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 = 'CF343B1' 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 = 'CF343B1' 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 SWIA200211366Floorbeam · crackedFS 280.0 RBL AND LBL 9.0 FLOORBEAM INBOARD ANGLES CRACKED. FOUND DURING C CHECK INSPECTION, NEW ANGLES FITTED AND INSTALLED IAW CRJ SRM 51-40-11, 51-42-06 AND 51-42-20.SDR SWIA200211367Intercostal · corrodedINTERCOSTAL AT FS 404.0 AND RBL 1.5 IN AVIONICS CRAWL WAY AFT OF MAIN AVIONICS DOOR HAS SURFACE CORROSION ON SIDE OF INTERCOSTAL, BEYOND LIMITS. FOUND DURING C-CHECK INSPECTION, NDT-ET CONDUCTIVITY CARRIED OUT AND FOUND MATERIAL TO BE 30.20 PERCENT IACS. INTSDR SWIA200211368Rib · crackedRIB AT AFT LOWER ATTACH SCREW OF LEFT PYLON LEADING EDGE PANEL IS CRACKED. FOUND DURING C CHECK INSPECTION. REPLACED RIB IAW CRJ SRM 51-42-06 & 51-23-11. P/N: 601-37004-85.SDR SWIA200211215Damper · faultyNR 1 YAW DAMPER WOULD ENGAGE UNTIL RUDDER MOVEMENT WAS INITIATED THEN NR 1 WOULD AGAIN DISCONNECT. REPLACED NR 1 YAW DAMPER LINEAR ACTUATOR IAW MM 22-22-01. OPS CHECK GOOD.SDR SWIA200211216Bearing · out of positionREMOVE LEFT ENGINE FOR 8:00 VG SHAFT AND BEARING SUPPORT REPAIR (LEFT ENGINE VG SHAFT BEARING 8 O'CLOCK POSITION HAS MIGRATED OUT). REMOVED AND REPLACED LT ENGINE IAW MM 71-00-00.SDR SWIA200211195Carbon Seal · defectiveCLIMBING THROUGH FL240, 250 KTS, APPROX 5 DEGREES PITCH, CLIMB-THRUST, RIGHT ENGINE OIL LOW PRESS WARNING ILLUMINATED. QRH LED TO INFLIGHT SHUTDOWN. OIL PRESS APPROX 23-26 PSI AT 89.0 PERCENT N1. INSTALLED OVERHAULED NR 6 & NR 7 CARBON SEALS AND EXHAUST FRASDR CA020905005Switch · jammed(CAN) CREW NOTED STAB TRIM RUNAWAY IN THE NOSE DOWN DIRECTION DURING CLIMB FROM ATL WHILE ACCELERATING TO 250 KTS. CREW DECLARED EMERGENCY AND RETURNED. MAINTENANCE CONTROL NOTIFIED. MAINTENANCE FOUND INDICATION OF PILOT'S TRIM SWITCH JAMMED IN THE MDC. REMOVSDR CA020827001Bolt · sheared(CAN) ON FINAL APPROACH FOR LANDING, CAPTAIN REPORTED THAT HIS YOKE STUCK AT ABOUT MID-TRAVEL & WAS UNABLE TO MOVE IT IN BOTH DIRECTIONS. CAPTAIN TRIED TO YANK YOKE BACK IN ATTEMPT TO FREE IT, PROCESS THE STICK SHAKER CAME ON. THE CREW FINALLY SUCCEEDED TOSDR CA020903011Precooler · cracked(CAN) WHILE TROUBLESHOOTING THE RT BLEED OVERHEAT PROBLEM HORIZON FOUND THAT THE RT PRE-COOLER HAD TWO CRACKS ONE ON EACH SIDE. THE CRACKS ARE IN THE WELDED AREAS OF THE INLET AND THE OUTLET.SDR CA020904008Apu · failed(CAN) ENGINE GEN NR 2 INOP - DISPATCHED IAW MEL 24-11-1-2 ON THE FLT. (APU GEN REQUIRED TO OPERATE CONTINUOUSLY DURING FLT) DURING FLT APU OIL TEMP CAUTION MSG APPEARED. DIVERTED. APU HAS BEEN REPAIRED AND AIRCRAFT RETURNED IN SERVICE.SDR CA020821001Fitting · broken(CAN) FOUND COMBUSTOR DRAIN FITTING BROKEN ON TWO EXHAUST NOZZLE FAIRINGS DURING "C" CHECK. THIS HAS OCCURED TWICE ON TWO DIFFERENT AIRCRAFT. THE ENGINE SIDE WAS NOT SPECIFIED. INSPECTION OF THE INSIDE OF THE FAIRINGS SUGGESTS THAT UNDRAINED FUEL HAS PRODUCSDR SWIA200211151Brake Assy · malfunctionedON TAKEOFF ROLL, RECEIVED ANTI-SKID INBOARD CAUTION MSG AND PERFORMED A LOW SPEED ABORT (60 KTS) APPLIED LITTLE BREAKING, BUT NR 4 BRAKE TEMP CLIMBED TO 7 WHILE THE REST REMAINED AT (2 OR 3 UNITS). CYCLED POWER OFF & ON. COMPLETED OPS CHECK OF ANTI-SKID. OPSDR CA020822002Window · cracked(CAN) RT SIDE WINDOW CRACKED DURING DESCENT AT APPROX 5000FT. THE WINDOW WAS PRE SERVICE BULLETIN. RT WINDOW REPLACED AND AIRCRAFT RETURNED IN SERVICE.SDR SWIA200211122Torque Link · bentON DEPARTURE OUT OF DFW, DURING GEAR RETRACTION, WARNING MESSAGES GEAR DISAGREE AND NOSE DOOR ANNUNCIATED. THE NOSE GEAR INDICATED DOWN AND LOCKED WITH GEAR SELECTED UP. COMPLETED QRH PROCEDURES AND AFTER BURNING OFF EXCESS FUEL, A NORMAL LANDING WAS MADE BASDR CA020820002Mixer Box · damaged(CAN) WHILE ENROUTE, FLIGHT CREW EXPERIENCED AILERON CONTROL STIFFNESS AND JAM AT 25,000 FT. AUTO-PILOT DISSCONNECTED AND THE CREW WAS ABLE TO FREE THE JAM AND CONTINUED ON WITHOUT FURTHER INCIDENT. THE AIRCRAFT TOOK OFF IN HEAVY RAIN AND THERE WAS STANDING SDR SWIA200211224Angle · corrodedPAX DOOR LWR SILL VERTICAL FLOOR ANGLE CORRODED. DISCOVERED DURING C-CHECK. FITTED AND INSTALLED NEW ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13.SDR SWIA200211225Rivet · corrodedANCHOR NUTS FOR RT OVERWING EMERGENCY EXIT BOTTOM HINGE FITTINGS HAVE CORRODED RIVETS. DISCOVERED DURING C-CHECK. FITTINGS REMOVED FOR ACCESS. RIVETS INSTALLED IAW CRJ SRM 51-42-16. INSTALLED FITTINGS IAW MM 20-21-00.SDR CA020806001Engine · seized(CAN) "WHILE IN CRUISE FLIGHT, THE LEFT ENGINE DEVELOPED A HIGH FREQUENCY VIBRATION, REGISTERING ABOUT 1.5 ON THE VIBRATION METER. ABOUT 30 SECONDS LATER THE N2 WENT TO ZERO. ELECTED TO DIVERT TO IND AND LANDED ABOUT 20 MINUTES LATER. FOUND THE N2 SECTIONSDR CA020730001Selector Valve · failed(CAN) A/C WAS SITTING AT THE GATE WITH AC EXTERNAL POWER SELECTED ON AND HYDRAULIC SYSTEM NR 3 PRESSURIZED. AC POWER HAS BEEN SELECTED OFF WITH HYDRAULIC NR 3 SYSTEM STILL PRESSURIZED WHICH CAUSED THE NLG TO COLLAPSE. DUE TO CHOCKS BEING INSTALLED, NLG DIDSDR CA020807002Engine · failed(CAN) ON PASSING 400 FT ABOVE GROUND AFTER TAKEOFF, A SEVERE 4.5 VIBRATION WAS FELT AND CONFIRMED. ITT INCREASED TO 935 DEGREES CENTIGRADE WITH OIL PRESSURE MASTER WARNING LIGHT. ENGINE SEVERE/FIRE DRILL CARRIED OUT AND RETURN TO ELS. METAL CHIPS FOUND ON THSDR SWIA200211050Tire · blownAC RETURNED TO PHX DUE TO HIGH ENGINE VIBRATION ON LEFT ENGINE. VIBRATION CAUSED BY FOD INGESTION DURING GROUND OPERATION OR TAKEOFF. A LEFT MAIN TIRE BLEW ON ROTATION. ON LANDING THE OTHER LEFT MAIN TIRE FAILED. REPLACED BOTH LEFT MAIN WHEEL ASSYS IAW 32-SDR SWIA200211054Wire · shortedUPON ROTATION IN OKC, THROUGH 10 DEGREE PITCH UP, STICK SHAKER ACTIVATED. WINDSHEAR FAIL STATUS MESSAGE AND CONTINUOUS IGNITION, AIRSPEED WAS ROUGHLY 165 KTS. THEN ON FINAL IN SLC, GEAR WAS COMING DOWN, WINDSHEAR FAIL MESSGE APPEARED AGAIN, CONTINUOUS IGNITISDR SWIA200211057Switch · defectiveYAW DAMPER CH 1 INTERMITTENT, WILL NOT STAY ENGAGED. RETURNED TO THE GATE. REMOVED AND REPLACED CAPTAIN'S STAB TRIM DISCONNECT SWITCH. YAW DAMPER SYSTEM, OPS CHECKS GOOD.SDR CA020725001Acm · malfunctioned(CAN) QUOTE FROM MAINTENANCE CONTROL LOG: "CPT REPORTS THAT ON TAXI OUT SMOKE STARTED FILLING UP CABIN, A/C WAS EVAC THROUGH A/S/D ON TAXIWAY, NO EXITSWERE PULLED. PER CPT NO WARNING OR FAULTS NOTED IN COCKPIT." NO FIRE EXTINGUISHERS WERE UTILIZED. LOCAL MAINSDR CA020715008Handle · corroded(CAN) DURING A C CHECK INSPECTION , WHILE PERFORMING TASK 52-22-00-720-801 THE FUNCTIONAL TEST OF THE CREW ESCAPE HATCH THE MECHANIC FOUND THAT THE OUTER HANDLE OF THE CREW ESCAPE HATCH WOULD NOT UNLOCK PROPERLY ALLOWING THE HANDLE TO EXTEND AND ROTATE. THE HSDR CA020715005Window · cracked(CAN) CO-PILOT SIDE WINDOW CRACKED DURING FLIGHT AT 5000 FEET. DIVERTED FLIGHT TO KOLN, GERMANY.SIDE WINDOW REPLACED. AIRCRAFT RETURNED IN SERVICE.SDR SWIA200211023Control Unit · malfunctionedOUTBOARD GROUND SPOILER FAULT STATUS MESSAGE AND, AFTER ENGINE START, SPOILERONS AND FAULT SPOILER CAUTION MESSAGE. RESET SECU'S IAW FIM 27-61-00.SDR CA020705001Line · chafed(CAN) RT ENGINE OIL REPLENISH LINE WHERE IT EXITS THE AFT EQUIPMENT BAY AND ENTERS THE RT ENGINE PYLON WAS FOUND CHAFED AGAINST A STEEL BRAIDED HYD LINE. OIL LINE REPLACEDSDR SWIA200211006Seal · dirtyCLIMBING THROUGH 25,000 FEET, WITH A CABIN ALTITUDE OF 7.0, A VIBRATION STARTED THAT SEEMED TO BE COMING FROM THE FORWARD GALLEY DOOR. THE FLIGHT ATTENDANT ALSO REPORTED LOUD NOISE AND VIBRATION COMING FROM GALLEY DOOR.REPLACED DOOR SEAL IAW MM 52-41-07. FOSDR CA020704001Trim Switch · failed(CAN) CLIMBING THROUGH FL120 STAB CHANNELS 1 AND 2 DISCONNECTED (STAB TRIM SET AT 8.4 UNITS). CREW WAS UNABLE TO RECONNECT EITHER CHANNEL. CREW DECLARED AN EMERGENCY AND LANDED. AFTER NTSB RELEASE OF A/C MX REPLACED BOTH TRIM SWITCHES AND RETURNED A/C TO SESDR CA020701001Windshield · cracked(CAN) LT WINDSHIELD CRACKED DURING TURNAROUND REPLACED WINDSHIELD IAW AMM 56-11-01 - OPS TEST TEMP CONTROLLED STATUS. AND LEAK CHECK STATUS.SDR CA020704002Windshield · failed(CAN) CREW REPORTED CAPTAIN'S WINDSHIELD SHATTERED IN CRUISE FLIGHT. FLIGHT DIVERTED. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S WINDSHIELD. OPS CHECK AND PRESSURIZATION CHECK CARRIED OUT.THE WINDSHIELD INSTALLED WAS PRE SERVICE BULLETINSDR SWIA200212107Bulb · inoperativeFOUND ON PREFLIGHT INSPECTION SECOND EMERGENCY LIGHT AFT OF FORWARD DOOR (LEFT SIDE) BURNED OUT. RE-LAMPED SECOND EMERGENCY LIGHT ON LEFT OVERWING WITH SERVICEABLE BULB. OPS CHECK GOOD AT THIS TIME.SDR SWIA200210965Actuator · failedON FINAL APPROACH INTO LAX, SELECTED FLAPS 20 DEGREES AND FLAPS STOPPED AT 18 DEGREES. REMOVED AND REPLACED LEFT OUTBOARD NR 3 AND NR 4 FLAP ACTUATORS IAW CRJ MM 27-53-05. CYCLED FLAPS NUMEROUS TIMES. OPS CHECK GOOD ON GROUND. COMPLIED WITH AD 98-20-01.SDR CA020604006Strut · failed(CAN) A/C SLID DOWN RWY 4,000 FEET AT 21:55. WITH 50 PASSENGERS PLUS CREW. NOBODY HURT. A/C ENROUTE WHEN LDG, LT MLG FAILED JUST BELOW RADIUS BELOW AFT TRUNION FITTING. LT WING TIP LOWER SURFACE CONTACTED RWY AS A/C SLID DOWN RWY. LT INBOARD & OUTBOARD FLAPSSDR CA020610002Acm · unserviceable(CAN) AFTER TAKEOFF, WHILE CLIMBING THROUGH 10,000 FT, CREW GOT LT PACK HIGH PRESS CAUTION MESSAGE. PRESSURIZATION WAS NOT BEING MAINTAINED.REPLACED THE RT ACM TO ENABLE THE RIGHT PACK TO BE SERVICEABLE. THE PACKS WERE OPERATED AND FOUND TO BE SERVICEABLE.SDR CA020604001Aileron · jammed(CAN) AT FLIGHT LEVEL 310 AILERON SYSTEM PARTIALLY JAMMED RT AILERON 2 UNITS UP. REQUESTED LOWER ALTITUDE FLIGHT LEVEL 280 AND AILERON IMPROVED. AIRCRAFT FLOWN MANUALLY, APPROACH NORMAL (SUSPECT CABLE RUN HUMIDITY/FROZEN) AILERON REAR LT & RT QUADRANT LUBRISDR CA020531001Switch · failed(CAN) "DURING CLIMB OF THE FLIGHT, THE CREW EXPERIENCED UNCOMMANDED NOSE DOWN PITCH TRIM. THE CREW PERFORMED THE QRH PROCEDURES AND RETURNED TO BASE AND LANDED WITHOUT FURTHER INCIDENT." "MAINTENANCE PERSONNEL REMOVED AND REPLACED THE FIRST OFFICERS YOKE PITCSDR CA020605001Window · cracked(CAN) LEFT SIDE COCKPIT SIDE WINDOW CRACKED AT FL350. REMOVED AND REPLACED LT SIDE WINDOW. OPS AND LEAK CHECK GOODSDR CA020523001Actuator · failed(CAN) FLAPS FAIL ON SHORT FINAL, WITH FLAPS SELECTED AT 450, POST FLIGHT INSPECTION SHOWS RT OUTBOARD FLAP PANEL TWISTED. REMOVED AND REPLACED NR 3 AND 4 ACTUATORS ON RT SIDE. RT FLAP FLEX DRIVE TORQUE CHECKS CARRIED OUT, OK, AND BPSU BRAKE HOLDING CHECK C/WSDR CA020531002Engine · failed(CAN) MAINTENANCE WAS ADVISED BY THE FLIGHT CREW THAT OIL LOW PRESSURE NECESSITATED THE RT ENGINE TO BE SHUTDOWN AS PER THE QRH. VIBRATION DETECTED IMMEDIATELY BEFORE SHUT-DOWN. CONTRACT MAINTENANCE COMFIRMED A SIGNIFICANT AMOUNT OF METAL IN THE GEARBOX. AN ENSDR CA020524003Engine · lightning strike(CAN) LIGHTENING STRIKE TO NR 1 ENGINE. LT ENGINE SHUT DOWN AS A RESULT OF LIGHTENING STRIKE. CREW NEVER CALLED. MECH FOUND LIGHTENING STRIKE: LT AOA VANE, SEVERAL WINDOWS ALONG LEFT SIDE OF FUSELAGE HAD ARC MARKS AND TAILCONE HAD BURN MARKS. MECH INSPECTEDSDR CA020522001Windshield · failed(CAN) CLIMBING THUR 13,500 FT THE CAPT'S WINDSHIELD INNER PLY CRACKED. RETURNED AND REPLACED CAPT'S WINDSHIELD.SDR SWIA200210846Pin · brokenABORTED THE TAKEOFF DUE TO AN AMBER CAUTION IDG 2 MESSAGE ON THE EICAS AND IDG 2 FAULT ON THE OVERHEAD PANEL. INSPECTED IDG 2 & FOUND ELECTRICAL CONNECTOR FOR TEMP BULB HAS A BROKEN PIN. INSTALLED NEW PIN ON CONNECTOR & RESECURED CANNON PLUGS. RAN RIGHT ENGSDR SWIA200210843Window · brokenFIRST OFFICERS WINDOW BROKE WHILE EN ROUTE SMF. DIVERTED TO RNO. REMOVED AND REPLACED COPILOT'S WINDOW. PRESSURIZED AC, CHECKED FOR LEAKS. WINDOW HEAT CHECKS GOOD.SDR SWIA200210848Bpsu · failedFLAP FAIL MESSAGE ON CLIMBOUT. RECEIVED THE FAIL MESSAGE FROM FLAPS 8 DEGREES TO 0 DEGREES. UPON LANDING AND CHECKING THE FLAPS, FLAPS WERE AT 0 DEGREES OR FULLY UP. REMOVED AND REPLACED FLAP BRAKE POSITION SENSOR IAW MM 27-51-10. OPS CHECKED GOOD.SDR CA020517001Windshield · failed(CAN) ON FLIGHT THE CREW REPORTED RT WINDSHIELD INNER PLY SHATTERED UPON LANDING.ENGINEERS REPLACED WINDSHIELD BY S/N 01180H2136 THE WINDSHIELD INSTALLED WAS A POST SERVICE BULLETIN WINDSHIELD.SDR CA020620004Engine · failed(CAN) FOLLOWING TAKE OFF AND PASSING THROUGH 8000 FT ASL, THE FLIGHT CREW RECEIVED A RT ENGINE OIL PRESSURE WARNING MESSAGE. THE CREW COMPLIED WITH THE QRH AND INITIATED AN ENGINE SHUTDOWN. THE AIRCRAFT WAS RETURNED AND AN EMERGENCY WAS DECLARED FDR SHOWN ENGISDR SWIA200210839Bpsu · failedFLAPS FAIL CAUTION MESSAGE ILLUMINATED. REPLACED RIGHT BPSU. OPS CHECKS GOOD.SDR SWIA200210840Control Handle · failedUPON SELECTED FLAPS 20 FLAPS FAILED. LANDED AT FLAPS 6. REMOVED AND REPLACED FLAP SELECTOR HANDLE. OPS CHECK GOOD.
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