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 SIMA20221205001I/O Module · faultedBLEED 1 FAIL DURING CLIMB THRU 17000 LOSS BLEED 1 AND 2 DECLARED EMERGENCY. C/W FIM 36-10-00-810-018-A FOUND TO BE TRANSITORY CONDITION OF GENERIC I/O MODULE 1 OK FOR SERVICESDR QXEA2022112900331Pump · leakingFOUND THE #1 ENGINE FUEL PUMP TO BE LEAKING. REMOVED FUEL PUMP IAW E-175 A,, TASK 73-11-01-000-801-A. INSTALLED SERVICEABLE PUMP IAW E175 AMM 73-11-01-400-401-A. LEAK CHECKS GOOD.SDR SIMA20221110004Engine · overspeedATO*E1 EXCEEDANCE ON T/O ROLL. PER GE TREND EXCEEDANCE ON TAKEOFF PILOT RECEIVED ITT EXCEEDANCE 985.624 FORE 4 SEC. AFTER RETURNING TO GATE AND FURTHER INVESTIGATION METAL WAS FOUND IN TAIL PIPE. REMOVE AND REPLACED ENGINESSDR 2022F00444Bolt · looseDURING THE ENGINE ENTRANCE INSPECTION, PERFORMED AT CEES AFTER RECEIVING THE ENGINE FROM AN EXTERNAL ORGANISATION PERFORMING ITS MAINTENANCE (STROTHER) TWO UNTIGHTENED BOLTS WERE FOUND, FIXING THE ENGINE COMPRESSOR CASE. BOLT 05-170 (SEE ATTACHMENT 193787_IPC_SDR 3CEY20221102F01Bolt · looseDURING THE ENGINE ENTRANCE INSPECTION, PERFORMED AT CEES AFTER RECEIVING THE ENGINE FROM THE EXTERNAL ORGANIZATION CARRYING OUT ITS MAINTENANCE (STROTHER), TWO UNTIGHTENED BOLTS WERE FOUND, FIXING THE ENGINE COMPRESSOR CASE. BOLT 05-170 (SEE ATTAHCMENT 193787_SDR R61A2022100600619Pressure Valve · leakingSMOKE/FUMES IN CABIN. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R PRV.SDR R61A2022070700428Engine · vibrationENG 2 LP VIBES AT 4.0. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. THIS WAS ALREADY BEING TRACKED ON A DEFERRAL.SDR R61A2022060800383Engine · smokeSMELL OF SMOKE (PERHAPS ELECTRICAL BURNING). DECLARED EMERGENCY, REJECTED TAKEOFF BELOW 80 KTS. VISIBLE LIGHT SMOKE IN COCKPIT. FA EMERGENCY CALL STATING VISIBLE SMOKE AND BURNING SMELL IN FWD CABIN. EMERGENCY EVAC SLIDES 1L, 2L, AND 2R BLOWN. EVACUATED. ACCOSDR R61A2022012600060Panel · crackedDURING HEAVY CHECK MAINTENANCE FOUND #1 ENGINE ANTI ICE EXHAUST PANEL RIB CRACKED. #1 ENGINE ANTI ICE EXHAUST PANEL RIB REPAIRED IAW ETD2021-170-007878.SDR QXEA2021092000443Blade · damagedAFTER TAKEOFF WE ENCOUNTERED A FLOCK OF BIRD 30 + NOSE AND LEFT SIDE OF AIRCRAFT ENGINE 1 VIB 1.5 - 2.0 LP 1.5 +- .5 HP. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. CLEANED EFFECTED AREA OF BIRD STRIKE. C/W BIRD STRIKE INSPECTION IAW E175 AMM SDR R61A2021082500670Bleed Valve · faultyBLEED 2 OVERPRESSURE MESSAGE AFTER TAKE-OFF. RAN QRH PROCEDURE, NO FIX RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE PLACED BLEED 2 ON MEL AND RETURNED THE AIRCRAFT TO SERVICE. THE RIGHT HAND NAPRSOV WAS REPLACED IN LGA ON 8/24/2021 CLEARING THSDR R61A2021071800577Bushing · crackedRH IB TRUST REVERSER FWD MOUNTING LUG BUSHING CRACKED. REMOVED AND REPLACED RH IB THRUST REVERSER FWD MOUNT LUG BUSHING IAW CMM 78-30-02SDR R61A2021063000523Blade · damagedE2 HIGH NOISE/VIBRATIONS. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. DISCOVERED TO BE DAMAGE FROM A BIRD STRIKE. R&R FAN BLADES 1, 14, 2, AND 15. OPS CHECK GOOD.SDR SWIA202157574Engine · bird ingestionBIRD STRIKE #2 ENGINE. OBVIOUS DAMAGED BLADES. (FLIGHT 3557 ) PERFORMED BIRD STRIKE INSPECTION PER AMM TASK 05-50-02-800-A. ONLY DAMAGE FOUND IS TO THE RIGHT ENGINE. SEE FOLLOWING DISCREPANCY FOR DAMAGE. / REMOVED AND REPLACED ALL 28 RT ENGINE FAN BLADSDR R61A2021040500316Oil System · leakingE1 PRESSURE DROPPED TO 28. OIL INDICATING 2.1 QUARTS IN FLIGHT PRIOR TO SHUTDOWN. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R #1 ENGINE, LEAK AND OPS CHECKED GOOD IAW 72-10-400-0001.SDR SIMA20210327002Engine · vibration#2 ENGINE LP VIBRATION IN AMBER. 4.0 AT 15,000 FT -24,000- DECLARED EMERGENCY-OVERWEIGHT LANDING 80,000 LBS - 100 FPM- EQP CHANGE FLT CONT. -C/A-DEFERRED PER GE MM REF LMM 72-21-00-800-806 TDMI AUTHORIZATION NUMBER 026T72122.NO INSPECTIONS NEEDED FOR SINK RATESDR R61A2021030300211Panel · crackedDURING HEAVY CHECK MAINTENANCE FOUND RH ENGINE PANEL 421DR SLOTTED FIN CRACKED. RH ENGINE PANEL 421DR REPAIRED IAW ETD2021-170-004899. A/C REMAINS IN CHECK.SDR R61A202101130029Engine · vibrationENGINE 2 LP VIBES AT 4.1. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED ENG 2 HIGH POWER RUNS, NO DEFECTS NOTED. PERFORMED VIBRATION RUNS, ALL INDICATIONS NORMAL.SDR SIMA20201209001Engine · vibrationENGINE 2 LP VIBRATION 4.0 IN FLIGHT. C/A: PERFORMED RT ENGINE FAN BLADES AND PINS-N1 VIB TROUBLESHOOTING, IAW WORK CARD EA72-00-00-012. OPERATIONAL CHECK GOOD.SDR QXEA2020102300304Warning Message · false activationSHORTLY AFTER TAKEOFF TWO MASTER CAUTIONS ILLUMINATED A-I ENGINE 1 FAIL AND A-I ENGINE 2 FAIL. RAN APPROPRIATE CHECKLISTS, BOTH CLEARED. NO FURTHER ISSUES. NOTE WE WERE APPROXIMATELY 2,000' ABOVE THE FIELD WHEN WE GOT THE CAUTIONS. REMOVED FROM SERVICE. NSDR R61A2020101900686Igniter · corrodedDURING HEAVY CHECK MAINTENANCE FOUND LT ENGINE BOTH IGNITERS ARE CORRODED. LT ENGINE HV IGNITER LT AND RT BOTH REPLACED, IAW LMM 74-00-00-800-808 AND 74-00-00-800-809. A/C REMAINS IN CHECK.SDR R61A2020092800651Actuator · faultedENGINE 1 CONTROL FAULT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R & R E1 SLAVE VG ACTUATOR.SDR SWIA202052771Structure · chafedRT ENGINE, INBOARD AND OUTBOARD CHEVRON TURKEY FEATHERS ARE CHAFED. C-CHECK RO 9/24/2020. REMOVED AND REPLACED RT ENGINE, INBOARD AND OUTBOARD CHEVRON TURKEY FEATHERS. SEE CONTINUATION CARD FOR STEPS PERFORMED, REF SRM.SDR 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 GTIA2020082035317Engine · contaminatedFUME EVENT DESCENDING THROUGH 12,000' STRONG ODOR IN CABIN, SLIGHT ODOR IN COCKPIT (PACKS A320 WITH MOD 31283/MP P7125 FWC H2-F1 STND) AND WITH MOD. 30626/MP K6443 (ENHANCED ECS) - FAULT CAUTIONS ASSOCIATED WITH OPERATIVE SIDE NOT DISPLAYED, REF TSM 05-50-00-8SDR QXEA2020081700246Engine · contaminatedSMELL NOTICED DURING INITIAL CLIMB OUT AND WENT AWAY AROUND 3000 FEET. AT DESCENT, WE NOTICED THE SMELL AGAIN WHEN THROTTLES WERE REDUCED TO FLIGHT IDLE. SMELL IN FLIGHT DECK WAS NOTICED ALL THE WAY TO THE GATE. FLIGHT ATTENDANTS REPORTED NO SMELLS WERE NOTSDR QXEA2020062300194Fadec · inoperativeENG 2 NO DISPATCH AND A/T FAIL ON LANDING. REMOVED FROM SERVICE. FOUND FAULT CODE 73216117E2B IN CMC. REPLACED #2 FADEC REF FIM TASK 72-00-00-810-804. NO FAULTS NOTED AFTER GROUND RUN OPS CHECK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR QXEA2020060700177Warning Message · false activationBLEED 1 FAIL CAUTION CAS MSG ON CLIMB-OUT PASSING 13000'. ACCOMPANIED BY BLEED 1 OFF ADVISORY. ACCOMPLISHED QRH BLEED 1 FAIL CAUTION CHECKLIST - RESOLVED. SAME CAUTION OCCURRED AGAIN THRU FL 310 QRH - RESOLVED. CABIN ALTITUDE HELD BETWEEN 6700 AND 6900 ENTIRE SDR QXEA2020021300096Fadec · malfunctionedDURING CRUISE LOST INDICATIONS FOR N1, N2, FUEL FLOW ON NUMBER ONE ENGINE. ALSO ELEV THR COMP FAIL ON ICAS. ALSO AUTOBRAKE FAIL ON ICAS. DIVERTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. REMOVED AND REPLACED #1 ENGINE FADEC PER EMB 175 AMM TASKS 73-21-01-00SDR 3CEY202002120001Mount · out of positionDURING ENGINE INDUCTION GVI ON FEB 11 2020, DURING PREPARATION FOR ON-WING INSTALLATION IT WAS FOUND THAT RH / LH YOKE ENGINE MOUNT FRONT FRAME AND RH / LH LINK ENGINE MOUNT HAVE BEEN SWAPPED - RH COMPONENTS WERE ON LH SIDE AND LH COMPONENTS WERE ON RH SIDE. ASDR SWIA202047986Panel · crackedRH ENGINE INLET ANTI EXHAUST PANEL 421DR HAS 4 CRACKED WELDS ON THE FINS. (C-CHECK) RO:1/22/2020TIG WELDED 4 CRACKED FINS USING ER 6AL-4V PO# 134200 REF CF34-8E MHD REPAIR SCHEME.SDR SWIA202047973Clamp · meltedLH ENGINE ADEL CLAMP IS MELTED ON THE INBOARD SIDE OF THE PRE-COOLER. (C-CHECK) RO:1/22/2020REMOVED AND REPLACED LH ENGINE ADEL CLAMP ON THE I/B SIDE OF THE PRE-COOLER PER SWPM TASK.SDR SWIA2020012047823Structure · crackedRACK - RH ENGINE - 421DR GRILL FIN IS CRACKED AT WELD. (C-CHECK) RO:1/14/2020PERFORMED WELD REPAIR OF CRACKED WELDS USING ER REF MHD REPAIR SCHEME AEMRS.SDR SWIA2020012047825Structure · crackedL/H ENGINE PANEL 411DR EXHAUST GRILL CRACKED AT WELD. (C-CHECK) RO:1/14/2020PERFORMED WELD REPAIR OF CRACKED WELDS USING ER REF MHD REPAIR SCHEME AEMRS.SDR QXEA2020010600007Warning Message · illuminated#2 ENG AT FL 370 (4.0) LP. RAN CHECKLIST REDUCED TO 3.9 NO ICING CONDITIONS AT 10,000' VIB 2.0. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. GROUND RAN ENGINES. #2 ENG LP DID NOT EXCEED .1 AND HP DID NOT EXCEED 1.5. NO FURTHER DEFECTS NOTED. NOSDR SIMA201912230004Engine · smokeENG 1 NO DISPATCH LARGE CLOUD OF SMOKE FROM ENG 1-C/A-AIRCRAFT RETURNED TO GATE WITH FAULT CODE 73216314E1B. TROUBLESHOT IAW FIM 73-21-00 SEPTS 1, 2, 3, AND 4. FOUND TO BE TRANSITORY CONDITION OF THE ENGINE EXCITER IGNITION ELECTRICAL CIRCUT. NO FURTHER DEFECTSDR QXEA2019120900447Engine · vibrationON DEPARTURE #2 ENGINE LP VIB INDICATOR WENT TO 4.0 YELLOW CONDITION. QRH DIDN'T WORK, VIB INTENSIFIED. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. PERFORMED GVI OF #2 ENGINE - NO EVIDENCE OF BIRDSTRIKE OR FOD. OBSERVED FAN ROTOR TURNS FREELY SDR QXEA2019112000423Pin · failed#1 ENGINE ABNORMAL VIBRATION ON LP FAN. 4.0 IN YELLOW. RAN CHECKLIST. REDUCTION IN POWER BROUGHT VIBRATION INTO NORMAL, INCREASE IN POWER AND LP TURNED YELLOW & 4.0. MAINTAINED LOWER ALTITUDE FL260 AND 290 KTS AND ABLE TO MAINTAIN NORMAL SPEC. NEGATIVE ICE ON SDR SWIA2019110846730Anti-Ice Valve · failedA-I ENG 1 FAIL CAUTION MESSAGE DURING CLIMB WHILE IN ICING CONDITIONS. RAN QRH, MESSAGE DID NOT CLEARREMOVED AND REPLACED #1 ENGINE ANTI-ICE VALVE IAW AMM. PERFORMED OPERATIONAL TEST OF THE LEFT ENGINE ANTI-ICING SYSTEM IAW AMM. OPS CHECK GOOD AND NO DEFECTS NSDR R61A2019110841217Engine · leakingSMOKEY HAZE REPORTED BY FA SHORTLY AFTER TAKEOFF. FAINT BURNT SMELL. DECLARED EMERGENCY, RETURNED TO BOS, LANDED WITHOUT INCIDENT. DEFERRED BOTH PACK 2 AND BLEED 2. CLEARED DEFERRALS WHEN PERFORMED COMPRESSOR BORESCOPE, CONTAMINATION FOUND. R&R E2 PER JC 72-10SDR SIMA2019103029003Engine · odorDURING DESCENT PASSING THROUGH 10K FT VERY STRONG SWEET LIKE ODOR FILLED FLIGHT DECK CA & FO FELT SINUS PROBLEMS AND DIZZINESS AFTER A FEW MINUTES OF EXPOSURE. REMOVED AND REPLACED THE RT ENGINE IAW WORK CARDS 71-00--01-000-801 AND 71-00-01-400-801. FCF FOUNDSDR R61A201910241163Engine · shutdownE1 SHUTDOWN IN FLIGHT. DECLARED EMERGENCY, DIVERTED TO BNA, LANDED WITHOUT INCIDENT. R&R LH ENGINE IAW JC 72-10-400-0001.SDR C77A2019102800003Engine · failedENG 1 FAIL ON CLIMBOUT. LOUD BANG NOISE FOLLOWED BY LOSS OF THRUST AND ENG 1 FAIL MSG.UPON LANDING MZ PERFORMED A BORESCOPE OF AND CONFIRMED HPT BLADES MISSING. ENGINE CHANGE IN PROGRESS AS SDR SUBMITTED. SUPPLIMENTAL SDR TO FOLLOWSDR C77A2019102300002Engine · vibrationENG 1 LP VIBE 4.0 IN FLIGHT, RAN QRH 6.18. DECLARED EMERGENCY AND DIVERTED TO PHX. LP VIBE IS CONTROLLABLE WITH REDUCED THRUST. SHOOK #1 ENG FAN BLADES. NO BLADES STICKING. CLEANED ACCELEROMETERS AND PERFORMED ENG VIB CHECK IAW LMM 72-00-00. OPS CHK GOOD OK FOSDR MASA2019101512091Bleed Valve · dirtyENG FUMES IN COCKPIT DURING TAKEOFF. CLEANED OIL OFF OF NA PRSOVSDR C77A2019102300001Engine · damagedLOUD BANG ON TAKE OFF WITH ENGINE EXCEEDANCE AFTER LANDING. ENG2 AT 993 DEGREES FOR 114 SECONDS. CA DECLARED AN EMERGENCY. AIRCRAFT RETURNED SAFELY TO RNO WHERE MAINTENANCE REPLACED THE #2 ENGINE AND RETURNED THE AIRCRAFT TO SERVICE.SDR SIMA20191002003Pressure Switch · malfunctionedNR 2 ENGINE, FUEL HAD LOW PRESSURE CAUTION AFTER TAKEOFF. PERFORMED FIM TASK 73-21-00-810-804-A IAW FIM. R & R FUEL LOW PRESSURE SWITCH IAW 77-00-00-800-803. PERFORMED FUEL SYSTEM LEAK CHECK IAW 72-00-00-790-001. LEAK AND OPS CHECKED GOOD.SDR QXEA2019073100295Bumper · out of positionAFTER TO #2 ENGINE LPVIB WENT TO 4.0. CLIMBED TO 21K, RAN ENGINE VIB CKLST. VIB WOULD GO BELOW 4.0 BUT WOULD RETURN TO 4.0 WHEN THRUST LEVER WAS ADVANCED. ON DESENT ENGINE VIB WOULD BE BETWEEN 3.0 & 1.0 DEPENDING ON TLA. DIVERTED. LANDING UNEVENTFUL. REMOVED FSDR QXEA2019071800264Engine · vibrationWHILE CLIMBING (APPROX FL190) THE #2 ENGINE EXPERIENCED AN ELEVATED ENGINE VIBRATION. ENGINE VIBRATION INDICATED 4.0 W/ REVERSE VIDEO IN AMBER. THE ENGINE VIBRATION ABNORMAL CHECKLIST PROVIDED GUIDANCE TO REDUCE THRUST ON THE #2 ENGINE. VIBRATION WENT BACK TO SDR QXEA2019071800265Blade · stiffRECEIVED AMBER ENG VIB LP 4.0 ENG 1 DURING CLIMB WITH CLIMB THRUST, LEVELED OFF AT FL 330. DESCENDED TO FL310. ENG 1 LP VIB 3.1 AT FL310. REMOVED FROM SERVICE. DETERMINED TO BE ABNORMAL N1 VIBRATION. C/W INSPECTIONS PER MCN E770001-01. FOUND 3 BLADES STIFF, LO
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