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 QC42002F00003Bracket · brokenDURING INSPECTION, FOUND A MOUNTING LOBE COMPLETELY BROKEN OFF THE BRACKET THAT HOLDS THE AIR CONDITIONER COMPRESSOR ON THE FRONT OF THE LEFT ENGINE. THIS BRACKET IS ATTACHED TO THE ENGINE CASE WITH 4 BOLTS. WHILE INSTALLING THE NEW BRACKET, IT REQUIRED INSTNov 6, 2002 · N220SA · Beech 58 · Cabin Compressor SystemSDR QC42002F00000Bracket · crackedFOUND CRACKED BRACKETS IN THE AFT HINGE OF THE INBOARD MAIN GEAR DOOR. RIGHT SIDE, AFT HINGE, FORWARD BRACKET: CRACKED. LEFT SIDE, AFT HINGE, AFT BRACKET: CRACKED. BOTH BRACKETS CRACKED IN THE TRANSITION FROM THE .5 INCH FLANGE TO THE WIDE FLANGE THAT ATTACNov 4, 2002 · N220SA · Beech 58 · Landing Gear DoorsSDR AUS20021229Connector · corroded(AUS) RH WING MAIN FUEL TANK OUTLET FUEL RESERVOIR CONNECTOR CORRODED DUE TO WATER CONTAMINATION.Oct 23, 2002 · Beech 58 · Aircraft Fuel Distribution SystemSDR AUS20021228Connector · corroded(AUS) LH WING MAIN FUEL TANK OUTLET FUEL RESERVOIR CONNECTOR CORRODED DUE TO WATER CONTAMINATION.Oct 23, 2002 · Beech 58 · Aircraft Fuel Distribution SystemSDR AUS20021227Fitting · corroded(AUS) LH WING REAR UPPER ATTACHMENT BATHTUB FITTING CORRODED. PERSONNEL/MAINTENANCE ERROR.Oct 23, 2002 · Beech 58 · Wing, Fuselage Attach FittingsSDR AUS20021226Fitting · corroded(AUS) RH WING TOP FORWARD ATTACHMENT BATHTUB FITTING CORRODED.PERSONNEL/MAINTENANCE ERROR.Oct 23, 2002 · Beech 58 · Wing, Fuselage Attach FittingsSDR AUS20021225Fitting · corroded(AUS) RH WING REAR TOP ATTACHMENT BATHTUB FITTING CORRODED. PERSONNEL/MAINTENANCE ERROR.Oct 23, 2002 · Beech 58 · Wing, Fuselage Attach FittingsSDR AUS20021224Fitting · damaged(AUS) LH WING FORWARD TOP ATTACHMENT BATHTUB FITTING CORRODED AND DAMAGED. PERSONNEL/MAINTENANCE ERROR.Oct 23, 2002 · Beech 58 · Wing, Fuselage Attach FittingsSDR AUS20021223Fitting · damaged(AUS) RH WING FORWARD LOWER ATTACHMENT BATHTUB FITTING CORRODED AND DAMAGED. PERSONNEL/MAINTENANCE ERROR.Oct 23, 2002 · Beech 58 · Wing, Fuselage Attach FittingsSDR AUS20021222Fitting · damaged(AUS) LH WING FORWARD LOWER ATTACHMENT BATHTUB FITTING CORRODED AND DAMAGED. PERSONNEL/MAINTENANCE ERROR.Oct 23, 2002 · Beech 58 · Wing, Fuselage Attach FittingsSDR NZZ2002F00000Uplock Cable · brokenFOUND RT LANDING GEAR UP/DOWN LOCK CABLE BROKEN AT GEAR MOTOR IN FUSELAGE, RELEASING DOWN LOCK. CABLE HAD BROKEN AT SWAG. TUGGED ON LT CABLE, CABLE SEPARATED AT LOWER SWAGE.Oct 3, 2002 · N81FD · Beech 58 · Landing Gear Position and WarningSDR CQ92002F00001Motor · burnedGEAR MOTOR FAILED ON EXTENSION CYCLE. HAD DIFFICULTY MANUALLY EXTENDING LANDING GEAR. A/C WAS SLOWED MUCH AS POSSIBLE AND PLACED ON AUTOPILOT. AFTER SEVERAL ATTEMPTS, PILOT WAS ABLE TO GET GEAR DOWN SAFE. UPON INSP OF A/C, IT WAS FOUND THAT EMERGENCY EXTENSep 23, 2002 · N584MW · Beech 58 · Landing Gear Retraction/Extension SystemSDR BSY2002F00022Downlock Switch · inoperativeGOING INTO (DET) HAD NO NOSE GEAR DOWN AND LOCK LIGHT, LANDED OK. FOUND NOSE GEAR DOWN AND LOCK SWITCH BAD. REMOVED AND REPLACED SWITCH OPS CHECKS GOOD.Sep 10, 2002 · N2064V · Beech 58 · Landing Gear Position and WarningSDR TC42002F00000Line · chafedLUBRICATION LINE FROM PROPELLER UNFEATHERING ACCUMULATOR IS RUBBED BY FUEL LINE AT THROTTLE SERVO. RUBBED HOLE IN LINE CAUSING PROPELLER TO FEATHER.Sep 3, 2002 · N1888W · Beech 58 · Propeller GovernorSDR H3A2002F00000Duct · separatedUNSCHEDULED LANDING WAS MADE DUE TO RIGHT ENGINE SURGING. EXAMINATION OF ENGINE REVEALED A 1 X 2 INCH SECTION OF DUCT WAS MISSING BETWEEN THE AIR BOX AND THROTTLE BODY. PART OF DUCT SEPARATED AND WENT THROUGH INDUCTION SYSTEM AND CYLINDER CAUSING TEMPORARY SAug 26, 2002 · N58CK · Beech 58 · Engine Bleed Air SystemSDR 2002FA0001056Hinge · misalignedDURING ROUTINE MAINTENANCE, TECH NOTICED LT AILERON MISALIGNED WITH TRAILING EDGE OF WING AT AILERON WELL. FOUND THAT OUTBOARD AILERON HINGE BOTTOM ATTACH SCREWS NOT IN HINGE ATTACH HOLES BUT CAUGHT BETWEEN AFT PORTION OF HINGE AND AILERON ATTACH HOLES. SCREAug 22, 2002 · N793DW · Beech 58 · AileronsSDR BSY2002F00019Switch · bentLANDING GEAR WOULD NOT EXTEND EITHER ELECTRICALLY OR MANUALLY, FEATHERED ENGINES AND LANDED GEAR UP. FOUND UP LIMIT SWITCH ACTUATING TAB BENT, NOT ALLOWING TAB TO HIT. UP LIMIT SWITCH GEAR BOX WENT PAT UP LIMITS. JAMMING GEAR BOX, COULD NOT CRANK GEAR DOWN.Aug 14, 2002 · N58TA · Beech 58 · Landing Gear Retraction/Extension SystemSDR FFK2002F00000Adapter · inoperativeLEFT ENGINE STARTER ADAPTER ACCESSORY, INOPERATIVE. ENGINE WILL NOT TURN OVER, SUSPECT BROKEN SPRING, IN CLUTCH ACCESSORY UNIT HAS 59 HOURS.Jul 22, 2002 · N11HW · Beech 58 · Engine CrankingSDR 2002FA0000920Bracket · crackedDURING 100 HOUR INSPECTION FO THE LT ENGINE, THE UPPER ARM OF THE AIR CONDITION COMPRESSOR BRACKET WAS FOUND TO BE CRACKED. IT APPEARS AS IF IT WAS NOT SHIMMED CORRECTLY. DURING INITIAL INSTALATION WHICH PRELOADED THE ARM AND CRACKED. C/A: PROPERLY SHIM BRAJul 19, 2002 · N658DG · Beech 58 · Cabin Compressor SystemSDR HMG2002F00001Bulkhead · crackedDURING ANNUAL INSPECTION, CRACKS WERE FOUND IN BULKHEAD FS 257.6.Jul 8, 2002 · N82LB · Beech 58 · Fuselage Main, BulkheadSDR 2002FA0000832Magneto · failedON A GROUND RUN UP, PILOT REPORTED A BAD MAG DROP. AFTER PULLING MAGNETO OFF OF THE ENGINE, IT APPEARS THE MAGNETO FAILED. THE PLASTIC DRIVE GEARS WERE STRIPPED AS WELL AS THE MAGNETO RETAINER DRIVE COUPLING AND DRIVE COUPLING RUBBER BUSHING WERE DAMAGED. Jul 2, 2002 · N11HW · Beech 58 · Magneto/DistributorSDR CA020726008Throttle Cable · broken(CAN) APPROXIMATELY 6 INCHES FROM ENGINE END THROTTLE CABLE BROKE. REPLACED THROTTLE CABLE.Jun 18, 2002 · Beech 58 · Power LeverSDR BSY2002F00012Channel · wornON TAKEOFF, CABIN DOOR POPPED OPEN ON TOP SIDE, RETURNED TO AIRPORT. REPLACED UPPER TOP DOOR HOOK AND CHANNEL ASSEMBLY. REPLACED WORN DOOR HANDLE.Jun 7, 2002 · N297AT · Beech 58 · Passenger/Crew DoorsSDR BSY2002F00011Handle · wornON TAKEOFF, OUT OF CABIN DOOR POPPED OPEN ON TOP SIDE, RETURNED TO AIRPORT REPLACED UPPER TOP DOOR HOOK AND CHANNEL ASSEMBLY. REPLACED WORN DOOR HANDLE.Jun 7, 2002 · N297AT · Beech 58 · Passenger/Crew DoorsSDR BSY2002F00010Latch · failedON TAKEOFF, CABIN DOOR POPPED OPEN ON TOP SIDE, RETURNED TO AIRPORT. REPLACED UPPER TOP DOOR HOOK AND CHANNEL ASSEMBLY REPLACED WORN DOOR HANDLE.Jun 7, 2002 · N297AT · Beech 58 · Passenger/Crew DoorsSDR 2002FA0000863Brace · failedNOSE RETRACT BRACE FAILED ALLOWING NOSE GEAR TO RETRACT UPON LANDING.May 22, 2002 · N6577S · Beech 58 · Nose/Tail Landing GearSDR BSY2002F00009Throttle Cable · failedRIGHT THROTTLE CABLE BROKE ON FINAL APPROACH. SHUT ENGINE DOWN, FEATHERED PROP, LANDED. NO PROBLEM. REMOVED AND REPLACED RIGHT THROTTLE CABLE OPS. GOOD.May 9, 2002 · N4098S · Beech 58 · Power LeverSDR AUS20020473Fitting · worn(AUS) RT HORIZONTAL STABILISER ATTACHMENT HOLES WORN. HOLES IN STUB SPAR ALSO WORN.May 6, 2002 · Beech 58 · Horizontal Stabilizer Miscellaneous StructureSDR 181421Indicator · malfunctionedPILOT REPORTED NO GEAR DOWN AND LOCKED INDICATION WAS OBSERVED ON PREPARATION FOR LANDING. CYCLED THE GEAR WITH NO CHANGE IN THE INDICATION. AFTER A SAFE, NORMAL LANDING AND SHUTDOWN, HE TURNED THE MASTER BACK ON AND THE GEAR INDICATION WAS NORMAL. THE AIRCApr 9, 2002 · N18142 · Beech 58 · Landing Gear Position and WarningSDR 2002FA0000500Gyro · failedGYRO FAILURE.Apr 2, 2002 · N6726S · Beech 58 · Attitude Gyro and Indicating SystemSDR 2002FA0000499Gyro · failedGYRO FAILURE.Apr 2, 2002 · N6726S · Beech 58 · Attitude Gyro and Indicating SystemSDR 2002FA0000498Gyro · failedGYRO FAILURE.Apr 2, 2002 · N6726S · Beech 58 · Directional Gyro and Indicating SystemSDR AUS20020269Nut · wrong part(AUS) UPPER LT WING FORWARD ATTACHMENT NUT INCORRECT PART. UNAPPROVED PART.Mar 20, 2002 · Beech 58 · Wing, Fuselage Attach FittingsSDR AUS20020268Nut · wrong part(AUS) LOWER LT WING REAR ATTACHMENT NUT INCORRECT PART. UNAPPROVED PART.Mar 20, 2002 · Beech 58 · FastenersSDR AUS20020267Nut · wrong part(AUS) LOWER RT WING REAR ATTACHMENT NUT INCORRECT PART. UNAPPROVED PART.Mar 20, 2002 · Beech 58 · FastenersSDR FPI2002F00008Control Cable · frayedDURING A ROUTINE INSPECTION, THE ELEVATOR CONTROL CABLE WAS FRAYING IN THE AREA OF THE FORWARD LOWER CABLE PULLEY.Mar 15, 2002 · N950JP · Beech 58 · Elevator Control SystemSDR FPI2002F00007Control Cable · frayedDURING A ROUTINE INSPECTION, THE ELEVATOR CONTROL CABLE WAS FRAYING IN THE AREA OF THE FORWARD LOWER CABLE PULLEY.Mar 15, 2002 · N46US · Beech 58 · Elevator Control SystemSDR AUS20020190Fuel Tank · contaminated(AUS) RT WING TIP TANK CONTAMINATED. SUSPECT NON-APPROVED SEALANT USED. POSSIBLE FILTER BLOCKAGE.Mar 11, 2002 · Beech 58 · Fuel StorageSDR 2002FA0000385Gauge · mismanufacturedWHILE REPLACING LEFT WING FUEL SIGHT GAUGE IT WAS FOUND THE NEW PART HAD FLOAT ARM INDEXED 180 DEGREE FROM ORIGINAL GAUGE. THIS DIFFERENCE CAUSED FLOAT ARM TO CONTACT LEADING EDGE CURVE AND GAUGE WOULD NOT READ BELOW 45 GALLONS. WHEN ADDITIONAL PART WAS ORDEMar 11, 2002 · N872AN · Beech 58 · Fuel Quantity IndicatorSDR BSY2002F00002Connector · failedAFTER TAKEOFF, LT ENGINE, OIL TEMPERATURE, SHOT UP TO RED LINE, RETURNED TO AIRPORT AFTER FEATHERING ENGINE. FOUND PIN PULLED OUT OF OIL TEMPERATURE CONNECTOR PLUG, INSTALLED NEW CONNECTOR PLUG, OPS CHECKS GOOD.Feb 25, 2002 · N33DK · Beech 58 · Engine Oil TemperatureSDR AUS20020121Selector Switch · corroded(AUS) RT FUEL SELECTOR VALVE EXCESSIVELY CORRODED DUE TO CONTAMINATION.Feb 11, 2002 · Beech 58 · Fuel Selector/Shut-Off ValveSDR AUS20020120Selector Switch · corroded(AUS) LT FUEL SELECTOR VALVE EXCESSIVELY CORRODED DUE TO CONTAMINATION.Feb 11, 2002 · Beech 58 · Fuel Selector/Shut-Off ValveSDR BSY2002F00004Tach Generator · inoperativeLEFT TACH QUIT AFTER TAKE OFF, RETURNED TO AIRPORT. REMOVED AND REPLACED THE GENERATOR OPS CHECKS GOOD.Feb 8, 2002 · N3703Q · Beech 58 · Engine RPM Indicating SystemSDR BSY2002F00003Squat Switch · frozenLANDING GEAR WOULD NOT GO UP. FOUND SQUAT SWITCH FROZEN. THAWED OUT SWITCH CLEANED AND LUBED CYCLED GEAR. OPS CHECK GOOD.Feb 8, 2002 · N696BD · Beech 58 · Landing Gear Position and WarningSDR AUS20020095Cable · wrong part(AUS) LT PROPELLER CONTROL CABLE DIAMETER WAS FOUND TO BE LESS THAN THE DIAMETER OF THE RH SIDE CABLE. LT CABLE WAS4.762MM (0.1875IN) INDIAMETER AND THE RT CABLE WAS 6.350MM (0.25IN). UNAPPROVED PART.Feb 8, 2002 · Beech 58 · Propeller Controlling SystemSDR ODAR0184Pump · failedPILOT EXPERIENCED A DUAL VACUUM PUMP FAILURE IN VFR CONDITIONS.Feb 7, 2002 · N707PW · Beech 58 · Vacuum Distribution SystemSDR BSY2002F00005Heater · failedPILOT NOTICED SMOKE IN COCKPIT, LANDED AT AIRPORT. MAINTENANCE INSPECTED AIRCRAFT FOUND NO ELECRTICAL PROBLEMS, TURNED ON HEATER AND CABIN FILLED WITH SMOKE. REMOVED AND REPLACED HEATER ASSY.Feb 7, 2002 · N4AW · Beech 58 · Heating SystemSDR 2002FA0000333Pump · inoperativePILOT EXPERIENCED DUAL VACUUM PUMP FAILURE IN FLIGHT IN VFR CONDITIONS.Feb 7, 2002 · N58WC · Beech 58 · Vacuum SystemSDR 2002FA0000332Pump · inoperativePILOT EXPERIENCED DUAL VACUUM PUMP FAILURE IN FLIGHT IN VFR CONDITIONS.Feb 7, 2002 · N58WC · Beech 58 · Vacuum Distribution SystemSDR EWK2002F00001Line · corrodedDEEP CORROSION ON FUEL PRESSURE LINE AT CONJUNCTION OF FUEL LINE AND DEFROSTER HEAT DUCT. INSULATE FUEL LINE FROM HEAT DUCT. DANGER: POTENTIAL FOR FIRE.Feb 6, 2002 · N6652A · Beech 58 · Engine Fuel Distribution
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