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 = 'CT78A' 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 = 'CT78A' 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 CA100108006Gearbox · making metal(CAN) MAIN GEARBOX CHIP DETECTOR WARNING TRIGGERED IN FLIGHT. THE ACFT RETURNED TO BASE. THE MAIN CHIP DETECTOR WAS REMOVED FROM THE MGB FOR INSP. A PIECE OF FERROUS MATERIAL WAS FOUND ATTACHED . CYLINDRICAL IN SHAPE. APPOX .800IN LONG X .200 IN DIAMETER. ASDR CA091103002Mount · cracked(CAN) UPON PERFORMING THE 10 HR RECURRING INSP, A CRACK WAS DISCOVERED AT THE MAIN GEARBOX RT MOUNT FOOT. THERE ARE 2 BOLTS SECURING THIS FOOT, 1 FWD AND 1 DIRECTLY AFT APPROX3 INCHES APART. THE CRACK EXTENDS FROM THE AFT BOLT HEAD OTBD AND DOWN THE VERTICAL FSDR CA090930002Module · contaminated(CAN) NR 2 INPUT CHIP INDICATION TRIGGERED IN FLIGHT, AIRCRAFT RETURNED TO BASE. FOLLOW UP INSPECTION OF NR 2 INPUT MODULE CHIP DETECTOR WAS CARRIED OUT. TWO RIVETS HEADS WERE FOUND BRIDGING THE DETECTOR GAP. DURING REPLACEMENT OF THE INPUT MODULE TWO ADDITIONSDR CA090223008Web · cracked(CAN) DURING A ROUTINE MX INSP, A SMALL CRACK-LIKE INDICATION HAD BEEN DISCOVERED ON A WEB OF THE MGB HSG ON AIRCRAFT 920057. THE LOCATION OF THE INDICATION HAS BEEN DESCRIBED AS BEING ON (1) OF (4) STIFFENING WEBS THAT CONNECTS THE MAIN HSG WALL TO THE CYLINSDR CA081024002Heat Exchanger · cracked(CAN) ENROUTE AT 7000 FT, ACFT STARTED TO NOD UNCHARACTERISTICALLY. IT WAS NOTED THAT THE NR 1 HYD SYS PRESSURE WAS HIGH (IN THE RED). DECISION TO RETURN MADE AND NR 1 HYD SYS DE-SELECTED BUT PRESSURE REMAINED HIGH. NO OTHER ADVISORY/CAUTION LIGHTS WERE ON AT SDR CA081007002Engine · malfunctioned(CAN) POST LANDING AND TAXI. ACFT WAS STATIONARY WITH BOTH ENGINES IN THE GROUND IDLE POSITION WITH ROTORS TURNING. PILOT OBSERVED ROTOR SPEED WAS NEARING A KNOWN "AVOID RANGE" AND ELECTED TO NUDGE THE NR 1 ENGINE CONTROL LEVER FORWARD TO INCREASE ROTOR SPEESDR EGRR2008062577287Control Panel · defectiveDURING MX CHECK FLIGHT, LANDING GEAR WOULD NOT EXTEND. VERIFIED CIRCUIT BREAKERS WERE NOT OPEN. EXTENDED LANDING GEAR WITH EMERGENCY BLOW DOWN PROCEDURES. MX TROUBLESHOT SYS AND FOUND LANDING GEAR CONTROL PANEL DEFECTIVE. REPLACED PANEL WITH SERVICEABLE ASSY SDR CA080305003Pin · fod(CAN) ON RETURN FLIGHT AN EPAC (POWER CHECK) WAS ATTEMPTED BUT WOULD NOT COMPLETE (A USUAL CASE IN PARTICULAR ACFT) NRS WERE NOTED FOR MAINT STAFF AND ON RETURNING TO BASE ANOTHER EPAC WAS RUN AND COMPLETED. MAINT STAFF WAS NOTIFIED UPON ARRIVAL AT AIRPORT ANDSDR CA080207005Bearing · debonded(CAN) UPON A SCHEDULED 50HR INSP, A BOROSCOPING OF THE TAIL ROTOR BLADES HAD BEEN CARRIED OUT, TO CHECK PIVOT BEARINGS FOR DEBONDING FROM TAIL ROTOR SPARE. ON ONE TAIL ROTOR BLADE A BEARING WAS SUSPECTED TO BE DEBONDED. UPON FURTHER INSPECTION WITH REMOVAL OF SDR HEER118276Spar Cap · crackedFORWARD SPAR CAP ANGLE AT TOP OF THE DRIVESHAFT TUNNEL IS CRACKED AT TOP OF THE LAST LARGE HL64-8 PIN. CONTACTED MFG FOR 8110 REPAIR.SDR HEER118215Angle · crackedFWD LT CAP ANGLE CRACKED. REPORTED PROBLEM TO MFG.SDR CA071024007Beacon · failed(CAN) DURING FERRY FLIGHT (CRASH POSITION INDICATOR) DEPARTED AIRCRAFT FOR NO APPARENT REASON. UNIT DID NOT TRANSMIT. THE DEPLOYABLE BEACON WAS INSTALLED IAW MFG DWG NR 92604-40331. (TC NR 20071024007)SDR HEEA117386Pump · failedENROUTE, NR 2 HYDRAULIC GAUGE DECREASE TO ZERO RED RANGE. NO HYDRAULIC LIGHT ILLUMINATED. CONTINUED AND GAUGE DECREASED TO ZERO AT IDLE. MAINTENANCE FOUND THE NR 2 HYDRAULIC PUMP HAD FAILED. REPLACED PUMP.SDR HEER117431Flex Coupling · leakingAFTER ENGINE CHANGE COULD NOT CROSS START THE OPPOSITE ENGINE. FOUND THE FLEX COUPLING LEAKING AIR EXCESSIVELY. REMOVED AND REPLACED CROSS START FLEX COUPLING AND CROSS START WORKED PROPERLY.SDR HEER117365Engine · inoperativeON THE FOURTH START OF THE DAY, THE NR 2 ENGINE WOULD NOT TURN OVER WHEN THE STARTER WAS ENGAGED. REMOVED THE STARTER, APPLIED TORQUE TO THE A AXIS DRIVE, COULD NOT ROTATE THE GEARBOX SECTION OF THE ENGINE. REMOVED AND REPLACED THE NR 2 ENGINE.SDR HEER117344Stringer · crackedJ-STRINGER FOUND CRACKED ACROSS FWD 5 FASTENERS IN RT CABIN OVERHEAD AT STATION 292, BL 10.5. FIRST FASTENER ON STRINGER ATTACHES TO HAT SECTION SUPPORT FOR TRANSFER MODULE ON ROOF. REMOVED STRINGER, CONTACTED TECH REP FOR MATERIAL SPECS AND PN. ALSO DID NDSDR HEEA117201Sensor · malfunctionedDURING CRUISE INTERMEDIATE GEARBOX HOT LIGHT ILLUMINATED. PERFORMED EMERGENCY PROCEDURE. RETURNED TO HBP. LIGHT CAME ON AND OFF DURING RETURN FLIGHT. REPLACED CHIP DETECTOR-TEMP SENSOR AND HOUSING.
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