N370QS, cancelled Jul 28, 2025

Service difficulty reports · 54

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 = 'N370QS' AND deregistration_id = 'N370QS-2025-07-28'
  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.

SDR DXTA2024120201355Counterbalance · out of adjustENTRANCE STAIR: COUNTER BALANCE ON MAIN CABIN DOOR. DOOR IS VERY HEAVY TO CLOSE AND FALLS OPEN EASILY. CORRECTIVE ACTION; ADJUSTED BOTH REELS OPS CHECK GOOD. ALL WORK DONE IN REF, TO CE-680 AMM 52-10-50.Dec 1, 2024 · N370QS · Cessna 680SOV · Passenger/Crew DoorsSDR 2024F00296Skin · nickedDURING ELEVATOR TRAVEL CHECKS NOTICED SKIN DAMAGE AROUND THE TRIM ACTUATOR COVE AREA. UPPER ELEVATOR SKIN AND LOWER TRIM ACTUATOR COVE SKIN.Nov 20, 2024 · N370QS · Gulstm 680 · Vertical Stabilizer, Plate/SkinSDR 2024F00295Spar · chafedWHILE ACCOMPLISHING ELEVATOR TRAVEL CHECKS FOUND ELEVATOR CONTROL HORNS HITTING HILOCKS PREVENTING FULL TRAVEL, NEED TO LOOK INTO AQRD REPAIR DEFINITION OF VERTICAL REPAIR.Nov 20, 2024 · N370QS · Gulstm 680 · Vertical Stabilizer, Spar/RibSDR JGVR20231114002Unknown · unknownLH/RH H STAB UPPER AND LOWER SKINS ON THE TRAILING EDGE HAVE MULTIPLE AREAS OF CORROSION. MECHANICALLY BLENDED MULTIPLE AREAS OF CORROSION ON LH AND RH, UPPER AND LOWER HORIZONTAL STABILIZER TRAILING EDGE SKINS IAW CESSNA 680 SRM 51-70-02. AREAS DETERMINED TO Nov 14, 2023 · N370QS · Cessna 680A · Horizontal Stabilizer StructureSDR JGVR20231114001Unknown · unknownREPAIRED HORIZONTAL STABILIZER RH LOWER SKIN DUE TO LEVEL 2 CORROSION. MECHANICALLY BLENDED MULTIPLE AREAS OF CORROSION ON RH LOWER HORIZONTAL STABILIZER TRAILING EDGE SKINS. INSTALLED 2 001 DOUBLERS ON LOWER SIDE OF RH HORIZONTAL STAB WITH CR3524-4 AND CSR904Nov 14, 2023 · N370QS · Cessna 680A · Horizontal Stabilizer, Plate/SkinSDR JGVR20231113001Unknown · unknownRH VERT AFT SPAR IS HEAVILY CORRODED. LOCATED ABOVE RUDDER UPPER HINGE. REPAIRED 2 BLENDED AREAS OF VERTICAL STABILIZER R/H AFT SPAR CAP AT APPROXIMATELY VFS 172 AND VFS 237 DUE TO CORROSION PER AQRD ERO-108612 REV. IR, TITLED,"RFTS-108612 - N370QS - VERTICAL Nov 13, 2023 · N370QS · Cessna 680A · Vertical Stabilizer, Spar/RibSDR JGVR20231005002Unknown · unknownREPAIRED CORRODED AREAS ON THE RUDDER LEADING EDGE NEAR THE BALANCE WEIGHT HARDWARE BY BLENDING AREAS, PERFORMING NDT AND REPORTING FOR REPAIR DISPOSITION. REPAIRED AREAS BY CLEANING, TREATING AND PRIMING AND INSTALLING REPAIR DOUBLERS PER NETJETS REQUEST FOR Oct 5, 2023 · N370QS · Cessna 680CE · Rudder, Plate/SkinSDR JGVR20201104005Support Bracket · corrodedFOUND LT AND RT LOWER RUDDER SUPPORT BRACKETS CORRODED BEYOND REPAIR AND REPLACED WITH NEW CESSNA P/NS 6931045-17 AND 69031045-18.Nov 4, 2020 · N370QS · Cessna 680CE · Vertical StabilizerSDR JGVR20201104004Plate · corrodedFOUND SEVERE CORROSION OF THE UPPER RIB PLATE OF THE VERTICAL STABILIZER’S RUDDER TRIM ACTUATOR MOUNT, REPLACED WITH A NEW CESSNA P/N 6961526-5 WET WITH PS870B SEALANT USING NEW HL40-4 HI-LOK PINS WITH NEW HL97DU4 COLLARS AND NAS1097AD4 SOLID RIVETS, REFERENCINov 4, 2020 · N370QS · Cessna 680CE · Vertical StabilizerSDR JGVR20201104003Skin · corrodedBLENDED CORRODED AREA ON THE UPPER SURFACE OF THE UPPER WING SKIN, JUST INBOARD OF THE LT OVER-WING FUEL FILLER, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED REPAIR AREA, PER TEXTRON REPAIR.Nov 4, 2020 · N370QS · Cessna 680CE · Wing, Plate/SkinSDR JGVR20201104002Spar Cap · corrodedBLENDED MULTIPLE CORRODED AREAS ON THE LT AND RT SPAR CAPS AND WEB OF THE VERTICAL STABILIZER AFT SPAR, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPLACED BLENDED AND/OR CORRODED FASTENERS AS REQUIRED, TREATED AND PRIMED REPAIR AREAS, PER TEXTRON REPNov 4, 2020 · N370QS · Cessna 680CE · Vertical Stabilizer, Spar/RibSDR JGVR20201104001Skin · corrodedREMOVED THE LT UPPER WING DRAG MIDDLE AND AFT ANGLES (WING-TO-FUSELAGE FAIRINGS) AND BLENDED CORRODED AREAS OF THE UPPER SURFACE OF THE LT UPPER WING SKIN, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPLACED 17 CORRODED HI-LOCS IN THE REPAIR AREA. TRNov 4, 2020 · N370QS · Cessna 680CE · Wing, Plate/SkinSDR 2020FA0000217Inlet · damagedLH ENGINE INLET DUCT DEEP COUNTERSINK. REFERENCE TEXTRON AVIATION ENGINEERING MEMO: DQ25329M1 RRL DATED: 3/31/2020.Apr 6, 2020 · N370QS · Cessna 680CE · Engine Air Intake SystemSDR 2020FA0000216Skin · corrodedR/H HORIZONTAL STABILIZER UPPER SKIN CORROSION. REFERENCE FAA FORM 8100-9, FR-680-0099-7851 REV- DATED: 4/3/2020.Apr 6, 2020 · N370QS · Cessna 680CE · Horizontal Stabilizer, Plate/SkinSDR 2020FA0000215Skin · corrodedMINOR CORROSION AROUND HILOCK COLLARS IN LH AND RH MLG WHEEL WELL ABOVE TRUNNION. REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ25322M1 RRL DATED: APRIL 1, 2020.Apr 6, 2020 · N370QS · Cessna 680CE · Wing, Plate/SkinSDR 2020FA0000214Door · corrodedEMERGENCY EXIT DOOR CORROSION. REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ25313M1 RRL DATED: MARCH 31, 2020.Apr 6, 2020 · N370QS · Cessna 680CE · Emergency ExitsSDR DXTA2019121203190Unknown · odorCOCKPIT ODOR BURNING SMELL - BURNING ODOR NOTICED BY CREW AT 11000 FEET IN CRUISE. SOURCE COULD NOT BE IDENTIFIED AND CRASH/FIRE/RESCUE COULD NOT IDENTIFY A HEAT SOURCE. CFR NOTICED THE ODOR EVEN AFTER AIRCRAFT ON THE GROUND WITH CABIN DOOR OPEN. A LIGHT HAZE Dec 11, 2019 · N370QS · Cessna 680CE · Air Distribution SystemSDR 2019F00205Fairing · crackedLT LOWER WING FAIRING TRIM CRACK REPAIR RFTS-103325 REV 0 DATED MAY 15, 2019.May 15, 2019 · N370QS · Cessna 680SOV · Aerodynamic FairingsSDR 2019F00193Truss · corrodedAPU TRUSS MOUNT (FLANGE) CORROSION. REFERENCE ENGINEERING MEMO DQ19368M1 DATED: MAY 3, 2019.May 6, 2019 · N370QS · Cessna 680CE · Nacelle/Pylon, Attach FittingsSDR DXTA2019011001901Display · overheatedDU3 WENT BLANK AND ELECTRICAL SMOKES FUMES NOTICED CLIMBING THROUGH FL360. RAN EMERGENCY CHECKLIST AND DIVERTED INTO KFSM. **SUPPLEMENTAL INFORMATION: REMOVED & INSPECTED NR 3 DU, FOUND TO BE INTERNALLY FAILED & SMELLED FRIED. REMOVED & REPLACED NR 3 DU IAW MMJan 10, 2019 · N370QS · Cessna 680CE · Central DisplaySDR DXTA2018123101854Actuator · faultyAFTER RETRACTING THE GEAR ON TAKEOFF, THE LEFT MAIN INDICATOR CONTINUED TO SHOW IT WAS DOWN AND LOCKED. WE DIDN'T HAVE A RED UNLOCK, OR ANY HORN. PER THE CHECKLIST PROCEDURE, GEAR WAS EXTENDED AND SHOWED ALL NORMAL INDICATORS **SUPPLEMENTAL INFORMATION: REMOVEDec 31, 2018 · N370QS · Cessna 680CE · Landing Gear ActuatorSDR JGVR20171206002Axle · corrodedLH MLG AXLE HAS AREAS OF MISSING CHROME AND RUST. REMOVED LH MLG TRAILING LINK FOR AXLE REPLACEMENT AND FOUND BOTH TRUNNION LUGS TO BE CORRODED ON OUTER SURFACES. REPLACE LH MLG TRUNNION AND TRAILING LINK ASSEMBLIES. REMOVED LH MLG TRUNNION AND TRAILING LINK Dec 6, 2017 · N370QS · Cessna 680CE · Main Landing Gear Strut/Axle/TruckSDR JGVR20171206001Panel · corrodedLEVEL 1 CORROSION AROUND MULTIPLE FASTENERS ON LH AND RH H-STAB IB CLOSEOUT PANELS 351AC AND 352AC. BLENDED LEVEL 1 CORROSION AROUND MULTIPLE FASTENERS ON LH AND RH H-STAB IB CLOSEOUT PANELS 351AC AND 352AC. APPLIED ALODINE, CORROSION RESISTANT PRIMER, AND TOPDec 2, 2017 · N370QS · Cessna 680CE · Horizontal Stabilizer, Plate/SkinSDR DXTA2017031906386Circuit Board · failedENGINE FIRE DETECT FAIL LEFT CAS MESSAGE DISPLAYED INFLIGHT. CB TRIPPED. TROUBLESHOT TO LEFT ENG FIRE & SMOKE PRINTED CIRCUIT BOARD. REMOVED AND REPLACED THE PCB IAW MM 24-60-10. OPS CHECKED GOOD.Mar 19, 2017 · N370QS · Cessna 680CE · Fire Protection System WiringSDR JGVR201609210008Attach Angle · corrodedCORROSION ON UPPER TAIL CONE COVER FAIRING ATTACH ANGLES. THE AREAS THAT CORRODE ONLY HAVE PRIMER PAINT. SHOULD BE PAINTED WITH AN ADDITIONAL CORROSION RESISTANT PAINT FOR A TOP COAT TO PREVENT CORROSION.Sep 21, 2016 · N370QS · Cessna 680CE · Aerodynamic FairingsSDR JGVR201609210007Spar Web · corrodedCORROSION ON THE FORWARD WEB IN LT WHEEL WELL AROUND LT INBD BRAKE FITTING. SUGGEST APPLYING CPC TO WHEEL WELL SPARS.Sep 21, 2016 · N370QS · Cessna 680CE · Wing SparSDR JGVR201609210006Fitting · corrodedCORROSION FOUND AROUND EMERGENCY BRAKE LINE FITTING ON OTBD SIDE OF WS 37.00 IN RT MLG WHEEL WELL. SUGGEST APPLYING CPC IN WHEEL WELLS.Sep 21, 2016 · N370QS · Cessna 680CE · Wing Miscellaneous StructureSDR JGVR201609210005Spar Web · corrodedCORROSION ON THE FORWARD WEB IN THE RT MLG WHEEL WELL AROUND THE RT INBD BRAKE FITTING. SUGGEST APPLYING CPC ON THE WHEEL WELL SPARS.Sep 21, 2016 · N370QS · Cessna 680CE · Wing SparSDR JGVR201609210004Thrust Reverser · corrodedCORROSION ON THE OUTER SKIN OF THE LT AND RT THRUST REVERSER LOWER BUCKETS. SUGGEST PAINTING WITH A HIGH TEMPERATURE CORROSION RESISTANT PAINT SIMILAR TO WHAT IS USED ON THE INSIDE OF THE AFTER BODIES.Sep 21, 2016 · N370QS · Cessna 680CE · Engine Thrust ReverserSDR JGVR201609210003Thrust Reverser · corrodedCORROSION ON THE OUTER SKIN OF THE LT AND RT THRUST REVERSER BUCKETS. SUGGEST PAINTING WITH A HIGHER TEMPERATURE CORROSION RESISTANT PAINT SIMILAR TO WHAT IS USED ON THE INSIDE OF THE AFTER BODIES.Sep 21, 2016 · N370QS · Cessna 680CE · Engine Thrust ReverserSDR JGVR201609210002Skin · corrodedCORROSION ON UPPER SURFACE OF LT ELEVATOR FORWARD OF TRIM TAB.Sep 21, 2016 · N370QS · Cessna 680CE · Elevator, Plate/SkinSDR JGVR201609210001Thrust Reverser · corrodedCORROSION ON THE OUTER SKIN OF THE LT AND RT THRUST REVERSER LOWER BUCKETS. SUGGEST PAINTING WITH A HIGH TEMPERATURE CORROSION RESISTANT PAINT SIMILAR TO WHAT IS USED ON THE INSIDE OF THE AFTER BODIES.Sep 21, 2016 · N370QS · Cessna 680CE · Engine Thrust ReverserSDR DXTA2015110606118Circuit Board · failedUPON GEAR RETRACTION, ENCOUNTERED A LOUD CONTINUOUS BANGING NOISE ALONG WITH SEVERE VIBRATIONS. RED GEAR UNLOCK LIGHT REMAINED ON UNTIL THUMPING STOPPED. PROBLEM APPEARED TO BE COMING FROM THE NOSE WHEEL. DECLARED AN EMERGENCY & LANDED UNEVENTFULLY. INSPENov 7, 2015 · N370QS · Cessna 680CE · Landing Gear Retraction/Extension SystemSDR DXTA2014102805918Fire Warning · false activationAMBER CAS MESSAGE FOR RT ENGINE FIRE DETECTION ILLUMINATED INFLIGHT 15 - 20 TIMES. PERFORMED ENGINE RUNS AND COULD NOT DUPLICATE FAULT. MEASURED RESISTANCE OF RT ENGINE OUTTER FIRE LOOP, ALL READERS WITH IN LIMITS PER AMM 26-10-30, REMOVED COCKPIT RT CIRCUIT Oct 27, 2014 · N370QS · Cessna 680CE · Fire DetectionSDR DXTA2014100105902Module · failedAMBER CAS MESSAGE FOR THE RT ENGINE FIRE DETECTION FAILED ILLUMINATED 15 MINUTES INTO FLIGHT. RAN ENGS & ATTEMPTED TO DUPLICATE SQUAWK. NO FAIL LIGHT PRESENT AFTER EXTENSIVE RUNS & TAXIING. REPLACED THE RT FIRE DETECTION CIRCUIT BREAKER & THE CUSTOM VO BOASep 30, 2014 · N370QS · Cessna 680CE · Fire DetectionSDR DXTA2014092905898Fire Detector · failedAMBER ENGINE FIRE DETECTOR FAILED RT CAS MESSAGE ILLUMINATED DURING FLIGHT. RANG OUT INNER FIRE LOOP, RINGS GOOD. INSPECTED WIRING HARNESS, NO DAMAGE FOUND. R & R INNER FIRE LOOP IAW MM 26-10-1. OPS CHECKED GOOD. RAN ACFT & CHECKED FOR BLEED LEAKS. OPSep 26, 2014 · N370QS · Cessna 680CE · Fire DetectionSDR DXTA2014092505892Printed Ckt Board · faultyDURING INITIAL CLIMB OUT ENG FIRE DETECT FAIL R CAS MSG POSTED. THE MSG CLEARED & RE-POSTED SEVERAL TIMES DURING FLIGHT. THIS WAS NOT ASSOCIATED WITH ANY THROTTLE MOVEMENTS. PERFORMED ENG FIRE DETECT FUNCTIONAL CHECK WITH NO DEFECTS FOUND. ACCESSED COMS & Sep 23, 2014 · N370QS · Cessna 680CE · Fire DetectionSDR DXTA2014092205890Fire Loop · faultyUPON DEPARTURE ENG FIRE DETECT FAIL R ILLUMINATED STEADY. DURING DESCENT BECAME INTERMITTENT & EXTINGUISHED ITSELF ON SHORT FINAL. R & R RT ENG FIRE LOOP IAW MM 26-10-30. OPERATIONS CHECKED GOOD.Sep 21, 2014 · N370QS · Cessna 680CE · Fire DetectionSDR 2014F00140Coalescer Bag · dirtyTWENTY MINUTES AFTER TAKEOFF AND CRUISING AT 15,000 FT, THE APU WAS STARTED AND A STRONG ELECTRICAL BURNING ODOR WAS NOTED. THE BLEED AIR WAS TURNED OFF AND APU SHUTDOWN. DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE RAN ACFT AND INSPECTED ACFT, COULDJul 19, 2014 · N370QS · Cessna 680SOV · Humidity Control SystemSDR DXTA2014072105823Coalescer Bag · dirtyTWENTY MINUTES AFTER TAKEOFF AT 15000 FT, APU STARTED USING THE APPROPRIATE CHECKLIST. AFTER THE APU STABILIZED & THE BUSS TIE WAS OPENED, A STRONG BURNING ELECTRICAL ODOR WAS NOTED. BLEED AIR WAS OFF. APU WAS IMMEDIATELY SHUTDOWN. DIVERTED TO THE NEARESJul 19, 2014 · N370QS · Cessna 680CE · Humidity Control SystemSDR DXTA2014060505793Brake Assy · wornBRAKES CHATTER AT SLOW SPEED COMING TO A COMPLETE STOP, FEEL GRABBY DURING TAXI, PULLS TO THE LEFT DURING DECELERATION. INSPECTED BRAKES, FOUND NR 2 BRAKE LEFT INBD WEAR PIN FLUSH WITH HOUSING. REMOVED WORN BRAKE & INSTALLED AN OVERHAULED BRAKE ASSEMBLY. Jun 4, 2014 · N370QS · Cessna 680CE · Landing Gear Brake SystemSDR CWQR20131031048Solenoid · bindingACFT LANDED, AFTER ENGINES WERE SHUTDOWN, CREW WAS UNABLE TO OPEN CABIN DOOR. LINE CREW AND TECHNICIANS WERE NOT ABLE TO OPEN THE DOOR FROM THE OUTSIDE HANDLE. EGRESS WAS MADE BY EMERGENCY EXIT. TROUBLESHOT SYSTEM, FOUND THAT THE MCD ROTARY SOLENOID WOULD Oct 31, 2013 · N370QS · Cessna 680CE · Passenger/Crew DoorsSDR 2013FA0000512Actuator · malfunctionedTHE AILERON TRIM ACTUATOR WAS INSTALLED ON THE RT AILERON. AFTER THE INSTALLATION, IT WAS FOUND THAT THE COCKPIT EICAS DISPLAY SHOWED THE INDICATOR MOVING IN THE OPPOSITE DIRECTION OTHER THAN WAS SELECTED. FURTHER TROUBLESHOOTING REVEALED THAT THE AILERON TRSep 12, 2013 · N370QS · Cessna 680CE · Alternator-Generator DriveSDR DXTA2011120104807Display · failedNR 1MCDU SCREEN GOES BLANK FOLLOWED BY ELECTRICAL SMOKE EMINATING WITHIN THE COCKPIT. AFTER POWER UP WITH AVIONICS ON, FLIGHT PLAN PROGRAMMED AND READY TO GO. NR 1 MCDU SCREEN SUDDENLY GOES BLANK. THE ODOR OF ELECTRICAL SMOKE BEGINS AND THE EICAS MOMENTARILY DNov 30, 2011 · N370QS · Cessna 680CE · Central WarningSDR DXTA2011031604509Display · failedDURING CRUISE FLIGHT, DU NR 2 WENT BLACK ACCOMPANIED BY A SMALL AMOUNT OF ELECTRICAL SMOKE AND ODOR. WHILE ACCOMPLISHING THE ELECTRICAL SMOKE OR FIRE CHECKLIST, UPON SELECTION OF EICAS BUTTON OFF, THE "REMOTE CB TRIPPED" CAS MESSAGE DISPLYED AND ALL ELECTRICALMar 15, 2011 · N370QS · Cessna 680CE · Central DisplaySDR DXTA2010072604174Anti-Skid Sys · failedANTI-SKID FAILED ON TAKEOFF ROLL AT 45 KTS. ABORTED TAKEOFF, MESSAGE REMAINED ON UNTIL SPEED DROPPED BELOW 45 KTS. POWERED ACFT, NO ANTI-SKID FAIL. SPUN EACH WHEEL HOLDING BRAKES. ANTI SKID SYS OPS CHECKED GOOD. RANG OUT SKID XDRIVERS FROM CONTROL. ALL REAJul 24, 2010 · N370QS · Cessna 680CE · Brake Anti-Skid SectionSDR DXTA2010062804133Unknown · odorCREW REPORTED PUNGENT ODOR IN COCKPIT DURING PREFLIGHT. ODOR DISSIPATED QUICKLY AFTER APU BLEED AIR WAS SELECTED ON. REMOVED ALL FOUR DISPLAY UNITS, INSPECTED DU COOLING FANS AND CLEANED. REINSTALLED DUS AND OPS CHECK GOOD IAW MM 34-23-10. GAINED ACCESS AND CJun 25, 2010 · N370QS · Cessna 680CE · Air Distribution SystemSDR DXTA2010010703932Strut · leakingUPON LANDING GEAR RETRACTION, NOSE GEAR MADE HEAVY BANGING NOISE REPEATEDLY IN WHEEL WELL AND RED NOSE GEAR UNLOCK LIGHT REMAINED ON. EXTENDED GEAR NORMALLY AND RETURNED FOR A NORMAL LANDING. REMOVED LOWER BARREL AND REPACKED THE SEALS. INSTALLED LOWER BARRJan 6, 2010 · N370QS · Cessna 680CE · Main Landing Gear Strut/Axle/TruckSDR 2009F00108Warning Light · illuminatedRED CAS MESSAGE "CABIN ALTITUDE" CAME ON PASSING THRU 13,500 FT. PRESS CONTROL FAULT LIGHT WAS ON AS WELL AS CABIN DUMP SWITCH IN DUMP.Nov 13, 2009 · N370QS · Cessna 680CE · Cabin Pressure Control SystemSDR 2008FA0000771Rudder Pedal · jammedON ACFT DEPARTURE, THE RUDDER PEDALS JAMMED ON THE COCKPIT SIDE PANELS ON THE TAKEOFF. AN EMERGENCY WAS DECLARED AND THE ACFT LANDED UNEVENTFULLY. DURING THE PREVIOUS MAINT VISIT, THE RUDDER WAS REPLACED WITH A RENTAL UNIT, THE RUDDER WAS PROPERLY INSTALLED Oct 26, 2008 · N370QS · Cessna 680CE · Rudder Control System
Back to N370QS, cancelled Jul 28, 2025