Cessna 510

Service difficulty reports · 88

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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 = '510'
  ORDER BY difficulty_date DESC"

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SDR CA120814003Fuel Tank · fod(CAN) DURING SCHEDULED INSPECTION OF THE INTERNAL FUEL TANK A 24" BY 29" CLOTH RAG WAS DISCOVERED IN THE FUEL BAY COVERED BY ACCESS PANEL 147EB. THIS WAS THE FIRST TIME ACCESSING THIS AREA SINCE THE ACFT WAS BUILT IN 2009. ON A PREVIOUS FLIGHT A LOW FUEL PREAug 10, 2012 · Cessna 510 · Fuel StorageSDR CA120716003Oil System · low pressure(CAN) 20 MINUTES INTO THE FLIGHT, NOISE HEARD FROM THE LT ENGINE AND MASTER WARNING WITH LOW OIL PRESSURE AND ITT EXCEEDING LIMITS OCCURRED. THE CREW REDUCED POWER TO IDLE, N1 AT 15 PERCENT, AND SHUTDOWN THE ENGINE AFTER 2 MINUTES. A SINGLE ENGINE LANDING WAJul 2, 2012 · Cessna 510 · Engine Oil Indicating SystemSDR CNQR2012052286445Gearbox · crackedA CRACK WAS DISCOVERED IN THE ENGINE ACCESSORY GEARBOX NEAR THE STARTER/GENERATOR MOUNTING FLANGE. DURING THE AIRCRAFT`S LAST FLIGHT IT EXPERIENCED A GENERATOR BEARING FAILURE. DURING THE POST RUNS, AFTER PART REPLACEMENT AN OIL LEAK WAS DISCOVERED COMING FROMay 22, 2012 · N1EL · Cessna 510 · Accessory GearboxesSDR A8JA201204100013Transmitter · failedWHILE PERFORMING A CHECK FLIGHT AFTER MX, PILOT AND MECHANIC NOTICED AN ERRATIC OIL PRESSURE INDICATION ON THE NR 2 ENGINE. OIL PRESSURE WOULD GO FROM ZERO TO NORMAL, WITH RAPID FLUCTUATIONS. NO OTHER ENGINE PARAMETERS WERE AFFECTED. PILOT ELECTED TO RETURNApr 10, 2012 · N510GJ · Cessna 510 · Engine Oil Indicating SystemSDR A8JA201204060012Connector · damagedACFT DEPARTED, IN CRUISE AT FL360, CREW NOTICED "OIL PRESS LO L" CAS MESSAGE ON THE CENTER MFD. THE CREW REFERRED TO THE ACFT CHECKLIST, WHICH INSTRUCTED THE CREW TO PERFORM A PRECAUTIONARY SHUTDOWN TO AVOID DAMAGE TO THE ENGINE. THE CREW PERFORMED THE RECOApr 6, 2012 · N510CJ · Cessna 510 · Engine Oil System WiringSDR CA120409001Bearing · failed(CAN) IN LEVEL FLIGHT AT FL 360. LEFT ENGINE BEGAN MAKING POPPING SOUNDS ACCOMPANIED BY METALLIC CLUNKING/GRINDING NOISES. POWER LOSS AND NOTICEABLE ODOR AND MINOR VISIBLE SMOKE WAS NOTED, ALONG WITH IMMEDIATE MASTER WARNING ANNUNCIATOR LT. LT ENGINE INTERNApr 5, 2012 · Cessna 510 · Turbine SectionSDR CA120411003Engine · making metal(CAN) WHILE CRUISING AT 36,000 FT, THE PILOT HEARD A LOUD NOISE FROM THE LT ENGINE. SHORTLY AFTER, ITT WAS INCREASING AND THE ENGINE WAS LOSING POWER. THE PILOT ELECTED TO SHUTDOWN THE ENGINE AND MADE AN UNEVENTFUL SINGLE ENGINE LANDING. POST-FLIGHT INSPECTIApr 4, 2012 · Cessna 510 · Engine (Turbine/Turboprop)SDR 2012FA0000139Pin · misinstalledDURING MLG GVI INSPECTION, MX FOUND NR 4 PIN, AND NR 6 WASHER, WERE NOT INSTALLED THROUGH AFT NR 3 LINK, UNDER NR 2 SPRING, IN LT UP-LOCK ASSEMBLY. LINK WAS LOOSE IN THE ASSY AND ALL UP-LOCK MOVEMENT WAS PROVIDED THROUGH THE FWD LINK. THE FWD LINK WAS BENT DUFeb 27, 2012 · N610PT · Cessna 510 · Main Landing GearSDR CA120228011Transducer · failed(CAN) RIGHT ENGINE OIL PRESSURE INDICATION WENT TO PSI 12 MINUTES INTO FLIGHT. ENGINE WAS SHUTDOWN AND ACFT LANDED WITHOUT INCIDENT. OIL PRESSURE TRANSDUCER WAS PRESSURE TESTED TO 80 PSI AND TRANSDUCER SUBJECTED TO VIBRATION. WIRING WAS CHECKED. ALL INDICATFeb 24, 2012 · Cessna 510 · Engine Oil Indicating SystemSDR CA120213015Oil System · high pressure(CAN) THE PILOT SAW INCREASING OIL PRESSURE ON ONE ENGINE. THE PRESSURE WENT INTO THE AMBER AND THEN INTO THE RED. THE THROTTLE WAS PULLED BACK TO IDLE AND THE OIL PRESSURE WENT INTO THE GREEN. THE OIL PRESSURE DROPPED AGAIN INTO THE AMBER AND THEN RED. THFeb 8, 2012 · Cessna 510 · Engine Oil Indicating SystemSDR CA110810002Transmitter · faultyIFSD, CLIMBING THROUGH 14,000 FT THE PILOT NOTED THE RT ENGINE OIL PRESSURE DROPPING LOWER INTO THE AMBER, THEN RED ZONE. THE LOW OIL PRESS R CAS MESSAGE CAME ON AND PILOT SHUT DOWN THE ENGINE AND LANDED SAFELY. THE OIL PRESSURE TRANSMITTER WAS BENCH CHECKED AAug 4, 2011 · Cessna 510 · Engine Oil PressureSDR T192011F00000Uplock Switch · failedSWITCH FAILED IN THE OPEN POSITION CAUSING THE LANDING GEAR " UNLOCKED" INDICATION TO REMAIN ILLUMINATED AFTER LANDING GEAR EXTENSION. SWITCH WAS REPLACED TO CORROECT THE PROBLEM.Jun 6, 2011 · N136MC · Cessna 510 · Landing Gear Position and WarningSDR CA110602008Controller · failedTHE CREW REPORTED THAT AFTER TAKEOFF AND DURING CLIMB THAT THE ACFT WOULD NOT PRESSURIZE. THE ACFT RETURNED TO BASE WHERE MX INVESTIGATED THE PROBLEM. IT WAS FOUND THAT THE PRESSURIZATION CONTROLLER HAD FAILED. THE PART WAS CHANGED WITH A SERVICEABLE REPAIRMay 31, 2011 · Cessna 510 · Cabin Pressure ControllerSDR CA110616007Manifold · leaking(CAN) THE ENGINE EXHIBITED A LOSS OF PERFORMANCE MARGIN AND A BORESCOPE INSPECTION OF THE HOT SECTION WAS CARRIED OUT. THE INTERNAL FUEL MANIFOLD WAS DETERMINED TO BE LEAKING WITH ASSOCIATED DAMAGE, BURNING, OF THE MANIFOLD OUTER SHIELD AND THE COMBUSTION LINMay 25, 2011 · Cessna 510 · Engine Fuel DistributionSDR A8JA20110504001Connector · dirtyACFT DEPARTED. WHILE CLIMBING THROUGH, CREW NOTED AN AMBER CAS MESSAGE OF "RT FUEL BOOST". THIS INDICATES A LOW FUEL PRESSURE DETECTION AND ALERTS THE CREW THAT THE BOOST PUMP WAS AUTOMATICALLY ACTIVATED. THE CREW PERFORMED THE ACTIONS FROM THE EMERGENCY CHMay 4, 2011 · N510CJ · Cessna 510 · Fuel System WiringSDR CA110316007Bolt · defective(CAN) DURING MA INSPECTION FOUND PILOT & COPILOT BRAKE ROD LINK BOLT CHAFING COCKPIT FLOORBOARD MFG ADMITTED TO A PN CHANGE DURING PRODUCTION TO SPEED UP INSTALLATION. RECEIVED AUTHORIZATION TO USE THE ORIGINAL PN VIA EMAIL. NO MENTION WAS MADE OF ANY KIND OMar 16, 2011 · Cessna 510 · Landing Gear Brake SystemSDR CA110214006Engine · smokeSMOKE IN COCKPIT THE CREW EXPERIENCED SMOKE IN THE COCKPIT AND AN OIL BURNING ODOR AFTER TAKEOFF. THEY SELECTED THE RT SIDE ENGINE AS THE ONLY BLEED SOURCE AND THE SMOKE WENT AWAY. FLIGHT DIVERTED TO SERVICE CTR. TROUBLESHOOTING ONGOING WITH MFG ASSISTANCE.Feb 5, 2011 · Cessna 510 · Engine (Turbine/Turboprop)SDR FCPR201000234ASwitch · stuckLT MLG SWITCH PN 65-430087 STUCK AND CAUSED UNLOCK (RED) INDICATION WITH GEAR DOWN AND LOCKED AND 3 GREEN INDICATION. CHANGING THIS SWITCH CORRECTED THE INDICATION PROBLEM,.Nov 9, 2010 · N136M · Cessna 510 · Landing Gear Position and WarningSDR CA110202002Oil System · low pressure(CAN) IFSD DURING A REPOSITIONING FLIGHT, THE PILOT OBSERVED LH ENGINE OIL PRESSURE DROP INTO THE YELLOW BAND. PILOT REDUCED POWER AND IT CONTINUED INTO THE RED. THE PILOT SHUTDOWN ENGINE AND LANDEDWITHOUT INCIDENT. TROUBLESHOOTING IS ONGOING.Oct 29, 2010 · Cessna 510 · Engine Oil Indicating SystemSDR CA101014004Control Horn · looseON INSP LT AND RT ELEVATOR CONTROL HORNS WERE FOUND TO BE LOOSE ON THE ELEVATOR TORQUE TUBE. THE INSTALLED HARDWARE WAS CHECKED AGAINST THE IPC AND THE BUILDUP WAS CORRECT. IT WAS FOUND THAT THE NUTS HAD BOTTOMED ON THE BOLTS BEFORE TIGHTENING. A SECOND THIOct 13, 2010 · Cessna 510 · Elevator StructureSDR CA101006002Warning System · activated(CAN) ABORTED TAKEOFF DURING TAKEOFF ROLL, THE PILOT RECEIVED A FUEL FILTER BYPASS INDICATION, PILOT DECIDED TO ABORT THE TAKEOFF AND THE WARNING DISAPPEARED UPON REDUCTION OF POWER. THE BYPASS WARNING REAPPEARED EVERY TIME THE POWER WAS INCREASED. TROUBLESHOOSep 28, 2010 · Cessna 510 · Engine Fuel and ControlSDR 2010FA0000504Uplock Switch · intermittent( CNQR ) DURING APPROACH THE ACFT WENT TO EXTEND THE LANDING GEAR AND RECEIVED A LANDING GEAR UNLOCK LIGHT. CYCLED THE GEAR SEVERAL TIMES WITH NO CHANGE OF STATUS. DECLARED AN EMERGENCY AND BLEW THE GEAR DOWN USING THE EMERGENCY EXTENSION SYSTEM. ACFT LANDEDMay 6, 2010 · N510KZ · Cessna 510 · Landing Gear Position and WarningSDR 2010FA0000213Pushrod · distortedDURING MX INSP IN THE AREA OF THE PILOT`S RUDDER PEDALS, IT WAS NOTICED THAT THE RT BRAKE PEDAL PUSH ROD HAD AT SOME POINT MADE CONTACT WITH AN ADJACENT FLOOR SUPPORT ANGLE CAUSING MINOR DISTORTION TO THE ANGLE VERTICLE FLANGE. THIS CONDITION COULD HAVE RESULFeb 21, 2010 · Cessna 510 · Rudder Control SystemSDR 2010FA0000181Engine · making metalCREW SHUTDOWN RT ENG AFTER HEARING A BANG AND NOTICING ITT RISE AT ALTITUDE 27,000 FT ON 18FEB2010. CREW LANDED. REMOVED THIS ENGINE AFTER FINDING METAL IN OIL & DEBRIS ON CHIP DETECTOR. COMPLETED A SOAP ANALYSIS WITH NORMAL RESULTS. REMOVED THE ENGINES FADEFeb 18, 2010 · N910SY · Cessna 510 · Engine (Turbine/Turboprop)SDR 2010FA0000041Uplock Switch · failedAFTER SELECTING GEAR SELECT HANDLE TO THE GEAR DOWN POSITION, THE PILOT NOTED THE ACFT RECEIVED ALL 3 GREEN "DOWN AND LOCK" LIGHTS AND THE RED IN-TRANSIT "UNSAFE" LIGHT. OPERATOR DECLARED AN EMERGENCY LANDING AND LANDED WITHOUT INCIDENT. A POST FLIGHT INSP FDec 14, 2009 · N620CM · Cessna 510 · Landing Gear Position and WarningSDR CNQR2009120600001Position Switch · out of adjustWHEN THE ACFT DEPARTED AND THE LANDING GEAR WAS RETRACTED AFTER TAKEOFF, THE LANDING GEAR TRANSITION LIGHT REMAINED ILLUMINATED. FLIGHT CREW CYCLED THE LANDING GEAR SEVERAL TIMES WITH SUCCESSFUL EXTENSIONS AND RETRACTIONS ON EACH EVENT. WITH EACH EVENT THE LDec 6, 2009 · N270MK · Cessna 510 · Landing Gear Position and WarningSDR 2009FA0001046Actuator · looseDURING MX ON 510-0032 WHILE CARYING OUT SB510-27-01 A LOUD RATTLE WAS NOTICED FROM INSIDE THE LT AILERON PRIOR TO REFIT. THE NOISE SOUNDED LIKE MUTIPLE LOOSE ITEMS TOWARDS THE INBD END OF THE AILERON. ON REMOVAL OF THE AILERON TRIM ACTUATOR ACCESS PANEL (532Nov 26, 2009 · N814WS · Cessna 510 · Aileron Tab Control SystemSDR 2009FA0000716Actuator · seizedCREW REPORTED A ONE-OFF INCIDENT ON 24 JUNE, 2009 WHERE FLAP SYS FAILED ON APPROACH. UNDER INVESTIGATION, SYS SHOWED NO FAULTS AND WAS CONSIDERED FIT FOR RETURN TO SERVICE. ACFT PERFORMED SATISFACTORILY FOR 15.4 FLYING HOURS/ 9 LANDINGS. ON 26 JULY, 2009 CRJun 24, 2009 · N80HQ · Cessna 510 · Trailing Edge Flap ActuatorSDR YGJA20090512001Speed Brake · inoperativePILOT DEPLOYED SPOILERS AND THE ACFT ROLLED TO THE RT. INVESTIGATION REVEALED THAT THE LT SPOILER WAS RETRACTED WITH THE RT, WAS DEPLOYED. SPOILERS WERE RETRACTED AND THE PILOT LANDED SAFELY.May 12, 2009 · N510LL · Cessna 510 · Drag Control ActuatorSDR 2008FA0000877Ground Stud · looseADJACENT TO RT WING ACCESS PANEL 623DB THERE IS A GROUNDING POINT TO GROUND THE ACFT DURING FUELING OR WHILE PERFORMING MAINTENANCE. IN AN ATTEMPT TO GROUND TO ACFT IN ORDER TO PERFORM MAINT, WE FOUND THE GROUNDING JACK MISSING. PANEL 632DB WAS REMOVED AND UNov 20, 2008 · N551WH · Cessna 510 · Static Discharge SystemSDR 2008FA0000887Autopilot Sys · malfunctionedWHEN A DISCREPENCY BETWEEN THE NAVDATA DATABASE & ACTUAL IMPLEMENTATION OF A LOCALIZER NAVAID, GFC700 WILL NOT INTERCEPT & TRACK LOCALIZER SIGNAL CORRECTLY. IT EITHER FLIES THROUGH COURSE OR WILL ACTIVATE LOC MODE & IMMEDIATELY TURN OFF COURSE. AFCS APPEARS Oct 28, 2008 · N510AZ · Cessna 510 · Autopilot ComputerSDR 26N2008F00004Selector · frozenACFT FLIGHT CONTROLS FROZE AT ALTITUDE ENROUTE. THIS IS THE SECOND SITUATION WHERE THIS CONDITION HAS HAPPENED TO THIS ACFT. ACFT PREVIOUS REGISTRATION N1693L. A TECH WAS WITH THE ACFT. INSPECTED AREAS OF PREVIOUS CONCERN AND SERVICE PREVIOUSLY WORKED BY MFG,Sep 29, 2008 · N83EM · Cessna 510 · Aileron Control SystemSDR 26N2008F00003Control Cable · frozenON CLIMB OUT, AT 20,000 FT THE AILERONS FROZE WITH AN OAT OF 0 DEGREES C. PILOT WAS GETTING THE AMBER AP LIGHT. HE WOULD TURN THE AP "OFF" AND FREE UP THE CONTROLS ABOUT EVERY 15 TO 20 MINUTES BY EXERTING A LOSS OF FORCE TO FREE THE ICING. AT 33,000 FT WITH ANSep 29, 2008 · N83EM · Cessna 510 · Aileron Control SystemSDR ZESA2008018Fuel Nozzle · overtorquedDURING START UP, CREW NOTICED AND REPORTED WHITE SMOKE AND A SLOW START FROM THE RT ENGINE. WHEN THE ENGINE WAS SHUTDOWN AND RESTARTED, THE CONDITION COULD NOT BE DUPLICATED. SEVERAL DAYS LATER, THE SAME CONDITION OCCURRED. THE TECH WAS NOTIFIED (9/8/08) ANSep 8, 2008 · N75ES · Cessna 510 · Fuel Injector NozzleSDR 26N2008F00005Selector · unknownCREW REPORTED AILERONS FROZE AFTER FLYING THROUGH MOISTURE. 07/25/2008 AC REPOSITIONED TO SERVICE CENTER FOR FURTHER EVALUATION AND RESOLUTION. MFG HEAVILY INVOLVED WITH THIS ISSUE. (K)Aug 4, 2008 · N1693L · Cessna 510 · Flight Control SystemSDR 26N2008F00002Control Cable · frozen7/24/2008, AC TT: 461.8, TC:302 CREW REPORTED AILERONS FROZEN AFTER FLYING THROUGH MOISTURE (FROM FORM 26NA-210A, ATTACHED) 7/25/2008, AC REPOSITIONED TO MFG SERVICE CENTER FOR FURTHER EVALUATION AND RESOLUTION. 8/1/2008, AC TT: 462.3 MFG MTR FOR RESOLUTION. Aug 4, 2008 · N1693L · Cessna 510 · Elevator Control SystemSDR 26N2008F00001Control Cable · frozenCREW REPORTED AILERONS FROZE AFTER FLYING THROUGH MOISTURE. AC REPOSITIONED FOR FURTHER EVALUATION AND RESOLUTION. (K)Aug 4, 2008 · N1693L · Cessna 510 · Aileron Control SystemSDR CA071003021Engine · malfunctioned(CAN) IN CRUISE IN LIGHT ICING CONDITIONS, ENGINE N1 SPEED REDUCED UNCOMMANDED. THE N1 RETURNED TO NORMAL SETTINGS IN DESCENT. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED.Aug 7, 2007 · Cessna 510 · Turbine Engine Compressor Section
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