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 aircraft_model_key = '73737Q' 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 aircraft_model_key = '73737Q' 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 2023F00067Pump · inoperativeHYDRAULIC SYSTEM "A" PUMP (ELECTRICAL N°2) WITH LOW PRESSURE. CORRECTIVE ACTION: HAS BEEN CHANGED PUMP. IN TEST NO FOUND DISCREPANCIES.SDR 2023F00065Pump · failedQRF TO SLCB. AFTER TAKOFF HIDRAULIC ENGINE DRIVEN PUMP LOW PRESSURE ILLUMINATED. CORRECTIVE ACTION: REMOVED AND REPLACED HY SYSTEM "A" IAWAMM29-15-12. REPLACED EDP CASE DRAIN FILTER ELEMENT IAW AMM 29-15-91.SDR 2022F00346None · noneRESULT OF AD 2012-26-02 INSPECTION, CRACK WAS FOUND ON S10RH BETWEEN BS 500 AND BS 500ASDR 2022FA0000419Control Panel · failedDURING FLIGHT AUTO FAIL LIGHT ON, UNNABLE TO CONTROL DE CABIN FLT ALT AND ALT BOTH WITH DASHES. CORRECTIVE ACTION: HAS BEEN REPLACED PRESSURE CONTROL PANEL IN TEST NORMAL OPERATIONSDR 2022F00133None · noneFIRE WARNING AND FIRE BELL DURING TAKEOFF ROLL. REJECTED TAKEOFF PERFORMED. CORRECTIVE ACTION: REPLACED FIRE DETECTION MODULE AND FIRE CONTROL PANEL. IN TEST NORMAL. FIRE DETECTION MODULE P/N 472622 S/N 2316, FIRE CONTROL PANEL P/N 69-37307-300 S/N D04389.SDR 2021FA0000425None · noneIN SPECIAL DETAILED INSPECTION IAW AD 2012-26-02 WAS FOUND CRACK ON STR10R BETWEEN BS510 AND BS520 WITH 1,2" OF LENGHTSDR 2021FA0000361Flap · out of adjustABNORMAL LH DEVIATION EXCESIVE RH RUDDER AND AILERON CORRECTION NEEDED FOR STRAIGHT LEVEL FLIGHT ON LANDING CONFIGURATION. CORRECTIVE ACTION: OUTBOARD TRAILING EDGE FLAP WAS ADJUSTED AMM 27-51-34/501 AND AFT FLAP BOOM MECHANISM CABLE WAS ADJUST AMM 27-51-24/40SDR 2021F00328None · failedREJECTED TAKEOFF DUE TO FIRE WARNING ACTIVATION (LIGHT AND SOUND) DURING TAKEOFF, BUR NO LIGHT ON FIRE HABDLES OR CARGO. CORRECTIVE ACTION: HAS BEEN REPLACED FIRE DETECTION MODULE AND REPLACED FIRE CONTROL PANEL. IN TEST NORMAL.SDR 2020F00473Egt Indication · illuminatedQRF TO CBB, ENGINE LT ON TAKEOFF EGT REACHES 953°C DURING 30 SECS APPROXIMATELY. CORRECTIVE ACTION: AFTER TURNBACK WAS PERFORMED EGT EXCEEDANCE INSPECTION, IAW AMM TASK 72-00-00-216-0602(B). PERFORMED EGT TRIM BOX THERMOCOUPLE HARNESS AND PROBE SYSTEM TEST. SDR 2020F00119Control Panel · failedWITH F/D ROLL MODE DISSAPEAR FROM FMA AND F/D. FOR FLAP RETRACTION WITH SPEED ON MCPREMAINED AT 198KTS AND A/T DISENGAGED (NO MCP CONTROL). QRF PERFORMED. NORMAL LANDING.SDR 2019FA0000323Relay · failedAFTER TAKEOFF LANDING GEAR LEVER DID NOT MOVE UP. QRF PERFORMED. CORRECTIVE ACTION: HAS BEEN REPLACED LANDING GEAR CONTROL LEVER LOCK SOLENOID AND RELAY.SDR 2020F00008Solenoid · failedAFTER TAKE OFF, THE LANDING GEAR LEVER WOULD NOT MOVE UP. REPLACED THE LANDING GEAR CONTROL LEVER LOCK SOLENOID IAW AMM 32-31-31/401 AND MAIN GEAR EXTENTION AND RETRACTION NORMAL OPERATION IAW AMM 32-32-00.SDR 2019F00221Actuator · out of adjustQRF BECAUSE OF FWD CARGO DOOR LIGHT ILLUMINATED DURING CLIMB. CORRECTIVE ACTION: DISPATCH IAW MEL 52-03-01 CAT C. THE TERMINATIVE CORRECTIVE ACTION:ADJUSTED SENSOR ACTUATOR IN FWD CARGO DOOR IAW/AMM 52-71-32/205 AND CARGO DOOR INDICATION OK.SDR 2019FA0000091Adc · failedFLIGHT INST/NAVIGATION. TOTAL LOST OF INSTRUMENTS AFTER T/O. RUNWAY STABILIZER STICK SHAKER, LOST OF IAS/PITCH INDICATOR, ALTIMETER/RMI/HIS ON RT. NO FLAPS INDICATOR. CORRRECTIVE ACTION: WAS CHANGED AIR DATA COMPUTER NR 1 IAW AMM 34-12-11/401 ON GROUND OPERATISDR 2019FA0000079Shimmy Dampener · failedDURING LANDING ROLL AFTER NOSE GEAR CONTACT WITH THE RUNWAY HIGH VIBRATION STARTED. (NOTE: LEFT MLG SHIMMY DAMPER EVENT CAUSED TORSION LINK FRACTURE). CORRECTIVE ACTION: REMOVED AND REPLACED SHIMMY DAMOER, TORSION LINK, TIRES 1 AND 2, BRAKE 1 AND 2.SDR 2019FA0000177Cdu · failedBOTH CDU FAILED. QRF TO VVI. AFTER TROUBLESHOOTING IN FMCS BOTH CDU WERE CLEANED. OPERATIONAL CHECK OK.SDR 2018FA0000534Shimmy Dampener · failedAFTER LANDING THERE WAS STRONG VIBRATION IN THE LEFT LANDING GEAR (SHIMMY DAMPER FAILURE AT LANDING IN HIGH ALTITUDE AIRPORT). CORRECTIVE ACTIONS: - HAS BEEN CHANGED BRAKE ASSY #1 AND 32; MAIN WHEEL ASSY #1 AND #2 DAMPER ASSY MLG; TORSION LINK UPPER AND TORSIOSDR 2018FA0000166Sensor · out of adjustLANDING GEAR DISAGREE DURING APPROACH. PERFORMED CLEANING AND ADJUSTMENT OF SENSOR IAW AMM 32-611-31 AND AMM 32-61-00 DURING TEST GEAR INDICATION WORKS NORMAL.
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