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 CA061006019Bearing Cage · fractured(CAN) ENGINE TORQUE WAS SEEN TO FLUCTUATE IN CRUISE, REDUCING TO ZERO UNCOMMANDED DURING DESCENT. POWER WAS RECOVERED USING THE FUEL CONTROL MANUAL OVER-RIDE SYSTEM. ON A SUBSEQUENT START THE ENGINE ACCELERATED UNCOMMANDED. SUBSEQUENT INSPECTION REVEALED A PSep 27, 2006 · Cessna 208B · Fuel Control/Turbine EnginesSDR CA061006018Engine · fire(CAN) ON TAXI FOLLOWING LANDING, FLAMES WERE SEEN COMING FROM THE ENGINE EXHAUST. MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20061006018)Sep 27, 2006 · Cessna 208B · Engine (Turbine/Turboprop)SDR CA060925001Fairing · loose(CAN) DURING LANDING A SLIGHT THUMP AND A VIBRATION WAS FELT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE RT MAIN LANDING GEAR FAIRING (GEAR TO FUSELAGE FAIRING) WAS MISSING THE LOWER PORTION. THIS FAIRING IS A ONE PIECE Sep 25, 2006 · Cessna 208B · Landing Gear/Wheel FairingSDR AMCR200600002Indicator · leakingPILOT REPORTED AN AIRSPEED SPLIT BETWEEN THE 2 INDICATORS. MAINTENANCE FOUND THE CO-PILOTS INDICATOR LEAKING INTERNALLY. FOUND INDICATOR TO BE AN OLDER, SUPERSEDED TYPE. LATEST UNIT IAW IPC INSTALLED. MFG P/N C661064-0237.Sep 25, 2006 · N479DV · Cessna 208B · Airspeed/Mach IndicatorSDR BSYA200600026Door · unsecureON TAKEOFF OUT OF BOS PILOT HAD A DOOR AJAR LIGHT COME ON. ABORTED TAKEOFF SECURED CARGO DOOR AND CONTINUED WITH FLIGHT.Sep 21, 2006 · N1026V · Cessna 208B · Door Warning SystemSDR 2006FA0001028Bearing · brokenUPON DISASSEMBLY OF THIS PROPELLER IAW WITH MFG TECH REPORT NR940. IT WAS DISCOVERED THAT THE PITCH CHANGE LINK BUSHINGS, P/N A4564, ON BLADES NR 2 AND NR 3 WERE BROKEN AND PARTIALLY MISSING. AT LEAST 50 PERCENT OF THE BUSHINGS WERE NOT IN THE LINK. THE THICKNSep 12, 2006 · N324SJ · Cessna 208B · Propeller SystemSDR CA060908001Boot · distorted(CAN) THE CARGO POD DEICER BOOT EXHIBITS DETERIORATION DUE TO OIL/FUEL CONTAMINATION. SUSPECTED CAUSE IS LEAKING OR OPEN STOP COCKS ON THE ENGINE DRAINS. (TC NR 20060908001)Sep 8, 2006 · Cessna 208B · Airfoil Anti/De-ice SystemSDR CA060921006Line · chafed(CAN) APPROXIMATELY 10 MIN. INTO THE FLIGHT AT 5500 FT ALTITUDE AND IN CRUISE, THE PILOT NOTICED LIGHT SMOKE COMING FROM THE GENERAL LOCATION OF THE CIRCUIT BREAKER PANEL, AND A DISCOLORING OF THE LT CREW DOOR FWD POST PANEL, LOCATED JUST ABOVE THE CB PANEL. TSep 5, 2006 · Cessna 208B · Engine Bleed Air SystemSDR CA061006013Compressor · seized(CAN) THE ENGINE WAS REPORTED TO EMIT A LOUD NOISE AND SUBSEQUENTLY FLAMED OUT IN FLIGHT. POST-FLIGHT INSPECTION REVEALED METAL DEBRIS IN THE OIL, RUBBING NOISES FROM THE POWER SECTION AND A SEIZED COMPRESSOR. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOAug 15, 2006 · Cessna 208B · Turbine Engine Compressor SectionSDR CA060906015Engine · flamed out(CAN) THE ENGINE WAS REPORTED TO EMIT A LOUD BANG IN FLIGHT FOLLOWED BY A FLAMEOUT. A DEAD-STICK LANDING WAS ACCOMPLISHED. SUBSEQUENT INSPECTION REVEALED DEBRIS IN THE ENGINE OIL FILTER AND SEIZURE OF THE COMPRESSOR. MFG WILL INVESTIGATE THE EVENT AND ADVSEAug 15, 2006 · Cessna 208B · Engine (Turbine/Turboprop)SDR PNSA060804Turbine Blades · failedIN CRUISE AT 9000 FT, PILOT HEARD A LOUD GRINDING NOISE & ENGINE LOST ALL POWER. DECLARED AN EMERGENCY, ATTEMPTED ENGINE RESTART, NO SUCCESS. STARTER WAS ENGAGED NG SHOWED NO ROTATION & INSTRUMENT LIGHTS DIMMED. PROP FEATHERED, NORMAL LANDING. PRELIMARY REPAug 15, 2006 · N9310F · Cessna 208B · Engine (Turbine/Turboprop)SDR PNSA060807Alternator · failedDURING CRUISE FROM DLG TO TOG, STANDBY ALTERNATOR WARNING LIGHT ILLUMINATED. PILOT RETURNED TO DLG WHERE MAINTENANCE REPLACED STANDBY ALTERNATOR AND RETURNED AIRCRAFT TO SERVICE.Aug 15, 2006 · N9820F · Cessna 208B · AC Generator-AlternatorSDR CA060807001Wheel · cracked(CAN) APPROX 1.5 INCH CRACK AROUND CIRCUMFERENCE OF BEARING RACE, INSIDE OF WHEEL HALF, SUSPECT MIS-ALIGNMENT OF WHEEL HALF SPACER DURING BUILD-UP (TC NR 20060807001)Aug 4, 2006 · Cessna 208B · Wheel/Ski/FloatSDR SAI080601Fuel Control · bindingON FINAL APPROACH THE PILOT MADE AN ADJUSTMENT TO THE POWER LEVER WITH NO ENGINE RESPONSE. USED THE EMERGENCY POWER LEVER TO CONTROL ENGINE POWER AND LANDED. AFTER LANDING PILOT COULD NOT DUPLICATE DISCREPANCY AT RAMP BEFORE SHUTDOWN. REPLACING FUEL CONTROLAug 1, 2006 · N1120N · Cessna 208B · Fuel Control/Turbine EnginesSDR SAI070601Brake Assy · leakingNO BRAKING EFFECT TO RT BRAKE. REMOVED AND REPLACED BRAKE ASSY. COULD NOT FIND LEAKING SOURCE FROM REMOVED BRAKE ASSY. SENT REMOVED BRAKE ASSY IN FOR OVERHAUL. WAITING ON OVERHAUL WORK REPORT.Jul 22, 2006 · N1037 · Cessna 208B · BrakeSDR CA060906018Engine · damaged(CAN) DURING CLIMB THE ENGINE EMITTED A LOUD BANG ACCOMPANIED BY A LOSS IN POWER AND AN AGB CHIP DETECTOR INDICATION. THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED DEBRIS IN THE ACCESSORY AND REDUCTION GEARBOXES AND POWER TURBINE ROTOR DAJul 17, 2006 · Cessna 208B · Turbine SectionSDR AXS2006F00001Circuit Breaker · faulty10 MINUTES AFTER DEPARTURE, THE PILOT NOTICED A SMELL OF SMOKE. ONE MINUTE LATER THE PILOT SAW A PUFF OF SMOKE FROM THE CB PANEL AND REPORTED IT TO ATC. THE PILOT DIVERTED BACK AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL WAS DISPATCHED TO THEJun 15, 2006 · N865FE · Cessna 208B · DC Generating SystemSDR HSY2006F00000Drive Assy · shearedINCRUISE FLIGHT WITH AUTOPILOT ENGAGED, FLAPS WENT TO THE FULLY EXTENDED POSITION UNCOMMANDED. STANDBY FLAP CIRCUIT BREAKER POPPED. PILOT RESET CIRCUIT BREAKER AND RETRACTED FLAPS TO THE 10 DEGREE POSITION IN THE STANDBY MODE. PILOT LANDED WITH FLAPS AT 10 Jun 3, 2006 · N765FE · Cessna 208B · Trailing Edge Flap Control SystemSDR CA060731016Turbine Blades · fractured(CAN) DURING CRUISE THE ENGINE EMITTED A NOISE ACCOMPANIED BY AN UNCOMMANDED REDUCTION IN POWER. THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE. SUBSEQUENT INSPECTION REVEALED A FRACTURED POWER TURBINE BLADE. MFG WILL INVESTIGATE THE EVENT AND WILL ADVISE OF RMay 25, 2006 · Cessna 208B · Turbine SectionSDR CA060501001Engine · failed(CAN) DURING CRUISE THE ENGINE EMITTED A LOUD NOISE ACCOMPANIED BY AN UNCOMMANDED POWER LOSS. THE ENGINE WOULD NOT RESPOND TO THROTTLE INPUT. A SUCCESSFUL DEAD-STICK LANDING WAS ACCOMPLISHED. MFG WILL INVESTIGATE THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCApr 26, 2006 · Cessna 208B · Engine (Turbine/Turboprop)SDR CA060425014Engine · flamed outDURING CLIMB, THE ENGINE EMITTED A LOUD NOISE AND FLAMED OUT. A DEADSTICK LANDING WAS SUCCESSFULLY ACCOMPLISHED. P&WC WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE DETERMINED.Apr 16, 2006 · Cessna 208B · Engine (Turbine/Turboprop)SDR P912006F00000Pin · damagedTHESE PINS ARE LIFE-LIMITED TO 31500 LANDINGS, BUT WE REMOVE THEM AT INTERVALS FOR CORROSION INSPECTION OF THE LANDING GEAR INTERFACE. WE HAVE NEVER FOUND THE PINS THEMSELVES CORRODED, BUT THE PINS ON NEWER AIRCRAFT OR NEWER SPARE PINS ARE PLATED (EARLIER ONEApr 3, 2006 · N228PA · Cessna 208B · Main Landing GearSDR 2006FA0000387Deice System · leakingWATER LEAKS AROUND/THROUGH EDGE SEAL OF WINDSHIELD DE-ICE HOT PLATE AND OBSTRUCTS FORWARD VIEW OF PILOT. THIS WATER FREEZES BETWEEN THE HOT PLATE AND THE WINDSHIELD. IN RAIN CONDITIONS WITH TEMPERATURE ABOVE FREEZING WATER ACCUMULATES AND FILLS 4 TO 5 INCHESMar 28, 2006 · N208JH · Cessna 208B · Windshield/Door Rain/Ice RemovalSDR SAI030603Roll Pin · shearedDURING TAKE-OFF PILOT NOTED VIBRATION AND ABORTED TAKE-OFF. AIRCRAFT RETURNED TO RAMP. AIRCRAFT WAS INSPECTED AND FOUND FAULTY SHIMMY DAMPNER. ROLL PIN, P/N NAS561P5-18, SHEARED.Mar 21, 2006 · N1119V · Cessna 208B · Shimmy DamperSDR CA060403009Engine · power lossDURING CLIMB, THE ENGINE EXPERIENCED AN UNCOMMANDED LOSS OF POWER. THE AIRCRAFT CRASHED ON ATTEMPTING TO RETURN TO POINT OF DEPARTURE. P&WC WILL INVESTIGATE THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCE ESTABLISHED.Mar 9, 2006 · Cessna 208B · Engine (Turbine/Turboprop)SDR CA060309007Transducer · fluctuates(CAN) DURING CRUISE FLIGHT FUEL FLOW INDICATOR STATED FLUCUATING FROM 80 LBS - 350 LBS/HR. A/C RETURNED TO BASE AND UPON INSPECTION BY MAINT. IT WAS DISCOVERED THAT THE CANNON PLUG ATTACHED TO THE FUEL FLOW TRANSDUCER WAS DIRTY. CONNECTION WAS CLEANED, A/C Mar 8, 2006 · Cessna 208B · Fuel Flow IndicatingSDR CA060403011Engine · power lossTHE ENGINE EMITTED A LOUD NOISE FOLLOWED BY AN UNCOMMANDED INFLIGHT SHUTDOWN. THE AIRCRAFT DEPARTED THE RUNWAY ON LANDING RESULTING IN SIGNIFICANT AIRFRAME DAMAGE. P&WC WILL INVESTIGATE THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCE DETERMINED.Mar 5, 2006 · Cessna 208B · Engine (Turbine/Turboprop)SDR CA060403006Engine · flamed out(CAN) INFLIGHT THE ENGINE EMITTED A LOUD NOISE, INTERTURBINE TEMPERATURE INCREASED AND THE ENGINE FLAMED OUT. A DEAD-STICK LANDING WAS CARRIED OUT RESULTING IN SIGNIFICANT AIRCRAFT DAMAGE. MFG WILL INVESTIGATE AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NMar 5, 2006 · Cessna 208B · Engine (Turbine/Turboprop)SDR AWH2006F00014Coupling · corrodedPRECAUTIONARY INSPECTION OF THE FUEL PUMP DRIVE SPLINE IAW MM, FUEL PUMP COUPLING IN-SITU INSPECTION. MAINTENANCE FUND THE FUEL PUMP DRIVE SPINE CORRODED. THE FUEL PUMP ASSY WAS REPLACED WITH AN OVERHAULED UNIT AND THE AIRCRAFT RETURNED TO SERVICE. (K)Mar 1, 2006 · N707FX · Cessna 208B · Engine Fuel PumpSDR AWH2006F00013Coupling · corrodedPRECAUTIONARY INSPECTION FO THE FUEL PUMP DRIVE SPLINE IAW MM, FUEL PUMP COUPLING IN-SITU INSPECTION. MAINTENANCE FOUND THE FUEL PUMP DRIVE SPLINE CORRODED. THE FUEL PUMP ASSY WAS REPLACED WITH AN OVERHAULED UNIT AND THE AIRCRAFT RETURNED TO SERVICE. (K)Mar 1, 2006 · N872FE · Cessna 208B · Engine Fuel PumpSDR CA060223005Spring · weakAIRCRAFT DEPARTED AND AFTER TAKEOFF, ATC INFORMED THE PILOT THAT THE AFT POD CARGO DOOR WAS OPEN. THE AIRCRAFT RETURNED AND THE PILOT IN COMMAND INSPECTED THE DOOR, HINGES AND AND THE POD AND FOUND NO DAMAGE. THE AIRCRAFT DEPARTED AND MAINTENANCE INSPECTED TFeb 23, 2006 · Cessna 208B · Cargo/Baggage DoorsSDR AWH2006F00015Coupling · corrodedPRECAUTIONARY INSPECTION OF THE FUEL PUMP DRIVE SPLINE IAW MM, FUEL PUMP COUPLING IN-SITU INSPECTION. MAINTENANCE FOUND THE FUEL PUMP DRIVE SPLINE CORRODED. THE FUEL PUMP ASSY WAS REPLACED WITH AN OVERHAULED UNIT AND THE AIRCRAFT RETURNED TO SERVICE. (K)Feb 23, 2006 · N771FX · Cessna 208B · Engine Fuel PumpSDR CA060228009Jackscrew · failedAS A PRECAUTION FOLLOWING THE FAILURE ON INSTALLATION OF A SIMILAR TRIM JACK ON A DIFFERENT AIRCRAFT, BOTH ELEVATOR TRIM JACKS ON FSKS WERE REMOVED AND DISASSEMBLED TO INSPECT FOR CORRECT LUBRICATION. THE LT TRIM JACK (S/N CA0009) WAS FOUND TO BE CORRECTLY LUFeb 22, 2006 · Cessna 208B · Elevator Tab Control SystemSDR AWH2006F00012Coupling · corrodedPRECAUTIONARY INSPECTION OF THE FUEL PUMP DRIVE SPLINE IAW MM, FUEL PUMP COUPLING IN-SITU INSPECTION. MAINTENANCE FOUND THE FUEL PUMP DRIVE SPLINE CORRODED. THE FUEL PUMP ASSEMBLY WAS REPLACED WITH AN OVERHAULED UNIT AND THE AIRCRAFT RETURNED TO SERVICE. (KFeb 22, 2006 · N726FX · Cessna 208B · Engine Fuel PumpSDR AWH2006F00011Coupling · corrodedPRECAUTIONARY INSPECTION OF THE FUEL PUMP DRIVE SPLINE IAW MM, FUEL PUMP COUPLING IN-SITU INSPECTION. MAINTENANCE FOUND THE FUEL PUMP DRIVE SPLINE CORRODED. THE FUEL PUMP ASSY WAS REPLACED WITH AN OVERHAULED UNIT AND THE AIRCRAFT RETURNED TO SERVICE. (K)Feb 22, 2006 · N782FE · Cessna 208B · Engine Fuel PumpSDR AWH2006F00010Coupling · corrodedPRECAUTIONARY INSPECTION OF THE FUEL PUMP DRIVE SPLINE IAW WITH MM, FUEL PUMP COUPLING IN-SITU INSPECTION. MAINTENANCE FOUND THE FUEL PUMP DRIVE SPLINE CORRODED. THE FUEL PUMP ASSY WAS REPLACED WITH AN OVERHAULED UNIT AND THE AIRCRAFT RETURNED TO SERVICE. (Feb 22, 2006 · N722FX · Cessna 208B · Engine Fuel PumpSDR AWH2006F00008Coupling · corrodedPRECAUTIONARY INSPECTION OF THE FUEL PUMP DRIVE SPLINE IAW MM, FUEL PUMP COUPLING IN-SITU INSPECTION. MAINTENANCE FOUND THE FUEL PUMP DRIVE SPLINE CORRODED. THE FUEL PUMP ASSEMBLY WAS REPLACED WITH AN OVERHAULED UNIT AND THE AIRCRAFT RETURNED TO SERVICE. (KFeb 22, 2006 · N968FE · Cessna 208B · Engine Fuel PumpSDR AWH2006F00007Coupling · corrodedPRECAUTIONARY INSPECTION OF THE FUEL PUMP DRIVE SPLINE IAW MM. FUEL PUMP COUPLING IN SITU INSPECTION. MAINTENANCE FOUND THE FUEL PUMP FUEL PUMP DRIVE SPLINE CORRODED. THE FUEL PUMP ASSY WAS REPLACED WITH AN OVERHAULED UNIT AND THE AIRCRAFT RETURNED TO SERVIFeb 22, 2006 · N763FE · Cessna 208B · Engine Fuel PumpSDR AWH2006F00006Coupling · corrodedPRECAUTIONARY INSPECTION OF THE FUEL PUMP DRIVE SPLINE IAW MM, FUEL PUMP COUPLING IN-SITU INSPECTION. MAINTENANCE FOUND THE FUEL PUMP DRIVE SPLINE CORRODED. THE FUEL PUMP ASSY WAS REPLACED WITH AN OVERHAULED UNIT AND THE AIRCRAFT RETURNED TO SERVICE. (K)Feb 22, 2006 · N844FE · Cessna 208B · Engine Fuel PumpSDR AWH2006F00005Coupling · corrodedPRECAUTIONARY VISUAL INSPECTION OF THE FUEL PUMP DRIVE SPLINE IAW MM. FUEL PUMP COUPLING IN-SITU INSPECTION. MAINTENANCE FOUND THE FUEL PUMP DRIVE SPLINE CORRODED. DUE TO THE EVIDENCE OF CORRODION THE FULE PUMP ASSY WAS REPLACED WITH AN OVERHAULED UNIT AND Feb 22, 2006 · N908FE · Cessna 208B · Engine Fuel PumpSDR AWH2006F00004Coupling · corrodedPRECAUTIONARY INSPECTION OF THE FUEL PUMP DRIVE SPLINE IAW MM. FUEL PUMP COUPLING IN-SITU INSPECTION. MAINTENANCE FOUND THE FUEL PUMP DRIVE SPLINE CORRODED. THE FUEL PUMP ASSY WAS REPLACED WITH AN OVERHAULED UNIT AND THE AIRCRAFT RETURNED TO SERVICE. (K)Feb 22, 2006 · N713FX · Cessna 208B · Engine Fuel PumpSDR AWH2006F00003Coupling · corrodedPRECAUTIONARY INSPECTION OF THE FUEL PUMP DRIVE SPLINE IAW MM. FUEL PUMP COUPLING IN-SITU INSPECTION. MAINTENANCE FOUND THE FUEL PUMP DRIVE SPLINE CORRODED. THE FUEL PUMP ASSY WAS REPLACED WITH AN OVERHAULED UNIT AND THE AIRCRAFT RETURNED TO SERVICE. (K)Feb 22, 2006 · N790FE · Cessna 208B · Engine Fuel PumpSDR AWH2006F00002Coupling · corrodedPRECAUTIONARY INSPECTION OF THE FUEL PUMP DRIVE SPLINE IAW MM, FUEL PUMP COUPLING IN-SITU INSPECTION. MAINTENANCE FOUND THE FUEL PUMP DRIVE SPLINE CORRODED. THE FUEL PUMP ASSEMBLY WAS REPLACED WITH AN OVERHAULED UNIT AND THE AIRCRAFT RETURNED TO SERVICE. (KFeb 22, 2006 · N995FE · Cessna 208B · Engine Fuel PumpSDR AWH2006F00000Coupling · corrodedPRECAUTIONARY INSPECTION OF THE FUEL PUMP DRIVE SPLINE IAW MM, FUEL PUMP COUPLING IN-SITU INSPECTION. MAINTENANCE FOUND THE FUEL PUMP DRIVE SPLINE CORRODED. THE FUEL PUMP ASSEMBLY WAS REPLACED WITH AN OVERHAULED UNIT AND THE AIRCRAFT RETURNED TO SERVICE. (KFeb 22, 2006 · N744FX · Cessna 208B · Engine Fuel PumpSDR CA060227021Line · fracturedDURING FLIGHT, THE ENGINE LOW OIL PRESSURE WARNING ANNUNCIATED FOLLOWED BY AN UNCOMMANDED ROLL BACK IN ENGINE POWER. THE ENGINE WAS SECURED IN FLIGHT AND A SUCCESSFUL FORCED LANDING ACCOMPLISHED. SUBSEQUENT INSPECTION REVEALED A FRACTURED PRESSURE OIL TRANSFFeb 21, 2006 · Cessna 208B · Turbine Engine Oil SystemSDR CA060228005Jackscrew · damagedTHE LT ELEVATOR TRIM JACK WAS REMOVED AND DISASSEMBLED FOR INSPECTION AFTER THE RT TRIM JACK FAILED ON INSTALLATION. THE LT TRIM JACK WAS FOUND TO CONTAIN NO GREASE. THE JACK WAS INSPECTED, LUBRICATED IAW AMM 27-30-02, 9A, REASSEMBLED, TESTED AND RETURNED TOFeb 20, 2006 · Cessna 208B · Elevator Tab Control SystemSDR CA060223004Jackscrew · failedELEVATOR TRIM SCREW JACK (RT) FAILED ON INSTALLATION.Feb 20, 2006 · Cessna 208B · Elevator Control SystemSDR CA060223003Actuator · failedELEVATOR TRIM SCREW JACK FAILED ON INSTALLATION.Feb 20, 2006 · Cessna 208B · Elevator Tab Control SystemSDR CA060228014Wing · misinstalledDURING INSPECTION, FOUND INBD EDGES OF BOTH LT AND RT FLAP ASSEMBLIES WERE TOUCHING FUSELAGE IN FULL UP POSITION. MX DEPART COMPLETED INSPECTIONS OF FOLLOWING AREAS FLAP ATTACHMENT, FLAP RIGGING, FLAP STRUCTURE FOR BENDING OR WARPING, STRUCTURE OF WINGS FOR BFeb 6, 2006 · Cessna 208B · Wing StructureSDR CA060207004Boot · missing(CAN) WHILE ON A ROUTINE LOCAL TRAINING FLIGHT, THE PILOT EXPERIENCED SEVERE VIBRATION FROM THE ENGINE/PROPELLER. RETURNING TO THE AIRFIELD THE AIRCRAFT WAS LANDED SAFELY. INSPECTION REVEALED THAT ONE PROPELLER BLADE DE-ICER BOOT HAD DETACHED FROM THE BLADE ANFeb 5, 2006 · Cessna 208B · Propeller Deice Boot Section
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