Textron 680A
Service difficulty reports · 2,664
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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 DXTA2024121201458Handle · lack of lubeDOOR HANDLE IS VERY HARD TO OPEN AND IS GETTING WORSE. COMPLIED WITH CLEANING ALL 6 LATCHING PINS AND LUBRICATING !AW CE 680A AMM 12-20-40. NO FURTHER DEFECTS NOTED. COMPLIED WITH CABIN DOOR LATCH/LOCK SYSTEM FUNCTIONAL AND LATCH OPENS/ CLOSES UNDER 20 POUNDSDR DXTA2024121101448Handle · bindingWHEN LOCKING MAIN CABIN DOOR SILVER HANDLE IS DIFFICULT TO SLIDE INTO LOCKED POSITION. REMOVED THE CABIN DOOR STEPS AND EXAMINED LINKAGE AND LOCKING MECHANISM WITH NO DEFECTS NOTED. OPERATED DOOR AND FOUND IT WAS SLOW TO CLOSE THE LAST FEW INCHES AND SOMETIMESSDR DXTA2024121101426Battery · inoperativeSEAT 3 KICK PLATE LIGHT IS INOP REPLACED #2 EMERGENCY LIGHT BATTERY PACK DUE TO NOT HOLDING CHARGE. OPS CHECKED GOOD IAW CE680A AMM 33-50-06SDR DXTA2024121001414Battery · inoperativeSEAT 10 AND 2 FORWARD LIGHTS BY ENTRY DOOR DO NOT CHECK AFTER PERFORMING AFM RECHARGE PROCEDURE REMOVED INOP BATTERY AND REPLACED WITH NEW. OPS CHECK GOOD REF AMM 33-50-6SDR DXTA2024121001411Strut · failedMAIN DOOR GAS STRUT SNAPPED IN TWO PIECES. MAIN CABIN DOOR STILL OPERATES NORMALLY. NO BINDING OBSERVED ARRIVED ON SITE AND GAINED ACCESS TO THE AIRCRAFT. OPENED THE MED AND FOUND THE SUPPORT STRUT LOWER ROD SEPARATED FROM THE MIDDLE AND UPPER TUBES. FOUND THASDR DXTA2024121001404Strut · failedMAIN DOOR GAS STRUT SNAPPED IN TWO PIECES. MAIN CABIN DOOR STILL OPERATES NORMALLY. NO BINDING OBSERVED ARRIVED ON SITE AND GAINED ACCESS TO THE AIRCRAFT. OPENED THE MED AND FOUND THE SUPPORT STRUT LOWER ROD SEPARATED FROM THE MIDDLE AND UPPER TUBES. FOUND THASDR DXTA2024120601406None · noneCABIN EMERG LIGHT: EMERGENCY LIGHT BELOW SEAT 10, EXIT LIGHTS LOWER PORTION OF ENTRY DOOR INOP. DID AFM PROCEDURE AND STILL NOT WORKING CORRECTIVE ACTION; OPS CHECK OF CABIN EMERGENCY LIGHT SHOWS LIGHT ILLUMINATES WHEN SWITCH IS TURNED ON. NO FAULT FOUND.SDR DXTA2024120501367Aileron · ground damageAIRCRAFT WAS STRUCK BY LAS VEGAS OPERATIONS ESCORT PICKUP TRUCK (SECURITY). AIRCRAFT WAS STATIONARY AND WAS STRUCK FROM BEHIND AT THE AFT RIGHT WING AREA. THE AIRCRAFT WAS NOT CHOCKED BUT WAS HOOKED UP TO A TUG (ELECTRO). THE IMPACT HAS DAMAGED THE RIGHT AILERSDR DXTA2024120501378Proximity Switch · faultedNOSE DOOR OPEN L AMBER CAS MESSAGE ILLUMINATED IN FLIGHT CLIMBING THROUGH 15,000FT. ADJUSTED PROX SWITCH RIGGING OF LH AFT LOWER NOSE DOOR. REF. CE-680A AMM 52-70-00.SDR DXTA2024120401382Seal · leakingDURING FLIGHT, PASSENGERS NOTIFIED US OF A SQUEAL COMING FROM THE BACK. THE SQUEAL SEEMED TO BE COMING FROM THE UPPER EMERGENCY EXIT AREA. PREPARED AND PRESSURIZED THE AIRCRAFT AND WE DID NOT HEAR ANY NOISE AFTER DEPRESSURIZING WE REMOVED THE EMER DOOR AND ISDR DXTA2024120201333Sign · inoperativeEMERG EXIT SIGN/LIGHT: DURING THE AIRCRAFT PREFLIGHT IT WAS OBSERVED THAT THE EMERGENCY EXIT SIGN BELOW THE LAVATORY SEAT WAS NOT WORKING. IT WAS TESTED DURING THE POWER ON CHECKLIST. ADDITIONALLY, WE TURNED ON THE EMERGENCY LIGHTS TO SEE IF IT WOULD ILLUMINATSDR DXTA2024120201324Light · malfunctionedFLOOR EMERG EXIT LIGHT: UNDER SEAT 5, EMER LIGHT DOES NOT ILLUMINATE WHEN LIGHT SWITCH IS IN THE ON POSITION. CORRECTIVE ACTION; REPLACED FLOOR EMERGENCY LIGHT. OPS CHECK GOOD AT THIS TIME. ALL WORK ACCOMPLISHED IAW CE-680AS AMM 33-50-00,SDR DXTA2024120201318Light · defectiveON POST FLIGHT WALK NOTICED THE SMALLER EMER LIGHT ON THE RIGHT SIDE OVER WING LIGHT IS VERY DIM AND FLICKERING. CORRECTIVE ACTION; REMOVED OVER WING EMER LIGHT INSTALLED NEW OVER WING EMER LIGHT OPS CHECK GOOD. NO DEFECTS NOTED. REF. CE 680A AMM 33-50-20.SDR DXTA2024120201317Battery · inoperativeEMERGENCY LIGHTING: SEAT 3 FLOOR AND OVER HEAD EMER LIGHT OFF DURING EMER LIGHT TEST, AS WELL AS RIGHT WING INSPECTION LIGHT (SHARK LIGHT). FOLLOWED PROCEDURE TO CHARGE FOR 30 MINUTES, TEST AGAIN WITH SAME RESULTS. CORRECTIVE ACTION; PERFORMED THE NJA CESSNA 6SDR DXTA2024120201292Actuator · defectiveON APPROACH RECEIVED AMBER AP STAB TRIM & RETRIM NOSE DOWN CAS MESSAGES. CREW DISCONNECTED THE AUTOPILOT AND BEGAN TO NOTICE A HEAVINESS IN THE CONTROLS. THIS CONCERNED THEM AND PROMPTED THEM TO DECLARE AN EMERGENCY WITH ATC. CREW THEN ENGAGED THE SECONDARY TRSDR DXTA2024120201290Seal · leakingEMERG EXIT DOOR SEAL: WHILE SEATED IN THE COCKPIT, WE COULD HEAR A HIGH PITCH SQUEAL COMING FROM THE EMERGENCY DOOR SEAL. CORRECTIVE ACTION; PERFORMED EMERGENCY EXIT DOOR RIGGING PROCEDURE WITH REFERENCE TO CE-680A AM 52-20-00. REPOSITIONED AIRCRAFT OUTSIDE ANSDR DXTA2024120201278Door · stiffMAIN DOOR: MAIN CABIN DOOR IS HARD TO CLOSE. CORRECTIVE ACTION; CYCLED MED AND VERIFIED HARD TO CLOSE AND REQUIRED MORE THAT 20 POUND FORCE TO OPEN, VERIFIED LATCH PINS CLEARANCE FROM LATCH STRIKER WITHIN LIMITS, CHECKED PINS MOVEMENT CLEARANCE WITHIN LIMITS, SDR DXTA2024120201276Position Switch · malfunctionedWOW MISCOMPARE AMBER CAS: UPON GEAR RETRACTION COMMAND THE GEAR HANDLE REMAINED IN THE DOWN AND LOCKED POSITION. THEN AN AMBER WOW MISCOMPARE CAS DISPLAYED ALONG WITH GROUND IDLE AND OCASSIONALY THE HP VALVE CLOSED L/R. WE RAN APPROPRIATE CHECLIST. CAS MESSSDR DXTA2024112701265Step · separatedWHILE EXITING AIRCRAFT, TOP STEP SEPARATED FROM TOP HINGES, STILL ATTACHED AT THE BOTTOM. INSPECTED THE MAIN ENTRY DOOR UPPER STEP FOUND THE THREE HINGES SUPPORT OF THE UPPER STEP BROKEN . GAIN ACCESS TO THE MAIN ENTRY DOOR STEPS , REMOVED AND REPLACED THE TSDR DXTA2024112701269Battery Pack · no testEMER LIGHTS FAILED PREFLIGHT TEST, PATH AND DOWNWASH LIGHTS NOT ILLUMINATED. COMPLETED CHECKLIST AND ATTEMPTED BATT CHARGE NOT SUCCESSFUL. REMOVED AND REPLACED #2 AND #3 EMERGENCY LIGHT BATTERY PACKS !AW CE-680A MM 33-50-06, OPERATIONAL TEST PERFORMED, NO DESDR DXTA2024112501248Battery Pack · inoperativeEMERGENCY LIGHTING: EMER LIGHTS DO NOT TEST IN AUTO. FUNCTION WHEN SELECTED ON BUT DO NOT ILLUMINATE IN AUTO EVEN AFTER POWER REMOVED FROM AC REMOVED #1 EMER BATTERY PACK PN: CBS28-1 SN: 5575 AND INSTALLED NEW BATTERY PACK PN: 6430028-1 SN: F24-11024. OPS CHECSDR 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 DXTA2024112501224Control Switch · damagedPARK BRAKE LOW PRESS AMBER CAS: DURING TAXI TO THE RUNWAY, WE RECEIVED A YELLOW PARK BRAKE LOW PRESS CAS MESSAGE. THIS MESSAGE OCCURRED WITH BOTH ENGINES RUNNING AND DURING MOVEMENT OF THE AIRCRAFT. WE PULLED OFF TO THE SIDE TO DIAGNOSE THE ISSUE. WHEN WE SET SDR 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 JGVR2024112600871Deck Plate · corrodedFOUND POTTY DECK CORRODED ON UNDER SIDE. REMOVED CORRODED SKIN FROM UNDER POTTY DECK AND INSTALLED A NEW SKIN FROM .032 2024 T3 ALUMINUM ALLOY USING EA9394 ADHESIVE. COMPLIED WITH POTTY DECK REPAIR RFTS-112244 REV 0, DATED 12 NOV 24. TOILET SEAT PANEL CORROSIOSDR DXTA2024112101209Indicator · dirtyMAIN DOOR VISUAL INDICATOR: OCCASIONALLY WHEN CLOSING DOOR, PINS BECOME OBSTRUCTED BY DEBRIS. GAINED ACCESS TO BOTH FWD AND AFT MAIN DOOR VISUAL INDICATORS CLEANED AND CLOSE UP ALL OPENED ACCESS. ALL WORK DONE IAW CE680A AMM 52-10-50SDR DXTA2024112101193Battery · damagedEMERGENCY LIGHTING: DURING POST FLIGHT INSPECTION, WE DISCOVERED THAT THE #3 AND #7 SEAT OVERHEAD AND FLOOR LEVEL EMERGENCY LIGHTS WERE INOPERATIVE IN BOTH THE EMER LIGHT ARM, AND ON SWITCH POSITIONS. WE BELEIVE THESE LIGHTS ARE ASSOCIATED WITH EMERGENCY BATTESDR DXTA2024112101198Battery · damagedEMER LIGHTS OFF AMBER CAS: DURING PREFLIGHT INSPECTION, FOUND INTERIOR EMERGENCY LIGHTS AT SEAT 7 AND 5 DOES NOT ILLUMINATE. TRIED RECHARGE PROCEDURES TWICE, FAILED TO RECHARGE AND DID NOT ILLUMINATE. VERIFIED INTERIOR EMER LIGHT AT THAT CORRESPONDS WITH READISDR DXTA2024111901148Door · out of adjustWHEN CLOSING MAIN CABIN DOOR, AFTER ITS FULLY CLOSED, PUSHING SILVER HANDLE DOWN, IT JAMS UP , MIDWAY TO THE LOCKED POSITION. SILVER HANDLE WILL MOVE TO THE FULLY LOCKED POSITION, WITH EXCESSIVE PRESSURE ON THE SILVER HANDLE. DOOR MAY BE POSSIBLY OUT OF ALIGNMSDR DXTA2024111501149Door · out of adjustFUSELAGE STRUCTURE: REPEAT RIGHT UP. THERE IS A VERY PRONOUNCED AIRFRAME VIBRATION. THE VIBRATION BEGINS AT VARIOUS ALTITUDES MORE OFTEN AT FL260 AND 295KTS. THE VIBRATION REMAINS AT ANY ALTITUDE UNTIL SLOWING TO 250 KN. AT 250 KN THE VIBRATION SLOWLY DISSIPASDR DXTA2024111501134Fault Message · false activationENG CNTRL FAULT L AMBER CAS: ENG CNTRL FAULT L AMBER CAS MESSAGE APPEARED AT THE END OF RUNWAY BEFORE TAKEOFF. RAN QRH PROCEDURE AND DID NOT CLEAR. ALSO NOTICED THE L ITT GAUGE WOULD INTERMITTENTLY GO TO AMBER DASHES AND THE TO CARROT ON THE L N1 GAUGE WOULD GSDR DXTA2024111501125Battery Pack · inoperativeLAV EXIT SIGN/LIGHT: SOME EMERGENCY LIGHTING IS INOPERATIVE. EXIT SIGN ON BULKHEAD BEHIND SEAT 7, EXIT SIGN ON TOILET FACE PANEL, DOWN LIGHTS AT TOILET BASE ARE ALL INOP. PACK WAS CHARGED FOR 30 MINUTES ON APU WITH NO CHANGE. CORRECTIVE ACTION; REPLAED FAULTYSDR DXTA2024111401118Unknown · noiseSECOND FLIGHT OF THE DAY. RIGHT ENGINE STARTED NORMALLY. LEFT ENGINE AT GROUND IDLE HAD A NOTICABLE HARMONIC HUM / VIBRATION (SIMILAR TO A RUMBLE STRIP ON THE SIDE OF THE ROAD AT SLOW SPPED). VIBRATION DID CHANGE WITH CHANGE IN RPM. NO ABNORMAL INDICATIONS NSDR DXTR2024111101Vortex Gen · corrodedCORROSION UNDER LH LOWER VORTEX GENERATOR TAIL CONE STINGER. RESOLUTION: ACCOMPLISHED MINOR REPAIR IAW RFTS-112233SDR DXTA2024111401110Control Unit · faultedDURING APPROACH PRIM STAB TRIM FAIL APPEARED TWICE. DURING CLIMB AND DESCENT RECEIVED NOSE TRIM DOWN MESSAGES. FOLLOWED PROCEDURE AND THE STAB TRIM WAS AT 1.0 AND WOULD NOT MOVE. WE ARE UNABLE TO DESCEND FASTER THEN 270 KTS WITHOUT THE TRIM NOSE DOWN CAS MESDR DXTA2024111101102Battery Pack · dischargedCABIN EMERG LIGHT: READ LIGHT ABOVE SEAT 7 NOT ILLUMINATING DURING THE EMER LTS TEST NOR WHEN THE EMER LTS SWITCH IS IN THE ON POSITION. CORRECTIVE ACTION; POWERED ON AIRCRAFT AND LET THE EMERGENCY BATTERIES CHARGE.. OPS CHECK CHECK OF EMERGENCY LIGHTING IS GOSDR DXTA2024111101090Door · out of rigMAIN DOOR: REPEAT WRITEUP. MAIN CABIN DOOR STICKS AND REQUIRES FORCE TO OPEN. CORRECTIVE ACTION; ADJUSTED MAIN CABIN DOOR RIGGING IAW CE680A AMM 52-10-00. OPS CHECK GOOD. DOOR DOES NOT STICK IN CLOSED POSITION.SDR DXTA2024110801083Battery Pack · inoperativeLAV EMERG LIGHT: THE LAV RED EMERGENCY LIGHT, FLOOR KICK PLATE LIGHT, AND READING LIGHT WILL NOT ILLUMINATE. ALSO, THE OTHER EMERGENCY LIGHTS WILL ONLY ILLUMINATE WITH THE EMER SWITCH TO ON. WHEN THE SWITH IS ARMED, NONE OF THE LIGHTS ILLUMINATE. WE CHARGESDR DXTA2024110801065Switch · faultyELEVATOR CONTROL/TRIM: ON DEPARTURE NEITHER RIGHT/LEFT PRIMARY PITCH TRIM SWITCH HAD ANY AFFECT ON TRIM. SECONDARY TRIM INITIALLY DID NOT RESPOND BUT EVENTUALLY DID RESPOND. ONCE ON GROUND, AND SECONDARY TRIM SWITCH OFF, NEITHER LEFT/RIGHT PRIMARY TRIM SWITSDR DXTA2024110801068Door · bindingMAIN DOOR: MAIN CABIN DOOR DOES NOT OPEN ON IT'S OWN AS NORMAL. THE DOOR SEEMS TO BE BINDING ON THE FORWARD SIDE AND NEEDS TO BE PUSHED TO GET IT TO OPEN. CORRECTIVE ACTION; CHECKED THE DOOR AND COULD NOT FIND ANYTHING THAT WOULD CAUSE THE DOOR TO NOT OPEN. THSDR DXTA2024110801061Switch · defectiveWHILE AT CRUISE WE NOTICED THE MAIN CABIN DOOR EXIT LIGHT WAS FLICKERING WHEN THE PAX SAFETY SWITCH WAS OFF. CORRECTIVE ACTION; REMOVED AND REPLACED INERTIA SWITCH SC001 IAW CESSNA MODEL 680A MM 33-50-11. OPS CHECK GOOD.SDR DXTA2024110701053Handle · bindingMAIN DOOR HANDLE: MAIN DOOR HANDLE IS VERY SIFF WHEN CLOSING OR OPENING DOOR. CORRECTIVE ACTION; COMPLIED WITH OPERATIONAL TEST OF CABIN DOOR IAW CE680A AMM 52-10-00, MAX ALLOWABLE HANDLE FORCE IS 50 LBS, FOUND LESS THEN 2 LBS REQUIRED. LUBRICATED PINS IA W CESDR DXTA2024110501051Battery Pack · faultedDURING THE EMERGENCY LIGHTS TEST, WHEN PLACING THE SWITCH TO EMER LIGHTS ARM, NO EMERGENCY LIGHTS ILLUMINATE. PRIOR DAY HAD TO CHARGE THE LIGHTS PER THE CHECKLISTS. CORRECTIVE ACTION; REPLACED FAULTY #1 EMER LIGHT BATTERY PACK !AW CE-680A AMM CH. 33-50-06. CH
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