Cessna 310K

Service difficulty reports · 30

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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 = '310K'
  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 2023FA0000199Flow Divider · perforatedTHE FLOW DIVIDER ON TOP OF THE ENGINE AT THE SPINE HAS A SMALL COMPENSATION HOLE ABOVE THE DIAPHRAGM. IF THE DIAPHRAGM HAS A PERFORATION, RAW FUEL WILL RISE ABOVE THE DIAPHRAGM AND SPEW FROM THIS HOLE AND THUS CAUSE AND EXTREME FIRE HAZARD. I HAVE OBSERVED THIApr 6, 2023 · N6922L · Cessna 310K · Engine Fuel and ControlSDR 2023FA0000180Fairing · unknownSCREW TO HOLD FAIRING BETWEEN WING AND TIP TANK TOO LONG AND POSSIBLE PENETRATING / RUBBING ON FUEL TANK. THE INNER AERODYNAMIC FAIRING BETWEEN TIP TANK AND UPPER SURFACE OF WING HAS A TINNERMAN NUT PLATE TO CONNECT TO ANOTHER FAIRING. SCREWS IN THIS NUT PLATEMar 29, 2023 · N6922 · Cessna 310K · Standard Practices/StructuresSDR 2018FA0000111Idler Assy · brokenARM ASSY BELLCRANK IDLER BROKEN WHERE TUBE ASSY GEAR MAIN DRIVEIS BOLTED TO THE BELLCRANK.Mar 20, 2018 · Cessna 310K · Landing Gear Retraction/Extension SystemSDR 2015FA0000102Truss · corrodedAFTER LANDING, LT MLG STRUT WAS DISCOVERED TO BE FLAT. INITIAL INSPECTION REVEALED THAT THE SCHRADER VALVE HAD FAILED, BUT AFTER VALVE REPLACEMENT, THE STRUT WOULD STILL NOT REMAIN INFLATED. FURTHER INSPECTION REVEALED THAT THE STRUT WAS ALSO LEAKING FROM THMar 22, 2015 · N3826X · Cessna 310K · Main Landing Gear Strut/Axle/TruckSDR 2014FA0000670Throttle Cable · failedLEFT THROTTLE CABLE SEPARATED FROM STATIONARY SWEDGE IN THE ENGINE COMPARTMENT REDUCING ENGINE POWER DURING ROTATION PHASE OF A TOUCH AND GO PROCEDURE. ACFT HAD DIFFICULITY MAINTAINING A POSITIVE RATE OF CLIMB DUE TO REDUCED ENGINE POWER AND A HIGH DENSITY ALAug 27, 2014 · N101JB · Cessna 310K · Power LeverSDR 2013FA0000189Shaft · crackedINSTALLED NEW SHAFT, PN 0894000-12 ON BOTH MLG AT 3520.9 AND AT 3620.9. BOTH SHAFTS WERE CRACKED ON RT SIDE. THE NEW STYLE SHAFTS HAVE A LARGER DIAMETER ROLL PIN AND THIS HOLE IS WHERE THE CRACKS ARE STARTING FROM. THE NEW STYLE SHAFTS ARE MADE WEAKER BY HAMar 22, 2013 · N7017L · Cessna 310K · Main Landing GearSDR 2013FA0000188Shaft · crackedINSTALLED NEW SHAFT, ON BOTH MLG AT 3383.80 AND AT 3520.9 BOTH SHAFTS WERE CRACKED ON RT SIDE.Sep 27, 2012 · N7017L · Cessna 310K · Landing Gear Retraction/Extension SystemSDR 2009FA0000320Bellcrank · failedIDLER BELLCRANK FAILED DURING RETRACTION CYCLE. THIS BELLCRANK IS CAST ALLOY. IN MY OPINION IT SHOULD BE A MACHINE PART. (K)Mar 26, 2009 · N7022L · Cessna 310K · Landing Gear Retraction/Extension SystemSDR 2007FA0001072Warning System · malfunctionedAC EXPERIENCED FLAP ASYMMETRIC LIGHT IN CRUISE FLIGHT CREW DIVERTED TO ATL LIGHT WENT OUT AND FLAPS WORKED PROPERLY FOR AN UNEVENTFUL LANDING. PROBLEM COULD NOT BE DUPLICATED SO BOTH FLAP FOLLOW UPS WERE REPLACED IAW THE MM. AIRCRAFT OPS CHECK GOOD.Dec 8, 2007 · N418GJ · Cessna 310K · Trailing Flap Position Indicating SystemSDR DHL2007366001Skin · corrodedLT FUSELAGE BY LAP SEAM BULGE IN SKIN NEAR FRAME 61 AND 62 AND BETWEEN STRINGERS S-44L AND S-45L.May 30, 2007 · N366D · Cessna 310K · Fuselage Main, Plate/SkinSDR IGL032006007Strut · failedNOSE GEAR STRUT ASSEMBLY COLLAPSED DURING EITHER TAXI OR TAKEOFF. WHEN GEAR WAS RETRACTED THE NOSE FENDER CAUGHT ON THE GEAR DOOR BRACKETS. MOTOR CONTINUED UNTIL IDLER BELLCRANK BROKE. AIRCRAFT MADE AN EMERGENCY LANDING WITH THE NOSE GEAR COLLAPSED. PILOT Mar 29, 2006 · N7035L · Cessna 310K · Nose/Tail Landing Gear Strut/AxleSDR AU510002117Clamp · failedNR 2 PROPELLER BLADE COUNTERWEIGHT CLAMP FAILED.Dec 12, 2005 · Cessna 310K · Propeller Blade SectionSDR AUS20021201Beam · cracked(AUS) LH ENGINE CROSSOVER BEAM CRACKED. FURTHER INVESTIGATION FOUND THAT THE LH MOUNTS DROPPED IN MOUNT BRACKETS AND PUT OUTWARD LOAD ON THE ENGINE LONGITUDINAL BEAMS.Oct 10, 2002 · Cessna 310K · Engine Mount SectionSDR 20010413CW006Bulkhead · crackedDURING REPLACEMENT OF AIRCRAFT HEATER, DUCTING MECHANIC NOTICED THE RIGHT BULKHEAD AT STA 29.93 UNDER HEATER WAS CRACKED. REMOVED HEATER TO GAIN ACCESS TO BULKHEAD. NOTE THAT SUPPORT FOR NOSE WHEEL STEERING PULLEY IS ATTACHED TO BULKHEAD NEAR CRACK. MOVEMEMar 21, 2001 · N101JB · Cessna 310K · Fuselage Main, BulkheadSDR 20010413CW005Bulkhead · crackedDURING REPLACEMENT OF AIRCRAFT HEATER DUCTING, MECHANIC NOTICED THE RIGHT BULKHEAD AT STA 29.93 UNDER HEATER WAS CRACKED. ALSO CHECKED LEFT SIDE BULKHEAD AT STA 29.93 AND FOUND THAT BULKHEAD CRACKED IN THE SAME LOCATION. NOTE THAT SUPPORT FOR NOSE WHEEL STEMar 21, 2001 · N101JB · Cessna 310K · Fuselage Main, BulkheadSDR 20000505SH033Spinner · crackedBRAND NEW CESSNA SPINNER DOME INSTALLED ON 4-30-99. LAST INSPECTION ANNUAL ON 7/16/99. APRIL12, 2000, 100-HOUR INSPECTION REVEALS ONE INCH CRACK AT ONE MOST FORWARD SCREW. TWO SCREW HOLES ARE OVAL, NOT ROUND. TOTAL PART TIME PLUS/MINUS 120 HOURS. (X)Apr 13, 2000 · N6942L · Cessna 310K · Propeller Spinner SectionSDR 99ZZZX2148Mount · wornNEW SHOCK MOUNTS BY LORD COMPANY INSTALLED WITH ENGINE. MOUNTS SHOWED WEAR AFTER 150 HOURS (LAST MOUNTS LASTED DURATION OF ENGINE - 1,500 HOURS).May 5, 1999 · N6942L · Cessna 310K · Engine Mount SectionSDR AU990139Backplate · cracked(AUS) RT PROPELLER SPINNER BACKING PLATE FAILED. BACKING PLATE HAD CRACKED AROUND THE CIRCUMFERENCE BEND FOR APPROXIMATELY 100 DEGREES.Feb 3, 1999 · Cessna 310K · Propeller Spinner SectionSDR 20000714SH014Bellcrank · brokenRIGHT INBOARD GEAR DOOR FAILED TO CLOSE AFTER GEAR EXTENSION. (X)Feb 1, 1999 · N6942L · Cessna 310K · Landing Gear Retraction/Extension SystemSDR 99ZZZX4678Push Rods · corrodedDURING POST-CRASH EXAMINATION OF THE CONTROL SYSTEM, THE TYPICAL AILERON, ELEVATOR, AND RUDDER TRIM TAB ACTUATING RODS WERE FOUND INTERNALLY RUSTED AND CORRODED. THE TUBES HAVE ROD/FORKS ON EACH END AND APPEAR HOLLOW OR OPEN THROUGH THE FORKED END ALLOWING WASep 20, 1998 · N711CG · Cessna 310K · Elevator Tab Control SystemSDR AU981033Hub · cracked(AUS) PROPELLER HUB CRACKED THROUGH THE THREADS IN NR 2 BLADE SOCKET. CRACK LENGTH APPROXIMATELY 50.8MM (2 INCHES). CRACK DOES NOT FOLLOW THE THREADS AROUND THE SOCKET.Jul 23, 1998 · Cessna 310K · Propeller Hub SectionSDR 97ZZZX4637Magneto · defectiveDURING ANNUAL INSPECTION, NO RECORDS EXIST OF ANY MAGNETO MAINTENANCE. ALL 4 MAGS REMOVED FOR TCM 500-HOUR CHECK. THIS MAG HAD POINTS IN CONFIGURATION OF COUNTERCLOCKWISE ROTATION, SHOULD HAVE BEEN FOR CW BY P/N AND IPB. TWO MAGS HAD LOOSE BEARINGS, ALL 4 HAOct 7, 1997 · N6961L · Cessna 310K · Magneto/DistributorSDR 97ZZZX3788Bladder · mismanufacturedUNABLE TO INSTALL LT WING AUXILIARY FUEL CELLS, DUE TO INCORRECT DIMENSIONS BETWEEN CENTER OF AUX FUEL GAUGE TRANSMITTER FLANGE OPENING AND FUEL DRAIN HOSE NIPPLE. DISTANCE BTWN CENTERS OF AUX FUEL GAUGE XMITTER FLANGE OPENING AND ENG FUEL HOSE NIPPLE IS 6.31Jul 15, 1997 · Cessna 310K · Fuel StorageSDR 97ZZZX3787Bladder · mismanufacturedUNABLE TO INSTALL LT WING AUXILIARY FUEL CELLS, DUE TO INCORRECT DIMENSIONS BETWEEN CENTER OF AUX FUEL GAUGE TRANSMITTER FLANGE OPENING AND FUEL DRAIN HOSE NIPPLE. DISTANCE BTWN CENTERS OF AUX FUEL GAUGE XMITTER FLANGE OPENING AND ENG FUEL HOSE NIPPLE IS 6.31Jul 15, 1997 · Cessna 310K · Fuel StorageSDR EY2R9601342Ferrules · corrodedFERRULES CORRODED.Dec 1, 1996 · Cessna 310K · Propeller AssemblySDR EY2R9601141Blade · corrodedBLADE, SN F32834YS, FOUND CORRODED.Oct 1, 1996 · Cessna 310K · Propeller Blade SectionSDR EY2R9601140Blade · corrodedBLADE, SN F32952YS, FOUND CORRODED.Oct 1, 1996 · Cessna 310K · Propeller Blade SectionSDR EY2R9601139Blade · corrodedBLADE, SN F73319YS, FOUND CORRODED.Oct 1, 1996 · Cessna 310K · Propeller Blade SectionSDR 96ZZZX4239Gear · malfunctionedGEAR WOULD NOT EXTEND. HAND CRANKED 2-3 TURNS, THEN WAS OK. JACKED AIRCRAFT, CYCLED GEAR MANY TIMES, COULD NOT DUPLICATE.Jul 2, 1996 · N37223 · Cessna 310K · Landing Gear Retraction/Extension SystemSDR 95ZZZX2187Push-Pull Tube · damagedNOSE GEAR PUSH-PULL TUBE PROBABLY DAMAGED DURING TOWING OR HARD LANDING ON THE NOSE GEAR. THE PUSH-PULL TUBE REPLACEMENT RECEIVED FROM CESSNA AND INSTALLED INTO AIRCRAFT, APPEARS TO BE STRONGER COMPARED TO THE REMOVED PUSH-PULL TUBE.Feb 17, 1995 · N7017L · Cessna 310K · Landing Gear Retraction/Extension System
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