Continental IO-470-V

Service difficulty reports · 23

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 engine_model_key = 'IO470V'
  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 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 2009FA0000746Cylinder Head · brokenCYLINDER HEAD SEPARATED FROM BARREL.Aug 24, 2009 · N316RA · Cessna 310Q · Reciprocating Engine Cylinder SectionSDR AU510001703Bellcrank · shearedNOSE LANDING GEAR IDLER BELLCRANK SHEARED AT THE TWO BOLT HOLES FOR THE FORWARD AND AFT PUSH-PULL TUBES. SUSPECT CAUSED BY WORN UPLOCK.Dec 12, 2005 · Cessna 310Q · Nose/Tail Landing GearSDR AU510002117Clamp · failedNR 2 PROPELLER BLADE COUNTERWEIGHT CLAMP FAILED.Dec 12, 2005 · Cessna 310K · Propeller Blade SectionSDR 2005FA0000890Cylinder · crackedFOUND CASE CRACKED BEYOND REPAIR AT NR 1 CYLINDER, FOUND 2 THRU BOLTS SHEARED AND 5 CYLINDER STUDS BROKEN ON NR 1 CYLINDER. THRU BOLTS DEFECTIVE CAUSING A CHAIN REACTION IN SHEARING CYLINDER STUDS. SINCE CYLINDER WAS NO LONGER SEATED SQUARELY TO THE CASE, THJun 1, 2005 · N1249G · Cessna 310Q · Reciprocating Engine Cylinder SectionSDR AUS20040134Torque Tube · broken(AUS) LT MAIN LANDING GEAR TORQUE TUBE BROKEN.Jan 14, 2004 · Cessna 310Q · Landing Gear Retraction/Extension SystemSDR 2003F00331Screw · brokenON LANDING ROLLOUT AT 30 KNOTS, THE RIGHT MAIN LANDING GEAR COLLAPSED CAUSING RIGHT PROP TO STRIKE THE GROUND. THE ADJUSTMENT SCREW PN 0841111-1 BROKE. A SPAS PN QUERY SHOWED NO OTHER ACCIDENTS OR INCIDENTS.May 29, 2003 · N589DM · Cessna 310Q · Main Landing Gear Attach SectionSDR 2003F00103Line · failedFULE LEAK IN COCKPIT, PILOT DECLARED EMERGENCY AND RETURNED TO FARMINGTON, NM AIRPORT. RIGHT FUEL FLOW GAUGE INDICATION WENT TO ZERO. REMOVED AND REPLACED RIGHT FUEL FLOW GAUGE PRESSURE LINE P/N CM2944-2-18.Dec 20, 2002 · N591DM · Cessna 310Q · Fuel Flow IndicatingSDR 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 CA000928019Rack · chafed(CAN) UPON PERFORMING FLAIR DURING LANDING, THE PILOTS NOTICED THE ELEVATOR CONTROLS WERE FEELING A LITTLE STIFF. UPON MAINTENANCE INVESTIGATION, FOUND THE RADIO IN THE CENTER INSTRUMENT PANEL (RADIO RACK) WERE SETTING DOWN AND MAKING CONTACT WITH THE CONTROLAug 30, 2000 · Cessna 310L · Instrument PanelSDR CA990915072Camshaft · spalling(CAN) SEVERE SPALLNG OF REAR CAM LOBE.Sep 9, 1999 · Cessna 310Q · Reciprocating Engine Power SectionSDR AU990444Trunnion · cracked(AUS) NOSE LANDING GEAR TRUNNION CRACKED IN ONE PIVOT AS INDICATED IN AAC1-108.Apr 16, 1999 · Cessna 310Q · Nose/Tail Landing Gear Attach SectionSDR AU971627Rod End · seized(AUS) RH NOSE LANDING GEAR DOOR RETRACTION RODEND BROKEN. DOOR CAUGHT THE NOSE GEAR DURING RETRACTION AND JAMMED THE NLG HALFWAY UP.RODEND BEARING PARTIALLY SEIZED DUE TO LACK OF LUBRICATION.Dec 13, 1997 · Cessna 310Q · Landing Gear Door Retract 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 AU970274Cylinder · worn(AUS) ENGINE CYLINDER (PNO 649168CEA3) BORES WORN BEYOND LIMITS - CYLINDERS ARE CERMICHROME TYPEMar 21, 1997 · Cessna 310N · Reciprocating Engine Cylinder SectionSDR AU970266Propeller · faulty(AUS) LH PROPELLER SUSPECT OUT OF BALANCE - LH ENGINE FORWARD ENGINE MOUNT LOOSE - INVESTIGATION FOUND PROBLEM CAUSED BY BLADE ANGLES AND PROFILESMar 19, 1997 · Cessna 310Q · Propeller AssemblySDR AU970371Blade · faulty(AUS) INCORRECT PROPELLER BLADES FITTED TO PROPELLER - BLADES FITTED ARE NOT THE BLADES LISTED IN THE LOG BOOK - REDUCED DIAMETER PROPELLER FITMENT NOT RECORDED - PROPELLER BLADE ANGLES VARIED BETWEEN BLADES - BLADE PROFILE INCORRECT - NO2 BLADE ACTUATING PIN Mar 19, 1997 · Cessna 310Q · Propeller Blade SectionSDR 97ZZZX1244Pump · shaft shearedRIGHT ENGINE FUEL PUMP FAILED DURING FLIGHT. BOOST PUMP WOULD NOT RUN AND ENGINE STOPPED, UNEVENTFUL LANDING WAS MADE. FOUND FUEL PUMP DRIVESHAFT SHEARED. FOUND BOOST PUMPS WOLD PRIME ENGINE AND ALLOW ENGINE TO RUN, BUT WOULD NOT RUN IN HIGH OR LOW BOOST PUMar 11, 1997 · N7872Q · Cessna 310Q · Engine Fuel PumpSDR 97ZZZX1245Switch · dirtyRIGHT ENGINE FUEL PUMP FAILED DURING FLIGHT. BOOST PUMP WOULD NOT RUN AND ENGINE STOPPED, UNEVENTFUL LANDING WAS MADE. FOUND FUEL PUMP DRIVESHAFT SHEARED. FOUND BOOST PUMPS WOLD PRIME ENGINE AND ALLOW ENGINE TO RUN, BUT WOULD NOT RUN IN HIGH OR LOW BOOST PUMar 11, 1997 · N7872Q · Cessna 310Q · Fuel Boost PumpSDR AU961152Retention Nut · loose(AUS) NO3 PROPELLER BLADE RETENTION NUT LOOSE AND LOCK PLUGS MISSING - SUSPECT RETENTION NUT UNDERTORQUED - PERSONNEL/MAINTENANCE ERRORAug 15, 1996 · Cessna 310Q · Propeller Blade SectionSDR AU960829Rib · mis mfg(AUS) LH WING END RIB NOT RIVETTED TO THE MAIN SPAR - SUSPECT RIVETS NOT INSTALLED AT MANUFACTUREJun 6, 1996 · Cessna 310Q · Wing, Rib/BulkheadSDR AU960777Cylinder · separated(AUS) RH ENGINE NO5 CYLINDER HEAD SEPARATED FROM BARREL - SUSPECT PRE-EXISTING CRACKJun 3, 1996 · Cessna 310Q · Reciprocating Engine Cylinder SectionSDR AU960503Exhaust Valve · leaking(AUS) ENGINE COMPRESSION LEAKAGE FROM EXHAUST VALVES ON ALL 6 CYLINDERS- FOUND DURING COMPRESSION CHECK IAW AD/ENG/4 AMDT 5 - ENGINECALENDER TIME SINCE OVERHAUL WAS 19 YEARSApr 16, 1996 · Cessna 310J · Reciprocating Engine Cylinder Section
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