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 = '58' 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 = '58' 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 95ZZZX6913Stringer · corrodedREMOVED FLOORBOARDS IN AFT PASSENGER AREA AND FOUND TOPS OF STRINGER SEVERELY CORRODED. P/N 95-43038-119, DASH 120, DASH 36, DASH 35. P/N 002-440029-3, DASH 4. SUSPECT CAUSE, URINE SEEPAGE INTO AFT SECTOR. AIR AMBULANCE OPERATION.SDR 95ZZZX6305Pc Board · burnedPILOT REPORTED A RED GLOW AND BURNING SMELL BEHIND THROTTLE QUADRANT. FOUND CIRCUIT BOARD FOR FLAP POSITION INDICATOR BURNED. CIRCUIT BOARD IS MOUNTED TO AN ALUMINUM RAIL BEHIND THROTTLE QUADRANT. RESISTOR ON CIRCUIT BOARD WAS CHARRED. SUSPECT FAILURE OF RESDR 96ZZZX37Control Cable · separatedRIGHT ENGINE FAILED TO START. FOUND RT MIXTURE CABLE THREADED END AT ENGINE HAD SEPARATED FROM THE CABLE WHERE END IS SWAGED TO INNER CABLE.SDR 95ZZZX6304Pc Board · shortedFLAP POSITION INDICATION PC BOARD CAPACITOR SHORTED CAUSING GLOW IN PEDESTAL. REMOVED AND REPLACED PC BOARD AND INDICATOR. OPS CHECKS GOOD.SDR 95ZZZX6930Spar · crackedFOUND BOTTOM SKIN OF RT ELEVATOR CRACKED DURING PROGRESSIVE INSPECTION. UPON SKIN REMOVAL (FOR REPAIR), FOUND HINGE ATTACH BRACKET CRACKED AND END ATTACH TAB OF SPAR BROKEN OFF. SUGGEST WIDER RE-INFORCEMENT GUSSETS AT SPAR AND END CLOSURE RIB.SDR 95ZZZX6929Skin · crackedFOUND BOTTOM SKIN OF RT ELEVATOR CRACKED DURING PROGRESSIVE INSPECTION. UPON SKIN REMOVAL (FOR REPAIR), FOUND HINGE ATTACH BRACKET CRACKED AND END ATTACH TAB OF SPAR BROKEN OFF. SUGGEST WIDER RE-INFORCEMENT GUSSETS AT SPAR AND END CLOSURE RIB.SDR 96ZZZX59Counterweight · clamp brokeAIRCRAFT WAS ON TAKEOFF ROLL, NO INDICATION OF PROBLEM DURING RUN-UP OR INITIAL POWER APPLICATION DURING TAKEOFF. ABOUT 750 FEET DOWN THE RUNWAY, THE RT ENGINE'S RPM SURGED. THE PILOT THOUGHT MAYBE A CABLE BROKE. AS ACFT SLOWED DOWN, PILOT NOTICED THE RT SPSDR 95ZZZX5975Actuating Rod · brokenSHORTLY AFTER DEPARTURE, ACFT BEGAN A VIOLENT SHAKING AND FLUTTER. PILOT REDUCED SPEED AND RETURNED TO AIRPORT. PILOT STATED THE ACFT WAS ALMOST UNABLE TO BE CONTROLLED. AN UNEVENTFUL LANDING WAS MADE. INSP REVEALED THE LT ELEV TRIM TAB ACTUATING ROD HAD SDR 95ZZZX6020Bulkhead · crackedINSPECTION FOUND CRACKS IN WEB FACE, AREA HUCK BOLT FASTENER. SUBMITTER STATED SB 2269 AND AD 90-08-14 SERIAL NUMBERS SHOULD BE UPGRADED TO INCLUDE TH-1574. THIS AIRCRAFT'S TOTAL TIME IS 6,495 HOURS.SDR 95ZZZX5756Regulator · failedAIRCRAFT IN CLIMB TO CRUISE ALTITUDE, NOTICED SMOKE SMELL AND THEN SMOKE IN THE COCKPIT AND CABIN, CONTINUED TO GET WORSE AND THEN A TOTAL ELECTRICAL FAILURE OF ALL COMPONENTS. FOUND LEFT (NR 1) VOLTAGE REGULATOR INOP. SUSPECT THE OVERVOLTAGE RELAY INSIDE THSDR 95ZZZX4562Skin · crackedOUTBOARD LEADING EDGE BOTTOM SKIN CRACKED. CRACK LOCATED JUST OUTBOARD OF OUTBOARD ELEVATOR ATTACH POINT. SUBMITTER SUGGESTS THE WEIGHT OF ELEVATOR BALANCE WEIGHT MAY HAVE CREATED STRESS AND CRACKED THE SKIN.SDR 95ZZZX4573Bracket · brokenWHILE C/W AD 91-15-20, FOUND RIGHT ENGINE LOWER NR 1 CYLINDER BRACKET BROKEN IN TWO. NOTE: AD 95-03-14, PN 630695, APPLIES TO LEFT LOWER BRACKET. THIS WAS RIGHT LOWER BRACKET. SUBMITTER STATED AD 95-03-14 SHOULD APPLY TO BOTH ENGINE MOUNT BRACKETS.SDR 95ZZZX4305Control Cable · failedINSTALLED NEW MIXTURE CONTROL CABLE PURCHASED FROM BEECHCRAFT ON 7-14-95. PART FAILED INTERNALLY NEAR ROD END. AFTER 39.8 HOURS OF SERVICE, NO OBVIOUS DEFECTS WERE NOTED THAT COULD LEAD TO THE PREMATURE FAILURE.SDR 95ZZZX5796Connect Rod · failedRIGHT ENGINE, NR 6, CONNECTING ROD WENT THROUGH ENGINE CASE. REMOVED AND REPLACED ENGINE. CAUSE UNKNOWN AT THIS TIME.SDR 95ZZZX5795Lamp · failedNO GEAR DOWN AND LOCK INDICATION, FOUND BULB DEFECTIVE. REMOVED AND REPLACED BULB, CHECKS GOOD.SDR 95ZZZX4306Line · failedPILOT REPORTED OIL LOSS FROM RIGHT ENGINE COMPARTMENT. INSPECTION REVEALED THE METAL LINE CONNECTED TO THE PROPELLER GOVERNOR HAD SEPARATED JUST BELOW THE FLARE. A NEW LINE WAS INSTALLED. REASON FOR FAILURE IS UNKNOWN.SDR 95ZZZX3621Indicator · malfunctionBOTH FUEL GAUGES WENT TO ZERO. FOUND BOTH P.C. BOARDS INTERMITTENT. REMOVED AND REPLACED P.C. BOARDS, CALIBRATED, OPS CHECKS GOOD.SDR 95ZZZX3676Spar · unmarkedAIRCRAFT RECENTLY WAS PAINTED. FOUND AD 91-17-01 'PAINTING REAR SPAR' HAD BEEN PAINTED EVEN THOUGH PREVIOUSLY COMPLIED WITH. REPAINTED ACTUATORS AT REAR SPAR PER AD. ALSO, LOOKED AT AN A36 RECENTLY PAINTED (DIFFERENT PAINT SHOP) FOUND ALSO UNMARKED. SUGGESSDR 95ZZZX3281Control Assy · rod end failedDURING FLIGHT, LT THROTTLE ROD END BROKE OFF OF CABLE. FLIGHT CREW CARRIED OUT LT ENGINE SHUT-DOWN CHECK LIST AND LANDED WITHOUT INCIDENT. SUBMITTER SUGGESTS IN ORDER TO PREVENT RECURRENCE, A LIFE LIMIT SHOULD BE ESTABLISHED FOR THE CABLE ASSEMBLY.SDR 95ZZZX5214Throttle Cable · looseRIGHT THROTTLE CABLE SLEEVE AT ENGINE END OF CONTROL WAS FOUND LOOSE, SWAGED PORTION BROKEN WHERE IT ATTACHES AT THE THREADED END OF CABLE. THIS WAS FOUND AT 100-HOUR INSPECTION WHEN COMPLYING WITH TCM SB 95-2.SDR 95ZZZX5217Control Cable · brokenRIGHT MIXTURE CONTROL CABLE THREADED SWAGED END BROKE OFF AT ENGINE SHUT-DOWN. NEW CABLE WAS INSTALLED 5-15-95. AIRCRAFT HAS ONLY FLOWN 63.1 HOURS SINCE CABLE WAS REPLACED.SDR 95ZZZX3255Control Cable · brokenRIGHT THROTTLE CABLE BROKEN. REMOVED AND REPLACED THROTTLE CABLE.SDR 95ZZZX3526Oil Filter · defectiveRUBBER SEAL FOUND PROTRUDING FROM CENTER HOLE WHEN FILTER WAS REMOVED:SDR 95ZZZX3505Piston Pin · fracturedWHEN REMOVING NR 2 AND NR 5 CYLINDERS TO CORRECT LOW COMPRESSION (LEAKING PAST RINGS), BOTH PISTON PINS WERE FOUND BROKEN IN TWO.SDR 95ZZZX3504Piston Pin · fracturedWHEN REMOVING NR 2 AND NR 5 CYLINDERS TO CORRECT LOW COMPRESSION (LEAKING PAST RINGS), BOTH PISTON PINS WERE FOUND BROKEN IN TWO.SDR 95ZZZX3250Channel · crackedFOUND BOTTOM FORWARD CHANNEL CRACKED ON LEFT ELEVATOR INBOARD FORWARD RIB. SUBMITTER RECOMMENDS REINFORCING CHANNEL PLATES ON ELEVATOR RIBS.SDR 95ZZZX2893Control Cable · broken5,323,8 HOBBS TIME. PILOT REPORTED NR 2 ENGINE THROTTLE CABLE BROKEN AT FUEL INJECTION SERVO, CABLE WAS REPLACED WITH A NEW PART.SDR 95ZZZX3256Control Cable · failedLEFT MIXTURE CABLE FAILED, ENGINE QUIT ON TAKEOFF. RETURNED TO AIRPORT. REMOVED AND REPLACED CABLE.SDR BIER950012Mixture Cable · failedFOUND MIXTURE CABLE BROKEN AT MIXTURE END ROD END ATTACH. REMOVED AND REPLACED CABLE. SUBMITTER STATES PROBLEM SEEMS TO BE FROM INSUFFICIENT LUBRICATION OF CABLE, CABLE MOVEMENT WAS EXTREMELY STIFF WHEN REMOVED.SDR 95ZZZX2655Control Arm · brokenFUEL MIXTURE CONTROL LEVER BROKEN OFF. LOOKS AS IF THE PART WHEN CASTED HAD A DEFECT.SDR 95ZZZX2176Cylinder · stud shearedPILOT REPORTED OIL LEAK. UPON INSPECTION, 3 UPPER CYLINDER BASE STUDS FOUND SHEARED. REMOVED CYLINDER AND NOTICED CASE CRACKED AT LOWER RIGHT STUD.SDR 95ZZZX3127Drag Link · brokenPOST-FLIGHT INSPECTION DETECTED BROKEN NOSE DRAG LINK. OLD STYLE DRAG LINK IS MADE FROM WELDED TUBE STEEL. IT APPEARS PART CORRODED FROM INSIDE. INSTALLED SERVICE KIT 35-4012-1S. NEW DRAG LINK IS A CAST PART NOW.SDR 95ZZZX1873Bracket · brokenFOUND BOTH EXHAUST TAIL PIPE SUPPORT BRACKETS BROKEN, RT ENGINE. APPEAR TO BE BROKEN AT CREASE MARK FROM DIE DURING MANUFACTURE. FOUND DURING C/W WITH TCM CSB 9415. INSPECTION OF CRANKCASE STUDS.SDR 95ZZZX1872Bracket · brokenFOUND BOTH EXHAUST TAIL PIPE SUPPORT BRACKETS BROKEN, RT ENGINE. APPEAR TO BE BROKEN AT CREASE MARK FROM DIE DURING MANUFACTURE. FOUND DURING C/W WITH TCM CSB 94-15. INSPECTION OF CRANKCASE STUDS.SDR 95ZZZX1871Bracket · brokenFOUND BOTH EXHAUST TAIL PIPE SUPPORT BRACKETS BROKEN, RT ENGINE. APPEAR TO BE BROKEN AT CREASE MARK FROM DIE DURING MANUFACTURE. FOUND DURING C/W WITH TCM CSB 94-15. INSPECTION OF CRANCKCASE STUDS.SDR 95ZZZX1870Bracket · brokenFOUND BOTH EXHAUST TAIL PIPE SUPPORT BRACKETS BROKEN, RT ENGINE. APPEAR TO BE BROKEN AT CREASE MARK FROM DIE DURING MANUFACTURE. FOUND DURING C/W WITH TCM CSB 94-15. INSPECTION OF CRANCKCASE STUDS.SDR 95ZZZX2057Rod End · failedUPON RETRACT OF LANDING GEAR, PILOT HEARD A BANG. ON LANDING ROLL-OUT, NOSE LANDING GEAR COLLAPSED. INVESTIGATION FOUND AFT RETRACT ROD END HAD BROKEN IN THE THREADED PORTION. THIS ROD END CONNECTS TO THE LANDING GEAR ACTUATOR (TRANSMISSION). PART TOTAL TISDR 95ZZZX2723Control Cable · brokenLEFT MIXTURE CONTROL CABLE WAS FOUND BROKEN AT THREADED END AT ENGINE SHUT DOWN. SUBMITTER STATED THIS IS A CONTINUING PROBLEM. BEECHCRAFT HAS BEEN NOTIFIED OF PROBLEM.SDR 95ZZZX1207Rod Assy · failedBRACE ROD ASSEMBLY ON RIGHT GEAR MALFUNCTIONED CAUSING GEAR COLLAPSE ON LANDING.SDR 95ZZZX1417Control Cable · looseSWAGED SLEEVE AT ENGINE END OF THROTTLE CABLE WAS FOUND LOOSE AND SLIDING ON CABLE FREELY. FOUND DURING ANNUAL INSPECTION. THIS PROBLEM CONTINUES TO EXIST ON MANY AIRCRAFT ON ALL ENGINE CONTROL CABLES.SDR 95ZZZX1411Control Cable · brokenCONTROL CABLE BROKEN ON THE ENGINE END AT THE POINT WHERE INNER CABLE ATTACHES TO THREADED STEEL END. SUBMITTER STATED THIS IS A CONTINUING PROBLEM ON SEVERAL AIRCRAFT. BEECHCRAFT HAS BEEN NOTIFIED AND HAVE NOT RESPONDED SINCE FIRST NOTIFIED LAST OCTOBER.SDR 95ZZZX1612Elt1104 · activatedELT FOUND ACTIVATED (SENDING SIGNAL). RESET UNIT, SIGNAL STOPPED 15 MINUTES.SDR 95ZZZX2671Coil · failedNO HIGH TENSION RESISTANCE. SECOND COIL REPLACED ON AIRCRAFT. THIS COIL DATE CODE 91688.SDR 95ZZZX1220Retract Rod · failedFROM EVIDENCE SEEN, HARD LANDING BENT RT RETRACT ROD. WHEN GEAR WAS RETRACTED, THIS CAUSED RT GEAR TO COME UP TOO FAR, AND JAMMED UPLOCK BLOCK INTO SKIN. WHEN GEAR WAS LOWERED, RT RETRACT ROD FAILED CAUSING RT GEAR NOT TO EXTEND. RESULT, PROP STRIKE RT ENGISDR 95ZZZX690Heater · liner crackedWHILE COMPLYING WITH AD 82-07-3, FOUND COMBUSTION LINER CRACKED. REPLACED LINER WITH NEW. HEATER OPERATION CHECKED GOOD. AD IS 13 YEARS OLD, PERHAPS RE-ISSUE, SO IT IS NOT FORGOTTEN.SDR 95ZZZX645Control Cable · brokenTHROTTLE AND MIXTURE CONTROL CABLES ARE BREAKING AT THE THREADED END WHERE THE CABLE ATTACHES TO THREADED PORTION OF CABLE. THIS HAS OCCURRED 11 TIMES ON THIS AIRCRAFT SINCE MAY, 1994. SUBMITTER STATED THAT BEECH AIRCRAFT HAS BEEN NOTIFIED OF PROBLEM, WITH NSDR 95ZZZX640Controller · inoperativeINSTRUMENT PANEL FLOOD LIGHTS WENT OUT DURING NIGHT FLIGHT. TROUBLESHOT SYSTEM AND FOUND LIGHT CONTROLLER INOPERATIVE. REASON UNKNOWN. REPLACED UNIT. OPS CHECK GOOD.SDR 95ZZZX639Switch · defectivePILOT REPORTED FLAPS WOULD NOT RETRACT UP PAST THE APPROACH SETTING. SYSTEM WAS TROUBLESHOT AND THE FLAP UP SETTING SWITCH WAS FOUND DEFECTIVE. REASON UNKNOWN. REPLACED SWITCH, OPS CHECK GOOD.SDR 95ZZZX1599Socket Assy · failedDURING APPROACH HAD NO GEAR DOWN INDICATION. FOUND DOWN AND LOCK LIGHT SOCKET FAILED. REMOVED AND REPLACED SOCKET ASSY. CHECKS GOOD.SDR 95ZZZX811Crankcase · cyl separatedAFTER TAKEOFF, PILOT NOTICED ROUGHNESS IN RIGHT ENGINE, HE REDUCED POWER, ENGINE RAN SMOOTH FOR A SHORT TIME THEN BECAME ROUGH AGAIN. AT THIS TIME, OIL WAS NOTED ON THE TOP OF RIGHT COWL. THE PILOT FEATHERED THE ENGINE AND LANDED. NR 2 CYLINDER WAS FOUND SE
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