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 = '1900C' 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 = '1900C' 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 20010601CW007Spring · brokenFLIGHT CREW REPORTED PROPELLER NOT GOING INTO FULL FEATHER AT ENGINE SHUT DOWN. INSPECTION REVEALED THAT ALL PROP BLADES WERE FREE TO TWIST 45 DEG.+ BY HAND. THERE WERE NO EXTERNAL FAULTS VISIBLE AND THE DOME MOVED FREELY WITH THE BLADES. DETAILED INSPECTIOSDR CA000921004Line · cracked(CAN) ENGINE WENT TO FLIGHT IDEL JUST AFTER TAKE OFF ALONG WITH RESULTANT AUTOFEATHER AFTER TORQUE DROPPED BELOW 250 LBS. P3 LINE CRACKED AT FLARE.SDR NSVA20002Rod · misinstalledAFTER TAKEOFF FROM ACK ADJUSTED AILERON TRIM WHICH CAUSED THE LEFT POWER LEVER TO MOVE AFT (RETARD). LEFT ENGINE TORQUE DECREASED APPROXIMATELY 500 LBS. DIVERTED AIRCRAFT TO HYA AND LANDED UNEVENTFULLY. MAINTENANCE FOUND LEFT ENGINE POWER LEVER PUSH/PULL COSDR 20010601CW005Switch · disconnectedWHILE PERFORMING ENGINE FIRE EXTINGUISHER SYSTEM TEST IAW B1900C MM CAMP NR 2 INSPECTION TEMP REVISION, FOUND NR 2 ENGINE SQUIB POWER SWITCH DISCONNECTED FROM ANNUNCIATOR/ ACTUATOR ASSEMBLY DESIGN BE CHANGED FOR POSITIVE ATTACHMENT OF THE SQUIB SWITCH. FAILURSDR 20001128AP007Fuel Control · inoperativeFLT 9195 - NAS/PBI - ON APPROACH TO PBI, LEFT ENGINE HAD LOSS OF POWER WHEN THROTTLE RETARDED TO 1,000 LBS. SECURED ENGINE. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LEFT FUEL CONTROL UNIT. (M)SDR 20001128AP005Fuel Control · inoperativeFLT 9195 - NAS/PBI - ON APPROACH TO PBI, LEFT ENGINE HAD LOSS OF POWER WHEN THROTTLE RETARDED TO 1,000 LBS. SECURED ENGINE. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LEFT FUEL CONTROL UNIT. (M)SDR 20001127AP001Fuel Control · inoperativeFLT 9195 - NAS/PBI - ON APPROACH TO PBI, LEFT ENGINE HAD LOSS OF POWER WHEN THROTTLE RETARDED TO 1,000 LBS. SECURED ENGINE. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LEFT FUEL CONTROL UNIT. (M)SDR 20010425CW016Clamp · unsecureNR 1 ENGINE POWER FAILED TO REDUCE BELOW 2200 LBS. TORQUE FOR LANDING. THE ENGINE WAS SHUT DOWN IN FLIGHT JUST PRIOR TO LANDING. A NON EVENTFUL LANDING WAS ACCOMPLISHED AND THE ENGINE WAS RESTARTED FOR TAXI TO HANGAR. MAINTENANCE WAS UNABLE TO VERIFY THE CASDR 20010425CW014Windshield · crackedCOPILOTS WINDSHIELD OUTER PANE CRACKED AFTER TAKEOFF. AIRCRAFT RETURNED TO AIRPORT WITHOUT INCIDENT.SDR 20001024AP005Line · brokenRIGHT ENGINE GRADUAL POWER LOSS. FOUND PRIMARY GOVERNOR P-3 DUMPLINE BROKEN AT GOVERNOR END. (M)SDR 20001017AP004Panel · shortedFLT 9449 - RSW-TPA - DURING TAXI, HEARD AND SAW ELECTRICAL ARC ON MAIN CIRCUIT BREAKER PANEL, THERE WAS A SMELL OF ELECTRICAL SMOKE. REMOVED AND REPLACED LUMINESCENT PANEL IAW BEECHCRAFT MM CHAP 33. OPERATIONAL CHECK NORMAL. (M)SDR 20001128AP006Blade · wornFLT 9230 - TPA/MIA - ON TAKEOFF, THE RIGHT ENGINE ITT ROSE AND TORQUE DECREASED. DECLARED AN EMEGENCY AND RETURNED TO TPA. PERFORMED HOT SECTION INSPECTION AND REPLACED CT DISK AND INNER EXIT DUCT ASSEMBLY DUE TO WEAR. (M)SDR 20000721AP004Warning System · false indicationFLT 9261 - FPO/MIA - GEAR HANDLE WARNING ANNUNCIATORS ILLUMINATED IN FLIGHT REDUCED SPEED AND CYCLED GEAR PROBLEM REOCURRED. INSPECTED LANDING GEAR UP SWITCH FOR LOOSE CONNECTIONS AND PROPER ADJUSTMENT. FOUND TO BE NORMAL. PERFORMED LANDING GEAR RETRACTION SDR 20000721AP003Downlock Switch · out of adjFLT 2021 - FLL/FLL - LEFT MAIN LANDING GEAR INDICATING LIGHT INTERMITTENT. ADJUSTED LEFT LANDING GEAR DOWN POSITION SWITCH. LANDING GEAR EXTENSION AND RETRACTION NORMAL. (M)SDR 20001103AP007Block · wornFLT 9410 - MIA/EYW - AFTER ROTATION, RIGHT PROP RPM DROPPED TO APPROXIMATELY 1200 RPM. RETURNED TO MIA. DETERMINED RIGHT BETA BLOCK TO BE WORN. REPLACED RIGHT BETA BLOCK AND RIGGED. (M)SDR 20010425CW011Packing · wornLEFT BRAKE FAILED ON LANDING. LEFT BRAKE MASTER CYLINDER REPLACED. OPS CHECKED GOOD. REMOVED MASTER CYLINDER INSPECTED AND NO VISUAL FAULTS OR DISCREPANCIES WERE FOUND. COMPONENT INTERNAL INSPECTION REVEALED NO DAMAGE OTHER THAN GOUGED ORING.SDR CA000530048Bearing · failed(CAN) NR 4 MAIN WHEEL DISLODGED FROM ITS AXLE IN FLIGHT. NO OTHER APPARENT DAMAGE TO GEAR OR AIRFRAME.THE BRAKES AND TIRES ON THIS AXLE WERE REMOVED AND REPLACED JANUARY 06, 2000. NR 4 MAIN WHEEL HAS NOT BEEN LOCATED. SUPPLEMENTAL: RECORDS INDICATE NEW BEARISDR 20000725AP005Hinge · corrodedDURING SCHEDULED MAINTENANCE, LEFT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULAR CORROSION. REMOVED AND REPLACED LEFT ELEVATOR OUTBOARD HINGE. (M)SDR 20000622AP001Relay · stuckFLT 9493 - MIA-FLL - LANDING GEAR RELAY HAD A RINGING NOISE AND BURNING SMELL, RELAY POPPED. REMOVED AND REPLACED K3 RELAY. OPERATIONAL CHECK GOOD. (M)SDR CA000419009Cone · scored(CAN) BEARINGS RECEIVED FROM CANADIAN DISTRIBUTOR WITH NEW CERTIFICATION BUT VISUALLY INSPECTED TO BE USED PARTS. ISSUE SENT TO MAINTENANCE AND MANUFACTURING FOR FOLLOW-UP. (X)SDR 20000622AP002Bolt · shearedFLT 9424 - EYW/MIA - ON APPROACH TO MIA, THE FLAPS WERE SELECTED TO THE LANDING POSITION. THE AIRCRAFT WENT TO THE LEFT. PERFORMED MISSED APPROACH PROCEDURES. UNABLE TO RAISE THE FLAPS OUT OF LANDING POSITION, SUSPECTED DIFFERENTIAL FLAP LOCKOUT, RETRIMMED SDR CA000410006Blade · corroded(CAN) BLADE BUT CORROSSION REQUIRED APPROVED REPAIR SCHEME.SDR CA000410005Blade · delaminated(CAN) BLADE SCRAPPED DUE TO CREASE DELAMINATION.SDR 20000619AP012Nozzle · looseFLT 9209 - ON CLIMB-OUT FROM TAMPA, RIGHT T-HANDLE FIRE WARNING ILLUMINATED. PILOT SHUT DOWN ENGINE, DECLARED EMERGENCY AND RETURNED TO TAMPA. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED RIGHT ENGINE. NO EVIDENCE OF FIRE. DETERMINED TO BE HOT AIR LEAKING SDR CA000329028Actuator · corroded(CAN) AFTER TAKE OFF IT TOOK THE NOSE GEAR LIGHT 7-8 SECONDS BEFORE IT WOULD ILLUMINATE. INVESTIGATION FOUND FALSE INDICATION WAS DUE TO A CORRODED MICROSWITCH. THE MICROSWITCH IS A PART OF THE ACTUATOR ASSEMBLY.ACTUATOR ASSY. REPLACED.SUBMITTER STATED THE FRSDR 20000505AP032Fuel Line · leakingON APPROACH, THE LEFT ENGINE LOST TORQUE. THE ENGINE WAS SHUTDOWN. FOUND FUEL LINE FROM THE FUEL FLOW TRANSMITTER TO THE FUEL CONTROL LEAKING. REPLACED FUEL LINE. (M)SDR CA000328007Switch · seized(CAN) WHILE CARRYING OUT BEECH COMMUNIQUE NR 169, THE SUBSEQUENT TESTING OF FLAP ASSYMETRY SWITCHES SHOWED THE RT SWITCH FAILING THE TEST. IT WAS NOTED THAT WHEN THE ADJUSTABLE ROD WAS DISCONNECTED FROM ITS MATING ARM AND THE ARM WAS MOVED SO AS TO CAUSE THE SDR 20000414SH006Encoder · malfunctionedPILOT REPORTED THAT ALTIMETER FLAGGED. COULD NOT DUPLICATE PROBLEM ON TEST BENCH. RE-CERTIFIED ALTIMETER AND RETURNED TO SERVICE. (X)SDR CA000320013Switch · failed(CAN) DURING COMPLIANCE TO RAYTHEON, UPON TESTING FOR POWER (AC VOLTAGE) ON RT SQUIB WIRES, IT WAS NOTED THAT THE RT ENGINE FIRE PUSH TO EXT SWITCH FELT INCORRECT AND NO AUDIBLE CLICK WAS HEARD. FURTHER INVESTIGATION REVEALED THAT THE TRIGGER SWITCH WHICH IS SDR AU000213Pipe · worn(AUS) LT ENGINE FUEL PIPE CHAFED ON STARTER/GENERATOR DUCT.SDR 20000427AP008Engine · failedFLT 9330 - TPA-JAX - WHILE IN DESCENT INTO JACKSONVILLE AT 10,000 FT, A LOUD SQUEALING NOISE WAS HEARD. LEFT ENGINE INDICATED ITT AND TORQUE FLUCTUATIONS. PILOT MADE THE DETERMINATION TO SHUT THE LEFT ENGINE DOWN. REMOVED ENGINE ASSEMBLY AND ROUTED TO PRATTSDR CA000301025Engine · failed(CAN) BURNING SMELL NOTED IN COCKPIT, NR 2 ENGINE NOISE AND VISIBLE FLAME FROM EXHAUST DUCTS. REPORT TO FOLLOW.SDR NSVA0002011Wheel · separatedON JAN 30 AT 1200 HOURS AIRCRAFT SN UC-19 THE NR 4 RIGHT OUTBOARD WHEEL ASSEMBLY SEPARATED FROM THE AIRCRAFT DURING TAKEOFF. THE CREW WAS NOTIFIED BY GROUND PERSONNEL AND THE AIRCRAFT WAS REROUTED TO AN ADEQUATE FACILITY. THE AIRCRAFT LANDED WITHOUT INCIDENTSDR 20010601CW008Stud · improperTHREADED STUD ON THIS TERMINAL ADAPTER LUG HAS IMPROPER THREAD PITCH/DIAMETER FOR PROPER INSTALLATION OF WIRE TERMINAL NUT. IF THE NUT IS THREADED ON THE TERMINAL AS DELIVERED FROM MFG., THE THREADS ON THE TERMINAL STRIP OUT. IF THE ADAPTER IS USED AS DELIVESDR 2000ZZZX493Terminal Lug · mismanufacturedTHREADED STUD ON THIS TERMINAL ADAPTER LUG HAS IMPROPER THREAD PITCH/DIAMETER FOR PROPER INSTALLATION OF WIRE TERMINAL NUT. IF THE NUT IS THREADED ON THE TERMINAL AS DELIVERED FROM RAYTHEON, THE THREADS ON THE TERMINAL STRIP OUT. IF THE ADAPTER IS USED AS DESDR 20000404SH021Encoder · failedALTIMETER QUIT AT 950 FEET. ENCODING FUNCTION ALSO QUIT. FLAG DROPPED AND STAYED IN VIEW. UNIT BENCH CHECKED AS INOPERABLE. SUBMITTER STATED THIS IS THE SECOND UNIT, OF THIS PART NUMBER, IN A WEEK TO FAIL. (X)SDR CA000118053Relay · loose(CAN) FIRST INCIDENT, THE AIRCRAFT LANDING GEAR SYSTEM FUNCTION TESTED OK IN THE HANGAR SO PERSONNEL WERE UNABLE TO DUPLICATE PROBLEM. AFTER SECOND OCCURRENCE MAINTENANCE PERSONNEL COULD DUPLICATE THE PROBLEM ON THE GROUND AND ATTRIBUTED IT TO A BENT PIN AT TSDR 20010607CW008Switch · disconnectedWHILE PERFORMING OTHER MAINTENANCE, FOUND LEFT ENGINE SQUIB POWER SWITCH DISLOCATED FROM ENGINE FIRE EXTINGUISHER ANNUNCIATOR/ACTUATOR ASSEMBLY. FOUND SQUIB SWITCH MODULE NOT PROPERLY RETAINED BY TABS ON ANNUNCIATOR BODY. THIS CONDITION HAS BEEN FOUND ON HALSDR 2000ZZZX421Switch · disconnectedWHILE PERFORMING OTHER MAINTENANCE, FOUND LT ENGINE SQUIB POWER SWITCH DISLOCATED FROM ENGINE FIRE EXTINGUISHER ANNUNCIATOR/ACTUATOR ASSEMBLY. FOUND SQUIB SWITCH MODULE NOT PROPERLY RETAINED BY TABS ON ANNUNCIATOR BODY. THIS CONDITION HAS BEEN FOUND ON HALF SDR 20010607CW007Switch · disconnectedWHILE PERFORMING A NEW INSPECTION REQUIREMENT, FOUND BOTH SQUIB POWER SWITCHES DISLOCATED FROM MAIN ENGINE FIRE EXTINGUISHER ANNUNCIATOR/ACTUATOR ASSEMBLY. FOUND SQUIB SWITCH MODULE NOT PROPERLY RETAINED BY TABS ON ANNUNCIATOR BODY. THIS CONDITION HAS BEEN FSDR 2000ZZZX423Switch · disconnectedWHILE PERFORMING 'NEW' INSP REQUIREMENT, FND BOTH SQUIB POWER SWITCHES DISLOCATED FROM MAIN ENG FIRE EXTING ANNUNCIATOR/ACTUATOR ASSY. FOUND SQUIB SWITCH MODULE NOT PROPERLY RETAINED BY TABS ON ANNUNCIATOR BODY. THIS CONDITION HAS BEEN FND ON HALF OF INSPECTSDR YAD2001F00000Switch · disconnectedFOUND SQUIB POWER SWITCH DISLOCATED FROM MAIN ENG FIRE EXTING ANNUNCIATOR/ACTUATOR ASSY. SQUIB SWITCH MODULE NOT PROPERLY RETAINED BY TABS ON ANNUNCIATOR BODY. THIS CONDITION WAS FOUND ON TWO ASSEMBLIES OUT OF SIX CHECKED. NEW REPLACEMENT ASSY FOUND TO BE MSDR 2000ZZZX422Switch · disconnectedWHILE PERFORMING 'NEW INSP REQUIREMENT, FOUND SQUIB POWER SWITCH DISLOCATED FROM MAIN ENG FIRE EXTINGUISHER ANNUNCIATOR/ACTUATOR ASSY. FOUND SQUIB SWITCH MODULE NOT PROPERLY RETAINED BY TABS ON ANNUNCIATOR BODY. THIS CONDITION WAS FOUND ON 2 ASSYS OUT OF 6 CSDR CA991208064Guide Collar · failed(CAN) THE PITCH CHANGE GUIDE COLLAR WAS CHANGED DUE TO A CLOSE TOLERANCE FIT (STILL WITHIN LIMITS) FAILURE.SDR 99ZZZX4654Annunciator · failedFAILURE OF NON-FIELD REPLACEABLE IFR GPS 'LEG' ANNUNCIATION. THIS COMPONENT IS THE INDICATOR/SWITCHING UNIT OF A CERTIFIED IFR GPS NAVIGATION SYSTEM.SDR 99ZZZX4218Light · failed'GPS' MODE LIGHT OUT AFTER 726 HOURS/70 DAYS OF OPERATION.SDR CA991027042Relay · corroded(CAN) ON APPROACH, THE LANDING GEAR WAS SELECTED DOWN BUT SYSTEM FAILED TO OPERATE. THE MANUAL EXTEND SYSTEM WAS USED AND AN UNEVEVENTFUL LANDING WAS COMPLETED. UPON INSPECTION BY MAINTENANCE, THE RELAY CONTACTS FOR THE HYDRAULIC PUMP WERE FOUND TO HAVE SOMESDR CA991004034Spring · broken(CAN) LIGHTNING STRIKE SUSPECT IN CAUSING PART DAMAGE.SDR 99ZZZX3958P3 Line · brokenRIGHT ENGINE FAILED. ROLLED BACK TO IDLE. FOUND EXTERNAL P3 BLEED LINE BROKEN.SDR 20000505AP028Seal · leakingPILOT REPORTED HEAVY EXHAUST FUMES ENTERING CABIN THROUGH BLEED AIR SYSTEM. THIS WAS THE THIRD REPORT IN A ROW. PREVIOUS REPAIRS INCLUDED REPLACING A CRACKED EXHAUST STACK. COULD NOT DUPLICATE ON GROUND. THE FINAL DISCREPANCY REPAIRED WAS TO REPLACE NR 1 E
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