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 = '441' 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 = '441' 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 AU961195Bolt · sheared(AUS) PASSENGER MAIN ENTRANCE DOOR DRIVE CAPSTAN CABLE CLAMP BOLT SHEARED ALLOWING THE DOOR TO INDICATE `LOCKED' WHEN THE LOWERLOCK PINS WERE ONLY PARTIALLY LOCKEDSDR AU961188Collar · cracked(AUS) RH ELEVATOR TORQUE TUBE COLLAR CRACKEDSDR AU961036Valve · worn(AUS) PROPELLER FEATHERING VALVE WORN IN ROLL PIN AREA OF THE REAR CLEVISSDR AU960987Switch · faulty(AUS) PROPELLER BETA PRESSURE SWITCH FAULTYSDR CA960717001Wheel Half · cracked(CAN) OUTBOARD WHEEL HALF CRACKED FROM BASE OF BOLT HOLE COUNTER BORE TO INSIDE OF WHEEL HALF ABOVE O-RING AIR SEAL. CRACK ALLOWED TUBELESS TIRE TO SLOWLY DEFLATE.SDR AU961063Diffuser · bird strike(AUS) LH ENGINE SUFFERED BIRDSTRIKE - COMPRESSOR DIFFUSER VANE LEADING EDGES ROLLED BACK - BIRD REMAINS FOUND IN DIFFUSER, FUEL NOZZLES AND TURBINE EXHAUST PATHSDR AU960986Switch · faulty(AUS) PROPELLER BETA PRESSURE SWITCH FAULTYSDR 96ZZZX4247Valve · sticksWINDSHIELD HEAT VALVE SOLENOID STICKS ON. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR AU961062Valve · faulty(AUS) RH ENGINE ANTI-ICE VALVE AND PLENUM DRAIN VALVE FAULTYSDR AU961011Web · debonded(AUS) LH WING REAR SPAR WEB DISBONDED IN AREA BEHIND ENGINE FIRE BOTTLE- FOUND DURING ULTRASONIC INSPECTION IAW AD/CESSNA400/103 AMDT2SDR 96ZZZX3368Valve · failedPILOT REPORTED AIRCRAFT WOULD PRESSURIZE ON TAKEOFF UNTIL MAXIMUM DIFFERENTIAL WAS REACHED AND SAFETY VALVE WOULD ACTUATE. PILOT HAD NO CONTROL OVER RATE. GAINED ACCESS TO OUTFLOW VALVE AND FOUND SCREWS HOLDING THE DIFFERENTIAL SECTION OF CONTROLLER PULLED OSDR EY2R9600773Hub · corrodedHUB FOUND CORRODED.SDR EY2R9600772Hub · corrodedHUB FOUND CORRODED.SDR AU960575Bulkhead · cracked(AUS) FUSELAGE BULKHEAD LOCATED AT FS 155.76 CRACKED AT LOWER RH CORNER- CRACK EXTENDED FOR THE FULL WIDTH OF THE ANGLESDR AU960985Switch · faulty(AUS) PROPELLER BETA PRESSURE SWITCH FAULTYSDR AU960522Governor · faulty(AUS) LH ENGINE PROPELLER GOVERNOR (CSU) FAULTYSDR 96ZZZX2885Fitting · chafe wingINBOARD FORWARD SIDE OF RIGHT INBOARD FLAP IS CHAFING INTO SKIN ON WING STUB. FITTING WHICH IS RIVETED TO THE FORWARD INBOARD SIDE OF THE RIGHT INBOARD FLAP IS CHAFING AGAINST THE WING SKIN.SDR 96ZZZX2884Fitting · chafe wingINBOARD FORWARD SIDE OF RIGHT INBOARD FLAP IS CHAFING INTO SKIN ON WING STUB. FITTING WHICH IS RIVETED TO THE FORWARD INBOARD SIDE OF THE RIGHT INBOARD FLAP IS CHAFING AGAINST THE WING SKIN.SDR 96ZZZX2883Fitting · chafe wingINBOARD FORWARD SIDE OF RIGHT INBOARD FLAP IS CHAFING INTO THE SKIN AT THE WING STUB. FITTING WHICH IS RIVETED TO THE FORWARD INBOARD SIDE OF THE RIGHT INBOARD FLAP IS CHAFING AGAINST THE WING SKIN.SDR 96ZZZX2882Fitting · chafe wingINBOARD FORWARD SIDE OF RIGHT INBOARD FLAP IS CHAFING INTO THE SKIN AT THE WING STUB. FITTING WHICH IS RIVETED TO THE FORWARD INBOARD SIDE OF THE RIGHT INBOARD FLAP IS CHAFING AGAINST THE WING SKIN.SDR 96ZZZX2472Fitting · chafed skinINBOARD FORWARD SIDE OF RIGHT INBOARD FLAP IS CHAFING INTO THE SKIN AT THE WING STUB. FITTING PN 5825017-1 OR PN 5825017-2, WHICH IS RIVETED TO THE FORWARD INBOARD SIDE OF THE RIGHT INBOARD FLAP, IS CHAFING AGAINST THE WING SKIN.SDR AU960489Switch · faulty(AUS) PRESSURISATION SYSTEM AIRCYCLE MACHINE OVERTEMPERATURE SWITCH FAULTY GIVING FALSE ACM OVERTEMPERATURE INDICATION, CAUSINGCONSEQUENT CABIN PRESSURE FAILURE AND EMERGENCY PRESSURISATION ACTUATIONSDR AU960485Pipe · cracked(AUS) HYDRAULIC PRESSURE PIPE BETWEEN PUMP AND HYDRAULIC POWER PACK CRACKED AT BENDSDR 96ZZZX2186Ball Joint · failedAFTER LANDING WHEN REVERSE WAS SELECTED, THE LEFT ENGINE DID NOT REVERSE. INVESTIGATION REVEALED BALL SOCKET HAD WORN TO THE POINT THE BALL FELL OUT OF SOCKET AS PROPELLER CONTROL WAS MOVING AFT. THIS IS A SWAGED JOINT WITH NO SAFETY CLIPS TO PREVENT TOTAL SSDR 96ZZZX2652Solenoid · stuckWIPER/DEICE SOLENOID FAILED STUCK OPEN.SDR 96ZZZX2651Solenoid · stuckWIPER/DEICE SOLENOID FAILED STUCK OPEN.SDR 96ZZZX2650Solenoid · stuckWIPER/DEICE SOLENOID UNIT FAILED STUCK OPEN.SDR 96ZZZX2649Solenoid · stuckWIPER/DEICE SOLENOID STUCK. CYCLED UNIT 2 TIMES, UNIT STUCK IN OPEN POSITION. SOLENOID FAILED AFTER 2 TIMES. UNIT WOULD RESET AFTER PRESSURE WAS OFF. SUBMITTER STATED NEWLY OVERHAULED UNIT.SDR 96ZZZX3567Bracket Assy · brokenNOSE GEAR WOULD NOT EXTEND, CYCLED SEVERAL TIMES. USED EMERGENCY BLOW-DOWN BOTTLE, NOSE GEAR STILL WOULD NOT EXTEND. AIRCRAFT LANDED WITH NOSE GEAR UP. RIGHT NOSE GEAR DOOR RETREAT BRACKET BROKEN. NOSE GEAR PULLED RT DOOR UP INTO NOSE GEAR WELL AND JAMMED SDR 96ZZZX1959Diode · burnedPILOT REPORTED DESCENDING THROUGH 12,000 FEET, SMOKE OBSERVED COMING FROM UNDER COPILOT'S INSTRUMENT PANEL. DECLARED AN EMERGENCY, LANDED WITHOUT INCIDENT. FOUND DIODE ACROSS THE 'NO SMOKE' AND 'FASTEN SEAT BELT'. SWITCH WAS OVERHEATED AND THE CABIN INFO CISDR 96ZZZX2227Clip · rustedDURING THE REMOVAL OF THE INTERIOR AND HEADLINER IN PREPARATION FOR INSPECTION, NOTED THE SPRING STEEL CLIPS THAT RETAIN THE INNER WINDOWS WERE EXTENSIVELY RUSTED, SEVERAL TO A POINT OF TOTAL DESTRUCTION. IN ADDITION, THE MAIN CABIN STRUCTURE (TO WHICH THE CLSDR 96ZZZX2226Clip · rustedDURING THE REMOVAL OF THE INTERIOR AND HEADLINER IN PREPARATION FOR INSPECTION, NOTED THE SPRING STEEL CLIPS THAT RETAIN THE INNER WINDOWS WERE EXTENSIVELY RUSTED, SEVERAL TO A POINT OF TOTAL DESTRUCTION. IN ADDITION, THE MAIN CABIN STRUCTURE (TO WHICH THE CLSDR 96ZZZX1340Angle · crackedDURING PHASE INSPECTION, FOUND CRACK IN OUTBOARD END OF RT MAIN GEAR UPLOCK HOOK SUPPORT ANGLE THAT ATTACHES TO FORWARD WING SPAR WEB. CRACK ORIGINATES AT OUTBOARD HILOK HOLE AND EXTENDS FOR A TOTAL LENGTH OF 1.5 INCHES.SDR AU960206Blade · damaged(AUS) LH ENGINE 1ST STAGE IMPELLER DAMAGED - SECONDARY DAMAGE CAUSED TO 2ND STAGE IMPELLERSDR 96ZZZX1133Rib · crackedWHILE DOING A PHASE INSPECTION, FOUND A CRACK IN WING CANTED RIBS. CRACKS EXTEND FROM THE AFT SIDE OF THE FORWARD SPAR, REARWARD ALONG THE BEND RADIUS, 1.0 INCHES. CESSNA'S REPAIR IS TO STOP-DRILL THE ENDS OF THE CRACKS AND REINSPECT AT 200-HOUR INTERVALS.SDR 96ZZZX1132Rib · crackedWHILE DOING A PHASE INSPECTION, FOUND A CRACK IN WING CANTED RIBS. CRACKS EXTEND FROM THE AFT SIDE OF THE FORWARD SPAR, REARWARD ALONG THE BEND RADIUS, 1.0 INCHES. CESSNA'S REPAIR IS TO STOP-DRILL THE ENDS OF THE CRACKS AND REINSPECT AT 200-HOUR INTERVALS.SDR 96ZZZX1134Rib · crackedWHILE DOING A PHASE INSPECTION, FOUND A CRACK IN THE LT WING CANTED RIB, PN 5722206-1. CRACK EXTENDS FROM THE AFT SIDE OF THE FORWARD SPAR, REARWARD ALONG THE BEND RADIUS, 1.0 INCH. CESSNAS' REPAIR IS TO STOP-DRILL THE ENDS OF THE CRACK AND REINSPECT EACH 20SDR 96ZZZX1131Rib · crackedWHILE DOING A PHASE INSPECTION, FOUND A CRACK IN WING CANTED RIBS. CRACK EXTENDS FROM THE AFT SIDE OF THE FORWARD SPAR, REARWARD ALONG THE BEND RADIUS, 1.0 INCHES. CESSNA'S REPAIR IS TO STOP-DRILL END OF CRACK AND REINSPECT EACH 200 HOURS ACCORDING TO THE SUSDR 96ZZZX1130Rib · crackedWHILE DOING A PHASE INSPECTION, FOUND A CRACK IN WING CANTED RIBS. CRACK EXTENDS FROM THE AFT SIDE OF THE FORWARD SPAR, REARWARD ALONG THE BEND RADIUS, 1.0 INCHES. CESSNA'S REPAIR IS TO STOP-DRILL END OF CRACK AND REINSPECT EACH 200 HOURS.SDR AU960084Aircycle Machine · seized(AUS) AIR CYCLE MACHINE SEIZEDSDR 96ZZZX1588Transducer · defectiveTRANSDUCER UNIT WILL NOT MAINTAIN ADJUSTMENT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR CA960129013Check Valve · leaking(CAN)HYDRAULIC CHECK VALVE UNDER #2 PASSENGER SEAT LEAKED AND CONTAMINATED BOTH THE INSTRUMENT AIR PRESSURE LINES AND THE WATER SEPARATOR. UPON DISASSEMBLY OF THE VALVE, THE 'O' RINGS WERE FOUND DEFECTIVE.SDR AU960599Valve · faulty(AUS) ENGINE FUEL SHUTOFF VALVE FAULTY - PERSONNEL/MAINTENANCE ERRORSDR 96ZZZX1589Transducer · defectiveTRANSDUCER CAUSES GAUGE TO DROP TO ZERO. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR CA960304003Flash Tube · shorted(CAN) STROBE LIGHT FLASH TUBE INSTALLED, OVERHAULED AND FAILED WITHIN 7 HOURS OF USE. A SECOND FLASH TUBE ALSO FAILED WITHIN 39 HOURS OF USE.SDR AU960005Windshield · cracked(AUS) RH WINDSHIELD CRACKED IN LOWER INBOARD CORNER - FOUND DURING X-RAY INSPECTION - INSPECTION FOUND THAT THE OUTER LAMINATE HADBROKEN OFF ACROSS THE CORNERSDR 96ZZZX274Logic Box · malfunctionUPON APPROACH, PILOT SELECTED GEAR DOWN. GEAR CAME DOWN, THREE GREEN LIGHTS CAME ON, RED GEAR UNSAFE LIGHT ILLUMINATED AND MANY ANNUNCIATOR WARNING LIGHTS CAME ON. PILOT ELECTED TO BLOW GEAR DOWN, AND AN UNEVENTFUL LANDING WAS MADE. TROUBLESHOT MALFUNCTION SDR CA960103008Web · cracked(CAN)WEB P/N 5713050-5 AND DOUBLER P/N 5713050-11 CRACKED. CRACK EXTENDS 3/4" ABOVE L/H DRAG BRACE BRACKET TO APPROXIMATELY 3/4" BELOW BRACKET RUNNING VERTICAL ON THE AFT SIDE OF BRACKET. SERVICE NEWS LETT ER 85-44 ADDRESSES THIS PROBLEM.SDR 96ZZZX811Bellcrank · twistedCREW REPORTED LACK OF STEERING AUTHORITY TO THE LEFT. INSPECTION SHOWED STEERING BELLCRANK BENT AND TWISTED. STEERING LIMIT 'TATTLE TALE' FITTING WAS INTACT. PILOT REPORTED IT GOT WORSE OVER A PERIOD OF TIME. FINALLY, COULD NOT HOLD A HEADING ON THE TAXIWASDR 96ZZZX154Governor · malfunctionSURGING OF LEFT ENGINE DURING FLIGHT. PROP GOVERNOR, POSSIBLE FAILURE. REPLACED PROP GOVERNOR AND TESTED OVERSPEED SYSTEM, FOUND OVERSPEED FUNCTIONS PROPERLY AND LIMITS WERE NOT EXCEEDED DURING FLIGHT.
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