N302QS
Service difficulty reports not matched to an aircraft · 20
They name N302QS, 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 = 'N302QS' 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 = 'N302QS' 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 DXTA2010061704124Seal · failedAT FLT LEVEL 390, A SUDDEN, EXTREMELY LOUD SQUEALING NOISE FILLED CABIN, NO SECONDARY INDICATIONS OF A PRESSURE ISSUE AT THE TIME. STARTED A RAPID DESCENT AS A PRECAUTION, NOISE DID NOT DISSIPATE UNTIL BELOW 6000 FT WHEN CABIN & AIR PRESSURE EQUALIZED. COMPLESDR DXTA2010022504003Unknown · odorNOTED FAINT ELECT/ BURNED INSULATION TYPE ODOR IN FLIGHT. NO SMOKE. COULD NOT IDENTIFY THE SOURCE. PRECAUTIONARY LANDING MADE. INSPECTED ACFT AND PERFORMED NUMEROUS ENG RUNS LETTING THE HEAT BLOW FULL HOT EACH TIME. COULD NOT DUPLICATE ANY ODOR OR BURNED SMESDR DXTA200811123352Flow Divider · misriggedRT ENGINE QUIT ON LANDING ROLL OUT. ENGINE QUIT WHEN RT THROTTLE WAS BROUGHT TO IDLE. RT THROTTLE SEEMS TO HAVE AN EXCESSIVE AMOUNT OF SLOP WHEN BROUGHT BACK TO IDLE THRUST. VERIFIED DISCREPANCY, FOUND RT ENGINE CONTROLS AT FCU AND FUEL FLOW DIVIDER IMPROPERSDR DXTA2008111303352Engine · malfunctionedRIGHT ENGINE QUIT ON LANDING ROLL OUT.SDR DXTA200811113349Engine · unknownRT ENGINE QUIT ON LANDING APPROACH ABOUT 100 AGL THROTTLES IDLE. REMOVED LT/RT ENG LWR COWLS FOR ACCESS. RE-RIGGED RT FDV TO FUEL CONTROL RD. ADJUSTED RT THROTTLE CABLE. INSPECTED LT FDV TO FUEL CONTROL RIGGING AND THROTTLE RIGGING AT FCU NO DEFECTS NOTED. RASDR DXTA2008111203349Engine · shutdownRIGHT ENGINE QUIT ON LANDING APPROACH ABOUT 100 AGL THROTTLES AT IDLE.SDR DXTA200809283290Retainer · missingRT SEAT BRAKES NOT OPERATING PROPERLY. DURING TAXI, YOU MUST GO VERY FAR ON THE BRAKES TO GET ANY RESISTANCE. NORMAL BRAKING ON LT SEAT SIDE. NO FLUID NOTED UNDER PEDALS OR WHEELS. VERIFIED DISCREPANCY TROUBLESHOT AND FOUND RT RUDDER TORQUE TUBE SUPPORT ASSDR DXTA200803257Brake Sys · contaminatedCOPILOT RT BRAKE PEDAL IS LESS EFFECTIVE THEN THE LT PEDAL. MORE TRAVEL IS NEEDED TO PRODUCE BRAKE PRESSURE. PERFORMED VISUAL INSP, CHECKING BRAKE LINES IN COCKPIT, CHECKED MASTER CYLINDER FLEXIBLES AND BRAKE ASSY FOR CONTAMINATION OR POSSIBLE FLUID LEAK IAW SDR DXTA200803202Starter Gen · malfunctionedSTARTER DISENGAGE PROBLEM - ABORTED LT ENG START WHEN N2 AT 25% AND NO N1. ENG APPEARED TO SHUTDOWN NORMALLY. F/O CHECKED, ENG WAS STILL RUNNING AND SMOKE WAS COMING OUT OF GENERATOR EXHAUST VENT, SHUT THE ENG DOWN USING THE ENG FIRE SWITCH, ABOUT 20 SECONDSSDR DXTA200803103Brake Sys · weakCAPTAIN AND COPILOT RIGHT BRAKE PEDALS ARE LESS EFFECTIVE THEN THE LEFT PEDAL, MORE TRAVEL IS NEEDED TO PRODUCE BRAKE PRESSURE. ACCOMPLISHED TASK CARD TC-560-32-080602. BLED BRAKES IAW ENGINEERING MEMO M344-08-10. TAXI CHECK GOOD.
SDR DXTA200803064Brake Sys · malfunctionedON TAXI OUT BOTH PILOT AND CO-PILOT BRAKES WERE VERY HARD DURING APPLICATION, WHEN BRAKES WERE APPLIED (CO-PILOT OR PILOT), AIRCRAFT WOULD NOT SLOW UNTIL A GREAT DEAL OF PRESSURE WAS APPLIED. SUSPECTED AIR IN SYSTEM, BLED LEFT & RIGHT BRAKES SEVERAL TIMES & PSDR DXTA200803003Flow Divider · out of adjustDURING SPEED BRAKE TEST, LT ENGINE SHUTDOWN AND RT ENGINE SHUTDOWN. ADJUSTED TENSION ON BALL PLUNGER ON THE FUEL FLOW DIVIDER, PERFORMED OPS CHECK WITH NO DEFECTS NOTED REF ENGINE MM 71-01-03SDR DXTA200702581Squat Switch · reads highLOST CABIN PRESSURIZATION AT FL290. CABIN PRESSURE ROSE TO 13500 PA AND STABILIZED. ON DESCENT, CABIIN PRESSURE DESCENDED WITH THE AIRCRAFT ALTITUDE. FOUND LT SQUAT SWITCH TO HAVE HIGH RESISTANCE AND CHANGING WITH PRESSURE ON ARM. REPLACED SWITCH WITH NEW IASDR DXTA200500944Brake · failedON TAXI OUT DURING BRAKE CHECK CAPTAINS LEFT BRAKE WENT ALL THE WAY TO THE FLOOR. UPON ACTIVATION OF THE CO-PILOTS LEFT BRAKE, BOTH BECAME SPONGY. RESET BRAKE SHUTTLE VALVES, BLED BRAKE SYSTEM. PERFORMED SEVERAL BRAKE CHECKS STILL AND WHILE TAXIING WITH POWSDR DXTA200500774Engine · malfunctionedABORTED TAKEOFF, RIGHT ENGINE WOULD NOT MAKE TAKEOFF POWER (97.2) ONLY ACHIEVED 95.3 PERCENT. RAN RIGHT ENGINE TO TAKEOFF POWER [97.2], ALL PARAMETERS WERE WITHIN ACCEPTABLE LIMITS IAW CE 560 MM 71-01-02.SDR DXTA200400275Relay · failed400 FT ABOVE TOUCHDOWN THE POWER BRAKE LOW PRESSURE AND ANTI-SKID INOP ANNUNCIATOR LIGHTS INOP LIGHTS ILLUMINATED AND THE ANTI-SKID CB POPPED, AND BRAKES BECME INEFFECTIVE - TESTED ANTI-SKID SYSTEM, BREAKER WOULD NOT TRIP, METERED ALL ANTI-SKID WIRES, FOUND NOSDR DXTA200400273Connector · contaminated400 FEET ABOVE TOUCHDOWN THE POWER BRAKE LOW PRESSURE AND ANTI-SKID INOP ANNUNCIATOR LIGHTS INOP LIGHTS ILLUMINATED AND THE ANTI-SKID CB POPPED. - BLED AIRCRAFT BRAKE SYSTEM IAW CESSNA 560 MM CHAPTER 32-42-00. SERVICED EMERGENCY BRAKE BOTTLE IAW CESSNA 560 MMSDR DXTA200400268Circuit Breaker · trippedAPPROX 100 FT ABOVE TOUCHDOWN THE "POWER BRAKE LOW PRESS." AND "ANTISKID INOP." ANNUNCIATOR LIGHTS ILLUMINATED AND THE ANTI SKID CIRCUIT BREAKER POPPED. LANDING WAS UNEVENTFUL, USED BACKUP PNEUMATIC SYSTEM TO STOP AIRCRAFT. - RE-SET CIRCUIT BREAKER WITH NO SUBSDR DXTA200400261Warning Light · illuminatedON APPROACH POWER BRAKE LOW PRESS AND ANTI-SKID INOP, ANNUNCIATORS ILLUMINATED. EMERGENCY CHECKLIST PROCEDURE WAS COMPLIED WITH AND ANNUNCIATOR REMAINED ILLUMINATED. LANDING WAS MADE AND BRAKING ACCOMPLISHED USING BACK UP PNEUMATIC SYSTEM. ITEM IS UNDER INVSDR DXTA200300062Wire · brokenLEFT THRUST REVERSER UNLOCK LIGHT CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF. BLED BRAKE SYSTEM, TROUBLESHOT TO BROKEN WIRES ON THE ANTI-SKID TRANSDUCER. REPAIRED WIRING, PERFORMED OPERATIONAL CHECK AND TAXI CHECK OF THE BRAKE SYSTEM, CHECKED GOOD. ALL W
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