Piaggio P180

Service difficulty reports · 269

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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 V2JA131Electrical Box · failedDURING CLIMBOUT, CREW NOTED A STRONG ELECTRICAL ODOR WITH A SLIGHT "HAZE". CREW CONTACTED ATC AND DIVERTED. ACFT LANDED WITH NO INCIDENT.Mar 4, 2010 · N131SL · Piagio P180 · Electrical Power System WiringSDR V2JA159Connector · contaminatedRT ENGINE FIRE LIGHT ILLUMINATED IN FLIGHT AT FL 001 ON APPROACH. LANDED WITH NO ISSUE, TAXIED OFF RUNWAY AND SHUT MOTOR DOWN. FOUND MOISTURE IN FIRE LOOP CONNECTOR PLUG.Feb 2, 2010 · N159SL · Piagio P180 · Fire Protection System WiringSDR V2JA157Cable · frozenFLIGHT CONTROLS FROZE (ELEVATOR & RUDDER CABLE) AT CRUISE ALTITUDE. REGAINED MOVEMENT WITH DESCENT.Jan 27, 2010 · N157SL · Piagio P180 · Rudder Control SystemSDR V2JA200100103001Engine · overtempNR 2 ENG ITT BEGAN CLIMBING TO MAX ALLOWABLE, IAW PROCEDURES CREW SECURED ENG AND LANDING SAFELY.Jan 3, 2010 · N172SL · Piagio P180 · Engine (Turbine/Turboprop)SDR 2009FA0001019Blower · failedPILOT REPORTED RUBBNG SOUND AND ODOR OF BURNING ELECTRICAL COMPONENTS WITH COCKPIT FAN ON. FOUND FAN CASE PARTIALLY MELTED DUE TO OVERHEATING RESISTOR WHICH DETACHED FROM THE CASE. DAMAGES LIMITED TO THE BLOWER ASSY, NO FURTHER DAMAGES FOUND ON THE ACFT.Nov 4, 2009 · N145GS · Piagio P180 · Air Distribution FanSDR V2JA156Engine · malfunctionedRT ENGINE LOSS OF OIL PRESSURE INDICATION ON TAKE-OFF. SECURED ENGINE AND LANDED.Oct 7, 2009 · N156SL · Piagio P180 · Engine (Turbine/Turboprop)SDR 2009FA0000748Controller · malfunctionedAT ALTITUDE THE CABIN PRESSURE WARNING LIGHT ILLUMINATED AND THE RATE OF CLIMB FOR THE CABIN ALTITUDE WAS 4000' ASCENDING. PILOT'S MADE AN EMERGENCY DECEND TO 12,000 FT. BACK AT THE STATION THE FAULT LIGHT ON THE SELECTOR PANEL REMAINS ILLUMINATED INDICATING AAug 28, 2009 · N180BP · Piagio P180 · Cabin Pressure Control SystemSDR V2JA138SLEngine · malfunctionedAT APPROX 1130Z ON 7/6/09 CREW EXPERIENCED A MOMENTARY LOSS OF OIL PRESSURE ON THE NR 1 ENGINE. REDUCED POWER THEN INDICATION WENT AWAY, WENT BACK TO FULL POWER. AT 1135Z FELT A VIBRATION AND THEN ANOTHER TOTAL LOSS OF OIL PRESSURE WITH TORQUE INDICATION. CJul 6, 2009 · N138SL · Piagio P180 · Engine (Turbine/Turboprop)SDR 2009F00050Valve · leakingCREW REPORTED MAIN CABIN DOOR SEAL LEAKAGE AT FL350, DAYLIGHT VISIBLE PAST SEALS. FOUND MAIN DOOR SEAL NOT INFLATING DUE TO LOWER 3-WAY VALVE ASSY LEAKING INTERNALLY. REPLACED 3-WAY VALVE WITH NEW VALVE ASSY IAW P180 MM, GROUND RUN OPS CHECKS OK. TRANSIENT AJul 1, 2009 · N159SL · Piagio P180 · Passenger/Crew DoorsSDR 2009F00052Retainer · crackedAFTER DEPARTURE, FOR REPOSITIONING FLIGHT, CREW NOTED EXCESSIVE CABIN ENTRY DOOR SEAL LEAKAGE AT 16,000 MSL, CABIN ALTITUDE CHANGE RATE EXCESSIVE. RETURENED TO DEPARTURE. FOUND HOLE IN CABIN DOOR SEAL. AFTER REMOVAL OF SEAL FOR REPAIRS, FOUND PN 80-111388-0Jun 30, 2009 · N159SL · Piagio P180 · Passenger/Crew DoorsSDR BZU2009F00000Actuator · malfunctionedCREW REPORTS NOSE STEERING FAIL LIGHT COMES ON AND STEERING IS UNRESPONSIVE WHEN TAXI MODE IS SELECTED. THIS IS THE 4TH ACTUATOR USED ON THIS ACFT IN 506.8 HOURS. ALL OTHER HAVE FAILED IN A SIMILAR MODE. THE PROBLEM SEEMS TO BE IN THE ELECTRICAL FOLLOW UP MMay 27, 2009 · N5166P · Piagio P180 · Landing Gear Steering SystemSDR V2JA137Engine · shutdownCLIMBING OUT THROUGH FL 145 A LOUD POP WAS HEARD. ENGINE INDICATIONS AND ACFT YAW SHOWED THE RT ENGINE HAD FAILED. THE CREW THEN SECURED THE ENGINE AND DECLARED AN EMERGENCY. THROUGH THE ASSISTANCE OF ATC, DECIDED THE AIRPORT OF DESTINATION.May 26, 2009 · N137SL · Piagio P180 · Engine (Turbine/Turboprop)SDR 2009F00020Wire Harness · damagedLANDING GEAR FAILED TO RETRACT WHEN COMMANDED AFTER DEPARTURE. NO LANDING GEAR INTRANSIT INDICATION, HYD SYS PRESSURE NORMAL. FLIGHT CREW VERIFIED LANDING GEAR EMERGENCY EXTENSION HANDLE STOWED CORRECTLY AND RETURNED TO DEPARTURE. DURING TROUBLESHOOTING NOTED Mar 13, 2009 · N155SL · Piagio P180 · Landing Gear System WiringSDR CA090311003Oil System · malfunctioned(CAN) PILOT REPORTED OIL PRESSURE DROP SETTING OFF LOW OIL PRESSURE WARNING. PILOT ELECTED TO SHUTDOWN AND SECURE THE ENGINE. A SINGLE-ENGINE LANDING WAS ACCOMPLISHED. THE ENGINE WILL BE RETURNED TO MFG FOR INVESTIGATION, UPDATES WILL BE PROVIDED IN DUE COURSEFeb 27, 2009 · Piagio P180 · Turbine Engine Oil SystemSDR V2JA132Autopilot Sys · malfunctionedAT FL300 CREW BEGAN TO NOTICE SMOKE COMING FROM INSTRUMENT PANEL.Feb 18, 2009 · N132SL · Piagio P180 · Autopilot SystemSDR V2JA160Static Line · contaminatedDUAL ADC FAILURE, AIRCRAFT DIVERTED IN FLIGHT TO ROANAKE, (KROA). FAILURE WAS CAUSED BY MOISTURE FREEZING IN THE STATIC LINES, WHEN AIRCRAFT DESCENDED BELOW FL100, ALL SYSTEMS CAME BACK ON FUNCTIONING PROPERLY.Feb 2, 2009 · N160SL · Piagio P180 · Pitot/Static SystemSDR CA090204005Insulation · misinstalled(CAN) DURING AN AVIONICS SYS MODIFICATION, DIMMING CONTROL RELAY PANEL P/N 8090986-401 WAS REMOVED FROM PILOT`S SIDE OF COCKPIT FOR ACCESS. THE INSULATION BAG, P/N 80-909156-11C WAS OBSERVED TO HAVE (2) TWO BURN HOLES IN IT, APPARENTLY CAUSED BY THE (2) RESISTJan 22, 2009 · Piagio P180 · Cabin Equipment/FurnishingsSDR CA081112007Engine · making metal(CAN) DURING FLIGHT, THE ENGINE LOST TORQUE AND OIL PRESSURE. THE PILOT SHUT IT DOWN AND PERFORMED A SINGLE ENGINE LANDING. POST FLIGHT INSPECTION FOUND THE PROPELLER SEIZED AND METAL DEBRIS IN THE EXHAUST. MANUFACTURER WILL CONTINUE INVESTIGATING THE EVENTOct 31, 2008 · Piagio P180 · Engine (Turbine/Turboprop)SDR V2JA145103108Engine · power lossCREW NOTICED LOSS OF TORQUE AND OIL PRESSURE ON LT ENGINE. OIL PRESSURE LIGHT CAME ON. PER MANUAL, CREW CONTINUED WITH SECURING PROCEDURES AND SHUT DOWN LT ENGINE. AIRCRAFT LANDED WITH NO INCIDENT.Oct 31, 2008 · N145SL · Piagio P180 · Engine (Turbine/Turboprop)SDR 2008FA0000755Joint · damagedRT ENGINE POWER CONTROL CABLES FREEZING AT ALTITUDE. INSPECTED CABLE AND FOUND THE STAINLESS STEEL SLEEVE DISCONNECTED AT JOINT TO FLEX SLEEVE. IT APPEARS TO BE A SILVER SOLDERED JOINT, AND SOLDER FAILED ALLOWING MOISTURE TO ENTER THE INTERNAL OF CABLE AND FRESep 30, 2008 · N23RF · Piagio P180 · Power LeverSDR CA080722002Actuator · malfunctioned(CAN) THE HORIZONTAL STABILIZER PRIMARY TRIM FAILED IN THE DOWN MODE ONLY. THE ACFT THEN PROCEEDED TO THE NEAREST AIRPORT. MAINT CONFIRMED THE SNAG ON THE GROUND. AFTER REPLACING THE HORIZONTAL TRIM ACTUATOR THE SYS FUNCTIONED NORMAL.Jul 7, 2008 · Piagio P180 · Elevator Tab Control SystemSDR V2J2008F00002Relay · lockedRT ENGINE FIRE INDICATION AFTER TAKEOFF. (K)Jul 3, 2008 · N102SL · Piagio P180 · Fire DetectionSDR 147SL51808Blower Motor · seizedPILOT DESCRIBED A BURNING SMELL AND SAW SOME LIGHT SMOKE IN THE CABIN.May 18, 2008 · N147SL · Piagio P180 · Air Distribution FanSDR PAI52008S4858Skin · crackedDURING D-CHECK INSPECTION, FOUND CRACK 2.5 INCHES LONG IN HORIZONTAL STABILIZER LT LOWER COMPOSITE SKIN. CRACK IS AT IB END OF LT HORIZONTAL STABILIZER, 5 INCHES AFT OF LEADING EDGE.Feb 12, 2008 · N138SL · Piagio P180 · Horizontal Stabilizer, Plate/SkinSDR PAI52008S4818Structure · chafedDURING D-CHECK INSPECTION, FOUND RUDDER TORQUE CHAFED BY AFT FAIRING P/N 80-561004-401.Jan 30, 2008 · N134SL · Piagio P180 · Rudder StructureSDR V2J2008F00001Control Panel · inoperativeON APPROACH, THE FLIGHT CREW GOT INDICATION VIA THE FIRE CONTROL PANEL OF A NR (1) ENGINE FIRE. THE CREW FOLLOWED THE CHECKLIST AND PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN. AFTER THE ENGINE SHUTDOWN THE FIRE WARNING LIGHT EXTINGUISHED AND THE AC LANDED WITJan 19, 2008 · N149SL · Piagio P180 · Fire DetectionSDR FAA2508001Wire · burnedCREW SMELLED WHAT THEY DESCRIBED AS ELECTRICAL BURNING OR ARCING. NO SMOKE OR FLAMES SEEN. THEY LANDED WITHOUT INCIDENT AND SECURED THE AIRCRAFT. WE WILL SEND A MAINTENANCE TEAM INTO INVESTIGAGE 1.20.08.Jan 18, 2008 · N156SL · Piagio P180 · Electrical Power System WiringSDR 16301Breather Tube · kinkedAT FL280, CREW CALLED INTO OPERATIONS CONTROL CENTER TO ADVISE OF AN UNKNOWN ODOR IN THE AIRCRAFT, AND SLIGHT VISIBLE SMOKE. THE CREW PULLED BACK ON THE THROTTLES AND THE SMOKE DISAPPATED. THEY THEN POWERED BACK UP AND THE SMOKE WENT AWAY. THE ODOR REMAINEJan 4, 2008 · N163SL · Piagio P180 · Engine (Turbine/Turboprop)SDR 2007FA0001096Mount · chafedOIL COOLER RETURN LINE CHAFED AGAINST ENGINE MOUNT. DID NOT SHOW SIGNS OF CHAFING STATICALLY DURING ROUTINE INSPECTIONS, WAS CHAFING DURING FLIGHT. INSTALLED REDESIGNED OIL LINE THAT CANNOT COME IN CONTACT WITH MOUNT. MFG DID NOT INFORM OPERATORS ABOUT REDESINov 21, 2007 · N180AV · Piagio P180 · Engine Mount SectionSDR 2008FA0000386Steering Sys · contaminatedSTEERING SYSTEM DISENGAGEMENT DURING TAXI. STEERING DRIFT DURING ENGAGEMENT. STEERING HART TO TURN (NO INPUT). STEERING RELIABILITY VERY LOW. STEERING CONTAMINATION DURING MFG BENCH TESTING. AIRCRAFT RUNWAY EXCURRSION DURING LANDING AND TAXI DUE TO STEERINGNov 1, 2007 · Piagio P180 · Landing Gear Steering SystemSDR PAI52007S4724Duct · crackedDURING 3000 HOUR D-CHECK FOUND 3 OF 4 WING OB LEADING EDGE PANELS WITH CRACKED HEATING DUCTS.Sep 26, 2007 · N145SL · Piagio P180 · Airfoil Anti/De-ice SystemSDR 2007FA0000730Antenna · separatedRADAR ALTIMETER REPORTED INOPERATIVE. FOUND ANTENNA SENSOR GONE FROM THE BASE, LEAVING .2500 INCH HOLE THROUGH THE COAX CONNECTION. THE FLAT ANTENNA MOUNTS TO A CURVED FUSELAGE WITHOUT CONTOUR ADAPTATION. (K)Aug 13, 2007 · N395KT · Piagio P180 · Ground Proximity SystemSDR 2007F00039Drain Pan · warpedDUE TO THE HEAT IN THIS AREA, THIS DRAIN PAN IS CRACKING AND WARPING, WHICH IN TURN IS CAUSING THE WATER FROM THE EVAPORATOR TO SPILL INTO THE BELLY OF THE AIRCRAFT. THE RESOLUTION HAS BEEN TO REWORK THE PAN, REFORMING THE PAN FROM ALUMINUM STOCK, USING ORIGINJul 24, 2007 · Piagio P180 · Cabin Cooling SystemSDR CA070914002Turbine Blades · fractured(CAN) THE ENGINE SHUTDOWN IN FLIGHT ON APPROACH. SUBSEQUENT INSPECTION REVEALED FRACTURED POWER TURBINE BLADES. MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070914002)Jul 13, 2007 · Piagio P180 · Turbine SectionSDR 2007FA0000612Actuator · failedON APPROACH PITCH TRIM ACTUATOR FAILED TO MOVE. AIRCRAFT LANDED WITH PARTIAL FLAPS WITHOUT FURTHER INCIDENT. ONE HOUR LATER TRIM ACTUATOR GROUND TESTED REVEALING NO DEFECTS. ACTUATOR SENT TO MFG FOR INVESTIGATION.Jul 11, 2007 · N5166P · Piagio P180 · Stabilizer Position IndicatingSDR CA070704011Oil System · overtemp(CAN) IN FLIGHT, THE ENGINE OIL TEMPERATURE WAS SEEN TO INCREASE AND THE ENGINE WAS SHUTDOWN. POST-FLIGHT INSPECTION REVEALED OIL LEAKAGE AT THE ENGINE (C) FLANGE. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070704011)May 14, 2007 · Piagio P180 · Turbine Engine Oil SystemSDR CA070514047Turbine Blades · fractured(CAN) DURING CLIMB, THE ENGINE EMITTED A NOISE AND ENGINE PARAMETERS WERE SEEN TO FLUCTUATE. THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED FRACTURED POWER TURBINE BLADES. (TC NR 20070514047)Apr 11, 2007 · Piagio P180 · Turbine SectionSDR CA061004005Actuator · failed(CAN) PILOTS REPORTED NOSE GEAR STEERING FAILURE. NOSE GEAR ACTUATOR REPLACED. SYSTEM TESTED AND AIRCRAFT RETURNED TO SERVICE (TC NR 20061004005)Sep 26, 2006 · Piagio P180 · Landing Gear Steering SystemSDR PAI5200642731Duct · crackedDURING 3000 HOUR D-CHECK FOUND ALL 4 WING LEADING EDGE PANELS WITH CRACKED HEATING DUCTS. WING LEADING EDGE ASSY P/N'S 80-232116-401, 80-232116-402, 232117-401, 232117-402.Sep 1, 2006 · N107SL · Piagio P180 · Airfoil Anti/De-ice SystemSDR PAI5200642401Line · chafedDURING 3000 HOUR D-CHECK FOUND OIL SCAVENGE LINE PN 3040124 AT SCAVENGE PUMP CHAFED APPROX 50 PERCENT THROUGH BY CONTACT WITH CRIMP TYPE CLAMP THAT SECURES HEAT SLEEVE ON OIL COOLER FLEX LINE. SAME CONDITION FOUND ON BOTH LT AND RT ENGINES. INSTALLED NEW SCAAug 25, 2006 · N153SL · Piagio P180 · Turbine Engine Oil SystemSDR 2006FA0000714Attach Fitting · crackedON POST MAINTENANCE WALKAROUND INSPECTION, FOUND RUDDER TRIM TAB LOWER CONTROL ROD ATTACH LUG RADIALLY CRACKED. UNKNOWN CAUSE, NO OTHER DAMAGE OR DEFECTS NOTED. (K)Jul 13, 2006 · N29JS · Piagio P180 · Rudder, Tab StructureSDR PAI5200641881Stop · brokenDURING D CHECK (3000 HOUR INSPECTION) FOUND RUDDER STOP LOCATED AT BOTTOM OF RUDDER BROKEN IN TWO. BREAK OCCURRED AT SCREW HOLES USED TO ATTACH WEAR STRIP TO RUDDER STOP. SMALL AREA OF METAL EXISTS AROUND THE SCREW HOLES, SUGGEST REDESIGN OF THIS PART.Jun 28, 2006 · N153SL · Piagio P180 · Rudder StructureSDR PAI52006S4188Tube · chafedDURING D-CHECK (3000 HOUR INSPECTION) FOUND WING LEADING EDGE ANTI-ICE PLUMBING CHAFFED 50 PERCENT OF WALL THICKNESS BY LEADING EDGE TEMP SENSOR BRACKET.Jun 22, 2006 · N153SL · Piagio P180 · Airfoil Anti/De-ice SystemSDR CA060704016Tube · fractured(CAN) THE ENGINE FLAMED OUT IN CRUISE. SUBSEQUENT INSPECTION REVEALLED A FRACTURED FUEL SYSTEM P3 AIR TUBE. (TC# 20060704016)Jun 21, 2006 · Piagio P180 · Engine Fuel DistributionSDR 2005FA0001588Turbine Wheel · damagedAIRCRAFT WAS CLIMBING FROM 26,000 TO 28,000 WHEN THE PILOT HEARD A LOUD BANG. THE LT ENGINE TEMPERATURE PEGED. THE PILOT IMMEDIATELY PULLED THE LT ENGINE TO FLIGHT IDLE. AFTER LANDING AND SHUTDOWN, VISUAL INSPECTION OF THE LT ENGINE SHOWED SEVERE DAMAGE TO Nov 30, 2005 · N137SL · Piagio P180 · Turbine SectionSDR CA051223003Engine · overtempDURING CLIMB, THE ENGINE EMITTED A LOUD NOISE ACCOMPANIED BY AN INDICATED ITT OVER-TEMPERATURE. THE PILOT SHUT THE ENGINE DOWN IN FLIGHT AND DIVERTED TO POINT OF ORIGIN. SUBSEQUENT INSPECTION REVEALED FRACTURED POWER TURBINE BLADES. PWC WILL INVESTIGATE THENov 29, 2005 · Piagio P180 · Engine (Turbine/Turboprop)SDR CA051117008Wheel · crackedRT WHEEL ASSY WAS FOUND U/S AFTER INSPECTION. FOUND THAT THE INNER WHEEL WAS CRACKED AND THE WHEEL ASSY WAS REPLACED WITH A SERVICEABLE UNIT.Nov 15, 2005 · Piagio P180 · Wheel/Ski/FloatSDR V2J2005F00003Actuator · failedSYSTEM FAILED IN PRIMARY, SECONDARY SYSTEM OPERATION NORMAL TROUBELSHOT SYSTEM IAW THE MM, FOUND PROBLEM TO BE AN INTERNAL FAULT WITH THE ACTURATOR ASSEMBLY. INSTALLED AN O/H UNIT SAME PN, SN-70. SECURITY AND FUNCTION CHECKS PERFORMED WITH NO FAULTS FOUND. Sep 19, 2005 · N305SL · Piagio P180 · Rudder Tab Control SystemSDR V2J2005F00002Potentiometer · failedSTEERING SYSTEM FAILED TO STAY ENGAGED DURING TAXI. SYSTEM WAS ABLE TO RESET BUT FAILED SEVERAL SECONDS LATER. REPEATED ATTEMPTS TO RESET THE SYSTEM HAD NO POSITIVE EFFECT. REPLACEMENT OF UNIT WAS ACCOMPLISHED IAW THE AIRFRAME AND COMPONENT MFG MM. (K)Sep 19, 2005 · N109SL · Piagio P180 · Landing Gear Steering SystemSDR CA050829002Wire · burned(CAN) CO-PILOTS WINDSHIELD, NR 4 AREA, FAILED ON LOW SELECTION. HIGH HEAT WAS SELECTED AND ELECTRICAL BURNED SMELL WAS DETECTED. SYSTEM WAS SHUTOFF AND TRIP CONTINUED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING FOUND THE PROBLEM TO BE RELAY K61 WHEN IT WAAug 25, 2005 · Piagio P180 · Window System Wiring
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