Textron 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 O2GA2016053182101Vent Line · looseAT CRUISE ALTITUDE LT ENG OIL PRESS WENT TO 85 PSI & CONTINUED TO DROP. OIL WAS OBSERVED COMING FROM THE LT ENG BEHIND THE PROPELLER, AT 65 PSI ENG WAS SHUT DOWN. AN EMER WAS DECLARED & ACFT DIVERTED. SECURED THE OIL VENT LINE FROM THE TORQUE TRANSMITTER ATMay 29, 2016 · N821UP · Beech B300 · Engine Oil Distribution (Airframe Furnished)SDR O2GA2016053182301Dipstick · detachedON PREFLIGHT CREW NOTICED LT ENG OIL DIPSTICK WAS DETACHED FROM FILLER CAP ASSEMBLY & NOT VISIBLE INSIDE FILL TUBE. MX RETRIEVED OIL DIPSTICK FROM INSIDE OIL TANK. LATEST CONFIGURATION OIL FILLER TUBE & DIPSTICK ASSEMBLY WITH BALL CHECK VLV INSTALLED IAW SB May 27, 2016 · N823UP · Beech B300 · Turbine Engine Oil SystemSDR O2GA2016052782901Cabin Pressure · malfunctionedDURING CRUISE FLIGHT AT FL290 ACFT EXPERIENCED A CABIN PRESS LOSS. AN EMER DESCENT WAS ACCOMPLISHED. ALL CABIN MASKS WERE DEPLOYED. LANDING WAS UNEVENTFUL. ACFT HAS BEEN RELEASED FOR AN OPERATIONAL CHECK FLIGHT. REPLACED THE LT MAIN GEAR SAFETY SWITCH, OUMay 22, 2016 · N829UP · Beech B300 · Cabin Pressure Control SystemSDR J8UR20170901001Door · brokenDURING INSPECTION OF THE FLIR / LIFT ASSEMBLY INSTALLATION, IT WAS NOTED THAT UPPER PIVOT PIN WHICH IS PART OF DOOR ASSEMBLY WAS BENT. THERE HAVE BEEN MULTIPLE FAILURES OF THIS PART SOME DUE TO RIGGING AND ALIGNMENT ISSUES. THERE HAVE BEEN FAILURES OF THIS CMay 16, 2016 · N162FM · Beech B300 · Passenger/Crew DoorsSDR E07A2016051300001Brake Assy · warpedRIGHT OTBD NR 4 MAIN TIRE, BRAKE LOCKED UP AND FLAT SPOTTED TIRE TILL IT DEFLATED.May 12, 2016 · N291AS · Beech B300 · Landing Gear Brake SystemSDR O2GA2016040985301Fcu · defectivePOWER SPLIT IN THE THROTTLE LEVERS. WHEN REDUCING POWER RT ENG TORQUE INDICATIONS LAG BEHIND LT ENG BY 5 - 10%. R & R THE RT ENG FUEL CONTROL, RT STARTER GEN ALSO REMOVED FOR VIBE ANALYSIS. SUCCESSFUL GND HEAT & OPERATIONAL CHECK FLIGHT PERFORMED. ACFT WASMay 4, 2016 · N855UP · Beech B300 · Fuel Control/Turbine EnginesSDR O2GA2016042585502Actuator · faultyELEVATOR TRIM FROZE INFLIGHT AT CRUISE ALTITUDE. DURING DESCENT ELEVATOR TRIM OPERATES NORMAL. LUBRICATED THE LT & RT ELEVATOR TRIM JACKS. ELEVATOR TRIM OPERATIONAL CHECKS WERE GOOD. ACFT WAS FERRIED TO THE MFG SERVICE CENTER FOR FURTHER EVALUATION DUE TO Apr 22, 2016 · N855UP · Beech B300 · Elevator Tab Control SystemSDR O2GA2016042180101Fcu · defectiveLEFT ENG CONDITION LEVER DIFFICULT TO MOVE, MUCH MORE THAN RT LEVER. R & R THE LT ENG FCU. SUCCESSFUL GND & FLIGHT OPERATIONAL CHECK PERFORMED. ACFT WAS RETURNED TO SERVICE.Apr 18, 2016 · N801UP · Beech B300 · Fuel Control/Turbine EnginesSDR O2GA2016040483401Blower · defective30 MINUTES INTO FLIGHT CREW NOTICED AN ELECTRICAL BURNING SMELL. TURNING THE ECS TO MANUAL COOL, COCKPIT BLOWERS ON & CABIN BLOWER OFF, SMELL WENT AWAY. LANDING WAS UNEVENTFUL. REPLACED DEFECTIVE FWD & AFT CABIN EVAPORATOR BLOWER MOTORS. SYSTEM OPERATIONALMar 31, 2016 · N834UP · Beech B300 · Air Distribution FanSDR O2GA2016040885501Actuator · lack of lubeELEVATOR TRIM ELEC & MANUAL JAMMED IN FLIGHT. INSPECTED & LUBED THE LT & RT ELEVATOR TRIM TAB ACTUATORS. OPERATIONS CHECKED OK. ACFT RTS. NO OCCURRENCE SINCE ACFT WAS RTS.Mar 30, 2016 · N855UP · Beech B300 · Elevator Tab Control SystemSDR 2016FA0000141Angle · cracked5 SEAT TRACK SUPPORT FORMERS, BULKHEADS CRACKED UNDERFLOOR AFT OF SPAR.Mar 22, 2016 · N214ML · Beech B300 · Fuselage, Seat/Cargo Attach FittingsSDR O2GA2016031780101Link Assy · defectiveCREW FELT SNAP IN RUDDER PEDALS WHILE TAXIING, FOLLOWED BY NOSE WHEEL STEERING INOPERATIVE. REPLACED A DEFECTIVE NOSE STEERING LINK ASSEMBLY. RUDDER & TAXI SYS OPERATIONS CHECKS WERE GOOD. ACFT WAS RETURNED TO SERVICE.Mar 13, 2016 · N801UP · Beech B300 · Landing Gear Steering SystemSDR O2GA2016031783301Fcu · faultyRIGHT POWER LEVER MOVEMENT DOES NOT PRODUCE A POWER CHANGE. 10 SEC LAG FOR POWER TO CHANGE. R & R THE RT FCU. A SUCCESSFUL OPERATIONAL CHECK FLIGHT WAS PERFORMED. ACFT WAS RETURNED TO SERVICE. SDR IS BEING SUBMITTED DUE TO PT6A-60A HISTORY OF ENG POWER LEMar 8, 2016 · N833UP · Beech B300 · Fuel Control/Turbine EnginesSDR O2GA2016022782801Actuator · contaminatedAT FL240 THE PITCH TRIM WAS JAMMED AT THE 0* SETTING & THE CONTROLS REQUIRED A NOTICEABLE BUT NOT EXCESSIVE AMOUNT OF FWD PRESS TO MAINTAIN LEVEL FLIGHT. CREW LEFT THE PITCH TRIM IN CURRENT POSITION & LANDED WITHOUT INCIDENT. THE ELEC PITCH TRIM WAS PREVIOUSFeb 27, 2016 · N828UP · Beech B300 · Stabilizer ActuatorSDR O2GA2016022080701Bellcrank · defectiveFASTENER FOUND LOOSE IN THE RUDDER BAR BELL CRANK ATTACHMENT. ACFT WAS FERRIED FOR RUDDER BELL CRANK REPLACEMENT IAW ENGINEERING NTO. BELL CRANK WAS REPLACED & ACFT WAS RTS.Feb 20, 2016 · N807UP · Beech B300 · Rudder Control SystemSDR O2GA2016022082101Fcu · defectiveRIGHT ENG POWER LEVER DOES NOT RESPOND PROPERLY TO LEVER MOVEMENT. R & R THE RT ENG FCU. GND OPERATIONS & LEAK CHECKS WERE GOOD. A SUCCESSFUL OPERATIONAL CHECK FLIGHT WAS PERFORMED & ACFT IT WAS RTS.Feb 20, 2016 · N821UP · Beech B300 · Fuel Control/Turbine EnginesSDR O2GA2016021580401Fcu · defectiveLEFT ENG POWER LEVER IS DIFFICULT TO ADVANCE FWD. EXHIBITS A SPONGE LIKE FEELING. R & R THE LT ENG FUEL CONTROL UNIT. GND OPERATIONS & LEAK CHECKS WERE GOOD. A SUCCESSFUL OPERATIONAL CHECK FLIGHT WAS PERFORMED. ACFT WAS RTS.Feb 15, 2016 · N804UP · Beech B300 · Fuel Control/Turbine EnginesSDR O2GA2016021485501Brake · warpedAFTER REPLACING THE NR 3 & 4 WHEEL & TIRE ASSEMBLIES DUE TO FLAT SPOTTING, WHEELS WERE NOT SPINNING FREELY DUE TO POSSIBLE DEFECTIVE BRAKE ASSEMBLIES. BOTH RT BRAKE ASSEMBLIES WERE REPLACED. TAXI CHECKS PERFORMED WITH NO DEFECTS NOTED. ACFT WAS RTS.Feb 14, 2016 · N855UP · Beech B300 · BrakeSDR O2GA2016021283601Fuel Control · defectiveLEFT POWER LEVER BINDS WHEN ADVANCED FWD. IN CRUISE POWER LEVERS ARE SPLIT BY ONE KNOB WIDTH. R & R THE LT ENG FUEL CONTROL UNIT. A SUCCESSFUL OPERATIONAL CHECK FLIGHT WAS PERFORMED. ACFT WAS RETURNED TO SERVICE.Feb 12, 2016 · N836UP · Beech B300 · Fuel Control/Turbine EnginesSDR O2GA2016021282201Rivet · looseCREW PREFLIGHT NOTICED THE RUDDER PEDALS ARE LOOSE TO RUDDER MOVEMENT. TROUBLE SHOT THE DISCREPANCY TO LOOSE RIVETS ON RUDDER TORQUE SHAFT. TORQUE LINK & SHAFT WAS REPLACED WITH NEW PARTS. ACFT WAS RETURNED TO SERVICE.Feb 12, 2016 · N822UP · Beech B300 · Rudder Control SystemSDR CA160208008Fms · failed(CAN) UNIVERSAL AVIONICS FMS UNS 1K DATA BASE WAS UPDATED AND CDU DATA BUS FAIL IS DISPLAYED AFTER POWER UP.UNABLE TO PERFORM ANY OTHER FUNCTIONS.Feb 8, 2016 · Beech B300 · Flight Management Computing Hardware SystemSDR O2GA2016013182102Fcu · failedRIGHT ENG CONDITION LEVER WILL NOT ADVANCE OUT OF FUEL CUT OFF. REPLACED THE RT ENG FUEL CONTROL UNIT. A SUCCESSFUL OPERATIONAL CHECK FLIGHT WAS PERFORMED. ACFT WAS RTS.Jan 31, 2016 · N821UP · Beech B300 · Fuel Control/Turbine EnginesSDR O2GA2016012880101Tire · blownUPON LANDING BOTH LT MAIN TIRES BLEW OUT. R & R ALL 4 MLG WHEEL & TIRE ASSEMBLIES. ACFT WAS RETURNED TO SERVICE.Jan 28, 2016 · N801UP · Beech B300 · TireSDR CA160201008Switch · failed(CAN) WHILE MAINTENANCE WERE CARRYING OUT SOME TESTING IT WAS DISCOVERED THAT THE RT PUSH TO TALK SWITCH WAS UNSERVICEABLE, THIS SWITCH HAD BEEN REPLACED 22.7 HRS PREVIOUSLY. WHILE CHECKING THE HISTORY OF THESE SWITCH REPLACEMENTS, IT WAS DISCOVERED THAT WE HJan 26, 2016 · Beech B300 · Communications SystemSDR O2GA2016012582102Fcu · out of rigDURING OPERATIONAL CHECK FLIGHT FOR FCU REPLACEMENT EXCESSIVE TORQUE SPLIT WITH THROTTLES MATCHED. RIGGED & ADJUSTED THE RT ENG FCU. A SUCCESSFUL OCF WAS PERFORMED. ACFT WAS RTS.Jan 25, 2016 · N821UP · Beech B300 · Fuel Control/Turbine EnginesSDR O2GA2016012080201Tire · blownLEFT OTBD MLG TIRE BLEW ON LANDING. REPLACED THE LT OTBD & INBD MAIN WHEEL & TIRE ASSEMBLIES. NO FURTHER DEFECTS WERE NOTED. ACFT WAS RTS.Jan 20, 2016 · N802UP · Beech B300 · TireSDR O2GA2016011782101Fcu · defectiveTHE RT FUEL CUT OFF LEVER IS VERY HARD TO MOVE IN EITHER DIRECTION. REPLACED THE RIGHT FCU. OPERATION & LEAK CHECKED OK. ACFT WAS RTS.Jan 17, 2016 · N821UP · Beech B300 · Fuel Control/Turbine EnginesSDR O2GA2016011583701Light · inoperativeON DESCENT, MOVED GEAR HANDLE TO DOWN POSITION & RT GEAR GREEN ANNUNCIATOR DID NOT ILLUMINATE. MISSED APPROACH, CYCLED GEAR HANDLE, DECLARED AN EMER & DIVERTED. LANDING WAS UNEVENTFUL. REPLACED INOPERATIVE BULBS ON RT GEAR INDICATOR. ANNUNCIATOR TEST WAS GJan 15, 2016 · N837UP · Beech B300 · Landing Gear Position and WarningSDR O2GA2016011284302Lever · stiffDURING OPERATIONAL CHECK FLIGHT, LT ENG CONDITION LEVER STILL STIFF AFTER COLD SOAK. ACFT IS CURRENTLY IN MX AT THE MFG FACTORY. SDR SUPPLEMENT TO FOLLOW.Jan 12, 2016 · N843UP · Beech B300 · Power LeverSDR O2GA2016010784301Fcu · defectiveLEFT ENG CONDITION LEVER STUCK IN FUEL CUTOFF POSITION. FLIGHT CONTROL UNIT WAS REPLACED, RIGGING ACCOMPLISHED & SUCCESSFUL GROUND OPERATIONAL CHECK PERFORMED.Jan 7, 2016 · N843UP · Beech B300 · Fuel Control/Turbine EnginesSDR O2GA2015122883101Blower · failedWITH BATTERY POWER ON, EXTERNAL POWER CONNECTED & ON, ALONG WITH BLOWERS & ELECTRIC HEAT ON, THE CABIN FILLED WITH SMOKE. ACFT WAS POWERED DOWN. TROUBLE SHOT THE SQUAWK TO A FAULTY FWD CABIN EVAPORATOR BLOWER. EVAPORATOR BLOWER WAS REPLACED & THE ACFT WAS RDec 28, 2015 · N831UP · Beech B300 · Air Distribution FanSDR O2GA2015122885301Actuator · contaminatedDURING CRUISE FLIGHT, THE CREW NOTICED THE RUDDER & AILERON TRIM TABS BECOMING VERY STIFF & DIFFICULT TO OPERATE. THE ACFT WAS EXPOSED TO MOISTURE & FREEZING TEMPERATURES THROUGHOUT THE DAY. DURING LANDING TRIM OPERATED NORMALLY WITHOUT ANY ISSUES. REMOVED Dec 28, 2015 · N826UP · Beech B300 · Rudder Tab Control SystemSDR CA151214014Downlock Switch · intermittent(CAN) NO RT MAIN GEAR GREEN INDICATION ON APPROACH, GEAR RECYCLED BUT STILL NO INDICATION. ACFT DIVERTED TO MAINTENANCE BASE, EMERGENCY HAND PUMP USED TO LOWER GEAR AND GREEN INDICATION WORKED, ACFT LANDED SAFELY WITH 3 GREEN INDICATION AND TAXIED BACK TO MAIDec 12, 2015 · Beech B300 · Landing Gear Position and WarningSDR CA151212002Encoder · malfunctioned(CAN) INITIALLY THE NR 2 ENCODING ALTIMETER HAD VIBRATOR ISSUES. THE ALTIMETER WAS REPLACED WITH A O/H UNIT. UNIT FAILED ON INSTALLATION, ENCODER WAS MALFUNCTIONING. NEW ALTIMETER WAS ORDERED.Dec 10, 2015 · Beech B300 · Altimeter, Barometric/EncoderSDR O2GA2015121080801Hose · defectiveLEFT BRAKE INOPERATIVE DURING TAXI. REPLACED THE COPILOTS SIDE MASTER CYLINDER & HOSE. TAXI CHECK COMPLIED WITH. ACFT RTS.Dec 10, 2015 · N808UP · Beech B300 · Landing Gear Brake SystemSDR CA151216004Fcu · malfunctioned(CAN) DURING FLIGHT AT FL270, THE NR 1 ENGINE POWER ROLLED BACK TO IDLE. A SAFE LANDING WAS THEN ACCOMPLISHED. POST FLIGHT INSPECTION FOUND THE RIGGING OK BUT GROUND RUNS SHOWED THE ENGINE HANGING AT 58 PERCENT COMPRESSOR SPEED, NG AND THE PROPELLER NOT ABLEDec 2, 2015 · Beech B300 · Fuel Control/Reciprocating EnginesSDR O2GA2015120784301Fcu · defectiveAT CRUISE FLIGHT FL270, THE LT ENG SLOWLY ROLLED BACK TO IDLE 58% N1. EMER CHECKLIST FOLLOWED. AN EMER WAS DECLARED & DIVERTED. LANDING WAS UNEVENTFUL. REPLACED LT ENG FCU, RIGGING ACCOMPLISHED & SUCCESSFUL OPERATIONAL CHECK FLIGHT WAS PERFORMED. ACFT WASDec 2, 2015 · N843UP · Beech B300 · Fuel Control/Turbine EnginesSDR O2GA2015120180601Light · inoperativeGEAR EXTENSION, LT MAIN GEAR GREEN INDICATION DID NOT ILLUMINATE. A GO AROUND WAS INITIATED & CHECKLIST PROCEDURES FOLLOWED WITH NO HELP. AN EMER WAS DECLARED & LANDING WAS UNEVENTFUL. TROUBLE SHOT THE DISCREPANCY TO AN INOPERATIVE LT MAIN GEAR INDICATOR LINov 27, 2015 · N806UP · Beech B300 · Landing Gear Position and WarningSDR O2GA2015111980701Unknown · smokeSTRONG ELECTRICAL ODOR MINUTES AFTER DEPARTURE. CREW NOTICED SMOKE COMING FROM UNDERNEATH FLOOR, BETWEEN SEATS 6 & 8. AN EMER WAS DECLARED & ACFT DIVERTED. LANDING WAS UNEVENTFUL. ACCESSED & INSPECTED SURROUNDING AREA WITH NO DEFECTS NOTED. ENG GND RUNS PNov 16, 2015 · N807UP · Beech B300 · Air Distribution SystemSDR O2GA2015111283201Unknown · malfunctionedDURING CRUISE, RT GEN TIE OPEN, CAUTION LIGHT & ANNUNCIATOR LIGHTS ILLUMINATED. ABNORMAL CHECKLIST, FOR RT GEN TIE OPEN, WAS ACCOMPLISHED. A BUS RESET WAS PERFORMED. RT GEN TIE OPEN, CAUTION & ANNUNCIATOR LIGHTS ILLUMINATED AGAIN AFTER 45 SECONDS. AUTO PILNov 11, 2015 · N832UP · Beech B300 · Electrical Power SystemSDR O2GA2015110684901Actuator · lack of lubeDURING CRUISE AT -29 C, ALL THREE TRIM CONTROLS BEGAN TO FREEZE. A DESCENT TO WARMER AIR SOLVED THE ISSUE. NO LOSS OF ACFT CONTROL. DUE HANGER AVAILABILITY THE ACFT WAS PARKED IN BLOWING RAIN FOR TWO DAYS PRIOR TO THIS EVENT. LUBED THE AILERON, RUDDER & ELNov 1, 2015 · N849UP · Beech B300 · Aileron Tab Control SystemSDR CA151031007Bearing Cage · failed(CAN) AIRCRAFT WAS IN CRUISE THE CREW OBSERVED INTERMITTENT REDUCTION GEAR BOX CHIP DETECTOR LIGHT. CREW DIVERTED, AN UNEVENTFUL LANDING WAS COMPLETED. THE TROUBLESHOOTING REVEALED PROPELLER GOVERNOR, CSU BEARING CAGE PIECES WERE FOUND ON CHIP DETECTOR POLES.Oct 30, 2015 · Beech B300 · Turbine Engine Reduction GearSDR CA151104007De-Ice Valve · malfunctioned(CAN) ON TAXI THE FLIGHT CREW HAD AN UN-COMMANDED L/H BRAKE DEICE ANNUNCIATION, BRAKE DEICE SWITCH WAS CYCLED WITH NO CHANGE. ON RETURN TO THE MAINTENANCE HANGAR IT WAS FOUND THE BRAKE DEICE VALVE P/N 101-381012-7 HAD FAILED IN THE ON POSITION WHILE SELECTED OOct 29, 2015 · Beech B300 · Ice/Rain Protection SystemSDR CA151030018Engine · power loss(CAN) THE CREW ABORTED TAKEOFF DUE TO POWER ROLLBACK ON THE NR 2 ENGINE. NO OTHER DETAILS ARE AVAILABLE AT THIS TIME. TROUBLESHOOTING IS ON-GOING.Oct 28, 2015 · Beech B300 · Engine (Turbine/Turboprop)SDR O2GA2015102782101Fcu · defectiveDURING TAKEOFF ROLL, ACFT BEGAN TO YAW & RT ENG POWER ROLLED BACK. TAKEOFF WAS ABORTED & ACFT EXITED THE RUNWAY SAFELY. TROUBLE SHOT THE DISCREPANCY TO A FAULTY RT ENG FUEL CONTROL UNIT. THE RT ENG FUEL CONTROL UNIT WAS REPLACED & A SUCCESSFUL OPERATIONAL COct 27, 2015 · N821UP · Beech B300 · Fuel Control/Turbine EnginesSDR CA151016007O-Ring · leaking(CAN) LOSS OF BRAKE POWER DURING TAXI. FOUND BRAKE ASSY PISTON ORING LEAKING. BRAKE WEAR WAS IN GOOD CONDITION, PAD WEAR. BRAKE ASSY NR 1 AND NR 2 REPLACED NR 1 BRAKE ASSY, PN 101-380096-1, 2 BRAKE ASSY, PN 101-380096-1.Oct 14, 2015 · Beech B300 · Landing Gear Brake SystemSDR O2GA2015092584101Structure · missingDURING SCHEDULED INSPECTION LT TRAILING UPPER WING SKIN, UNDER WING LOCKER, CRACKED & FLAP COVE MISSING SECTION. REPAIRED IAW SRM & FAA 337 FORM.Sep 21, 2015 · N841UP · Beech B300 · Trailing Edge FlapsSDR O2GA2015092583701Flap · crackedDURING PREFLIGHT FOUND TWO CRACKS ON RT WING INBD TE FLAP UNDERNEATH WING LOCKER, REPLACED FLAP. ACFT WAS RETURNED TO SERVICE.Sep 19, 2015 · N837UP · Beech B300 · Trailing Edge FlapsSDR MNGR09072015Skin · crackedDURING ROUTINE INSPECTION, IT WAS NOTED THAT THERE WERE SOME RIVET HEADS MISSING AND SOME SKIN CRACKS AT BS 179.52 BETWEEN STR 15L AND 15R. A DETAILED REPORT WAS SENT TO MFG REPAIR DESIGN OFFICE FOR EVALUATION. MFG RDO DETERMINED THAT A DETAILED STRUCTURAL RESep 17, 2015 · N42ED · Beech B300 · Fuselage Main, Plate/SkinSDR O2GA2015091480701Brake Sys · contaminatedDURING TAXI RT BRAKE PEDAL WENT TO FLOOR & LT BRAKE PEDAL FELT SPONGY. BLED BRAKE SYS, RAN ENGS & PERFORMED TAXI CHECK WITH NO DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Sep 13, 2015 · N807UP · Beech B300 · Landing Gear Brake System
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