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 = '72723' 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 = '72723' 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 96ZZZX187Stringer · corrodedDURING AN INTERNAL VISUAL INSPECTION PER AD 90-26-09*, THE STRINGER SPLICE ON STR 28R AT BS 480 WAS FOUND SEVERELY CORRODED (EXFOLIATED). REMOVAL OF STRINGER SPLICE REVEALED CORROSION ON STRINGER END AFT OF SPLICE. AIRCRAFT HAS BEEN IN STORAGE SINCE 9/92 IN SDR AALA951181Assist Bottle · req'd serviceMIA - DURING OVERNIGHT CHECK, L4 EMERGENCY EXIT DOOR ASSIST BOTTLE HAD A LOW PRESSURE READING. SERVICED L4 EMERGENCY EXIT DOOR ASSIST BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR 95ZZZX4102Door · not closedKFLL/KGPT - FLT KYC630 - AIR TURN BACK. AIRCRAFT WOULD NOT HOLD CABIN PRESSURE, ISOLATED ALL SYSTEMS. RETURNED TO KFLL. UPON MAINTENANCE INSPECTION, FOUND DEBRIS IN AFT CARGO DOOR SILL, AND DOOR NOT LOCKED CLOSE. DOOR SWITCH STUCK CLOSED. INSPECTED DOOR ASDR 95ZZZX2281Hinge Fitting · corrodedTHREE HINGE FITINGS IN THE RT OTBD AILERON WERE FOUND SEVERELY CORRODED DURING A C-CHECK. THE FITTINGS ARE MAGNISIUM, THAT AND TIME ARE THE MOST LIKELY CAUSE. CAREFUL INSPECTION IS NEEDED IN THIS AREA.SDR 95ZZZX2280Hinge Fitting · corrodedTHREE HINGE FITINGS IN THE RT OTBD AILERON WERE FOUND SEVERELY CORRODED DURING A C-CHECK. THE FITTINGS ARE MAGNISIUM, THAT AND TIME ARE THE MOST LIKELY CAUSE. CAREFUL INSPECTION IS NEEDED IN THIS AREA.SDR 95ZZZX2290Chord · corrodedTHE RT VERTICAL STABILIZER TORQUE BOX LOWER CHORD WAS FOUND CORRODED DURING VERTICAL STABILIZER TERMINAL FITTING REPLACEMENT. THE CAUSE IS PROBABLY DISSIMILAR METALS AND A LACK OF DRAINAGE. DUE TO LACK OF ACCESSIBILITY, THE ONLY WAY TO FIND THIS DEFECT IS BYSDR 95ZZZX2289Attach Fitting · corrodedBOTH LT OTBD AILERON TAB PUSH ROD ATTACH FITTINGS WERE FOUND CORRODED BEYOND LIMITS DURING A C-CHECK. THE FITTINGS ARE MAGNISIUM, THAT AND TIME ARE THE MOST LIKELY CAUSES. CAREFUL INSPECTION IS NEEDED TO CATCH THIS KIND OF PROBLEM.SDR 95ZZZX2288Chord · corrodedTHE VERTICAL STABILIZER, REAR SPAR, LT CHORD AT STABILIZER, STA 225, WAS FOUND SEVERELY CORRODED DURING A RE-ENGINE MODIFICATION. THE CAUSE IS PROBABLY A LACK OF DRAINAGE AND AGE. THE ONLY WAY TO FIND THIS PROBLEM IS WITH AN X-RAY INSPECTION.SDR 95ZZZX2287Chord · corrodedTHE VERTICAL BEAM AT THE NR 2 ENGINE AFT MOUNT WAS FOUND SEVERELY CORRODED DURING A RE-ENGINE MODIFICATION. BECAUSE OF ITS LOCATION AND LACK OF ACCESSIBILITY THE ONLY WAY TO DISCOVER THIS DEFECT WOULD BE BY X-RAY INSPECTION.SDR 95ZZZX2286Hinge Fitting · corrodedTWO HINGE FITTINGS IN THE LT OTBD AILERON WERE FOUND SEVERELY CORRODED DURING A C-CHECK INSPECTION. THE FITTINGS ARE MAGNISIUM, THAT AND TIME ARE THE MOST LIKELY CAUSE. CAREFUL INSPECTION IS NEEDED TO CATCH THIS KIND OF PROBLEM.SDR 95ZZZX2285Hinge Fitting · corrodedTWO HINGE FITTINGS IN THE LT OTBD AILERON WERE FOUND SEVERELY CORRODED DURING A C-CHECK INSPECTION. THE FITTINGS ARE MAGNISIUM, THAT AND TIME ARE THE MOST LIKELY CAUSE. CAREFUL INSPECTION IS NEEDED TO CATCH THIS KIND OF PROBLEM.SDR 95ZZZX2274Chord · corrodedTHE LT VERTICAL STABILIZER TORQUE BOX LOWER CHORD WAS FOUND CORRODED DURING VERTICAL STABILIZER TERMINAL FITTING REPLACEMENT. THE CAUSE IS PROBABLY DISSIMILAR METALS AND A LACK OF DRAINAGE. DUE TO A LACK OF ACCESSIBILITY, THE ONLY WAY TO FIND THIS DEFECT IS SDR 95ZZZX2273Frame Rib · crackedBOTH THE LT AND RT STA 1362 FRAME RIBS WERE FOUND CRACKED DURING THE VERTICAL STABILIZER REAR SPAR TERMINAL FITTING CHANGE. FATIGUE IS THE LIKELY CAUSE AND MORE FREQUENT INSPECTION APPEARS TO BE REQUIRED.SDR 95ZZZX2298Chord · rustedTHE BS 1342, RT INBD FRAME CHORD WAS FOUND SEVERELY RUSTED DURING A RE-ENGINING MODIFICATION. THIS CONDITION HAS BEEN DISCOVERED ON ALL 38 A/C MODIFIED SO FAR. THE CONDITION IS PROBABLY CAUSED BY DISSIMILAR METAL AND A LACK OF DRAINAGE. NOTE: THE RUST CANNOSDR 95ZZZX2299Chord · rustedTHE BS 1342, LT INBD FRAME CHORD WAS FOUND SEVERELY RUSTED DURING A RE-ENGINING MODIFICATION. THIS CONDITION HAS BEEN FOUND ON ALL 38 A/C MODIFIED SO FAR. THIS CONDITION IS PROBABLY CAUSED BY DISSIMILAR METALS AND A LACK OF DRAINAGE. NOTE: THE RUST CANNOT SDR 95ZZZX2297Channel · rustedTHE BS 1342, AFT CENTER CHANNEL (AT TOP OF FIREWALL) WAS FOUND SEVERELY RUSTED DURING A RE-ENGINE MODIFICATION. THIS CONDITION HAS BEEN FOUND ON ALL 38 A/C MODIFIED SO FAR. THE CONDITION IS PROBABLY CAUSED BY DISSIMILAR METAL AND LACK OF DRAINAGE. NOTE: THSDR 95ZZZX2296Chord · rustedTHE BS 1342, LBL 30 CHORD WAS FOUND SEVERELY CORRODED (RUSTY) DURING A RE-ENGINING MODIFICATION. THIS CONDITION HAS BEEN DISCOVERED ON ALL 38 A/C MODIFIED SO FAR. THE RUST IS PROBABLY CAUSED BY DISSIMILAR METAL AND LACK OF DRAINAGE. NOTE: THE RUST CANNOT BSDR 95ZZZX2295Chord · rustedTHE BS 1342, RT LOWER FRAME CHORD WAS FOUND SEVERELY RUSTED DURING A RE-ENGINING MODIFICATION. THIS CONDITION HAS BEEN DISCOVERED ON ALL 38 A/C MODIFIED THUS FAR. THE CONDITION IS PROBABLY CAUSED BY DISSIMILAR METALS AND LACK OF DRAINAGE. NOTE: THE RUST CASDR 95ZZZX2294Chord · rustedTHE BS 1342, LT LOWER FRAME CHORD WAS FOUND SEVERELY RUSTED DURING A RE-ENGINING MODIFICATION. THIS CONDITION HAS BEEN DISCOVERED ON ALL 38 A/C MODIFIED SO FAR. SUSPECT CAUSED BY DISSIMILAR METAL AND LACK OF DRAINAGE. THE RUST CANNOT BE SEEN WITHOUT REMOVINSDR 95ZZZX2293Chord · rustedTHE BS 1342, LBL 30 CHORD WAS FOUND SEVERELY RUSTED. THE DEFECT WAS DISCOVERED DURING A RE-ENGINING MODIFICATION. THIS CONDITION HAS BEEN FOUND ON ALL 38 A/C MODIFIED THUS FAR. THE CONDITION IS PROBABLY CAUSED BY DISSIMILAR METAL AND LACK OF DRAINAGE. NOTESDR 95ZZZX2292Channel · rustedTHE BS 1342, RBL 18 CHANNEL WAS FOUND SEVERELY RUSTED WHERE IT ATTACHES TO THE STRUCTURE. DEFECT WAS DISCOVERED DURING A RE-ENGINING MODIFICATION. THIS CONDITION HAS BEEN FOUND ON ALL 38 AIRCRAFT MODIFIED THUS FAR. CONDITION IS PROBABLY CAUSED BY DISSIMILARSDR 95ZZZX2291Channel · rustedTHE BS 1342, LBL 18 CHANNEL WAS FOUND SEVERELY RUSTED WHERE IT ATTACHES TO THE STRUCTURE. DEFECT WAS DISCOVERED DURING A RE-ENGINING MODIFICATION. THIS CONDITION HAS BEEN FOUND ON 38 OF THE 38 AIRCRAFT MODIFIED SO FAR. CONDITION IS PROBABLY CAUSE BY DISSIMISDR 95ZZZX2282Chord · crackedTHE BS 1342 FORWARD CENTER CHORD WAS FOUND CRACKED DURING A RE-ENGINING MODIFICATION. THE CHORD PROBABLY CRACKED DUE TO FLEXING OF THE 1342 BULKHEAD WEB CAUSED BY THE S-DUCT.SDR 95ZZZZ85Tr Switch · inopNR 3 THRUST REVERSER LIGHT ILLUMINATED DURING TAKEOFF ROLL, APPROXIMATELY 1.6 EPR. TAKEOFF REJECTED. REMOVED AND REPLACED NR 3 THRUST REVERSER SWITCH. GROUND RAN TO 1.93 EPR. OPS CHECKS GOOD IAW DHL B727 M 78-30-91.SDR 95ZZZW56Switch · dirtyTHE NR 3 THRUST REVERSER LIGHT ILLUMINATED DURING TAKEOFF ROLL. AFTER CLEARING RUNWAY, CYCLED REVERSER. LIGHT WENT OUT. CLEANED CONNECTOR AND SWITCH AT THRUST REVERSER. ALSO, CHECKED THRUST REVERSER FOR DAMAGE. CHECKED GOOD. GROUND RAN, CHECK NORMAL.
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