Cessna 414A

Service difficulty reports · 339

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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 = '414A'
  ORDER BY difficulty_date DESC"

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SDR 2009FA0000733Cylinder Head · crackedCYLINDER HEAD FOUND CRACKED FROM INJECTOR BOSS TO THE UPPER PLUG HOLE. AFTER INSPECTION OF ALL CYLINDERS ON BOTH ENGINES 5 OTHER OF THE ORIGINAL CYLINDERS INSTALLED AT O/H WERE FOUND CRACKED. ALL CRACKS WERE EITHER FROM THE INJECTOR BOSS TO THE UPPER PLUG HOJun 5, 2009 · N441TP · Cessna 414A · Reciprocating Engine Cylinder SectionSDR 2009FA0000732Cylinder Head · crackedCYLINDER HEAD FAILED IN FLIGHT AND BLEW OUT A SECTION OF THE HEAD AND FINS. INVESTIGATION REVEALED A .5 INCH HOLE DEVELOPED FROM A CRACK THAT PROGRESSED FROM THE EXHAUST VALVE SEAT TO UPPER SPARK PLUG HOLE. ADDITIONAL CRACK WAS FOUND ON THIS CYLINDER FROM THJun 5, 2009 · N441TP · Cessna 414A · Reciprocating Engine Cylinder SectionSDR 2009FA0000248Mount · debondedDURING NR 1 ENGINE REMOVAL FROM ACFT, FOUND NR 1 ENGINE ISOLATOR MOUNT ALIGNMENT PUCK DEBONDED AND SEPARATED FROM THE MAIN BODY OF THE ISOLATOR. (K)Mar 19, 2009 · N79PP · Cessna 414A · Engine Mount SectionSDR 2009FA0000016Pan · crackedOIL LEAK CAME FROM CRACK IN OIL PAN. CAUSE UNKNOWN. ENG TSMOH 95 HRS. CRACK/ FITTING WITH HOSE ATTACHED FOR REMOTE OIL DRAIN. (K)Dec 17, 2008 · N414PS · Cessna 414A · Reciprocating Engine Oil SystemSDR CA081205007Line · corroded(CAN) UPON REACHING CRUISE FLIGHT AND ACTIVATING AIRFRAME PNEUMATIC DE-ICE SYSTEM, THE BOOTS WOULD REMAIN PARTIALLY TO MOSTLY INFLATED. THIS PROBLEM WOULD NOT DUPLICATE ON A GROUND RUN. THE VACUUM LINE TO THE FLOW VALVES WAS INSPECTED AND A LINE ASSEMBLY TODec 4, 2008 · Cessna 414A · Vacuum Distribution SystemSDR 2008FA0000859Support · crackedON THE FWD TRUNNION SUPPORT, A CRACK WAS LOCATED ON THE LT AND RT SIDES. EDDY CURRENT INSP USED. (K)Nov 13, 2008 · N901BA · Cessna 414A · Main Landing Gear Attach SectionSDR 2008FA0000690Cylinder · crackedUPON INSPECTION FOUND THAT NR 1 AND NR 5 CYLINDERS WERE CRACKED AND LEAKING FUEL ORIGINATING JUST INBOARD OF THE FUEL NOZZLE BETWEEN THE 16TH AND 18TH COOLING FINS. CYLINDERS WERE NEW WHEN INSTALLED AT ENGINE OVERHAUL.Oct 17, 2008 · N414AN · Cessna 414A · Reciprocating Engine Cylinder SectionSDR 2008FA0000624Bushing · crackedDURING CYLINDER NR 2 REMOVAL TO CORRECT CRACKED CYLINDER, FOUND CONNECTING ROD PISTON P/N BUSHING CRACKED WITH LARGE PIECE MISSING FROM EDGE. FAILURE IS AS NOTED IN MFG SB071. REMOVED ALL 6 CYLINDERS FROM ENGINE AND FOUND 4 MORE BUSHINGS CRACKED IN SAME LOCATSep 5, 2008 · N414NC · Cessna 414A · Reciprocating Engine Power SectionSDR N416RAValve Spring · brokenENGINE VIBRATION PROMPTED INFLIGHT SHUTDOWN OF ENGINE.Jan 14, 2008 · N416RA · Cessna 414A · Reciprocating Engine Cylinder SectionSDR R6QA245DCDuct · damagedAFT HEATER DUCTS ARE FOAMED LINED. THE DUCTS START TO BREAK DOWN AND THE FOAM CAUSED SMOKE IN THE COCKPIT. ACFT AND LOGS ARE NO LONGER AT THIS FACILITY. TIMES AND PN ARE ESTIMATIONS. NO OTHER INFORMATION IS AVAILABLE FROM THIS LOCATION. THIS SDR IS BEING GENENov 9, 2007 · N245DC · Cessna 414A · Heating SystemSDR 2007FA0000996Tube · brokenDURING FLAP EXTENSION THE RT SIDE FLAPS RETRACTED SUDDENLY LEAVING THE LT FLAPS DOWN. FOUND THE PUSHROD TUBE CONNECTING THE IB AND MIDDLE FLAP BELLCRANK TO HAVE FAILED AT THE OB END OF THE TUBE. THE TUBE APPEARS TO HAVE BEEN ABOUT 60 PERCENT CRACKED THROUGH Nov 7, 2007 · Cessna 414A · Trailing Edge FlapsSDR 0001Cylinder · crackedPILOT WAS INFORMED BY LINE PERSONNEL DURING TAXI TO TIE DOWN, THAT ENGINE WAS MAKING A LOUD (AIR PULSING) SOUND. PILOT COULD ONLY HEAR THE SOUND AFTER REMOVING NOISE CANCELLING HEAD SET. PILOT THEN SHUTDOWN ENGINE. INSPECTION REVEALED THE NR 4 CYLINDER TO BE CSep 25, 2007 · N919FA · Cessna 414A · Reciprocating Engine Cylinder SectionSDR 4757Cylinder · crackedPILOT WAS INFORMED BY LINE PERSONNEL DURING TAXI TO TIE DOWN, THAT ENGINE WAS MAKING A LOUD (AIR PULSING) SOUND. PILOT COULD ONLY HEAR THE SOUND AFTER REMOVING NOISE CANCELLING HEAD SET. PILOT THEN SHUTDOWN ENGINE. INSPECTION REVEALED THE NR 4 CYLINDER TO BE CSep 25, 2007 · N919FA · Cessna 414A · Reciprocating Engine Cylinder SectionSDR 2007FA0000648Display · malfunctionedSETTING AN EVENT IN THE AUX PAGE FOR A FUTURE TIME CAUSES AUX EVENTS PAGE TO NO LONGER FUNCTION. SELECTING THIS PAGE CAUSES THE NAV6, GPS SATELLITE STATUS PAGE TO DISPLAY FOR 1 SECOND, THEN NAV2 PAGE(MAP) TO BE SELECTED. AS A SIDE EFFECT, THE FLIGHT TIMER ISJul 20, 2007 · Cessna 414A · Global Positioning SystemSDR EAVA200701117Engine · vibrationAT CRUISE ENGINE DEVELOPED VIBRATION. REQUESTED DESCENT AND TURN TO NEAREST SUITABLE FIELD. REDUCED ENGINE POWER TO IDLE ON DOWNWIND, FELT A JOLT AND SAW RIGHT ENGINE ACCESS PANEL PUSH OUT. FEATHERED AND SECURED RIGHT ENGINE AND LANDED.May 3, 2007 · N416RA · Cessna 414A · Engine (Reciprocating)SDR 2007FA0000388Actuator · corrodedLT LANDING GEAR ACTUATOR FAILED WHILE TAXING. COLLAPSED LT WING. DAMAGED LT PROP AND WING TIP. ACTUATOR INSPECTED AND FOUND WATER INSIDE. ACTUATOR OVERHAULED AND REINSTALLED NOSE AND RT LG ACTUATOR REMOVED FOR INSPECTION AND CHECKED GOOD. (K)Apr 13, 2007 · N6672C · Cessna 414A · Landing Gear ActuatorSDR FMOR20070001Uplock Hook · crackedPILOT REPORTED THAT THE LANDING GEAR CAME UNHOOKED FROM THE UP POSITION IN FLIGHT. THE GEAR WAS EXTENDED AND THE AIRCRAFT LANDED. THE AIRCRAFT WAS JACKED AND THE GEAR CYCLED TO THE UP POSITION. WHEN ALL (3) UPLOCK SWITCHES WERE MADE THE RT MAIN GEAR FELL FRApr 9, 2007 · N6161Z · Cessna 414A · Landing Gear Retraction/Extension SystemSDR FMOR477KUplock Hook · distortedPILOT REPORTED THAT THE LANDING GEAR CAME UNHOOKED FROM THE UP POSITION IN FLIGHT. THE GEAR WAS EXTENDED AND THE AIRCRAFT LANDED. THE AIRCRAFT WAS JACKED AND THE GEAR CYCLED TO THE UP POSITION. WHEN ALL (3) UPLOCK SWITCHES WERE MADE THE RT MAIN GEAR FELL FRApr 9, 2007 · N6161Z · Cessna 414A · Landing Gear Retraction/Extension SystemSDR 2007FA0000295Bearing · wornFAILURE OF RT TURBOCHARGER SEAL AND CENTER BEARING CAUSED SMOKE OUT OF EXHAUST AND SQUEALING NOISE RESULTING IN THE FLIGHT CREW TO FEATHER PROPELLER AND SHUTDOWN THE ENGINE. CAUSE OF FAILURE DO TO WEAR. (K)Mar 20, 2007 · N3247M · Cessna 414A · Exhaust TurbochargerSDR AKCA001Washer · shearedON LANDING AIRCRAFT VEERED TO THE RT, INSPECTION SHOWED WASHER PN 5045018-1 HAD SHEARED ALLOWING BOTTOM TORQUE LINK AND WHEEL ASSY TO TURN 180 DEGREES ROTATION. ADDITIONAL ROTATION WAS STOPPED WHEN BRAKE ASSY CONTACTED UPPER TORQUE LINK. CONSIDERING TORQUE LMar 7, 2007 · N414AN · Cessna 414A · Main Landing GearSDR PAI52007S4448Stud · brokenDURING ANNUAL INSPECTION FOUND 5 BROKEN HOLD DOWN STUDS ON NR 4 CYLINDER. ENGINE WAS MODIFIED IAW RAM STC SE3630SW AND SE3631SW AT PREVIOUS OVERHAUL.Jan 30, 2007 · N414CJ · Cessna 414A · Reciprocating Engine Power SectionSDR FCPR20070002Pressure Switch · intermittentAIRCRAFT COMBUSTION HEATER WORKS ON THE GROUND BUT NOT IN FLIGHT. TROUBLESHOOTING FOUND PRESSURE SWITCH INTERMITTENT. MANUFACTURE DATE 08/05.Dec 29, 2006 · N919FA · Cessna 414A · Heating SystemSDR 2006FA0000385Cylinder Head · separatedDURING FLIGHT, VIBRATION WAS NOTED ON RT ENGINE. INSPECTED ENGINE AND FOUND NR 6 CYLINDER SEPARATED WHERE BARREL MEETS HEAD. PROBABLE CAUSE: UNKNOWN. RECOMMENDATIONS: THIS IS AN ECI CYLINDER. REFERENCE NEEDS TO BE MADE TO THEM TO RESOLVE THE PROBLEM. (K)Mar 31, 2006 · N414AM · Cessna 414A · Reciprocating Engine Cylinder SectionSDR 2006FA0000007Boot · failedBOOT PN P6592SW DEPARTED PROPELLER BLADE IN FLIGHT. CUSTOMER LANDED, REMOVED OTHER BOOTS AND CONTINUED TRIP TO HOME STATION. BOOTS HAVE 393.6 HOURS SINCE INSTALLATION. AD NOTE 2005-18-20 INSPECTION WAS ACCOMPLISHED WITH NO DEFECTS NOTED. (K)Dec 12, 2005 · N414SH · Cessna 414A · Propeller/Rotor Anti-Ice/De-Ice SystemSDR 2005FA0001603Bolt · brokenWHILE CHECKING RT ENGINE OVER FOR OIL LEAKS, FOUND NUT AND PART OF BOLT FROM TOP FORWARD NR 2 CYLINDER THRU BOLT LODGE BY OIL FILLER TUBE. BREAK ON BOLT APPEARS TO BE OLD BY THE DARK COLOR. REMOVAL OF CYLINDER NECESSARY TO REPLACE BOLT. (K)Nov 23, 2005 · N4837A · Cessna 414A · Reciprocating Engine Cylinder SectionSDR AU510001704Elbow · wornRT ENGINE AIR INDUCTION HOSE FLEXIBLE ELBOW TORN ON INSIDE RADIUS.Oct 1, 2005 · Cessna 414A · Engine Air Intake SystemSDR 2005FA0001357Motor · malfunctionedRT AIR CONDITIONER BLOWER MOTOR LOCATED UNDER CO-PILOTS SEAT MALFUNCTIONED AND PRODUCED SMOKE WHICH WAS DRAWN THROUGH THE RT SIDE VENTILATION DUCTS. PILOT FOLLOWED EMERGENCY PROCEDURES AND LANDED SAFELY. (EA09200505819) (K)Sep 23, 2005 · N414AK · Cessna 414A · Cabin Cooling SystemSDR AHD2005F00000Blower Motor · smokeAFTER A FLIGHT SEPT 22, 2005, ABOUT 1905 HRS, SMOKE WAS NOTED IN THE COCKPIT WHILE TAXING TO THE RAMP. FIRETRUCKS WERE REQUESTED BY THE PILOTS, THE AC WAS SHUTDOWN ON THE TAXI WAY AND PASSENGERS AND CREW WERE OFF-LOADED. THE FIRE CREW FOUND NO SIGNS OF HEAT Sep 22, 2005 · N414AK · Cessna 414A · Air Distribution SystemSDR IMD2005F00000Oil Filter · leakingPILOT REPORTED FINDING AN OIL LEAK ON RT ENGINE DURING PREFLIGHT. ENGINE WASHED AND RUN, OIL FILTER FOUND CRACKED AND LEAKING AT THE WRENCH LUG FLANGE ON TOP OF THE FILTER. FILTER APPEARED TO BE OVERTORQUED UPON REMOVAL. FILTER RETAINED FOR WARRANTY AND QUAAug 29, 2005 · N245DC · Cessna 414A · Reciprocating Engine Oil SystemSDR 2005F00095Circuit Breaker · burnedFLIGHT WAS TERMINATED WHEN THE AVIONICS MASTER CIRCUIT BREAKER/SWITCH OVERHEATED AND FAILED IN THE (ON) POSITION. MECHANICALLY, THE SWITCH COULD BE MOVED TO THE (OFF) POSITION, BUT ELECTRICALLY WOULD REMAIN (ON). DUE TO ELECTRICAL ODOR AND FAILURE OF THE SWIAug 10, 2005 · N36934 · Cessna 414A · Electrical Power System WiringSDR 2006FA0000520Cylinder · cracked418.6 HRS SINCE COMPLIANCE W19TH AD2004-08-10 ON ECI CYLINDERS. LT ENG NR2 AND RT ENG NR 4 CYLINDERS FOUND CRACKED THROUGH FROM UPPER PLUG HOLE TO EXHAUST VALVE. BOTH CYLINDERS HAVE IDENTICAL CRACKS ON RELATIVELY NEW HEADS. (K)Jul 16, 2005 · N6822U · Cessna 414A · Reciprocating Engine Cylinder SectionSDR U8DA011105Shuttle Valve · stuckNOSE LANDING GEAR DID NOT SHOW DOWN AND LOCKED. GEAR LAMP WOULD INTERMITTENTLY LIGHT AND HYDRAULIC PRESSURE LIT WOULD INTERMITTNETLY ILLUMINATE. DISASSEMBLY AND T/S SHOWED SHUTTLE VALVE STUCK. CLEANED, REASSEMBLED AND TESTED. N2 BOTTLE REMOVE, CLEANED, INSJun 11, 2005 · N415ST · Cessna 414A · Landing Gear Retraction/Extension SystemSDR 2005FA0000568Cylinder Head · separatedTHE NR 6 CYLINDER, LT ENGINE. THE AC WAS RUNNING FINE AND ALL OF THE SUDDEN A VIBRATION WAS FELT. INVESTIGATION: THE HEAD WAS FOUND SEPARATED FROM CYLINDER. THE HEAD WAS BEING HELD ON BY THE INTAKE PIPE AND EXHAUST. THE ENGINE AND THIS CYLINDER HAD 72.4 TApr 1, 2005 · N901BA · Cessna 414A · Reciprocating Engine Cylinder SectionSDR 2005F00039Door Frame · crackedLOWER DOOR FRAME CRACKING BY THE REAR HINGE.Mar 8, 2005 · N4057C · Cessna 414A · Fuselage Main, StructureSDR 2005FA0000354Magneto · failedLT MAGNETO, PN 6320, SN 02091734 FAILED AFTER 54 HOURS TT IN SERVICE. INVESTIGARTION FOUND BROKEN CONTACT ASSY. VISUAL INSPECTION OF BOTH LT AND RT CONTACT ASSY IF SN IS WITHIN 100 HOUR OF FAILED PART. NOTE; RT MAGNETO SAME ENGINE, PN 6320, SN 02091744 FAIFeb 24, 2005 · N468TW · Cessna 414A · Magneto/DistributorSDR 2005FA0000353Magneto · failedRT MAGNETO, PN 6320, SN 02091774 FAILED AFTER 58.0 HOURS TOTAL TIME IN SERVICE. INVESTIAGATION FOUND BROKEN CONTACT ASSY. VISUAL INSPECTION OF BOTH RT AND LT CONTACT ASSY IF SN IS WITHIN 100 OF FAILED PART. NOTE: LT MAGNETO SAME ENGINE PN 6320, SN 02091734 Feb 24, 2005 · N468TW · Cessna 414A · Magneto/DistributorSDR 2004F00391Wheel · separatedON TAKEOFF, LT OB HALF OF WHEEL, TIRE AND TUBE SEPARATED FROM AC. THE IB HALF OF WHEEL STAYED ON THE AXLE AS WELL AS THE AXLE NUT, BEARING CONE AND INNER RACE FOR OUTER HALF. DUE TO HIGH SPEED AT THE TIME OF INCIDENT THE TIRE AND TUBE HAVE NOT BEEN LOCATED. Aug 26, 2004 · N678JS · Cessna 414A · Wheel/Ski/FloatSDR H48A2004002Pushrod · failedAILERON TRIM PUSH ROD ASSY (PN 51155464) FAILED, CAUSING THE AILERON TRIM TAB TO BIND IN THE UP POSITION. AIRCRAFT LANDED AT AN AUXILIARY AIRFIELD WITHOUT INCIDENT. PUSH ROD REPLACED WITH NEW MFG PUSH ROD ASSY (PN 51155464). OLD PUSH ROD, ROD END BEARING FAAug 24, 2004 · N5614C · Cessna 414A · Aileron Tab Control SystemSDR 2005FA0000166Crankshaft · crackedCRANKSHAFT CRACKEDJul 12, 2004 · N36934 · Cessna 414A · Reciprocating Engine Power SectionSDR HFB2004F00001Line · corrodedLT ENGINE LOST OIL PRESSURE. OIL PRESSURE LINE IN LT SIDE PANEL BY PILOTS LT LEG HAD CORROSION HOLE IN IT. APPROXIMATELY 5 WEEKS LATER LT ENGINE LOST OIL PRESSURE AGAIN. OIL PRESSURE LINE UNDER FLOOR UNDER PILOTS SEAT HAD CORROSION HOLE IN IT.Jul 9, 2004 · N812SR · Cessna 414A · Turbine Engine Oil SystemSDR HFB2004F00000Line · corrodedLT ENGINE LOST OIL PRESSURE. OIL PRESSURE LINE IN LT SIDE PANEL BY PILOT`S LT LEG HAD CORROSION HOLE IN IT. APPROXIMATELY 5 WEEKS LATER LT ENGINE LOST OIL PRESSURE AGAIN. OIL PRESSURE LINE UNDER FLOOR UNDER PILOTS SEAT HAD CORROSION HOLE IN IT.Jul 9, 2004 · N812SR · Cessna 414A · Turbine Engine Oil SystemSDR BHA05RSCylinder Head · separatedDURING POWER REDUCTION FROM TAKE-OFF POWER TO CLIMB POWER, A (POP) WAS HEARD AND ONE OF THE ENGINES BEGAN RUNNING ROUGH. THERE WAS NO INSTRUMENT/GAGE INDICATION AS TO WHICH ENGINE. AIRCRAFT LANDED WITH OUT INCIDENT. POST FLIGHT EXAMINATION FOUND NR 1 ENGINE, NApr 23, 2004 · N414PG · Cessna 414A · Reciprocating Engine Cylinder SectionSDR 40590Bearing · corrodedDURING ANNUAL INSPECTION FOUND THE ELEVATOR TRIM TAB HORN BEARING FROZEN. WHEN HORN WAS REMOVED TO REPLACE THE BEARING THE 2 ATTACHMENT SCREWS IN THE FORWARD HOLES OF THE BEARING WERE FOUND SEVERELY CORRODED. MORE THAN 50 PERCENT OF THE ORRIGINAL DIAMETER WAApr 20, 2004 · N6815T · Cessna 414A · Elevator Tab Control SystemSDR BHA04RSAttach Fitting · corrodedIN COMPLYING WITH SUPPLEMENTAL INSPECTION 57-10-20, FOUND THE RT WING LOWER SPAR ATTACH FITTING HAD SIGNIFICANT CORROSION IN SOME OF THE FITTING MOUNTING HOLES. THE FITTING WAS REPLACED. NO FURTHERDEFECTS WERE NOTED.Apr 8, 2004 · N414PG · Cessna 414A · Fuselage, Wing Attach FittingsSDR CLS2004F00000Hose · leakingDURING 100 HOUR, INSPECTION FOUND LT MAIN LANDING GEAR HYDRAULIC ACTUATOR HOSE LEAKING HOSE WAS HARD AND NOT FLEXIBLE HOSE TAG SHOWS MFG DATE 3Q77 AND APPEARS TO BE ORIGNAL HOSE INSTALLED. AC MFG DATE 1978 WITH 7221.9 HOURS TT. RECOMMEND TO REPLACE FLEX HOSEMar 26, 2004 · N678JS · Cessna 414A · Hydraulic System, MainSDR CSL2004F00000Thru Bolt · brokenDURING 100 HOUR INSPECTION, FOUND CRANKCASE THRU BOLT BROKEN AT LOWER FORWARD NR 2 CYLINDER.Mar 26, 2004 · N678JS · Cessna 414A · Reciprocating Engine Power SectionSDR AIHR109CCylinder · crackedPILOT REPORTED VIBRATION AFTER 2 HRS INTO FLIGHT, COULD NOT DETERMINE ORIGIN OF VIBRATION. ANOTHER PILOT PERFORMED GROUND RUN-UP AND COULD NOT DETECT VIBRATION. PILOT FLEW AIRCRAFT AND AFTER 15 MINUTES A VIBRATION OCCURRED, PILOT NARROWED VIBRATION ORIGIN TOJan 9, 2004 · N468TW · Cessna 414A · Reciprocating Engine Cylinder SectionSDR J4P2004F00001Fuel Tank · corrodedDURING ANNUAL INSPECTION, IT WAS DISCOVERED TO HAVE SURFACE CORROSION AT THE LT AND RT WING UNDERNEATH COMING FROM THE FUEL TANK AREA. LOCATION WAS IMMEDIATELY AFT OF THE FWD SPAR. THE PATCH IS LOCATED AT WS 119.29 AND ENDS AT WS 133.29 AND EXTENDS FROM THEOct 9, 2003 · N4837A · Cessna 414A · Fuel StorageSDR S9K2003F00000Skin · debondedDURING A ROUTINE PHASE INSPECTION ON A CESSNA 414A WITH RAM WINGLETS, INSTALLED UNDER STC NR SA4943SW A 6 INCH CRACK WAS DISCOVERED IN THE BOND LINE WHERE THE BOTTOM WINGLET SKIN IS BONDED TO THE BOTTOM OF THE WINGLET MAIN SPAR, ON THE FORWARD AND AFT SIDE. AOct 7, 2003 · N414CS · Cessna 414A · Fuselage Main, Plate/SkinSDR 2003FA0000914Brace · crackedCRACK LIKE INDICATION WHICH EXCEEDS 0.020 INCH IAW MEB 91.11 REV 1 (02/24/03) CRACK LIKE INDICATION DETECT BY EDDY CURRENT INSPECTION.Aug 25, 2003 · N6631C · Cessna 414A · Fuselage Miscellaneous Structure
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