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.
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
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 WX0A2025110332623Power Supply · no test(AIRCRAFT NOT GROUNDED) FAILED EPSU BITE CHECK / REMOVED AND REPLACED EPSU REF WO535097"SDR 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 RESDR 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 21-23SDR 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.SDR 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 52-10-00-410-00SDR 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"SDR WX0A2024030131968Megaphone · expiredMEGAPHONE FOUND TO BE EXPIRED / REPLACED MEGAPHONE BATTERIES IAW AMM 25-61-51-920-001-A"SDR 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 INSTSDR 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 JACKINGSDR 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. AIRBUSSDR 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 SATISFACSDR 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 BYSDR 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 COVEREDSDR 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 DATED08-01SDR 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 DATED08-0SDR 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 08SDR 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."SDR 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."SDR WX0A2022013173948Epsu · failed inspBATTERY FAILED TEST / REMOVED AND REPLACED BATTERY IAW 33-51-38-400-002A. NO DEFECTS NOTED"SDR WX0A2022013173947Epsu · failed inspBATTERY FAILED TEST / REMOVED AND REPLACED BATTERY IAW 33-51-38-400-002A. NO DEFECTS NOTED"SDR WX0A2022013173946Epsu · failed inspBATTERY FAILED TEST / REMOVED AND REPLACED EPSU IAW 33-51-38-400-002A. NO DEFECTS NOTED"SDR WX0A2022013173945Epsu · failed inspBATTERY TEST FAIL / REMOVED AND REPLACED EPSU IAW 33-51-38-400-002A. NO DEFECTS NOTED"SDR 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#
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