N290NV
Service difficulty reports · 28
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 = 'N290NV' 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 = 'N290NV' 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 WX0A2026070832886Door Sill · corroded(AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING AC HEAVY MX VISIT) NRC 2000-0025: 404-34 L2 DOOR SILL BEAM FOUND CORRODED AT BOTH GIRT BAR FITTING AREA / L2 DOOR CUTOUT LOWER SILL BEAM BTW FR66-68 REPLACED AS PER SRM 51-72-11-911-001 REV.158. "SDR WX0A2026070832882Floor Support · corroded(AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING AC HEAVY MX VISIT) NRC 1000-0053: 404-14 AFT CARGO COMPARTMENT FLOOR STRUCTURE, PROFILE AT STGR38LH FOUND CORRODED AT FR55 / AFT CARGO COMPARTMENT FLOOR STRUCTURE, PROFILE AT STGR38LH AT FR55 REPLACED IAW SRM 5SDR WX0A2026070832884Floorbeam · corroded(AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING AC HEAVY MX VISIT) NRC 1000-0067: REAR FUSELAGE CABIN FLOOR STRUCTURE, CORROSION FOUND ON LONGITUDINAL BEAM AT -Y160 FR69 AREA / REAR FUSELAGE CABIN FLOOR STRUCTURE, LONGITUDINAL BEAM AT -Y160 BTW FR 67-70 RSDR WX0A2026070632879Seat Track · corroded(AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING AC HEAVY MX VISIT) NOSE FWD FUSELAGE CABIN FLOOR STRUCTURE, SEAT TRACK FOUND CORRODED AT Y1292 FR16 AREA / NOSE FWD FUSELAGE CABIN FLOOR STRUCTURE, SEAT TRACK AT Y1292 FR16 AREA WAS REPLACED AS PER SRM 51-72-SDR WX0A2026070632878Seat Track · corroded(AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING AC HEAVY MX VISIT) NOSE FWD FUSELAGE CABIN FLOOR STRUCTURE, RAIL FOUND CORRODED AT Y503.2 FR16 AREA / NOSE FWD FUSELAGE CABIN FLOOR STRUCTURE, RAIL BTW FR12-16 AND Y503.2 REPLACED AS PER SRM 51-72-11-911-001 SDR WX0A2026070632877Shear Plate · corroded(AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING AC HEAVY MX VISIT) AFT CARGO COMPARTMENT FLOOR STRUCTURE, SHEAR PLATE FOUND CORRODED AT STGR38LH BTW FR62-FR63 / AFT CARGO COMPARTMENT FLOOR STRUCTURE, AT STRG38LH BTW FR62-FR63 SHEAR PLATE REPLACED PER SRM SDR WX0A2026070632876Web · corroded(AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING AC HEAVY MX VISIT) NOSE FWD FUSELAGE CABIN FLOOR STRUCTURE, RH OUTBD WEB FOUND CORRODED AT FR16 AREA / NOSE FWD FUSELAGE CABIN FLOOR STRUCTURE R/H OUTBD WED AT FR 16 AREA REPLACED AS PER SRM 51-72-11-911-001 SDR WX0A2026070832885Stringer · corroded(AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING AC HEAVY MX VISIT) NRC 1000-0078: 404-08 AFT CARGO COMPARTMENT, PREVIOUS STRINGER REPAIR SECTION FOUND CORRODED AT STGR42LH BTW FR58-FR59 / AFT CARGO COMPARTMENT, STRINGER 42L BTW FR57 AND 60 PERMANENTLY REPAISDR WX0A2026070832883Stringer · corroded(AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING AC HEAVY MX VISIT) NRC 1000-0079: 404-10 AFT CARGO COMPARTMENT, PREVIOUS STRINGER REPAIR SECTION FOUND CORRODED AT S43L BTW FR57-FR58 / AFT CARGO COMPARTMENT, STRINGER AT STGR43L BTW FR56-FR60 PERMANENTLY REPASDR WX0A2026070132869Seat Track · corroded(AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING AC HEAVY MX VISIT) NRC 1000-0076: 404-30 NOSE FWD FUSELAGE CABIN FLOOR STRUCTURE, RAIL FOUND CORRODED AT Y-254 FR21 / NOSE FWD FUSELAGE CABIN FLOOR STRUCTURE, RAIL BTW FR12-24 AND Y-254 REPLACED AS PER SRM 51SDR WX0A2026062632861Floor Support · corroded(AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING AC HEAVY MX VISIT) REAR FUSELAGE CABIN FLOOR STRUCTURE, CORROSION FOUND ON LONGITUDINAL BEAM AT Y599.5 BTW FR68-R69. CABIN FLOOR STRUCTURE, LONGITUDINAL BEAM AT Y599.5 BTW FR68-FR70 REPLACED AS PER SRM 51-72-1SDR WX0A2026030932751Epsu · faulted(AIRCRAFT NOT GROUNDED) EPSU BATTERY FAULT AT 11WL / REMOVED AND INSTALLED NEW EPSU BATTERY AT 11WL IAW A320 AMM 33-51-38-000-002-A / 400-002-A. BITE CHECK AND INTERFACE & POWER UP TEST OF CIDS OPS TEST GOOD."SDR WX0A2026030432747Epsu · faulted(AIRCRAFT NOT GROUNDED) EPSU 10WL, 12WL, 13WL BATTERY FAULT. REMOVED AND REPLACED 10WL, 12WL AND 13WL IAW AMM 33-51-38-000-002-A - 400-002-A. PERFORMED OPS TEST OF EPSU THRU BITE CHECK, OPS CHECK GOOD. PERFORMED INTERFACE AND POWER-UP TEST OF THE CIDS, OPS CSDR WX0A2025060232443A/C Pack · odor(AIRCRAFT NOT GROUNDED) IN CRUISE FLIGHT AFT FA'S REPORTED A STRONG DIRTY SOCK SMELL ROW 30 AND AFT. WE FOLLOWED QRH PROCUDURE. TURNED OFF PACK #2, SMELL SLOWLY DISIPATED. WE CONTINUED TO OUR DESTINATION PACK #2 REMAINED OFF FOR THE DURATION OF THE FLIGHT, SDR WX0A2025020532300Unknown · odor(AIRCRAFT GROUNDED) FLIGHT ATTENDANTS REPORTED DIRTY SOCK SMELL DURING DESCENT. C/W TASK CARD 21-000-002ITEM: 1C/W TASK CARD 21-000-002. REF TO LP 1981927 DIRTY SOCK SMELL/ WORK CARD #21-000-001 APU INOP. LEAK IN LUBE MODULE SEAL. R & R APU OIL LUBE MODULE RSDR EE4Y2024103121224Skin Panel · corrodedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-ZL-500-02-1-002_P1-OP-UP-WINGS/004 , RH WING TIP RIB 27 TRAILING EDGE LOWER SKIN WITH CORROSION WAS FOUND.AIRBUS WAS CONTACTED FOR REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRUCTIONS AND THE AFFECTED AREA WSDR EE4Y2024103121223Plate · corrodedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-545156-01-1-001_P1-OP-UP-ENG/001 ,ENGINE# 1 PYLON OUTBOARD CENTER SECTION AT RIB 8 STR 5R BOTTOM REINFORCEMENT PLATE WITHCORROSION WAS FOUND. OEM WAS CONTACTED FOR REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIRINSTSDR EE4Y2024103121222Plate · corrodedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-545156-01-1-002_P1-OP-UP-ENG/001 ,ENGINE # 2 PYLON OUTBOARD CENTER SECTION AT RIB 8 STR 5R BOTTOM REINFORCEMENT PLATE WITH CORROSION WAS FOUND. OEM WAS CONTACTED FOR REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR ISDR WX0A2024041632010Battery · no testAFT L/H EMERGENCY FLIGHTLIGHT INOP. / REMOVED AND REPLACED AFT L/H FLASHLIGHT BATTERY IAW AMM 25-65-00 AND 320 LOPA"SDR WX0A2023050331762Epsu · unknownFOWARD EPSU FAILED EMERGENCY LIGHT TEST / REMOVED AND REPLACED FWD EPSU BATTERY IAW AMM 33-51-38-000-002-A & 33-51-38-400-002-A OPS CHECK GOOD"SDR WX0A2022120931670Power Supply · inoperativeRIGHT OVERWING EMERGENCY EXIT LIGHTS AND SIGN INOP / REMOVED AND REPLACED EMERG BATTERY AT RT OVERWING EXIT PER AMM 33-22-01, OPS CK GOOD"SDR 1E1R20221206R0151None · noneE2571-0005 80VU RACK SPECIAL DETAILED INSPECTION REPAIR.SDR WX0A2022072974171Slide · low pressure(L1) ESCAPE SLIDE PACK PRESSURE INDICATION DOWN TO LIMITS / REMOVED AND REPLACED LEFT ( L1) ESCAPE SLIDE PACK ASSEMBLY IAW AMM 25-62-44-000-002-A AND 25-62-44-400-006-A. OPS TEST GOOD AT THIS TIME. A/C OKAY FOR SERVICE."SDR WX0A2022010373915Light · misinstalledOVERWING EMERGENCY EXIT LIGHT OUT ON AIRCRAFT RIGHT / CONNECTED LIGHTED SIGN LEADS AS NUMBERED ON SIGN, OPS CHECKS GOOD IAW AMM 33-51-15 PB 401."SDR WX0A2021083073821Warning Message · illuminatedINFLIGHT RECIEVED HYD G RSVR LO LVL. HYD SD PAGE INDICATED AMBER LEVEL. / (AIRCRAFT IS CURRENTLY AOG)"SDR WX0A2021072373784Epsu · no testDURING EPSU TEST FWD AND CENTER R/H BATTERY FAILED. / REMOVED AND REPLACED EPSU FWD AND CENTER R/H BATTERIES IAW AMM 33-51-38. BITE CHECK GOOD."SDR WX0A2021052873725Bowl · leakingDIRTY MUSTY SOUR SMELL THRU 10000 RAN QRH PROCEDURES WAS UNABLE TO REMOVE SMELL UNTIL BOTH PACKS WERE OFF. ONCE BOTH PACKS WERE OFF FOR SEVERAL MINUTES THE SMELL SEEMED TO DISSIPATE. FOLLOWING AMM 49-00-00-200-812-A, .INSPECTED APU AND FOUND FUEL LEAK COMING SDR WX0A2021031773662Epsu · no testNRC 7000-0007: ALL OUTPUT LIGHT OF EPSU 11WL (MID L/H CABIN) FOUND INOP DURING EMERGENCY LIGHT TEST. / EPSU 11WL (MID L/H CABIN) REPLACED IAW AMM 33-51-38-400-001-A. SEE AWS FOR TESTING."
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