N558QS, cancelled Jul 8, 2025
Service difficulty reports · 23
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 = 'N558QS' AND deregistration_id = 'N558QS-2025-07-08' 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 = 'N558QS' AND deregistration_id = 'N558QS-2025-07-08' 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 DXTA2024120201277Precatch · faultedMAIN DOOR PRECATCH: WHEN OPENING THE MAIN CABIN DOOR FROM THE OUTSIDE THE DOOR WILL NOT RELEASE UNLESS THE PRECATCH IS PUSHED IN. FROM THE INSIDE THE DOOR WILL OPEN NORMALLY WITHOUT THE PRE CATCH BEING USED. SEE ATTAT HED VIDEO. CORRECTIVE ACTION; RESECURED SDR DXTA2024090900452Unknown · odorCOCKPIT ODOR: WHILE TAXIING FOR TAKEOFF, WE SUDDENLY GOT A STRONG HOT BURNING SMELL, IT HAD AN ELECTRICAL SMELL TO IT. CORRECTIVE ACTION: PERFORMED MULTIPLE ENGINE RUNS AND APU RUNS. PERFORMED TC-5XL-21-120902MR1 (ENVIRONMENTAL CONTROL SYSTEM BLEED AND TRIM AISDR DXTA2024032511297Door · bindingMAIN DOOR REQUIRES EXCESSIVE FORCE TO OPEN OR CLOSE LATCH. GAINED ACCESS TO MED BOLTING LINKAGE SYSTEM. FOUND PRECATCH LATCHING BOLT OUT OF ADJUSTMENT READJUSTED BOLTING SYSTEM LINKAGE. CHECKED DOOR SEVERAL TIMES FOR PROPER LATCHING AND RELEASE, OP CHECK GOOD.SDR DXTA2024013010757Handle · unknownMAIN DOOR PRECATCH: AFTER FLIGHT WHEN WE GO TO OPEN THE MAIN ENTRANCE DOOR. WE HAVE TO PULL THE PRECATCH HANDLE TO GET THE DOOR TO OPEN. ADJUSTED PRECATCH CABLE IMPROVE ACTUATION OF THE PRE CATCH, PRECATCH CONSISTENTLY DISENGAGES WHEN CABIN DOOR HANDLE GOES SDR DXTA2024012210667Fire Bottle · low pressureAT ALTITUDE, GOT A FIRE BOTTLE LOW ANNUNCIATOR. CREW RAN QRH & DECLARED AN EMERGENCY. FIRE DEPART CHECKED ACFT & OBSERVED NO EVIDENCE OF FIRE. THERE ISN'T A WAY TO VERIFY WHICH FIRE BOTTLE WOULD HAVE TRIGGERED ANNUNCIATOR. FOUND NO CASS MESSAGE AT ARRIVAL TOSDR DXTA2023052687120Unknown · unknownMAIN DOOR PRECATCH: THE PRE CATCH WILL NOT RELEASE THE MAIN CABIN DOOR. // SIGNOFF// ADJUSTED MED PRE CATCH IAW CE 560XL AMM 52-10-01. MED PRE CATCH OPERATIONAL CHECK GOOD AT THIS TIME.SDR EBVR202304280001Unknown · unknownEMERGENCY EXIT INTERIOR REVEAL PANEL FASTENERS RUB ON EMERGENCY EXIT DOOR SURROUND DOUBLER. FASTENERS ARE RUBBING DEEP WEAR MARKS OR HOLES IN THE STRUCTURAL DOUBLER.SDR DXTA2023040483590Unknown · unknownRIGHT ENGINE FIRE DETECTION LIGHT: DURING CLIMB OUT FROM DAL THROUGH 12000 FT THE RH ENGINE FIRE LIGHT ILLUMINATED AND EXTINGUISHED A FEW SECONDS LATER THE LIGHT ILLUMINATED AGAIN AND EXTINGUISHED. NO ENGINE SHUT DOWN WAS REQUIRED PER CHECKLIST AND NO FIRE BOTSDR DXTA2022090769860None · noneMAIN DOOR: WHEN MAIN CABIN ENTRY DOOR IS OPEN, TOP HINGED STEP IS LOOSE AND MOVES WHEN STEPPED ON. DISCOVERED BROKEN HARDWARE CLIP NEXT TO STEP.SDR DXTA2022060363240Isolator · leakingLEFT ENGINE ENGINE VIBRATION: ENGINE VIBRATION OCCURRED ABOVE 10K WHEN REDUCING POWER SETTING FROM CLIMB POWER TO CRUISE. VIBRATION CAME BACK AS WE WENT BACK TO CLIMB THEN AGAIN WHEN WE REDUCED POWER. VIBRATION ALSO OCCURRED DURING LIGHT TURBULENCE LEVEL FLIGHSDR DXTA022220213845Screw · brokenMAIN DOOR HANDLE: MAIN ENTRANCE DOOR INSIDE HANDLE BROKEN. HANDLE MOVES FREELY. REMOVED STEPS AND INSPECTED HANDLE ASSY, FOUND BOTH SCREWS ATTACHING THE HANDLE TO THE SHAFT SHEARED OFF. REMOVED FAILED FASTENERS AND REPLACED WITH NEW. REINSTALLED STEPS. DOSDR DXTA2021010804570Bulb · burned outEMERGENCY LIGHT OVER SEAT 7 INOPERABLE. REMOVED AND REPLACED BURNT OUT BULB, IAW CE-560XLS AMM 33-20-00, ALL CHECKS GOOD AT THIS TIME.SDR DXTA2019120213138Circuit Card · defectiveRIGHT ENGINE FIRE DETECTION LIGHT INTERMITTENT - IN FLIGHT AT FL280, THE R/H ENGINE FIRE WARNING LIGHT FLICKERED ON AND OFF CONTINUOUSLY FOR APPROXIMATELY FIVE MINUTES. THERE WERE NO SECONDARY INDICATIONS OF A POSSIBLE ENGINE FIRE. WING AND ENGINE ANTI ICE WERSDR DXTA2019112503113Motor · defectiveBOV INTERMITTENT - AT FL410, FO MADE A SLIGHT POWER INCREASE WHEN WE HEARD A FLUTTERING FOUND/POSSIBLE COMPRESSOR STALL FROM LEFT ENGINE. LEFT ENGINE ITT WENT UP AND DOWN ABOUT 100 POINTS. THE RANGE WAS BETWEEN 500 AND 600 DEGREES. THIS HAPPEN TWICE IN FLIGHSDR DXTA2019051302380Fire Warning · false activationRIGHT ENGINE FIRE DETECTION LIGHT INTERMITTENT - RT ENGINE FIRE LIGHT ILLUMINATED INTERMITTENT AT CRUISE ALTITUDE. CORRECTIVE ACTION, VISUALLY INSPECTED RT ENGINE FIRE LOOP FOUND NO DEFECTS. RAN ENGINE AT VARIOUS POWER SETTINGS WITH ENGINE ANTI-ICE ON AND OFFSDR JGVR20180914001Spar Cap · corrodedREPAIRED CORRODED AREA ON THE LT FWD VERTICAL STABILIZER SPAR CAP, WHERE ACCESS PANEL 340ATC ATTACHES, BY BLENDING, TRIMMING SPAR WEB AND CHAMFERING THE SPAR CAP, TREATING AND PRIMING IAW FIELD REPAIR FR-560-5568-4523 REVISION (-) APPROVED BY FAA FORM 8100-9 DSDR DXTR2017040801Skin · crackedTHE RT ELEVATOR HAS A CRACK ON THE LOWER SKIN AT THE OUTBOARD HINGE CUTOUT. THE CRACK MEASURES APPROXIMATELY 0.25 INCHES LONG.SDR DXTA2016090600177Spar · corrodedLEFT HORIZONTAL STABILIZER REAR SPAR CORRODED.SDR DXTA2016090600412Spar · corrodedLEFT WING AFT SPAR SPLICE CORROSIONSDR DXTA2016F00184Spar · corrodedLEFT HORIZONTAL STABILIZER REAR SPAR CORROSION BETWEEN SS 9.3 TO SS 19.00.SDR DXTA2016072206269Display · malfunctionedPILOT SIDE PRIMARY FLIGHT DISPLAY GOT EXCESSIVELY HOT AND BURNED A HOLE IN THE IMAGE. R & R NR 1 PFD WITH NEW, REPAIRED UNIT IAW AMM 34-26-00. OPS CHECK GOOD INSPECTED CONNECTOR BEHIND PFD 1 WITH NO DEFECTS.SDR DXTA2014092505893Brake Sys · contaminatedDURING TAXI THE ACFT PULLS HARD TO THE LT WHEN EVEN BRAKE PRESS APPLIED FROM THE RT SEAT. OPERATIONS CHECKED BRAKES & LT BRAKE FEELS SPONGY. HOOKED BRAKE BLEEDING HOSE & COMPLIED WITH BRAKE BLEEDING PROCEDURE IAW MM CH 32-44-00. REMOVED A LOT OF AIR OUT OFSDR DXTA2014091505882Metering Valve · unserviceableDURING TAXI AT SLOW SPEED RT BRAKE GRABS & PULLS ACFT TO THE RT. ALSO MAKES AN AUDIBLE NOISE. REPLACED BRAKE METERING VALVE WITH A UNIT OVH'D. OPERATIONAL CHECK AND LEAK CHECK SATISFACTORY. ALL WORK IAW CE-560XL MM CH 32-44-20.
Back to N558QS, cancelled Jul 8, 2025