N324QS
Service difficulty reports · 26
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 = 'N324QS' 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 = 'N324QS' 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 DXTA2026062608572Battery Pack · inoperativeAFT LAV EMERGENCY EXIT LIGHT AND OVERHEAD LIGHT AS WELL AS THE AFT BULKHEAD EMERGENCY EXIT LIGHTS DO NO ILLUMINATE AS REQUIRED. GAINED ACCESS TO NR 3 AND 4 EMERGENCY LIGHT POWER SUPPLY. REMOVED BOTH POWER SUPPLYS AND INSTALLED 2 TRUE BLUE POWER EMERGENCY LIGHSDR DXTA2026061508434Light · malfunctionedEMER LIGHTS BY THE EMERGENCY EXIT AND EXTERIOR ARE INOP. EMER LIGHTS BY THE MAIN CABIN DOOR ARE STILL WORKING PROPERLY. ARRIVED AT AIRCRAFT, PERFORMED OPS CHECK OF EXTERIOR AND INTERIOR EMER LIGHTS. OPS CHECK GOOD. STARTED APU AND CHARGE THE EMERGENCY BATTERSDR DXTA2025112505794Check Valve · faultedAFTER DEPARTURE AND AFTER LIFTING THE GEAR RETRACTION HANDLE, THE RIGHT MAIN GEAR LIGHT REMAINED ILLUMINATED. THE TOWER ALSO CONFIRMED THAT THE RIGHT MAIN GEAR WAS STILL EXTENDED IN THE DOWN POSITION. WE RAN THE QRH AND EXTENDED THE LANDING GEAR AND ALL THREE SDR DXTA2025100105132Pump · leakingWHEN LEVEL IN FLIGHT, SELECTED CROSSFEED LEFT, AFTER APPROX 2 MIN SELECTED OFF AND RECEIVED AMBER FUEL BOOST PUMP ON RT, CONDUCTED QRH CHECKLIST AND COULD NOT CLEAR. CHECKLIST SAID TO LAND AS SOON AS PRACTICAL. THIS OCCURRED ON THE PREVIOUS FLIGHT/LEG. THE CASSDR DXTA2025092605080Brake Assy · vibrationTHE MLG BRAKE ASSY GENERATING FRICTION & DRAGGING WHEN BRAKES RELEASED & ACFT IN MOTION. ACFT GROUND BEHAVIOR IS SLIGHTLY PULL TO RT WITHOUT BRAKING APPLIED. CANNOT DETERMINE WHICH BRAKE SYS ON RT MLG MALFUNCTIONING. CARBON SMOKE EMANATING FROM RT MLG. VIBRSDR DXTA2025033102850Flap System · faultedFLAPS FAIL AMBER CAS: UPON FLAP SELECTION DURING APPROACH CAUSING A FLAPS FAIL CAS MESSAGE (ALSO TRIGGERED GRD PROX FAIL AND WINDSHEAR FAIL CAS MESSAGE). SYSTEM DID NOT RESET BY FOLLOWING QRC AND FLAPS FAIL STAYED ILLUMINATED. UPON POST FLIGHT NOTED FLAPS WERESDR 2025FA0000077Spar · corrodedMECHANICALLY REMOVED 3 AREAS OF CORROSION WITH 1 ADDITIONAL AREA LOCATED ON THE LH AFT WING SPAR, AFT FACE AROUND THE CARRY THROUGH FITTINGS INSIDE FLAP WELL BAY 523AB. MECHANICALLY REMOVED 1 AREA OF CORROSION LOCATED AROUND SPOILER HYDRAULIC PRESSURE LINE CARSDR 2025FA0000011Rib · corrodedLH MLG WING RIB LWS 52 INBD SIDE HAS 14 HI-LOK COLLARS WITH CORROSION AROUND THEM. MECHANICALLY REMOVED CORROSION LOCATED IN LH GEARWELL ON INBD/UPPER SIDE OF LWS 52.00 CROSSOVER RIB WHERE 14 HI-LOK'S PLUS 1 ADDITIONAL HI-LOK WERE REMOVED IAW C680 SRM 51-70-02SDR 2024FA0000966Door Frame · corrodedBLENDED TWO AREAS OF CORROSION FOUND ALONG THE EMERGENCY EXIT DOOR CONTOUR RINGS. REMOVED THE CONTOUR RINGS AND BLENDED ADDITIONAL CORROSION FOUND. PERFORMED NDT AND REPORTED RESULTS OR REPAIR DISPOSITION. EMERGENCY EXIT DOOR P/N 6911251-6 WAS SENT OUT FOR REPSDR DXTA2023091295230Unknown · unknownON ENTRY TO THE AIRCRAFT NOTICED THAT IN THE FULL DOWN POSITION WITH THE ENTRY HANDLE IN THE OVER CENTER LOCKED POSITION. THE DOOR IS NOT LOCKED DOWN IT STILL TRYS TO GO BACK UP ABOUT 2-3 INCHES. THE DOOR IS LOOSE AND NOT SECURED. WHEN WEIGHT IS PUT BACK OSDR DXTA2023063091890Unknown · unknownAFTER ENGINES ARE SHUTDOWN WITH APU RUNNING AND BLEED AIR ON APU, THE CABIN FILLS WITH A VERY HEAVY JET FUEL SMELL. THIS WAS POINTED OUT BY PASSENGERS AS WELL. WHEN AIRCRAFT WAS SHUTDOWN WINDS WERE CALM. REMOVED TEMP CONTROLLER AND INSTALLED OVERHAULED CONDITSDR DXTA2023011078290Light · failedCABIN EMERG LIGHT: TEST OF EMERGENCY LIGHTS FAILED. IN ARM POSITION, NO INTERIOR OR EXTERIOR LIGHTS ARE FUNCTIONING. IN ON POSITION, EXTERIOR LIGHTS FUNCTION BUT THE FORWARD SECTION OF INTERIOR LIGHTS ARE DEAD. THE BACK SECTION OF CABIN THE LIGHTS ARE DIM.SDR EBVR202305300001Unknown · unknownCORROSION WAS FOUND ON THE LH & RH AFT FUSELAGE SKIN ALONG THE AFT FUSELAGE CLOSEOUT FAIRING ATTACHMENT LINE. REPAIRED PER AQRD ERO 972834. THIS IS A MAJOR/PERMANENT REPAIR.SDR DXTA2021091748950Control Panel · defectiveCABIN ODOR: PRESSURIZATION CONTROLLER FAULT LIGHT ILLUMINATED IN FLIGHT, ACCOMPANIED BY LIGHT OILY SMELL IN COCKPIT AND CABIN AIR CONDITIONING SYSTEM. APU WAS RUNNING ON GROUND AND UP TO 10,000 FT AGL (T2PL6D008M0Y4). R & R PRESSURIZATION CONTROL IAW MM 21·31SDR JGVR20210126001Spar Web · corrodedREPAIRED CORROSION ON THE RT WING FWD SPAR WEB, IAW AEROSPACE QRD ERO-104487 REV: A TITLED "N324QS - RT WING MID SPAR WEB CORROSION REPAIR" DATE: JANUARY 26, 2021 AND SUPPORTED BY FAA FORM 8110-3 DATED JANUARY 26, 2021.SDR DXTA2020111204337Autopilot Sys · failedWHILE LEVELING AT FL260, FO FLYING FROM RIGHT SEAT, WE NOTED THE LEFT SIDE ALTIMETER WAS READING APPROXIMATELY 300' LOW AND VSI SHOWED A DESCENT. FD MODE OFF CAS MESSAGE CAME ON AND AUTOPILOT FAILED. WE VERIFIED THAT THE RIGHT SIDE SYSTEM WAS CORRECT AND DIVSDR JGVR20201029001Skin · damagedBLENDED 85 AREAS OF CORROSION ON THE UPPER SURFACE OF THE LOWER FUSELAGE SKIN AND STRINGERS, COMMON TO THE DROPPED AISLE FLOOR. PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREAS FOUND ACCEPTABLE. FABRICATED AND INSTALLED SDR JGVR201806054001Hinge Bracket · corrodedMECHANICALLY BLENDED CORROSION ON THE MIDDLE RUDDER HINGE BRACKET UPPER HINGE HALF ON VERTICAL STABILIZER NEAR THE BONDING STRAP HOLE, PERFORMED EDDY CURRENT AND ULTRASONIC THICKNESS INSPECTIONS AND SUBMITTED FINDINGS TO MANUFACTURER ENGINEERING. TREATED METALSDR DXTA2017062106414Transmitter · malfunctionedAT FL410 IN CRUISE FLAPS WENT TO 7 DEGREE AMBER INDICATION WITH ASSOCIATED FLAPS FAIL, GROUND PROX AND WINDSHEAR WARNINGS WITH ASSOCIATED AURAL WARNING. FLAPS DID NOT EXTEND, NO LIMITATION EXCEEDED. ON APPROACH, MATCHED 7 DEGREE INDICATION WITH FLAP HANDLE ANDSDR DXTA2015091106078Link · shearedDURING TAKEOFF ROTATION, A DISTINCT BUMP & REARWARD FORCE OCCURRED IN THE CONTROL YOKE. AS THE ACFT ACCELERATED, EXCESSIVE NOSE DOWN TRIM WAS REQUIRED. AT MAXIMUM NOSE DOWN SETTING -1.2, ANY SPEED ABOVE 156 KNOTS WAS OUT OF TRIM & REQUIRED FWD CONTROL YOKE FSDR DXTA2015062206034Transistor · failedWITH BATTERY POWER ON, THERE IS A STRONG ELECTRICAL ODOR, NO SMOKE. WHILE REPAIRING THE FLOOD LIGHTS, FOUND RESISTOR & TRANSISTOR BURNED OUT IN THE FLOOD LIGHT CIRCUIT. ODOR WENT AWAY AFTER REPLACING THESE COMPONENTS. FLOOD LIGHTS OPS CHECKED GOOD. IAW AMSDR DXTA2014052805785Monitor · failedRIGHT ENGINE VIBRATION MASTER WARNING, CLIMBING THROUGH 11,000 FT FOR 12,000 FT IN CLIMB DETENT. NO VIBRATION WAS PHYSICALLY FELT. REMOVED AND REPLACED ENGINE VIBRATION MONITOR IAW MM 77-20-00. REMOVED AND REPLACED RIGHT ENGINE VIBRATION ACCELEROMETER IAW MMSDR 2012F00127Pump · damagedEXTENSIVE FRETTING DAMAGE ON PRIMARY JET PUMPS WHERE CLAMP W991-18DE ATTACHES TO. DAMAGE ALSO OCCURS TO ADJACENT PLUMBING. DAMAGE IS NOT SEEN UNLESS CLAMPS ARE REMOVED.SDR DXTA2010122704380Adc · inoperativeAT FL410, STDBY HORIZON HAD RED X'S OVER AIRSPEED, AND ALTITUDE. ON DECENT THRU FL200 THE DATA DISPLAYED. INSTALLED A REPAIRED STBY ADC. OPS CHECKED GOOD. WORK DONE IAW MM 34-22-00 AND CH 34-11-00 AND FAR 91.411, PART 43, APPENDIX E.SDR DXTA2010012903960Pressure Switch · faultyRT ENG FUEL FILTER BYPASS AMBER CAS MESSAGE FL 410 REPEAT WRITE UP. R & R RT ENG FUEL FILTER AND PRESSURE SWITCH. OPS AND LEAK CHECKS GOOD AT THIS TIME. THERE ARE NO FURTHER CAS MESSAGES. ALL WORK DONE IAW MM, CHAPTER 73-10-03.SDR DXTA200802831Oxygen Mask · malfunctionedBOTH PILOT AND COPILOT OXYGEN MASK HAVE REDUCED OXYGEN FLOW, AS IF AN OBSTRUCTION OF VALVE FAILURE OCCURED. RESEATED OXYGEN MASKS OPS CHECKED SATISFACTORY IAW MM 35-00-00.
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