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 = 'CF348C1' 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 = 'CF348C1' 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 SIMA200432911Charger · shortedAPU BATTERY CHARGER SHORTED INTERNALLY AND CAUGHT FIRE WHILE AIRCRAFT POWER WAS ON. POWER WAS REMOVED AND FIRE WAS PUT OUT. FIRE WAS NOT SEVERE AND NO DAMAGE WAS NOTED TO THE AREA. BATTERY CHARGER WAS CONTAMINATED WITH SKYDROL FROM ECOLOGY BOTTLE THAT WAS NSDR CA041224005Door · separated(CAN) FOLLOWING DEPARTURE, FLIGHT CREW HEARD A BUMP. POST FLT INSPECTION REVEALED THAT THE RT INBOARD MLG DOOR WAS MISSING. IN ADDITION IT WAS FOUND THAT THE RT IB FLAP SUFFERED SEVERAL DEEP GOUGES, THE RT PROXIMITY HARNESS CONDUIT WAS DENTED, THE RT OB MLSDR SIMA200432701Battery Pack · dischargedCREW REPORTS ON PRE-FLIGHT EMERGENCY LIGHTS WILL NOT TEST. FOUND EMERGENCY LIGHT SWITCH LEFT IN THE ON POSITION. REPLACED BATTERY PACK NR 1,2,3, AND 4, IAW CRJ700 MM 33-50-17. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. SN 1) 85317 2) 85318 SDR VNAA0411003Tiller · failedTHE CREW OF FLIGHT 2239 RECEIVED A STEERING INOP CAUTION MESSAGE ON ROLLOUT AFTER LANDING AT DAY. USING DIFFERENTIAL THRUST & BRAKING THE AIRCRAFT WAS TAXIED OFF OF RUNWAY 24L ONTO THE PARALLEL TAXIWAY AND STOPPED. THE AIRCRAFT WAS THEN TOWED TO THE GATE WHESDR ASOA04898Step · brokenDURING HANGER MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN AT THE ATTACH LINK. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.SDR ASOA04892Vane · false indicationFOLLOWING TAKEOFF, CREW RECEIVED A STALL FAIL CAUTION MESSAGE. QRH WAS COMPLIED WITH AND APPROXIMATELY 250 KNOTS THE STICK SHAKER BEGAN TO SHAKE THE CONTROLS. THE AIRSPEED WAS INCREASED ABOVE 250 KNOTS AND PITCH LOWERED TO INCREASE ABOVE THE LOW SPEED CUE. SDR VNAA0411001Engine · malfunctionedON TAKEOFF ROLL THE RT ENGINE FAILED TO MAKE RATED POWER AND THE CREW OF FLIGHT 2219 ABORTED THE TAKEOFF AND RETURNED TO THE GATE. TARGET POWER WAS 89.1 PERCENT, THE ENGINE SPOOLED TO 80.2 PERCENT. PSA MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND PERFORMEDSDR SIMA200431703Ejector · crackedDURING CRUISE FLIGHT, CREW REPORTED FUEL TRANSFERRED FROM THE RT WING TO THE CENTER TANK WITH BOOST PUMPS OFF. MAINTENANCE FOUND THE RT PRIMARY EJECTOR CRACKED. THE EJECTOR WAS REPLACED WITH A NEW TYPE EJECTOR IAW EO CR-2800-019. OPERATIONAL AND LEAK CHECKSSDR QXEA200400737Chimney · damagedMAINTENANCE FOUND THE FORWARD CARGO BAY FIRE DETECTION CHIMNEY DAMAGED WHILE PERFORMING THE LINE CHECK. THE CHIMNEY WAS REPLACED AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR COMA0470078Engine · flamed outFLIGHT 5655 LT ENGINE FLAMED OUT DURING DESCENT FROM FL 410. NO FAULTS IN MDC, RAN ENGINE, NO DEFECTED NOTED.SDR QXEA200400728Pump · leakingFLIGHT RETURNED TO FIELD AFTER THE NR 2 HYDRAULIC SYSTEM FAILED. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR 2 ENGINE DRIVEN PUMP LEAKING. A NEW PUMP WAS INSTALLED, OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR CA041031002Window · cracked(CAN) THE PILOT SIDE WINDOW CRACKED WHILE IN CRUISE. THE WINDOW WAS REPLACED IN ACCORDANCE WITH AMM.SDR QXEA200400727Chimney · tornDURING MAINTENANCE INSPECTION, MAINTENANCE FOUND THE FORWARD CARGO BAY CHIMNEY DAMAGED. MAINTENANCE REMOVED AND REPLACED THE CHIMNEY. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR ASOA04815Step · crackedDURING AN A-CHECK, THE BOTTOM STEP ON THE PASSENGER DOOR NEXT TO THE ATTACH LINK WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.SDR SIMA200429815Bulb · inoperativeCREW REPORTED THE OVERHEAD REAR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED THE BULB. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.SDR VNAA0410012Pump · failedDURING CRUISE THE CREW REPORTED A NR 1 HYDRAULIC SYSTEM HIGH TEMP CAUTION MESSAGE. TWO SECONDS LATER O/B SPLRON, O/B FLT SPLRS, O/B GND SPLRS, & HYD 1 LOW PRESS CAUTION MESSAGES WERE RECEIVED. THE CREW ELECTED TO DIVERT FLIGHT 2219 TO DAY WHERE MAINTENANCE WSDR QXEA200400726Bulkhead · corrodedCORROSION ON BULKHEAD WEB JUST ABOVE FLOOR SUPPORT BEAM AT STATION FS280.0 AT APPROXIMATELY 25 DEGREES LT BL. REPAIRED IAW EA R-53-214.SDR QXEA200400725Bulkhead · corrodedCORROSION ON BULKHEAD WEB JUST ABOVE FLOOR WEB APPROXIMATELY RT BL 12.0, REPAIRED IAW EA R-53-514.SDR QXEA200400721Floorbeam · corrodedCOCKPIT FLOORBEAM WITH CAMLOCK RECEPTACLES ON IT AT JUST FORWARD OF FS 280 HAS CORROSION ON TOP OF C CHANNEL. REPAIRED IAW REO 670-53-1-095 AND SRM 51-42-06-001-001.SDR ASOA04796Step · crackedDURING A C-CHECK, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE TOP STEP ON THE PASSENGER DOOR.SDR ASOA04783Lamp · burned outDURING AN A-CHECK, THE RT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RT EXTERIOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.SDR ASOA04778SCompressor · damagedDURING TAKEOFF, CREW EXPERIENCED A RUMBLE AND YAW IN A/C ACCOMPANIED BY A COMPRESSOR STALL ON RT ENGINE ALONG WITH TOWER ADVISING OF FLAMES COMING OUT OF ENGINE. CREW REDUCED RT ENGINE TO IDLE WITH ALL PARAMETERS REMAINING AT NORMAL, NO FIRE INDICATIONS PRESESDR CA041010002Compressor · stalled(CAN) DURING TAKE-OFF, THE RT ENGINE EXPERIENCED COMPRESSOR STALLS. MAINTENANCE BORESCOPED THE RT ENGINE AND FOUND FOD DAMAGE IN THE COMPRESSOR SECTION. ENGINE WAS THEN REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR CA041010003Valve · leaking(CAN) CREW REPORTED HYD 2 LOW PRESS, NR 2 EDP FAIL, IB AND OB SPOILERS FAIL, NR 2 HYD QUANTITY READING ZERO. AIRCRAFT DIVERTED, DUE TO WEATHER. MAINTENANCE FOUND THE MLG DOWNLOCK ASSIST VALVE LEAKING. MAINTENANCE REPLACED THE DOWNLOCK ASSIST VALVE, THE SYSSDR QXEA200400700Floorbeam · corrodedCABIN FLOORBEAM, AFT SIDE OF FS 280 BULKHEAD, UPPER SURFACE IS CORRODED IN MULTIPLE LOCATIONS BETWEEN LBL 36 AND RBL 16. REPAIRED IAW HORIZON AIR EA R-53-209 AND CRJ SRM 51-21-06, PARAGRAPH 3A, B, D, PAGE 2 AND 4.SDR QXEA200400698Floorbeam · crackedCABIN FLOORBEAM LOCATED AT FS 280.00 HAS CRACK AT WL 69.95, EXTENDING FROM RBL 8.2 TO RBL 10.1. REPAIRED IAW EA R-53-209.SDR QXEA200400691Bulkhead · corrodedUPPER SURFACE OF CABIN FLOOR SUPPORT CHANNEL IMMEDIATELY AFT OF COCKPIT BULKHEAD AT FS 280.00 IS CORRODED FROM LBL 22.0 TO RBL 22.00. REPAIRED IAW EA R-53-203.SDR QXEA200400686Floor Support · crackedUPPER SURFACE OF CABIN FLOOR SUPPORT CHANNEL, IMMEDIATELY AFT OF COCKPIT BULKHEAD AT FS 280.00 IS CRACKED AT TWO PLACES. REPAIRED IAW EA R-53-205 AND REO 670-53-11-042 AND REO 670-53-11-043.SDR QXEA200400685Floor Panel · corrodedAFT SUPPORT BEAM FOR COCKPIT FLOOR PANEL 221 ALF IS CORRODED ON UPPER SURFACE. REPAIRED IAW CRJ-700 SRM 51-40-11 AND SRM 51-25-06.SDR CA040918002Control Unit · failed(CAN) WHILE CLIMBING THROUGH 7200 FEET, THE CAPTAIN WAS MAKING SMALL INPUTS TO STAB TRIM. MACH TRIM CAUTION MESSAGE APPEARED FOLLOWED RIGHT AFTER BY A STAB TRIM CAUTION. THE STAB WAS NOT RESPONDING TO INPUTS. PILOT TRIED TO RE-ENGAGE THE STAB AND NEITHER CHASDR COMA0470069Selector Valve · malfunctionedFLIGHT 5369 GEAR DISAGREE WARNING. REPLACED THE LANDING GEAR SELECTOR VALVE.SDR SIMA200425901Hydraulic Line · leakingIN CRUISE, HYDRAULIC SYS, 2 FAIL. QUANTITY WENT TO 10 PERCENT. CREW FOLLOWED AOM AND SHUT NR 2 SYS DOWN, DIVERTED/LANDED AT NEAREST SUITABLE AIRPORT, AND DECLARED EMERGENCY. LANDED WITHOUT INCIDENT AND DID NOT LAND OVERWEIGHT. HYDR TEMP REMAINED AT 48 DEGRSDR QXEA200400648Windshield · failedTHE FLIGHT DIVERTED WHEN THE CREW HEARD A LOUD BANG AND NOTICED THE FIRST OFFICERS WINDSHIELD HAD SHATTERED. MAINTENANCE INSPECTED THE A/C AND REPLACED THE RT WINDSHIELD. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR QXEA200400628Chimney · tornMAINTENANCE FOUND THE FORWARD CARGO BAY CHIMNEY TORN. MAINTENANCE REPLACED THE CHIMNEY AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR VNAA0408006Warning Light · illuminatedDURING CLIMBOUT, THE CREW RECEIVED A MACH AND STAB TRIM FAIL INDICATION AND RETURNED TO CLT. MAINTENANCE INSPECTED AND RESET CIRCUIT BREAKERS CBP-1, F-1, P-2, R-4, R-3, AND F-1 AND THE MESSAGE CLEARED. THEN MAINTENANCE ALSO PERFORMED OPERATIONAL CHECKS ON TSDR CA040815001Window · cracked(CAN) PILOT'S SIDE WINDOW CRACKED DURING CRUISE. SIDE WINDOW WAS REMOVED AND REPLACED.SDR CA040830015Blade · damaged(CAN) DURING TAKEOFF ROLL, CREW NOTED VIBRATION FROM NR 2 ENGINE, FOLLOWED BY ENGINE SURGE AND UNCOMMANDED POWER ROLL-BACK. THE NR 1 ENGINE WENT INTO APR MODE AND THE TAKEOFF WAS ABORTED. BORESCOPE INSPECTION OF THE NR2 ENGINE COMPRESSOR REVEALED MOST BLADESSDR QXEA200400577Control Panel · failedFLIGHT 4199, ON TAKE OFF ROLL, THE CREW RECEIVED A MASTER WARNING FOR "CONFIG RUDDER" AND OBSERVED THE RUDDER TRIM CONTINUE TO MOVE OUT OF THE TAKE OFF RANGE. THE TAKE OFF WAS ABORTED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE AILERON/RUDDER CONTROL SDR QXEA200400622Bulkhead · crackedBULKHEAD CRACKED AT BATHTUB FITTING RT SIDE OF AFT PRESSURE BULKHEAD. REPAIRED IAW REO 670-53-61-034.SDR QXEA200400623Pan · crackedRT PYLON PRESSURE PAN CRACKED AT AFT HYDRO, FITTING. REMOVED RT PYLON PRESSURE PAN. DRILLED UP AND INSTALLED INTERNAL DOUBLER IN NEW PAN. INSTALLED NEW PAN AND COMPLETED INSTALLATION AT FASTENERS THROUGH NEW PAN IAW SRM 51-42-06.SDR QXEA200400561Blade · vibrationBOI - FLIGHT 2520 ON CLIMB, RIGHT ENGINE N1 VIBRATION 1.8. REDUCED POWER/CHECKLIST, DROPPED TO 1.3. MAINTENANCE COMPLIED WITH INSPECTION OF FAN BLADES, LOOSENED STIFF BLADE. COMPLIED WITH VIBRATION CHECK, WITHIN LIMITS. PLACED ON RSI TO LUBE FAN BLADE TANGSDR ASOA04491Blade · damagedFLT 4509 - DURING CRUISE FROM ONT-DFW, AT APPROXIMATELY 37,000 FEET THE CREW NOTICED THE RIGHT ENGINE FAN VIBRATION ENTER THE CAUTION RANGE OF 1.8 AND DECREASED THE ENGINE POWER, AT WHICH TIME THE FAN VIBRATION INCREASED TO 2.1. THE AIRCRAFT DIVERTED INTO TUSSDR VNAA0406017B-Nut · failedON CLIMBOUT, THE CREW RECEIVED A NR 2 LOW PRESSURE AMBER CAS MESSAGE. THE AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE RESECURED THE B-NUT ON THE LEFT HAND SIDE OF THE NOSE GEAR AND INSPECTED THE NR 2 SYSTEM HYDRAULIC LINE PRESSURE IN ACSDR CA040704001Windshield · cracked(CAN) ENROUTE THE F/O'S WINDSHIELD SHATTERED, CREW ELECTED TO DIVERT. MAINTENANCE REPLACED WINDSHIELD.(SEE ALSO: US NR 2004071600072)SDR QXEA200400427Impeller · vibrationPDX - ON FLIGHT NUMBER 2555, ON CLIMBOUT, NR 1 FAN VIBRATION ROSE ABOVE 1.7. AFTER LERCHING AT 29,000 FT, AIRCRAFT COULD NOT MAINTAIN CRUISE SPEED WITH POWER SET TO KEEP FAN ON THE GREEN ARC. FOUND ONE BLADE TIGHT. LOOSENED AS REQUIRED. GROUND RAN AIRCRAFTSDR QXEA200400430Shutoff Valve · inoperativePDX - ON FLIGHT NUMBER 2555, AFTER DEPARTURE THE AFT LAVATORY SMOKE DETECTOR WARNING MESSAGE APPEARED. FLIGHT ATTENDANT REPORTED SEEING SMOKE NEAR THE CEILING OF CABIN. SMOKE HAD AN ACRID SMELL TO IT. REPLACED THE 4TH STAGE SHUT OFF VALVE ON NR 2 ENGINE, FOSDR ASO2004F00019Torque Link · disconnectedDURING CLIMB OUT, THE CREW SELECTED GEAR UP AND THE GEAR HANDLE WOULD NOT MOVE FROM THE DOWN POSITION. SEVERAL SECONDS LATER THEY RECEIVED A WEIGHT ON WHEELS INPUT CAUTION MESSAGE FOLLOWED BY A NOSE WHEEL STEERING INOPERATIVE CAUTION MESSAGE. QRH PROCEDURES SDR COMA0470046Fan Blade · vibratesFLIGHT 5672 NR 2 ENGINE FAN VIBE INDICATES 2.4. REPLACED THE RT ENGINE FAN BLADES.SDR QXEA200400354Fan Blade · lack of lubeOKC FLIGHT 4182 ON CLIMBOUT OF DEN, NR 2 ENGINE VIBRATION AT 1.3, CLIMBING THRU 26K FT VIBRATION WENT TO 1.8 AS PER CHECKLIST, REDUCED POWER ON NR 2 ENGINE, VIBRATION BACK IN GREEN AT 1.6. MAINTENANCE COMPLIED WITH TASK 72-21-02-200-803-A01, PART 2, FAN BLADESDR COMA0470043Fan Blade · vibrationFLIGHT 5249 LT ENGINE FAN AT 2.3 VIBES. REPLACED THE LT ENGINE FAN BLADES.
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