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 engine_model_key = 'CF348E5' 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 engine_model_key = 'CF348E5' 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 C77A273714Crossbeam · corrodedDURING BASIC CHECK NR1 INSP VISIT, FR17 CROSSFRAME 14 PN 170-21768-403. TEMPORARY REPAIR WAS ACCOMPLISHED IAW ETD2010-170/06961 AND COMPASS EO E175-53MR-040. PERMENANT REPAIR WILL BE ACCOMPLISHED AT NEXT BASIC CHECK WITH REPLACEMENT OF CROSSFRAME 14.SDR R61A20100396Slide · inoperativeMX REPORTED L-2 EMERGENCY EVACUATION SLIDE INOP, AND FOUND THE BUSTLE RETAINING PIN BEING AT FAULT. MX R & R L-2 EMERGENCY EVACUATION SLIDE IAW AMM.SDR UHLA2010080800157Seal · leakingCREW REPORTED BAD SMELL IN COCKPIT THROUGHOUT THE FLIGHT, AND GOT WORSE AS FLIGHT PROGRESSED. TURNED OFF PACK 1 BUT SMELL DID NOT SUBSIDE. MAINTENANCE RAN PACKS FOR 30 MINUTES AND DID NOT NOTICE ANY SMELL. PERFORMED HIGH POWER ENGINE RUNS AND FOUND NO OIL PSDR C77A296874Valve · malfunctionedHYD SYS 1 EXPERIENCED LOW QTY LEVELS IN FLIGHT. R & R MANUAL SAMPLE VALVE IAW AMM 29-11-10. OPS CHECK, LEAK CHECK GOOD.SDR C77A293595Battery Pack · dischargedWHILE TESTING THE EMERGENCY LIGHTING SYS, THE FIRST CLASS EMERGENCY LIGHTS DID NOT ILLUMINATE. TROUBLESHOT PROBLEM TO THE FWD/LT EMERGENCY LIGHT POWER UNIT. R & R IAW AMM 33-50-01-04. OPS CHECKED GOOD.SDR CA100929001Pressure Switch · failedFLIGHT CREW REPORTED AN "ENG 1 AND ENG 2 FIRE EXT BOTTLE B FAIL" MESSAGE ON EICAS. THE TEMP COMPENSATED PRESSURE SWITCH ASSY ON THE FIRE BOTTLE FAILED THE OPS TEST. SUSPECTED PRESSURE SWITCH ASSY TO BE CAUSE OF FAULT. FIRE BOTTLE ASSY REPLACED.SDR CA100708008Light · inoperative(CAN) LT FORWARD MAIN NAV LIGHT ASSEMBLY PN 30-2683-13 NOT ILLUMINATING. UPON INSPECTION THE BULB WAS SERVICEABLE, HOWEVER THE ASSEMBLY WIRES TO ENVIRONMENTAL SPLICE WERE FOUND OVERHEATED AND THE SECURING TYE-WRAPS WERE DISCOLORED AND BRITTLE INDICATING AN OVSDR C77A288395Coffeemaker · failedDURING CRUISE, DECLARED AN EMERGENCY & DIVERTED DUE TO A REPORT OF SMOKE IN THE AFT CABIN AREA. IN FLT, AFT F/A REALIZED THAT THEY HAD INADVERTENTLY TURNED ON THE AFT INBD COFFEEMAKER, WHICH WAS CURRENTLY ON MEL. F/A ADMITTED THAT THEY KNEW COFFEEMAKER WAS ONSDR UHLA2010062900075Seal · leakingSMOKE AND SMELL IN THE COCKPIT ON TAKEOFF ROLL. ABORTED TAKEOFF AND SMOKE QUICKLY DISSIPATED. TAKEOFF ABORTED BELOW 80KTS. MAINTENANCE REPLACED SEAL PRESSURE REGULATING VALVE PER GMM 72-00-00. RAN ENGINES AND NO SMOKE OR SMELL PRESENT. FLIGHT 7619, FIRST SDR C77A055010Fan Blade · bentBIRD STRIKES ON ENG 1, ENG 2, RADOME, NOSE GEAR, LT SIDE FUSELAGE, OVER WING, LT SIDE L/E WING, LT SIDE HORIZ STAB, ONLY DAMAGE FOUND WAS BEND BLADE ON NR 1 ENGINE, NO INDICATION OF CORE INGESTION. REPLACED MATCHED PAIR OF FAN BLADES IAW MM 72-00-00 SPEC PROCDSDR 2010F00129Battery Pack · dischargedAFT CABIN EMERGENCY LIGHTS STAYED ILLUMINATED WITH POWER OFF. R & R AFT/RT ELPU IAW AMM 33-50-01. OPS CHECK GOOD.SDR C77A276800Battery Pack · dischargedAFT CABIN EMERGENCY LIGHTS STAYED ILLUMINATED WITH POWER TURNED OFF. R & R AFT/RT BATTERY PACK IAW AMM 33-50-01. OPS CHECK GOOD.SDR C77A2768001Battery Pack · dischargedAFT CABIN EMERGENCY LIGHTS STAYED ILLUMINATED WITH POWER TURNED OFF. R & R AFT/LT ELPU IAW AMM 33-50-01. OPS CHECK GOOD.SDR CA100708009Light · inoperative(CAN) RT FORWARD MAIN NAV LIGHT ASSEMBLY PN 30-2683-14 NOT ILLUMINATING. UPON INSPECTION THE BULB WAS SERVICEABLE. HOWEVER, THE ASSEMBLY WIRES TO ENVIRONMENTAL SPLICE WERE FOUND OVERHEATED AND THE SECURING TYE-WRAPS WERE DISCOLORED AND BRITTLE INDICATING AN OSDR C77A257089Floor Support · corrodedDURING BASIC 1 INSPECTION, MX VISIT CORROSION WAS FOUND ON THE LT FLOOR TRACK, PN 170-03264-001 AT FR17,18, AND 19. PERMENENT REPAIR WAS ACCOMPLISHED IAW COMPASS EO E175-53MR-034 IR AND ETD2010/170/03710.SDR C77A257089AExtinguisher · misinstalledDURING BASIC CHECK MX VISIT, TESTING OF THE CARGO COMPARTMENT FIRE EXTINGUISHING SYS WAS SUCCSESSFULLY ACCOMPLISHED, REF TASK CARD 26-23-13-001-U. OPPORTUNITY INSPECTION WHILE ACCOMPLISHING THIS TASK REVEALED THAT THE HIGH RATE FIRE EXTINGUISHER (HRD) HAD THE SDR C77A268359Connector · damagedEMERGENCY EXIT SIGN AT RI DOOR WILL NOT ILLUMINATE. FOUND WIRE CONNECTOR AT WIRE NR W10204467-20 WITH PUSHED BACK PIN. RESECURRED PIN IN CONNECTOR. PERFORMED OPS TEST OF EMERGENCY LIGHTS IAW AMM 33-50-1. ALL SIGNS CK GOOD.SDR UHLA2010051400048Seat Track · corrodedLEVEL 2, CORROSION FRAME 17 AT RT SEAT TRACK BEAM TOP CAP. R & R BEAM IAW SRM 51-41-01 AND 51-43-01.SDR UHLA2010051200047Acm · smokeON CLIMB OUT , 3000 FT, F/A CALLED COCKPIT AND REPORTED A CLOUD OF SMOKE IN THE CABIN AND A BURNING SMELL. CAPTAIN DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. MX PERFORMED ENGINE RUNS AND FOUND NO EVIDENCE OF SMOKE OR SMELL IN CABIN. INSPECTED PACK 2 ANSDR UHLA2010051200049Shear Plate · corrodedLEVEL 2 CORROSION MIDDLE SHEAR PLATE BETWEEN FR87 AND FR88. R & R SHEAR PLATE IAW SRM 51-42-01.SDR UHLA2010051200050Shear Plate · corrodedLEVEL 2 CORROSION RT SHEAR PLATE BETWEEN FR87 AND FR88. R & R SHEAR PLATE IAW SRM 51-42-01.SDR C77A267189Sensor · defectiveSLAT FAIL MESSAGE ON TAKEOFF. SLATS WOULD NOT RETRACT. RETURNED TO DEPARTURE.SDR UHLA2010042900046Skin · crackedMAJOR REPAIR - VERTICAL STAB RT SIDE SKIN IS CRACKED JUST ABOVE AFT UPPER HOIST POINT. PERFORMED DEFINITIVE REPAIR ON RT UPPER VERT STAB IAW ETD2010-170/02797. REMOVED DAMAGED AREA IAW ETD, PERFORMED EDDY CURRENT ON CUTOUT, NO CRACK LINE INDICATIONS FOUND IAWSDR C77A260018Pressure Switch · faultyENGINE 2 FUEL LOW PRESS CAUTION MESSAGE. RAN QRH. PROCEEDED WITH NORMAL OPERATIONS. REPLACED NR 2 ENG FUEL LOW PRESSURE SWITCH IAW AMM 73-31-01. PERFORMED ENG RUN LEAK CHECK IAW GE ESM 72-00-00. ALL CHECKS GOOD.SDR C77A259116Control Module · failedLOST CONTROL OF NOSE WHEEL STEERING MOMENTARILY AND ACFT MOVED LT/ RT AND BACK TO CTR AT HIGH SPEED JUST PRIOR TO LIFT OFF. R & R STEERING HAND WHEEL IAW E175 AMM 32-53-05-04. OPS CHECK GOOD. ALSO PERFORMED DVDR AND FHDB DOWNLOAD FORWARD THEN TO MFG FOR ANASDR C77A255753Battery Pack · dischargedAFT EMERGENCY LIGHTS CAME ON, WHEN POWER WAS OFF AND EMERGENCY LIGHT SWITCH WAS OFF DURING SCHEDULED REPLACEMENT OF NEW BATTERIES. FOUND NEW BATTERY ON RT AFT POSITION DEFECTIVE. REMOVED AND REPLACED RT AFT ELPU IAW AMM 33-50-01, OPS CHECK OK.SDR C77A251094Floor Support · corrodedDURING BASIC CHECK INSP, CORROSION WAS FOUND ON LT FLOOR TRACK PN 170-03264-001 BETWEEN FR17 AND FR19 (BL265L). PERMANENT REPAIR WAS ACCOMPLISHED REF ETD 2010-170/02106 AND COMPASS EO E175-53MR-029.SDR C77A251402Power Supply · dischargedEMERGENCY EXIT LIGHT OVER MAIN CABIN DOOR IS INOP. INSTALLED NEW EMERGENCY LIGHT POWER UNIT IN THE NR 2 POSITION. NO FURTHER ISSUES WITH THE ACFT.SDR C77A249106Floor Support · corrodedDURING BASIC CHECK INSP, CORROSION WAS FOUND ON LT FLOORTRACK PN 170-03264-001 (BL265L) AT FR18. REPAIR WAS ACCOMPLISHED IAW ETD 2010-170/01968 AND COMPASS EO E175-53MR-028.SDR C77A248526Unknown · unknownON TAKE-OFF, AT V1 ACFT PULLED HARD TO THE LT. ON LANDING, NOTHING ABNORMAL NOTICED. MX PERFORMED NOSE GEAR STEERING INSP IAW AMM 32-49-01, NO DEFECTS NOTED ACFT OK FOR SERVICE AT THIS TIME. ALSO INTERROGATED CMC NO LATCHED MESSAGES.SDR UHLA2010031700023Engine · vibrationWAITING TO TAKEOFF CAPTAIN NOTICED A VIBRATION IN RUDDER PEDALS. NOTHING ABNORMAL NOTED. AT V1, HEARD A LOUD THUMP, THEN A CONTINUOUS LOUD NOISE AND VIBRATION. NO EICAS MESSAGES OR ANY OTHER INDICATIONS OF A PROBLEM. ASKED TO RETURN TO FIELD AND DECLARED ASDR C77A245851Battery · dischargedDURING ACFT POWER-DOWN IT WAS DISCOVERED THAT THE LOWER EMERGENCY EXIT SIGN NEAR THE R2 DOOR REMAINED ILLUMINATED WITH THE SWITCH IN THE "DISARMED" POSITION. TROUBLESHOOTING REVEALED A FAULTY NR 4 EMERGENCY LIGHT BATTERY (ELPU). BATTERY WAS REPLACED IAW AMM 33SDR C77A225873ABattery · dischargedAT THR R1 DOOR EMERGENCY EXIT LOWER LT LIGHT INOP DUE TO EMERGENCY BATTERY DISCHARGED.SDR C77A235118Floorbeam · corrodedDURING BASIC CHECK INSP MX VISIT CORROSION WAS FOUND ON FLOORBEAM PN 170-21766-409. PERMANENT REPAIR WAS MADE IAW ETD 2010-170/00794 AND COMPASS EO E175-53MR-023.SDR C77A230267A/C Pack · contaminatedACFT ABORTED TAKEOFF, SMOKE AND STRONG ODOR IN THE COCKPIT AND CABIN. THE ACFT HAD COMPRESSOR WASHES PERFORMED DURING OVERNIGHT MX AND RESIDUAL WASH FLUID WAS IN THE AIR CONDITIONING SYS. ENGINE DRY PROCEDURES WERE PERFORMED AND SMOKE AND ODOR WERE REMOVED FSDR 2010F00015Battery · failedWITH ACFT POWERED DOWN AND EMERGENCY LIGHTS SWITCH IN OFF POSITION, EMERGENCY LIGHTS IN FWD CABIN CAME ON.SDR UHLA2009122200147Fan Blade · damagedON TAKEOFF INGESTED BIRD IN NR 2 ENGINE. AFTER LEVELING OFF AT 3000 FEET, NOTICED HIGH LP ENGINE VIBES 4.2 ON NR 2 ENGINE. REDUCED THRUST UNTIL VIBES WERE NORMAL. NOTIFIED TOWER TO RETURN TO FIELD. ATC DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. MAINSDR CA091125008Clamp · broken(CAN) DURING REMOVAL OF OUR NR 1 PACK ACM FOUND TWO CLAMPS BROKEN OFF AND LAYING IN THE AIR CONDITIONING BAY BOTTOM. INSPECTED THE AREA AND FOUND THEM MISSING FROM THE PACK RAM AIR INLET SCOOPS LT AND RT. ALSO THE RUBBER BOOTS WHERE THE CLAMPS BELONG ARE TORSDR UHLA2009110200112Blade · lack of lubeIN CLIMB REACHING FL300, EXPERIENCED A HIGH ENGINE VIBRATION OF 4.0 ON THE LP NUMBER TWO ENGINE. FOLLOWED THE QRH PROCEDURE TO REDUCE THE THRUST ON THE NUMBER TWO ENGINE TO AROUND 75 N2. THIS BROUGHT THE INDICATION BACK TO THE GREEN AROUND 3.8. THEN ELECTEDSDR CA091029004Seal · deteriorated(CAN) ON COMPLETION OF A REGULAR SLAT TRACK LUBE, A SLIGHT `CLICKING` SOUND WAS NOTED DURING THE FINAL STEP OF A SLAT OPS CHECK. UPON INSPECTION IT WAS NOTED THAT THE SOUND WAS BEING CAUSED BY: 1- RT WING OTBD SEAL ON NR 4 SLAT IS WORN AND CRACKED. 2- RT WINGSDR 2009FA0000785Floor Support · corrodedDURING BASIC-1 CHECK MX VISIT, CORROSION WAS FOUND ON LT FLOOR TRACK BETWEEN FR 16-19. PN 170-03264-001. PERMANENT REPAIR WAS ACCOMPLISHED IAW IC2009-170/07126 AND COMPASS EO E175-53MR-010.SDR C772009F00000Frame · corrodedCORRODION AT BUTT SPLICES AT FRAMES 86,19, 14-18, 16-19, UNDER FLOOR. THESE ARE GALLEY/ENTRANCE WAY AREAS. THIS REPORT IS SUBMITTED DUE TO RECURRING PROBLEM. (K)SDR UHLA2009082800088Wire Harness · corrodedEVIDENCE OF CORROSION ON OVERBRAID LOCATED AT REAR OF RIGHT ENGINE PYLON AND EVIDENCE OF CHAFING. REMOVED AND REPLACED RT ENGINE W604 HARNESS IAW EMB 170 WM 73-21-50, AMM 20-10-01 AND IPC 24-02-73.SDR R61A20090027Compressor · damagedCREW REPORTED SEVERE VIBRATION, PARTIAL LOSS OF THRUST, AND E-1 CONTROL FAULT MSG DURING CRUISE TO PHL. CREW SHUTDOWN E-1 AND DECLARED EMERGENCY INTO MDT. LANDED WITHOUT INCIDENT, AND MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. MX PERFORMED BOROSCOPE ON E-1SDR R61A20090008Fan Blade · damagedON CLIMBOUT OF CLE CREW RECEIVED A RIGHT ENG VIB EXCEEDANCE OF 4.0. CREW FOLLOWED QRH AND SHUTDOWN ENGINE, DECLARED EMERGENCY INTO CMH. CMH MAINTENANCE FOUND SEVERAL FAN BLADES DAMAGED UPON INITIAL INSPECTION. ENGINE WAS BOROSCOPED, AND SEVERAL BLADE SETS RSDR UHLA2008110700003Engine · malfunctionedFLIGHT 5952 ATL-HPN ON FINAL APPROACH WITH GEAR DOWN AND FLAPS AT NR 5 POS, NR 2 ENG SPOOLED UP TO 80% UN-COMMANDED. CREW SHOT MISSED APPROACH. ON SECOND APPROACH AND SAME THING HAPPENED. CREW SHUT DOWN ENGINE. CREW DID NOT RECEIVE ANY MESSAGES IN AIR OR ON GRSDR R612008F00002Engine · malfunctionedDURING AC DESCENT CREW RECEIVED AN EICAS ENGINE CONTROL FAULT MESSAGE, AND ENGINE WAS DECELERATING. CREW FOLLOWED QRH PROCEDURES AND SHUTDOWN NR 2 ENGINE. DECLARED AN EMERGENCY LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO AC RESET POWER AND CLEARESDR R612008F00003Engine · power lossDURING AC DESCENT, CREW RECEIVED AN EICAS ENGINE CONTROL FAULT MESSAGE AND ENGINE WAS DECELERATING. CREW FOLLOWED QRH PROCEDURES AND SHUTDOWN NR 2 ENGINE. DECLARED AN EMERGENCY LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO AC RESET POWER AND CLEARESDR R612008F00000Sensor · failedCREW RECEIVED A SLAT FAIL MESSAGE ON APPROACH DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT TO EVALUATE. MAINTENANCE REMOVED AND REPLACED LT OB SLAT SKEW SENSOR SYSTEM OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURSDR R612008F00005Software · failedCREW REPORTED DURING CRUISE FLIGHT NUMBER 2 ENGINE HAD A HIGH VIBRATION MESSAGE. CREW FOLLOWED QRH PROCEDURE SHUTDOWN NR 2 ENGINE AND THEN DIVERTED TO PITTSBURGH LANDED WITHOUT INCIDENT, TAXIED TO GATE MAINTENANCE WAS DISPATCHED TO A/C. MAINTENANCE TROUBLESH
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