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 J7SA2026092900520Ecu · unserviceableDIVERTED DUE TO R FADEC FAIL CAS PRESENTED AND R ENGINE SHUTDOWN ON DESCENT INTO KPNE AT 9000 FT AND 230-250 KTS. CREW COMPLETED CHECKLIST, NOTIFIED ATC, AND DECLARED AN EMERGENCY. ATTEMPTED RELIGHT OF THE #2 ENGINE WAS UNSUCCESSFUL (N1, N2, AND OIL PRESSURE ISDR 2026FA0000839Bracket · out of positionRIGHT ENGINE (#2) REAR COWLING BRACE PIN CABLE CAUGHT AROUND THROTTLE LEVER AND WOULD NOT ALLOW THROTTLE MOVEMENT. CABLE AND BRACKET WERE ADJUSTED TO PREVENT FUTURE ISSUES. THIS OCCURRED AFTER ENGINE START ON THE GROUND.SDR QR9R2026091100002Control Box · faultyROTOR RPM REMAINED IN LOW RED RANGE (95%) IN FLIGHT. LOW ROTOR RPM LIGHT AND HORN CAME ON INTERMITTENTLY. REMOVED AND REPLACED VARTOMS CONTROL BOX IAW AMM 76-13-00, 4-1. FUNCTIONAL CHECK COMPLETED OK.SDR 141A2026090600001Power Lever · malfunctionedFLYING IFR, BUT SAW THE FIELD, GOT CLEARED FOR THE VISUAL APPROACH AT MIMLE. WHEN TURNING BASE TO FINAL AT AROUND 1100 FT FLYING AT 120 KNOTS, SUDDENLY THE NG STUCK. SAW THE POWER LEVER AT IDLE & NG WAS AT 88.2. COULDN’T SLOW DOWN. BUT CYCLED THE POWER LEVER,SDR QR9R2026082000001Cable · bindingDURING INSTALLATION OF NEW N2 CABLE (NR 1 ENGINE) COULD NOT ACHIEVE SMOOTH CABLE MOVEMENT AFTER CABLE WAS ROUTED. REMOVED CABLE AND FOUND TO BE ROUGH AND BINDING.SDR 2026FA0000621Fadec · failed3 MINUTES INTO THE FLIGHT, BOTH ENG MANUAL 2 AND FADEC FAIL 2 CAUTION ILLUMINATED. WHEN THE CAUTIONS ILLUMINATED THERE WAS NO INDICATION OF A FAIL ON THE FLI, TEMPERATURES, OR PRESSURES. FOLLOWING ACTIONS WERE TO REFER TO SECTION 3-27 OF THE FLIGHT MANUAL FOR SDR QR9R2026071400001Control Box · bindingRECEIVED FROM AIRBUS UNSERVICEABLE. CONTROL BOX ASSEMBLY FOUND TO BE RATCHETING AND BINDING.SDR 2026FA0000432Fadec · faultedPART 91 FLIGHT, NO PAX ONBOARD. FLIGHT LEVEL 27,000 PILOT RECEIVED A FADEC NO DISPATCH, AND THEN SUBSEQUENTLY FADEC FAIL. HAD RED X’S ON MULTIPLE ENGINE DATA READOUTS, BUT NO ENGINE PERFORMANCE CHANGE. PILOT WAS ENROUTE TO ADDISON, HE FOLLOWED ONBOARD CHESDR SWAA2026032080133Resolver · out of adjustASYMETRIC THRUST WHEN SETTING TAKEOFF POWER AUTOTHROTTLE SPLIT AFTER TOGA IS PRESSED<[01] FOUND #2 TLA RESOLVER VALUE OUT OF LIMITS. ADJUSTED PER AMM 76-11-05SDR BIGA20260205001Flex Coupling · contaminatedTHE CREW WAS CONDUCTING A MAINTENANCE ACCEPTANCE FLIGHT ON AIRCRAFT FOR THE REPLACEMENT OF LEFT AND RIGHT PROPELLERS. THE NTS SHUTDOWN PROCEDURE WAS BEING PERFORMED IN-FLIGHT AS REQUIRED ON THE RT ENG. DURING THE NTS SHUTDOWN, THE RT PROPELLER DID NOT FULLY SDR ABXA20260117015Circuit Breaker · faultedON PUSHBACK, ALL T/O SPEEDS DUMPED AND UNABLE TO SET ANY T/O PWR SETTING ON TMC OR SET A TEMPERATURE A/C RETURNED TO THE GATE AND MTX GROUNDED A/C .MTX RESET CIRCUIT BREAKER IAW B767 AMM 20-60-01. OPS CHECK GOOD. NO FAULT NOTED AT THIS TIME. ACFT REMAINS CASDR 2025FA0000765Fadec · failedSEVENTEEN MINUTES INTO THE FLIGHT, A FADEC FAIL 2 CAUTION ILLUMINATED. AT THAT TIME, THE #2 ENGINE TORQUE DECREASED FROM 58.8 TO 6.9, THEN INCREASED TO 19.9 WITHIN THREE SECONDS. THE #2 ENGINE TORQUE REMAINED AT 19.9 FOR THE REMAINDER OF THE FLIGHT. THE PILOT SDR HEEA202511100001Sensor · dirtyFADEC1 FAULT ILLUMINATED FOLLOWED BY FADEC 2 FAULT SEVERAL MINUTES LATER DURING CRUISE FLIGHT. RTB. DURING RTB BOTH CAS EXTINGUISHED PRIOR TO LANDING.SDR QMLA2025091520094Engine · power lossWE WERE TAKING OFF FROM THE PAD AT PRESCOTT WITH A PATIENT ONBOARD. HAD GOOD POWER IN HOVER AND ON TAKEOFF ABOUT 200-300 FT AND GOT JUST PAST THE STREETLIGHTS IN FRONT OF THE PAD. POWER SETTING BELOW THE YELLOW RANGE, FOR A BRIEF SECOND THE NOSE ROTATING TO LESDR ABXA20250909224Hmu · inoperativeDURING DESCENT, ON THE ARRIVAL TO MIA, L & R ENG CONTROL STATUS MESSAGES. RIGHT ENGINE WOULD NOT ACCELERATE FROM IDLE. DECLARED EMERGENCY AT APPROX. 1930Z AND LANDED AT MIA. AFTER LANDING L & R ENGINE CONTROL EICAS MESSAGES APPEARED. MIA FIRE DEPARTMENT CHESDR CHIA202508149804Switch · failedNR 1 ENGINE BEEP SWITCH ON THE LT COLLECTIVE BECAME INTERMITTENTLY UNRESPONSIVE IN FLIGHT, RESULTING IN PILOTS INITIATING ENGINE BEEP FAILURE/FREEZE EMERGENCY PROCEDURES AND RETURNING TO BASE FOR AN UNSCHEDULED LANDING. SUBSEQUENT INSPECTION DETERMINED THE LTSDR YENA2025081400839Interface Unit · faultedFLT#1908, CDG-JFK. (ETOPS) "ENG SOFT FAULT ON TOGA TAKEOFF. A/THR KICKED OFF AS WELL BUT WAS ABLE TO RESET USING A/THR PUSH BUTTON ON THRUST LEVERS. ( LOST A/THR AFAIN ON APPROACH); TROUBLESHOT ENGINE SOFT FAULT AND AUTO THROTTLE FAULT PER TSM 78.00.810.808.A SDR R61A2025052100249Metering Unit · faultedENGINE 2 FAIL IN FLIGHT, RELIGHT SUCCESSFUL. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. NO EICAS MESSAGES AT THE TIME, R&R ENGINE 2 FADEC AND FMU.SDR CTUR20250528001Lever · missingTRIED FLYING N817PA MORNING OF MAY 7TH AND THE RIGHT SIDE DOESN'T COME OUT OF THE GROUND PITCH. DOING THE AUTO FEATHER TEST, THE RIGHT PROP WAS AT 1700 RPM. TRIED DOING THE GROUND IDLE STOP TEST AND THE RIGHT SIDE FAILED THAT TEST. COULDN'T GET IT TO SWITCH TOSDR 2025FA0000013Motor · disengagedON APPROACH THE VARTOMS SYSTEM DISENGAGED AND TORQUE MATCHING HAD TO BE PERFORMED MANUALLYSDR 2025FA0000003Governor · faultedON TAXI OUT, THE LT FUEL COMPUTER WENT OFF-LINE, THE PILOTS SELECTED BOTH FUEL COMPUTERS OFF AND PROCEEDED TO FLY IN MANUAL IAW THE MANUAL. WHILE APPLYING TAKE OFF POWER SOME SURGING WAS NOTICED ON THE LT ENGINE. ABORTED TAKE OFF. FOUND THE MONOPOLE MALFUCTIONSDR QXEA2024112600281Throttle · malfunctionedFLIGHT 2146. 5 MIN AFTER POWER UP AT FAIL MESSAGE. REMOVED FROM SERVICE AND PLACED ON MEL 22-30-00B. RETURNED TO SERVICE. MEL CLEEARED 11/26/24 BY AT FAULT NOT PRESENT ON STARTUP OR THROUGHOUT TROUBLESHOOTING REF FIM 22-31-00-810-818/860-A AND FAULT CODE AND SDR QMLA2024102120135Potentiometer · faultedTORQUE SPLIT ON TAKE OFF. REDUCED COLLECTIVE, AND TORQUE MATCHED. TORQUE SPLIT AGAIN IN CRUISE FLIGHT. #1 TORQUE WAS 12-15% HIGHER AND FLUCTUATING. TORQUES HELD THAT SPLIT, THEN # 1 WOULD FLUCTUATE. UNABLE TO MATCH TORQUES. DIVERTED BACK TO BASE WITH PATIENT OSDR QXEA2024091900215Throttle · malfunctionedFLIGHT 2061. ENG 1 REV FAIL CAUTION ON LANDING. REMOVED FROM SERVICE AND PLACED ON MEL 78-30-00D. RETURNED TO SERVICE. MEL CLEARED 9/18 BY INTEROGATED CMC & FOUND FC: 73217627E1B & 73217627E1A. PER FIM 73-21-00-810-81B-A REPLACED TQC ASSY (REF AMM 76-11-01-00SDR CHIA202407187623Control Box · activation errorTHREE MINS AFTER TAKEOFF, THE COPILOT NOTED A SPLIT IN TORQUE SHOWING THE #1 ENGINE HAD ROLLED BACK TO 40% TORQUE. THE ENGINE WAS BEEPED UP AND THE AIRCRAFT WAS RETURNED TO BASE. TROUBLESHOOTING FOUND NO DEFECTS NOTED. FOR PRECAUTIONARY MEASURES, REPLACED #1 ESDR CHIA202407167614Control Box · activation errorSHORTLY AFTER INITIAL TAKE OFF FROM OUA, PILOT NOTED THE #1 ENGINE SOUNDING LIKE IT WAS ROLLING BACK. LOOKING AT THE GAUGES HE FOUND A 35% TORQUE SPLIT BETWEEN THE #1 AND #2 ENGINES. HE THEN PUT THE #1 ENGINE IN MANUAL AND CONTROLLED THE BEEPS FROM THERE. RETUSDR 2024FA0000526Start Button · deactivatedFLIGHT CREW REPORTED THAT THE RIGHT ENGINE SHUTDOWN DURING THEIR TAKEOFF ROLL. CREW ABORTED THEIR TAKEOFF AND TAXIED THE AIRCRAFT BACK TO A LOCATION TO FURTHER EVALUATE THE RIGHT ENGINE'S CONDITION. CREW CONTACTED JET OUT'S MAINTENANCE DEPARTMENT, IT WAS THEN SDR QR9R2024061700001Monitor · failedVARN NR CAUTION DOES NOT ILLUMINATE ON THE CAD AS REQUIRED FOR FLIGHT. A T/F EVALUATION REVEALED VAR NR LIGHT ON CAD WENT OFF WHEN AVIONICS MASTER SWITCHES WERE TURNED ON. VAR NR LIGHT IS SUPPOSED TO REMAIN ILLUMINATED. REMOVED AND REPLACED VARTOMS MONITOR BOXSDR QXEA2024061200154Control Quadrant · malfunctionedPER ENGINEERING REQUEST TCQ REPLACEMENT REG. REMOVED AND REPLACED THUST CONTROL QUADRANT IAW E175 AMM 76-11-01-000/400-801-A. OPS TEST GOOD. AIRCRAFT STATUS REMAINS CAT III QUALIFIED COCKPIT PLACARD READS CAT III MTX CTRL ADVICED.SDR QMLA2024052420054Fadec · faultedFADEC RESTART FAULT ILLUMINATED IN FLIGHT. NO OTHER ABNORMALITIES. DIVERTED TO NEARBY AIRPORT WHERE MAINTENANCE COULD BE PERFORMED. FOUND WFMV FAULT CODE. CLEARED FAULT CODE. PERFORMED NORMAL START UP AND RETURNED TO BASE.SDR QR9R2024051500001Spring · excess playPART RECEIVED UNSERVICEABLE FROM AIRBUS. EXCESSIVE PLAY WAS DETECTED IN CENTER BOLT OF OVERRIDE-SPRING ASSY-N2 AND CONFIRMED BY AHI REP.SDR ANCF20240502011Control Unit · unserviceableENG 1 THR LEVER DISAGREE DURING APPROACH ENG 1 WENT AT IDLE WHEN SLATS WERE EXTENDED LDGW 64.300 KG. IN ACCORDANCE WITH ASM 73-25-12 THE WIRING BETWEEN THE CTL-UNIT THROTTLE ENG1 8KS1 CONNECTOR D AND ECU 4000KS J4; AND BETWEEN CTL-UNIT THROTTLE ENG1 8KS1 COSDR QMLA2024042520043Potentiometer · wornTOOK OFF FROM BASE GOT TO LEVEL FLIGHT STARTED POWER CHECK GOT THE SOLID AMBER GOV LIGHT. RETURNED TO BASE.SDR R61A2024042900193Fadec · faultedHALFWAY THROUGH CLIMB, E2 ROLLED BACK TO IDLE. ENG 2 CAME BACK, EICAS CLEARED. E2 TLA FAIL. E2 NO DISPATCH AND E2 SHORT DISPATCH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R E2 FADEC. R&R THRUST CONTROL QUADRANT.SDR IPXA2024041597990Relay · faultedTHRUST CONTROL MODULE MAKING SPORADIC AUDIBLE NOISES " CLICKING NOISE" T/S REF WDM 78-34-01-1.1, REPLACED FAULTY TERMINAL BLOCK 37BA REF SWPM 20-26-03. #1 REVERSER INTERLOCK OPS OK REF MM 78-30-00.SDR ABXA2024033171Control Module · faultyAPPROXIMATELY 25 MINS INTO FLIGHT THE EICAS DISPLAYED "R ENG SHUTDOWN" AND "R ENG FUEL VAL". IN-FLT START PARAMETERS WERE ALSO DISPLAYED. RIGHT "ENG VALVE" LIGHT ON CONTROL DISPLAYED CONTINUED PANEL. CONDUCTED T/S PER FIM 76-11 F.T. 813 R MEC REPLACEMENT REQUISDR CALA2024031500743Sense Line · leakingENG EEC MODE R EICAS ADVISORY RIGHT ENGINE ELECTRONIC ENGINE CONTROL (EEC) IS IN THE ALTERNATE CONTROL MODE (EITHER BY DEFAULT DUE TO A CONTROL FAILURE OR MAN UALLY SELECTED BY THE FLIGHT CREW). FIM TASK REF : FIM TASK REFERENCE NOT FOUND CMC MSG# 7761032 FLISDR HALA20240305061Master Switch · faultedETOPS - ENG 1 HP VALVE DID NOT CLOSE WHEN COMMANDED BY ENGINE MASTER. ENGINE DID NOT SHUTDOWN. AFTER 2 MINS ENGINE FINALLY SHUTDOWN. REMOVED AND REPLACED ENG 1 MASTER SWITCH 2KC1 PER ESPM 20-45-21. INSTALLED 125VU. PERFORMED ENGINE RUN PER AMM 71-00-00-810-810SDR ASAA2023111346164Unknown · unknownDURING ENG FAULT CDU TASKCARD FOUND LONG TIME FAULT FOR ENG #1 MSG NBR 76-31361. THE START LEVER SIGNALS DISAGREE FAULT LEG 0. GROUNDED - YES. REF FIM 76-11 TASK 801, EEC BITE CHECK ENG 1, NO FAULTS. C/W ENG 1 DISCRETES TEST REF AMM 73-21-00 PB 501, ALL TESTS SDR QMLA2023110220099Unknown · unknownAFTER AMBER AND RED GOV LIGHT ILLUMINATED, MYSELF AND THE CREW COULD SMELL AN ELECTRICAL SMOKE ODOR. AFTER LANDING AND SHUTDOWN. ARRIVED AT AIRCRAFT, CLEANED ELECTRICAL CONNECTORS ON FADEC AND NF SENSOR. GOV LIGHT WENT OUT.SDR ASAA2023103045951Unknown · unknownON SHUTDOWN #2 START LEVER DOES NOT GO ALL THE WAY DOWN. IT SITS ABOUT 1/2 KNOB WIDTH ABOVE #1. GROUNDED - YES. C/W OP CHECK ENG START 2 LEVER PER AMM 76-11-03 OPS CHECK NORMAL.SDR ASAA2023102945876Unknown · unknownFOUND ENG 1 EEC C1 LATCHED MESSAGE DURING TC 31-005-00. GROUNDED - YES. FOUND CORRELATED MESSAGE 73-44141. PERFORMED IFIM G73-20-00-810-847 FAULT IS INTERMITTENT. LATCHED MESSAGE ERASED.SDR ASAA2023102845870Unknown · unknownREFERENCE TC 78273000, #2 ENGINE DISPLAYS LONG TIME FAULT 76-31362, "THE START LEVER SIGNALS DISAGREE". GROUNDED - YES. ON DEFERRAL.SDR QXEA2023102700155Control Quadrant · malfunctionedAHEAD HAS REPORTED FAILURES OF THE TCQ QUICK DISCONNECT BUTTON. REMOVED THRUST CONTROL QUADRANT REF. E175 AMM RASK 76-11-01-000-801-A. STARTED INSTALLING THRUST QUADRANT REF. E175 AMM TASK 76-11-01-400-801-A STEPS 1-7D. TEST OF TCQ INSTALLATION AND FUNCTIONAL SDR ASAA2023100945547Unknown · unknownENGINE #2 LONG TIME FAULT MSG #76-31362 THE START LEVER SIGNALS DISAGREE. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023100445442Unknown · unknownON ENG #2; LONG TIME FAULT 76-31362 THE START LEVER SIGNALS DISAGREE. GROUNDED - YES. (RESOLVED ON W/O: 1971953 TASKCARD: N/R-00005 ) REF L/P 60165285, ACCOMPLISHED FIM 76-11 TASK 801 FAULT ISOLATION, OPS CK NML. AIRCRAFT RELEASED FROM PLT DEFERRAL, C/N 040165SDR HALA20231003217Unknown · unknownATB - CREW REPORTING LIGHTNING STRIKE AND ENG2 STALL MSG, BUT REPORTS TO DISPATCH BOTH ENGS ARE OPERATIONAL. PER POWERPLANT ENGINEERING, MUST ACCOMPLISH ENG SURGE AMM TASK WHICH WILL REQUIRE A BORESCOPE. NO REPORTS OF ANY FINDINGS ON THE LIGHTNING STRIKE AND OSDR HNAA2023092400247Unknown · unknownNO.2 ENG SHUT DOWN INFLIGHT AND WOULD NOT RESTART. R/R #200 ENGINE IRT WORKCARD 71-00-00SDR QMLA2023092520075Unknown · unknownDEPARTED BASE AT 1254 TO CAMDEN CLARK FOR PATIENT TRANSFER TO RUBY. APPROXIMATELY HALFWAY TO CAMDEN GOT #2 ENG MANUAL AND FADEC FAIL CAUTION LIGHTS AND MINOR SPLIT IN FLI 1/2 NEEDLES. TOLD THE CREW ABOUT THE CAUTIONS AND INFORMED THEM THAT THIS IS NOT A MAJOSDR QXEA2023091800129Control Quadrant · malfunctionedATUOTHROTTLE FAILED IN FLIGHT MULTIPLE TIMES. REMOVED FROM SERVICE. PLACED ON MEL 22-30-00B. RETURNED TO SERVICE. MEL CLEARED 9/17 BY REPLACING THE THRUST CONTROL QUADRANT REF E175 AMM TASK 76-11-01-000-801-A & 76-11-01-400-801-A. OPS TEST GOOD. THIS CLEARS
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