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 = 'A100' 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 = 'A100' 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 CA971231015Control Cable · misinstalled(CAN) ON LANDING, THE RUDDER CABLES JAMMED. INVESTIGATION REVEALED THAT THE CABLES WERE ROUTED UNDER THE RUDDER SERVO ATTACH BRACKET. THE SWAGED ENDS CAUGHT THE EDGE OF THE BRACKET AND COULD NOT BE MOVED. CABLES REROUTED.SDR CA971216066Window · bubbled(CAN) PILOTS SIDE WINDOW FOUND BUBBLED ON THE EDGE OF THE WINDSHIELD.SDR CA971216063Pinion Gear · loose(CAN) INTRANSIT LIGHT ON IN-FLIGHT. LANDED OK. NOSE ACTUATOR HAD EXCESSIVE PLAY IN THE PINION GEAR AND WAS VERY NOISY. PART TC: 317.SDR CA971216059Duct · misaligned(CAN) BLEED AIR DUCTS FOUND MISALIGNED UNDER THE COPILOT'S FLOOR AFTER MAINTENANCE.SDR CA971216058Distribution Box · pin hole(CAN) AIRCRAFT RETURNED TO POINT OF ORIGIN WHEN A BLEED AIR WARNING INDICATION WAS RECEIVED. INSPECTION FOUND A PIN HOLE IN THE BELLY OF THE DISTRIBUTION BOX.SDR CA971216056Line · melted(CAN) BLEED AIR WARNING LINE HAD MELTED WHICH GAVE READING OF BLEED AIR FAIL LIGHT. NO FAILURE OF BLEED AIR SYSTEM JUST LACK OF INSULATION BY DISTRIBUTION BOX.SDR CA971216052Flow Divider · leaking fuel(CAN) AFTER TAKEOFF, PILOT NOTED FUMES IN THE COCKPIT AND SMOKE FROM INBOARD EXHAUST STACK ON NR 1 ENGINE. AFTER FLIGHT, MAINTENANCE SPOOLED THE ENGINE AND FOUND FUEL LEAKING FROM THE FLOW DIVIDER. IT IS THOUGHT WHEN THE ELBOW FITTINGS WERE TRANSFERRED TO THSDR CA971216053Skin · cracked(CAN) AIRCRAFT SKIN FOUND CRACKED ON THE BOTTOM OF FUSELAGE AFT OF THE MAIN SPAR ON EACH OUTBOARD SIDE. CRACKS OUTSIDE OF BELLY SPLICE PLATES. AIRCRAFT TT: 17,540 HOURS.SDR CA971118011Bolt · wrong part(CAN) DURING AN HSI ON THE NR 2 ENGINE, THERE WERE SEVEN P/N MS9574-04 BOLTS FOUND INSTALLED ON THE COMPRESSOR TURBINE SHROUD HOUSING. THESE BOLTS ARE THE WRONG MATERIAL FOR THIS INSTALLATION. THE PROPER BOLTS SHOULD BE P/N 3012061 OR P/N MS9714-04.SDR CA971020011Circuit Board · shorted(CAN) SMOKE NOTED AND SMELT COMING FROM BEHIND INSTRUMENT PANEL DURING DESCENT. BATTERY AND BOTH GENERATORS WERE SHUT OFF AND THE SMOKE STOPPED AVIONICS MASTER RESELECTED ON AND SMOKE OBSERVED AGAIN INVESTIGATION FOUND THE GPS RECEIVER CIRCUIT BOARD HAD OVESDR CA970904036Spar · cracked(CAN) REAR SPAR CRACKED UNDER MIDDLE AND UPPER HINGE AT ANCHOR NUT LOCATION.SDR CA970815008Hinge · corroded(CAN) CORROSION FOUND ON THE LOWER RUDDER HINGE BOLT HOLES. CORROSION ALSO FOUND ON THE BRACKET.SDR CA970728001Frame · cracked(CAN) FRAME AT STA 207 APPROXIMATELY EIGHT INCHES ABOVE FLOOR LEVEL ON LEFT SIDE CRACKED FROM LOWER TWO LIGHTING HOLES TO THE STRINGER CUT-OUT. REPAIRED.SDR CA970715025Fuel Cap · departed(CAN) AIRCRAFT HAD BEEN REFUELED AND PREPARED FOR DEPARTURE WHEN THE PILOT NOTICED THE LEFT HAND AUXILIARY FUEL CAP MISSING. AIRCRAFT RETURNED TO BASE AND IT WAS DETERMINED THAT THE CAP COULD BE LOCKED AND STILL RELEASE FROM THE TANK. NEW CAPS WERE INSTALLED OSDR CA970620010Bleed Air Tube · cracked(CAN) ON CLIMB THROUGH 5,000 FEET THE LEFT HAND "BLEED AIR DETECT" WARNING LIGHT ILLUMINATED ON THE GLARE SHIELD. LEFT HAND ENGINE SHUTDOWN AS PER PROCEDURES. AIRCRAFT LANDED SAFELY. MAINTENANCE FOUND A CRACKED BLEED AIR LEAK DETECT TUBE IN THE LEFT HAND WHEELSDR CA970609018Governor · faulty(CAN) WHILE IN CRUISE THE #2 PROPELLER BEGAN TO FLUCTUATE BETWEEN MAX AND MIN AND THEN STARTED TO GO TO FEATHER. THE ENGINE WAS SHUTDOWN AND THE PROPELLER FEATHERED. THE GOVERNOR WAS RECENTLY INSTALLED TO REPLACE A T/X'D UNIT. THIS AND THREE OTHER PROPELLER GOSDR CA970603011Shim · loose(CAN) ACTUATOR FAILED EARLY IN LIFE.SDR CA970603010Pinion Shim · loose(CAN) PINION SHAFT LOOSE AFTER SHORT TIME IN SERVICE.SDR CA970528030Bolt · loose(CAN) BORESCOPE INSPECTION FOUND A BOLT LODGED IN THE CT VANE. THE BOLT WAS IN THE GAS PATH AND WAS SLOWLY ERODING, IT WOULD HAVE HIT THE CT DISK AND THE ENGINE WOULD HAVE DESTRUCTED. THE CAUSE OF THIS FAILURE IS THE SERRATIONS ON THE LOCKWIRE PLIERS JAWS, WHISDR CA970520004Piston Rod · corrosion(CAN) PISTON ROD FOUND CORRODED AT CONTACT POINT OF FELT WIPER IN DOWN POSITION. REPLACED. PART TC: 879.SDR 97ZZZX2933Toruqe Tube · crackedFOUND DURING AIRCRAFT PRIMARY INSPECTION. SMALL CRACK FOUND IN RIGHT ELEVATOR TORQUE TUBE FITTING NEXT TO TAPER PIN. REPLACED TORQUE TUBE ASSEMBLY.SDR CA970513011Wire · broken(CAN) WHILE ON TRAINING, THE CREW SELECTED THE GEAR DOWN AND THE AIRCRAFT RESPONDED NORMALLY, EXCEPT RT GEAR DOWN LIGHT FAILED TO ILLUMINATE. FLY-BY CONFIRMED THAT GEAR DOWN. A/C LANDED. FOUND BROKEN WIRE, REPAIRED.SDR CA970624028Pressure Switch · shorted(CAN) WATER CONTAMINATION IN THE CANNON CONNECTOR IN THE LEFT HAND MAIN WHEEL WELL CAUSED A GROUND WHICH KEPT THE HYDRAULIC MOTOR RUNNING AND EVENTUAL OVERHEAT.SDR CA970423021Cockpit Window · shattered(CAN) AIRCRAFT WAS IN LEVEL CRUISE AT 14,000 FEET AND APPROXIMATELY 4.5 PSI. WITHOUT WARNING THE CAPTAIN'S SIDE "D" WINDOW DISINTEGRATED, CAUSING A RAPID DECOMPRESSION. EMERGENCY DESCENT WAS ACCOMPLISHED AND AIRCRAFT LANDED SAFELY. INVESTIGATION FOUND APPROXIMSDR CA970312007Cam · failed(CAN) ON PREFLIGHT, PILOT COULD NOT GET THE MAIN DOOR LOWER BAYONETS TO RETRACT ALLOWING HIM TO SHUT THE DOOR. THE WELD THAT HOLDS THE SHAFT TO THE DOOR FAILED ALLOWING THE SHAFT TO SPIN FREELY. REPLACED.SDR CA970312006Lintel · chafed(CAN) DOOR CHAFING ON THE UPPER DOOR LINTEL CAUSING LINTEL TO WEAR THIN. LINTEL REPLACED AND DOOR ADJUSTED.SDR CA970226062Switch · failed(CAN) ON DESCENT, NOSE GEAR DID NOT INDICATE GREEN. GEAR SWUNG THREE OR FOUR TIMES, NO GO. FLY-BY CONFIRMED GEAR DOWN. AIRCRAFT LANDED OK. NOSE DOWN LOCK SWITCH REPLACED AS NO PROBLEM COULD BE FOUND, AND SWITCH HAD BEEN A PROBLEM A FEW DAYS EARLIER.SDR CA970226061Windshield · cracked(CAN) WINDSHIELD CRACKED DURING CRUISE. PART TT: 17,086 HOURS.SDR CA970226059Switch · out of adjust(CAN) WHEN GEAR SELECTED DOWN, NOSE GEAR DID NOT SHOW GREEN. EMERGENCY PROCEDURES GOT GREEN. AIRCRAFT LANDED OK. FOUND NOSE GEAR SWITCH REQUIRED ADJUSTMENT.SDR CA970226058Regulator · not engaged(CAN) SHORTLY AFTER TAKEOFF THE #1 ENGINE LOST OIL PRESSURE AND HAD TO BE SHUTDOWN. INSPECTION OF THE OIL PRESSURE REGULATOR FOUND THE CLIP ON THE OIL PRESSURE HOUSING WAS NOT FULLY ENGAGED. THE REGULATOR WAS DISASSEMBLED AND INSPECTED, NO FAULT WAS FOUND. THESDR 97ZZZX752Support · brokenAFTER READING A REPORT IN THE JAN ISSUE ABOUT AIR STAIR STRUCTURE CRACKS, EXAMINED OUR (ACFT DOOR). FOUND THAT THE AIR STAIR DAMPNER UPPER ATTACH POINT WAS FLEXING DURING TRANSITION. FURTHER INVESTIGATION REVEALED THAT THE STRINGERS THAT THE ATTACH POINT IS SDR CA970128007Indicator · faulty(CAN) AIRCRAFT WAS IN CRUISE WHEN THE RIGHT HAND OIL PRESSURE INDICATOR WAS FLICKERING, ALL OTHER PARAMETERS WERE NORMAL. SEVERAL MINUTES LATER THE OIL PRESSURE WENT TO "0". THE #2 ENGINE WAS SHUTDOWN. POST FLIGHT INSPECTION FOUND THE OIL PRESSURE/TEMPERATURE SDR CA970121009Switch · intermittent(CAN) DURING APPROACH, PILOTS UNABLE TO GET GEAR DOWN INDICATION. RETURNED TO BASE AND FLYBY CONFIRMED GEAR DOWN. MAINTENANCE FOUND THE DOWNLOCK SWITCH TO BE INTERMITTENT.SDR CA961218008Engine · failed(CAN) DURING FLIGHT LOUD BANGS WERE HEARD FROM THE #1 ENGINE WITH FLAMES COMING FROM THE EXHAUST STACKS. AN ENGINE FIRE DRILL WAS CARRIED OUT AND THE ENGINE SHUTDOWN. THE AIRCRAFT RETURNED TO BASE WITHOUT INCIDENT. THE ENGINE WAS REMOVED FOR INVESTIGATION. REPSDR CA961205001Tube Assembly · cracked(CAN) THE PILOT NOTICED A SUBSTANTIAL INCREASE IN FUEL FLOW PRIOR TO LANDING. POST FLIGHT INSPECTION FOUND THE FUEL SYSTEM BYPASS LINE CRACKED AT THE SLEEVE, WHICH IS SILVER SOLDERED ONTO THE END OF THE STAINLESS STEEL LINE. THE SUBMITTER STATES THIS SAME FAULSDR CA961203007Skin · cracked(CAN) LEFT AILERON UPPER AND LOWER SKINS CRACKED ALONG SPAR AT TRAILING EDGE OF LEADING EDGE SKIN. RIGHT AILERON LOWER SKIN CRACKED SAME PLACE. ALSO, P/N 99-13000-197 AND -199.SDR CA961112028Latch Receiver · bent(CAN) AT 11,000 FEET, PILOT NOTICED A LARGE VIBRATION AND A PITCH DOWN ATTITUDE. CREW DETERMINED THAT THE RIGHT WING LOCKER WAS OPENED. EMERGENCY DECLARED AND AIRCRAFT LANDED OK. BOTH LATCH RECEIVER ASSEMBLIES WERE BENT NOT ALLOWING THE LATCH ASSEMBLY PIN TO ESDR CA961030002Spar · cracked(CAN) AT THE SPAR CUTOUT WHICH THE INBOARD FLAP TRACK PASSES AS THE FLAP IS RETRACTED, A .50 INCH CRACK WAS FOUND, EXTENDING FROM THE TOP INBOARD CORNER INTO THE BEND RADIUS BETWEEN THE WEB AND FLANGE. PART TC: 10,196. AIRCRAFT TT: 10,017 HOURS.SDR CA961029006Spar · cracked(CAN) SMALL CRACK, APPROXIMATELY 0.750 INCH IN LENGTH FOUND ON INBOARD FLAP SPAR. CRACK LOCATED AT INBOARD FLAP TRACK ATTACHMENT POINT IN THE MAIN SPAR. FURTHER INVESTIGATION FOUND A LARGER CRACK ABOUT 6 INCHES LONG FURTHER OUTBOARD IN THE UPPER SPAR RADIUS.SDR CA961025012Torque Knee · cracked(CAN) BOLT P/N 99-810061-3 FOUND LOOSE AT THE TORQUE KNEE UNION. WHEN DISASSEMBLED TO ADD WASHERS FOR SHIMMING, THE LOWER KNEE WAS FOUND CRACKED AT THE INSIDE RADIUS OF KNUCKLE. LPI CONFIRMED CRACK. BUSHING AT STRUT ATTACH POINT WAS WORN, POSSIBLY RESULTING INSDR CA960923017Controller · burnt(CAN) GEAR WOULD NOT EXTEND. EMERGENCY EXTENSION CARRIED OUT. FOUND THE GEAR MOTOR CONTROLLER BURNT. THE UNIT HAD JUST BEEN OVERHAULED.SDR CA960826028Tube · no flare(CAN) WHILE PERFORMING A STATIC SYSTEM LEAK CHECK IT WAS FOUND THAT THE TUBE DID NOT HAVE A FLARE ON THE END.SDR CA960712101Arm Assembly · bent(CAN) ON TAKEOFF THE #2 PROP RPM WAS OBSERVED TO BE DECREASING, TORQUE WAS INCREASING. THROTTLE WAS RETARDED AND PROPELLER WENT TO FEATHER. INVESTIGATION FOUND THE LOW PITCH ARM WAS BENT AND INTERFERING WITH THE PROXIMITY SWITCH AND CREATING A CONTINUOUS LOW PSDR CA960808104Support · cracked(CAN) ON INSPECTION PER SB 2145, THE LEFT AND RIGHT ELEVATOR TORQUE TUBES CENTRE SUPPORTS WERE BOTH FOUND CRACKED. A SISTER SHIP FOUND ONE SUPPORT CRACKED. CRACKS COME FROM INBOARD TAPER PIN HOLES. ALL THREE TORQUE TUBE ASSEMBLIES REPLACED WITH NEW P/N'S.SDR CA960729006Plate · bent(CAN) RIGHT HAND DOWN LOCK PLATE BENT ON LANDING GIVING UNSAFE GEAR.SDR CA960722005Engine · making metal(CAN) DURING FLIGHT THE #1 ENGINE OIL PRESSURE WAS LOWER AND THE OIL TEMPERATURE HIGHER THAN NORMAL, WITH THE TORQUE INDICATION FLUCTUATING. THE ENGINE OIL SCREEN WAS PULLED AND FOUND CONTAMINATED WITH BRASS/BRONZE AND STEEL FLECKS OF METAL. ENGINE WAS REMOVEDSDR CA960725104Motor · intermittent(CAN) LANDING GEAR MOTOR INTERMITTENT WHEN SELECTED DOWN. BRUSHES FOUND IMPROPERLY INSTALLED.SDR 96ZZZX5545Intercostal · crackedTHIS PART SUPPORTS THE AFT CABIN DOOR CABLE POST BRACKET (PN 50-430043-1259). OVERLOADING OF DOOR IS THE SUSPECT CAUSE. SUBMITTER SUGGESTS MANUFACTURING INTERCOSTAL FROM STRONGER MATERIAL.SDR CA960703004Skin · cracked(CAN) SKIN CRACKS FOUND FROM THREE (3) FASTNER LOCATIONS AT THE UPPER INBOARD BATHTUB FITTING. BEECH CONTACTED AND REPLIED WITH A 25 HOUR INSPECITON AS PER BEECH MESSAGE 52-5870.SDR 96ZZZX3396Bearing · failedBEARING (AFT) FAILED. PART NUMBER AS ORDERED FROM BEECH WOULD BE 9000-11. BEARING SUPPLIED BY BEECH IS IDENTIFIED AS (PEER CHINA 600ZD). SUBMITTER SUSPECTS QUALITY CONTROL MAY BE LACKING.
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