N510TA, cancelled Jul 25, 2012
Service difficulty reports · 24
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 = 'N510TA' AND deregistration_id = 'N510TA-2012-07-25' 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 = 'N510TA' AND deregistration_id = 'N510TA-2012-07-25' 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 WRN2009F00000Fire Loop · defectiveENGINE NR 1 SHUT DOWN IN FLIGHT DUE TO A FIRE INDICATION DURING FLIGHT FROM BDL TO BQN. BOTH FIRE BOTTLES WERE DISCHARGED. WARNING LIGHT EXTINGUISHED. ACFT LANDED NORMALLY. NO FUEL DUMPED. MX REPLACED 3 FIRE LOOPS AND AN AMPLIFIER. RUN UP CHECK OK. ACFTSDR WRN2008F00004Sill · fodAC AFTER TAKEOFF, LOUD WHISTLING NOISE HEARD AND AC HAD PROBLEMS PRESSURIZING. AC MADE UNSCHEDULED STOP, WITH NORMAL LANDING. FOUND F.O.D. AND DEBRIS IN MAIN CARGO DOOR SILL AREA. REMOVED F.O.D. AND DEBRIS FROM CARGO DOOR SEAL AREA IAW 52-70-00. SEAL FOR MAIN SDR WRN2008F00002Valve · stuckAFTER TAKEOFF, PRESSURIZATION MALFUNCTION OCCURRED. ACCOMPLISHED ABNORMAL PROCEDURES. AC RETURNED TO FIELD. LANDING NORMAL. MX FOUND GROUND VENT VALVE STUCK CLOSED. MX CLEANED AND RESET GROUND VENTING VALVE IAW 21-31-17, PG 501. OPS CHECKED SATISFACTORYSDR WRNA200800037Csd · malfunctionedDURING FLIGHT, NR 1 CONSTANT SPEED DRIVE LOW OIL PRESSURE LIGHT ILLUMINATED FOLLOWED BY RISING OIL TEMPERATURE. DISCONNECTED CSD AND RETURNED TO MFM FOR A SAFE LANDING. REPLACED CSD IAW MM 24-11-11 PG 401 AND CSD OIL COOLER IAW 24-11-21 PAGE 401. AIRCRAFT RSDR WRNA200700064Damper · malfunctionedAFTER DEPARTURE WHEN RAISING GEAR, LEVER WOULD NOT GO PAST THE MID POSITION, GEAR POSITION LIGHTS REMAINED 'GREEN'. RETURNED TO FIELD AND MADE A SAFE LANDING. AIRCRAFT MAINTENANCE FERRIED TO CTS IN JAPAN FOR CORRECT ACTION. REPLACED LT GEAR PITCH DAMPER, AISDR WRNA200700058Line · obstructedDURING TAKEOFF ROLL, FIRST OFFICERS AIR SPEED LAGGED BEHIND CAPTAINS BY 40-60 KNOTS, ABORTED TAKEOFF. FLUSHED DEBRIS FROM PITOT PRESSURE LINES, ACCOMPLISHED PITOT/STATIC TEST IAW 34-11-10 PAGE 501. TEST NORMAL. AIRCRAFT RELEASED FOR SERVICE.SDR WRNA200700057Pitot Tube · leakingDURING TAKEOFF THE FIRST OFFICERS AIRSPEED INDICATOR LAGGED 40-60 KNOTS BEHIND CAPTAINS AIRSPEED INDICATOR. FOUND RT PITOT PROBE LEAKING, REPLACED RT PITOT PROBE IAW A300 MM 34-11-15 PAGE 401. ACCOMPLISHED LEAK CHECK IAW A300 MM 34-11-10 PAGE 501. AIRCRAFT SDR WRNA200700051Circuit Breaker · weakAFTER TAKEOFF, FUEL PUMP NR 1; 1A; 2 CIRCUIT BREAKERS POPPED, AND AFCS AND FLIGHT ENGINEER PANEL LIGHTS WENT OFF. RETURNED TO FIELD AND MADE A SAFE LANDIBG. REPLACED FAULTY BREAKER IN 101VU PANEL.SDR WRNA200700065Bulkhead · crackedDURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD AT STR TIE END ANGLE FITTING AT 35R. FABRICATED FITTING FROM 7076 T6511 EXTRUSION IAW SRM 51-10-40. APPLIED PROTECTIVE COATINGS IAW SRM 51-40SDR WRNA200700070Fitting · corrodedDURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD STR TIE END ANGLE FITTING AT 38R. FABRICATED FITTING FROM 7076 T6511 EXTRUSION IAW SRM 51-10-40, APPLIED PROTECTIVE COATINGS IAW SRM 51-40-12,SDR WRNA200700069Fitting · corrodedDURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD STR TIE END ANGLE FITTING AT 37R. FABRICATED FITTING FROM 7076 T6511 EXTRUSION IAW SRM 51-10-40, APPLIED PROTECTIVE COATINGS IAW SRM 51-40-12,SDR WRNA200700068Fitting · corrodedDURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD STR TIE END ANGLE FITTING AT 36R. FABRICATED FITTING FROM 7076 T6511 EXTRUSION IAW SRM 51-10-40, APPLIED PROTECTIVE COATINGS IAW SRM 51-40-12,SDR WRNA200700067Fitting · corrodedDURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD STR TIE END ANGLE FITTING AT 35R. FABRICATED FITTING FROM 7076 T6511 EXTRUSION IAW SRM 51-10-40, APPLIED PROTECTIVE COATINGS IAW SRM 51-40-12,SDR WRNA200700066Bolt · corrodedDURING ACCOMPLISHMENT OF CPCP C54-400-03-00 AT M96 CHECK LEVEL II CORROSION WAS FOUND ON 4 HORIZONTAL BOLTS OF NR 2 ENGINE AFT MOUNT. REMOVED AND REPLACED 4 HORIZONTAL MOUNT BOLTS IAW MM 20-21-17 AND MM 70-00-00.SDR WRNA200700049Indication Sys · malfunctionedDURING TAKEOFF FOR TEST FLIGHT AFTER HEAVY MAINTENANCE VISIT, CONFIGURATION LIGHT AND WARNING HORN CAME ON, TAKEOFF ABORTED. REPLACED LEADING EDGE INSTRUMENTATION UNIT IAW MM 27-84-11. AIRCRAFT RELEASED, TEST FLIGHT COMPLETED SATISFACTORY.SDR WRNA200700053Support · crackedDURING M-96 CHECK, A 3 INCH CRACK WAS FOUND IN THE NR 2 ENGINE OUTBOARD CORE COWL SUPPORT. ACCOMPLISHED WELD REPAIR IAW ENGINEERING ORDER 2-54907-800 FROM EMTEQ.SDR WRNA200700052Trunnion · corrodedDURING M-96 CHECK, CORROSION WAS FOUND IN LT MAIN LANDING GEAR AFT TRUNNION FORWARD LUG FITTING BORE AND FACE. REMOVED CORROSION BY OVERSIZING BORE AND SPOT FACING THE LUG FACE AND INSTALLED NEW BUSHING IAW REPAIR DESIGN APPROVAL SHEET RAS/BAE/1005347/2007.SDR WRNA200700055Rib · unserviceableDURING M96 COMPLY WITH S/B A300-57-0245, REPLACEMENT OF LT INBOARD FLAP RIB NR 7. REMOVED LEFT WING INBOARD FLAP, RIB NR 7, PERFORMED HFEC INSPECTION IAW A300-57-0245, NO DEFECTS NOTED. INSTALLED NEW NR 7 RIB P/N A5796005000400 IAW S/B A300-57-0245.SDR WRNA200700056Floorbeam · crackedDURING M-96 CHECK, FOUND LOWER CROSS BEAM OF FLOORBEAM AT FRAME 57 BL 0 CRACKED. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-30.SDR RNA200700054Floorbeam · corrodedDURING M-96 CHECK, FLOOR SUPPORT BEAM IN AFT CARGO AT FRAME 63 WAS FOUND CORRODED AND HAD A 5 INCH CRACK BETWEEN STR 41L AND 43L. CUT OUT DAMAGED SECTION OF FLOORBEAM CAP ANGLE AND INSTALLED 12 INCH LENGTH OF FLOORBEAM AND REPAIR DOUBLER IAW SRM 51-41-40.SDR WRNA200700054Floorbeam · corrodedDURING M-96 CHECK, FLOOR SUPPORT BEAM IN AFT CARGO A7 FRAME 63 WAS FOUND CORRODED AND HAD A 5 INCH CRACK BETWEEN STR 41L AND 43L. CUT OUT DAMAGED SECTION OF FLOORBEAM CAP ANGLE AND INSTALLED 12 INCH LENGTH OF FLOORBEAM AND REPAIR DOUBLER IAW SRM 51-41-40.SDR WRNA200700028Slide · deployedON GROUND, CREW OPENED LEFT HAND DOOR WITH DOOR ARMED, SLIDE WAS DEPLOYED. SLIDE WAS PLACED ON MEL 52-61-01 AND AIRCRAFT RELEASED FOR SERVICE. SLIDE WAS REPLACED ON 6-6-07 PER MM 25-61-00 PAGE 401.SDR WRNA200600026Slide · will not armR2 DOOR SLIDE WILL NOT ARM. REPLACED DOOR SLIDE IAW A300 25-61-11. RETURNED TO SERVICE.SDR WRNA200500007Adc · unserviceableAFTER TAKEOFF, CAPTAINS AIRSPEED INDICATOR DECREASED TO ZERO (0). CAPTIANS ALTIMETER REMAINED AT 300 FT. DURING CLIMB OUT. AIRCRAFT RETURNED TO AIRPORT, LANDING NORMAL. REMOVED AND REPLACED AIR DATA COMPUTER IAW 34-12-34. OPS AND FUNCTIONAL CHECK SATISFACTO
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