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 QR9R20220913001None · warning messageVAR NR CAUTION REMAINED ON AT HOVER. NRO AND TORQUE SEQUENCED CORRECTLY. REMOVED AND REPLACED VARTOMS MONITOR BOX ASSEMBLY IAW AMM 76-13-00, 4-2.SDR MDGA8733081722Fuel Control · power lossENGINE POWER REDUCED FOR DESCENT AND UPON LEVEL OFF ENGINE WOULD NOT ACCELERATE ABOVE FLIGHT IDLE. ENGINE WOULD NOT RESPOND IN MANUAL MORE. ENGINE SECURED AND AIRCRAFT LANDED WITHOUT FURTHER ISSUE. FUEL CONTROL REPLACED.SDR HDNA20220812001Sensor · failedPILOT'S STATEMENT - WAS AT CRUISE FLIGHT AT 2000 MSL ON LEG BETWEEN ECU NORTH HOSPITAL AND ECU MEDICAL CENTER WHEN OVSP FAIL (#2) CAUTION ILLUMINATED AND THEN EXTINGUISHED ON ITS OWN FOLLOWING ACKNOWLEDGEMENT. AUTOPILOT WAS COUPLED AND THERE WERE NO SECONDARY SDR ASAA2022070138918Starter Brake · defectiveAT THE GATE, AFTER ENGINE #2 WAS SHUT DOWN NORMALLY ENGINE FAIL APPEAR IN EGT DISPLAY. GROUNDED - YES. REMOVED F/O #2 ENGINE START BRAKE ASSY, REMOVED BOTH CAPT AND F/O CHAIRS REF B737-900 AMM 76-11-10-010-801-F00. NEW PART WAS DEFECTIVE, HARNESS MISMATCHED. ISDR CALA2022061501512None · failedONE TLA FAULT DISPLAYED ON UPPER ECAM SCREEN. - ENG 2 CAME ON AND EXTINGUISHED. REPEAT GRIPE. 1 UPDATE. STARTED TS TASK 76-00-00-810-802-B , FOUND FADECA AND 2 UPDATE , ENG #2 WIRING CHECK ALL OK FROM EEC 4000KS TO TCU FADECB FAULT CODE TRAXCF , NEXT STEP CHESDR 2022FA0000278None · shutdownAFTER DEPARTURE FROM BRUNSWICK AT 1319 ZULU ON 5 JUNE RUNWAY 07. WE WERE CLIMBING OUT THROUGH APPROXIMATELY LEVEL 160 WE GOT A BLUE CAS “L ENGINE MAINTENANCE LTD” WE HAD SEEN THIS BEFORE AND THIS WAS THE REASON WE WERE IN BRUNSWICK FOR MAINTENANCE. WE CONTINUESDR ASAA2022060338546Brake Assy · failedREPORTS OF #2 ENGINE FAIL MESSAGE AT ENGINE SHUTDOWN. GROUNDED - YES. REMOVED AND REPLACED #2 ENGINE START BRAKE ASSEMBLY REF B737-900 AMM 76-11-10/401. OPERATIONAL CHECK GOOD REF AMM 76-11-10-420-801-F00 STEP H. ETOPS GROUND VERIFICATION SUCCESSFUL.SDR NACA2022060200002None · noneRIGHT FCS IN RUN BUT NO FUEL FLOW ON ENGINE START. RESTARTED, OK NORMAL START. ACCOMPLISHED FIM FAULT TREE 76-11 FT 812, REMOVED AND REPLACED FUEL IGN/CONTROL RELAY K169 PER AMM 76-11-11. ACCOMPLISHED ENGINE RUN PER AMM 71-00, OPS CHECK NORMAL ETOPS GROUND VERSDR ASAA2022050838247Switchpack · faultyTAKE OFF WARNING HORN #2 THROTTLE DOES NOT SOUND ABOVE 73 TRA. #1 OPS NML AMM 31-51-00. GROUNDED - YES. DISCONNECTED CONN D11132P, VERIFIED RH AUTOTHROTTLE SWITCHPACK SWITCH S8 PINS 16-17 CLOSES AT 52 DEG TRA AND OPENS AT APPROX 74 DEG TRA. REPLACED RH AUTOTHRSDR ASAA2022043038178Unknown · unknown1/4 KNOB SPLIT IN LOW POWER RANGE #2 ENGINE LAGS #1 WITH THROTTLE EVEN #1 40% N1 #2 36%. GROUNDED - YES. PEFORMED B737-900 FIM 22-31 TASK 801, NO FAULTS FOUND. INTERACTIVE TEST ALL PASS. EEC TEST PASS REF FIM 73-21-00. PERFORMED ENGINE POWER RUN, WITH THROTTLESDR ASAA2022042038111Lever · cracked#1 THRUST LEVER CRACKED AT THE KNOB MOUNT. GROUNDED - YES. REMOVED AND REPLACED #1 ENG THRUST LEVER REF B737-800 AMM 76-11-01.SDR ASAA2022041838140Switchpack · warning light#2 ENGINE "REVERSER" LIGHT ILLUMINATED ON ON OVERHEAD PANEL. GROUNDED - YES. REMOVED AND REPLACED R/H AUTOTHROTTLE SWITCHPACK REF B737-800 AMM 76-11-07/401. OPS CHECK OK. REMOVED 4 SLEEVE PINS, REMOVED LOCKWIRE FROM #2 T/R HANDLE, RESET 2 C/BS.SDR ASAA2022041037992Lever · faultyFAULT CODE 76-21362. THE START LEVER SIGNALS DISAGREE. ENGINE 2 LONG TIME FAULT. DEFERRED PER T/C 78273000. GROUNDED - YES. REPLACED #2 ENG EEC REF B737-800 AMM 73-21-60-400-801. ALL EEC OP CHKS AND SOFTWARE CONFIG CHKS GOOD REF B737-800 IPC 73-21-60-01A. #2 ESDR ASAA2022041037986Lever · faultedENGINE 2 FAULT CODE 76-11362 LONG TIME FAULT. THE START LEVER SIGNALS DISAGREE. DEFERRED PER T/C 78273000. GROUNDED - YES. REPLACED #2 ENG EEC REF B737-800 AMM 73-21-60-400-801. ALL EEC OP CHKS AND SOFTWARE CONFIG CHKS GOOD REF B737-800 IPC 73-21-60-01A. #2 EESDR SWAA2022041493707Switchpack · faulty#2 ENG THRUST REVERSER SLOW TO DEPLOY. #2 THRUST REVERSER LIGHT ILLUMINATED. 09APR EMAIL SENT REQUESTING FIELD TECH SUPPORT F/C AT TIME OF DEFERRAL LH SLEVE STOW SENSOR S831***SCHD 04/10 MCO***3-21 OPS CK GOOD 3-29 R/R #2 ENG LH T/R SYNC LOCK 4-9 R&R T/RSLEEVESDR ASAA2022040738110Brake Assy · faultyREF T/C 78273000 ENG 1 SHOWS LONG TIME FAULT 76-31361 THE START LEVER SIGNALS DISAGREE. GROUNDED - YES. 450 FH LONG TIME FAULT DEFERRED TO PLT PER T/C 78273000. REPLACED #1 START BRAKE ASSY B737-900 AMM 76-11-10-420-801 UP TO STEP (H) ASSY TEST. PERFORMED ENGISDR 2022FA0000172Throttle Cable · brokenON MARCH 11, 2022, DURING ENGINE RUN-OP FOR 10FNS SECOND TAKEOFF OF THE DAY, THE R/H ENGINE BECAME UNRESPONSIVE TO THROTTLE INPUTS. TROUBLESHOOTING IDENTIFIED A BROKEN AFT THROTTLE CABLE. THE CABLE WAS REPLACED AND OPS CHECK GOOD ON MARCH 24, 2022. THIS CABSDR 2023FA0000382Transducer · abnormalAIRCRAFT HAS A MOMENTARY POWER LOSS WITH ENGINE OUT INDICATION AND TORQUE SPLIT WITH A YAWING MOTION,SDR 2023FA0000381Transducer · abnormalINFLIGHT MOMENTARY ENGINE ROLLBACK WITH YAW KICK AND TORQUE LOSSSDR 2022FA0000257Power Lever · abnormalPALANCA DE POTENCIA NO ESTAN ALINEADAS DURANTE VUELO/ DESAJUSTE DE PALANCAS DE POTENCIA, FALLA DE RESOLVEDOR THRUST LEVER OUT OF ALIGNMENT DURING FLIGHT/THROT LEVER MISADJUSTMENT, SOLVER FAILURESDR 2022FA0000154Power Lever · loose@1922.5HRS AND 321CY THROTTLE RESISTANCE FAILED APPLICABLE LIMITS PER THE MANUFACTURE MAINTENANCE MANUAL. AIRCRAFT WAS GROUNDED AND MAINTENANCE TEAM BEGAN TROUBLESHOOTING. PER THE MANUFACTURES FAULT ISOLATION AND TROUBLESHOOTING GUIDANCE FROM BOMBARDIER TECHNISDR ASAA2022021437441Unknown · unknown#1 START LEVER BINDS ON SOMETHING WHEN SEATING INTO THE CUTOFF DETENT. GROUNDED - YES. PERFORMED GVI OF #1 START LEVER AS REQ'D, NO DEFECTS NOTED OPERATED START LEVER MULTIPLE TIMES COULD NOT DUPLICATE. OPS CHECK OF START LEVER NORMAL, REF737-900 AMM 76-11-02.SDR YENA2022021600062None · noneFLT 1052, RSW-HPN. ENG 1 SPOOLED DOWN TO UNDER 50% N1 DURING CRZ FLT. LP VIBE 1.4, NO OTHER INDICATIONS. ENG 1 SPOOLED BACK UP AFTER 5 SECONDS TL'S DID NOT MOVE.; VERIFIED EEC SOFTWARE IAW AMM 76-00-00-050-004. CHECK CMC FOR FAULT EXCEEDANCES NO FAULTS FOUND PSDR QR9R20220207001Control Box · faultyDURING REPLACEMENT OF VARTOMS CONTROL BOX, MAINTENANCE DETECTED #2 ACT EXTENDS TO THE END STOP INSTEAD OF RETRACTING AS IT SHOULD. VARTOMS CONTROL BOX REPLACED; TEST FLIGHT EVAL COMPLETED IAW AMM O5-60-00, 6-1.SDR COEA2022011101803Relay · faultedFLIGHT 8663, ENROUTE ANC - FAI/AIR TURNBACK DISCREPANCY: IDLE GATE FAIL ON TAKEOFF. RESET BUT IDLE GATE CAP LIGHT STAYED ILLUMINATED. RETURNED AIRCRAFT TO ANC. NO EMERGENCY DECLARED. LANDED WITHOUT FURTHER INCIDENT. CORRECTIVE ACTION: MAINTENANCE CLEANED IDSDR QR9R20211227007None · warning lightVAR NR CA LIGHT CAME ON AND WOULD NOT EXTINGUISH WHILE TWIST GRIP IN THE RIGHT POSITION AT A HOVER. THE 4-WAY TRIM APPEARED TO BE WORKING BUT VAR NR CA WILL NOT EXTINGUISH. T/F: VARNR LIGHT REMAINS ILLUMINATED DURING HOVERING FLIGHT AND DOES NOT EXTINGUISH DURSDR QR9R20211227002None · faultyDURING TAKEOFF WHEN NR REDUCES FROM 101% TO 96% VARNAR CAUTION APPEARS, VARTOMS REVERTS TO MANUAL MODE AND FLI SPLITS MORE THAN 15% WITH THE #2 ENGINE DROPPING BELOW THE #1 ENGINE ON BOTH ATTEMPTS TO DEPART. NO AIRCRAFT LIMITATIONS WERE EXCEEDED. #1 ENGINE VARSDR ABXA20211211129None · noneDURING RIGHT ENG START WHEN ADVANCING RT FUEL CONTROL , EICAS MESSAGE R ENG FUEL VALVE APPEARED AND DISAGREE ENGINE VALVE LIGHT ILLUMINATED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE FOUND DAMAGED WIRING IN FORWARD CARGO COMPARTMENT. WIRISDR IPXA2021120976806Relay · failedINSPECTION TYPE:N/AWHEN ENGINE #2 FUEL SN MOVED TO OFF ENGINE DID NOT SHUTDOWN BUT RECEIVED LEVEL 2 SEL FADEC ALT SELECTED BUT ENG STILL DID NOT SHUTDOWN, CONSULTED MMOC AND USED FINE HANDLE TO SHUT ENGINE DOWNR&R #2 ENG FUEL SWITCH IAW MD11 AMM 76-12-01, NO HSDR QR9R20211119003Monitor · failedDURING RUN UP, VAR NR CAUTION WOULD NOT COME ON BEFORE TAKEOFF. ALL OTHER INDICATIONS WERE CORRECT. NEEDLES STAYED TOGETHER AND NR WENT TO 101% WHEN PITCH WAS PULLED.SDR QR9R20211029007Actuator · illuminatedVAR NR CAUTION ILLUMINATED IN FLIGHT AND FLI SPLIT GREATER THAN 1 FLI. PUT VARNR SWITCH TO MANUAL AND SYNC'D THE FLI'S. GOING BACK TO NORM CAUSED THE FLI'S TO SPLIT AGAIN AND VAR NR CAUTION DID NOT EXTINGUISH. TQ SPLIT DID NOT EXCEED 15 %. MTF: VARTOMS FOUND TSDR JIKA2021102801Interface Unit · defectiveAMF FLT# 6905 EXPERIENCED A LH ENGINE FLAMEOUT AT 1500 FT DURING CLIMB, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. SJU MAINTENANCE TROUBLESHOT STARTING L/H ENGINE NORMALLY AND FOUND L/H ENGINE BYPASSING AND SURGING IN IDLE WITH NO OTHER INPUTS. DURINGSDR QR9R20211028003Actuator · intermittentVAR NR CAUTION LIGHT ON AND OFF CONSTANTLY THROUGH FLIGHT. WHEN PLACED INTO MANUAL TRIM SWITCH- WOULD NOT ADJUST NR BUT WOULD DRIVE #2 FLI. PASSING THROUGH 50-55KTS THE NR WOULD NOT SEQUENCE TO THE APPROPRIATE SPEED.
T/F EVALUATION: NUMBER 1 VARTOMS TRIM ACTSDR 2021FA0000280None · noneWHILE TROUBLESHOOTING A FUEL COMPUTER FAULT, IT WAS DISCOVERED THAT BOTH DEECS WERE IMPROPERLY INSTALLED. EACH DEEC WAS ATTACHED TO THE P2 SENSE LINE FOR THE RACK POSITION THAT IS WAS INSTALLED IN. THE J1 CONNECTIONS WERE TO THE OPPOSITE ENGINE. THE J2 CONNECSDR AALA202109287804Controller · fault messageAIRCRAFT WAS GROUNDED: DURING TAKEOFF ROLL BOTH ELECTRONIC ENGINE CONTROL ALTERNATE LIGHTS ILLUMINATED AT 62KTS ABORTED TAKEOFF 150100 TAKE OFF WEIGHT. RAN NUMBER 1 AND NUMBER 2 ENGINE PER TASK 71-00-00-700-808 AT IDLE FOR 5 MIN. PERFORMED ENGINE SHUT DOWN, PESDR ASAA2021082035767Switch · faultyUPON LANDING. MASTER CAUTION OVERHEAD PSEU LIGHT ILLUMINATED. GROUNDED - YES. PERFORMED FIM TASK 32-09 TASK 801 FOUND FAULT CODE 31-52002 MP80017 INIT MIG-2C # 40-0003313. MP80017 REF L/P 60222388 FOR "BP" DEFERRAL. 77899. R&R ENG1 SWITCH PACK ASSEMBLY (M1766)SDR 2026FA0000152Master Switch · faultedDURING INITIAL CLIMBOUT, PILOT FLYING (PF) REACHED WITH BOTH HANDS TO TURN OFF THE TWO FUEL PUMPS IAW THE CLIMB CHECK IN THE NORMAL PROCEDURES. PF INSTEAD TURNED OFF THE TWO ENGINE MASTER SWITCHES. AFTER APPROXIMATELY TWO SECONDS, DURING WHICH THE PF HEARD THESDR 9JLA09AUG20213306Switch · defectiveTHE FLIGHT CREW REPORTED OF RECEIVING A LEFT ENGINE CONTROL FAULT MESSAGE. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED A FAULTY LEFT ENGINE SHUTOFF SWITCH. THE DEFECTIVE SWITCH WAS REMOVED AND A NEW SWITCH WAS INSTALLED. OPS CHECKS WERE GOOD AND FAULT MASDR 9JLA2021072827589Control Module · defectiveTHE FLIGHT CREW REPORTED THE RIGHT THRUST REVERSER INTERMITTENTLY WILL NOT DEPLOY WHEN REVERSER LEVER WAS RAISED. OPERATIONS WERE CONTINUED PER MEL. ONCE INTO MAINTENANCE THE VENDOR TROUBLESHOT AND DETERMINED THAT THE THROTTLE CONTROL MODULE (TCM) WAS DEFECTISDR 2022F00167Switch · failedPRECAUTIONARY LANDING DUE TO POWER REDUCTION, BYPASS LIGHTS OF BOTH ENGINES REMAIN ON ALL THE TIME.SDR 2021FA0000111Alt Air Door · separatedPILOT REPORTED THROTTLE STUCK HALF WAY OPEN DURING FLIGHT. INSPECTED THROTTLE CONTROL AFT OF FIREWALL WITH NO DEFECTS. DISASSEMBLED Y PIPE THAT HOUSES THE ALTERNATE AIR FLAPPER VALVE AND FILTER. DISCOVERED MOST OF THE FLAPPER VALVE UP TO THE HINGE BOLT BROKSDR ASAA2021030134219Valve · crackedREF T/C 78273000 FAULT FOUND ENGINE #1 76-31361. LONG TIME FAULT. THE START LEVER SIGNALS DISAGREE. GROUNDED - YES. REMOVED AND REPLACED #1 ENGINE ESN # 893814 DUE FAILED BORESCOPE INSPECTION PER LOGPAGE 60083784. TRANSFERRED TO SHOP W/O #1865895.SDR 2021FA0000030Governor · failedDURING AIRCRAFT RUN-UP PROCEDURES PILOT ENGAGED GOVERNOR SWITCH INCREASED THROTTLE TO 832% FOR GOVERNOR TO TAKE OVER. GOVERNOR FAILED TO ENGAGE, AIRCRAFT SHUT DOWN NORMALLY. MECHANIC PERFORMED TROUBLESHOOTING PROCEDURES FOUND GOVERNOR CONTROLLER PN D278-1 TOSDR 9JLA2021021215735Torque Motor · inoperativeTHE FLIGHT CREW REPORTED OF AN INTERMITTENT RIGHT ELECTRONIC ENGINE CONTROL ANNUNCIATOR WHILE IN FLIGHT. THE FLIGHT CREW RAN THE APPROPRIATE CHECKLIST. LANDING WAS UNEVENTFUL. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED THE TORQUE MOTOR WAS INOP. P/N 30JSDR SIMA20201204001Throttle Control · out of toleranceABORTED TAKE OFF 80KTS FOR THRUST LEVER DISAGREE. FLT RTG DFW. REJECTED T/O DUE TO CAUTION CAS MESSAGE RLA TOGA BELOW 80 KNOTS AFTER EXIT ING RUNWAY BRAKES OVER TEMP MESSAGE CAME ON EICAS. "TRANSFERRED FROM AML PAGE 4690503 ITEM 1". C/A: PERFORMED TROUBLESHSDR ABXA20200803217Actuator · failedRT ENGINE WOULD NOT START, AIRCRAFT BACK TO BLOCK AND AIRCRAFT GROUNDED. TROUBLESHOT, PER B767 FIM 76-11-FT803 VERIFIED 28 VDC ON PIN 8, GROUND ON PIN 7. REMOVED AND REPLACED RIGHT ENGINE FUEL CONDITION MOTOR ACTUATOR, IAW AMM 76-11-04. REMOVED AND REPLACEDSDR ASAA2020110133477Switch · faultedON ENGINE START OF ENGINE NR 1 WHEN START LEVER WAS RAISED TO IDLE NO FUEL FLOW WAS SHOWN, NO N1 OR N2 ACCELERATION START WAS ABORTED. GROUNDED-YES. PERFORMED IGNITION SYSTEM TEST, IAW B737-800 AMM 74-00-00-750-801-F00. OPERATIONS CHECK GOOD. MANUALLY EXERSDR CHIA2020091064669Control Box · failedPILOT ACCOUNT: DURING FIRE FIGHTING MISSION, NR 2 ENGINE ROLLED BACK TO INTERMEDIATE SETTING (LESS THAT FLIGHT RPM WITH RRPM DECAY, ABOVE GROUND IDLE). THIS OCCURRED WHILE DROPPING WATER. EMERGENCY POWER WAS NECESSARY TO MAINTAIN RRPM. AFTER GAINING AIRSPEESDR QXEA2020090700276Control Quadrant · faultedDUE TO FAULTS CAPTURED IN A RECENT FHDB DOWNLOAD FOR INCREASING FAILURES OF THE THRUST CONTROL QUADRANT ALONG WITH A RECENT PILOT REPORT OF CAS MESSAGE ENG TLA NOT TOGO. REPLACE THE THRUST CONTROL QUADRANT, REF AMM TASKS 76-11-01-04 AND 76-11-01-05. REPLACESDR CHIA2020090624671Control Box · failedNR 2 ENGINE ROLLBACK ON APPROACH TO WATER SOURCE. ENGINE SECURED PER EMERGENCY ABNORMAL CHECKLIST. COULD NOT FIND ANY DEPENDENCY DURING T/S. REMOVED AND REPLACED NR 2 CONTROL BOX AND ACTUATOR FOR T/S. ALL SUBSEQUENT CHECKS GOOD AND AIRCRAFT RETURNED TO SER
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