Textron 208B

Service difficulty reports · 1,669

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 = '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 MTNA201801110003HBulkhead · buckledBUCKLED BULKHEADS AT LOWER LEFT CENTER BS 237.5Jan 11, 2018 · N874FE · Cessna 208B · Fuselage Main, BulkheadSDR MTNA201801110002HTorque Tube · corrodedCORROSION FOUND IN THE ELEVATOR CONTROL COLUMN TORQUE TUBE.Jan 11, 2018 · N874FE · Cessna 208B · Control Column SectionSDR 2017F00207Coupler · corrodedUPON APPROACH ON FINAL TO LAND, PILOT NOTICED THE AIRCRAFT WAS APPROXIMATELY 1 MILE EAST OF THE RUNWAY. PILOT PERFORMED A MISSED APPROACH, NOTIFIED TOWER OF THE MISSED APPROACH AND THEN LOADED THE GPS APPROACH. THE PILOT EXECUTED THE GPS APPROACH AND LANDED WDec 19, 2017 · N3910F · Cessna 208B · Navigation System WiringSDR 2017FA0000640Flapper Valve · crackedTHE HEATER FOR THE PASSENGERS WAS NOT WORKING. FOUND FLAPPER VALVE CRACKED IN HALF AT THE PASSENGER/COCKPIT DUCT.Dec 7, 2017 · N404BA · Cessna 208B · Heating SystemSDR 2018F00045Cowling · crackedTHE RH LOWER COWLING IS CRACKING WHERE THE EXHAUST HANGER IS ATTACHED. WE HAVE SEEN WHERE THE COWLING HAS A "PUCKER" IN THAT LOCATION AFTER THE FASTENERS ARE INSTALLED. WHERE THAT "PUCKER" IS IS WHERE THE EXHAUST HANGER IS LOCATED. WE HAVE ALSO SEEN ON AT LESDec 6, 2017 · N404BA · Cessna 208B · Powerplant SystemSDR FXTA2017120600204Rib · crackedTHE RIB IN THE LT HORIZONTAL IS CRACKING AT SS 80.60 THE RIB CRACKS AT THE LAST RIVET AFT OF THE WHERE THE LATERAL STRINGER RUNS THROUGH THE RIB. THIS IS THE SECOND ONE THAT HAS CRACKED. THIS RIB CRACKED ON THE TOP AND BOTTOM OF THE RIB ALONG WITH THE UPPER SKDec 6, 2017 · N404BA · Cessna 208B · Horizontal Stabilizer, Spar/RibSDR COEA2017112701895Skin · corrodedWHILE PERFORMING A SCHEDULED PHASE INSPECTION, FOUND MODERATE CORROSION ON LOWER FUSELAGE BELLY SKIN JUST OUTBOARD OF THE FUEL RESERVOIR TANK. REPAIRED THE LOWER FUSELAGE BELLY SKIN IAW MM D2078, REV 33, AND AC4313-1B.Nov 27, 2017 · N895FE · Cessna 208B · Fuselage Main, Plate/SkinSDR 2017F00201Pin · looseBRAKE CALIPER ANCHOR PIN LOOSE IN CALIPER HOUSING. IF ANCHOR PIN FAILS CALIPER WILL CAUSE MAIN WHEEL TO LOCK UP, CAUSING A VERY UNSAFE CONDITION FOR LANDING.Nov 25, 2017 · N848BA · Cessna 208B · BrakeSDR FXTA20210505006Pressure Switch · failedLOW FUEL PRESSURE LIGHT CAME ON DURING START-UP. SENSOR ON ENGINE HAD FAILEDNov 7, 2017 · N867BA · Cessna 208B · Fuel Pressure IndicatorSDR 2017FA0000630Threshold · corrodedDURING A PHASE INSPECTION THE TECHNICIAN FOUND THAT THE INSIDE OF THE THRESHOLD COVER WAS SEVERELY CORRODED DUE TO WEATHER.Nov 6, 2017 · N9956B · Cessna 208B · Fuselage Miscellaneous StructureSDR 2017FA0000631Bolt · corrodedFOUND RT HAND FWD HORIZONTAL ATTACH BOLT CORRODED WHILE PERFORMING MARTINAIRE FLEET CAMPAIGN DIRECTIVE FCD-170301 HORIZONTAL STABILIZER MOUNT BOLTS REPLACEMENT INSPECTION. REPLACING WITH NEW BOLT AND COATING WITH COR-BAN 27L BM53-36B CORROSION INHIBITING COMPOct 26, 2017 · N9956B · Cessna 208B · Horizontal Stabilizer StructureSDR FXTA2017120600624Rib · crackedTHE RIB IN THE LT HORIZONTAL STABILIZER AT SS 80.60 CRACKED ON THE UPPER SIDE OF THE RIB WHERE THE LATERAL STRINGER GOES THROUGH THE RIB. I HAVE PICTURES THAT CAN BE SENT TO HELP SHOW THIS ISSUE.Oct 26, 2017 · N679BA · Cessna 208B · Horizontal Stabilizer, Spar/RibSDR EPUA20171024001Unknown · odorDURING FLIGHT PILOT REPORTS "BURNING ODOR IN CABIN" MAINTENANCE INSPECTED ENGINE AND AIRFRAME FOR SOURCE OF SMELL AND NO CONCLUSIVE CAUSE COULD BE FOUND. IT IS SUSPECTED THAT DEICE FLUID MAY HAVE BEEN THE SOURCE OF SMELL. AN ENGINE COMPRESSOR TURBINE WASH WOct 24, 2017 · N409GV · Cessna 208B · Air Distribution SystemSDR COEA2017101401876Cable · out of adjustELEVATOR TRIM WHEEL WOULD NOT OPERATE IN FLIGHT. AIRCRAFT RETURNED TO DEPARTURE, NO EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE RIGHT TRIM ACTUATOR CABLE. OPS CHECKED GOOD.Oct 14, 2017 · N876FE · Cessna 208B · Elevator Tab Control SystemSDR FXTA2017101300001Pin · failedANCHOR PIN IN THE LT BRAKE CALIPER FAILED, CAUSING THE CALIPER TO ROTATE INTO MAIN TIRE LOCKING TIRE AND DAMAGING THE TREAD, WHEEL BOLTS, BRAKE ROTOR AN CALIPER.Oct 13, 2017 · N241BA · Cessna 208B · Landing Gear Brake SystemSDR 2017F00194Bolt · shearedTWO AN5-40A BOLTS SHEARED UPON LANDING. TORQUES WASH VERIFIED TO BE CORRECT AND WHEN WHEEL WAS BUILT UP TORQUE SEAL WAS USED. THREADED PORTION OF THE BOLT SHEARED CLEAN THIS IS THE SECOND AIRCRAFT IN THE FLEET TO HAVE THIS ISSUE. WHEEL WAS REMOVED AND A NEW WHOct 11, 2017 · N9820F · Cessna 208B · Wheel/Ski/FloatSDR EPUA2017101117001Boot · shortedPILOT REPORTED THAT AN ELECTRIC PROPELLER DEICE BOOT FAILED DURING FLIGHT. VISUAL INDICATIONS OF A BRIGHT ORB EMANATING FROM DEICE BOOT ARC AREA WAS PROFOUND ENOUGH FOR THE PILOT TO DECLARE AN EMERGENCY AND RETURN TO LAND AS SOON AS POSSIBLE. MAINTENANCE DETOct 11, 2017 · N405GV · Cessna 208B · Propeller/Rotor Anti-Ice/De-Ice SystemSDR COEA2017092801983Indicator · failed20 MINUTES AFTER DEPARTURE, THE NG INDICATION DROPPED TO 20 PERCENT AT FULL POWER. ALL OTHER ENGINE PARAMETERS WERE NORMAL. THE PILOT DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NG INDICATOR. OPS CHECKED GOOD. AIRCRAFT RETURNSep 28, 2017 · N983FE · Cessna 208B · Engine Integrated Instrument SystemSDR EPUA20170926001Fire Warning · false activationFIRE ALARM ACTIVATED WITH AUDIBLE PORTION ONLY , (NO LIGHT ILLUMINATED ON INSTRUMENT PANEL). FIRE DETECT WARNING HORN DEFERRED. NO FURTHER INFORMATION AVAILABLE AT THIS TIME.Sep 24, 2017 · N411GV · Cessna 208B · Fire DetectionSDR HSYA201709200001Gauge · failedMIDWAY THROUGH FLIGHT, ON THE EMPTY STAGE LEG, THE PILOT NOTICED OIL APPEARING IN THE OIL PRESSURE GAUGE. ALL ENGINE INDICATIONS WERE NORMAL THE FLIGHT CONTINUED TO DESTINATION, WHEN THE STAGE FLIGHT GOT CLOSER TO THE AIRPORT, THE PILOT SAW THAT OIL HAD FISep 19, 2017 · N904FE · Cessna 208B · Engine Oil Indicating SystemSDR EPUA201708220001Bolt · brokenMAIN LANDING GEAR BRAKE CALIPER WAS NOTED AS BEING BROKEN. MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THE RT BRAKE ASSEMBLY GUIDE BOLT HAD BROKEN.Aug 20, 2017 · N405GV · Cessna 208B · Landing Gear Brake SystemSDR 2017F00189Friction Lock · failedTHE PILOT WILL LOOSEN THE FRICTION KNOB ON THE ENGINE CONTROL QUADRANT AND THE LITTLE PIECES THAT LOCK AROUND THE CONDITION LEVER GET COCKED AND JAMMED. SO THE PILOT WILL THEN SCREW THE FICTION KNOB OUT EVEN FURTHER UNTIL IT IS COMPLETELY UNSCREWED THE FLAP LEAug 14, 2017 · N573BA · Cessna 208B · Engine ControlsSDR EPUA20170807001Bolt · brokenDURING AIRCRAFT GROUND OPERATIONS, IT WAS NOTED THAT THE LEFT WHEEL BRAKE CALIPER WAS DISCOVERED BROKEN. MAINTENANCE INSPECTED THE DEFECT AND NOTED THAT THE LEFT MAIN LANDING GEAR BRAKE CALIPER ANCHOR BOLT BROKEN. REPLACED THE BRAKE ASSEMBLY, TORQUE PLATE, AAug 7, 2017 · N750RV · Cessna 208B · Landing Gear Brake SystemSDR EPUA20170803001Bolt · brokenPILOT REPORTED THAT THE LEFT MAIN BRAKE IS INOPERATIVE. MAINTENANCE INSPECTED THE BRAKE ASSEMBLY AND NOTED THAT A BRAKE ASSEMBLY GUIDE PIN BOLT HAD BROKEN AND CAUSED THE BRAKE ASSEMBLY TO BECOME INEFFECTIVE. REPLACED THE LEFT BRAKE ASSEMBLY, TORQUE PLATE, TIAug 3, 2017 · N717PA · Cessna 208B · Landing Gear Brake SystemSDR MUIA20170802001Pump · unknownCREW REPORTED ABNORMAL ENGINE INDICATIONS. REPLACED ENGINE DRIVEN FUEL PUMP AND FCU.Aug 2, 2017 · N732MD · Cessna 208B · Engine Fuel PumpSDR 2017FA0000580Mount Bolt · corrodedWHILE PERFORMING A FLEET CAMPAIGN DIRECTIVE, CREATED TO INSPECT THE HORIZONTAL STABILIZER MOUNT BOLTS, IT WAS FOUND THAT ALL OF THEM WERE CORRODED.Jul 21, 2017 · N9761B · Cessna 208B · Horizontal Stabilizer, Attach FittingsSDR 2017FA0000581Mount Bolt · corrodedWHILE PERFORMING A FLEET CAMPAIGN DIRECTIVE, CREATED TO INSPECT THE HORIZONTAL STABILIZER MOUNT BOLTS, IT WAS FOUND THAT ALL FOUR OF THEM WERE CORRODED.Jul 21, 2017 · N9762B · Cessna 208B · Horizontal Stabilizer, Attach FittingsSDR 2017FA0000572Mount Bolt · corrodedWHILE PERFORMING A FLEET CAMPAIGN DIRECTIVE CREATED TO INSPECT THE HORIZONTAL STABILIZER MOUNT BOLTS, IT WAS FOUND THAT ALL FOUR OF THEM WERE CORRODED.Jul 21, 2017 · N9760B · Cessna 208B · Horizontal Stabilizer, Attach FittingsSDR 2017FA0000571Mount Bolt · corrodedWHILE PERFORMING A FLEET CAMPAIGN DIRECTIVE CREATED TO INSPECT THE HORIZONTAL STABILIZER MOUNT BOLTS, IT WAS FOUND THAT ALL FOUR OF THEM WERE CORRODED.Jul 21, 2017 · N9714B · Cessna 208B · Horizontal Stabilizer, Attach FittingsSDR 2017FA0000570Mount Bolt · corrodedWHILE PERFORMING A FLEET CAMPAIGN DIRECTIVE CREATED TO INSPECT THE HORIZONTAL STABILIZER MOUNT BOLTS, IT WAS FOUND THAT ALL OF THEM WERE CORRODED.Jul 21, 2017 · N9594B · Cessna 208B · Horizontal Stabilizer, Attach FittingsSDR 2017FA0000569Mount Bolt · corrodedWHILE PERFORMING A FLEET CAMPAIGN DIRECTIVE CREATED TO INSPECT THE HORIZONTAL STABILIZER MOUNT BOLTS, IT WAS FOUND THAT ALL FOUR OF THEM WERE CORRODED.Jul 21, 2017 · N9505B · Cessna 208B · Horizontal Stabilizer, Attach FittingsSDR 2017FA0000568Mount Bolt · corrodedWHILE PERFORMING A FLEET CAMPAIGN DIRECTIVE CREATED TO INSPECT THE HORIZONTAL STABILIZER MOUNT BOLTS, IT WAS FOUND THAT ALL FOUR OF THEM WERE CORRODED.Jul 21, 2017 · N4687B · Cessna 208B · Horizontal Stabilizer, Attach FittingsSDR 2017FA0000567Mount Bolt · corrodedWHILE PERFORMING A FLEET CAMPAIGN DIRECTIVE CREATED TO INSPECT THE HORIZONTAL STABILIZER MOUNT BOLTS, IT WAS FOUND THAT ALL FOUR OF THEM WERE CORRODED.Jul 21, 2017 · N4662B · Cessna 208B · Horizontal Stabilizer, Attach FittingsSDR 2017FA0000566Mount Bolt · corrodedWHILE PERFORMING A FLEET DIRECTIVE CREATED TO INSPECT THE HORIZONTAL STABILIZER MOUNT BOLTS, IT WAS FOUND THAT ALL FOUR OF THEM WERE CORRODED.Jul 21, 2017 · N4591B · Cessna 208B · Horizontal Stabilizer, Attach FittingsSDR 2017FA0000562Mount Bolt · corrodedWHILE PERFORMING A FLEET CAMPAIGN DIRECTIVE CREATED TO INSPECT THE HORIZONTAL STABILIZER MOUNT BOLTS, IT WAS FOUND THAT ALL FOUR OF THEM WERE CORRODED.Jul 21, 2017 · N1119V · Cessna 208B · Horizontal Stabilizer, Attach FittingsSDR 2017FA0000561Mount Bolt · corrodedWHILE PERFORMING A FLEET CAMPAIGN DIRECTIVE CREATED TO INSPECT THE HORIZONTAL STABILIZER MOUNT BOLTS, IT WAS FOUND THAT ALL FOUR OF THEM WERE CORRODED.Jul 21, 2017 · N1116N · Cessna 208B · Horizontal Stabilizer, Attach FittingsSDR 2017FA0000560Mount Bolt · corrodedWHILE PERFORMING A FLEET CAMPAIGN DIRECTIVE CREATED TO INSPECT THE HORIZONTAL STABILIZER MOUNT BOLTS, IT WAS FOUND THAT ALL FOUR OF THEM WERE CORRODED.Jul 21, 2017 · N1037N · Cessna 208B · Horizontal Stabilizer, Attach FittingsSDR 2017FA0000559Bolt · corrodedWHILE PERFORMING A FLEET CAMPAIGN DIRECTIVE CREATED TO INSPECT THE HORIZONTAL STABILIZER MOUNT BOLTS, IT WAS FOUND THAT ALL FOUR OF THEM WERE CORRODED.Jul 21, 2017 · N1031P · Cessna 208B · Elevator Tab, Attach FittingsSDR 2017FA0000558Mount Bolt · corrodedWHILE PERFORMING A FLEET CAMPAIGN DIRECTIVE CREATED TO INSPECT THE HORIZONTAL STABILIZER MOUNT BOLTS, IT WAS FOUND THAT ALL FOUR OF THEM WERE CORRODED.Jul 21, 2017 · N802AA · Cessna 208B · Horizontal Stabilizer, Attach FittingsSDR 2017FA0000557Mount Bolt · corrodedWHILE PERFORMING A FLEET CAMPAIGN DIRECTIVE CREATED TO INSPECT THE HORIZONTAL STABILIZER MOUNT BOLTS, IT WAS FOUND THAT ALL FOUR OF THEM WERE CORRODED.Jul 21, 2017 · N208TF · Cessna 208B · Horizontal Stabilizer, Attach FittingsSDR 2017FA0000556Mount Bolt · corrodedWHILE PERFORMING A FLEET CAMPAIGN DIRECTIVE CREATED TO INSPECT THE HORIZONTAL STABILIZER MOUNT BOLTS, IT WAS FOUND THAT ALL FOUR OF THEM WERE CORRODED.Jul 21, 2017 · N162SA · Cessna 208B · Horizontal Stabilizer, Attach FittingsSDR 2017FA0000555Mount Bolt · corrodedWHILE PERFORMING A FLEET CAMPAIGN DIRECTIVE CREATED TO INSPECT THE HORIZONTAL STABILIZER MOUNT BOLTS, IT WAS FOUND THAT ALL OF THEM WERE CORRODED.Jul 21, 2017 · N78SA · Cessna 208B · Horizontal Stabilizer, Attach FittingsSDR 2017FA0000554Mount Bolt · corrodedWHILE PERFORMING FLEET CAMPAIGN DIRECTIVE CREATED TO INSPECT THE HORIZONTAL STABILIZER MOUNT BOLTS, IT WAS FOUND THAT ALL FOUR OF THEM WERE CORRODED.Jul 21, 2017 · N208N · Cessna 208B · Horizontal Stabilizer, Attach FittingsSDR 2017FA0000553Mount Bolt · corrodedDURING A SCHEDULED INSPECTION IT WAS FOUND THAT ONE OF THE HORIZONTAL STABILIZER MOUNT BOLTS HAD BEEN SHEERED IN HALF. CLOSER INSPECTION FOUND THE BOLT WAS SEVERELY CORRODED. THE OTHER THREE MOUNT BOLTS WERE REMOVED AND EXAMINED, ALL WERE CORRODED. A FLEET Jul 21, 2017 · N9594B · Cessna 208B · Horizontal Stabilizer, Attach FittingsSDR JDWA20170720001Clamp · deterioratedFIRE LOOP SHIFTED POSITION DUE TO A LOOSE CLAMP AND TOUCHED THE BURNER CAN. INSTALLED A NEW CLAMP AND MOVED ELEMENT AWAY FROM BURNER CAN. OPERATED NORMAL.Jul 18, 2017 · N864SF · Cessna 208B · Fire DetectionSDR EPUA20170718001Rivet · looseTHE RIGHT ELEVATOR HAS SMOKING RIVETS ON THE INBOARD BUTT RIB WHERE THE TORQUE TUBE ATTACHES. VISUAL INSPECTION INDICATES THAT ALL OF THE ATTACH RIVETS EXCEPT FOR THREE ARE SMOKING. THE LEFT ELEVATOR LOOKS CONSIDERABLY BETTER THAN THE RIGHT SIDE BUT ONE RIVEJul 18, 2017 · N750RV · Cessna 208B · Elevator StructureSDR COEA2017071401953Wire Harness · damagedDURING TAKEOFF ROLL, THE PROPELLER INDICATOR GAUGE EXCEEDED THE RED LINE AND FLUCTUATED. THE PILOT RETURNED THE AIRCRAFT TO PHX RAMP. NO EMERGENCY DECLARED. MAINTENANCE TROUBLESHOT AND FOUND DAMAGED WIRING AT THE NP TACH GENERATOR. MAINTENANCE REPAIRED THE Jul 14, 2017 · N953FE · Cessna 208B · Propeller/Propulsor System WiringSDR COEA2017070502873Nut · damagedAFTER TAKEOFF, THE ITT GAUGE BEGAN TO FLUCTUATE RAPIDLY. PILOT ELECTED TO RETURN TO DEPARTURE, NO EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE T5 TERMINAL BLOCK NUT. GROUND RUN UP AND OPS CHECKED GOOD. AIRCRAFT RETURNED TOJul 5, 2017 · N873FE · Cessna 208B · Engine Indicating System WiringSDR 2017F00100Torque Tube · looseON A NON ROUTINE INSPECTION FOUND THE LEFT AND RIGHT ELEVATOR CONTROL TORQUE TUBES LOOSE WHERE IT ATTACHES TO THE ELEVATOR. THE RIVETS HAD BEEN WORKING IN THE FLANGE THAT ATTACHES THE TORQUE TUBE TO THE ELEVATOR AT THE BUTT RIB INBOARD AND THE SPAR ATTACHMENT Jun 26, 2017 · N848BA · Cessna 208B · Elevator Control SystemSDR COEA2017060101700Skin · chafedDURING SCHEDULED MAINTENANCE INSPECTION, DISCOVERED LOWER RT WING STRUT CUFF, CHAFED AT THE FUSELAGE SKIN FROM CONTACT WITH LIFT STRUT FAIRING. PERFORMED REPAIRS IAW SRM 51-75-00.Jun 1, 2017 · N700FX · Cessna 208B · Fuselage Main, Plate/Skin
Back to Textron 208B