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 97ZZZX4486Air Filter · failedTHE IN-LINE AIR FILTER FOR THE INSTRUMENT AIR WAS FOUND SEVERELY CRACKED ALMOST TO THE POINT OF COMPLETE SEPARATION. AN AD 97-16-10 WAS ISSUED ON THESE TYPE FILTERS, BUT THESE FILTERS WERE NOT INCLUDED BECAUSE OF LOT NUMBER. BATCH NR 02797.SDR 97ZZZX4485Air Filter · crackedTHE IN-LINE AIR FILTER WAS FOUND CRACKED ALTHOUGH NOT SEVERE AT THIS TIME. PART MAY HAVE ONLY LASTED ANOTHER 25-50 HOURS. AD 97-16-10 WAS ISSUED AGAINST THESE TYPE FILTERS, BUT THE FILTER IS NOT IN THE LOT NUMBER SPECIFIED BY AD.SDR 97ZZZX4385Combustion Tube · crackedPRESSURE CHECKED HEATER FOR COMBUSTION TUBE LEAK CHECK. FAILED CHECK AND HEATER WAS DISASSEMBLED. LOCATED SEVERAL CRACKS AT HEATER WELDS. INSTALLED NEW COMBUSTION TUBE PN 45C40, SN 970902. RE-CHECK FOR LEAKS OK.SDR 97ZZZX4484Crankcase · crackedRIGHT ENGINE CRANKCASE CRACKED AT THE UPPER STUD AREA OF THE NR 6 CYLINDER ALLOWING THE CYLINDER TO COMPLETELY SEPARATE FROM THE CASE CAUSING ENGINE FAILURE UNDER NORMAL FLIGHT CONDITIONS. SUBMITTER RECOMMENDATION: DYE PENETRANT, INSPECTION CRANKCASE REF: ASDR 97ZZZX4450Rod End · bearing failedCLT - NOSE GEAR COLLAPSED ON LANDING. FOUND ROD END BROKEN ON NOSE GEAR RETRACT ROD. REPLACED ROD END, GEAR OPERATED NORMALLY.SDR 97ZZZX4150Shaft · failedPILOT REPORTED A GROUND OBSERVER INFORMED NLG DOORS REMAINED OPENED AFTER THE GEAR WAS UP. PILOT HEARD NOISES COMING FROM NOSE AREA DURING RECENT FLIGHTS. INSP REVEALED LOWER PORTION OF CAM PLATE SLOT ON THE SHAFT THAT CLOSES THE NOSE GEAR DOORS BROKE OFF ANSDR 97ZZZX3915Lining · misdrilledTHE ATTACHMENT HOLES OF BRAKE LININGS ARE IN DIFFERENT LOCATIONS FROM ONE BRAKE LINE TO ANOTHER. ON CERTAIN LININGS, IT WILL NOT SIT FLUSH ON THE BRAKE SHOE.SDR 97ZZZX3904Control Cable · defectiveDURING FLIGHT, PILOT COULD NOT GET PROPER MIXTURE CONTROL ON LEFT ENGINE. P.I.C. SHUT ENGINE OFF AND LANDED AIRCRAFT WITHOUT ANY FURTHER INCIDENT. MECHANIC DISCOVERED DEFECTIVE MIXTURE CONTROL CABLE. CABLE WAS REMOVED AND REPLACED. AIRCRAFT OPS CHECKED OK.SDR 97ZZZX3809Bulkhead · crackedDURING PHASE 2 INSPECTION OF TAIL AREA, CRACKING AND STOP-DRILLING NOTICED ON STA 257.6 BULKHEAD AT HORIZONTAL SPARE ATTACH POINTS. STOP-DRILLING IS NOT AN APPROVED REPAIR PER BEECH SI 990, REV 2 PART II. A P/N 55-4030-5S REINFORCEMENT KIT NEEDED TO BE INSTASDR CA970820017Lifter · worn(CAN) DURING INSPECTON FINE METAL METAL (STEEL) PARTICLES WERE FOUND IN THE OIL FILTER. FURTHER INSPECTION REVEALED THE NR1 AND NR5 CYLINDERS EXHAUST VALVE LIFTERS WERE FOUND WORN ON THE LIFTER FACES. THE ENGINE WILL BE RETURNED TO CONTINENTAL TO DETERMINE THESDR 97ZZZX3676Mount · crackedRIGHT ENGINE MOUNT CRACKED AT THE TOP OUTBOARD ISOLATOR ATTACH WELD JOINT. THIS ENGINE HAD THE MODIFIED BRACKETS INSTALLED PREVIOUSLY WHICH RELIEVES THE AD INSPECTION.SDR 97ZZZX3543Control Cable · failedRIGHT ENGINE FAILED APPROXIMATELY 5 MINUTES AFTER TAKEOFF. ENGINE SECURED IAW ENGINE OUT CHECK LIST AND RETURNED TO AIRPORT WITH NO FURTHER PROBLEMS. CABLE FAILED .50 INCH FROM ROD-END ON ENGINE SIDE OF CABLE. CABLE WAS INSTALLED CORRECTLY, CLEANED, AND LUBSDR 97ZZZX3399Tube · chafedDURING 100-HOUR INSPECTION, FOUND RUDDER INTERCONNECT TUBE CHAFED THROUGH BY A FLOOR ATTACHMENT SCREW - TOO LONG OR WRONG LOCATION. SUBMITTER STATED HAVE FOUND SIMILAR DAMAGE ON OTHER AIRCRAFT. THIS TUBE HAS A THICK SIDE WALL AND HAS A 1.50 INCH LONG ARCING SDR 97ZZZX4151Crankshaft · lockupLEFT ENGINE - SUDDEN STOPPAGE, IN-FLIGHT CRANKSHAFT LOCK-UP. ENGINE WAS RETURNED AS A CORE TO MANUFACTURER. NEW FACTORY RE-MANUFACTURED ENGINE PURCHASED.SDR 97ZZZX3152Control Cable · brokenLEFT THROTTLE CABLE BROKE GOING FROM ALB TO AUG. DIVERTED TO PWM. REMOVED AND REPLACED THROTTLE CABLE.SDR AU970891Selector · broken(AUS) LANDING GEAR SELECTOR SWITCH SHAFT BROKEN. INSPECTION FOUND LOCATING TANG ON EMERGENCY LANDING GEAR EXTENSION HANDLE ALSO BROKEN AND FORK END TO DRIVE SHAFT DAMAGED. EXTENSION HANDLE HOUSING ALSO CRACKED.SDR AU970484Uplock Cable · failed(AUS) LANDING GEAR UPLOCK CABLE FAILED AT OUTBOARD SWAGED FITTING DUE TO CORROSION OF THE EXPOSED STRANDSSDR 97ZZZX2351Hinge Cap · wornRT WING, SPAR, LOWER, FORWARD, INBOARD - FOUND SEVERAL WORKING RIVETS WITH HEAVY BLACK STREAKING AFT OF THE RIVET HEADS. FURTHER INSEPCTION REVEALED LEADING EDGE HINGE PIN SEVERELY WORN. REQUIRES REPLACEMENT OF SPAR ASSY AND LEADING EDGE HARDWARE ASSY. SUSPSDR 97ZZZX2350Spar · rivets workingRT WING, SPAR, LOWER, FORWARD, INBOARD - FOUND SEVERAL WORKING RIVETS WITH HEAVY BLACK STREAKING AFT OF THE RIVET HEADS. FURTHER INSPECTION REVEALED LEADING EDGE HINGE PIN SEVERELY WORN. REQUIRES REPLACEMENT OF SPAR ASSY AND LEADING EDGE HARDWARE ASSY. SUSPSDR AU970532Crankcase · cracked(AUS) ENGINE CRANKCASE LH HALF CRACKED IN AREA OF NO2 BEARING SADDLE -NO6 CONNECTING ROD CAP CONTAINED MULTIPLE CRACKING - SUSPECT CRACKING ORIGINATED FROM CORROSION PITTINGSDR AU970482Linkage · worn(AUS) LH ENGINE CONTROL LINKAGES FAULTY - THE FOLLOWING DEFECTS WERE FOUND:- 1. THROTTLE CONTROL LINKAGE SEVERELY WORN 2. THROTTLE ROD END SEPARATED FROM CAGE 3. NYLEX NUT USED ON THROTTLE CROSS SHAFT 4. NYLEX NUT ON MIXTURE CONTROL NOT IN SAFETY 5. MIXTURE COSDR 97ZZZX2021Bearing · failedPILOT REPORTED LEFT ENGINE LEFT MAGNETO WAS 'DEAD' ON RUN-UP. REMOVED MAGNETO AND OPENED UP FOR INSPECTION. FOUND INTERNAL DAMAGE - MATERIAL BEING WORN AWAY BY ROTATING MAGNET. FURTHER DISASSEMBLY REVEALED DRIVE END BEARING P/N M3006 BALL RETAINER CAGE AND SDR AU970883Spar · cracked(AUS) WING FORWARD SPAR FORWARD AND REAR RH WEBS CRACKED - FOUND DURING INSPECTION IAW AD/BEECH55/62 AMDT4 AND BEECH SB2269SDR AU970880Elt · corroded(AUS) ELT COMPLETELY DESTROYED DUE TO BUILDUP OF WATER IN MOUNTING TRAY - WATER IN TRAY GETS INTO ELT BATTERY COMPARTMENT CAUSING CORROSION AND EVENTUAL FAILURESDR 97ZZZX1885Alternator · failedAFTER AN IN-FLIGHT ALTERNATOR FAILURE, FOUND THAT THE SHAFT HAD NO SUPPORT AND WOBBLED FREELY, THAT THE ALT GEAR P/N 640932 WAS CHEWED UP AND SO WAS THE DRIVE GEAR FROM THE CRANKSHAFT P/N 632018. ALSO, ONE EACH LOCKPLATE P/N 641909 WAS MISSING AS WELL AS THE SDR AU970374Circuit Breaker · failed(AUS) LANDING GEAR RELAY CIRCUIT BREAKER FAILEDSDR AU970309Spring · faulty(AUS) PROPELLER CONTAINED THE FOLLOWING DEFECTS:- 1. LATCH PNO B318 BROKEN. 2. LATCH BOLTS PNO A1595 (2OFF) SHEARED AND ONE BOLT BENT 3. CYLINDER PNO B2423-1 DAMAGED 4. PISTON PNO B3237 WORN 5. INCORRECT PRESSURE DECAL FITTED. PERSONNEL/MAINTENANCE ERRORSDR 97ZZZX2098Lever · misinstalledDURING ROUTINE MAINTENANCE, FUEL INJECTION ASSY FOUND LOOSE. OF THE 3 BOLTS THAT ATTACH THIS TO THE THROTTLE CONTROL ASSY, 2 BOLTS MISSING, 1 LOOSE. ASSY ABOUT TO BREAK LOOSE. ALSO, SHROUD P/N 646673 BROKEN AND LOOSE, AND CHAFING ON FUEL LINE FITTINGS. FITSDR 97ZZZX1857Tube · scoredTHE RUDDER PEDAL BELLCRANK INTERCONNECT TUBE WAS SCORED ENTIRELY THROUGH THE TUBE WALL BY A 1 INCH LONG PK TYPE UPHOLSTERY SCREW USED TO SECURE THE PILOT'S KICKPLATE TO THE FLOOR BOARD. REPLACED TUBE. NEW SCREW INSTALLED NO LONGER THAN .75 INCH. SUBMITTER SSDR CA970408001Brush Cage · broken(CAN) DURING LANDING GEAR MOTOR INSPECTION, PLASTIC BRUSH CAGE FOUND BROKEN. POSSIBLY CAUSED ON INSTALLATION. REPLACED.SDR GLBA97049Truss · crackedFOUND LEFT ENGINE TRUSS CRACKED UNDER RT LOWER ENGINE MOUNT ATTACH POINT. THIS TUBE WAS CRACKED DUE TO RUBBING OF ISOLATOR MOUNT ON TUBE. IT APPEARED THAT CLEARANCE WAS MINIMAL WHEN TRUSS WAS MANUFACTURED. (X)SDR CA970401014Strut · cracked(CAN) CRACK FOUND IN OLEO TO STRUT CASTING. REPLACED.SDR 97ZZZX1248Crankcase · crackedDURING OIL CHANGE, FOUND 1 INCH CRACK EXTENDING FROM CYLINDER NR 6 UPPER REAR STUD. AD 77-13-22 PARA(A) ADDRESSES THIS SUBJECT, BUT IS NOT INCLUDED IN THE SERIAL NUMBER REQUIREMENT LIST.SDR AU970234Rib · cracked(AUS) RH FLAP RIB CRACKED IN AREA OF FLAP ACTUATOR ATTACHMENT - CRACK EMANATES FROM FORWARD ATTACHMENT BOLT HOLE IN A PREVIOUSLY REPAIRED AREA - SUSPECT CRACK DUE TO INCORRECT REPAIRSDR AU970233Trim Jack · incorrect wired(AUS) RUDDER TRIM JACK INCORRECTLY LOCKWIRED - THE TRIM JACK ROD END WAS LOCKED TO THE TRIM JACK HOUSING RETAINING NUT ALLOWING THE TRIM JACK TO ONLY ROTATE ONE TURN - THIS CONDITION HAD EXISTED FOR APPROXIMATELY 800 HOURS - PERSONNEL/MAINTENANCE ERRORSDR 97ZZZX1234Through Bolt · failedUPON INSPECTION OF LT ENGINE, FOUND NR 2 CYLINDER SEPARATED FROM CASE BY 2-3 INCHES. UPPER THROUGH-BOLT APPEARS TO BE BROKEN INTERNALLY AS WELL AS LOWER THROUGH-BOLT, ALL UPPER AND LOWER CASE STUDS TO CYLINDER HOLD-DOWN APPEAR TO BE BROKEN AT THREAD AREA OR ASDR 97ZZZX1199Motor · runs backwardFOUND HEATER RUNS RICH, AFTER A LONG TROUBLESHOOTING TIME DISCOVERED COMBUSTION AIR FAN MOTOR RAN BACKWARDS.SDR 97ZZZX1312Latch · required adjSHORTLY AFTER TAKEOFF, COPILOT'S DOOR POPPED OPEN. AIRCRAFT RETURNED TO AIRPORT AND LANDED SAFELY. READJUSTED UPPER LATCH. SUBMITTER SUGGESTION: EXTRA CARE BE TAKEN DURING 100-HOUR INSPECTION TO ENSURE PROPER LATCH RIGGING.SDR AU970077Spring · faulty(AUS) PROPELLER LATCH SPRING KIT FOUND TO BE MADE UP OF SUPERCEEDED PARTS - FITTED AT LAST OVERHAUL IN USA - PERSONNEL/MAINTENANCE ERRORSDR AU970106Circuit Breaker · miswired(AUS) TRANSPONDER SYSTEM WIRED TO PRIMARY AH CIRCUIT BREAKER FOLLOWING FAILURE OF CORRECT CB WHICH HAD BEEN DISCONNECTED - CIRCUIT BREAKER MARKED `RADAR' WAS REALLY THE COMPASS SYSTEM (COMPASS SYSTEM CB WAS FOUR CIRCUIT BREAKERS AWAY) - HF CIRCUIT BREAKER NOT SDR 97ZZZX1105Main Gear · failedLEFT LANDING GEAR FROZEN IN WHEELWELL, GEAR SELECTED DOWN, ROD BENT, AND GEAR STAYED IN WELL. REMOVED AND REPLACED BENT ROD AND MOTOR AND GEARBOX ASSY, LEFT PROPELLER AND LEFT ENGINE FOR PROPELLER STRIKE INSPECTION.SDR 97ZZZX683Wire · shortedTHE RIGHT ENGINE STARTER CABLE (WIRE) NR J12A4) WAS FOUND TO HAVE SHORTED TO THE ENGINE MOUNT. THIS CAUSED DAMAGE TO THE ENGINE MOUNT P/N 96-910010-85 WHICH IN TURN WAS REPLACED WITH A NEW MOUNT. A NEW STARTER WIRE WAS INSTALLED AND ROUTED TO PREVENT ANY FUTSDR 97ZZZX537Gear · corrodedINSP FOUND COOKED, CORRODED BRUSH IN DIST GEAR DUE TO ARCING. CARBON BRUSH IN LARGE GEAR ASSY RT MAGNETO, PN 10-349350-5, MAY HAVE BEEN BROKEN PRIOR TO OR DURING ASSY OF MAGNETO.SDR 97ZZZX633Shaft Assy · brokenPILOT REPORTED THAT NOSE GEAR DOORS FAILED TO CLOSE WHEN THE GEAR WAS RETRACTED. INFORMED THAT THE DOORS WERE OPEN BY CONTROL TOWER PERSONNEL; PILOT HAD NO COCKPIT INDICATION THAT THE GEAR WAS FUNCTIONING ABNORMALLY. THE PILOT MANUALLY EXTENDED THE GEAR AND SDR 97ZZZX629Cover Assy · leakingPILOT COMPLAINING OF OIL LEAK. FOUND OIL PUMP LEAKING FROM CASTING SCAR IN UNIT.SDR 97ZZZX362Drive Gear · bolts failedPILOT REPORTED LOW OIL PRESSURE, AND ALTERNATOR INOP. FOLLOWED MM FOR OIL PRESSURE RELIEF VALVE AND FOUND METAL. REMOVED ALTERNATOR AND FOUND GEAR, FACE, ALTERNATOR DRIVE BOLTS HAD SHEARED.SDR 97ZZZX360Circuit Breaker · failedTOTAL LOSS OF DC POWER 10 MINUTES INTO FLIGHT. REPAIRED INOPERATIVE BATTERIES. REPAIRED INOPERATIVE ALTERNATOR FIELD CIRCUIT BREAKER. REPLACED. (CAUSE - CORROSION).SDR CA961218003Pump · failure(CAN) OVERHAULED VACUUM PUMP INSTALLED AFTER VACUUM PUMP FAILURE. EIGHT HOURS LATER THE VACUUM PUMP SEIZED AND FAILED FOR NO APPARENT REASON. THIS IS THE SECOND "RAPCO" PUMP TO FAIL EARLY.SDR 96ZZZX6159Spar · crackedINSP SPAR CARRY-THROUGH WEB STRUCTURE. FOUND LT FWD AND AFT RT FWD CORNERS CRACKED. THIS AIRCRAFT IS 4 SERIAL NUMBERS NEWER THAN BEECH AD 90-18-14 APPLIES TO. SUBMITTER STATED AD 90-18-14 NEEDS REVISING TO INCLUDE NEW AIRCRAFT.SDR EY2R9601682Rod · strippedPROP ASSY ROD THREAD STRIPPED
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