Continental IO-470-U

Service difficulty reports · 27

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 = 'IO470U'
  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 2005FA0001244Attach Fitting · corrodedDURING THE ANNUAL INSPECTION, THE WING FITTING WAS FOUND TO BE CORRODED SO SEVERE THAT IT WAS ALMOST .2500 OF THE WAY THRU THE FITTING. PICTURES ENCLOSED THAT SHOW DAMAGE. FITTING WAS LOCATED ON THE LT SIDE, AFT TOP FITTING. (K)May 16, 2005 · N700MA · Cessna 310J · Fuselage, Wing Attach FittingsSDR 310EESupport Bracket · brokenRH LANDING GEAR COLLAPSED ON LANDING. FOUND THAT THE UPPER BELLCRANK BRACKETT P/N 0811303-1 WHICH SUPPORTS AND GUIDES THE RT MAIN LANDING GEAR PUSH/PULL TUBES FROM GEAR BOX TO GEAR ASSEMBLY SEPERATED FROM BULKHEAD DUE TO MOUNTING RIVET FAILURE. THIS SEPERATIONAug 8, 2003 · N310EE · Cessna 310J · Fuselage Miscellaneous StructureSDR AUS20020003Door · misinstalled(AUS) EMERGENCY EXIT INCORRECTLY INSTALLED. ONLY TWO OF THREE LATCHING PINS ENGAGED. EMERGENCY RELEASE CABLE LOOPED AND THE TWO LATCHING PINS WERE FITTED BACKWARDS. IT WOULD HAVE BEEN IMPOSSIBLE FOR THE EMERGENCY EXIT TO BE RELEASED.Jan 2, 2002 · Cessna 310L · Emergency ExitsSDR 20010412CW009Cylinder · leakingAIRCRAFT LANDED. OIL LEAKING FROM LEFT ENGINE. INSPECTION REVEALED NR 4 CYLINDER VALVE COVER BROKEN DUE TO VALVE ROCKER ASSEMBLY BROKEN FROM CYLINDER BOSS. PROBABLE CAUSE STUCK VALVE OR METAL FATIGUE AT BOSS.Mar 1, 2001 · N515HW · Cessna 310J · Reciprocating Engine Cylinder SectionSDR CA001005010Downlock · misaligned(CAN) - RIGHT GEAR COLLAPSED AFTER LANDING. DOWNLOCK FOUND MISADJUSTED (TOO SHORT). DOWNLOCK BELLCRANK, SIDE BRACE LINK REPLACED. DOWNLOCK READJUSTED. (X)Apr 9, 2000 · Cessna 310J · Landing Gear Retraction/Extension SystemSDR CA990318038Window · separated(CAN) AFTER T/F EMERGENCY WINDOW DEPARTED AIRCRAFT. UPON FURTHER INVESTIGATION, THE WINDOW SEPARATED FROM THE FRONT AND PROCEEDED TO PEEL BACKWARDS. THE EMERGENCY CABLE WAS NOT PULLED. THE REAR LOCKING PINS WERE BENT AND THE WINDOW TABS WERE RIPPED FROM THEFeb 23, 1999 · Cessna 310J · Emergency ExitsSDR 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 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 AU980422Bulkhead · cracked(AUS) FORWARD FUSELAGE BULKHEAD AND BRACKET AT LOCATED AT STN 27.25 CRACKED. BULKHEAD SUPPORTS THE PULLEYS FOR THE NOSE WHEEL STEERING CABLE. PART TC: 6,445.Apr 9, 1998 · Cessna 310L · Fuselage Main, BulkheadSDR AU971345Control · jammed(AUS) AILERON CONTROL SYSTEM JAMMED. EVIDENCE OF FOD LODGED BETWEEN CHAIN AND SPROCKET.Oct 16, 1997 · Cessna 310Q · Aileron Control SystemSDR AU970682Electrical Sys · faulty(AUS) AIRCRAFT EXPERIENCED ELECTRICAL PROBLEMS. FIBREGLASS PROTECTIVE SHIELD OVER LH AND RH FIELD FUSES ON THE LH FIREWALL HAD CHAFED THROUGH THE LH ALTERNATOR FIELD CABLE. PERSONNEL/MAINTENANCEERRORJun 19, 1997 · Cessna 310L · Electrical Power SystemSDR AU970688Cylinder · damaged(AUS) NO2 AND NO6 CYLINDERS DAMAGED BY INGESTION OF SEPARATED ALTERNATE AIR DOOR BRACKET. PERSONNEL/MAINTENANCE ERROR.Jun 19, 1997 · Cessna 310L · Reciprocating Engine Cylinder SectionSDR AU970689Bracket · separated(AUS) ENGINE ALTERNATE AIR DOOR BRACKET SEPARATED AND INGESTED INTO ENGINEJun 19, 1997 · Cessna 310L · Engine Air Intake SystemSDR AU970690Nut · loose(AUS) ENGINE MIXTURE CONTROL CABLE OUTER SHEATH NUT NOT ATTACHEDJun 19, 1997 · Cessna 310L · Mixture ControlSDR AU970691Alternator · inoperative(AUS) ALTERNATOR EMERGENCY FIELD SYSTEM INOPERATIVE. SEE MDR 97/0682FOR ADDITIONAL INFORMATION.Jun 19, 1997 · Cessna 310L · DC Generator-AlternatorSDR AU970692Diode · inoperative(AUS) BATTERY MASTER SYSTEM DIODE INOPERATIVE.Jun 19, 1997 · Cessna 310L · Battery/Charger SystemSDR AU970693Mount · worn(AUS) RH ENGINE RH REAR ENGINE MOUNT LANDS WORN EXCESSIVELY. SEE MDR97/0685 FOR DEFECT ON RH ENGINE LH REAR MOUNT FAILUREJun 19, 1997 · Cessna 310L · Engine Mount SectionSDR AU970428Striker · cracked(AUS) RH MAIN LANDING GEAR MICROSWITCH STRIKER ARM CRACKED AND SEPARATED FROM SWITCHApr 26, 1997 · Cessna 310L · Landing Gear Position and WarningSDR AU970505Headset · damaged(AUS) HEADSET LEAD MELTED DUE TO SHORT CIRCUIT BETWEEN CO-PILOTS PHONEJACK AND INSTRUMENT LIGHTING WIREApr 20, 1997 · Cessna 310L · Audio Integrating SystemSDR AU970679Plate · damaged(AUS) NOSE LANDING GEAR FACE PLATE DAMAGEDMar 11, 1997 · Cessna 310L · Nose/Tail Landing Gear Attach SectionSDR AU970685Mount · broken(AUS) RH ENGINE REAR ENGINE MOUNT RUBBER BROKEN.Mar 11, 1997 · Cessna 310L · Engine Mount SectionSDR AU970686Door · loose(AUS) ENGINE ALTERNATE AIR DOOR BRACKET LOOSE AND INCORRECTLY RIGGEDMar 11, 1997 · Cessna 310L · Engine Air Intake SystemSDR AU970687Exit Door · sealed(AUS) EMERGENCY EXIT DOOR SEALED CLOSED. SEALANT HAD TO BE CUT TO ALLOW THE EXIT TO BE REMOVED. AD/GEN/37 LAST CARRIED OUT ON THE 15TH OCTOBER 1996. PERSONNEL/MAINTENANCE ERROR.Mar 11, 1997 · Cessna 310L · Emergency ExitsSDR AU961083Spinner Blkhd · cracked(AUS) PROPELLER SPINNER BULKHEAD CRACKED FROM ATTACHMENT SCREW HOLES - SUSPECT CRACKS HAD EXISTED FOR SOME TIME - INVESTIGATION FOUND THAT THE DOUBLER ASSEMBLY PNO 0895008-4 HAD NOT BEEN FITTED - PERSONNEL/MAINTENANCE ERRORJul 31, 1996 · Cessna 310L · Propeller Spinner SectionSDR AU961082Switch · dirty(AUS) RH MAIN LANDING GEAR DOWNLOCK MICROSWITCH DIRTYJul 26, 1996 · Cessna 310L · Landing Gear Position and WarningSDR AU961081Torque Tube · failed(AUS) LH MAIN LANDING GEAR RETRACTION SYSTEM TORQUE TUBE SPLIT - INBOARD LANDING GEAR DOOR ACTUATING ROD ROD-END PNO 5045025-1MISSING FROM MLG RETRACTION LINKAGE IDLER BELLCRANK PNO 0841106-5DUE TO LOSS OF TORQUE OF THE ATTACHMENT NUTJul 18, 1996 · Cessna 310L · Landing Gear Retraction/Extension SystemSDR AU960737O-Ring · wrong part(AUS) PROPELLER CONTAINED THE FOLLOWING FAULTS:- 1. INCORRECT RETENTION NUT 'O' RINGS FITTED2. RETENTION NUT NOT TORQUED 3. NO MOLY KOTE LUBRICANT ON FERRULE THREADS OR BLADE THREADS4. OLD TYPE PRESSURE LATCH STILL FITTED - SHOULD HAVE BEENREPLACED WITH LATESTMay 24, 1996 · Cessna 310L · Propeller Assembly
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