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 = 'CF343A' 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 = 'CF343A' 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 2021FA0000132Flap Track · bindingFAILURE OF THE FLAPS AT 10 DEGREES. CORRECTIVE ACTION WAS LUBRICATION OF THE FLAP ACTUATORS IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUALS FOLLOWED BY AN OPERATIONAL CHECKSDR CA190416014Actuator · failed(CAN) AOG DUE TO HSTA FAILURE PREVIOUSLY INSTALLED HSTA HAS BEEN A NFF. (TC# 20190416014)SDR WWQA20180213001Carbon Seal · leakingWITH PACKS SELECTED OFF AND APU BLEED AIR SELECTED ON, STARTED THE RT ENGINE. NOTICED SMOKE COMING OUT OF FORWARD AIR CONDITIONING VENTS IN COCKPIT. STARTED THE LT ENGINE AND SMOKE BEGAN BILLOWING OUT OF COCKPIT FORWARD AND SIDE CONSOLE AIR CONDITIONING VENTSDR MXIA2016051800001Hinge · crackedDURING A SCHEDULED NDI INSPECTION OF THE CABIN DOOR HINGE A CRACK WAS DETECTED ON 1 OF THE LOBES OF THE DOOR SIDE HINGE HALF. EDDY CURRENT METHOD OF NDI WAS USED.SDR 2016FA0000247Tire · failedRIGHT MAIN INBD TIRE HAS A PORTION OF THE TREAD THAT SEPARATED ON LANDING. NEW TIRE WAS INSTALLED AT WHEEL ASSY O/H.SDR CA160311002Lever · stuck(CAN) DURING OPERATIONAL CHECKS OF LANDING GEAR SYSTEM GEAR SWINGS, THE EMERGENCY SYSTEM HAS BEEN ACTIVATED. THE GEAR EXTENDED WITH OUT ANY ISSUES. FOLLOWING STEPS CALLED FOR PLACEMENT OF TARGETS ON THE MAIN GEAR TO ACTIVATE NR 2 ELECTRICALLY DRIVEN HYDRAULIC SDR CA150327002Screw · broken(CAN) LT ACME SCREW ADJUSTING FOUND BROKEN FOLLOWING PILOT REPORT.SDR CA150108002Engine · shutdown(CAN) CUSTOMER REPORTS THE LEFT ENGINE SHUT DOWN UN-COMMANDED. THE AIRCRAFT WAS ON DESCENT. THE PILOTS THINK THEY HAD A COMPRESSOR STALL. THE LEFT ENGINE SHUTDOWN. THE PILOTS DIVERTED TO HOME BASE AND LANDED UNEVENTFULLY.SDR LOMA2015F00009Shutoff Valve · leakingRIGHT 10TH STAGE BLEED AIR WARNING ILLUMINATED. DIVERTED FOR REPAIR. REPLACED 10TH AND 14TH STAGE BLEED AIR SHUTOFF VALVES.SDR CA141114001Landing Gear · failed(CAN) AT APPROX. 5 MILES FINAL RUNWAY 16, AN EXECAIRE CANADAIR CL600-2B16 REPORTED A POSSIBLE NOSE GEAR PROBLEM. DID A FLY BY AND NOSE GEAR WAS NOT OBSERVED TO BE DOWN. DID A VFR CIRCUIT AND RECYCLED THE GEAR WHICH RESULTED IN A "THREE GREEN" INDICATION. AIRCRSDR CA140606002Control Cable · failed(CAN) DURING AN 60 MONTH INSPECTION. THE TECH FOUND BY VISUAL CHECK UP, WHEN HE OPEN THE PANEL IN THE VERTICAL STABILIZER RT SIDE.SDR CA140408007Switch · malfunctioned(CAN) DURING A MAINTENANCE INSPECTION OF THE AIR CONDITION OVERHEAT SWICHES ON BOTH ACU FAIL THE TEST, FOUND INOPERATIVE, DURING THE FUNCTIONAL TEST AS REQUIRED BY THE MM PSP 601-2 , CHAP 21-51-3, P201, THIS CHECK IS REQUIRED AT EVERY 4800 HRS MCN 05-0000-048SDR KW3R2014032617085Windshield · crackedDURING APPROACH, LT WINDSHIELD CRACKED, CREW PERFORMED ABNORMAL PROCEDURES AND LANDED WITH NO FUTHER PROBLEMS.SDR CA130626005Wire · failed(CAN) DURING A PREFLIGHT CHECK THE PILOT COULD NOT OPERATE THE PITCH TRIM AND FOUND THE BREAKER CHANNEL NR 2 POP OUT. AFTER THE INVESTIGATION BY THE AME HE FOUND THAT THE BUNDLE WIRES THAT GOES ON THE CANNON PLUG P8CD ATTACH TO THE TRANSIENT SUPPRESSOR BOX WASSDR CA130610014Selector Valve · failed(CAN) ON DEPARTURE WHEN THE LANDING GEAR WAS SELECTED TO THE UP POSITION THE NOSE GEAR WOULD NOT RETRACT, A FERRY FLIGHT PERMIT WAS ISSUED TO FACILITATE POSITIONING TO BASE FOR REPAIR. THIS IS THE SECOND TIME THIS FAILURE OCCURED ON THIS ACFT, THE PREVIOUS OCCSDR CA130528010Control Handle · failed(CAN) DURING TAKE-OFF THE GEAR HANDLE WAS SELECTED TO THE UP POSITION. THE MAIN LANDING GEAR RETRACTED AND INDICATED AS BEING RETRACTED HOWEVER, THE NOSE LANDING GEAR INDICATED DOWN ON THE LANDING GEAR LIGHT PANEL AND THE GEAR HANDLE FLASHING RED. THE QRH GEARSDR CA120529001Door · separated(CAN) PASSAGER DOOR DEPARTED IN FLIGHT. INVESTIGATION TEAM HAS RETURNED FROM THE ACCIDENT SITE. THE ACFT DAMAGE AND GOLF COURSE, WHERE THE PASSENGER DOOR LANDED, WAS SURVEYED BY THE INVESTIGATION TEAM. ADDITIONAL DOOR REMAINS WERE FOUND AT THE GOLF COURSE. THESDR CA120405004Fuel Control · malfunctioned(CAN) DURING DESCENT, BOTH THRUST LEVERS WERE RETARDED TO IDLE. THE RT ENGINE FLAMEDOUT. THE CREW ELECTED TO CONTINUE WITH THE APPROACH SINGLE ENGINE. THE CUSTOMER IS REQUESTING TROUBLESHOOTING GUIDE LINES. ACFT WAS 5.5 HRS INTO FLIGHT LEG, STARTING DESCENTSDR CA120321004Actuator · failed(CAN) AFTER TAKE OFF THE FLAP FAIL AT 20 DEGREES DOWN, THE AIPLANE FLEW TO DESTINATION WITH THE FLAPS AT 20 DEGREES AND LANDED WITHOUT INCIDENT.SDR CA120127001Window · cracked(CAN) IN CRUISE THE PILIOT SUDDENLY SEE THAT THE LT SIDE WIDOW CRACKED, WENT FROM 24,000 TO 13,000 WITHOUT PANIC SLOWLY TO MAKE SURE THAT THE WINDOW DOESN`T BREAK AS A SAFETY PRECAUTION AND BECAUSE HE WAS GOING TO THE THE HOME BASE HE DIDN`T HAVE TO CANCEL HISDR CA120104009Line · leaking(CAN) HYDRAULIC NR 3 LOSS CAUSING AN EMERGENCY GEAR EXTENSION. THE HYDRAULIC LEAK WAS LOCATED ON ACMP 3 A HOSE PUMP PRESS LINE.SDR CA110328003Strut · binding(CAN) DURING AN APPROACH IN CYUY MARCH 27 2011 ,THE NLG REFUSE TO DESCENT .THEY DID THE EMERGENCY LANDING GEAR PROCEDURE AND IT DIDN`T WORK.THEY HAD IN THE COCKPIT AN INDICATION OF NLG IN TRANSIT AND WOW INPUT FAIL.SO WITH THE MTCE THEY PRESUME THAT THE GEAR WSDR CA110112009Support Beam · crackedTHIS SDR SHOULD HAVE BEEN ISSUED IN JULY 2010 WHEN DISCOVERED. MISTAKENLY OMITTED. DURING EXCHANGE OF AN APU, THE TECHNICIAN NOTICE A CRACK ON THE UPPER WEB, AFT WEB AJ RGL 9.5 AND UPPER ATLBL 9.5 ENG SUPPORT BEAM FS 640. TEMPORARY REPAIR WAS DONE IAW RE 0 SDR 2010FA0000201Frame · crackedFWD FUSELAGE FRAME AT FS235 ABOVE FLOOR, PILOTS AND COPILOTS SIDE, FOUND CRACKED. DURING 240 MONTH INSP.SDR CA091216003Fuel Control · malfunctioned(CAN) THE ENGINE WAS IN FLIGHT AT 9000 FT WHEN A REQUEST WAS MADE TO AIR TRAFFIC TO INCREASE TO NEXT ALTITUDE. AFTER THE REQUEST WAS GRANTED, THE PILOT ADVANCED THE THROTTLE TO ACHIEVE SPEED AND ALTITUDE. AT THIS TIME, AN ENGINE FLAMEOUT OCCURED. THE PILOT WASDR CA090529001Cable · worn(CAN) DURING APPROACH THE CREW EXPERIENCED MULTIPLE COMPRESSOR STALLS ON THE LT ENG. THEY CARRIED OUT THE APPROACH WITH THAT ENGINE AT IDLE. AT ONE POINT, THE ITT STARTED RISING AND THE CREW ELECTED TO SHUTDOWN THE ENGINE FOR THE REMAINING OF THE APPROACH. THESDR CA090525006Cowling · departed(CAN) OPERATOR REPORTED THE FOLLOWING TO MFG: DURING A PASSENGER FLIGHT THE LT UPPER ENGINE COWL ACCESS PANEL (PN 228-50080-801) DEPARTED THE ACFT DURING FLIGHT. THE INCIDENT PANEL WAS REMOVED FOR MX ON THE THRUST REVERSER THE NIGHT PRIOR TO THE INCIDENT FLIGHSDR 2008FA0000358Control Box · failedCREW REPORTED FLAP FAILURE DURING APPROACH APPROXIMATELY 8 HOURS AFTER INSTALLATION. RESET SYSTEM AND FLAPS WORKED FINE. FLEW AIRCRAFT HOME AND NO DISCREPANCIES. UNABLE TO DUPLICATE PROBLEM UNTIL SEVERAL WEEKS LATER DURING MAINTENANCE RUN. FLAPS WOULD IMMEDIATSDR CA070403005Water Heater · odor(CAN) WHILE EN ROUTE, A BURNING ODOR WAS NOTICED BY THE CREW AND PASSENGERS. NO SMOKE WAS APPARENT IN THE CABIN OR COCKPIT. THEN SEARCHED THE LAVATORY AND BAGGAGE COMPARTMENT. A TRACE OF SMOKE WAS FOUND IN THE BAGGAGE COMPARTMENT. A QUICK VISUAL INSPECTIONSDR 2007FA0000298Inverter · shortedWHEN TURNING MAIN BATTERY SWITCHES ON, MECHANIC HEARD A LOUD POPPING SOUND, FOLLOWED BY THE AROMA OF SMOKE IN THE ENTRANCE AREA OF THE AIRCRAFT. THE FLOORBOARD WAS REMOVED AND FOUND THAT WATER FROM THE FORWARD LAVATORY AREA HAD BEEN RUNNING ONTO THE TOP OF THSDR CA070125001Actuator · inoperative(CAN) RT MAIN LANDING GEAR UNLOCK INDICATION APPROX. 15 - 20 MIN. AFTER ARRIVAL, NO PUMP, NO GEAR COMMAND, LOCK PARTIALLY MOVED TO UNLOCK POSITION. RETRACTING ACTUATOR REPLACED AND AC RETURNED TO SERVICE.SDR CA061227006Windshield · broken(CAN) RT WINDSHIELD FACE PLY BROKEN IN FLIGHT. APPROX. 7000 INCH ON APPROACH. FOD INSPECTION CARRIED OUT ON ENGINE INTAKE AND WINDSHIELD REPLACED. A/C HOURS; 6836 A/C CYCLES; 7326 (TC NR 20061227006)SDR CA061218015Pump · damaged(CAN) LOST OF NR 3 SYSTEM HYDRAULIC FLUID IN FLIGHT. THE NR 3B PUMP HAS FAILED ON FLANGE GASKET. THE PUMP HAS BEEN REPLACED AND A\C RETURNED TO SERVICE. A/C HOURS: 6816:27 A/C CYCLES ; 7302 (TC NR 20061218015)SDR CA061208001Actuator · cracked(CAN) DURING SCHEDULE LUBRICATION OF THE FLAP ACTUATORS, THE TECHNICIAN NOTICED GREASE WAS OOZING OUT OF A CRACKED WELD ON THE HOUSING OF THE LT OB FLAP ACTUATOR JACK SCREW. (TC NR 20061208001)SDR CA061116003Bulkhead · cracked(CAN) BULKHEAD STRUCTURE AT STATION 559.00 CRACKED ON TWO AILERON MIXER (P/N 600-91154-5) ATTACHMENTS BOLTS. A/C HOURS:25688 A/C CYCLES:30488SDR CA061103011Control Unit · failed(CAN) DURING TAKE OFF FLAP FAIL DURING FLAP RETRACTION, A/C RETURN TO TERMINAL .BREAKER RESET AS PER OPERATING MANUAL NR 1 ABNORMAL PROCEDURE SECTION 10 P 3-4. A/C RETURN TO SERVICE ,NO FURTHER SNAG.TWO MORE TAKE -OFF WERE CARRIED OUT FOLLOWING THAT INCIDENT,SDR CA061010005Flap System · malfunctioned(CAN) FLAP FAIL BETWEEN 20 DEGREES TO 0 DEGREE DURING RETRACTION OF THE FLAPS AT TAKEOFF , FLAPS RESET ON GROUND IAW OPERATING MANUAL NR 1 ABNORMAL PROCEDURE SECTION 10 P3-4. A/C RETURN TO SERVICE. NO SNAG. FLAP FAIL BETWEEN 20 DEGREES TO 0 DEGREE DURING RETSDR CA060918001Flap System · malfunctioned(CAN) FLAP FAILED ON TAKEOFF, A/C RETURNED AND LANDED SAFELY AT QB MAIN BASE, BREAKER WAS RESET IAW OPERATING MANUAL, COULDN`T DUPLICATED THE SNAG. A/C DID ONE FLIGHT AND RETURN TO BASE WITHOUT ANY SNAG.SDR CA060828001Pump · broken(CAN) LT MAIN AND SCAVENGE EJECTOR FAILURE (MOTIVE FLOW FAILURE). FUEL PUMP SHAFT FOUND BROKEN. FUEL PUMP REPLACED AND AIRCRAFT RETURNED TO SERVICE. A/C HOURS; 25194:25 CYCLES; 29896 (TC NR 20060828001)SDR CA060712003Feeder Cable · arced(CAN) RT GEN TRIPPED OFFLINE DURING APPROACH. GEN OFF ANNUNCIATOR CAME ON, PWR AUTO TRANSFERED FROM GEN 1. NO LOSS OF PWR ON ANY AC BUSES. AC FERRIED WITH GENERATOR 2 SELECTED OFF. ON 3RD ENGINE RUN, PROBLEM WAS DUPLICATED. PROBLEM WAS ISOLATED TO A WIRING PROSDR CA060428002Transformer · inoperative(CAN) LOSS OF NR 1 MASI, NR 1 ALTIMETER, FDR, NR 1 ADI PITCH AND ROLL INFO, COMPASS INFO, NR 1 ESSENTIAL BUS AND LOSS 26 VAC. CAUSE OF FAULT FOUND TO BE BROKEN WIRES AT T2XD POST NR 3. TRANSFORMER LOCATED ON BACK OF C/B PANEL C. (TC NR 20060428002)SDR DJFA2005143Engine · overservicedKAPA - KSMO - WHILE CLIMBING THROUGH 15,000 FEET, THE NR 2 ENGINE OIL TEMPERATURE BEGAN TO RISE INTO THE AMBER BAND. WHEN POWER WAS REDUCED THE OIL TEMPERATURE CONTINUED TO RISE INTO THE RED BAND. ENGINE POWER WAS REDUCED TO IDLE. AN EMERGENCY WAS DECLARED SDR CA050920004Wire · overheated(CAN) POST FLIGHT INSPECTION REVEALED EVIDENCE OF OVERHEAT CONDITION FOUND AT 6 O'CLOCK POSITION AT THE COMBUSTOR SECTION FWD FRAME WHEN COWLINGS OPENED TO INVESTIGATE IDG FAILURE. MAINTENANCE PERSONNEL FOUND LOCALIZED AREA WITH OVERHEATED WIRE AND FUEL MANIFSDR UG82005F00006Warning Light · illuminated(REF CNTRL NR PA05003) THERE WAS NOT GREEN (DOWN AND LOCKED) INDICATION ON THE NOSE GEAR. THERE WAS ALSO NO RED (UNSAFE) INDICATION. THE CREW WENT THROUGH THE REQUIRED CHECKLIST AND DECLARED AN EMERGENCY TO TOWER. (K)SDR UG82005F00010Indicator · defective( REF: PA 05-003) THERE WAS NO GREEN DOWN AND LOCKED INDICATION ON THE NOSE GEAR. THERE WAS ALSO NO RED UNSAFE INDICATION. THE CREW WENT THROUGH THE REQUIRED CHECKLIST AND DECLARED AN EMERGENCY TO KDAL TOWER. THERE WERE MULTIPLE FAILURES IN THE GEAR INDICATSDR 2005FA0001071Tire · separated(REF: PA05002) VIBRATION NOTED AT ROTATION SPEED. FLIGHT CREW RETURNED TO POINT OF ORIGIN AND LANDED UNEVENTFULLY. NR 4 TIRE TREAD SEPARATED. THE NR 4 MAIN WHEEL AND TIRE ASSY WERE CHANGED IAW MM. THE AC WAS THEN FERRIED TO A MAINTENANCE BASE TO REPAIR THESDR CA050324002Sensor · inoperative(CAN) ON JANUARY 02, 2005, AFTER TAKE OFF THE LANDING GEAR WERE SELECTED UP (RETRACT). LANDING GEAR REMAINED ON EXTENDED POSITION. AIRCRAFT RETURNED TO DEPARTURE AND LANDED SAFELY WITH NO INCIDENCE. POST FLIGHT INSPECTION REVEALED NO MECHANICAL DAMAGE. LT AND SDR CA041223003Engine · malfunctioned(CAN) UNCOMMANDDED ACCELERATION ON THE LT ENGINE ON TAKE OFF AROUND + 7 PERCENT ABOVE RETURN TO NORMAL 40 SECONDS LATER.SDR DJFA2004032Engine · malfunctionedCREW REPORTED, THAT DURING CLIMB WHILE EN ROUTE FROM KBRO TO KATL CLIMB POWER WAS NOT ACHIEVED. THE NR 1 ENGINE POWER WAS 2 PERCENT LOWER THAN REQUIRED. AIRCRAFT DIVERTED TO KDAL. MAINTENANCE SWAPPED THE P2 AND T2 PROBES BETWEEN THE LEFT AND RIGHT ENGINES ASDR ASOA04576Scavenge Pump · cloggedDURING CRUISE FROM AEX-DFW, AT APPROXIMATELY 22,000 FT WHILE FERRYING THE AIRCRAFT TO DFW THE CREW RECEIVED A RT ENGINE OIL PRESSURE WARNING. THE QRH WAS COMPLIED WITH AND THE CREW WAS ABLE TO MAINTAIN ADEQUATE THRUST TO MAINTAIN LEVEL FLIGHT AT 22,000 FT. T
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