N7455U, cancelled Oct 19, 2012
Service difficulty reports · 22
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 = 'N7455U' AND deregistration_id = 'N7455U-2012-10-19' 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 = 'N7455U' AND deregistration_id = 'N7455U-2012-10-19' 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 2002UALA01143Skin · damagedFORWARD LOWER FUSELAGE SKIN, BODY STATION 312-328, DRAIN HOLE AFT OF NOSE LANDING GEAR WHEEL WELL IS PUNCTURED AND BROKEN OUT. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR.SDR 2002UALA01118Stringer · corrodedFORWARD PIT STRINGER 27R CORRODED BEYOND LIMITS BODY STATION 630. MAJOR REPAIR ACCOMPLISHED. HAT SECTION REPAIR.SDR 2002UALA01117Stringer · corrodedFORWARD CARGO PIT AT BODY STATION 480, STRINGER 27L IS CORRODED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. STRINGER SPLICE REPAIR.SDR 2002UALA01101Shear Tie · corrodedFORWARD CARGO PIT AT BODY STATION 480-500, STRINGER 28R, INTERCOSTAL LOWER FLANGE IS CORRODED AND SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. REPAIRED INTERCOSTAL LOWER FLANGE & SHEAR TIE.SDR 2002UALA01100Skin · corrodedFORWARD PIT INTERNAL SKIN STATION 500 AT STRINGER 28R IS BLENDED BEYOND LIMITS DUE TO CORROSION REMOVAL. MAJOR REPAIR ACCOMPLISHED. INSTALLED EXTERNAL DOUBLER REPAIR.SDR 2002UALA01099Stringer · corrodedFORWARD PIT STRINGER 28R CORRODED ON LOWER SIDE AT BODY STATION 494. MAJOR REPAIR ACCOMPLISHED. SPLICE REPAIR.SDR 2002UALA01083Frame · corrodedAFT PIT FRAME AT BODY STATION 950F BETWEEN STRINGER 27L AND 28L, FRAME AND SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. REPAIRED SHEAR TIE.SDR 2002UALA01082Doubler · damagedSLIGHT EDGE DAMAGE TO REPAIR DOUBLER FOUND UNDER AFT PIT BELOW LOADING THRESHOLD. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND QUADRUPLER.SDR 2001UALA00323Regulator · failedAT DEPARTURE TIME CREW LOST ALL OXYGEN PRESSURE TO ALL MASKS IN THE FLIGHT DECK. SUPPLEMENTAL DATA UPDATE FOUND THAT PRESSURE REDUCING REGULATOR WAS NOT LETTING AIR OUT OF PRESSURE REGULATOR VALVE. REPLACED CREW OXYGEN PRESSURE REDUCING REGULATOR PER MAINTENSDR 2000UALA00222Valve · stuckNR 1 ENGINE OIL TEMPERATURE AT 135 TO 140 DEGREES FOR 13 MINUTES. WENT TO 150 DEGREES AT SHUT DOWN. WINDMILLED ENGINE FOR 25 MINUTES. RE-STARTED ENGINE ON FINAL, RAN ENGINE FOR 9 MINUTES AND OIL TEMPERATURE 120 DEGREES. OIL PRESSURE AND QUANTITY GOOD ENTIRSDR 98UAL900556Coffeemaker · defectiveMINOR SMOKE IN AFT GALLEY. SUBMITTER STATES, SUSPECTED CAUSE WAS EITHER A LIGHT BULB OR A COFFEE MAKER. SUBSEQUENT INSPECTION SHOWED THAT THE COFFEE MAKER WAS DEFECTIVE. THE COFFEE MAKER WAS REPLACED AND CHECKED FOR PROPER OPERATION.SDR 98UAL900502Control Mech · malfunctionedWHEN THE SPEED BRAKE IS DEPLOYED, AIRCRAFT BANKS TO THE LEFT EXCESSIVELY. AILERON TRIM SET AT 0. WHEN THE B-SYSTEM IS OFF, THE AIRCRAFT DOES NOT ROLL.SDR 98UAL900467Drive Motor · leakingAFTER DEPARTURE LOST HYDRAULIC SYSTEM A PRESSURE. CONTINUED TO ORD AND WAS TOWED TO THE GATE. *S/D* REPLACED HYD FLAP DRIVE MOTOR AND NR 1 AND NR 2 ENGINE DRIVEN HYDRAULIC PUMPS PRECAUTIONARY. ALSO, REPLACED CASE DRAIN AND PRESSURE FILTERS PER MAINTENANCE SDR 97UAL900832Prox Sensor · failedAFTER TAKEOFF, INTERMITTENT AURAL WARNING HORN SOUNDED. TCAS FAILED AND BOTH TRANSPONDERS STOPPED WORKING. CABIN PRESSURE CONTROLLER WAS NOT CONTROLLING PRESSURE. FIFTY MINUTES LATER EVERYTHING STARTED WORKING AGAIN. FORTY MINUTES LATER THE MALFUNCTIONS RESDR 97UAL900532Connector · leakingHAD A RIGHT STRUT OVERHEAT LIGHT ON CLIMBOUT. REDUCED POWER AND LIGHT WENT OUT. SLOWLY INCREASED BACK TO CLIMB POWER AND LIGHT REMAINED OUT. *S/D* FOUND SMALL IDLE LEAK BLOWING ON FIRE LOOP. REPLACED WEAR RING IN 13TH STAGE DUCT CONNECTOR FOR NR 3 ENGINESDR 97UAL900424Actuator · failedSTABILIZER MAIN ELECTRIC TRIM SLOW. CRUISE TRIM OK. FORWARD TRIM STALLS OUT, AFT TRIM OK. BRAKE ASSEMBLY SEEMS TO BE INOPERATIVE. COULD NOT MANUALLY CRANK STABILIZER TRIM FULL NOSE DOWN. ALSO, TRIMS ELECTRIC NOSE DOWN VERY SLOWLY. *S/D* REPLACED MAIN TRSDR 97UAL900302Seal · wornSMOKE IN CABIN AT DISPATCH TIME APU LOAD CONTROL VALVE WOULD NOT OPEN AFTERWARDS. SUPPLEMENTAL DATA UPDATE, SEALS ON THE OIL BREATHER FITTING HAD WORN AND OIL WAS LEAKING EXTERNALLY INTO THE EXHAUST. ALSO, THE AIR/OIL COMPRESSOR SEAL AND THE TURBINE SEAL WERSDR 97UAL900293Oil Seal · leakingDISPATCH MECHANIC NOTED SMOKE COMING FROM APU IN THE RT WHEEL WELL AREA AROUND EXHAUST DUCT. SUPPLEMENTAL DATA UPDATE, THE CAUSE OF THE SMOKE WAS BELIEVED TO BE RESIDUAL GLYCOL. HOWEVER, THE SEALS ON THE OIL BREATHER FITTING HAD WORN AND OIL WAS LEAKING EXTESDR 96UAL900923Inflation Tube · leakingSLIDE REMOVED PER AIR CRUISERS SERVICE INFORMATION LETTER 25-98. DURING SHOP OVERHAUL A SEAM LEAK DEVELOPED ON THE INFLATION TUBE. SCRAPPED SLIDE.SDR 96UAL900325Input Rod · out of adjustEN ROUTE, STABILIZER STUCK IN NOSEDOWN POSITION. LANDED DEN UNDER AMBER ALERT. *S/D* STABILIZER BRAKE UNDER COCKPIT FLOOR WAS NOT COMPLETELY DISENGAGING. ADJUSTED STABILIZER TRIM INPUT ROD PER THE MAINTENANCE MANUAL.SDR 95UAL900319Retract Mech · malfunctionedNR 5 L.E. FLAP WOULD NOT RETRACT WHEN FLAPS RETRACTED FROM 2 DEGREES TO ZERO DEGREES. RETURNED TO ORD.SDR 95UAL900106Light · inopEMERGENCY EXIT LIGHT INOP AT AIRSTAIRS DOOR. REPLACED LIGHT AND POWER CABLE ASSEMBLY, CHECKS OK.
Back to N7455U, cancelled Oct 19, 2012