N376QS
Service difficulty reports · 70
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 = 'N376QS' AND registry_match = 'registration' 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 = 'N376QS' AND registry_match = 'registration' 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 JGVR20180307001Door · corrodedMECHANICALLY BLENDED CORRODED AREA ON THE LOWER SIDE OF THE EMERGENCY EXIT DOOR. REMOVED CONTOUR RINGS AND FOUND ADDITIONAL CORROSION. BLENDED AREA FOUND UNDER CONTOUR RINGS AND FOUND ONE AREA CORRODED THROUGH. REPLACED THE EMERGENCY EXIT DOOR WITH A NEW ONE.SDR JGVR20180301002Bellmouth · corrodedBLENDED CORRODED APU EXHAUST DUCT BELL MOUTH, PERFORMED ULTRASONIC THICKNESS AND EDDY CURRENT CRACK INSPECTION AND REPORTED TO TEXTRON FOR DISPOSITION. REINSTALLED DUCT PER TEXTRON MEMO.SDR JGVR20180301001Deflector · corrodedBLENDED CORRODED APU COOLING DUCT INLET DEFLECTOR, PERFORMED ULTRA SONIC THICKNESS AND EDDY CURRENT CRACK INSPECTION AND REPORTED TO TEXTRON FOR DISPOSITION. TREATED, PRIMED AND PAINTED AND REINSTALLED PART PER TEXTRON MEMO.SDR 2017F00101Skin · corrodedUPPER TAILCONE SKIN CORRODED. REPAIRED.SDR DXTA201701230659Unknown · odorENROUTE AT FL430 AFTER 20 MINUTES OF FLIGHT TIME, BEGAN TO DETECT A WARM ELECTRICAL ODOR. TURNED OFF INTERIOR SWITCH AND ODOR APPEARED TO GO AWAY. NEVER SAW ANY VISUAL CLUES OF SMOKE OR HAZE. THERE WERE NO INCREASE OR ABNORMAL GENERATOR AMPS ETC. NEVER HADSDR DXTA2016060206245Circuit Breaker · trippedTHE CIRCUIT BREAKER LG CONT 2 POPPED AT TAKEOFF & GEAR UP. THE GEAR SPEED OF 210 WAS EXCEEDED BY 40K UNTIL WE DETERMINED THE GEAR NEVER RETRACTED. WE ACCOMPLISHED THE CHECKLIST BLOW DOWN PROCEDURE, INCLUDING THE MAIN GEAR & NOSE GEAR MANUAL UNLOCK RELEASE PRSDR DXTA2015070806040Data Unit · failedTEN SECS AFTER RT ENGINE START, LT ENGINE RUNNING, EICAS RT WINDSHIELD HEAT INOP AMBER MESSAGE ILLUMINATED FOLLOWED BY AN ELECTRICAL ODOR & LIGHT SMOKE IN COCKPIT. ENGINES & APU SHUTDOWN. POWERED ACFT, STBY SFD POWERS UP BOTH AIRSPEED & ALT TURNED RED & FAILSDR DXTA2014072905838Rib · crackedCORROSION AT TOP, FWD OF LT WW WHERE BRAKE LINES FEED THROUGH LWS 52 RIB. ACCOMPLISHED REPAIR DEFINITION NR S-680-0180 05RD, MAJOR REPAIR, REPAIR OF CORROSION ON LWS 52 RIB DATED JULY 22, 2014 & FAA FORM 8100-9 DATED 7/25/2014. WEIGHT & BALANCE WAS NOT AFFECSDR DXTA2013052005395Hydraulic System · unknownWHILE DROPPING THE LANDING GEAR, THE HYD VOLUME LOW CAS MESSAGE ILLUMINATED AND THE HYD VOLUME DROPPED TO ZERO. THE LANDING GEAR INDICATED THREE GREEN, CONDUCTED THE HYD VOLUME LOW CHECKLIST, AND LANDED WITHOUT INCIDENT.SDR CWQR02130204008Heat Exchanger · crackedDURING A SCHEDULED INSPECTION, REPLACED A DUCT ASSY OFF OF THE HEAT EXCHANGER WITH AN IMPROVED DUCT ASSY. AT DISASSEMBLY, DISCOVERED THAT RIGHT HEAT EXCHANGER HAD CRACKS FROM THE BOLT ATTACH POINTS. THE CRACKS WERE FROM .25 TO .75 IN LENGTH. IT APPEARS THE CSDR DXTA2011042504555Generator · inoperativeWHEN THROTTLES WERE ADVANCED FOR T/O THE LT WINDSHIELD INOPERATIVE CAS MESSAGE POSTED. TOWER REPORTED SEEING SMOKE COMING FROM THE REAR OF THE ACFT. VERIFIED A SMALL AMOUT OF SMOKE COMING FROM THE LT AC GENERATOR EXHAUST. INSPECTED LT ACFT GENERATOR AND FOSDR CWQR201104APump · leakingDURING UNSCHEDULED MX, THE RT ENGINE HYD PUMP WAS REPLACED DUE TO INTERNAL LEAKAGE.SDR CWQD201103Pump · leakingDURING UNSCHEDULED MX, THE LT ENGINE HYD PUMP WAS REPLACED DUE TO INTERNAL LEAKAGE.SDR DXTA2010121504364Strut · leakingON DEPARTURE RT MAIN GEAR DID NOT RETRACT. JACKED ACFT CHECKED RT MAIN WOW SWITCH OK. NOSE GEAR IAW CMC SHOWED ON GROUND. DETERMINED NOSE GEAR LEAKING INTERNALLY. DISASSEMBLED NOSE GEAR, FOUND METAL IN FLUID. INSTALLED AND SERVICED WITH N2. OPS CHECKED SASDR DXTA2010081804199Actuator · inoperativeROLL SYSTEM CONTROL FAULT AMBER CAS ILLUMINATED IN FLIGHT. ACCESSED THE ROLL RATIO CHANGER ACTUATOR. NOTED GOOD CONNECTIVITY. ACTUATOR & AREA CLEAN. CONNECTED PITOT/STATIC. PERFORMED THE RAIO CHANGER POSITION CHECK. AT 300 KNOTS DIMENSION OF MALMENT IS ISDR DXTA2010010403923Strut · dischargedWHEN GEAR HANDLE RAISED, RED UNLOCK ILLUMINATED, NOSE WHEEL DOWN AND LOCKED EXTINGUISHED, BOTH MAIN GEAR DOWN & LOCKED REMAINED ILLUMINATED AND AFTER 15 SECONDS GEAR RAISED NORMALLY. JACKED AIRPLANE, CONNECTED HYD GEAR HANDLE WOULD NOT ALLOW GEAR TO RETRACT ISDR DXTA2009121003890Wire · chafedAFTER T/O, FLAP INDICATOR SHOWED FLAPS AT 7 DEGREES. FLAP RESET WOULD NOT WORK. FLAPS VISUALY CHECKED UP IN FLIGHT. ON GROUND FLAPS WOULD NOT RESET OR TRAVEL UP/DOWN. EMERGENCY DECLARED. TROUBLESHOT TO A CHAFED TWISTED SHIELDED PAIR OF CONDUCTORS. REPAIRESDR 2009FA0000441Warning Light · illuminatedON CLIMB OUT IN ICING AT 35,000 FT " SUPPLY BLEED LEAK- R " CAS MESSAGE ILLUMINATED COMPLETED CHECKLIST L-10 IAW ABNORMAL PROCEDURES AND LIGHT WENT OUT AFTER STEP NR 2 ON DESCENT WITH ALL ANTI-ICING ON FROM FL 350 TO 10,000 FT. NO REOCCURENCE OF CAS MESSAGE. SDR DXTA2009012603475Strut · dischargedFOUND NOSE STRUT NOT FULLY EXTEND WITH ACFT ON JACKS. FOUND NO AIR IN LWR NOSE STRUT CHAMBER. FOUND CAUSE TO BE 2 O-RINGS INSTALLED ON LWR CHAMBER SHREADER VALVE. SERVICED NOSE STRUT WITH FLUID AND IAR. REPLACED O-RING ON LWR SHREADER VALVE WITH SINGLE O-RSDR DXTA2009012703475Landing Gear · malfunctionedAFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. WOW MISCOMPARE CAS MSG CAME ON.
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