N315QS
Service difficulty reports · 38
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 = 'N315QS' 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 = 'N315QS' 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 2026F00213Spar Cap · corrodedCORROSION, VERTICAL STABILIZER, LH AFT SPAR CAP, VFS 116 - VFS 121. ACCOMPLISHED TEXTRON AVIATION FIELD REPAIR FR-680-0220-54511 REV -; FIELD REPAIR - CORROSION, VERTICAL STABILIZER, LH AFT SPAR CAP, VFS 116 - VFS 121 DATED 8 SEP 2026. FAA FORM 8100-9 DATED 10SDR DXTA2026072809019Strut · dischargedWE WERE CLIMBING THROUGH APPROXIMATELY FL200 WHEN WE FELT A CLUNK IN THE NOSE AREA, & THE RED, GEAR UNLOCK LIGHT ILLUMINATED & STAYED ON FOR THE DURATION OF THE FLT UNTIL SELECTED GEAR DOWN AGAIN FOR LANDING. GOT LIGHT IN CLIMB & AT THE TIME WE WERE CLIMBING ASDR 2026072609019Landing Gear · faultedWE WERE CLIMBING THROUGH APPROXIMATELY FL200 WHEN WE FELT A CLUNK IN THE NOSE AREA WE THINK, AND THE RED, "GEAR UNLOCK" LIGHT ILLUMINATED AND STAYED ON FOR THE DURATION OF THE FLIGHT UNTIL WE SELECTED GEAR DOWN AGAIN FOR LANDING. WE GOT THE LIGHT IN THE CLIMB SDR DXTA2026072709019Warning Message · illuminatedWE WERE CLIMBING THROUGH APPROXIMATELY FL200 WHEN WE FELT A CLUNK IN THE NOSE AREA WE THINK, AND THE RED, GEAR UNLOCK LIGHT ILLUMINATED AND STAYED ON FOR THE DURATION OF THE FLIGHT UNTIL WE SELECTED GEAR DOWN AGAIN FOR LANDING. WE GOT THE LIGHT IN THE CLIMB ANSDR JGVR20251209002Skin · corrodedMECHANICALLY BLENDED CORRODED AREA ON LOWER AFT RT WING SKIN, INBOARD OF FLAP, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED AND PRIMED AREAS IAW REQUEST FOR TECHNICAL SERVICES REPORT.SDR JGVR20251209001Drag Angle · corrodedBLENDED AREAS OF CORROSION ON THE LOWER AFT DRAG ANGLE, LEFT WING INBD OF FLAP, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPLACED BLENDED FASTENERS WITH NEW, CLEANED, TREATED AND PRIMED AREAS PER REQUEST FOR TECHNICAL SERVICES REPORT.SDR DXTA2025111005625Battery · inoperativeON PREFLIGHT INSPECTION THE ONLY EMERGENCY LIGHTS THAT ILLUMINATE ARE ADJACENT TO THE MAIN CABIN DOOR AND THE FORWARD AISLE LIGHTS. ALL OTHER INTERIOR EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED EMERGENCY BATTERY #1 P/N CBS28-1 S/N 3730M, BATTERY#2 P/N CBS28-1 SSDR JGVR20250710001Spar · corrodedMECHANICALLY BLENDED 1 EA. AREA OF CORROSION ON AFT SPAR, LOWER CLIP OUTBD AREA, IN THE RH MLG WHEEL WELL, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREA BY CLEANING, TREATING, AND PRIMING PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR DXTA2025053003695Elec Connector · openGEAR SELECTED DOWN. RIGHT MAIN GEAR DID NOT ILLUMINATE DOWN. AND THE UNLOCKED LIGHT WAS ILLUMINATED. WE RAN THE FULL GEAR DID NOT EXTEND QRH WITH NO CHANGE TO THE INDICATIONS. CORRECTIVE ACTION: WE PERFORMED TS OF THE RH MLG INDICATION DISCREPANCY. AT RH CONNESDR DXTA2025031702683Flap System · faultedFLAPS FAIL AMBER CAS: WHEN SELECTING FLAP POSITION 15 AMBER CAS FLAP FAIL MESSAGE APPEARED. FLAPS DID NOT MOVE FROM ZERO POSITION. CORRECTIVE ACTION; POWERED UP AIRCRAFT AND DISCOVERED 'BITE 2' AND 'BITE 6' FAULTED ON FLAP CONTROLLER AS A RESULT OF FLAP FAIL. SDR DXTA2025010701838Landing Gear · faultedDURING DEPARTURE OUT OF TNCM RAISED THE GEAR AFTER T/O AND HEARD A NOISE THEN NOTICED THAT BOTH MAIN LANDING GEAR STILL INDICATED DOWN WITH GREEN DOWN GEAR INDICATION. THE NOSE GEAR LIGHT WAS OUT. PERFORMED THE QRH PROCEDURE AND LOWERED GEAR HANDLE AND GOT ALLSDR 2024F00304Skin · corrodedLH AND RH HORIZONTAL STAB UPPER AND LOWER SKIN HAS AREAS OF CORROSION JUST FWD OF ACCESS PANELS 351AC AND 352AC. MECHANICALLY REMOVED CORROSION ON LH UPPER AND LOWER HORIZONTAL STAB SKIN TRAILING EDGE JUST FWD OF ACCESS PANEL 351AC AND CORROSION ON RH UPPER ANSDR 2024F00303Fitting · corrodedRH WING SPOILER HYDRAULIC LINE CARRY THRU FITTINGS ON AFT WING SPAR JUST INBD OF WING JACKING POINT HAS 2 CARRY THRU FITTINGS WITH CORROSION AROUND THEM. MECHANICALLY BLENDED 2 EA. AREAS OF CORROSION AROUND RH WING HYDRAULIC LINE CARRY THROUGH FITTINGS ON AFT SDR 2024F00301Stringer · crackedREPAIRED CRACKED TAILCONE/STRINGER FIREWALL WEB CRACK PER NETJETS RFTS-112267. REV.0 TITLED "N315QS (680-0220) TAILCONE FIREWALL WEB CRACK" DATED 18NOV24.SDR 2024F00300Control Cable · chafedDURING TASK 27-60-00-2200, FOUND RH WING AILERON OUTPUT CABLE CHAFFING DRAIN TUBE NEXT TO SPOILER MIXER BOX. REMOVED EXISTING DRAIN TUBE FROM AIRCRAFT. REPAIRED DRAIN TUBE PER NJA RFTS-112277, REV 0, TITLE: N315QS (680-0220) WATER DRAIN LINE CHAFE, DATED: 15NOSDR 2024F00299Stringer · corrodedSTINGER HAS 1 AREA OF CORROSION ON LOWER AFT SIDE NEAR DRAIN HOLE. MECHANICALLY BLENDED 1 AREA OF CORROSION ON STINGER LOWER AFT SIDE NEAR DRAIN HOLE. EVALUATED AND FOUND AREA TO BE BEYOND LIMITS. SUBMITTED AREA TO NJA ENGINEERING FOR REPAIR. REPAIRED AREA PERSDR 2024F00298Hinge · corrodedFOUND AN AREA OF CORROSION ON LOWER RUDDER HINGE. MECHANICALLY REMOVED 1 AREA OF CORROSION LOCATED ON RUDDER LOWER HINGE, AFT END, LH SIDE UPPER AREA. EVALUATED AND FOUND TO BE BEYOND LIMITS PER CESSNA 680 SRM 51-70-02. SUBMITTED TO NJA ENGINEERING AND TEXTRONSDR 2024F00297Rib · corrodedLH WING INBD FLAP COVE SUPPORT RIB HAS CORROSION WHERE HYD STAND-OFF BRACKET IS ATTACHED. MECHANICALLY REMOVED CORROSION LOCATED ON LH WING INBD FLAP COVE SUPPORT RIB, OUTBD SIDE WHERE HYD STAND-OFF BRACKET IS ATTACHED IAW C680 SRM 51-70-02. FOUND CORROSION BLSDR 2024F00302Fitting · corrodedLH WING SPOILER HYDRAULIC LINE CARRY THRU FITTINGS ON AFT WING SPAR JUST INBD OF WING JACKING POINT HAS 2 CARRY THRU FITTINGS WITH CORROSION AROUND THEM. MECHANICALLY BLENDED 3 EA. AREAS OF CORROSION AROUND LH WING HYDRAULIC LINE CARRY THROUGH FITTINGS ON AFT SDR 2024FA0000859Spar · corrodedLH MLG WHEEL WELL AFT SPAR, FWD FACE HAS 1 AREA OF CORROSION INBD OF WS 37.00. MECHANICALLY REMOVED CORROSION LOCATED IN LH MLG WHEEL WELL, AFT SPAR, FWD FACE INBD OF WS 37.00 APX 21 INCHES IAW C680 SRM 51-70-02. FOUND CORROSION BLEND TO BE BEYOND LIMITS IAW CSDR DXTA2023090594410Unknown · unknownAVIONICS POWER: WITH THE MAIN POWER ON DURING FINAL DESCENT MY SIC IN THE RIGHT SEAT SMELLED A FAINT ELECTRICAL SMELL RIGHT BEFORE I DID. IT SEEMED TO GO AWAY AND WE LANDED VERY SHORTLY AFTERWARD. UPON STARTING APU THE SMELL CAME BACK MUCH STRONGER AND SMELLEDSDR DXTA2022112274220Spring · brokenMAIN DOOR COUNTER WEIGHT SPRING BROKE UNABLE TO CLOSE DOOR WITHOUT HELP. REMOVED AND REPLACED MED FWD COUNTERBALANCE SPRING. PERFORMED RIGGING OF MED COUNTERBALANCE SYSTEM IAD CE680 AMM 52-10-50. MED COUNTERBALANCE SYSTEM OPS CHECK GOODSDR DXTA2021121053290None · noneRIGHT MLG BRAKE: RIGHT BRAKE REQUIRED MUCH GREATER THAN NORMAL APPLICATION FORCE BEFORE IT WOULD ENGAGE DURING LANDING ROLLOUT (REPORTED FROM RIGHT SEAT PILOT) // SIGNOFF// VISUALLY INSPECTED BOTH INBOARD AND OUTBOARD RH BRAKE ASSEMBLES FOR ANY DEFECTS/ LEAKS.SDR DXTA2021090948510Engine · leakingCOCKPIT ODOR: ABNORMAL ODOR IN COCKPIT AT TAKEOFF POWER. LENGTHY 10-15 MIN TAXI WITH APU OFF. APPLIED TAKEOFF POWER AND WITHIN 5 SECS NOTED UNUSUALLY STRONG ABNORMAL ENVIRON ODOR. ABORTED TAKEOFF AND ODOR APPEARED TO QUICKLY DISSIPATE AS POWER BACK TO IDLESDR DXTA2021090748310Unknown · odorCOCKPIT ODOR: REPEAT WRITE UP. WITH APU OFF UNPLEASANT STRONG ABNORMAL ODOR IN COCKPIT AND CABIN AFTER TAKEOFF. ODOR WAS ENVIONMENTAL IN NATURE AND WAS STRONGEST AFTER TAKEOFF, IT DISSIPATED DURING THE CLIMB BUT DID BECOME STRONGER IN THE DESCENT OR WITH LASDR DXTA2021090748150Condenser · dirtyCOCKPIT ODOR: UNPLEASANT UNUSUALLY STRONG ABNORMAL ODOR IN COCKPIT JUST AFTER TAKEOFF. ODOR SEEMED TO BE ENVIRONMENTAL, ALMOST OILY IN NATURE BUT NOT ELECTRICAL OR GAS. NO SMOKE/HAZE OBSERVED. ODOR DISSIPATED AND THEN REOCCURRED ON INITIAL DESCENT AND POWER CHSDR JGVR20200303001Not Reported · corrodedREPAIRED SPOTS OF CORROSION ON LH AND RH SIDES OF FORWARD DROPPED AISLE PER AEROSPACE QRD ERO-965791, TITLED "FUSELAGE REPAIR", DATED 27 FEB 2020 AND SUPPORTED BY FAA FORM 8110-3 DATED FEBRUARY 27, 2020.SDR JGVR20180110001Door · corrodedEMERGENCY EXIT DOOR CORRODED BEYOND ECONOMIC REPAIR, REPLACED THE DOOR.SDR JGVR20180109001Rib · corrodedREPAIRED AREAS OF CORROSION ON LOWER FLANGE OF WING RIB P/N 6922037-20, AT WING STATION 18.50 IN RT MLG WELL PER ENGINEERING MEMO DQ10680M1, DATED JANUARY 5, 2018.SDR JGVR20170915001Structure · corrodedEMERGENCY EXIT HAS CORROSION AROUND MULTIPLE NUT PLATES UNDER CONTOUR RING. BLENDED AREAS. PERFORMED EDDY CURRENT INSPECTION ON BLENDED AREAS. NO CRACKS OR CORROSION INDICATIONS NOTED. PERFORMED ULTRASONIC THICKNESS INSPECTION ON BLENDED AREAS. PREPPED, TSDR DXTAT2PL6D0059SG2Uplock Switch · out of adjustDURING TAKEOFF, THE GEAR HANDLE WAS PLACED IN THE FULL UP POSITION. ALL GREEN GEAR INDICATIONS EXTINGUISHED BUT THE RED UNLOCK LIGHT REMAINED ILLUMINATED. CHECKLIST PROCEDURES WERE PERFORMED AND ALL GEAR EXTENDED AND LOCKED DOWN. PERFORMED LANDING GEAR SWINGSSDR DXTA2017033106391Apu · cokedWHEN HEAT CAME ON AT CRUISE ALTITUDE, A VERY STRONG BURNED OIL ODOR COMES OUT OF THE VENTS. HAD TO TURN THE HEAT DOWN TO AN UNCOMFORTABLY COOLER TEMPERATURE TO REDUCE THE ODOR. TROUBLESHOT THE OIL ODOR, REMOVED THE INLET TO THE APU AND BORESCOPING THE INTAKE ASDR CWQR20131002041Tube · crackedDURING SCHEDULED INSPECTION, WE FOUND APU BLEED AIR TUBE ASSY CRACKED AT THE APU COMPARTMENT ATTACH FLANGE. THE FLANGE WAS CRACKED 2 TO 3" WHERE THE FLANGE IS WELDED TO THE TUBE ASSY.SDR DXTA2012043004966Hose · damagedDEPARTED, MOVED GEAR HANDLE TO UP, NOSE GEAR FAILED TO RETRACT FOLLOWED BY BOTH A HYD PRESSURE LOW LT AND HYD VOLUMN LOW AMBER CAS MESSAGES. RETURNED TO DEPARTURE WITH 3 GREEN INDICATIONS AND LANDED UNEVENTFULL. HYD FLUID CAME OUT OF NOSE GEAR AREA AND ON RSDR 2011FA0000341Tube · crackedFOUND SERVICE AIR TUBE ASSY CRACKED IN BEND RADIUS THAT LEADS TO THE RUDDER ACTUATOR IN THE TAILSDR DXTA2009090803773Engine · vibrationRED ENGINE VIBRATION R CAS MSG POSTED REPEATEDLY FOR A FEW SECONDS EACH TIME AND THEN DISAPPEARED ( N1 96.3 , N2 95.4, FL 360, SAT -52*C , RAT -25*C , ISA +3) CRUISE PWR WAS SET. NO VIBRATION WAS EVER EXPERENCED. REPLACED ENGINE HARNESS WIRE PINS AND SOCKETSDR DXTA2008122303425Tire · failedBOTH RIGHT MAIN TIRES BLEW ON LANDING. LEFT INBOARD MAIN TIRE FLAT. LEFT OUTBOARD MAIN TIRE FLAT. RIGHT MAIN GEAR DOOR DAMAGED ON LANDING.SDR DXTA20082907Unknown · unknownAFTER DEPARTING, A CONTAMINATING RUNWAY GEAR UNLOCKED LIGHT, ILLUMINATED. CLEANED GEAR AND FLAP WELLS, INSPECTED, AND OPERATED SYSTEMS NUMEROUS TIMES WITH NO DEFECTS NOTED.
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