N305QS, cancelled Feb 18, 2026
Service difficulty reports · 70
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 = 'N305QS' AND deregistration_id = 'N305QS-2026-02-18' 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 = 'N305QS' AND deregistration_id = 'N305QS-2026-02-18' 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 DXTA2025111105628Switch · out of positionIAW PREFLIGHT CHECKS THE EMERGENCY LIGHT SWITCH WAS PLACED TO ON POSITION. NONE OF THE EMERGENCY LIGHT ILLUMINATED. PER DISCUSSION WITH MAINTENANCE A 30 MINUTE CHARGE CYCLE IS NOT AUTHORIZED ON THE DISCREPANCY 5.1: IW PREFLIGHT CHECKS THE EMERGENCY LIGHT SWITCSDR DXTA2025110705559Battery Pack · defectiveTWO FORWARD RIGHT EXTERIOR , ONE MAIN CABIN ENTRY, THREE MAIN CABIN OVERHEAD EMER LIGHTS REMAINED INOP AFTER 2 30 MINUTE CHARGE CYCLES. REPLACED BATTERY PACKS. OPS CHECK GOOD. IAW MM 33-50-10SDR DXTA2025082704732Warning Message · false activationMED WAS CLOSED WITH THE KEYLOCK IN THE LOCKED POSITION. THE CABIN DOOR CAS MESSAGE ILLUMINATED. COULD NOT DUPLICATE. MAINTENANCE PERFORMED IAW 52-10-00 AND 52-20-00.SDR DXTA2025052203567Light · unknownEMERGENCY EXIT LIGHT ON LAV SEAT DOES NOT ILLUMINATE(PRE-FLIGHT) COMPLETED OPS CHECK OF THE EMERGENCY LIGHTING SYSTEM IAW MM 33-50-00. OPS CHECK GOOD AT THIS TIME.SDR JGVR20250517001Hinge Fitting · corrodedBLENDED CORRODED AREAS ON THE UPPER AND LOWER BRACKETS OF THE UPPER RUDDER HINGE AT THE BONDING STRAP BOLT HOLE, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED BLENDED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR JGVR20250515001Frame · crackedFOUND CRACK IN THE MID FRAME OF THE NOSE LANDING GEAR WHEEL WELL, CUT OUT CRACKED AREA, PERFORMED NDT, FABRICATED AND INSTALLED REPAIR DOUBLER AND SHIMS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR JGVR20250512001Skin · damagedBLENDED CORRODED AREAS LOCATED ON THE UPPER SURFACE OF THE UPPER WING SKINS LOCATED UNDER AND ADJACENT TO THE LH WING AFT DRAG ANGLE (WING-TO-FUSELAGE FAIRING STRUCTURE), AND THE RH WING MIDDLE AND AFT DRAG ANGLES, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSISDR JGVR20250506001Skin · corrodedREPAIRED THE CORRODED FUSELAGE SKIN AT THE LOWER TCAS ANTENNA CABLE FEED-THROUGH BY BLENDING CORRODED AREAS, PERFORMING NDT AND REPORTING FOR REPAIR DISPOSITION, FABRICATED AND INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH AVIATION QUALITY RESEARCH AND DEVELOPMESDR JGVR20250429001Attach Bolt · corrodedMECHANICALLY REMOVED AREAS OF CORROSION LOCATED ON LH ELEVATOR CABLE PULLEY ATTACHMENT BRACKET LOCATED INSIDE BELLY PANEL BAY 154AC AND EXTENDING FORWARD SEVERAL INCHES ONTO FUSELAGE STIFFENER AND DRAIN ATTACHMENT RIVETS PERFORMED NDT AND REPORTED FOR REPAIR DSDR JGVR202504007006Panel · corrodedMECHANICALLY REMOVED 2 AREAS OF CORROSION FROM LH WING TRAILING EDGE PANEL 532GB, PERFORMED NDT, REPORTED FOR REPAIR DISPOSITION, CLEANED, TREATED, AND, PRIMED PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR JGVR202504007005Bulkhead · corrodedMECHANICALLY REMOVED CORROSION LOCATED IN RH MLG WHEEL WELL AT MIDDLE EMERGENCY BRAKE LINE CARRY THRU ON WS 52.00 INBOARD SIDE, PERFORMED NDT, REPORTED FOR REPAIR DISPOSITION, CLEANED, TREATED, AND, PRIMED PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR JGVR202504007004Bulkhead · corrodedMECHANICALLY REMOVED CORROSION LOCATED IN LH MLG WHEEL WELL AT MIDDLE EMERGENCY BRAKE LINE CARRY THRU ON WS 52.00 INBOARD SIDE, PERFORMED NDT, REPORTED FOR REPAIR DISPOSITION, CLEANED, TREATED, AND, PRIMED PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR JGVR202504007003Hinge Bracket · corrodedREMOVED 3 AREAS OF CORROSION LOCATED ON LH #1 SPOILER OUTBOARD HINGE BRACKET, PERFORMED NDT, REPORTED FOR REPAIR DISPOSITION, CLEANED, TREATED, AND, PRIMED PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR JGVR202504007001Attach Fitting · chafedMECHANICALLY REMOVED CHAFFING MARKS ON RH MIDDLE WING ATTACHMENT FITTING, PERFORMED NDT, REPORTED FOR REPAIR DISPOSITION, CLEANED, TREATED, AND, PRIMED PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR JGVR20250402004Structure · corrodedREPAIRED CORRODED AREAS OF THE AFT TAILCONE SKINS LOCATED UNDER AND ADJACENT TO THE AFT CHIN FAIRINGS, BY R&R THE FAIRINGS, BLENDING CORRODED AREAS, PERFORMING NDT AND REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLING REPAIR DOUBLERS IN ACCORDANCE WSDR JGVR20250402003Pulley Bracket · corrodedMECHANICALLY REMOVED 1 AREA OF CORROSION FROM LH ELEVATOR CABLE PULLEY BRACKET LOCATED INSIDE LOWER TAIL ACCESS BAY 323AC, PERFORMED NDT, REPORTED FOR REPAIR DISPOSITION, CLEANED, TREATED, AND, PRIMED PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR JGVR20250402002Fitting · corrodedMECHANICALLY REMOVED CORROSION LOCATED ON LH AND RH MLG WHEEL WELL WS 37.00 FWD END, EMERGENCY BRAKE LINE CARRY THRU FITTINGS, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED BLENDED AREAS PER MRO ENGINEERING REPAIR ORDER.SDR JGVR20250402001Spar · corrodedREPAIRED CORRODED AREA IN THE LH MLG WHEEL WELL ON THE AFT WING SPAR LOWER CLIP IN BAY 730DL, PERFORMED NDT, REPORTED FOR REPAIR DISPOSITION, CLEANED, TREATED, AND, PRIMED PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR JGVR20250331003Spar · corrodedREPAIRED TWO CORRODED AREAS IN THE RH MLG WHEEL WELL ON THE AFT WING SPAR LOWER CLIP, PERFORMED NDT, REPORTED FOR REPAIR DISPOSITION, CLEANED, TREATED, AND PRIMED PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR JGVR20250331002Spar Web · corrodedREPAIRED CORRODED AREAS AT OF THE LH WING AFT SPAR WEB AFT FACE AT THE #4 SPEED BRAKE PANEL HYDRAULIC LINE CARRY-THRU FITTINGS, PERFORMED NDT, REPORTED FOR REPAIR DISPOSITION, CLEANED, TREATED, AND, PRIMED PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR JGVR20250331001Skin · corrodedREPAIRED CORRODED AREA OF THE RIGHT WING LOWER SKIN JUST OUTBOARD OF THE MAIN JACKPOINT BY BLENDING AREA, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, CLEANING, TREATING, AND PRIMING REPAIR AREA PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR JGVR20250317003Skin · corrodedBLENDED AREA OF CORROSION FROM FUSELAGE SKIN LOCATED AFT OF E-EXIT DOOR OPENING, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS BY CLEANING, TREATING AND PRIMING IAW NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR JGVR20250317002Skin · corrodedMECHANICALLY REMOVED 2 AREAS OF CORROSION FROM LH LOWER WING SKIN TRAILING EDGE JUST INBD OF FLAP ISLAND, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS BY CLEANING, TREATING AND PRIMING IAW NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR JGVR20250317001Door · corrodedBLENDED MULTIPLE AREAS OF CORROSION ON THE EMERGENCY EXIT DOOR, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS BY CLEANING, TREATING AND PRIMING IAW NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR DXTA2024040811427Cable · reads highDOOR MECHANISM NOT BALANCED. VERY DIFFICULT TO OPEN AND CLOSES VIOLENTLY. ADJUSTED CABIN DOOR CABLES FORWARD AND AFT AFTER FINDING TENSIONS TO BE EXTREMELY HIGH. CABLE TENSIONS SET TO CORRECT RANGE AND OPS CHECK OF MAIN CABIN DOOR IS GOOD. IAW MM 52-10-50.SDR 2024F00079Spar Cap · corrodedCORROSION, LH/RH WING, LOWER FORWARD REAR SPAR CAP, W.S. 17-46.SDR 2024FA0000229Fairing · corrodedR/H ELEVATOR WEDGE FAIRING SKIN CORROSION BLEND-OUT.SDR 2023FA0000475Spar Web · corrodedCORROSION AROUND AFT SPAR GEAR EXTEND AND RETRACT FEED-THROUGHS RH WHEEL WELL. ACCOMPLISHED TEXTRON AVIATION FIELD REPAIR S-680-ATA-57/03RD.SDR 2023FA0000474Spar Web · corrodedCORROSION AROUND AFT SPAR EMERGENCY EXTENSION AND EMERGENCY BRAKE FEED-THROUGHS LH WHEEL WELL. ACCOMPLISHED TEXTRON AVIATION FIELD REPAIR S-680-ATA-57/03RD.SDR 2023F00259Spar Web · corrodedCORROSION AROUND AFT SPAR GEAR EXTEND AND RETRACT FEED-THROUGHS RH WHEEL WELL. ACCOMPLISHED TEXTRON AVIATION FIELD REPAIR S-680-ATA-57/03RD.SDR 2023F00258Door · damagedTWO FASTENERS (1EA SCREW AND 1EA 1/4 TURN) HAVE GOUGED THE STRUCTURE ABOVE THE EMERGENCY EXIT DOOR P/N 6711141-30.SDR DXTA2023071090550Unknown · unknownCABIN EMERG LIGHT: THE EMERGENCY LIGHTS ON BATTERY PACK NUMBER 1 ARE NOT FUNCTIONING PROPERLY. //SIGNOFF// REMOVED WORN CABIN EMERGENCY LIGHT BATTERY PACK P/N: CBS28-1 S/N: 000342 WITH A DOM OF 04/15 AND INSTALLED REPAIRED P/N: CBS28-1 S/N:006929 WITH A DOM OFSDR DXTA2023061288360Unknown · unknownEMERG LIGHT SWITCH: NO INTERIOR OR EXTERIOR EMERGENCY EXIT LIGHTS ILLUMINATE WITH THE EMERGENCY LIGHT SWITCH IN THE ARMED POSITION AND BATTERY SWITCHES OFF. EMERGENCY EXIT LIGHTS ILLUMINATE WHEN EMERGENCY EXIT LIGHT SWITCH IS IN THE ON POSITION. PERFORMED EMESDR DXTA2023033183450Unknown · unknownRIGHT SIDE TELESCOPING ROD IS BENT AND THE DOOR WILL NOT CLOSE. GAINED ACCESS TO THE RIGHT SIDE TELESCOPING ROD AND REMOVED AND REPLACED TELESCOPING ROD. IAW CE68 AMM 52-10-30. PERFORMED A SATISFACTORY OPS CHECK, NO DISCREPANCY NOTED AT THIS TIME.SDR DXTA2022081868320Engine · defectiveRIGHT ENGINE ENGINE VIBRATION INDICATION: WHILE IN CRUISE FLIGHT (FL330). RIGHT ENGINE BEGIN TO VIBRATE, ACCOMPANIED BY MOMENTARY "ENGINE SHUDOWN" CAS MESSAGE IN CYAN. POWER WAS REDUCED TO 60% N1 WHERE VIBRATION STOPPED. ENGINE VIBRATION QRH WAS ACCOMPLSHESDR DXTA2021121353430Battery · defectiveCABIN EMERG LIGHT: WHEN PERFORMING THE EMER LTS TEST, THE SEAT NUMBER 8 CABIN EMERGENCY LIGHT/READING LIGHT DID NOT ILLUMINATE WHEN THE MAIN BATTERY SWITCHES WERE OFF AND THE EMER LTS SWITCH WAS SELECTED TO THE ARM POSITION. TROUBLE SHOOTING SHOWED THAT THE LISDR DXTA2021101750410None · noneMAIN DOOR HANDLE: WHEN THE MAIN DOOR IS CLOSED AND LATCHED IN NORMAL CLOSED POSITION, THE RED BUTTON CAN NOT BE DEPRESSED TO OPEN MAIN CABIN DOOR. THE CREW MADE SURE THAT THE CABIN WAS DEPRESSURIZED AND THE SEAL WAS DEFLATED. WHEN UPWARD PRESSURE ON THE DOOR HSDR DXTA2021101750390Handle · not reportedMAIN DOOR HANDLE: WHEN THE MAIN DOOR IS CLOSED AND LATCHED IN NORMAL CLOSED POSITION, THE RED BUTTON CAN NOT BE DEPRESSED TO OPEN MAIN CABIN DOOR. THE CREW MADE SURE THAT THE CABIN WAS DEPRESSURIZED AND THE SEAL WAS DEFLATED. WHEN UPWARD PRESSURE ON THE DOOR HSDR DXTA2021013104657Door · out of balanceMAIN CABIN DOOR NEEDS ADJUSTING. THE DOOR LOWERS VERY QUICKLY WITH VERY LITTLE COUNTERBALANCE WEIGHT HOLDING DOOR IN THE CLOSED POSITION. THE CONDITION MAY HAVE CAUSED UPPER STEP PANEL TO COME OFF. CORRECTIVE ACTION: GAINED ACCESS TO MAIN CABIN DOOR SPRING SDR DXTA2019073102693Windshield · failedFIRST OFFICER COCKPIT WINDOW - PASSING FL 220 RIGHT COCKPIT SIDE WINDSHIELD BEGAN TO CRACK. QRH WAS RUN AND WINDOW CONTINUED TO SLOWLY CRACK UNTIL 3000FT. ALL SWITCHES AND CIRCUIT BREAKERS ARE IN QRH CONFIGURATION. "CORRECTIVE ACTION" REMOVED AND REPLACED WISDR DXTA201904230188Truss · corrodedAPU TRUSS MOUNT (FLANGE) CORROSION. REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ19152M1 DATED APRIL 12, 2019.SDR DXTA201904230187Drag Angle · crackedVERTICAL FIN DRAG ANGLE DAMAGE. REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ19155M1 DATED APRIL 15, 2019.SDR DXTA201904230186Spar Cap · corrodedVERTICAL STAB. AFT SPAR CAP DAMAGE (CORROSION). REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ19154M1 DATED APRIL 12, 2019.SDR DXTA201904230185Truss · corrodedAPU TRUSS MOUNT (FLANGE) CORROSION. REFERENCE ENGINEERING MEMO DQ19152M1.SDR DXTA201904230184Drag Angle · crackedVERTICAL FIN DRAG ANGLE DAMAGE. REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ19155M1 DATED APRIL 15, 2019.SDR DXTA201904230183Spar Cap · corrodedVERTICAL STAB. AFT SPAR CAP DAMAGE (CORROSION). REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ19154M1 DATED APRIL 12, 2019.SDR DXTA201902051975Switch · defectiveALL LANDING GEAR RETRACTION DID NOT RETRACT - GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE HANDLE WAS LOCKED OUT AND COULD NOT BE MOVED. A SHORT TIME LATER WE RECEIVED A WOW MISCOMPARE CAS MESSAGE. RETURNED TO LANDING AND MESSAGE CLEARED AFTER TOUCHDOWN. ALL SYSTSDR JGVR2018110200001Inlet · corrodedBLENDED THREE AREA OF CORROSION ON THE APU INLET DEFLECTOR SCOOP. FOUND INLET/DEFLECTOR SCOOP NOT REPAIRABLE AND REPLACED WITH NEW.SDR DXTA2018022300633Water Separator · odorDURING THE FINAL STAGES OF A HIGH ALTITUDE 3 HOUR FLIGHT WHILE MANEUVERING BELOW 10,000 FEET WITH THE THROTTLES PULLED BACK NEAR IDLE TO DESCEND AND SLOW DOWN A STRONG OILY MUSTY ODOR PERMEATED THE COCKPIT AND CABIN. UPON ARRIVAL AT AIRCRAFT, LEFT AND RIGHT SDR JGVR20171219002Skin · corrodedRIGHT WING UPPER WING SKIN OTBD OF MIDDLE DRAG ANGLE AFT END UNDERNEATH PAINT AND SEALANT HAS 4 AREAS OF SUSPECTED CORROSION. MECHANICALLY BLENDED LEVEL 1 CORROSION ALONG OUTBD SIDE RH UPPER WING TO FUSELAGE MIDDLE DRAG ANGLE, AFT END, ON WING SKIN P/N 692268
Back to N305QS, cancelled Feb 18, 2026