Textron 208B

Service difficulty reports · 1,669

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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 = '208B'
  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 CA071221007Turbine Blades · distressed(CAN) OPERATOR REPORTED (TECHNICAL PROBLEMS) WHICH RESULTED IN A FORCED LANDING ON A PUBLIC MOTORWAY. INITIAL INVESTIGATION REVEALED COMPRESSOR TURBINE BLADE DISTRESS. THE ENGINE IN BEING RETURNED TO MFG FOR INVESTIGATION. UPDATES WILL BE PROVIDED WHEN AVAILABDec 2, 2007 · Cessna 208B · Turbine SectionSDR COEA0701850Connector · looseAIR TURN BACK, FLT 8673 PDX-MFR - DURING TAKEOFF, THE HORIZONTAL SITUATION INDICATOR FLAGGED. PILOT COULD NOT RESET. PILOT ELECTED TO RETURN TO PDX. AIRCRAFT LANDED SAFELY. RECONNECTED LOOSE CONNECTOR TO HSI UNIT. (M)Nov 30, 2007 · N850FE · Cessna 208B · Navigation System WiringSDR CA071212028Tire · flat(CAN) TIRE WENT FLAT. (TC NR 20071212028)Nov 28, 2007 · Cessna 208B · TireSDR CA071121001Bushing · worn(CAN) THE PILOTS FELT A VIBRATION ON CLIMB. THEY REDUCED THE POWER BUT THE VIBRATION REMAINED. THEY RETURNED TO THE AIRPORT WHERE THE AME INSPECTED THE ENGINE AND PROPELLER. NO DISCREPANCIES WERE NOTED ON THE ENGINE. ONE BLADE OF THE PROP WAS ABLE TO BE TWISTENov 18, 2007 · Cessna 208B · Propeller Blade SectionSDR CA071128013Fuel Control · failed(CAN) ENGINE POWER LOSS AND SUBSEQUENT INFLIGHT SHUTDOWN REPORTED. MFG IS ATTEMPTING TO RECOVER THE FUEL CONTROL UNIT FOR INVESTIGATION AND WILL ADVISE. (TC NR 20071128013)Nov 9, 2007 · Cessna 208B · Fuel Control/Turbine EnginesSDR CA071113003Engine · power loss(CAN) SHORTLY AFTER TAKEOFF WHILE PERFORMING A LOW LEVEL TURN, THE ENGINE REPORTEDLY LOST POWER. EMERGENCY POWER LEVER WAS ACTIVATED WITH NO RESPONSE. AIRCRAFT LANDED ON A STREET, NO FATALITIES. INITIAL INVESTIGATION REVEALED NO EVIDENCE OF PRE-IMPACT ANOMALIENov 6, 2007 · Cessna 208B · Engine (Turbine/Turboprop)SDR 2007FA0000981Relief Valve · separatedRELIEF VALVE FOR BLEED AIR PNEUMATIC SYSTEM END WASHER AND CAP SEPARATED FROM VALVE AND LAYING IN BOTTOM OF COWLING. SUSPECT RIVET HOLDING PARTS ON IS TOO SOFT. THIS IS THE THIRD VALVE TO FAIL LIKE THIS ON DIFFERENT AIRCRAFT IN THE LAST MONTH. AND ALL WERE NNov 3, 2007 · N1232Y · Cessna 208B · Vacuum Distribution SystemSDR CA071102002Switch · overheated(CAN) SHORTLY AFTER DEPARTURE THE PILOT BECAME AWARE OF A BURNING ODOR. HE NOTICED THAT THE AVIONICS 2 SWITCH WAS HOT TO TOUCH. THE PILOT RETURNED TO BASE. INVESTIGATION FOUND THAT THE AVIONICS 2 SWITCH HAD OVERHEATED TO THE POINT OF FAILURE. A NEW SWITCH P/N Oct 31, 2007 · Cessna 208B · Electrical Power System WiringSDR COEA0701788Engine · low pressureENROUTE- PILOT NOTICED OIL PRESSURE LOSS. PILOT SECURED THE ENGINE AND COMPLETED EMERGENCY CHECK LIST. EMERGENCY CREWS WERE CALLED. AIRCRAFT LANDED IN EUG WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED ENGINE. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SOct 24, 2007 · N788FE · Cessna 208B · Turbine Engine Oil SystemSDR CA071109007Gear · broken(CAN) THE PILOT WAS ON DECENT AND WENT TO SELECT FLAPS AND THE CIRCUIT BREAKER POPPED AFTER THE FLAPS WERE AT ABOUT 10 DEGREES. HE THEN LANDED THE AIRCRAFT NORMALLY. MAINTENANCE FOUND THE FLAP TRANSMISSION TO BE MAKING NOISE OUT OF THE NORM. THE INTERNAL GEAR Oct 13, 2007 · Cessna 208B · Trailing Edge Flap Control SystemSDR CA071016010Engine · power loss(CAN) FOLLOWING TAKEOFF THE ENGINE LOST POWER. THE AIRCRAFT WAS DAMAGED IN THE RESULTING FORCED LANDING.Sep 11, 2007 · Cessna 208B · Engine (Turbine/Turboprop)SDR 2007FA0000856Receiver · smokeSHORTLY AFTER TAKEOFF FROM ISP THE PILOT NOTICED SMOKE IN THE COCKPIT. THE PILOT IMMEDIATELY RETURNED TO DEPARTURE AND LANDED. THE PILOT REPORTED THAT THE SMOKE APPEARED TO BE CAUSED BY AN ELECTRICAL PROBLEM. THE PILOT REPORTED THAT THE GPS NO LONGER OPERATSep 11, 2007 · N24MG · Cessna 208B · Global Positioning SystemSDR CA071016003Engine · power loss(CAN) IN CRUISE, THE ENGINE EMITTED A NOISE ACCOMPANIED BY VIBRATION AND A COMPLETE LOSS OF POWER. THE AIRCRAFT CRASHED DURING FORCED LANDING. WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20071016003)Sep 5, 2007 · Cessna 208B · Engine (Turbine/Turboprop)SDR EPUA092007ASkin · crackedDURING ROUTINE INSPECTION, DISCOVERED 4" CRACK ON UPPER RT AFT WING SKIN 18" FROM WING ROOT AT WS 53.00. DAMAGE WAS REPAIRED IAW CESNNA MM 51-75-00. AIRCRAFT WAS RETURNED TO SERVICE.Sep 5, 2007 · N407GV · Cessna 208B · Wing, Plate/SkinSDR CA071016011Engine · power loss(CAN) THE ENGINE LOST POWER FOLLOWING TAKEOFF AND THE AIRCRAFT WAS DAMAGED IN THE RESULTING FORCED LANDING.Aug 31, 2007 · Cessna 208B · Engine (Turbine/Turboprop)SDR COEA0701897Button · looseJUST AFTER TAKEOFF, ON FLIGHT NR 7797 THE PILOT RECEIVED A FIRE WARNING. HE DECLARED AND EMERGECY AND RETURNED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE DISCOVERED THE FIRE WARNING TEST BUTTON HAD FALLEN OFF CAUSING A FALSE WARNING. MAINTENANCE REINSTJul 23, 2007 · N897FE · Cessna 208B · Detection SystemSDR CA070914014Engine · unknown(CAN) FOLLOWING TAKEOFF A LOUD NOISE WAS HEARD ACCOMPANIED BY AN UNCOMMANDED REDUCTION IN ENGINE POWER. A FORCED LANDING WAS CARRIED OUT RESULTING IN AIRFRAME DAMAGE. MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070914Jul 21, 2007 · Cessna 208B · Engine (Turbine/Turboprop)SDR MT92007F00000Tube · splitAIRCRAFT LANDED ON ITS SCHEDULED ROUTE, WHEN IT EXPERIENCED A FLAT TIRE ON ROLL OUT. THIS CAUSED THE CLOSURE OF THE ACTIVE RUNWAY. MAINTENANCE PERSONNEL REPLACED THE TIRE AND TOWED THE PLANE BACK TO THE RAMP. THE TIRE WAS DISASSEMBLED AND IT WAS FOUND THAT Jul 16, 2007 · N162SA · Cessna 208B · Tire TubeSDR COEA0702899Indicator · erraticAIR TURN BACK PDT: FUEL FLOW INDICATING ERRATIC ON CLIMB OUT. TORQUE ITT AND NG DID NOT FOLLOW FUEL FLOW CHANGES. AS A PERCAUTION PILOT ELECTED TO RETURN TO BASE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED FUEL FLOW INDICATOR. AIRJul 12, 2007 · N899FE · Cessna 208B · Engine Fuel Indicating SystemSDR CA070704004Brushes · worn(CAN) PILOT ATTEMPTED TO START AIRCRAFT. AIRCRAFT FAILED TO START. FURTHER INVESTIGATION REVEALED A STARTER BRUSH HAD FRACTURED AND SEPARATED INTO A FEW PIECES. DAMAGE TO THE COMMUNTATOR WAS FOUND. IT WAS APPROXIMATELY 240 HRS SINCE THE LAST BRUSH INSPECTION AJul 3, 2007 · Cessna 208B · Starter-GeneratorSDR CA070619001Actuator · binding(CAN) EXCESSIVE RESISTANCE IN ELEVATOR TRIM REPORTED. RT ELEVATOR TRIM ACTUATOR FOUND TO BE BINDING AND REPLACED WITH OVERHAULED UNIT. ACFT HAS FLOWN WITH NO REOCCURENCE OF THE DEFECT. THE SUBJECT ACTUATOR WAS OVERHAULED AND FITTED IAW THE MAINT SCHEDULE IN JUJun 17, 2007 · Cessna 208B · Elevator Tab Control SystemSDR CA070607006Hose · leaking(CAN) HOSE PN-AE366372460330 REPLACED DUE TO SHEDULED MAINTENANCE AND LEAK CHECKED SERVICEABLE, AFTER 1.4 HRS AND 4 CYCLES FOUND LEAKING DURING GROUND HANDLING. HOSE REPLACED AND LEAK CHECKED SERVICEABLE (TC NR 20070607006)Jun 6, 2007 · Cessna 208B · Standard Practices/StructuresSDR 2007FA0000573Pin · unserviceableON A ROUTINE INSPECTION, A MECHANIC FOUND THAT THE PILOTS RT RUDDER PEDAL PIN WAS ABOUT TO FALL OUT OF THE RUDDER PEDAL. FURTHER INSPECTION FOUND THAT THE ROLL PIN PN: NAS561C318 HAD FALLEN OUR OF ITS HOLE CAUSING THE RUDDER PEDAL PIN TO MIGRATE FROM ITS POSIJun 6, 2007 · N4365U · Cessna 208B · Rudder Control SystemSDR CA070530005Boot · worn(CAN) DE-ICE BOOT, FOUND WORN RUBBER THAT WAS MELTED FROM EXHAUST GASES. MINOR BLISTERING FOUND ON TOP RT OF BOOT. (TC NR 20070530005)May 20, 2007 · Cessna 208B · Airfoil Anti/De-ice SystemSDR CA070705004Engine · power loss(CAN) IN CRUISE FLIGHT, THE ENGINE EMITTED A LOUD NOISE AND LOST POWER, RESULTING IN A FORCED LANDING. MFG WILL MONITOR INVESTIGATION OF THE INCIDENT AND REPORT ROOT CAUSE ONCE DETERMINED. (TC NR 20070705004)May 19, 2007 · Cessna 208B · Engine (Turbine/Turboprop)SDR CA070507009Relief Valve · malfunctioned(CAN) IN CRUISE FLIGHT, OIL PRESSURE BEGAN TO FLUCTUATE FROM BOTTOM TO MIDDLE OF GREEN RANGE, 80 TO 90 PSI. FAULT CONFIRMED ON GROUND RUN, NOT RELATED TO INDICATION. CONSULTATION WITH ENGINE OVERHAULER, OIL PRV VALVE TO BE CHECKED. PARTS AT TOOLS DISPATCHED, May 3, 2007 · Cessna 208B · Engine Oil PressureSDR 26519ABushing · crackedVIBRATION REPORTED BY PILOT. OPERATOR WAS UNABLE TO DYNAMIC BALANCE. OPERATOR NOTICED ONE BLADE HAS ROTATIONAL PLAY. UPON DISASSEMBLY NR 2 BLADE LINK BUSHING P/N A4564 WAS FOUND CRACKED WITH PIECES MISSING. THE LINK P/N B4743 AND BLADE ACTUATING PIN P/N B5May 2, 2007 · N122JB · Cessna 208B · Propeller Blade SectionSDR AOD2007F00000Cylinder · leakingLT BRAKE CYLINDER LEAKING AT PISTON O-RING CAUSING LOS OF BRAKE PRESSURE AT THE LT BRAKE PEDAL. (K)Apr 24, 2007 · N910HL · Cessna 208B · Landing Gear Brake SystemSDR 2007FA0000355Exhaust Duct · crackedCRACKING OCCURRED IN A SHORT TIME SPAN, DURING NORMAL OPERATION. CRACKS WERE OVER AN AREA APPROX 7 INCHES X 7 INCHES. ONE PIECE APPROX 3 INCHES X 3 INCHES SEPARATED FROM THE PART. AFTER CRACKING, DEFORMATION OF LOWER TRAILING EDGE OCCURRED BECAUSE IT WAS NOApr 17, 2007 · N4365U · Cessna 208B · Engine Collector/Tailpipe/NozzleSDR HYT2007F00000Skin · damagedSMOKING RIVETS IN LEADING EDGE SKIN UPPER SEAM. EVERY COUNTERSUNK HOLE FROM WS 35 TO WS 141 WAS FRETTING AGAINST THE RIVET HEAD. SAME CONDITION TO SAME EXTENT ON BOTH WINGS. IT APPEARS THE SKIN WAS COUNTERSUNK TOO DEEPLY. SAME CONDITION TO LESSER EXTENT FOApr 1, 2007 · N900WA · Cessna 208B · Wing, Plate/SkinSDR 2007FA0000300Housing · defectiveTHE MAIN CASTING, WHICH HOUSES THE BRAKE CALIPER PISTONS LEAKS FLUID UNDER NORMAL BRAKING PRESSURE. THE LEAKS ARE FROM EXCESSIVE POROSITY IN THE CASTING. CASTING THIS IS THE SECOND OCCURRENCE IN OUR OPERATIONS. THE FIRST WAS NOT REPORTED. (K)Mar 27, 2007 · Cessna 208B · Landing Gear Brake SystemSDR CA070514028Turbine Blades · damaged(CAN) ON ENGINE SHUTDOWN FLAMES WERE SEEN EXITING THE EXHAUST. SUBSEQUENT INSPECTION REVEALED DAMAGED COMPRESSOR TURBINE BLADES. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070514028)Mar 22, 2007 · Cessna 208B · Turbine SectionSDR CA070320002Stud · loose(CAN) DURING FIRST FUEL NOZZLE INSPECTION FROM OVERHAUL -9 OF 28 FUEL NOZZLE STUDS WERE REMOVED WITH NUTS ON STUDS P/N 3038589. HAVE A CODE H19 STAMPED ON THE END -DURING A PHONE CONVERSATION WITH AN EMPLOYEE AT MFG, THEY INDICATED THAT OVERSIZED STUDS WERE PMar 17, 2007 · Cessna 208B · Fuel Injector NozzleSDR CA070514018Gearbox · making metal(CAN) DURING CRUISE THE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION ACCOMPANIED BY A NOISE AND SMOKE IN THE CABIN AIR. SUBSEQUENT INSPECTION REVEALED OIL AT THE ENGINE INLET AND METALLIC DEBRIS ON THE REDUCTION GEARBOX CHIP DETECTOR. MFG WILL MONITOR Mar 9, 2007 · Cessna 208B · Turbine Engine Reduction GearSDR AXS2007F00000Carbon Seal · damagedAIRCRAFT DEPARTED AS FLIGHT 81391 REPOSITIONING EMPTY UNDER FAR 91. 15 MINUTES INTO FLIGHT THE PIC NOTED OIL PRESSURE FLUCTUATIONS FOLLOWED BY DECREASING OIL PRESSURE. THE PIC DIVERTED AND ENROUTE NOTED TORQUE FLUCTUATIONS OF APPROXIMATELY 500 FT/LBS. THE PFeb 20, 2007 · N731FX · Cessna 208B · Turbine Engine Oil SystemSDR 2007FA0000084Tube · wornRT MAIN GEAR TIRE REPORTED LOW. REMOVED TIRE TO CHECK THE TUBE. THE TUBE APPEARED TO LOOK OLD AND CHECKED. TECHNICIAN REPLACED WITH NEW TUBE. 1 WEEK LATER TIRE REPORTED LOW AGAIN ON SAME POSITION. WE REMOVED THE TIRE AND INSPECTED THE TUBE. THE TUBE LEAKING ONJan 19, 2007 · N1293E · Cessna 208B · Tire TubeSDR 2007FA0000081Tube · damagedRIGHT MAIN GEAR TIRE REPORTED LOW. REMOVED TIRE TO CHECK THE TUBE. THE TUBE APPEARED TO LOOK OLD AND CHECKED. TECHNICIAN REPLACED WITH NEW TUBE. ONE WEEK LATER TIRE REPORTED LOW AGAIN ON SAME POSITION. REMOVED THE TIRE AND INSPECTED THE TUBE. THE TUBE LEJan 19, 2007 · N1293E · Cessna 208B · Tire TubeSDR CA070514057Blade · damaged(CAN) DURING DESCENT ENGINE OIL PRESSURE REDUCED ACCOMPANIED BY AN INCREASE IN INTER-TURBINE TEMPERATURE. ENGINE POWER WAS REDUCED AND A LANDING ACCOMPLISHED AT LOW POWER. SUBSEQUENT INSPECTION REVEALED COMPRESSOR TURBINE BLADE DAMAGE. MFG WILL MONITOR INVEJan 13, 2007 · Cessna 208B · Turbine Engine Compressor SectionSDR CA070105003Turbine Blades · fractured(CAN) THE ENGINE SUFFERED AN INFLIGHT SHUTDOWN IN CRUISE. SUBSEQUENT INSPECTION REVEALED THE AIRFRAME INLET AIR BOX PARTIALLY OPEN WITH A FASTENING PIN MISSING. THE ENGINE COMPRESSOR WAS FOUND STIFF TO ROTATE WITH DAMAGE EVIDENT TO THE SECOND STAGE STATOR ANDec 14, 2006 · Cessna 208B · Turbine SectionSDR BSYA200600032Engine · stoppedAIRCRAFT WAS EN ROUTE FROM BHM TO CPS FLYING AT 11,000 FEET WHEN THE ENGINE QUIT. PILOT FOUND A SMALL AIRPORT (61A) AND LANDED NO PROBLEMS WITH PILOT OR AIRCRAFT. CAUSE OF THE ENGINE FAILURE UNKNOWN AT THIS TIME.Dec 8, 2006 · N1115M · Cessna 208B · Engine (Turbine/Turboprop)SDR BSYA200600033Engine · failedAIRCRAFT WAS EN ROUTE FROM BHM TO CPS FLYING AT 11,000 FEET WHEN THE ENGINE QUIT. PILOT FOUND A SMALL AIRPORT (61A) AND LANDED NO PROBLEMS WITH PILOT OR AIRCRAFT. CAUSE OF THE ENGINE FAILURE UNKNOWN AT THIS TIME.Dec 8, 2006 · N1115M · Cessna 208B · Engine (Turbine/Turboprop)SDR BSYA200600031Engine · stoppedAIRCRAFT WAS EN ROUTE FROM BHM TO CPS FLYING AT 11,000 FEET WHEN THE ENGINE QUIT. PILOT FOUND A SMALL AIRPORT (61A) AND LANDED NO PROBLEMS WITH PILOT OR AIRCRAFT. CAUSE OF THE ENGINE FAILURE UNKNOWN AT THIS TIME.Dec 8, 2006 · N1115M · Cessna 208B · Engine (Turbine/Turboprop)SDR CA061102004Rudder · stiff(CAN) AIRCRAFT WAS BEING TAXIED TO THE RAMP FROM THE HANGER. THE PILOT NOTICED THAT THE RUDDER CONTROLS FELT STIFF. THE PILOT DECIDED TO RETURN TO THE HANGER AND ADVISE MAINTENANCE. THE AIRCRAFT IS BEING EXAMINED AT THIS TIME AND WILL UP-DATE THIS SDR WHEN A Nov 2, 2006 · Cessna 208B · Rudder Control SystemSDR CA061219012Engine · unknown(CAN) IN FLIGHT A LOUD NOISE WAS HEARD AND THE WINDSHIELD BECAME COVERED IN OIL. A FORCED LANDING FOLLOWED RESULTING IN AIRFRAME DAMAGE. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE DETERMINED.Oct 22, 2006 · Cessna 208B · Engine (Turbine/Turboprop)SDR SBAA200600001Cooling Fan · burned outUPON ARRIVAL, PILOT HAD AN ODOR OF BURNED WIRES IN THE COCKPIT. AVIONICS COOLING FAN CIRCUIT BREAKER WAS PULLED. REPLACED AVIONICS COOLING FAN, OPS CHECK NORMAL.Oct 11, 2006 · N986FE · Cessna 208B · Air Distribution FanSDR SBAA1106001Cooling Fan · burned outUPON ARRIVAL, PILOT HAD AN ODOR OF BURNED WIRES. AVIONICS COOLING FAN WAS FOUND TO BE INOP. INSTALLED NEW AVIONICS COOLING FAN. OPS CHECK NORMAL.Oct 11, 2006 · N986FE · Cessna 208B · Air Distribution FanSDR SBAA2124Cooling Fan · burned outUPON ARRIVAL INTO TVC PILOT HAD AN ODOR OF BURNED WIRES. AVIONICS COOLING FAN WAS FOUND TO BE INOP. INSTALLED NEW AVIONICS COOLING FAN. OPS CHECK NORMAL.Oct 11, 2006 · N986FE · Cessna 208B · Air Distribution FanSDR CA061010003Line · chafed(CAN) WIRE BUNDLE SECURED INCORRECTLY LEADING TO CHAFING ON/THRU PNEUMATIC DEICE AIR SUPPLY LINES. DURING THE INITIAL COMPLETION OF THE DEICE SYSTEM TEST AND SERVICE IT WAS FOUND THAT THE WIRING BUNDLE FOR THE DEICE SOLENOIDS AND PRESSURE SWITCHES HAD BEEN SECOct 10, 2006 · Cessna 208B · Windshield/Door Rain/Ice RemovalSDR CA061103010Fuel Control · faulty(CAN) ON TAKEOFF ENGINE POWER INCREASED UNCOMMANDED AND THE ENGINE WOULD NOT RESPOND TO THROTTLE INPUT. THE ENGINE WAS SHUTDOWN IN FLIGHT AND THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE DETERMINEDOct 7, 2006 · Cessna 208B · Fuel Control/Turbine EnginesSDR CA061103003Engine · overheated(CAN) DURING TAXI FOLLOWING LANDING THE ENGINE EXPERIENCED AN ITT OVER-TEMPERATURE. SUBSEQUENT INSPECTION REVEALED DEBRIS IN THE EXHAUST AND HEAT DISCOLORATION OF THE AIRCRAFT COWLING IN THE EXHAUST REGION. MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOSep 27, 2006 · Cessna 208B · Engine (Turbine/Turboprop)
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