N955QS
Service difficulty reports not matched to an aircraft · 31
They name N955QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N955QS' AND registry_match IS NULL 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 = 'N955QS' AND registry_match IS NULL 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 DXTA2016060306252Bracket · damagedDAMAGE FOUND IN TAILSTAND AREA WHILE INSTALLING TAIL STAND PRIOR TO MAINTENANCE. NO RECORD OF DAMAGE FOUND. REMOVED TAIL STAND BRACKET, PN 6712405-10 IAW SRM 51-40-03. IAW ENGINEERING REQUEST, RECONTOURED CREASED AREA AND BLENDED SHARP EDGES. STARTED FITTINGSDR DXTA2016032306214Skin · corrodedCORROSION WAS FOUND UP TO 0.003 INCHES DEEP ON THE SKIN, PN 6711032-9, OF THE LOWER SKIN BOND ASSEMBLY, PN 6711030-4, ALONG THE FWD PRESS BULKHEAD PLANE AT LBL 17.5. ALL CORROSION DAMAGE WAS REMOVED BY BLENDING. THE REMAINING THICKNESS WAS MAPPED USING ULTRASDR DXTA2016032306213Skin · corrodedCORROSION WAS FOUND ON THE 6711070-2 RT AFT CABIN SKIN UNDER THE TCAS ANTENNA AT FS 205.00, RBL 4.17. ALL CORROSION DAMAGE WAS REMOVED BY BLENDING. THE REMAINING THICKNESS WERE MAPPED USING ULTRASOUND. THE MINIMUM REMAINING THICKNESS WAS 0.025 INCHES. THE SDR DXTA2016032306212Skin · corrodedCORROSION WAS FOUND UP TO 0.012 INCH DEEP ON THE LT SKIN, PN 6711032-21, OF THE LT SKIN BOND ASSEMBLY, PN 6711033-3, AT FS 187 ABOVE STRINGER 12L. ALL CORROSION DAMAGE WAS REMOVED BY BLENDING. THE REMAINING THICKNESS WAS MAPPED USING ULTRASOUND.SDR DXTA2016032306211Tail Cone · corrodedCORROSION WAS FOUND AT SEVERAL LOCATIONS ON THE TAIL CONE. ALL CORROSION WAS REMOVED BY BLENDING. THE REMAINING THICKNESSES WERE MAPPED AT EACH SITE USING ULTRASOUND. ACCOMPLISHED REPAIR DEFINITION S-750-0055 25RD, MAJOR REPAIR, REPAIR OF BAGGAGE DOOR & TAISDR DXTA2016032306210Skin · corrodedCORROSION WAS FOUND AT FOUR LOCATIONS ON THE TAIL CONE UPPER SKIN, AROUND THE PERIPHERY OF THE DORSAL FAIRING. ALL CORROSION DAMAGE WAS REMOVED BY BLENDING. THE REMAINING THICKNESSES WERE MAPPED AT EACH SITE USING ULTRASOUND. ACCOMPLISHED REPAIR DEFINITION SDR DXTA2016032306209Skin · corrodedSEVERAL CORROSION SITES WERE FOUND ON THE FUSELAGE SKINS. PRESS VESSEL SKIN IS CORRODED AT THE FOLLOWING ATA 53 LOCATIONS ALONG THE UPPER SURFACE, FS 527 3 SPOTS, FS 413 1 SPOT, FS 388 3 SPOTS, FS 362 1 SPOT, FS 370 1 SPOT, FS 327, FS 316, FS313, FS 298, FS 2SDR DXTA2013092305514Squat Switch · failedAFTER DEPARTURE, LANDING GEAR WOULD NOT RETRACT. LANDING GEAR HANDLE WOULD NOT MOVE. REMOVED AND REPLACED NLG SQUAT SWITCH IAW MM 32-20-00. OPS CHECKED GOOD.SDR DXTA2013091605505Module · failedLANDING GEAR WOULD NOT RETRACT AFTER LIFTOFF. NOSE GEAR GREEN LIGHT STAYED ILLUMINATED ALONG WITH RED ULOCKED LIGHT. GEAR LOWERED IAW THE EMERGENCY CHECKLIST. GEAR HANDLE WAS STIFF ON SELECTION TO DOWN. MAINS ILLUMINATED IMMEDIATELLY AND "HYD PUMP FAIL A" MOSDR DXTA2013091305502Circuit Board · failedDURING GEAR RETRACTION AFTER TAKEOFF, RED UNLOCK STAYED ON. WITH NOISE LIKE GEAR DOORS WHERE OPEN. PERFORMED ROTARY TEST FOR GEAR LIGHTS, RED UNLOCK LIGHT DOES NOT TEST. COMPLIED WITH LANDING GEAR FUNCTIONAL CHECKS AND GEAR OPS CHECKED GOOD. CHECKED INTEGRISDR DXTA2013080605469Uplock Switch · inoperativeAFTER TAKEOFF, GEAR HANDLE PLACED IN UP POSITION. NOSE GEAR DID NOT RETRACT. ALL THREE LANDING LIGHTS WERE OUT AND UNLOCK LIGHT WAS ILLUMINATED. COULD HEAR THAT IT WAS NOSE GEAR THAT WAS DOWN. RAN GEAR RETRACT CHECKLIST AND RECEIVED THREE GREEN GEAR DOWN LIGSDR DXTA2013062405422Ball End · disconnectedON LANDING, AROUND 80 KTS, LOST ALL NOSEWHEEL STEERING. ACFT PULLED RIGHT THEN TURNED LEFT HAD TO USE DIFFERENTIAL BRAKING TO KEEP ACFT ON RUNWAY. FOUND THE ROD END OF BALL SWIVEL HAD COME OFF. BALL SWIVEL ALSO ATTACHES TO CONTROL ASSY POWER STEERING DRIVE SDR DXTA2013052105401Bungee · contaminatedDURING DESCENT WITH AUTOPILOT OFF, ELEVATOR JAMS AT CERTAIN CONTROL COLUMN POSITIONS. THE CONTROL COLUMN FELT LIKE IT WAS IN A DETENT AND REQUIRED FORCE TO MOVE IT OUT. THIS WAS AT 170 KNTS WITH FLAPS 15. OPERATED SYSTEM WITH AND WITHOUT ENGINES RUNNING, NOSDR DXTA2013042905363Elevator System · malfunctionedON LT BASE TO FINAL WITH GEAR AND FLAPS 35 AND 145KTS WITH AUTOPILOT OFF. ELEVATOR PRESSURE STUCK WHEN APPLYING DOWNWARD PRESSURE. IT TOOK EXCESSIVE FORCE TO PULL YOKE FWD AND AFT AND LANDING WAS MADE MOSTLY WITH TRIM.SDR DXTA2012081305090Cable · out of toleranceRED GEAR UNLOCK LIGHT ON WHEN GEAR WAS RETRACTED. NO NOISE OR VIBRATIONS. 3 GREEN WITH NO RED WHEN GEAR WAS EXTENDED. HANDLE WENT TO THE FULL UP POSITION. ADJUSTED NOSE LANDING GEAR EMERGENCY RELEASE CABLE TENSION IAW CE-750 M/M 32-30-06. LANDING GEAR OPS SDR DXTA2012070905044Unknown · unknownENROUTE THE CREW HEARD 4 LOUD "BUMPS IN THE NIGHT". PERFORMED TROUBLESHOOTING STEPS, NO DEFECTS FOUND. PERFORMED ADJUSTMENT TO THE NOSE GEAR EMERGENCY EXTEND CABLE. CYCLED GEAR NUMEROUS TIMES, NO FAULTS FOUND. CHECKED ADJUSTMENT TO THE UPLOCK SWITCHES, NO FSDR DXTA2011111504790Uplock Switch · failedNOSE GEAR BUMP HEARD AND FELT 3 TIMES DURING THE FIRST 30 MINS OF THE FLIGHT. R & R NOSE UPLOCK SWITCH. CYCLED GEAR SEVERAL TIMES. OPS CHECKED GOOD IAW MM CH 32-60-00.SDR DXTA2011100204714Acm · seizedDURING TAXI OUT CABIN PAC RAN AWAY HOT (SUPPLY 220+) AND WAS UNCONTROLLABLE IN AUTO OR MANUAL. THE CABIN APPEARED HAZY AS THOUGH THEIR MIGHT BE SMOKE BUT LACKED ODOR. FOUND CABIN ACM SEIZED. R & R CABIN ACM IAW AMM 21-51-00. OPS NORMAL.SDR DXTA2011050404572Strut · damagedGEAR UNLOCK LIGHT (RED) ILLUMINATED IN FLIGHT WHILE CLIMBING OUT OF 38,000 FT. AT THE SAME TIME WE HEARD A THUD NOISE COME FROM THE NOSE GEAR COMPARTMENT AREA. UNLOCK LIGHT REMAINED ILLUMINATED FOR ABOUT 30 THEN EXTINGUISHED 10 MIN FROM LANDING. LANDING GEARSDR DXTA2010081204188Acm · seizedSMOKE IN THE COCKPIT AND CABIN. TURNED BOTH PAC'S OFF AND SMOKE CLEARED. FOUND COCKPIT ACM SEIZED, R & R COCKPIT ACM, OPS CHECKS GOOD IAW MM 21-51-00. ALSO R & R COCKPIT WATER SEPARATOR COALESER, OPS CHECKS GOOD IAW MM 12-10-01. PN 246451-3, ALSO CLEANED CASDR DXTA2009030103527Wire · damagedCOMPLETED OPS CHECKS OF FLAP SYS WIRING, FLAP SYS BREAKOUT BOX WITH NO FAILURE. INSP WIRING FROM FLAP RESOLVERS TO CONVERTER BOXES AS DESCRIBED IN EXPERT SYS FLAP TROUBLESHOOTING AND FOUND DAMAGED WIRING NEAR LT WING/FUSELAGE CONNECTOR PL003 REPAIRED WIRE 21PSDR DXTA2009030203527Controller · malfunctionedDURING CRUISE AT FL410, AMBER (FLAPS FAIL) EICAS MESSAGE ILLUMINATED, AND FLAP RESET BUTTON ILLUMINATED. FLAP CONTROLLER DID NOT RESET IN FLIGHT. COMPLETED OPS CHECKS OF FLAP SYS WIRING, FLAP SYS BREAKOUT BOX WITH NO FAILURE. INSPECTED WIRING FROM FLAP RESOSDR DXTA2009021603506Unknown · odorINFLIGHT, DURING DESCENT WITH APU RUNNING, PASSING 14,000 FT, HAD SMOKE ODOR IN COCKPIT. CLEANED AND LUBRICATED POPPET VALVES. VALVES ARE MOVING FREELY AND NO LONGER STICKING. REINSTALL COALESCER SOCK AND CLOSED WATER SEPARATOR IAW MM 21-51-00. OPERATION WISDR DXTA2009020603494Converter · shortedREPLACED GROUND SEAL PN S3521-6 AT GT048 REMOVED AND REPLACED RT RESOLVE CONVERTER (DUE TO FAIL MSG) ELECTRICAL RIG CHECK GOOD, FLAPS SYS CHECK GOOD IAW MM CH 27-50-00.SDR DXTA200807213184Wheel · unbalancedSEVERE NOSEWHEEL SHIMMY VIBRATION STARTED AT APPROX 100KTS ON TAKEOFF ROLL. DID NOT STOP UNTIL APPROX 60 KTS DURING ABORT. SUB:T/S IAW AMM 32-20-00. REPLACED LT NOSE WHEEL IAW MM 32-41-01. REPLACED UPPER TORQUE LEAK IAW AMM 32-20-00. CHECKS GOOD IAW AMM 32-SDR DXTA200803184Wheel · vibrationSEVERE NOSE WHEEL SHIMMY VIBRATION STARTED AT APPROX 100KTS ON TAKEOFF ROLL. DID NOT STOP UNTIL APPROX 60 KTS DURING ABORT. (A)SDR DXTA200803136Roller · damagedNOSE GEAR "BUMP" OCCURED MULTIPLE TIMES DURING CLIMBOUT. WHILE LUBING NOSE UPLOCK ROLLERS FOUND NOSE ROLLERS SCARED & ROUGH. REPLACED NOSE UPLOCK ROLLERS, BUSHINGS & BOLTS IAW MM 32-20-00.SDR DXTA200601402Battery · overtempBATT 2 O'TEMP MASTER WARNING MESSAGE ILLUMINATED IN CRUISE FLIGHT BATT NR 2 TEMP WAS OVER 70DEG AND CONTINUED TO RISE TO 100 DEG AFTER BATT NR 2 WAS TURNED OFF. REMOVED DEFECTIVE BATTERY AND INSTALLED NICAD BATTERY. NICAD SENT FOR NR 2 POSITION, WORK DONE ISDR DXTA200601388Engine · failedDURING TAXI, RIGHT ENGINE SHUT DOWN, HAD JUST ADVANCED TLA TO CROSS A RUNWAY AND RIGHT ENGINE FAILED. CHECKED THE RIGHT ENGINE FADECS FOR FAULTS, NO FAULTS INDICATED. RAN THE RIGHT ENGINE NUMEROUS TIMES WITH NORMAL STARTS AND ACCELERATION EACH TIME. INSPECTSDR DXTA200601254Controller · malfunctionedAFTER TAKEOFF, ONCE THE FLAP RETRACTION SEQUENCE HAD COMPLETED, THE AMBER MESSAGE "FLAPS FAIL" ILLUMINATED. ABNORMAL CHECKLIST PROCEDURES WERE COMPLIED WITH (FLAP RESET BUTTON), MESSAGE DID NOT CLEAR. FOUND FLAP CONTROLLER HAVE FAULTS. RESET FLAP CONTROLLERSDR DXTA200400324Engine · overtempDURING TAKEOFF ROLL, RIGHT ENGINE ITT EXCEEDED LIMITS, ENGINE EICAS EXCEEDED PAGE INDICATES 898 DEGREE CELSIUS FOR 5 SECONDS. ABORTED TAKEOFF. ITEM IS UNDER INVESTIGATION.
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