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 = '2422' 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 = '2422' 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 FDEA201501300391Latch · wornADG DEPLOYED DURING CLIMB OUT. FLIGHT CONTINUED TO DESTINATION. VERIFIED DOOR LINK AND ADG DOWN POSITION ARE CORRECTLY ADJUSTED IAW AMM 24-25-01-5. OPS TEST FOR ADG SNUBBER CARRIED OUT AND TESTED NORMALLY IAW AMM 24-25-04-2.SDR FDEA201501300396Adg · unwanted deployAPPROXIMATELY 10 MIN AFTER TAKEOFF, ADG AUTOMATICALLY DEPLOYED ON ITS OWN. FOLLOWED MTSI 24-25 7243 DISCONNECTED RELEASE CABLE & ADG DOOR LINKAGE, THEN INSPECTED RELEASE CABLE FOR ROUTING & BINDING, NO DEFECT NOTED. INSPECTED ADG & LATCH MECHANISM FOR WEAR OSDR X3MY2015FA0000006Coupling · failedFOUND THAT IT WOULD TAKE 3-5 MINUTES OF RUNNING BEFORE THE ALTERNATOR WOULD COME ONLINE. AT THAT POINT THE VOLTAGE OF 28.6-28.7 V. CHANGING THE REGULATOR DID NOT AFFECT THE SYMPTOMS AND ONCE THE ENGINE WAS WARM ALL SEQUENTIAL STARTS WERE NORMAL. SUSPECTED TSDR RU3A20141120042Relay · faultyINVERTER FAILURE MASTER CAUTION & FLASHING INDICATORS ILLUMINATED 3 DAYS IN A ROW. AFTER FIRST FAILURE PERFORMED OPERATION TEST OF INVERTERS UNDER CART & UNDER ENG POWER. NO DEFECTS SAME FAILURE THE NEXT DAY 15 MIN INTO FLIGHT. FOUND AUXILIARY CONNECTOR LOOSSDR 2014FA0000614Inverter · leakingAIRCRAFT WAS POWERED BY POWER CART AND MISSION SYSTEMS CHECK WAS IN PROGRESS. SMOKE SUDDENLY APPEARED IN CABIN, SOURCE FOUND IN REAR AVIONICS RACK INSTALLED IN BAGGAGE COMPARTMENT. NOTE: THIS IS NOT A NORMAL AIRCRAFT CONFIGURATION, THIS IS A GOVERNMENT ACFT, SDR 2014FA0000612Alternator · failedALTERNATOR FAILED CAUSING ENGINE TO QUIT. PILOT MADE OFF AIRPORT LANDING, FLIPPING ACFT OVER, DUE TO SOYBEAN PLANTS GETTING CAUGHT IN AIRCRAFT BRAKES.SDR CA140908016Inverter · failed(CAN) ACFT DEPARTED AND A FEW MINUTES INTO THE FLIGHT REQUESTED TO RETURN TO THE AIRPORT DUE TO AN AC BUS FAILURE, RESULTING IN SOME INSTRUMENT FAILURES. NO EMERGENCY OR ASSISTANCE REQUIRED AND THE ACFT LANDED WITHOUT INCIDENT. AFTER THE ACFT LANDED MAINTENASDR HNAA2014082200246Inverter · odorINVERTERS, FISH ODOR ON FLIGHT DECK. R & R SECONDARY INVERTER IAW MM 24-22-00. OPS CHECKED GOOD AT THIS TIME.SDR ERAA20140050Inverter · failedDURING PREFLIGHT WITH ENGS COLD 1ST OFFICER NOTED ELEC SMOKE ON THE FLIGHT DECK & HEARD 115 VOLT BUSS TIE CB POP. FOUND SECONDARY INVERTER BURNT UP. REPLACED INVERTER & GND TESTED GOOD.SDR O2GA2014080482201Static Inverter · defectiveSMOKE IN COCKPIT & CABIN DURING FLIGHT. CREW USED OXYGEN MASK DURING LANDING AS PRECAUTION. LANDING WAS UNEVENTFUL. TROUBLE SHOT THE DISCREPANCY TO A FAULTY STATIC INVERTER IN AFT CABIN. STATIC INVERTER WAS REPLACED. OPERATIONS CHECKED OK & ACFT WAS RETURSDR CA140731015Inverter · malfunctioned(CAN) INVERTER FAILED IN CRUISE, SLIGHT SMELL OF BURNING ODOUR, FLIGHT CONTINUED ON USING THE ALTERNATE INVERTER. SECONDARY INVERTER REPLACED BUT FOUND PARALLELING CONTROL BOX ALSO BURNT. PARALLELING CONTROL BOX REPLACED AND GROUND TESTED SERVICEABLE.SDR SWAA2014062429338Inverter · inoperativeDIVERSION, STANDBY POWER OFF LIGHT ILLUMINATED INFLIGHT. R & R STATIC INVERTER IAW MM.SDR HDNA2014F00129Static Inverter · malfunctionedIN CRUISE FLIGHT, THE ACFT ROLLED RT AND LT UN-COMMANDED ABOUT 5 PERCENT. THE INVERTER CAUTION LIGHT ALSO ILLUMINATED. PILOT MADE A PRECAUTIONARY LANDING. SYSTEM AFFECTED WAS THE ROLL SAS BECAUSE OF THE INVERTER FAILURE.SDR HNAA2014060900173Inverter · odorPASSENGER CABIN HAS STRONG UNDESIRABLE ODOR. R & R SECONDAY INVERTER IAW MM 24-22-01. OPS CHECKED GOOD. NO NOTICEABLE ODOR. OK FOR SERVICE.SDR 2014F00085Alternator · crackedWHILE CLIMBING THROUGH, FL 140, THE FLIGHT CREW REPORTED LOSS OF OIL PRESSURE ON THE RT ENGINE. THEY IMMEDIATELY FEATHERED THEN SHUTDOWN THE ENGINE AND RETURNED TO THE DEPARTURE AIRPORT. THE MAINTENANCE REPAIR TEAM DISCOVERED THE RT ENGINE'S ALTERNATOR HALVESDR HNAA2014040400122Inverter · failedSTRONG FISH ODOR IN COCKPIT. INSPECTED PRIMARY, SECONDARY AND AUX INVERTER. NO DEFECTS NOTED. OPS CHCKED INVERTERS. NO ODOR, OPS CHECKED GOOD.SDR HNAA2014040400120Inverter · odorSTRONG FISH ODOR IN COCKPIT, THROUGH ENTIRE FLIGHT. R & R SECONDARY INVERTER IAW MM 24-22-00. OPS CHECKED GOOD.SDR 9JLA2014040907167Inverter · failedCREW REPORTED THAT THE NR 1 INVERTER FAILED IN FLIGHT. THE FAILED INVERTER WAS REMOVED PN 140-380010-7, SN SG1347 & A REPAIRED INVERTER WAS INSTALLED.SDR HNAA2014021200038Inverter · inoperativeDURING BOARDING, SMOKE ODOR INDICATED ON FLIGHT DECK WITH POSSIBLE CIRCUIT BREAKER TRIPPED, IMEDIATELY FOLLOWED BY SMOKE BEHIND CAPTAIN`S SEAT AND FLASH OF POSSIBLE SECONDARY INVERTER CAUTION LIGHT. FOUND AUXILARY INVERTER INOPERATIVE. R & R INVERTER. OPS CSDR CA140211013Cotter Pin · failed(CAN) COTTER PIN HOLDING NUT ON TO GEAR DRIVE FAILED.SDR WX0A071825Static Inverter · faultyEMERGENCY POWER TEST FAILED. CAPTAIN`S PFD, ND, AIRSPEED & ALTIMETER REMAIN OFF. FIRST OFFICER`S FUNCTIONS ON EMERGENCY POWER. R & R STATIC INVERTER IAW AMM 24-23-01, OPERATIONS CHECKED GOOD.SDR 9JLA2014012407272Inverter · failedTHE FLIGHT CREW REPORTED THAT THE NR 1 INVERTER FAILED IN FLIGHT. TROUBLESHOOTING IDENTIFIED THE INVERTER AS DEFECTIVE. THE INVERTER WAS REMOVED & AN OVERHAULED INVERTER WAS INSTALLED IAW AMM 24-20-00. FUNCTIONAL CHECKS SATISFACTORY.SDR UIEA2013122700617Inverter · faultySTATUS MESSAGE STANDBY INVERTER DISPLAY. R & R STATIC INVERTER IAW AMM 24-33-05 TESTED OK.SDR SWIA201335459Circuit Breaker · failedON CLIMB OUT NR 2 INVERTER INOPERATIVE LIGHT ILLUMINATED, RETURN TO FIELD. FLT 1352 REPLACED CIRCUIT BREAKER 0414 IAW AMM 0-13-03.SDR CALA2013120293344Generator · faultyAPU ELEC NOT AVAILABLE, PNEUMATICS OK. REPLACED APU GEN IAW MM. RAN APU, OPERATIONS CHECKED GOOD.SDR DALA13064435653Static Inverter · odorCREW REPORTED FUMES AND AN ELECTRICAL ODOR IN THE CABIN AND COCKPIT JUST PRIOR TO LANDING WITH ASSOCIATED STANDBY INVERTER EICAS MESSAGE. MAINTENANCE FOUND THE STANDBY INVERTER TO BE THE SOURCE OF THE ODOR. REPLACED INVERTER IAW AMM 24-33-03. CHECKED OK.SDR SWIA201335460Relay · failedON TAKEOFF THE NR 2 INVERTER INOPERATIVE LIGHT ILLUMINATED, RETURNED TO FIELD. FLT 6286 REPLACED INVERTER 2 RELAYS K0008 & K0004 IAW EMB MM.SDR CA131118019Control Unit · failed(CAN) DURING A ROUTINE FLIGHT THE PILOT NOTICED THE THE STANDBY ALTERNATOR HAD FAILED. THE FLIGHT CONTINUED WITH OUT INCIDENT. MAINTENANCE REPLACED THE ACU AND THE SYSTEM WAS GROUND FUNCTION CHECKED SERVICEABLE.SDR CALA2013111292856Inverter · faultyIAW EQ3333 STATIC INVERTER DOES NOT TEST. REPLACED STATIC INVERTER, OPERATIONS NORMAL, TESTED NORMAL.SDR CA131001001Bolt · sheared(CAN) DURING A NIGHT WALKAROUND THE PILOT NOTICED THAT THE ALTERNATOR BELT APPEARED TO BE TWISTED. MAINTENANCE FOUND THAT THE ALTERNATOR LOWER PIVOT BOLT HAD SHEARED HALFWAY IN THE THREADS, CAUSING THE BOLT TO BACK OUT OF THE PIVOT AND COME IN CONTACT WITH THESDR HNAA2013093000522Inverter · odorSTRONG FISH ODOR IN COCKPIT. R & R PRIMARY INVERTER 400HZ IAW 24-22-01, OPS CHECKED GOOD. RETURNED TO SERVICE.SDR BSYR20120913060Alternator · failedAFTER DEPARTURE, PILOT DISCOVERED ALTERNATOR FAILURE. PILOT RETURNED AND LANDED SAFELY AT DEPARTURE. OPENSDR 9JLA2013092604677Inverter · failedCREW REPORTED NR 1 INVERTER FAILED AFTER ENGINE START DURING AVIONICS POWER UP. TROUBLESHOT & FOUND NR 1 INVERTER DEFECTIVE. INVERTER REMOVED AND REPLACED WITH A REPAIRED UNIT. OPS CHECKED SATISFACTORY.SDR CALA2013090591000Inverter · no testSTATIC INVERTER TR WILL NOT TEST. REPLACED STATIC INVERTER & STATIC INVERTER CONTACTOR 2XB IAW MM 24-28-51 & MM 24-28-55. ALSO REPLACED RELAYS 30XU1 & 30 XU2. REPLACED RELAY (7XB), RELAY (13XC), RELAY (14XC), & CNTOR- AC ESS BUS SWITCHING (15- XE). REPLACSDR CALA2013090290911Unknown · faultySTATIC INVERTER WILL NOT TEST. REPLACED STATIC INVERTER & STATIC INVERTER CONTACTOR 2XB PER MM 24-28-51 & MM 24-28- 55 WITH NO HELP. ALSO REPLACED RELAYS 30XU1 & 30XU2 WITH NO HELP. REPLACED RELAY 7XB, 13XC, 14XC, & CNTOR- AC ESS BUS SWITCHING (15- XE), NO SDR 2013FA0000575Belt · failedALTERNATOR BELT WILL NOT HOLD TENSION. WILL STRETCH FROM A PROPER TENSION IN A SHORT PERIOD OF TIME; 10-25 HOURS.SDR CA130610003Inverter · failed(CAN) WHILE IN THE HOLDING PATTERN OVER, CREW RECEIVED A PRIMARY INVERTER MALFUNCTION INDICATION AND SMOKE APPEARED IN THE COCKPIT. THE CREW DONNED THEIR OXYGEN MASKS, WORKED THE RELEVANT CHECKLISTS AND NOTICED AFTER ABOUT 1-2 MINUTES THAT THE SMOKE WAS SUBSISDR CA130522008Pulley · loose(CAN) DURING TAXI A SQUEEL WAS HEARD FROM THE ENGINE. AFTER SHUTDOWN PILOT OBSERVED THAT PULLY WAS LOOSE ON FRONT ALTERNATOR, 2. THE PULLY HAD BEEN RUBBING ON ALTERNATOR CASE, CAUSING THE NOISE. THE ALTERNATOR BELT WAS REMOVED AND ACFT FLEW BACK VFR TO BASESDR 39LA2013050600004Inverter · burnedPRIMARY INVERTER LIGHT WILL NOT EXTINGUISH AND ACCOMPANIED BY BAD ODOR. PERFORMED T/S OF PRI INVERTER SYS, FOUND PRIMARY INVERTER SHORTED/BURNED, R & R PRI INVERTER ASSY PN OFF DH-1030-24-600-CSIIB, SN OFF AB3130-S8, PN ON DH-1030-24-600-CSIIB, SN ON AB3023-SSDR ERAA201304181032Inverter · inoperativeSECOND INVERTER FAILED FOLLOWED BY PRIMARY INVERTER. REPLACED BOTH INVERTERS AND PARALLEL CONTROL AND 400HZ CONTROL. SYSTEM OPS CHECKS GOOD ON GROUND.SDR CA130327004Inverter · failed(CAN) DURING A TRAINING FLIGHT THE INVERTER FAILURE NR 2 WARNING LIGHT CAME ON. AT APPROXIMATELY THE SAME TIME SMOKE WAS DETECTED IN THE CABIN. EMERGENCY WAS DEALT WITH IAW THE CHECK LIST. AFTER LANDING AT MAINTENANCE FACILITY, THE AME QUICKLY DETERMINED THSDR JJBA20130110004Inverter · faultedSHORTLY AFTER TAKEOFF, THE CREW OBSERVED THE AUX INVERTER LIGHT HAD ILLUMINATED. THE CREW ALSO REPORTED DETECTING FUMES IN THE COCKPIT. THE CREW DECLARED AND EMERGENCY AND MADE AN UNSCHEDULED LANDING. THE GROUND MX CREW R & R THE AUX INVERTER. ALL OPS CHECSDR HNAA2013010900001Inverter · failedOILY BURNING SMELL AROUND FORWARD CABIN AREA AND FLIGHT DECK. FOUND AUX INVERTER FAILED. R & R AUX INVERTER. OPS CHECKED GOOD.SDR DXTA2013010405229Inverter · failedAFTER SHUTDOWN DETECTED A VERY STRONG ELECTRICAL BURNING ODOR FROM THE AFT CLOSET INSIDE THE ELECTRICAL BOX. NO FIRE. TROUBLESHOT ELECTRICAL BURNING ODOR TO THE 110V AC INVERTER IN AFT CLOSET. R & R INVERTER WITH AN OVERHAULED UNIT IAW MM 25-40-03. OPS CHECKSDR 9JLA2013030504421Inverter · defectiveCREW REPORTED THAT THE AC OUTLETS IN THE CABIN WERE INOPERATIVE. REMOVED THE DEFECTIVE AC INVERTER, SN 294 AND INSTALLED A REPAIRED UNIT. FAILED AFTER 7.6 HRS OF OPERATIONS .SDR 9JLA2013020504421Inverter · failedTHE CREW REPORTED THAT THE CABIN AC OUTLETS ARE INOPERATIVE. THE INVERTER FAILED AFTER ONLY 8 HRS OF OPERATION. THE DEFECTIVE INVERTER PN SS-200, SN 294 WAS REMOVED. A REPAIRED INVERTER WAS INSTALLED. REF: MM 24-21-01.SDR FDEA201212294399Warning Light · illuminatedRECEIVED LEVEL 1 "BUSS R EMER AC OFF" ALERT, 2 HOURS INTO FLIGHT. SELECT FADEC ALT,TANK 2 AFT PUMP LO, SINGLE LAND, FO PITOT HEAT, GPWS FAULT, SEL ALT CADC. FAILURE WENT AWAY AND ALL SYS NORMAL AFTER APPROX 20 MIN, DIVERTED AND LANDED WITHOUT INCIDENT. SDR 9JLA2013011803542Inverter · defectiveTHE CREW REPORTED THAT NR 2 INVERTER FAILED DURING FLIGHT. TROUBLESHOOTING IDENTIFIED THE NR 2 INVERTER DEFECTIVE. THE DEFECTIVE INVERTER WAS REMOVED AND A REPAIRED UNIT WAS INSTALLED. FUNCTIONAL CHECKED SATISFACTORY. ACFT WAS RETURNED TO SERVICE.SDR 2012FA0000791Inverter · failedNR 1 INVERTER FAILED ON CLIMBOUT. LEFT MICROPHONE STUCK IN TRANSMIT POSTION. PILOT DESENDED BELOW 18,0000 AND SQUAWKED 7600. PILOT REPORTED HSI EFIS SCREEN FAILED. PILOTS SIDE HSI WAS SWITCHED TO DISPLAY ON MFD. LANDING WAS MADE UNEVENTFUL. INSTALLED INVESDR UALA2012110506351Inverter · faultyNO LAND 3 EICAS ON FINAL AT APPROX 1500 AGL. REPLACED STATIC INVERTER PER MM. (ACTION). REPLACED STATIC INVERTER PER MM. AIRCRAFT IS IN CAT 111 STATUS.
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