Beech 58TC

Service difficulty reports · 20

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 aircraft_model_key = '58TC'
  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 KC2R1008201449413Flyweight · crackedDURING ROUTINE 500 HOUR INSPECTION OF MAGNETOS, DISCOVERED THAT ALL FOUR MAGNETOS HAD CRACKED IMPULSE COUPLING FLYWEIGHT PLATES. CRACKS WERE DISCOVERED DURING NDT MAGNETIC PARTICLE INSPECTION OF IMPULSE COUPLINGS. SUSPECT THE SHARP-CORNERED FEATURE OF THEOct 8, 2014 · N110CW · Beech 58TC · Magneto/DistributorSDR 20010227CW004Gyro · defectivePILOT REPORTS ELECT STANDBY GYRO HORZ, INOPERATIVE. REMOVED INSTRUMENT, CAN HEAR LOOSE PARTS MOVING AROUND INSIDE INSTRUMENT. REMOVED AND RETURNED TO MFG.Dec 29, 2000 · N117HS · Beech 58TC · Attitude Gyro and Indicating SystemSDR 20000713SH009Case · crackedCASE FOUND CRACKED AT NR 5 CYLINDER STUD NR 3, NUT ON STD NR 7 LOOSE AND STUD NR 8 PULLED FROM CASE AND RESTING ON CYLINDER COOLING FINS. (X)Jul 13, 2000 · N1865L · Beech 58TC · Reciprocating Engine Power SectionSDR 20000407SH015Support Bracket · crackedDURING ANNUAL INSPECTION, FOUND RT ENGINE TURBO MOUNT BRACKET CRACKED UNDER AND NEAR END OF LOWER STIFFENER BEND. CRACK IS APPROXIMATELY ONE INCH LONG AND EXTENDING TOWARD BUT NOT TO LOWER LIGHTING HOLE. NO EVIDENCE OF CAUSE FOR CRACK. (X)Feb 21, 2000 · N227BR · Beech 58TC · Exhaust TurbochargerSDR 2000ZZZX606Bellcrank · damagedWHILE INSPECTING AIRCRAFT, FOUND RUDDER WAS LOOSE AT THE ATTACHMENT TO RUDDER CABLE BELLCRANK. REMOVED BOLTS AND FOUND 2 EACH BOLT HOLES ELONGATED. SUBMITTER STATED CAUSE UNKNOWN, BOLTS WERE TIGHT. SUBMITTER SUGGESTED CLOSE INSPECTION OF THIS AREA AT INSPECFeb 17, 2000 · N23712 · Beech 58TC · Rudder StructureSDR 2000ZZZX605Rudder Mast · damagedWHILE INSPECTING AIRCRAFT, FOUND RUDDER WAS LOOSE AT THE ATTACHMENT TO RUDDER CABLE BELLCRANK. REMOVED BOLTS AND FOUND 2 EACH BOLT HOLES ELONGATED. SUBMITTER STATED CAUSE UNKNOWN, BOLTS WERE TIGHT. SUBMITTER SUGGESTED CLOSE INSPECTION OF THIS AREA AT INSPECFeb 17, 2000 · N23712 · Beech 58TC · Rudder StructureSDR 99ZZZX1413Cables · misinstalledWHEN C/W ANNUAL INSPECTION, FOUND CABLE FOR RUDDER ROUTED ACROSS FS 271.92 BULKHEAD INSTEAD OF THROUGH IT. THIS CAUSED A CHAFING NOISE. CABLE TENSION WAS WAY OUT OF LIMITS ON THE LOW SIDE, SO NO 'SAWING' DAMAGE WAS NOTICED. COMPONENTS INSPECTED AND RESTORED TFeb 22, 1999 · N23712 · Beech 58TC · Rudder Control SystemSDR 99ZZZX1388Exhaust Stack · misoverhauledDURING ANNUAL INSPECTION, INSPECTORS FOUND ENGINE MOUNT PN 102-91002B-131 PARTIALLY GROUND AWAY. CHARGER ILLEGALLY REPAIRED AND WOULD NOT FIT PROPERLY. PARTIES UNKNOWN GROUND AWAY MAJOR ENGINE TRUSS TO ALLOW INSTALLATION OF AN IMPROPER PART. PER RAYTHEON, TRUFeb 22, 1999 · N23712 · Beech 58TC · Engine Collector/Tailpipe/NozzleSDR 99ZZZX67Elbow · corrodedWHILE PERFORMING HEATER TEST PER AD NOTE 96-20-07, FOUND ELBOW FITTING FOR HEATER COMBUSTION CHAMBER DRAIN LEAKING. FURTHER INVESTIGATION SHOWED ALUMINUM FITTING WAS BADLY CORRODED THROUGH AND FUEL DRAIN PASSAGE WAS COMPLETELY CLOGGED WITH CORROSION. WITH THDec 2, 1998 · N23712 · Beech 58TC · Heating SystemSDR 98ZZZX2620Mount · damagedTHE EXHAUST SHIELD HAD COME LOOSE ON BOTH LT AND RT ENGINES. BOTH SHIELDS HAD CAUSED ENOUGH DAMAGE TO WARRANT REMOVAL OF BOTH ENGINE MOUNTS FOR REPAIR.Jun 30, 1998 · N110CW · Beech 58TC · Engine Mount SectionSDR 98ZZZX2619Mount · damagedTHE EXHAUST SHIELD HAD COME LOOSE ON BOTH LT AND RT ENGINES. BOTH SHIELDS HAD CAUSED ENOUGH DAMAGE TO WARRANT REMOVAL OF BOTH ENGINE MOUNTS FOR REPAIR.Jun 30, 1998 · N110CW · Beech 58TC · Engine Mount SectionSDR 98ZZZX2618Shield · looseTHE EXHAUST SHIELD HAD COME LOOSE ON BOTH LT AND RT ENGINES. BOTH SHIELDS HAD CAUSED ENOUGH DAMAGE TO WARRANT REMOVAL OF BOTH ENGINE MOUNTS FOR REPAIR.Jun 30, 1998 · N110CW · Beech 58TC · Engine Collector/Tailpipe/NozzleSDR 97ZZZX1057Retract Rod · failedDURING ANNUAL INSPECTION PERFORMING EMERGENCY EXTENSION, LOUD BANG HEARD. UPON FURTHER INVESTIGATION, FOUND LEFT RETRACT ROD ASSY CRACKED ABOUT 8 INCHES OUTBOARD OF ACTUATOR. ROD ASSY COMPLETELY FAILED ON NEXT RETRACTION NOT ALLOWING LEFT GEAR TO EXTEND OR RFeb 27, 1997 · N97R · Beech 58TC · Landing Gear Retraction/Extension SystemSDR 97ZZZX1150Distributor Gear · brokeDISTRIBUTION GEAR BROKE AND CONTACT STUCK ON NR 2 CYL LEAD. MAG CONTINUED TO ROTATE CAUSING ONLY NR 2 CYL TO FIRE EACH TIME POINTS OPENED. THIS CAUSED SEVERE DETONATION IN NR 2 CYL BURNING A HOLE THROUGH PISTON. THIS RESULTED IN AN INFLIGHT SHUT DOWN. ENGIFeb 7, 1997 · N117HS · Beech 58TC · Magneto/DistributorSDR 97ZZZX785Cover Assy · leakTHE COVER TO OIL PUMP IS SEALED WITH GASKET CEMENT (FORM-A-GASKET PERMATEX) AND A NR 50 SILK THREAD. THE COVER WAS NOT PROPERLY INSTALLED AND TORQUED CAUSING IT TO LEAK OIL WHEN THE SEAL FAILED AFTER A TWO HOUR FLIGHT HAD LEAKED 3 QTS OIL.Feb 3, 1997 · N6669X · Beech 58TC · Reciprocating Engine Oil SystemSDR 97ZZZX894Rod Assy · crackedDURING ANNUAL INSPECTION WHILE PERFORMING GEAR SWING, AN UNUSUAL NOISE (THUD) WAS HEARD. FOLLOWING EMERGENCY GEAR EXTENSION, FOUND CRACKED ROD ASSY AT 8 INCHES OUTBOARD OF ATTACH BOLT. ALSO, NOTED DOWN TENSION SPRING WAS STACKED. SUSPECT CAUSE INCORRECT TENJan 1, 1997 · N97R · Beech 58TC · Landing Gear Retraction/Extension SystemSDR EY2R9601066Split Bearing · corrodedCORROSION FOUND ON SPLIT BEARING.Sep 1, 1996 · Beech 58TC · Propeller AssemblySDR 96ZZZX3322Support Assy · wornMLG MALFUNCTIONED, ACFT EXAMINED AND FND FOLLOWING PARTS DAMAGED: RT RETRACT ROD (35-81512547), RT INBD GEAR DOOR (35-8150055-169), RT BRAKE ASSY (03014500) FLAP SHAFT (3X5K8720A63-5/16), AND FLAP ACT WIRES. RT WING, STEP, AILERON, PROP, AND ENG SUSTAINED DAJun 1, 1996 · N60234 · Beech 58TC · Landing Gear Position and WarningSDR 95ZZZX3984Stub Spar · damagedDURING ROUTINE MAINTENANCE, DAMAGE TO HORIZ STABILIZER REAR STUB SPAR WAS FOUND. CAUSE OF DAMAGE WAS CONTACT TO UPPER SURFACE WITH DRILL BIT WHILE DRILLING HOLES THROUGH BULKHEAD FLANGE. SUSPECT DAMAGE MAY HAVE OCCURRED AT FACTORY. BEECH SI0990 R2 CALLS ANYJul 10, 1995 · N60234 · Beech 58TC · Horizontal Stabilizer, Spar/RibSDR 95ZZZX3983Bulkhead · crackedDURING ROUTINE MAINTENANCE CRACKS WERE FOUND IN AFT BULKHEAD (FS 271.92) AT LOWER LT AND RT CORNERS OF CUT-OUT AREA FOR STUB SPAR. BEECH SI0090 R2 DEALS WITH THIS SUBJECT, BUT ONLY APPLIES TO EARLIER AIRCRAFT S/N. BOTH CRACKS WERE LESS THAN .25 INCH, SO ALL Jul 10, 1995 · N60234 · Beech 58TC · Fuselage Main, Bulkhead
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