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 jasc_code = '2424' 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 jasc_code = '2424' 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 UALA2011061402932Gcu · faultyELEC GEN OFF R RIGHT GENERATOR CONTROL BREAKER (GCB) OPEN OR GENERATOR CONTROL SWITCH OFF, AND ENGINE NOT SHUT DOWN. ADVISORY. CREW COMMENTS: ATTEMPTED 1 RESET, UNSUCCESSFUL. APU NOW RUNNING FOR ELECTRICS. MSG-2431632 LATCHD TA MODE. REPLACED GCU PER MMSDR UALA2011060902851Gcu · faultyLEFT GEN TRIPPED OFF START OF TAKEOFF. RAN CHECKLIST AND DID NOT RESET. REPLACED LT ENG GCU. RAN BOTH ENGINES, SYSTEM WORKED NORMAL. REPLACED LT GEN TIE BREAKER. BPCU BITE CHECK HAD LT GEN DP TRIP MAIN BUS-OVERLAP ZONE MSG TWICE. GCU WAS REPLACED ON THE SDR UALA2011060702788Gcu · faultyELEC GEN SYS L FAULTS. DUE TO RECENT HISTORY OF ELEC GEN SYS L FAULT, ACP FIM TASK 24-23-837. ACCOMPLISH FIM TASK INCLUDING WIRING CKS. INCLUDE OHMS AND CONTINUITY READINGS IN SIGNOFF. IF NO FAULTS ARE FOUND REPLACE THE RIGHT GCB (566-0549) PER AMM THE LESDR TRBA2011068Gcu · inoperativeON FLIGHT 4739 WHILE ON THE GROUND BOTH ENGINES FEATHERED WHEN SHUT DOWN. NR 1 ENGINE AND NR 2 DC GEN FAULTED, AN ELECTRICAL BURNING ODOR FILLED THE COCKPIT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED NR 2 GENERATOR CONTROL UNIT ATR 72 JICSDR C2XA11RI088Gcu · inoperativeFLIGHT 2808 - EWR - FLIGHT CREW REPORTED THAT ON APU START RECEIVED APU FIRE INDICATION THAT CLEARED ITSELF UPON RE-START - APU RE-STARTED BUT ZERO AMPS. EWR MX PERFORMED FIRE DETECTION ON APU - NO FAULTS FOUND. MX REMOVED AND REPLACED APU GCU AND PERFORMED SDR YENA20110520257Gcu · failedFLT 47 JFK-FLL, AIR RETURN BACK TO JFK- GEN 2 FAULT ON ECAM AFTER TAKEOFF AT 5000FT 250 KNOTS. CYCLE PUSH BUTTON GEN 2, NEVER CAME BACK ONLINE. REMOVED AND REPLACED ENGINE NR 2 GCU IAW AMM 24-22-34. OPS CHECK OK.SDR CALA2011051200361Gcu · malfunctionedAFTER NR 2 ENG START IN AUS, THE APU GEN DISCONNECTED FROM BOTH B USES WHEN NR 2 ENG GEN CONNECTED. APU GEN WOULD NOT CONNECT TO ANY BUS AFTER THAT. THERE WAS A STRONG ELECTRICAL ODOR DURING T HIS EVENT. T/S AND FOUND APU GCU AT FAULT, WITH A GCU FAULT LIGHSDR UALA2011051102336Gcu · faultyAPU FIELD OFF LT IS ON. WHEN GND PWR WAS DISCONNECTED PLANE WENT DARK. HMG VERIFIED TO OP NORMAL AS PER MEL. NEED TO REPLACE APU GENERATOR PER MM. NEED LEAK CHECK AND SYS TEST PER MM. REPLACED GENERATOR PER MM. OPS CHECK OF APU GEN NORMAL. REPLACED GCU SDR LR7A2011040600173Volt Regulator · overheatedON CLIMB OUT, FLIGHT CREW NOTED SMOKE COMING FROM THE NR 3 VOLTAGE REGULATOR. ISOLATED IAW QRH, RETURNED TO DEPARTURE AND LANDED. REPAIR ACCOMPLISHED BY REPLACING NR 3 GENERATOR, VOLTAGE REGULATOR, AND GENERATOR CONTROL PANEL IAW LOCKHEED SMP581 24-20.SDR UALA2011032401400Gcu · faultyAPU NO GO ON LINE WITH GENERATORS. AIR OUTPUT OK. NO TIME TO TS. REPLACED APU GEN CONTROL UNIT PER AMM. TEST OK, OPERATIONAL CHECK OKAY.SDR UALA2011032101355Gcu · inoperativeCREW REPORTS APU GEN WILL NOT COME ON LINE. APU GEN INOP PER MEL. REPLACED GENERATOR CONTROL UNIT PER MM. RAN ENGINE. OPS CHECK OK.SDR YENA20110213196Gcu · failedFLT 523 EWR-MCO, CREW DECLARED EMERGENCY DUE TO DURING CRUISE ELEC MALFUNCTIONS CAUSED NUMEROUS FAULTS INCLUDING SEC 3, FAC 2, F/O PFD, F/O ND, LWR ECAM, COCKPIT DOOR, CABIN LIGHTING, LIVE TV. ALL OF THESE ITEMS FLICKERED ON/OFF NUMEROUS TIMES. THE ECAM ACTISDR A6WA201140063Gcu · malfunctionedAC1 AUTOTRANSFER AND AC2 AUTOTRANSFER CAUTION MSG`S ON GROUND. WILL NOT ACCEPT EXT AC PWR. WILL NOT ACCEPT GEN PWR. MAIN GEN`S WON`T SUPPLY OPPOSITE SIDE. R & R GCU NR 3 IAW AMM 24-11-07. PERFORMED OPS CHECK IAW 24-22-01. OPS CK GOOD AT THIS TIME.SDR CALA2011052000374Gcu · malfunctionedDURING CLIMBOUT LEVEL AT 10000FT 300KTS CAPTS EFIS SCREENS BEGAN TO FLICKER ACCOMPANIED BY A CASCADE OF LIGHTS EICAS MSGS AND THEN A STRONG ELECTRICAL BURNING SMELL/SMOKE STRONGEST ON CAPTS SIDE. OVERWEIGHT APPCH AND TOUCHDOWN. BRAKES OK CREW EXPERIENCED A LSDR AALA20100929JFK01Gcu · failedJFK - INFLIGHT DFW-LHR. CREW REPORTED RIGHT ENGINE GENERATOR FAILED IN FLIGHT. EMERGENCY DECLARED DIVERTED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT GENERATOR CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR A6WA201040703Gcu · malfunctionedWHILE IN FLT, AC 1 AUTO TRANSFER AC BUS 1 GEN 1 OFF AND LT WINDOW HEAT CAUTION MSG ILLUMINATED ON ED1 CW QRH FLAP .5 SPEED ON ED2 IN FLAP SELECTION OTHER AS MSG. R & R GEN CONTROL UNIT.SDR AXSA996FE8/18/10Control Unit · inoperativeFLIGHT WIG046A DEPARTED MHT-MVY NORMALLY. WHILE CLIMBING THRU 4500 FEET THE PILOT NOTED ELECTRICAL FUMES. THE PILOT DID NOT NOTICE SMOKE BUT ELECTED TO RETURN TO MHT AS A PRECAUTION AND LANDED WITHOUT INCIDENT. MAINTENANCE EVALUATED THE AIRCRAFT AND DETERMISDR AALA20100807TUL02Gcu · inoperativeMEM - CREW REPORTED RIGHT GENERATOR FAILED ALONG WITH CROSS TIE LOCK-OUT DURING APPROACH. EMERGENCY DECLARED LANDED MEM WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT GENERATOR CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR AALA20100808TUL01Gcu · inoperativeSLC - INFLIGHT SEA-DFW. CREW REPORTED ELECTRICAL POWER INTERRUPTIONS AND AUXILIARY POWER UNIT FAULT LOW OIL PRESSURE. EMERGENCY DECLARED, DIVERTED SLC LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED GENERATOR CONTROL UNIT. SYSTEM GROUND CSDR C2XA10CL127Gcu · faultyCLE FLT 5839 THE CREW REPORTED AN APU GENERATOR OFF BUS MESSAGE ON TAKEOFF. MAINTENANCE REPLACED THE APU GENERATOR CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD.SDR UALA2010072302627Gcu · faultyLT & RT ENG GEN FAILURE, RTFL. RT GENERATOR TRIPPED OFF LINE AND UNABLE TO RESET. REPLACED GCU(S) AND OPERATIONS CHECK GOOD IAW MM.SDR USAA20100716BB042Circuit Board · faultedPHL FLT 740 EN ROUTE SJU TO PHL. DURING APPROACH, RECEIVED "L ENG LP PUMP" MESSAGE. THE LEFT ENGINE UNSPOOLED AND THE LEFT ENGINE OIL PRESSURE WENT TO 16 PSI AND WITHIN 45 SECONDS CAME BACK TO ALL NORMAL INDICATIONS. THE FLIGHT LANDED WITHOUT FURTHER INCISDR MZZA2010063000314Gcu · failedELECTRICAL SOURCE OFF LIGHT AND DRIVE LIGHT ON NR 2 GEN SMELL OF ACRID, SMOKE POSSIBLE OIL OR ELECTRICAL SOURCE. PERFORMED INSP PER AMM 05-51-26. FOUND NR 2 GCU BURNED OUT. CHECKED WIRING & NO EVIDENCE OF HEAT DAMAGED. REPLACED NR 2 GCU AND PERFORMED TEST SDR YENA20100623086Gcu · failedFLT 35 JFK-PBI (ON GROUND) OPERATIONAL CHECK OF EMERGENCY GENERATION SYSTEM FAILED ON WEEKLY CHECK. REMOVED AND REPLACED GCU 1 XE IAW AMM 24-24-34-04. OPS CHECK NORMAL.SDR AALA20100603DFW04Gcu · faultyDFW - CREW REPORTED MULTIPLE ELECTRICAL PROBLEMS. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED GENERATOR CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR UALA2010051201618Gcu · failedBOTH UTILITY BUSSES SHED WHEN THROTTLES ADVANCED FOR TAKEOFF. REPLACED RIGHT GCU AND RELAY K10109 PER MM. TOOK ACFT OFF GATE FOR ASSURANCE RUN AND CONFIGURED FOR TAKEOFF. ADVANCED THROTTLES TO TAKEOFF POWER SEVERAL TIMES, OPS CHECKS NORMAL.SDR UALA2009112303654Gcu · malfunctionedRT GEN FIELD MAN RESET LIGHT IS ON. REPLACED GCU, OPS CHECKS GOOD.SDR CALA2009112000685Gcu · malfunctionedLT AND RT UTILITY BUSES TRIPPED FOR ABOUT 3-4 SECONDS IN FLIGHT. ALSO LT AND RT UTILITY BUS MESSAGE APPEARED ON EICAS. UTILITY BUSES RESET THEMSELVES. GALLEY POWER AND VIDEO TURNED OFF. T/S PER MM 24-22-00, REMOVED AND REPLACED LT AND RT GCU AND BPCU AS PESDR 2009FA0000824Suppressor · failedWHILE RETURNING FROM A SALES DEMONSTRATION, PILOT REPORTED SMOKE IN THE COCKPIT AND LANDED. UPON FURTHER INVESTIGATION, FOUND THAT VOLTAGE SUPPRESSOR D4 (REF WIRING DIAGRAM 91-34-20 FIG 4 SHEET 5 OF 5) HAD FAILED. SUPPRESSOR D3 (MOUNTED DIRECTLY NEXT TO D4) SDR UALA2009100703152Gcu · malfunctionedAT ABOUT 500FT' ON FINAL APPROACH L GEN TRIPPED OFF LINE. BITE TEST OF BPCU SHOWED "IDG HIGH RISE TEMP" AND "RPL GCU (D9)". MSGS CALL FOR RPL OF GCU. REPLACED LEFT ENG GCU. IDG OIL LEVEL WAS OK. IDG ELEC CONNECTOR WAS CLEANED. BITE TEST WAS GOOD AND MSGSSDR UALA2009100203094Gcu · malfunctionedEICAS MSG L GEN OFF DISPLAYED AT FL 240. OPERATED NORMAL AFTER RESET. REMOVED AND REPLACED LEFT GENERATOR CONTROL UNIT AND TEST PERFORMED. FOUND GOOD.SDR UALA2009092503027Gcu · faultyELEC GEN DRIVE L LEFT IDG FAULT (LOW INTERNAL OIL PRESSURE). REPLACED LT GCU AND SERVICED LT IDG, RAN ENGINE. GEN OPS CHECK OKAY. FOUND GEN DRIVE LIGHT INOPERATIVE. L IDG REPLACEMENT DEFERRED. HAVE ALL PARTS IN HAND, REMOVING IDG AT THIS TIME. REPLACED ISDR DL76L091471Gcu · failedATB RIGHT GEN OFF LIGHT STARTED APU OK, BUT WILL NOT PICKUP RIGHT BUS. REPLACED RIGHT GCU AND BPCU RUN-UP AND OPS NORMAL. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK.SDR 2009F00067Gcu · malfunctionedLEFT GEN CAUTION LIGHT ON DURING T/O ROLL. ABORTED T/O. RESET GEN AS PER CHECKLIST. GOOD VOLTAGE OBSERVED BUT GEN WOULD NOT RESET TO ON. ON POSTFLIGHT OBSERVED FLASHING SYS LIGHT ON LT GCU IN APU COMPARTMENT.SDR UALA2009083102705Gcu · malfunctionedLEFT IDG FAULT (LOW INTERNAL OIL PRESSURE). MESSAGE ILLUMINATED LEAVING FL260. APU STARTED NORMALLY. REPLACED GCU AND CORE WIRE HARNESS W0623. RAN ENGINE, ALL FUNCTIONS NORMAL.SDR UALA2009070201907Gcu · faultyLOST BOTH GENERATORS. RTFL. RMV'D & RPL'D NR 1 & NR 2 GCU(S) DUE TO RECENT LOSS OF POWER. CKS OK WITH CFDS. RAN ENG, OPS OKAY.SDR UALA2009060501617Gcu · inoperativeELEC GEN SYS L STATUS MESSAGE. FOLLOWED BY GALLEY LOAD SHED INDICATIONS. BUS TIE SWITCH DID NOT INDICATE ISOLATED HOWEVER NO CONNECTION ON SYNOPTIC PAGE TO BUS TIE. APU GEN & BUG ALSO DID NOT INDICATE IT WAS POWERING THE L BUS. CREW CYCLED L GEN SWITCH TO SDR UALA2009050601304Gcu · malfunctionedF/A REPORT CABIN LIGHTING NO SMOKE LIGHTS F/A CALL LIGHTS AND EXIT LIGHTS FLICKERING THROUGHOUT. MAINT TEXT: SUSPECT GENERATOR MALFUNCTION. NEED BOTH ENGINE RUN TO ISOLATE SUSPECTED GENERATOR. FOUND THRESHOLD FLUORESCENT LIGHT ABOVE DOOR 1L FLICKERING, RELASDR UALA2009042001146Gcu · failedAPU INOP ELECTRICAL. UNABLE TO LOAD GENERATOR. REPLACED APU GENERATOR UNIT. OPS CHECKS GOOD. REPLACED GENERATOR CONTROL UNIT. OP CHECKS GOOD.SDR UALA2009040600982Gcu · malfunctionedDURING TOWING APU GEN FELL OF LINE, LEFT 115 VAC MAIN BUS TIE HAS UNBALANCED CURRENT. REPLACED APU GCU.SDR HNAA2009040700106Gcu · failedLEFT ALTERNATING CURRENT BUS FAILED IN FLIGHT. REMOVED AND REPLACED NR 1 ALTERNATING CURRENT GENERATOR CONTROL UNIT AND CLEANED CONNECTOR TO NR 1 ALTERNATING CURRENT GENERATOR. GROUND OPERATIONS CHECK GOOD. REFERENCE AIRCRAFT MAINTENANCE MANUAL AMM 24-21-02SDR CA090316003Volt Regulator · unserviceable(CAN) SMELL OF SMOKE WAS PRESENT IN THE COCKPIT. ALL POWER WAS SHUTOFF IN ACFT. ACFT LANDED WITHOUT 0 INCIDENT. THE AC GENERATOR VOLTAGE REGULATOR WAS FOUND DEFECTIVE. REGULATOR REPLACED AND GROUND CHECKED SERVICEABLE.SDR USAA20090224BB039Gcu · faultySTT FLT 1041 EN ROUTE STT TO CLT. DURING CLIMBOUT FROM STT, AT APPROXIMATELY 800 FEET, THE CAPTAIN'S COCKPIT INSTRUMENTS WENT BLANK. THE CREW PERFORMED A CROSS TIE RESET, AND GOT THE INSTRUMENTS MOMENTARILY OPERATING AGAIN, THEN FAILED ONCE MORE. AN EQUIPMSDR HNAA2009022300072Gcu · intermittentEMERGENCY LIGHT CAME ON DURING FLIGHT. FOUND AC GENERATOR CONTROL UNIT BAD. REMOVED AND REPLACED AC GENERATOR CONTROL UNIT ON BOTH ENGINES. REMOVED AND REPLACED FUSES 2421 F8 AND F10, OPS CHECK GOOD.SDR HNAA2008122000352Gcu · odorELECTRICAL SMELL ABOUT CABIN CIRCUIT BRAKER PANEL. INSPECT CABIN CIRCUIT BRAKER PANEL NO DEFECT FOUND. FOUND NUMBER 1 GENERATOR CONTROL UNIT BURNED SMELL. REMOVED AND REPLACE GENERATOR CONTROL UNIT AND STARTER GENERATOR REFERENCE HA 300 SEQUENCE 5. REMOVED SDR USAABB08164Gcu · loosePHX - FLT 45 PHX TO KOA. UPON ROTATION, THE LEFT AC BUS TRIPPED OFF AND COULD NOT BE RESET, OR POWERED BY ANOTHER GENERATOR. THE FLIGHT RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE BITE CHECKED THE BUS PROTECTION CONTROL UNIT (BPCU) ANDSDR UALA2008111303975Gcu · malfunctionedLEFT GENERATOR FAILURE. FLT DIVERTED. BELIEVED TO BE A POWER TRANSFER PROBLEM. REPLACED L ENG GCU. CHECKS OK ON B PCU.SDR AALA200801639Gcu · failedSTL INFLIGHT T2361/17JUN ORD TO DFW. CREW REPORTED LOSS OF RT AC BUD POWER AND RT ENGINE DRIVEN GENERATOR WOULD NOT HOLD A LOAD. LANDED STL WITHOUT INCIDENT. REPLACED GENERATOR CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)SDR 2008UALA02956Gcu · faultyELEC GEN OFF R RIGHT GENERATOR CONTROL BREAKER (GCB) OPEN OR GENERATOR CONTROL SWITCH OFF, AND ENGINE NOT SHUT DOWN. ADVISORY MSG01- NOT ACTIVE DESCENT MODE DEPENDENT; INTEGRATED DRIVE GENERATOR (R) FREQUENCY IS LOW. DB- GENERATOR CONTROL UNIT (R) MSG02- LATSDR ASAA0852826Gcu · defectiveDURING CLIMB APU GENERATOR INDICATED 16 AMPS WITH APU NOT RUNNING. REPLACED GCU GENERATOR CONTROL UNIT.
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