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 HCMA075311Rod · wornPART IS WORN BEYOND LIMITS.PLEASE REPLACE BEARINGS UNDER WARRANTY.SDR HCMA075310Rod · wornPART IS WORN BEYOND LIMITS.PLEASE REPLACE BEARINGS UNDER WARRANTY.SDR HCMA075309Rod · wornPART IS WORN BEYOND LIMITS. PLEASE OVERHAUL PC LINKS. TOTAL TIME UNKNOWN.SDR HCMA075308Rod · wornPART IS WORN BEYOND LIMITS. PLEASE OVERHAUL PC LINKS.SDR 20001215SH018Control Rod · wornPITCH CONTROL ROD WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR HCMA075303Bearing · defectivePART IS DEFECTIVE. FAILED "J" GAP.SDR HCMA075297Bearing · wornBEARING IS WORN BEYOND LIMITS.SDR CA010921004Bolt · broken(CAN) - TAILROTOR GEARBOX RETENTION HARDWARE, BOLT HEAD FOUND MISSING DURING SCHEDULED MAINTENANCE. - 3 REMAINING BOLTS WERE INSPECTED WITH NO FAILURES FOUND. ALL THE TAILROTOR GEARBOX RETENTION HARDWARE WAS REPLACED WITH NEW. A 300 HOUR RETIREMENT SCHEDULE SDR CA000801009Bearing · failed(CAN) T/R BECAME UNBALANCED. INSPECTED HUB AND FOUND BEARING TEFLON LINER CAME OFF FROM OUTER RACE.SDR 20000804SH013Pitch Horn · corrodedDURING FIRST 2,500 HOUR OVERHAUL, FOUND CORROSION BEYOND LIMITS UNDER PLATE, POSSIBLY CAUSED BY INCOMPATIBLE ADHESTIVE PRIMER. (X)SDR 20001219SH019Arm · crackedARM ASSEMBLY HAD CRACK INDICATION ON OUTBOARD MOUNTING LUG EXTENDING FROM .256 INCH/.252 INCH DIAMETER THROUGH-HOLE TO .34 INCH RADIUS. CIRCUMSTANCES UNDER WHICH CRACKING OCCURRED ARE UNKNOWN. POSSIBLE CAUSE IS FROM FRETTING MOVEMENT BETWEEN SLEEVE MOUNTING SDR 20001218SH006Arm · crackedARM ASSEMBLY HAD CRACK INDICATION ON OUTBOARD MOUNTING LUG EXTENDING FROM .256 INCH/.252 INCH DIAMETER THROUGH HOLE TO .34 INCH RADIUS. CIRCUMSTANCES UNDER WHICH CRACKING OCCURRED ARE UNKNOWN. POSSIBLE CAUSE IS FROM FRETTING MOVEMENT BETWEEN SLEEVE MOUNTING SDR CA000706029Bearing · failed(CAN) THE ENGINEER WAS INSPECTING THE T/R SWASHPLATE ASSEMBLY AS PER AD 2000-222-076(A) AND FOUND THE PAINTED INDENT MARKS WERE NOT ALIGNED. THE T/R SWASHPLATE ASSEMBLY WAS REMOVED AND SENT TO OUR COMPONENT SHOP. UPON DISASSEMBLE IT WAS FOUND THAT THE BEARING SDR CA000706026Housing · sheared(CAN) DURING HUB REMOVAL TO C/W SB 65.00.38 (T/R SPYDER BEARING KIT INSTALLATION) THE KEY THAT ALIGNS HUB TO T/R SHAFT WAS FOUND SHEARED & THE HUB HAD SPUN APPROX. 110 DEGREES. THE T/R LONG DRIVE SHAFT P/N 350A34-0110-07 WAS FOUND TO HAVE AN APPROX 60 DEGREES SDR 20000801SH031Spider · wornLOSS OF BEARING TORQUE CAUSED DAMAGE TO THE ROTATING SPIDER. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR 20000801SH048Bar · wornLAMINATED TORSION BAR WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR 20000801SH047Bar · wornLAMINATED TORSION BAR WORN BEYOND LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR 20000801SH046Bar · wornLAMINATED TORSION BAR WORN BEYOND LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR 20000801SH045Spider · wornPITCH CHANGE SPIDER ASSY WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR CA001013018Bearing · failed(CAN) EXCESSIVE PLAY FOUND BETWEEN THE BEARING AND SPIDER HOUSING. ALSO FOUND SIGNS OF OVERHEATING WITH LOSS OF GREASE AND PAINT MELTING.SDR 20000801SH036Ball Joint · wornBALL JOINT WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR 20000710SH009Disc Pack · looseDISC TO FLANGE INTERFACE FOUND LOOSE DURING QUILL SEAL CHANGE. REPLACED BOTH DISC AND FLANGE WHICH WAS MEASURED AND FOUND BEYOND LIMITS. (X)SDR 20000710SH008Flange · looseDISC TO FLANGE INTERFACE FOUND LOOSE DURING ROTOR BRAKE QUILL SEAL CHANGE. REPLACED BOTH DISC AND FLANGE WHICH WERE MEASURED AND FOUND WORN BEYOND LIMITS. (X)SDR CA000614008Bearing · failed(CAN) AIRCRAFT WAS GROUND RUN TO GROUND IDLE. TAIL ROTOR PEDDLES STARTED TO STIFFEN UP. AS THE AIRCRAFT RPM WAS INCREASED TO 100 PERCENT NR, TAIL ROTOR PEDDLES STIFFENED TO BEYOND LIMITS APPROXIMATELY 35 POUNDS. FORCE REQUIRED TO MOVE THE PEDDLES. AT THISSDR CA001013014Bearing · failed(CAN) DURING A 50 HR INSPECTION ON THIS SPIDER, THE BEARING WAS FOUND TO BE ROUGH. NOTE THE BEARING ONLY REACHED 10 PERCENT OF ITS SERVICE LIFE.SDR 20000801SH032Laminated Hinge · wornELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM ONE EACH KIT P/N 355A33. (X)SDR 20000801SH017Spider · wornTEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR AU000429Bearing · worn(AUS) TAIL ROTOR TEETER BEARINGS WEARING PREMATURELY.SDR 20000718SH003Bearing · wornDURING DAILY SERVICE CHECK, FOUND INBOARD FEATHER BEARING WEAR, CAUSING THE OUTER RACE OF FEATHER BEARING TO SHIFT IN YOKE CAUSING BORE TO WEAR BEYOND LIMITS. (X)SDR CA000511004Bushing · loose(CAN) PILOT STARTED AIRCRAFT AND FOUND PEDAL FORCES EXCESSIVE. AIRCRAFT WAS SHUT DOWN. T/R WAS DISASSEMBLED AND IT WAS FOUND THAT ONE OF THE OUTBOARD BUSHING HAD SLID APPROXIMATELY .25 INCH OFF THE INNER SLEEVE AND WAS RUBBING THE OUTBOARD SPACER, LOCATED INSISDR 20000801SH030Spider · wornTEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR 20000607SH016Bearing · unserviceableBEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. (X)SDR CA000412003Bushing · cracked(CAN) PILOT COMPLAINED THAT EXCESSIVE LEFT PEDAL WAS REQUIRED. TAIL ROTOR ASSEMBLY WAS MEASURED WITH SPRING SCALE AND FORCES WERE FOUND EXCESSIVE. TAIL ROTOR DISASSEMBLED TO CLEAN INNER SLEEVE BUSHINGS AND TEFLON BUSHINGS. THE OUTBOARD SLEEVE BUSHING WAS FOUNSDR 20000607SH012Bearing · wornBEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH2 EACH NEW UNITS, CORRECTED PROBLEM. (X)SDR CA000320001Bearing · worn(CAN) A T/R SPINDLE WAS REMOVED TO REPLACE A LIFE LIMITED PART. WHILE THE SPINDLE WAS OFF, A VISUAL INSPECTION OF THE FLAPPING BEARING INNER RACE REVEALED A CRACK. BEARING REPLACED.SDR 20000607SH011Bearing · wornBEARING WORN BEYOND SERVICEABLE LIMITS. CORE SCRAPPED LOCALLY BY MECHANIC. REPLACED 2 EACH WITH NEW UNITS, CORRECTED PROBLEM. (X)SDR 20000605SH023Bearing · wornLAMINATED TAIL BEARING - ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR AC2A0000029Bearing · wornBEARING BEYOND LIMITS. REPLACED ROD END. (X)SDR AC2A0000025Bearing · crackedALL FEATHERING BEARINGS CRACKED. REPLACED TAIL ROTOR HUB AND BLADE ASSY WITH CHEVRON OWNED TAIL ROTOR AND HUB SPARE. (X)SDR LS1R066009Ring Assy · wornRING ASSY WORN EXCESSIVELY BEYOND LIMITS.SDR HEEA066515Mount · wornRUBBER ON MOUNT DETERIORATED.SDR HEEA066507Hub · damagedFEATHERING BEARINGS WORN AND TEFLON COMING OUT FROM AROUND BEARING.SDR HEEA066501Bearing · damagedREMOVED TAIL ROTOR ASSEMBLY DUE TO TRUNNION ELASTOMERIC BEARING SEPARATION AND EXTRUDING.SDR HEEA065898Bearing · wornWORN BEARINGS.SDR HEEA065892Bearing · wornBEARINGS WORN.SDR GJQR0000280Yoke · wornYOKE WORN BEYOND ALLOWABLE LIMITS AT CONTACT AREA WITH STATIC STOP BUMPER. BUMPER MATERIAL IS VERY HARD. (X)SDR ERAA065957Hub · mismanufacturedBEARING JOURNALS SLIGHTLY OVERSIZED FROM LAST REPAIR.SDR 20000605SH022Bearing · wornLAMINATED TAIL BEARING - ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR CA000215029Bearing · wrong part(CAN) T/R SPIDER MODIFICATION KITS P/N 350A08-0756-0071 SUSPECT UNNAPROVED BEARINGS RECEIVED. ISSUE SENT TO M&M FOR FOLLOW-UP.SDR 20000405SH008Stud · looseTAIL ROTOR PITCH HORNS, PITCH CHANGE LINK STUDS LOOSE. REPLACED PART. (X)
Back to JASC 6420