Cessna 310

Service difficulty reports · 91

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 = '310'
  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 2026FA0000835Switch · malfunctionedLANDING GEAR SWITCH, DOWN POSITION SAFETY FAILED DUE TO WEAR ALLOWING INADVERTENT UP POSITION ACTUATION WHEN BUMPED.Oct 14, 2026 · N3618G · Cessna 310 · Landing Gear Position and WarningSDR 2021FA0000285Heat Exchanger · damagedRIGHT ENGINE FUEL LEAK OF HEAT EXCHANGER OIL-FUEL DRAIN, DURING TRANSIT CHECK, IT WAS DETECTED A FUEL LEAK AT RIGHT ENGINE. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING THE RIGHT ENGINE FUEL LEAK OF HEAT EXCHANGER OIL-FUEL DRAIN; RH ENGINE HEAT EXCHANGESep 13, 2021 · N116BG · Cessna 310 · Engine Oil CoolerSDR 2021FA0000235Landing Gear · collapsedLANDED AND ON ROLL OUT THE PILOT NOTICED A VIBRATION ON RIGHT SIDE OF AIRCRAFT. AFTER NOTICING THE VIBRATION THE RIGHT MAIN GEAR COLLAPSED CAUSING DAMAGE TO RIGHT WING. MAINTENANCE PERSONNEL FOUND THE RIGHT MAIN GEAR PUSH PULL ROD BROKEN.Aug 17, 2021 · Cessna 310 · Main Landing GearSDR 2017FA0000471Relay · shortedAIRCRAFT LOST ALL AVIONICS POWER WHILE IN LEVEL FLIGHT, PILOT DECLARED EMERGENCY LANDING AND LANDED AIRCRAFT WITHOUT INCIDENT. MECHANICS DETERMINED THAT THE STARTER RELAY SHORTED INTERNALLY CAUSING A SHORT THAT TOOK OUT THE AVIONICS BUSS CAUSING THE POWER LOAug 30, 2017 · N3647D · Cessna 310 · Engine Starting System WiringSDR CA150820003Warning Light · illuminated(CAN) DURING TAKEOFF ROLL, WHEN SET POWER WAS ACHIEVED, THE RIGHT OIL FILTER BYPASS LIGHT ILLUMINATED. POWER WAS REDUCED TO IDLE, LIGHT WENT OUT, AIRCRAFT RETURNED TO THE HANGAR.Aug 11, 2015 · Cessna 310 · Engine Oil Indicating SystemSDR 2010FA0000003Rod End · brokenROD END BROKE WHEN ATTEMPTING TO EXTEND THE LANDING GEAR IN FLIGHT. COULD NOT EXTEND THE GEAR, RESULTING IN A GEAR-UP LANDING. UPON INSPECTION OF THE ROD END, FOUND THAT IT HAD BEEN CRACKED PRIOR TO THE INCIDENT. PROBABLE CAUSE IS FATIGUE FAILURE DUE TO THEDec 11, 2009 · N2640C · Cessna 310 · Landing Gear Retraction/Extension SystemSDR 2004FA0000149Counterweight · crackedPART HAD APPROX 700.00 HOURS SINCE OVERHAUL, FATIGUE CRACK APPEARS TO HAVE ORIGINATED AT FORWARD BOLT HOLE. PROPELLER/ENGINE BEGAN VIBRATING IN FLIGHT DUE TO COUNTER WEIGHT SHIFTING ON FERRULE. AIRCRAFT REDUCED POWER, LANDED AND WAS REPAIRED BEFORE FURTHER Jan 20, 2004 · N1312J · Cessna 310 · Propeller AssemblySDR 2003FA0001063Skin · corrodedAFTER REMOVAL OF NACELLE AUX FUEL TANK, DISCOVERED A LARGE AREA OF CORROSION ON THE TOP WING SKIN. THE TANK HAD TRAPPED MOISTURE BETWEEN IT AND THE WING TOP OVER A PERIOD OF YEARS. THE CORROSION WAS CLEANED AND THE SKIN HAD LOST LESS THAN 10 PERCENT OF ITS ORIOct 15, 2003 · N244S · Cessna 310 · Wing, Plate/SkinSDR 2003FA0001085Rivet · looseTHE RIVETS THAT ATTACH THE RUDDER TORQUE TUBE TO THE BELLCRANK ADDAPTOR PLATE BECAME LOOSE. THIS CAUSED THE RUDDER TO DEFLECT AS MUCH AS FIVE DEGREES FROM ITS PROPER POSSITION.Oct 15, 2003 · N244S · Cessna 310 · FastenersSDR 2003FA0001084Rivet · looseTHE RIVETS THAT ATTACH THE RUDDER TORQUE TUBE TO THE BELLCRANK ADDAPTOR PLATE BECAME LOOSE. THIS CAUSED THE RUDDER TO DEFLECT AS MUCH AS FIVE DEGREES FROM ITS PROPER POSSITION.Oct 15, 2003 · N244S · Cessna 310 · FastenersSDR 20000817SH013Nut · crackedPROPELLER IN FOR OVERHAUL. DISASSEMBLED, FOUND BOTH RETENTION NUTS CRACKED. (X)Jul 31, 2000 · Cessna 310 · Propeller AssemblySDR 20000407SH012Torque Tube · brokenPART FAILED AT GEAR RETRACTION AFTER TAKEOFF, NOSE GEAR COLLAPSED AT LANDING. COMPONENT WAS REDESIGNED STARTING WITH A/C SN 35042. SUBMITTER SUGGESTED ADDED EMPHASIS INSPECTION THIS AREA ON EARLY CE-310 A/C. (X)Jan 31, 2000 · N2640C · Cessna 310 · Landing Gear Retraction/Extension SystemSDR 99ZZZX4659Control Cable · looseDURING ROUTINE 100-HOUR ANNUAL, NOTED AILERON CABLE TENSION WAS SLACK ENOUGH THAT THE CABLES WERE RUBBING ON THE STRINGER WHERE THEY PASSED THROUGH (BELOW THE FLOOR UNDER THE COCKPIT). THE TENSION WAS SO LOW AS NOT TO READ ON THE TENSIONMETER. THE CABLES WERDec 11, 1999 · Cessna 310 · Aileron Control SystemSDR 20000621SH011Cooler · leakingOIL COOLER RUPTURED AT POINT OF PREVIOUS EPOXY REPAIR CAUSING SEVERE LEAK. EPOXY FAILURE IS COMMON AND SHOULD BE ELIMINATED FROM BEING USED IN OIL COOLERS. (X)Oct 6, 1999 · Cessna 310 · Engine Oil CoolerSDR 20000712SH036Cooler · leakingPART BEGAN LEAKING DURING NORMAL SERVICE DUE TO EPOXY REPAIR FAILURE. SUBMITTER RECOMMENDED ELIMINATING USE OF EPOXY REPAIR ON AND IN OIL COOLERS AS EPOXY REPAIR FAILURE IS VERY COMMON WHEN USED ON OIL COOLERS. (X)Jun 9, 1999 · Cessna 310 · Engine Oil CoolerSDR 99ZZZX2633Torque Tube · wornUPON INSPECTION, FOUND BOTH FUEL SELECTOR TORQUE TUBE ASSEMBLIES, PN 0820000-5 AND PN 0812000-13, SUFFERED SEVERE WEAR. TUBE, PN 082000-5, WORN AT FUSELAGE GROMMET AREA AND TUBE, PN 0812000-13, WORN AT BULKHEAD WL 557.50 DAMAGE TO TUBES, WAS ONLY DETECTABLE UJun 1, 1999 · Cessna 310 · Fuel Selector/Shut-Off ValveSDR 99ZZZX2397Tube · failedUPON LANDING TOUCHDOWN AT YIP, THE LEFT MLG COLLAPSED. INVESTIGATION SHOWED A FAILURE OF THE LT MAIN GEAR DRIVE TUBE ASSY WHICH PREVENTED THE LEFT MAIN GEAR FROM LOCKING DOWN AFTER EXTENSION WAS SELECTEDMay 9, 1999 · N4846B · Cessna 310 · Landing Gear Retraction/Extension SystemSDR CA981116006Control Cable · frayed(CAN) ELEVATOR CABLE FOUND FRAYED DOWN CENTER JUST FORWARD OF THE THE REAR SPAR AT THE PULLEY AND THE ELEVATOR TRIM CABLE FRAYED DOWN CENTER BEHIND THE REAR SPAR, UNDER MIDDLE SLATS AT THE FAIRLEAD.Oct 15, 1998 · Cessna 310 · Elevator Control SystemSDR 98ZZZX229Idler Bellcrank · failedPILOT AND 1 PASSENGER DEPARTED ON A LOCAL VFR FLIGHT. UPON RETRACTING LANDING GEAR, PILOT HEAR A LOUD THUMP AND AT THE SAME TIME, FELT A THUD UNDER HIS FEET. THE LANDING GEAR UP INDICATION NEVER ILLUMINATED. PILOT CHECKED TIP-TANK MIRRORS AND CONFIRMED THEJan 1, 1998 · N5332A · Cessna 310 · Landing Gear Retraction/Extension SystemSDR EY2R9601087Blade · corrodedBLADE, SN C41944YS, FOUND CORRODED.Oct 1, 1996 · Cessna 310 · Propeller Blade SectionSDR EY2R9601086Hub · corrodedHUB FOUND CORRODED.Oct 1, 1996 · Cessna 310 · Propeller Hub SectionSDR EY2R9601085Blade · corrodedBLADE FOUND CORRODED.Oct 1, 1996 · Cessna 310 · Propeller Blade SectionSDR EY2R9601033Blade · corrodedBLADE, SN B29888YS, FOUND CORRODED.Oct 1, 1996 · Cessna 310 · Propeller Blade SectionSDR EY2R9601032Blade · corrodedBLADE, SN C30806YS, FOUND CORRODED.Oct 1, 1996 · Cessna 310 · Propeller Blade SectionSDR EY2R9600136Hub · crackedHUB CRACKED IN BLADE SOCKETOct 1, 1996 · Cessna 310 · Propeller Hub SectionSDR EY2R9600117Blade · crackedBLADE NR1 SOCKET CRACKEDOct 1, 1996 · Cessna 310 · Propeller Blade SectionSDR CA961007005Piston Rod · broken(CAN) ROD FAILURE AT CRANKSHAFT, ROD BROKE IN HALF. ROD EXITED THROUGH TOP OF CRANKCASE REAR LEFT SIDE.Sep 19, 1996 · Cessna 310 · Reciprocating Engine Power SectionSDR EY2R9601064Nut · corrodedNUT CORRODED.Sep 1, 1996 · Cessna 310 · Propeller AssemblySDR EY2R9601063Retain Bearing · corrodedRETAIN BEARING FOUND CORRODED.Sep 1, 1996 · Cessna 310 · Propeller AssemblySDR EY2R9601575Hub · damagedPROP HUB STAKING PIN HOLE TOO DEEPJul 1, 1996 · Cessna 310 · Propeller Hub SectionSDR EY2R9601574Hub · mis drilledNR1 SOCKET, STAKNG PIN DRILLED WRONGJul 1, 1996 · Cessna 310 · Propeller Hub SectionSDR EY2R9600100Hub · crackedHUB CRACKED IN NR2 SOCKETJul 1, 1996 · Cessna 310 · Propeller Hub SectionSDR EY2R9600099crackedHUB CRACKED IN THREAD AREAJul 1, 1996 · Cessna 310 · Propeller Hub SectionSDR EY2R9600748Hub · corrodedHUB FOUND CORRODED.Jun 1, 1996 · Cessna 310 · Propeller Hub SectionSDR EY2R9600732Blade · corrodedBLADE, SN F75090YS, FOUND CORRODED.Jun 1, 1996 · Cessna 310 · Propeller Blade SectionSDR EY2R9600731Blade · corrodedBLADE, SN K76877YS, FOUND CORRODED.Jun 1, 1996 · Cessna 310 · Propeller Blade SectionSDR EY2R9600730Blade · corrodedBLADE, SN K76239YS, FOUND CORRODED.Jun 1, 1996 · Cessna 310 · Propeller Blade SectionSDR EY2R9600729Blade · corrodedBLADE, SN K76240YS, FOUND CORRODED.Jun 1, 1996 · Cessna 310 · Propeller Blade SectionSDR EY2R9600728Blade · corrodedBLADE, SN K76165YS, FOUND CORRODED.Jun 1, 1996 · Cessna 310 · Propeller Blade SectionSDR EY2R9600727Blade · corrodedBLADE, SN BG348YS, FOUND CORRODED.Jun 1, 1996 · Cessna 310 · Propeller Blade SectionSDR EY2R9600726Blade · corrodedBLADE, SN BG409YS, FOUND CORRODED.Jun 1, 1996 · Cessna 310 · Propeller Blade SectionSDR EY2R9600725Blade · corrodedBLADE, SN BF119YS, FOUND CORRODED.Jun 1, 1996 · Cessna 310 · Propeller Blade SectionSDR EY2R9600724Blade · corrodedBLADE, SN BD1015YS, FOUND CORRODED.Jun 1, 1996 · Cessna 310 · Propeller Blade SectionSDR EY2R9600723Blade · corrodedBLADE, SN BD1029YS, FOUND CORRODED.Jun 1, 1996 · Cessna 310 · Propeller Blade SectionSDR EY2R9600722Hub · corrodedHUB FOUND CORRODED.Jun 1, 1996 · Cessna 310 · Propeller Hub SectionSDR EY2R9600721Hub · corrodedHUB FOUND CORRODED.Jun 1, 1996 · Cessna 310 · Propeller Hub SectionSDR EY2R9600720Hub · corrodedHUB FOUND CORRODED.Jun 1, 1996 · Cessna 310 · Propeller Hub SectionSDR EY2R9600716Hub · corrodedHUB FOUND CORRODED.Jun 1, 1996 · Cessna 310 · Propeller Hub SectionSDR EY2R9600715Hub · corrodedHUB FOUND CORRODED.Jun 1, 1996 · Cessna 310 · Propeller Hub SectionSDR EY2R9600714Nut · corrodedNUT CORRODED.Jun 1, 1996 · Cessna 310 · Propeller Assembly
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