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 = '7GCAA' 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 = '7GCAA' 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 2024FA0000132Spar · crackedRIGHT WING MAIN SPAR CRACKED IN TWO LOCATIONS, ADJACENT TO THE DOUBLER FOR THE WING STRUT ATTACH FITTING. TOP EDGE OF SPAR CRACKED AT INBOARD AND OUTBOARD ENDS OF DOUBLER PLATES. LAMINATED SPAR, COMPRESSION CRACKS STOPPED AT GLUE JOINT OF TOP LAMINATION, ABOUSDR 2019FA0000365Tube · crackedUPON VISUAL INSPECTION, FOUND THE MOST AFT VERTICAL TUBING OF AIRCRAFT STRUCTURE SHEARED ABOVE TAIL GEAR ATTACH POINT BUT BELOW 45 ANGLE BRACE. AIRCRAFT USED DAILY FOR FLIGHT TRAINING WITH AN AVERAGE OF 100 HOURS OF FLIGHT TIME EVERY 90 DAYS.SDR 2016FA0000289Fastener · looseUPON PERFORMING INSPECTION, FOUND 1 RIB NAIL MISSING AND 1 RIB NAIL LOOSE IN RT OTBD WING, 2 BAYS OTBD OF WING LIFT STRUT. INSPECTION DID NOT INDICATE A CRACK, IT APPEARS THAT THE NAILS WERE LOOSE IN THE HOLE, NAILS WERE SMOOTH NAILS AND DID NOT CONTAIN A RIBSDR 2013FA0000314Power Supply · dislodgedACFT HAD A STROBE POWER SUPPLY IN THE OTBD LT WING TIP COME LOOSE FROM ITS MOUNTING LOCATION ON THE OUTSIDE OF THE LAST FULL LENGTH RIB. IT PROCEEDED TO BOUNCE AROUND THE INSIDE OF THE WING FROM FRONT TO BACK. IT CAUSED CONSIDERABLE DAMAGE TO THE PAINT AND PSDR 2013FA0000170Tab · crackedAFTER LANDING AND ROLLOUT, LT MLG COLLAPSED. TAB ON THE LT FWD LANDING GEAR ATTACH CLUSTER FAILED CAUSING THE GEAR TO COLLAPSE.SDR 2012FA0000456Attach Fitting · crackedDURING PRE-FLIGHT INSPECTION. PILOT OBSERVED THAT THE LEFT ELEVATOR TORQUE TUBE JUST OTBD OF THE BELLCRANK ATTACH FITTING HAD A SPIRAL CRACK AFFECTING APPROX 80 PERCENT OF THE TUBE.SDR CA080416003Elt · inoperative(CAN) WHEN TESTING UNIT FOR ITS 12 MONTH CERTIFICATION IAW CAR 571 APPENDIX G, UNIT DID NOT HAVE ANY TRANSMIT POWER. ELT TRANSMITTER BOARD REPLACED AND UNIT TESTED SERVICEABLE. (TC NR 20080416003)SDR 2008FA0000267Rib · bowedREMOVED THE RT AILERON DUE TO REPORTS OF BINDING BETWEEN THE AILERON AND WING DURING AEROBATIC MANEUVERS. ON THE GROUND THE IB AILERON TO AILERON BAY RIB CLEARANCE WAS APPROX .0625 INCH. IAW TECH SUPPORT THE CLEARANCE SHOULD BE .2500 INCH. THE WING IB AILERSDR 2007FA0000631Spar · cracked(2) LONGITUDINAL CRACKS AT SPAR HINGE FITTING. SHAKING AND EXPANDING OF WOOD FIBERS DUE TO MOISTURE OR LACK OF. RECOMMEND USING ALUMINUM SPARS OF SUFFICIENT SIZE AND STRENGTH. (K)SDR 2005FA0001194Spar · crackedTWO COMPRESSION CRACKS ON RIGHT WING REAR SPAR, ONE ON EITHER SIDE OF PLYWOOD DOUBLER AT STRUT ATTACH POINT. OUT BOARD CRACK EXTENDS APPROX ONE THIRD DEPTH OF SPAR, EXTENT OF INBOARD CRACK AS YET UNKNOWN, MAY GO BEHIND DOUBLER, CRACKS FOUND DURING INSPECTION RSDR 2003FA0000779Fabric · rottedWING FABRIC WAS FOUND TO BE ROTTED ALONG THE EDGE OF THE STRAIGHT EDGED FIBREGLASS SURFACE TAPE ON A TWO YEAR OLD FACTORY COVERED WING. THE PAINT PPG SYSTEM DELTA, SHOWS CRACKS ALONG THE EDGES OF ALL SURFACE TAPES ON THE TOP OF BOTH WINGS IN THE PROP ARC. THSDR 2003FA0000681Axle · brokenSTEEL AXLE BROKE AT WELD WHILE MOVING A/C BY HAND. NO HARD LANDINGS REPORTED.SDR AUS20011454Bolt · failed(AUS) TAIL WHEEL ATTACHMENT BOLT FAILED. TAIL WHEEL SEPARATED FROM TAIL LEAF SPRING.SDR 2002FA0000242Spar · failedCRACK IN REAR SPAR OF LEFT WING OUTBOARD OF DOUBLER AT SPAR ATTACH FITTING. WING HAS HIT GROUND BEFORE WHEN INBOARD LANDING GEAR BOLT FAILED. TIP OF FORWARD SPAR HAS REPAIR AND DOUBLER.SDR AUS20010642Bolt · corroded(AUS) LOWER RH SIDE STRUT LOWER BOLT SEIZED. FOLLOWING BOLT REMOVAL ITWAS FOUND TO BE VERY RUSTED AND PITTED.SDR 2002FA0000238Spar · crackedINSPECTED AIRCRAFT AS PER AD, FOUND LEFT AFT SPAR HAS COMPRESSION CRACK AT OUTBOARD END OF DOUBLER PLATES FOR STRUT ATTACH FITTING.SDR 2002FA0000263Spar · crackedWINGS REMOVED FROM AC, THE REPAIR ON THE LT REAR SPAR STRUT ATTACH POINT. ALL FABRIC COVERING REMOVED, LT REAR SPAR HAD A 1 INCH X 16 INCHES LONG .1250 PLYWOOD STRIP GLUED TO THE TOP OF THE SPAR WHICH HID THE CRACK TO BUSHING HOLE. IT WOULD APPEAR THAT CRACKSDR 20000601SH013Hinge · brokenDURING WINDS OF APPROX 40 KNOTS, AILERON HINGE THAT ATTACHES TO CONTROL ROD TORE LOOSE FROM INBOARD END OF AILERON. FURTHER INVESTIGATION REVEALED THAT HINGE TABS, TOP AND BOTTOM, THAT ARE RIVETED ONTO SPAR CAPS HAD BROKEN PREVIOUSLY. THIS EVIDENCED BY THE STSDR 99ZZZX3159Spar · crackedINSPECTED SPARS ON LEFT WING AFTER GROUND LOOP. FOUND A COMPRESSION FAILURE ON THE REAR SPAR. COULD NOT TELL CONCLUSIVELY IF FRONT SPAR WAS CRACKED OR NOT. AFTER DISASSEMBLY OF WING, 5 COMPRESSION FAILURES WERE FOUND IN THE AFT SPAR.SDR 98ZZZX2442Mount Bolt · chafedINSPECTION FOUND LEFT AND RIGHT EXHAUST PIPES RUBBING ENGINE LOWER MOUNT BOLTS AT FIREWALL. SUBMITTER STATED CHECKED SEVERAL AIRCRAFT OF SAME MAKE/MODEL AND ALL HAD SAME PROBLEM.SDR 95ZZZX2181Strut · defectiveOLEO STRUT DEFECTIVE AT THREADED CONNECTION.
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