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 = '99A' 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 = '99A' 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 CA990311032Blade · loose(CAN) THE POWER SECTION WAS REMOVED FOR MAINTENANCE AND FOUND THE PT BLADES WERE LOOSE. THE UNIT WAS SHIPPED TO AN OVERHAUL FACILITY FOR REPAIR. 23 BLADES REQUIRED REINSTALLATION AND RIVETING.SDR CA990311014Duct · cracked(CAN) CRACK FOUND ON THE EXHAUST DUCT BY THE INBOARD FLANGE EAR. NOT IN SEAM OR WELD AREA, JUST OUTSIDE OF SEAM STITCH WELD.SDR CA990311031Wire · broken(CAN) AIRCRAFT FERRIED HOME DUE TO FLAPS NOT OPERATING. UPON INSPECTION, A BROKEN WIRE WAS FOUND AT THE DOWNLIMIT SWITCH.SDR 98ZZZX4685Start/Gen · failedON TAKEOFF ROTATION, THE PILOT NOTICED THE LEFT GENERATOR OFF LIGHT CAME ON AND THEN A COMPLETE LOSS OF ELECTRICAL POWER ON THE RIGHT SIDE WITH LOSS OF COMMUNICATION AND VARIOUS LIGHTS AND INSTRUMENTS. THE AIRCRAFT LANDED SAFELY WITH THE AID OF LIGHTS FROM THSDR 98ZZZX4710Actuator · failedON POST-FLIGHT INSPECTION, PILOT REPORTED HYDRAULIC FLUID ON LOWER FUSELAGE AND TAIL. MECHANICS WERE NOTIFIED AND CLOSER INSPECTION REVEALED FLUID LEAKING FROM LOWER SHAFT SEAL. AIRCRAFT WAS JACKED AND GEAR SWUNG TO VERIFY SOURCE OF LEAKAGE. PROBLEM DUPLICASDR CA981027013Angle · cracked(CAN) DURING 100 HOUR ANNUAL INSPECTION, THE RIGHT INBOARD UPPER NACELLE AREA REVEALED SMOKING RIVETS ATTACHING STIFFENER ANGLE TO ENGINE MOUNT ATTACHMENT ASSY P/N 50-980089. CLOSER INSPECTION REVEALED APPROXIMATELY A 2 INCH CRACKING STIFFENER ANGLE. DURING SDR 98ZZZX3882Pedal Arm · wornHINGE POINT FROM RUDDER PEDALS TO RUDDDER ARM BUSHING IS WEARING DEEP GROOVES INTO TANGS ON RUDDER PEDAL ARMS.SDR 98ZZZX3881Pedal Arm · wornHINGE POINT FROM RUDDER PEDAL TO RUDDER ARM BUSHING IS WEARING DEEP GROOVES INTO TANGS ON RUDDER PEDAL ARMS.SDR CA980318002Boss · damaged(CAN) PIVOT BOSSES WERE UNDER LIMITS FOR THE BEARING. REPLACED.SDR CA980318001Ball Lock · failed(CAN) ON DEPARTURE THE GEAR WAS SELECTED UP AND THE NOSE GEAR DOWN GREEN STAYED ON. AIRCRAFT RETURNED AND NOSE GEAR ACTUATOR REPLACED.SDR CA980318016Fuel Control · surges(CAN) FUEL CONTROL UNIT CAUSED 200 FT/LB SURGE WHEN POWER WAS REDUCED.SDR 98ZZZX1171Nut · corrodedRUDDER TAB ACTUATOR NUT FOUND CORRODED DURING ROUTINE INSPECTION.SDR 98ZZZX534Rod End · defectiveENGINE POWER WOULD NOT DECREASE DUE TO TIGHT ROD END CONNECTOR FROM CAM BOX TO FCU DEFECTIVE. TAT: 30,824 HOURS. ENGINE TSN: 4,295 HOURS. ENGINE TSO: 1,129 HOURS.SDR 98ZZZX2711Rod End · bindingENGIEN POWER WOULD NOT DECREASE DUE TO BINDING ROD END CONNECTOR CAM BOX TO FCU. TAT: 30,824 HOURS. ENG TSN: 4,295 HOURS. ENG TSO: 1,129 HOURS.SDR CA971231005Engine · chip light(CAN) PILOT REPORTED NR 1 ENGINE CHIP DETECTOR LIGHT CAME ON 6 MINUTES AFTER TAKEOFF. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT RETURNED TO BASE. REMOVAL OF CHIP DETECTOR REVEALED A LARGE PIECE OF METAL ACROSS THE LUGS. THE ENGINE WAS A LOANER AND WAS RETURNESDR CA971216064Switch · failed(CAN) LEFT MAIN NOT INDICATING SAFE. POSITION SWITCH REPLACED.SDR CA970528031Exhaust Duct · cracked(CAN) PWC SB 1430 EMBODIED AT LAST OVERHAUL WITH WRONG TYPE OF SEAM WELD COMPLETED. SB CALLS FOR RESISTANCE SEAM OR STITCH WELD TO BE ACCOMPLISHED IN ORDER TO WELD THE INNER LINER TO THE EXHAUST DUCT. IN THIS CASE A TIG WELD WAS COMPLETED WHICH CAUSED THE DUSDR CA970401012Diffuser Tube · broken bolt(CAN) INSPECTION FOUND THE RETAINING BOLTS THAT HOLD THE DIFFUSER IN PLACE WAS FRACTURED. THE BOLT WAS BORKEN IN HALF AND WAS HELD IN THE DIFFUSER BY LOCKING WIRE ONLY.SDR 96ZZZX5204Tire · recap failedDEN - FLT 1825 - NO GEAR DOWN AND LOCKED INDICATION ON LT MLG ON DESCENT INTO DEN. PILOT PERFORMED TOWER FLYBY AND COMPLETED EMERGENCY GEAR EXTENSION PROCEDURES. ACFT LANDED WITHOUT FURTHER INCIDENT. ENGINES WERE SHUT DOWN AND PROPS WERE FEATHERED UPON LANDSDR 96ZZZX3559Latch Pin · bindingKING CARGO SYSTEMS COCKPIT CREW DOOR, STC SA1438GL. PILOT HAD DIFFICULTY LATCHING DOOR. TOOK OFF, DOOR CAME OPEN DURING CLIMB. AIRCRAFT LANDED WITHOUT INCIDENT. EXAMINATION FOUND LATCH PINS BINDING IN GUIDES; LUBRICATED AND INSTALLED LIGHT SPRINGS TO HOLD SDR CA960418006Spar Cap · cracked(CAN) SPAR CAP FOUND CRACKED IN THE RIGHT HAND WHEEL WELL. SECONDARY DAMAGE FOUND TO BE CRACKED SPLICE PLATES.
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