Beech G35

Service difficulty reports · 19

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 = 'G35'
  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 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 2005FA0000657Brace · corrodedCORROSION PITS APPROXIMENTLY 30 TO 50 PERCENT OF WALL THICKNESS. THIS PART ONLY 10 PERCENT OF WALL THICKNESS ALLOWED BY MFG. THIS PART IS MAGNESUM. THE PITTING IS UNDER THE FLET 35, ABOVE THE LOWER BUSHING, THE FELT IS SATURATED WITH MOISTURE AND GREASE WApr 17, 2005 · N52WR · Beech G35 · Nose/Tail Landing GearSDR 2005FA0000500Tube · disintegratedTHIS AUTOPILOT WAS INSTALLED 1/23/95. IT HAS A TUBE THAT IS TEE`D INTO THE STATIC SYSTEM AND RUNS TO THE ALTITUDE HOLD PRESSURE TRANSDUCER. THIS PLASTIC TUBE LOST IS MECHANICAL PROPERTIES AND FELL APART. THIS OPEND UP THE STATIC SYSTEM TO CABIN PRESSURE. RMar 27, 2005 · N4606D · Beech G35 · Auto Flight SystemSDR 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 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 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 UIE2002F00009Magneto · failedAIRCRAFT ENGINE RIGHT MAGNETO FAILED DURING MAGNETO CHECK. FOUND IMPULSE COUPLER SPRING IN TWO PIECES. SPRING BROKE INTO TWO PIECE FOR UNKNOWN REASON. ALSO FOUND PREVIOUS TECHNICIAN SPLICED MAG (P) LEAD AND GROUND WIRE TOGETHER CAUSING THE MAG TO GROUND OUTMay 28, 2002 · N348G · Beech G35 · Magneto/DistributorSDR 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 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 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 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 AU980015Battery · corroded(AUS) BATTERY CORRODED.Jan 13, 1998 · Beech G35 · Battery/Charger SystemSDR AU980014Antenna · broken(AUS) ADF SENSOR ANTENNA BROKEN.Jan 13, 1998 · Beech G35 · Automatic Direction Finder (ADF) SystemSDR AU980013Cap · faulty(AUS) MAIN FUEL CAPS (2OFF) FAULTY.Jan 13, 1998 · Beech G35 · Fuel StorageSDR AU980012Bushing · worn(AUS) NOSE LANDING GEAR STRUT ASSEMBLY BUSHES WORN EXCESSIVELY.Jan 13, 1998 · Beech G35 · Nose/Tail Landing Gear Strut/AxleSDR AU980009Torque Link · worn(AUS) LANDING GEAR TORQUE LINKS WORN EXCESSIVELY.Jan 13, 1998 · Beech G35 · Main Landing Gear Strut/Axle/TruckSDR 96ZZZX5020Instrument Panel · poor supportA PORTION OF TOP FUSELAGE SKIN EXTENDING FROM WINDSHIELD LINE AFT TO INSTRUMENT PANEL WAS REMOVED. SUBMITTER SUSPECTS THIS SECTION OF SKIN REMOVED TO MAKE IT EASIER TO INSTALL A NEW 1-PIECE SPEED SLOPE WINDSHIELD. THIS SECTION PROVIDES STRUCT STRENGTH AND SSep 1, 1996 · N4645D · Beech G35 · Instrument PanelSDR 96ZZZX3061Line · deterioratedDURING ANNUAL INSPECTION, ALL FLEXIBLE FUEL AND BRAKE LINES WERE FOUND SEVERELY DETERIORATED. SUBMITTER STATES THIS IS AN ONGOING PROBLEM. A TIME LIMIT SHOULD BE PLACED ON THESE ITEMS. RECOMMEND 10 YEARS OR 1500 HRS. THESE LINES APPEARED TO BE ORIGINAL.Mar 28, 1996 · N4575D · Beech G35 · Aircraft Fuel Distribution SystemSDR 96ZZZX3060Line · chafedDURING ANNUAL INSPECTION AND GEAR RETRACTION TEST, DISCOVERED RT AUXILIARY FUEL TANK LINE WHICH PASSES ACROSS THE TOP OF THE LANDING GEAR HAD BEEN CHAFED ABOUT ONE-HALF OF ITS THICKNESS DUE FROM A GREASE FITTING ON THE FORWARD ROLLER WHICH WAS RUBBING EACH TIMMar 28, 1996 · N4575D · Beech G35 · Aircraft Fuel Distribution System
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