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 DXTA2026052708211Uplock · faultedAFTER TO GOT GEAR DISAGREE N. SOUNDED LIKE GEAR WAS UP BUT COUPLE MINUTES LATER HEARD A BANG IN THE NOSE GEAR WELL AND NOSE GEAR INDICATED UP. GEAR WENT DOWN WITH NO ISSUES REMOVED NOSE GEAR UPLOCK SWITCH P/N: S3177-1 S/N: NSN. -INSTALLEDSUPPLIED NEW SWITCH SDR DXTA2026052608214Pressure Switch · faultyAT CRUISE ALTITUDE FL410 ATTEMPTED TO CROSSFEED L TANK TO R ENG IMMEDIATLEY RECEIVED AMBER FUEL BST PUMP ON L R RAN QRH MESSAGE REMAINED BUT TURNED WHITE AS QRH SAID IT WOULD AFTER TURNING BOOST PUMPS ON. CORRECTIVE ACTION: REMOVED AND REPLACED LH ENGINE FUESDR DXTA2026052208177Link · corrodedPOTENTIAL PITTING FOUND ON THE RH TRAILING LINK WHILE COMPLETING SL680A-32-11 REMOVED ORIGINAL RT MLG TRAILING LINK 32-10-15. PERFORMED ALL POST MAINTENANCE CHECKS IAW MM CHECKS GOOD. REMOVED & INSTALLED REPAIRED TRAILING LINK IAW MM 32-00-00. ALL POST MAINTSDR DXTA2026052208176Link · damagedPOTENTIAL ARCING, CRACKING, & PITTING FOUND ON THE LH TRAILING LINK WHILE COMPLETING SL680A-32-11. REMOVED ORIGINAL LT MLG TRAILING LINK 32-10-15. PERFORMED ALL POST MAINTENANCE CHECKS IAW MM CHECKED GOOD. REMOVED AND INSTALLED A REPAIRED TRAILING LINK IAW MMSDR DXTA2026052608164Uplock Switch · faultedR MAIN LANDING GEAR DISAGREE IN FLIGHT. CREW PERFORMED CHECKLIST, INCLUDING BOTTLE FOR BLOWDOWN AND REAR MAIN LANDING GEAR RELEASE. REMOVED UPLOCK LANDING GEAR SWITCH AND INSTALLED CUSTOMER SUPPLIED NEW IAW AMM 32-32-25, OPS CHECK GOODSDR DXTA2026052608171Lift Strut · faultedUPON LANDING WHEN OPENING MAIN CABIN DOOR DOOR DID NOT FULLY GRAVITY FALL TO THE OPEN POSITION STAYED RAISED 3 TO 5 INCHES FROM FULLY OPEN. INSTALLED NEW LIFT ARM AND LIFT ARM LINK. INSTALLED NEW GAS STRUT WITH NEW BOLTS, INSTALLED NEW STRUT DRIVE ARM ASSY,SDR DXTA2026052608167Bracket · brokenUPON LANDING WHEN OPENING MAIN CABIN DOOR DOOR DID NOT FULLY GRAVITY FALL TO THE OPEN POSITION STAYED RAISED 3 TO 5 INCHES FROM FULLY OPEN. GAINED ACCESS TO MCD FRAME. FOUND SNUBBER SUPPORT BRACKET EAR BROKEN OFF AND AFT SUPPORT / BRACKET CRACKED. REMOVED DOSDR DXTA2026052108172Pin · lack of lubeMAIN CABIN DOOR HANDLE DIFFICULT TO FULLY ENGAGE IN LOCKED POSITION WHEN CLOSING DOOR FROM EITHER INSIDE OR OUTSIDE. HANDLE TRAVELS FREELY WHEN DOOR IS OPEN. OPERATED DOOR/DOOR HANDLE MULTIPLE TIMES FROM BOTH INSIDE AND OUTSIDE WITH DOOR IN THE OPEN AND CLOSSDR DXTA2026052108168Pin · out of alignmentWHILE CLOSING THE MAIN ENTRY DOOR, WHEN TRYING TO CLOSE THE DOOR, THE HANDLE IS VERY DIFFICULT TO GET DOWN INTO THE STOWED POSITION. WE ALLOWED THE DOOR TO GO TO THE FULL OPEN POSITION CHECKING THE DOOR PINS AND LOOKING FOR MISALIGNMENT. WE THEN LIFTED THE DSDR DXTA2026052108152Check Valve · leakingNOSE GEAR FAILED TO RETRACT IN NORMAL SEQUENCE UPON SELECTING GEAR -UP AFTER TAKEOFF. CAS MSG APPEARED. APPROX 30SEC LATER, WITH NO ADDITIONAL INPUT, NOSE GEAR RETRACTED AND NORMAL GEAR -UP ICONS DISPLAYED. GEAR DEPLOYED NORMALLY TO 3GREEN UPON SELECTING GSDR DXTA2026052108146Uplock Switch · faultedAFTER TAKEOFF AND GEAR UP SELECTED WE RECEIVED GEAR DISAGREE N CAS MSG. BASED ON NOISE LEVEL WE BELIEVE THE GEAR WAS UP. RAN CHECKLIST INCLUDING LANDING GEAR WILL NOT RETRACT WITH (BLACK AND YELLOW BOX WITH SLASHED LINES). GOT THE GEAR DOWN SUCCESSFULLY WITH SDR DXTA2026052008145Door Seal · damagedMED THE MIDDLE OF THE THREE DOOR SEALS HAS COME LOSE FROM THE AFT DOOR POST. ENOUGH OF THE SEAL IS LOSE THAT IT MIGHT IMPEDE THE DOOR NORMAL OPERATIONS. REMOVED OLD EDGE TRIM AND REPLACED WITH NEW PN 3619065-6. BONDED EDGE TRIM TO DOOR SURROUND STRUCTURE RESDR 2026F00110Landing · corrodedFOUND SIGNS OF CORROSION UNDER 9 NUTPLATES UNDER PANEL 154BC. MECHANICALLY REMOVED 9 AREAS OF CORROSION LOCATED WHERE 8 NUTPLATES WERE PREVIOUSLY REMOVED INSIDE FUSELAGE BAY 154BC IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW CESSSDR 2026F00109Landing · corrodedBUBBLING PRIMER AND WHITE POWDER AROUND AND UNDER 26 NUTPLATES UNDER PANEL 154AC. MECHANICALLY REMOVED CORROSION LOCATED WHERE 26 NUTPLATES WERE PREVIOUSLY REMOVED IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW CESSNA 680 SRM 51-7SDR 2026F00108Support · corrodedFOUND CORROSION UNDER MULTIPLE NUTPLATES FOR PANEL 342AB.MECHANICALLY REMOVED CORROSION LOCATED WHERE 13 NUTPLATES WERE PREVIOUSLY REMOVED ON INNER AND OUTER SKIN SURFACES INCLUDING AREAS OF CORROSION LOCATED ALONG ANGLE STRAP EDGES IAW CESSNA 680 SRM 51-70-02SDR DXTA2026051808122Elec Connector · disconnectedSEAT 10 CABIN EMERGENCY LIGHT DIODE STRIP COMPLETELY INOP. NO LUMINOSITY IN EITHER ARM, OR ON, AFTER A BRIEF CHARGE. GAINED ACCESS TO SEAT 10 TOE KICK LIGHTING CONNECTOR AND FOUND IT TO BE DISCONNECTED. GAINED FURTHER ACCESS TO PHYSICALLY CONNECT THE TWO CONSDR 2026F00104Stringer · corrodedCENTER STRINGER UNDER PANEL 164BC HAS 3 AREAS OF CORROSION. REMOVED BUBBLED PRIMER FROM 3 AREAS AND VERIFIED CORROSION LOCATED INSIDE FUSELAGE BAY 164BC ON CENTER STRINGER. MECHANICALLY REMOVED CORROSION AND PITTING PER CESSNA 680 SRM 21-70-02. FOUND CORROSIONSDR 2026F00103Landing · corrodedCORROSION ON PANEL LANDS FOR PANEL 164AC. REPAIRED CORROSION ON PANEL LANDS FOR PANEL 164AC IN REFERENCE TO NETJETS REQUEST FOR TECHNICAL SERVICES (RFTS): RFTS-117178 REV. 0; TITLED: N361QS (680-0235) PANEL 164AC NUTPLATE CORROSION; DATED: 11 MAY 2026.SDR 2026F00102Stringer · corrodedCENTER STRINGER UNDER PANEL 164AC HAS 5 AREAS OF CORROSION. REMOVED BUBBLED PRIMER FROM 5 AREAS LOCATED IN FUSELAGE BAY 164AC ON CENTER STRINGER AND VERIFIED CORROSION. MECHANICALLY REMOVED CORROSION AND PITTING PER CESSNA 680 SRM 21-70-02. FOUND CORROSION BLESDR DXTA2026051108009Control Handle · inoperativeAFTER TAKEOFF THE AMBER WOW MISCOMPARE CAS MESSAGE CAME ON AND THE GEAR HANDLE WOULD NOT MOVE TO RETRACT THE GEAR.SDR 2026F00101Fitting · corrodedAFTER REMOVAL OF NLG ACTUATOR FOUND CORROSION ON THE AFT FITTING ASSEMBLY. PERFORMED NLG SKIN CUTOUT, REMOVED EXISTING CORRODED NLG ACTUATOR FITTING P/N 7411213-5, S/N 31533942U AND INSTALLED A NEW CUSTOMER SUPPLIED FITTING P/N 7411213-5, S/N 34783587V, IN SAMSDR DXTA2026050707992Actuator · defectiveDURING CLIMB AFTER TAKE OFF NOSE DOWN PRIMARY TRIM WAS SELECTED AS THE AIRCRAFT ACCELERATED TO NO EFFECT. THE TRIM REMAINED AT -2.9. EACH TIME NOSE DOWN TRIM WAS ATTEMPTED THE AMBER CAS PRI STAB TRIM FAIL MESSAGE APPEARED. SECONDARY TRIM WAS ACTIVATED AND MANSDR DXTA2026050707950Anti-Ice Valve · faultedDURING DESCENT WE SELECTED ALL A/I SYSTEMS ON FOR ICING CONDITIONS. ALL SYSTEMS OPERATED NORMALLY. UPON EXITING ICING CONDITIONS AT FL270, SELECTED ALL A/I SYSTEMS OFF. ABOUT 3 MINUTES AFTER SELECTING ALL A/I OFF, WE RECEIVED A/I ENGINE HOT R. ACCOMPLISHEDSDR 2026FA0000317Structure · corrodedACCOMPLISHED REMOVAL OF CORROSION TO AFFECTED AREAS OF VERTICAL STABILIZER. INSPECTED THE REMAINING MATERIAL USING ULTRASONIC TESTING AND EDDY CURRENT FOR CRACKS. NO CRACKS NOTED. ACCOMPLISHED DOUBLER REPAIR TO ONE NOTED LOCATION AND RESTORED FINISH TO ALL SURSDR 3J7R2026050400001Light Sys · dimRH OVER WING EMERGENCY LIGHT DIMSDR DXTA2026050407897Windshield · crackedRIGHT SIDE WINDOW CRACKED ON DECENT. FOLLOWED ABNORMAL PROCEDURE AND LANDED UNEVENTFULLY. YOU CAN FEEL IT FROM THE INSIDE. AND HEAVILY CRACKED AT THE TOP. WE HEARD IT IN FLIGHT. REMOVED RIGHT SIDE COCKPIT CRACKED WINDOW DUE TO IT CRACKING ON DECENT AND INSTALSDR DXTR2026050100314Skin · corrodedPOSSIBLE CORROSION ON LOWER LT WING SKIN AT TIP CAP. REMOVED CORROSION FROM SKIN REF SRM 51-10-01. NDT SERVICES PROVIDED BY TOLEDO JET CENTER, CRS 2TJR420B ON WORK ORDER 85280. NO CRACKS NOTED IN THE AREA OF INSPECTION AT THIS TIME. COMPLIED WITH STEPS 1 TSDR DXTA2026050407930Link · damagedACCOMPLISHED SL680A-32-11. (LANDING GEAR - MAIN LANDING GEAR TRAILING LINK ENHANCED INSPECTION) RT IAW SERVICE LETTER INSTRUCTIONS, PITTING NOTED AT THE UPPER AND LOWER BORE JUNCTION. CORRECTIVE ACTION: PERFORM FIELD REPAIR SR-680A-ATA32-52468 REV A ACCOMPLISSDR DXTA2026050407931Link · damagedACCOMPLISHED SL680A-32-11. (LANDING GEAR - MAIN LANDING GEAR TRAILING LINK ENHANCED INSPECTION) LT IAW SERVICE LETTER INSTRUCTIONS, PITTING NOTED AT THE UPPER AND LOWER BORE JUNCTION. PERFORM FIELD REPAIR SR-680A-ATA32-52468 REV A ACCOMPLISHED EDDY CURRENT ISDR DXTA2026050407871Light · faultedEXTERIOR EMERGENCY LIGHT ABOVE THE RIGHT WING IS NOT ILLUMINATING PROPERLY. BRIGHTNESS LEVEL IS NOT NORMAL (IT IS EXTREMELY ANEMIC) AND DOES NOT REALLY ILLUMINATE ANYTHING ANY MORE EVEN WITH THE APU RUNNING. REMOVED OVERWING EMERGENCY LIGHT ASSEMBLY. WIRE HASDR DXTA2026050107871Light · dimEXTERIOR EMERGENCY LIGHT ABOVE THE RIGHT WING IS NOT ILLUMINATING PROPERLY. BRIGHTNESS LEVEL IS NOT NORMAL (IT IS EXTREMELY ANEMIC) AND DOES NOT REALLY ILLUMINATE ANYTHING ANY MORE EVEN WITH THE APU RUNNING.SDR DXTA2026050407853Uplock Switch · out of adjustWHEN SELECTING THE MLG DOWN, RECIEVED MLG DISAGREE RT CAS MESSAGE ALONG WITH A RT MAIN AMBER X FOR RT MLG IND. RAN QRC FOR GEAR DISAGREE RT CAS MESSAGE & STILL DID NOT HAVE A GREEN DOWN & LOCKED. ONCE FLAPS SELECTED TO FULL, AMBER X FOR RT MLG CHANGED TO ASDR DXTA2026043007844Door · bindingTHE MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN OR CLOSE. WHEN CLOSING, IT TAKES SEVERAL ATTEMPTS BEFORE THE LIGHT WILL EXTINGUISH AND WHEN OPENING THIS LAST TIME IT TOOK A LOT OF FORCE TO LIFT THE HANDLE FROM INSIDE THE CABIN. MAIN CABIN DOOR HANDLES WERE CLEASDR DXTA2026042807808Pressure Switch · failedFUEL BOOST PUMP ON RIGHT INDICATION WHEN SELECTING LEFT CROSSFEED. WE RAN THE QRH AND MESSAGE CLEARED. WHEN WE SELECTED CROSSFEED AGAIN NOTHING ABNORMAL HAPPENED. WHEN WE SELECTED CROSSFEED OFF WE GOT BOTH FUEL BOOST PUMP ON MESSAGES. WE RAN THE QRH AND MESSAGSDR DXTA2026042807810Pcb · faultedJUST BEFORE LANDING WE HAD A CABIN DOOR OPEN CAS MESSAGE. WHILE ON THE GROUND WE TRIED TO RESET IT USING THE PROCEDURE IN THE QRH. STEP FOUR WAS UNSUCCESSFUL, WE COULD NOT GET THE CHECK HANDLE /PUSH TO OVERRIDE LIGHT TO FLASH. : REMOVED AND REPLACED NC105 CABISDR DXTA2026042707812Handle · bindingINSIDE MAIN CABIN DOOR HANDLE REQUIRES EXCESSIVE FORCE TO OPEN AND CLOSE. CYCLED THE DOOR SEVERAL TIMES AFTER THE FLIGHT WITH MIXED RESULTS. THE HANDLE INCONSISTENTLY APPEARS TO HANG UP DURING LATCHING OR UNLATCHING. GAINED ACCESS TO MED MECHANISM AND VISUALSDR 2026FA0000298Skin · corrodedLH HORIZONTAL STAB UPPER SKIN 3 SPOTS OF CORROSION FWD OF PANEL 351AC. FIX... COMPLIED WITH RFTS 117040 DATED 24APR26 AND REF CE 680A CSPM CH 20-50-00 TO NETJETS STANDARDS.SDR DXTA2026042707769Pump · leakingAT FL430 WE RECEIVED HYD PRESS LOW R CAS MESSAGE. ON HYDRAULIC SYSTEMS PAGE WE COULD SEE THE VOLUME OF FLUID SLOWLY DECREASING. EVENTUALLY CAS MESSAGE HYD VOLUME LOW ILLUMINATED. FOLLOWED QRH & UNLOADED BOTH HYDRAULIC PUMPS. PULLED BLOWDOWN BOTTLE FOR GEAR & LSDR DXTA2026042707759Switch · unsecureTHREE POSITION EMERGENCY LIGHT SWITCH SEEMS SHORTED IN THE ON POSITION. LIGHTS FLICKER WHEN THE SWITCH IS MOVED LEFT OR RIGHT WHILE IN THE ON POSITION. CAN HEAR CLICKING NOISE ABOVE PILOTS SIDE SEAT IN THE OVERHEAD. LIGHTS WORK NORMALLY IN OTHER POSITIONS. GSDR DXTA2026042407745Battery Pack · inoperativeBATTERY PACK NR 1 SEEMS INOPERATIVE. EMERGENCY LIGHTS WON'T TEST IN THE ARM POSITION AT ALL. EMERGENCY LIGHTS ASSOCIATED WITH PACK #1 WILL NOT TEST IN THE ON POSITION. THE EMERGENCY LIGHTS ASSOCIATED WITH THE OTHER BATTERY PACKS ILLUMINATE IN THE ON POSITIOSDR 2026FA0000289Stringer · debondedDISBONDS ON THE UPPER WINGS BETWEEN THE OUTBOARD END OF STRINGERS AND THE COMMON SKIN DOUBLERS. THE SKIN AND COMMON DOUBLERS MAY ALSO EXHIBIT A GRADUAL DEVIATION FROM CONTOUR IN THESE REGIONS. THE EXTENT OF THE DEFECT IS LOCATED USING ULTRASONIC INSPECTION ANDSDR DXTA2026042107700Switch · faultedAFTER CLOSING MAIN CABIN DOOR, DOOR WOULD NOT LATCH. TRIED CLOSING AGAIN WITH NO CHANGE. RAN CABIN DOOR OPEN ON GROUND QRH AND DOOR LATCHED BUT UNLATCHED IMMEDIATELY. COMPLETED A POWER CYCLE WITH NO CHANGE. DOOR WILL LATCH WHEN MOVING PUSH BUTTON SLIGHTLY TO TSDR DXTA2026041707665Power Supply · defectiveDURING PRE-FLIGHT, EMER LIGHTS SET TO ARM & NOTHING HAPPENS. CHARGING BATTERY RESOLVED MOMENTARILY BUT THIS HAS HAPPENED 2 DAYS IN A ROW. BATTERY NOT HOLDING CHARGE. CORRECTIVE ACTON: REMOVED AND REPLACED ALL 4 EMERGENCY LIGHT BATTERY PACKS IN REFERENCE TO CE-SDR DXTA2026041607654Rub Block · bindingAFTER UNLATCHING THE MAIN CABIN DOOR HANDLE, THE DOOR DID NOT OPEN AND NEEDED TO BE FORCED TO START DOWN. AFTER ENGINE SHUTDOWN AND WITH APU RUNNING. TECH CONFIRMED SQUAWK; WHILE OPENING THE MAIN DOOR, IT REQUIRES LITTLE HELP WITH HAND TO OPEN AND NOTED NOISSDR DXTA2026041407623Door Seal · defectiveWHILE ON DESCENT AT APPROXIMATELY 5000', 250 KIAS, AND A CABIN DIF OF 2.4, AN AUDIBLE HUM/WHISTLING COULD BE HEARD FROM THE CABIN DOOR. IT SEEMS TO HAVE GOTTEN PROGRESSIVELY LOUDER WITH THE LAST FEW FLIGHTS. CORRECTIVE ACTION: ACCESSED AIRCRAFT AND REMOVED ANDSDR DXTA2026041407617Handle · stiffMED HANDLE IS STIFF TO CLOSE TO THE POINT IT AT TIMES WOULD LOCK. WHEN IT DOES LOCK, HAVE TO RESET THE SYSTEM IN ORDER FOR THE DOOR CAS MESSAGE TO CLEAR. C/W REPOSITIONED THE AIRCRAFT TO THE HANGAR DUE TO WEATHER. WE PERFORMED THE MAIN CABIN DOOR HEALTH CHESDR 2026F00070Angle · crackedREPAIRED CRACKED CLIP INSIDE EQUIPMENT BAY ON RH SIDE OF CANTED BULKHEAD PER AQRD ERO-988018, REV. IR, TITLED "N317QS- TAILCONE CANTED BULKHEAD RH CLIP CRACKS", DATED APR 06, 2026. F&DT EVALUATION DUE DATE: MAR 31, 2027. NOTE 1: THE FATIGUE AND DAMAGE TOLERANCSDR 2026F00069Spar · corrodedFOUND 2 AREAS OF CORROSION ON VERTICAL STAB AFT SPAR LH CLIP. MECHANICALLY REMOVED CORROSION VERTICAL STAB LEFT AFT SPAR IN 2 AREAS. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW CESSNA 680 SRM 51-70-02. REPAIRED LEVEL 2 CORROSION ON VERTICAL STAB AFT SPAR LHSDR DXTA2026041307577Uplock Switch · defectiveDURING CLIMB THRU ABOUT FL320 WE RECEIVED BOTH LEFT AND RIGHT MAIN GEAR YELLOW DN AND NOSE GEAR WAS YELLOW HASH MARKS VIBRATIONS FROM GEAR. AFTER WE SLOWED AND DESCENDED BELOW 15000 WE RAN THE QRH LANDING GEAR DID NOT RETRACT CHECKLIST WE RECEIVED 3 GREESDR DXTA2026041007573Controller · defectiveWHILE AT CRUISE 43K FT, FLAP FAIL CAS MSG ILLUMINATED 3 TIMES, AND WOULD NOT RESET PER THE QRH. REPLACED FLAP CONTROLLER. OPS CHECK GOOD. IAW AMM 27-50-25
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