N288NV

Service difficulty reports · 23

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 = 'N288NV' 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 WX0A2025110332623Power Supply · no test(AIRCRAFT NOT GROUNDED) FAILED EPSU BITE CHECK / REMOVED AND REPLACED EPSU REF WO535097"Nov 3, 2025 · N288NV · Airbus A320214 · Emergency LightingSDR WX0A2025102032605Unknown · odor(AIRCRAFT NOT GROUNDED) FAS REPORTED EARTHY & MUSKY SMELL DURING CLIMB IN AFT 4 ROWS AND GALLEY THEN AFTER LANDING DESCRIBED SMELL WORSENED IN DESCENT AND DESCRIBED AS DIRTY SOCK SMELL. CLEANING AND DECONIMATION FO DIRTY SOCK /LOCKER ROOM/MUSTY SMELL REPORT REOct 20, 2025 · N288NV · Airbus A320214 · Air Distribution SystemSDR WX0A2025062332471Fan · failed(AIRCRAFT NOT GROUNDED) FA REPORTED BURNING HAIR / ELECTRICAL SMELL FROM AFT GALLEY AREA DURING CRUISE. REMOVED AND REPLACED LAV/GALLEY EXTRACT FAN IAW AMM 21-23-51-400-001-A AND AMM 21-23-51-000-001-A. OPS TEST GOOD AND NO DEFECTS NOTED. THIS CLEARS MEL 21-23Jun 21, 2025 · N288NV · Airbus A320214 · Air Distribution FanSDR WX0A2025021932321Unknown · odor(AIRCRAFT GROUNDED) LEAD FA REPORTED IN CRUISE DIRTY SOCK ODOR IN FWD GALLEY AREA. 2 TIMES FOR A FEW MINUTES EACH. DISSIPATED ON ITS OWN. 36000 FEET. / COMPLETED TC 21-000-002 OIL PHASE TASK CARD, NO DEFECTS NOTED.Feb 17, 2025 · N288NV · Airbus A320214 · Air Distribution SystemSDR WX0A2025020732308Girt Bar · misinstalled(AIRCRAFT NOT GROUNDED) SLIDE INDICATOR FRO R2 DOOR ON ECAM INTERMITTENT. / FOUND GIRT BAR ASSEMBLY IMPROPERLY FOLDED AND DRAGGING ON FLOOR. RE-SECURED GIRT BAR FOLD PER AMM 25-62-44-400-803-A. R2 DOOR ECAM ARMED/DISRAMED INDICATIONS OK PER AMM 52-10-00-410-00Feb 6, 2025 · N288NV · Airbus A320214 · Emergency EquipmentSDR WX0A2025012732283Indication Sys · malfunctioned(AIRCRAFT GROUNDED) R2 DOOR SLIDE INDICATION WENT AWAY IN FLIGHT / PERFORMED OPS CHECK ON R2 DOOR INDICATION IAW 52-71-00-710-001-A, OPS CK GOOD. NO DEFECTS NOTED. A/C OK FOR SERVICE"Jan 26, 2025 · N288NV · Airbus A320214 · Door Warning SystemSDR WX0A2024030131968Megaphone · expiredMEGAPHONE FOUND TO BE EXPIRED / REPLACED MEGAPHONE BATTERIES IAW AMM 25-61-51-920-001-A"Mar 1, 2024 · N288NV · Airbus A320214 · Emergency EquipmentSDR EE4Y2024011719221Skin · corrodedDURING ACCMPLISHMENT OF THE ALLEGIANT TASK ZL-574-01-1-002 TEOH SKIN LOWER SURFACE WASFOUND WITH CORROSION BETWEEN RIBS 7-8.DUE THE REWORKED AREAS ARE BEYOND SRM LIMITS AIRBUS WAS CONTACTED FOR FURTHER INSTRUCTIONS.AIRBUS PROVIDED STRESS JACKING ANDREPAIR INSTJan 17, 2024 · N288NV · Airbus A320214 · Wing, Plate/SkinSDR EE4Y2024011619220Skin · corrodedDURING ACCMPLISHMENT OF THE ALLEGIANT TASK 572112-01-01-1-002 TEOH SKIN LOWER SURFACE WAS FOUND WITH CORROSION BETWEEN RIBS 7-8 AND 14-15.DUE THE REWORKED AREAS ARE BEYOND SRM LIMITS AIRBUS WAS CONTACTED FOR FURTHER INSTRUCTIONS.AIRBUS PROVIDED STRESS JACKINGJan 16, 2024 · N288NV · Airbus A320214 · Wing, Plate/SkinSDR EE4Y2024011619219Rib · corrodedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 572112-01-1-001 LH WING RIBLET E CORRODED WAS FOUND. DUE TO FLIGHT BY WIRE CABLES PASSING THROUGH THE RIBLET E AND THE AMOUNT OF WORK TO REMOVE THEM, AIRBUS WAS CONTACTED FR ALTERNATIVE METHOD OF INSTALLATION. AIRBUSJan 16, 2024 · N288NV · Airbus A320214 · Wing, Rib/BulkheadSDR EE4Y2024011619218Battery · unknownDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 335100-03-1-001 CABIN EMERGENCY LIGHTING TEST FOUND BATTERY OF THE FWD LH AND EMERGENCYT RIGHT THE BATTERIES WERE REPLACED IAWA319 AMM TASK 33-51-38-000-002-A AND 33-51-38-400-002-A , AFTERTEST WAS FOUND IN SATISFACJan 16, 2024 · N288NV · Airbus A320214 · Emergency LightingSDR EE4Y2024011619217Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIAN ENGINEERING ORDER E5316-0003 FR20 LH DOOR STOP # 1FRAME WEB I/B UPPER HOLE SCRATCHES WERE FOUND.AIRBUS WAS CONTACTED FOR REPAIRINSTRUCTIONS, THEY PROVIDE REPAIR INSTRUCTIONS UNDER DOSSIER 81330428.THIS REPAIR IS COVERED BYJan 16, 2024 · N288NV · Airbus A320214 · Fuselage Main, FrameSDR EE4Y2024011619215Frame · scratchedDURING ACCOMPLISHMENT OF THE ALLEGIAN ENGINEERING ORDER E5316-0003 FR16 LH DOOR STOP # 1 FRAME WEB I/B UPPER HOLE SCRATCHES WERE FOUND.AIRBUS WAS CONTACTED FOR REPAIR INSTRUCTIONS, THEY PROVIDE REPAIR INSTRUCTIONS UNDER DOSSIER 813304281.THIS REPAIR IS COVEREDJan 16, 2024 · N288NV · Airbus A320214 · Fuselage Main, FrameSDR EE4Y2024011619212Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 53-260-002 FR68 RH DOOR STOP # 4 UPPER I/B ONWEB AREA CRACK WAS FOUND. THE FRAME WAS REPAIRED FOLLO REPAIR INSTRUCTIONS IAW A320 SRM53-41-12-300-008 AND 53-41-12-300-010 PARAG 2A FIG 01 AND FIG 002 REV 146 DATED08-01Jan 16, 2024 · N288NV · Airbus A320214 · Fuselage Main, FrameSDR EE4Y2024011619211Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 53-260-002 FR68 LH DOOR STOP # 3 UPPER I/B ONWEB AREA CRACK WAS FOUND. THE FRAME WAS REPAIRED FOLLO REPAIR INSTRUCTIONS IAW A320 SRM53-41-12-300-008 AND 53-41-12-300-010 PARAG 2A FIG 001 AND FIG 002 REV 146 DATED08-0Jan 16, 2024 · N288NV · Airbus A320214 · Fuselage Main, FrameSDR EE4Y2024011619210Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 53-260-003 FR68 LH DOOR STOP # 2 LOWER I/B ON WEB AREA CRACK WAS FOUND. THE FRAME WAS REPAIRED FOLLO REPAIR INSTRUCTIONS IAW A320 SRM 53-41-12-300-008 AND 53-41-12-300-010 PARAG 2A FIG 01 AND FIG 002 REV 146 DATED 08Jan 16, 2024 · N288NV · Airbus A320214 · Fuselage Main, FrameSDR WX0A2023071231791Epsu · unknownWHILE PERFORMING EPSU BATTERY CAPACITY TEST, TEST FAULTED 11WL AND 13WL BATTERY. / REMOVED AND REPLACED EPSU BATTERY AT FIN LOCATION 11WL AND 13WL IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A."Jul 11, 2023 · N288NV · Airbus A320214 · Emergency LightingSDR WX0A1900010074132None · noneECAM. Y RSVR LO LVL CAUSING TOTAL Y HYD FAILURE./REPLACMENT OF #2 ENG DRIVEN PUMP,REMOVED AND REPLACED UNION FITTING. REF AMM 29-13-43.REMOVED AND REPLACED CHECK VALVE. REF AMM 29-13-37.REMOVED THE TOP CASE DRAIN HOSE/ TUBE ASSEMBLY REF 39-13-49-400-003-A."Jun 27, 2022 · N288NV · Airbus A320214 · Hydraulic Pump (Electric/Engine), MainSDR WX0A2022013173948Epsu · failed inspBATTERY FAILED TEST / REMOVED AND REPLACED BATTERY IAW 33-51-38-400-002A. NO DEFECTS NOTED"Jan 30, 2022 · N288NV · Airbus A320214 · Emergency LightingSDR WX0A2022013173947Epsu · failed inspBATTERY FAILED TEST / REMOVED AND REPLACED BATTERY IAW 33-51-38-400-002A. NO DEFECTS NOTED"Jan 30, 2022 · N288NV · Airbus A320214 · Emergency LightingSDR WX0A2022013173946Epsu · failed inspBATTERY FAILED TEST / REMOVED AND REPLACED EPSU IAW 33-51-38-400-002A. NO DEFECTS NOTED"Jan 30, 2022 · N288NV · Airbus A320214 · Emergency LightingSDR WX0A2022013173945Epsu · failed inspBATTERY TEST FAIL / REMOVED AND REPLACED EPSU IAW 33-51-38-400-002A. NO DEFECTS NOTED"Jan 30, 2022 · N288NV · Airbus A320214 · Emergency LightingSDR EE4Y2023031017357Skin · nickedDURING THE VISUAL INSPECTION PER TASK CARD CR 20-3_P1-VISUAL INSP/011, MULTIPLE NICKS WERE FOUND COMMON TO LOWER REAR FUSELAGE SKIN BETWEEN FR55 AND FR56 AND BETWEEN STR 39R AND STR 40R. CORRECTIVE ACTION: PERMANENT REPAIR WAS PERFORMED AS PER AIRBUS DOSSIER#Mar 27, 2021 · N288NV · Airbus A320214 · Fuselage Structure (General)
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