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 SIMA20190713001Warning System · activatedCLIMBING THROUGH FL220 ENG 2 LP VIBE AMBER AT 4.0. LEVELED OFF REDUCED THRUST PER QRH AND ENG 2 VIBE REDUCED TO GREEN, MID 3.4-3.6 AT 79% N1. UNABLE TO MAINTAIN MAX THRUST AND STAY GREEN. "TRANSFERRED TO NRWC 042-ORD-01186". C/A-REF NRWC 042T01186 FOR ACTION TSDR CA190702021Buss Bar · shorted(CAN) REPORTED A CHEMICAL/CHLORINE SMELL DURING THE CLIMB FROM FL180-FL250. IT DISSIPATED AFTER 5 MINUTES AND DID NOT RETURN. MAINTENANCE MET THE A/C ON ARRIVAL AND THE SMELL WAS STILL PRESENT IN THE FLIGHT DECK, IT APPEARED TO RESEMBLE AN ELECTRICAL BURNINGSDR CA190702020Flex Hose · worn(CAN) UPON ARRIVAL THE AIRCRAFT HAD `HYD 2 LO PRESS` CAUTION MSG DISPLAY ON THEIR EICAS. UPON INITIAL INSPECTION A LARGE PUDDLE OF HYDRAULIC FLUID WAS FOUND AROUND THE RH MLG STRUT AND WHEEL WELL AREA. MAINTENANCE RAN #2 HYDRAULIC SYSTEM MOMENTARILY AND IT BECSDR QXEA2019051300209Engine · vibrationNR 2 ENGINE LP VIBRATION EXCEEDED 4.0 DURING CLIMB AND ENTERED AMBER CAUTION RANGE. RE-ENTERED NORMAL RANGE DURING DECENT APPROACH AND LANDING. AT FL330 VIBRATION LEVEL REMAINED IN AMBER CAUTION RANGE FOR 5 MINUTES AT CRUISE THRUST SETTING. ENTERED CAUTION RANSDR CA190502012Oven · failed(CAN) OCM ADVISED MOC THAT FLT WAS DIVERTING DUE TO SMOKE/BURNING ODOR IN AFT GALLEY/CABIN. OVEN OPERATED FOR SEVERAL MINUTES AND ELECTRICAL BURNING ODOR WAS OBSERVED. MAINT OPENED OVEN COMPARTMENT DOOR AND THE SMELL WASN`T VERY STRONG. MAINT REMOVED OVEN CONTSDR SIMA20190420002Engine · vibrationNUMBER ONE ENGINE LP VIB AMBER 4.0 IN FLIGHT APPROX 14,000 FT IN CLIMB ,COMPLIED W/QRH PROCEDURE , POWER REDUCTION TO 75% N1 NESSORY TO BRING LP BACK TO GREEN RANGE ,DID NOT OCCURE WHILT TL WAS IN MOTION ,DID NOT OCCURE WHILE IN ICING CONDITIONS.-C/A-COMPLIED SDR C77A2019040100001Pump · failedIN CRUISE A NR 2 ENGINE LO OIL PRESSURE EICAS MESSAGE WAS RECEIVED FOLLOWED BY LO OIL QUANTITY MSG. FLT CREW SECURED #2 ENGINE & DIVERTED TO SMF DECLARING AN EMERGENCY. ENG 2 PEAK 17 SEC 546 (ENG EXCEEDANCE). MX INSPECTED #2 ENG FOR EXTERNAL OIL LEAKS-FOUND NOSDR R61A201901310145Engine · shutdownENGINE 1 AUTO SHUTDOWN ON ROTATION. DECLARED EMERGENCY, RETURNED TO FIELD, LANDED WITHOUT INCIDENT. R&R E1 IAW 72-10-400-001. OPS AND LEAK CHECK GOOD.SDR R61A2019020130141Connector · dirtyENGINE 1 CONTROL FAULT AND E1 NO DISPATCH EICAS MESSAGE. DECLARED EMERGENCY, RETURNED TO FIELD, LANDED WITHOUT INCIDENT. PERFORMED FIM 72-00-00-810-123 AND CLEANED MASTER VG ACTUATOR CANNON PLUGS. PERFORMED ENGINE RUNS ON BOTH CHANNELS, OPS CHECK GOOD.SDR MASA2019010311634Engine · failedEMERGENCY DECLARED DUE LT ENGINE FAIL IN FLT IN ICING.SDR R61A2018121711242Engine · vibrationON CLIMB OUT THROUGH FL150 E1 STARTED VIBRATING, N1 WENT TO 0% AND ITT WENT RED TO 1008 FOR A COUPLE SECONDS WITH HIGH VIBE 4.1 FOR 2 SECONDS. CREW PERFORMED ENGINE FIRE SEVERE DAMAGE QRC PROCEDURE AND SECURED MOTOR AND FIRED #1 BOTTLE. DECLARED EMERGENCY AND SDR C77A2018111500001Wire Harness · shortedCREW REPORTED A LOSS OF POWER WITH AC AND DC BUS 1 FAIL AND AVNX MAU FAIL, ALONG WITH ALL ASSOCIATED COMPONENTS. CREW DECLARED AN EMERGENCY AND STARTED THE APU WITH NO RAT DEPLOYMENT AND NO ENGINE ISSUES. LANDED SAFELY AND WAS TOWED TO THE GATE. PERFORMED MX ESDR R61A2018110841122Pressure Valve · leakingSTRONG "OIL" BURNING SMELL IN CABIN IMMEDIATELY AFTER TAKEOFF. RAN QRC/QRH FOR RETURN TO FIELD. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R E2 SEAL PRESSURE REGULATOR VALVE PER GE LMM 75-00-00 SP 008.SDR SWIA2018103145191Vane · crackedPANEL 411DR VANE IS CRACKED AT THE WELD. (C-CHECK) RO: 10/24/2018. TIG WELDED CRACK REF MM.SDR SWIA2018103145192Vane · crackedPANEL 421DR VANE IS CRACKED AT THE WELD.(C-CHECK) RO: 10/24/2018. TIG WELDED CRACK REF MM.SDR QXEA2018092800352Engine · vibration#1 ENGINE VIB CAUTION DURING CRUISE FLT @ 350 VIB @ 4.0 FOLLOWED CHECKLIST. VIB RETURNED TO NORMAL RANGE W/ N1 REDUX TO 84 ON #1 ENG. AIRCRAFT DID NOT ENCOUNTER ICING CONDITIONS DURING FLT. REMOVED FROM SERVICE. C/W E175 LMM TASK 72-00-00-810-803 SUBTASK 72-00SDR CA180823005Contactor · burned(CAN) FLIGHT CREW REPORTED THAT HYD LOW PRESS INDICATION ON EICAS AND CB TRIPPED AFTER PUSH BACK. MAINTENANCE INVESTIGATED AND FOUND ONE OF CONTACT ON HYD NR 2 PUMP CONTACTOR SHORTED IN LICC. LICC WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. (TC# 201808230SDR R61A2018081080851Connector · dirtyNR 2 ENGINE LP VIBRATION AT 4.0, DURING CRUISE, BUT ONLY FOR 5 SECONDS. THIS HAPPENED SEVERAL TIMES WHILE AT CRUISE. DURING DESCENT, VIBRATION WENT TO 4 WITH DESCENT POWER. AT 8,000 FEET, NR 2 ENGINE LP VIBRATION WHEN TO 4.1 AND PEAKED AT 4.4 BY THE TIME TSDR MASA2018071013401Pin · wornRETURNED TO THE FIELD AND DECLARED AN EMERGENCY DUE TO NR 2 ENG N1 VIBE IN CLIMB FLIGHT. MX REPLACED SOME WORN BLADE PINS AND PERFORMED A BLADE LUBE.SDR SIMA20180623002Engine · failedE1 FAIL AT 8700 FEET IN CLB - 1 POWER. REMOVED AND REPLACED LT ENG IAW W/C 71-00-01-400-801. ENG OPERATES CORRECTLY AFTER PERFORMANCE RUNS. REF AMM TASK 71-00-01-710-801-A/500.SDR C77A2018062100001Actuator · failedCREW RECEIVED A NR 2 ENGINE CONTROL FAULT MESSAGE DURING DESCENT. DECLARED AN EMERGENCY. ENGINE PULL BACK TO IDLE FOR LANDING. LANDED SAFELY AND TAXIIED OFF RUNWAY. NR 2 ENGINE CONTROL FAULT EICAS MESSAGE DURING LANDING AT IDLE THRUST. REMOVED THE SLAVE SDR QXEA2018060400211Engine · vibrationOBSERVED THE NR 1 ENGINE VIBRATION LP 3.0 AT TAKEOFF ROLL. MONITORED VIBRATION DURING CLIMB, AND AS THE AIRCRAFT CLIMBED THROUGH FL250 FT, OBSERVED THE NR 1 LP VIBRATION TURN AMBER AND INDICATED 4.0 AU OTHER ENGINE PERIMETERS INDICATED NORMAL. COMPLIED WITH SDR SIMA20180529005Retainer · damagedNR 1 ENGINE LP VIBRATION INDICATED AMBER AND 4.0. ABNORMAL INDICATION REMAINED AFTER COMPLYING WITH APPROPIATE CHECKLISTS, INCLUDING A REDUCED THRUST SETTING. REPLACED NR 1 ENGINE FAN BLADES IAW EA72-00-00-011, OPS CHECKED GOOD. REPLACED THE NR 1 ENGINE FANSDR QXEA2018043000165Engine · contaminatedBURNING ODOR IN CABIN AND FLIGHT DECK, NO VISUALLY SIGNS OF SMOKE. ALL BLEEDS NORMAL. RETURNED TO FIELD. REMOVED FROM SERVICE. COMPLIED WITH FIM 21-20-00-810-802. AS A PRECAUTION, PREFORMED ENGINE PRFORMANCE RECOVERY WASH POST RUNS IAW MM 72-00-00, CLESDR QXEA2018032100107Pin · stuckDURING CLIMB, THE NR 2 ENGINE LP VIBRATION READ AMBER 4.0. IAW THE ABNORMAL CHECKLIST, DISCONNECTED THE AUTO THROTTLE, REDUCED POWER. LP READING RETURNED TO NORMAL, GREEN READING. OPERATED WITH THE AUTO THROTTLE OFF FOR THE REMAINDER OF THE FLIGHT. THSDR QXEA2017122700713Exciter · faultedDURING NR 1 ENGINE START, AN ENGINE SHORT TERM DISPATCH ADVISORY MESSAGE POSTED. MESSAGE CLEARED DURING ENGINE SHUTDOWN. ENGINE FADEC SYSTEM SYSTEM FAULTS, FAILED A IGNITOR. R & R THE NR 1 ENG LEFT EXCITER BOX IAW AMM 74-11-01-000/400-801-A. STATIC CHECSDR SWIA201744008Fmu · failedWHILE IN CRUISE AT FL34, RT ENGINE ACCELERATED, DISCONNECTED AUTOTHROTTLE, NO CHANGE, ENGINE DID NOT RESPOND TO THE THRUST LEVER INPUTS, PERFORMED A NORMAL ENGINE SHUTDOWN IAW QRH. CLEANED THE RT ENGINE HARNESS CONNECTIONS AT THE FMU, OBV, N2 SPEED SENSOR, ASDR QXEA2017101700627Engine · leakingDURING CRUISE, A PASSENGER NOTED FLUID LEAKING AROUND RIGHT ENGINE PYLON. PILOTS CHECKED AND IT APPEARS TO BE FUEL. DIVERTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE.SDR SIMA20171010001Warning Message · false activationNR 2 ENGING VIBRATION WENT TO 4.0 , AMBER DURING TAKEOFF. TOOK A LARGE POWER REDUCTION TO KEEP OUT OF AMBER VIBRATION. RETUREND TO AMBER AT LOW THRUST AS WELL ON DESCENT. PERFORMED AN OPS CHECK ON THE NR 2 ENGINE IAW ETN EJ-72-004, SECTION E, WITHIN LIMSDR MASA2017100212682Engine · vibrationEMERGENCY DECLARED AND DIVERTED DUE TO A NR 2 ENGINE N2 VIBRATION 4.0. OPENSDR SIMA20170927001Blades · stuckVIBRATION IN AMBER RANGE FOR THE NR 1 ENGINE DURING CLIMBING OUT. REDUCED THRUST & COMPLIED WITH QRH TO KEEP ENGINE PARAMETERS IN LIMITS. FOLLOWED ETN-EJ-72-004 FOUND TWO FAN BLADES STICKING AT POS 20 AND 21. EXERCISED BLADES WHICH ARE FREE AT THIS TIME. PSDR SIMA20170923002Engine · damagedRT ENGINE FAN DISK EXHIBITS FORE AND AFT MOVEMENT OF APPROXIMATELY .040 INCH. REMOVED AND REPLACED OF RT ENGINE IAW W/C 71-00-01-00-801 AND W/C 71-00-01-400-801.SDR SIMA20170716002Engine · power lossON TAKE -OFF ROLL AT APPROXIMATLY 80 KTS E1 TLA NOT TOGA. E1 TOGA. PERFORMED AUTOTHROTTLE FUNCTION OP CHECK IAW AMM 22-31-00. OP CHECKS GOOD. BRK OVERHEAT AFTER REJECTING TAKE-OFF. RIGHT NR 2 SIDE AMBER. PERFORMED BRAKE OVERHEAT INSPECTION IAW 05-50-12-200-SDR SIMA20170625001Warning Message · false indicationLEVELING OFF AT FL370, E1 LPVIB IND 4.0, REDUCED THROTTLE AND IT REDUCED TO 3.0. RAN THE QRH CHECKLIST AND MADE PRECAUTIONARY LANDING. PERFORMED ESM 72-00-00 SUBTASK 72-00-00-700-801. FOUND THE NR 1 ENGINE TO BE OPERATING WITHIN LIMITS. OPS CHECKED GOOD.SDR SIMA20170614002Blade · damagedNR 2 ENGINE LP VIBRATION WENT AMBER AT 4.0 AND 34000FT. COMPLIED WITH N1 VIBRATION WORKSCOPE ON RT ENGINE IAW MM 72-00-00 SPECIAL PROCEDURE 097. MAX LP VIBRATION LEVEL NOW 1.5 AU. DURING ACCOMPLISHEMENT OF N1 VIBRATION WORKSCOPE ON RT ENGINE, FOUND BASE COATSDR SIMA20170606006Blades · dirtyPASSING THROUGH APPROXIMATELY 27000 FT WHILE CLIMBING, THE NR 2 LP VIBRATION INDICATOR WAS AT 4.0 IN THE CAUTION RANGE. REDUCED N1 TO 77% BEFORE INDICATION WENT GREEN. RAN CHECKLIST AND PERFORMED A PERCAUTIONARY ENGINE SHUTDOWN IAW ENGINE ABNORMAL VIBRATIONSDR SIMA20170516001Pin · unknown15000 FEET, 89 PERCENT N1, 4.0 VIBRATION NORMAL AT CRUISE, NR 1 ENGINE BELOW LANDING WT74300 MAX LANDING. REMOVED AND REPLACED FAN BLADE RETAINING PINS IAW ESM 72-00-00 SPECIAL PROCEDURES 096.SDR SIMA20170513001Engine · vibrationDURING CLIMB, NR 1 ENGINE LP VIBRATION WENT TO 4.0, IAW QRH REDUCED THRUST ON ENGINE SETTING JUST ABOVE IDLE. RESULTED IN AMBER READING. PERFOMED EMERGENCY LANDING. PERFORMED MAINTENANCE FOR ENGINE VIBRATION TASK 72-00-00. OPS CHECKED GOOD.SDR SIMA20170503001Blades · out of balanceDURING CLIMB, NR 2 ENGINE VIBRATION REACHED AMBER AT 4.0 . ENGINE VIBRATION PEAKED AT 4.0 ON APPROACH AT 40% N1 WITH NOTICEABLE AIRFRAME VIBRATION. PERFORMED N1 VIBRATION WORKSCOPE ON RT ENGINE IAW MM 72-00-00 SPEC. PROC. 097. REMOVED AND REPLACED ALL FAN BSDR C77A20170502002Engine · faultedDURING LANDING, THE CREW SLOWED TO 210KTS, CAUSING THRUST TO REDUCE TO IDLE, ONCE AT IDLE A NR 2 ENGINE CONTROL FAULT MESSAGE APPEARED. THE CREW RAN THE QRH AND THE ENGINE WAS UNRESPONSIVE AND WAS STABLIZED IN AN IDLE. DECLARED AN EMERGENCY. A SINGLE ENGINE LASDR UHLA201612040505Oil System · low pressureNR 1 ENGINE LOW OIL PRESSURE IN FLIGHT. EXECUTED INFLIGHT SHUTDOWN PROCEDURE QRH 6-28. DECLARED EMERGENCY, DIVERTED AND LANDED WITHOUT INCIDENT. R & R THE NR1 ENGINE.SDR ASCB201611080001Valve · failedTHE AFT LT DOOR SLIDE FAILED THE OPERATIONAL CHECK. THE FAILURE WAS A RESULT OF FAILED VALVE WHICH WAS SEPARATED AT THE RIVET JOINT WHICH SEEMED TO BE A RESULT OF THE VALVE NOT SUSTAINING THE PRESSURESDR C77A20161027002Engine · vibrationAFTER TAKEOFF, THE CREW EXPERIENCED A VIBRATION IN THE AMBER INDICATION ON THE NR 1 ENGINE. AIRCRAFT RETURNED TO DEPARTURE. DECLARED AN EMERGENCY. THROTTLE RETARDED AND VIBRATION DECREASED. VIBRATION INCREASED WHEN THROTTLE ADVANCED. NO VIBRATION FELT. 72-0SDR UHLA201609150440Engine · auto shutdownNR 1 ENGINE AUTO SHUTDOWN. LOUD BANG, OIL WAS GOOD, NO VIBRATION. ATTEMPTED RESTART, N1 READING WHEN WINDMILLING. AFTER START, CREW HEARD NOISE, ITT FLUCTUATED 4-500, THEN PROCEEDED TO CHECKLIST FOR SHUTDOWN. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R & R SDR C77A20160523001Tire · separatedSUFFERED LT INBD MAIN TIRE TREAD SEPARATION, WHICH RESULTED IN THE FOLLOWING OBSERVED DAMAGES. LT INBD AFT FLAP, PN 170-39011-411, THROUGH DAMAGE, 8 INCHES IN LENGTH BY 1/8 INCH IN WIDTH ON THE BOTTOM OF THE FLAP. ONLY PASSES THROUGH THE BOTTOM OF THE FLAP CSDR C77A20160404025Engine · bird ingestionENGINE BIRD INGESTION ON CLIMB OUT. CREW NOTED ABNORMAL ENG INDICATIONS & VIBRATIONS. CREW DECLARED EMER & RETURNED. ENG WAS NOT SHUTDOWN. LANDED & TAXIED TO GATE NORMAL. NO PAX NOR CREW INJURIES. COMPLIED WITH A BIRD STRIKE INSPECTION IAW AMM 05-50-02 WSDR C77A20160325012Engine · failedENGINE FAIL CASS MSG. ENG AUTOMATICALLY SHUT DOWN IN FLIGHT.SDR UHLA201603110113Engine · failedPASSING THROUGH 11,000 FT, HEARD A LOUD BANG AND HAD AN ENGINE FAILURE OF THE NR 1 ENGINE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R & R THE NR 1 ENGINE IAW CR72-10-400-0001.SDR MASA2016022612771Unknown · failedMULTIPLE SYSTEM FAILURES AT 8,000 FT AND LOST BOTH ENGINE DATA. RESET POWER TO MAU 3.SDR CA160226001Windshield · failed(CAN) PILOTS WINDSHIELED SHATTERED DURING THE APPROACH. AIRCRAFT PROCEEDED TO LAND SAFELY. UPON REMOVAL OF THE SHATTERED WINDSHIELD THERE IS EVIDENCE OF ARCING. NEW WINDSHIELD INSTALLED AND AIRCRAFT RETURNED TO SERVICE.
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