Continental O-470 series
Service difficulty reports · 138
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 = 'O470' 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.
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 = 'O470' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR AUS20020764Connector · deteriorated(AUS) FLEXIBLE FUEL LINE CONNECTORS PERISHED.SDR AUS20020697Structure · corroded(AUS) BOTH HORIZONTAL STABILISER AND FIN CONTAINED EXTENSIVE SURFACECORROSION.SDR 2002FA0000833Intake Valve · failedTHIS ENGINE WAS OVERHAULED 6/10/99 BY REPAIR STATION, IT NOW HAS 563 HOURS AND ALL THE INTAKE VALVES WERE BAD, ALL EXHAUST GUIDES WERE BAD, AND ALL LIFTERS ARE BAD. CYLINDERS WERE NEW FROM PARTS MFG AND SUPPLY. THIS AIRCRAFT HAS NOT SET FOR OVER 1 MONTH AT ASDR 2002FA0000834Guide · failedTHIS ENGINE WAS OVERHAULED 6/10/99 BY REPAIR STATION. IT NOW HAS 563.3 HOURS AND ALL THE INTAKE VALVES WERE BAD, ALL EXHAUST GUIDES WERE BAD, AND ALL LIFTERS ARE BAD. CYLINDERS WERE NEW FROM PARTS MFG AND SUPPLIER. THIS AIRCRAFT HAS NOT SET FOR OVER 1 MONTH SDR 2002FA0000835Lifter · failedTHIS ENGINE WAS OVERHAULED 6/10/99 BY REPAIR STATION. IT NOW HAS 563.3 HOURS AND ALL THE INTAKE VALVES WERE BAD, ALL EXHAUST GUIDES WERE BAD, AND ALL LIFTERS ARE BAD. CYLINDERS WERE NEW FROM PARTS MFG AND SUPPLY. THIS AIRCRAFT HAS NOT SET FOR OVER 1 MONTH ASDR 2002FA0000836Lifter · failedTHIS ENGINE WAS OVERHAULED 6/10/99 BY REPAIR STATION. IT NOW HAS 563.3 HOURS AND ALL THE INTAKE VALVES WERE BAD, ALL EXHAUST GUIDES WERE BAD, AND ALL LIFTERS ARE BAD. CYLINDERS WERE NEW FROM PARTS MFG AND SUPPLY. THIS AIRCRAFT HAS NOT SET FOR OVER 1 MONTH ASDR AUS20020657Alternator · faulty(AUS) ALTERNATOR SUSPECT FAULTY. INVESTIGATION FOUND THAT ALTERNATORWINDINGS HAD SHORT CIRCUITED.SDR CA020430003Rib · failed(CAN) RT WING STA 172.00 - DURING INSTALATION OF AUXILIARY WING TANKS, AN INSPECTION ACCESS HOLE WAS CUT IN LOWER RING SKIN AT STA. 169.00 SURVEILLANCE INSPECTON OF THE WING RIB AT STA 172.00 REVEALED AN EXTENSIVE COMPRESSION FAILURE ALONG THE ENTIRE LENGTH OSDR 2002FA0000589Air Box · crackedSEVERAL CRACKS IN HOUSING, BOTH IN ALUMINUM AND STAINLESS STEEL. SERVICEABLE PART INSTALLED ABOUT 375 HOURS OPERATING TIME. SUGGEST MORE ATTENTION BE GIVEN THIS ITEM AND THE WAY IT IS ATTACHED, FOR SECURITY. HIGH VIBRATION AREA. CHECK PROPELLER FOR BALANCESDR EVC2002F00000Connecting Rod · brokenNR 1 CONNECTING ROD BOTS BROKEN.SDR AUS20020087Blade · misrepaired(AUS) INSPECTION OF PROPELLER WHEN RECEIVED FOR REPAIR FOUND THAT THE BLADE THREADS HAD BEEN TRUNCATED TO COMPLY WITH AD/PMC/24/3 BUT HAD NOT BEEN SHOT PEENED. THE RETENTION NUTS DID NOT HAVE THE O-RING GROOVE WIDENED AS LISTED IN SL 1990-2. AD/PMC/41HAD NOT BSDR AUS20020015Impulse Coupling · worn(AUS) MAGNETO IMPULSE COUPLING FLYWEIGHTS WORN BEYOND LIMITS.SDR 2002FA0000088Handle · strippedWHILE INVESTIGATING A COMPLAINT OF A DEFECTIVE DOOR LATCH IT WAS DISCOVERED THAT THE INTERNAL SPLINES OF THE DOOR HANDLE WERE STRIPPED.SDR 2002FA0000443Rheostat · shortedFLYING LOW THRU MOUNTAIN PASS, TRIED TO TURN ON INSTRUMENT LIGHTS. MUCH SMOKE IN CABIN, TURNED OFF MASTER. FOUND RESISTOR WINDINGS FAILED, CONTACT ARM BURNED THRU TO CASE, ALSO CIRCUT BREAKER DID NOT OPEN. FOUND PLASTIC TRIM PANEL HOLE HAD EGG SHAPE, BUTTOSDR 2002FA0001052Rheostat · shortedFLYING LOW THROUGH A MOUNTAIN PASS TRIED TO TURN ON INSTRUMENTS LIGHTS. SMOKE IN CABIN. TURNED OFF MASTER. FOUND RESISTOR WINDINGS FAILED. CONTACT ARM BURNED THRU TO CASE. ALSO CIRCUIT BREAKER DID NOT OPEN.SDR FGQ2001F00000Fitting · corrodedINSPECTION OF LEFT WING ASSEMBLY REVEALED SEVERE EXFOLIATION CORROSION OF WING ATTACH FITTING (FWD) EXTENDING, APPROXIMATELY 18 INCHES OUTBOARD WING SKIN WAS LIFTED UP FROM SPAR.SDR 2001FA0000656Idler Gear · crackedRELEVANT INDICATION. (CRACK)SDR HYI2002F00009Master Switch · failedON PRE-FLIGHT INSPECTION, AVIONICS MASTER SWITCH FAILED. MAINTENANCE REPLACED SWITCH AND RETURNE AIRCRAFT TO SERVICE.SDR 2001F00248Detector · inoperativeUPON INSTALLING NEW LIFT DETECTION NOTED THAT WHEN WIRED AS ORIGINALLY REMOVED FROM AIRCRAFT, WITH HEAT TURNED ON, DETECTION WAS INOPERATIVE. GROUND FOR HEATER WAS INSTALLED ON COMMON FOR DETECTION; CAUSING A NO POTENTIAL WHEN HEATER TURNED ON.SDR 2001FA0000229Detector · inoperativeUPON INSTALLING NEW LIFT DETECTION, NOTED THAT WHEN WIRED AS ORIGINALLY REMOVED FROM AIRCRAFT, WITH HEAT TURNED ON, DETECTION WAS INOPERATIVE. GROUND FOR HEATER WAS INSTALLED ON COMMON FOR DETECTION; CAUSING A NO POTENTIAL WHEN HEATER TURNED ON.SDR 2001FA0000108Hose · disintegratedCUSTOMER REPORTED LOW VACUUM INDICATION BUT GYROS RUNNING OK. INITIAL INVESTIGATION ALL HOSES LOOKED OK, HOWEVER WHEN HOSES WERE TOUCHED, FELL APART. THE ABOVE REFERENCED PN IS FOR ONE OF THE VACUUM GAUGE HOSES, HOWEVER ALL INSTRUMENT HOSE WERE OF THE SAME TSDR CA011116016Tail Wheel · separated(CAN) AFTER TAKEOFF FROM ROUGH STRIP ON HERSEL ISLAND, PILOT HEARD LOUD BANGING SOUND. HE WAS ABLE TO SEE TAIL WHEEL MISSING. ON LANDING AT AKLAVIK, STEERING CONTROL LOST. MINOR DAMAGE TO TAIL STRINGER. NEW TAIL WHEEL ASSEMBLY INSTALLED WITH PROPER AIRCRAFT BSDR 20010418CW001Gyro · inoperativeDURING ROUTINE ANNUAL INSPECTION THE ELEVATOR WAS FOUND TO TRAVEL ONLY 19 DEGREE UP. THE TYPE CERTIFICATE CALLS FOR 25 DEGREE. INVESTIGATION FOUND THE D. G. MOUNTED DIRECTLY ABOVE THE CONTROL WHEEL TUBE. AS THE WHEEL WAS PULLED AFT THE AN3-10A BOLT CONTACTESDR 20010418CW004Wire · damagedTHE BATTERY CABLE WAS BARE IN MANY PLACES INCLUDING THE PENETRATION OF THE FIREWALL. IT HAD ALSO BEEN PENETRATED BY A SCREW THROUGH THE BELLY OF AIRCRAFT, JUST FORWARD OF THE BATTERY BOX.SDR 20010507CW001Separator · contaminatedOIL FILTER INSPECTION REVEALED EXCESSIVE AMOUNT OF CONTAMINATION. INVESTIGATION REVEALED AIR/OIL SEPERATOR INTERNAL SCREEN COMING APART. YEARS OF VIBRATION MAY HAVE CAUSED SCREEN SEPARATION. FACTORY RECOMMENDS 100 HOURS CLEANING. THERE IS NO WAY TO INSPECTSDR 20010416CW017Volt Regulator · failedVOLTAGE REGULATOR WAS INSTALLED, AIRCREW SQUAWKED LOW VOLTAGE WARNNG LIGHT REMAINED ON AT ALL POWER SETTINGS. TROUBLESHOOTING DETERMINED OUTPUT VOLTAGE WAS BELOW MINIMUM OUTPUT AND ERRATIC. VISUAL INSPECTION OF THE REGULATOR INDICATED NO SIGNS OF EXTERIOR DESDR 20010416CW007Bulkhead · crackedWHILE PERFORMING A PRE PURCHASE LOOKOVER, FOUND A STOP DRILLED CRACK IN THE UPPER RADIUS ABOVE THE LEFT RUDDER STOP BOLT. FURTHER INSPECTION FOUND ANOTHER CRACK RADIATING OUTWARD FROM THE UPPER OUTBOARD EDGE OF THE UPPER RIGHT LIGHTENING HOLE.SDR 20010424CW009Bulkhead · crackedWHILE PERFORMING 100 HOUR INSPECTION, FOUND A CRACK IN THE UPPER RADIUS ABOVE THE RIGHT RUDDER STOP BOLT. PROBABLE CAUSE WOULD BE FROM THE RUDDER CONTACTING TOO HARD, POSSIBLE WIND DAMAGE. RECOMMED A SOFT HEADED STOP BOLT.SDR 20010502CW004Skin · damagedDURING A POST FLIGHT INSPECTION, A 10.25 INCH TEAR IN THE LEFT FLAP UPPER SKIN. TRAILING EDGE WAS DISCOVERED. THE UPPER AND LOWER FLAP SKIN TRAILING EDGES SHOWED EVIDENCE OF NEW CRACKS AROUND THE RIVETS IN THE TRAILING EDGE BEYOND THE DAMAGED SECTION. THE SDR 20000329SH038Spring · damagedNEW PARTS HAVE FINGER PRINTS ON THEM. PARTS ARE NEW, NOT REMOVED FROM MANUFACTURER''''S BAG SINCE TIME OF BAGGING AT SUPPLY CENTER. SUBMITTER STATED PROBLEM IS SPRING STEEL WITH SWEAT FROM THE PERSONS WORKING ON THE PART.SDR AU990053Mount · cracked(AUS) ENGINE MOUNT CRACKED AS INDICATED IN AD/CESSNA180/4 AMDT1. PART TC: 1,880.SDR AU970142Crankcase · cracked(AUS) CRANKCASE NO2 MAIN BEARING SUPPORT CRACKED - EVIDENCE OF MAIN BEARING SADDLE FRETTING - FOUND DURING BULK STRIP FOLLOWING PROPELLER STRIKESDR 97ZZZX415Gasket · deterioratedUPON USING A NEW SERIES VALVE COVER GASKET 653191D, FOUND THAT ALL OF THE GASKETS RECEIVED FROM THE VENDOR LEAKED. ALL OF THE GASKETS WERE FOUND TO DEVELOP AN AREA WHERE THE GASKET WAS LITERALLY FALLING APART. THERE DID NOT APPEAR TO BE ANY LONG FIBER MATERISDR 95ZZZX3508Rotor Coil · failedSUPERIOR AIR PARTS VALVE ROTOR FAILED. NR 6 CYLINDER EXHAUST VALVE POSITION CAUSING ENGINE METAL CONTAMINATION.SDR 95ZZZX3509Rotor Coil · failedSUPERIOR AIR PARTS VALVE ROTOR FAILED. NR 2 CYLINDER EXHAUST VALVE POSITION CAUSING ENGINE METAL CONTAMINATION.SDR 95ZZZX3517Rotor Coil · failedSUPERIOR AIR PARTS VALVE ROTOR FAILED. NR 3 CYLINDER EXHAUST VALVE POSITION CAUSING ENGINE METAL CONTAMINATION.SDR 95ZZZX5642Tube · dislocatedDURING WILDLIFE SURVEY, ENGINE BECAME ROUGH AND WAS SHUT DOWN. AIRCRAFT LANDED ON RIVER LEVEE. CARBURETOR TO MANIFOLD TUBE HAD BECOME DISLODGED. REPLACED TUBE, ENGINE FUNCTIONED NORMALLY. THIS AIRCRAFT FUEL SYSTEM IS GRAVITY FLOW AND IS PLACARDED TO TURN OSDR 95ZZZX2715Adapter · defectiveWHEN INSPECTING FILTER ADAPTER IAW SEB 93-1R1A, FOUND FRETTING OF THE MOUNTING THREADS. THIS RENDERED THE ADAPTER UNAIRWORTHY. ADAPTER REPLACED WITH NEW UNIT.
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