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 O2GA2015091482201Controller · defectiveDURING DESCENT, GEAR HANDLE SELECTED DOWN, CREW HEARD A LOUD CLUNK. THE RED GEAR UNSAFE LIGHT ILLUMINATED & GEAR DID NOT EXTEND. MISSED APPROACH & FLEW OVER TOWER WHO CONFIRMED GEAR WAS NOT EXTENDED. GEAR HANDLE WAS SELECTED UP & LOUD CLUNK WAS HEARD AGAIN.Sep 7, 2015 · N822UP · Beech B300 · Landing Gear SelectorSDR O2GA2015090483201Blower Motor · defectiveAFTER STARTING THE RT ENG ELEC SMELL & SMOKE CAME THROUGH THE AIR CONDITIONING VENTS, ACFT WAS SHUT DOWN. TROUBLE SHOT THE DISCREPANCY TO A DEFECTIVE CABIN AFT BLOWER MOTOR. THE SYS WAS DEFERRED IAW MEL & THE BLOWER MOTOR WAS REPLACED A DAY LATER. ACFT WAS Sep 2, 2015 · N832UP · Beech B300 · Air Distribution SystemSDR O2GA2015090283801Door Seal · defectiveDURING CLIMB DOOR UNLOCKED ANNUNCIATION CAME ON. CREW FOLLOWED EMER CHECKLIST PROCEDURES, DECLARED AN EMER LANDING & DIVERTED. TROUBLE SHOT THE DISCREPANCY TO A BAD MAIN ENTRY DOOR SEAL. THE MAIN ENTRY DOOR SEAL WAS DEFERRED IAW THE MEL. ACFT WAS MOVED FORAug 25, 2015 · N838UP · Beech B300 · Passenger/Crew DoorsSDR CA150901004Engine · fluctuates(CAN) CUSTOMER REPORTED THAT ON DESCENT BOTH ENGINES TORQUE FLUCTUATING BETWEEN 20 PERCENT -7 PERCENT WHILE OTHER ENGINE PARAMETERS WERE SAID TO BE STABLE. EVENT LASTED APPROXIMATELY 3 MINUTES AND THE ACFT WAS REPORTED TO BE, FISH TAILING, DURING THAT EVENT. Aug 24, 2015 · Beech B300 · Engine (Turbine/Turboprop)SDR O2GA2015080582101Controller · defectiveAT 25,000' CRUISE THE ACFT SUDDENLY DEPRESSURIZED. CABIN ALTITUDE INDICATED 25,000', WHITE ALT & RED CAB ALT LIGHTS ILLUMINATED. PAX OXYGEN MASKS DEPLOYED, LIGHT ILLUMINATED & WARNING HORN SOUNDED. ACFT LANDED SAFELY. R & R THE CABIN PRESSURIZATION CONTROLJul 26, 2015 · N821UP · Beech B300 · Cabin Pressure ControllerSDR O2GA2015070680001Starter Gen · defectiveWHEN LT ENG START SWITCH WAS PLACED INTO, IGNITION & ENG START POSITION, NO N1 ROTATION WAS OBSERVED & VOLTAGE ON THE VOLTAGE SELECTOR DROPPED TO ZERO. APPROX THREE SECONDS INTO THE START SEQUENCE, SMOKE WAS OBSERVED BELLOWING OUT FROM TOP OF ENG COWL VENT. Jul 3, 2015 · N800UP · Beech B300 · Starter-GeneratorSDR O2GA2015070684501Fuel Cell · leakingFUEL LEAK DISCOVERED UNDER RT ENG NACELLE. REPLACED RT ENG NACELLE FUEL CELL. LEAK CHECKED GOOD. ACFT WAS RETURNED TO SERVICE.Jun 29, 2015 · N845KA · Beech B300 · Fuel StorageSDR O2GA2015070183601Stop Fitting · out of adjustON DESCENT THROUGH ABOUT FL 270 THE YELLOW ELEC PITCH TRIM INDICATION ON PFD FOLLOWED BY RED PITCH TRIM ANNUNCIATOR LIGHT. CONTROLS WERE VERY HARD TO PUSH FWD. USED POWER TO ASSIST IN THE CONTROL OF THE ACFT. AN EMERGENCY WAS DECLARED AT FL 200 & DIVERTED. Jun 27, 2015 · N836UP · Beech B300 · Elevator Tab Control SystemSDR O2GA2015062483701Starter Gen · inoperativeAT FL 260, RT DC GEN, CAUTION LIGHT CAME ON. RAN QRH, RT GEN DID NOT RESET. FOLLOWED QRH PROCEDURES & TURNED RT GEN OFF & REDUCED LOAD. LANDING WAS UNEVENTFUL. REPLACED THE RT STARTER GEN SYS. OPERATIONAL CHECK WERE GOOD. ACFT WAS RETURNED TO SERVICE.Jun 24, 2015 · N837UP · Beech B300 · Starter-GeneratorSDR O2GA2015062483301Fuel Cell · leakingFUEL LEAK COMING FROM AFT OF LT MLG WW. R & R LT OTBD & INBD FUEL CELLS, LEAK CHECKS GOOD. ACFT WAS RETURNED TO SERVICE. OTBD FUEL CELL PN REMOVED 002-920013-1 & SN 13-27059. INBD FUEL CELL PN REMOVED 101-381002-13 & SN CR-917.Jun 13, 2015 · N833UP · Beech B300 · Fuel StorageSDR O2GA2015062482001Fuel Cell · leakingUPON SHUTDOWN POST FLIGHT FUEL LEAK DISCOVERED FROM RT ENG NACELLE. REPLACED THE RT FUEL CELL. LEAK CHECKED GOOD. ACFT WAS RETURNED TO SERVICE.Jun 11, 2015 · N820UP · Beech B300 · Fuel StorageSDR O2GA2015060583201Packing · defectiveON POST FLIGHT, FUEL WAS LEAKING OUT OF THE RT ENG NACELLE. REPLACED THE RT ENG FUEL FILLET PACKING. ENG RUNS PERFORMED & NO LEAKS WERE NOTED. ACFT WAS RETURNED TO SERVICE.Jun 2, 2015 · N832UP · Beech B300 · Engine Fuel DistributionSDR CA150602023Coupling · disconnected(CAN) ON FIRST FLIGHT FOLLOWING THE 5 YEAR ENGINE HOSE REPLACEMENT, THE NR 1 ENGINE WAS SHUTDOWN DUE TO AN OIL LEAK. INITIAL MAINTENANCE INVESTIGATION FOUND THE QUICK DISCONNECT SELF SEAL COUPLING, PN 6000F14AD12 AND 6005F14AE12 ON THE HOSE BETWEEN THE SCAVENMay 30, 2015 · Beech B300 · Engine Fuel/Oil CoolerSDR O2GA2015052280201Proximity Switch · defectiveON CLIMB OUT THE RT PROPELLER PITCH ANNUNCIATOR ILLUMINATED. ACFT WAS DIVERTED BACK FOR MX. TROUBLE SHOT THE DISCREPANCY & FOUND A DEFECTIVE RT PROXIMITY SWITCH. ENG RUNS WERE PERFORMED & SYS OPERATIONAL CHECKS WERE GOOD. ACFT WAS RETURNED TO SERVICE.May 18, 2015 · N802UP · Beech B300 · Propeller Indication SystemSDR O2GA2015052283301Transducer · intermittentPILOT REPORTS RUDDER BOOST TEST HAS OPPOSITE RUDDER MOVEMENT WHEN TEST IS PERFORMED. LT THROTTLE HAS RT RUDDER MOVEMENT. RT THROTTLE HAS LT RUDDER MOVEMENT. TROUBLE SHOT THE DISCREPANCY & FOUND A DEFECTIVE LT ENG RUDDER BOOST TRANSDUCER. ENG TRANSDUCER WASMay 15, 2015 · N833UP · Beech B300 · Rudder Control SystemSDR O2GA2015051580101Duct · separatedAFTER LEVELING OFF AT FL 260 & COMMENCING THE CRUISE PHASE OF FLIGHT, PAXS REPORTED A BURNING SMELL POSSIBLY COMING FROM THE VENTS IN THE CABIN. AT THE SAME TIME THE, RT BLEED FAIL, ANNUNCIATOR LIGHT ILLUMINATED. AN EMER LANDING WAS DECLARED & THE ACFT RETUMay 11, 2015 · N801UP · Beech B300 · Air Distribution SystemSDR 2015FA0000244Seal · leakingTHE SEAL USED AT THE ACCESSORY GEARBOX LOCATION FOR THE FUEL PUMP/FUEL CONTROL UNIT PAD ON THE ENGINE IS LEAKING. AFTER REMOVING THE LEAKING THE LEAKING SEAL, WE OBSERVED THAT THE RUBBER LIP ASSEMBLY OF THE SEAL WAS DETACHED/ DISBONDED FROM THE METAL SEAL PORMay 8, 2015 · N187V · Beech B300 · Turbine Engine Oil SystemSDR O2GA2015043082101Fuel Cell · leakingFUEL LEAK ON RT WING BY WW. REPLACED THE RT AFT BOX & NACELLE FUEL BLADDERS. LEAK CHECKED OK. ACFT WAS RETURNED TO SERVICE. THIS SDR IS BEING SUBMITTED DUE TO A TREND OF NUMEROUS B300 WHEELS UP FLEET FUEL BLADDER LEAK REPORTS. BELIEVES THAT THE LEAKING FUApr 20, 2015 · N821UP · Beech B300 · Fuel StorageSDR O2GA2015042484501Skin · damagedDURING INSPECTION, FOUND TAIL OF WING LOCKER HARDWARE CAUSING DAMAGE TO THE UPPER SKIN OF THE LT INBD FLAP ASSEMBLY. THE FLAP ASSEMBLY WAS REMOVED & SENT FOR REPAIR. FLAP ASSEMBLY WAS RE-INSTALLED. COMPLIED WITH SERVICE BULLETIN SB-14-BC-01 FOR WING LOCKER Apr 19, 2015 · N845KA · Beech B300 · Trailing Edge FlapsSDR CA150420003Roller · missing(CAN) DURING TROUBLESHOOTING OF A CABIN DOOR UNLOCK INDICATION IT WAS NOTICED THAT THE UPPER FWD DOOR LATCH ASSY ROLLER AND PIN WERE MISSING.Apr 17, 2015 · Beech B300 · Passenger/Crew DoorsSDR O2GA2015042483701Skin · damagedDURING THE SCHEDULED 200 HOUR INSPECTION, MX FOUND A GOOD SIZED HOLE ON THE TOP OF THE LT INBD FLAP. THE CREW DIDN'T NOTICE IT BECAUSE THE DAMAGE WAS DIRECTLY UNDERNEATH THE WING LOCKER & UNNOTICEABLE WITH THE FLAPS UP. R & R THE LT INBD FLAP ASSEMBLY. ACFTApr 9, 2015 · N837UP · Beech B300 · Trailing Edge FlapsSDR O2GA2015032980401Pressure Switch · faultyAUTO PROP FEATHER TEST FAIL RT & LT ENGS. LT PROP LINGERS BETWEEN 670 & 680 RPM, TORQUE BETWEEN 13.5 & 16.1. RT PROP LINGERS BETWEEN 670 & 690 RPM, TORQUE BETWEEN 12.9 & 15.2. TROUBLE SHOT THE DISCREPANCY & FOUND A FAULTY LT & RT ENG AUTO FEATHER OIL PRESS Mar 29, 2015 · N804UP · Beech B300 · Propeller Feathering/ReversingSDR 2015FA0000115Nipple · leakingFLIGHT CREW REPORTED FUEL DRIPPING FROM LT WING. MAINTENANCE REMOVED SUSPECTED FUEL TANK, LEFT, L/E OTBD TANK AND PRESSURE TESTED. AIR WAS FOUND TO BE COMING OUT OF THE MAIN TANK OUTLET NIPPLE. MAINTENANCE REMOVED TH PSI TEST PLUG AND INSPECTED THE NIPPLE AMar 19, 2015 · N1867 · Beech B300 · Fuel StorageSDR O2GA2015031383501Computer · weakPILOT REPORTS RUDDER BOOST TEST HAS OPPOSITE RUDDER MOVEMENT WHEN TEST IS PERFORMED. LT THROTTLE HAS RT RUDDER MOVEMENT. RT THROTTLE HAS LT RUDDER MOVEMENT. MX WAS UNABLE TO DUPLICATE THE DISCREPANCY WITH THE CREW. DURING TEST IT WAS NOTED THAT THE SYS WASMar 13, 2015 · N835UP · Beech B300 · Rudder Control SystemSDR O2GA2015030282001Accumulator · defectiveDEPARTED, SHORTLY AFTER LEVELING OFF AT FL 250, HYD FLUID LOW, CAUTION ANNUNCIATOR ILLUMINATED. FOLLOWED CHECKLIST & CONTINUED TO DESTINATION. DURING NEXT SEVERAL MINUTES CREW HEARD GEAR PUMP MOTOR CYCLING FOLLOWED BY LG RELAY CB EXTENDED. DURING APPROACH LMar 2, 2015 · N820UP · Beech B300 · Landing Gear Retraction/Extension SystemSDR O2GA2015022483301Switch · out of adjustUPON TAKEOFF THE LG WOULD NOT RETRACT, FOLLOWED BY THE PROP GND SOL INDICATION. FOLLOWED CHECKLIST CONFIRMED GEAR DOWN & LOCKED. RETURNED & LANDING WAS UNEVENTFUL. VERIFIED THE DISCREPANCY & ADJUSTED THE RT LG SAFETY SWITCH. GEAR SWINGS PERFORMED WITH NO DFeb 20, 2015 · N833UP · Beech B300 · Landing Gear Position and WarningSDR O2GA2015021782401Control Valve · defectiveON DESCENT AT AN ALTITUDE OF 5,000 THE CABIN DIFFERENTIAL WENT TO .3 & THE CABIN ALTITUDE DESCENDED AT THE RATE OF DESCENT THAT THE ACFT WAS DESCENDING AT, LANDING WAS UNEVENTFUL. TROUBLE SHOT THE DISCREPANCY TO A FAULTY PRESSURIZATION CONTROL VLV. CONTROLLEFeb 17, 2015 · N824UP · Beech B300 · Cabin Pressure Control SystemSDR O2GA2015021283601Knob · malfunctionedDURING PREFLIGHT INSPECTION RUDDER TRIM DIFFICULT TO ROTATE & SKIPS UNITS MAKING POSITION INDICATION INACCURATE. MX DISASSEMBLED RUDDER TRIM TAB KNOB & POINTER ASSEMBLY, CLEANED, LUBED & RE-INDEXED TRIM INDICATOR ASSEMBLY. NO DEFECTS NOTICED. ACFT WAS RETURFeb 10, 2015 · N836UP · Beech B300 · Rudder Tab Control SystemSDR O2GA2015020380101O-Ring · wornLIGHT OIL COATING ON RT ENG NACELLE & PROPELLER BLADES. APPEARS TO BE COMING FROM PROPELLER HUB. REMOVED THE SPINNER & PISTON TO REPLACE ORINGS. REPLACED ORINGS, PN C3317-20 & C33160426-2, PERFORMED ENG RUNS & NO LEAKS NOTED. ACFT WAS RETURNED TO SERVICE.Jan 25, 2015 · N801UP · Beech B300 · Propeller Hub SectionSDR O2GA2015010783101Safety Switch · out of adjustON APPROACH, WHEN FLAP HANDLE WAS SELECTED TO FLAP APPROACH, FLAP FAILED TO EXTEND. AN UNEVENTFUL FLAPS UP LANDING WAS PERFORMED IAW THE QRH. TROUBLE SHOT THE DISCREPANCY TO A RT WING FLAP LIMIT SAFETY SWITCH ADJUSTMENT. THE RT WING FLAP LIMIT SAFETY SWITCHDec 31, 2014 · N831UP · Beech B300 · Trailing Flap Position Indicating SystemSDR O2GA2014122380702Solenoid Valve · overheatedDURING CRUISE CREW SMELLED ELEC TYPE BURNING SMELL. CREW DONNED OXYGEN MASK. FEW MINUTES LATER CREW REMOVED MASK & SMELL WAS UNDETECTABLE. DURING DESCENT CREW NOTICED THE SMELL AGAIN & ELECTED TO DIVERT TO & DECLARED AN EMER. LANDING WAS UNEVENTFUL. ACFT Dec 16, 2014 · N807UP · Beech B300 · Cabin Pressure Control SystemSDR O2GA2014121580701Unknown · hazeDURING CLIMB THROUGH 6000’ CREW SMELLED AN ELEC TYPE BURNING SMELL FOLLOWED BY SLIGHT HAZE IN CABIN. ACFT DIVERTED & LANDING WAS UNEVENTFUL. FIRE TRUCKS WERE STANDING BY. MX APPLIED POWER TO ACFT & PERFORMED OPERATIONAL CHECKS OF ELEC SYS & COMPONENTS. INSDec 12, 2014 · N807UP · Beech B300 · Air Distribution SystemSDR O2GA2014112582901Circuit Breaker · trippedDURING APPROACH, WHEN THE GEAR HANDLE WAS SELECTED TO DOWN POSITION THE GEAR FAILED TO EXTEND. REFERENCED THE QRH & DISCOVERED THE LG RELAY CIRCUIT BREAKER TRIPPED. RESET THE CIRCUIT BREAKER, GEAR EXTENSION WAS NORMAL & LANDING WAS UNEVENTFUL. SERVICED THE Nov 17, 2014 · N829UP · Beech B300 · Landing Gear Retraction/Extension SystemSDR O2GA2014112583101Indication Sys · malfunctionedON TAKEOFF ROLL OUT APPROX 40 - 50 KTS THE MASTER CAUTION LIGHT FLASHED FOLLOWED BY THE HYD FLUID LOW ANNUNCIATOR. TAKEOFF WAS ABORTED. TAXI BACK WAS UNEVENTFUL. MX CHECKED THE HYD RESERVOIR FLUID LEVEL & THE ACCUMULATOR PRE-CHARGE WITH NO DEFECTS NOTED. INov 15, 2014 · N831UP · Beech B300 · Hydraulic Indicating SystemSDR 2014FA0000655Gear · wornDURING 1200 HOUR LUBRICATION OF THE FLAP DRIVE GEARBOX, NOTED THE FORWARD GEAR WAS WORN TO THE END OF SERVICEABLE LIMITS. THE FLAP SYSTEM OPERATED NORMALLY GIVING NO INDICATION OF IMPENDING FAILURE. A NEW GEAR AND BEARING WAS INSTALLED AND THE GEARBOX SERVICNov 11, 2014 · N5626Y · Beech B300 · Trailing Edge Flap Control SystemSDR O2GA2014112482001Unknown · smokeBEFORE TAXIING CREW EXPERIENCED SMOKE ENTERING THE CABIN AFTER ENG START. SMOKE WENT AWAY WHEN RT ENG BLEED AIR WAS TURNED OFF. CREW IMMEDIATELY SHUTDOWN THE ENG. PERFORMED ENG RUNS WITH CREW. ENG BLEED & ENVIRONMENTAL SYS WAS OPERATED & NO DEFECTS WERE NOOct 17, 2014 · N820UP · Beech B300 · Air Distribution SystemSDR O2GA2014201483301Switch · out of adjustSHORTLY AFTER TAKEOFF PROP GND SOL LIGHT CAME ON. RAN ABNORMAL CHECKLIST & RETURNED, LANDING WAS UNEVENTFUL. MX ADJUSTED THE GND IDLE STOP SWITCH & A SUCCESSFUL OPERATIONAL CHECK WAS PERFORMED. ACFT WAS RETURNED TO SERVICE.Oct 14, 2014 · N833UP · Beech B300 · Engine ControlsSDR KX5R20140914003Actuator · crackedLEFT INBD FLAP ACTUATOR FOUND SPLIT LENGTHWISE ALONG LENGTH OF ACTUATOR PISTON DURING ROUTINE PHASE 1 INSPECTION. PHASE 1 INSPECTION CONSISTS OF EMPHASIS ON THE WINGS STRUCTURE AND ASSOCIATED COMPONENTS. FLAPS OPERATED NORMALLY BUT LT INBD FLAP ACTUATOR MADE Sep 8, 2014 · N1525C · Beech B300 · Trailing Edge Flap ActuatorSDR O2GA2014090282001Sense Line · faultyDURING CLIMB THE RT ENG BLEED FAIL ANNUNCIATOR LIGHT CAME ON. ACCOMPLISHED THE BLEED AIR FAILURE CHECKLIST THEN REQUESTED CLEARANCE TO LAND. LANDING WAS UNEVENTFUL. TROUBLE SHOT THE DISCREPANCY & FOUND A FAULTY RT BLEED AIR SENSE LINE. SENSE LINE WAS REPLAAug 27, 2014 · N820UP · Beech B300 · Pneumatic Indicating SystemSDR O2GA2014082782501Transducer · faultyDURING FLIGHT LT ENG OIL PRESS INDICATION ON MFD. DISCOVERED OIL PRESS INDICATOR CB EXTENDED. ENG OIL TEMP WAS NORMAL. LANDING WAS UNEVENTFUL. DISCREPANCY WAS TROUBLE SHOT TO A FAULTY OIL PRESS TRANSDUCER. LT ENG OIL PRESS TRANSDUCER WAS REPLACED. OPERATAug 22, 2014 · N825UP · Beech B300 · Engine Oil PressureSDR O2GA2014080482201Static Inverter · defectiveSMOKE IN COCKPIT & CABIN DURING FLIGHT. CREW USED OXYGEN MASK DURING LANDING AS PRECAUTION. LANDING WAS UNEVENTFUL. TROUBLE SHOT THE DISCREPANCY TO A FAULTY STATIC INVERTER IN AFT CABIN. STATIC INVERTER WAS REPLACED. OPERATIONS CHECKED OK & ACFT WAS RETURAug 1, 2014 · N822UP · Beech B300 · AC InverterSDR O2GA2014072480401Light · inoperativeON FINAL APPROACH THE LT MAIN GEAR LIGHT DID NOT ILLUMINATE. THE NOSE GEAR & RT MAIN GEAR LIGHTS ILLUMINATED NORMALLY. A GO AROUND WAS INITIATED TO TROUBLESHOOT & IT WAS DETERMINED THAT THERE WAS NO GEAR UNSAFE RED INDICATED & THE GEAR WARNING HORN DID NOT SJul 23, 2014 · N804UP · Beech B300 · Landing Gear Position and WarningSDR O2GA2014071582701Switch · intermittentPROP GND SOL ANNUCIATOR ILLUMINATED IN FLIGHT. COMPLIED WITH CHECKLIST & ANNUNCIATOR EXTINGUISHED. REPLACED THE PROPELLER GND FINE SWITCH IN THE PEDESTAL & PERFORMED A SUCCESSFUL OPERATIONAL CHECK. ACFT RETURNED TO SERVICE.Jul 7, 2014 · N827UP · Beech B300 · Propeller Indication SystemSDR O2GA68134Bladder · leakingFUEL LEAK FROM RT GEAR WELL AT 2 - 3 DROPS PER SECOND. FUEL BLADDER LEAKING. THIS ACFT HAD THE FUEL BLADDERS REPLACED.Jun 22, 2014 · N806UP · Beech B300 · Fuel StorageSDR O2GA2014052082601Sense Line · defectiveCLIMBING THROUGH 18000’ MSL THE RT BLEED FAIL ANNUNCIATOR ILLUMINATED. CREW SECURED RT BLEED SWITCH TO PNEUMATIC & ENVIRONMENTAL OFF. COMPLIED WITH CHECKLIST & DIVERTED TO KBEC. LANDING WAS UNEVENTFUL. R & R THE RT OTBD NACELLE BLEED AIR SENSE LINE. A SUCCMay 14, 2014 · N826UP · Beech B300 · Pneumatic Indicating SystemSDR CA140508008Controller · failed(CAN) THE SPEED CONTROLLER FOR THE FORWARD CABIN VENT BLOWER FAILED. THE CREW NOTED A STRONG ELECTRICAL ODOR AND SMOKE ON FINAL TO LAND. THEY CONTINUED THE LANDING SAFELY. THE SPEED CONTROLLER BOX WHICH IS MOUNTED IN THE FORWARD AVIONICS BAY, IN A PRESSURIZMay 6, 2014 · Beech B300 · Air Distribution FanSDR CA140421002Skin · cracked(CAN) DURING A SCHEDULED INSPECTION A 4.5" CRACK RUNNING LONGITUDINALLY WAS DISCOVERED IN THE BELLY SKIN. IT IS LOCATED BETWEEN FS 254.5 AND FS 259.0 AND ON THE FIRST STR TO THE RT SIDE OF CENTER. IT RUNS DIRECTLY UNDER A STR AND APPEARS TO BE WHERE THE BONDApr 18, 2014 · Beech B300 · Fuselage Main, Plate/SkinSDR CA140401013Filter · contaminated(CAN) DURING REVENUE FLIGHT, ON APPROACH FOR LANDING, THE PILOT DID NOT HAVE ANY POWER RESPONSE FROM ENG NR 2. THE ENGINE POWER WAS LEFT AT IDLE DURING APPROACH AND LANDED UNEVENTFULLY. DURING GROUND RUN, THE ENGINE POWER STAYED AT 48.5 PERCENT NG, WHICH IS CMar 29, 2014 · Beech B300 · Engine (Turbine/Turboprop)SDR O2GA2014051584501Line · damagedDURING CRUISE, LT BLEED FAIL & RT BLEED FAIL ANNUNCIATORS ILLUMINATED. EMERGENCY PROCEDURES CHECKLIST WAS FOLLOWED & COMPLETED. CABIN PRESSURIZATION WAS NORMAL & LANDING WAS UNEVENTFUL. TROUBLESHOT & FOUND THE LT & RT EVA BLEED AIR WARNING SENSE LINES DAMAMar 24, 2014 · N845KA · Beech B300 · Pneumatic Distribution SystemSDR XA1R201403210001Actuator · crackedPILOT REPORTED THAT HE HEARD A LOUD BANG AND LANDING GEAR EXTENDED UNCOMMANDED. ACFT FLEW BY CONTROL TOWER AND CONFIRMED GEAR EXTENDED BUT NOSE NOT LOCKED. PILOT PERFORMED EMERGENCY GEAR EXTENSION PROCEDURE AND LANDED WITHOUT FURTHER INCIDENT. UPON VISUAL IMar 18, 2014 · N345DG · Beech B300 · Landing Gear Actuator
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