N512QS
Service difficulty reports · 19
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 = 'N512QS' 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 = 'N512QS' 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 DXTA2026090209498Switch · faultedCLIMBING THROUGH FLIGHT LEVEL 380 UP TO FLIGHT LEVEL 430 WE ENCOUNTERED SOME HEAVY VIBRATIONS COMING FROM THE NOSE SECTION FOR ABOUT 10 SECONDS. ABOUT FIVE MINUTES LATER THE GEAR DISAGREE N CAS MESSAGE APPEARED ALONG WITH A AMBER CROSSHATCHED SQUARE ON THE NOSSDR DXTA2026060408323Pcb · defectiveTOP LOCKING PIN DOES NOT STOW FULLY. CAUSING ASSOCIATED CHECK DOOR CAS, AND CABIN DOOR OPEN CAS. REMOVED FWD PRINTED LH PCB NC105 PN:7468101-20 SN:33674927-3 DUE TO CHECK DOOR CAS AND INSTALLED CUSTOMER SUPPLIED NEW PCB PN:7468101-20 SN: 35064311-4. REPLACESDR DXTA2025090204764Wire · pulledLAV EMERGENCY TOE KICK LIGHT DOES NOT ILLUMINATE WITH ANY POWER SOURCE. REMOVED LAV FASCIA & FOUND THE WIRES FOR THE TOE KICK LIGHT PULLED OUT OF THE CONNECTOR. LOOKED UP & PLACED NEW CONNECTOR & PINS ON ORDER. 8/30 JT-VJG. INSTALLED NEW PINS ONTO WIRE & INSSDR DXTA2025071004164Warning Message · false indicationRECIVED CHECK DOORS CAS. FOLLOW CHECK DOORS QRH AND CYCLED ALL DOORS ASSOCIATED ALSO COMPLETED POWER UP ANOMALY CHECKLIST. CAS REMAINS WITH THE MAIN CABIN DOOR CLOSED. DOOR OPEN LIGHT ALSO REMAINS ON.(HANDLE STIFF AND NOT STOWING) POWERED UP ACFT. CONFIRMED ASDR 2025FA0000387Closeout Panel · corrodedCORROSION UNDER LH AND RH AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURESDR DXTA2025040702985Anti-Ice System · faultedDURING CLIMB AROUND 14000' WE OBSERVED A/I ENGINE HOT R CAS MSG. WE RAN THE QRH PROCEDURE AND DECREASED RIGHT ENGINE POWER. THE MSG EXTINGUISHED. BUT THEN REOCCURED WHEN POWER WAS INCREASED. ENG BLD AIR KNOB WAS SECLECTED TO LP AND DIVERTED WHILE REMAININGSDR DXTA2024122701687Fuse · blownDURING THE FIRST STEP OF THE POWER ON CHECKLIST, EMERGENCY LIGHTS DO NOT ILLUMINATE WITH THE SWITCH PLACED IN "ARM" (NO DC POWER ON). LIGHTS DO WORK IN THE "ON" POSITION. WE PERFORMED THE "EMERGENCY LIGHTS FAIL PREFLIGHT TEST" CHECKLIST VIA MAINTANENCE'S INSTRSDR DXTA2024121601517Battery Pack · inoperativeEMER LIGHTS STILL ILLUMINATED IN ARM WTIH MAIN DC APPLIED. CYCLED TO COLD/ DARK AND RESET BUTTON, CONDITION STILL REMAINED. CORRECTIVE ACTION; CONFIRMED DISCREPANCY. ACTUATED ALL G SWITCHES, NO CHANGE TO CONDFFION. ELECTRICALLY CHECKED ALL G SWITCHES PER CE·6SDR DXTA2023111310027Unknown · inoperativeGEA FAIL 3 AMBER CAS: GEA FAIL 3 CAS MESSAGE ILLUMINATED DESCENDING THROUGH FL 240. REMOVED GEA 3 PN 011-02635-00 SN 2BY005258 AND INSTALLED CUSTOMER SUPPLIED REPAIRED GEA7100 (UNIT 3) PN 011-02635-00 SN 2BY005444 AS REQUIRED. PERFORMED CONFIGURATION AS REQUISDR DXTA2023091495400Unknown · unknownCABIN EMERG LIGHT: EMERGENCY LIGHT ABOVE SEAT 7 IS STUCK IN THE ON POSITION WHEN THE EMER LIGHT SWITCH IS IN ARM POSITION. LIGHT WILL NOT TURN OFF UNLESS EMER LIGHT SWITCH IS SET TO OFF POSITION. RESET THE #1 EMERGENCY LIGHT INERTIA SWITCH AS REQUIRED, OPERATSDR DXTA2023032783230Unknown · unknownLAV EMERG LIGHT: THE EVACUATION PATH LIGHT UNDER THE LAV SEAT WAS FLICKERING ON AND OFF, AND THEN EXTINGUISHED. TRACED BACK TO A WIRE PUSHED PIN IN THE WIRING HARNESS CONNECTOR. RESEATED THE PIN INSIDE THE CONNECTOR & FOUND LIGHT ASSY TO WORK AS NORMAL. SECURSDR 2022F00229Engine · corrodedRH ENGINE AGB AFT COVER IS CORRODING.SDR 2022F00228Engine · corrodedLH ENGINE AGB AFT COVER IS CORRODING.SDR DXTA2021122754170Switch Panel · defectiveLIFT BLACK BUTTON LOCATED IN THE CABIN WHICH FUNCTIONS TO CLOSE THE MAIN CABIN DOOR IS INTERMITTENT WHEN PRESSED TO LIFT THE DOOR. // SIGN OFF// GAINED ACCESS TO SWITCH PANEL REMOVED AND REPLACED SWITCH PANEL PN: SWP500-01 SN: 277000086 WLTH INSPECTED SWITCSDR DXTA2021111852140Pcb · damagedACM BLD LEAK AMBER CAS: AT FLIGHT LEVEL 220, THE ACM BLEED LEAK QUICKLY FOLLOWED BY THE EMER PRESS CAS MESSAGES ILLUMINATED. WE COMPLETED THE ACM BLEED LEAK AND EMER PRESS QRH CHECKLISTS. THE CABIN TEMP WENT TO 124 DEGREES AND THE COCKPIT TEMP WENT TO 93 DEGRESDR 2021FA0000257Skin · corrodedHORIZONTAL STABILIZER LOWER SKIN DAMAGE(CORROSION).SDR 2021F00008Doubler · crackedCRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL. ACCOMPLISHED TEXTRON AVIATION FIELD REPAIR SR-680A-ATA53-25890 REV- DATED 6/1/2020: STANDARD REPAIR-CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL NWW, FRAME, WEB, AND DOUBLERS, FS 75.SDR DXTA2018110901653Filter · dirtyAFTER TAKEOFF, SMOKE APPEARED IN CABIN (LIGHT HAZE) AND ACRID SMELL. SUPPLEMENTAL INFORMATION: REMOVED AND REPLACED CABIN HEPA FILTER IAW CE680A MM 21-70-10. REMOVED PN 9914836-1 SN 0102. INSTALLED PN 9914836-1 SN 0244SDR DXTA2016120900000Shroud · detachedRIGHT WING AILERON TRAILING EDGE SHROUD FORWARD OF THE AILERON HAS BECOME DETACHED. THE SHROUD IS ATTACHED TO THE WING VIA 8 SCREWS. THE TRAILING EDGE WING STRUCTURE THAT THE SHROUD ATTACHED TO FAILED AT 3 SCREW ATTACH POINTS AT THE TOP AND 2 AT THE BOTTOM ARE
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