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 = '407' 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 = '407' 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 HEEA0015509Brushes · wornSTARTER HAS WORN BRUSHES, FOUND BRUSHES WERE HANGING UP AND EXCESSIVELY WORN. ALSO FOUND FRICTION RING WORN. REPAIRED BY PHI.SDR HEEA0015505Duct · crackedEXHAUST DUCT CRACKED CAUSED BY WORKING RIVETS ON BLOWER HOUSING.SDR HEEA0015504Switch · failedTRANSMISSION PRESSURE LIGHT WILL NOT GO OUT WHEN OIL PRESSURE GOES THROUGH 38 PSI.SDR HEEA0015503Bearing · wornBEARING SEAT HAS BLUE EPOXY WORN OFF.SDR HEEA0015502Bearing · roughTAIL ROTOR HAS ROUGH BEARING. SERIAL NUMBERS REMOVED ARE A98-0440 AND A98-0512.SDR HEEA0015501Shutoff Valve · inoperativeSHUT-OFF VALVE INOPERATIVE. HEATER WOULD NOT TURN ON WHEN POWER WAS DISTRIBUTED.SDR HEEA0015496Freewheel · leakingMAIN ROTOR FREEWHEEL UNIT LEAKING.SDR HEEA0015492Indicator · intermittentTORQUE INDICATOR INTERMITTENTLY INDICATING ZERO, LCD TEST GOOD, INDICATOR CAN SOMETIMES BE RESTROYED BY REMOVING AND RE-APPLYING POWER.SDR HEEA0015491Indicator · failedMGT INDICATOR GOES BLANK AND GOES THROUGH LCD TEST MODE INTERMITTENTLY.SDR HEEA0015490Indicator · failedAT LEAST HALF OF TORQUE INDICATOR LED LIGHTS BLINK OFF DURING FLIGHT.SDR 98ZZZX3371Horn · corrodedAT 2,500 HOUR OVERHAUL OF M/R HUB, DISCOVERED 1 EACH PITCH HORN CORRODED BEYOND LIMITS UNDER PLATE, 3 EACH PITCH HORNS CORRODED BEYOND LIMITS IN DOWEL PIN BORE.SDR 98ZZZX3370Horn · corrodedAT 2,500 HOUR OVERHAUL OF M/R HUB, DISCOVERED 1 EACH PITCH HORN CORRODED BEYOND LIMITS UNDER PLATE, 3 EACH PITCH HORNS CORRODED BEYOND LIMITS IN DOWEL PIN BORE.SDR 98ZZZX3369Horn · corrodedAT 2,500 HOUR OVERHAUL OF M/R HUB, DISCOVERED 1 EACH PITCH HORN CORRODED BEYOND LIMITS UNDER PLATE, 3 EACH PITCH HORNS CORRODED BEYOND LIMITS IN DOWEL PIN BORE.SDR 98ZZZX3368Horn · corrodedAT 2,500 HOUR OVERHAUL OF M/R HUB, DISCOVERED 1 EACH PITCH HORN CORRODED BEYOND LIMITS UNDER PLATE, 3 EACH PITCH HORNS CORRODED BEYOND LIMITS IN DOWEL PIN BORE.SDR 98ZZZX3154Window · departedWHILE IN-FLIGHT, LT SLIDING WINDOW DEPARTED AIRCRAFT. AIRCRAFT CONTINUED TO LAND BASE. AFTER LANDING, A 'NICK' WAS DISCOVERED ON THE INBOARD TRAILING EDGE OF ONE T/R BLADE. REMOVED BLADE ASSEMBLY FOR REPAIR. REF: IPC, (407) FIGURE 152-8, ITEM 11.SDR 98ZZZX3519Disc · wornDURING 25 HOUR INSPECTION, GAP BETWEEN DISCS NR 1 AND NR 2, NR 2 AND NR 3, OF THE 10-DISC PACK EXCEED LIMITS.SDR 98ZZZX3518Disc · wornDURING 25 HOUR INSPECTION, FOUND GAP BETWEEN DISC NR 1 AND NR 2, NR 9 AND NR 10, EXCEED LIMITS. (TOTAL NUMBER OF DISCS IN THE DISC PACK IS 10).SDR 98ZZZX3367Inserts · looseUPON VISUAL INSPECTION OF PARTS, FOUND 1 EACH INSERT PULLED OUT OF GEARBOX HOUSING AND 2 EACH INSERTS LOOSE AT EXCITER BOX MATING SURFACE. ONE EACH INSERT P/N NAS1394-3L WAS PULLED OUT AND 2 EACH INSERTS WERE FOUND LOOSE. POSSIBLE CAUSE IS EXCESSIVE CLEARANCSDR 98ZZZX3363Insert · looseUPON VISUAL INSPECTION OF ALL PARTS, FOUND 1 EACH INSERT PULLED OUT AND 2 EACH INSERTS LOOSE AT EXCITER BOX MATING SURFACE ON GEARBOX HOUSING. ONE EACH INSERT P/N NAS1394-3L PULLED OUT AND 2 EACH INSERTS LOOSE. POSSIBLY CAUSED BY EXCESSIVE CLEARANCE BETWEEN SDR 98ZZZX3356Gear · galledENGINE REMOVED FOR EXCESSIVE METAL ON BOTH PLUGS. DISASSEMBLED AND FOUND T/M GEAR TO PINION GEAR GALLING CAUSING METAL CONTAMINATION. SUBMITTER STATES IMPROPER MESHING BETWEEN T/M GEAR AND PINION GEAR WAS CAUSE FOR GALLING. SECONDARY DAMAGE - PINION GEAR P/SDR 98ZZZX3516Bolt · looseON DAILY SERVICE CHECK, 4 MOUNTING BOLTS FOR VERTICAL FIN WERE FOUND TO HAVE LOST TORQUE.SDR 98ZZZX3515Bolt · looseON DAILY SERVICE CHECK, 4 MOUNTING BOLTS FOR VERTICAL FIN WERE FOUND TO HAVE LOST TORQUE.SDR 98ZZZX3514Bolt · looseON PHASE INSPECTION FOUND 3 OF THE 4 VERTICAL FIN MOUNTING BOLTS LOST TORQUE.SDR 98ZZZX3513Bolt · looseON PHASE INSPECTION FOUND 3 OF THE 4 VERTICAL FIN MOUNTING BOLTS LOST TORQUE.SDR 98ZZZX3517Bolt · looseDURING DAILY SERVICE CHECK, FOUND UPPER AND LOWER AFT BOLTS TO HAVE LOST TORQUE.SDR 98ZZZX3521Disc · wornDURING 25 HOURS INSPECTION, FOUND GAP BETWEEN DISCS 9 AND 10 OF THE 10-DISC PACK EXCEED LIMITS.SDR HEEA0015359Encoder · failedENCODER READS HIGH OUT OF TOLERANCE.SDR HEEA0015356Indicator · stuckCLIMB RATE INDICATOR NEEDLE STICKS EXCESSIVELY.SDR HEEA0015319Audio Selector · malfunctionedRADIO TRANSMISSION WEAK AND DISTORTED.SDR HEEA0015290Gyro · brokenDIAL SCREW BACKED OUT OF CENTER DIAL SHAFT AND IS WEDGED BETWEEN DIAL AND FLAG IN DIRECTIONAL GYRO.SDR HEEA0015236Gauge · destroyedPRESSURE GAUGE SCRAPPED (PARTS IN PIECES).SDR 98ZZZX3362Bolt · looseBLEED VALVE WAS SET UP ON TEST BENCH AND A RE-ALIGNMENT OF 90 DEGREE ELBOW WAS NEEDED TO INSTALL TEST ORIFICE AND JUMPER TUBE AND NOTICED THAT UPON SLIGHT TENSION, BOLT WHICH WAS SAFTIED, MOVED. THESE BOLTS HAVE A 30 TO 35 INCH/POUND TORQUE ATTACHED AND UPON SDR 98ZZZX3359Bolts · losePRIOR TO INSTALLING BLEED VALVE ON TEST BENCH, AN INSPECTION OF ALL SAFETIES WAS ACCOMPLISHED AND FOUND 3 EACH BOLTS WERE SAFTIED BUT LOOSE. THESE BOLTS WERE IMPROPERLY TORQUED AND CAUSED A MAJOR AIR LEAK AT SPLIT LINES OF BLEED VALVE.SDR 98ZZZX3365Indicator · failedDURING GROUND RUN AFTER ANNUAL INSPECTION, ENGINE OIL PRESSURE GAUGE WENT FROM A NORMAL INDICATION TO ZERO. TROUBLESHOOTING THE PROBLEM, FOUND ENGINE OIL PRESSURE INDICATOR FAILED. REMOVED FAULTY INDICATOR AND INSTALLED NEW INDICATOR. FUNCTIONAL CHECK OK.SDR HEEA0015228Indicator · failedTURBINE NEEDLE WOULD NOT MOVE.SDR HEEA0015227Bearing · wornWORN BEARINGS ON TAIL ROTOR LINK.SDR HEEA0015226Bearing · wornWORN BEARINGS ON TAIL ROTOR LINK.SDR HEEA0015222Indicator · failedNR FAILED TO TEST.SDR HEEA0015221Clock · reads highOUTSIDE AIR TEMPERATURE READS HIGH.SDR HEEA0015220Stack · crackedEXHAUST STACK CRACKED.SDR HEEA0015219Disk Coupling · corrodedDISK COUPLING HAS CORROSION.SDR HEEA0015218Valve · leakingCHECK VALVE LEAKING.SDR HEEA0015217Bearing · corrodedBEARING WORN AND CORRODED.SDR HEEA0015216Link · wornTAIL ROTOR LINK WORN.SDR 98ZZZX3092Disc Pack · cracked25 HOUR AD 97-234-17 PTS A, B, AND E. BOTH DISC PACKS HAD NR 1 DISC CRACKED. NR 1 DISC PER DISC PACK CRACKED, NR 4 AND N4 7 T/R DRIVE SHAFT.SDR HEEA0015198Switch · failedLOW LEVEL LIGHT ON SWITCH STAYS ON.SDR 98ZZZX3366Vertical Fin · damagedDURING C/W ASB 407-98-17, THE VERTICAL FIN WAS FOUND DAMAGED BEYOND THE MAXIMUM LIMIT. ACTUAL DEPTH IS APPROXIMATE DEPTH OF .027 INCH. REPLACED FIN WITH NEW FIN P/N 206-020-113-255A S/N BP-2653.SDR HEEA0015191Disk Coupling · crackedDISK COUPLING CRACKED.SDR HEEA0015190Disk Coupling · crackedDISK COUPLING CRACKED.SDR HEEA0015189Indicator · failedMGT INDICATOR ERRATIC, THEN WENT TO ZERO DEGREES.
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