Textron 680A
Service difficulty reports · 2,664
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 DXTA2025081104561Pcb · faultedON CLIMB OUT, THROUGH 38,000 FT, HAD AN AMBER CHK DOORS & AMBER CABIN DOOR OPEN LIGHT. CABIN DOOR OPEN LIGHT ON DOOR HANDLE ILLUM. RAN QRH & CONTINUED TO DESTINATION UNEVENTFULLY WITH NO CHANGES. ONCE ON GROUND RECYCLED DOOR & CAS MESSAGES & HANDLE LIGHT REMASDR DXTA2025081204539Wire Harness · damagedENERGENCY LIGHTS ARE INOPERATIVE: OVERHEAD LIGHTS OVER SEATS 3 & 7, LIGHT UNDER SEAT 3. ATTEMPTED CHARGING IAW QRH, NO IMPROVEMENT. MAIN POWER ON, LIGHT UNDER SEAT 3 WOULD ILLUMINATE WHILE 2 OVERHEAD LIGHTS REMAINED OFF. WITHOUT MAIN POWER. NONE OF THE 3 LIGSDR DXTA2025080804512Door · faultedDOOR HANDLE IS STIFF AND FEELS LIKE ITS CATCHING ON SOMETHING. INSPECTED THE DOOR AND FOUND NO ABNORMALITIES AT THIS TIME. PERFORMED CABIN DOOR OPERATIONAL CHECK IAW AMM 52-10-00, AND THE OPS CHECK WAS FOUND SATISFACTORY. PERFORMED THE OPS CHECK AGAIN WITH ASDR DXTA2025080604492Elec Connector · looseTHE LAV FLOOR EMER LIGHT IS INTERMITTENT AND FLICKERS ON AND OFF. ACCESSED AIRCRAFT AND POWERED UP VIA APU. POWERED ON EMERGENCY LIGHTS AND ALL LIGHTS WORKING PROPERPLY INCLUDING LAV FLOOR LIGHTING, WHILE LIGHTS WERE POWERED ON, TAPPED ON TOILET SEAT AND TOILSDR 2025F00174Spar · corrodedRH WING AFT SPAR HAS 1 AREA OF CORROSION AROUND HI-LOK ON LOWER CLIP BEHIND PANEL 720DR. MECHANICALLY REMOVED CORROSION FROM RH WING AFT SPAR. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW C680 SRM 51-70-02 EXCEEDING .002" OF MATERIAL REMOVED FROM NOMINAL THISDR 2025F00173Spar Web · corrodedRH WING AFT SPAR HAS 2 AREAS OF CORROSION ON FWD FACE BEHIND PANEL 720DR. MECHANICALLY REMOVED CORROSION FROM RH WING AFT SPAR WEB. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW C680 SRM 51-70-02 EXCEEDING .002" OF MATERIAL REMOVED FROM NOMINAL THICKNESS. SUBSDR 2025FA0000535Nut Plate · corrodedUPON REMOVAL OF 316CBC AND 316DBC FOR L5 INSTALLATION, FOUND CORROSION UNDER MULTIPLE NUTPLATES. REMOVED NUTPLATES AND BLENDED CORROSION FROM AFFECTED AREA ON APROX. F.S. 500-570 INSIDE PANEL 316CBC AND 316DBC ON STRINGERS IAW CESSNA 680A SRM 51-10-01 & 51-40-SDR 2025F00172Stringer · mechanic errorDOUBLE DRILLED HOLES, TAILCONE, STRINGER 9R SPLICE, W.L. 121.5 F.S. 560.3-576.2. ACCOMPLISHED FR-680A-0376-15468 REV. -, FIELD REPAIR - DOUBLE DRILLED HOLES, TAILCONE, STRINGER 9R SPLICE, W.L. 121.5 F.S. 560.3-576.2; DATED JULY 23, 2025.SDR DXTA2025080504450Proximity Switch · faultedAMBER CABIN DOOR OPEN CAS MESSAGE. RAN EMER CHECKLIST FOR CABIN DOOR OPEN CAS MESSAGE ON GROUND N1 MESSAGE WILL NOT CLEAR. SPOKE WITH MCC RAN CHECKLIST AGAIN SAME RESULT. DID A POWER CYCLE MESSAGE STILL WILL NOT CLEAR. PERFORMED TROUBLESHOOTING !AW AMM 52-00-0SDR DXTA2025080504460Strut · dirtyMAIN CABIN DOOR IS BINDING UPON CLOSING. DOOR REQUIRES REALIGNMENT. SPOKE WITH PILOTS AND RECREATED THE BINDING. THE SUPPORT STRUT WAS CREATING A CHATTER NOISE BUT WAS NOT CAUSING THE DOOR TO OPERATE IMPROPERLY. WAITED FOR AIRCRAFT TO COME INTO HANGER TO FURTHSDR DXTA2025080404433Door · faultedCABIN DOOR OPEN CASS MESSAGES DISPLAYED. CHECK HANDLE MEASAGE FLASHING ON MED DISPLAY. QRH PROCEDURE ACCOMPLISHED TWICE. DOOR HANDLE FEELS LIKE IT BINDS WHILE CLOSING. MED TROUBLESHOOTING CARRIED OUT IAW AMM 52-00-00 REV 22 AND WDM 52-10-01 REV A6. WIRING PIN SDR DXTA2025073004395Door Seal · leakingDURING CLIMBOUT PRESSURIZATION, THERE IS A NOTICABLE MAIN DOOR SQUEAL LEADING TO A THUNK NEAR 12000 FEET. DURING DESCENT AND DEPRESSURIZATION THERE IS A THUNK AND THEN A NOTICABLE DOOR SQUEAL BEGINNING SOMEWHERE BELOW 10000 FEET. CLEANED AND INSPECTED MAIN DOOSDR 3J7R2025072800525Battery · dischargedWHEN THE EMERGENCY LIGHTS SWITCH IS SET TO ARM, THE LAVATORY SEAT OVERHEAD LIGHT, EXIT SIGN FOR THE BULKHEAD BEHIND SEAT SEVEN, EXIT SIGN BELOW THE LAVATORY SEAT, AND THE EVACUATION PATH LIGHTS UNDER THE LAVATORY SEAT DO NOT COME ON.SDR DXTA2025072804354Hinge · damagedON THE GROUND IN VNY, WE WENT TO RAISE THE MAIN CABIN DOOR & THE MAIN CABIN LIFT MOTOR ARM CAME APART AT THE HINGE. THE BOLT & BUSHING THAT WAS FOUND ON THE RAMP PUT IN PLASTIC BAG & LEFT IN GALLEY. RE-INSTALLED UPPER HINGE PIN, WASHERS, AND RETAINER RING BACKSDR DXTA2025072404327Battery Pack · inoperativeEMER LIGHTS NOT WORKING IN ARMED POSITION FOR THE FIRST FLIGHT IN THE MORNING, IF YOU START THE APU AND CHARGE THEM FOR 30 MINUTES THEN THEY WORK. SAME THING HAPPENED THE FOLLOWING MORNING. THIS AFTERNOON WE SHUT DOWN THE AIRCRAFT FOR TWO HOURS AND THEY WOULD SDR 2025FA0000509Frame · crackedA CRACK WAS FOUND ON THE LUG FOR DOOR STRUT ARM ON THE 7411351-8 SURROUND FRAME. ACCOMPLISHED FR-680A-139-15365 REV - DATED: 25-JUN-2025 - FIELD REPAIR - CRACK, FUSELAGE, AFT DOOR SURROUND FRAME, DOOR STRUT DRIVE ARM ATTACH.SDR DXTA2025072204292Uplock Switch · defectiveLEFT MAIN GEAR HAS YELLOW X WHEN EXTENDED. RAN CHECKLIST AND GEAR STILL DOES NOT SHOW DOWN AND LOCKED. CORRECTIVE ACTION: REPLACED LH MLG UPLOCK SWITCH OPS CHECK GOOD IAW CE680A AMM 32-32-25SDR DXTA2025071804268Relay · faultedFLAPS FAIL CAS MESSAGE WHEN MOVING THE FLAPS POSITION SWITCH FROM UP TO 1 ON APPROACH AT 3000FT. FLAPS REMAINED IN UP POSITION. RAN QRH AND QRC PROCEDURES, FLAPS WOULDNT RETURN TO NORMAL FUNCTION. EMERGENCY DECLARED, LANDED WITHOUT INCIDENT IN THE NO FLAP CONFSDR DXTA2025071604250Battery Pack · faultedOVERWING AND FLOOR LIGHT AT SEAT 5 WILL NOT ILLUMINATE WITH EMERGENCY POWER SELECTED ON. BATTERIES WERE SUFFICIENTLY CHARGED. LIGHTS ILLUMINATE WITH MAIN BATTERY POWER AND EMER POWER ON. REMOVED #3 EMERGENCY BATTERY AND INSTALLED A REPAIRED EMERGENCY BATTERY OSDR DXTA2025071604254Window Frame · crackedTHERE APPEARS TO BE A CRACK IN THE LOWER PORTION OF THE AFT EMERGENCY EXIT HATCH WINDOW. AFTER INSPECTION FOUND OUTER FROST PAIN TO BE SCRATCHED. REMOVED PANE AND REPLACED WITH CUSTOMER PROVIDED OUTER FROST PANE PER 680A AMM 5-20-20SDR DXTA2025071504228Light · inoperativeEXIT SIGN OVER SEAT 7 WILL NOT ILLUMINATE DURING PRE-FLIGHT EMERGENCY LIGHTING TEST. ATTEMPTED TO CHARGE BATTERY PACK PER TEXTRON PROCEDURE WITH NO RESULTS. MAIN CABIN DOOR EMERGENCY LIGHTS ARE ALL FUNCTIONING NORMALLY AS REQUIRED PER MEL 33-50-03. REMOVED DSDR DXTA2025071404208Engine · faultedDURING CRUISE AT FL430 WITH RAT OF -39 RECEIVED AN AMBER ENG CNTRL FAULT L CAS MESSAGE. ALONG WITH THIS CAS MESSAGE WE RECEIVED THE R ENG. THE ENG CNTRL FAULT QRH PROCEDURE (U1) COMPLETED. PROCEDURE INDICATED TO LAND AND CONTINUED TO DESTINATION. DURING DESCESDR JGVR20250711002Skin · corrodedREPAIRED 5 CORRODED AREAS ON LH HORIZONTAL STAB UPPER AND LOWER SKINS FORWARD OF PANEL 351A AND REPAIRED 3 CORRODED AREAS ON RH HORIZONTAL STAB UPPER SKIN FORWARD OF PANEL 352AC BY MECHANICALLY BLENDING AREAS, PERFORMING NDT AND REPORTING FOR REPAIR DISPOSITIOSDR JGVR20250711001Skin · corrodedREPAIRED CORRODED AREAS OF THE LH & RH HORIZONTAL STABILIZER LOWER TRAILING EDGE SKINS BY MECHANICALLY BLENDING AREAS, PERFORMING NDT AND REPORTING FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREA PER NETJETS REQUEST FOR TECHNICAL SUPPORT REPORT.SDR DXTA2025071404191Control Unit · faultedENG CNTRL FAULT L, PRESSURIZATION FAULT AND GEA FAIL 2. WHILE RUNNING THE CHECK LIST FOR GEA FAIL 2 IT INSTRUCTED US TO PRESS AUTO/MAN FOR THE PRESSURIZATION, WHEN WE PUSHED IT THE CABIN DUMPED ALL PRESSURE.(ATC DECLARED EMERGENCY) CORRECTIVE ACTION: REMOVED FSDR DXTA2025071404193Pressure Switch · faultedFUEL PRESS LOW L AMBER CAS MESSAGE DISPLAYED IN FLIGHT. MESSAGE CYCLED REPEATEDLY UNTIL THE L BOOST PUMP WAS TURNED ON PER THE QRH. CORRECTIVE ACTION: REMOVED AIRFRAME FUEL PRESSURE SWITCH P/N 9914488-3 S/N 1927564 INSTALLED NEW SWITCH S/N 2315974 OPS CHECK SDR DXTA2025071404196Trim System · faultedIMMEDIATELY AFTER TAKEOFF WE HAD NO ABILITY TO TRIM THE AIRCRAFT USING PRIMARY TRIM AND RECEIVED PRI STAB TRIM FAIL.(ATC DECLARED EMERGENCY) SENT IN ARES DOWNLOAD TO TEXTRON IAW CE·680A AMM CH 31-33-00. TEXTRON STATED THAT THE REASON THE PRIMARY STAB TRIM FASDR DXTA2025071604261Hinge · mechanic errorWHILE WORKING TO INSTALL THE LH WING AILERON ON AOG AIRCRAFT N649QS, SOMEHOW THROUGHOUT THE PROCESS IT MANAGED TO SLIP AND DAMAGE THE LH AILERON OUTBOARD HINGE OPENING ON THE TOP SIDE. IT APPEARS THAT THERE IS A CRACK AND THE DAMAGED AREA AROUND THE CRACK IS SDR DXTA2025071404185Door · faultedMAIN DOOR BEGINS TO OPEN BUT FAILS TO COMPLETE THE OPENING CYCLE. PERFORMED CABIN DOOR LATCHING/LOCKING SYSTEM AND DOOR WARNING SYSTEM TEST SECTION 3 PER CESSNA 680A MM 52-70-00. NO DEFECTS NOTED, MED OPENS AS ADVERTISEDSDR DXTA2025071404189Panel · looseINFLIGHT VIBRATION FELT DURING DESCENT PHASES OF FLT AT HIGH SPEEDS AND DESCENT PITCH ATTITUDES ONLY (HIGHEST AROUND 290 & DECREASES UNTIL NEGLIGABLE BELOW 225KNOTS). VIBRATION SEEMS TO CORRELATE WITH SPEED & SEEMS UNRELATED TO ENGINES/ THRUST. IT ONLY OCCURS SDR DXTA2025071104181Smoke Detector · defectiveREPEAT WRITE-UP, DURING PREFLIGHT AND AFTER BAGGAGE FIRE TEST WAS COMPLETED WE GOT RED BAGGAGE FIRE CAS AND A RED BAGGAGE FIRE PUSH BUTTON ILLUMINATED. APU SHUT DOWN. RAN CHECKLIST BUT DID NOT DISCHARGE FIRE BOTTLE. WENT TO VIZUALLY INSPECT BAGGAGE BAY, NO FISDR DXTA2025071004164Warning Message · false indicationRECIVED CHECK DOORS CAS. FOLLOW CHECK DOORS QRH AND CYCLED ALL DOORS ASSOCIATED ALSO COMPLETED POWER UP ANOMALY CHECKLIST. CAS REMAINS WITH THE MAIN CABIN DOOR CLOSED. DOOR OPEN LIGHT ALSO REMAINS ON.(HANDLE STIFF AND NOT STOWING) POWERED UP ACFT. CONFIRMED ASDR DXTA2025070904168Bellcrank · out of adjustTHE DOOR COMES UP, BUT THE LATCHING HANDLE WILL NOT ENGAGE, STUCK IN THE OPEN POSITION CORRECTIVE ACTION: REALIGNED PIN BELL CRANK. IAW CE680A AMM 52-10-04. OPS CHECK GOOD.SDR DXTA2025071004161Detection Sys · no testON CABIN PREP SYSTEMS TEST THE RED BAGGAGE FIRE TEST FAILS. THE RES CAS MESSAGE STAYS ILLUMINATED AND RED BAGGAGE FIRE BUTTON STAYS ILLUMINATED. UNABLE TO REAT OR TEST. CORRECTIVE ACTION; POWERED ON AIRCRAFT, COMPLETED MULTIPLE BAGGAGE COMPARTMENT SMOKE DETECSDR DXTA2025070904160Battery · no testEMERGENCY LIGHTS TEST FAILED DURING PREFLIGHT. TWO UNSUCCESSFUL SEPARATE 30' CHARGING CYCLES (60' CUMULATIVE) WERE PERFORMED PER QRH CHARGING PROCEDURE. NO LIGHTS ILUMINATE WITH SWITCH IN ARM POSITION. CORRECTIVE ACTION: REPLACED BATTERIES IAW CE-680A MM CHAP SDR DXTA2025070704147Battery · no testNONE OF THE EMER LTS ILLUMINATE WITH SWITCH IN ARM POSITION. RAN QRH RECHARGE PROCEDURE, STILL FAILED AFTER ALLOTTED CHARGING TIME. CORRECTIVE ACTION: REMOVED AND REPLACED POSITION 1, 2, 3, AND 4 EMERGENCY LIGHTING BATTERY PACKS AND INSTALLED NEW BATTERY PACKSSDR DXTA2025070304120Wire Harness · disconnectedFOUND EMERGENCY FLOOR PATH LIGHT AT SEAT 8 INOPERATIVE. CORRECTIVE ACTION: GAINED ACCESS TO EMERGENCY LIGHT AT SEAT 8, FOUND THAT HARNESS FOR THE LIGHT WAS DISCONNECTED. RECONNECTED AND OPS CHECKS GOOD. WORK PERFORMED WITH REFERENCE TO CE680A AMM 33-50-00SDR DXTA2025070304095Static Wick · ground damageDURING TOW OF N541QS THE THIRD STATIC WICK FROM THE WINGTIP OF THE LEFT WING MADE CONTACT WITH THE RIGHT LEADING EDGE OF N959QS. WING LEADING EDGE IS GOUGED. COMPLIED WITH TEMPORARY REPAIR OF RH WING LEADING EDGE IAW RFTS-114342.SDR DXTA2025070304103Yoke · out of adjustCAPTAIN CONTROL YOKE: IN THE AIR WHEN THE YOKE IS CENTERED, THE AIRPLANE WILL TURN TO THE LEFT. WHEN THE AIRPLANE IS CENTERED THE YOKE IS OFF TO THE RIGHT. THERE IS A SPLIT BETWEEN THE LEFT AND RIGHT YOKE. THE LEFT YOKE IS OPERATING NORMALLY. FOUND LEFT YOKE TSDR DXTA2025070204096Static Wick · brokenDURING TOW OF N541QS THE THIRD STATIC WICK FROM THE WINGTIP OF THE LEFT WING MADE CONTACT WITH THE RIGHT LEADING EDGE OF N959QS AND BROKE OFF. CORRECTIVE ACTION; VISUALLY INSPECTED LEFT WING TRAILING EDGE. THE ONLY DAMAGE APPEARS TO BE A BROKEN STATIC WICK. RESDR DXTA2025070304084Steering Sys · faultedNOSE WHEEL STEERING PULLS HARD TO THE RIGHT . NOTICED DURING TO AND LANDING AND DOES AFFECT DIRECTIONAL CONTROL. NWS TRAVEL CHECKS WERE GOOD, BUT WE WANTED TO VERIFY CABLE TENSIONS AND ROUTING. ROUTING CHECKED GOOD, FOUND CABLE TENSIONS HIGH, SUPPOSED TO BE 18SDR DXTA2025070304089Starter Gen · vibrationCONSISTENT RESONANCE VIBRATION IN YOKE FLIGHT CONTROLS WITH AUTO PILOT ON AND OFF IN FAIRLY STABLE AIR. NOTICEABLE IN MULTIPLE SPEEDS AND PITCH ANGLES. CORRECTIVE ACTION: VISUALLY EXAMINED ALL TRIM TABS AND CONTROL SURFACES AND GEAR DOORS (WELGHT ON WHEELS) FSDR DXTA2025070204087Switch · defectiveON APPROACH AFTER SELECTING LANDING GEAR DOWN RECEIVED AN AMBER CAS PARK BRAKE ON. RAN THE QRH AND MESSAGE REMAINED. CALLED MAINTENANCE AND AT THEIR SUGGESTION PUMPED THE BRAKES AND CYCLED THE PARKING BRAKE HANDLE TO TRY AND CLEAR THE MESSAGE. ALL ATTEMPTS TO SDR DXTA2025063004066Battery Pack · faultedFIRST FLIGHT OF THE DAY PRE FLIGHT CHECKS WE NOTED THAT THE EMER LIGHT WERE NOT WORKING. WE RAN APU FOR 30 MIN SHUT DOWN AND RECHECKED THE EMER LIGHT AND THEY WORKED NORMALLY. NEXT MORNING THE SAME ISSUE PRESENTED. RAN APU AND EMER LIGHTS WORKED NORMALLY AGAINSDR DXTA2025063004058Battery Pack · no testFLOOR EMERG EXIT LIGHT: UNDER SEATS 5&8 AND SEAT 7- OVERHEAD EMER LIGHTS INOP WHEN TESTED. FULLY ACCOMPLISHED ABNORMAL CHECKLIST, 2 ATTEMPTS, TO RECHARGE BUT DID NOT WORK. CORRECTIVE ACTION; REPLACED ALL 4 EMERGENCY LIGHTING BATTERY PACKS IAW CE 680A AMM 33-50SDR DXTA2025062704046G Switch · failedUPON COMPLETION OF LAST FLIGHT OF DAY & POST FLIGHT SHUTDOWN AND INSPECTION, DISCOVERED EMERGENCY LIGHTS IN AFT OF PLANE ON & COULD NOT EXTINGUISH (EXIT SIGN ABOVE TOILET, EMER LIGHT ABOVE TOILET, FLOOR LIGHT BELOW TOILET, & EXIT SIGN ON BULKHEAD ABOVE SEAT 7)SDR DXTA2025062704029Seal · leakingDURING CRUISE WE NOTICED AN AUDIBLE SQUEAL COMING FROM THE EMERGENCY EXIT DOOR AREA. THERE WAS NO PRESSURIZATION ISSUES NOTED. AS WE DESCENDED THE SQUEAL WENT AWAY AROUND 27000 FEET WITH A PSI OF 8.6. NO VISIBLE ISSUES WITH THE EMERGENCY EXIT DOOR FROM INSISDR DXTA2025062704020Pcb · faultedCABIN DOOR OPEN AMBER CAS: DURING DESCENT CABIN DOOR AMBER CAME ON PRESSURIZATION WAS FINE. AFTER LANDING PLANE WAS SHUT DOWN AND TURNED BACK ON CABIN DOOR WAS OPENED AND CLOSED AND DOOR WOULD NOT LOCK AND NO FLAGS. REMOVED PCB NC105 AND INSTALLED AS RECEIVED SDR DXTA2025062504016Battery Pack · inoperativeDURING POWER ON CHECKLIST, CHECKING THE EMERGENCY LIGHTS THE SEAT 3 PATHWAY LIGHT DOES NOT ILLUMINATE. WE CHARGED THE BATTERY ON TWO 30 MIN CHARGE CYCLES AND THE LIGHT STILL DOES NOT ILLUMINATE. REMOVED #2 EMER BATTERY DUE TO SEAT 3 PATHWAY FAILED TO ILLUMINATSDR DXTA2025062504000Control Module · faultedDURING APPROACH TO LAND, GEAR HANDLE WAS MOVED TO DOWN POSITION. AN AMBER CAS GEAR DISAGREE L-R-N DISPLAYED AND NO MOVEMENT HEARD. ALL THREE GEAR POSITION INDICATORS WERE AMBER UP. A GO AROUND WAS INITIATED. GEAR HANDLE WAS AGAIN MOVED TO UP POSITION, AGAIN
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