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 = 'GE9090B' 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 = 'GE9090B' 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 2005FA0000645Seal · debondedPART WAS PREVIOUSLY REPAIRED. REP REQUIRES USE OF BRAZE AMS 4777 OR SUITABLE TAPE ALTERNATIVE, USED TAPE SPEZ AMS 4779F, WITH OVEN TEMP 1050 DEGREES C. AMS 4779F DOES NOT MELT UNTIL 1068 DEGREES C. HONEYCOMB BECAME DISBONDED AND LIBERATED CAUSLING HPT 1 BLASDR 2005FA0000567Seal · crackedMDR/001/05: DURING ENG O/H, 2 CRACKS WERE NOTED ING THE HPT INTERSTAGE SEAL. CRACKS ARE ABOUT 45 DEGREES APART AND APPEAR TO ORIGINATE IN THE FWD ARM, OUTER DIAMETER. BOTH CRACKS ARE THROUGH FORWARD RETAINER AND CATENARY. 1 PASSES THROUGH BOTH SEAL TEETH ASDR MALA050255Control Unit · malfunctionedCLIMBING THROUGH 12800 AIRCRAFT YAWED TO THE RIGHT. RIGHT ENGINE SHOWED ZERO TORQUE, ZERO NP AND APPROXIMATELY 900 ITT. WHEN POWER WAS REDUCED RIGHT ENGINE OVERTEMP LIGHT ILLUMINATED BUT ITT REDUCED BELOW 900. OTHER ENGINE PARAMETERS APPEARED NORMAL. IGNITSDR CALA0400682Line · cloggedNR 2 ENG INDICATED A RAPID LOSS OF OIL, FOLLOWED BY LOW OIL PRESSURE IND. CREW SHUTDOWN NR 2 ENG & DIVERTED FLT, LANDED WITHOUT INCIDENT. TROUBLESHOOTING FOUND NR 2 ENG C-SUMP LINE CLOGGED WITH COKE AT 9 O'CLOCK STRUT UNDER AFT CENTER BODY. LINE CLEARED. ENGINSDR 2004FA0000672Bushing · missingDURING SHOP VISIT, IT WAS OBSERVED THAT BUSH CMM REF 71-21-03 FIG 3, ITEM 170 WAS MISSING FROM THE ASSEMBLY OF THE FWD MOUNT. THE LOAD BEARING SHOULDER BOLT WAS SUBJECTED TO A SINGLE SHEAR LOAD AS OPPOSED TO A DOUBLE SHEAR IAW DESIGN INTENT. SIMILARLY, ONLY SDR CALA0400005Starter · leakingTHE NR 1 ENGINE OIL QUANTITY AND PRESSURE BEGAN TO DECREASE DURING CRUISE. THE ENGINE WAS SHUTDOWN AS A PRECAUTIONARY MEASURE AND THE AIRCRAFT WAS DIVERTED WHERE IT LANDED WITHOUT INCIDENT. THE STARTER SIGHT GLASS HOUSING WAS FOUND SHEARED. THE NR 1 ENGINE STASDR QEM2003F00000Turbine Wheel · damagedLPT BLADE LIBERATION, QTY 1 AT DISK SLOT NR 24. DISK POST SHOWS EVIDENCE OF HEAT EXPOSURE. BLADE RETENTION DOVETAIL HAS YIELDED ALLOWING BLADE LIBERATION. BLADE PLATFORM RECOVERED AND NO VISIBLE DAMAGE TO DOVETAIL. NO VISIBLE DAMAGE TO DOVETAIL. PARTS (DISDR CALA0300399Battery · faultyTHE CREW RECEIVED A BATTERY AND BATTERY CHARGER STATUS MESSAGE AT LEVEL OFF AFTER DEPARTING IAH. THE MESSAGES WERE ACCOMPANIED BY A STRONG ELECTRICAL SMELL IN THE COCKPIT. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED ASDR MDR00402Seal · crackedFPI INDICATIONS FOUND IN STAGE 1 BLADE RETAINER ARM AT EACH BLADE LOCATION. ITEM TO BE RETURNED TO MFG FOR DETAILED ANALYSIS. PART WOULD HAVE BEEN REDUNDANT TO SB 72455.SDR 20010312CW008Clutch · destroyedIMPROPER INSTALLATION OF CLUTCH PAWL SPRING RETAINING RIVETS DURING LAST MAINT., RESULTED IN CLUTCH FAILURE AND DAMAGE TO ENGINE STARTER. NEW TOOLING, ASSEMBLY AND INSPECTION PRACTICES WILL BE IMPLEMENTED TO PREVENT RECURRENCE, FIELD EVALUATION OF OTHER POSSISDR 20001024SH004Seal · crackedSEAL EXHIBTS TWO SHORT CRACKS, 0.150 INCH LENGTH EACH, IN THE FORWARD ARM OUTSIDE DIAMETER AT THE STAGE 1 BLADE INTERFACE. THIS PART HAD ACCUMULATED 954 CSN. (X)
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