Textron 680A
Service difficulty reports · 2,663
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '680A' 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 aircraft_model_key = '680A' 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 DXTR2026071701Fuel Line · crackedFOUND L/H ENG FUEL LEAK AT FUEL PRESSURE SWITCH ON FUEL SUPPLY LINE WITH FUEL RUNNING AFT OF SWITCH AND DRIPPING FROM ADEL CLAMPSDR DXTA2026071508824Door · lack of lubeTHE MAIN CABIN DOOR HANDLE REQUIRES EXCESSIVE FORCE TO LATCH. DURING SEVERAL CLOSURES, THE RESISTANCE VARIED, BUT WHEN IT DID HANG UP, THE INSIDE HANDLE WAS ABOUT IN THE MIDDLE OF THE THROW. CLEANED AND LUBRICATED DOOR STOP. PREFORMED SATISFACTORY OPS CHECK SDR DXTA2026071508798Valve · defectiveDURING CRUISE & SELECTING XFEED TO LT TANK, RT ENG, BST PUMP ON, R AMBER CAS MESS ILLUM. RAN QRH, LIGHT REMAINED, LANDED ASAP. AFTER START OF DIVERT, LIGHT EXTING. REMOVED RT MOTIVE FLOW PRESSURE SWITCH. INSTALLED PRESS SWITCH IAW MM 28-40-02. INSTALLED SDR DXTA2026071408796Elec Connector · disconnectedLOWER LAV EXIT LIGHT DOES NOT ILLUMINATE. FOUND LOWER LAV EXIT LIGHT CONNECTOR NOT HOOKED UP. REATTACHED CONNECTOR. OPS CHECK GOOD. DONE IN ACCORDANCE WITH CESSNA 680A MM 33-50-01.SDR DXTA2026071008734Anti-Ice Valve · faultedDESCENDING THROUGH 28,000 FEET, WE TURNED ON THE ANTI-ICE SYSTEM. A FEW MOMENTS LATER RECEIVED CAS WARNING MSG: ANTI-ICE WING XFLOW OPEN. AFTER TURNING TO AVOID THE IMPENDING ICING CONDITIONS, WE RAN THE QRH. TRIED TO CYCLE THE XFLOW VALVE BUT THE MESSAGE REASDR 2026F00140Stringer · corrodedFOUND EVIDENCE OF CORROSION ON THE APU STINGER ASSY, LOWER AREA, AFT OF PANEL 330BBC. MECHANICALLY REMOVED SEVERAL AREAS OF CORROSION LOCATED ON APU STINGER, LOWER SKIN EDGE JUST FWD OF ACCESS PANEL 330BBC. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW CESSNASDR DXTA2026070708690G Switch · faultedAFTER LANDING AND SHUTDOWN THE FOLLOWING EMERGENCY LIGHTS HAVE REMAINED ON DESPITE THE EMERGENCY LIGHT SWITCH BEING SELECTED TO OFF: LIGHTED SIGN ABOVE EMERGENCY ESCAPE HATCH ABOVE THE TOILET. TOE KICK LIGHT UNDER SEAT 8. TOE KICK LIGHT UNDER SEAT 5. LEFTSDR DXTA2026070608666Bellcrank · brokenDOOR MOTOR CLUTCH REMAINS DISENGAGED & DOOR WILL FREE-FALL UNLATCHED. OPENED DOOR. DOOR OPENED NORMALLY UNTIL APPROX 2/3RDS OF WAY DOWN, HEARD A LOUD BANG AS IF SOMETHING BROKE. DOOR FINISHED OPENING & REMAINED COMPLETELY OPEN REVEALING NOTHING OUT OF ORDINSDR DXTA2026070608655Actuator · failedDURING TAKEOFF & CRUISE, RETRIMED R WING DOWN CAS MSG CONSTANTLY DISPLAYED. RAN QRH BUT MSG WOULD NOT CLEAR. DISCONNECTED AUTOPILOT & PLANE ROLLED LEFT. AFTER ADDING ADDITIONAL AILERON TRIM RT, WAS ABLE TO FLY STRAIGHT & LEVEL. DURING ARRIVAL, W/ AUTOPILOTSDR DXTA2026070208631Elec Connector · no testEMERGENCY READING LIGHT ABOVE SEAT 3 IS INOP. HAD AIRCRAFT RELOCATED TO HANGAR AS REQUIRED. POWERED AIRCRAFT AND PERFORMED EMERGENCY LIGHT OPERATIONAL CHECK IAW AMM 33-50-00 CONFIRMING SEAT 3 READING LIGHT DOES NOT ILLUMINATE WITH EMER LIGHTS. VERIFIED SEAT 3SDR DXTA2026070208627Window · failedAT FL430 STARTED TO SMELL LIKE SMOKE AND ABOUT 1 MIN LATER SAW THE DELAMINATION STARTING AND SMALL AMOUNTS OF SMOKE . SMOKE STOPPED ABOUT 3 MINS LATER . INSIDE WINDOW PAINE COMPLETLY CRACKED AT AROUND 8500 FEET. GLASS FLEW ALL THROUGH COCKPIT .LABORSDR DXTA2026063008617Handle · bindingTHE HANDLE ON THE MAIN DOOR SEEMS TO BE BINDING UP WHEN OPENING. IT IS A LITTLE STIFF. C/W MED PIN LUBRICATION IAW CE-680A AMM 12-20-40. C/W MAIN CABIN DOOR HEALTH CHECK IAW CE-680 AMM 52-10-04. OPS CHECK GOOD. NO DEFECTS NOTED.SDR 2026FA0000544Switch · miswiredMODIFIED AIRCRAFT WITH AN STC FOR GOGO LX5 TO CONNECT THE AIRCRAFT TO A 5G NETWORK FOR IN FLIGHT ENTERTAINMENT. ALL WORK COMPLETED PER WIRING DRAWINGS SUPPLIED AND WERE CURRENT AT THE TIME. IT WAS FOUND LATER THAT THE ON / OFF SWITCH WIRING (DRAWING CA25174) SSDR DXTA2026062908588Light · misinstalledEMERGENCY FLOOR LIGHTING UNDER LAV IS INOPERATIVE. FOUND LIGHT STRIP CONNECTOR INSTALLED INCORRECTLY. RECONNECTED CONNECTOR PROPERLY AND LIGHTS OPS CHECK GOOD.WORK PERFORMED IN REF TO AMM 33-20-00.SDR DXTA2026062608559Door · out of adjustTHE MAIN CABIN DOOR HANDLE REQUIRES EXCESS FORCE TO PLACE IN THE LOCKED POSITION. DOOR LOCKS AS NORMAL AFTER THAT. ARRIVED TO ACFT & PREPPED FOR MAINTENANCE. WHILE TROUBLESHOOTING DOOR FOUND THAT WHEN PRESSURE APPLIED TOWARDS TOP OF DOOR WHILE IT CLOSED MOSSDR DXTA2026062408536Control Handle · faultedAFTER TAKEOFF AND POSITIVE RATE WAS CALLED PM TRIED TO RETRACT THE LANDING GEAR, NOTHING HAPPENED WITH THE GEAR, WE WERE STILL SHOWING 3 GREEN DN SYMBOLS. WHILE TRYING TO RETRACT THE GEAR THE GEAR LEVER DID FEAL POSSIBLY OUT OF PLACE OR NOT QUIT CONNECTED. EVESDR DXTA2026062208486Link Assy · corrodedLEFT TRAILING LINK ASSEMBLY CORROSION, LINK PIN DAMAGE AND AXLE CHIPPING. ACCOMPLISHED STEPS 3A, 1-9C OF MLG TRAILING LINK REMOVAL IAW MM 32-10-15. DE-PINNED & REMOVED WIRE BUNDLE FROM LT TRAILING LINK IAW SPM 20-30-20. REMOVED LWR OLEO BOLT FOR LT TRAILING SDR DXTA2026062208495Wire Harness · faultedWE RECIEVED AN ENG CNTRL FAULT R CAS MESSAGE DURING CRUISE. RAN THE QRH PROCEDURE BUT MESSAGE DID NOT CLEAR. POWERED UP ACFT VIA APU AND INTERROGATED CMC FOUND 2 FAULT CODES SA & SB. BOTH ISSUES HAPPENED AT CRUISE, CONTINUED. GAINED ACCESS TO DCU CONNECTOR INSDR DXTA2026062208488Link · corrodedRIGHT MLG HAS CORROSION LEACHING . FOUND PITTING AROUND TRAILING LINK / BRAKE MATING SURFACE. REPLACED TRAILING LINK. OPS CHECK GOOD. IAW MM 32-10-15.SDR DXTA2026062208484Link · corrodedRIGHT TRAILING LINK ASSEMBLY CORROSION, LINK PIN DAMAGE AND AXLE CHIPPINGSDR DXTA2026061908478Link Pin · corrodedWEAR AND CORROSION ON RT MLG TRAILING LINK PIN FOUND DURING MAIN LANDING GEAR TRUNNION, TRAILING LINK, AND LINK PIN DETAIL INSPECTION.SDR DXTA2026061908479Link Pin · corrodedWEAR AND CORROSION ON LT MLG TRAILING LINK PIN FOUND DURING MAIN LANDING GEAR TRUNNION, TRAILING LINK, AND LINK PIN DETAIL INSPECTIONSDR DXTA2026061808455Diode · faultyRECEIVED AN AMBER ENG CNTRL FAULT R CAS MESSAGE DURING OUR CLIMB TO CRUISING ALTITUDE. WE RAN THE QRH PROCEDURE BUT THE MESSAGE DID NOT CLEAR. REMOVED PZ012 DIODE MODULE AND INSTALLED NEW DIODE MODULE. PERFORMED ENGINE RUN OF RT ENGINE WITH NO DEFECTS NOTED SDR DXTA2026061808471Control Module · faultyLANDING GEAR LEVER WOULD NOT MOVE ON DEPARTURE, COULD NOT RETRACT LANDING GEAR. GEAR HANDLE REMAINED DOWN, GEAR SHOWED THREE GREEN DN FOR DURATION OF FLIGHT. REFERRED TO EMERGENCY/ABNORMAL CHECKLIST AND COULD NOT FIND APPLICABLE PROCEDURE PER INDICATIONS. NO LSDR DXTA2026061608458Brake Assy · faultedAFTER TAXIING IN TO A STOP ON THE RAMP POST LANDING THE MAIN BRAKES WILL EXTENSIVELY VIBRATE FROM A SLOW SPEED UNTIL COMING TO A COMPLETE STOP. CHECKED ALL BRAKE PINS AND EVERYTHING LOOKED GOOD. CHECKED THE BRAKES THEMSELVES AND DIDN'T SEE ANY UNUSUAL WEAR. SDR DXTA2026061608432Pcb · faultyAMBER CAS MESSAGE CABIN DOOR OPEN AND ASSOCIATED CHECK DOORS CAME ON AT CRUISE 39000. RAN QRH AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED CED MONITOR PCB NC105, REF MM 24-60-40. PERFORMED SUCCESSFUL CABIN DOOR LATCHING/LOCKING SYSTEM AND CABIN DOOR WARSDR DXTA2026070708721Link Assy · corrodedPITTING FOUND ON THE LH TRAILING LINK WHILE COMPLETING SL680A-32-11. COMPLIED WITH REPLACEMENT OF LT TRAILING LINK ENHANCED INSPECTION IAW SL680A-32-11 REV 2. NO DEFECTS NOTED AT THIS TIME.SDR DXTA2026061208420Light Sys · faultedCABIN PREP TEAM REPORTS THE EMER LIGHTS ON N554QS ARE STUCK ON AND WILL NOT SHUT OFF. ACCESSED INERTIAL SWITCH IN COCKPIT CENTER PEDESTAL, PERFORMED RESET / PROCEDURE AND VERIFIED LIGHTS EXTINGUISHED, RAN APU FOR ABOUT 30 TO 45 MINUTES TO PROPERLY CHARGE LIGSDR DXTA2026061208409Ground Stud · misinstalledEMER LIGHTS DID NOT TEST PROPERLY DURING PREFLIGHT TEST. ATTEMPTED RECHARGE IAW CHECKLIST. CHARGED 30 MINS CHECKED AGAIN, DID NOT WORK. CHARGED 30 MORE MINS, CHECKED AGAIN, DID NOT TEST PROPERLY. EMER LIGHTS DO WORK IN ON POSITION. PERFORMED GROUND CHECK OF EMSDR DXTA2026061008392Pin · dirtyWHEN CLOSING THE MAIN CABIN DOOR FROM EITHER INSIDE OR OUTSIDE, THE DOOR COMES UP NORMALLY BUT THE LOCKING HANDLE DOES NOT MOVE. CLEANED CABIN DOOR LOCKING PINS IAW CABIN DOOR SERVICING IAW AMM 12-20-40.SDR DXTA2026060908388Door · no discrepancyCLOSING THE MAIN CABIN DOOR, THE HANDLE IS VERY STIFF. IT DOES CLOSE FLUSHED WITH THE FUSELAGE, AND ALL LOCKING PIN ARE BEING ENGAGED. JUST SEEMS TO BE A LOT OF RESISTANCE WHEN CLOSING THE DOOR. INSPECTED MAIN CABIN DOOR WITH NO DEFECTS NOTED, VERIFIED RIGGISDR DXTA2026061108379Actuator · defectiveON DESCENT RECEIVED AMBER CAS AP TRIM STAB FAIL. RAND QRH. ONCE AP DISCONNECTED HAD PUSHING FORCE (NOSE DOWN) ON CONTROLS. MANUAL TRIM WORKED. LANDED. AP SYSTEM MEL APPLIED ALONG WITH MX REQUIREMENTS. YD MEL 22-10-05 WAS REFERENCED AND IS CONSIDERED INOP. REPSDR DXTA2026061008381Monitoring Unit · defectiveAFTER DEPARTING KDAL AND CLIMBING THROUGH APPROXIMATELY 4,000 FEET WE RECEIVED TWO CAS MESSAGES. AMBER CHECK DOORS AND THE CABIN DOOR OPEN CAS MESSAGES. WE RETURNED TO KDAL AND UPON INSPECTING THE CABIN DOOR ALL SIX PINS WERE SHOWING LATCHED AND SECURED. HOWEVSDR DXTA2026060808352Controller · defectiveUPON DEPARTURE FROM PSP FLAPS WERE SELECTED TO THE UP POSITION AS USUAL. FLAPS FAIL AMBER CASS MESSAGE CAME UP INDUCTIONS SHOWED FLAPS WERE STUCK IN THE FLAPS 1 POSITION. POSITION CONFIRMED VISUALLY OUTSIDE. QRH COMPLETED WITH NO SUCCESS. FLAPS CURRENTLY REMAISDR DXTA2026060808353Unknown · odorON TAKE-OFF OUT OF KHPN, AS SOON AS WE LEFT THE GROUND, A VERY BAD SMELL WAS NOTICED BY BOTH CREW MEMBERS. THE ODOR DESCRIBED AS A DIRTY SOCK/ DEAD ANIMAL ODOR. THERE WAS NO INDICATIONS OF ANYTHING BURNING NOR WAS THERE ANY ELECTRICAL OR SMOKE ODORS, DECISSDR DXTA2026060808359Battery Pack · defectiveRIGHT HAND WING INSPECTION LIGHT IS VERY DIM WHEN PAX SAFETY AND BATTERIES ON OR WHEN BATTERIES OFF AND EMERGENCY LIGHTS ARMED. LIGHT IS BRIGHT WHEN SELECTING WING INSPECTION LIGHTS ON. CORRECTIVE ACTION: T/S RIGHT HAND WING INSPECTION LIGHT IS VERY DIM. FOUNDSDR DXTA2026060808350Handle · faultedWHEN CLOSING THE MAIN CABIN DOOR THE LEVER GOES DOWN AND THE YELLOW LIGHT STAYS ON. AFTER JIGGLING THE HANDLE THE LIGHT WILL GO OUT. WHEN OPENING PRESSING THE RED BUTTON THE DOOR HANDLE WOULD NOT LIFT UP WITHOUT PUSHING DOWN HARD FIRST AND THEN UP. WHEN OPENINSDR DXTA2026060808328Link · corrodedDURING SL680A-32-11(RH LANDING GEAR - MAIN LANDING GEAR TRAILING LINK ENHANCED INSPECTION). FOUND SOME PITTING/ARCHING, INSIDE OF THE RT TRAILING LINK. REMOVED RT MLG TRAILING LINK PN 7441030-5 SN 33614842 AND INSTALLED A REPAIRED UNIT IAW MM 32-10-15. LEAK &SDR DXTA2026060508322Motor · faultedWHEN CLIMBING, WITH THE AUTOPILOT ENGAGED, BETWEEN FL210 AND FL220, THE AMBER STAB TRIM MONITOR MESSAGE POSTED. WE RAN THE QRH AND MANUALLY USED THE PRIMARY STAB TRIM FOR AIRSPEED CHANGES. FODM WAS CONTACTED AND A DIVERSION WAS INITIATED. CORRECTIVE ACTION: SDR DXTA2026060508327Actuator · faultedON TAKEOFF JUST AFTER POWER WAS SET, NOSE PULLED HARD TO THE LT. LT RUDDER PEDAL ALSO WENT FULL. CORRECTED WITH RIGHT RUDDER & ABORTED TAKE OFF. RUDDER BIAS CHECK BEFORE WAS GOOD. PERFORMED RUDDER BIAS CHECK AFTER AND IT WAS GOOD. PERFORMED A DETAILED INSPESDR DXTA2026060408318Inhibitor · corroded(LANDING GEAR - MAIN LANDING GEAR TRAILING LINK ENHANCED INSPECTION) INTERNAL CORROSION AFTER NDT NO CRACKS CLEANED AND APPLIED CORRISION INHIBITOR IAW SPM 51-30-10 THE LH TRAILING LINK PN#7441030-5 SN#3015789 WAS FOUND TO BE GOOD IN SERVICEABLE CONDITIONSDR DXTA2026060408319Inhibitor · corrodedSL680A-32-11 (LANDING GEAR - MAIN LANDING GEAR TRAILING LINK ENHANCED INSPECTION) - INTERNAL CORROSION. AFTER NDT NO CRACKS FOUND. CLEANED AND APPLIED CORRISION INHIBITOR IAW SPM 51-30-10 THE RH TRAILING LINK PN#7441030-5 SN# 30194768 WAS FOUND TO BE GOOD ISDR DXTA2026060408323Pcb · defectiveTOP LOCKING PIN DOES NOT STOW FULLY. CAUSING ASSOCIATED CHECK DOOR CAS, AND CABIN DOOR OPEN CAS. REMOVED FWD PRINTED LH PCB NC105 PN:7468101-20 SN:33674927-3 DUE TO CHECK DOOR CAS AND INSTALLED CUSTOMER SUPPLIED NEW PCB PN:7468101-20 SN: 35064311-4. REPLACESDR DXTA2026060208281Elec Connector · disconnectedEMERGENCY LIGHT OUT AT SEAT 8. FOUND SEAT 8 EMER LIGHT DISCONNECTED, RE-CONNECTED LIGHT CONNECTOR, AND OPS GOOD. WORK PERFORMED IN REF TO CE 680A AMM 33-20-05, 33-50-00.SDR DXTA2026060108256Generator · faultedDURING CRUISE ENG CONTROL FAULT R CASS MESSAGE ILLUMINATED. RAN QRH AND MESSAGE CLEARED. WHEN STARTING DESCENT FELT A VIBRATION THAT CHANGED WITH POWER SETTING CHANGES. OBSERVED THAT THE RIGHT ENGINE POWER CHANGES LAGGED BEHIND THE LT ENGINE BY 2-5%. REMOVED SDR DXTA2026060108258Filter · odorUPON DEPARTURE AFTER FLAP RETRACTION AT ABOUT 1000' NOTICED A STRONG BURNING SMELL IN COCKPIT AREA. DID NOT SEE SMOKE, LOOKED BACK IN CABIN AREA AND ALSO DID NOT SEE SMOKE, DID NOT GET ANY CAS MESSAGES NOR AUDIO WARNINGS , JUST A STRONG BURNING ODOR THAT STAYESDR DXTA2026052908250Pressure Switch · faultedSELECTED FUEL CROSSFEED L TANK TO R ENGINE INFLIGHT AND RECIEVED FUEL PRES LOW L CAS AS WELL AS AN AMBER FUEL BST PUMP ON L. RAN QRH AND FUEL BST PUMP L MESSAGE REMAINED AMBER. REMOVED LH SUSPECTED DEFECTIVE FUEL PRESSURE SWITCH P/N:9914488-2, S/N:2423753 ANSDR DXTA2026052708229Squat Switch · damagedAFTER TAKE OFF, SELECTED GEAR UP, GEAR HANDLE WOULD NOT ALLOW FOR GEAR TO BE SELECTED UP. CAS MESSAGE HP VALVE CLOSED L-R, WOW MISCOMPARE AND GROUND IDLE L-R. RAN QRH CHECKLIST AND AFTER RUNNING CHECKLIST AND ADVISING COMPANY MCC RETURN TO KMIV AND LANDED NORMSDR DXTA2026052808219Warning Message · illuminatedDURING APPROACH AFTER GEAR SELECTED DOWN WE RECEIVED A WHITE "GEAR UPLK FAULT R" CAS MESSAGE. PERFORMED POST MX CHECKS AFTER UPLOCK SWITCH WAS REPLACED IAW AMM 32-32-25, DO THE LANDING GEAR OPERATIONAL CHECK. REFER TO CHAPTER 32, LANDING GEAR - ADJUSTMENT/TSDR DXTA2026052708220Door · bindingAFTER PARKING, ATTEMPTED TO OPEN THE MAIN CABIN DOOR. WHEN MOVING THE HANDLE UPWARD WITH THE RED BUTTON PUSHED THE HANDLE WAS EXTREMELY DIFFICULT TO MOVE UPWARD. THE AMOUNT OF FORCE REQUIRED WAS ACTUALLY FLEXING THE HANDLE BROUGHT IT UPWARD. AT THE TOP OF THE
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