Beech B300

Service difficulty reports · 598

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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 O2GA2017071986301Starter Gen · intermittentLEFT ENGINE N1 SLOW TO ACCELERATE AND ITT RAPID RISE WITH NO EXCEEDANCE. MAINTENANCE REPLACED THE LEFT ENGINE STARTER GENERATOR. OPS OK NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE.Jul 14, 2017 · N863UP · Beech B300 · Starter-GeneratorSDR O2GA2016062180101Fcu · defectiveAT CRUISE ALTITUDE RIGHT ENGINE ROLLED BACK FOLLOWED BY ENGINE VIBRATION AND ENGINE GENERATOR OFF LINE. DECLARED AN EMERGENCY AND DIVERTED TO KDOV. LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED THE RIGHT ENGINE STARTER GENERATOR AND FUEL CONTROL UNIT. A SUCCESSJun 17, 2017 · N801UP · Beech B300 · Fuel Control/Turbine EnginesSDR 2017FA0000322Filter · leakingDURING THE ENGINE PERIODIC INSPECTION THE FUEL FILTER PN 3033355 WAS INSPECTED AND REINSTALLED USING A NEW O-RING PN M25988/1-928 IAW MAINTENANCE MANUAL 731002, -TECH PUMP WHICH STATES TORQUE TO BE 30 TO 50 INCH POUNDS TORQUE TO THE FILTER BOWL. THE LEAK CHECJun 7, 2017 · N846DJ · Beech B300 · Aircraft Fuel SystemSDR O2GA2017060782201Brake · wornDURING CREW RUN UP CHECKS PARKING BRAKES AND TOE BRAKES WILL NOT EFFECTIVELY HOLD AIRCRAFT. MAINTENANCE TROUBLESHOT THE DISCREPANCY TO LEFT AND RIGHT OUTBOARD MAIN BRAKES APPROACHING THE MAXIMUM WEAR LIMITS. BRAKES WERE REPLACED. OPERATIONAL AND LEAK CHECKS COJun 2, 2017 · N822UP · Beech B300 · BrakeSDR O2GA2017060686401Flight Dir · defectiveAFTER PRESSING A KEY ON MKP THE SVS WAS LOST. MFD WENT BLACK, FMS ILLUMINATED ON PFD1 IN RED, A/P REVERTED TO ROLL AND PITCH MODES. THE MFD SLOWLY CAME BACK ONLINE OVER THE COURSE OF APPROXIMATELY 60 SECONDS. DURING SUCH TIME, TOPO FAIL, PFD COMPARE FAIL, PFD May 30, 2017 · N864UP · Beech B300 · Flight Management Computing Hardware SystemSDR O2GA2017052687101Trim System · frozenWHILE IN CRUISE FLIGHT AT FL260, AUTOPILOT HOLDING ND MISTRIM ANNUNCIATOR ILLUMINATED. ELEVATOR TRIM WAS FROZEN. TRIM OPERATED NORMAL AT DURING DESCENT TO LOWER ALTITUDES 13,000FT. FLIGHT DIVERTED. MAINTENANCE PERFORMED THE REQUIREMENTS OF PITCH TRIM NTO LETTEMay 26, 2017 · N871UP · Beech B300 · Elevator Tab Control SystemSDR O2GA2017052685901Trim System · frozenRUDDER AND AILERON TRIM FROZE IN FLIGHT AT FL310, TEMP -32*C. TRIM WORKED NORMAL DURING DESCENT TO LOWER ALTITUDE FL250, TEMP -12*C. MAINTENANCE PERFORMED THE REQUIREMENTS FOR THE RUDDER AND AILERON LUBE. A SUCCESSFUL OPERATIONAL CHECK FLIGHT WAS PERFORMED. May 25, 2017 · N859UP · Beech B300 · Rudder Tab Control SystemSDR O2GA2017052686301Trim System · frozenRUDDER TRIM FROZE IN FLIGHT. HEAVY RAIN BEFORE TAKE-OFF. TRIM WORKED NORMAL DURING DESCENT TO LOWER ALTITUDES.May 24, 2017 · N863UP · Beech B300 · Rudder Tab Control SystemSDR O2GA2017052680701Engine · oil consumptionAT CRUISE ALTITUDE, FL310 RIGHT ENGINE OIL PRESSURE DROPPED TO 111 PSI. ENGINE OIL PRESSURE RETURNED TO NORMAL DURING DESCENT WENT TO 123 PSI. ENGINE OIL LEVEL CHECKED ONCE AIRCRAFT WAS ON THE GROUND AND FOUND ENGINE TO BE CONSUMING OIL. ENGINE CHANGED.May 23, 2017 · N807UP · Beech B300 · Engine (Turbine/Turboprop)SDR O2GA2017053180601Switch · defectiveNOSE GEAR GREEN DOWN LIGHT FAILED TO ILLUMINATE DURING GEAR EXTENSION. PERFORMED EMERGENCY GEAR EXTENSION AND GO AROUND FOR TOWER CONFIRMATION OF GEAR EXTENSION. LANDING WAS UNEVENTFUL. AIRCRAFT WAS FERRIED FROM THE BAHAMAS TO TAMPA FLORIDA FOR MAINTENANCE. MMay 15, 2017 · N806UP · Beech B300 · Landing Gear Position and WarningSDR O2GA2017050285701Trim System · frozenRUDDER TRIM FROZE DURING INITIAL CLIMB OUT. AT LOWER ALTITUDES RUDDER TRIM FUNCTIONED NORMAL. MAINTENANCE PERFORMED THE REQUIREMENTS OF NTO 940-2017-00253 & 940-2017-00250. A SUCCESSFUL OPERATIONAL CHECK FLIGHT WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.May 2, 2017 · N857UP · Beech B300 · Rudder Control SystemSDR O2GA2017050286901Rudder · frozenRUDDER TRIM FROZE IN FLIGHT AND FREED UP ON DESCENT TO WARMER AIR. MAINTENANCE PERFORMED THE REQUIREMENTS OF NTO LETTER FOR RUDDER AND PITCH TRIM ACTUATORS. A SUCCESSFUL OPERATIONAL CHECK FLIGHT WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.Apr 27, 2017 · N869UP · Beech B300 · Rudder Control SystemSDR O2GA2017042586301Trim System · frozenPITCH TRIM FROZE IN FLIGHT FL260. CAS MESSAGE 'AP HOLDING ND". ON DESCENT TO WARMER AIR AT 16,00 FT TRIM WORKED FINE. AIRCRAFT FERRY FLIGHT TO TPA ACCOMPLISHED FOR MAINTENANCE. SDR SUPPLEMENT TO FOLLOW.Apr 21, 2017 · N863UP · Beech B300 · Stabilizer Control SystemSDR O2GA2017041783902Module · intermittentON APPROACH, AFTER LOWERING LANDING GEAR THE RED GEAR INDICATION REMAINED ILLUMINATED WITH NO GREEN INDICATIONS. FOLLOWED CHECKLIST AND MANUALLY LOWERED LANDING GEAR. LOW APPROACH FOR TOWER CONFIRMATION COMPLIED WITH. LANDING WAS UNEVENTFUL. MAINTENANCE REPLAApr 14, 2017 · N839UP · Beech B300 · Landing Gear Retraction/Extension SystemSDR O2GA2017041283901Pressure Switch · failedLANDING GEAR WOULD NOT EXTEND ON APPROACH (NO GREEN INDICATION. FOLLOWED CHECKLIST. EMERGENCY DECLARED. MANUAL GEAR EXTENSION COMPLIED WITH AND TOWER CONFIRMED. LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED A FAILED GEAR UP PRESSURE SWITCH. GEAR SWINGS PERFORMEApr 6, 2017 · N839UP · Beech B300 · Landing Gear Position and WarningSDR 2017FA0000154Connector · damagedWHEN BATTERY CONNECTOR WAS DISCONNECTED DURING MAINTENANCE EVENT, DISCOVERED THAT ONE OF THE BATTERY PINS HAD OVERHEATED AND WELDED ITSELF TO THE QUICK DISCCONNECT CONNECTOR. WHEN THE QUICK DISCCONNECT WAS DISCONNECTED, THE PIN FROM THE BATTERY TORE LOOSE FROApr 5, 2017 · N350W · Beech B300 · Electrical Power System WiringSDR O2GA2017032983301Bulb · inoperativeON FINAL, CREW SELECTED NOSE GEAR HANDLE TO DOWN POSITION AND NOSE GEAR INDICATION LIGHT DID NOT ILLUMINATED. CREW PERFORMED A GO AROUND AND COMPLIED THE ABNORMAL PROCEDURES CHECKLIST. LANDING WAS UNEVENTFUL. MAINTENANCE TROUBLESHOOT THE DISCREPANCY TO A FAULTMar 27, 2017 · N833UP · Beech B300 · Landing Gear Position and WarningSDR O2GA2017033186201Trim System · frozenRUDDER TRIM FROZE IN FLIGHT "0" POSITION. UNABLE TO USE RUDDER TRIM. ONCE DESCENDED TO LOWER ALTITUDE THE RUDDER TRIM WORKED FINE. AIRCRAFT IS CURRENTLY STILL IN SCHEDULED MAINTENANCE AT THE SERVICE CENTER. SDR SUPPLEMENT TO FOLLOW.Mar 26, 2017 · N862UP · Beech B300 · Rudder Control SystemSDR O2GA2017032985601Unknown · smokeAFTER SHUTDOWN, SMOKE WAS NOTICED COMING FROM BOTH ENGINE EXHAUST STACKS ON THE RIGHT ENGINE. MAINTENANCE INSPECTED THE RIGHT ENGINE WITH NO DEFECTS NOTED. ENGINE OIL WAS SERVICED. PERFORMED ENGINE RUNS AT DIFFERENT POWER SETTINGS WITH NO DEFECTS NOTED. AIRCRAMar 24, 2017 · N856UP · Beech B300 · Engine (Turbine/Turboprop)SDR O2GA2017032785801Trim System · frozenPITCH, AILERON, AND RUDDER TRIM FROZEN IN FLIGHT. DESCENDING THROUGH 15,000 FT TEMPERATURE OF +3 DEGREES C, TRIM WORKED FINE. AUTO PILOT RE-ENGAGED AND FLIGHT WAS CONTINUED. MAINTENANCE INSPECTED TRIM SYSTEM NO DEFECTS NOTED. PERFORMED THE REQUIREMENTS OF NTMar 20, 2017 · N858UP · Beech B300 · Flight Control SystemSDR O2GA2017031387101Trim System · frozenRUDDER TRIM FROZE IN FLIGHT AT FL310, -38*C. UNFROZE DURING DESCENT THROUGH 15,000 FEET, -8*C. MAINTENANCE COMPLIED WITH RUDDER TRIM NTO 940-2016-01658. SUCCESSFUL OPERATIONAL CHECK FLIGHT PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.Mar 13, 2017 · N871UP · Beech B300 · Rudder Tab Control SystemSDR O2GA2017032486501Rudder · bindingON REACHING CRUISING ALTITUDE OF 18,000 FT. ATTEMPTED TO ADJUST THE RUDDER TRIM AND NOTICED IT WAS STIFF BUT OPERATIONAL. ON THE GROUND TRIM OPERATED NORMAL. MAINTENANCE COMPLIED WITH RUDDER TRIM NTO 940-2016-01658. NO DEFECTS NOTED. OPERATIONAL CHECK FLIGHT PMar 12, 2017 · N865UP · Beech B300 · Rudder Control SystemSDR O2GA2017031683101Circuit Card · intermittentUPON SELECTING LANDING GEAR HANDLE TO THE DOWN POSITION, GEAR HANDLE ANNUNCIATOR REMAINED RED WITH NO GREEN LIGHT INDICATIONS. MANUAL LANDING GEAR EXTENSION WAS PERFORMED. LANDING WAS UNEVENTFUL. MAINTENANCE TROUBLESHOT THE DISCREPANCY TO A RELAY CARD THAT WAMar 12, 2017 · N831UP · Beech B300 · Landing Gear System WiringSDR O2GA2017031682401Switch · unsecureDURING POST FLIGHT INSPECTION, 4 MINUTES AFTER POWERING THE EMERGENCY INSTRUMENT LIGHTS, THE PILOT SAW SMOKE ASSOCIATED WITH A BURNING ODOR COMING FROM THE LEFT MASTER WARNING LIGHT SWITCH. SYSTEM WAS POWERED DOWN. MAINTENANCE INSPECTED THE SWITCH AND WIRE BUMar 10, 2017 · N824UP · Beech B300 · Instrument System WiringSDR O2GA2017021384801Switch · defectiveON APPROACH, THE NOSE LANDING GEAR DOWN AND LOCKED ANNUNCIATOR FAILED TO ILLUMINATE. GEAR ANNUNCIATOR TEST WAS GOOD. FOLLOWED CHECKLIST. TOWER CONFIRMED GEAR DOWN. LANDING WAS UNEVENTFUL. TROUBLESHOT AND FOUND A FAULTY NOSE GEAR DOWN AND LOCKED SWITCH. THE Feb 9, 2017 · N848UP · Beech B300 · Landing Gear Position and WarningSDR O2GA2017013187501Actuator · defectiveDURING CRUISE FLIGHT 'AP TRIM NOSE DOWN' CAS MESSAGE ILLUMINATED, AUTOPILOT WAS DISCONNECTED. MANUAL AND ELECTRIC TRIM WAS FROZEN AND INOPERATIVE. DESCENDING TO A LOWER ALTITUDE RESOLVED THE FROZEN TRIM ISSUE. AIRCRAFT CONTINUED TO DESTINATION. LANDING WAS UNEJan 26, 2017 · N875UP · Beech B300 · Elevator Tab Control SystemSDR O2GA2017013086101Servo · intermittentELEVATOR TRIM ANNUNCIATION TOOK A LONG TIME TO EXTINGUISH AFTER ENGINE START. ELEVATOR TRIM IN CRUISE FLIGHT WAS BINDING. UNABLE TO MOVE WITH AUTO-PILOT ON. SUDDEN NOSE DOWN PITCH. TRIM STABILIZED FEW SECONDS AFTER. NO LOSS IN ALTITUDE EXPERIENCED. LANDING WASJan 24, 2017 · N861UP · Beech B300 · Stabilizer Control SystemSDR O2GA2017012785501Actuator · malfunctionedAUTOPILOT MISTRIM (E) ILLUMINATED AT FL310 AFTER START OF DESCENT. MANUAL PITCH TRIM WAS FROZEN. BEGAN WORKING AFTER DESCENDING INTO WARMER ALTITUDE FL120. MAINTENANCE REPLACED THE LEFT AND RIGHT PITCH TRIM ACTUATORS. REMOVED ACTUATORS SENT FOR EVALUATION. AJan 22, 2017 · N855UP · Beech B300 · Autopilot SystemSDR O2GA2017012580101Blower Motor · overheatedCREW REQUESTED DESCENT TO FL230 DUE TO LIGHT CHOP IN CABIN AND SMELL OF SMOKE. DURING DESCENT COCKPIT AND CABIN BEGAN TO FILL WITH SMOKE. RAN CHECKLIST, COCKPIT AND CABIN MASKED DEPLOYED AND DIVERTED TO KTUL. LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED THE AFJan 21, 2017 · N801UP · Beech B300 · Air Distribution SystemSDR O2GA2017011082101Switch · intermittentDURING CRUISE FLIGHT, THE RUDDER BOOST ANNUNCIATOR INTERMITTENTLY CAME ON SEVERAL TIMES DURING FLIGHT. FOLLOWED ABNORMAL PROCEDURES, DIVERTED AND LANDED UNEVENTFULLY. MAINTENANCE TROUBLESHOT AND REPLACED THE AUTOPILOT TRIM SWITCH. SYSTEM OPS CHECKED WERE GOODJan 5, 2017 · N821UP · Beech B300 · Auto Flight SystemSDR O2GA2016122200001Squat Switch · intermittentLOSS OF CABIN PRESSURIZATION AT FL270. EMERGENCY DESCENT WAS INITIATED AND AIRCRAFT DIVERTED. DONNED OXYGEN MASKS AND CABIN OXYGEN MASKS WERE DEPLOYED. LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR SQUAT SWITCH. A SUCCESSFUL OPERADec 18, 2016 · N839UP · Beech B300 · Landing Gear Position and WarningSDR O2GA2016121985601Bulb · failedWHILE PICKING UP CLEARANCE AT NIGHT WITH INSTRUMENT EMERGENCY LIGHTS IN THE ON POSITION. CREW NOTICED SMOKE FROM THE COPILOTS SIDE EMERGENCY INSTRUMENT LIGHT BULBS. LIGHTS WENT OUT AND BATTERY MASTER SWITCH WAS TURNED OFF. MAINTENANCE NOTICED A BURNT INOPERATIDec 15, 2016 · N856UP · Beech B300 · Emergency LightingSDR O2GA2016120687001Actuator · frozenDESCENDING OUT OF CRUISE FROM FL310 TO FL300, TEMP -33*C "AP MISTRIM ND" ANNUNCIATOR ILLUMINATED. ELECTRIC PITCH TRIM WAS FROZEN. AT APPROXIMATELY 12,000 FT., TEMP +1*C ELECTRIC PITCH TRIM FREED UP, A/P ENGAGED, AND CONTROL OF THE AIRCRAFT WAS NORMAL. LANDING Dec 3, 2016 · N870UP · Beech B300 · Stabilizer ActuatorSDR O2GA2016120682701Windshield · crackedCLIMBING OUT FROM KCAK THE LEFT WINDSHIELD CRACKED. DIVERTED BACK TO KCAK. LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED THE LEFT WINDSHIELD. AIRCRAFT WAS RETURNED TO SERVICE.Dec 1, 2016 · N827UP · Beech B300 · Flight Compartment WindowsSDR O2GA2016110786901Elevator System · malfunctionedDURING CRUISE AT FL260, THE MASTER CAUTION LIGHT ILLUMINATED FOLLOWED BY AP HOLDING ND, AND MIS-TRIM CAS MESSAGES. ATTEMPTS TO TRIM ELEVATOR MANUALLY AND ELECTRICALLY WERE UNSUCCESSFUL. LANDING WAS UNEVENTFUL AND ELEVATOR TRIM OPERATED NORMAL ONCE ON THE GRNov 3, 2016 · N869UP · Beech B300 · Elevator Tab Control SystemSDR O2GA2016103183301Fcu · intermittentLEFT ENGINE POWER LEVER BINDS AND POWER CHANGES RESPOND SLOWLY. MAINTENANCE REPLACED THE LEFT ENGINE FUEL CONTROL UNIT AND REPLACED THE STARTER GENERATOR. A SUCCESSFUL OPS CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.Oct 26, 2016 · N833UP · Beech B300 · Fuel Control/Turbine EnginesSDR 2016FA0000540Skin · crackedAT PHASE INSPECTION , FOUND FOUR INCH CRACK IN LOWER FORWARD AREA OF THE LEFT OUTER WING LEADING EDGE SKIN,1 INCH CRACK.Oct 26, 2016 · N15WS · Beech B300 · Wing, Plate/SkinSDR O2GA2016102486001Actuator · frozenAT FL270 AND -22*C RUDDER TRIM WAS FROZEN AND WOULD NOT MOVE. RUDDER TRIM BECAME FREE AFTER DESCENDING INTO WARMER AIR. LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED THE RUDDER TRIM ACTUATOR. A SUCCESSFUL OPERATIONAL CHECK FLIGHT WAS ACCOMPLISHED. AIRCRAFT WAS Oct 21, 2016 · N860UP · Beech B300 · Rudder Tab Control SystemSDR O2GA2016102484901Actuator · defectiveDURING APPROACH, GEAR DOWN AND FLAPS FULL DOWN PILOT NOTICED CONTROL YOKE BECAME VERY STIFF AND DIFFICULT TO CONTROL AIRCRAFT BANK ROLL. FLAP INDICATOR DID NOT INDICATE FULL DOWN. DECISION WAS MADE TO LEAVE THE FLIGHT CONTROL SETTINGS AS IS AND LAND USING RUDDOct 20, 2016 · N849UP · Beech B300 · Trailing Edge FlapsSDR O2GA2016101784201Bulb · burned outDURING APPROACH AFTER LOWERING THE LANDING GEAR, NOTICED RIGHT MAIN GEAR DID NOT SHOW A DOWN AND LOCKED INDICATION. TEST OF GEAR INDICATORS RESULTED IN RIGHT MAIN GEAR BULB BURNED OUT. TOWER FLY-BY CONFIRMED ALL THREE GEARS WERE DOWN. LANDING WAS UNEVENTFUL. Oct 16, 2016 · N842UP · Beech B300 · Landing Gear Position and WarningSDR O2GA2016092682401Fuel Control · defectiveCREW REPORTED RT ENGINE POWER LEVER LAGS AND IS VERY SLOW TO RESPOND TO FORWARD AND AFT MOVEMENT. MAINTENANCE R & R THE RT ENGINE FUEL CONTROL UNIT. SUCCESSFUL OPS CHECK FLIGHT WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.Sep 22, 2016 · N824UP · Beech B300 · Fuel Control/Turbine EnginesSDR O2GA2016091982801Annunciator · defectiveDURING CLIMB MASTER WARNING ANNUNCIATOR ILLUMINATED FOLLOWED BY CABIN DOOR UNLOCKED ANNUNCIATOR. RETURNED TO DEPARTURE, LANDING WAS UNEVENTFUL. CABIN DOOR UNLOCKED ANNUNCIATOR SYSTEM WAS DEFERRED IAW MINIMUM EQUIPMENT LIST. ACFT WAS RETURNED TO SERVICE.Sep 13, 2016 · N828UP · Beech B300 · Door Warning SystemSDR O2GA2016082786001Handle · out of adjustDURING CRUISE, FLIGHT CREW HEARD POPPING SOUND COMING FROM CABIN. NOTICED RIGHT EMERGENCY EXIT DOOR HANDLE CAME OUT OF STOWED POSITION. PRESSURIZATION WAS NORMAL. LANDING WAS UNEVENTFUL. MAINTENANCE ADJUSTED THE EMERGENCY EXIT DOOR HANDLE STOW TENSION. OPS CHAug 27, 2016 · N860UP · Beech B300 · Emergency ExitsSDR O2GA2016090183001Transducer · intermittentSTALL WARNING TRIPPED IN FLIGHT AND WOULD NOT RESET. LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED THE STALL WARNING LIFT TRANSDUCER. A SUCCESSFUL OPS CHECK FLIGHT WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.Aug 24, 2016 · N830UP · Beech B300 · Stall Warning SystemSDR O2GA2016072284301Knob · bindsRUDDER TRIM STUCK AT 0-POSITION IN FLIGHT. ABLE TO MOVE ON THE GROUND BUT STILL BINDS UP. MAINTENANCE WAS ABLE TO DUPLICATE THE DISCREPANCY, TRIM KNOB BINDING. TECHNICIAN REMOVED THE RUDDER TRIM KNOB WITHOUT ANY FORCE OR TOOLS. DURING INSTALLATION TECHNICIJul 21, 2016 · N843UP · Beech B300 · Rudder Tab Control SystemSDR O2GA2016071880001Engine · fodDURING SCHEDULED ROUTINE RIGHT ENGINE MAINTENANCE BORESCOPE INSPECTION, REVEALED FOD DAMAGE. ENGINE WAS REMOVED AND REPLACED WITH A RENTAL UNIT. A SUCCESSFUL OPERATIONAL CHECK FLIGHT WAS PERFORMED. AIRCRAFT WAS RTS.Jul 14, 2016 · N800UP · Beech B300 · Engine (Turbine/Turboprop)SDR O2GA2016082280201Hinge Bracket · out of alignmentAFTER DEPARTURE, EXCESSIVE AILERON INPUT REQUIRED TO MAINTAIN LEVEL FLIGHT. CREW LEVELED THE ACFT AT 3000 FT AFTER NOTIFYING ATC. CREW TRIED TO RETRIM THE ACFT SEVERAL TIMES AND DETERMINED THERE WAS AN AILERON/AILERON TRIM ISSUE. ACFT RETURNED TO DEPARTUREJul 7, 2016 · N802UP · Beech B300 · AileronsSDR O2GA2016070585901Actuator · defectiveAT FL300, AUTO PILOT HOLDING NOSE DOWN, CAUTION MESSAGE AND MIS-TRIM ANNUNCIATOR LIGHT ILLUMINATED INDICATING PITCH TRIM FROZEN. CREW WAS ABLE TO MAINTAIN CONTROL OF THE ACFT. AT FL220 PITCH TRIM AND AP OPERATED NORMAL. AIRCRAFT LANDING WAS UNEVENTFUL. MAIJun 29, 2016 · N859UP · Beech B300 · Stabilizer ActuatorSDR O2GA2016062480101Fire Bottle · dischargedCLIMBING OUT OF DEPARTURE, CREW HEARD POPPING NOISE AND SMELLED A CHEMICAL ODOR. ACFT DIVERTED BACK TO DEPARTURE. ACFT LANDING WAS UNEVENTFUL. MAINTENANCE FOUND THE COCKPIT PORTABLE FIRE EXTINGUISHER DISCHARGED. THE CABIN PORTABLE FIRE EXTINGUISHER WAS PLAJun 20, 2016 · N801UP · Beech B300 · Fire Bottle, PortableSDR O2GA2016062086101Actuator · intermittentDURING FLIGHT AT FL290, AP HOLDING ND, CAUTION ANNUNCIATOR ILLUMINATED. UNABLE TO TRIM THE ACFT DUE TO FROZEN TRIM WHEEL. ONCE BELOW 11,000 FT TRIM WHEEL AND AUTOPILOT BEGAN WORKING NORMAL. LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED BOTH ELEVATOR TRIM ACJun 15, 2016 · N861UP · Beech B300 · Elevator Tab Control System
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