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 = '337G' 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 = '337G' 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 2020FA0000346Feeder Cable · shortedIMMEDIATELY AFTER LEVEL-OFF PILOT SMELLED ELECTRICAL FUMES OR VAPORS, FOLLOWED BY ELECTRICAL FAILURE, AND BEGAN RETURN TO AIRPORT. LANDING GEAR PUMPED DOWN MANUALLY AND VISUALLY VERIFIED IN POSITION FROM GROUND BEFORE LANDING, AND AIRCRAFT LANDED SUCCESSFULLY.SDR CA150810002Clamp · malfunctioned(CAN) ON LANDING PILOT REPORTED GEAR DOORS OPEN BUT GEAR DID NOT FULLY EXTEND. THERE WAS NO GREEN GEAR DOWN LIGHT AND GEAR WAS NOT VISIBLE. ELECTRIC GEAR POWER PAK MOTOR WAS RUNNING CONTINOUSLY. THE PILOT DID A LOW OVERHEAD AND IT WAS NOTED THAT THE GEAR WAS HSDR CA150609006Pressure Switch · faulty(CAN) DURING TAKEOFF, THE PILOT SELECTED GEAR UP BUT THE RT MAIN GEAR WOULD NOT RETRACT. THE ELECTRIC HYDRAULIC PUMP SHUTOFF, BUT DID NOT POP THE CIRCUIT BREAKER. GEAR WAS LOWERED USING EMERGENCY HAND PUMP. MAINTENANCE INSPECTION REVEALED THAT THE PRESSURE SSDR 2014FA0000265Alternator · failedFRONT ENGINE CHARGING SYSTEM, INTERMITTENT, THEN CONSTANT ALTERNATOR INOPERATIVE LIGHT. CHECKED CHARGING SYSTEM IAW MM. FOUND THREE BOLTS THAT HOLD THE ALTERNATOR FRAME TOGETHER FOUND LOOSE DESPITE FACTORY SAFETY WIRE BEING SECURE AND UNTOUCHED. DISASSEMBLY SDR CA131002004Clamp · broken(CAN) DURING OPS CHECKS OF THE ENGINE AFTER ENGINE INSPECTION, IT WAS NOTED THAT THE FRONT ENGINE LT MAG HAD A DROP OF 250. THE MAGNETO WAS REMOVED AND DISASSEMBLED FOR INSPECTION. IT WAS THEN NOTICED THAT THE CLAMPS THAT BOTH OF THE CLAMPS THAT HOLD DOWN THSDR CA120420004Cam · cracked(CAN) ON ENGINE SHUTDOWN PILOT NOTICES OIL LEAKING. INSPECTION REVEALED MAGNETO HAD A HOLE NEAR MOUNTING FLANGE. THE MAGNETO WAS REMOVED AND FOUND THAT 1 OF THE FLYWEIGHTS HAD CRACKED BY MOUNTING PIN AND THE FLYWEIGHT HAD EXITED THE MAGNETO THROUGH THE CASE.SDR CA120507018Cable · frayed(CAN) INSPECTED FLAP CABLES AND FOUND FLAP CABLES 1460100-7 AND 1460100-8. FRAYED AT LOCATIONS SHOWN IN ALERT. CABLES R & R WITH NEW.SDR CA110728005Cable · brokenPILOT REPORTED DURING ENGINE RUN UP, THE PROPELLER WOULD NOT GO INTO FEATHER ON THE REAR ENGINE. UPON INSP, THE PROPELLER CABLE, PN S1391-17 WAS FOUND TO BE BROKEN WHERE IT CLAMPS TO THE ENGINE.SDR CA110720008Clevis Pin · brokenTHE PILOT REPORTED THAT HIS UNDERCARRIAGE WARNING LIGHT FOR THE LT MAIN GEAR DID NOT GIVE A SAFE INDICATION WHEN THE GEAR WAS SELECTED DOWN. (GREEN INDICATIOR LIGHT WAS NOT ILLUMINATED) THE ACFT WAS PLACED ON JACKS AND MX CREW DISCOVERED THAT CLEVIS PIN, PN MSDR CA110707004Line · crackedPILOT REPORTED REAR ENGINE RUNNING TO LEAN CONDITION. NO MIXTURE ADJUSTMENT AVAILABLE. FOUND A CRACK IN THE NR 6 CYLINDER FUEL SUPPLY LINE TO NR 6 CYLINDER. REPLACED LINE WITH NEW LINE PN 630662, LEAK TESTED AND TEST FLIGHT PERFORMED, SATISFACTORY.SDR CA100805001Crankcase · crackedDURING A ROUTINE INSP, DISCOVERED A 2.5" CRACK IN THE ENGINE CASE RUNNING FWD FROM NR 5 C4L BASE TO THE FRONT BEARING AREA. THE CRANK WAS ALLOWING ENGINE OIL SEEPAGE AT THE CRACK AREA. THE ENGINE WAS REMOVED FROM SERVICE AND SENT TO O/H.SDR 2010FA0000045Track · brokenPN 1513055-1 CAM TRACK ASSY BROKE UPON GEAR RETRACTION. NOSE GEAR THEN WOULD NOT RETRACT PROPERLY OR EXTEND AND LOCK PROPERLY. PUMP MOTOR C/B CONTINUED TO TRIP DURING THE FLIGHT. ACFT WAS LANDED WITHOUT INCIDENT. IT WAS NOTICED THAT THE NOSE GEAR WAS COCKESDR 2010FA0000005Stud · damagedDURING THE TORQUE SEQUENCE FOR THE ENG O/H FINAL ASSY, FASTENERS ON THE ENG CASE WERE BROUGHT TO HALF THEIR FINAL TORQUE VALUES WITHOUT ISSUE IAW THE CURRENT MM AND PERTINENT SB`S. THEN WHILE ATTEMPTING TO REACH FINAL TORQUE VALUES, NOTED THAT MANY OF THE STUSDR 2009FA0000782Control Cable · frayedFOUND BOTH OF THE RT WING FLAP EXTEND CABLES WITH BROKEN INTERNAL WIRES. CABLES HAD TO BE REMOVED AND TWISTED AGAINST THEIR NORMAL WIND TO FIND THE TROUBLE. BOTH WERE DAMAGED AT THE POINT WHERE THEY GO AROUND THE BELLCRANKS IN THE WING, ABOUT 2 INCHES FROM THSDR CA090712001Valve · failed(CAN) ON LANDING, THE PILOT NOTED THE ACFT PULLED TO THE LT. AFTER LANDING, IT WAS NOTED THAT THE LT TIRE HAD A FLAT SPOT THAT MIGHT HAVE BEEN DUE TO BRAKE BEING ON. INSP OF THE PARKING BRAKE REVEALED THAT WHEN THE PARK BRAKE WAS PUT ON AND THEN TURNED OFF SSDR CA080918003Alternator · damaged(CAN) THE ACFT, A CESSNA 337G WAS ON A RETURN FLIGHT TO MAIN BASE WHEN THE PILOT NOTICED A INDICATION OF A FAILED FRONT ENGINE ALTERNATOR. THE ACFT LANDED WITHOUT INCIDENT AND MX INVESTIGATED THE PROBLEM. DURING REMOVAL OF THE FRONT ALTERNATOR, IT WAS DISCOVSDR CA070823009Engine · failed(CAN) REAR ENGINE EXPERIENCED A LOSS OF OIL PRESSURE DURING FLIGHT. ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO BASE. ENGINE WAS REPLACED. UNABLE TO DETERMINE OIL PRESSURE PROBLEM WITH FAILED OIL PRESSURE ON ENGINE. ENGINE WAS SHIPPED TO ENGINE SHOP. (TC NRSDR CA060508001Fuel Line · brokenSHORTLY AFTER TAKEOFF, THE PILOT OF A CESSNA 337 NOTICED THAT FUEL PRESSURE ON THE REAR ENGINE BEGAN TO DROP OFF AND THE ENGINE BEGAN TO RUN ROUGH. TURNED ON THE ELECTRIC BOOST PUMP AND THE ENGINE CONTINUED TO RUN NORMALLY. ELECTED TO RETURN TO THE AIRPORT ANSDR CA051027005Ignition Lead · deteriorated(CAN) ON GROUND RUN, LT MAGNETO ON FRONT ENGINE HAD A 200 RPM DROP. DURING TROUBLESHOOTING FOUND NR 4 CYLINDER TOP LEAD SHORTING FROM INNER COIL THROUGH INSULATOR TO CAP. LEAD REPAIRED, AIRCRAFT RELEASED INTO SERVICE. AFTER A FEW HOURS OF FLIGHT, THE PROBLEM RSDR CA050404009Crankcase · cracked(CAN) THE INITIAL PROBLEM WAS AN OIL LEAK FOUND DURING INSPECTION, AFTER SEVERAL ENGINE GROUND RUN-UPS, CRACK OF 2 INCHES FOUND FWD OF CYLINDER NR 5 ON CRANKCASE UPPER SECTION, ENGINE REMOVED AND SEND TO REPAIR SHOP.SDR CA041019004Hub · corroded(CAN) PROP RECEIVED FOR O/H. UPON INSPECTION CORROSION PITS WERE FOUND IN THE PROP MOUNTING FLANGE. THIS DAMAGE WAS TOO DEEP TO BE REMOVED WITHIN MANUFACTURERS SPECIFICATIONS. PROP HAS EXCEEDED THE MANUFCTURERS RECCOMENDED CALENDAR TBO BY 31 MONTHS.SDR CA040720007Uplock Switch · crackedDISCOVERED SWITCH CRACKED ALONG MATING HALVES. SWITCH HALVES DO NOT APPEAR TO HAVE BEEN BONDED PROPERLY.SDR CA040130007Housing · cracked(CAN) ON INSPECTION OF ALTERNATOR HOUSING 2 RIBS WERE FOUND CRACKED COMPLETELY THROUGH. THERE HAVE BEEN TWO OTHER SIMILAR ALTERNATORS FOUND WITH CRACKED RIBS.SDR AUS20031296Hose · deteriorated(AUS) REAR ENGINE FUEL PRESSURE HOSE LOCATED BETWEEN FIREWALL AND FUEL MANIFOLD DETERIORATED AND LEAKING ONTO LT EXHAUST STACK.SDR CA031001010Control Cable · damaged(CAN) A SPECIAL INSPECTION WAS INITIATED TO COMPLY WITH REMOVAL AND INSPECTION OF FLAP CONTROL CABLES THAT ARE CONNECTED TO THE INBOARD FLAP BELLCRANK. CABLE PN 14601007 AND 14601008 WERE BOTH FOUND TO HAVE SEVERAL BROKEN STRANDS AND REQUIRED REPLACEMENT SERVISDR CA031001009Control Cable · damaged(CAN) A SPECIAL INSPECTION WAS INITIATED TO COMPLY WITH REMOVAL AND INSPECTION OF FLAP CONTROL CABLES THAT ARE CONNECTED TO THE INBOARD FLAP BELLCRANK. CABLE P/N 1460 100-7 AND 1460100-8 WERE BOTH FOUND TO HAVE SEVERAL BROKEN STRANDS AND REQUIRED REPLACEMENT. SDR AUS20030912Structure · corroded(AUS) LT TAILBOOM LOWER STRUCTURE CORRODED IN AREA OF ATTACHMENT TO WING STRUCTURE. CORROSION IS BOTH INTERNAL AND EXTERNAL. RT TAILBOOM CONTAINED INTERNAL CORROSION ONLY.SDR CA030602001Control Cable · damaged(CAN) AFTER RECEIVING SDR ALERT AL-2003-05 AN INSPECTION WAS CARRIED OUT ON OUR 337G. TWO CABLES ON BOTH SIDES WERE FOUND DAMAGED. THE DAMAGE WAS LOCATED EXACTLY IN THE SAME LOCATION AS MENTION IN THE ALERT IE AROUND THE SHARP BEND OF THE BELLCRANK. ALL CABLESSDR CA030227005Control Cable · frayed(CAN) DURING 100 HR INSPECTION THE INBOARD RIGHT HAND FLAP CABLE WAS INSPECTED FOR WEAR IN THE AREA OF THE INBOARD FLAP BELLCRANK. CABLE WAS FOUND FRAYED APPROX. 1 INCH FROM CABLE END ATTACH FITTING.CABLE R EPLACED.SDR CA020621007Retainer · failed(CAN) PILOT INBOUND FOR LANDING & SELECTED GEAR DOWN. REPORTED THAT GEAR DID NOT EXTEND & GEAR MOTOR CONTINUED RUNNING. BEGAN EMERGENCY EXTENSION OF GEAR WITH HAND PUMP BUT NO PRESSURE BUILDING ON HAND PUMP. SEVERAL PROCEEDURES WERE CARRIED OUT BY PILOT & GRSDR CA020611006Bevel Gear · failed(CAN) - VACUUM PUMP DRIVE NOT TURNING.- INSPECTION REVEALS NO TEETH ON DRIVE BEVEL GEAR.- METAL CONTAMINANTS CONTAINED INSIDE STARTER ADAPTER.- TCM SB 01-5 ADDRESSES PROBLEM.- TCM WARRANTS FULL REPLACEMENT.SDR LU42001F00002Bearing · failedRELEVANT INDICATION.SDR CA010627062Piston · broken(CAN) ON A GROUND RUN-UP PRIOR TO A SCHEDULED INSPECTION A PARTIAL POWER LOSS WAS DETECTED. A MOTO-STAT WAS CARRIED OUT AND #6 CYL. HAD VERY LOW COMPRESSION. A FILTER CHECK WAS CARRIED OUT AND SUBSTANIAL METAL PARTS, ALM, CHROME AND STEEL WERE FOUND THAT ARE CSDR 20010605CW017Alternator · failedOWNER OF THIS AIRCRAFT EXPERIENCED FWD ENGINE ALTERNATOR FAILURE (AS INDICATOR BY FAILURE LIGHT) DURING FLIGHT. TECHNICIAN AND OWNER REMOVED ALTERNATOR FROM ENGINE AND DISCOVERED THE DRIVE SHAFT SHEARED. THE GEAR RETAINING BOLT HAD RUBBED INTERNALLY AND BUSSDR CA010529023Nut · damaged(CAN) AFTER LANDING PILOT WAS TAXIING FOR SHUTDOWN WHEN HE HEARD A BANKING NOISE AND REAR ENGINE ROUGHNESS. INSPECTION REVEALED A DENT IN VALVE COVER. COVER REMOVED AND FOUND BOTH ROCKER SHAFT HOLD DOWN STUDS SHEARED. IT HAS BEEN NOTED BEFORE ON OTHER AIRCRAFTSDR 20010501CW022Bevel Gear · shearedA DETAILED INVESTIGATION OF THE STARTER DEIVE REVEALED THAT ALL TO THE GEAR TEETH WERE WORN EXCESSIVELY ON ONE OF THE BEVEL GEARS WHICH DRIVES THE VACUUM PUMP. THIS IS THE FIFTH FAILURE OF THIS GEAR THAT WE HAVE DETECTED.SDR 20010424CW006Gear · shearedDETAILED INVESTIGATION OF THE STARTER DRIVE REVEALED THAT ALL OF THE GEAR TEETH WERE WORN EXCESSIVELY ON ONE OF THE BEVEL GEARS WHICH DRIVES THE VACUUM PUMP.SDR 20010424CW010Bevel Gear · shearedPILOT REPORTED LOSS OF INSTRUMENT VACUUM FROM REAR ENGINE DURING BEFORE TAKEOFF GROUND RUN UP. INVESTIGATION REVEALED THAT THE VACUUM PUMP WAS STILL SERVICEABLE. FURTHER INVESTIGATION REVEALED THAT ALL OF THE GEAR TEETH WERE SHEARED OFF OF ONE OF THE BEVEL GSDR CWA1Gear · wornDURING RUN-UP, FOLLOWING ANNUAL INSPECTION, NO VACUUM INDICATION OBSERVED FROM REAR ENGINE. REMOVED PUMP FOR REPLACEMENT AND OBSERVED DRIVE ON ENGINE DID NOT TURN WITH PROPELLER. REMOVED ACCESSORY DRIVE COVER AND FOUND NO TEETH LEFT ON DRIVING BEVEL GEAR. DSDR AU001098Gear · failed(AUS) VACUUM PUMP DRIVE GEAR FAILED. (X)SDR CA000804012Accessory Unit · failed(CAN) - ON SCHEDULED MAINTENANCE, THE VACUUM PUMP ACCESSORY DRIVE GEAR WAS OBSERVED AS FAILING TO TURN WITH PROPELLER ROTATION. ENGINE OIL SCREEN COVERED IN METAL PARTICLES, SLIVERS AND FLAKES ALL MAGNETIC. ENGINE REMOVED, SENT TO TELEDYNE CONTINENTAL FACTSDR 20000417SH010Skin · corrodedDURING A 100-HOUR INSPECTION, A SECTION OF MATERIAL USED FOR DAMPING ''OIL CANNING'' WAS REMOVED FROM THE INTERIOR FUSELAGE SKIN BELOW THE AFT SIDE WINDOW. HEAVY CORROSION WAS FOUND ACROSS THE ENTIRE AREA COVERED BY THE MATERIAL. THIS MATERIAL IS USED EXTENSSDR AU990090Piston · damaged(AUS) NR 6 CYLINDER PISTON DAMAGED DUE TO DETONATION. METAL CONTAMINATION OF THE ENGINE. ENGINE FACTORY REMANUFACTURED 457.1 HOURS PREVIOUSLY. PART TC: 457.SDR CA981230030Rib · cracked(CAN) .75 INCH CRACK FOUND ON RIGHT RUDDER UPPER RIB WHERE THE MASS BALANCE WEIGHT ATTACHES. REPLACEMENT RIB FABRICATED PER SRM AND AC43.13 GUIDELINES.SDR CA981109010Crankcase · cracked(CAN) THE REAR ENGINE OF A 337G SKYMASTER WAS REPORTED AS RUNNING ROUGH. INSPECTION FOUND THE SPARK PLUGS FOULED, SO THE PLUGS WERE REPLACED. THE ENGINE RAN SMOOTH AND IT WAS RELEASED FOR RETURN TO SERVICE. ON THE SECOND FLIGHT WHEN POWER WAS REDUCED, THE ENSDR AU981084Cylinder · damaged(AUS) NR 2 CYLINDER ROCKER ARM SHEARED OFF AT ATTACHMENT POINT.SDR 98ZZZX2231Gear · failedVACUUM PUMP FAILED. NEW PUMP WOULD NOT WORK. FOUND GEAR TEETH (ALL) MISSING FROM DRIVE GEAR.SDR CA980602057Wing · bird strike(CAN) IN CRUISE, PILOT CAUGHT A FLASH OF MOTION AND HEARD A BIRD IMPACT WITH HIS LEFT WING. DAMAGE WAS VISIBLE FROM THE COCKPIT. WIRES WERE VISIBLE SO ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO BASE. DAMAGE WAS FOUND TO EXTEND FROM STN 204 TO 222. LEADINSDR CA980504019Bearing · corroded(CAN) PROPELLER RECEIVED FOR FIVE YEAR CORROSION INSPECTION. INSPECTION FOUND NR 1 BLADE BEARING RACE CORRODED. BEARING RACE REPLACED.SDR 98ZZZX1598Diode · failedPOWER DIODE FAILED CAUSING DAMAGE TO: REGULATOR, ALTERNATOR, AUTOPILOT. RECOMMEND REPLACING BOTH DIODES WITH HEAVIER DUTY (HIGHER CAPACITY) DIODES.
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