N628BR, cancelled Dec 6, 2006
Service difficulty reports · 20
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 = 'N628BR' AND deregistration_id = 'N628BR-2006-12-06' 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 = 'N628BR' AND deregistration_id = 'N628BR-2006-12-06' 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 VTZA200500110Door Frame · crackedPASSENGER DOOR FRAME TOP RADIUS CRACKED AT 1 INCH IN LENGTH FORWARD OF DATUM 1 AT FS 338.90.SDR VTZA200500115Angle · crackedRIGHT 280 VERTICAL ANGLE IS CRACKED AT .5 INCH BETWEEN FASTENERS.SDR VTZA200500111Angle · crackedLEFT 280 VERTICAL ANGLE IS CRACKED AT .5 INCH BETWEEN FASTENERS.SDR VTZA200500113Bulkhead · crackedRIGHT SIDE COPILOTS BULKHEAD AT FS 280 RBL 9.0 IS CRACKED AT 1.0 INCH IN WEB RADIUS.SDR VTZA200500112Rib · crackedLEFT BATT RIB IS CRACKED 1.5 INCH.SDR VTZA200500114Rib · crackedRIGHT BATT RIB IS CRACKED .750 INCH BETWEEN THE ATTACHING FASTENERS.SDR 05055628Contactor · failedEVENT SUMMARY STATED 628BR RTF DUE TO ELECTRICAL FAILURE. REMOVED AND REPLACED ESS BUSS CONTACTOR & ADG AUTO DEPLOY CONTROL.SDR 05025628Engine · splitEVENT SUMMARY STATED THAT 1 N2 SPLIT AFTER TAKEOFF, READ AS HIGH AS 2.2. ALL OTHER PARAMETERS MATCHED. REMOVED AND REPLACED ENG SPEED CONTROL PANEL IAW AMM 73-21-00. OPS CHECK GOOD.SDR 04235628Motor · weakCABIN DOOR HEAVY TO OPEN. REMOVED AND REPLACED PAX DOOR COUNTERBALANCES. DOOR ASSIST MOTOR WEAK.SDR 04127628Bulb · burned outDURING INSPECTION THE NR 3 OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR 04035628Control Unit · faultyDURING APPROACH THE CREW REPORTED A FLAP SYSTEM FAILURE WITH FLAPS AT 0 DEGREE POSITION. FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY. THE FLAP ELECTRONIC CONTROL UNIT WAS FOUND FAULTY AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORSDR 03301628Landing Gear · corrodedDURING FLIGHT CREW RECEIVED A NOSE GEAR DISAGREE WARNING MESSAGE. UPON TROUBLESHOOTING ON GROUND THE NOSE LANDING GEAR ASSEMBLY WAS FOUND TO BE CORRODED AND GOUGED. THE BRACKETS AND STRUCTURE ON WHICH THE PROXIMITY SENSORS WERE MOUNTED WERE ALSO FOUND CORRODSDR 03268628Tire · separatedDURING LANDING THE NR 3 MAIN TIRE HAD TREAD SEPARATION. NO EMERGENCY DECLARED AIRCRAFT TAXIED TO GATE WITHOUT INCIDENT PASSENGERS WERE DEPLANED NORMALLY. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE NR 3 MAIN TIRE.SDR 03265628Light · inoperativeDURING INSPECTION THE 2ND CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT BULB. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.SDR 03121628Bulb · burned outDURING PREFLIGHT INSPECTION THE CREW DISCOVERED A CEILING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE PERSONNEL REPLACED A BULB AND PERFORMED A SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.SDR 03101628Battery · inoperativeDURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS WOULD NOT STAY ILLUMINATED. MAINTENANCE PERSONNEL REMOVED AND REPLACED THREE EMERGENCY EXIT LIGHT BATTERIES. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SDR 03088628Bulb · burned outDURING MAINTENANCE INSPECTION, THE CABIN DOOR AND SERVICE DOOR EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY EXIT LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RSDR 03086628Connector · damagedDURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK AT SEAT ROW 1 WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE CONNECTOR FOR THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETSDR 02174628Mechanism · lack of lubeDURING TURN AROUND SERVICING, THE CREW NOTED THAT THE GALLEY SERVICE DOOR COULD NOT BE OPENED FROM THE OUTSIDE. MAINTENANCE PERSONNEL LUBRICATED THE GALLEY SERVICE DOOR HANDLE OPERATING MECHANISM. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RESDR 02132628Line · failedPASSING THROUGH 8000 FT IN THE CLIMB, THE CREW NOTED THE R ENG OIL PRESS RED WARNING ON THE EICAS. THE QRH WAS COMPLIED WITH, THE ENGINE WAS SHUT DOWN. THE AIRCRAFT RETURNED TO CAE, AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL FOUND THE B-SUMP OIL LIN
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