Beech 58

Service difficulty reports · 1,000

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 = '58'
  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 PT196042Jam-Nut · looseRT PROPELLER RPM DECREASES TOWARD FEATHER BEFORE PROP CONTROL IS BROUGHT BACK INTO FEATHER DETENT. FOUND JAM NUT ON FEATHER SPEED ADJUSTMENT SCREW HAD WORKED LOOSE AND THE ADJUSTMENT SCREW WAS BACKING OUT. THE DESIGN OF THESE NUTS HAS BEEN CHANGED IN THE LASJun 15, 2006 · N376W · Beech 58 · Propeller Feathering/ReversingSDR BSYA200600016Indicator · malfunctionedAFTER 20 MINS INTO FLIGHT PILOT REPORTED AIR SPEED WENT TO ZERO AND THE ALTIMETER READ 3000 FEET HIGH. RETURNED TO LCK WHERE MAINTENANCE REMOVED AND REPLACED VSI INDICATOR AND REPLACED TWO PINCHED STATIC LINES, SYSTEM OPS CHECKS GOOD.May 11, 2006 · N65FS · Beech 58 · Rate of Climb IndicatorSDR BSYA200600014Squat Switch · out of adjustON TAKEOFF OUT OF LCK PILOT SELECTED GEAR UP BUT NOTHING HAPPENED, RETURNED TO LCK NO PROBLEMS. MAINTENANCE FOUND RIGHT SQUAT SWITCH OUT OF ADJUSTMENT. ADJUSTED SWITCH AND SWUNG GEAR SEVERAL TIMES, OPS CHECKS GOOD.May 11, 2006 · N2027V · Beech 58 · Landing Gear Position and WarningSDR 2006FA0000488Gasket · swollenTHE FUEL FILTER GASKETS SWELLED CAUSING THE FUEL FILTERS TO LEAK A LARGE AMOUNT OF FUEL OVERBOARD WHILE IN FLIGHT. THE PILOT WAS UNAWARE OF THE LOSS OF FUEL UNTIL AFTER HE LANDED. APPARENTLY GASKETS ARE NOT COMPATIBLE WITH CURRENT BLENDS OF 100LL. WAS TOLD BY May 11, 2006 · N2335R · Beech 58 · Aircraft Fuel Filter/StrainerSDR 2006FA0000487Gasket · swollenTHE FUEL FILTER GASKETS SWELLED CAUSING THE FUEL FILTERS TO LEAK A LARGE AMOUNT OF FUEL OVERBOARD WHILE IN FLIGHT. THE PILOT WAS UNAWARE OF THE LOSS OF FUEL UNTIL AFTER HE LANDED. APPARENTLY GASKETS ARE NOT COMPATIBLE WITH CURRENT BLENDS OF 100LL. WAS TOLD BYMay 11, 2006 · N2335R · Beech 58 · Aircraft Fuel Filter/StrainerSDR 2006FA0000486Gasket · swollenTHE FUEL FILTER GASKETS SWELLED CAUSING THE FUEL FILTERS TO LEAK A LARGE AMOUNT OF FUEL OB WHILE IN FLIGHT. THE PILOT WAS UNAWARE OF THE LOSS OF FUEL UNTIL AFTER LANDING. APPARENTLY GASKETS ARE NOT COMPATIBLE WITH CURRENT BLENDS OF 100LL. WAS TOLD BY MFG TECHMay 11, 2006 · N2335R · Beech 58 · Aircraft Fuel Filter/StrainerSDR 2006FA0000538Camshaft · wornCOMPRESSION CHECKED ENGINE, NR 2 CYLINDER 40/80. REMOVED NR 2 CYL FOR REPAIR. INSP INSIDE OF ENG, FOUND NR 1 CYL EXHAUST LIFTER/CAM LOBE BADLY WORN. UNKNOWN HOW LONG IT HAS BEEN LIKE THIS, KNOW IT WOULD NOT HAVE LASTED TOO MUCH LONGER. REBUILT/ZERO TIMED. May 10, 2006 · N866SH · Beech 58 · Reciprocating Engine Power SectionSDR 2006FA0000580Connecting Rod · unknown50 MILES OUT OF HOME BASE, PILOT HEARD A (POP) CAME FROM LEFT ENGINE, THEN NOTICED OIL PRESSURE START THE FALL. FEATHERED PROP AND SECURED ENGINE. MADE A UNEVENTFUL LANDING. INSP FOUND NR 4 CYLINDER ON L/E DDEPARTED FROM ENGINE AND NR 4 ROD BROKEN. SUSPECMay 8, 2006 · N106GA · Beech 58 · Reciprocating Engine Power SectionSDR XGN2006F00050Cylinder · crackedCYLINDERS WERE FOUND DURING COMPRESSION CHECK AT THE 100 HR INSPECTION. WE ARE USING A SOAP SOLUTION TO DETECTED CRACKS IN THE EXHAUST SIDE OF THE CYLINDER WHILE DOING A COMPRESSION CHECK. WE ARE DOING COMPRESSION CHECKS EACH 50 HRS. 3 CRACKED CYLINDER WEREMay 4, 2006 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR XGN2006F00049Cylinder · crackedCYLINDERS WERE FOUND DURING COMPRESSION CHECK AT THE 100 HR INSPECTION. WE ARE USING A SOAP SOLUTION TO DETECT CRACKS IN THE EXHAUST SIDE OF THE CYLINDER WHILE DOING A COMPRESSION CHECK. WE ARE DOING COMPRESSION CHECKS EACH 50 HRS. 3 CRACKED CYLINDER WERE FMay 4, 2006 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR 2006FA0000511Line · chafed2 LINES CHAFFING TOGETHER. NEED TO SEPARATE THE LINES. LOW OIL PSI IN FLIGHT. PILOT SHUTOFF ENGINE IN FLIGHT AND LANDED THE AIRCRAFT. REMOVED AND REPLACED THE LINE. (K)May 4, 2006 · N251P · Beech 58 · Engine Oil Distribution (Airframe Furnished)SDR CA060512001Window · separated(CAN) EMERGENCY EXIT WINDOW OPENED ON TAKEOFF. WINDOW WENT FROM VENT POSITION TO EXIT POSITION INTO FREE AIR AND HINGE BROKE OFF AND WINDOW DETACHED FROM AIRCRAFT. IT IS POSSIBLE THAT AT SOME PRIOR FLIGHT THE WINDOW WAS OPENED INCORRECTLY. WE HAVE OPERATED AMay 1, 2006 · Beech 58 · Passenger Compartment WindowsSDR 2006FA0000457Cylinder · crackedNR 4 CYLINDER CRACKED AFT OF VALVES. (STILL HAD GOOD COMPRESSION BUT COULD HEAR AIR) (LT ENGINE) (K)Apr 18, 2006 · N3149P · Beech 58 · Reciprocating Engine Cylinder SectionSDR 2006FA0000456Cylinder · crackedNR 6 CYLINDER CRACKED AFT OF VALVES. (STILL HAD GOOD COMPRESSION COULD HEAR AIR.) (LT ENGINE) (K)Apr 18, 2006 · N3149P · Beech 58 · Reciprocating Engine Cylinder SectionSDR 2006FA0000455Cylinder · crackedNR 2 CYLINDER COMPLETELY CRACKED ALL THE WAY AROUND AFT OF VALVES. (LT ENGINE) (K)Apr 18, 2006 · N3149P · Beech 58 · Reciprocating Engine Cylinder SectionSDR 2006FA0000454Cylinder · crackedNR 5 CYLINDER CRACKED AFT OF VALVES. (STILL HAD GOOD COMPRESSION BUT COULD HEAR AIR) (LT ENGINE) (K)Apr 18, 2006 · N3149P · Beech 58 · Reciprocating Engine Cylinder SectionSDR 2006FA0000453Cylinder · crackedNR 1 CYLINDER CRACKED AT SPARK PLUG HOLE. (RT ENGINE) (K)Apr 18, 2006 · N3149P · Beech 58 · Reciprocating Engine Cylinder SectionSDR 79965Hub · corrodedHUB CORRODED BEYOND REPAIR IAW MFG OVERHAUL MANUAL.Apr 4, 2006 · Beech 58 · Propeller Hub SectionSDR BSYA200600011Rod · brokenON APPROACH INTO BDL PILOT HAD NO GEAR DOWN AND LOCK INDICATION, TRIED TO HAND CRANK NO HELP. TRIED RESETTING CIRCUIT BREAKER THEN GEAR MOVED AND DOWN AND LOCK LIGHT CAME ON. LANDED, NO PROBLEMS. MAINTENANCE FOUND GEAR EXTEND/RETRACT RODS LEFT AND RIGHT BENMar 15, 2006 · N33DK · Beech 58 · Landing Gear Retraction/Extension SystemSDR 2006FA0000360Spinner · crackedSPINNER HAS CRACKS IN 3 PLACES NEAR SCREW HOLES ADJACENT TO PROPELLER BLADES. (K)Mar 14, 2006 · Beech 58 · Propeller Spinner SectionSDR BSYA200600009Motor · burned outEN ROUTE FROM BFM TO BHM PILOT DECLARED AN EMERGENCY LANDING DUE TO AN OVERWELMING ODOR OF NOXIOUS GAS IN COCKPIT. MAINTENANCE FOUND LANDING GEAR MOTOR BURNED OUT. REMOVED AND REPLACED MOTOR, OPS CHECKS GOOD.Feb 24, 2006 · N36901 · Beech 58 · Landing Gear Retraction/Extension SystemSDR 3969Line · chafedDURING SCHEDULED INSPECTION FOUND FUEL CROSSFEED LINE IN RT WHEEL WELL CHAFED 75 PERCENT THROUGH BY LANDING GEAR RETRACT ROD.Feb 24, 2006 · N6458C · Beech 58 · Aircraft Fuel Distribution SystemSDR BSYA200600005Throttle Cable · unknownAIRCRAFT EN ROUTE FROM SDF TO BNA, RIGHT ENGINE GO TO FULL THROTTLE, PILOT ELECTED TO SHUT ENGINE DOWN AND CONTINUE TO BNA, LANDED NO PROBLEMS. REMOVED AND REPLACED CABLE, OPS CHECKS GOOD.Feb 17, 2006 · N3695V · Beech 58 · Power LeverSDR 2006FA0000173Line · wornTHE CROSS FEED LINE PN 002-92000-51 WAS IMPROPERLY MANUFACTURED WHICH CAUSED THE RT LANDING GEAR DRIVE TUBE TO CONTACT, AND ABRADE THE LINE DURING LANDING GEAR RETRACTION. THE ABRASION HAD PROGRESSED TO THE POINT THAT ONLY 10 PERCENT OF THE WALL THICKNESS REMFeb 13, 2006 · N202P · Beech 58 · Aircraft Fuel Distribution SystemSDR 2006FA0000307Engine · unknownRT ENGINE WAS STARTED AND PILOT NOTICED LOW OIL PRESSURE. INSTALLED ANOTHER GAUGE IN LINE TO VERIFY PROBLEM RAN ENGINE, OIL PRESSURE CERTIFIED LOW. CHANGED OIL AND INSPECTED FILTER. FOUND NO OBVIOUS PROBLEMS, STARTED ENGINE, HAD NO OIL PRESSURE, PULLED RELIFeb 8, 2006 · N106GA · Beech 58 · Engine (Reciprocating)SDR 917SFRod · chafedDURING SCHEDULED INSPECTION IT WAS DISCOVERED THAT THE LANDING GEAR RETRACT PUSH-PULL TUBE HAD BEEN STRIKING THE FUEL LINES IN THE RT GEAR WELL. DAMAGE TO THE PUSH-PULL TUBE WAS MINIMAL AND LIMITED TO THE PAINT BEING REMOVED, DAMAGE TO THE FUEL LINES WAS SUCHFeb 1, 2006 · N917SF · Beech 58 · Main Landing GearSDR 2006FA0000141Pump · malfunctionedFUEL PUMP FAILED AFTER LANDING. ENGINE QUIT ON ROLL OUT. PUMP WOULD NOT PRODUCE ENOUGH PRESSURE TO SUSTAIN AN ENGINE RPM ABOVE IDLE. (K)Jan 26, 2006 · N3214H · Beech 58 · Engine Fuel PumpSDR 2006FA0000077Cylinder Head · separatedAPPEAR THAT THERE WAS A CRACK IN THE CYLINDER HEAD AT THE EXHAUST VALVE SEAT, WHICH PROPOGATED DURING OPERATION UNTIL THE CYLINDER HEAD FAILED AND SEPARATED FROM THE CYLINDER. (K)Jan 16, 2006 · N7209B · Beech 58 · Reciprocating Engine Cylinder SectionSDR BSYA20060001Door · departedCHECK RIDE PILOTS WERE SHOWING TRAINING PILOTS EMERGENCY EXIT PROCEDURES, AFTER THEY WERE FINISHED REQUESTED MAINTENANCE TO RE-SAFETY EMERGENCY EXIT. BEFORE MAINTENANCE HAD A CHANCE TO SAFETY WINDOW A CHECK RIDE PILOT AND TRAINEE WENT OUT FOR TRAINING, ON TAKJan 13, 2006 · N367S · Beech 58 · Emergency ExitsSDR 2006FA0000084Cylinder Head · crackedENGINE CYLINDER CRACKED AT BARREL AND HEAD. (K)Jan 10, 2006 · N8195R · Beech 58 · Reciprocating Engine Cylinder SectionSDR FPI2006F00003Cylinder · crackedCRACKED AT BARREL AND HEAD. (K)Jan 10, 2006 · N8195R · Beech 58 · Reciprocating Engine Cylinder SectionSDR FPI2006F00000Cylinder · crackedCRACKED AT BARREL AND HEAD. (K)Jan 10, 2006 · N955HE · Beech 58 · Reciprocating Engine Cylinder SectionSDR 2006FA0000051Cylinder · crackedENGINE CYLINDER CRACKED AT BARREL AND HEAD. (K)Jan 10, 2006 · N8195R · Beech 58 · Reciprocating Engine Cylinder SectionSDR 2006FA0000050Cylinder · crackedENGINE CYLINDER CRACKED AND BARREL AND HEAD.Jan 10, 2006 · N8195R · Beech 58 · Reciprocating Engine Cylinder SectionSDR 2006FA0000060Bushing · wornAILERON TRIM MADE POPPING NOISE AS CONTROL WAS ROTATED. FOUND BUSHING FOR CONTROL SHAFT IN PEDESTAL SEVERELY WORN ALLOWING U-JOINT TO CONTACT STRUCTURE AS CONTROL WAS ROTATED. TRIM CABLE TENSION WAS WITHIN LIMITS, NO REASON FOR ACCELERATED WEAR NOTED. BUSHIJan 5, 2006 · N376W · Beech 58 · Aileron TabsSDR BSYA200500032Landing Gear · malfunctionedON TAKEOFF OUT OF DTW PILOT SELECTED GEAR UP AND NOTHING HAPPENED. RETURNED TO DTW.Dec 20, 2005 · N78RE · Beech 58 · Landing Gear Retraction/Extension SystemSDR BSYA20050034Door · openON DEPARTURE, PILOTS DOOR POPPED OPEN, PILOT RETURNED TO BLOCK REOCCURRED DOOR AND CONTINUED ON WITH FLIGHT.Dec 20, 2005 · N3695V · Beech 58 · Passenger/Crew DoorsSDR BSYA200500031Door · openON TAKEOFF OUT, CREW DOOR CAME OPEN AND PILOT RETURNED TO BASE SECURED DOOR THEN TOOK OFF TO CONTINUE FLIGHT.Dec 19, 2005 · N3695V · Beech 58 · Passenger/Crew DoorsSDR AU510002188Bolt · shearedCRANKSHAFT GEAR RETAINING BOLTS SHEARED. LOSS OF DRIVE TO GOVERNOR.Dec 12, 2005 · Beech 58 · Reciprocating Engine Power SectionSDR AU510002007Drive Shaft · failedCSU DRIVE ASSEMBLY FAILED. INVESTIGATION CONTINUING.Dec 12, 2005 · Beech 58 · Reciprocating Engine Rear SectionSDR AU510001900Coupling · shearedRT VACUUM PUMP FAILED. INVESTIGATION FOUND THE PUMP JAMMED AND FULL OF CARBON VANE DEBRIS. DRIVE SHAFT FAILED AT SHEAR POINT. PUMP IS OUTSIDE OF THE SN RANGE AS INDICATED IN TEMPEST SB-003.Dec 12, 2005 · Beech 58 · Vacuum Distribution SystemSDR AU510001670Arm · shearedPILOT`S LT RUDDER PEDAL ARM SHEARED.Dec 12, 2005 · Beech 58 · Rudder Control SystemSDR AU510001656Line · leakingMAIN FUEL LINE LOCATED IN RT NACELLE LEAKING IN AREA ABOVE THE ELECTRIC FUEL PUMP. INVESTIGATION FOUND LINE CORRODED.Dec 12, 2005 · Beech 58 · Aircraft Fuel Distribution SystemSDR AU510001653Vent Line · leakingRT FUEL VENT LEAKING. INVESTIGATION FOUND THAT THE SEALANT AROUND THE VENT TUBE IN THE RT WET WING FUEL TANK HAD DETERIORATED ALLOWING FUEL TO LEAK INTO THE VENT LINE.Dec 12, 2005 · Beech 58 · Aircraft Fuel Distribution SystemSDR BSYA200500030Seal · slippedON TAKEOFF, PILOT NOTICED SMOKE COMING FROM LT ENGINE, PILOT ELECTED TO RETURN TO DEPARTURE. MAINTENANCE FOUND THAT THE NEWLY INSTALLED VACUUM PUMP SEAL HAD SLIPPED DURING INSTALLATION. REMOVED AND REPLACED SEAL, OPS CHECKS GOOD.Dec 12, 2005 · N400RP · Beech 58 · Vacuum SystemSDR 2006FA0000006Valve · out of rigTHE NEW VALVE RECEIVED FROM THE MFG WAS INTERNALLY CLOCKED INCORRECTLY. AFTER INSTALLATION, NO FUEL WAS AVAILABLE FROM EITHER THE ON OR CROSSFEED PORTS. AFTER MALVE REMOVAL, IT WAS CONFIRMED THAT THE VALVE REMAINED IN THE OFF POSITION REGARDLESS OF MOVMENT TDec 8, 2005 · N2347G · Beech 58 · Standard Practices/StructuresSDR AU510001580Frame · cracked(AUS) FUSELAGE FRAMES PN P1756-02/1 AND PN P1756-01/1 LOCATED IN WING FORWARD SPAR CARRY THROUGH SECTION CRACKED. FOUND DURING INSPECTION IAW AD. (CASA NR 510001580)Dec 7, 2005 · Beech 58 · Wing SparSDR BSYA200500027Squat Switch · frozenON TAKEOFF, PILOT SELECTED GEAR UP AND NOTHING HAPPENED, THEN RETURNED TO DEPARTURE, NO PROBLEMS. MAINTENANCE FOUND LT MAIN GEAR SQUAT SWITCH PACKED WITH SNOW, THAWED OUT SWITCH OPS CHECKS GOOD.Dec 6, 2005 · N2064V · Beech 58 · Landing Gear Position and WarningSDR 2005FA0001620Tube · chafedWHILE RETRACTING AND EXTUENDING LANDING GEAR FOR ADJUSTMENT OF DROOPING IB MAIN WHEEL DOOR NOTED ABNORMAL NOISE AND VIBRATION DURING APPROXIAMTE MID-TRAVEL. INVESTIGATED FURTHER, FOUND RT MLG RETRACT ROD ASSY. CHAFING ON PN 002-920000-49 AND PN 002-920000-51Dec 2, 2005 · N200KH · Beech 58 · Aircraft Fuel Distribution SystemSDR 2005FA0001582Pneumatic System · contaminatedPNEUMATIC SYSTEM INSPECTED AND TRACES OF WATER WERE FOUND IN THE EJECTOR VALVE AND AREA BELOW THE VALVE. FURTHER INSPECTION REVEALED WATER IN THE PNEUMATIC MANIFOLD VALVE AND ASSOCIATED PLUMBING. APPROXIMATELY .5 OZ OF WATER WAS REMOVED FROM THE SYSTEM. THENov 30, 2005 · N202P · Beech 58 · Pneumatic Distribution System
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