Lycoming O-320-E2D
Service difficulty reports · 494
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 = 'O320E2D' 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 = 'O320E2D' 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 CA021010003Mount · cracked(CAN) ENGINE MOUNT ASSEMBLY CRACKED AT LOWER CROSS MEMBER RT SIDE.SDR AUS20020945Strap · broken(AUS) LH FUEL TANK REAR STRAP ASSEMBLY LOOSE. RH FUEL TANK REAR STRAP ASSEMBLY BROKEN NEAR THE SCREW END. FOUND DURING INSPECTION IAW CESSNA CONTINUED AIRWORTHINESS PROGRAM 28-30-01.SDR CA020830013Riser · cracked(CAN) FOUND CRACK JUST BELOW THE EXHAUST FLANGE WELD. CRACK HAD PROGRESSED HALF WAY AROUND THE BACK OF THE RISER ASSEMBLY. CRACK WAS FOUND DURING A REGULARLY SCHEDULED INSPECTION. CRACK HAD NOT BEEN VISIBLE AT THE PREVIOUS INSPECTION, SO CRACK DID PROGRESS QUISDR CA030502002Magneto · failed(CAN) ROUGH RUNNING ENGINE DUE TO LT MAGNETO MALFUNCTION. INTERNAL DEFECTS, THEREFORE EXACT MALFUNCTION UNKNOWN.SDR AUS20020913Cable · corroded(AUS) CONTROL CABLE CORRODED WITH APPROXIMATELY 50% OF THE STRANDSBROKEN/FRAYED.SDR AUS20020916Cable · corroded(AUS) CONTROL CABLE RUSTED IN AREA OF REAR FUSELAGE.SDR CA020830006Sensor · failed(CAN) HIGH VOLTAGE LIGHT CAME ON DURING FLIGHT. FLIGHT TERMINATED. OVER VOLTAGE SENSOR FAILED. RESULTED IN DAMAGE TO VOLTAGE REGULATOR AND BATTERY CONTACTOR. ELECTRICAL COMPONENTS REPLACED.SDR AUS20020914Cable · worn(AUS) MIXTURE CONTROL CABLE INNER WIRE WORN TO LESS THAN 50% OF NORMALTHICKNESS. CABLE DIAMETER WAS 62MM (0.024IN) INSTEAD OF THE NORMAL DIAMETER 1.6MM (0.062IN).SDR AUS20020915Cable · worn(AUS) THROTTLE CONTROL INNER CABLE WORN BY MORE THAN 60% OF THE DIAMETER. WIRE DIAMETER WAS 0.5MM (0.019IN) INSTEAD OF THE NORMAL 1.5MM (0.059IN).SDR CA020731014Stop · missing(CAN) UPON COMPLETING INSPECTION OF RUDDER STOPS PER AD CF-2000-20, IT WAS FOUND THAT THE RUDDER STOPS WERE BOTH MISSING. THERE WERE NO HOLES IN THE TAILCONE SKIN WHERE THE STOPS SHOULD HAVE BEEN, BUT THE ANCHOR NUTS WERE RIVETS TO THE BULKHEAD. THIS SKIN WAS SDR CA020617002Spar · cracked(CAN) DURING A RECENT PAINT SHOP VISIT IT WAS DISCOVERED THAT A SIGNIFICANT NUMBER OF SERIOUS STRUCTURALLY DAMAGED AREAS WERE AHMMERED OUT WITH A DOLLY, NOT REINFORCED, AND EITHER FILLED IN WITH BODY PUTTY OR COERED OER WITH A PATCH. THE LEFT WING MAIN SPAR APSDR CA020610010Gyro · unserviceable(CAN) AFTER INSTALLATION OF A NEW OVERHAULED GYRO HORIZON, IT HAD BEEN FOUND UNSERVICABE. THAT GYRO HAD BEEN OVERHAULED BY AERONEUF INSTRUMENTS LTEE APPROVAL 27-91 ON RELEASE NOTE 28244 DATED MAY 27, 2002. IT IS THE SECOND SDR SUBMIT FOR THE SAME PROBLEM. ON RSDR CA020610009Gyro · unserviceable(CAN) AFTER INSTALLATION OF A NEW OVERHAULED GYRO HORIZON, IT HAD BEEN FOUND UNSERVICABE. THAT GYRO HAD BEEN OVERHAULED BY AERONEUF INSTRUMENTS LTEE APPROVAL 27-91 ON RELEASE NOTE 28017 DATED FEB. 05, 2002SDR CA020522006Tube · defective(CAN) FAILURE OF CENTER SEAM OF 600 X 6 - 6 PLY TIRE TUBE. THIS HAS OCCURED ON 2 OTHER SEPERATE OCCASIONS. SUPPLIER HAS BEEN NOTIFIED AND HAS INDICATED THAT HE WAS GOING TO CONTACT MICHELIN AND INQUIRE ABOUT THE PROBLEM. PICTURES OF DEFECT ARE ON FILE AND MSDR CA020425003Rudder Horn · cracked(CAN) DURING ROUTINE INSPECTION THE RUDDER HORN ASSY AT THE AREA WERE THE HORN STRIKES THE RUDDER STOPS HAD BEEN DAMAGED. WE BELIEVE BY GUSTY WINDS WITHOUT THE RUDDER LOCK ON. THE RUDDER STOP SCREW HAD ACTUALLY ROLLED THE ALUMINIUM BACK ON THE HORN WHICH MADESDR 2002FA0000469Coil · burnedDURING ROUTINE FLIGHT ENGINE BECAME ROUGH. PILOT CONTINUED TOWARDS AIRPORT, WITH NO OTHER OPTIONS, AND LANDED SAFELY. ONCE ON THE GROUND, THE PILOT/ MECHANIC DID AN ENGINE RUN-UP AND FOUND LEFT MAGNETO DEAD. FURTHER INSPECTION REVEALED A HOLE BURNED THROUGSDR AUS20020332Mount · cracked(AUS) ENGINE MOUNT CRACKED IN AREA OF LOWER CROSSOVER TUBE.SDR AUS20020333Mount · cracked(AUS) ENGINE MOUNT CRACKED IN AREA OF LOWER CROSSOVER TUBE.SDR CA020312002Camshaft · worn(CAN) METAL FOUND IN OIL FILTER DURING SCHEDULED MAINTENANCE. ENGINE DISMANTLED AT OVERHAUL FACILITY. NR 4 EXHAUST LOBE FOUND TO BE WEARING AFTER 85.2 HOURS SINCE NEW.SDR CA020226002Muffler · cracked(CAN) FOUND DURING AD CF90-03R2 MUFFLER INSPECTION. CRACK FOUND AT BASE OF TAIL PIPE TO MUFFLER CAN CONNECTION. (ALONG WELD BEAD.)MUFFLER REPLACED IN ACCORDANCE ADCF90-03R2. PART 1 SUB PART 5.SDR CA020213007Spring · broken(CAN) RUDDER WAS ANGLED TO ONE SIDE UPON FURTHER INSPECTION FOUND THAT IT WOULD NOT RETURN TO NEUTRAL.RUDDER SPRING WAS FOUND HANGING IN POSITION DETACHED FROM ONE SIDE, THE END HAD BROKEN OFF. PART WAS REPALCED AND AIRCRAFT WAS RETURNED TO SERVICE.SDR CA020208002Vane · stuck(CAN) COPPER VANE RUBS AGAINST POT ALUMINUM GYRO CASE CREATING BLACK RESIDUE CAUSING VANE TO STICK. THIS CAUSES HORIZION TO DIPLAY A PITCH OR ROLL WHEN LEVEL.SDR CA020325003Bearing · missing(CAN) PILOT OF AIRCRAFT FOUND "A PART" BENEATH THE COWLING. COWLINGS WERE REMOVED & ENGINE INSPECTED FOR "MISSING PARTS". REAR SUPPORT BEARING (ROLLER TYPE) FOUND MISSING ON LAMAIR STARTER. PILOT REPORTED FURTHER THAT STARTER WAS STILL ENGAGED TO FLYWHEEL AT TSDR CA020116002Bushing · worn(CAN) BUSHING WAS FOUND TO BE ROTATING IN BELLCRANK ASSEMBLY.SDR AUS20020002Spar · corroded(AUS) FORWARD SPAR ASSEMBLY CONTAINED SEVERE EXFOLIATION CORROSIONBETWEEN THE SPAR PNO 0523014-2 AND THE ATTACHMENT PLATE PNO 0523016-1. THE THICKNESS OF THE ASSEMBLY WAS REDUCED BY APPROXIMATELY 50% DUE TO THE CORROSION. THE RIVETS HOLDING THEASSEMBLY TOGETHESDR CA011105015Case · cracked(CAN) CRACK FOUND IN CASE AROUND FORWARD UPPER THROUGH BOLT.SDR 2001FA0000487Tube · separatedDURING DECENT, THE PILOT WAS UNABLE TO REDUCE POWER. USING THE MIXTURE CONTROL, THE PILOT MADE AN UNEVENTFUL LANDING. MAINTENANCE PERSONNEL FOUND THE ACCELERATOR DISCHARGE TUBE LAYING ON THE BOTTOM OF THE INTAKE AIRBOX. IT WAS DETERMINED THAT THE ACCELERATOSDR CA011011012Mount · cracked(CAN) ENGINE MOUNT WAS FOUND CRACKED DURING 50 HOUR INSPECTION. NO CRACKS WERE NOTICED AT THE PREVIOUS INSPECTION AND THE CRACK SHOWED NEW MATERIAL. THIS WOULD INDICATE DETERIORATION DURING THE LAST 50 HOUR.SDR CA010912017Stiffener · cracked(CAN) COMMON PROBLEM ON OLDER CESSNA 150 SERIES, MANUFACTURER HAS BEEN REPLACED THIS PART WITH A NEW IMPROVE PART P/N 0432169-1 ALSO INCLUDING NEW IMPROVE BULKHEAD ASSY P/N 0412177-2.SDR CA011004010Bolt · broken(CAN) ONE OF THE 6 BOLTS ATTACHING THE PROPELLER TO THE ENGINE CRANK SHAFT FLANGE BROKE AT THE TOP OF THE THREADED AERA ON INITIAL TORQUE.THE PROPELLER HAD A PLACARD INDICATING TORQUE SPED FOR 1/2" BOLTS. PROLLER IS ATTACHED WITH 7/16" BOLTS. IT IS SUSPECTED TSDR CA010907010Stringer · cracked(CAN) DURING ROUTINE MAINTENANCE INSPECTION, IT WAS DISCOVERED THAT THE RIGHT HAND ENGINE RAIL WAS CRACKED. P/N 0513132-4 STRINGER ASSEMBLY IN FUSELAGE FRONT SECTION STRUCTURE ASSEMBLY WAS REPLACED.SDR AUS20010930Float · damaged(AUS) CARBURETTOR FLOAT CONTAMINATED WITH FUEL CAUSING CARBURETTOR TO FLOOD.SDR AUS20011088Brushes · worn(AUS) ALTERNATOR BRUSHES WORN PREMATURELY.SDR CA010814022Control Cable · frayed(CAN) AIRCRAFT DAMAGE ON LANDING AT PICTOU ISLAND. AIRCRAFT BEING STRIPPED FOR REPAIR WHEN THE CABLE, ABOVE WAS FOUND FRAYED WHERE IT PASSES OVER THE PULLEY. LT SIDE TOP OF FUSELAGE.SDR AUS20010826Hose · leaking(AUS) ENGINE OIL COOLER HOSE POROUS AND LEAKING IN THE AREA ON THEOUTSIDE OF THE BEND AT THE ENGINE END. FIRE SLEEVINGCONTAMINATED. HOSE MANUFACTURED 30 DECEMBER 1996.SDR CA011105014Arm · cracked(CAN) THIS PROBLEM WAS DISCOVERED DURING THE AIRCRAFTS ANNUAL INSPECTION. THE CRACK IS ALL OF THE WAY THROUGH THE FORWARD SIDE OF THE ARM, VERTICALLY ORIENTED AND PASSES THROUGH THE GREASE FITTING HOLE.IT APPEARS TO HAVE ORIGINATED AT THE FILLET FORMED BY THE SDR CA010724011Spinner · cracked(CAN) CRACK IN PROPELLER CUTOUT OPENING IN SPINNER NOTED DURING PREFLIGHT INSPECTION. AIRCRAFT WAS GROUNED FOR REPAIRS.SDR CA010509007Stiffener · cracked(CAN) THE REINFORCEMENT RIVETED TO THE FIREWALL AT THE MIDDLE RT LOWER COWL ATTACH BRACKET WAS FOUND CRACKED. THE ATTACH BRACKET SITS ON TOP OF THE REINFORCEMENT (SANDWICHED BETWEEN THE FIREWALL AND BRACKET). THE CRACK WAS FOUND AT A 200 HR INSPECTION AND WAS SDR CA010504010Spring · disconnected(CAN) LT RUDDER AND BRAKE PEDAL RETURN SPRING P/N 0310196-5 BECAME DISLODGED FROM FRONT ANCHOR POINT BRACKET P/N 510128 IN FORWARD CENTRE TUNNEL ASSEMBLY P/N 0591301-11.THIS ALLOWED THE LEFT BRAKE & RUDDER PEDAL TO MOVE FULL FWD. THE PEDALS WOULD NOT RETURN TOSDR CA010502006Spar · cracked(CAN) HORIZONTAL STAB SPAR FOUND CRACKED FROM CENTRE RELIEF HOLE (LIGHTNING HOLE) OUTWARD APPROXIMATELY 1/2 INCH. PART REPLACED WITH NEW UNIT. THIS PROBLEM IS PROBABLY DUE TO INAPPROPRIATE GROUND LANDING OF THE AIRCRAFT, I.E. USING STAB AS SURFACE TO PUSH ON TSDR CA010323013Clamp · loose(CAN) THROTTLE SHEAF HAD VIBRATED LOOSE FROM CONNECTING CLAMP WHICH LEFT NO CONTROL FOR THROTTLE ADJUSTMENT. THROTTLE CABLE WAS RE-POSITIONED IN THE SHEAF AND NEW HARDWARE WAS INSTALLED.AIRCRAFT WAS GROUND UN AND ALL PARAMETERS NORMAL.SDR CA010313024Battery · failed(CAN) PILOT ENCOUNTERED COMPLETE (GREATER THAN 50 PERCENT) ELECT. FAILURE IN FLT. AFTER ATTEMPTING TO GET A/C RADIOS TO TRANSMIT/RECEIVE, PILOT SQUAKED RADIO FAILURE CODE. FURTHER ATTEMTPS AT GETTING OTHER ELECT. SYSS TO FUNCTION, PILOT FOUND THAT ALL ELECT. SDR 20010412CW002Carburetor · defectiveDURING FLIGHT, AIRCRAFT WAS DOING TOUCH AND GO LANDINGS. PILOT PULLED BACK ON THROTTLE FOR MORE POWER BUT COULD NOT MOVE THROTTLE. LANDED SHORT OF RUNWAY, IN A FIELD. INVESTIGATION OF THROTTLE , FOUND CARBURETOR STUCK IN IDLE POSITION. REMOVED CARBURETOR ASDR CA010307004Wheel · damaged(CAN) REPORTED TO MAINTENANCE OF CLICKING NOISE FROM FRONT AREA DURING TAXI. INSPECTION REVEALED THREE (3) THRU BOLTS MISSING ON WHEEL RIM RESULTING IN DAMAGE TO NOSE FORK. TWO OF THREE REMAINING BOLTS FOUND LOOSE. SUSPECT INCORRECT TORQUE ON WHEEL BOLTS.SDR CA010219010Spring · broken(CAN) HOOK BROKEN OFF SPRING (FOR LT RUDDER BAR) AND ALLOWED R/H SPRING TO PULL RUDDER TO RIGHT. PILOT HAD TO MAINTAIN PRESSURE ON LEFT PEDAL TO MAINTAIN CONTROL OF AIRCRAFT. UNEVENTFUL LANDING CARRIED OUT AFTER COMPLETE CIRCUIT AND APPROACH. SPRING DID NOT BRSDR CA010226018Magneto · failed(CAN) ENGINE STARTING RUNNING ROUGH IN CRUISE FLIGHT PILOT RETURNED TO STATION. GROUND RUN INDICATED EXCESSIVE RPM LOSS ON RT MAGNETO. MAGNETO REPLACED AND FOLLOW UP GROUND RUN CARRIED OUT RESULTING IN NORMAL RPM (STATIC) AND RT RPM DROP WITHIN LIMITS. NO APPASDR 20010206CW002Engine · failedENGINE HAD LOW OIL PRESSURE AND HIGH OIL TEMPERATURE IN CLIMB. TEMP STABILIZED IN DESCENT BUT OIL PRESSURE STILL LOW. LANDED AIRCRAFT. MAINTENANCE FOUND ALUMINUM ON OIL PRESSURE RELIEF VALVE. OIL PRESSURE SCREEN COVERED WITH ALUMINUM, STEEL FLAKES. SUSPECSDR CA010119005Screw · bent(CAN) NAS 603 RUDDER STOP SCREWS FOUND BENT AT ANNUAL INSPECTION. SUSPECT DAMAGE CAUSED BY RUDDER BEING BLOWN AGAINST STOPS AND RUDDER LOCKS NOT USED.SDR 20010409CW017Exhaust Valve · brokenAIRCRAFT ARRIVED WITH A ROUGH ENGINE. OPERATIONAL CHECK OF ENGINE REVEALED DANAGE IN NR 2 CYLINDER. FOUND THAT EXHAUST VALVE HAD BROKEN AND DESTROYED PISTON ALSO. ENGINE HAD 1122.7 TIME SINCE OVERHAUL. PREVIOUS COMPRESSION CHECK SHOULD HAVE REVEALED ANSDR CA001229011Mount · cracked(CAN) CRACK DEVELOPED IN CORNER WELD OF CROSS TUBE MEMBER.
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