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 N6WA2017081002Engine · failedLEFT ENGINE FAILED IN FLIGHT.SDR SWIA201743443Engine · vibrationNR 1 ENGINE VIBRATION EXCESSIVE, N1 VIBRATION INDICATION APPROXIMATELY 2.1. VIBRATION REDUCED BY REDUCING THRUST. SHOOK BLADES OUT. RAN ENGINE, VIBRATION REMAINED AT .2 OR LESS.SDR VNAA2016091000007Engine · bird ingestionAIRCRAFT HIT A FLOCK OF BIRDS DURING CLIMBOUT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND ENGINE DAMAGE. REMOVED AND REPLACED LEFT ENGINE AND PERFORMED CHECKS IAW AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR N6WA2016082902Actuator · leakingNR 2 ENGINE FUEL LEAK. R & R PRIMARY VG ACTUATOR IAW AMM 75-30-01, LEAK AND OPS CHECK GOOD.SDR ASOA2016081115239Engine · failedAFTER TAKE OFF, ACFT BEGAN TO SHAKE, RT ENGINE VIBRATION CAUTION UP TO 6.8. AND ITT WENT RED. SHUT RT ENGINE DOWN AND RETURNED TO DEPARTURE. REMOVED AND REPLACED THE RT ENGINE IAW AMM 71-00-00. INSTALLED RT ENGINE IDG IAW AMM 24-11-01.SDR V0XD20160314058Latch · brokenRIGHT AFT THRUST REVERSER LATCH PIN BROKEN. R & R RT AFT THRUST REVERSER LATCH IAW AMM 78-33-03 & 20-21-00.SDR CA160314007Sensor · failed(CAN) LEFT ENGINE HIGH OIL TEMP, TEMP SENSOR REPLACED.SDR CA160122007Connector · arced(CAN) ESS TRU FAIL MESSAGE WITH CB POPPED. UPON TROUBLESHOOTING FOUND CONNECTOR PL108P1/J1 BURNT. CONNECTOR REPLACED.SDR CA151217003Frame · corroded(CAN) DURING CHECK CORROSION WAS FOUND IN AVIONICS BAY ON ATTACHED FLANGE OF 5EA FRAMES. REMOVAL OF CORROSION WAS PERFORMED IAW SRM 51-21-06, AFTER BLEND OUT NDT INSPECTION FOR CRACKS AND REMAINING THICKNESS WAS PERFORMED WITH NO FINDINGS. FOR DETAILS OF DAMAGSDR SIMA20151012005Stand Off · crackedLEFT ENG, LOWER TRANS COWL, INBD STANDOFF ANGLE IS CRACKED, APPROX .500 INCHES. R & R LT LOWER TRANS COWL STANDOFF IAW SRM 51-42-06 & ETN CR-54-015R1.SDR SIMA20151012004Stand Off · crackedLEFT ENG, UPPER TRANS COWL, INBD STANDOFF ANGLE IS CRACKED, APPROX .500 INCHES. R & R STANDOFF ANGLE IAW SRM CHAPTERS 51-42-20, 51-42-28 & ETN-CR-54-015R1.SDR CA150916014Windshield · cracked(CAN) LT WINDSHIELD CRACKED ON CLIMB AND PERFORMED AN AIR TURN BACK.SDR CA150827001Boot · out of position(CAN) LEFT BLEED DUCT WARNING DURING FLIGHT. COMPLIED WITH QRH. RT BLEED CLOSED CAUSING ULTIMATE LOSS OF PRESSURE. CREW INITIATED AN EMERGENCY DESCENT DUE TO THE LOSS OF CABIN PRESSURE, THE PASSENGER OXYGEN MASKS WERE RELEASED. INSPECTED LT BLEED DUCTS, FOSDR SIMA20150709001Unknown · odorUPON ROTATION NOTICED A BURNING SMELL FROM THE PACK SYS, A SMALL LIKE FEATHERS OR BIRD. POSSIBLE INJECT OF BIRD ON LT ENGINE. PERFORMED FIM TASK 21-22-00, NO ABNORMAL ODOR IN COCKPIT OR CABIN AREA. RAN LT ENGINE & PACK IAW AMM 7100-00, NO DEFECTS NOTED.SDR CA150710007Cable · corroded(CAN) AIRCRAFT HAS A HISTORY OF AUTOPILOT DISENGAGING ON ITS OWN WHILE IN FLIGHT. MDC LOGGED PITCH SERVO CIRCUIT. WHILE TROUBLESHOOTING THE PITCH SERVO CIRCUIT ISSUE, MX NOTICED THAT THE CONTROL WHEEL WAS NOT MOVING DURING THE CHECK OF THE AUTOPILOT AND THAT TSDR CA150710003Proximity Switch · failed(CAN) ON DESCENT CREW GOT A STRONG ELECTRICAL SMELL IN THE COCKPIT, DONNED O2 MASKES & DECLARED AN EMERGENCY. A/C LANDED WITHOUT INCIDENT. MX FOUND PAX DOOR SENSOR PX 107 SMOKED.SDR N6WA2015060601Connector · dirtyLEFT FADEC CAUTION IN FLIGHT. CLEANED CONNECTORS ON THE FMU & MASTER VG ACTUATOR. PERFORMED GND ENG RUN IAW AMM 71-00-00. NO MSGS OR DEFECTS NOTED.SDR ASOA2015060312972Bulb · burned out12 AB AND 12CD LOWER EXIT SIGN HAVE 2 LIGHT BULBS BURNED ON EACH SIGN. R & R LIGHT BULBS IAW AMM 33-51-11. OPS CHECKED GOOD.SDR CA150605004Wire Harness · chafed(CAN) CHAFED NAV LIGHT HOUSING WITH WIRE HARNESS. IT WAS ONLY FOUND AFTER SEVERAL FAILURE OF THE LIGHT AND A MORE EXTENSIVE FAULT ISOLATION.SDR SIMA20150303003Engine · vibrationNUMBER 2 ENG VIBRATION 1.8 - 1.9 IN CRUISE. AMBER VABS ABOVE 10,000 FT. INSPECTED NR 2 ENG FAN BLADES IAW AMM 72-21-02, NO DEFECTS NOTED. PERFORMED VI CHECK IAW PARAMETERS WITHIN LIMITS SEE PIREP NR 4 FOR FURTHER ACTION. DEFERRED IAW MM REF 72-00-00-810-01SDR CA150303008Compressor · stalled(CAN) NR 1 ENGINE COMPRESSOR STALL.SDR MASA2015021612908Engine · power lossNR 2 ENGINE LOST THRUST WITH A HIGH ITT & VIBE CREW SHUTDOWN ENGINE IN FLIGHT, EMERGENCY WAS DECLARED. THERE WAS NO BRACING BY PASSENGERS, ACFT LANDED & TAXIED TO GATE WITHOUT INCIDENT. ENGINE REPLACEMENT WILL BE REQUIRED DUE TO HIGH ITT. THERE ARE NO VISUSDR CA150227007Check Valve · faulty(CAN) ENGINE NR 2 ITT OVERTEMP. ENGINE 2 SHUTDOWN IN FLIGHT IAW QRH. EMER DECLARED. WE WERE IN THE INITIAL DESCENT, ABOUT 25 MINUTES OUT. WE ELECTED TO CONTINUE TO DESTINATION. ALL PROCEDURES & CHECKLISTS WERE FOLLOWED. LANDED & TAXIED TO GATE WITHOUT INSDR CA150107006Control Panel · failed(CAN) - AFTER TAKE OFF RT RUDDER FULL SCALE DEFLECTION WE WERE ABLE TO CENTER USING RUDDER TRIM, FULL SCALE DEFECTION WAS UNCOMMANDED ATB REMOVED AND REPLACED RUDDER TRIM ACTUATOR IAW AMM 27-22-01 REMOVED AND REPLACED AITLERON/RUDDER TRIM PANEL IAW AMM 27-12-SDR CA141217016Actuator · failed(CAN) CREW REPORTED UNCOMMANDED YAW OSCILLATIONS IN FLIGHT, QRH PROCEDURES FOLLOWED AND WAY DAMPERS DISENGAGED BUT OSCULLATIONS CONTINUED. ADJUSTING RUDDER TRIM TENDED TO INCREASE OSCILLATIONS. THE ACFT LANDED WITHOUT EVENT. MAINT. REPLACED THE FCP, BOTH YAW SDR CA141208003Control Panel · failed(CAN) DUAL YAW DAMPER FAILURE. DIFFICULTY CONTROLLING THE A/C. EMERGENCY DECLARED. REPLACED RELAY K58, K59. REPLACED YAW DAMPER PANEL , REPLACED RELAYS IAW AMM 22-22-07, PANEL IAW AMM 22-22-04 OK FOR SERVICESDR CA150911011Hose · failed(CAN) BOMBARDIER RECEIVED A DISCLOSURE LETTER REGARDING THE CAPABILITY OF HOSE ASSEMBLIES THAT ARE USED ON THE POWERPLANT HYDRAULIC SYSTEM INSTALLATIONS. BOMBARDIER ASSESSED THE POTENTIEL SAFETY CONCERNS THEN. A REVIEW OF THIS FORMER ASSESSMENT WILL BE CONDUCTSDR CA141031005Valve · failed(CAN) WHILE TAXING WITH ANTI-ICE FOR ICE CONDITIONS BOTH THE LT AND RT WING ANTI-ICE FAIL MESSAGE APPEARED. SUBSEQUENTLY THE LT WING ANTI-ICE FAIL MESSAGE CLEARED BUT THE RT WING ICE REMAINED FAILED. CONTINUOUS LT AND 5 WING AMBER INDICATION. THE FLIGHT CRESDR CA150123008Hose · cracked(CAN) DURING TAKE-OFF ROLL, ANOTHER A/C REPORTED WHITE SMOKE COMING FROM THE CUSTOMER AIRCRAFT. CAPTAIN DECIDED TO ABORT TAKE-OFF AT ABOUT 80 KTS. CAUTION MESSAGE HYD EDP 2 IS POSTED. ONCE THE RUNWAY WAS CLEARED, CREW NOTICED THAT THE QUANTITY OF HYDRAULIC IN SDR ASOA2014102211471Skin · damagedRT ENGINE CORE COWL HAS CHAFE DAMAGE DUE TO CONTACT WITH GREEN HARNESS. REPAIRED IAW REO 670-54-23-959. MAJOR REPAIR.SDR SIMA20140908003Compressor Blade · lack of lubeAT INITIAL CRUISE FLIGHT, NR 2 ENG FAN REACHED APPROX 3.5 VIBRATION. AOM VOL 1 PROCEDURE FOLLOWED. REDUCTION IN THRUST EVENTUALLY HELPED A BIT. FOLLOWED PROCEDURE IN AMM 22-21-02 & PERFORMED THE VIBRATION CHECK IAW 71-00-00. PERFORM BLADE LUBE WITHIN 50 F SDR SWIA201439213Battery Pack · inoperativeAFT F/A FLASHLIGHT NOT WORKING. REPLACED AFT F/A FLASHLIGHT BATTERY.SDR WVER0815201450919Skin · damagedRT ENGINE AFT CORE COWL HAS TWO SCREWS LOOSE AND PULLING THROUGH OUTER SKIN AT UPPER 9 O'CLOCK POSITION.SDR CA140807015Mcu · failed(CAN) JUST AFTER TAKE-OFF, THE STAB TRIM AND MACH TRIM FAILED AND WOULD NOT RESET. THE AIRCRAFT RETURNED TO AIRPORT. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL MCU. OK.SDR MASA2014062702193Engine · unknownNR 1 ENGINE PRODUCED A LOUD BANG DURING CLIMB AT 12000 FEET. OPENSDR SIMA20140620004Fmu · failedFUEL BURN MUCH HIGHER THAN PLANNED LT NR 1 ENG BURNED 300 LBS HIGHER THAN NR 2 ENG. R & R NR 1 FMU IAW AMM 73-21-00. LEAK CHECKED IAW AMM 73-10-00, NO LEAK FOUND.SDR CA140428003Unknown · odor(CAN) RETURNED TO THE GATE, SMOKE ODOR IN THE CABIN. SIMULTANEOUSLY EICAS DISPLAYED RT PACK FAULT. RT PACK HAS BEEN PLACED UNDER MEL.SDR CA140420001Warning Message · activated(CAN) OTBD SPOILERON AND OTBD FLT SPOILER CAUTION MSG.SDR N6WA20141330001Oil System · lowLEFT ENGINE OIL LOW. SERVICED ENGINE OIL IAW AMM 12-13-79, NO LEAKS NOTED AT THIS TIME.SDR ASOA2014031910158Sensor · failedAT LT ENG OIL TEMP STARTED TO CLIMB RAPIDLY TO 249C. NEVER RECEIVED MASTER WARNING OR CAUTION, ONLY RED TEMPERATURE ON EICAS, FOLLOWED QRH & SHUTDOWN LT ENGINE, ENROUTE, ACFT DIVERTED DUE TO MAINTENANCE EMERGENCY ACTIONS. R & R OIL LEVEL/TEMP SENSOR IAW AMM SDR CA140314013Coffeemaker · burned(CAN) F/A REPORTED SMOKE IN THE CABIN AND THAT THE FUMES WERE BAD ENOUGH TO BURN SOME PASSENGERS THROATS WHEN BREATHING. EMERGENCY WAS DECLARED AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CHEWING GUM STUCK TO A COFFEE POT THAT WAS BURNING AND CREATING THESDR CA140317001Cascade · broken(CAN) AIRPORT AUTHORITY FOUND PARTS ON THE AIRFIELD ON MARCH 7TH AND PROVIDED THE PARTS TO OPERATOR FOR THEIR REVIEW. DURING A SCHEDULED VISIT ON MARCH 11TH, MAINTENANCE FOUND SECTIONS OF THE THRUST REVERSER CASCADES WERE FOUND MISSING.SDR CA140304004Safety Valve · failed(CAN) CABIN ALT CAUTION MESSAGE. AIRCRAFT DIVERTED. CONTROLLER PREVIOUSLY DEFERRED. FOLLOWED QRH, UNABLE TO CONTROL CABIN PRESSURE. EMERGENCY DECLARED AS A PRECAUTION.SDR CA140306010Unknown · odor(CAN) STRONG ELECTRICAL BURNING ODOR IN COCKPIT THEY REPORT WATER DRIPPING FROM ESCAPE CATCH ON PEDESTAL. STRONG ELECTRICAL BURNED ODOR COMING FROM THE TRIM PANEL WITH A SLIGHT DISCOLORATION. AFTER REMOVING THE PANEL AND PUTTING BACK POWER ON THE ACFT, IT SESDR SIMA20140204005Engine · vibrationON TAKEOFF TKO E1 VIB ON 1.4. VIBE CLIMBED DURING ACCENT AT 17,500 E2 VIB WENT AMBE AT 1.8. THRUST REDUCED TO CRUISE POWER TO LOWER VIB. GOT VIB REDUCED TO 1.6 THEN WITHOUT INPUT VIB RETURNED TO AMBER 1.8 BOTH REDUCED TO TAKE VIB TO GREEN RANGE AT 1.4 AT 22SDR SWIA201435966Engine · failedPERFORMED A REJECTED TAKE OFF AT APPROXIMATELY 105 KNOTS DUE TO LOSS OF DIRECTIONAL CONTROL & APPARENT LOSS OF POWER FROM THE NR 2 ENG. FLT 1301 REPLACED ENG ON CP 10385995.SDR CA140106011Servo · locked(CAN) AT 1000 FT AGL FLIGHT CONTROLS LOCKED UP AND WERE FREE AND NORMAL THEN LOCKED UP AGAIN. HAPPENED A TOTAL OF 3 TIMES.SDR ASOA2014013109822Doubler · chafedRIGHT ENGINE LOWER CORE COWL, INNER SKIN DOUBLE REPAIR HAS CHAFE DAMAGE. REMOVED DOUBLER ON RT LOWER COWL DOOR IAW SRM 51-42-06-001-001. COMPLIED WITH REPAIR OF THE FWD CORE COWL IAW REO 670-54-23-959. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOPSDR CA140106005Windshield · cracked(CAN) CRACKED RIGHT WINDSHIELD.SDR CA131216015Wire · broken(CAN) PRIOR TO TAKEOFF WE HAD ACFT DEICED. JUST 15 MINUTES AFTER TO CLIMBING THROUGH 17000 FT AT 290 KTS. WE HEARD A LOUD BANG ON THE LT SIDE OF ACFT, THEN GEAR DISAGREE WARNING POSTED ON ED1. LT MAIN GEAR WAS INDICATING RED AND ALL HYDRAULIC PRESSURES NOR
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