N630QS
Service difficulty reports not matched to an aircraft · 26
They name N630QS, 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 = 'N630QS' 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 = 'N630QS' 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 DXTA2014121605949Motor · failedMAIN BRAKE SYS FAILED WITH LOW BRAKE PRESSURE & ANTI-SKID INOPERATIVE LIGHTS ON LANDING. POWERED ACFT UP, AND RAN THE BRAKE SYSTEM SEVERAL TIMES AND COULD NOT FIND ANY DISCREPANCIES. INSPECTED THE WIRING FROM THE MOTOR, PRESSURE SWITCHES, AND THE RELAY COULDSDR EBVR20140923002Fitting · crackedFOUND 2 HORIZONTAL STAB PIVOT FITTING ASSEMBLY CRACKED PN 6631102-15 DURING OUR INSPECTION. MECHANICS NEED TO PAY CLOSE ATTENTION TO THIS AREA WHILE DOING INSPECTIONS ON THE HORIZONTAL & VERTICAL TAIL AREA.SDR 2014FA0000483Fitting · crackedFOUND A CRACKED HORIZONTAL STAB PIVOT BOLT FITTING ASSY. WHICH WAS POSSIBLY CAUSED BY IMPROPER INSTALLATION OF THE LOWER SUPPORT CLIP. UPON REMOVING THE LOWER SUPPORT TEE CLIP WE NOTICED THE HOLES WERE ELONGATED A LITTLE SO WE REQUESTED FROM MFG STRUCTURES ENSDR DXTA2014033005702Wire · chafedDURING ROUTINE COCKPIT INSPECTION WITH MAIN BATTERY ON, AILERON TRIM BOUND DURING CHECK, AUTOPILOT SERVO CIRCUIT BREAKER TRIPPED & SMOKE WAS DETECTED. TRIM KNOB WAS ROLLED TO RT THEN BOUND & STUCK 2/3 OF THE WAY. TRIM KNOB WAS THEN ROLLED LT PAST NEUTRAL, BOSDR DXTA2012060504989Tire · failedRT MAIN TIRE TREAD SEPARATED FROM TIRE ON LANDING ROLLOUT. R & R RT MLG WHEEL & TIRE ASSY IAW MM 32-41-02.SDR DXTA2012021004867Control Handle · malfunctionedGEAR WOULD NOT RETRACK WHEN GEAR HANDLE WAS PULLED UP, HAD ALL 3 GREEN INDICATORS, GROUND CONFIRMED GEAR WERE WAS DOWN AND EMERGENCY WAS NOT DECLARED. HANDLE WAS PLACED DOWN TO MATCH CONDITION. PERFORMED GEAR SWING SEVERAL TIMES. DUPLICATED SQK ONCE MOVINGSDR DXTA2011111404784Trim System · frozenELEVATOR TRIM STUCK. FROZE UP INFLIGHT. IT WOULD NOT OPERATE ELECTRICALLY OR MANUALLY. IT COULD NOT BE MOVED ANY AT ALL MANUALLY. IT CREATED POSITIVE FORWARD FORCE ON THE CONTROLLS INFLIGHT. ONCE ON THE GROUND IT STARTED TO WORK AGAIN. PERFORMED ELEVATORSDR CWQR2001101824Angle · crackedDURING A SCHEDULED MX CHECK, ANGLE WAS FOUND CRACKED THROUGH THE FREE FLOATING LEG INTO THE ANGLE RADIUS, THIS CRACK WAS 4.2 INCHES FROM THE END OF THE PART. THE ANGLE WAS REPLACED WITH A NEW PART.SDR DXTA2011080104675Ahrs · malfunctionedLEFT PFD: "HEADING FAILURE - SINGLE" AT ALTITUDE. R & R LT AHRS COMPUTER. OPS CHECKED GOOD. WORK DONE IAW MM 34-21-01.SDR DXTA2010062504131Wire Harness · faultyLEFT ENGINE ITT SPIKED TO 800° IN FLIGHT. TRIED TO CONTROL TEMP WITH THROTTLE, BUT WHEN WE DESCENDED TO 5000', ITT EXCEEDED 760°. SHUTDOWN ENGINE, BUT ITT NEVER DROPPED BELOW 500° - EVEN WHEN ON GROUND. FOUND T1 SENSOR HARNESS OUT OF LIMITS AND ERRATIC. INSTSDR DXTA2010052504101Bulb · inoperativeAFTER LANDING GEAR EXTENSION, GREEN NLG LIGHTS FAILED TO ILLUMINATE. COMPLIED WITH THE LANDING GEAR WILL NOT EXTEND CHECKLIST. LANDING WAS NORMAL. AFTER LANDING, BULBS DID NOT ILLUMINATE ON ROTARY TEST. R & R BOTH NLG DOWN & LOCK LIGHT BULBS. JACKED ACFT, CYCSDR DXTA2010050304084Eec · malfunctionedCLIMBING THROUGH FL280 HAD PARTIAL LOSS OF POWER ON THE RT ENGINE, POWER LEVERS IN CLIMB. MAX POWER WAS 64.5 % WITH FUEL FLOW OF 360. LT ENG APPROX 85 % & FUEL FLOW AROUND 800. DESCENDING THROUGH FL250 ENG POWER RETURNED TO NORMAL. R & R RT ENG EEC IAW MM 7SDR DXTA2009101903815Bleed Valve · inoperativeRT ENGINE FAILED TO ATTAIN T/O N1 POWER. AFTER MULIPLE ATTEMTS AND AN A/C "RESET" THE BEST N1 ATTITUDE WAS 68%, N1 WITH 100% N2 INDICATED. ON FINAL ATTEMT A COMPRESSOR STALL OCCURRED. REPLACED COMPRESSOR BLEED VALVE. SERVO VALVE/TORQUE MOTOR. INSTALLED SECONDSDR DXTA2009031603550Acm · smokeWHEN APU BLEED AIR IS SELECTED CABIN AND COCKPIT AREA BEGINS TO FILL WITH BLUE SMOKE. REMOVED ACM DUCTING & SEALS, R&R ACM. BEGAN INSTALLATION OF OVERHAULED ACM COMPLETED INSTALLED DUCTING, AND NEW SEALS. TORQUED AND/OR SAFETIED CLAMPS. INSTALLED APU ACCESSSDR DXTA2009030503529Oil System · leakingBORESCOPED EXHAUST AND INLET OF APU. FOUND OIL IN INLET. REMOVED AND REPLACED APU AND ECU IAW MM CH 49-10-00 LEAK AND FUNCTIONAL CHECKED GOOD.SDR DXTA2009030603529Ecu · leakingAFTER TURNING ON APU BLEED AIR, EXCESSIVE FUMES AND ODOR ENTERED THE CABIN. REMOVED AND REPLACED APU AND ECU IAW MM CH 49-10-00 LEAK AND FUNCTIONAL CHECKED GOOD.SDR DXTA2008122403434Elevator System · stiffELEVATOR CONTROL FEELS STIFF.SDR DXTA2008122303434Control Cable · looseDURING CLIMB THROUGH 12,000 FT AT 200 KIAS, AUTO PILOT OFF, ELEVATOR CONTROL FELT STIFF FROM LT SEAT. AN ABNORMAL BUMP COULD BE FELT WHEN MOVING YOKE FORE AND AFT. ADDITIONALLY, A GRINDING SENSATION OR VIBRATION COULD BE FELT THROUGH THE FLOOR. ALL 3 SYMPTOSDR DXTA200811143357Actuator · inoperativeGEAR UNLOCK HYD PRESS AND STAB MISCOMPARE LTS ALL REMAINED ILLUMINATED AFTER GEAR AND FLAP RETRACTION. ALL LIGHTS REMAINED ILLUMINATED UNTIL GEAR / FLAPS WERE PUT BACK DOWN. REMOVED AND REPLACED LT MLG ACTUATOR WITH RENTAL UNIT IAW CUSTOMER REQUEST. WORK DONE SDR DXTA2008111703357Warning System · activatedGEAR UNLOCK HYD PRESS REMAINED ILLUMINATED AFTER GEAR AND FLAP RETRACTION.SDR DXTA2008102903326Relief Valve · faultedGEAR "UNLOCK" LIGHT, "HYD PRES" LIGHT, AND "STAB MISCOMPARE" LIGHT ALL ILLUMINATED AFTER TAKEOFF. THEY REMAINED ILLUMINATED WHILE RUNNING THE CHECKLIST AND DID NOT EXTINGUISH UNTIL THE GEAR WAS EXTENDED. REPEAT WRITEUP. REMOVED FAULTY HYD RELIEF VALVE. INSTALSDR DXTA200702558Brake Assy · malfunctionedTHE TOE BRAKES ON RT PEDAL GOES TO THE FLOOR. PERFORMED BRAKE BLEED IAW AMM 32-42-01. OPS CHECK GOOD.SDR DXTA200601772Duct · separatedWHILE ACCELERATING IN CRUISE FLIGHT FL280 HEARD A THUMP SOUND ACCOMPANIED BY AN INCREASED SLIP STREAM NOISE AND A SLIGHT VIBRATION ON THE CONTROL YOKE. DECREASED AIR SPEED AND VIBRATION LESSENED. PERFORMED VISUAL INSPECTION OF EXTERIOR OF AIRCRAFT TO INCLUDESDR DXTA200500951Acm · seizedAPU RUNNING ON THE GROUND WITH BLEED AIR ON. SMOKE IN CABIN AND COCKPIT SHUTDOWN BLEED AIR AND APU REMOVED BATTERY POWER FROM AIRCRAFT. ACM WAS FOUND SEIZED UP, INSTALLED REPAIRED ACM PACK IAW 560XL M/M 21-51-00.SDR DXTA200300189Control Cable · chafedPERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03.SDR DXTA200300044Relay · inoperativeLOST BRAKES ON LANDING ROLLOUT. USED EMERGENCY BRAKES TO STOP ACFT. POWER BRAKES AND ANTI SKID ANNUNCIATORS DID COME ON WHEN ACFT LOST BRAKES. POST FLIGHT REVEALED A PUDDLE OF FLUID ON THE GROUND AND ON THE NOSE GEAR, UNDER THE NOSE OF THE ACFT. TROUBLESHO
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