N308QS
Service difficulty reports · 43
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 = 'N308QS' 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 = 'N308QS' 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 DXTA2026012006591Battery Pack · faultyRIGHT FORWARD EXTERIOR EMERGENCY LIGHT DOES NOT COME ON DURING EMERGENCY LIGHT TEST. REMOVED NR 3 BATTERY. INSTALLED CUSTOMER SUPPLIED NEW EMER BATTERY. OPS CHECKED GOOD. WORK DONE IAW AMM 33-50-10. NO DEFECTS NOTED.SDR DXTA2026011606557Light · inoperativeDURING EMERGENCY LIGHT PREFLIGHT CHECK THE FORWARD OVER WING LIGHT, SEAT 8 LIGHT, AND AFT WALL EXIT SIGN LIGHT DID NOT ILLUMINATE. WE POWERED UP THE AIRPLANE TO DO THE REST OF THE PREFLIGHT CHECKS AND ALL EMERGENCY LIGHTS ILLUMINATED EXCEPT THE AFT WALL EXIT SSDR DXTA2025053003669G Switch · trippedUPON SHUTDOWN EMER LIGHTS WOULD NOT EXTINGUISH. RESET PILOT/CP 5G SWITCH AND ATTEMPTED POWER CYCLE RESET WITH NEGATIVE RESULT. CORRECTIVE ACTION: CONFIRMED THE ISSUE AND WORKED THROUGH T/S WITH MCC. AND DETERMINED THAT A G·SWITCH HAS BEEN ACTIVATED, FOUND THESDR DXTA2025052303593Actuator · tightDURING CLIMBOUT PASSING 32000 WE GOT A VERY NOTICABLE THUD IN THE COCKPIT FLOOR, A "BUMP IN THE NIGHT". IT COULD BE FELT AND HEARD. IT HAPPENED 3 MORE TIMES AND WERE LESS INTENSE. THE LAST ONE OCCURRED AT CRUISE AT 40000. THERE WERE NO ABNORMAL COCKPIT INDSDR DXTA2025031702721Battery · defectiveBATTERY O'TEMP L RED CAS: AT APPROXIMATELY 4000 FEET ON CLIMB OUT RED MASTER, WARNING, LIGHT, ORAL ALERT, AND BATTERY OVER TEMP LEFT CAS MESSAGE ILLUMINATED. ACCOMPLISHED QRC CHECKLIST. LEFT BATTERY APPEARED TO BE APPROXIMATELY AT 50°C AND RIGHT AT 35°C ONCESDR JGVR20250214001Door · corrodedBLENDED MULTIPLE AREAS OF CORROSION ON THE EMERGENCY EXIT DOOR P/N 6911251-4, REMOVED CONTOUR RING FOR ACCESS AND BLENDED ADDITIONAL AREAS OF CORROSION PERFORMED NDT AND SENT DOOR OUT FOR REPAIRS. REINSTALLED REPAIRED DOOR P/N 6911251-4.SDR JGVR20250123001Spar · corrodedMECHANICALLY REMOVED 3 AREAS OF CORROSION LOCATED IN LH MLG WHEEL WELL, AFT WING SPAR LOWER CLIP INBOARD OF BAY 730DL PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED BLENDED AREAS PER TEXTRON REPAIR MEMO.SDR JGVR20250117001Skin · corrodedMECHANICALLY BLENDED 3 AREAS OF CORROSION UNDER RH LOWER WING SKIN, AFT SIDE, INBD OF FLAP PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED BLENDED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR DXTA2024111401130Pressure Switch · faultedFUEL PRESSURE LOW L AMBER CAS: AFTER TAKEOFF ABOUT 300 FT AGL WE RECEIVED THE FUEL PRESSURE LOW L CAS MESSAGE. RAN THE QRH MESSAGE DID NOT CLEAR. ON FINAL BACK INTO PWK THE MESSAGE CLEARED CORRECTIVE ACTION; REPLACED LH ENGINE FUEL PRESSURE SWITCH IAW CE 680 ASDR 2024F00201Spar Cap · corrodedCORROSION WAS FOUND ON THE 6922435-4 REAR SPAR CAP, LOWER FORWARD ANGLE-RH, NEAR RWS 41. ACCOMPLISHED FIELD REPAIR: FR-680-0116-1466 REV -, FIELD REPAIR-CORROSION, RH WING LOWER AFT SPAR CAP, RWS 39.4-43.2.THE DAMAGE WAS BLENDED OUT AND THE REMAINING THICKNESSSDR EBVR450D121923001Attach Fitting · corrodedFRETTING CORROSION ON AFT HORIZONTAL ATTACH FITTINGS, ON THE HORIZONTAL STAB AND VERTICAL STAB. TEXTRON ENGINEERING PER MINOR RECOMMENDED REPAIR MEMO DQ40986M1 DATED 9-8-2023 RESTORE PAINT PROTECTION AND APPLY CORROSION INHIBITING SOLID FILM LUBRICANT.SDR DXTA2023012378980Fuse · blownCABIN EMERGENCY LIGHTS INOP. EXIT SIGN OVER MAIN CABIN DOOR INOPERATIVE. EXIT SIGNS LT AND RT OF MAIN CABIN DOOR INOPERAITVE. EMERGENCY LIGHT OVER GALLEY INOPERATIVE. AFTER REPLACING #1 BATTERY PACK BLOWN FUSE AND PERFORMING FULL OPERATIONAL CHECK OF THE BATTSDR DXTA2023011778680Apu · defectiveAFTER STARTING APU, AND AFTER TURNING BLEEDS ON CABIN, AND FLIGHT DECK STARTED TO FILL WITH A THICK HAZE FROM THE INTERIOR OUTLETS. APU REMOVED AND REPLACED IAW AMM 49-00-00SDR 3J7R2023011200001Power Supply · blownTHE FORWARD EMERGENCY LIGHTS IN THE CABIN AT THE CABIN DOOR ARE INOP, AT LEAST THREE SIGNS ARE OUT. THESE INCLUDE THE EXIT SIGN IN THE OVERHEAD AND THE EXIT SIGNS AT KNEE LEVEL IN THE DOOR WAY.TROUBLESHOT AND FOUND THE FUSE BLOWN ON THE #1 POWER SUPPLY. ISOLATSDR DXTA2022122376910Battery Pack · defectiveWHEN THE PASSENGER SAFETY PUSH SWITCH WAS TURNED ON DURING DESCENT, NONE OF THE EMERGENCY LIGHTS ILLUMINATED. WITH THE EMERGENCY LIGHTS SWITCH IN THE ARM POSITION AND THE PAX SAFETY SWITCH ON, ALL EMERGENCY LIGHTS SHOULD ILLUMINATE. UPON FURTHER INVESTIGATION SDR DXTA2021122854310Unknown · unknownCABIN EMERG LIGHT: CABIN EMERGENCY LIGHTS INOP. WOULD NOT COME ON DURING PREFLIGHT, LIGHTS WORK ON NORMAL BATTERY POWER. (PRE-FLIGHT) // SIGNOFF // COMPLIED WITH TC-FLT ·33-1001 ;CESSNA 680 / 680A / 700 / EMBRAER EMERGENCY LIGHTING POWER SUPPLY REV 0 DATED 15DSDR JGVR20210429001Spar · corrodedBENDED CORRODED ARE AROUND THE LH WING MIDDLE SPAR AFT SIDE AROUND THE BRAKE LINE BULKHEAD FITTING, PERFORMED ULTRASONIC THICKNESS INSPECTION AND REPORTED FOR REPAIR DISPOSITION. CLEANED AND TREATED BLENDED AREA, APPLIED PRIMER AND TOPCOAT IAW TEXTRON REPAIR SDR DXTA030120213881Pcb · defectiveWING ANTI-ICE COLD L AMBER CAS: AT FL220 IN ICING CONDITIONS, WING ANTI-ICE COLD L&R AMBER MSG ILLUMINATED. DUE TO ATC CONDITIONS AND COMM ISSUES, WE DECLARED AN EMERGENCY TO GET AN IMMIDIATE CLIMB TO FL270 AND OUT OF ICING CONDITIONS. ONCE AT FL270, AND CLEARSDR 2020FA0000558Spar Cap · corrodedVERTICAL STABILIZER AFT SPAR CAP DAMAGE (CORROSION). ENGINEERING MEMO DQ28088M1 DATED DECEMBER 7, 2020.SDR DXTA2020111504357Battery Pack · inoperativeEMERGENCY LIGHTS ON RIGHT SIDE INOPERABLE. 2 RIGHT SIDE EXTERIOR OVER WING, RIGHT SIDE SHARK LIGHT, INTERIOR LAV OVERHEAD AND EXIT LIGHTS, AFT FLOOR LIGHTING, RIGHT SIDE AFT READING LIGHT ALL INOPERABLE. APU WAS RUN FOR 1/2 HOUR AND NO CHANGE TO STATUS. CORRSDR DXTA2020092804144Battery Pack · inoperativeEMERGENCY LIGHTS DO NOT ILLUMINATE WHEN SWITCH IS PLACED TO ARM WITH BATTERIES OFF. FOUND DURING PREFLIGHT. R & R THE NR 1 EMERGENCY BATTERY, CHARGED BATTERY WITH AIRCRAFT SYSTEM ON PERFORMED OPERATIONAL CHECK, ALL CHECKED GOOD. WORK DONE, IAW CE-680 CHAPT SDR DXTA2020011303322Actuator · malfunctionedRIGHT MLG LANDING GEAR RETRACTION DID NOT RETRACT - RIGHT MAIN DID NOT RETRACT. THE NOSE AND LEFT MAIN RETRACTED NORMALLY. THE RED UNLOCK LIGHT WENT OUT WITH THE RIGHT MAIN DOWN AND LOCKED GREEN LIGHT ON. THE RIGHT MAIN NEVER UNLOCKED AND RETRACTED. DISCONNESDR DXTA2019123093266Converter · dirtyCABIN ODOR OIL SMELL - AT 45000 SLIGHT ORDER AND A LOT OF HAZE IN CABIN. DROPPED OX MASK, RAN CHECK LIST . SELECTED L PRESSURE SOURCE , CABIN CLEARED. REMOVED OILED LEFT OZONE CONVERTER WITH NEW UNIT IAW MM 21-71-00. REMOVED DIRTY COALECER SOCK WITH NEW UNITSDR DXTA2019071502611Engine · malfunctionedREPEAT WRITE UP. DECENDING FROM FL410, POWER WAS REDUCED TO IDLE. AIRCRAFT BEGN TO SHUDDER AND RIGHT ENGINE SHUTDOWN CAS MESSAGE DISPLAYED. RIGHT ENGINE UNCOMMANDED SHUTDOWN FOLLOWED BY AUTO RELIGHT. DID NOT REDUCE POWER TO IDLE AGAIN UNTIL LANDING. NO OTHER SDR DXTA2019061402501Bleed Valve · abnormalAT FLIGHT LEVEL 43000 WE WERE CLEARED TO DECENT TO 35000. AS WE REDUCED THRUST LEVERS TO IDLE, FELT A RUMBLE, CYAN RIGHT ENGINE SHUTDOWN CAS MESSAGE. RIGHT ENGINE SHUTDOWN FOR A SPLIT SECOND AND RE-LIT IMMEDIATELY. REST OF FLIGHT INTO KMDW NORMAL.// SIGNOFF//PSDR DXTA2019052302430Solenoid · abnormalSHORTLY AFTER INITIATING DESCENT FROM FL430, AND EVENTUALLY AT FLIGHT IDLE, EXPERIENCED TWO SHORT BURSTS OF ENGINE VIBRATION, AND NOTICED THAT THE CYAN ENGINE SHUTDOWN R CAS MESSAGE BRIEFLY DISPLAYED THEN EXTINGUISHED. NO FURTHER VIBRATIONS WERE FELT DURING SDR DXTA2019F00018Spar Cap · damagedRT WING FORWARD SPAR CAP ANGLE REPAIR. ACCOMPLISHED IAW AQRD ENGINEERING ORDER ERO-102798 DATED 01/15/2019.SDR JGVR20180316002Structure · corrodedCORRODED AREAS ON THE UPPER AND LOWER SURFACES OF THE EMERGENCY EXIT DOOR ALONG THE CONTOUR RINGS. BLENDED THE CORROSION. PERFORMED EDDY CURRENT INSPECTION FOR CRACKS, NO CRACKING INDICATIONS FOUND. PERFORMED ULTRASONIC THICKNESS INSPECTION. REPLACED TWO BLSDR JGVR20180316001Skin · corrodedREPAIRED TWO CORRODED AREAS ON THE UPPER LT WING SKIN AT WS 37 NEAR THE DRAG ANGLE.SDR DXTA20170406156Skin · debondedREPAIR OF NOSE SKIN DISBONDS AROUND ACCESS DOOR OPENINGS. REPAIRED.SDR DXTA2014060905797Bearing · failedWHEN STOPPING THE ACFT ON THE RAMP BOTH MAIN GEAR BRAKES GROWL & GRAB WHEN MAKING A COMPLETE STOP. TAXIED ACFT FOUND LT & RT BRAKE GROWLING AT VERY SLOW SPEEDS. JACKED ACFT & REMOVED ALL FOUR MAIN WHEEL ASSEMBLIES, REMOVED ALL BEARINGS & CLEANED BEARINGS. CSDR DXTA2014021005643Water Separator · dirtyINFLIGHT AT FL 430 PAX COMPLAINED OF SOMETHING BURNING. WE SMELLED IT IN THE FLIGHT DECK., I WENT TO THE BACK & THE ODOR WAS STRONGEST NEAR THE LAVATORY. CREW DONNED MASKS UPON INITIAL SMELL, RAN ALL CHECKLISTS & DIVERTED THE FLIGHT. PERFORMED OZONE CONVERTSDR DXTA2013090305491Converter · failedWHILE RUNNING APU, NOTICED ODOR LIKE DIRTY SOCK. AFTER TAKEOFF, NOTICED ODOR LIKE BURNING OIL. NO SMOKE SEEN. REMOVED AND CLEANED OZONE CONVERTERS REMOVED AND CLEANED HEAT EXCHANGER. RE-INSTALLED HEAT EXCHANGER, PER NETJETS REPLACED R/H OZONE CONVERTER. CSDR DXTA2013081905478Coalescer Bag · contaminatedON GROUND, DURING APU START WITH BATTERIES, CABIN FILLED WITH WHITE SMOKE. APU BLEED AIR AND GENERATOR SWITCHES ON. ENVIROMENTAL SWITCHES AUTO AND COLD. WHITE SMOKE SEEMED TO BE ATOMIZED OIL AND NOT A HARSH ODOR. REMOVED WATER SEPARATOR AND FOUND SOCK TO BSDR DXTA2013081305474Pump · leakingENVIRONMENTAL SMOKE NOTICED FROM FRONT WEMAC VENTS. MORE PRONOUNCED IN HP MODE AND DURING POWER REDUCTION. CHECKLIST WAS USED AND IT WOULD SEEM TO BE ISOLATED TO THE LEFT PRESSURE SOURCE. DETERMINED SMOKE TO BE FROM RT ENGINE. REPLACED RT ENGINE OIL PUMP DUSDR DXTA2013020705278Strut · damagedON DEPARTURE GEAR WOULD NOT RETRACT. 3 GREEN AND RED UNLOCK ILLUMINATED. PUT THE GEAR HANDLE BACK DOWN TO MATCH 3 GREEN CONDITION. SHORTLY AFTER, AMBER "WOW MISCOMPARE" CAS MESSAGE ILLUMINATED. RAN CHECKLIST AND DIVERTED. CAS MESSAGE EXTINGUISHED ON TOUCHDSDR CWQR20120613040Cable · frayedDURING A SCHEDULED MX EVENT, FOUND THE PILOT'S RT BRAKE CONTROL CABLE FRAYED ABOUT 50 PERCENT. DID NOT SEE ANY ISSUES WITH THE CABLE RUN OR RUBBING ON STRUCTURE, ETC.SDR DXTA2011121904826Flap System · failedWHEN SELECTING FLAPS 15, FLAPS FAILED, AMBER CAS MESSAGE DURING APPROACH AT 180KTS. OBSERVED BITE CODES 5 & 8 ON AFT BAY CONTROLLER. OPS CK OF FLAPS GOOD. MCC REQUEST INSTALLED NEW SOFT START MODULE. OPS CHECKED GOOD. WORK DONE IAW MM 27-51-00.SDR DXTA2011030704495Packing · damagedUPON GEAR RETRACTION, NOSE GEAR MADE SEVERAL LOUD "BANGS" WHILE ENTIRE AIRCRAFT SHUDDERED AND VIBRATED. AFTER APPROX 10 SECONDS, NOSE GEAR FINALLY FULLY RETRACTED AND UNSAFE LIGHT EXTINQUISHED. ON GEAR EXTENSION FOR LANDING, WOW MISCOMPARE CAUTION ILLUMINATED SDR DXTA2010111504306Ecu · inoperativeWITH APU "ON" AND APU BLEED "ON", SMOKED FILLED COCKPIT. FOUND ECU TURBINE TO BE NOT OPERATING. R & R ECU TURBINE. OPS AND LEAK CHECKED GOOD. IAW MM 21-51-00.SDR DXTA2010031904042Downlock Switch · failedRT GREEN GEAR INDICATOR LIGHT ILLUMINATED DURING FLIGHT. NO GEAR UNSAFE LIGHT WAS ASSOCIATED WITH IT. REMOVED RT MAIN GEAR DOWNLOCK SWITCH AND INSTALLED NEW SWITCH IAW MM 32-30. OPS CHECK IS GOOD.SDR DXTA200702562Warning Light · false indicationGEAR UNLOCK LIGHT REMAINED ILLUMINATED. CYCLED GEAR ONE TIME. PERFORMED VISUAL INSPECTION OF LANDING GEAR UPLOCK SYSTEM. NO DEFECTS NOTED. VERIFIED PROPER ENGAGMENT OF ALL (3) UPLOCK SWITCHES WITH GEAR IN THE WELL. CYCLED GEAR SEVERAL TIMES AND PERFORMED INDICSDR DXTA200702309Lever · out of adjustSPEED BRAKE LEVER DOES NOT STAY IN THE FULLY DEPLOYED DETENT, IT TENDS TO (SPRING) BACK TO A HALF DEPLOYED POSTION. ADJUSTED SPEED BRAKE LEVER DETENT. OPERATIONAL CHECK NORMAL IAW MM 76-10-00.
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