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 = '414' 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 = '414' 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 20000626SH021Switch · failedTHE STANDBY/MAIN VOLTAGE REGULATOR SWITCH FAILED INTERNALLY CAUSING THE NOISE FILTERS, PN CM221, TO SHORT AND CATCH ON FIRE. (X)SDR 20000407SH033Crankcase · crackedCRANKCASE CRACKED FROM BASE OF NR 4 CYLINDER ACROSS THE TOP OF THE BACKBONE TO THE BASE OF NR 3 CYLINDER. CAUSE UNKNOWN AT THIS TIME. (X)SDR AU000128025Engine · making metal(AU) ENGINE MAKING METAL.SDR CA000118026Bolt · missing(CAN) DURING SERVICING OF THE AIRCRAFT TIRES, MAINTENANCE PERSONNEL NOTICED A WHEEL THRU BOLT MISSING FROM A MAIN WHEEL. 300 HOURS LATER A SECOND BOLT WAS FOUND MISSING AT WHICH TIME ALL WHEEL BOLTS WERE REPLACED WITH NEW,AND NEW NUTS AND WASHERS WERE ALSO INSSDR 99ZZZX4151Wheel · failedWHEEL FLANGE, PN D30210-4, SEPARATED FROM HUB ASSY. PN D30321 AND TUBE BLOW-OUT ON LANDING ROLL-OUT AFTER MAINT TEST FLIGHT AT THIS REPAIR STATION. A NEW TIRE HAD BEEN INSTALLED AT CRS BUER634C BEFORE A FERRY FLIGHT TO ACT FOR ENG OVERHAUL. FLIGHT TIME SINCSDR 99ZZZX3599Exhaust Riser · crackedEXHAUST RISER SPLIT OPEN AT PIPE TO RISER CONNECTION. HOT SPOTS AT CLUSTER IS NORMAL, CAUSING FATIGUE WITH AGING PIPES. NEW INCONEL RISER, PN 9912095-12, ASSY INSTALLED.SDR 99ZZZX2710Spar · crackedOPERATOR OF AIRCRAFT PERFORMED ROUTINE INSPECTION. FOUND FRONT SPAR OF THE HORIZONTAL STABILIZER CRACKED APPROXIMATELY 1 INCH OUTOARD OF EACH ATTACH POINT TO THE FUSELAGE. SUBMITTER STATED CAUSE OF CRACKS IS UNKNOWN.SDR 99ZZZX2650Fender · brokePILOT REPORTED HEARING A 'BANG' SHORTLY AFTER SELECTING GEAR DOWN. NOSE GEAR DID NOT EXTEND. INVEST REVEALED THE NOSE WHEEL FENDER LODGED ABOVE NOSE GEAR IN THE WHEELWELL. THIS JAMMED THE UPLOCK MECHANISM. THE NOISE WAS CAUSED BY THE RETRACT ROD FITTING BRSDR 99ZZZX1190Switch · out of adjustPILOT HAD NOT LEFT GEAR DOWN AND LOCKED LIGHT, TRIED TO REPLACE THE BULB. WHEN TRYING TO REPLACE THE BULB, THE CIRCUIT BREAKER TRIPPED. THE PILOT CYCLED GEAR TO THE UP POSITION ELECTRICALLY, THEN PULLED THE GEAR MOTOR CIRCUIT BREAKER AND PUT THE GEAR DOWN WISDR 99ZZZX967Beam · corrodedDURING REMOVAL OF THE LT ENGINE TURBO TO F.O.M., THE TURBO ATTACH BRACKET SEPARATED FROM THE OUTBOARD ENGINE BEAM, PN 0851121-9. THIS AREA IS VERY DIFFICULT TO INSPECT. SUBMITTER SUSPECTED GALVANIC CORROSION FROM DISSIMILAR METAL CONTACT. REMOVED AND REPLACSDR 99ZZZX934Doubler · crackedDOUBLER ASSY, P/N 5013046-1, DEVELOPED COMPOUND CRACKS UNDER NORMAL LANDING LOADS. NOSE WHEELWELL SKIN ALSO EXPERIENCED CRACKS DUE TO DOUBLER FAILURE. SUBMITTER SUGGESTED CAUSE OF CRACKS MAY BE ATTRIBUTED TO CROSS WIND AND HARD LANDINGS OR OVERBAGGAGE LOADINGSDR CA990129017Crankcase · cracked(CAN) DURING CRUISE ,THE PILOT NOTICED FLUCTUATING MANIFOLD PRESSURE ON NR 1 ENGINE. THE ENGINE THEN LOST POWER AND BEGAN TO LOSE OIL PRESSURE. THE ENGINE WAS SECURED AND THE AIRCRAFT MADE AN UNEVENTFUL EMERGENCY LANDING. POST-FLIGHT INSPECTION FOUND TWO HOSDR 98ZZZX4779Cylinder · crackedDURING 100-HOUR INSPECTION COMPRESSION CHECK, FOUND NR 3 CYLINDER CRACKED FROM THE EXHAUST VALVE GUIDE TO THE SPARK PLUG HOLE.SDR CA981109025Mount · corroded(CAN) AFTER ENGINE REMOVAL FROM RIGHT HAND POSITION, AN AREA ON OUTBOARD ENGINE RT BEAM HAD A SLIGHT BUMP. FURTHER EXAMINATION REVEALED A PORTION OF THE Z-SECTION WHICH MAKES UP THE BEAM WAS CORRODED RIGHT THROUGH. INBOARD BEAM ALSO CORRODED. SUBMITTER SUGGSDR CA981109023Alternator · cracked(CAN) ALTERNATOR REMOVED AT SAME TIME AS ENGINE REMOVAL. ONE ATTACHING EAR WAS FOUND CRACKED, TO THE POINT THAT THE ONLY THING HOLDING IT WAS THE MOUNTING FLANGE GASKET. SUBMITTER STATED CRACK VERY HARD TO SEE AS ENGINE BAFFLING OBSCURES CLEAR VIEW.SDR 98ZZZX4593Header · mismanufacturedHWS RECEIVED FROM CUSTOMER A NEW TURBOCHARGER EXHAUST HEADER WYE WHICH WAS PURCHASED FROM A CESSNA DISTRIBUTOR RECENTLY FOR INSPECTION. THE CUSTOMER WAS CONCERNED ABOUT THEIR PART BECAUSE ATTEMPTING TO INSTALL CORRESPONDING PARTS IN THEIR RESPECTIVE POSITIONSSDR CA981109022Crankcase · cracked(CAN) PILOT REPORTED OIL LEAK ON NR 2 ENGINE. ENGINE WAS WASHED DOWN AND RUN-UP. INSPECTION FOUND A 1.5 INCH CRACK JUST BELOW THE FORWARD TOP THROUGH-BOLT AREA, NEAR THE THRUST BEARING AREA OF THE FRONT OF THE CRANKCASE. THE ENGINE WAS REMOVED AND SENT FOR SDR CA980610007Seat Arms · cracked(CAN) PILOTS AND COPILOTS SEAT ARMS INSPECTED AND FOUND CEACKED. HAD BEEN WELDED AND DID NOT HOLD. NEW ARMS INSTALLED. MSB 89-3.SDR 98ZZZX1709Dowel Pin · shearedRIGHT ENGINE TACHOMETER INTERMITTENT. ALWAYS ACTED FINE ON GROUND RUN-UP. AFTER SOME TROUBLESHOOTING, FOUND THE DOWEL PIN THAT HOLDS ONE BEVEL GEAR TO THE TACHOMETER DRIVE GEAR SHEARED.SDR 98ZZZX2179Elt · failedELT UNIT 1-1/2 YEARS OLD. GOT TEST LIGHT, BUT NO OUTPUT SIGNAL.SDR CA980325025Exhaust Valve · worn(CAN) ENGINE RECEIVED FOR CRANKCASE REPAIR. ON DISASSEMBLY THE TIP OF THE EXHAUST VALVE STEMS, ON 2 CYLINDERS, WERE FOUND TO BELOW THE VALVE KEEPERS. THE VALVE KEEPERS WERE FOUND DAMAGED AND THE EXHAUST ROCKER ARMS WERE FOUND SEVERELY WORN. AS THE CYLINDERS WESDR 98ZZZX1472Attach Bolt · missingDURING AN ANNUAL INSPECTION, HORIZ STAB MOVED UP AND DOWN FROM THE RT SIDE. AN EXCESSIVE AMOUNT OF MOVEMENT WAS NOTED. DUIRNG CLOSER INSPECTION, FOUND BOLT, P/N NAS1306-4, MISSING FROM THE RT FORWARD ATTACH POINT. INSIDE THE STABILIZER AFT OF THE FORWARD SPSDR CA980317087Coupling · sheared(CAN) MAGNETO APPEARS TO HAVE SEIZED, SHEARING DRIVE COUPLING. MAGNETO WAS REPLACED.SDR 98ZZZX209Casting · crackedMLG SUPPORT STRUCTURE LT AND RT MLG WELL, INSPECTION FOUND MLG SIDEBRACE SUPPORT CASTINGS, P/N 822180-7, AND P/N 0822180-8, BOLTED TO RIBS, WERE LOOSE AND ONE DASH 8 CRACKED.SDR 98ZZZX208Casting · looseMLG SUPPORT STRUCTURE LT AND RT MLG WELL, INSPECTION FOUND MLG SIDEBRACE SUPPORT CASTINGS, P/N 822180-7, AND P/N 0822180-8, BOLTED TO RIBS, WERE LOOSE AND ONE DASH 8 CRACKED.SDR 98ZZZX207Skin · crackedMLG SUPPORT STRUCTURE LT AND RT MLG WELL, INSPECTION FOUND WING SKINS, P/N 08220009, UPPER INBOARD CRACKED ABOVE RIB INSIDE THE NACELLE BAG LOCKER.SDR 98ZZZX206Rib · crackedMLG SUPPORT STRUCTURE LT AND RT MLG WELL, INSPECTION FOUND CRACKS IN RIBS, P/N 0822175-79, AND P/N 0822175-74, CENTER RIB WEB AT THE UPPER AFT CORNER OF CUT-OUT HOLE WHERE OPERATING PUSH/PULL ROD PASSES THROUGH, TOWARD TOP OF RIB.SDR 98ZZZX205Rib · crackedMLG SUPPORT STRUCTURE LT AND RT MLG WELL, INSPECTION FOUND CRACKS IN RIBS, P/N 0822175-79, AND P/N 0822175-74, CENTER RIB WEB AT THE UPPER AFT CORNER OF CUT-OUT HOLE WHERE OPERATING PUSH/PULL ROD PASSES THROUGH, TOWARD TOP OF RIB.SDR 98ZZZX204Doubler · crackedNOSE WHEELWELL SUBSTRUCTURE INSPECTION FOUND DOUBLERS, P/N 5213045-3 LT, AND P/N 5213045-2 RT, CRACKED AT UPPER AFT CORNER RADIUS RELIEF CUT-OUTS.SDR 98ZZZX203Doubler · crackedNOSE WHEELWELL SUBSTRUCTURE INSPECTION FOUND DOUBLERS, P/N 5213045-3 LT, AND P/N 5213045-2 RT, CRACKED AT UPPER AFT CORNER RADIUS RELIEF CUT-OUTS.SDR 98ZZZX202Stiffener · looseNOSE WHEELWELL SUBSTRUCTURE INSPECTION FOUND STIFFENERS, P/N 5013044-3, P/N 5013044-11, WITH LOOSE AND WORKING RIVETS.SDR 98ZZZX201Stiffener · looseNOSE WHEELWELL SUBSTRUCTURE INSPECTION FOUND STIFFENERS, P/N 5013044-3, P/N 5013044-11, WITH LOOSE AND WORKING RIVETS.SDR 98ZZZX200Rivets · shearedNOSE WHEELWELL SUBSTRUCTURE INSPECTION FOUND BULKHEAD RIVETS SHEARED WHERE T-ANGLES, P/N 5213028-6, AND P/N 5013022-5, ARE RIVETED TO GUSSETS, P/N 521328-4, AND P/N 5013022-801.SDR 98ZZZX199Bulkhead · crackedNOSE WHEEL WELL SUBSTRUCTURE INSPECTION FOUND BULKHEAD, PN 501302014, HAD CRACKED BUTT END.SDR 97ZZZX4640Torque Tube · crackedCRACK FOUND AT THE FORK BOLT ATTACHMENT. FOUND DURING ANNUAL INSPECTION. CRACK LENGTH WAS .50 INCH.SDR 97ZZZX4524Doubler · crackedNOSE WHEELWELL SUBSTRUCTURE - CRACKS, LOOSE AND SHEARED RIVETS WERE FOUND ON BOTH SIDES OF NOSE GEAR WHEELWELL SUBSTRUCTURE. BULKHEAD, P/N 5013020-14, HAD CRACKED BUTT END, RIVETS SHEARED WHERE T-ANGLES, P/N 5213028-6 AND P/N 5013022-5 ARE RIVETED GUSSETS, P/SDR 97ZZZX4523Doubler · crackedNOSE WHEELWELL SUBSTRUCTURE - CRACKS, LOOSE AND SHEARED RIVETS WERE FOUND ON BOTH SIDES OF NOSE GEAR WHEELWELL SUBSTRUCTURE. BULKHEAD, P/N 5013020-14, HAD CRACKED BUTT END, RIVETS SHEARED WHERE T-ANGLES, P/N 5213028-6 AND P/N 5013022-5 ARE RIVETED GUSSETS, P/SDR 97ZZZX4522Stiffener · rivets looseNOSE WHEELWELL SUBSTRUCTURE - CRACKS, LOOSE AND SHEARED RIVETS WERE FOUND ON BOTH SIDES OF NOSE GEAR WHEELWELL SUBSTRUCTURE. BULKHEAD, P/N 5013020-14, HAD CRACKED BUTT END, RIVETS SHEARED WHERE T-ANGLES, P/N 5213028-6 AND P/N 5013022-5 ARE RIVETED GUSSETS, P/SDR 97ZZZX4521Stiffener · rivets looseNOSE WHEELWELL SUBSTRUCTURE - CRACKS, LOOSE AND SHEARED RIVETS WERE FOUND ON BOTH SIDES OF NOSE GEAR WHEELWELL SUBSTRUCTURE. BULKHEAD, P/N 5013020-14, HAD CRACKED BUTT END, RIVETS SHEARED WHERE T-ANGLES, P/N 5213028-6 AND P/N 5013022-5 ARE RIVETED GUSSETS, P/SDR 97ZZZX4520T Angle · rivet shearedNOSE WHEELWELL SUBSTRUCTURE - CRACKS, LOOSE AND SHEARED RIVETS WERE FOUND ON BOTH SIDES OF NOSE GEAR WHEELWELL SUBSTRUCTURE. BULKHEAD, P/N 5013020-14, HAD CRACKED BUTT END, RIVETS SHEARED WHERE T-ANGLES, P/N 5213028-6 AND P/N 5013022-5 ARE RIVETED GUSSETS, P/SDR 97ZZZX4519T Angle · rivet shearedNOSE WHEELWELL SUBSTRUCTURE - CRACKS, LOOSE AND SHEARED RIVETS WERE FOUND ON BOTH SIDES OF NOSE GEAR WHEELWELL SUBSTRUCTURE. BULKHEAD, P/N 5013020-14, HAD CRACKED BUTT END, RIVETS SHEARED WHERE T-ANGLES, P/N 5213028-6 AND P/N 5013022-5 ARE RIVETED GUSSETS, P/SDR 97ZZZX4518Bulkhead · crackedNOSE WHEELWELL SUBSTRUCTURE - CRACKS, LOOSE AND SHEARED RIVETS WERE FOUND ON BOTH SIDES OF NOSE GEAR WHEELWELL SUBSTRUCTURE. BULKHEAD, P/N 5013020-14, HAD CRACKED BUTT END, RIVETS SHEARED WHERE T-ANGLES, P/N 5213028-6 AND P/N 5013022-5 ARE RIVETED GUSSETS, P/SDR 97ZZZX4517Rib · crackedMAIN LANDING GEAR SUPPORT STRUCTURE, LT AND RT, MLG WHEELWELL - CRACKS ARE OCCURRING IN THE RIBS, PN 0822175-79, -74, CENTER RIB WEB, ORIGINATING AT UPPER AFT CORNER OF THE CUT-OUT HOLE (WHERE THE OPERATING PUSH/PULL ROD PASSES THROUGH) PROPAGATING TOWARDS TOPSDR 97ZZZX4516Skin · crackedMAIN LANDING GEAR SUPPORT STRUCTURE, LT AND RT, MLG WHEELWELL - CRACKS ARE OCCURRING IN THE RIBS, PN 0822175-79, -74, CENTER RIB WEB, ORIGINATING AT UPPER AFT CORNER OF THE CUT-OUT HOLE (WHERE THE OPERATING PUSH/PULL ROD PASSES THROUGH) PROPAGATING TOWARDS TOPSDR 97ZZZX4515Casting · crackedMAIN LANDING GEAR SUPPORT STRUCTURE, LT AND RT, MLG WHEELWELL - CRACKS ARE OCCURRING IN THE RIBS, PN 0822175-79, -74, CENTER RIB WEB, ORIGINATING AT UPPER AFT CORNER OF THE CUT-OUT HOLE (WHERE THE OPERATING PUSH/PULL ROD PASSES THROUGH) PROPAGATING TOWARDS TOPSDR 97ZZZX4514Casting · crackedMAIN LANDING GEAR SUPPORT STRUCTURE, LT AND RT, MLG WHEELWELL - CRACKS ARE OCCURRING IN THE RIBS, PN 0822175-79, -74, CENTER RIB WEB, ORIGINATING AT UPPER AFT CORNER OF THE CUT-OUT HOLE (WHERE THE OPERATING PUSH/PULL ROD PASSES THROUGH) PROPAGATING TOWARDS TOPSDR 97ZZZX4513Rib · crackedMAIN LANDING GEAR SUPPORT STRUCTURE, LT AND RT, MLG WHEELWELL - CRACKS ARE OCCURRING IN THE RIBS, PN 0822175-79, -74, CENTER RIB WEB, ORIGINATING AT UPPER AFT CORNER OF THE CUT-OUT HOLE (WHERE THE OPERATING PUSH/PULL ROD PASSES THROUGH) PROPAGATING TOWARDS TOPSDR 97ZZZX4528Bearing · crackedIN C/W AD 90-02-13, THE MAIN GEAR BARREL INNER BEARING WAS FOUND CRACKED. NEW P/N 5141109-1 BEARING INSTALLED.SDR CA970212004Static Tube · split(CAN) SUSPECT WATER IN THE LINE, BETWEEN THE STATIC PORT AND THE SUMP, FROZE AND SPLIT THE PIPE.SDR 97ZZZX573Exhaust Wye · crackedTURBO EXHAUST WYE RECEIVED FOR INSP AND REPAIR. FOUND UNIT HAD A CRACK AROUND WELD ON OUTLET TUBE SIDE. IT WAS EVIDENT TUBE AND INTERNAL DIVIDER HAD BEEN REPLACED. IMPROPER MATERIALS HAD BEEN UTILIZED IN THE FABRICATION OF THE OUTLET TUBE AND DIIVDER.
Back to Cessna 414