Continental E225-8

Service difficulty reports · 24

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 = 'E2258'
  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 2014FA0000626Bearing · failed10-1-14, 15:43 LOCAL TIME, ACFT WAS ON A PRACTICE ILS APPROACH, RECEIVING VECTORS FROM SOCAL ON 125.5 HEADING OF 030 AT APPROX 3500`, WHEN PILOT ENCOUTERED UNCOMMANDED HIGH RPM. PILOT IMMEDIATELY REDUCED THROTTLE, RPMS SETTLED AT APPROX 1500 RPMS. PILOT FOUNOct 1, 2014 · N2041D · Beech C35BEECH · Propeller SystemSDR 2011FA0000169Oil Filter · failedAFTER START UP AND A SHORT TAXI, THE PILOT NOTICED THAT THE ENGINE RAN ROUGH. SHUTDOWN & NOTICED THAT OIL WAS LEAKING FROM THE RT SIDE COWLING. IT WAS FOUND THAT THE OIL FILTER CAN WAS SEPARATING FROM THE BASE. THIS OCCURRED AFTER 6 CYLINDERS WERE REPLACED.Mar 1, 2011 · N85J · Beech E35 · Reciprocating Engine Oil SystemSDR 2009FA0000668Diaphragm · crackedACFT EXPERIENCED AN IN FLIGHT FAILURE OF THE PROPELLER PITCH CHANGE DIAPHRAGM. THE PILOT PERFORMED AN EMERGENCY DECENT AND A NORMAL LANDING AT THE AIRPARK. UPON SHUTDOWN A TOTAL OF 7 QUARTS OF OIL HAD BEEN LOST. THE DIAPHRAGM HAD BEEN REPLACED 2 YEARS AGO AJul 21, 2009 · N504B · Beech A35 · Propeller AssemblySDR 2008FA0000660Contact · failedRT MAGNETO FAILED COMPLETELY IN FLIGHT DUE TO THE TIP OF THE CONTACT POINTS HAVING SEPARATED FROM HE ASSY. THIS LEFT THE CONTACTS AND THEREFORE PRIMARY ELECTRICAL CIRCUIT IN A CONTINUALLY OPEN POSITION. RENDERING THE MAGNETO INOPERATIVE. IN A PHONE CONVERSATSep 17, 2008 · N4998B · Beech G35 · Magneto/DistributorSDR 2008FA0000181Piston · failedNR 6 PISTON DISINTEGRATED. CAUSE UNKNOWN. PISTON P/N AEC633099 WAS ORIGINALLY MANUFACTURED BY AIRMOTIVE ENGINEERING, INC.(AEC). ENGINE COMPONENTS, INC. (ECI) HAS SINCE BOUGHT OUT AEC. ECI HAS NOT PRODUCED THIS P/N.Mar 4, 2008 · Beech B35 · Reciprocating Engine Cylinder SectionSDR 2006FA0000430Mount · crackedMOUNT WAS CROOKED IN WELD. THINK IT HAPPENED DUE TO TIME ON PORT AND AGE OF AIRCRAFT. CLOSE INSPECTION OF THIS AREA DURING ROUTINE MAINTENANCE (UPPER LT, MOUNT CLUSTER/ WEB .1250 INCH CRACK). (K)Mar 31, 2006 · N2950B · Beech D35 · Engine Mount SectionSDR 2003FA0001117Roll Pin · brokenROLL PIN BROKE ALLOWING SLIP RING TO MOVE OUT OF POSITION CAUSING A HYDRAULIC LOCK IN PROPELLER OPERATION. PROPELLER REMAINED IN LOW PITCH, HIGH RPM. REASON FOR PIN FAILURE UNKNOWN.Sep 25, 2003 · N5836C · Beech C35BEECH · Propeller Hub SectionSDR 2003FA0000004Oil Filter · burstAFTER STARTING ENGINE AND PERFORMING A ROUTINE WARM UP. PILOT NOTICED OIL PRESSURE DROPPING. AFTER SHUTDOWN, THE OIL FILTER WAS SHOWN TO HAVE PARTIALITY BLOWN OPEN AT THE BASE WHERE IT IS CRIMPED. ALSO THE PRESSURE RELIEF VALVE WAS FOUND TO HAVE 14 WASHERS UNDDec 20, 2002 · N4575D · Beech G35 · Reciprocating Engine Oil SystemSDR 2002FA0001185Collar · crackedGUIDE COLLAR CRACKED DUE TO VIBRATION FROM PROPELLER. BOTH BLADES SLIPPED IN CLAMP CREATING A SPLIT IN ANGLES.Sep 25, 2002 · N34TT · Beech G35 · Propeller Hub SectionSDR 2002FA0001189Collar · crackedGUIDE COLLAR CRACKED DUE TO VIBRATION FROM PROPELLER. BOTH BLADES SLIPPED IN CLAMP CREATING A SPLIT IN ANGLES. THIS CAUSED VIBRATION.Sep 25, 2002 · N34TT · Beech G35 · Propeller Hub SectionSDR 20000622SH011Cylinder · failedENGINE WAS REMOVED 3 TIMES FOR LOW OIL PRESSURE, AND IT HAD NEW CYLINDERS AT OVERHAUL. SUBMITTER REMOVED ALL 6 CYLINDERS AT 89.9 TSO FOR LOW COMPRESSION LEAKING BY EXHAUST VALVES, 3 CYLINDERS REMOVED AT 154.3 TSO WHICH IS 64.4 HOURS FROM THE LAST REMOVAL AND Jun 6, 2000 · N231B · Beech G35 · Reciprocating Engine Cylinder SectionSDR 20000531SH020Primer Line · crackedAT CYLINDER REPLACEMENT, FOUND PRIMER LINES NR 1, NR 3 CYLINDERS CRACKED (3/4 AROUND) UNDER ADEL CLAMP AREA. EVIDENCE OF FATIGUE AND CORROSION. (X)May 4, 2000 · N7382B · Beech E35 · Engine Fuel DistributionSDR 20000531SH022Cylinder · separatedAT ANNUAL INSPECTION, FOUND SIGNS OF SEEPAGE AT BARREL (INDICATIONS OF BARREL SEPARATING FROM HEAD) IN NR 4, NR 5, NR 6 CYLINDERS. POSSIBLE CAUSE IS AGE ON CYLINDERS AND TIME IN SERVICE. (X)May 4, 2000 · N7382B · Beech E35 · Reciprocating Engine Cylinder SectionSDR 99ZZZX652Gasket · brokenTHE GASKETS THAT SEAL THE INTAKE MANIFOLD (WHICH HAS ENGINE OIL CIRCULATING THROUGH IT) HAVE BRASS EYELETS FORMED INTO THE PAPER GASKET AROUND THE BOLT HOLES. USING STANDARD TORQUE OF 175 INCH/POUND FOR THE .3125 INCH - 18 EACH BOLTS RESULTED IN THE GASKET LEJan 1, 1999 · N4254D · Beech G35 · Reciprocating Engine Power SectionSDR 99ZZZX653Gasket · brokenTHE GASKETS THAT SEAL THE INTAKE MANIFOLD (WHICH HAS ENGINE OIL CIRCULATING THROUGH IT) HAVE BRASS EYELETS FORMED INTO THE PAPER GASKET AROUND THE BOLT HOLES. USING STANDARD TORQUE OF 175 INCH/POUND FOR THE .3125 INCH - 18 EACH BOLTS RESULTED IN THE GASKET LEJan 1, 1999 · N4254D · Beech G35 · Reciprocating Engine Power SectionSDR 99ZZZX536T Drive · leakingENGINE T-DRIVE (THIS UNIT MOUNTS THE ENGINE FUEL PUMP AND PROP GOVERNOR ONTO A SINGLE ACCESSORY PAD) DEVELOPED A LEAK. UNIT REMOVED AND SENT FOR OVERHAUL. UNIT WAS CERTIFIED AND RE-INSTALLED ONLY TO FIND THE GOVERNOR DRIVE GEAR TO BE THE WRONG ONE. UNIT REWDec 22, 1998 · N8945A · Beech C35BEECH · Turbine Engine Accessory DriveSDR AU980009Torque Link · worn(AUS) LANDING GEAR TORQUE LINKS WORN EXCESSIVELY.Jan 13, 1998 · Beech G35 · Main Landing Gear Strut/Axle/TruckSDR AU980012Bushing · worn(AUS) NOSE LANDING GEAR STRUT ASSEMBLY BUSHES WORN EXCESSIVELY.Jan 13, 1998 · Beech G35 · Nose/Tail Landing Gear Strut/AxleSDR AU980013Cap · faulty(AUS) MAIN FUEL CAPS (2OFF) FAULTY.Jan 13, 1998 · Beech G35 · Fuel StorageSDR AU980014Antenna · broken(AUS) ADF SENSOR ANTENNA BROKEN.Jan 13, 1998 · Beech G35 · Automatic Direction Finder (ADF) SystemSDR AU980015Battery · corroded(AUS) BATTERY CORRODED.Jan 13, 1998 · Beech G35 · Battery/Charger SystemSDR AU980016Bushing · worn(AUS) NOSE LANDING GEAR DRAG BRACE BUSHES WORN AND ONE ATTACHMENT BOLT LOOSE.Jan 13, 1998 · Beech G35 · Landing Gear Retraction/Extension SystemSDR 97ZZZX2598Screw · strippedDURING CYLINDER INSTALLATION ATTEMPTING TO TORQUE ROCKER SHAFT HOLD-DOWN SCREWS RESULTED IN 2 SCREWS STRIPPING BEFORE THE MINIMUM TORQUE OF 180 INCH/POUND WAS REACHED. THIS IS THE 2ND OCCURRENCE ON THIS ENGINE. BOTH TIMES THE CORRECTIVE ACTION WAS REPLACING May 19, 1997 · N3251C · Beech E35 · Reciprocating Engine Cylinder SectionSDR 95ZZZX956Impulse Coupling · crackedDURING INSPECTION OF IMPULSE COUPLING, I.E., AD 78-09-07R3, NUT WAS LOOSE DUE TO CRACK IN BORE OF IMPULSE COUPLING. TCM BENDIX SB 639 REFERS TO INSTALLATION OF COUPLINGS. AD 78-09-07R3 DOES NOT REQUIRE REMOVAL OF COUPLING FOR INSPECTION. MAYBE IT SHOULD TO Jan 20, 1995 · N3376C · Beech F35 · Magneto/Distributor
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