, #2, #3), PERMANENTLY REPAIRED AS PERMay 31, 2022 · N224NV · Airbus A320214 · Wing, Plate/SkinSDR WX0A2022062274120Skin · corrodedNRC 5000-0019: AT L/H WING TOP SKIN, CORROSION FOUND AT TRAILING EDGE OVERHANG BTW STATION WX 3494.5 AND WX 4490.52 (APPROX. RIB 7 TO 8). / LH WING TOP SKIN TRAILING EDGE OVERHANG BETWEEN STA WX 3494.5 AND WX 4490.52 (AREAS #1, #2, #3) PERMANENTLY REPAIRED AS May 31, 2022 · N224NV · Airbus A320214 · Wing, Plate/SkinSDR WX0A2022022574009Megaphone · inoperativeDURING A/C WAKE UP FOUND FWD FA MEGA PHONE INOP (LOUD SQUEALS) WATER CAME OUT OF UNIT / REMOVED AND REPLACED FWD MEGA PHONE REF AMM 25-60-00 OPS CHECK GOOD"Feb 23, 2022 · N224NV · Airbus A320214 · Emergency EquipmentSDR WX0A202002073470Battery Pack · no testEMERGENCY LIGHT TEST FAILS AFT EPSU BATTERY / REMOVED AFT EPSU BATTERY"Feb 6, 2020 · N224NV · Airbus A320214 · Emergency LightingSDR WX0A202002073469Battery Pack · no testEMERGENCY LIGHT TEST FAILS MID-RIGHT EPSU BATTERY / REPLACE MID-RIGHT EPSU BATTERY"Feb 6, 2020 · N224NV · Airbus A320214 · Emergency LightingSDR WX0A201908143412Slide · unwanted deployR1 DOOR SLIDE DEPLOYED. R&R R1 DOOR SLIDE"Aug 12, 2019 · N224NV · Airbus A320214 · Escape SlideSDR WX0A2019071573405Megaphone · inoperativeFWD MEGAPHONE INOP. R&R MEGAPHONE.Jul 14, 2019 · N224NV · Airbus A320214 · Emergency EquipmentSDR 39HR201707030001Connector · disconnectedEMERGENCY LIGHT TEST DISPLAYS EXT LOAD AFT L FAULT. TROUBLESHOT AND FOUND CONNECTOR OF R2 DOOR SLIDE. RECONNECTED AND OPS CHECKED GOOD IN ACCORDANCE WITH TSM 33-51-00.Jun 30, 2017 · N224NV · Airbus A320211 · Light System WiringSDR 39HR2018031200001Window Frame · crackedCRACK FOUND IN LOWER RADIUS LEFT HAND LATERAL WINDOW FROM EMITTING FROM FASTENER HOLE. REMOVED AND REPLACED LEFT HAND WINDOW FRAME IN ACCORDANCE WITH ERO R5311-002.May 24, 2017 · N224NV · Airbus A320214 · Flight Compartment WindowsSDR WX0A2015113000001Battery Pack · inoperativeF/A FOUND AFT RT LOWER EMERGENCY FLASHLIGHT INOPERATIVE. R & R BATTERY ON AFT RT LOWER EMERGENCY FLASH LIGHT. OPS CHECKED NORMAL, REF AMM 25-65-00.Nov 25, 2015 · N224NV · Airbus A320214 · Emergency EquipmentSDR WX0A2015081672804Blade · unknownENG 2 N1 VIBRATION FLASHING RANGE OF VIBRATION WAS 4.3 - 6.8 N1, CONDITIONS WERE AT 10,000 FEET 250 KNOTS 67% N1 90% N2 EGT 549, ALL MATCHED OTHER ENG. REMOVED NR 2 ENG FAN ROTOR BLADES 12, 13, 14 FOR FURTHER EVALUATION. IAW AMM 72-21-00 CL 11730 REMOVED NR Aug 11, 2015 · N224NV · Airbus A320214 · Turbine Engine Compressor Section
Back to N224NV