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 jasc_code = '6420' 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 jasc_code = '6420' 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 CA040916009Hub · cracked(CAN) DURING NDT INSPECTION THE HUB WAS FOUND TO HAVE A CRACK INDICATION ON ONE OF THE EARS. THE INDICATION WAS BLENDED, WITH APPROX. .010-.015 INCH OF MATERIAL BEING REMOVED. THE HUB WAS THEN RE-INSPECTED AND INDICATIONS OF THE DEFECT WERE STILL EVIDENT UNDSDR ALGA097281Trunnion · corrodedTAIL ROTOR TRUNNION HAS CORROSION DAMAGE ON SPLINES. REPLACED W/SERVICEABLE HOUSING BY OVERHAUL SHOP.SDR ALGA097279Bearing · damagedTAIL ROTOR BEARING HAS FLAT SPOTS ON NEEDLE ROLLERS. REPLACED W/NEW PART BY OVERHAUL SHOP.SDR ALGA097278Housing · peelingBLUE EPOXY COATING PEELING. REPLACED W/SERVICEABLE HOUSING BY OVERHAUL SHOP.SDR I7LA0002746Trunnion · overheatedSEPT 5, 2004. AIRCRAFT TT: 3518.7 UPON 25 HOUR INSPECTION, TAIL ROTOR TRUNION ENAMEL PAINT DISCOLORED. SIGNS OF EXCESSIVE HEAT.SDR I7AL0002748Trunnion · overheatedUPON DAILY INSPECTION, MECHANIC FOUND ABNORMAL PLAY IN TAIL ROTOR ASSEMBLY. TRUNION- FURTHER INSPECTION FOUND SIGNS OF EXCESSIVE HEAT TO TRUNION ENAMEL PAINT DISCOLORED (BROWN).SDR CA040821001Spherical Bearin · failed(CAN) A/C WAS CLIMBING AFTER FILLING THE WATER BUCKET WHEN HE LOST COMPLETE TAIL ROTORAUTHORITY.THE A/C MADE SEVERAL 360 DEGREE TURNS AFTER COMING TO REST IN A CON FINED AREA. SUBSTANTIAL DAMAGE WAS DONE TOTHE MAIN ROTOR BLADES AS THEY STRUCK A TREE UPON LANDISDR I7LA0002736Trunnion · looseUPON DAILY INSPECTION, MECHANIC NOTED EXCESSIVE PLAY IN TAIL ROTOR HUB AT TRUNION AREA. TAIL ROTOR HUB WAS REMOVED FOR INSPECTION A SOFT FACE MALLET WAS REQUIRED TO FREE THE TRUNION FROM TAIL ROTOR GEARBOX OUTPUT SHAFT. REMOVAL OF TRUNION NOTED SIGNS OF EXCESDR MDR04061Bearing Race · crackedTAIL ROTOR HEAD WAS REMOVED FROM AC DUE TO SUDDEN LEAKAGE FROM TAIL ROTOR GRIP. DISASSEMBLED TAIL ROTOR HEAD AND FOUND THE SHOULDER BOLT INNER RACE CRACKED ON THE BACK SLEEVE AND SPINDLE. CRACK TRAVELS COMPLETELY ACROSS BEARING CONTACT SURFACE AND COMPLETELYSDR ERAA097079Bushing · roughNEW BUSHING THAT IS ROUGH AND UNFINISHED. ID IS TOO LARGE. WHEN INSTALLED ON INNER SLEEVE, BUSHING SPINS LOOSE. SUSPECT IMPROPER MANUFACTURE OF BUSHING. RETURNING ON ERA PACK SLIP NR 5956 REQUESTING CREDIT FOR REPLACEMENT PART.SDR I7LA0002728Trunnion · overheatedUPON 25 HOUR INSPECTION, SIGNS OF HEAT NOTED. ENAMEL PAINT WAS BROWN-DISCOLORED.SDR KBM2004F00191Bearing · wornT/R SPIDER END BALL BEARINGS WORN BEYOND LIMITS. REMOVED AND REPLACED.SDR I7LA0002725Trunnion · overheatedUPON 25 HOUR INSPECTION, TRUNION SHOWS SIGNS OF EXCESSIVE HEAT, DISCOLORED (BROWN) COATING. ENAMEL PAINT.SDR ERAA097521Rotor Head · damagedINNER SLEEVE HAT BUSHING DIMENSION TOO LARGE. COULD NOT INSTALL. REMOVED MOUNTING FORK AND BLADE ASSEMBLIES. REMOVED AND REPLACED 2 EA INNER SLEEVE HAT BUSHINGS. MILLED TO PROPER DIMENSIONS AND LINE REAMED BORGS AS REQUIRED. VISUALLY INSPECTED AND FOUND NSDR HXSD2004802Gearbox · making metalPILOT REPORTED A CHIP LIGHT FOR THE TAIL ROTOR GEAR BOX. MECHANIC INVESTIGATED AND FOUND FOUR HAIR LINE SLIVERS ON THE CHIP PLUG ALL WHICH EXCEEDED LIMITS AS DESCRIBED BY THE MM. REMOVED THE GEAR BOX (PN 369D25400 SN 0295) AND INSTALLED SERVICEABLE GEAR BOX SDR ERAA098189Rotor Head · crackedTAIL ROTOR CRACKED INNER SLEEVE BUSHING. TEFLON BUSHINGS WORN, INNER SLEEVE STEEL BUSHINGS WORN, GASKETS ROTTEN, 2 SLEEVES CORRODED, 1 RING CORRODED. COMPLETELY DISASSEMBLED FOR INSPECTION. REPLACED UNSERVICEABLE PARTS. C/W 1200 HR AND 2400 HR INSPECTIONS SDR ERAA097094Rotor Head · out of balanceUNABLE TO BALANCE HIGH FREQ, TRUNNION HAS PLAY. PITCH HORN BUSHINGS MISSING, NO PLAY IN YOKE BRHS, TRUNNION FEELS GOOD, NO DETECTABLE PLAY. TRUNNION SPLINES ARE WEAR STEPPED. SCRAPPED TRUNNION. DISASSEMBLED T/R ASSY, REPAIRED T/R BLADE A-10206, INSTALLED NSDR KBM2004F00154Pin · wornT/R EXPANDABLE PIN WORN. REMOVED AND REPLACED.SDR KBM2004F00152Bearing · wornT/R HALF SHELLS WORN BEYOND LIMITS. REMOVED AND REPLACED.SDR KBM2004F00187Spider · wornT/R SPIDER BALL END WORN. REMOVED AND REPLACED.SDR KBM2004F00066Ball End · wornTAIL ROTOR SPIDER END BEARINGS WORN, REQUS REPLACEMENT. REMOVED AND REPLACED.SDR AUS20040343Fitting · cracked(AUS) TAIL ROTOR GEARBOX MOUNT CRACKED FROM BOLT HOLE.SDR BAQA094295Bearing · wornBEARINGS WORN IN FORK LINK. REPLACED WITH SERVICABLE ASSET UNIT. 04/29/2004SDR BAQA094294Bearing · wornBEARINGS WORN IN FORK LINK. REPLACED WITH SERVICABLE ASSET UNIT. 04/29/2004SDR BAQA094069Bearing · wornFORK LINK BEARING WORN PREMATURELY. S/N 3040 WAS TAKEN FROM ASSET AND USED ON PBH. REC'D S/N 3675 FROM AEC TO REPLACE ASSET STOCK. REPLACED WITH SERVICABLE UNIT FROM AEC.SDR ERAA097101Rotor Head · bindingBINDING TAIL ROTOR BLADE. NORMAL WEAR ON BUSHINGS AND SLEEVES ACTION TAKEN: DISASSEMBLED, CLEANED AND VISUALLY INSPECTED ALL PARTS. C/W 300 HR / 2400 HR BLADE INSPECTION ON BLADES SN 658 AND 663. INSTALLED NEW INNER SLEEVE BUSHING AND NEW GRIP BUSHING. NESDR CA040805008Bearing · worn(CAN) WHILE PERFORMING A 100 HOUR INSPECTION THE TAIL ROTOR SPIDER WAS DISCONNECTED FROM THE INPUT BELLCRANK TO CHECK THE SPIDER SWASHPLATE BEARING. NOTICED THAT THE BALL END BEARING ON THE SWASHPLATE INPUT WAS WORN OUT. ( IPC 65.20.30 FIG 1A ITEM 95 ) MEASURSDR CA040318004Grease Fitting · clogged(CAN) DURING 50 HOUR LUBRICATION INTERVAL. FITTINGS WOULD NOT PASS GREASE. FITTING REPLACED.SDR KBM2004F00028Bearing · wornTAIL ROTOR BLADE HALF SHELL BEARING WORN OUT. REMOVED AND REPLACED.SDR KBM2004F00042Ball · excess playTAIL ROTOR PC SPIDER END BALL BEARING HAS EXCESSIVE PLAY. REMOVED AND REPLACED.SDR KBM2004F00036Case · wornTAIL ROTOR HALF SHELLS WORN AND TORN. REMOVED AND REPLACED.SDR KBM2004F00071Bearing · shearedTAIL ROTOR HUB HINGE SPHERICAL LAMINATED BEARING IS SHEARED. REMOVED AND REPLACED.SDR KBM2004F00017Bearing · wornTAIL ROTOR HUB LAMINATED RUBBER HINGE BEARING ARE WORN BEYOND LIMITS. REMOVED AND REPLACED WITH NEW.SDR JYD2004F00002Rotor Head · crackedDURING NORMAL AC INSPECTION, THE FOLLOWING WAS FOUND; THE OB SIDE OF THE POCKET IS CRACKED 1.8125 INCH FROM THE TRAILING EDGE AND .25 INCH FROM THE TIP END. THE CRACK IS RUNNING SPAN WISE AND IS 6875 INCH LONG. PROBABLE CAUSE UNKNOWN. (MDR04-042)SDR JYD2004F00001Rotor Head · crackedDURING NORMAL AC INSPECTION, THE FOLLOWING WAS FOUND; THE OB SIDE OF THE POCKET HAS 3 CRACKS RUNNING SPANWISE APPROXIMATELY .398 INCH FROM THE TRAILING EDGE. THE FIRST CRACK IS 7.5 INCH FROM THE TIP END AND .835 INCH LONG. THE SECOND CRACK IS 9 INCHES FROM SDR JYD2004F00000Rotor Head · crackedDURING NORMAL AIRCRAFT INSPECTION, THE FOLLOWING WAS FOUND: TWO SPANWISE CRACKS EXIST AT THE T/E ON THE OB SIDE. THE FIRST CRACK IS 7.25 INCHES FROM OB END OF THE POCKET AND IS 1.25 INCHES IN LENGTH. THE SECOND CRACK IS 14.5 INCHES FROM THE OB END OF THE POCSDR KBM2004F00106Pitch Link · crackedTAIL ROTOR PITCH LINK, CRACKED BUSHING. REMOVED AND REPLACED.SDR KBM2004F00076Bearing · wornHALF SHELL BEARING IS WORN BEYOND LIMITS. REMOVED AND REPLACED.SDR BAQA091942Torsion Bar · distortedTAIL ROTOR TORSION BAR DISTORTED. REPLACED WITH SERVICABLE UNITS. 01/23/2004SDR KBM2004F00057Housing · crackedTAIL ROTOR LAMINATED HALF SHELLS CRACKED BEYOND LIMITS. REMOVED AND REPLACED.SDR KBM2004F00068Bearing · wornTAIL ROTOR LAMINATED HALF BEARINGS WORN. REMOVED AND REPLACED WITH SERVICEABLE UNIT.SDR ERAA092653Bushing · misinstalledUNABLE TO ADJUST FOR PEDAL FORCE. TEFLON ON GRIP BUSHINGS FLAKING. COMPLY PREINSPECTION AND NOTED NO DEFECTS. DISASSEMBLED AS FAR AS NECESSARY FOR REPAIR. VISUALLY NOTED TEFLON FLAKING ON GRIP BUSHING. POSSIBLE CAUSE OF ABOVE DISCREPANCY. NO OTHER DISCRESDR ERAA094450Rotor Head · debondedBEARING DEBONDING CAUSING BINDING. OB BUSHING ON INNER SLEEVE HAD SLIPPED. GRIP BUSHINGS WORN. ACTION TAKEN: C/W PRE INSPECTION AND FOUND INNER SLEEVE BUSHING NOT SEATED. DISASSEMBLED AS FAR AS NECESSARY FOR REPAIR, CLEANED AND VISUALLY INSPECTED PARTS. SDR 2003121Roll Pin · loosePILOT COMPLAINED OF NOISE AND VIBRATION ON SHUT DOWN. INSPECTED MAIN ROTOR HUB, FOUND ROLL PINS ON DROOP STOP FOLLOWER ASSEMBLIES HAD BACKED OUT AND WERE CONTACTING THE LOWER SHOE. THE INTERFERENCE WAS CAUSING THE FOLLOWERS TO BE FROZEN IN PLACE. WHEN THE ASDR BAQA091589Torsion Bar · bentTAIL ROTOR TORSION BAR BENT OUT OF TOLERANCE. REPLACE SERVICEABLE UNIT.SDR BAQA090674Bearing · wornFORK LINK BEARING HAS PLAY. REPLACED WITH SERVICEABLE UNIT.SDR CA040114008Rotor Head · inoperative(CAN) UPON RECEIPT OF AD2003-24-51 HELICOPTER WAS INSPECTED FOR THE SUSPECT NAS6605-31BOLTS. EVEN THOUGH THE R44 S/N WAS NOT LISTED IN THE AD OR ROBINSON HELICOPTER SERVICE BULLETIN 51 THE T/R HUB NAS6605-31BOLTS WERE FOUND TO HAVE THE VENDOR IDENTIFICATION MASDR S9HA265YASpar · crackedPILOT HEARD USUAL NOISE WHILE FLEXING TAIL ROTOR BLADES DURING PREFLIGHT. MAINTENANCE REPLACED THE TAIL ROTOR WITH A SERVICEABLE TAIL ROTOR FROM A ANOTHER AIRCRAFT. UPON TEAR DOWN INSPECTION A CRACK IN THE SPAR 10MM WIDE BY 150MM IN LENGTH ON THE LEADING OF SDR BAQA091233Laminate Stop · corrodedTEFFLON WORN OUT, CORROSION.SDR BAQA091232Sleeve · wornTAIL ROTOR SLEEVE WORN IN O-RING CONTACT AREA. CORROSION INSIDE. REPLACED WITH SERVICEABLE UNIT.
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