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 = 'CF3410E6' 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 = 'CF3410E6' 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 RJEF20150513001Gcu · inoperativeAFTER LANDING AS FLIGHT TAI 536, THE PILOT REPORTED DC BUS 2 OFF DUE TO TR 2 FAILURE. IAW FIM 24-31-00-810-806-A & AMM 24-21-19-000 400-801-A THE GCU NR 2 WAS REPLACED. THE APPLICABLE OPERATIONAL TEST PERFORMED WITH NO FAILURE MSGS. ONCE THE CORRECTIVE MX ASDR RJEF20150411001Circuit Card · unserviceableDURING FLIGHT TAI 425, THE PILOT REPORTED AMS CTRL FAIL MSG ON EICAS AT FL370. THEREFORE, THE FLIGHT WAS DIVERTED TO ITS ALTERNATE AIRPORT. NO OWL WAS REPORTED. REPLACED THE AMS CONTROLLER CHA 1 & CHA 2 IAW FIM 21-00-00-810-805-A & AMM 21-00-01-000 400-801-SDR RJEF20150313001Seal · damagedDURING THE CLIMBING PHASE OF FLIGHT, THE ACFT DISPLAYED LANDING GEAR WOW FAILURE MESSAGE, DIVERTED. UNEVENTFUL LANDING. THE NLG SHOCK STRUT SEALS WERE DAMAGED. REPLACED IAW AMM 32-21-04-000 400-801A. AFTER SERVICING THE NLG, NLG RETRACTION & EXTENSION TESTSDR SOKF20150210001Controller · malfunctionedAFTER TAKEOFF, THE ACFT RETURNED DUE EICAS MSG CABIN ALTITUDE HI. ON GND PERFORMED FIM 21-31-00-810-822-A. R & R CPCS IAW AMM 21-31-01. OPERATIONAL TESTED OK. THE ACFT RETURNED TO NORMAL OPERATION.SDR SOKF20141117001Bellows · damagedDURING FLIGHT THE ACFT DIVERTED DUE WHILE A FL 350, CABIN ALTITUDE RAISED UP TO 9600FT. WHILE ON DESCENT CABIN ALTITUDE KEPT RISING. IAW FIM 21-31-00-810-824-A PERFORMED LT & RT AIR CONDITIONING PACK'S INSPECTION & FOUND RT PACK BELLOWS FROM PACK OUTLET DUCTSDR SOKF20141113Bleed Air Sys · malfunctionedDURING CLIMB, THE ACFT RETURNED DUE BLEED 2 OVER PRESS MSG DISPLAYED ON CAS, STATION WAS ENTERED BLEED SYS AS DMI MEL IAW 36.00.00.1. THE ACFT RETURN TO NORMAL OPERATION.SDR RJEF20141112001Compressor · bird ingestionDURING APPROACH, THE PILOT REPORTED A BIRD STRIKE ON ENG 2 & SMOKE FROM ENG 2 EXHAUST WAS NOTED. ENG 2 WAS SHUTDOWN INFLIGHT & THE ACFT WAS RETURNED. NO OVERWEIGHT LANDING WAS REPORTED.
PERFORMED AIRCRAFT VISUAL INSPECTION FOR FOD PER AMM 05-50-02-200-801SDR RJEF20141031002Door · out of adjustDURING CLIMB, THE PILOT REPORTED STRONG NOISE FROM THE NOSE SECTION. THE ACFT RETURNED FOR AN UNEVENTFUL LANDING. PERFORMED THE CABIN PRESSURIZATION LEAKAGE TEST USING APU AS PNEUMATIC SOURCE, AMM TASK 21-31-00-720-802-A/500 & A GENERAL VISUAL INSPECTION ONSDR RJEF20141030001Structure · dentedPREVIOUS TO DEPARTURE, MX FOUND A DENT ON THE LOWER EDGE OF THE AFT SERVICE DOOR, THE DAMAGE IS OUT OF THE SCOPE OF THE SRM. CONTACTED THE MANUFACTURER WHO PROVIDED INSTRUCTIONS TO PERFORM A DRESS BACK OF THE DENT TO THE ORIGINAL CONTOUR BY COLD FORMING & TESSDR YENA20140819163Engine · vibrationNR 1 ENGINE VIBRATION DURING CRUISE, ITT +50-60 HOTTER THAN NR 2, N1 + 1%> NR 2, FF + 150> NR 2 APPROXIMATE SPEED .5 ROLL TO RT SIDE TO HOLD LEVEL TRIM. NR 1 ENG SURGE IND DURING DESCENT. TROUBLESHOT IAW FIM 72-00-00-810-807-A & EMM 72-00-00-810-311/100; NO SDR RJEF20140630008Line · leakingDURING CLIMB, PILOT REPORTED NR 2 BLEED OSCILLATING DURING CLIMB +/-30 PSI. RETURNED & PERFORMED AN UNEVENTFUL LANDING. PERFORMED FAULT ANALYSIS IAW FIM 36-14-00-810-811-A, LEAK TESTED THE SERVO LINES OF THE RT TORQUE MOTOR CONTROLLER IAW AMM 36-11-06-790-SDR RJEF20140526005Seal · missingPREVIOUS TO DEPART AS FLIGHT TA537 FROM MIA TO SAP IT WAS FOUND THAT THE WEATHER SEAL BETWEEN SLATS 2 & 3 OF THE RT WING IS MISSING. THE ACFT WAS HELD ON GND IN ORDER TO PERFORM THE SEAL INSTALLATION IAW AMM 57-42-11-04. AFTER THE WEATHER SEAL INSTALLATION TSDR SOKF20140423003Shutoff Valve · damagedDURING DESCENT FROM SAL TO TGU THE ACFT RETURN TO SAL DUE DURING LG EXTENSION. BRAKE RT FAULT & BRAKE LT FAULT COMES ON EICAS & BOTH MSG`S KEPT STEADY ON THE REMAINING TIME OF FLIGHT. AT SAL STATION PERFORMED CHECK IAW FIM 32-41-00-810-804A & REPLACED MAIN BSDR R61A201404190590Strip · corrodedDURING HEAVY CHECK, LT ENGINE OTBD FAN COWL FWD METALLIC STRIP WORN AND CORRODED. MX R & R LT ENGINE OTBD FAN COWL FWD METALLIC STRIP IAW SRM 51-41-02, PN 341-2309-503 STRIP.SDR R61A201404190591Strip · corrodedDURING HEAVY CHECK, LT ENGINE FAN COWL AFT METALLIC STRIP IS WORN AND CORRODED. MX R & R LT ENGINE FAN COWL AFT METALLIC STRIP IAW SRM 51-42-02.SDR RJEF20140404002Pa System · inoperativePILOT REPORTED THAT THE FLIGHT ATTENDANT INTERPHONE SYS DOES NOT WORK. PERFORMED A FAULT ANALYSIS IAW FIM 44-10-00-810-801-A, FINDING THAT THE PA CIC IS NOT WORKING PROPERLY. REPLACED IAW AMM 44-11-01, PERFORMED THE CORRESPONDING OPERATIONAL TESTS WITH NORSDR YENA20140323062Transmitter · failedDURING FLIGHT "ENG OIL LOW PRESSURE" ON EICAS. ACCOMPLISH QRH THAT LED THE CREW TO A PRECAUTIONARY ENGINE SHUTDOWN DUE TO ABNORMAL OIL INDICATION. ACFT DIVERTED. TROUBLESHOT "ENG OIL LOW PRESS" MSG IAW FIM 79-33-00. R & R NR 1 ENG OIL PRESSURE TRANSMITTER SDR SOKF20140321002Manifold · malfunctionedDURING TAKEOFF ROLL FLIGHT 310 FROM SAL TO MIA STEER FAIL MSG ON CAS & REJECTED TAKEOFF WAS PERFORMED. AT SAL STATION DUE REJECTED TAKEOFF WAS PERFORMED HIGH ENERGY STOP CONDITION INSPECTION IAW AMM 05-50-12, NO FAULTS WERE FOUND. IAW FIM 32-52-00-810-801-A SDR USAA2013123100001Engine · malfunctionedFLIGHT 2099, PHL - DFW, DURING CRUISE AT FL 390 THE CAPTAIN REPORTED VIA ACARS FUMES & DECLARED AN EMERGENCY. FLIGHT LANDED UNEVENTFULLY & TAXIED TO THE GATE. CAPTAIN ADVISED FUMES OF A BURNING PLASTIC SMELL REPORTED IN COCKPIT & CABIN. R & R THE NR 1 ENG.SDR SOKF20131213012Torque Tube · disconnectedDURING CLIMB FROM SAL TO TGU THE AIRCRAFT RETURN TO SAL STATION DUE SLAT FAIL CAS MESSAGE. AT SAL STATION PERFORMED FIM TASK CARD 27-81-00-220-801-A600 & FOUND RT TORQUE TUBE DISCONNECTED. INSPECTED & RECONNECTED TORQUE TUBE IAW AMM 27-81-03, PERFORMED CMC CSDR YENA20131206241Pressure Switch · failedAIRCRAFT RETURN TO DEPARTURE, DUE TO NR 1 ENGINE FUEL LOW PRESSURE MESSAGE ILLUMINATED IN FLIGHT WITH FUEL FEED 1 FAULT ASSOCIATED MESSAGE ADVISORY. R & R NR 1 ENGINE FUEL LOW PRESSURE SWITCH IAW AMM 73-31-01. LEAK & OPS CHECKED NORMAL IAW FIM 73-31-00-810-8SDR RJEF20131126010Blades · damagedAFTER ARRIVAL, FOUND DAMAGE ON FAN BLADES DUE FOD ON NR 2 ENGINE. PERFORMED INSPECTION IAW AMM 05-50-02-200-801-A. BLADES REPLACED IAW MM 72-21-05/400.SDR SOKF20131120001Warning System · false activationDURING CLIMB FROM GYE TO SAL THE ACFT RETURN TO GYE DUE LG WOW SYS FAIL CAS MESSAGE. PERFORMED INSPECTION TO CMC NO MESSAGE WAS FOUND & POWER DOWN & UP IAW AMM 24-42-02-860-802-A 860-801-A OK NORMAL. THE ACFT WAS RETURNED TO NORMAL OPERATION.SDR RJEF20130924008Resolver · faultyAT ARRIVAL, PILOT REPORTED FLIGHT CONTROL NO DISPATCH ON TOUCH DOWN AND NO PITCH TRIM INDICATION, PERFORMED FAULT ANALYSIS IAW FIM 27-41-00-810-804-A AND FOUND A FAULTY POSITION RESOLVER OF CHANNEL 2 OF HORIZONTAL STABILIZER TRIM ACTUATOR, RESOLVER REPLACED SDR USAA2013090600001Pump · contaminatedON CLIMBOUT CREW REPORTED EICAS FUEL NR 2 LOW LEVEL REQUIRING LANDING AT NEAREST SUITABLE AIRPORT. MX FOUND PLASTIC PAPER ABSORBANT ON ENGINE FEED EJECTOR PUMP. REMOVED DEBRIS AND R & R ENGINE FEED EJECTOR PUMP.SDR SOKF201308230001Duct · damagedDURING CLIMB, RETURNED TO DEPARTURE DUE TO STRONG ODOR OF BURNED RUBBER ON AIR CON SYSTEM. PERFORMED FIM 21-20-00-810-801-A, SUBTASK 810-011-A, GENERAL VISUAL INSPECTION ON PACK RT. FOUND AIR DUCT DAMAGE.SDR SOKF20130726009Warning Light · false activationDURING CRUISE, OPEN EMERGENCY DOOR WARNING INDICATION ON EICAS. ACFT RETURN TO DEPARTURE. AT STATION, PERFORMED AMM 52-20-00 OPENED AND CLOSED, APPLIED FIM 52-75-00-810-802-A AND WAS FOUND INDICATION WORKING FINE, PERFORMED CABIN PRESURIZATION LEAKAGE TESTSDR SOKF20130624008Deflector · damagedDURING CLIMB, WHILE LEAVING 12.000 FT, VIBRATION AND LOUD SOUND HEARD FROM FWD DOOR. IAW FIM TASK 05-50-00-810-801-A FOUND FWD SERVICE DOOR DEFLECTOR DAMAGED, DEFLECTOR WAS DEACTIVATED IAW AMM 52-11-28-040-801-A.SDR SOKF20130618007Duct · damagedDURING FLIGHT, ACFT DIVERTED DUE TO STRONG VIBRATION AND RAPIDLY INCREASE OF CABIN ALTITUDE, UP TO 12000 FT, RED LABEL. PERFORMED FIM 21-31-00-810-824-A, GENERAL INSPECTION IAW 21-51-21-210-801A-600 IN PACK OUTLETS 1 & 2 AREA ON ACFT PRESSURIZED 4 PSI AND WASDR SOKF20130621001Radar · malfunctionedDURING CRUISE, DIVERTED DUE TO WEATHER RADAR INOPERATIVE. PERFORMED FIM 34-42-00-810-801-A, RESET CIRCUIT BREAKER SPDA 1 AND FOLLOWING FAULT CODE 34615212CD1, PERFORMED FIM 34-61-00-810-801-A, RESET AND TEST THE CONTROL I/O MODULE 1 VIA CMC, TEST PASSED PERFSDR SOKF20130612005Contactor · damagedDURING CRUISE, ACFT DIVERTED DUE NR 2 IDG OFF BUSS, GLC 2 FAULT, CMC MESSAGE, AT STATION. PERFORMED FIM 24-21-00-810-850-A AS T/S SWAPPED GLC 2 WITH APU ALC, TEST IAW AMM 24-21-21-400-801-A, TEST WAS SATISFACTORY, ADDITIONALLY CHECK WITH ENGINE RUNNING IAW AMSDR SOKF20130611004Bonding Jumper · looseDURING CRUISE, ACFT DIVERTED DUE A STRONG BURNING ODOR SIMILAR TO PLASTIC. GALLEYS WERE INSPECTED, OVENS BURNED OFF. SMOKE ASSOCIATED ODOR INCREASE WITH TIME. PERFORMED FIM 25-30-00-810-801 AFT GALLEY AREA INSPECTION AND FOUND A BONDING JUMPER LOOSE, TIGHTESDR USAA2013032100015Engine · vibrationFLT 1607 EN ROUTE. NR 2 ENGINE VIBRATION HIGH, AT TIMES MOMENTARILY EXCEEDING LIMITS (AMBER INDICATION). HIGHEST READING 4.1. STILL NOTICED VIBRATION AT GROUND IDLE. MX R & R NR 2 ENGINE.SDR YENA20130224052Engine · failedFLT 575 SWF-MCO, CREW DECLARED EMERGENCY AND AIRCRAFT DIVERTED TO JFK. AT APPROX 30,000FT ON CLIMBOUT ENGINE 2 LP VIB REACHED 4.7. LEVELED OFF PER QRH PULLED NR 2 ENGINE LEVER TOWARD IDLE. LP VIB WENT TO 5.7 COMPRESSOR STALLING BEGUN OCCURING. ALSO RAN QRH SDR YENA20130220049Engine · fireFLT 615 JFK-JAX, ENGINE NR 2 TAILPIPE FIRE EXTINGUISHED WITH PURPLE K DRY AGENT. REMOVED AND REPLACED NR 2 ENGINE ASSY PER TASK CARDS E190-71-00-01-400-801 + E190-71-00-01-000-801. LEAK CHECKS AND ENGINE RUNS ACCOMPLISHED, ALL OPS CHECK NORMAL.SDR USAA2012122400002Spinner · misalignedON TAKEOFF ROLL ABOUT 100 KIAS ENGINE NR 1 LP VIB INDICATED 4.6. AFTER TAKEOFF FOLLOWED QRH ENGINE ABNORMAL VIBRATION CHECK LIST AND ENGINE VIB (ENGINE 1 LP). RETURNED TO GREEN AT 60%. MAINTENANCE FOUND SPINNER MISALIGNED RE-INSTALLED SPINNER. PERFORMED ENSDR YENA20121216670Fadec · failedFLT 117 JFK-MSY, CREW DECLARED EMERGENCY DUE TO TLA COMP FAIL FOLLOWED SHORTLY AFTER BY ENGINE 1 FAIL. FOLLOWED BY NORMAL SINGLE ENGINE LANDING AT MSY. NO ABNORMAL SIGNS PRIOR TO ENGINE FLAMEOUT ENGINE WINDMILLED THROUGHOUT LANDING ROLL AUTO AND MANUAL RELIGSDR YENA20121211664Fadec · failedFLT 1242 CLT-BOS, CREW DECLARED EMERGENCY AND AIR RETURN TO CLT DUE TO NR 2 ENGINE FAILED AT 16000FT. REIGNITED APPROX 20 SECONDS LATER WITH NO EICAS MESSAGES. THE NR 2 ENGINE FADEC WAS REMOVED AND REPLACED PER AMM 73-00-00-800-812. PERFORMED GROUND POWER ASDR RJEF2012120498501Engine · vibrationDURING CLIMB OF THE AIRCRAFT AS FLIGHT TP-831 FROM LIM TO CUZ, THE PILOT IN COMMAND REPORTED: "ENGINE NR 1 ABNORMAL VIBRATION 4.2 LP WITH SOUND DURING CLIMB", THEREFORE, THE AIRCRAFT WAS RETURNED TO LIM AIRPORT (ATB). ADDITIONAL THE PILOT REPORTED: "LANDING WSDR YENA20121129655Engine · vibrationFLT 1283 BOS-RIC, AIR RETURN TO BOS DUE TO ENGINE 2 HIGH VIBRATION LP 4.1 IN CLIMB. PERFORMED FULL BALANCE OF NR 2 ENGINE ADDED B+03 10.13 B+04 11.90 B+05 3.49 B+06 11.90 B+07 10.13 OPS TEST GOOD PER EMM 72-00-00.SDR RJEF2012102501Actuator · malfunctionedDURING FLIGHT, PILOT REPORTED "SLATS FAILURE"; AIRCRAFT RETURNED TO AIRPORT AND LANDED WITH 45,000 KGS OVERWEIGHT AND 300 FPM SINK RATE. ONCE THE AIRCRAFT WAS POSITIONED AT THE MAINTENANCE RAMP, FIM 27-83-00-810-818-A AND FIM 27-81-00-810-805-A WAS PERFORMED SDR USAA2012101600002Engine · bird ingestionFLIGHT 880, IAH-PHL - ON APPROACH THE CAPTAIN SAW A LARGE BIRD FLASH BY HIS LEFT WINDOW. IMMEDIATELY THEREAFTER, THE LEFT ENGINE SHUT DOWN AND THE CREW EXPERIENCED SEVERAL EICAS FAULTS. AN EMERGENCY WAS DECLARED AND AS LANDING FLAPS WERE SELECTED THE AIRCRAFSDR YENA20120908600Blade · lack of lubeFLT 1047 HPN-NAS, AIRCRAFT DIVERTED TO JFK DUE TO ENGINE NR 1 VIB AMBER (4.1) AT HIGHER POWER SETTINGS. PERFORMED FAN BLADE LUBRICATION PER T/C E190-72-21-05-400-801 AND PERFORMED FAN TRIM BALANCE (STANDARD) IAW EMM 72-00-00-760-321, HIGHEST VIB VALUE RECORD SDR SOKF20120910003Windshield · crackedDURING FLIGHT TA255 FROM MIA TO TGU THE AIRCRAFT DIVERTED TO SAP DUE FIRST OFFICER WINDSHIELD CRACKED. REMOVED AND REPLACED FIRST OFFICER WINDSHIELD IAW AMM 56-11-00. PERFORMED OPERATIONAL TEST IAW AMM 30-42-00 OK NORMAL. PERFORMED CABIN PRESURIZATION LEAKASDR YENA20120907596Engine · leakingFLT 686 DCA-BOS, AIRCRAFT DIVERTED TO JFK DUE TO NR 1 ENGINE INDICATION OF RAPID OIL LOSS FROM 11.4 TO 7.2. FOUND OIL LEAKING ON NR 5 SUMP DRAIN. REMOVED AND REPLACED NR 1 ENGINE PER TASK CARD E190-71-00-01-400-801. OPS AND LEAK CHECK GOOD. ON THE SAME FLISDR RJEF2012082406Structure · damagedAT ARRIVAL, FLIGHT TP148, A BIRD STRIKE WAS FOUND NEAR LEFT WING TIP AREA OVER RIB 42. IAW FIM 05-50-02-200-801-A, THE RIB 42 WAS FOUND DAMAGED. PERFORMED PERMANENT REPAIR FOR STRUCTURAL DAMAGED LOCATED AT RIB 42 WING LT IAW EO ERJPR57-015/12 REVISION 00. SDR SOKF20120814002Detector · damagedEICAS MESSAGE BLEED 1 LEAK. FOLLOWED FIM 36-21-00 AND WAS FOUND LT LEAK DETECTOR LOOP 3 DAMAGED REMOVED AND REPLACED IAW AMM 36-21-02 PERFORMED OPERATIONAL CHECK WITH ENGINE 1 RUNNING IAW AMM 71-00-00 OK NORMAL. THE AIRCRAFT RETURNED TO NORMAL OPERATION.SDR USAA2012071900001Oil System · overservicedLGA FLT 2117 BOS-LGA DIRTY/MUSTY OIL SMELL DURING TAXI, TAKEOFF, CRUISE, DESCENT, TAXI-IN. DRAINED NR 1 ENGINE OIL TANK. RAN PACKS, WITH AIR SOURCE FROM THE APU AND ENGINES NR 1 & 2. NO ODOR DETECTED. AIRCRAFT OK FOR CONTINUED SERVICE.SDR 2012F00125Filter Element · dirtyDURING FLIGHT, THE ACFT RETURN TO DEPARTURE DUE TO EICAS WARNING MESSAGE, BLEED 2 FAIL. REPLACED TORQUE MOTOR CONTROLLER FILTER IAW AMM 36-11-06. OPS TEST ON GROUND, OK NORMAL. THE ACFT RETURN TO NORMAL OPERATION.SDR RJEF20120706001Float Valve · inoperativeDURING CLIMB, FLIGHT TP-054, SCL TO LIM. PIC REPORTED: "LIQUID SPILL FROM RIGHT WING ONCE TAKEOFF. RETURNED TO AIRPORT. IT WAS INSPECTED AS PER FIM 28-11-00-810-801-A; REPLACEMENT OF THE FLOAT VENT VALVE IN ACCORDANCE WITH AMM 28-12-05-000/400-801-A; PERFOR
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