N651QS
Service difficulty reports not matched to an aircraft · 29
They name N651QS, 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 = 'N651QS' 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 = 'N651QS' 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 JGVR201812200006Rib · crackedCRACKED RIB IN LH FLAP WELL NEAR OB FLAP, OB BELL CRANK. RIB P/N 6565042-32-1SDR JGVR20181220005Rib · crackedCRACKED RIB IN THE RH FLAP WELL NEAR THE OB FLAP, OB BELL CRANK. FOUND DURING THE B INSPECTION, AFT WING SPAR GVI, TASK 57-10-00-210.SDR JGVR20181220004Skin · corrodedAPPROXIMATELY 13 AREAS OF SUSPECTED LEVEL 1 CORROSION ON RH ELEVATOR UPPER AND LOWER SKINS. FOUND DURING TASK B273005-RH ON THE B INSPECTION. REPAIRED CORRODED AREA ON TRAILING EDGE OF R/H ELEVATOR P/N 6634200-6 S/N 5165SDR JGVR20180201001Closeout Panel · corrodedAPU CLOSEOUT PANEL IS SEVERELY CORRODED ON THE INSIDE, AROUND THE OIL SERVICE DOOR LATCHES, AND AROUND THE CAMLOCKS. REMOVED CORRODED APU ACCESS DOOR ASSY. AND INSTALLED NEW APU ACCESS DOOR ASSY IAW MM 52-40-02.SDR JGVR20180131003Skin · corrodedBLENDED TWO AREAS OF CORROSION ON THE EXTERIOR FUSELAGE SKIN FWD OF THE CABIN DOOR AT BS 187, PERFORMED EDDY CURRENT CRACK AND ULTRASONIC THICKNESS INSPECTIONS, PREPPED AND TREATED IAW SRM 51-10-03, MM 51-10-00, AND 51-70-08.SDR JGVR20180131002Skin · corrodedBLENDED 10 AREAS OF CORROSION ON THE LT UPPER WING SKIN, PERFORMED EDDY CURRENT CRACK AND ULTRASONIC THICKNESS INSPECTION, PREPPED AND TREATED AREAS IAW SRM 51-10-03, AND MM 51-10-00.SDR JGVR20180131001Skin · corrodedCORROSION ON THE RT UPPER WING SKIN, BLENDED AND PERFORMED AN EDDY CURRENT AND ULTRASONIC THICKNESS INSPECTIONS, PREPPED AND TREATED AREAS IAW SRM 51-10-03, 51-70-08, AND MM 51-10-00.SDR CWQR20160720024Cable · unserviceableTHIS CABLE ASSEMBLY IS REPLACED AT THE AIRCRAFT OPERATOR REQUEST BECAUSE OF RELIABILITY ISSUES. INSPECTED CABLE AFTER REMOVAL, PREFORMED LOOP TEST AND FOUND TO BE UNSERVICEABLE PER AMM CHAPTER 20-10-04. NEW CABLE ASSEMBLY INSTALLED.SDR CWQR20160720023Cable · brokenTHIS CABLE ASSEMBLY IS REPLACED AT THE AIRCRAFT OPERATOR REQUEST BECAUSE OF RELIABILITY ISSUES. INSPECTED CABLE AFTER REMOVAL, PREFORMED LOOP TEST AND FOUND TO BE UNSERVICEABLE PER AMM CHAPTER 20-10-04. NEW CABLE ASSEMBLY INSTALLED.SDR CWQR20060622019Hinge Bracket · crackedDURING A SCHEDULED INSPECTION, WE FOUND THE LT OTBD ELEVATOR HINGE BRACKET CRACKED. THE BRACKET IS A CASTING AND IS CRACKED IN THE RADIUS WHERE IT ATTACHES TO THE HORIZONTAL STABILIZER. THE RADIUS CRACK IS .20" LONG WAS FOUND VISUALLY AND CONFIRMED WITH EDDYSDR DXTA2014121905950Trim System · frozenTRIED ELECTRICAL & MANUAL TRIM, FOUND TO BE FROZEN. THE ELEVATOR WAS SHAKING. BOTH HAD TO PUSH FULL FWD ON THE YOKE TO ARREST THE CLIMB. IT FELT AS IF THE ELEVATOR WAS ALSO FROZEN. DECLARED AN EMERGENCY & REDUCED THROTTLES AS MUCH AS POSSIBLE TO DESCEND. SDR DXTA2014062605808Cylinder · leakingRIGHT BRAKE MAKES A LOUD SQUEAL DURING APPLICATION. EVEN APPLICATION OF BRAKE PEDALS RESULTS IN UNEVEN BRAKING. TAXIED AIRCRAFT AND DID NOT HEAR ANY SQUEAL FROM RIGHT OR LEFT BRAKES. JACKED AIRCRAFT AND REMOVED LEFT AND RIGHT WHEEL ASSEMBLIES, SET BRAKES ANDSDR DXTA2013103005552Display · failedON ARRIVAL, CREW NOTICED AN ELECTRICAL BURNING ODOR, FOLLOWED QUICKLY BY THE MFD GOING BLANK. PULLED THE MFD CIRCUIT BREAKER AND FLT CONTINUED UNEVENTFULLY. ALL OTHER AVIONICS OPERATED NORMALLY. REMOVED INOPERATIVE MFD AND INSTALLED A REPAIRED UNIT IAW AMM SDR DXTA2013101105536Circuit Breaker · trippedAFTER TAKEOFF, LANDING GEAR FAILED TO RETRACT. THREE GREEN LANDING GEAR LIGHTS ALONG WITH THE RED UNLOCK LIGHT. PUT THE GEAR HANDLE BACK DOWN AND HAD THREE GREEN AND NO RED. NOTICED AFTER LEVELING OFF THE GEAR CONTROL CIRCUIT BREAKER OUT. LEFT IT OUT AND MSDR DXTA2013010405230Unknown · smokeWITH THE APU ON, BLEED AIR OFF, DURING NR 2 ENGINE START, WHICH WAS FIRST TO BE STARTED, SMOKE STARTED TO COME INTO COCKPIT, PARTICULARLY THRU THE RT SIDE EYEBALL VENT BUT ALSO THRU BOTH WEMACS. IT CONTINUED DURING THE 2ND ENGINE START. SHUTDOWN BOTH APU AND SDR DXTA2012120405200Water Separator · odorWITH THE APU ON, BLEED AIR OFF, DURING THE NUMBER 2 ENGINE START (WHICH WAS FIRST TO BE STARTED) SMOKE STARTED TO COME INTO COCKPIT.PARTICULARLY THRU THE RT SIDE EYEBALL VENT BUT ALSO THRU BOTH WEMACS. IT CONTINUED DURING THE 2ND ENGINE START. WE SHUTDOWN BOTHSDR DXTA2012013004857Control Handle · intermittentDURING GEAR RETRACTION AFTER TAKEOFF, THE RED GEAR UNLOCK LIGHT REMAINED ON. SOUNDED LIKE THE GEAR RETRACTED NORMALLY. NO ABNORMAL NOISES OR VIBRATIONS WERE NOTED. RAN THE STAB MISCOMPARE AND HYD PRESSURE ANNUNCIATOR CHECKLISTS. THAT DID NOT FIX PROBLEM. SDR DXTA200810143306`Computer · inoperativeLOST PFD ON CAPTAINS SIDE AND MFD ON TAKEOFF (70KT) ROLL. BOTH HAD RED X DISPLAYED ON THEM. STAYED ON WITH RED X UNTIL BACK IN THE CHOCKS AND FOR A FEW MINUTES AFTER THAT. REMOVED AND REPLACED CAPT'S IAC COMPUTER IAW MM CH 34-25-02. GROUND CHECKED GOOD.SDR DXTA2008101503306Display · failedLOST PFD ON CAPTAINS SIDE AND MFD ON TAKEOFF (70KT) ROLL.SDR DXTA200802867Pressure Switch · malfunctionedCAB ALT 10, 000 CAME ON AT 10,500 FEET WITH MASTER WARNING. REMOVED CABIN ALTITUDE PRESSURE SWITCH. REPLACED WITH NEW SWITCH. OPERATIONAL CHECK GOOD. WORK IAW MM 21-30-00.SDR DXTA200702540Landing Gear · malfunctionedLT LANDING GEAR INDICATOR LIGHT REMAINED ON WHEN GEAR RETRACTED. CYCLED GEAR WITH THE SAME RESULT AND UNABLE TO VERIFY GEAR UP OR DOWN. PERFORMED EMERGENCY GEAR BLOW DOWN PROCEDURE AS PRECAUTION.SDR DXTA200702066Hook · stickingGEAR UNLOCK LIGHT REMAINED ILLUMIATED AND HYDRALIC PRESSURE LIGHT REMAINED ON, RAN CHECKLIST AND LIGHTS EXTINGUISH WHEN HYDRAULIC CONTROL CIRCIUT BRAKER RESET IAW CHECKLIST. REMOVED AND REPLACED NOSE GEAR UPLOCK SWITCH WITH NEW. NOSE GEAR UPLOCK HOOK WAS STICSDR DXTA200701943Control Module · inoperativeRT WINDSCREEN FAULT ANNUNCIATOR ILLUMINATED, WHILE COMPLETING CHECKLIST, THE RIGHT WINDSHIELD SHATTERED. REMOVED CRACKED RT WINDSHIELD INSTALLED NEW WINDSHIELD. INSTALLED REPAIRED WINDSHIELD CONTROL RT PN ON 856-1-1 SN ON 205080073 RT WINDSHIELD TEMP CONTROLSDR 2006FA0001002Downlock Switch · failedAFTER TAKEOFF AND GEAR RETRACTION ALL GEAR LIGHTS WENT OUT. APPROX 5-10 INTO FLIGHT, NOTICED RT GREEN GEAR LIGHT WAS ON. NO OTHER ABNORMAL LIGHTS NOTED. 40 MINUTES LATER LIGHT EXTINGUISHED. TROUBLESHOT SYS BY RIGING ALL DOWN LOCK SWITCH WIRING AND SWITCH MSDR DXTA200601593Actuator · failedAFTER TAKEOFF AND GEAR RETRACTION, ALL THREE GEAR LIGHTS EXTINGUISHED. APPROX 5-10 MINUTES INTO FLIGHT, NOTICED THAT THE "RT" GREEN GEAR LIGHT WAS ILLUMINATED. NO OTHER ABNORMAL LIGHTS OR INDICATIONS NOTED. 40 MINUTES LATER LIGHT EXTINGUISHED. REPLACED RT SDR CWQR2006008Retainer · looseFOUND THE STATIC SYSTEM DRAIN VALVE POPPET RETAINING RING COMING LOOSE FROM VALVE BASE.SDR DXTA200500761Line · leakingBRAKE SYSTEM FAILURE ON GROUND. AIRCRAFT PUMPED BRAKE LINE FLUID OUT OF NOSE COMPARTMENT ON TO GROUND AROUND NOSE WHEEL. ASSOCIATED AMBER ANNUNCIATORS + M/C (LOW BRAKE PRESS, ANTI-SKID FAIL). ITEM IS UNDER INVESTIGATION.SDR DXTA200500739Apu · overservicedAFTER TAKEOFF, HAD A SMOKE SELL FROM AN UNIDENTIFIABLE SOURCE. NO SMOKE WAS VISIBLE. NO UNUSUAL INDICATIONS, NO C/B OPENED, SMELL DISSIPATED WITH APU SHUT DOWN) - FOUND APU OIL TANK OVERSERVICED, OPERATED APU FOR AN EXTENSIVE PERIOD WAS ABLE TO DUPLICATE SMESDR DXTA200300101Control Handle · defectiveAFTER TAKEOFF THE GEAR WOULD NOT RETRACT, NO UNLOCK LIGHT OR ANY FLICKERING OF THE 3 GREEN LIGHTS, ACCOMPLISHED AIR TURN BACK TO SJC. - FOUND LANDING GEAR CONTROL HANDLE DEFECTIVE, REMOVED DEFECTIVE LANDING GEAR CONTROL HANDLE AND INSTALLED NEW UNIT IAW MFG 5
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