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 DXTA2025091904997Battery Pack · no testDURING PREFLIGHT, POWER ON CHECKLIST, EMER LTS CHECK, THE FLOOR EMEGENCY EXIT LIGHT AT SEAT 8 WOULD NOT ILLUMINATE. ALL OTHER LIGHTS EXCEPT SEAT 5 WORKED AS DESIGNED. SEE SEPERATE WRITE UP FOR SEAT 5. EMERGENCY LIGHT COMES ON BRIEFLY, THEN GOES OUT. SUSPECT BASDR DXTA2025091704961Actuator · defectiveDURING LANDING GEAR EXTENSION WE RECEIVED GEAR DISAGREE L CAS MESSAGE FOLLOWED BY CROSS HATCHED LEFT MAIN GEAR INDICATION. FOLLOWED THE QRH USING THE LANDING GEAR BLOWDOWN AND MAIN MANUAL RELEASE HANDLE. WE NEVER GOT A 3 GREEN, LANDED NORMALLY. REPLACED LT MLSDR DXTA2025091504962Door · bindingINTERMITTENT MAIN CABIN DOOR HANDLE BINDING, WON`T MOVE TO THE CLOSED POSITION. IF YOU PLAY WITH THE HANDLE, IT WILL CLOSE BUT THEN BIND AGAIN AFTER A COUPLE MORE CYCLES OF THE HANDLE. GAINED ACCESS TO DOOR INTERIOR AND VERIFIED RIGGING WAS WITHIN LIMITATIONSSDR DXTA2025091504936Fuse · failedLEFT EXTERIOR EMERGENCY LIGHT INOP REPLACE FUSE . SUPPLIED BY NET JETS. ALL WORK DONE IN ACCORDANCE WITH CE-680A SPM 20-30-00. PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTING. ALL WORK DONE IN ACCORDANCE WITH C6 AM 33-50-00. OPS CHECK GOOD.SDR 2025F00219Skin · gougedMECHANICALLY BLENDED HIGH SPOTS ON A GOUGE ON THE RH WING LEADING EDGE APPROXIMATELY 3.25 INCHES OTBD OF THE START OF THE LEADING EDGE. POLISHED AND RETURNED AREA TO ORIGINAL SURFACE FINISH IAW CESSNA 680 SPM 51-70-02 AND NETJETS ENGINEERING RFTS-114953 REV. 0SDR DXTA2025091504916G Switch · faultedTHE FOLLOWING EMERGENCY LIGHT COMPONENTS REMAIN ILLUMINTED AFTER THE EMERGENCY SWITCH IS TURNED OFF- WHITE MAIN DOOR EXIT SIGN, SEAT 3 READING LIGHT AND FLOOR LIGHT, WING INSPECTION LIGHT. EMERGENCY LIGHTS REMAIN ON AFTER SHUTDOWN PROCEDURE DID NOT CLEAR THE SDR DXTA2025091104905Battery · dischargedAFT EMERGENCY LIGHTS WILL NOT TURN OFF CORRECTIVE ACTION: POWERED AIRCRAFT USING EXTERNAL POWER PER AFM NOTING THE AFT LAV EMERGENCY LIGHTS ILLUMINATED. GAINED ACCESS TO #4 EMERGENCY LIGHTING INERTIA SWITCH AND RESET AS REQUIRED NOTING LIGHTS WERE NO LONGERSDR DXTA2025091004896Torque Link · defectiveDURING LANDING ROLLOUT AT ABOUT 50KTS, AIRCRAFT EXPERIENCED A TOTAL LOSS OF HYDRAULIC STEERING ACCOMPANIED BY A SEVERE NOSE GEAR CAVITATION. DURING INVESTIGATION IT WAS DISCOVERED THAT NOSE PIN HAD SHEARED FROM THE T-HANDLE INTO TWO SEPARATE PIECES. OUTER BASDR DXTA2025091004898Arm · detachedMAIN CABIN DOOR LIFT ACTUATOR ARM HAS SEPARATED FROM MAIN CABIN DOOR. ARRIVED AT AC AND PREPPED FOR MX. INSTALLED NEW WASHERS PN: S1438-20, HINGE PIN PN: 7411323-5, BEARING PN: M81934/1-04C005 AND RETAINER RING PN: MS16625-4032 THAT ATTACH THE CABIN DOOR LISDR DXTA2025090904884Handle · unknownDOOR HANDLE PHYSICALLY WILL NOT ROTATE TO CLOSED POSITION, EITHER FROM OUTSIDE OR INSIDE THE CABIN. FOUND DOOR TO OPEN AND CLOSE NORMAL. PERFORMED DOOR HEALTH CHECK PER CE680A AMM 52· 10-04, ALL CHECKS ARE NORMAL AND WITHIN LIMITS. NO FURTHER ACTION IS REQUSDR DXTA2025090904876Wire Harness · defectiveON DEPARTURE AFTER GEAR SELECTED UP, WE GOT AN AMBER GEAR DISAGREE CAS MSG WITH AN INDICATION OF THE RIGHT MAIN GEAR AMBER DN ON THE EICAS DISPLAY. WE RAN THE QRH AND LOWERED THE GEAR. GEAR THEN INDICATED 3 GREEN. PROCEEDED TO AN UNEVENTFUL LANDING. REMOVSDR DXTA2025090804846Power Supply · defectiveDURING PREFLIGHT WHILE CHECKING THE EMERGENCY BATTERY, WE DISCOVERED THE EMERGENCY AISLE LIGHT UNDER SEAT 3 AND THE RIGHT WING INSPECTION LIGHT DO NOT WORK ON THE EMERGENCY BATTERY PACK. LIGHTS DO WORK ON SHIPS POWER. CORRECTIVE ACTION: REMOVED #2 EMERGENCY BASDR DXTA2025090804837Power Supply · defectiveALL EMERGENCY EXIT LIGHTS FAIL PREFLIGHT TEST ON FIRST FLIGHT OF DAY. BATTERIES FAIL TO HOLD CHARGE. REPEAT WRITE UP. CORRECTIVE ACTION: REMOVED #4 EMERGENCY BATTERY PACK P/N: CB528-1 S/N: 009475 INSTALLED CUSTOMER SUPPLIED SERVICEABLE BATTERY PACK P/N: 643002SDR DXTA2025090804831Battery Pack · malfunctionedEMERGENCY BATTERY PACK NUMBER TWO WILL NOT TURN OFF. ACCOMPLISHED AN EMERGENCY CHECKLIST TO PUSH PEDESTAL BUTTON. THE LIGHTS DID NOT GO OUT. THE EMERGENCY LIGHTS THAT ARE ILLUMINATED ARE THE EXIT SIGN OVERHEAD CABIN DOOR, SEAT THREE EMERGENCY FLOOR LIGHT, SESDR DXTA2025090404807Pin · recessedCLOSING THE MAIN CABIN DOOR FEELS LIKE ONE OF THE PINS IS BINDING. A LOT OF PRESSURE IS NEEDED TO CLOSE IT. UPON INITIAL MX INSPECTION OF MCD, FOUND THE MCD LOWER AFT TAPER PIN RECESSED SLIGHTLY TOO FAR INTO THE DOOR WHICH RESTRICTED THE OPERATION OF THE INNSDR DXTA2025090404809Battery · defectiveUPON POST FLIGHT WE NOTICED AS WE TURNED THE BATTERIES OFF AND THE EMER LIGHTS STILL ARMED THE EMER LIGHTS UNDER SEAT 5 AND 8 DID NOT STAY LIGHT. CORRECTIVE ACTION: PICKED UP PART FROM FBO. SET UP TOOLING. REMOVED FAILED BATTERY PACK #3 PN 6430028-1 SN E25-130SDR DXTA2025090404784Handle · malfunctionedREPEAT RIGHT UP. THE LATCHING HANDLE ON THE MAIN CABIN DOOR WILL NOT ENGAGE. THE HANDLE WILL NOT MOVE INSIDE OR OUTSIDE WHEN THE DOORS IN THE CLOSED POSITION DOOR IS CURRENTLY OPEN. CORRECTIVE ACTION: LUBED PINS AND DOUBLE CHECKED ALL HARDWARE SAFETIES. REASSESDR DXTA2025090304778Latch · faultedTHE LATCH WILL NOT ENGAGE ON THE MAIN CABIN DOOR FROM THE INSIDE OR THE OUTSIDE. THE DOOR IS CURRENTLY OPEN. ARRIVED AT AIRCRAFT AND CONFIRMED PILOT WRITE UP MAIN CABIN DOOR WILL NOT LATCH. TECH ATTEMPTED TO MOVE THE INTERIOR DOOR HANDLE TO FIND THE DOOR LATSDR DXTA2025090204765Power Supply · defectiveCABIN EMERGENCY LIGHTING NOT FULLY ILLUMINATING: FLOOR LIGHTING NEAR SEATS 5 AND 7 AND OVERHEAD READING LIGHT AT SEAT 7 INOP AS WELL AS EXTERIOR OVER WING LIGHT OVER RIGHT WING ARE ALL INOP. COMPLIED WITH QRH RECHARGING PROCEDURES FOR 60 MINUTES TO NO AVAIL. SDR DXTA2025090204764Wire · pulledLAV EMERGENCY TOE KICK LIGHT DOES NOT ILLUMINATE WITH ANY POWER SOURCE. REMOVED LAV FASCIA & FOUND THE WIRES FOR THE TOE KICK LIGHT PULLED OUT OF THE CONNECTOR. LOOKED UP & PLACED NEW CONNECTOR & PINS ON ORDER. 8/30 JT-VJG. INSTALLED NEW PINS ONTO WIRE & INSSDR DXTA2025090204759Proximity Switch · defectiveAMBER CAS "CHECK DOORS" AND "CABIN DOOR OPEN" WILL NOT EXTINGUISH AFTER DOOR CLOSED AND QRH PROCEDURES COMPLETED. AMBER DOOR OPEN LIGHT ON CABIN DOOR STAYS ILLUMINATED WITH DOOR HANDLE ENGAGED. CORRECTIVE ACTION: REPLACED MAIN CABIN DOOR LATCH PAWL PROXIMITY SSDR 2025F00214Skin · damagedREPAIRED CORROSION UNDER THE BAGGAGE FLOOR BOARDS ON THE TAILCONE SKIN AND STRINGERS BETWEEN FS 501.25 AND FS 548.50 PER AQRD ERO-985795 REV.A, TITLED "N357QS TAILCONE SKIN CORROSION" DATED AUG 28, 2025. SUPPORTED BY FAA FORM 8110-3 DATED 08/28/2025. THE FATIGSDR DXTA2025082904738Warning Message · false activationAT THE FINAL APPROACH FIX SELECTED FLAPS FULL. WITH FLAPS ALMOST INDICATING FULL THE INDICATION WENT YELLOW AND RECEIVED THE FLAPS FAIL CAUTION. CHECKED FLAP LEVER DETENT, PRESSED RESET BUTTON AND FLAPS FAIL CAUTION REAPPEARD. PERFORMED FLAP CONTROL SYS TROUBSDR DXTA2025082904740Sign · inoperativeEMER SIGN LIGHT, BEHIND SEAT 7, FACING FORWARD INTO CABIN- LIGHT INOP. NEITHER BATTERY OR SHIP POWER LIGHT THE SIGN CORRECTIVE ACTION: REMOVED THE DEFECTIVE EMER EXIT SIGN LIGHT, BEHIND SEAT 7, FACING FORWARD INTO CABIN, P/N 9919054-1, S/N 21A82 AND INSTALLED SDR 2025F00201Skin · corrodedMECHANICALLY BLENDED 7 AREAS OF CORROSION LOCATED BELOW AFT BAGGAGE FLOOR BETWEEN FS534.70 AND FS548.50 IAW SRM 51-70-02. FOUND CORROSION BLEND TO BE BEYOND LIMITS IAW SRM 51-70-02 EXCEEDING 0.002" OF MATERIAL REMOVED FROM NOMINAL THICKNESS. REPAIRED CORROSISDR 2025F00200Skin · corrodedMECHANICALLY BLENDED 12 AREAS OF CORROSION LOCATED BELOW AFT BAGGAGE FLOOR BETWEEN FS519.37 AND FS534.70 IAW SRM 51-70-02. FOUND 10 AREAS OF CORROSION BLENDING TO BE WITHIN LIMITS IAW SRM 51-70-02. PROTECTED BARE METAL IAW C680 SRM 51-20-01. THIS IS A PSE ARESDR 2025F00199Skin · corrodedMECHANICALLY BLENDED 17 AREAS OF CORROSION LOCATED BELOW AFT BAGGAGE FLOOR BETWEEN FS468.05 AND FS484.65 IAW SRM 51-70-02. FOUND CORROSION BLEND TO BE BEYOND LIMITS IAW SRM 51-70-02 EXCEEDING 0.002" OF MATERIAL REMOVED FROM NOMINAL THICKNESS. REPAIRED CORROSIOSDR 2025F00198Structure · corrodedMECHANICALLY BLENDED 7 AREAS OF CORROSION LOCATED BELOW AFT BAGGAGE FLOOR BETWEEN FS501.25 AND FS519.37 IAW SRM 51-70-02. FOUND 5 AREAS OF CORROSION BLENDING TO BE WITHIN LIMITS IAW SRM 51-70-02. PROTECTED BARE METAL IAW C680 SRM 51-20-01. THIS IS A PSE AREA ISDR DXTA2025082804725Motor · faultedMAIN ENTRY DOOR LATCHING HANDLE DOES NOT MOVE TO THE LATCHED POSITION SMOOTHLY, REGARDLESS WHETHER IT IS BEING CLOSED FROM THE INSIDE OR OUTSIDE. IT FEELS LIKE ONE OR MORE OF THE LATCHING PINS IS OUT OF ALIGNMENT. REMOVED AND REPLACED MAIN CABIN DOOR LIFTINSDR DXTA2025082704720Light · intermittentLAV FLOOR EMERGENCY LIGHT ILLUMINATES ONLY INTERMITTENTLY. LAV EMER LIGHT STRIP INTERMITTENT: REMOVED LIGHT STRIP AND INSTALLED ABOVE UNIT. OPS CHECKS GOOD. IAW AMM 33-50-00.SDR DXTA2025082504719Warning Light · false activationAMBER CABIN DOOR LIGHT WILL NOT EXTINGUISH AFTER FULLY CLOAING DOOR. AMBER CAS MESSAGE CHECK DOORS AND CABIN DOOR OPEN DISPLAYED. PERFORMED MED CABIN DOOR SYS RESET IAW QRH PROCEDURES AND CE680A MM 52-10-00 OPS/CK GOOD. CMC DOOR SENSOR INDICATION BECAME AVSDR DXTA2025082604711Unknown · odorSLIGHT BURNING ODOR IN THE ACFT AT FL 210. OUTSIDE RAM AIR TEMP WAS 12 DEGREES C. NO SMOKE WAS PRESENT. NO UNUSUAL ODOR OR BURNING SMELL WAS NOTICED. STARTED APU FOR POWER AND BLEED SOURCE, OPERATED ALL CABIN SYSTEMS WITH NO ABNORMAL SMELLS. VISUALLY INSPECSDR DXTA2025082604714Flt Controls · faultedCLEARED FOR VISUAL APPROACH, DISCONNECTED AUTOPILOT ON LEFT BASE LEG (YD AND AT STILL ENGAGED). AT APRX 1800FT INITIATED A LT TURN & NOSE DOWN PITCH WITH YOKE. ACFT UNRESPONSIVE & WOULDN'T ROLL OR PITCH. ACFT FELT SLUGGISH. CHECKED SPEED, ASKED FO IF CONFIGURESDR DXTA2025082504718Latch · out of adjustMAIN DOOR LATCH HANDLE WON'T CLOSE FROM OUTSIDE. FOUND AFT LATCHES/LOCKOUT OF ADJUSTMENT. PERFORMED CABIN DOOR LATCH/LOCK RIGGING REF AMM 52-10-04 OPS CHECKS GOOD. REF AMM 52-10-00.SDR DXTA2025082604706Flap System · failedFLAPS FAIL AMBER CAS MSG ON APPROACH. RESET 1X & MSG REMAINED. FLAPS FAILED IN NR 1. INSPECT, BITES 2, 5, 6, & 8 SET ON FLAP CONTROLLER. FLAPS OPS. CLEARED FAULTS. LINXUS HAD NUMEROUS CASCADING FAULTS IN 2 MINS, FLAPS FAIL, NO FAULTS, FLAP CONTROLLER INVALID ISDR DXTA2025082504703Light · no testSECOND DAY IN A ROW EMERGENCY LIGHTS DO NOT TEST PROPERLY IN POWER ON CHDCKLIST. IN THE ON POSITION, NONE OF THE EMERGENCY LIGHTS COME ON. REMOVED AND REPLACED ELBP NR 1, 2, 3, 4,SDR 2025FA0000564Stringer · corrodedFABRICATE STRINGER TO REPLACE CORRODED STRINGER UNDER PANEL 316CBC DUE TO PART AVAILABILITY. COMPLIED WITH RFTS-114737 N532QS (680A-0073) AFT FAIRING SUPPORT FRAME 09 STRAP FABRICATION. REV.0 DATED 18AUG25. THIS IS A PERMANENT MINOR REPAIR.SDR DXTA2025082504682Stop Fitting · out of adjustMAIN CABIN DOOR LATCH REQUIRES MORE FORCE THAN NORMAL CLOSING. "CORRECTIVE ACTION" PERFORMED THE MAIN CABIN DOOR HEALTH CHECK/DATA COLLECTION CHECK LIST REFERENCING CESSNA MODEL 680A MAINTENANCE MANUAL CH 52-10-04 NOTING THAT THE INNER HANDLE DID NOT CONTACT TSDR DXTA2025081904632Battery Pack · no testDURING PREFLIGHT FOUND EMERGENCY LIGHT UNDER SEAT 5, SEAT 8 AND OVER SEAT 7 TO BE INOP. PERFORMED CHARGING PROCEDURE IN QRH AND LIGHTS REMAINED INOP. REMOVED FAULTY #3 EMERGENCY BATTERY PACK & INSTALLED REPAIRED BATTERY PACK IAW CE-680A MM CHAP 33-50-06. PERFOSDR DXTA2025081904629Actuator · malfunctionedON FINAL, GEAR WAS EXTENDED AND NG DID NOT EXTEND. WE RETRACTED THE HANDLE, PAUSED, AND GEAR EXTENDED NORMALLY ON THAT ATTEMPT. REMOVED FAULTY NLG UPLOCK ACTUATOR AND INSTALLED THE NEW UPLOCK ACTUATOR USING ONE NEW SPRING IAW MM 32-32-15. APPLIED ELECTRICAL &SDR DXTA2025081804624Light · inoperative33-50-04 RIDE SIDE OVERWING EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE DURING TEST OR ANY OTHER MODE WHEN IT SHOULD BE ILLUMINATED. R & R RT OVERWING EMERGENCY LIGHT IAW AMM 33-50-20. OPS CHECKED GOOD.SDR DXTA2025081504605Warning Light · illuminatedRED AUTO THROTTLE HOLD FAIL CAS CAME ON AT 30KTS ON TAKEOFF AND THE AUTO THROTTLES WERE REDUCING POWER AS THIS OCCURRED. PERFORMED TWO SETS OF OPS CHECKS SUCCESSFULY AND SENT AN ARES DOWNLOAD TO MCC AND TEXTRON. MCC ELECTED TO KEEP ORIGINAL A/T INSTALLED DUESDR DXTA2025081504607Steering Unit · malfunctionedUPON GEAR RETRACTION DURING CLIMB OUT, THE NOSE LANDING GEAR TOOK AN EXCESSIVELY LONG TIME TO RETRACT AND RESULTED IN A TEMPORARY NOSE GEAR DISAGREE CAS MESSAGE, AS WELL AS THE WHITE HASH MARKS ON GEAR INDICATOR. NOSE GEAR DID EVENTUALLY COME UP WITHOUT FURTHESDR DXTA2025081504609Pressure Switch · faultedAT ABOUT 5000FT AFTER TAKEOFF THE FUEL BOOST PUMP ON YELLOW CAS MASSAGE CAME ON. COMPLETED QRH AND LANDED AS SOON AS PRATICAL. RT ENG FUEL PRESSURE SWITCH, RT ENG FUEL PRESSURE SWITCH, RT ENGINE FUEL BOOST PUMP CP, RT ENGINE FUEL BOOST PUMP CP. RT ENGINE FUSDR DXTA2025081504612Door · out of adjustENTRY DOOR IS DIFFICULT TO OPEN. HAD TO CYCLE IT COUPLE TIMES TO GET AMBER DOOR OPEN LIGHT OUT CORRECTIVE ACTION: FOUND DOOR TOO FAR FORWARD IN FRAME (0.050 FWD AND 0.200 AFT). ADJUSTED DOOR AFT TO 0.125" FWD CLEARANCE AND 0.125" AFT CLEARANCE. PERFORMED MULSDR DXTA2025081404594Pin · missingWHILE OPENING MAIN CABIN DOOR THE LEFT CONNECTING LINKAGE CAME APART. PARTS ARE ON THE COUNTER. CORRECTIVE ACTION: ACCESSED AIRCRAFT AND NOTED THE DOOR LINKAGE HARDWARE ON THE GALLEY COUNTY AS LEFT BY THE / CREW. TECHS NOTED THAT THE HARDWARE WAS MISSING THESDR DXTA2025081204582Pin · over extendedTRIED TO CLOSE THE DOOR FROM BOTH INSIDE AND OUTSIDE. NEITHER HANDLE WILL MOVE. UPON ARRIVAL TO THE AIRCRAFT WE FOUND THAT THE DOOR WOULD NOT CLOSE. TRIED TO MOVE. THE HANDLE TO THE LOCKED POSITION AND FOUND THAT THE DOOR WAS BINDING UP INSIDE. GAINED ACCESS TSDR 2025F00188Skin · corroded1 AREA OF CORROSION FOUND ON E-EXIT OUTER SKIN, UPPER /AFT CORNER. MECHANICALLY REMOVED 1 AREA OF CORROSION LOCATED ON E-EXIT, EXTERIOR SKIN, UPPER AFT CORNER AREA IAW C680 SRM 51-70-02. FOUND CORROSION BLEND TO BE BEYOND SRM LIMITS IAW C680 SRM 51-70-02 EXCEESDR 2025F00187Thrust Reverser · faultedDURING INSPECTION OF THE LH TR NOTED MULTIPLE SPOTS OF CORROSION ON THE INSIDE SIDES OF THE UPPER BUCKET. MECHANICALLY BLENDED 13 EA. AREAS OF CORROSION ON THE LH THRUST REVERSER UPPER DOOR, INBD AND OUTBD AREAS IAW CE680A SRM 51-10-01 AND SRM 51-70-03. AFTER SDR 2025F00180Structure · corrodedFOUND THAT LH EMERGENCY BRAKE CARRY THROUGH CORRODED AROUND FITTING ON RIB LOCATED AT W.S. 37.00. DISCONNECTED EXISTING LH MLG EMERGENCY BRAKE PNEUMATIC LINE AND REMOVED EXISTING CARRY-THROUGH FITTING ON RIB LOCATED AT W.S. 37.00 FOR ACCESS. MECHANICALLY BLEND
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