Beechcraft B300

Service difficulty reports · 598

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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 O2GA2014031784501Line · damagedDURING CRUISE FLIGHT, RT BLEED AIR FAIL ANNUNCIATOR ILLUMINATED. FOLLOWED AFM PROCEDURES & DIVERTED, LANDED UNEVENTFUL. TROUBLESHOT DISCREPANCY TO A FAULTY RT ETHYLENE VINYL ACETATE BLEED AIR WARNING LINE. BLEED AIR LINE WAS REPAIRED & A SUCCESSFUL LEAK CHMar 12, 2014 · N845KA · Beech B300 · Pneumatic Distribution SystemSDR CA140217006Shaft · failed(CAN) ACFT WAS PASSING 14,000 FT, WHEN THE LT ENGINE ACCELERATED UNCONTROLLABLY. ALL ENGINE INSTRUMENTS WENT BEYOND MAX LIMITS, THE CREW PULLED THE LT POWER LEVER BACK TO IDLE WITH NO ENGINE RESPONSE, THE LT ENGINE WAS THEN SHUTDOWN AND SECURED. DECLARED ANDFeb 14, 2014 · Beech B300 · Fuel Control/Turbine EnginesSDR CA140217025Intercostal · cracked(CAN) WHILE REPAIRING MAIN CABIN DOOR FOR ANOTHER DEFECT THE INTERCOSTAL WAS FOUND TO BE CRACKED. THIS IS A COMMON REPLACEMENT ITEM IN THIS FLEET DUE TO USAGE OF THE DOOR. WHILE PREPARING TO INSTALL THE REPLACEMENT PART, THE AME NOTICED THAT THE PART DID NOTFeb 13, 2014 · Beech B300 · Passenger/Crew DoorsSDR CA140507007Brake · frozen(CAN) ACFT DEPARTED, WEATHER IFR SNOW OVER THE PREVIOUS 8 HRS APPROXIMATELY 1-3 CMSIC TAKEOFF. ON THE TAKEOFF ROLL THE LT MAIN GEAR WENT THROUGH SNOW. DURING THE FLIGHT IT WAS DECIDED THAT THE PIC WOULD HAVE CONTROL FOR THE LANDING. ON LANDING RUNWAY BOTH Feb 13, 2014 · Beech B300 · Landing Gear Brake SystemSDR KX5R20140214002Floorbeam · damagedFLOORBEAM FS 158 WHERE ATTACHES TO FUSELAGE LT FRAME FS 158, BL 25 FOUND TO BE MISSING 4 RIVETS. PILOT HOLES WERE PRESENT IN FLOORBEAM BUT NOT DRILLED THROUGH FRAME. THIS ACFT WAS TRANSITIONING TO A DIFFERENT INSP PROGRAM PROVIDED BY THE MFG CALLED HUIP (HIGH Feb 7, 2014 · N385H · Beech B300 · Fuselage Main, Floor BeamSDR O2GA2014022680601Transponder · malfunctionedAIRCRAFT DEPARTED, CREW SWITCHED THE NR 1 TRANSPONDER FREQUENCY FROM TOWER TO DEPARTURE & WAS NOTIFIED THAT THEIR TRANSPONDER SIGNAL WAS INTERMITTENT. CREW SWITCHED OVER TO THE NR 2 TRANSPONDER & DEPARTURE NOTIFIED THEM THAT THE NR 2 TRANSPONDER SIGNAL WAS NOFeb 6, 2014 · N806UP · Beech B300 · ATC Transponder SystemSDR CIEA20131212005Tire · debondedVIBRATION FELT FROM NOSE AFTER LIFTOFF. JACKED ACFT NOSE, ROTATED NOSE WHEEL ASSEMBLY & HEARD LOOSE COUNTER WEIGHT INSIDE OF TIRE. CONFIRMED AFTER DISASSEMBLY OF NOSE WHEEL THAT THE RUBBER WEIGHT HAD DISBONDED FROM INNER PORTION OF NOSE TIRE.Dec 11, 2013 · N825TT · Beech B300 · TireSDR CA131022002Bearing · corroded(CAN) THE ACFT WAS ON A 3RD PHASE INSPECTION WHEN MAINTENANCE CREWS HEARD A CLICKING SOUND IN THE LOWER RUDDER AREA WHEN IT WAS MOVED FROM LT TO RT. THE TAIL CONE WAS REMOVED FOR AN INSPECTION OF THE RUDDER LOWER HORN ASSY PN 101-524059-1. THE LOWER BEARING WOct 18, 2013 · Beech B300 · Rudder Control SystemSDR CA131029005Skin · corroded(CAN) LOCATED DEEP CORROSION AT LT AND RT WING SKIN UPPER BONDED PANEL ASSY AT AUX TANK ACCESS PANEL FLANGE. HAD BEEN REPORTED BY A 3RD PARTY CRS ON OTHER COMPANY ACFT, FL-273, FL-125, EVALUATED AND RECEIVED FIELD REPAIR FROM MFG. LT WING WAS WORSE THAN RT WOct 16, 2013 · Beech B300 · Wing, Plate/SkinSDR CA130809004Bearing · failed(CAN) ACFT EXPERIENCED GENERATOR FAILURE ON NR 2 ENGINE IN FLIGHT AT 951.9 HRS TSO. AME REMOVED STARTER/GENERATOR AND BROUGHT IT TO AMO FOR INSPECTION. FOUND THE BEARING AT ADE END HAD FAILED. ALL 8 BALLS REMAINED IN THE BEARING, BUT THE SHIELDS AND CAGE WAug 8, 2013 · Beech B300 · Starter-GeneratorSDR CA130516001Stiffener · cracked(CAN) WHILE PERFORMING A SCHEDULED PHASE CHECK, MAINTENANCE DISCOVERED THE LT WING T/E STIFFENER, CRACKED IN 3 SEPARATE PLACES. THE CRACKS WERE LOCATED AT WING STA 147, 156 AND 167 JUST BEHIND THE REAR SPAR. THE WING SKIN AT BS 148 WAS ALSO CRACKED. THE RT May 13, 2013 · Beech B300 · Wing Miscellaneous StructureSDR CA130301003Latch · unsecure(CAN) AIRCRAFT WAS ON A ROUTINE MEDIVAC FLIGHT WHEN THE PILOTS NOTICED WHAT APPEARED TO BE THE RT UPPER NOSE COWLING LIFTING IN FLIGHT. THE ACFT DIVERTED TO THE CLOSEST ALTERNATE AIRPORT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE NOSE COWLING LATFeb 12, 2013 · Beech B300 · Fuselage Structure (General)SDR CA130225007Pump · leaking(CAN) CUSTOMER CALLED TO REPORT A STATIC FUEL LEAK FROM THE HIGH PRESSURE PUMP DRAIN. CUSTOMER IS LOOKING FOR TROUBLESHOOTING ASSISTANCE.Feb 11, 2013 · Beech B300 · Engine Fuel PumpSDR E07A201302070001Governor · overspeedWHILE TESTING AUTO FEATHER DURING RUN UP THE RH PROP WENT TO FEATHER AND WOULD NOT COME OUT OF FEATHER. DETERMINED CAUSE TO BE OVERSPEED GOVERNOR. INSTALLED OH GOVERNOR OPS CHECKED OK.Feb 5, 2013 · N299AS · Beech B300 · Propeller GovernorSDR 2013FA0000074Wire Harness · chafedRIGHT MLG UPLOCK SAFETY AND WARNING SWITCH WIRING HAD CHAFED AGAINST PIVOT IN DRAG BRACE AND CHAFED THROUGH THE PLASTIC CONDUIT SLEVE AND WIRING. THE WIRE HARNESS APPEARED TOO SHORT AND CAUSED THE CHAFE. THE LEFT SIDE WAS ALSO CHAFED, BUT NOT TO THE EXTENT OFFeb 4, 2013 · N7RC · Beech B300 · Landing Gear System WiringSDR CA121218004Connector · burned(CAN) OVERHEAD FLOURESCENT CABIN LIGHTING CAUSING ELECTRICAL SHOCKS IN AFT CABIN, WAS REPORTED BY MEDICAL FLIGHT TEAM. UPON INSPECTION BY MAINTENANCE DEPARTMENT THE WIRING HARNESS, PN 130-364-044-9 FOR THE COLD CATHODE LIGHTING SYS WAS FOUND TO HAVE A BURNED Dec 11, 2012 · Beech B300 · Light System WiringSDR CA121210001Windshield · failed(CAN) DURING FLIGHT, AT 27000 FEET WITH A OUTSIDE AIR TEMP. OF -33 DEGREES AND A AIRSPEED OF 198 THE PILOTS LT SIDE WINDSHIELD SHATTERED. THE ACFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED THE UNSERVICEABLE WINDSHIELD AND REPLACED WITH A SERVICEABLDec 5, 2012 · Beech B300 · Flight Compartment WindowsSDR PCPR20121212001Antenna · crackedDURING A POST FLIGHT INSPECTION CRACKS WERE DISCOVERED ON THE LT AND FRONT SIDE OF THE ELT 406 ROD ANTENNA APPROX 6" FROM THE BASE. ON THE LT SIDE IN THE CENTER OF THE CRACKS WAS A CIRCULAR SHAPED VOID IN THE MATERIAL APPROX .1250" IN DIAMETER AND .0625" DEEPNov 27, 2012 · N350K · Beech B300 · Emergency Locator BeaconSDR CA121102006Actuator · failed(CAN) PILOT REPORTED AFTER LOWERING GEAR HYDRAULIC FLUID LOW CAUTION LIGHT CAME ON..FOUND LEAKING FLUID AFTER LANDING. RIGHT MAINLANDING GEAR ACTUATOR FOUND CRACKED AT SHAFT END OF ACTUATOR.ACTUATOR WAS REPLACED.Oct 31, 2012 · Beech B300 · Landing Gear ActuatorSDR CA121004004Bolt · broken(CAN) ACFT WAS PARKED OUTSIDE SINCE SEPT 17-2012. THE FLIGHT CREW NOTICED STRONG WINDS AND KEPT MOVING THE AIRCRAFT SO IT WAS PARKED INTO THE WIND. CONFIRMED THE CONTROL LOCKS WERE IN PLACE ON THE 19TH OF SEPT. WHEN THEY DID THEIR WALKAROUND TO DEPART THE ASep 26, 2012 · Beech B300 · Rudder StructureSDR CA120921009Bearing · seized(CAN) ON THE GROUND, THE PROPELLER WAS FOUND SEIZED. THE PROPELLER WOULD NOT ROTATE ON START-UP AND COULD NOT BE MANUALLY ROTATED. VERY LITTLE METAL WAS FOUND IN THE OIL SYS, ALTHOUGH SOME TRACES OF METAL WERE OBSERVED ON THE MAIN OIL FILTER, THE CHIP DETECTSep 20, 2012 · Beech B300 · Turbine Engine Reduction GearSDR CA120831001Fitting · corroded(CAN) THE RT, CO-PILOTS, AIRSPEED INDICATOR WAS BEING REPLACED DUE TO A LIGHTING ISSUE. A NEW INDICATOR WAS INSTALLED AND PITOT/STATIC TEST PERFORMED. A MASSIVE LEAK WAS DETECTED AND AN INVESTIGATION WAS INITIATED. AN INSPECTION OF THE NR 2 PITOT/STATIC SYS Aug 30, 2012 · Beech B300 · Pitot/Static SystemSDR 2012F00162Uplock Switch · shortedON LOWERING LANDING GEAR. CIRCUIT BREAKER TRIPPED. LANDING GEAR HAD TO BE MANUALLY LOWERED FOR LANDING. ACFT LANDED WITHOUT INCIDENT. FOUND SAFETY WIRE PIGTAIL, WHICH SAFETIED THE LT UP-LATCH SWITCH, HAD CHAFED INTO AN ADJACENT WIRE BUNDLE, SHORTING OUT THEAug 10, 2012 · N450CR · Beech B300 · Landing Gear Position and WarningSDR CA120802010Engine · unknown(CAN) NR 2 ENGINE TORQUE STARTED TO DECREASE FOLLOWING THE FUEL FLOW, WF, DECREASE PASSING BY 3000 FT SHORTLY AFTER TAKEOFF. THE POWER PLANT WENT TO AUTOFEATHER AND ENGINE WAS STABILIZED. NO DETAIL OF PARAMETER WERE GIVEN. THE PILOT TRIED TO RESTART THE ENJul 26, 2012 · Beech B300 · Engine (Turbine/Turboprop)SDR CA120711001Relay · failed(CAN) DURING A ROUTINE TAKE OFF THE AIRCRAFT EXPERIENCED A R/H GENERATOR FAILURE AND R/H AC BUS FAILURE. THE AIRCRAFT RETURNED TO THE RUNWAY AND LANDED WITHOUT INCIDENT. DURING THE INVESTIGATION BY MAINTENANCE THE 250AMP REVERSE CURRENT LIMITER WAS BLOWN AND TJul 1, 2012 · Beech B300 · Engine Starting System WiringSDR CA120627002Cross Tie · broken(CAN) DURING INSPECTION FOUND CROSS TIE AFT OF EMERGENCY EXIT HAD BEEN BROKEN AND 3 EA RIVETS WERE SHEARED. THE MFG WAS CONTACTED FOR A POSSIBLE REPAIR AS NONE WAS DICTATED IN THE SRM. OUR ENGINEER WAS ADVISED TO REPLACE THE ENTIRE CROSS TIE. MFG ACKNOWLEDGEJun 25, 2012 · Beech B300 · Emergency ExitsSDR CIEA201206180003Tire · debondedSTRONG SHIMMY FELT FROM NOSE AFTER LIFTOFF AND ON LANDING ROLL. RETURNED TO DEPARTURE. DISASSEMBLED NOSE WHEEL PN 101-8026-5, SN 5951. FOUND THE RUBBER PATCH INSIDE THE TIRE HAD DISBONDED. A NEW TIRE PN 265F86-8, SN 10822332 WAS INSTALLED, BALANCED AND MOUJun 17, 2012 · N825TT · Beech B300 · Wheel/Ski/FloatSDR 2012FA0000238Smoke Goggles · failedWHILE VISUALLY INSPECTING PILOT’S AND CO-PILOT’S SMOKE GOGGLES, BOTH RT AND LT RIVETS THAT ATTACH THE STRAPS TO THE GOGGLES LENSES FAILED, CAUSING THE STRAPS TO FALL OFF ALONG WITH THE GOGGLE LENSES. THIS WAS THE CASE WITH BOTH THE PILOT AND CO-PILOTS SIDES.Apr 26, 2012 · N291B · Beech B300 · Emergency EquipmentSDR CA120419002Boot · burned(CAN) DISCOVERED DURING NIGHTLY INSPECTION, DEICER WAS BURNED AT ROOT END NEAR WIRE ATTACH POINTS. PART IS AN OEM SUPPLIED UNIT ON A NEWLY O/H PROPELLER. FIRST DEFECT OF THIS KIND NOTED BY THIS OPERATOR. PART IS BEING RETURNED TO PROPELLER AMO FOR CONSULTATApr 18, 2012 · Beech B300 · Propeller/Rotor Anti-Ice/De-Ice SystemSDR CA120402004Fuel Control · malfunctioned(CAN) ACFT ABORTED TAKEOFF BECAUSE ENGINE POWER WAS UNMATCHED. CONDUCTED RUN-UP AND FOUND NO PROBLEMS, STATIC RUN ON GROUND ABLE TO ACHIEVE 95 PERCENT TORQUE AS WELL. STATIC POWER CHECK CONDUCTED AGAIN JUST BEFORE TAKEOFF WITH NO PROBLEMS. AT 2000 FT AGL THEMar 31, 2012 · Beech B300 · Fuel Control/Turbine EnginesSDR CIEA201203210001Truss · chafedTHE LOWER AFT COWLING HARDWARE AND CHANNEL FOR AFT ICE VANE DOOR HINGE HAS WORN INTO THE LOWER ENGINE MOUNT TRUSS ON BOTH LT AND RT ENGINE TRUSSES.Mar 21, 2012 · N350PJ · Beech B300 · Engine Mount SectionSDR LX5R2012021400001Lockwasher · brokenON CLIMBOUT, TOWER REPORTED THAT THE LT MAIN GEAR WAS STILL EXTENDED. CREW NOTED THAT THEY STILL HAD THE "DOWN AND LOCKED" GREEN LIGHT FOR THE LT GEAR. PROCEEDED TO EXTEND THE GEAR AND TRYED TO RETRACT AGAIN WITH THE SAME RESULTS. THE RT & NOSE GEAR RETRACTFeb 10, 2012 · N971LL · Beech B300 · Main Landing GearSDR CA120206003Governor · malfunctioned(CAN) ON TAKEOFF, THE LT ENGINE WOULD NOT PRODUCE T/O POWER, ONLY GOT 40 PERCENT. MAINTENANCE INSPECTED RESET LINKAGE FOR BINDING NONE FOUND. RESET LINKAGE GAP FOUND TO BE SLIGHTLY UNDER MM SPECIFICATION AND RESET TO 0.10". LINKAGE LUBRICATED IAW MM. PROP GFeb 2, 2012 · Beech B300 · Propeller GovernorSDR CA120206002Switch · malfunctioned(CAN) SELECTING FLAPS APPROACH AND DOWN DID NOT ACTUATE FLAPS IN FLIGHT. MAINTENANCE FOUND LT ASSYMETRIC SWITCH, FLAP SAFETY SWITCH, WIRE TERMINALS TO BE IN POOR CONDITION, TERMINALS REPLACED AND WIRES SECURED FLAPS FUNCTION CHECKED NUMEROUS TIMES WITH NO FURTJan 31, 2012 · Beech B300 · Trailing Edge Flap Control SystemSDR CA120119004Spar Cap · damaged(CAN) EDDY CURRENT INSPECTION WAS CARRIED OUT ON THE REMAINING REAR HORIZONTAL STABILIZER SPAR CAPS AND AS A RESULT OF THE NDI INSPECTION THE LEFT UPPER SPAR CAP WILL ALSO BE REPLACED. RESULT SHOWED 0.008 TO 0.020 DEPTH INTERGRANULAR CORROSION THROUGH THE LENJan 18, 2012 · Beech B300 · Horizontal Stabilizer, Spar/RibSDR CA111228006Indicator · malfunctioned(CAN) ACFT WAS ENROUTE, APPROXIMATELY 1 HR INTO THE FLIGHT THE LOW FUEL QTY LIGHT ILLUMINATED ON THE RT ENGINE IAW CHECKLIST THE AUXILIARY TRANSFER CIRCUIT BREAKER WAS PULLED. NO CHANGE TO THE LOW FUEL LEVEL LIGHT. APPROXIMATELY 25 MIN LATER THE CREW NOTED FDec 28, 2011 · Beech B300 · Fuel Indicating SystemSDR CA111114013Bracket · broken(CAN) DURING PHASE 2 INSPECTION, FOUND THE FLOW CONTROL UNIT UNSERVICEABLE. BLEED AIR FIREWALL SHUTOFF VALVE ACTUATOR BRACKET BROKEN. THE METAL BRACKET CRACKED AND BROKEN OFF SEEMS VERY POROUS IN NATURE.Nov 13, 2011 · Beech B300 · Compressor Bleed ValveSDR CA110930009Line · leaking(CAN) PILOTS REPORTED RT BLEED AIR WARNING LIGHT CAME ON IN FLIGHT AND COULD NOT EXTINGUISH THE LIGHT. TROUBLESHOOTING OF THE RT BLEED AIR WARNING SYS WAS CONDUCTED AND A HOLE IN THE WARNING LINE WAS FOUND AT THE WARNING TUBE CONNECTION ON THE BLEED AIR MANIFSep 27, 2011 · Beech B300 · Engine Bleed Air SystemSDR CA110923004Solenoid · failed(CAN) DURING THE GROUND RUN, PRE-DEPARTURE CHECKS, THE TEST SOLENOID FAILED ON THE LT OVERSPEED GOVERNOR (OSG). SUBSEQUENT TESTS WOULD NOT WORK AT ALL. SECOND FAILURE OF THIS TYPE ON THIS PARTICULAR OSG. NO EFFECT IN FLIGHT AT ALL, BUT YOU CANNOT TEST THE Sep 22, 2011 · Beech B300 · Propeller GovernorSDR CA111003014Armature · shorted(CAN) GENERATOR WAS TRIPPING OFF LINE, AND FAILED IN FLIGHT. ACFT RETURNED TO AIRPORT. STARTER-GENERATOR WAS REMOVED. INITIAL INSPECTION FOUND BRUSHES VERY WORN AND ARMATURE WORN WITH HEAT DAMAGE. THERE WAS CONSIDERABLE BRUSH DUST RESIDUE BLOWN OUT FROM ARSep 7, 2011 · Beech B300 · Starter-GeneratorSDR ZLWA20110421001Skin · chafedRT FLAP TOP SKIN CHAFED BY INBD EDGE OF WING LOCKER. INSUFFICIENT CLEARANCE ALLOWED FOR CONTACT BETWEEN THE INBD BOTTOM EDGE OF THE WING LOCKER AND THE UPPER SKIN OF THE FLAP RESULTING IN 80 PERCENT LOSS OF THE MATERIAL ON THE TOP OF THE FLAP. THE CHAFING WASApr 18, 2011 · N214ML · Beech B300 · Trailing Edge FlapsSDR 2011FA0000249Cross Tie · damagedFOUND 2 SHEARED RIVETS IN GUSSET ON FRAME AT FS 201.775 AND STRINGER/CROSS TIE 7R. DISCREPANCY FOUND DURING SCHEDULED INSP, THIS AREA WAS RECENTLY INCLUDED IN THE INSPECTION GUIDE. THE SIDEWALLS MUST BE REMOVED TO INSPECT CROSS TIES. THE LT SIDE HAD PREVIOUSLApr 15, 2011 · N37TD · Beech B300 · Fuselage Main, StructureSDR 2011FA0000212Dipstick · brokenOIL DIPSTICK SEPARATED AT OIL CAP, STEM AND FELL INTO OIL TANK. THE STICK AND STEM WERE NOT ASSEMBLED CORRECTLY. THE STICK WAS NOT PUSHED FAR ENOUGH IN THE STEM SO THE RETENTION PIN DID NOT ENGAGE.Mar 30, 2011 · N980BC · Beech B300 · Turbine Engine Oil SystemSDR 2011F00057Display · failedTHE COPILOTS EHSI WOULD NOT POWER UP, SCREEN REMAINED BLANK.Mar 3, 2011 · N17WC · Beech B300 · Central DisplaySDR CA100916004Bolt · shearedON APPROACH TO AIRFIELD, THE LANDING GEAR DEPLOYED WITHOUT INPUT FROM THE PILOTS. SHORTLY AFTER, THE PUMP RELAY CIRCUIT BREAKER POPPED. PILOTS USED MANUAL PUMP TO EXTEND THE GEAR TO A LOCKED POSITION AND LANDED. FURTHER INVESTIGATION REVEALED THAT THE "MANISep 15, 2010 · Beech B300 · Hydraulic Pump (Electric/Engine), MainSDR CA100902001Bypass Valve · bindingACFT WAS ON A ROUTINE FLIGHT AND DURING DESCENT THE FLIGHT CREW SELECTED A COOLER TEMP FOR THE CABIN. UPON THAT SELECTION CABIN TEMP ROSE AND THE CREW DECIDED TO INVESTIGATE. THEY DISCOVERED THAT THE ENVIRONMENTAL CIRCUIT BREAKER HAD POPPED WHICH ACCOUNTED FAug 22, 2010 · Beech B300 · Cabin Temperature Control SystemSDR GSPA NRS103265Compressor · seizedPILOT REPORTED AIR CONDITIONER SYS WAS NOT PUTTING OUT COLD AIR. UPON INVESTINGATING THE PROBLEM IT WAS DISCOVERED THAT THE AIR COMPRESSOR WAS SEIZED AND THE DRIVE BELT BURNED THOUGH. 2 NEW FREOM COMPRESSORS WERE INSTALLED AND BOTH SEIZED CASUING THE BELT TO BAug 20, 2010 · N89WC · Beech B300 · Cabin Compressor SystemSDR CA100823005Switch · stickingIN PREPARATION FOR TOUCHDOWN THE FLIGHT CREW MOVED THE ENGINE POWER LEVERS AFT TO THE FLIGHT IDLE GATE, RESULTING IN THE PROPELLER GROUND LOW PITCH SOLENOIDS CHANGING THE PROPR BLADE ANGLES TO A FINER PITCH WHILE THE ACFT WAS STILL AIRBORNE. RESULTING IN A SAug 11, 2010 · Beech B300 · Propeller Controlling SystemSDR CA100806005De-Ice Valve · malfunctionedBRAKE DEICE VALVE OPENED SUPPLYING BLEED AIR TO BRAKE DEICE SYS WITHOUT BEING ELECTRICALLY ACTUATED VIA THE BRAKE DEICE SWITCH. (BRAKE DEICE INDICATION AND RT ENGINE TORQUE INDICATION CONFIRMED VALVE WAS OPENED.) ON CLIMB OUT, THE RT BRAKE DEICE ANNUCIATOR ILJul 1, 2010 · Beech B300 · Ice/Rain Protection SystemSDR 2010FA0000601Relay · intermittentOWNER REPORTED THE FLAP SYS TO BE INTERMITTENT WHEN THE FLAPS SELECTED TO DOWN POSITION. OPERATED THE FLAP SYS IN THE HANGER AND VERIFIED THE INTERMITTENT FLAPS. FOUND THE FLAP MOTOR CONTROL RELAY TO BE CAUSING THE INTERMITTENT PROBLEM. AFTER REMOVAL OF THE FLJun 16, 2010 · N374BH · Beech B300 · Trailing Edge Flap Control System
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