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 = 'CF343B' 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 = 'CF343B' 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 DXTA2026091509695Engine · faultedDURING LT ENGINE START , TECHNICIANS ENCOUNTERED A RAPID INCREASE IN ITT AND THE FIRE WATCH NOTIFIED THEM OF VISIBLE FIRE. THE CHECKLIST WAS USED AND THE ENGINE FIRE BOTTLE WAS DISCHARGED. REMOVED CUSTOMERS LEFT ENGINE INSTALLED REPAIRED ENGINE . WORKED PESDR 2026FA0000529Structure · ground damageTHE AIRCRAFT WAS PARKED OUTSIDE THE HANGAR AND UNOCCUPIED. WHILE OPENING THE BIFOLD HANGAR DOOR, THE DOOR CONTACTED THE TIP OF THE HORIZONTAL STABILIZER. THE AIRCRAFT HAD BEEN POSITIONED CLEAR OF THE PAINTED CLEARANCE LINE AT THE TIME OF THE EVENT. THE TECHNICSDR DXTA2026010906445Engine · vibrationWHILE IN CLIMB POWER AT FL310 THE LEFT ENGINE VIBRATION INDICATOR TURNED AMBER AND WAS INDICATING 3.1. AT COMPLETION OF THE CLIMB TO FL390 POWER WAS REDUCED TO 95.7 AND THE VIBRATION INDICATOR WAS STILL AMBER INDICATING 2.7. WHEN POWER WAS REDUCED TO 89.0 THSDR DXTA2025071404204Engine · vibrationIN FLIGHT, AT CRUISE, THE RIGHT ENGINE AMBER VIBRATION DISPAYED AT 2.7. PER QRH, AFTER PULLING BACK POWER, VIBRATION INDICATOR REDUCED BACK TO GREEN BUT AT AN ELEVATED READING OF 2.5 TO 2.6. A SLIGHTLY SLOWER CRUISE SPEED WAS REQUIRED TO KEEP INDICATOR IN SDR DXTA2025071004166Engine · no discrepancyRH ENGINE - POTENTIAL FOD ISSUE WITH POSSIBLE BIRDSTRIKE (10'CLOCK POSITION WHEN FACING RH ENGINE). REQUESTING INSPECTION FOR POTENTIAL DAMAGE. CORRECTIVE ACTION; COMPLIED WITH ENGINE INSPECTIONS REF GECF34BJ SM72·0!HL0 M(L), NO EVIDENCE OF BIRD STRIKE ATTHISDR DXTA2025012001982Engine · overtempLEFT ENGINE ENGINE OVERTEMP: FOLLOWING LEFT ENGINE START ITT ROSE RAPIDLY ACCOMPANIED BY A RED HOT MESSAGE ON THE ITT GAUGE. TEMP CONTINUED TO RISE AND CREW TERMINATED THE START AT 804°. CREW FOLLOWED THE HOT START QRH PROVEDURE. ALSO, THE MARSHALER HAD A CSDR DXTA2025011401913Cable · defectiveRIGHT ENGINE ENGINE TEMP INDICATION: AT APPROXIMATELY 100' AGL ON LANDING, RED ENGINE EICAS ILLUMINATED, ASSOCIATED WITH RED HOT INDICATION DISPLAY IN MFD ITT GUAGE AND RED ITT EXCEDENCE ON RIGHT ENGINE. CONTINUED LANDING AND SHUT DOWN RIGHT ENGINE ON GROUND ISDR DXTA2024120901388Engine · vibrationLEFT ENGINE ENGINE VIBRATION INDICATION: DURING INITIAL CLIMBOUT THE LEFT FAN VIB STARTED INCREASING AS HIGH AS 3.0. WE LEVELED OFF AND PULLED THE POWER BACK AND THE VIB DECREASED TO 2.0 AND REMAINED THIS HIGHER SETTING ON ARRIVAL. THE FLYING PILOT ALSO FELTSDR 2024FA0000839Bracket · crackedON THIS DATE, BRACKET PN: 3888525-2 UTILIZED TO ATTACH IGNITION UNIT TO HONEYWELL APU 36-150[CL] FOUND TO BE CRACKED. - SUSPECT POSSIBLE VIBRATION. ISSUE DISCOVERED DURING REMOVAL OF IGNITION UNIT.SDR 2024FA0000840Bracket · crackedON THIS DATE - BRACKET PN: 3888525.2 UTILIZED TO ATTACH IGNITION UNIT TO HONEYWELL APU 36-150[CL] FOUND TO BE CRACKED - SUSPECT POSSIBLE VIBRATION ISSUE. DISCOVERED DURING REMOVAL OF IGNITION UNIT. SECOND REPORT SENT. ISSUE NOTED ON TWO SEPARATE AIRCRAFT.SDR DXTA2024112201240Warning Light · illuminatedDURING CLIMB TO CRUISE ALTITUDE JUST A FEW MINUTES PRIOR TO LEVEL OFF WITH AUTOPILOT AND ATS ON, THE RED ENGINE ICAS ILLUMINATED (FOR A DURATION OF 1-2 SECONDS). NO EXCEEDANCE LEVELS WERE OBSERVED FOR EITHER ENGINE FOR ITT, N1 NOR N2 THAT WOULD NORMALLY SPUR SDR DXTA2024102100894Blades · lack of lubeRIGHT ENGINE ENGINE VIBRATION: VIBRATION FELT AND HEARD DURING CLIMBOUT. RIGHT ENGINE FAN VIB WAS 3.0, AMBER COLOR. QRH RAN. FELT NO VIBRATION IN FLIGHT CONTROLS. FLIGHT ATTENDANT HEARD LOUD NOISES AND VIBRATION FROM THE CABIN. CORRECTIVE ACTION; REMOVED & CLSDR 2024FA0000194Spacer · missingDURING A SCHEDULED MAINTENANCE INPUT AT BOMBARDIER SERVICES (UK) LTD AT BIGGIN HILL AIRPORT, UNDER WO 267540 - UPON REMOVAL OF #4 MAIN WHEEL ASSY, IT WAS DISCOVERED THAT THE SPACER WAS MISSING FROM THE INCOMING INSTALLATION. AIPC 32-41-01, ITEM 142, PN 19095-1SDR V6NA2024022701.1Throttle · faultedDURING THE FIELD ACCIDENT INVESTIGATION FOR N823KD CL604 S/N 5584, IT WAS MENTIONED THAT SEVERAL YEARS AGO A CHALLENGER 600 SERIES, DURING TAXI ACROSS AN ACTIVE RUNWAY, HAD A DUAL ENGINE FAILURE CAUSED BY THE AUTO THROTTLE SYSTEM. IN AN INTERNAL INVESTIGATION,SDR 2023F00204Wire Harness · brokenON ARRIVAL INTO HOU AFTER LEVELING AND THE THRUST LEVERS ADVANCING THE EICAS, AURAL WARNINGS, RH ENGINE FIRE PUSH, AND FIRE BOOTLE SWITCH LIGHTS ALL ILLUMINATED AND GAVE THE INDICATION OF THERE BEING A FIRE ON THE #2 ENGINE. RETARDING THE THRUST LEVERS CAUSED SDR U5QA202212010110Engine · power lossDIVERTED TO KDSM. DURING FLIGHT, FL380, AUX AOA CASE HEAT FAIL. COMPLETED THE CHECKLIST AND SHORTLY AFTER NR 1 ENGINE FAILED, ROLLED BACK TO 9% N2. TRIED INFLIGHT CROSSBLEED AND APU START WITH NO RESULTS. LANDING UNEVENTFUL. : AFTER APPLYING POWER TO AIRCRASDR 2022FA0000682Line · destroyedDURING INSPECTION FOR ROUTINE MAINTENANCE, THE #2 ENGINE CORE COWLS DOORS WERE OPENED UP. UNDER THE UPPER DOOR FOR THE ENGINE, THE 14TH STAGE BLEED AIR LINE P/N 228-56336-103 (13866-101 REV B) S/N K97991 WAS FOUND TO BE RUPTURED. THE LINE IS DESTROYED AND SDR U5OA_N36VVEngine · low pressureON A PART 91 TRIP SCHEDULED FROM KAUS TO KVNY CREW NOTICED THE RH ENG OIL PRESS FLUCTUATING BETWEEN 31 AND 39 PSI AT CRUISE FL340, AS FLIGHT PROGRESSED THE OIL PRESS CONTINUED TO DROP, WHEN PRESS READING DROPPED TO 25 PSI THE CAS MSG R LOW OIL PRESS ILLUMINATESDR 2022FA0000494None · wornON TAKEOFR ROLL, AT 50 KNOTS, PILOT STATED "#2 GEN FAIL" CAS MESSAGE DISPLAYED, AND TAKEOFF ABORTED. FINAL INVESTIGATION REVEALED #2 ENG INTEGRATED DRIVE GENERATOR (IDG) DELTA P INDICATOR WAS SET. REMOVAL AND INSPECTION OF FILTER REVEALED NUMEROUS METAL PARTSDR GZXA2020061200001Connector · chafed14TH STAGE DUCT CAS MESSAGE.SDR BN5A2019121200001Sensor · faultyAIRCRAFT DEPARTED, DURING CLIMB OUT THE RIGHT ENGINE 14TH DUCT OVERHEAT MESSAGE ALERTED THE CREW. POWER WAS PULLED BACK TO IDLE AND THE 14TH STAGE BLEED AIR VALVE WAS POSITION TO CLOSE. RIGHT 14TH DUCT MESSAGE REMAINED. RIGHT ENGINE WAS SHUT DOWN AND FLIGHT CRSDR CA190814005Oil System · low pressure(CAN) AIRCRAFT HAD AN ENGINE SHUT DOWN IN FLIGHT, DECLARED A PAN PAN AND DIVERTED INITIAL INFORMATION IS THAT DURING FLIGHT OIL PRESSURE DROPPED ON ONE ENGINE AND AFTER THEY THROTTLED BACK IT STABILIZED ABIT BUT THEN CONTINUED TO DROP. CREW SHUT DOWN THE ENGINSDR CA190802010Computer · malfunctioned(CAN) STALL ALT COMP LIGHT AND STALL FAIL ARE ANNUNCIATIED. FIELD SERVICE REPRESENTATIVE INPUT AUG 1, 2019: FAULT CLEARED THE NEXT MORNING. ADVISED CUSTOMER TO REPLACE THE STALL COMPUTER. (TC# 20190802010)SDR CA190806003Rib · cracked(CAN) L/H WING @ WS112.3, CANTED RIB, DRAWING #600-10332, IPC 57-51-01, P8 (ITEM 75) FOUND CRACKED, 1` LONG WITH SPIDER CRACKING AND 2 RIVETS SHEARED AT TRAILING EDGE GUSSET , IPC 57-51-001 (ITEM 155). (TC# 20190806003)SDR CA190709004Limiter · damaged(CAN) CREW REPORTED THAT WHEN DEPLOYING SPOILERS THEY DEPLOYED ASYMMETRICALLY AND THE AIRCRAFT ROLLED TO THE RIGHT. THE CREW NOTED THAT ON THE EICAS THE INDICATION SHOWED THAT THE RH SPOILER HAD EXTENDED FURTHER THAN THE LEFT. ENGINEERS REVISITED THE AIRCRAFTSDR CA190614011Flt Controls · binding(CAN) THE CREW NOTED THE FLIGHT CONTROLS WERE EXTREMELY STIFF ABOUT PITCH AND ROLL AXIS WITH OR WITHOUT AIR LOAD. THE AIRCRAFT HYDRAULIC PRESSURE SHOWED NORMAL IN ALL THREE SYSTEMS. UPON LANDING THE FLIGHT CREW VERIFIED THE PROBLEM PERSISTED WITHOUT AIR LOADSDR CA190527011Hose · leaking(CAN) APPROX 100PSI O2 LEAK OVERNIGHT. LOCATED LEAK AT BASE OF HOSE FITTING UNDER CO-PILOTS SIDE PANEL. FURTHER INVESTIGATION ALSO REVEALED THE HOSE WAS BULGING AT SAME LOCATION. ATTACHMENT POINT FOR THIS LINE IS TO THE `IN` PORT FITTING OF THE PASSENGER OXYGESDR CA190514008Motor · failed(CAN) DURING PRE-FLIGHT, TECHNICIAN NOTICED THE #2 FLAP MOTOR C/B (CB2-B5) TRIPPED. PUSH C/B BACK IN AND SELECTED FLAPS TO 20 DEG. ONCE FLAPS STARTED TO MOVE THE C/B TRIPPED AGAIN. FLAP MOTOR REPLACED. (TC# 20190514008)SDR CA190506011Pump · failed(CAN) AIRCRAFT HAD AN INFLIGHT SYSTEM 3 HYDRAULIC PRESSURE LOW INDICATION IN FLIGHT AND DIVERTED FOR LANDING CREW INFORMED THAT CB HYD 3 A WAS POPPED. (TC# 20190506011)SDR CA190430014Pdu · overheated(CAN) FLAP MOTOR 1 AND 2 OVERHEAT AT THE SAME TIME. CARRIED OUT OPS TESTS FLAPS AND CB PULLED OUT ONE BY ONE OF THE FLAP MOTORS. AND OPS CHECK ON ONE MOTOR EACH TIME. NO OVERHEAT OCCURRED. ALL SATISFACTORY DUE TO BOTH FLAP MOTORS OVERHEAT AT THE SAME TIME IT SDR CA190425017Flap System · stuck(CAN) FLAP STUCK AT 5 DEGREES. WE HAVE FIXED ALL THE DISCREPANCY`S ON A/C. THE FLAPS WE WHERE ABLE TO RESET AND PERFORMED MULTIPLE OPS CHECKS WITH SATISFACTORY RESULTS. (TC# 20190425017)SDR CA190415007Door · malfunctioned(CAN) DURING TAKE OFF THE NOSE LANDING GEAR (NLG) DOORS DID NOT CLOSE. AIRCRAFT LANDED AT DEPARTURE AIRPORT WITHOUT FURTHER INCIDENT. NO RECTIFICATION OR PARTS ISSUES HAVE BEEN PROVIDED. BOMBARDIER TRYING TO CONTACT SUBMITTER FOR DETAILS. SDR REVIEWED (TC# 20SDR CA190820015Servo Valve · defective(CAN) AC LANDED AT AIRPORT AND AFTER TOUCH DOWN, AT AROUND 80-60 KTS, NOSE WHEEL STEERING (NWS) FAILED. AC STOPPED ON RUNWAY AND NOSE WHEEL WAS FOUND 90 DEG DEFLECTED. MAINTENANCE MANAGED TO GET THE AC OFF RUNWAY AND INTO FACILITY. BOMBARDIER, CUSTOMER RESPONSSDR A6WA2019013146348Flap System · malfunctionedON FINAL APPROACH TO LAND, FLAP FAIL CAUTION MESSAGE WHEN FLAPS SELECTED TO 30 DEGREES. FLAPS FAILED IN 20 DEGREE POSITION. COMPLIED WITH QRH.SDR CA190314018Adc · malfunctioned(CAN) OPERATOR REPORTED HAVING TWO UNRELIABLE AIRSPEED EVENTS ON THE SAME AIRCRAFT WITHIN TWO WEEKS, IN DECEMBER 2018 AND JANUARY 2019. THE FIRST EVENT OCCURRED ON DECEMBER 28TH, 2018, EN ROUTE PRIOR TO TOP OF DESCENT AT FL400. THE CREW RECEIVED AN EFIS COMP MSDR DXTA2018101601558Engine · unserviceableAFTER ROTATION AND INITIAL CLIMB, LEFT ENGINE ITT HOT MESSAGE ILLUMINATED, RETURNED TO LAND, PRECAUTIONARY LEFT ENGINE SHUT DOWN. SIGNOFF REMOVED LEFT HAND ENGINE SERIAL NUMBER 801515. INSTALL REPAIRED ENGINE SERIAL NUMBER 801433. INSTALLED ENGINE SERIAL NUMBSDR RU3A20180529022Accelerometer · faultyRIGHT ENGINE VIBRATION LIGHT ILLUMINATED AT 75% N1 AT 16000 FEET. REMOVED AND REPLACED ENGINE VIBRATION ACCELEROMETER.SDR 2018FA0000214Track · crackedMAIN REVERSER TRACK, RIGHT SIDE AT THE 7 O`CLOCK POSITION, CRACKED ALMOST COMPLETELY THROUGH. FOUND DURING ROUTINE LUBRICATION OF REVERSER SCREWJACKS.SDR CA160127002Strut · leaking(CAN) AIRCRAFT ENCOUNTERED RETRACTION PROBLEMS (NLG TRANSIT LIGHT WOULD NOT EXTINGUISHED) AND HAD TO COMPLETE ITS FLIGHT WITH GEAR DOWN AND CONFIRMED LOCKED. FOLLOWING SUCCESSFUL LANDING AND PRELIMINARY INVESTIGATION THE NLG ASSY WAS FOUND DEFLATED AND COULD SDR CA160111007Outlet · arced(CAN) THE CABIN OUTLET AT THE LT FORWARD SEAT WHEN THE TABLET CHARGER WAS PLUGGED IN THE OUTLET, CHARGER HAD ELECTRICAL ARCHING AND SMOKE.SDR CA151208008Pdu · malfunctioned(CAN) AS REPORTED BY PILOT IN COMMAND IN INCIDENT REPORT DURING TAKEOFF ROLL, AT APPROXIMATELY 100 KTS, THE ATS DISENGAGED IMMEDIATELY FOLLOWED BY RT THRUST REVERSER UNLOCKED AMBER MESSAGE AND UNLOCK PBA AMBER. NO EVIDENCE OF YAW OR ACTUAL THRUST REVERSER DEPSDR J7SA20151129001Fire Detector · failedRIGHT ENG FIRE WARNING ACTIVATED IN FLIGHT. SHUTDOWN THE ENG & WARNING ALARM STOPPED. DECLARED AN EMER & LANDED SAFELY WITHOUT NEED TO EXPEND FIRE EXTINGUISHER. ON LANDING CREW FOUND NO EVIDENCE OF ACTUAL FIRE ON THE ENG. FOUND THE RT ENG PYLON SENSING ESDR CA151203011Fire Warning · false activation(CAN) DURING CLIMBOUT, THE RT ENGINE FIRE WARNING TRIPPED OFF WITH RED, RT ENGINE FIRE, POSTED. CREW SHUTDOWN THE RT ENGINE AND WARNING WENT OUT. ACFT DECLARED EMERGENCY AND DIVERTED, LANDING WITHOUT INCIDENT. CREW DID NOT NOTICE ANY EVIDENCE OF A FIRE FROMSDR CA151203017Fire Loop · failed(CAN) IT WAS REPORTED TO THE CUSTOMER RESPONSE CENTER (CRC) THAT THE CREW OBSERVED A FIRE INDICATION FOR THE RIGHT-HAND ENGINE AS THE AIRCRAFT WAS CLIMBING OUT. THE CREW FOLLOWED THE CHECKLIST. THE CREW THEN SHUT DOWN THE ENGINE AND THE FIRE INDICATION WENT OUSDR CA151118008Bracket · chafed(CAN) NLG CHANNEL 600-33045 CHAFED BY RH EDGE OF DOWN LOCK SWITCH BRACKET 20046-101.SDR CA150925017Wheel · missing(CAN) DOM REPORTED THAT CREW NOTICED THE RT OUTBOARD WHEEL ASSEMBLY MISSING UPON LANDING.SDR CA150828010Ribbon Heater · overheated(CAN) DURING AN INSPECTION, THE OPERATOR NOTICED THAT THE INSULATION INSTALLED OVER THE HEATED SILICONE GALLEY DRAIN HOSE (INSTALLED BY MODIFICATION DATA SUMMARY D48100) SHOWED SIGNS OF OVERHEATING. AFTER REMOVING THE INSULATION, IT WAS DISCOVERED THAT THE RIBSDR CA150703005Stab System · failed(CAN) AFTER DEPARTURE, HAD THE STAB TRIM AMBER CAS MESSAGE POST ON THE EICAS. CONTINUOUSLY RE-EVALUATED THE SITUATION AND EXPLORED SOME POTENTIAL OPTIONS. FLEW AT A REDUCED ALTITUDE AND AIRSPEED AND REMAINED CLEAR OF RVSM AIRSPACE. MAINTENANCE REPORTED FAUSDR CA150527002Bushing · migrated(CAN) LEFT & RIGHT MAIN GEAR AFT MOUNTING BUSHINGS MIGRATING. DISCOVERED DURING SCHEDULED INSPECTION. MANUFACTURER CORRESPONDENCE HAS INDICATED THAT NO MIGRATION IS ALLOWED.SDR EBVR20150423001Nut · missingOPENING ENGINE COWLING FOUND A USED VARIABLE GEOMETRY VANE SPINDLE TAB WASHER P/N 3044T06P01 LAYING IN THE BOTTOM CORE COWLING. INSPECTION DISCOVERED ONE SPINDLE NUT, P/N 4037T84P04 MISSING. GENERAL ELECTRIC SERVICE BULLETIN CF34BJ 72-0157 - STAGES IGV-5 SEL
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