N589QS
Service difficulty reports · 24
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 = 'N589QS' AND registry_match = 'registration' 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 = 'N589QS' AND registry_match = 'registration' 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 DXTA2026071008770Light Sys · malfunctionedEMERGENCY LIGHTS REMAIN ILLUMINATED WITH THE EMERGENCY LIGHTS SWITCH IN THE ARM POSITION. THE FIRST TIME AFTER OPENING THE MAIN CABIN DOOR THEY EXTINGUISHED AND OPERATED NORMALLY. THE SECOND TIME THEY WOULD NOT EXTINGUISH UNTIL EMERGENCY LIGHTS SWITCH WAS PLACSDR DXTA2025101305271Control Unit · defectiveWHILE CLIMBING OUT WE NOTICED THE NO LIGHT ( NOSE GEAR GREEN LIGHT ) ILLUMINATED . WE RAN THE QRH AND DIVERTED TO MEM. REMOVED SUSPECTED FAULTY LANDING GEAR CONTROL UNIT PN 049801-001 SN L2104 AND INSTALLED REPAIRED LANDING GEAR CONTROL UNIT PN 049801-001 SNSDR DXTA2025030602555Pressure Switch · defectiveUPON LANDING GEAR RETRACTION, THE RED UNLOCK LIGHT STAYED ILLUMINATED. THE HYD PRESS LIGHT STAYED ILLUMINATED AND STARTED FLASHING WITH ASSOCIATED MASTER CAUTION LIGHT. STAB MISCOMPARE LIGHT ALSO ILLUMINATED. EXTENDED GEAR, GOT THREE GREEN AND ALL LIGHTS WENTSDR DXTA2023101297810Pressure Switch · defectiveLEFT HORIZONTAL STAB: AFTER EXTENDING FLAPS TO 15 FOR LANDING, WE RECEIVED A STAB MISCOMP APPROX 1 MIN AFTER THE HYD PRESS HAD BEEN CONTINUISLY ILLUMINATED. THE STAB MISCOMP EXTINGUISHED AND APPROX 1 MIN LATER THE STAB MISCOMP RETURNED A SECOND TIME PRIOR TOSDR DXTA2023091194860Unknown · unknownELEVATOR CONTROL/TRIM: DURING FLIGHT THE ELEVATOR TRIM KEPT TRYING TO TRIM NOSE DOWN BUT KEPT SPRINGING BACK, SEE VIDEO. WITH AP DISCONNECTED I TRIED TO MANUALLY TRIM BUT TRIM WAS FROZEN IN PLACE. //SIGNOFF// PERFORMED SUCCESSFUL OPS CHECK OF ELEVATOR TRIM TSDR DXTA2023080392210Battery · defectiveFLOOR EMERG EXIT LIGHT: RIGHT AFT FLOOR EMER LIGHTS INOP. REMOVED AND REPLACED THE AFT EMERGENCY BATTERY PACK IAW CESSNA CE-560XL AMM 33-50-01. OPS CHECK GOOD.SDR DXTA2022100571640Seal · unsecureMAIN DOOR: A SEAL UNDER THE BOTTOM STEP ON THE MAIN CABIN DOOR HAS BECOME UNSEATED AND COULD INTERFERE WITH CLOSING THE DOOR. // SIGNOFF// RE-ATTACHED THE SEAL TO THE CABIN ENTRY DOOR FIXED STEPS REF CE560XL AMM 52-10-02 AND SPM 20-40-30SDR DXTA2022051962150None · defectiveAFT EMERGENCY LIGHT WILL NOT ILLUMINATE USING THE EMERGENCY LIGHTS BATTERY. THEY DO WORK WITH MAIN DC POWER. // SIGNOFF// VERIFIED AFT EXIT SIGNS AT DIVIDER AND OVER LAVATORY DO NOT ILLUMINATE ON EMERGENCY POWER ALONE, ALSO NOTED EXTERIOR OVER-WING LIGHTS DO NSDR DXTA2021061443670Control Unit · defectiveCABIN PRESSURIZATION CONTROL: AIRCRAFT OVER PRESSURIZED ON TAKEOFF OUT OF TETERBORO. RAN CHECKLIST ENDED UP HAVING TO DUMP THE CABIN WITH EMER DUMP. RETURNED TO FIELD DID NOT LAND OVERWEIGHT. // SIGNOFF// WHILE STARTING THE APU APU BLEED AIR SWITCH OFF VISUALLSDR DXTA2021051441960Relay · intermittentBRAKE PRESSURE LIGHT: DURING TAXI OUT BOTH LOW PRESSURE AND ANTISKID LIGHTS ILLUMINATED ALONG WITH MASTER CAUTION. CIRCUIT BREAKERS DID NOT POP. USED EMERGENCY BRAKES TO STOP THE AIRCRAFT DUE TO COMPLETE LOSS OF BRAKE PRESSURE. // SIGNOFF // TROUBLE SHOT AND SDR EBVR20181203001Tab · crackedRUDDER TRIM TAB IS CRACKED APROX. 1" ON LOWER AFT CORNER. PERFORMED DOUBLER REPAIR TO RUDDER TRIM TAB LOWER TRAILING EDGE. WORK DONE IAW AQRD ERO-935680 REV IR DATED 11/30/2018SDR DXTA2018092101444Brake Sys · contaminatedMLG BRAKE PRESSURE, BRAKING ON LANDING ROLLOUT IS WEAK AT SLOWING AIRCRAFT. ALSO EXCESSIVE FORCE IS NEEDED WHEN DOING BRAKE ASSISTED TURNS. BLED LT & RT BRAKE ASSEMBLIES IAW MM 32-32-00. TAXI CHKS GOOD AT THIS TIME.SDR JGVR20170614002Shaft · corrodedAILERON AFT SECTOR SHAFT ASSEMBLY HAS CORROSION. REMOVED AND REPLACED THE AILERON AFT SECTOR SHAFT IAW MM 27-10-03.SDR JGVR20170614001Torque Tube · corrodedLEFT ELEVATOR HAS A CORRODED TORQUE TUBE. REMOVED AND REPLACED THE TORQUE TUBE IAW SRM 51-40-03, 51-40-06, AND 55-20-01.SDR DXTA2016041306225Skin · damagedAIRCRAFT HAS HAIL DAMAGE. R & R THE LT & RT AILERONS IAW MM 27-10-01 & SRM 51-60-00 & 51-60-01. R & R THE LT & RT ELEVATORS IAW MM 27-31-01 & SRM 51-60-00 & 51-60-02. PARTS REPLACED RT AILERON PN 6624032-3, SN 0000070, ELEVATOR PN 6634200-9 & SN 0000313 & ESDR DXTA2014040405717Seal · pinchedACOUSTIC SEAL WILL NOT RETRACT WITH APU & OR ENGINES RUNNING. CAN NOT OPEN MAIN CABIN DOOR WITHOUT DIFFICULTY. GAINED ACCESS TO THE ACOUSTIC SEAL DEFLATION VALVE. WHEN MED TRIM PANEL WAS REMOVED FOUND ONE OF THE ACOUSTIC DOOR LINES PINCHED BY THE PRE CATCHSDR DXTA2013073105461Control Unit · failedWHILE EXITING THE RUNWAY, THE ANTI-SKID LIGHT CAME ON AND ALL NORMAL BRAKING ABILITY WAS LOST. STOPPED ACFT ON THE TAXIWAY WITH THE EMERGENCY BRAKING SYSTEM. PERFORMED ANTI-SKID OPS CHECK & FOUND RT TRANSDUCER FAULT BIT ON THE CONTROL FAULT BIT INDICATOR, ASDR DXTA2013071705448Motor · failedON TAXI OUT, OBSERVED POWER BRAKES CIRCUIT BREAKER TRIPPED WITH MASTER CAUTION AND ANTI-SKID INOPERATIVE ANNUNCIATORS ILLUMINATED. RAN ANTI-SKID INOPERATIVE ABNORMAL CHECKLIST AND RETURNED TO RAMP. NO BRAKING AFTER CAUTIOUSLY MOVING FWD AND HAD TO USE EMERSDR DXTA2012070505028Motor · inoperativeDURING TAXI OUT THE "ANTISKID INOP" LIGHT ILLUMINATED FOLLOWED SHORTLY THEREAFTER BY THE "PWR BRKS" CIRCUIT BREAKER POPPING. R & R THE HYD PUMP MOTOR IAW MM 32-44-20. OPS & LEAK CHECKED GOOD. TAXI CHECKED GOOD.SDR DXTA2012062505013Motor · inoperativeDURING TAXI OUT THE "POWER BRAKES" CIRCUIT BREAKER TRIPPED. LOST ALL BRAKING SHORTLY THEREAFTER AND USED THE "EMERGENCY BRAKE" SYS TO STOP THE ACFT. R & R THE POWER BRAKE MOTOR, (PN MP50B-1, SN 3905) PRESSURE SWITCH, (PN GPP1250-73 S/N 0236273) MOTOR TO HYD SDR DXTA2010102704276Shutoff Valve · bindingON TAKEOFF, RUDDER PEDALS VERY STIFF. CONFIRMED YAW DAMPER OFF. RETURNED. RUDDER BIAS CHECKED NORMAL ON TAXI. AFTER LANDING, ON TAXI IN, CHECKED RUDDER STIFFNESS AND FOUND NORMAL AT IDLE POWER BUT RUDDER BECAME PROGRESSIVELY STIFFER AS POWER ADVANCED. COULSDR DXTA2009042303615Brake Sys · stickingWHEN APPLYING THE RT BRAKE, THE BRAKE GRABS AND THE ACFT SHUTTERS, MOST NOTICEABLE AT TAXI SPEED.SDR DXTA2008122403435Rudder Control · malfunctionedRUDDER PEDALS HAVE GRINDING FEELING DURING TAKEOFF ROLL AND IN-FLIGHT.SDR DXTA20081223034Arm · wornRUDDER PEDALS GRINDING DURING TAKEOFF ROLL AND IN-FLIGHT. GRINDING IS FELT W/POWER ON OR IDLE, & W/ AUTO-PILOT AND YAW DAMP ON OR OFF. GRINDING IS NOT FELT DURING STATIC CHECKS OR LOW SPEED TAXI REGARDLESS OF POWER SETTINGS. FOR BINDING AND DEFECTS. NONE NOTE
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