Beech B300

Service difficulty reports · 598

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 = 'B300'
  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 JEM2002F00005Crossbeam · crackedCROSSBEAM IS RIVETED TO THE FUSELAGE IMMEDIATELY FORWARD OF THE RIGHT EMERGENCY EXIT OPENING. THE CRACK WAS LOCATED ON THE CROSSBEAM ADJACENT TO THE FORWARD, LOWER CORNER OF THE EMERGENCY EXIT OPENING.Aug 16, 2002 · N350KG · Beech B300 · Fuselage Main, StructureSDR JEM2002F00004Crossbeam · crackedTHE CROSSBEAM IS RIVETED TO THE FUSELAGE IMMEDIATELY AFT OF THE RIGHT EMERGENCY EXIT OPENING. THE CRACK WAS LOCATED ON THE CROSSBEAM ADJACENT TO THE AFT, LOWER OF THE EMERGENCY EXIT OPENING.Aug 16, 2002 · N350KG · Beech B300 · Fuselage Main, StructureSDR JEM2002F00003Tie · crackedTHIS CROSS TIE IS RIVETED TO THE FUSELAGE IMMEDIATELY AFT OF THE LT EMERGENCY EXIT OPENING. THE CRACK WAS LOCATED ON THE CROSS TIE ADJACENT TO THE AFT, LOWER CORNER OF THE EMERGENCY EXIT OPENING.Aug 16, 2002 · N350KG · Beech B300 · Fuselage Main, StructureSDR CGH2002F00004Crossbeam · crackedTHIS CROSS TIE IS RIVETED TO THE FUSELAGE IMMEDIATELY AFT OF THE RIGHT EMERGENCY EXIT OPENING. THE CRACK WAS LOCATED ON THE CROSS TIE ADJACENT TO TE AFT, LOWER CORNER OF THE EMERGENCY EXIT OPENING.Aug 16, 2002 · N711VN · Beech B300 · Fuselage Miscellaneous StructureSDR CGH2002F00003Crossbeam · crackedTHIS CROSS TIE IS RIVETED TO THE FUSELAGE IMMEDIATELY AFT OF THE RIGHT EMERGENCY EXIT OPENING. THE CRACK WAS LOCATED ON THE CROSS TIE ADJACENT TO THE AFT, LOWER CORNER OF THE EMERGENCY EXIT OPENING.Aug 16, 2002 · N470MN · Beech B300 · Fuselage Miscellaneous StructureSDR CGH2002F00002Crossbeam · crackedTHIS CROSS TIE IS RIVETED TOT HE FUSELAGE IMMEDIATELY FORWARD OF THE RIGHT EMERGENCY EXIT OPENING. THE CRACK WAS LOCATED ON THE CROSS TIE ADJACENT TOT HE FORWARD, LOWER CORNER OF THE EMERGENCY EXIT OPENING.Aug 16, 2002 · N470MN · Beech B300 · Fuselage Miscellaneous StructureSDR CGH2002F00001Crossbeam · crackedTHIS CROSS TIE IS RIVETED TO THE FUSELAGE IMMEDIATELY AFT OF THE LEFT EMERGENCY EXIT OPENING. THE CRACK WAS LOCATED ON THE CROSS TIE ADJACENT TO THE AFT, LOWER CORNER OF THE EMERGENCY EXIT OPENING.Aug 16, 2002 · N470MN · Beech B300 · Fuselage Miscellaneous StructureSDR LX52002F00001Skin · crackedINNER DOOR SKIN CRACKS, FITTING SUPPORT CRACKS LOCATED AT DOOR LINK ATTACHMENT. LEFT NOSE LANDING DOOR. THIS IS THE THIRD AIRCRAFT WITH THIS SAME DAMAGE, SAME LOCATION. PROBABLE CAUSE IMPROPER RIGGING FROM MANUFACTURE.Aug 12, 2002 · N961LL · Beech B300 · Landing Gear DoorsSDR 2002FA0000616Rivet · looseUNDERSIDE OF WINGS AT WING STATION 209 HAVE LOOSENING RIVETS (CRACKED PAINT AND SMOKING). APPROXIMATELY HALF THE RIVETS SHOW SYMPTOMS.May 9, 2002 · N272SW · Beech B300 · FastenersSDR 2002FA0000615Rivet · looseUNDERSIDE OF WINGS AT WING STATION 209 HAVE LOOSENING RIVETS (CRACKED PAINT AND SMOKING), 45 OF 66 ON LEFT WING, 30 OF 66 ON RIGHT WING.May 9, 2002 · N160AR · Beech B300 · FastenersSDR 2002FA0000696Windshield · failedWAS AT FL 280 WHEN LOUD POP WAS HEARD AND SAW THE PILOT FRONT WINDSHIELD WAS SHATTERED. INITIATED AND EMERGENCY DESCENT AND LANDED AT AIRPORT FOR REPAIRS.Mar 22, 2002 · N350WH · Beech B300 · Flight Compartment WindowsSDR 2001FA0000323Piston · crackedRIGHT OUTBOARD FLAP ACTUATOR CRACKED AT BASE OF PISTON WHERE THE END PLUG IS ATTACHED. THE CRACK WAS 1.5 INCHES LONG AND RESULTED IN THE LOSS OF THE LUBRICATING OIL FROM OUT OF THE PISTON AND SCREW ASSEMBLY. THE LOSS OF OIL WAS THE FIRST INDICATION OF A PROBSep 18, 2001 · N988ME · Beech B300 · Trailing Edge Flap ActuatorSDR N988MEPiston · crackedRIGHT OUTBOARD FLAP ACTUATOR CRACKED AT BASE OF PISTON WHERE THE END PLUG IS ATTACHED. THE CRACK WAS 1.5 INCHES LONG AND RESULTED IN THE LOSS OF THE LUBRICATING OIL FROM OUT OF THE PISTON AND SCREW ASSEMBLY. THE LOSS OF OIL WAS THE FIRST INDICATION OF A PROBSep 18, 2001 · N988ME · Beech B300 · Trailing Edge Flap ActuatorSDR CA010627061Circuit Board · failed(CAN) ON APPROACH AIRCRAFT LOSS ALL GREEN ADVISORY LIGHTS AIRCRAFT MADE 3 FLY BY'S TO VERIFY GEAR DOWN & LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. THE LANDING GEAR LIGHTS ARE DIMMED THROUGH THE ABOVE P.C. BOARD.Jun 14, 2001 · Beech B300 · Landing Gear Position and WarningSDR 20010501CW015Switch · inoperativeLEFT BRAKE DEICE VALVE INDICATING LIGHT CIRCUIT OPEN IN VALVE.Apr 12, 2001 · N971LL · Beech B300 · Ice/Rain Protection SystemSDR CA010406011Starter Gen · failed(CAN) WHILE IN CRUISE FLIGHT THE RT GENERATOR FELL OFF LINE AND WOULD NOT RESET. AIRCRAFT CONTINUED TO FUEL STOP AIRPORT. MAINTENANCE DISCOVERED FAULTY STARTER/GENERATOR WITH OBVIOUS DAMAGE TO FORWARD (DRIVE SPLINE END) BEARING. GENERATOR SENT FOR OVERHAUL WITMar 16, 2001 · Beech B300 · Starter-GeneratorSDR CA010423007Windshield · broken(CAN) AIRCRAFT IN CRUISE FLIGHT 29,000 FEET ALTITUTE OAT 45 WEATHER CLEAR NO TURBULENCE. SIMULTANEOUS LOUD BANG AND LT (PILOTS) WINDSHIELD (INNER PANE)INSTANT SPIDER WEB CRACKS.Mar 15, 2001 · Beech B300 · Flight Compartment WindowsSDR 20010403CW010Tube · meltedPILOT REPORTED BLEED AIR WARNING INDICATION ON LEFT SIDE. TROUBLE SHOT AND FOUND EVA TUBING MELTED BELOW HEAT DUCT. DISCOVERED EARLIER REPAIR (WITHIN 1O HOURS) OF RIGHT SIDE TUBING 2 INCHES FROM LATEST FAILURE. TUBING IS COMING IN CONTACT WITH DUCT AND MELTMar 2, 2001 · N701FC · Beech B300 · Engine Bleed Air SystemSDR CA010314003Windshield · cracked(CAN) WHILE IN CRUISE FLIGHT AT FL310 AND OAT -50 DEGREES C, FLIGHT CREW OBSERVED RT WINDSHIELD OUTER PANE CRACK DEVELOP. CRACK WAS DIAGONAL IN LOWER INBOARD CORNER (APPROXIMATELY 6 INCHES). POH ABNORMAL CHECKLIST FOLLOWED AND FLIGHT RETURNED TO POINT OF DEPARFeb 26, 2001 · Beech B300 · Flight Compartment WindowsSDR ERYAFL288Motor · failedON APPROACH INTO HAYWARD, UNABLE TO EXTEND FLAPS. REPLACED FLAP MOTOR (P/N 100-384040), (S/N 3070) WITH (S/N 2536) NEW COMPONENT. PERFORMED RIGGING AND OPERATIONAL CHECKS. NO MALFUNCTIONS OR DEFECTS NOTED.Feb 22, 2001 · N168ET · Beech B300 · Trailing Edge Flap ActuatorSDR CA010308013Boot · detached(CAN) AIRCRAFT WAS IN CLIMBOUT FROM ST.JOHNS AIRPORT, AT 22,000 FEET, AIRSPEED 140 KNOTS, RATE OF CLIMB 1,800 F.P.M., PILOT EXPERIENCED SEVERE BUFFETING TO THE POINT THAT A/C WAS ABOUT TO STALL. STALL WARNING DID NOT ACTIVATE, A/C WAS PLACED IN LEVEL FLIGHT ANFeb 12, 2001 · Beech B300 · Horizontal Stabilizer StructureSDR CA010302014Windshield · cracked(CAN) WHILE IN CRUISE FLIGHT AT FL310 AND OAT -46 DEGREES C, A LOUD BANG WAS HEARD AND THE RT WINDSHIELD CRACKED. (WINDSHIELD HEAT HAD BEEN ON FOR THE ENTIRE FLIGHT (1 HOUR PLUS)). FLIGHT CREW REFERENCED ABNORMAL OCCURRENCE IN POH AND MADE AN UNSCHEDULED, UNEVFeb 9, 2001 · Beech B300 · Windshield/Door Rain/Ice RemovalSDR 20010222CW007Receptacle · damagedCABIN FLUORESCENT LIGHTS WOULD BLINK ON AND OFF IN FLIGHT. FOUND BAD SOCKET AND PINS AT K1 RELAY OF CABIN LIGHTING PANEL ASSEMBLY. SOCKET PINS OF RECEPTACLE WERE CRIMPED AND INSTALLED BACKWARDS.Jan 26, 2001 · N2SC · Beech B300 · Passenger Compartment LightingSDR 20010228CW006Windshield · crackedPILOT SIDE WINDSHIELD WAS INSTALLED . AC COMPLETED 1 FLIGHT APPROX 4.2 HRS WHEN OUTER PLY OF WINDSHIELD CRACKED. AC LANDED AT MAIN FACILITY FOR REPLACEMENT OF THE WINDSHIELD. PER PROCEDURES, INSTALLATION IS ACCOMPLISHED USING STRESS FREE KITS AND PROCEDURESJan 18, 2001 · N2298B · Beech B300 · Flight Compartment WindowsSDR 20010215CW001Valve · inoperativeLT BRAKE DE-ICE LIGHT NOT ILLUMINATING. LIGHT SYSTEM / SWITCH IS INOPERATIVE.Jan 11, 2001 · N991LL · Beech B300 · Ice/Rain Protection SystemSDR CA010206003Attach Fitting · worn(CAN) DURING ROUTINE MAINTENANCE TECHNICIAN NOTICED MOVEMENT IN RIGHT WING FRONT SPAR ATTACHMENT. FURTHER INVESTIGATION REVEALED THAT THE LOOSENNESS WAS CAUSED BY WORN BUSHINGS AND BOLT P/N 130909B175. BEECH CRAFT WAS NOTIFIED AND FIELD CREW ARE ON THEIR WAY TJan 8, 2001 · Beech B300 · Wing, Fuselage Attach FittingsSDR 20010124CW003Mount · crackedCOWL ATTACH LUGS CRACKED ON ENGINE MOUNT. ALSO, CORROSION FOUND AT MOUNT TO FUSELAGE ATTACH POINT BOLTS AND SPACING WASHERS.Jan 3, 2001 · N309M · Beech B300 · Engine Mount SectionSDR 20001102SH030Actuator · crackedNOTED DURING REMOVAL OF ACTUATOR FOR ROUTINE 1,200-HOUR LUBE THAT ACTUATOR PISTON WAS CRACKED FOR ENTIRE LENGTH IN AN APPROXIMATELY STRAIGHT LINE. A NEW P/N''D ACTUATOR AND ACTUATOR SHAFT WAS INCORPORATED ON AIRCRAFT, SN R-129, AND UP. REPLACED ACTUATOR WITNov 2, 2000 · Beech B300 · Trailing Edge Flap ActuatorSDR 20001113SH001Valve · stuckLEFT BRAKE DEICE VALVE STUCK IN ''ON'' POSITION. (X)Oct 26, 2000 · N961LL · Beech B300 · Landing Gear Brake SystemSDR 20001108SH025Terminal · looseRESET TRIPPED COFFEE BAR CIRCUIT BREAKER. DETECTED BURNING SMELL. FOUND WIRE TERMINALS LOOSE AND HEAT DAMAGED ON CIRCUIT BREAKER. REPLACED WIRE TERMINALS AND RE-INSTALLED ON CIRCUIT BREAKER. OPERATION CHECKED OK. (X)Oct 18, 2000 · N64GG · Beech B300 · AC Power Distribution SystemSDR 20001120SH064Light · inoperativeLEFT MAIN GEAR BRAKE DEICE LIGHT WOULD NOT COME ON WHEN ACTIVATED. (X)Oct 17, 2000 · N961LL · Beech B300 · Landing Gear Brake SystemSDR 20001103SH009Valve · failedBRAKE DE-ICE VALVE FAILED IN ''ON'' POSITION. (X)Oct 3, 2000 · N971LL · Beech B300 · Landing Gear Brake SystemSDR 20001013SH025Seat · misinstalledIMPROPERLY INSTALLED SEAT MOUNTING HARDWARE. DURING INSPECTION, SEATS WERE FOUND IMPROPERLY INSTALLED. TWO FWD FACING AND ONE AFT FACING SEAT WERE FOUND WITH NO LOCKING RETAINERS INSTALLED. THREE OTHER SEATS HAD LOCKING RETAINERS ON ALL FOUR LEGS OF THE SEASep 25, 2000 · N2SC · Beech B300 · Passenger Compartment EquipmentSDR 20001017SH047Valve · intermittentRIGHT BRAKE DEICE ANNUNCIATOR INTERMITTENT. (X)Sep 12, 2000 · N961LL · Beech B300 · Landing Gear Brake SystemSDR 20000925SH013Valve · failedWHEN BRAKE DE-ICE SYSTEM IS TURNED ON, THIS VALVE ASSY FAILS TO ILLUMINATE THE LEFT DE-ICE LIGHT. (X)Sep 5, 2000 · N971LL · Beech B300 · Landing Gear Brake SystemSDR 20000814SH013Shutoff Valve · stuckBRAKE DE-ICE VALVE ON INDICATION SWITCH STICKING AND WOULD NOT INDICATE ON. (X)Jul 28, 2000 · N971LL · Beech B300 · Ice/Rain Protection SystemSDR 20000517SH014Shutoff Valve · stuckVALVE STICKING PARTIALLY OPEN WHEN SELECTED OFF. (X)May 5, 2000 · N991LL · Beech B300 · Engine Bleed Air SystemSDR 20000613SH016Pressure Switch · inoperativePRESSURE SWITCH INOPERATIVE ON AIR CONDITIONING COMPRESSOR.Apr 17, 2000 · N991LL · Beech B300 · Cabin Compressor SystemSDR 20000619SH025Pressure Switch · stuckMOTIVE FLOW RESSURE SWITCH STUCK IN OPEN POSITION CAUSING NO TRANSFER LIGHT TO STAY ILLUMINATED. (X)Apr 10, 2000 · N961LL · Beech B300 · Fuel Pressure IndicatingSDR 20000613SH019Altimeter · stuckNEEDLE STICKS AT HIGHER ALTITUDE. (X)Apr 10, 2000 · N971LL · Beech B300 · Altimeter, Barometric/EncoderSDR 20000613SH018Display · intermittentDISPLAY INTERMITTENTLY GOES BLANK. (X)Apr 10, 2000 · N971LL · Beech B300 · Rate of Climb IndicatorSDR 20000613SH017Transducer · reads lowFUEL FLOW TRANSDUCER INDICATED LOW FUEL FLOW. (X)Apr 4, 2000 · N971LL · Beech B300 · Fuel Flow IndicatingSDR 20000504SH007Valve · inoperativeBRAKE DEICE VALVE INOPERABLE AFTER OVERHAUL. (X)Apr 4, 2000 · N961LL · Beech B300 · Ice/Rain Protection SystemSDR 20000504SH006Valve · inoperativeBRAKE DEICE VALVE INOPERABLE. (X)Apr 4, 2000 · N961LL · Beech B300 · Ice/Rain Protection SystemSDR 20000425SH017Master Cylinder · leakingCOPILOT''S LEFT BRAKE/RUDDER PEDAL MASTER CYLINDER LEAKS INTERNALLY. (X)Mar 27, 2000 · N961LL · Beech B300 · Landing Gear Brake SystemSDR 20000425SH016Master Cylinder · leakingCOPILOT''S RIGHT BRAKE/RUDDERPEDAL MASTER CYLINDER CLEAKS INTERNALLY. (X)Mar 27, 2000 · N961LL · Beech B300 · Landing Gear Brake SystemSDR 20000613SH020Master Cylinder · leakingPILOTS LEFT BRAKE BLEEDS DOWN WHEN STEADY PRESSURE IS PUT ON IT. RIGHT BRAKE, AS WELL AS THE COPILOTS, WORK FINE.Mar 10, 2000 · N981LL · Beech B300 · Master Cylinder/Brake ValveSDR 20000619SH024Relay · failedTHERE IS AN OPENING IN THE K-3 RELAY WHEN THE AUXILIARY AIR CONDITIONER SYSTEM IS BEING ACTIVATED WHICH DOES NOT ALLOW THE CONDENSER BLOWER MOTOR TO ACTIVATE, CAUSING A HIGH PRESSURE FAULT, SHUTTING DOWN THE AIRFRAME AIR CONDITIONING SYSTEM. (X)Mar 2, 2000 · N961LL · Beech B300 · Electrical Power SystemSDR MEA200302Windshield · failedA/C WAS ENROUTE TO TEB AT FL290, WINDSHIELD ANTI-ICE WAS SELECTED FOR 1HOUR WHEN A LOUD CRACK WAS HEARD AND THE PILOTS WINSHIELD SHATTERED THE INNER PANE INTO PEA SIZED PIECES. CREW FOLLOWED AIRCRAFT ABNORMAL PROCEDURES AND DESCENDED BELOW 25,000 FEET AND KEEPFeb 2, 2000 · N593MA · Beech B300 · Flight Compartment WindowsSDR 99ZZZX4174Switch · malfunctionedTHE RED LIGHT IN THE LANDING GEAR HANDLE, 'GEAR UNSAFE LIGHT', WOULD NOT EXTINGUISH WITH LANDING GEAR IN FULLY RETRACTED POSITION. JACKED AIRCRAFT, CHECKED ALL UP AND LOCK SWITCHES, AND ASSOCIATED WIRING. CYCLED LANDING GEAR THROUGH TEN COMPLETE EXTENSION/REOct 25, 1999 · N991LL · Beech B300 · Landing Gear Position and Warning
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