N626QS
Service difficulty reports not matched to an aircraft · 18
They name N626QS, 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 = 'N626QS' 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 = 'N626QS' 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 DXTA2011052504590Actuator · failedAFTER TAKEOFF, MLG & FLAPS RETRACTED. HYD PRESSURE, STAB MISCOMPARE & GEAR UNLOCK LIGHTS STAYED ON. ON RETURN FOR LANDING FLAPS & MLG LOWERED, ALL NORMAL. R & R THE LT MLG ACTUATOR IAW MM 32-30-04. PERFORMED MLG HYD SYS ADJUSTMENTMENT TEST IAW MM 32-01-00SDR DXTA2010122204372Rudder Control · frozenON LANDING, DISCOVERED RUDDER FROZEN. TAXIED BY BRAKING ONLY. ONLY ABLE TO MOVE RUDDER AFTER APPROX 15 MINUTES ON GROUND. INSPECTED FUSELAGE STINGER FAIRING DRAIN HOLE AND FOUND TO BE CORRECT SIZE IAW SL 53-05. REMOVED STINGER FAIRING AND BELLY ACCESS PANEL SDR DXTA2010081704195Relay · malfunctionedON FINAL AFTER GEAR EXTENSION, LOW BRAKE PRESSURE ANNUNCIATOR AND ANTI-SKID INOP ANNUNCIATOR BOTH CAME ON AND STAYED ILLUMINATED. EMERGENCY BRAKE WAS USED TO STOP THE AIRPLANE ON THE RUNWAY CIRCUIT BREAKERS PULLED FOR SAFETY. ANTI-SKID PUMP MOTOR DOES NOT RUNSDR DXTA2009041303597Warning System · malfunctionedRT ENGINE ANTI-ICE ANNUNCIATOR AND MASTER CAUTION COMES ON WITH THE ENGINE/WING ANTI-ICE SWITCH IN THE OFF POSITION. REMOVED AND REPLACED R/H ENGINE STATOR VALVE. OP/LEAK CHECKS GOOD. IAW CE560XL MM CH 21-30-00SDR DXTA2009040603579Uplock Switch · illuminatedAFTER TAKEOFF, GEAR WAS RETRACTED AND UNLOCK LIGHT WOULD NOT GO OUT. CYCLED GEAR AND LIGHT REMAINED ON HYD PRESS LIGHT WAS NOT ON. HYD PRESS LIGHT WAS NOT ON. FOUND RT GEAR UPLOCK SWITCH OUT OF ADJUSTMENT. C/W RIGGING OF SWITCH IAW MM 32-61-00. OPS CHECKS GSDR DXTA2009010403461Control Valve · inoperativeON TAKEOFF, INTIAL GEAR RETRACTION WAS NORMAL. 3-5 SEC LATER DURING FLAP RETRACTION RED UNLOCK LIGHT ILLUM. A LOUD THUMPING SOUND FROM THE NOSE GEAR. HYD PRESS LT AND STAB MISCOMPARE LIGHT ILLUM. RE-EXTENDED GEAR NORMALLY AND HYD PRESS, STAB MISCOMPARE. RSDR DXTA2009010503461Warning Light · illuminatedDURING FLAP RETRACTION, RED LANDING GEAR UNLOCK LIGHT ILLUMINATED.SDR DXTA200702726Actuator · bypassingEMERGENCY DECLARED. ON POST FLT DISCOVERED LEFT FLAP EXTENDED ABOUT ONE INCH & RT FLAP FULLY RETRACTED FLUSH WITH THE FLAP HANDLE IN THE FULL UP POSITION. ' HYD PRESS' AMBER ANNUNCIATOR REMAINED ILLUMINATED IN FLT AFTER FLAP RETRACTION. PERFORMED 'HYD PRESS' ASDR DXTA200701907Trim System · stuckAFTER TAKEOFF, COULD NOT ENGAGE AUTOPILOT. MANUAL PITCH TRIM STUCK, COULD NOT MOVE. ELECTRIC TRIM NORMAL. YAW DAMPER OPS NORMAL, PRESSED AUTOPILOT RELEASE BUTTON SEVERAL TIMES IN ORDER TO GET AUTOPILOT TO ENGAGE WITH NO SUCESS . AFTER LANDING , MANUAL SDR DXTA200601518Uplock Switch · looseGEAR UNLOCK LIGHT ILLUMINATED (FLAPS AND STAB IN NORMAL POSITION) GEAR CYCLED,LIGHT REMAINED ON W/HYD PRESS SEGMENT LIGHT. - INSPECTED LANDING GEAR UPLOCK SYSTEM WIRES, SWITCHES AND PLUGS. NO DEFECTS NOTED. JACK AIRCRAFT. CHECK UPLOCK SWITCH FOR LIGHT RESISTANSDR DXTA200601506Landing Gear · malfunctionedAFTER GEAR RETRACTION UNLOCK LIGHT STAYED ON. CYCLED THE GEAR WITH SAME INDICATION PLUS HDY PRESS ANNUNCIATOR REMAINED ON. EXERCISED CHECKLIST PROCEDURE AND THEN EXTENDED GEAR WITH ALL INDICATIONS NORMAL. TROUBLESHOT SYSTEM, RANG OUT 3 UPLOCK SWITCHES, ALL OPSSDR DXTA200601487Control Cable · brokenELEVATOR TRIM MALFUNCTIONED DURING FLIGHT. REMOVED & REPLACED LT & RT AFT ELEVATOR TRIM CABLES AND PULLEY IAW CESSNA 560XL M/M CHAPT 27-31-00& 27-32-02.SDR DXTA200601294Position Switch · out of adjustLANDING GEAR UNLOCK LIGHT REMAINS ON WITH LANDING GEAR RETRACTED AND WITH FLICKERING HYD LIGHT. ADJUSTED LT MLG UPLOCK SWITCH TO MATCH NLG AND RT MLG. CYCLED GEARS THROUGH NUMEROUS TIMES. NO FLICKERING HYD LIGHTS. OPS CHECK GOOD IAW CE560XL M/M 32-30-05.SDR DXTA200500687Relay · failedLO BRAKE PRESS & ANTISKID INOP ANNUNCIATOR ILLUMINATED AT START OF T/O ROLL CAUSING WHEEL BRAKE FAILURE, THE EMERGENCY BRAKING SYSTEM WAS USED. TROUBLESHOT TO POWER BRAKE CONTROL RELAY KN003. RELAY WOULD NOT CLOSE. REMOVED AND REPLACED RELAY IAW CC 560XL WISDR CWQR20050004Support Bracket · misinstalledDURING PHASE 1-4 INSPECTION FOUND LOWER OUTBOARD BARREL SUPPORT BRACKETS INSTALLED INCORRECTLY DURING MANUFACTURE.SDR DXTA200400501Brake · fireON TAXI IN, GROUND PERSONNEL NOTICED THE LT WHEEL WELL HAD A FIRE, FLIGHT CREW DID NOT NOTICE ANY GRINDING, PULLING, OR VIBRATION INDICATING A PROBLEM. INSPECTED LT MAIN LANDING GEAR AND SURROUNDING WING AREA FOR DAMAGE, NONE NOTED. REMOVED LT MAIN WHEEL ASSSDR DXTA200400445Anti-Skid Sys · inoperativeON APPROACH, BROUGHT THE LANDING GEAR DOWN BOTH ANTI-SKID INOP AND LOW BRAKE PRESSURE ANNUNCIATORS REMAINED ILLUMINATED. CYCLED THE GEAR AND RAN THE CHECKLIST, THE POWER BRAKES CB WAS IN WHEN RUNNING THE CHECKLIST. EMERGENCY BRAKES WERE USED TO STOP AIRCRAFTSDR DXTA200400302Landing Gear · malfunctionedAFTER TAKE OFF FROM FFC NOSE LANDING GEAR WOULD NOT RETRACT, DIVERTED TO ATL AND LANDED SAFELY. ITEM IS UNDER INVESTIGATION.
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