N611US, cancelled Mar 29, 2001
Service difficulty reports · 23
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 = 'N611US' AND deregistration_id = 'N611US-2001-03-29' 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 = 'N611US' AND deregistration_id = 'N611US-2001-03-29' 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 9902056311Hyd Line · leakingDURING CLIMB, THE NR 3 HYDRAULIC SYSTEM LOST FLUID. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. RETORQUED HYDRAUALIC SUPPLY LINE IN THE NR 3 PYLON, OPERATIONAL CHECK GOOD.SDR 9806816611Actuator · malfunctionedDURING CLIMB, THE NR 3 LEADING EDGE FLAP WOULD NOT RETRACT. AIRCRAFT RETURNED TO NRT AND LANDED WITHOUT INCIDENT. REPLACED THE NR 3 LEADING EDGE FLAP ACTUATOR, OPERATIONAL CHECK GOOD.SDR 9803166611Fuel Control · failedON TAKEOFF ROLL, THE NR 4 ENGINE WOULD NOT PRODUCE TAKEOFF EPR WITH THE THRUST LEVER AT THE MECHANICAL STOP. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE FUEL CONTROL AND THE FOLLOW-UP ENGINE RUN WAS NORMAL.SDR 9717116611Gear Light · illuminatedDURING CLIMB, THE RED LANDING GEAR LIGHT ILLUMINATED. RECYCLED THE LANDING GEAR AND THE LIGHT EXTINGUISHED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. VISUALLY INSPECTED LANDING GEAR, ALL CHECKED NORMAL.SDR 9715166611Wire Harness · crossedAIRCRAFT EXPERIENCED A TIRE FAILURE DURING LANDING. AIRCRAFT COMPLETED LANDING WITHOUT FURTHER INCIDENT. REPLACED THE NR 3 AND NR 4 TIRE ASSEMBLIES AND REPOSITIONED WIRE HARNESS FOR THE NR 3 AND NR 4 ANTI-SKID TRANSDUCERS. OPERATIONAL CHECK GOOD.SDR 9714806611Tire · failedAIRCRAFT EXPERIENCED A TIRE FAILURE DURING LANDING. AIRCRAFT COMPLETED LANDING WITHOUT INCIDENT. REPLACED THE NR 3 AND NR 4 TIRE ASSEMBLIES, ALL OPERATIONAL CHECKS GOOD.SDR 9714546611Gearbox · leakingWHILE IN CRUISE, THE NR 4 ENGINE OIL QUANTITY DROPPED TO ZERO. OIL PRESSURE FELL TO THE YELLOW BAND AND THE ENGINE POWER WAS REDUCED TO IDLE FOR TWO MINUTES. THE ENGINE WAS THEN SHUT DOWN. MAINTENANCE FOUND A COVER ON THE ENGINE ANGLE GEARBOX LOOSE. THIS WSDR 9710236611Tire · failedDURING LANDING, THE NR 3 TIRE FAILED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REPLACED THE NR 3 AND NR 4 TIRE ASSEMBLIES, NBR 3 ANTI-SKID VALVE, AND ANTI-SKID CONTROL UNIT, OPERATIONAL CHECK GOOD.SDR 9709986611Bulkhead · crackedDURING TRANSITION CHECK, FOUND CRACK IN NR 4 PYLON REAR ENGINE MOUNT BULKHEAD STRAP NACELLE STA 223. REPAIRED PER EA 66-150141.SDR 9627726611Web · corrodedDURING CHECK, FOUND CORROSION ON THE MAIN DECK PRESSURE WEB INTERIOR SURFACE. REPAIRED PER EA 66-120205.SDR 9623776611Frame · crackedDURING ARMAR VISIT, FOUND CRACKS IN THE BS 400 FRAME INNER CHORD AND WEB AT STR 26R. REPAIRED CHORD AND WEB (P/N 65B07936-328) PER EA 66-110297.SDR 9627716611Skin · corrodedDURING CHECK, FOUND CORROSION ON SKIN INTERNAL DOUBLER. REPLACED DOUBLER PER EA 66-120221.SDR 9617336611Logic Card · defectiveDURING CLIMB, THE RED NOSE LANDING GEAR LIGHT ILLUMINATED AFTER LANDING GEAR RETRACTION. RECYCLED LANDING GEAR AND LIGHT EXTINGUISHED. AIRCRAFT CONTINUED TO SEA AND LANDED WITHOUT INCIDENT. RESEATED GEAR CARDS IN HOLDERS AND GREASED NOSE LANDING GEAR, OPERASDR 9604746611Power Supply · inoperativeDURING LINE CHECK, FOUND 'A' ZONE EMERGENCY FLOOR PATH LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES.SDR 9516426611Longeron · crackedDURING PERIODIC CHECK, FOUND TWO CRACKS, 1.1 AND 0.5 INCH IN STR 9R BS 1430, 1458 RESPECTIVELY. REPAIRED STRINGER (P/N 65B07229-8), PER EA 66-99128, -99157.SDR 9516416611Longeron · crackedDURING PERIODIC CHECK, FOUND TWO CRACKS, 0.75 AND 0.90 INCH STR 8R BS 1307, 1331 RESPECTIVELY. REPAIRED STRINGER (P/N 65B07229-34), PER EA 66-99128.SDR 9516406611Longeron · crackedDURING PERIODIC CHECK, FOUND A CRACK IN STR 8R, BS 1466. REPAIRED STRINGER (P/N 65B07229-34), PER EA 66-99123.SDR 9516396611Floorbeam · crackedDURING PERIODIC CHECK, FOUND A ONE INCH CRACK IN THE UPPER DECK FLOORBEAM WEB, FS 460 RBL 88. REPAIRED WEB (P/N 65B10933-502), PER EA 66-99126.SDR 9515246611Fittings · corrodedDURING PERIODIC CHECK, FOUND CORROSION IN THE LBL 120 TO 125 OVERWING LONGERON AT THE FORWARD AND AFT UPLOCK SUPPORT CASTINGS, BS 1301 AND 1309. REPLACED FITTINGS (P/N 65B01332-7, 65B01331-15), PER SRM 53-10-01 FIG 1.SDR 9508066611Transmission · failedDURING CLIMBOUT, THE OUTBOARD TRAILING EDGE FLAPS WOULD NOT RETRACT PAST 10 DEGREES IN NORMAL OR ALTERNATE POSITION. CREW FOLLOWED COCKPIT OPERATING MANUAL, DUMPED 58,000 LBS OF FUEL, AND MADE AN UNEVENTFUL LANDING IN NRT. MAINTENANCE REPLACED SCREW ASSEMBLYSDR 9507906611Dnlock Actuator · malfunctionedDURING APPROACH FOR LANDING AND AFTER LOWERING THE LANDING GEAR, EXPERIENCED RAPID LOSS OF HYDRAULIC FLUID ON NO.1 SYSTEM. HYDRAULIC PRESSURE DECREASED TO ZERO AND BOTH LOW PRESSURE AND QUANTITY LIGHTS ILLUMINATED. CREW FOLLOWED COCKPIT OPERATING MANUAL PROCEDSDR 9506596611Oil Filter · dirtyDURING CRUISE, NR 2 ENGINE OIL FILTER CLOG LIGHT ILLUMINATED. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT DIVERTED TO ANCWHERE AN UNEVENTFUL THREE ENGINE LANDING WAS MADE. NO FUELWAS DUMPED. DEBRIS WAS FOUND IN THE MAIN OIL FILTER. THE FILTER WAS REPLACED ANDSDR 9503596611Oil Filter · cloggedDURING CRUISE NR 2 ENGINE OIL FILTER CLOG LIGHT ILLUMINATED. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT DIVERTED TO ANC WHERE AN UNEVENTFUL THREE ENGINE LANDING WAS MADE. NO FUEL WAS DUMPED. DEBRIS WAS FOUND IN THE MAIN OIL FILTER. THE FILTER WAS REPLACED AN
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