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 = 'F33A' 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 = 'F33A' 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 2010FA0000644Relay · failedPILOT REPORTED AFTER PUTTING THE GEAR SELECTOR IN THE DOWN POSITION THE GEAR WOULDN’T EXTEND, PILOT CRANKED THE GEAR DOWN AND RETURNED TO BASE. ON TROUBLESHOOTING THE MECHANIC FOUND RELAY FAILED INTERNALLY, 384 FLIGHT HOURS, ESTIMATED CYCLES 1536. PROBABLE CASDR 2010FA0000577Cylinder · crackedTHE NR 6 CYLINDER BARREL CRACKED 2.5 INCHES UP THE BARREL FROM THE FACE OF THE MOUNTING FLANGE. CRACKED EXTENDED APPROX 330 DEG AROUND THE CIRCUMFERENCE OF THE BARREL. BARREL EXHIBITS HEAT DAMAGE ON THE BARREL IN LINE WITH THE PISTON PIN AND THE PISTON PIN HASDR 2010FA0000524Relay · failed((VJ3R)) ON ROUTINE PHASE INSP, MECHANIC FOUND THE DYNAMIC BREAKER FAILED ON RELAY. PROBABLE CAUSE AT THIS TIME UNKNOWN. RECOMMENDATION IS TO REPLACE RELAY UNTIL MFG DESIGNS A BETTER RELAY.SDR 2010FA0000523Circuit Breaker · inoperativePILOT REPORTED TAXI LIGHT INOP. ON TROUBLESHOOTING , TECH FOUND CIRCUIT BREAKER/ SWITCH TO BE AT FAULT. AD 2008-13-17 HAD BEEN COMPLETED 1516 FLIGHT HOURS PRIOR AND ESTIMATED CYCLES 6064. NOTICED NEW CIRCUIT BREAKER, NO PROBABLE CAUSE OR RECOMMENDATIONS AT THISDR 2010FA0000464Circuit Breaker · inoperativePILOT REPORTED TAXI LIGHT INOP. ON TROUBLESHOOTING TECHNICIAN FOUND CIRCUIT BREAKER / SWITCH TO BE AT FAULT. A.D. 2008-13-17 HAD BEEN COMPLETED 1180 FLIGHT HOURS PRIOR AND ESTIMATED CYCLES 4720. NOTICED NEW CIRCUIT BREAKER MANUFACTURER IS TYCO ELECTRONICS. NO SDR 2010FA0000442Circuit Breaker · inoperative(VJ3R) NO POWER THROUGH THE C/B SWITCH.SDR 2010FA0000441Circuit Breaker · inoperative(VJ3R) NO POWER THROUGH THE SWITCH.SDR 2010FA0000422Circuit Breaker · inoperative(VJ3R) PILOT REPORTED STROBE LIGHTS INOP. ON TROUBLESHOOTING, TECH FOUND CIRCUIT BREAKER/SWITCH TO BE AT FAULT. AD 2008-13-17 HAD BEEN COMPLETED 1405 FLIGHT HOURS PRIOR AND ESTIMATED CYCLES 5620. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME.SDR 2010FA0000420Relay · intermittent(VJ3R) PILOT REPORTED AFTER PUTTING THE GEAR SELECTOR IN THE UP POSITION HE STILL HAD (3) GREEN LIGHTS AND NO IN TRANSIT LIGHT, PILOT THEN PUT THE GEAR SELECTOR IN THE DOWN POSITION AND RETURNED TO BASE. ON TROUBLESHOOTING THE MECHANIC CYCLED GEAR SEVERAL TIMESDR 2010FA0000340Circuit Breaker · failed(VJ3S) PILOT REPORTED LANDING LIGHT INOP. ON TROUBLESHOOTING TECH FOUND CIRCUIT BREAKER/ SWITCH TO BE AT FAULT AD 2008-13-17 HAD BEEN COMPLETED 1248 FLIGHT HOURS PRIOR AND ESTIMATED CYCLES 4992. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME.SDR 2010FA0000339Circuit Breaker · failed(VJ3S) NO POWER THROUGHT THE C/B SWITCH. INTERNAL FIALURE.SDR 2010FA0000294Circuit Breaker · failed(VJ3S) PILOT REPORTED LANDING LIGHT INOP. ON TROUBLESHOOTING, TECH FOUND CIRCUIT BREAKER/ SWITCH TO BE AT FAULT. AD 2008-13-17 HAD BEEN COMPLETED 1500 FLIGHT HOURS PRIOR AND ESTIMATED CYCLES 6000. NOTICED NEW CIRCUIT BREAKER. NO PROBABLE CAUSE OR RECOMMENDASDR 2010FA0000293Circuit Breaker · failed(VJ3R) PILOT REPORTED TAXI LIGHT INOP. ON TROUBLESHOOTING TECH FOUND CIRCUIT BREAKER/SWITCH TO BE AT FAULT. AD 2008-13-17 HAD BEEN COMPLETED 859 FLIGHT HOURS PRIOR AND ESTIMATED CYCLES 3436. NOTICED NEW CIRCUIT BREAKER. NO PROBABLE CAUSE OR RECOMMENDATIONS ATSDR 2010FA0000292Circuit Breaker · failed(VJ3R) PILOT REPORTED TAXI LIGHT INOP. ON TROUBLESHOOTING, TECH FOUND CIRCUIT BREAKER/ SWITCH TO BE AT FAULT. AD 2008-13-17 HAD BEEN COMPLETED 1271 FLIGHT HOURS PRIOR AND ESTIMATED CYCLES 5084. NOTICED NEW CIRCUIT BREAKER. NO PROBABLE CAUSE OR RECOMMENDATIONS SDR 2010FA0000291Circuit Breaker · failed(VJ3R) PILOT REPORTED TAXI LIGHT INOP. ON TROUBLESHOOTING, TECH FOUND CIRCUIT BREAKER/SWITCH TO BE AT FAULT. AD 2008-13-17 HAD BEEN COMPLETED 1072 FLIGHT HOURS PRIOR AND ESTIMATED CYCLES 4288. NOTICED NEW CIRCUIT BREAKER. NO PROBABLE CAUSE OR RECOMMENDATIONS ASDR 2010FA0000290Circuit Breaker · failed(VJ3R) PILOT REPORTED TAXI LIGHT INOP. ON TROUBLESHOOTING, TECH FOUND CIRCUIT BREAKER/SWITCH TO BE AT FAULT. AD 2008-13-17 HAD BEEN COMPLETED 1319 FLIGHT HOURS PRIOR AND ESTIMATED CYCLES 5276. NOTICED NEW CIRCUIT BREAKER. NO PROBABLE CAUSE OR RECOMMENDATIONSSDR 2010FA0000288Pump · low pressure(VJ3R)ON PHASE RUN UP MECHANIC NOTICED THE GYRO WARNING LIGHT ON. UP ON TROUBLESHOOTING THE MECHANIC DETERMINED THE VANES ON THE AIR PUMP WERE WORN AND WAS NOT PRODUCING ENOUGH PRESSURE. INSTALLED NEW PUMP, SYS WORKED NORMAL. NO PROBABLE CAUSE OR RECOMMENDATSDR 2010FA0000255Pump · failedPILOT REPORTED INSTRUMENT AIR PRESSURE LOW AND GYRO WARNING LIGHT ON. UPON TROUBLESHOOTING THE MX DETERMINED THE AIR PUMP WAS NOT PRODUCING ENOUGH PRESSURE AT DIFFERENT POWER SETTINGS. INSTALLED NEW PUMP, SYSTEM WORKED NORMAL. NO PROBABLE CAUSE OR RECOMMENDATSDR 2010FA0000254Transmitter · inoperativePILOT REPORTED FUEL FLOW WAS FLUCTUATING ON TAKEOFF. ON TROUBLESHOOTING, THE MX DETERMINED FUEL FLOW TRANSMITTER WAS BAD. MX RECEIVED A UNIT FROM PARTS AND INSTALLED ON ACFT, WHEN THE MX WENT TO RUN THE ACFT HE WAS UNABLE TO KEEP THE ENGINE RUNNING, INSTALLESDR 2010FA0000082Relay · failedLANDING GEAR WILL NOT RETRACK OR EXTEND. DYNAMIC RELAY FAILED.SDR 2010FA0000081Relay · intermittentLANDING GEAR WILL NOT RETRACK .SDR 2010FA0000077Circuit Breaker · failedWHEN PILOT SELECTED LANDING LIGHT, LIGHT DID NOT WORK. TECH TROUBLESHOT AND FOUND FAULT TO BE WITH LANDING LIGHT CIRCUIT BREAKER, INTERNAL FAILURE OF CIRCUIT BREAKER.SDR 2010FA0000064Switch · shortedDURING THE USE OF THE NAVIGATION LIGHTS, THE NAVIGATION LIGHT CIRCUIT BREAKER SWITCH WOULD POP AND NOT RESET. TROUBLESHOT SYS AND FOUND FAULT TO BE WITH CIRCUIT BREAKER SWITCH. REMOVED AND REPLACED SWITCH WITH SAME PN 35-380132-101. THESE SWITCHES ARE SUPPOSDR 2010FA0000066Switch · shortedPILOT REPORTED TAXI LIGHT INOPERATIVE, INVESTIGATION BY TECH, FOUND TAXI LIGHT CIRCUIT BREAKER SWITCH WAS AT FAULT. REPLACED CIRCUIT BREAKER SWITCH SYS OPS CHECKED NORMAL. THIS CIRCUIT BREAKER SWITCH WAS REPLACED 888 HOURS FLIGHT TIME PRIOR TO FAILURE IAW AD SDR 2010FA0000037Terminal · looseCONTACT TERMINALS ARE LOOSE AND CAN BE MOVED BY HAND. SWITCH THROW HANDLE IS ALSO LOOSE AND CAN BE MOVED FROM ANY POSITION.SDR 2010FA0000036Terminal · looseCONTACT TERMINALS ARE LOOSE AND CAN BE MOVED BY HAND. SWITCH THROW HANDLE IS ALSO LOOSE AND CAN BE MOVED FROM ANY POSITION.SDR 2010FA0000027Circuit Breaker · failedDURING USE OF NAV LIGHTS, NAVIGATION LIGHT CIRCUIT BREAKER SWITCH WAS PLACED IN ON POSITION AND NAVIGATION LIGHTS DID NOT COME ON. PROBABLE CAUSE TO FAILURE WAS DUE TO INTERNAL FAILURE OF CIRCUIT BREAKER SWITCH. SEPARATE THE SWITCH FOR AN INDEPENDENT TOGGLE SDR 2010FA0000024Circuit Breaker · unserviceableAFTER TURNING ON TAXI LIGHT, A STRONG ELECTRICAL BURNING ODOR WAS NOTICED, WITH THE CIRCUIT BREAKER HOT TO THE TOUCH. FURTHER INSPECTION REVEALED A BURN MARK ON THE SIDE OF TAXI LIGHT CIRCUIT BREAKER. AD 2008-13-17 HAD BEEN COMPLETED 691 FLIGHT HOURS PREVIOUSDR 2010FA0000025Circuit Breaker · failedDURING POST FLIGHT INSP OF LIGHTS, LANDING LIGHT CIRCUIT BREAKER WAS PLACED IN THE ON POSITION AND LANDING LIGHTS DID NOT COME ON. PROBABLE CAUSE TO THE FAILURE WAS DUE TO INTERNAL FAILURE OF THE CIRCUIT BREAKER. RECOMENDATION WOULD BE TO SEPARATE THE SWITCHSDR CA101012005Shim · failedTHE BRASS SHIMS ARE "BRAKING" AND CAUSING THE TRIM TO TEMPORARY STICK WHEN GOING FROM ELECTRIC TRIM TO MANUAL OPERATION. PN OF THE AFFECTED PART IS P/N 4602.SDR 2009FA0000301Relay · intermittentPILOT REPORTED AFTER PUTTING THE GEAR SELECTOR IN THE UP POSITION, THE GEAR FAILED TO RETRACT, PILOT THEN PUT THE GEAR SELECTOR IN THE DOWN POSITION AND RETURNED TO BASE. ON TROUBLESHOOTING, THE MECHANIC CYCLED GEAR SEVERAL TIMES AND WAS UNABLE TO GET THE GESDR 2009FA0000300Circuit Breaker · unserviceablePILOT REPORTED AFTER LANDING, THE LANDING LIGHT CIRCUIT BREAKER SWITCH WAS VERY HOT TO THE TOUCH, AFTER FURTHER INVESTIGATION, WE REPLACED THE SWITCH. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME. (K)SDR CA090504003Plate · cracked(CAN) AFTER INSP, CAUSE OF FAILURE WAS DUE TO THE PLATE (PN 643629) HOLDING THE REAR COUNTERWEIGHT PINS IN, CRACKING AND FALLING OUT OF PLACE. ONCE PLATE HAS FAILED AND FALLEN OUT OF POSITION, THE COUNTERWEIGHT PIN IS FREE TO DRIFT OUT AND MAKE CONTACT WITH TSDR 2009FA0000220Relay · intermittentPILOT REPORTED AFTER PUTTING THE GEAR SELECTOR IN THE UP POSITION, THE GEAR WOULD NOT RETRACT. ON TROUBLESHOOTING, THE MECHANIC CYCLED GEAR SEVERAL TIMES AND GOT GEAR RETRACTION TO FAIL. REPLACED RELAY WITH NEW IAW DATE CODE MFD RW 0734. NO RECOMMENDATIONSSDR 2009FA0000094Fuel Control · faultyPILOT REPORTED ENGINE QUIT WHEN EXITING RUNWAY. UPON TROUBLESHOOTING, MECHANIC FOUND FCU HAD A ROUGH SPOT WHEN MOVING FUEL CONTROL ARM. FCU WAS REPLACED AND RUN-UP WAS PERFORMED AND OPS CHECK GOOD. NO RECOMMENDATIONS AT THIS TIME. (K)SDR 2009FA0000062Relay · intermittentPILOT REPORTED AFTER PUTTING THE GEAR SELECTOR IN THE DOWN POSITION THE GEAR WOULDN`T EXTEND, AFTER CYCLING GEAR SELECTOR GEAR WENT DOWN, ACFT RETURNED TO BASE. ON TROUBLESHOOTING THE MECHANIC CYCLED GEAR SEVERAL TIMES AND WAS UNABLE TO FAIL, THIS WAS A REPEASDR 2009FA0000025Metering Unit · malfunctionedWHILE ON A TRAINING MISSION, THE PILOT NOTICED THE FUEL FLOW WAS 18 GPH DURING CLIMB, PILOT REPORTED FUEL FLOW WAS NORMAL ON TAKEOFF. ON TROUBLESHOOTING, THE MX FOUND THE ARM ON THE MIXTURE SIDE WAS VERY ROUGH. FUEL METERING UNIT WAS REPLACED AND RUN-UP WAS SDR 2009FA0000026Pump · low pressurePILOT REPORTED INSTRUMENT AIR PRESSURE LOW AT IDLE ON RUN UP. ON TROUBLESHOOTING, THE MECHANIC DETERMINED THE AIR PUMP WAS NOT PRODUCING ENOUGH PRESSURE AT IDLE. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME. (K)SDR 2008FA0000856Relay · intermittentPILOT REPORTED AFTER PUTTING THE GEAR SELECTOR IN THE UP POSITION. THE GEAR FAILED TO RETRACT, 3-4 MINUTES LATER THE PILOT REPORTED THE GEAR CAME UP ON ITS OWN. PILOT THEN PUT THE GEAR IN THE DOWN POSITION AND RETURNED TO BASE. PROBABLE CAUSE AT THIS TIME USDR 2008FA0000865Rod · bentON LANDING, PILOT OBSERVED THREE GREEN LIGHTS. ON TOUCHDOWN AND ROLL OUT NOSE GEAR COLLAPSED INTO NOSE GEAR WHEEL WELL. UPON INVESTIGATION GEAR TRANSMISSION WAS DOWN AND LOCKED. NOSE GEAR ROD END BENT FWD SIDE OF AFT RETRACT ROD. NOSE GEAR ROD END CAN BE ASDR 2008FA0000487Bulkhead · crackedPROPELLER SPINNER BULKHEAD CRACKING BETWEEN ATTACH BOLT HOLES IN (2) PLACES. CRACK COULD BE INDUCED FROM VIBRATION. INSPECT VISUALLY EVERY PRE-FLIGHT. A BETTER HEAT TREATING PROCESS MAY STRENGTHEN THE BULKHEAD AND REDUCE THE CRACKING FROM VIBRATION. (K)SDR 2007FA0001089Rib · crackedAT ANNUAL INSPECTION, FOUND RT FLAP ROD ATTACH POINT RIB CRACKED. (K)SDR 2007FA0000955Cylinder Head · separatedIN-FLIGHT NR 2 CYLINDER HEAD SEPARATED FROM CYLINDER BASE AT TOP OF SLEEVE. PUSHRODS AND TUBES BENT. EXHAUST MANIFOLD BENT. NOZZLE ASSEMBLY DAMAGED. (K)SDR CA070523001Line · fractured(CAN) OIL PRESSURE LINE FRACTURED AT FIREWALL CAUSING AN OIL LEAK ON THE INSIDE OF THE FIREWALL. LINE APPEARS TO BE HARD FROM AGE. AIRCRAFT LANDED WITHOUT ANY FURTHER PROBLEMS. (TC NR 20070523001)SDR 2007FA0000391Magneto · failedDURING NORMAL FLIGHT, VFR CONDITIONS, LT MAGNETO FAILED TO CONTINUE FIRING. AC LANDED WITHOUT INCIDENT. UPON TROUBLESHOOTING LT MAGNETO FOUND TO ONLY FIRE ON ONE LEAD. MAGNETO REPLACED WITH NEW UNIT. DEFECTIVE MAGNETO FOUND TO HAVE LOOSE PARTS RATTLING INSSDR XGN2007F00019Cylinder · crackedCRACKED CYLINDER HEADS. (K)SDR XGN2007F00017Cylinder · crackedCRACKED CYLINDER HEADS. (K)SDR XGN2007F00003Cylinder Head · crackedCRACKED CYLINDER HEADS. (K)SDR XGN2007F00002Cylinder Head · crackedCRACKED CYLINDER HEADS. (K)SDR 2006FA0000913Shaft · shearedPILOT REPORTED INSTRUMENT AIR PRESSURE WENT TO -0- IN FLIGHT, PILOT THEN SELECTED STANDBY PUMP AND RETURNED TO BASE. UPON TROUBLESHOOTING, THE MECHANIC REMOVED THE AIR PUMP AND FOUND THE SHAFT WAS SHEARED. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME.
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