Cessna 414

Service difficulty reports · 234

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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 = '414'
  ORDER BY difficulty_date DESC"

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SDR 2025F00273Support · corrodedDURING A PREFLIGHT WALKAROUND, SURFACE CORROSION WAS OBSERVED ON THE VERTICAL STABILIZER AFT SECTION. AFTER CLOSER INSPECTION SEVERE DELAMINATION WAS SEEN ON THE AFT VERTICAL SUPPORT ANGLES AND AFT STAB BULKHEAD SECTION. THE RUDDER TRIM TAB BRACKET ALSO HAD SINov 26, 2025 · N86VS · Cessna 414 · Vertical Stabilizer Miscellaneous StructureSDR KISA202602050001Angle · corrodedDURING A PREFLIGHT WALK AROUND CORROSION WAS OBSERVED ON THE AFT SPAR ANGLE CHANNEL OF THE VERTICAL STABILIZER. UPON FURTHER INVESTIGATION SIGNIFICANT INTERGRANULAR CORROSION WAS FOUND RESULTING IN EXFOLIATION OF THE SURFACE OT THE SPAR ANGLE. THIS RESULTED INNov 25, 2025 · N86VS · Cessna 414 · Vertical Stabilizer Miscellaneous StructureSDR 2021FA0000079Oxygen System · leakingAIRCRAFT OWNER REPORTED HISSING SOUND ABOVE CABIN HEADLINER WHEN CABIN OXYGEN CONTROL WAS TURNED ON. PRESSURIZED OXYGEN SYSTEM AND CONFIRMED LOUD HISSING SOUND COMING FROM HEADLINER BETWEEN FIRST ROW OF PASSENGER SEATS. USED BORESCOPE TO INSPECT THE AREA, AND Mar 9, 2021 · Cessna 414 · Oxygen SystemSDR 2018FA0000375Trim Tab · crackedDURING ANNUAL/100 INSPECTION, SURFACE CORROSION WAS OBSERVED NEAR AND ON THE ATTACHMENT SCREWS FOR THE ELEVATOR TRIM TAB HORN (P/N: 0831000-50). CORROSION WAS CLEANED. CRACKS WERE OBSERVED IN THE AFT TWO SCREW HOLES ON THE TOP SURFACE OF THE ELEVATOR TRIM TAB.Sep 15, 2018 · N414AC · Cessna 414 · Elevator, Tab StructureSDR 2018FA0000340Fork · brokenNOSE GEAR WOULD NOT LOCK IN DOWN POSITION UPON LANDING.Jun 23, 2018 · N3758C · Cessna 414 · Nose/Tail Landing GearSDR 2RM2017F00001Lifter · spalledENGINE WAS DISASSEMBLED FOR PROP STRIKE INSPECTION. FOUND LIFTERS BEGINNING TO SPALL AND WERE REPLACED WITH NEW LIFTERS AT THIS TIME TO PREVENT DAMAGE TO CAMSHAFT. LIFTERS WERE INSTALLED IN MAY OF 2010 AND HAVE 303.7 HOURS SINCE NEW.Oct 17, 2017 · N414AW · Cessna 414 · Reciprocating Engine Power SectionSDR 2RM2017F00000Lifter · spalledENGINE WAS DISASSEMBLED FOR PROP STRIKE INSPECTION. FOUND LIFTERS BEGINNING TO SPALL AND WERE REPLACED WITH NEW LIFTERS AT THIS TIME TO PREVENT DAMAGE TO CAMSHAFT. LIFTERS WERE INSTALLED IN MAY OF 2010 AND HAVE 303.7 HOURS SINCE NEW.Oct 17, 2017 · N414AW · Cessna 414 · Reciprocating Engine Power SectionSDR 2017FA0000379Beam · corrodedWHILE REMOVING THE TURBO CHARGER, NOTICED SEVERAL RIVET HEADS MISSING ON THE DOUBLER FOR THE TALL PIPE SUPPORT CLAMP. ON FURTHER INVESTIGATION, IT WAS DISCOVERED THAT THE DOUBLER WAS PUSHED UP FROM CORROSION. THE TALL PIPE SUPPORT WAS REMOVED AND THE ENGINMar 17, 2017 · N620CA · Cessna 414 · Engine Mount SectionSDR 2016FA0000239Bellcrank · brokenON LANDING ROLLOUT, THE LT MAIN GEAR COLLAPSED. 1 OF THE LOWER EARS OF THE LT LANDING GEAR RETRACTION BELLCRANK WAS SHEARED AND NOT FOUND. THE BELLCRANK CAME OFF THE DOWNLOCK PIN. ALSO THE UPPER ATTACH BOLT SHEARED AND 1 OF THE ATTACHMENT EARS OF THE UPPERMay 13, 2016 · Cessna 414 · Landing Gear Retraction/Extension SystemSDR 4MCA2015F00094Magneto · malfunctionedATC KEPT ACFT AT 3000 FT FOR APPROXIMATELY 15 MINUTES. DURING THIS TIME, KEPT FULL POWER AND MIXTURE FULL RICH, WAS EXPECTING A CLIMB TO FILED ALTITUDE. AFTER ABOUT 15 MINUTES, SET POWER TO CRUISE SETTING AND LEANED MIXTURE. A FEW MINUTES LATER, WAS TOLD TAug 4, 2015 · N999RK · Cessna 414 · Magneto/DistributorSDR 7IL2015F00008Bulkhead · crackedWHILE PERFORMING 100 HR INSPECTION OF ACFT, FOUND SPINNER REAR BULKHEAD CRACKED. BULKHEAD SN DY-1863.Jan 16, 2015 · N490KM · Cessna 414 · Propeller Spinner SectionSDR 7IL2015F00007Bracket · crackedWHILE PERFORMING 100 HR INSPECTION OF ACFT, FOUND RT REAR INNER GEAR DOOR ATTACH BRACKETS CRACKED AT INBD BOLT HOLE. BRACKET WAS STILL SECURED BY REMAINING MOUNT TABS. SIMILAR BRACKETS ARE USED ON FWD SIDE OF GEAR DOOR AS WELL AS LT GEAR DOOR, NO DAMAGE FOUNJan 16, 2015 · N490KM · Cessna 414 · Landing Gear DoorsSDR 7IL2015F00006Bracket · crackedWHILE PERFORMING 100 HR INSPECTION OF ACFT, FOUND RT REAR INNER GEAR DOOR ATTACH BRACKETS CRACKED AT INBD BOLT HOLE. BRACKET WAS STILL SECURED BY REMAINING MOUNT TABS. SIMILAR BRACKETS ARE USED ON FWD SIDE OF GEAR DOOR AS WELL AS LT GEAR DOOR, NO DAMAGE FOUNJan 16, 2015 · N490KM · Cessna 414 · Landing Gear DoorsSDR 7IL2015F00005Cylinder Head · crackedWHILE PERFORMING 100 HR INSPECTION OF ACFT, FOUND CRACKS IN CYLINDERS: NR 3 LOCATION, SN60652-27, NR 5 LOCATION, SN 60652-25, NR 4 LOCATION, SN 606652-23. CRACKS WERE FOUND IN THE HEAD CASTING ON THE INTAKE VALVE SIDE IN THE VICINITY OF FINS 15-17 AS COUNTED Jan 16, 2015 · N490KM · Cessna 414 · Reciprocating Engine Cylinder SectionSDR 7IL2015F00004Cylinder Head · crackedWHILE PERFORMING 100 HR INSPECTION OF AIRCRAFT, FOUND CRACKS IN CYLINDERS: NR 3 LOCATION, SN60652-27, NR 5 LOCATION, SN 60652-25, NR 4 LOCATION, SN 606652-23. CRACKS WERE FOUND IN THE HEAD CASTING ON THE INTAKE VALVE SIDE IN THE VICINITY OF FINS 15-17 AS COUNJan 16, 2015 · N490KM · Cessna 414 · Reciprocating Engine Cylinder SectionSDR 7IL2015F00003Cylinder Head · crackedWHILE PERFORMING 100 HR INSPECTION OF ACFT, FOUND CRACKS IN CYLINDERS: NR 3 LOCATION, SN60652-27, NR 5 LOCATION, SN 60652-25, NR 4 LOCATION, SN 606652-23. CRACKS WERE FOUND IN THE HEAD CASTING ON THE INTAKE VALVE SIDE IN THE VICINITY OF FINS 15-17 AS COUNTED Jan 16, 2015 · N490KM · Cessna 414 · Reciprocating Engine Cylinder SectionSDR 7IL2015F00002Cylinder Head · crackedWHILE PERFORMING 100 HR INSPECTION OF ACFT, FOUND CRACKS IN CYLINDERS NR 3 LOCATION, SN64015-16, NR 5 LOCATION, SN64016-17, NR 6 LOCATION, SN 63936-02. CRACKS WERE FOUND IN THE HEAD CASTING ON THE INTAKE VALVE SIDE IN THE VICINITY OF FINS 15-17 AS COUNTED OTBJan 16, 2015 · N490KM · Cessna 414 · Reciprocating Engine Cylinder SectionSDR 7ILA2015F00001Cylinder Head · crackedWHILE PERFORMING 100 HR INSPECTION OF ACFT, FOUND CRACKS IN CYLINDERS NR 3 LOCATION, SN 64015-16, NR 5 LOCATION, SN 64016-17, NR 6 LOCATION, SN 63936-02. CRACKS WERE FOUND IN THE HEAD CASTING ON THE INTAKE VALVE SIDE IN THE VICINITY OF FINS 15-17 AS COUNTED OJan 16, 2015 · N490KM · Cessna 414 · Reciprocating Engine Cylinder SectionSDR 7ILA2015F00000Cylinder Head · crackedWHILE PERFORMING 100 HR INSPECTION OF ACFT, FOUND CRACKS IN CYLINDERS NR 3 LOCATION, SN64015-16, NR 5 LOCATION, SN64016-17, NR 6 LOCATION, SN 63936-02. CRACKS WERE FOUND IN THE HEAD CASTING ON THE INTAKE VALVE SIDE IN THE VICINITY OF FINS 15-17 AS COUNTED OTBJan 16, 2015 · N490KM · Cessna 414 · Reciprocating Engine Cylinder SectionSDR 2014FA0000541Cylinder · burstPROPELLER CYLINDER C3550 BURST FROM OIL PRESSURE, PROBABLE FROM GOVERNOR. GOVERNOR MUST BE TESTED BEFORE PROPELLER REINSTALLED. PROPELLER HUB SERIAL 700239. REJECTED DUE TO FORCE PUT ON SCREW HOLES.Aug 10, 2014 · N698D · Cessna 414 · Propeller AssemblySDR 2014FA0000156Landing Gear · collapsedLEFT MLG COLLAPSED ON LANDING ROLLOUT.Mar 13, 2014 · N606PP · Cessna 414 · Main Landing GearSDR 2013FA0000741Pivot Assy · failedPIVOT ARM SUPPORTING THE PILOT SEAT BACK FAILED DURING TAXI, ALLOWING SEAT BACK TO PARTIALLY RECLINE. SPECIFIC INSPECTION FOR CRACKS AND CORROSION ON THE SEAT PIVOT ARMS RECOMMENDED. THERE WAS EVIDENCE OF CRACK/CORROSION THAT MAY HAVE CAUSED THE FAILURE.Dec 5, 2013 · N2694H · Cessna 414 · Flight Compartment EquipmentSDR CA130826006Bellcrank · sheared(CAN) AFTER FLIGHT, IT WAS NOTED THAT THE RT INBD MLG DOOR WAS HANGING OPEN. NO NOISE WAS HEARD IN FLIGHT DURING EXTENSION AND RETRACTION AND THE LANDING GEAR SYS FUNCTIONED NORMALLY. IT WAS FOUND THAT THE IDLER BELLCRANK THAT CONTROLS THE DOOR MOVEMENT HAD Aug 22, 2013 · Cessna 414 · Landing Gear Door Retract SectionSDR CA130410019Tach Generator · failed(CAN) DURING TAKEOFF, NON FLYING PILOT NOTED THE CO-PILOTS ENGINE RPM, TACH, INDICATOR LT NEEDLE DROPPING FROM TAKEOFF RPM TO ZERO WITH NO CHANGE IN ENGINE PERFORMANCE. PRIMARY FLIGHT DISPLAY TACHOMETER INDICATION REMAINED UNCHANGED. INSPECTION DETERMINED THAApr 9, 2013 · Cessna 414 · Engine RPM Indicating SystemSDR 2013FA0000469Trunnion · crackedNLG LT TRUNNION LUG FAILED UPON LANDING.Apr 5, 2013 · N37480 · Cessna 414 · Fuselage, Landing Gear Attach FittingsSDR CA121112006Cylinder · cracked(CAN) DURING TROUBLESHOOTING, DIFFERENTIAL COMPRESSION TEST AND CYLINDER LEAKAGE TEST. FOUND CYLINDER LEAKING AIR FROM AREA OF COOLING FINS ON THE EXHAUST PORT. VISUAL INSPECTION FOUND INTERNAL CRACK EXHAUST PORT OF CYLINDER WITH EXHAUST REMOVED.Nov 7, 2012 · Cessna 414 · Reciprocating Engine Cylinder SectionSDR CA121112005Cylinder · cracked(CAN) DURING TROUBLESHOOTING, DIFFERENTIAL COMPRESSION TEST AND CYLINDER LEAKAGE TEST, FOUND CYLINDER LEAKING AIR FROM AREA OF COOLING FINS ON THE EXHAUST PORT. BOROSCOPE INSPECTION FOUND INTERNAL CRACK IN THE HEAD OF THE CYLINDER.Nov 7, 2012 · Cessna 414 · Reciprocating Engine Cylinder SectionSDR CA121112004Antenna · intermittent(CAN) DURING FLIGHT PILOT HAD LOSS OF ALL GPS NAVIGATION TO THE GARMIN 430W , GARMIN 530W AND THE GARMIN G600 SYS. SYSTEM REVERTED TO DEAD, RECONNING MODE. TROUBLESHOOTING DETERMINED THE GARMIN GA-35 WAAS GPS ANTENNA FOR THE GARMIN 430W FAILED CAUSING AN OSCIOct 24, 2012 · Cessna 414 · Global Positioning SystemSDR J7B2012F00000Bearing · wornSHORTLY AFTER DEPARTURE, A MINOR FLUCTUATION OF MANIFOLD PRESSURE WAS OBSERVED ON THE RT ENGINE. THE ACFT RETURNED TO DEPARTURE WITHOUT INCIDENT. UPON INSPECTION IT WAS DISCOVERED THAT THE RT ENGINE TURBOCHARGER CENTER BEARING HAD EXCESSIVE WEAR CAUSING THE Mar 1, 2012 · N4243C · Cessna 414 · Exhaust TurbochargerSDR CA111026007Skin · cracked(CAN) NUMEROURS SKIN CRACKS FOUND IN UPPER SKIN ON LT ELEVATOR AND LT HORIZONTAL STABILIZER.Oct 23, 2011 · Cessna 414 · Horizontal Stabilizer, Plate/SkinSDR 2011FA0000684Skin · crackedAFTER FINDING SIMILAR ACFT WITH SIMILAR ISSUES, PERFORMED A VISUAL INSP OF BOTH RT AND LT UPPER INBD RT WING SKIN AND LT WING SKIN FROM WHEEL WELL AREA AND NOTED CRACKS IN SKIN, (APPROX 2-3 INCHES IN LENGTH), IN AREA OF RIB THAT ATTACHES UPPER MLG SIDE BRACE SOct 14, 2011 · N414EL · Cessna 414 · Wing, Plate/SkinSDR CA110429001Connecting Rod · broken(CAN) TWO CONNECTING RODS BROKEN. SCRAP CRANKCASE BROKEN. SCRAP CAMSHAFT BROKEN - SCRAP OIL SUMP, SCRAP PISTON BROKEN.Dec 8, 2010 · Cessna 414 · Reciprocating Engine Power SectionSDR CA101112006Turbine · stuck(CAN) ON TAKEOFF, THE NR 2 ENGINE WOULD NOT DEVELOP FULL POWER. THE TURBOCHARGER HOT SIDE TURBINE WAS RUBBING ON THE TURBO HOUSING, PREVENTING IT SPINNING. THE TURBO WAS REPLACED.Nov 12, 2010 · Cessna 414 · Exhaust TurbochargerSDR CA091116007Skin · cracked(CAN) DURING AN INSP, THE UPPER WING SKIN WAS FOUND CRACKED. THE CRACK WAS LOCATED AT THE AFT ATTACHMENT POINT OF THE MAIN FUEL TIP TANK. THE CRACK WAS 3/4 OF AN INCH IN LENGTH JUST FWD OF THE AFT WING SPAR. 2 RIVETS THAT GO THROUGH THE OTBD AILERON ATTACH BRANov 13, 2009 · Cessna 414 · Wing, Plate/SkinSDR J7B2009F00000Cylinder Head · separatedWHILE IN FLIGHT, AT CRUISE POWER, A LOSS OF MANIFOLD PRESSURE AND ENGINE ROUGHNESS WAS EXPERIENCED. THE ENGINE WAS SHUTDOWN. A NORMAL LANDING WAS MADE AT THE INTENDED DESTINATION. INSP REVEALED THAT NR 2 CYLINDER HEAD HAD SEPARATED. NO STRUCTURAL DAMAGE OCMay 20, 2009 · N4243C · Cessna 414 · Reciprocating Engine Cylinder SectionSDR CA090403002Connecting Rod · worn(CAN) PISTON PIN BUSHING FAILED DUE TO LACK OF LUBRICATION. ENG DISMANTLED AND FAILURE DETERMINED TO BE CASUED BY SEALANT BLOCKING THE PISTON COOLING JET TO NR 2 CYLINDER. THE PROBLEM SEEMED TO BE CAUSED BY THE USE OF EXCESSIVE SEALANT (POSSIBLY LOCKTITE 515) Mar 17, 2009 · Cessna 414 · Reciprocating Engine Power SectionSDR 2009FA0000014Arm · brokenON LANDING, THE PILOT SELECTED THE GEAR DOWN AND NEVER GOT A GREEN DOWN AND LOCK LIGHT IN THE CABIN FOR THE RT MAIN GEAR. THE GEAR DOWNLOCK MICRO-SWITCH ACTUATOR ARM WAS BROKEN AND WOULD NOT ACTUATE THE MICRO-SWITCH. THESE ACTUATOR ARMS SEEM TO GET WEAK OVERDec 10, 2008 · N52CS · Cessna 414 · Landing Gear Position and WarningSDR A6WA200840624Support · crackedAFT COMPARTMENT RT HYDRAULIC SUPPORT AT FS 718 FOUND CRACKED IN AFT LOWER CORNER. AFT COMPARTMENT RT HYDRAULIC SUPPORT AT FS 718 ON AFT LOWER CORNER REPAIRED IAW CRJ200 REO 601R-53-62-031 REV A.Dec 1, 2008 · N414AW · Cessna 414 · Fuselage Main, Attach FittingsSDR CA080410009Cylinder Head · crackedPILOT FLYING IN CRUISE FLIGHT, WHEN HE HEARD A POP AND EXPERIENCED LOSS OF ENGINE POWER. FEATHERED PROPELLER AND LANDED AT NEAREST AIRPORT. ENGINE CYLINDER REPLACED.Mar 12, 2008 · Cessna 414 · Reciprocating Engine Cylinder SectionSDR CA071004006Cable · broken(CAN) DURING THE ENGINE RUN-UP, THE RT ENGINE DID NOT RESPOND TO MIXTURE CONTROL. THE MIXTURE CONTROL CABLE WAS FOUND BROKEN UNDER THE ENGINE CONTROL PEDISTAL. THE BRAKE WAS INSIDE THE CONTROL CABLE HOUSING AND COULD NOT BE SEEN WITH ANY INSPECTION. (TC NR 200Oct 1, 2007 · Cessna 414 · Mixture ControlSDR 2007FA0000749Exhaust Pipe · crackedDURING COMPLIANCE WITH AD 2000-01-16 THE TAIL PIPE ON THE RT ENGINE WAS FOUND WITH A 6 INCH CRACK. THE LAST INSPECTION WAS 40 HRS PRIOR.Aug 29, 2007 · N22MG · Cessna 414 · Engine Collector/Tailpipe/NozzleSDR 2007FA0000396Switch · stuckAVIONICS MASTER SWITCH STUCK IN THE ON POSITION AD 2005-20-25 WAS PREVIOUSL COMPLIED WITH AND DID NOT APPLY. DATE CODE OF THE SWITCH WAS 7647. THERE WAS NO BURNING SMELL WHEN THE SWITCH BECAME STUCK. (K)Apr 30, 2007 · N42SG · Cessna 414 · Navigation SystemSDR 155SW112206Exhaust Stack · crackedAPPROXIMATELY 5 MINUTES AFTER TAKEOFF FROM ST MARY'S COUNTY, MD (2W6) EN ROUTE TO CLARKSBURG, WV (KCKB), THE PILOT NOTICED AN UNUSUAL SOUND COMING FROM THE LEFT ENGINE. THE PILOT THEN NOTICED THE LEFT MANIFOLD PRESSURE BEGIN TO DROP TO APPROXIMATELY 28 INCHESNov 22, 2006 · N155SW · Cessna 414 · Engine Collector/Tailpipe/NozzleSDR CA061123006Cap · cracked(CAN) CRACK NOTED AT LT NACELLE CANTED BULKHEAD CAP. CAP REPAIRED. (TC NR 20061123006)Nov 20, 2006 · Cessna 414 · Nacelle/Pylon Miscellaneous StructureSDR 155SW111506Pump · leakingAPPROXIMATELY 40 MINUTES INTO A FLIGHT FROM CLARKSBURG, WV (KCKB) TO ST. MARY'S COUNTY, MD (2W6), OIL WAS OBSERVED ON THE RIGHT ENGINE NACELLE STARTING AT THE VENT ON TOP OF THE NACELLE AND EXTENDING BACK TO THE TRAILING EDGE. AS A PRECAUTIONARY MEASURE, THE Nov 15, 2006 · N155SW · Cessna 414 · Vacuum Distribution SystemSDR 2006FA0000622Skin · crackedDURING AN ANNUAL INSPECTION, A CRACK WAS FOUND ON THE RT WING SKIN AT THE OB AILERON ATTACH POINT, WHICH IS ALSO THE MAIN FUEL TANK AFT ATTACH POINT. UPON FURTHER INSPECTION OF AREA, THE RIVETS THAT ATTACH THE AILERON SUPPORT TO THE REAR SPAR WERE FOUND SHEAREJun 22, 2006 · N414JS · Cessna 414 · Wing, Plate/SkinSDR 2006FA0000621Skin · crackedDURING AN ANNUAL INSPECTION, A CRACK WAS FOUND ON THE RT WING SKIN AT THE OB AILERON ATTACH POINT, WHICH IS ALSO THE MAIN FUEL TANK AFT ATTACH POINT. UPON FURTHER INSPECTION OF AREA, THE RIVETS THAT ATTACH THE AILERON SUPPORT TO THE REAR SPAR WERE FOUND SHEAREJun 22, 2006 · N414JS · Cessna 414 · Wing, Plate/SkinSDR 2006FA0000498Cylinder · crackedDURING DECENT TO AIRPORT, PILOT REPORTED RT ENGINE STARTED HAVING EXCESSIVE VIBRATION. NO OTHER MAJOR ENGINE INDICATIONS WERE NOTED. AFTER LANDING, A MAGNETO CHECK WAS CONDUCTED AND NO DESCREPANCIES WERE FOUND. UPON REMOVAL OF COWLING, RT ENGINE NR 6 CYLINDMay 11, 2006 · N710US · Cessna 414 · Reciprocating Engine Cylinder SectionSDR 2006FA0000493Fitting · crackedDURING ANNUAL INSP FOUND LT STUB WING AFT SPAR, UPPER FITTING CRACKED AT OB BOLT HOLE. FOUND NO CORROSION OR STRESS IN SURROUNDING AREAS. SUSPECT BOLT WAS OVERTORQUED. (K)May 4, 2006 · N352TS · Cessna 414 · Wing, Attach FittingsSDR 2006FA0000202Turbocharger · disintegratedTURBOCHARGER CAME APART INTERNALLY RESULTING IN LOSS OF MANIFOLD PRESSURE AND ENGINE METAL CONTAMINATION. ENGINE REMOVED FROM SERVICE. (K)Feb 21, 2006 · N4243C · Cessna 414 · Exhaust Turbocharger
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