N122UX
Service difficulty reports · 64
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 = 'N122UX' 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 = 'N122UX' 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 20030827Frame · crackedDURING ROUTINE INSPECTION, A .63 INCH CRACK WAS FOUND ON THE INTERCOSTAL FRAME FLANGE AT FS 482.75 BELOW STRINGER 2L. CRACK WAS REPAIRED IAW WITH EO. AIRCRAFT RETURNED TO SERVICE.SDR 20030779Propeller · defectiveWHILE MAINTENANCE WAS PERFORMING A PRE-RELEASE AUTOFEATHER TEST, UNUSUAL VIBRATION WAS NOTED COMING FROM LT ENGINE AND PROP. ENGINE WAS SHUTDOWN WITHOUT INCIDENT AND UPON INVESTIGATION INTERNAL FAILURE WAS OBVIOUS DUE TO BLADE MOVEMENT. PROPELLER REMOVED FROSDR GLBA20030757Bracket · crackedLT SIDE OF VERT STAB TO FUSELAGE L BRKT CRACK AT APPROX FS 70.107. REPAIRED CRACK IAW EO 04-122UE-01 AND B1900 SRM 51-70 MLS52057 ITEM 1.SDR GLBA20030756Bracket · crackedLT SIDE OF VERT STAB TO FUSELAGE L BRACKET CRACKED. REPAIRED CRACK IAW B1900 SRM 51-70 AND EO 04-UE122-01.SDR GLBA20030753Web · crackedIN PANEL 332 ATC WHERE DE-ICE LINE GOES THROUGH METAL CRACKED AROUND GROMMET ( FWD WEB). REPAIRED HORIZ MAIN SPAR WEB.SDR GLBA20030697Skin · crackedLOWER COMM ANTENNA SKIN CRACKED, REPAIRED SKIN.SDR GLBA2001168Probe · defectiveLEFT ENGINE WILL NOT MAKE TAKEOFF TORQUE. REPLACED TRIM PROBE, OPS CHECKED SYSTEM SATISFACTORY.SDR GLBA2001052Indicator · inoperativeRIGHT TORQUE INDICATOR FROZE ON T/O ROLL. REPLACED TORQUE INDICATOR.SDR GLBA2001039Cable · brokenAIRSTAIR DOOR WOULD NOT OPEN. INSPECTED DOOR, FOUND INNER DOOR CABLE BROKEN. REPLACED DOOR CABLE.SDR GLBA2001024Annunciator · false indicationABORTED T/O, CABIN DOOR ANNUNCIATOR ILLUMINATED. INSPECTED SYSTEM CND OPS CHECKED GOOD.SDR GLBA2001Warning Light · illuminatedABORTED T/O, CABIN DOOR ANNUNCIATOR ILLUMINATED ON ROLL-OUT. INSPECTED SYSTEM CND.SDR 20000620SH014Altimeter · reads highALTIMETER REMOVED FROM AIRCRAFT FOR RECERTIFICATION. ENCODER FUNCTIONED PROPERLY. ALTITUDE READOUT WAS 60 FEET TO 110 FEET HIGH IN REFERENCE TO A CALIBRATED PITOT STATIC TEST SET. THE ALTITUDE READOUT WAS OBSERVED HIGH PR AT -1,000 FEET TO 2,000 FEET. NO FSDR 20000508SH015Altimeter · malfunctionedUNIT PULLED FROM AIRCRAFT FOR RE-CERTIFICATION. BENCH TEST REVEALED ALTITUDE READ OUT WAS CONSISTENLY LOW PF ABOUT 20 FEET TO 150 FEET IN THE RANGE OF -1000 FEET 4,000 FEET. A CHECK ABOVE 4,000 FEET WAS NOT COMPLETED DUE TO THE LARGE ERROR AT THE LOW END. SDR 99ZZZX3261Wire · failedNR 2 COMM CONTROL HEAD STARTED SMOKING ON CLIMB-OUT. REMOVED AND REPLACED NR 2 COMM CONTROL (PN 622-6520-008) AND REPAIRED CHAFED AND BURNED WIRES ON PIN 28 AND PIN 37 OF CONNECTOR J176. WIRING HAD CHAFED AND SHORTED OUT. COMM CONTROL CIRCUIT BOARD WAS BURN
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