Continental IO-540 series
Service difficulty reports · 270
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 = 'IO540' 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 = 'IO540' 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 2004FA0000882Magneto · brokenPILOT REPORTED OIL UNDER COWLING AFTER A WEEKEND OVERNIGHT. INVESTIGATED OIL LEAK AND FOUND THE MAGNETO MOUNTING FLANGE CRACKED. MAGNETO WAS PROPERLY TORQUED, SUSPECT MAGNETO HOUSING FATIGUED.SDR LU42004F00000Flyweight · brokenGOVERNOR FAILED TO PRODUCE PRESSURE, UPON DISASSEMBLY FOUND BROKEN FLYWEIGHT DISC PN D20880, SPRING DRIVE PN C20886 DAMAGED, PN B208821, SPRING BROKEN. NOTE: NO IMPACT KNOWN PARTS SENT TO MFG FOR INSPECTION.SDR 2004FA0000518Fabric · failed5 FEET OF THE TOP RT WING FABRIC FAILED. POLYFIBER AC COATINGS TB 89-1D. STATES FABRIC WEIGHING LESS THAN 2.4 OZ SHOULD BE USED ON AC WITH ENGINES UP TO 145 HORSEPOWER THIS AC HAD A 300 HP ENGINE INSTALLED LT WING HAD BROKEN RIB STITCHING BUT FABRIC HAD NOT SDR 2004FA0000517Brace · inoperativeIN FLIGHT, AC LOST HYDR PRESSURE FOR UNRELATED CAUSE. HYDR PRESSURE NORMALLY ASSISTS L/G TO REMAIN IN DOWN AND LOCKED POSITION. ON LANDING, AC TOUCHED DOWN NORMALLY. ON ROLLOUT, NOSE LANDING COLLAPSED. LANDING GEAR SYS IS DESIGNED TO REMAIN DOWN AND LOCKEDSDR 2004F00149Control System · malfunctionedDURING A NORMAL FLIGHT AND LANDING PROCEDURE, PLACED THE GEAR SWITCH IN THE DOWN POSITION WITH NO RESPONSE. TRIED THIS SEVERAL TIMES STILL NO RESPONSE. DID A MANUAL DROP OF THE GEAR AND RECEIVED GREEN GEAR DOWN AND LOCKED LIGHTS. SET THE UNIT BACK TO COMPOSDR 2004FA0000414Wire · burnedCOCKPIT BEGAN TO FILL WITH SMOKE WHILE TAXIING FOR TAKE-OFF. AIRCRAFT WAS SHUTDOWN AND UPON INSPECTION FOUND AVIONIOCS FAN TO BE BURNT ON CORNER WHERE WIRES ENTER FAN ASSEMBLY. THE DATE STAMPED ON FAN IS NOV. 1979. SUSPECT THE AGE AND TIME IN SERVICE WOULD SDR 2004FA0000656Support · crackedOB BATTERY SUPPORT ANGLE CRACKED AT BOTH ENDS. THIS IS THE THIRD INSTANCE IN FLEET. THE BATTERY SUPPORT STRUCTURE NEEDS TO STRENGTHENED WITH ADDITIONAL STRUCTURE TO PREVENT THIS. (NM01200410074)SDR AUS20040396Shield · separated(AUS) EXHAUST SHIELD MISSING. ATTACHMENT TABS REMAINED ON EXHAUST ASSEMBLY.SDR AUS20040319Pump · leaking(AUS) AIRCRAFT MOUNTED ENGINE FUEL PUMP LEAKING.SDR 2004FA0000306Bearing · missingDURING THE ANNUAL INSPECTION, IT WAS DETERMINED THAT THE BEARING FOR THE CO-PILOT RT RUDDER BAR TO BRAKE BELLCRANK WAS MISSING. THE FACTORY TORQUE SEAL ON THE ATTACHING HARDWARE WAS UNDISTURBED.SDR IS42004F00000Tube · crackedRECEIVED HEATER CORE FROM CUSTOMER. THE COMBUSTION TUBE END PLATE HAS TWO VISUAL CRACKS. ONE AT THE TWO O’CLOCK POSITION AND ONE AT THE SEVEN O’CLOCK POSITION. THIS HEATER IS THE (FR) SERIES THAT HAS THE CERAMAKOTE COMBUSTION TUBE WITH NO AD AGAINST IT. BYSDR 2004FA0000836Receiver · malfunctionedTHIS RECEIVER WAS INSTALLED AS PART OF THE EFIS-SV SYSTEM. AFTER APPROXIMATELY 30 HOURS OF OPERATION FOLLOWING THE INSTALLATION, AN LOI MESSAGE DISPLAYED ON THE INTEGRATED DISPLAY UNIT (IDU). THE RECEIVER WAS REPLACED, AND THE ERROR MESSAGE WAS NO LONGER DISSDR 2004FA0000399Strap · crackedDURING AN ANNUAL INSPECTION THE BUTT WELDS IN THE LOWER MAIN SPAR REINFORCEMENT STRAP. APPROX 6.50 INCHES IB FROM EACH END OF THE REINFORCEMENT STRAP. DO NOT HAVE PROPER PENETRATION AND ARE CRACKED THRU THE WELD. MFG WAS CONTACTED AND REPAIR INSTRUCTIONS WERSDR LU4R349MCylinder · damagedCYLINDER (PN B-2452-1) SEPARATED FROM PROPELLER ON GROUND RUN. INSPECTION SHOWED THREAD DAMAGE OF CYLINDER. AFTER DISCUSSION WITH MFG, THE LIKELY CAUSE IS DIE TO HIGH PRESSURE FROM GOVERNOR, USUALLY CAUSED BY STICKING PRESSURE RELIEF VALVE.SDR 2004FA0000512Cylinder · damagedCYLINDER (PN B2452-1) SEPARATED FROM PROPELLER ON GROUND RUN. INSPECTION SHOWED THREAD DAMAGE OF CYLINDER. AFTER DISCUSSION WITH MANUFACTURER THE LIKELY CAUSE IS DUE TO HIGH PRESSURE FROM GOVERNOR, USUALLY CAUSED BY STICKING PRESSURE RELIEF VALVE.SDR 2004FA0000289Diaphragm · improperMATERIAL TOO THIN OR TOO SOFT. WHEN TORQUING RETAINING SCREW MATERIAL SQUEEZES OUT WITH NR 5 TORQUE. FUEL FLOW DIVIDER, BENDIX.SDR X072004F00000Actuator · inoperativePILOTS FOUND AILERON SYSTEM ROUGH ON PREFLIGHT. MECHANICS IN CHECKING OUT CAUSE, FOUND AILERON SYSTEM TO LOCKUP AND WOULD NOT FREE UP UNTIL SERVO WAS REMOVED. APPEARS BEARING IN GEAR BOX IS SLOPPY AND GEAR WILL BIND UP WHEN TURNED.SDR X6PA200400002Booster · inoperativeDURING RUNUP THE PILOT FOUND LT MAGNETO WAS INOPERATIVE. A MECHANIC INSPECTED THE AIRCRAFT AND FOUND THE SLICK START MAGNETO START BOOST BOX STC NR SA593CH MALFUNCTIONED AND GROUNDED THE LEFT MAGNETO OUT. THE MECHANIC REPLACED THE SLICK START BOX; THIS FIXED SDR 2004FA0000144Trunnion · crackedNOSE TRUNNION FOUND CRACKED AT ASSIST SPRING ATTACH BOSS. THIS WAS A NEW MFG TRUNNION WITH 16 MONTH AND 71 HOURS IN SERVICE. THE CRACK OCCURRED AT A POINT THAT IS NOT SUBJECT TO OPERATING STRESS.SDR 2003FA0001296Wire · misroutedDURING OPERATIONAL TEST OF AIRCRAFT PRIOR TO BEGINNING ANNUAL INSPECTION, FOUND WHEN RUNNING MANUAL ELECTRIC TRIM, WHILE PRESSING AND HOLDING DOWN TRIM INTERRUPT BUTTON, TRIM WOULD CONTINUE TO RUN THOUGH AT A MUCH SLOWER RATE. IF TRIM INTERRUPT SWITCH WAS HELDSDR 2004FA0000015Skin · corrodedAFTER REMOVING RT SIDE LOWER CENTER FUSELAGE EXTERIOR HAD ASSY STIFFENER AND PN 62544-01 FORWARD FAIRING TO FACILITATE OTHER REPAIRS, FOUND CONSIDERABLE CORROSION ON MOUNTING FLANGES AND ADJACENT FUSELAGE SKIN. AREA IS SUBJECT TO ENGINE EXHAUST AND MUD/DIRT, SDR 2003FA0001229Fuel Control · out of adjustPILOT, UPON TOUCHDOWN TO LANDING, HAD HIS ENGINE QUIT AND WOULD NOT START AND NEEDED A TOW IN. HE ALSO FOUND THAT HE COULD NOT ADVANCE HIS THROTTLE. INSPECTED FUEL SERVO AND FOUND PIN OUT ON THE IDLE MIXTURE SETTING. INSTALLED OLD PIN, WITH HAS HELD PARTICASDR CMR2003F00000Rod · brokenIMMEDIATELY AFTER TAKE OFF, THE PILOT NOTICED MINIMAL REACTION FROM AILERON CONTROL INPUTS. PILOT LANDED SAFELY. INVESTIGATION REVEALED LT AILERON DISCONNECTED FROM CONTROL ROD. FOUND THAT CONTROL ROD HAD BROKEN IN THREADED AREA JUST FORWARD OF AILERON CONTSDR 2003FA0001170Housing · corrodedDURING NORMAL INSPECTION, HEAVY CORROSION WAS FOUND ON BOTH MAIN LANDING GEAR HOUSING`S UNDER AND AROUND CLAMPS SECURING LANDING LIGHTS AND HYDRAULIC HOSES AND TUBES. REMOUND CLAMPS FOUND CLAMP WHERE INSTALLED PRIOR TO FINAL PAINT WITH NO PRIMER OR ANY CORROSSDR 2003FA0001171Actuator · frozenDURING NORMAL INSPECTION, CYCLED LANDING GEAR. HEARD A SQUEAL FOLLOWED BY APOP FROM THE RT MAIN LANDING GEAR, FOUND THAT THE LANDING GEAR HYD ACTUATOR ATTACH BEARING WAS FROZEN CAUSING THE ACTUATOR HOUSINGS AROUND THE BEARING TO BREAK AND PULL APART. DURING SDR 2003FA0001123Diode · shortedDURING FLIGHT, WHEN GEAR IS INTRANSIT, HYDRAULIC PRESSURE ANNUNCIATOR LIGHT ILLUMINATES. CAUSE OF MALFUNCTION IS UNKNOWN. NO RECOMMENDATION AT THIS TIME.SDR 2003FA0001124Relay · shortedDURING FLIGHT, GEAR MOTOR WAS SLOW TO EXTEND LANDING GEAR. FURTHER INVESTIGATION DETERMINED THAT EXTENSION VALVE HAD A RESTRICTION IN THE LINE WHICH CAUSED THE LANDING GEAR MOTOR TO REQUIRE MORE CURRENT BECAUSE OF THIS DEMAND IT CAUSED THE LANDING GEAR RELAY SDR 2004FA0000151Gasket · leakingRED DYE OIL LEAKAGE AT THE CYLINDER TO HUB ATTACH POINT. OIL IS LEAKING PAST THE CYLINDER GASKET TO THE ATTACHING SCREWS AND FOLLOWING THE THREADS OUT. ADDITIONAL SEALANT NEEDS TO BE ADDED TO THE SCREWS DURING INSTALLATION AND PARTICULAR ATTENTION SHOULD BE SDR 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.SDR 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.SDR 2004FA0000150Gasket · leakingRED DYE OIL LEAKAGE AT THE CYLINDER TO HUB ATTACH POINT. OIL IS LEAKING PAST THE CYLINDER GASKET TO THE ATTACHING SCREWS AND FOLLOWING THE THREADS OUT. ADDITIONAL SEALANT NEEDS TO BE ADDED TO THE SCREWS DURING INSTALLATION AND PARTICULAR ATTENTION SHOULD BE SDR 2004FA0000152Gasket · leakingRED DYE OIL LEAKAGE AT THE CYLINDER TO HUB ATTACH POINT. OIL IS LEAKING PAST THE CYLINDER GASKET TO THE ATTACHING SCREWS AND FOLLOWING THE THREADS OUT. ADDITIONAL SEALANT NEEDS TO BE ADDED TO THE SCREWS DURING INSTALLATION AND PARTICULAR ATTENTION SHOULD BE SDR 2004FA0000153Gasket · leakingRED DYE OIL LEAKAGE AT THE CYLINDER TO HUB ATTACH POINT. OIL IS LEAKING PAST THE CYLINDER GASKET TO THE ATTACHING SCREWS AND FOLLOWING THE THREADS OUT. ADDITIONAL SEALANT NEEDS TO BE ADDED TO THE SCREWS DURING INSTALLATION AND PARTICULAR ATTENTION SHOULD BE SDR 2004FA0000154Gasket · leakingRED DYE OIL LEAKAGE AT THE CYLINDER TO HUB ATTACH POINT. OIL IS LEAKING PAST THE CYLINDER GASKET TO THE ATTACHING SCREWS AND FOLLOWING THE THREADS OUT. ADDITIONAL SEALANT NEEDS TO BE ADDED TO THE SCREWS DURING INSTALLATION AND PARTICULAR ATTENTION SHOULD BE SDR 2004FA0000155Gasket · leakingRED DYE OIL LEAKAGE AT THE CYLINDER TO HUB ATTACH POINT. OIL IS LEAKING PAST THE CYLINDER GASKET TO THE ATTACHING SCREWS AND FOLLOWING THE THREADS OUT. ADDITIONAL SEALANT NEEDS TO BE ADDED TO THE SCREWS DURING INSTALLATION AND PARTICULAR ATTENTION SHOULD BE SDR 2004FA0000156Gasket · leakingRED DYE OIL LEAKAGE AT THE CYLINDER TO HUB ATTACH POINT. OIL IS LEAKING PAST THE CYLINDER GASKET TO THE ATTACHING SCREWS AND FOLLOWING THE THREADS OUT. ADDITIONAL SEALANT NEEDS TO BE ADDED TO THE SCREWS DURING INSTALLATION AND PARTICULAR ATTENTION SHOULD BE SDR 2004FA0000158Gasket · leakingRED DYE OIL LEAKAGE AT THE CYLINDER TO HUB ATTACH POINT. OIL IS LEAKING PAST THE CYLINDER GASKET TO THE ATTACHING SCREWS AND FOLLOWING THE THREADS OUT. ADDITIONAL SEALANT NEEDS TO BE ADDED TO THE SCREWS DURING INSTALLATION AND PARTICULAR ATTENTION SHOULD BE SDR 2003FA0001006Crankshaft · brokenCRANK BROKE ON NR 4 AND NR 6 CHEEK.SDR 2003FA0000901Elt · failedDURING AN ACCIDENT INVESTIGATION THAT DESTROYED THIS AIRCRAFT. IT WAS NOTED THAT THE ELT DID NOT ACTIVATE THE ELT WAS FOUND IN THE ARMED SWITCH POSITION. THIS AIRCRAFT HIT SEVERAL TREES AND IMPACTED THE GROUND VERY HARD.SDR 2003FA0000704Float · wornFUEL QUANTITY FLOAT P/N 38230-002. COMPOSITE FLOAT HAS BEEN HITTING THE UPPER BODY OF THE ASSY WHEN IN A FULL CONDITION AND HAS WORN .2500 INCH GROOVE ON ONE SIDE OF FLOAT AND .1875 INCH GROOVE ON THE OTHER SIDE. GAUGE STILL OPERATED, BUT PARTICLES OF THE COMSDR PNSA030602Line · leakingDURING CRUISE SMELLED A BURNING ODOR AND SLIGHT SMOKE IN COCKPIT WITH CABIN HEAT TURNED ON. OPENED COCKPIT VENTS AND SMOKE WENT AWAY, RETURNED TO CDB AIRPORT WHERE MAINTENANCE FOUND HYDRAULIC LINE FOR BRAKE RES. LEAKING ONTO HEAT DUCT, REPLACED LINE AND GROUNSDR AUS20030553Hinge · mislocated(AUS) VERTICAL STABILIZER CENTRE HINGE FITTED IN WRONG LOCATION. MANUFACTURING ERROR.SDR 2003FA0000631Check Valve · loosePILOT REPORTED RIGHT VACUUM PUMP WARNING LIGHT WAS ON. DURING TROUBLESHOOTING, DISCONNECTED HOSE FROM RIGHT SIDE OF CHECK VALVE MANIFOLD TO CONNECT TEST KIT AND DISCOVERED TWO MISSING RIVETS, TWO RIVETS ABOUT TO FALL OUT AND TWO LOOSE RIVETS ALL ON THE RIGHTSDR CTU2003F00006Support Bracket · brokenWHILE INSPECTING THE AIR DURING AN ANNUAL INSPECTION THE TECHNICIAN FOUND THE PILOT SEAT SUPPORT BRACKET TO BE CRACKED, WHICH ALLOWED THE SEAT STOP BRACKET TO MOVE AWAY FROM THE LOCKING POSITION WHEN A PERSON IS IN THE PILOTS SEAT. THIS ALLOWED THE SEAT STOP SDR 2003FA0000603Master Cylinder · inoperativeSPRING AROUND MASTER CYLINDER SHAFT HUNG UP TO BURR AND DID NOT EXTEND TO HOLD THE PARKING BRAKE LEVER DOWN AGAINST TOP OF CYLINDER. PREVENTING APPLICATION OF PARKING BARKE BY NATURAL MOTION OF RUDDER PEDAL IN FLIGHT. BRAKE LOCKED DURING FLIGHT UNKNOWN TO PRSDR GXPA0303Engine · leakingAIRCRAFT DOWN IN EL DORADO, AR DUE TO LOW OIL PRESSURE IN RT ENGINE. CORRECTIVE ACTION WILL BE COMMUNICATED WHEN TROUBLESHOOTING IS COMPLETED.SDR AUS20030425Bearing · fractured(AUS) PROPELLER BLADE BEARING FRACTURED.SDR 2003FA0000622Actuator · separatedACTUATOR PISTON SEPARATED AT THE ROD END BEARING THREADED AREA. MFG SB NR 109 DATED 1-1092 RECOMMENDED INSTALLATION OF A THREADED REINFORCEMENT BARREL (PN 523-5627-001) BE INSTALLED TO REPLACE TO ORIGINAL BEARING JAM NUT. THIS SB HAD BEEN INSTALLED AT THE TISDR 2003FA0000249Skin · crackedBELLY SKIN CRACKED AT NUTPLATE FOR FAIRING AFT OF NOSE GEAR. CAUSED BY VIBRATION OF FAIRING. INCREASE STRUCTURE STRENGTH INSTEAD OF USING .025 2024 USE .032 2024 T-3.SDR 2003FA0000382Bolt · looseDURING 100 HOUR INSPECTION, THE HORIZONTAL STABILIZER WAS FOUND LOOSE. REMOVED DORSAL FIN, RUDDER AND ELEVATORS. FORWARD ATTACH BOLTS FOR HORIZONTAL STABILIZER WERE FOUND LOOSE. 9 RIVETS ON RIGHT HAND AFT VERTICAL SUPPORT ANGLE, (PN 442682 WERE FOUND SHEARE
Back to Continental IO-540 series