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 COEA2011110402899Seat Track · corrodedINSP AT GEG - LEVEL 2 CORROSION: DURING INSPECTION, FOUND 3 CARGO AREA SEAT TRACKS CORRODED BEYOND SERVICEABLE LIMITS. DAMAGE IS MOSTLY FOUND BETWEEN FUSELAGE STATION 282 AND 332, HOWEVER, SOME DAMAGE DOES EXIST IN THE AREAS BETWEEN FUSELAGE STATION 166-332.Nov 4, 2011 · N899FE · Cessna 208B · Fuselage, Seat/Cargo Attach FittingsSDR COEA2011110201960Seat Track · corrodedINSP AT PDX - LEVEL 2 CORROSION: DURING INSPECTION, FOUND 5 CARGO AREA SEAT TRACKS CORRODED BEYOND SERVICEABLE LIMITS. DAMAGE IS MOSTLY FOUND BETWEEN FUSELAGE STATION 282 AND 332, HOWEVER, SOME DAMAGE DOES EXIST IN THE AREAS BETWEEN FUSELAGE STATION 166-332.Nov 2, 2011 · N960FE · Cessna 208B · Fuselage, Seat/Cargo Attach FittingsSDR PNSA111101AAnnunciator · smokeSMOKE COMING FROM TOP OF PANEL IMMEDIATELY BELOW GLARE SHIELD.Nov 2, 2011 · N9820F · Cessna 208B · Central WarningSDR COEA2011103101778Cargo Track · corrodedDURING INSPECTION, FOUND CARGO AREA SEAT TRACK CORRODED BEYOND SERVICEABLE LIMITS. DAMAGE IS MOSTLY FOUND BETWEEN FUSELAGE STATION 282 AND 332, SOME DAMAGE DOES EXIST IN THE AREAS BETWEEN FUSELAGE STATION 166-332. REMOVED AND REPLACED CARGO SEAT TRACK.Oct 31, 2011 · N788FE · Cessna 208B · Fuselage, Seat/Cargo Attach FittingsSDR FXGAN575JD001Deice System · malfunctionedPROP DE-ICE C/B TRIPPED, RESET AND IT TRIPPED AGAIN AS SOON AS PROP DE-ICE SWITCH WAS TURN ON, STRONG SMELL OF ELECTRICAL SMOKE FOR ABOUT 30 SEC.Oct 26, 2011 · N575JD · Cessna 208B · Propeller/Rotor Anti-Ice/De-Ice SystemSDR M36R20111026004Vernatherm · detachedWHILE IN CRUISE THE PILOT REPORTED ENGINE OIL INDICATORS SHOWING OIL PRESSURE LOWER AND TEMPERATURE HIGHER THAN NORMAL. LATER UPON REMOVAL AND INSPECTION OF THE ENGINE OIL COOLER VERNATHERM IT WAS NOTED THAT IT HAD STARTED TO COME APART DUE TO THE FAILURE OF Oct 26, 2011 · N1120W · Cessna 208B · Engine Oil Temperature RegulatorSDR AWHA102511Master Cylinder · failedDURING A RIGHT TURN ENTERING THE PARKING AREA AT THE RAMP, THE PILOT APPLIED RIGHT BRAKE AND RUDDER TO MAKE THE TURN. THE RIGHT BRAKE PEDAL WENT "FULL TRAVEL" WITH NO BRAKING EFFECT. HE MAINTAINED FULL RIGHT RUDDER AND FOLLOWED UP WITH 2 PUMPS OF THE RIGHT BOct 25, 2011 · N771FE · Cessna 208B · Master Cylinder/Brake ValveSDR AWHA101811Master Cylinder · malfunctionedTHE PILOT REPORTED WHILE TAXIING INTO THE SMF RAMP, EXPERIENCED A RIGHT BRAKE FAILURE. HE WAS AT NORMAL TAXI SPEED ENTERING THE RAMP WHEN HE ATTEMPTED TO APPLY SMOOTH RIGHT RUDDER AND BRAKE TO MAKE A RIGHT TURN. THE PEDAL WENT TO THE FLOOR AND THE AIRCRAFT DOct 18, 2011 · N771FE · Cessna 208B · Master Cylinder/Brake ValveSDR ENHA201110140001Tube · deflatedUPON LANDING, RT MLG TIRE WENT FLAT. PILOT WAS UNABLE TO TAXI THE ACFT CLEAR OF THE ACTIVE RUNWAY WITHOUT DOING DAMAGE TO THE ACFT, DUE TO DEFLATED TIRE. THIS RESULTED IN RUNWAY BEING CLOSED FOR A PERIOD OF 30 MINUTES. MX WAS SUMMONED TO THE ACFT AND THEY ROct 14, 2011 · N804TH · Cessna 208B · Tire TubeSDR AWHA101411Elbow · strippedTHE PILOT REPORTED AFTER NORMAL LANDING WITH NORMAL BRAKING HE FELT THE RIGHT BRAKE PEDAL GO TO THE FLOOR WITH NO BRAKING ACTION. AFTER SHUTDOWN NOTICED THE RIGHT BRAKE FITTING DISCONNECTED FROM THE BRAKE CALIPER. THEN CONTACTED MAINTENANCE WHO FOUND THE FITOct 14, 2011 · N790FE · Cessna 208B · BrakeSDR AWHA2011F00215Brake Assy · failedPILOT REPORTED AFTER NORMAL LANDING AND DURING TAXI THE RT BRAKE PEDAL WENT TO THE FLOOR WITH NO BRAKING ACTION. AFTER SHUTDOWN AND SECURING THE ACFT HE NOTICED THE RT BRAKE CALIPER LEAKING FLUID ON THE RAMP. ON FURTHER INVESTIGATION HE FOUND THE BRAKE LINE LOct 14, 2011 · N790FE · Cessna 208B · BrakeSDR ENHA2011F00213Tube · failedUPON LANDING, RT MLG TIRE WENT FLAT. PILOT WAS UNABLE TO TAXI THE ACFT CLEAR OF THE ACTIVE RUNWAY WITHOUT DOING DAMAGE TO THE ACFT, DUE TO DEFLATED TIRE. THIS RESULTED IN RUNWAY BEING CLOSED FOR A PERIOD OF 30 MINUTES. MX WAS SUMMONED TO THE ACFT AND THEY Oct 14, 2011 · N804TH · Cessna 208B · Tire TubeSDR CA111017009G Switch · failed(CAN) IN FLIGHT, THE PILOT NOTICED HIS ELT WAS GOING OFF. HE NOTIFIED FLIGHT SERVICE THAT HE WAS OK AND IT WAS A FALSE INDICATION. HE RESET THE ELT AND IT WENT OFF. IT THEN CAME BACK ON AFTER ABOUT 10 MINUTES. HE RESET THE ELT SEVERAL TIMES DURING THE FLIGHOct 11, 2011 · Cessna 208B · Emergency Locator BeaconSDR AWHA100611Master Cylinder · malfunctionedAFTER LANDING AT OAK TAXIED TO THE RAMP WITHOUT INCIDENT. AFTER THE UNLOAD, DURING FIRST MAJOR LT TURN AT TAXI SPEED, WHILE APPLYING STEADY LIGHT BRAKE PRESSURE TO THE LT BRAKE, THE BRAKE PEDAL SLOWLY BUT CONTINUOUSLY FADED ALL THE WAY TO THE FLOOR. IMMEDIATOct 6, 2011 · N985FE · Cessna 208B · Master Cylinder/Brake ValveSDR AWHA2011F00209Master Cylinder · failedDURING FIRST MAJOR LEFT TURN AT TAXI SPEED, WHILE APPLYING STEADY LIGHT BRAKE PRESSURE TO THE LT BRAKE, TO SHARPEN UP THE TURN, THE BRAKE PEDAL SLOWLY BUT CONTINUOSLY FADED ALL THE WAY TO THE FLOOR. IMMEDIATELY PUT THE POWER LEVER INTO BETA TO SLOW THE ACFT. Oct 6, 2011 · N985FE · Cessna 208B · Master Cylinder/Brake ValveSDR CA111024006Elt · dislodged(CAN) ELT FOUND DISLODGED FROM MOUNTING BASE AND HANGING FROM ANTENNA LEAD. THE REMOTE ACTIVATION SWITCH WIRING FOUND BROKEN. THE ELT WAS FOUND STILL FUNCTIONAL. THE ELT WAS SLID BACK INTO THE VELCRO MOINTING STRAP WHICH WAS FOUND LOOSE. COMPANY ISSUED A FOct 4, 2011 · Cessna 208B · Emergency Locator BeaconSDR CA110914003Elbow · fractured(CAN) DURING THE EARLY STAGES OF T/O ROLL, THE PROPELLER FEATHERED AND OIL COVERED THE WINDSHIELD. T/O WAS ABORTED AND THE PILOT SHUTDOWN ENGINE. THE ACFT WAS TOWED TO A LOCAL HANGER WHERE INITIAL INSPECTION FOUND A FRACTURED RGB OIL SCAVENGE ELBOW, A PARTIALLSep 10, 2011 · Cessna 208B · Turbine Engine Oil SystemSDR CA110829003Engine · malfunctioned(CAN) ON CLIMB OUT THROUGH 1000 FT AGL. A LOAD WOOF SOUND WAS HEARD BY THE CREW WITH AN INCREASE IN TORQUE INDICATION. THE CREW DECIDED TO SHUTDOWN THE ENGINE AND RETURN FOR LANDING. LANDING WAS UNEVENTFUL AND THE ACFT WAS TOWED TO THE HANGER. ENGINE WAS INAug 27, 2011 · Cessna 208B · Compressor Bleed ValveSDR HSYA2011082311Switch · defectivePILOT REPORTED THAT ENROUTE, THE NR 1 NAV RADIO TRIPPED OFF-LINE AND HE CONTINUED INTO CPR USING NR 2 NAV. AFTER LANDING PILOT STATED HEARD A POP AND SMELLED A BURNED ODOR - BUT WAS UNSURE IF THE ODOR WAS FROM FOREST FIRES IN THE AREA. STATED THAT THE NR 1 NAug 23, 2011 · N964FE · Cessna 208B · AC Power Distribution SystemSDR HSYA2011082211Master Cylinder · deterioratedPILOT TAXIED, AT HOLD SHORT LINE TO RUNWAY, THE LEFT BRAKE FAILED. PILOT APPLIED FULL RT BRAKE AND WAS ABLE TO REGAIN FULL LT BRAKE EFFECTIVENESS BY PUMPING THE BRAKE. ACFT RETURNED TO BLOCKS FOR TROUBLESHOOTING. MX TROUBLESHOT SYS TO LT BRAKE MASTER CYLINDEAug 22, 2011 · N903FE · Cessna 208B · Master Cylinder/Brake ValveSDR CA110818007Shaft · sheared(CAN) ON LANDING AND TAXIING TO MX BASE, PILOT APPLIED PRESSURE TO THE BRAKES, AND FOUND THAT THEY HAD FAILED. FOUND THAT THE SHAFT OF THE BRAKE MASTER CYLINDER HAD SHEARED. THERE WAS NO FURTHER INCIDENT. MX REPLACED THE MASTER CYLINDER AND THE ACFT WAS Aug 16, 2011 · Cessna 208B · Master Cylinder/Brake ValveSDR CA110815013Shaft · brokenWHEN THE PILOTS GOT INTO THE AFT, THEY PRESSED IN ON THE BRAKES TO RELEASE THE PARKING BRAKE, AND THE LT SIDE MASTER CYLINDER SHAFT SNAPPED. NO FURTHER INCIDENT WAS REPORTED. MX REPLACED THE MASTER CYLINDER. ACFT RETURNED TO SERVICE.Aug 12, 2011 · Cessna 208B · Master Cylinder/Brake ValveSDR 2011FA0000511Antenna · brokenANTENNA, PN 110-773 APPEARS TO BE BROKEN INTERNALLY. THE TOP PORTION OF THE ANTENNA, INCLUDING THE WIRE WHIP, CAN BE EASILY LIFTED OFF THE BASE. VISUAL INSP ALONE WILL NOT REVEAL THIS DISCONNECT. THIS ANTENNA IS PART OF THE ME406 ELT SYSTEM. THIS IS THE 4TH IAug 9, 2011 · N976E · Cessna 208B · Emergency Locator BeaconSDR 2011FA0000528Compressor Wheel · damagedALUMINUM, STANDARD, 470 RIVETS ATTATCHING THE GASKET ON THE INTAKE SHROUD HAVE CORRODED HEADS THAT SEPERATED AND WERE SUCKED INTO THE COMPRESSOR THROUGH THE SCREEN AND CAUSING DAMAGE TO FIRST STAGE COMPRESSOR WHEEL. COMPRESSOR WHEEL WAS REPAIRED.Aug 1, 2011 · N682AC · Cessna 208B · Turbine Engine Compressor SectionSDR CA110830006Engine · failed(CAN) DURING A PARACHUTING MISSION, THE PILOT REPORTED THAT THE ENGINE MADE A LOUD NOISE AND THE PROPELLER STOPPED SUDDENLY. THE ACFT WAS IN CLIMB PASSING 1,000 FT. THE PILOT ATTEMPTED A RELIGHT UNSUCCESSFULLY. AS THE ACFT WAS STILL IN RANGE OF THE AIRFIELD,Jul 29, 2011 · Cessna 208B · Engine (Turbine/Turboprop)SDR JDWA864SF001Actuator · malfunctionedELEVATOR TRIM STIFF.Jul 18, 2011 · N864SF · Cessna 208B · Elevator Tab Control SystemSDR 2011F00158Master Cylinder · malfunctionedPILOT REPORTED ON TAXI LT BRAKE PEDAL WENT TO THE FLOOR, SUBSEQUENT BRAKE ACTIONS THE BRAKES OPERATED NORMALLY. THE LT BRAKE MASTER CYLINDER WAS R & R AS A PRECAUTION. BLED BRAKES. OPS CHECK GOOD. TAXI AND STEERING CHECKS GOOD.Jun 30, 2011 · N984FE · Cessna 208B · Master Cylinder/Brake ValveSDR BSYA2011025Indicator · failedPILOT'S ATTITUDE INDICATOR FAILED SHORTLY AFTER DEPARTING LUK, DIVERTED TO LCK. MAINTENANCE REMOVED AND REPLACED ATTITUDE INDICATOR, OPS CHECKED GOOD.Jun 28, 2011 · N3RY · Cessna 208B · Integrated Flight SystemSDR HSYA2011060411Brake Sys · malfunctionedDURING TAXI OUT, CAPTAIN REPORTED THAT THE BRAKES FAILED. CAPTAIN ATTEMPTED PUMPING BRAKES & RECEIVED PARTIAL BRAKING ON THE LT SIDE WHILE THE RT SIDE SHOWED NO IMPROVEMENT, ACFT VEERED LT AND THE PROP IMPACTED A TAXI WAY LIGHT AT LOW IDLE. BRAKE CHECKS WEREJun 4, 2011 · N787FE · Cessna 208B · Landing Gear Brake SystemSDR CA110601012Support · tornON FINAL APPROACH, FLAPS SELECTED FROM 10 TO 20 DEGREES. AROUND 20 DEGREE MARK, FLAP CIRCUIT BREAKER POPPED. JUST BEFORE TOUCHDOWN PILOT HEARD BANGING SOUND IN CABIN AREA. ACFT LANDED NORMAL. ON INSPECTION, FLAP ACTUATOR MOTOR ASSY FOUND TO BE LOOSE AND BOUNMay 26, 2011 · Cessna 208B · Trailing Edge FlapsSDR HSYA2011052411Master Cylinder · failedPILOT REPORTED AFTER BLOCK OUT FOR FLIGHT 8691 - RIGHT BRAKE ON AIRCRAFT FELT SPONGY AND BRAKE PEDAL, WHEN FULLY APPLIED, WENT TO THE FLOOR - FAILED. THE ACFT WAS RETURNED TO THE PARKING RAMP FOR MX TROUBLESHOOTING. R & R RT BRAKE ASSEMBLY IAW MM 32-40-00. RMay 24, 2011 · N926FE · Cessna 208B · Master Cylinder/Brake ValveSDR AWH2011F00001Master Cylinder · inoperativePILOT REPORTED WHILE TAXIING TO THE RAMP, A RT TURN WAS MADE AND WAS SLIGHTLY OVER STEERED CAUSING THE PILOT TO INPUT LT BRAKE TO CORRECT. HE REPORTED WHEN HE APPLIED THE LT BRAKE PEDAL, THE PEDAL WENT TO THE FLOOR AND THE LT BRAKE WAS NOT EFFECTIVE. HE THENMay 19, 2011 · N930FE · Cessna 208B · Master Cylinder/Brake ValveSDR AWH2011F00000Master Cylinder · failedPILOT REPORTED DURING STRAIGHT TAXI TO LOADING POSITION, THE LT BRAKE PEDAL WENT TO THE FLOOR 3 TIMES. THE ACFT WAS SHUTDOWN AND SECURED AND THE PILOT CALLED MX. 30 MINUTES LATER, THE PILOT CALLED AND REPORTED THE LT BRAKE OPERATED NORMALLY. MX REPLACED THEMay 16, 2011 · N987FE · Cessna 208B · Master Cylinder/Brake ValveSDR 2011FA0000315Fitting · detachedIN-FLIGHT, A LOUD "POP" WAS HEARD, FOLLOWED BY A LOUD HISSING SOUND. ACFT APPEARED TO OPERATE NORMALLY. CREW ASSUMED THE SOUND CAME FROM A BLOWN DEFROSTER LINE. ACFT LANDED WITHOUT INCIDENT BUT AFTER THE THROTTLE WAS PULLED BACK AFTER PROPELLER REVERSE THE May 16, 2011 · N1229C · Cessna 208B · Pneumatic Distribution SystemSDR HSYA2011051211Starter Gen · shortedWHILE CREW WAS WAITING AT THE END OF THE RUNWAY FOR CLEARANCE TO TAKE OFF, THE STANDBY POWER LIGHT AND GENERATOR OFF LIGHTS CAME ON. SHORTLY AFTER THOSE LIGHTS CAME ON THE CREW ALSO NOTED A STRONG ELECTRICAL BURNING SMELL. CREW ELECTED TO RETURN TO PARKING RMay 12, 2011 · N926FE · Cessna 208B · Starter-GeneratorSDR 2011FA0000313Barrel · corrodedDURING THE 12 MONTH CORROSION INSP ON THE NOSE STRUT ASSY; AFTER DISASSEMBLY THE BARREL ASSY-OUTER NOSE GEAR AND ALL ASSOCIATING BEARINGS WERE FOUND TO BE EXCESSIVELY CORRODED.May 12, 2011 · N684SA · Cessna 208B · Nose/Tail Landing Gear Strut/AxleSDR CA110506001Elbow · cracked(CAN) DURING A PHASE INSPECTION, A CRACK WAS DISCOVERED AT THE BOLT HOLE OF ELBOW, PRESSURE OIL TRANSFER TUBE LOCATED ON FLANGE A, REDUCTION GEARBOX TO EXHAUST CASE, ON THE BOTTOM SIDE. PART REPLACED.May 5, 2011 · Cessna 208B · Engine Oil Distribution (Airframe Furnished)SDR CA110516007Blade · failedABORTED TAKEOFF, APPLYING POWER FOR TAKEOFF. HEARD A LOUD WHINING SOUND. IMMEDIATELY REDUCED POWER, CHECKED ALL OF THE ENGINE INDICATIONS, AND ALL WERE WITHIN LIMITS, TAXIED BACK TO PARKING. POWER SECTION REMOVED, AND REMAINDER OF ENGINE INSPECTED FOR DAMAMay 5, 2011 · Cessna 208B · Turbine SectionSDR MTNA05041100005Connector · damagedWHILE EN ROUTE FLIGHT 8115 BQN-PLS THE PILOT REPORTED A FIRE WARNING INDICATION (LIGHT & HORN). THE PILOT EXECUTED AN AIR TURNBACK TO BQN. THE PILOT DID NOT REPORT ANY VISUAL INDICATION OF SMOKE OR FIRE. THE FLIGHT LANDED WITHOUT INCIDENT. AFTER TROUBLESHOMay 5, 2011 · N921FE · Cessna 208B · Fire Protection System WiringSDR 2011F00094Spring · fracturedNOSE GEAR DRAG LINK SPRING FRACTURED AT THE FWD BEARING SUPPORT. FRACTURE WAS CONTAINED INSIDE THE SUPPORT BEARING AND WAS DETECTED BY THE NOSE GEAR STRUT BEING BOTTOMED OUT. THIS FAILURE APPEARS TO BE THE RESULT OF CORROSION/FATIGUE. FAILURE OCCURED WHILE AApr 27, 2011 · N862MA · Cessna 208B · Nose/Tail Landing GearSDR MTNA04261100004Fire Loop · out of positionDURING CLIMBOUT OF FLIGHT 8115 BQN-PLS THE PILOT OBSERVED THE ENGINE FIRE WARNING LIGHT ILLUMINATED WITH ACCOMPANIED AURAL ALARM. THE PILOT RETURNED THE AIRCRAFT TO BQN. AFTER TROUBLESHOOTING THE MECHANIC FOUND A SECTION OF FIRE LOOP IN CONTACT WITH THE VACUApr 26, 2011 · N921FE · Cessna 208B · Fire DetectionSDR CA110516001Engine · power loss(CAN) POWER LOSS, SINGLE ENGINE, 2 MINUTES AFTER T/O AT APPROXIMATELY 500 FT AGL, THE PILOT NOTICED ENGINE PARAMETER OSCILLATIONS AND SUBSEQUENT POWER LOSS. MINOR DAMAGE WAS REPORTED ON THE RT WING TIP. POST EVENT INSPECTION FOUND NO DAMAGE ON THE ENGINE AApr 20, 2011 · Cessna 208B · Engine (Turbine/Turboprop)SDR 2011FA0000806G Switch · no testELT G-SWITCH FAILED TEST.Apr 15, 2011 · N1314X · Cessna 208B · Emergency Locator BeaconSDR BSYA2011019Servo · faultyWHILE EN ROUTE FROM CLT TO LCK PILOT SMELLED SMOKE COMING FROM AFT COMPARTMENT, DIVERTED INTO LNP. MAINTENANCE FOUND THAT THE PITCH SERVO CAUSING THE SMOKE, PULLED AND TYRAPED CIRCUIT BREAKER FOR PITCH SERVO, MEL'D AUTO-PILOT AND FLEW IT BACK TO MAINTENANCE BApr 12, 2011 · N107AN · Cessna 208B · Autopilot Trim ServoSDR FXTA20110426007Bolt · brokenFLAP OPERATION INOP. UPON INSPECTION FOUND FLAP MOTOR HOUSING ATTACH BOLT BROKEN AND STAND BY MOTOR HOUSING ABLE TO ROTATE (HOUSING BOLTS NOT PROPERLY TORQUED). THESE ARE THE BOLTS THAT HOLD THE MOTOR TOGETHER NOT THE STUDS THAT ATTACH THE MOTOR TO THE FLAP Apr 12, 2011 · N205BA · Cessna 208B · Trailing Edge Flap Control SystemSDR CA110413003Fuel Control · malfunctioned(CAN) ABORTED T/O, SINGLE ENGINE, AFTER APPLYING T/O POWER, THE PILOT NOTICED THAT THE ENGINE KEPT ACCELERATING. THE THROTTLE WAS RETARDED TO NO AVAIL. THE T/O WAS ABORTED AND THE ENGINE SHUTDOWN. TROUBLESHOOTING LED TO THE REPLACEMENT OF THE FUEL CONTROL UNMar 23, 2011 · Cessna 208B · Fuel Control/Turbine EnginesSDR COEA2011031801756Engine · contaminatedFLIGHT 8676 FORM ANC TO HOM: DURING THE TAKEOFF ROLL, PILOT OBSERVED SMOKE OR STEAM IN THE COCKPIT, ALONG WITH A HOT SMELL. PILOT ABORTED THE TAKEOFF, CLEARED THE RUNWAY AND DECLARED AN EMERGENCY. UPON INITIAL INSPECTION IT WAS DETERMINED THE ENGINE WAS SOAMar 18, 2011 · N756FE · Cessna 208B · Engine (Turbine/Turboprop)SDR CA110331005Engine · power loss(CAN) IFSD (SINGLE ENGINE) DURING T/O ROLL, A LOSS OF POWER OCCURRED ACCOMPANIED BY OIL SPLATTERING THE WINDSHIELD. THE T/O WAS ABORTED.Mar 15, 2011 · Cessna 208B · Engine (Turbine/Turboprop)SDR COEA20110314899Indicator · failedATB: ON FLIGHT 100 FROM GEG TO YKM PILOT NOTICED THE NR 1 ATTITUDE INDICATOR FAILED. CREW NOTIFIED ATC AND RETURNED TO GEG. MAINTENANCE REMOVED AND REPLACED ATTITUDE INDICATOR.Mar 14, 2011 · N899FE · Cessna 208B · Integrated Flight SystemSDR CA110228018Engine · failed(CAN) IFSD SINGLE ENGINE, DURING FLIGHT THE PILOT HEARD A LOUD BANG FOLLOWED BY OIL COVERING THE WINDSHIELD AND PROPELLER GOING TO FEATHER POSITION. THE PILOT DECLARED AN EMERGENCY AND MADE A SUCCESSFUL LANDING WITHOUT INCIDENT AT AIRPORT.Feb 23, 2011 · Cessna 208B · Engine (Turbine/Turboprop)
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