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 = 'CF348C5' 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 = 'CF348C5' 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 MASA2021050200100Engine · fire#1 ENGINE CAUGHT ON FIRE DURING ENGINE START- BSI, VISUAL CHK, ENG RUN GOODSDR MASA2021012200025Fadec · faultedRT ENGINE FLAMEOUT 10000FT (EMER DECLARED). REPLACED RT FADEC.SDR MASA2021012200026Fadec · faultedRT FADEC FAULT 1 STATUS MESSAGE (EMERGENCY DECLARED). REPLACED RT FADEC.SDR V0XD20202212016Cascade · crackedLT THRUST REVERSER IN BOARD LOWER CASCADE CRACKED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 4019.SDR MASA2020121110645Oil System · leakingE2 START ABORT X'3 W/SMOKE & NO START & OIL LEAK.SDR REXA2020103000731Engine · flamed outDURING CLIMB OUT AROUND 19,500 FT ENGINE FLAMED OUT NUMBER 2 ENGINE. REPLACED NR 2 ENGINE, IAW JC 900-72-430-902. OPERATIONS/LEAK CHECKS GOOD.SDR V0XD20201910001Stringer Splice · corrodedSTRINGER 24R SPLICE AT FS 333.00 CORRODED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVAMX W/O: 80889 W/C: 1236.SDR VNAA2020102011118Warning Message · false activationPRECAUTIONARY ENGINE SHUTDOWN DUE TO HIGH OIL TEMPERATURE. AIR RETURN TO CLT FOR RT ENGINE OIL HIGH TEMPERATURE. REMOVED AND REPLACED DCU 1, IAW CRJ 900 AMM 31-41-04-000/400-801. OPERATIONS CHECKED GOOD. PERFORMED OPERATIONS CHECK OF DCU 1, IAW CRJ 900 AMMSDR VNAA2020101511101Sensor · abnormalPER FLIGHT CREW, RIGHT ENGINE OIL TEMP FLUCTUATIONS FROM 155-158 ON CLIMB OUT FL 210 TO FL 230. LEVELED OFF FLIGHT LEVEL 230 AND THE OIL TEMP WENT TO 163C. RAN THE QRH. SHUT THE ENGINE DOWN. REMOVED AND REPLACED RT ENGINE OIL LEVEL/TEMP SENSOR, IAW CRJ-900 SDR SWIA202053051Engine · vibrationRT ENGINE EXPERIENCED LP VIBE TO 9.9. CREW RETURNED TO FIELD AND ENGINE LOCKED UP AFTER SHUTDOWN WITNESSED BY MX STANDING BY. REMOVED AND REPLACED RIGHT ENGINE ASSEMBLY, IN REF TO THE AMM. OPERATIONS AND LEAK CHECK GOOD. COMPLIED WITH TASK CARD ENGINE INSTSDR SWIA202008252080Engine · contaminatedDURING TAKEOFF ROLL, BLUEISH ELECTRICAL SMELLING SMOKE BEGAN TO ENTER THE FLIGHT DECK ALONG EACH SIDE OF THE FLIGHT DECK A SMOKE LAV (DID NOT CATCH FWD OR AFT) MASTER WARNING APPEARED. FLIGHT ATTENDANTS REPORTED THE SMELL AND HAZE IN THE CABIN. FLIGHT 3614SDR MASA2020081631152Engine · flamed outR ENG FLAME OUT AT 7K FT AUTO RELIGHT. PERFORMED FDR DOWNLOAD/FOLLOWED FIM/INSPECTED ENGINE/RAN ENGINE/CW BOROSCOPE INSPECTION. NO PARAMETERS EXCEEDED. NO DEFECTS NOTED, OPS CHECK GOOD.SDR SWIA202053118Slider · chafedRT ENGINE UPPER TRANSLATING COWL SLIDER CHAFED. C-CHECK RO 10/9/2020. PERFORMED PERMANENT REPAIR ON RT ENGINE UPPER TRANSLATING COWL SLIDER, REF BOMBARDIER REO.SDR VNAA2020073011101Bleed Valve · failedL ENG DEGRADED, L ENG SURGE OPEN CAUTION, L ENG ITT EXCEEDED. CREW SENT ACARS TO DISPATCHER STATING THEY WERE RETURNING TO FIELD, DUE TO MX. CREW DID DECLARE AN EMERGENCY. CREW STATES THEY RECEIVED L ENGINE DEGRADED MESSAGE AND L ENGINE SURGE OPEN CAUTION SDR SWIA2020071550920Seal Ring · damagedSMOKE AFT LAV WARNING MESSAGE ON DESCENT. COMPLIED WITH QRH PROCEDURE, NO VISIBLE SMOKE OR SMELL OF BURNING NOTED IN FLIGHT OR AFTER LANDING. FLIGHT 4609 - FILED CLOSED. TROUBLE SHOT REPORTED SMOKE IN THE CABIN IN REFERENCE TO FIM; COULD NOT DUPLICATE FINDINSDR REXA2020052200569Fuel Filter · not reportedON THE APPROACH INTO KTYS CREW OBSERVED L MAIN EJECTOR, L ENGINE FLAME OUT CAUTION MSG'S BOTTLE ARMED PUSH TO DISCHARGE ILLUMIATED ON GLARES-
HEILD L ENGINE DID FLAMEOUT TEMPORARILY BUT RESTARTED ON ITS OWN, ALL MSGS CLEARED AS WELL. SDR REXA2020042800564Pin · bentRH ENGINE LOWER COWLING ALIGNMENT PIN AFT OF THE 2ND LATCH IS BENT, UNDERLYING STRUCTURE POSSIBLY DAMAGED.
REMOVED & REPLACED ALIGNMENT PIN & OB EDGE MEMBER IAW CRJ 900 SRM 51-41-02-001-001-A01, 51-40-11-001-001-A01, 51-42-06-00SDR VNAA2020032411101Blade · stuckON TAKEOFF ROLL, LH VIB GAUGE AT 1.5, OUT OF 6,000 FT VIBE GAUGE HIT 1.9 IN THE CAUTION RANGE. RETURNED TO FIELD. NO EMERGENCY WAS DECLARED. INSPECTED FAN BLADES FOR STIFFNESS ON LH ENGINE AND FREED STUCK BLADE. PERFORMED VIBRATION CHECK . VIB CHECK NORMAL NO SDR SWIA2020042750344Latch · wornR/H LOWER TRANSCOWL LANDING FOR PANEL 443AR LATCHES ARE WORN THROUGH (C-CHECK) RO 4/23/2020 REPLACED DOUBLER REF REO. SKYWEST TASK CARD COMPLIED WITH.SDR REXA2020041500488Baffle · crackedINITIAL INSPECTION: CRACK ON BAFFLES 2E/A ON RH ENGINE LOWER THRUST REVERSER CASCADE FITTINGS.(MOT2)
BAFFLES 2E/A ON RH ENGINE LOWER THRUST REVERSESDR REXA2020042300537Retainer · wornINITIAL INSPECTION : WEAR ON RETAINER 8E/A OF LOWER AND UPPER RH ENGINE TRASCOWL (MOT 2)
SUMMARY: RETAINER 8E/A OF LOWER AND UPPER RH ENGINE TRASCOWL WERE REPLACED PER CRJ900 SRM 51-42-20-001-001-A01.SDR REXA2020042200511Pad · wornINITIAL INSPECTION: WEAR ON PAD WHERE SEATS THE LATCH OF UP/LWR COWL BLOW-OFF DOORS AT LH ENGINE (MOT)
PADS WHERE SEATS THE LATCH OF UP/LWR COWL BLOW-OFF DOORS AT LH ENGINE WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01SDR SWIA202005140615Slider · chafed*RH ENGINE UPPER TRANSLATING COWL SLIDER ON COWL, IS CHAFFED ON THE END (MARKED) (C-CHECK) RO 5/10/2020 BLENDED RH ENGINE UPPWER TRANSLATING COWL SLIDER REF CRJ900 SRM. IN LIMITS AND RESTORED REF BOMBARDIER REO AND BOMBARDIER REO.SDR VNAA2020020811101Anti-Ice Valve · failedON TAKEOFF ROLL AT APPROXIMATLY 60KTS, A ANTI ICE CAUTION MSG WAS RECIEVED. CREW ABORTED TAKEOFF CONTACTED MX AND RETURNED TO GATE WITHOUT FURTHER INCIDENT. TROUBLESHOT PER B1-031999. PROCEEDED TO R&R LEFT CAIV PER CRJ900 AMM. OPS CHECK GOOD AT THIS TIME.SDR REXA2020010700002Latch · damaged"INITIAL INSPECTION : ELONGATED HOLE ON COAMING LATCH DOOR AT LOWER HALF TRANSCOWL RH ENGINE ( MOT 2 )
"SUMMARY: ON NRC. 00038 COAMING LATCH DOOR, DOUBLER COAMING LATCH DOOR AND PAD BEARINGAT ON LOWER HALF TRANSCOWL RH ESDR REXA2020010770005Spigot · worn"INITIAL INSPECTION : WEAR ON SPIGOT AT LATCH DOOR ASSEMBLY OF LOWER HALF TRANSCOWL LH ENGINE ( MOT 1 )
"SUMMARY OF NRC 00049: SPIGOT AT LATCH DOOR ASSEMBLY OF LOWER HALF TRANSCOWL LH ENGINE WAS REPLACED PER CRJ-900 SRM 5SDR REXA2020010750004Latch · damaged"INITIAL INSPECTION : ELONGATED HOLE ON COAMING LATCH DOOR AT UPPER HALF TRANSCOWL LH ENGINE ( MOT 1 )
""SUMMARY:ON NRC 00046: DOUBLER COAMING LATCH DOOR WAS REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01 AND SRM 51-42-06SDR REXA2020010740003Spigot · worn"INITIAL INSPECTION : WEAR ON SPIGOT AT LATCH DOOR ASSEMBLY OF UPPER HALF TRANSCOWL RH ENGINE ( MOT 2 )
"SUMMARY OF NRC 0040: SPIGOT AT LATCH DOOR ASSEMBLY OF UPPER HALF TRANSCOWL RH ENGINE WAS REPLACED PER CRJ-900 SRM 51SDR MASA2019122112192Engine · contaminatedSMOKE IN CABIN ON T/O ROLL, FWD/AFT LAV SMOKE WARNINGS. CONFIRMED ENG 2 CONTAMINATION OF ATTEMPTED COMPRESSOR WASH FROM NIGHT BEFORE, PREFORMED HIGH POWERED ENG RUNS TO BURN OFF FLUID. NO SMELL OR FUMES NOTED.SDR REXA2019123051838Latch · wornWEAR FOUND ON THE COAMING LATCH DOOR AT THE TRANSCOWL FOR THE RT ENGINE. THE COAMING LATCH DOOR WAS REPLACED IAW SRM 51-42-13-001-001-A01.SDR REXA2019123051839Door · damagedWORN AND BENT CUTOUT OF THE COWLING LATCH DOOR FOR THE RT NACELLE. THE COAMING LATCH DOOR WAS REPLACED IAW SRM 51-42-13-001-001-A01, AND SRM 51-42-21-001-001-A01.SDR MASA2019103012112Engine · fodLH ENG SHUT DOWN IN FLIGHT. FOD DAMAGE. CURRENTLY OUT OF SERVICE.SDR REXA2019101491474Shield · perforatedWEAR ON PRODUCTION DOUBLER OF PANEL BLOW OFF DOOR AT FORWARD CORE COWL ASSEMBLY UPPER RIGHT SIDE.(INNER FACE) ENGINE NR 2. A NEW BLOW OFF DOOR FIRESHIELD WAS INSTALLED PER SRM 51-22-00-001-001-A01, PAR.5, SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01, ASDR SWIA2019090646260Engine · malfunctionedIN CRUISE AFT LAV SMOKE WARNING. FA REPORTED NO SMOKE, DURING DESCENT AFT LAV SMOKE WARNING RETURNED. FA'S REPORTED SMOKE SMELL AND HAZE. DIVERTED. UPON LANDING PAX EVACUATED ON RUNWAY. (FLT#3608) FO: 09/05/2019 CLOSED REMOVED AND REPLACED RT ENGINE IAW AMM. OSDR CA190813019Detector · faulty(CAN) FLAPS FAIL C/M DISPLAYED IN CRUISE AT FL370. AIRCRAFT RETURNED TO BASE. REPEAT DEFECT 1)SKEW DETECTOR MT3 REPLACED AS PER AMM 27-52-45-400-802. SKEW DETECTOR MT2 REMOVED. 2)SKEW DETECTOR MT2 INSTALLED TASK 27-52-45-400-802 3)SKEW DETECTOR MT83 REPLACESDR MASA2019072811974Engine · failedRT ENGINE FAILED ON APPRCH/CREW SHUTDWN.SDR CA190726024Frame · cracked(CAN) DURING SCHEDULED MAINTENANCE A CRACKED FRAME WAS OBSERVED AT FS235, STRINGER 13. APPROVED REPAIR CARRIED OUT. FRAME PN CC670-34133-3. (TC# 20190726024)SDR CA190726016Floorbeam · corroded(CAN) DURING SCHEDULED MAINTENANCE THE FLOOR BEAM AT FS 280 WAS OBSERVED TO HAVE EXCESSIVE PITTING/LEVEL 2 CORROSION BEYOND REPAIRABLE LIMITS REQUIRING PART REPLACEMENT. THIS AREA WAS PREVIOUSLY REPAIRED IAW SB670BA-53-041. (TC# 20190726016)SDR CA190719002Sensor · faulty(CAN) ABOUT 15 MIN AFTER LEAVING DEPARTURE POINT, THE CREW HAD A BRAKE OVERHEAT WARNING. THE CREW ACTIONED THE QRH, REDUCED THEIR SPEED AND LOWERED THE GEAR TO ALLOW THE GEAR TO COOL. ONCE COOLED, THEY RETRACTED THE GEAR. ON THE WAY INTO DESTINATION POINT, THESDR CA191003003Pin · defective(CAN) ON CLIMB OUT FAN 1 VIBRATIONS REACHED 4.0. RETURN TO FIELD. CORRECTIVE ACTION: REMOVED AND REPLACED THE FAN BLADE PINS ON THE #1 ENGINE AND ENSURED THAT FAN DISK AND FAN BLADE BORES ARE FREE OF DEBRIS. (TC# 20191003003)SDR CA190730019Control Unit · failed(CAN) CREW REPORTS RUDDER LIMITER CAUTION MESSAGE AND RUDDER LIMITER STATUS MESSAGE, THE SSCU1 WAS INITIALLY REPLACED BUT THE MOTR REQUESTED THE RTLA1 TO BE REPLACED AS WELL. RTLA P/N DL2428M9MOD1, S/N 1667 (ORIGINAL TO A/C) SSCU P/N C13045BA05, S/N 2661 (ISDR CA190702019Pulley · broken(CAN) DURING A ROUTINE CHECK OF THE AFT BAGGAGE COMPARTMENT, MTC NOTED NOISE COMING FROM THE CABLE ASSIST MECHANISM, A CLOSER LOOK REVEAL THAT THE FWD PULLEY HAD SPLIT IN HALF. WITH THE PULLEY DAMAGED, THE CARGO DOOR`S BALANCE SPRING`S CABLE HAD CHAFED AGAINSTSDR CA190629002Hinge Fitting · corroded(CAN) CORROSION TO AILERON HINGE FITTING #2 & #3 BORE AT WS 323.058 AND WS 319.604 REMOVED BY REAMING BOREHOLES TO FINAL DIAMETER OF 0.8840`. P/N: CC670-18054-3 AND CC670-18052-11 (TC# 20190629002)SDR CA190618014Bpsu · failed(CAN) ON APPROACH, WHILE LOWING THE FLAPS, THE CREW RECEIVED A FLAP FAIL CAUTION MESSAGE WHEN FLAPS WERE SELECTED FROM 8 TO 20 DEGREES. THE FLAPS STOPPED AT APPROXIMATELY 13-17 DEGREES. THE CREW CONDUCTED A GO AROUND, DECLARED AN EMERGENCY AND THEN LANDED WITHSDR CA190629005Floor Support · corroded(CAN) CORROSION DAMAGE ON LHS AND RT PRESSURE FLOOR ANGLE AT FS693.00 - FS847.00, (TC# 20190629005)SDR CA190610021Duct · cracked(CAN) BLEED LEAK FOUND IN REAR AIR CONDITIONING COMPARTMENT. FOUND CRACKED TEN STAGE BLEED CROSS OVER DUCT. REPLACEMENT DUCT INSTALLED IN REFERENCE WITH AMM TASK 36-19-09-400-801. LEAK CHECK COMPLETED. SERVICEABLE (TC# 20190610021)SDR CA190605011Shaft · sheared(CAN) UPON REPORT OF THE MCD FORWARD COUNTER BALANCE CABLE ATTACHMENT BROKEN. MTC DISCOVERED THE PASSENGER DOOR GUIDE SHAFT HAD SHEARED. THE FWD COUNTER BALANCE GUIDE SHAFT WAS REPLACED AND DOOR RIGGING WAS COMPLETED WITH NO FURTHER FAULT NOTED. (TC# 201906050SDR CA190529008Transceiver · intermittent(CAN) CAPTAIN`S SIDE RAD ALT ERRATIC ON THE APPROACH, SPLR STAB FAULT MESSAGE ALSO POSTED ON EICAS. UPON SAFE LANDING, MTC REPLACED THE #1 RAD ALT AND GROUND TESTED SERVICEABLE. FDR DOWNLOADED AND READING SHOW THE L/H RAD ALT INTERMITTENTLY FAILING. L/H RADIO SDR CA190527017Intercostal · corroded(CAN) DURING SCHEDULED MAINTENANCE, LEVEL 2 CORROSION WAS IDENTIFIED ON AN INTERCOSTAL LOCATED FORWARD OF THE AVIONICS DOOR AT STRINGER 27, STATION 349-364. PART REPLACED IN ACCORDANCE WITH THE SRM. (TC# 20190527017)SDR CA190528006Floor Support · corroded(CAN) LIGHT CORROSION ON THE LEFT HAND SIDE OF THE AIRCRAFT BETWEEN F.S 728 TO F.S 827 ON THE PRESSURE DECK FLOOR (TC# 20190528006)
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