Piaggio P180

Service difficulty reports · 269

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 = 'P180'
  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 CA050621010Blade · fractured(CAN) DURING CRUISE, THE ENGINE EXPERIENCED AN UNCOMMANDED CHANGE IN POWER ACCOMPANIED BY VIBRATIONS. THE ENGINE WAS SHUTDOWN IN FLIGHT AND A SINGLE ENGINE LANDING WAS ACCOMPLISHED. SUBSEQUENT INSPECTION REVEALED FRACTURED POWER TURBINE BLADES.Jun 11, 2005 · Piagio P180 · Turbine SectionSDR CA050324011Cable · worn(CAN) THE CABIN LOWER DOOR'S CABLE ASSEMBLIES WERE FOUND WORN AND THEY WERE REPLACED.Mar 20, 2005 · Piagio P180 · Passenger/Crew DoorsSDR CA050307011Wire · overheated(CAN) OVERHEATED WIRES ON TB-10 WERE REPAIRED THIS WAS DUE TO LOOSE NUT ON MAIN POWER FEED.Mar 4, 2005 · Piagio P180 · Electrical Power System WiringSDR 2005FA0000346Seal · leakingPROPELLER SHAFT SEAL WAS LEAKING, CAUSING HIGH OIL CONSUMPTION. (K)Feb 21, 2005 · N106SL · Piagio P180 · Propeller AssemblySDR CA041220004Wheel · cracked(CAN) THE LEFT MAIN TIRE WAS LOOSING AIR. UPON INSPECTION, A CRACK WAS DISCOVERED IN THE LEFT INBOARD WHEEL HALF, AT THE TIRE BEAD AREA. NO INDICATIONS OF HARD LANDING WERE FOUND. THE WHEEL WAS REPLACED WITH AN OVERHAULED UNIT AND THE OLD WHEEL WAS SENT OUT FODec 14, 2004 · Piagio P180 · Wheel/Ski/FloatSDR CA041019006Mount · corroded(CAN) RUDDER AND AILERON STATIC WICK BASE FOUND LOOSE. PARTS REMOVED CORROSION WAS FOUND ON MATING SURFACE WHICH WAS CLEANED AND BASES ATTACHED SEALED AND PAINTED.Oct 18, 2004 · Piagio P180 · Static Discharge SystemSDR 4046Rudder Pedal · looseTHE RUDDER PEDAL FOOT ASSEMBLIES ARE MADE UP OF A FOOT PEDAL WHICH SLIPS INTO A TUBE AND RIVETED TOGETHER WITH 6 BLIND RIVETS. (FOOT PEDAL IS OFFSET FROM THE TUBE, SO THE PEDAL WANTS TO ROTATE IN THE TUBE WHEN PUSHING FORWARD ON THE PEDAL) THE RIVETS WERE LOOSSep 10, 2004 · N122PA · Piagio P180 · Rudder Control SystemSDR CA040908002Control Unit · frozen(CAN) LT CONDITION LEVER FROZEN, BECAME INOPERABLE AT ALTITUDE.Sep 3, 2004 · Piagio P180 · Propeller Controlling SystemSDR CA040712004Valve · failedPILOTS REPORTED GREEN WING DE-ICE LIGHT CAME ON LEFT SIDE AFTER WING DE-ICE WAS SELECTED OFF AND REMAINED ON FOR FLIGHT. THE LEFT WING VALVE WAS REMOVED AND FOUND TO BE NOT COMPLETELY CLOSED.Jul 8, 2004 · Piagio P180 · Windshield/Door Rain/Ice RemovalSDR 2004F00267Bearing · crackedDISCREPANCY WAS FOUND DURING A SCHEDULED INSPECTION, NO FURTHER DAMAGE WAS NOTED IN THE SURROUNDING AREAS DURING INSPECTION PROCESS. (M)Jul 7, 2004 · N29JS · Piagio P180 · Main Landing GearSDR 2004F00241Seal · separatedAC CLIMBED THRU 25,000 FT, VERY LOUD HOWL, EMANATING FROM EMERG EXIT BEHIND COPILOT SEAT. COMMUNICATION IN AC WAS NEARLY IMPOSSIBLE AND AC WAS FORCED TO RETURN TO BASE. AT 15,000 FT NOISE SUBSIDED AND AC RETURNED TO DEPARTURE. UPON EXAM OF EMERGENCY EXIT, Jun 15, 2004 · N106SL · Piagio P180 · Emergency ExitsSDR CA040528003Line · damagedTHE BRAKE LINE WAS FOUND WITH MECHANICAL DAMAGE DURING THE 600 HOUR INSPECTION. DAMAGE TO THE LINE WAS ON THE UNDER SIDE AND COULD ONLY BE SEEN WITH A MIRROR. THE LINE IS LOCATED OVER A FLIGHT CONTROL CABLE WITH ABOUT 3 INCHES OF CLEARANCE. THE MARKS ON THE May 16, 2004 · Piagio P180 · Landing Gear Brake SystemSDR 4007053Rudder Pedal · looseTHE RUDDER PEDAL FOOT ASSEMBLIES ARE MADE UP OF A FOOT PEDAL WHICH SLIPS INTO A TUBE AND RIVETED TOGETHER WITH 6 BLIND RIVETS. (FOOT PEDAL IS OFFSET FROM THE TUBE, SO THE PEDAL WANTS TO ROTATE IN THE TUBE WHEN PUSHING FORWARD ON THE PEDAL) THE RIVETS WERE LOOFeb 25, 2004 · N109MS · Piagio P180 · Rudder Control SystemSDR CA040120003Wheel · damaged(CAN) THE AIRCRAFT ABORTED THE TAKE OFF DUE TO A FLAT NOSE TIRE. THE WHEEL ASSEMBLY WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. THE WHEEL REMOVED WAS FOUND TO HAVE BEEN PUNCTURED BY THE TOW BAR.Jan 18, 2004 · Piagio P180 · Wheel/Ski/FloatSDR CA040113008Lamp · inoperative(CAN) DURING CRUISE, COCKPIT ROOF MOUNTED MAP LIGHT FAILED, C/B ACTIVATED, CREW NOTICED A SLIGHT ODOR. DURING TROUBLESHOOTING THE ROOF PANEL WAS REMOVED AND IT WAS DISCOVERED THAT THE LAMP TERMINAL HAD BEEN IN CONTACT WITH AIRFRAME STRUCTURE CAUSING THE RUBBERJan 8, 2004 · Piagio P180 · Flight Compartment LightingSDR CA031027001Shutoff Valve · leaking(CAN) THE ENGINE COWLS WERE REMOVED FOR 150 HOUR INSPECTION AND A SMALL AMOUNT OF FUEL WAS FOUND IN THE BOTTOM RIGHT COWL. WHEN THE RT FUEL BOOST PUMP WAS TURNED ON TO LOCATE THE SOURCE FUEL WAS OBSERVED DRIPPING AT ABOUT 1 DROP PER 2 SECONDSFROM THE RT ENGINOct 24, 2003 · Piagio P180 · Engine Fuel DistributionSDR CA030930001Breather Tube · kinked(CAN) THE AIRCRAFT WAS WORKED ON FOR HOT ENVIRONMENTAL ODOR. THE ENVIRONMENTAL SYSTEM WAS CHECKED OVER AND THE DUCT WORK WAS CHECKED WITH A BORESCOPE. PILOTS REPORTED THE ODOR WAS BACK WITH SMOKE WHEN THE POWERED UPTHE ENGINES.THE ENGINE COWLS WERE REMOVED ANSep 25, 2003 · Piagio P180 · Turbine Engine Air Inlet SectionSDR 2001FA0000314Propeller · damagedAIRCRAFT LANDED RENO, PILOTS NOTICED DIFFICULTY GETTING PROP INTO BETA AND SLIGHT VIBRATION DURING ROLLOUT. AT HANGER, PILOTS NOTICED LOWER NG ON NR 1 ENGINE ADN ON SHUTDOWN. NR 1 PROP STAYED IN A FLIGHT PITCH ANGLE WHILE NR 2 PROP WENT TO FEATHER PER NORMALAug 5, 2001 · N705PA · Piagio P180 · Propeller AssemblySDR 99ZZZX395Switch · malfunctionedFLAPS 'LOCKED OUT' IN THE MID-POSITION WHILE MOVING FROM THE FULL DOWN TO UP POSITION. THE MALFUNCTION WAS DUE TO A HIGH RESISTANCE IN THE INTERNAL MICROSWITCHES OF THE FLAP DRIVE UNIT. THE AIRCRAFT MANUFACTURER IS AWARE OF THE PROBLEM. THE FLAP DRIVE UNIT WDec 16, 1998 · N220TW · Piagio P180 · Trailing Edge Flap Control System
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