N610QS
Service difficulty reports not matched to an aircraft · 16
They name N610QS, 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 = 'N610QS' 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 = 'N610QS' 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 JGVR20170614005Door Frame · damagedCABIN DOOR LOWER PINS HAVE CONTACTED MAIN ENTRY DOOR FRAME PREVIOUSLY AND CAUSED DAMAGE TO FRAME. FOUND WHILE PERFORMING DOOR SEALS GENERAL VISUAL INSPECTION 52-90-10-210. REPAIRED THE DOOR FRAMES IAW REPAIR DEFINITION AND 8100-9.SDR JGVR20170613001Fastener · pulledRIGHT OUTBOARD FLAP OUTBOARD ISLAND LOWER WING TRAILING EDGE SKIN HAS NINE SMOKING RIVETS, FIVE PULLING THROUGH. REPAIRED IAW REPAIR DEFINITION.SDR CWQR20150119003Frame · crackedDURING A SCHEDULED INSPECTION WE FOUND A HYD LINE STAND OFF BRACKET BROKEN & THE LINE CHAFING THE STRUCTURE. UPON FURTHER INSPECTION WE FOUND THE HYD LINE STAND OFF BRACKET ATTACH RIVET HOLES IN THE FRAME WERE CRACKED. TWO CRACKS WERE MEASURED AT 1.65 & .65 ISDR DXTA2014031405687Unknown · odorAFTER TAKEOFF, EXPERIENCED A VERY STRONG PUNGENT ODOR IN THE COCKPIT. AFTER LEVELING AT 9000 FT, REDUCED POWER & ODOR INCREASED. DID NOT SWITCH PRESSURE SOURCE DUE TO RETURN TO BASE. AFTER LANDING, ODOR WAS PRESENT THROUGHOUT CABIN. NO SMOKE WAS DETECTEDSDR DXTA2013120905594Door · out of adjustAFTER TAKEOFF & GEAR SELECTED UP, ALL THREE GEAR LIGHTS EXTINGUISHED BUT RED, GEAR UNLOCKED, LIGHT REMAINED ILLUMINATED. THE STAB MISS COMPARE & HYD PRESS LIGHTS ILLUMINATED AS EXPECTED. AFTER PULLING THE HYD CONTROL CB IAW HYDRAULIC PRESS CHECKLIST, THE RT SDR DXTA2009050403629Warning Light · illuminatedWHEN TAKEOFF POWER WAS APPLIED, RT WING OVERHEAT LIGHT ILLUMINATED. PERFORMED GROUND RUN AT TAKOFF POWER WITH ANTI-ICE WING/ENG IN OFF POSITION. DID NOT GET R WING OVHT ANNUNCIATOR. REMOVED RH INBOARD CUFF UPPER PANEL. NO DEFECTS FOUND INSIDE OF AREA. RAN ENGSDR DXTA200807253198Acm · seizedSMOKE IN CABIN, AFTER LANDING AIR SUPPLY TEMP ROSE FROM 81 DEGREES TO 155 DEGREES IN LESS THAN ONE MINUTE. SMOKE MAY HAVE BEEN COMING FROM AIR CONDITIONING VENTS. 30 MINUTES AFTER SHUTDOWN ACM TEMP WAS 155 DEGREES. TROUBLESHOT SYS, FOUND ACM SEIZED UP. REMOVSDR DXTA200803198Unknown · smokeSMOKE IN CABIN. KMDW-KMKG. (A)SDR CWQR200620Control Cable · frayedDURING A PHASE B-INSPECTION, OPERATOR REQUESTED WE INSPECT THE AFT ELEVATOR TRIM CABLES. UPON INSPECTION WE FOUND BROKEN WIRES, TOOK CABLE TENSIONS, FOUND TO BE WITHIN LIMITS AND CABLE WAS CENTERED IN PULLEY.THE CABLE WAS REMOVED AND LOOP TEST SHOWED MORE BROKSDR DXTA200601441Actuator · failedLEFT MAIN GEAR WOULD NOT LOCK DOWN. CYCLED THE GEAR, AND STILL NO GREEN LIGHT ON THE LEFT MAIN. -HYD PRESS- LIGHT STARTED FLASHING, AND THE GEAR EVENTUALLY LOCKED DOWN AFTER APPROX 2-3 MINUTES. REMOVED AND REPLACED LT MAIN GEAR ACTUATOR AND OPS CHECKED GOODSDR DXTA200501151Line · unknownAFTER TAKEOFF GEAR WAS SELECTED UP, RED UNLOCK LIGHT REMAINED ON AND HYD PRESS. ANNUNCIATOR WOULD NOT EXTINGUISH. SERVICED HYDRAULIC RESERVOIR TO FULL, JACKED AIRCRAFT TO SWING GEAR. CLEANED INDICATING SWITCH ON THE NOSE GEAR, CHECKED THE WIRING AND CANNONSDR DXTA200500821Pump · malfunctionedANTI-SKID AND POWER BRAKE FAILURE. PUMP RUNNING CONTINUOUSLY (BOTH LIGHTS ON). REMOVED BRAKE PUMP AND INSTALLED NEW PUMP. OPERATIONAL CHECKS GOOD. LEAK CHECK GOOD. WORK PERFORMED IAW CH 32-42-06 OF CESSNA 560XL MM.SDR DXTA200300169Bowl · crackedLOW BRAKE PRESSURE AND ANTISKID INOPERATIVE LIGHTS ILLUMINATED, FOLLOWED BY BRAKE FAILURE. USED EMERGENCY BRAKE TO STOP AIRCRAFT. TROUBLESHOT CRACKED ANTI-SKIP PUMP FILTER BOW, CHANGED FILTER BOWL, O RING ALONG WITH FILTER, ALSO AS PRECAUTION REPLACED PUMSDR DXTA200300153O-Ring · failedDURING TAXI "LO BRAKE PRESS" AND "ANTISKID INOP" ILLUMINATED. LOST BRAKE PEDAL PRESSURE, STOPPPED AIRCRAFT WITH EMERGENCY BRAKES. HAD AIRCRAFT TOWED TO PARKING POSITION, POST FLIGHT INSPECTION FOUND LEAKING OIL FROM AVIONICS BAY AND NOSE GEAR ASSEMBLY. - FOUNDSDR DXTA200300078Line · leakingDURING POST FLIGHT INSPECTION FOUND HYDRAULIC FLUID LEAKING OUT OF RIGHT WHEEL WELL. INSPECTED RIGHT WHEEL WELL AND FOUND FLUID LEAKING OUT FROM SPEED BRAKE RETRACT LINE. FURTHER INSPECTION FOUND SPEED BRAKE EXTEND LINE, FLAP EXTEND AND RETRACT LINES CHAFED SDR DXTA200300018Motor · lack of lubeCLIMBING THROUGH 35,000 FT YOKE JERKED ABRUPTLY, AUTOPILOT WAS DISCONNECTED AND AIRCRAFT NEED NOSE DOWN TRIM. FIFTEEN SECONDS LATER WITH AUTOPILOT OFF SECOND JERK OCCURRED IN YOKE.
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