N336QS
Service difficulty reports not matched to an aircraft · 21
They name N336QS, 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 = 'N336QS' 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 = 'N336QS' 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 DXTA2010020103963Pedal · bindingON LANDING WHILE APPLYING BRAKES, PEDALS SEEMED SOLID INITIALLY, THEN THERE WAS ADDITIONAL TRAVEL TO MAINTAIN THE SAME BRAKING. WHEN THE BRAKE PEDALS WERE RELEASED, THE LT PEDAL IS BINDING AND A LOUD "SNAPING" SOUND IS HEARD AND FELT. R & R RUDDER PEDAL BRACSDR DXTA2009120103876Control Valve · overheatedWINDSHIELD O'HEAT ANNUNCIATOR CAME ON IN FLIGHT WHILE WINDSHIELD HEAT WAS ON, -20ºC RAT. ANNUNCIATOR DID NOT EXTINGUISH AUTOMATICALLY AND WAS ACCOMPANIED BY BURNING ODOR. BOTH WERE RESOLVED WHEN WINDSHIELD HEAT WAS TURNED OFF. REPLACED TEMPERATURE CONTROL VASDR DXTA2009092803799Brake Assy · malfunctionedBRAKES SPONGY AT HIGH SPEED ROLL OUT AND PULL LEFT AS YOU INCREASE PRESSURE. WHEN AC REACHES 30 KTS & SLOWER BRAKES GRAB AS IF ANTI-SKID IS WORKING. BLED BRAKES AS REQUIRED IAW MM 32-42-08. ALSO CHECKED BOTH LT AND RT WHEEL SPEED TRANSDUCERS WITH NO DEFECTS SDR DXTA2009051403649Throttle · out of rigDURING SPEED BRAKE TEST WITH ENGINES RUNNING, RT THROTTLE WAS MOVED FWD AND THEN BACK TO IDLE. AT THE IDLE STOP, RT ENGINE SHUTDOWN. INSPECTED NR 2 ENGINE S/N PCE-JC0408 THROTTLE RIGGING. FOUND THROTTLE RIGGING TO BE OUT OF MM LIMITS. RE-RIGGED THE NR 2 ENGINSDR DXTA200810043294Relay · inoperativeBOTH BRAKES ON BOTH SIDES FAILED ON LANDING. BRAKE RESERVOIR IS FULL. ACCUMULATOR PRESSURE GAUGE READS RESIDUAL PRESSURE ONLY. CIRCUT BREAKER WAS CHECKED IN. NO BRAKE PRESSURE WAS SHOWN ON ANNUNCIATOR PANEL. REMOVED AND REPLACED RELAY K-745 WITH NEW. SYSTEM OSDR DXTA200803294Brake Sys · failedBOTH BRAKES ON BOTH SIDES FAILED ON LANDING. (K)SDR DXTA200807213189Control Handle · wornAFTER TAKEOFF, THE FLAP HANDLE WOULD NOT MOVE IN ORDER TO RETRACT. THE FLAP HANDLE WOULD NOT MOVE IN ORDER TO EXTEND FLAPS EITHER. FLAPS ARE STUCK AT 7 DEGREES. REMOVED THE FLAP HANDLE KNOB AND STUD THREAD. INSTALLED NEW FLAP HANDLE STUD THREAD AND NEW KNOB.SDR DXTA200803189Flap System · malfunctionedAFTER TAKEOFF, THE FLAP HANDLE WOULD NOT MOVE IN ORDER TO RETRACT. THE FLAP HANDLE WOULD NOT MOVE IN ORDER TO EXTEND FLAPS EITHER. FLAPS ARE STUCK AT 7 DEGREES. (A)SDR DXTA200702583Fitting · loose1ST OFFICERS BRAKES ARE MUSHY AND REQUIRE A COUPLE OF PUMPS AFTER INTITAL PRESSURE TO FIRM UP. INSPECTED BRAKE SYSTEM, FOUND PILOTS LT MASTER CYLINDER FITTINGS LOOSE. TIGHTENED FITTINGS. BLEED BRAKE SYS MULTIPLE TIMES. OPS LEAK CHECK GOOD IAW CESSNA 560 MM 32SDR DXTA200702546Anti-Skid Sys · stickingBRAKE RELEASE, GRAB WITH THE ANTISKID ON. BLED BRAKES IAW CE560 MM 32-42-00.SDR DXTA200702400Wire Harness · wornAFTER APPLYING BRAKE PRESSURE THE BRAKES GRAB AND THEN QUICKLY RELEASE. THET THEN GRAB AGAIN IN A JERKY FASHION. BLED A/C BRAKES. REMOVED AND REPLACED THE LEFT ANTI SKID HARNESS P/N 6508012-201 AND THE RIGHT ANTI SKID HARNESS P/N 8508012-202. OPS CHECK GOOD. ISDR DXTA200702348Ignition Lead · misinstalledNR1 ENGINE (LT) WOULD NOT MAKE TAKEOFF POWER. AIRPORT, 318 FT ELEV,TEMP 18C, TARGET T/O PWR 97.8 PERCENT. COULD ONLY GET 87.2 PERCENT AT 580 ITT. POWER LEVEL FULL FORWARD. TROUBLESHOT TO THE IB IGNITER LEAD POSITIONED INCORRECTLY AND OBSTRUCTING THE THROTTSDR DXTA200702249Brake Assy · weakBOTH PILOTS + COPILOTS LEFT BRAKE SOFT. BOTH PILOTS & COPILOTS RIGHT BRAKE EXTREMLY SOFT PEDAL HAS TO BE PUSHED ALL THE WAY FORWARD TO GET ANY BRAKING ACTION ON RIGHT (COPILOTS) SIDE. BLED ANTI-SKID BRAKE SYSTEM SEVERAL TIMES. OPS & LEAK CHECKS GOOD. TAXI CSDR DXTA200701917Engine · malfunctionedLT ENGINE SHUTDOWN DURING SPEED BRAKE RETRACTION TEST. N2 WAS 11 PERCENT. N1 WAS 7 PERCENT AND ITT STARTED TO RISE TO 550.SDR DXTA200601748Control Cable · bindingRT ENGINE SHUTDOWN WHEN THROTTLE WAS BROUGHT TO IDLE DETENT ON THE GROUND WITH IDLE SWITCH IN HIGH IDLE. THROTTLES FEEL NOTCHY NEAR THE LOW STOP. REMOVED RT ENGINE FWD THROTTLE CONTROL CABLE AND INSTALL NEW CABLE IAW THE MM CH 76-11-02. RIG CABLES IAW CH 76-SDR DXTA200500765Indicator · failedDURING TAKEOFF ROLL, STANDBY AIRSPEED INDICATOR STAYED AT 0 KTS. BOTH PFD AIRSPEED INDICATIONS WERE ACCELERATING THROUGH 60 KTS. ITEM IS UNDER INVESTIGATION.SDR CWQ2004F00007Wire · misinstalledWHEN COMPLYING WITH SB ON AC, THE RT WING FUEL BOOST PUMP WIRING WAS FOUND TO BE UNACCEPTABLE IAW SB OUTER JACKET, WIRE BRAID AND WIRE INSULATION CHAFED THRU, ALSO ABOUT HALF OF WIRE WAS ALSO CHAFED. THE WIRING WAS CHAFED ON A FUEL SUPPLY TUBE PN 652635548 WHSDR DXTA200300063Wire · brokenBRAKES FAILED UPON TOUCHDOWN DEPLOYED EMERGENCY BRAKING SYSTEM. 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 WORK DONE IAW CESSDR 97ZZZX32Inverter · malfunctionALTITUDE AND HEADING FAIL ON PILOT AND COPILOT PFD DISPLAYS. FOUND NR 1 INVERTER MALFUNCTIONING.SDR 97ZZZX34Gyro · malfunctionAUTOPILOT INOPERATIVE. RATE GYRO CIRCUIT BREAKER POPPED. FOUND RATE GYRO MALFUNCTIONING.SDR 96ZZZX3390Tube · misadjustedCABIN ENTRY DOOR FAILED TO OPEN UPON ARRIVAL. CREW HAD TO EGRESS THROUGH ESCAPE HATCH. FOUND LOWER FORWARD 3 PINS FAILING TO RETRACT FULLY. SUBMITTER STATED CAUSE, FOUND EVIDENCE OF PIN CONTACT WITH CABIN DOOR FRAME. THIS CAUSED THE ABOVE TUBE TO BEND SLIG
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