N535QS
Service difficulty reports · 28
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 = 'N535QS' 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 = 'N535QS' 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 DXTA2026042807810Pcb · faultedJUST BEFORE LANDING WE HAD A CABIN DOOR OPEN CAS MESSAGE. WHILE ON THE GROUND WE TRIED TO RESET IT USING THE PROCEDURE IN THE QRH. STEP FOUR WAS UNSUCCESSFUL, WE COULD NOT GET THE CHECK HANDLE /PUSH TO OVERRIDE LIGHT TO FLASH. : REMOVED AND REPLACED NC105 CABISDR DXTA2025121206055Fitting · defectiveAFTER LANDING LINE TECH INFORMED US THAT LEFT MAIN WAS SMOKING. FOUND SMOKE COMING FROM LEFT MAIN. REPLACED BRAKE TOP BLEED FITTING. OPS CHECK GOOD. IAW MM 32-48-00SDR DXTA2025081804624Light · inoperative33-50-04 RIDE SIDE OVERWING EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE DURING TEST OR ANY OTHER MODE WHEN IT SHOULD BE ILLUMINATED. R & R RT OVERWING EMERGENCY LIGHT IAW AMM 33-50-20. OPS CHECKED GOOD.SDR DXTA2025012001991Unknown · odorODORS IN COCKPIT / CABIN: REPEAT WRITEUP. WE DEPARTED KIAD AND CLIMBED TO 3000FT. AT LEVEL OFF, WE TURNED ON THE ENG AND WING ANTI ICE. AS SOON AS WE TURNED ON THE ANTI ICE, WE NOTICED AN UNUSUAL ODOR, SORT OF LIKE A PLASTIC FUME TYPE OF ODOR. WE ELECTED TSDR DXTA2025011601963Seal · defectiveON CLOMB OUT AT 7-8K FT, A BURNING SMELL STARTED . THE ENTIRE FLIGHT THE BURNING SMELL CAME IN STRONG WAVES. THE STRONGEST WAS DURING THE DECENT OUT OF 18K FT AND BELOW . REPLACED ENGINE HP VALVE SEALS. OPS CHECK GOOD. IAW CE-680A AMM 36-10-05SDR DXTA2024011110577Module · faultedLANDING GEAR HANDLE: AFTER TAKEOFF LANDING GEAR HANDLE WOULD NOT COME OUT OF LOCK DETENT AND GEAR WOULD NOT RETRACT. AFTER LEVELING OFF AT 4000 AND TRYING SEVERAL MORE TIMES GEAR FINALLY RETRACTED WITHOUT ISSUE. NO CAS MESSAGES WERE PRESENT. GEAR EXTENDED ON LSDR DXTA2023101698000Unknown · unknownWHEN BRAKING AFTER LANDING THERE IS A LOUD CHATTERING FROM THE BRAKES AND A VERY NOTICABLE VIBRATION AND SHUDDERIG THAT ACCOMPANIES RHE NOISE. WE CAN NOT TELL WHICH MAIN BRAKE IS CAUSING THE PROBLEM. BLED BRAKES AND FOUND A GOOD AMOUNT OF AIR IN THE SYSTEM. SDR DXTA2023092596260Unknown · unknownWORN BRAKES: UPON LANDING, WHEN BRAKES APPLIED, HEARD EXCESSIVE SCREECHING AND FELT A SHIMMY COMING FROM BOTH MAINS. . ARRIVED ONSITE AND GAINED ACCESS TO THE AIRCRAFT. PERFORMED GVI OF GEAR, BRAKES AND TIRES WITH NO DEFECTS NOTED. SET BRAKES AND MEASURED WEARSDR DXTA2023092696140Light · defectiveEMERGENCY OVERWING EXIT LIGHT INOP. (PRE-FIGHT) REMOVED AND REPLACED OVERWING EMERGENCY EXIT LIGHT OPS CHECK GOOD WORK DONE IAW CE 680A MM 33-50-20.SDR JGVR20230324007Unknown · unknownBLENDED 2 AREAS OF CORROSION UNDER AND AROUND NUTPLATES ON PANEL 134BBC MOUNTING FRAME, FOUND AN ADDITIONAL 6 AREAS. BLENDED ADDITIONAL 6 AREAS. NDT VERIFIED CORROSION REMOVAL AND REMAINING THICKNESS. EVALUATED NDT FINDINGS. REPAIRED BLENDED AREAS WITHIN LIMITSDR JGVR20230324006Unknown · unknownBLENDED 5 AREAS OF CORROSION UNDER AND AROUND NUTPLATES ON PANEL 144ABC MOUNTING FRAME, FOUND AN ADDITIONAL 10 AREAS. BLENDED ADDITIONAL 10 AREAS. NDT VERIFIED CORROSION REMOVAL AND REMAINING THICKNESS. EVALUATED NDT FINDINGS. REPAIRED BLENDED AREAS WITHIN LIMSDR JGVR20230324005Unknown · unknownBLENDED 6 AREAS OF CORROSION UNDER AND AROUND NUTPLATES ON PANEL 144BBC MOUNTING FRAME, FOUND AN ADDITIONAL 6 AREAS. BLENDED ADDITIONAL 6 AREAS. NDT VERIFIED CORROSION REMOVAL AND REMAINING THICKNESS. EVALUATED NDT FINDINGS. REPAIRED BLENDED AREAS WITHIN LIMITSDR JGVR20230324004Unknown · unknownBLENDIED 3 AREAS OF CORROSION UNDER AND AROUND NUTPLATES ON PANEL 144CBC MOUNTING FRAME, FOUND AN ADDITIONAL 21 AREAS. BLENDED ADDITIONAL 21 AREAS. NDT VERIFIED CORROSION REMOVAL AND REMAINING THICKNESS. EVALUATED NDT FINDINGS. REPAIRED BLENDED AREAS WITHIN LISDR JGVR20230324003Unknown · unknownBLENDING 12 AREAS OF CORROSION UNDER AND AROUND NUTPLATES ON PANEL 166AR MOUNTING FRAME, FOUND AND BLENDED AN ADDITIONAL 3 AREAS. BLENDED ADDITIONAL 3 AREAS. NDT VERIFIED CORROSION REMOVAL AND REMAINING THICKNESS. EVALUATED NDT FINDINGS. REPAIRED BLENDED (LEVESDR JGVR20230324002Unknown · unknownREPLACED CORRODED RUDDER FAIRING INNER SUPPORT RIB P/N UNKNOWN WITH NEW TEXTRON P/N 6912670-5 PER CESSNA 680A SRM 51-40-05 AND 51-40-11 AND DUNCAN AVIATION PROCESS GPP-0105 REV. 9.SDR JGVR20230324001Unknown · unknownBLENDED AND TREATED CORRODED AREAS ON THE LH AND RH SKINS OF THE HORIZONTAL STABILIZER. INSTALLED AN EXTERNAL DOUBLER ON THE RH UPPER SKIN TRAILING EDGE IAW ENGINEERING REPAIR ORDER.SDR DXTA2022082268500Panel · defectiveMAIN DOOR: LIFT BUTTON ON THE INTERIOR DOOR PANEL FOR THE MAIN ENTRY DOOR ONLY WORKS INTERMITTENTLY // SIGNOFF// REMOVED ANDREPLACED DOOR LIFT PANEL IAW CE-680A IMM 25-20-36-01 OPS CHECK GOODSDR DXTA2022080867580Wire Harness · damagedWOW MISCOMPARE AMBER CAS: WOW MISCOMPARE MESSAGE ON SHORT FINAL. WENT AROUND. UPON GEAR RETRACTION, GEAR STAYED DOWN AND GESR DISAGREE LRN MESSAGE APPEARED. RAN CHECKLIST. AFTER PUTTING GEAR HANDLE DOWN GEAR MESSAGE WENT AWAY. FOLLOWED A MINUTE OR TWO LATERSDR DXTA2022022157050Battery · defectiveRECEIVED THE EMERGENCY POWER SUPPLY PACKS. GAINED ACCESS AND REMOVED #1 EMERGENCY POWER SUPPLY PACKS PN: CBS28-1, SN: 3533M DUE TO INTERNAL FAILURE. INSTALLED REPAIRED
EMERGENCY POWER SUPPLY PACKS PN: CBS28-1, SN: 005693. GAINED ACCESS AND REMOVED #2 EMERGENCSDR DXTA2022011755180None · noneEMERGENCY LIGHTS BATTERY: LAV EMER OVERHEAD LIGHT & FLOOR LIGHTS ARE DIM // SIGNOFF// COMPLIED WITH NJA TASK CARD TC-FLT-33-1001 CESSNA CE-680A EMERGENCY LIGHTING POWER SUPPLY BATTERY EXCERCISE PROCEDURE (REV.0, DATED: 15-DEC-2021) ALL EMERGENCY LIGHTS OPERATESDR 2021F00353Axle · chippedRH MLG AXLE PLATING DAMAGE (CHIPPED). ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ32824M1 DATED DECEMBER 10, 2021; 680A-0078 (N535QS) RIGHT MAIN LANDING GEAR AXLE PLATING DAMAGE (CHIPPED).SDR 2022F00020Axle · chippedREPAIR OF RIGHT MAIN LANDING GEAR AXLE PLATING DAMAGE. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ32824M1 DATED: DEC. 10, 2021, 680A-0078 (N535QS) RIGHT MAIN LANDING GEAR AXLE PLATING DAMAGE (CHIPPED).SDR 2021F00079Frame · crackedCRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, FS 75. ACCOMPLISHED TEXTRON AVIATION FIELD REPAIR SR-680A-ATA53-25890 REV- DATED JUNE 1, 2020 AND 8100-9 DATED 6/1/2020; STANDARD REPAIR - CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NSDR DXTA2020052803715Manifold · defectiveAT FL 430 HEAVY BANGING / VIBRATION COMING FROM NOSE WHEEL AREA WITH RAPID CONCESSION. NO CASS MESSAGES. NO GEAR ERROR INDICATION OTHER THAN UP. BELOW 16000 AND 210 KNOTS BANGING / VIBRATION WENT AWAY. NORMAL GEAR EXTENSION WITH DOWN LOCKED INDICATIONS. HAD AISDR DXTA2020031603583Door · out of adjustCLIMBING THRU FL370 WE HEARD A LOUD NOISE WITH LOUD AND HEAVY VIBERATIONS, CONSTANT PITCH VIBRATIONS WITH OCCASIONAL HARD YAWS TO THE LEFT AND RIGHT... COMING THRU A SINGLE DIGET ALTITUDE THE VIBERATIONS JUST STOPPED.//SIGNOFF//PERFORMED ARES DOWNLOAD, CHECKEDSDR DXTR20190702301Skin · damagedWING ANTI ICE CROSS FLOW VALVE STUDS HAVE DAMAGED LOWER FUSELAGE SKIN IN TWO PLACES. BLENDED, OUT DAMAGE TO PREPARE FOR NDT. NO CRACKS NOTED. COMPLETED STANDARD REPAIR SR-680A-ATA53-22175.SDR DXTR2019070901Anti-Ice Valve · interferenceWING ANTI-ICE CROSSFLOW VALVE HAS CAUSED DAMAGE TO THE LOWER FUSELAGE SKIN. DURING INSPECTION FOUND THERE IS A CHAFFED SPOT ON THE LOWER SKIN P/N: 7411392-12 OF SKIN BOND ASSEMBLY P/N: 7411391-2 FROM A STUD PROTRUDING FROM THE ANTI-ICE CROSS FLOW VALVE THAT HASDR DXTA2018102201583Actuator · unserviceablePRI STAB TRIM FAIL EICAS AMBER MESSAGE IN FLIGHT. PERFORMED THE APPROPRIATE QRH CHECKLIST, FOLLOWED BY THE EMERGENCY/ABNORMAL PROCEDURES, FLAPS NOT IN LANDING POSITION // SIGNOFF // REMOVED THE PRIMARY STAB TRIM ACTUATOR AND INSTALL A NEW SERVCEABLE PRIMARY ST
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