JASC 5302
Service difficulty reports · 965
Reports filed under 5302 · Rotorcraft Tail Boom, newest first.
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 = '5302' 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 = '5302' 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 HEEA955580Cap · mis mfgMILLED AREA OF VERTICAL LEG, WHERE COWLING CAMLOC RAIL ATTACHES, IS NOT WIDE ENOUGH TO MAINTAIN REQUIRED EDGE DISTANCE ON BOTH CAP ANGLE AND CAMLOC RAIL.SDR HEEA955579Cap · mis mfgIMPROPER DISTANCE FROM LOWER EDGE OF CAP TO MILLED AREA FOR CAMLOC RAIL. DISTANCE ON NEW PART IS .650. DISTANCE ON OLD PART IS .550.SDR 95ZZZX5042Tailboom · dentedTAILBOOM HAS DENT IN FORWARD RIGHT SIDE DUE TO LANDING WITH SIDEWARD MOTION.SDR HEEA955376Frame · crackedTAILBOOM RING CRACKED AT UPPER R/H ATTACHMENT POINT. REMOVED CRACKED RING AND REPLACED WITH SERVICEABLE RING AND RETURNED AIRCRAFT TO SERVICE.SDR HEEA955232Frame · crackedLOOSE FITTING CAUSED TAILBOOM RING P/N 206-032-308-103S AND LONGERON P/N 206-031-314-037S TO CRACK. SEE MMIR # 5233 FOR LONGERON INFORMATION.SDR 95ZZZX3368Attach Fitting · corrodedDISCOVERED DURING A/C REFURB, T/B ATTACH FITTING, STA 300, WITH EXCESSIVE CORROSION, PART UNSERVICEABLE.SDR HEED955Tailboom · corrodedLONGERON CORRISON AT SPLICE JOINT. CAUSE BY MANUFACTURER'S LEAVING PEEL-PLY MATERIAL ON SPLICE JOINT. HAD TAILBOOM REPAIR LOCALLY.SDR HEEA954683Frame · crackedTAILBOOM RING CRACKED IN SEVERAL PLACES ON UPPER L/H ATTACHMENT POINT. SCRAPPED PART. SENT TO BELL HELICOPTER-CANADA, ATTENTION: CLAUDE PAQUETTE PER HIS REQUEST FOR EVALUATION.SDR HEEA954682Fitting · brokenUPPER L/H CASTING BROKEN INTO THREE SEPARATE PIECES. SCRAPPED PART.SDR 95ZZZX2216Support Assy · defectiveFOUND ON INCOMING INSPECTION, 90 DEGREE GEARBOX ALIGNMENT HOLES IN SUPPORT, ELONGATED BEYOND LIMITS. HOLES HAVE A VERY TIGHT TOLERANCE (.253 INCH - .255 INCH) AND COME FROM FACTORY AT .254 INCH. A STEEL PIN GOING THROUGH CAST ALUMINUM MAY AGGRAVATE THE PROBLSDR 95ZZZX2088Nut · failedWHILE INSTALLING TAIL BOOM WHEN COMING UP TO REQUIRED TORQUE ON UPPER RT TAIL BOOM TO FUSELAGE ATTACHMENT BOLT PN NAS 628, A 'POP' NOISE WAS HEARD AND THE BOLT THREADS SEEMED TO BE STRIPPED. THE BOLT AND NUT WERE REMOVED AND THE NUT WAS FOUND SPLIT IN TWO PIESDR 95ZZZX1503Fitting · crackedTAILBOOM ATTACH FITTING FOUND CRACKED ON ROUTINE INSPECTION. FITTING AND LONGERON WERE REPLACED IAW BELL 206 SRM.SDR 95ZZZX838Casting · workingDURING DAILY INSPECTION NOTED VERTICAL FIN WORKING AGAINST TAILBOOM CASTING.SDR 95ZZZX1059Fittings · loose rivetsDURING PHASE INSPECTION, FOUND WORKING (LOOSE) RIVETS ON ALL FOUR TAILBOOM ATTACH FITTINGS. SUSPECT CAUSE IS USE OF E-RIVETS AND SOME BAD RIVET BUCK TAILS.SDR 95ZZZX1058Fittings · loose rivetsDURING PHASE INSPECTION, FOUND WORKING (LOOSE) RIVETS ON ALL FOUR TAILBOOM ATTACH FITTINGS. SUSPECT CAUSE IS USE OF E-RIVETS AND SOME BAD RIVET BUCK TAILS.
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