Piper PA-31T2

Service difficulty reports · 62

Newest first. General aviation reporting is voluntary.

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 = 'PA31T2'
  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.

SDR 97ZZZX866Bolt · brokenLEFT LANDING GEAR WOULD NOT GO DOWN. AFTER REPEATED ATTEMPTS, CO2 EMERGENCY DOWN WAS ACTUATED AND GEAR DID GO DOWN AND LOCK. LANDING WAS NORMAL. INSPECTION REVEALED THE BOLT SECURING THE LANDING GEAR ACTUATOR CYLINDER HAD BROKEN. REF: PA31T2 PARTS FIG 41, Feb 7, 1997 · N107MC · Piper PA31T2 · Landing Gear ActuatorSDR 97ZZZX466Fuel Cell · leaksPURCHASED AS A DIRECT REPLACEMENT FOR PIPER P/N 462-722. FUEL CELL S/N A343 WAS INSTALLED AND LEAKED IMMEDIATELY AFTER INSTALLATION. THREE ADDITIONAL FUEL CELLS WERE SHIPPED TO INSTALLER, TWO OF THREE WERE INSTALLED, BUT WOULD NOT FIT FOR VARIOUS REASONS. TJan 6, 1997 · Piper PA31T2 · Fuel StorageSDR 96ZZZX3776Cylinder Assy · splitDURING BRAKE TESTING AFTER OVERHAUL, HYDRAULIC PRESSURE EQUAL TO 150 PSI WAS APPLIED TO BRAKE CYLINDER LEAK CHECK. THE ACTUAL TEST PRESSURE IS 180 PSI PER MANUAL. AT 150 PSI, THE BRAKE CYLINDER ASSY SPLIT FROM ONE END OF BOLT HOLE APPROXIMATELY ONE-HALF WAY Jun 24, 1996 · N774KV · Piper PA31T2 · Master Cylinder/Brake ValveSDR CA960711201Flange · broken legs(CAN) THE STARTER/GENERATOR QUICK ATTACH-DETACH FLANGE WAS FOUND TO HAVE BROKEN LEGS DURING AN INSPECTION. THE PILOT NOTED A DIFFERENT NOISE WHILE STARTING THE AIRCRAFT.Jun 18, 1996 · Piper PA31T2 · Starter-GeneratorSDR CA960515005Static Sensor · leaking(CAN) PIEZO STATIC SENSOR HOUSING LEAKING IN EXCESS OF LIMITSMar 26, 1996 · Piper PA31T2 · Pitot/Static SystemSDR 96ZZZX1478Breakers · failedCIRCUIT BREAKERS BURN UP/MELT INTERNALLY BEFORE TRIPPING, THEN REMAIN OPEN WHEN RESET.Mar 14, 1996 · N2325W · Piper PA31T2 · DC Power Distribution SystemSDR 96ZZZX4419Fuel Cell · mount separatedAFT FUEL PUMP MOUNTING PAD SEPARATED FROM FUEL CELL, LOWER LEFT CORNER. 3-13-96 INSTALLED.Mar 13, 1996 · N2501Y · Piper PA31T2 · Fuel StorageSDR 96ZZZX4418Cell · leakingLEFT INBOARD FUEL CELL LEAKING AT PUMP MOUNTING PAD. 3-12-96- REMOVED.Mar 12, 1996 · N2501Y · Piper PA31T2 · Fuel StorageSDR CA960306005Hyd Hose · leaking(CAN) PILOT SELECTED GEAR DOWN AND RECEIVED INDICATION FROM MAIN GEAR ONLY, NO NOSE GEAR LIGHT. GEAR WAS RECYCLED AND INDICATION WAS RECEIVED. INVESTIGATION FOUND THE NOSE GEAR DOWN HYDRAULIC LINE LOOSE AND LEAKING HYDRAULIC FLUID. SUSPECT A VIBRATION PROBLJan 29, 1996 · Piper PA31T2 · Landing Gear Retraction/Extension SystemSDR CA960116008Rib · broken(CAN)DURING INSPECTION THE LEFT HAND STABILIZER OUTBOARD RIB WAS FOUND BROKEN. BREAK LINE INDICATES THAT THE PART HAD BEEN CRACKED FOR AN UNDETERMINED AMOUNT OF TIME PRIOR TO BREAKING, DUE TO ALUMINUM STREAKING ALONG THE BREAK LINE. SUBMITTER SENT THE PART IN Jan 8, 1996 · Piper PA31T2 · Horizontal Stabilizer, Spar/RibSDR CA951221014Potentiometer · defective(CAN)FLAP SYSTEM GIVING FALSE INDICATION ON PANEL. RIGGING PERFORMED AND ELECTRICAL ADJUSTED. DURING FLIGHT IN COLD CONDITIONS -20 DEGREES C OAT, THE SAME LIGHT ILLUMINATED. LEFT AND RIGHT HAND POTENTIOMETERS TESTED AND THE LEFT HAND POTENTIOMETERS WAS FOUND DDec 8, 1995 · Piper PA31T2 · Trailing Flap Position Indicating SystemSDR 95ZZZX6239Bulkhead · crackedLEFT ENGINE NACELLE INBOARD LONGITUDINAL BULKHEAD IS CRACKED AT INBOARD UPPER BIRDCAGE MOUNT. CRACK IS AT AFT RIVET HOLE. CRACK WAS DISCOVERED DURING ROUTINE INSPECTION.Oct 25, 1995 · N37SR · Piper PA31T2 · Nacelle/Pylon, Bulkhead/Firewall
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