N610CZ
Service difficulty reports · 123
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 = 'N610CZ' 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 = 'N610CZ' 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 C77A20130820016Firewall · crackedAPU FIREWALL 351BZ, HAS TWO CRACKS IN THE RADIUS AT BOTH ENDS. UPPER CRACK IS 0.400" AND LWR CRACK IS 0.500" X=28868.0. BOTH CRACKS ROUTED OUT AND NDT PERFORMED VERIFYING NO MORE CRACKING EXISTS IAW ETD 2013-170-027936 AND EA E175-53-372, REV IR.SDR C77A20130820015Bushing · migratedNLG RETRACT ACTUATOR LWR INBD BUSHING IS MIGRATED. REPLACED NLG RETRACT ACTUATOR FITTING BUSHINGS IAW ED-LLI-10-0008 AND EO E17X-3200-007, REV IR.SDR C77A20130820014Seal Depressor · corrodedFORWARD CARGO DOOR CUTOUT STRUCTURE CENTER SEAL DEPRESSOR, PN 170-66804-401, HAS CORROSION AT X=7120-7675 Y=450. R & R CENTER SEAL DEPRESSOR IAW SRM 51-41-01 AND 51-43-01.SDR C77A20130820013Threshold · corrodedFWD CARGO DOOR CUTOUT STRUCTURE HORIZONTAL BEAM HAS CORROSION AT X=7200- 7625 Y= 390. R & R THRESHOLD BEAM IAW SRM 51-41-01 AND 51-43-01.SDR C77A20130820012Floorbeam · corrodedCORROSION ON RT FLOORBEAM, AT FR 87 X= 23850 Y=273. R & R FLOORBEAM IAW SRM 51-41-01 AND 51-43-01.SDR C77A20130820011Floorbeam · corrodedCORROSION ON FLOORBEAM AT FR 87 X=23850, Y=273. R & R FLOORBEAM IAW SRM 51-41-01 AND 51-43-01.SDR C77A20130820010Splice Plate · corrodedCORROSION ON RT SPLICE PLATE AT FR 89 X=24435, Y=273. R & R SPLICE PLATE IAW SRM 51-41-01 AND 51-43-01.SDR C77A20130820009Gusset · corrodedCORROSION ON RT INBD GUSSET AT FR 90 X=24867, Y= 273 . R & R GUSSET IAW SRM 51-41-01 AND 51-43-01.SDR C77A20130820008Gusset · corrodedCORROSION ON RT OTBD GUSSET, AT FR 90 X=24740 Y=508. R & R RT OTBD GUSSET IAW SRM 51-41-01 AND 51-43-01.SDR C77A20130820007Floor Support · corrodedCORROSION ON RT FLOOR SUPPORT AT FR 88 TO FR 90 X=24028 TO X=24866, Y=635. R & R FLOOR SUPPORT IAW SRM 51-41-01 AND 51-43-01.SDR C77A20130820006Floor Support · corrodedCORROSION ON LT FLOOR SUPPORT, AT OF FR 88 TO FR 90 X=24028 - 24866 , Y= -635. R & R LT FLOOR SUPPORT IAW SRM 51-41-01 AND 51-43-01.SDR C77A20130820005Shear Plate · corrodedLEFT SHEAR PANEL IS CORRODED ALONG THE FWD RIVET LINE. X=23865.0, Y= -304.8 - 1041.4. R & R LT SHEAR PANEL IAW SRM 51-41-01 AND 51-43-01.SDR C77A20130820003Panel · corrodedRT SHEAR PANEL IS CORRODED ALONG THE FWD RIVET LINE. R & R RT SHEAR PANEL IAW SRM 51-41-01 AND 51-43-01.SDR C77A20130820004Shear Plate · corrodedCENTER SHEAR PANEL, IS CORRODED ALONG THE FWD RIVET LINE. X=23865.0, Y= -222.3 - 222.3. R & R CENTER SHEAR PANEL IAW SRM 51-41-01 AND 51-43-01.SDR C77A20130820002Upper Sheet · corrodedCORROSION ON LT UPPER SHEET, BETWEEN FR 85 & FR 86. R & R LT UPPER SHEET IAW SRM 51-41-01 AND 51-43-01.SDR C77A20130820001Upper Sheet · corrodedRT UPPER SHEET , IS CORRODED ALONG THE TOP SURFACE. R & R RT UPPER SHEET IAW SRM 51-41-01 AND 51-43-01.SDR C77A20130816002Seat Track · corrodedCORROSION DAMAGE TO THE AFT CABIN FLOOR STRUCTURE RT AFT SEAT TRACK, AT FR84. THE NOMINAL THICKNESS OF THE FLANGE IS 0.080". THE CORROSION DAMAGE WAS BLENDED OUT.SDR C77A20130815001Skin · crackedONE CRACK WAS FOUND IN THE CRITICAL FASTENER HOLE ON THE RT SIDE AFTER IT HAD BEEN ENLARGED TO 8MM (.314") DIAMETER IAW THE SB. ACCOMPLISHED MAJOR REPAIR IAW EO E17X-57MA-004.7SDR C77A20130814002Floorbeam · damagedFASTENER HOLE ELONGATED ON CROSSBEAM AT FRAME 89.SDR C77A343204Battery Pack · dischargedCOCKPIT EMERGENCY LIGHT INOP. R & R BATTERY ELPU FOR COCKPIT LIGHT, OPS CH OK IAW AMM 33-50-01.SDR C77A292168Coffeemaker · failedDURING CRUISE, DECLARED AN EMERGENCY AND DIVERTED DUE TO A REPORT OF SMOKE IN THE AFT CABIN AREA. WHILE STILL IN FLIGHT, THE F/A DETERMINED THE SMOKE WAS COMING FROM THE AFT INBD COFFEEMAKER AND TURNED THE COFFEEMAKER TO OFF. THE SMOKE DISSIPATED. THE ACFT LASDR C77A230021Battery Pack · failedEMERGENCY LIGHT BATTERY FAULTY.SDR C77A204663Floor Support · corrodedDURING BASIC CHECK INSPECTION MX VISIT, CORROSION WAS FOUND ON RT FLOOR TRACK PN 170-03263-001 FROM FR14 TO FR 17 AT BL 273R. TEMPORARY REPAIR WAS MADE REF ETD 2009-170/09173A AND COMPASS EO E175-53MR-018. PERMANENT REPAIR TO BE MADE AT NEXT BASIC CHECK WITH
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