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 = '2612' 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 = '2612' 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 DALA12002340861Fire Warning · false activationAPU FIRE INDICATOR. RAN QRH PROCEDURE. CREW THEN DISCHARGED BOTH BOTTLES FOR APU. INSPECTED APU COMPARTMENT. NO FIRE DAMAGE OR EVIDENCE FOUND. RAN APU AND INSPECTED AREA. ALL CHECKS GOOD. REMOVED AND REPLACED BOTH FIRE BOTTLES.SDR UALA2012070103503Insulator · unsecureLEFT WING LOOP A FAULT. FOUND FIRE LOOP INSULATOR OUT OF CLAMP CAUSING METAL ON METAL CONTACT. RESECURED FIRE LOOP. OPS CHECKS GOOD.SDR HALA2012062900163Module · malfunctionedFIRE BELL WARNING AT 95 KTS ON TAKEOFF. ABORT EXERCISED. COULD NOT CANCEL/MUTE BELL CHIME AND NO VISUAL INDICATION NOTED. INSPECTED WIRING AT CONNECTOR D4349P & P51 PANEL DISCONNECTS, NO BENT OR PUSH BACK PINS. R & R M1000 BELL CHIME MODULE IAW AMM 31-51-SDR SWAA2012070205432Detector · faultyDIVERSION -- MOMENTARY WHEEL WELL FIRE INDICATION. NO SECONDARY INDICATIONS OF OVERHEAD OR IN WHEEL WELL. REMOVED AND REPLACED WHEEL WELL FIRE WARNING LOOP & WING TO BODY FAIRING OVERHEAD DETECTION UNIT PER MM.SDR CALA2012062700416Control Module · inoperativeNR 1 ENG OVERHEAT LIGHT ILLUMINATED. FOLLOWED QRH LIGHT REILLUMINATED. RETURNED, REMOVED & REPLACED FIRE DETECTION MODULE IAW AMM 26-10-01-401 & PERFORMED ENGINE FIRE DETECTION, OPS TEST AMM 26-1 1-00-710-801. OPS CHECKED GOOD.SDR FLHA20120626001Fire Warning · false activationABOUT 10 MINUTES AFTER TAKEOFF THE RIGHT ENGINE FIRE MESSAGE APPEARED AND THE CREW RETURNED THE RIGHT THROTTLE TO FLIGHT IDLE AND WITHIN 10 TO 12 SECONDS THE LIGHT EXTINGUISHED. RETURNED TO DEPARTURE AIRPORT WHICH WAS HOME BASE AND THE AIRCRAFT WAS INSPECTED SDR UALA2012062203392Fire Loop · faultyREF DF836, MEASURED 1.2K OHMS TO GND AT PIN 3 OF CONNECTOR D4154P REF WDM 26-11-44, ISOLATED TO UPPER AFT DETECTOR. REPLACED UPPER AFT FIRE LOOP DETECTOR PER AMM. ENGINE FIRE SYSTEM OPS TEST OK.SDR UALA2012062203377Pin · out of positionFIRE LOOP B FAULT DISPLAYED ON UPPER ECAM SCREEN.-ENGINE 2. ENGINE 2 FIRE LOOP B FAIL ECAM MSG PROG TEXT: ACCOMPLISH CHRONIC REVIEW. NR 2 FDU LAST LEG REPORT. (CHECK ENGINE 2 FIRE LOOP B 26-12-15). FLIGHT CREW REPORTS MESSAGE WAS INTERMITTENT. UPON ON ARSDR CA120702002Fire Detector · false activation(CAN) DURING REVENUE FLIGHT ON APPROACH TO AIRPORT, THE PILOTS NOTICED THE ENGINE NR 2 FIRE ALERT ILLUMINATED. THE PILOT DECIDED TO SHUTDOWN THE ENGINE AND RELEASED BOTH FIRE AGENT BOTTLES WHICH EXTINGUISHED THE ENGINE FIRE INDICATION, AND CONTINUED FOR A SAFSDR IPXA12674009Element · inoperativeLEFT DUCT LEAK LIGHT ILLUMINATED EICAS MESSAGE LEFT BLEED DUCT LEAK DISPLAYED. LIGHT EXTINGUISHED AFTER ENGINE BLEED AIR SUPPLY AND ISOLATION VALVE CLOSED. TROUBLESHOT IAW FIM 26-18-10, SSM 26-18-01,& WDM 26-18-11. REPLACED M691 DUCT LEAK & WW CARD. RAN BOSDR SWAA2012061805032Control Panel · faultyDIVERSION/EMERGENCY DECLARED -- MULTIPLE LIGHTS ILLUMINATED WITH SMELL IN FLIGHT DECK. REMOVED AND REPLACED ENGINE/APU FIRE CONTROL PANEL IAW MM.SDR J7SA20120614001Fire Warning · false activationRED EICAS MESSAGE APU FIRE, IN FLIGHT APPROX 13K DURING FLIGHT. PERFORMED OPS CHECK OF APU WITH NO DEFECTS NOTED.SDR J7SA201200614001Fire Warning · illuminatedRED EICAS MESSAGE, APU FIRE IN FLIGHT APPROX 13K DURING FLIGHT.SDR HEEA20120611075Fire Detector · false activationDURING CRUISE FLIGHT AT 8,500, NR 2 FIRE LIGHT ILLUMINATED WITH AUDIO. COURSE WAS ALTERED TO WEST AND A DESCENT MADE TO 6,500. ENGINE SECURED AND FIRE LIGHT REMAINED ILLUMINATED WITH AUDIO. FIRE BOTTLE WAS SELECTED AND FIRE LIGHT AND AUDIO EXTINGUISHED. SDR HEEA20120611048Detector · false activationAFTER LEVELING OFF, NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED WITH AURAL INDICATION. THEN WENT OUT. INDICATIONS RETURNED, AND WENT OUT AGAIN AND THIRD TIME STAYED ON. ENGINE SECURED AND EMERGENCY CHECKLIST FOLLOWED AND RETURNED TO DEPARTURE. INSPECTED WIRSDR FDEA201206082161Fire Detector · inaccurateFSS DISCHARGE 7L AND 7R TEMP READS 451 ON FSS PANEL BUT NO OTHER FIRE INDICATIONS. FSS PANEL SHOWED TEMP OF 451 DEGREES. EMERGENCY DECLARED, DIVERTED. COMPLIED WITH EA 1-2624-160811A. REACTIVATED MAIN DECK FIRE SUPPRESSION SYS.SDR QXEA2012060400421Amplifier · malfunctionedCHECK FIRE DET MASTER WARNING LIGHT ILLUMINATED IN FLIGHT WITH ASSOCIATED NR 1 FAULT A AND FAULT B LIGHTS ILLUMINATED. R & R FIRE CONTROL AMPLIFIER IAW AMM 26-10-01-000-801 AND 26-10-01-400-801. C/W OP TEST OF NACELLE FIRE DETECTION SYS, BAGGAGE SMOKE DETECTOSDR CALA2012060400389Fire Loop · damagedENGINE NR 2 OVERHEAT INDICATION ON CLIMBOUT CONSURTED QRH LIGHT WENT OUT AT IDLE POWER RETURNED TO LAS. T/S REF FIM 26-10 TASK 811 NO SIGN OF FIRE OR OVERHEAT HEATH CHECK GOOD MM 36-11-00. DID ENG BLEED SYS LEAK CHECK MM 36-11-00, NO LEAKS NOTED CONTROL MODUSDR UALA2012060303084Switch · damagedLEFT ENGINE OVERHEAT LIGHT DOES NOT ILLUMINATE DURING FIRE TESTS. REPLACED LEFT ENGINE OVERHEAT SWITCH BASE, FIRE TEST AND LIGHT TEST OK.SDR ASAA2012062892446Detector · failedAPU FIRE WARNING WILL NOT TEST. FOUND APU FIRE HARNESS CONNECTOR D40060P TO BE LOOSE. TIGHTENED CONNECTOR, OPS CK GOOD REF AMM 26-10-00. IMMEDIATELY REPEATED, APU DET INOP LIGHT ILLUMINATED. REPLACED APU LOWER OVERHEAT DETECTOR ASSY AS RECOMMENDED. OPS CK GSDR ASAA2012061492349Warning Light · false activationAPU OVERHEAT DETECTOR INOPERATIVE LIGHT ON WITH MASTER CAUTION. CAME ON AT 500 AND WENT OUT AT TOUCH DOWN. APU WAS NOT RUNNING. ACFT GROUNDED. PERFORMED FIM 26-10-00-810-801, ENF/APU FIRE DETECTIONS CONTROLLER MOD BITE PROCEDURE. PASSED SEVERAL TIMES. VISDR FDEA201206012043Fire Warning · illuminatedA LEVEL 3 CARGO FIRE LOWER FWD ILLUMINATED. PUSHED FLASHING DISCHARGE SWITCH, LANDED & ROLLED OUT TO FULL STOP. FIRE DEPTARTMENT REPORTED SLIGHT HEAT SIGNATURE ON LOWER FORWARD BELLY. ALL CHECKLIST COMPLETED.SDR DXTA2012060104982Fire Detector · false activationCARGO BAY FIRE WARNING ILLUMINATED DURING FLIGHT FOR 30 SECONDS THEN WENT OUT. NO FIRE, SMOKE, OR FUMES. ALL SMOKE DETECTORS TEST NORMAL. SYS OPS CHECKED GOOD IAW MM CH 26-10-00.SDR HALA2012053000151Circuit Card · failedACFT ARRIVED SAFELY, NR 1 & 2 FIRE BOTTLES FOR RT ENGINE WERE DISCHARGED BY THE FLT CREW DURING APPROACH. WHILE LINING UP FOR APPROACH RECEIVED "FIRE WARNING" ANNUNCIATION, FLT CREW DISCHARGED NR 1 BOTTLE. "WARNING DID NOT EXTINGUISH, THEN NR 2 BOTTLE DISCHSDR HEEA20120530987Flex Coupling · wornTHE NR 2 ENGINE FIRE LIGHT FLICKERED WITH FIRE ENG 2 AUDIO ABOUT HALF OF THE TIME. ACFT WAS CRUISING AT 6500 FT. DURING DESCENT THE FIRE LIGHT DID NOT FLICKER. NR 2 ENGINE OTBD LOWER AFT CABIN TUBE ASSY WAS REPLACED DUE TO WEAR.SDR HEEA20120528966Fire Detector · false activationDURING DESCENT FOR LANDING, THE NR 2 ENGINE FIRE WARNING AND AUDIO CAME ON FOR ABOUT 30 SECONDS 2 TIMES. FOUND THE NR 2 INBD FIRE DETECTOR FAILED.SDR HEEA20120524983Fire Detector · false activationTWENTY MINUTES FROM DESTINATION, FIRE LIGHT AND AUDIO TRIGGERED THREE TIMES WITH DURATION OF LESS THAN 5 SECONDS EACH TIME. ACFT RETURNED TO DEPARTURE WITH EIGHT MORE TRIGGERS ENROUTE TO BASE. NO OTHER INDICATIONS NOTED. AVIONICS TECH OHMED ALL WIRES IN SYSSDR ASAA12511594Fire Detector · inoperativeAPU FIRE DETECTOR INOPERATIVE LIGHT CAME ON INFLIGHT. ACFT GROUNDED. PERFORMED APU FIRE DET BITE, INDICATED TAIL PIPE DET FAULT. R & R APU TAILPIPE DETECTOR REF MM 26-15-01, OPS CHECK NORMAL.SDR UALA2012052502924Warning Light · illuminatedFIRE LOOP "A" FAULT DISPLAYED ON UPPER ECAM SCREEN, NR 2 ENGINE.SDR ASAA12511586Fire Warning · malfunctionedFIRE WARNING TEST FAIL, NO LIGHT, ENG 1 OVERHEAT AND NR 1 RED HANDLE LIGHT. ACFT GROUNDED. PERFORMED OPS TEST 26-11-00-710-801, STEP E. OPS NORMAL. PERFORMED BITE 26-10-00-810-801, NO FAULTS. NO RECENT HISTORY.SDR QMLA2012052212087Lamp · inoperativeNR 2 FIRE LIGHT MALFUNCTIONED. APPROX 15 MINUTES INTO A NIGHT FLIGHT, A DIM, ALMOST BACKLIGHT GLOW CAME ON THE NR 2 FIRE WARNING LIGHT. FIRE LIGHT DID NOT ILLUMINATE. ALL OTHER ENGINE INSTRUMENTS WERE NORMAL AND NO WARNING LIGHTS ON THE ANNUNCIATOR PANEL. SDR HALA2012052100143Fire Detector · false activationRIGHT ENGINE FIRE LP2 EICAS ILLUMINATED. PERFORMED FIM 26-11-00/101, FIG 104, ENGINE FIRE DETECTION SYS BITE PROCEDURE RESECURED COUPLINGS AT HIGH STAGE BLEED MANIFOLD LEAK CHECKED NORMAL AT NR 2 POS.SDR CA120523014Fire Warning · activatedCREW REPORTED AN AFT CARGO FIRE INDICATION, AND FIRE BOTTLE WAS DISCHARGE. MAINTENANCE WAS UNABLE TO FIND FAULT WITH DETECTION SYS. ALL SMOKE DETECTORS IN THE AFT CARGO PIT WHERE REPLACED ALSO DISCHARGED BOTTLE AND DRIER WERE REPLACED IAW MM. ON SUBSEQUENT SDR UALA2012051802812Circuit Card · faultedSTATUS MESSAGE 'RT ENG FIRE LP ONE' REPLACED CARD M683. OPS CHECKED OK.SDR IPXA12M73643Control Unit · malfunctionedAT APPROX 10 MINUTES INTO FLIGHT, THE FLIGHT CREW REPORTED NR 2 ENGINE FIRE INDICATION AND DIVERTED. 1 FIRE BOTTLE WAS BLOWN AND THE INDICATION WENT AWAY. DISCOVERED THE FAULT TO BE WITH IN THE NR 2 FDCU AND REPLACED IT IAW THE AMM. THE FIRE BOTTLE WAS REPSDR SWAA2012051604080Electronic Unit · faultyAIR TURNBACK/DECLARED EMERGENCY. AFT CARGO FIRE LIGHT FIRE BELL ILLUMINATED, SOUNDED CLIMBING THROUGH 17,000 FEET. PUSHED THE LIGHT & ACTIVATED THE AGENT DISCHARGE & LIGHT & BELL WENT OUT APPROX 5 MINS LATER FIRE LIGHT & BELL CAME BACK ON & REMAINED ON FOR ASDR HEEA20120514895Fire Detector · shortedACFT EXPERIENCED AN INFLIGHT FIRE WARNING HORN BUT NO WARNING LIGHT. FIRE BOTTLE WAS DISCHARGED INTO NR 1 ENGINE ON SHUTDOWN AS THE ENGINE PASSED 50 PERCENT AS DESIGNED. TROUBLESHOOTING REVEALED THE FWD FIRE DETECTOR TO HAVE A HIGH RESISTANCE SHORT. UNIT INSDR HALA2012051400139Fire Detector · malfunctionedAFTER PARKING, STATUS MESSAGE DISPLAYED RT ENGINE FIRE LOOP. AFTER A FEW MINUTES THE STAUS MESSAGE EXTINGUISHED. INSPECTED RT ENGINE FIRE LOOP WIRE HARNESS IAW WDM 26-11-21. NO DEFECTS NOTED. REPLACED RT ENGINE FIRE DETECTORS TS44, TS45, TS46 IAW AMM 26-11SDR HALA2012051400138Warning Message · false activationRECEIVED A STATUS MESSAGE "RT ENGINE FIRE LP 2". PERFORMED FIM 26-11-00/101 FIG 104. CHECKED RT ENG LP2 AND LP1 CONNECTIONS AND CLEANED. SECURITY/ATTACHMENT VERIFIED. OPERATION OF FIRE TEST NORMAL. REF AMM 26-11-00. STATUS MESSAGE EXTINGUISHED.SDR QXEA2012051300384Amplifier · malfunctionedWHILE ON DESCENT, RECEIVED A CHECK FIRE DETECTION WARNING LIGHT. THE APU BOTTLE LOW LIGHT FLICKERED. RESET THE MASTER WARNING LIGHT. THE CHECK FIRE DETECTION WARNING LIGHT EXTINGUISHED. AFTER A FEW SECONDS THE CHECK FIRE DETECTION WARNING LIGHT AGAIN FLASHSDR HALA2012051300137Circuit Card · malfunctionedRIGHT ENGINE FIRE LOOP, STATUS MESSAGE ILLUMINATED ON DECENT. EXTINGUISHED AFTER LANDING. CHECKED RESISTANCE AT M684, PINS 19 & 20 - 1.5 K OHMS. CHECKED INSULATION RESISTANCE BETWEEN PING 18 & 19, & PINS 18 & 20-54 OHMS. "SHAKE CHECKED" RT ENG FIRE LOOP HARNESDR QMLA2012051112077Fire Warning · false activationON ENGINE START, ENGINE FIRE LIGHT ILLUMINATED. IMMEDIATELY SHUT ENGINE DOWN. NO ENGINE FIRE WAS OBSERVED, ENGIE FIRE LIGHT REMAINED ILLUMINATED. COMPLETE ACFT SHUTDOWN, ACFT OUT OF SERVICE.SDR CLCA051020121Fire Warning · false activationDURING DESCENT TO MDSG, ENGINE 2 FIRE ALERT. ENGINE FIRE PROCEDURE EXECUTED PER QRH. CORRECTED ACTION (MDSG) INCLUDED VISUALLY INSPECTED NR 2 ENGINE FIRE SYSTEM IAW AMM 26 & PNEUMATIC DUCTS IAW MM 36-00-02. NO DEFECTS NOTED. SWAPPED FIRE BOTTLE FROM APU TO SDR VGCA201205100001Fire Loop · shortedINTERMITTENT FIRE WARNING.SDR UALA2012051102743Circuit Card · malfunctionedFIRE LOOP 2 RIGHT ENGINE FIRE DETECTION SYSTEM LOOP 2 FAILURE. STATUS MESSAGE 2610232 ACTIVE FL HARD: MAT SHOWS MESSAGE 26-10232 NOT ACTIVE. PERFORMED ENGINE/APU FIRE OVERHEAT TEST. TEST PASSED. REPLACED FIRE OVERHEAD DETECTION CARD. OPS OK.SDR UALA2012051102742Circuit Card · malfunctionedOVERHEAT CIRCUIT R2 RIGHT ENGINE OVERHEAT DETECTION CIRCUIT 2 FAILURE. STATUS MESSAGE 2610232 ACTIVE FL HARD: MAT SHOWS MESSAGE 26-10232 NOT ACTIVE. ENGINE/APU FIRE OVERHEAT TEST. TEST PASSED. REPLACED FIRE OVERHEAD DETECTION CARD (A10). OPS CHECKED OK.SDR ASOA201201601Warning Light · illuminatedAPU FIRE INDICATION ON LANDING FOLLOWING STRONG FUEL ODOR. EMERGENCY DECLARED. R & R APU FIRE BOTTLE AND SQUIB IAW AMM 26-22-10. OPS CHECKED GOOD.SDR EIAA20120506041Control Panel · malfunctionedAPU "A" FIRE LOOP INTERMITTENT WITH BELL. TROUBLESHOT SYSTEM FOUND "A" LOOP LIGHT ASSY HAS MASTER DIM/TEST TERMINAL BROKEN ON LIGHT ASSY IT'S SELF. LIGHT NR 6 PER WDM 26-15-11 DMI 543 CONTINUES. REMOVED AND REPLACED APU CONTROL PANEL PER AMM 31-10-00 SYSTESDR UALA2012051002700Fire Warning · false activationAFT CARGO FIRE WARNING ON, NO FIRE. DOWN POWERED AIRCRAFT MESSAGED ERASED. TESTED SYSTEM PER AMM 26-16-00.SDR ASAA12511506Fire Detector · inoperative"APU DET INOP" LIGHT IS ILLUMINATED. ACFT GROUNDED. PERFORMED APU FIRE DETECTOR CONTROL MODULE BITE IAW FIM 26-10, TASK 801. FAULTED APU TAILPIPE DETECTOR. RESISTANCE CHECK ON TAILPIPE DETECTOR IS 64 MEG OHMS. REPLACED APU DETECTOR WITH SERVICABLE ONE. ACCO
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