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 = '7600' 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 = '7600' 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 2011FA0000104Computer · failedDURING THE TAKEOFF ROLL AFTER REACHING TAKEOFF THRUST, AND AROUND 80 KIAS RECIEVED A RT ENG COMPUTER FAULT CASS MESSAGE. ABORTED TAKEOFF. RAN ABNORMAL CHECKLIST FOR FAULT AND WAS ABLE TO RESET THE RT ENGINE COMPUTER. TAXIED BACK TO TAKEOFF AGAIN. ON THE SESDR 2010FA0000931Control Cable · brokenPERFORMED NORMAL START, NOTED LOW IDLE LOW, MOVED CONDITION LEVER TO HIGH IDLE WITH NO RESPONSE FROM ENGINE, TRIED SEVERAL TIMES & HAD NO RESPONSE. PERFORMED ENGINE SHUTDOWN. MOVED CONDITION LEVER IN COCKPIT WHILE 2ND PERSON WATCHED MOVEMENT ON FCU. MOVEMENTSDR FDEA201007292721Hmu · failedAT APPROX 300 FT INSIDE OF 1 MILE, NR 1 ENG SPOOLED DOWN.NO INDICATIONS OR WARNINGS ON ECAM OR OTHERWISE ENT BY: 110437 RPT BY: 115143 30JUL10 03:18 MEM R POWERPLANT ENGR REQUESTS T/SHOOT NR 1 ENGINE PER TSM 72-00-30 FIG.108; STEPS 1-4 COMPLIED WITH. STESDR CA100601002Control Rod · damaged(CAN) DURING REPLACEMENT OF THE NR 2 MECHANICAL FUEL CONTROL (MFC), THE NR 2 ENGINE CONDITION LEVER CONTROL ROD THAT GOES TO THE MFC FROM THE NACELLE QUADRANT (REF. IPC 76-20-00, FIG 5-150, P/N 87620102-011) WAS FOUND TO BE MISSING THE SOLID RIVET AT THE TOP ESDR IPXA10659683Eec · faultyDURING ENGINE START ON NR 2 EGT DID NOT RISE. ON SECOND START WITH ENG 2 START SELECTOR IN BOTH. NORMAL START. T/S C/O IAW FIM 74-00-00 FIG, 107 SH2. R & R ENG NR 2 EEC IAW AMM 73-21-15-4 . REPLACED BOTH IGNITOR PLUGS IAW AMM 74-21-02-4. C/O TEST IAW AMM 74-SDR C2XA10IA068Switch · malfunctionedIAH - FLIGHT 2354, THE CREW REPORTED THAT THE CLIMB THRUST PUSHBUTTON WAS STUCK PUSHED IN. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PUSHBUTTON SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AISDR SWIA201023611Amplifier · malfunctionedWHILE SETTING TAKEOFF POWER THE LEFT ENGINE N1 ROLLED BACK 10-15 PERCENT. (FLT 4620) REPLACED LEFT ENGINE CONTROL AMPLIFIER P/N 5071T98P03, S/N ON LMDK2797, S/N OFF LMDK2532.SDR ASAA1057211Cdu · malfunctionedNR 2 ENG FMC CDU FAULT CODE FOUND 76 31362. THE START LEVER SIGNAL DISAGREE. LONG TERM FAULT. ON DEFERRAL.SDR ASAA1057201Unknown · malfunctionedNR 2 ENG FMC CDU FAULT CODE FOUND 76 31362. THE START LEVER SIGNAL DISAGREE. LONG TERM FAULT. ON DEFERRAL.SDR REXA200900144Amplifier · defectiveON CLIMBOUT OF KDTW THE FLIGHT CREW NOTICED THE LT N1 INDICATION ACCELERATE TO 96.7 PERCENT. THE THRUST LEVER WAS REDUCED AND THE LT N1 DECREASED, BUT FLUCTUATED 20-25 PERCENT. ALL OTHER ENGINE PARAMETERS WERE NORMAL. THE FLIGHT CREW CONTACTED ATC, REQUESTESDR HALA2009121600586Pseu · malfunctionedWITH AC CONFIGURED FOR LANDING OUT OF 1000 FT FINAL APPROACH PSEU FAIL FLASHED ON AND OFF SEVERAL TIMES, A/S FAST REF +10, AUTO THROTTLES WENT INTO LO SPEED PROTECT MODE, AND WENT FWD AUTO. REMOVED AND REPLACED PROX SENSE ELEC UNIT IAW AMM 32-41-01. RTS TEST SDR ASAA0957143Unknown · malfunctionedFOUND LONG TERM FAULT MSG 76 31361 START LEVER SIGNAL DISAGREE LEG 1 ENG NR 1. FFR SHOWS 2 FAULTS NR 1 ENGINE MSG 76 31361. ACCOMPLISHED FIM TASK 76 11 00 & INPUT MONITORING DISCRETES TESTS ON NR 1 START LEVER SEL POS SW DEU1 DEU2 GROUND VERIFICATION TEST OPSDR ASAA0957013Unknown · malfunctionedDURING ENGINE FMC CDU FAULT T/C 78273000 ENGINE NR 2 SHOWED A FAULT 76 31362. START LEVER SIGNAL DISAGREE (LONG TERM FAULT). NO FAULTS LOGGED LAST FOUR LEGS OF FLIGHTS. ACCOMPLISHED EEC TEST NO FAULTS LOGGED OPS NORMAL REF AMM TASK 73 21 00 700 804 F00. THSDR C2XA09CL107Panel · faultyEWR FLT 2609 - THE CREW REPORTED ENGINE NR 1 DEFAULTS TO T/O THRUST. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE THRUST RATING PANEL. OPERATIONAL CHECKS WERE GOOD.SDR REXA200900087Apr · faultyON CLIMBOUT FROM KDTW THE FLIGHT CREW FELT THE AIRCRAFT YAW TO THE RIGHT AND NOTICED THAT THE RIGHT ENGINE GAUGES WERE FLUCTUATING 5 TO 10 PERCENT. THE AIRCRAFT WAS LEVELED AT 5000 FEET AND THE CREW DECLARED AN EMERGENCY. AN UNWISE UNEVENTFUL APPROACH AND LASDR HALA2009072900337Mec · malfunctionedETOPS SIGNIFICANT SYS - DURING CRUISE L ENG EEC AND AUTOTHROTTLE DISCONNECT LIGHT ON EICAS. PERFORMED QRH AND L ENG EEC LIGHT WENT OUT. BITE OF MONITOR LT EEC MEC AMPS RANGE. T/S IAW FIM 71 EECM MESSAGE INDEX TABLE 101. EEC PREVIOUSLY REPLACED. CKD CIRCUIT BSDR QXEA2009012600035Switch · malfunctionedSEA - ON TAKEOFF, NR 1 ENG LAGS BEHIND NR 2 DOESN'T ACCELERATE. REPLACED THE SWITCH ROLLER ASSEMBLY. OPS CHECK GOOD. RETURNED TO SERVICE.SDR QXEA2009012300032Switch · contaminatedSEA - NR 1 ENGINE FAILED TO ACCELERATE ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO THE GATE. UPON INSPECTION FOUND MAX AND MIN POSITION ON THE CONDITION LEVERS SWITCHES BELOW THE COCKPIT FLOOR STICKY. CLEANED AND LUBED SWITCH, GROUND RAN ENGINES AT TAKEOFF SDR GVNA119695Actuator · jammedIN FLIGHT NR 2 ENGINE TRIM ACTUATOR FULLY RETRACTED, JAMMED, POPPED TRIM CIRCUIT BREAKER. AIRCRAFT LANDED USING MANUAL TRIM. REPLACED ACTUATOR.SDR CA071217004Control Cable · disconnected(CAN) AFTER FLIGHT, THE NR 2 CONDITION LEVER WOULD NOT MOVE TO FEATHER OR CUTOFF, THE ENGINE HAD TO BE SHUTDOWN USING THE T-HANDLE. FURTHER INVESTIGATION REVEALED THAT THE NR 2 TELEFLEX CABLE HAD BECOME UNSCREWED NEAR THE BEARING. WE WERE UNAWARE THAT THE CASDR HNAA0700283Switch · out of rigTAKEOFF WARNING HORN SOUNDED DURING TAKEOFF ROLL, ABORTED TAKEOFF, CYCLED ALL APPROPRIATE SWITCHES AND LEVERS, NO FIX. FOUND NR 1 CONDITION LEVER SWITCH OUT OF RIG. RIGGED SWITCH AND LUBED. GROUND RAN AIRCRAFT, SYSTEM OPERATIONAL CHECK GOOD.SDR QXEA200701528Switch · malfunctionedEUG - FLIGHT NR 2193, JUST AFTER ROTATION AS THE GEAR WAS COMING UP THE NR 2 ENGINE BEGAN SURGING BETWEEN TOP AND BETWEEN 125 PERCENT AND 140 PERCENT. AT 100 FT, THE ENGINE FAILURE CHECKLIST WAS COMPLETED PRIOR TO BEGINNING THE CHECKLIST BOTH NR 2 TORQUE AND SDR QXEA200701078Unknown · unknownYVR FLIGHT NR 2039 - AFTER SINGLE ENGINE TAXI, WHEN BRINGING NR 1 CL FROM START/FEATHER TO MAX FOR TAKEOFF TORQUE INDICATION SPIKED AT APPROXIMATELY 125 PERCENT. POWER LEVER WAS BELOW FLIGHT IDLE AND TAKEOFF WHEN TEST WAS NOT BEING PUSHED. PERFORMED OVER TORSDR NSVA20070157Control Quadrant · defectiveFI STOP OPEN LIGHT ILLUMINATED IN FLIGHT. REPLACED CONTROL QUADRANT IAW SAAB AMM 76-10-05, NO DISCREPANCIES NOTED, PN ON: 53162-4, SN ON: 074, PN OFF: 53082-16 SN OFF: 187.SDR QXEA200700940Pcu · malfunctionedEUG FLIGHT NR 2166, AFTER STARTING ENGINES AND RUNNING CHECKLIST. ADDED POWER TO INITIATE RIGHT RUN OUT OF PARKING SPOT. UPON ADDING POWER TO NR 1 ENGINE, NOTICED TORQUE INCREASE RAPIDLY TO YELLOW ARC. SOUNDED AS IF PROP FEATHERED, BUT DID NOT NOTICE NP GAUSDR HNAA0700206Control Cable · corrodedRIGHT ENGINE CONDITION CONTROL AND POWER CONTROL CABLES ARE CORRODED IN THE NACELLE AREA. INSTALLED NEW CONDITION AND POWER CABLES ON RIGHT ENGINE AS PER 76-10-00 RIGGED IAW 76-10-14.SDR HNAA0700205Control Cable · wornLEFT ENGINE CONDITION CONTROL UPPER CABLE AND POWER CONTROL UPPER AND LOWER CABLES ARE WORN TO LIMIT. ENGINE 1 UPPER CONDITION CABLE AND BOTH POWER CONTROL CABLES REPLACED AS PER 76-10-11 AND TASK 76-00-00.SDR 2007FA0000561Bushing · wornENGINE MOUNTED THROTTLE LINKAGE BUSHINGS WORN. FOUND ON INSPECTION WITH EXCESSIVE PLAY. PROBABLY OCCURRED DUE TO EXCESSIVE VIBRATION OR LACK OF SUBRICATION. RECOMMENDATION TO PREVENT WOULD BE TO LUBRICATE MORE FREQUENTLY OR DIFFERENT DESIGN OF LINKAGE. (K)SDR NSVA20070096Stop · intermittentFI IDLE STOP LT INTERMITTENT. PERFORMED ADJUSTMENT TEST OF THE FLIGHT IDLE STEP SYSTEM IAW SAAB 340 AMM 76-10-60. OPERATIONAL TEST PASSED.SDR PAI52007S4508Condition Lever · loosePILOT NOTED RT ENGINE CONDITION LEVER CONTROL FELT LOOSE AND IDLE N1 SPEED LOW. UPON INSPECTION, MAINTENANCE FOUND ALL SCREWS ATTACHING CONDITION LEVER TO QUADRANT LOOSE TO THE POINT OF ALMOST FALLING OUT.SDR 2007FA0000263Solenoid · unserviceable(REF NR: 186AE-2007-I-0032) WHILE PERFORMING A CHECK OF THE TWIST GRIP SOLENOID, ENGAGED THE SOLENOID BY PLACING THE AUTO/MAN SWITCH TO MAN MODE FOR A TOTAL OF 10 MINUTES. AFTER THE 10 MINUTE PERIOD HAD ELAPSED, RETURNED THE AUTO/MAN SWITCH TO AUTO. AFTER 1SDR NSVA20070039Control Quadrant · unknownCONFIG WARNING ON TAKEOFF ROLL. VERIFIED POWER TO RELAY 8 GA W PINX1. VERIFIED GROUND TO RELAY AT 8GA PIN X2.5. VERIFIED GROUNDS FROM RELAY 8GA PINS D1 AND A2. VERIFIED OPERATION OF L POWER LEVER QUADRANT SWITCH PINS 5 AND 6 AT P1. VERIFIED OPERATION OF RSDR CA070212002Condition Lever · stiff(CAN) DURING INSPECTION, IT WAS FOUND THAT THE CONDITION LEVER WAS EXTREMELY HARD TO MOVE. THE CONDITION LEVER CABLE WAS REPLACED. (TC NR 20070212002)SDR NSVA20070028Control Quadrant · unknownFOUND FLIGHT IDLE OPEN LIGHT ILLUMINATED AFTER TAKEOFF. REPLACED CONTROL QUADRANT IAW SA AMM 76-10-05 FUNCTIONAL TEST REQUIRED, PN: 531624, SN ON: 023 SN OFF: 061. PERFORMED OPERATIONAL CHECK OF QUADRANT CONTROL IAW SA MM 71-00-00. OPERATIONAL CHECK GOOD.SDR NSVA20070027Unknown · unknownAFTER TAKEOFF THE FLT IDLE STOP LIGHT ILLUMINATED. PERFORMED OPERATIONAL CHECK OF FLIGHT IDLE STOP MECHANISM AS PER SAMM 76-10-60-05. NO FAULTS NOTED, OPS CHECK GOOD AT THIS TIME.SDR CA070130003Condition Lever · cracked(CAN) PILOTS REPORTED LT FUEL CONDITION LEVER CRACKED HALF WAY DOWN LEVER. AIRCRAFT REMOVED FROM SERVICE. RT CONDITION LEVER INSPECTED AND SHOWED SIGNS OF WEAR. LT AND RT CONDITION LEVERS ON ORDER. (TC NR 20070130003)SDR NSVA200600205Control Panel · failedLT TQ INDICATION DROPPED TO 30 PERCENT ON TAKEOFF ROLL WHEN CTOT APR SWITCH SELECTED TO APR. REMOVED AND REPLACED CTOT PANEL. OPS CHECKS GOOD IAW AMM 76-10-50, P/N ON-OFF 7239060-503.SDR BAQA200600005Switch · wornBOTH ENGINE CONTROL SWITCHES (P/N 945UN01Q4AA8B) ON THE 20VE SWITCH PANEL (P/N L311M1009103, S/N 085) WERE FOUND TO BE ABLE TO MOVE FROM FLIGHT TO IDLE TO OFF BY JUST PUSHING ON THE SWITCH, NO LOCKING ACTION REMAINED IN THE SWITCH.SDR NSVA200600185Relay · failedFLIGHT IDLE STOP OPEN LIGHT ILLUMINATED IN FLIGHT. REPLACED RELAY 82KA P/N M83726/28 2001P IAW SAAB 76-10-60, OPS CHECK OK.SDR CA061026005Support · unserviceable(CAN) IN SOME CASES, THE WELD BRAZING THAT CONNECTS THE TELEFLEX CONTROL SUPPORT BEARINGS TO THE ENGINE CONTROL QUADRANT ASSEMBLY HAVE BEEN FOUND TO BE CRACKED OR HAVE INSUFFICIENT BONDING TO THE BEARING SUPPORT PLATE. THIS PROBLEM, IN ADDITION TO INTERNAL WEASDR COMA0660503Controller · surgesFLIGHT 5320 - EN ROUTE CVG-GSO ENCOUNTERED SURGING OF THE LEFT ENGINE N1 AND N2, FLIGHT RETURNED TO CVG. DEFERRED THE ENGINE SPEED CONTROLLERS PER MEL 76-11-01.SDR CA060816005Bearing · seized(CAN) DURING ROUTINE MAINTENANCE INSPECTION OF MFG TASK 422 (A CHECK 500 HR REPETITIVE TASK) ZONAL INSPECTION OF RT ENGINE COMPARTMENT. FOUND POWER AND CONDITION CABLE PULLEYS (2 EACH SYSTEM, TOTAL 4 PULLEYS) IN THE UPPER AFT NACELLE/FRONT OF WING SPAR, TO ALSDR MALA060510Relay · malfunctionedON TAKEOFF, CREW EXPERIENCED FAILURE OF THE FLIGHT IDLE STOP SYSTEM AND RETURNED TO MEM. REPLACED RELAY 82KA. OPS CHECK GOOD.SDR NSVA200600111Dcu · malfunctionedRT ENGINE BOTTOM GOVERNOR DISENGAGED DURING TAXI. CLEANED CONNECTOR PLUG CONTROLS ON DECU, PERFORMED OPS CHECK GOOD NO DEFECTS NOTED AT THIS TIME IAW 76-10-57SDR NSVA200600090Dcu · malfunctionedLEFT ENGINE WON'T COME OUT OF FEATHER WITH NO PROP RPM AND NO TORQUE. REMOVED AND REPLACED LT DECU IAW SAAB 340 AMM 76-10-57-04, GROUND RAN AC OPS CHECK GOOD, P/N 6071T20P17, S/N OFF LMDT2337S/N ON ECDT1399SDR DXTA200601411Beta Switch · out of adjustPERFORMED SPEED BRAKE AUTO-STOW CHECK. WHEN RETARDED LT THROTTLE TO IDLE, ENGINE SHUT DOWN. PERFORMED SPEED BRAKE SYSTEM TEST SEVERAL TIMES, COULD NOT DUPLICATE DISCREPANCY. ADJUSTED 85 PERCENT N2 SWITCH TO MANUFACTURE'S SPECS, OPS CHECK GOOD IAW MM 27-61-00SDR 2006FA0000634Link · wornDURING OPERATIONAL CHECK FLIGHT OF AIRCRAFT, PILOT ADVANCED POWER LEVERS FORWARD AND NOTED LT ENG (N) REACHED MAX OF 117 PERCENT N2, REACHED MAXIMUM OF 100 PERCENT. IT IS DETERMINED THAT PROBABLE CAUSE OF OVERSPEED WAS ACHIEVED BY WORN THROTTLE LEVER LINK NOTSDR EIA2006075Sensor · damagedAT FL 380, PWR WAS REDUCED FOR SPEED CONTROL AND WAS NOT RESPONSIVE UNTIL REACHING FL 250. REPLACED NR 3 TT2 SENSOR AS PER MM 72-21-04, OPS CHK GOOD PER MM 71-00-00 TEST 3.SDR SIMA200613501Fadec · malfunctionedDURING TAKEOFF, CREW NOTED THE AIRCRAFT SHUDDERED WHEN CLIMB THRUST SELECTED AFTER TAKEOFF. REPLACED FADEC 1A AND 1B IAW AMM. PASSED FCF. AIRCRAFT RETURNED TO SERVICE. (M)SDR P5CA0601477Relay · not seatedATTEMPTED TO START NR 3 ENGINE 2 TIMES. AFTER SECOND ATTEMPT FUEL FLOW INDICATED IN EXCESS OF 1100 KGPH. ENGINE WOULD NOT START. CHECKED CONDITION ACTUATOR, RESEATED RELAYS YBEK12 AND YBEK08, OPS CHECKED OK. ENGINE STARTED ON FIRST ATTEMPT.
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