N263AU, cancelled Aug 21, 2002
Service difficulty reports · 81
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 = 'N263AU' AND deregistration_id = 'N263AU-2002-08-21' 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 = 'N263AU' AND deregistration_id = 'N263AU-2002-08-21' 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 USAA991401Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 400, STRINGER 10R TIE CLIP. REPLACED TIE CLIP PER 51-10-01. (M)SDR USAA991400Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 907, STRINGER 16R TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-02. (M)SDR USAA991399Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 907, STRINGER 16L TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-02. (M)SDR USAA991398Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 767, STRINGER 4R TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-02. (M)SDR USAA991397Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 767, STRINGER 9L TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-02. (M)SDR USAA991396Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 767, STRINGER 47R, TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-01. (M)SDR USAA991395Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A . 5 INCH CRACK STATION 500B, STRINGER 10R TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-02. (M)SDR USAA991394Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 500A, STRINGER 10 TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-02. (M)SDR USAA991393Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 500, STRINGER 10R TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-02. (M)SDR USAA000002Skin · crackedFOUND CRACK ON SKIN AT BS 1140. INSTALLED NEW STRAP PER SRM 53-00-01 AND EA 66420. (M)SDR USAA000001Skin · crackedFOUND CRACK AT AFT FORWARD LOWER CORNER OF SERVICE DOOR BS 947.5 SKIN. INSTALLED REPAIR PLATES PER SRM 53-30-3 FIG 24. (M)SDR USAASB99160Wire · brokenCLT - PILOT REPORTED THAT THE OVERHEAD EMERGENCY LIGHTS AND THE FLOOR LEVEL EMERGENCY LIGHTS ILLUMINATE INTERMITTENTLY DURING FLIGHT. MAINTENANCE FOUND A BARE WIRE AT THE CONNECTOR FOR THE BATTERY PACK AT SEAT ROW 5ABC AND A BROKEN WIRE AT THE WIRE PLUG AT SESDR USAASB99083Connector · looseATL - PILOT REPORTED THA THE FLOOR LEVEL EMERGENCY LIGHTING ILLUMINATED SEVERAL TIMES DURING FLIGHT. MAINTENANCE FOUND A LOOSE CONNECTION AT THE MAIN HARNESS POWER SENSE WIRE. REPLACED CONNECTOR. OPERATIONAL CHECK GOOD. (M)SDR USAASB99080Switch · out of adjustPHL - FLT 2241 - EMERGENCY EXIT LIGHTS (SEAT LIGHTS ONLY) ILLUMINATED IN FLIGHT. MAINTENANCE IN PHL CHECKED OUT THE SYSTEM AND FOUND NOTHING WRONG. THE PROBLEM RETURNED, AND MAINTENANCE IN PVD ADJUSTED THE LEFT SIDE EMERGENCY EXIT OPERATED EMERGENCY LIGHT SWSDR USAASB99078Fuel Pump · failedPHL - FLT 637 - CAPTAIN REPORTED THAT THE NR 2 ENGINE FLAMED OUT AT FL120 ON DESCENT INTO PHL. RESTART WAS ATTEMPTED, BUT UNSUCCESSFUL. APU FAILED TO START ALSO. EMERGENCY WAS DECLARED. FLIGHT LANDED WITHOUT FURTHER INCIDENT AT PHL. TOTAL SINGLE ENGINE TISDR USAASB98292Line · chafedPIT - FLT 734 - EN ROUTE FROM MCI TO PHL, THE 'B' HYDRAULIC SYSTEM QUANTITY DECREASED AND THE LOW PRESSURE LIGHTS ILLUMINATED AT 1.8 GALLONS. DEGREE OF LOSS WAS SUCH THAT CAPTAIN DECIDED A DIVERSION WAS NECESSARY. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FUSDR USAASB98275Connector · looseTPA - PILOT REPORTED THAT THE EMERGENCY EXIT LIGHTS AND THE FLOOR EMERGENCY LIGHTS ILLUMINATED ON THEIR OWN DURING FLIGHT. MAINTENANCE FOUND A CONNECTOR AT SEAT ROW 13 LEFT, NO MAKING GOOD CONTACT. REMOVED AND REPLACED CONNECTOR. OPERATIONAL CHECK GOOD. (MSDR USAASB98272Switch · failedPHL - FLT 1244 - AFTER PUSHBACK, EMERGENCY EXI TLIGHTS IN SEAT ROWS ILLUMINATED AND COULD ONLY BE EXTINGUISHED BY TURNING OFF THE EMERGENCY EXIT LIGHTS SWITCH IN COCKPIT. AIRCRAFT RETURNED TO GATE. MAINTENANCE TROUBLESHOT SYSTEM AND REPLACED THE FLIGHT ATTENSDR USAASB98270Battery Pack · dischargedCLT - FLT 765 - DURING CRUISE, PILOT REPORTED THE EMERGENCY FLOOR TRACK LIGHTING ILLUMINATED WITH THE SWITCH IN THE ARMED POSITION. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT OVERHEAD BATTERY PACKS. OPERATIONAL CHECK GOOD. (M)SDR USAA980383Skin · crackedTPA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK UNDER WING TO BODY FAIRING FUSELAGE SKIN AFT OF STATION 727B AND STRINGER 18R .50 BELOW. INSTALLED DOUBLER .063 301 .5 H STAINLESS PER EA 62403 AND SRM 53-30-3. (M)SDR USAASB98203Fire Loop · failedPIT - FLT 278 - AIRCRAFT WAS RELEASED WITH THE NR 1 ENGINE GENERATOR ON MEL. WHILE EN ROUTE FROM PHL TO DTW, THE APU FIRE WARNING DETECTOR LIGHT ILLUMINATED NECESSITATING AN APU SHUTDOWN. WITH ONLY ONE ELECTRICAL POWER SOURCE REMAINING, FLIGHT DIVERTED TO NESDR USAASB97215Battery Pack · dischargedSYR - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY EVACUATION LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN M192 EMERGENCY LIGHT MODULE. OPS CHECK GOOD. (M)SDR USAASB97141Oil Quantity Ind · failedGSO - FL1267 - ON CLIMB-OUT FOR GSO AT APPROXIMATELY 6,000 FEET, THE NR 1 ENGINE OIL QTY GAUGE SLOWLY DROPPED TO ZERO. CREW CALLED GSO TOWER AND DECIDED TO RETURN TO FIELD. AS THE FLIGHT GOT CLOSER TO GSO, THE NR 1 ENGINE OIL QTY GAUGE STARTED TO CLIMB BACK TSDR USAA960321Stringer · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION ON STRINGER APPROXIMATELY 10 INCHES BY .5 INCH STRINGER 29L STATION 947 TO 957. REPLACED APPROXIMATELY 22.5 INCHES OF STRINGER. REPAIRED PER SRM 53-10-3. (M)SDR USAA960320Stringer · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK BS 767 STRINGER 19 RT. INSTALLED REPAIR, REPAIRED PER SRM 53-10-3. (M)SDR USAA960319Skin · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 767 STRINGER 19 R FUSELAGE SKIN. INSTALLED REPAIR, REPAIRED PER SRM 53-30-3. (M)SDR USAA960318Skin · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK BS 178 WL 210 AT SKIN. INSTALLED DOUBLER, REPAIRED PER TR 53-10-11. (M)SDR USAA960317Angle · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH LONG CRACK STATION 727 UPPER COMPRESSION CHORD ANGLE. INSTALLED REPAIR ANGLE, REPAIRED PER TR 53-10-03. (M)SDR USAA960316Bulkhead Skin · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 178 BULKHEAD SKIN. INSTALLED DOUBLER, REPAIRED PER TR 53-10-11. (M)SDR USAA960315Bulkhead Web · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK, 2 INCH CRACK, 1 INCH CRACK AND .5 INCH CRACK AT 178 BULKHEAD WEB AT LOWER LEFT RADAR DISH MOUNT. INSTALLED DOUBLER REPAIR, REPAIRED PER TR 53-10-11. (M)SDR USAA951050Stringer · corrosionROA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 12 INCHES, STRINGER 27L AT BSL 967. INSTALLED STRINGER SPLICE PER SRM 53-10-3. REPAIRED PER SRM 53-10-3, FIG 1. (M)
Back to N263AU, cancelled Aug 21, 2002