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 CA100809023Transmitter · erraticDURING A ROUTINE TAKEOFF, THE PILOT NOTED FUEL FLOW FLUCTUATIONS. HE DECLARED AN EMERGENCY AND RETURNED TO THE AIR FIELD OF DEPARTURE. UPON INSP OF THE FUEL FLOW SYS, IT WAS FOUND THAT THE TRANSMITTER WAS GIVING FALSE AND ERRATIC INDICATIONS.May 17, 2010 · Cessna 208B · Fuel Indicating SystemSDR HSYA2010042810Hsi · inoperativeAFTER TAKEOFF, THE CREW ADVISED BOTH THE CAPTAINS HSI AND RMI INDICATORS ROTATED NORMALLY AND THEN FROZE ON A 185 DEGREE HEADING (AT 700 FEET AGL). AN EMERGENCY WAS DECLARED AND THE ACFT LANDED BACK AT DEPARTURE WITHOUT FURTHER INCIDENT. MX WOULD TROUBLESHOOTApr 28, 2010 · N936FE · Cessna 208B · Turn and Bank/Rate of Turn IndicatorSDR HSYA2010042710Brake · contaminatedDURING TAXI OUT FOR FLIGHT 8827 SLC-SUN, THE PILOT OF N748FX ADVISED THAT THE RIGHT BRAKE OF THE AIRCRAFT PROVIDED NO BRAKING ACTION WHEN APPLIED. N748FX WAS RETURNED TO THE RAMP AND MET BY MAINTENANCE FOR TROUBLESHOOTING. MAINTENANCE BLED THE RIGHT BRAKE ANApr 27, 2010 · N748FX · Cessna 208B · BrakeSDR SBAA201000001Switch · overheatedDURING APPROACH INTO TVC PILOT NOTICED BURNT ELECTRICAL SMELL AND VERY SMALL AMOUNT OF SMOKE IN COCKPIT. PILOT DONNED OXYGEN MASK AND REDUCED ELECTRICAL LOAD PER EMERGENCY CHECKLIST. AIRCRAFT LANDED IN TVC WITHOUT INCIDENT. INSPECTION REVEALED OVERHEATED RIApr 20, 2010 · N993FE · Cessna 208B · Exterior LightingSDR BSYA2010021Chip Detector · contaminatedEN ROUTE FROM OMA TO DSM WHEN THE FORWARD ENGINE CHIP DETECTOR LIGHT CAME ON. LANDED IN DSM NO PROBLEMS. MAINTENANCE FOUND SMALL SLIVER OF METAL ON CHIP DETECTOR. CLEANED DETECTOR, CHECKED OIL FILTER COMPLIED WITH OIL SAMPLE ANALYSIS, RAN ENGINE FOR TEN MINApr 1, 2010 · N9448B · Cessna 208B · Turbine Engine Accessory DriveSDR 2010F00061Bulkhead · distortedWITH ACFT PARKED IN STRONG TAIL WIND NEAR GROSS WEIGHT WITH CG NEAR AFT LIMIT, ACFT SETTLED ON TAIL TIE DOWN ASSY AFTER PILOT EXITED THE COCKPIT. THE LOWER PORTION OF THE 2612059-2 BULKHEAD WAS DAMAGED AND WILL HAVE TO BE REPAIRED IAW THE FAA APPROVED MFG SRM Mar 7, 2010 · N865MA · Cessna 208B · Fuselage Main, BulkheadSDR COEA2010030601778Plunger · out of adjustON FLIGHT 7692 ATB TO RDM: AFTER DEPARTURE TO PDX FROM RDM THE CARGO DOOR LIGHT ILLUMINATED. PILOT ELECTED TO RETURN TO RDM AS A PRECAUTION. MAINTENANCE INSPECTED ALL DOOR LOCK MECHANISMS AND HINGES. ADJUSTED UPPER CARGO DOOR HANDLE DETENT PLUNGER. NO FURMar 6, 2010 · N778FE · Cessna 208B · Cargo/Baggage DoorsSDR HSYA2010022510Fuel Control · failedDURING APPROACH, ON FLIGHT 8785 SLC-PIH THE CAPTAIN REPORTED THAT AFTER REDUCING THE POWER LEVER, THE TORQUE WOULD NOT DROP BELOW 1200 LBS EVEN WITH THE POWER LEVER POSITIONED AT THE QUADRANT STOPS AND THE CONDITION LEVER IN THE LOW IDLE POSITION, HOWEVER THE Feb 25, 2010 · N997FE · Cessna 208B · Fuel Control/Turbine EnginesSDR CA100219007Hose · leaking(CAN) ENGINE OIL SUPPLY HOSE WAS REPLACED AS IT IS A LIFE LIMITED PART. THE NEW HOSE WAS INSTALLED AND FUNCTIONAL CHECKED. A LEAK WAS DETERMINED TO BE COMING FROM THE NEW HOSE FITTING. THE FITTING WAS CHECKED FOR TIGHTNESS BUT THIS DID NOT FIX THE LEAK. THE OLFeb 18, 2010 · Cessna 208B · Turbine Engine Oil SystemSDR HYT2010F00000Torque Tube · corrodedAFTER A "HEADS UP" FROM ANOTHER OPERATOR, THE RUDDER TORQUE TUBE PN 2633066-3 WAS INSPECTED FOR CORROSION. INITIAL INSP REAVEALED CORROSION ON MUCH OF THE EXPOSED SURFACES OF THE FRAME, PN 2633014-1 AND SUPPORT PLATE PN 2633017-1 WHICH ARE LOCATED INSIDE THE Feb 15, 2010 · N1314X · Cessna 208B · Rudder Control SystemSDR EPUA1553692Skin · chafedABRASION ON LT INBOARD WING SKIN CAUSED FROM LT INBOARD WING/FUSELAGE FAIRING. LOCATED LEFT WING STATION 35 TO 35.5 INCHES FROM TRAILING EDGE, EXTENDING FORWARD 11 INCHES.Feb 1, 2010 · N208SD · Cessna 208B · Wing, Plate/SkinSDR 2010FA0000095Starter Gen · unserviceablePILOT REPORTED HIS GENERATOR FAILED. MX FOUND THAT THE INPUT SHAFT HAS EITHER SHEERED INTERNAL OF THE UNIT OR BECAME DISCONNECTED. UNIT HAS NOT BEEN OPENED UP FOR INSP AT THIS TIME. A VIDEO SHOWING THIS CONDITION IS ACCOMPANYING THIS REPORT. UNIT WILL BE SJan 22, 2010 · N9766B · Cessna 208B · Starter-GeneratorSDR MTNA0110001Unknown · smokeTHE PIC REPORTED A SMOKE SMELL AND SAW SMOKE IN THE COCKPIT. DECLARED AN EMERGENCY AND DID AN AIR TURNBACK AND LANDED SAFELY. TAXIED CLEAR OF THE RUNWAY AND WAS MET BY EMERGENCY RESPONDERS. THE AIRCRAFT WAS SHUT DOWN AND TOWED TO THE RAMP. TROUBLESHOOTING Jan 22, 2010 · N924FE · Cessna 208B · Air Distribution SystemSDR CA100119011G Switch · defective(CAN) AFTER 1 YEAR OF OPERATION SINCE NEW, THE ELT WAS SENT OUT TO A LOCAL AVIONICS SHOP TO BE RE-CERTIFIED. THE AVIONICS SHOP FOUND THE G-SWITCH TO BE DEFECTIVE. A NEW G-SWITCH WAS INSTALLED AND THE UNIT WAS RECERTIFIED.Jan 19, 2010 · Cessna 208B · Emergency Locator BeaconSDR COEA2010011101863Rheostat · contaminatedON FLIGHT 7686 TO PDX INSTRUMENT LIGHTS CIRCUIT BREAKER POPPED ACCOMPANIED BY BRIEF SPARKS AND SMOKE. INSTRUMENT LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED WIRES AND SWITCHES AND FOUND DEBRIS ON RHEOSTAT. DEBRIS WAS REMOVED AND SWITCH POSTS CLEANED. AJan 11, 2010 · N863FE · Cessna 208B · Flight Compartment LightingSDR COEA2010010801880Timer · defectiveTAXI BACK FLT 8699 SEA: FLIGHT 8699 TAXIED OUT, ON RUN UP PILOT DISCOVERED THE DEICE BOOTS DID NOT INFLATE ALL 3 CYCLES IN AUTO MODE. AIRCRAFT TAXIED BACK TO RAMP FOR MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE DE-ICE TIMER. AIRCRAFT RETURNED TO SERVJan 8, 2010 · N880FE · Cessna 208B · Airfoil Anti/De-ice SystemSDR 2010FA0000099Trunnion · chafedRT MLG TRUNNION WAS FOUND CHAFED AND WORN BEYOND LIMIT BY CONTACT WITH MLG FAIRING PN 2641018-28. WEAR LIMIT IS ESTABLISHED IN CAB05-17 WHICH ADDRESSES THIS CONDITION IN EARLIER SN AIRPLANES BUT DOES NOT COVER THIS AIRPLANE MFG 6/5/08. CONDITION WAS NOT DETEJan 7, 2010 · N1314X · Cessna 208B · Fuselage, Landing Gear Attach FittingsSDR CA100112004Oil Filter · failed(CAN) INNER CONE (SCREEN) SEAMS ARE BECOMING UNGLUED. (TC NR 20100112004)Jan 7, 2010 · Cessna 208B · Turbine Engine Oil SystemSDR BSYA2010001Line · contaminatedAIRCRAFT EN ROUTE FROM CPS TO BKL WHEN THE TAIL BOOTS BECAME INOP, DIVERTED TO LCK. MAINTENANCE FOUND WATER IN THE LINES GOING TO THE BOOTS. REMOVED WATER, OPS CHECKS GOOD.Jan 6, 2010 · N1115M · Cessna 208B · Airfoil Anti/De-ice SystemSDR 2010FA0000020Tube · corrodedTHE RIGID STEEL TUBE THAT FEEDS INTO THE OIL/FUEL HEATER HAS DEVELOPED LITTLE PIN HOLES UNDERNEATH THE FIRE LOOP BRACKET THAT ATTACHES THERE. WHEN YOU TAKE THE LINE OFF, IT JUST LOOKS LIKE LITTLE DOTS OF CORROSION BUT WHEN YOU PRESSURIZE IT WITH AIR, IT LEAKSJan 5, 2010 · N4655B · Cessna 208B · Fuel HeaterSDR CA100127007Attach Fitting · damaged(CAN) THE HOLE FOR THE WING STRUT ATTACH BOLT APPEARED TO HAVE BEEN IMPROPERLY LINE BORED CAUSING A EGG SHAPED HOLE AT THE FACTORY BOTH FORE & AFT. FITTINGS WERE REPLACED AT THIS TIME.Dec 25, 2009 · Cessna 208B · Wing, Attach FittingsSDR CA100127006Oil Filter · separated(CAN) VISUAL INSP DETECTED SEPARATION OF INTERNAL SCREEN AT SEAM. TECH REP ADVISED UNIT REPLACED WITH NEW.Dec 24, 2009 · Cessna 208B · Turbine Engine Oil SystemSDR BSYA2009061Bearing · wornDEPARTING LCK TO DPA PILOT ABORTED TAKEOFF DUE TO LOUD NOISE COMING FROM ENGINE COMPARTMENT. MAINTENANCE FOUND NOSE GEAR SPRING BEARING BAD. REMOVED AND REPLACED NOSE GEAR SPRING BEARINGS AND LINER OK FOR SERVICE.Dec 11, 2009 · N3RY · Cessna 208B · Nose/Tail Landing GearSDR CA091207005Support Bracket · buckled(CAN) UNCOMMANDED RETRACTION OF FLAPS FROM 20 DEG TO 10 DEG ON APPROACH, RESULTING IN A DROP OF 50 FT. FLAP MOTOR CIRCUIT BREAKER POPPED. INSP FOUND THAT THE FLAP TRANSMISSION SUPPORT BRACKET PN 2611144-1 HAD BUCKLED & TWISTED PULLING THE FLAP TRANSMISSION ODec 4, 2009 · Cessna 208B · Trailing Edge FlapsSDR CA091206006Flow Divider · faulty(CAN) THE CREW REPORTED LARGE AMOUNTS OF WHITE SMOKE COMING OUT OF THE ENGINE COWLING AFTER SHUTDOWN. THERE WAS A POSSIBLE CHANCE THAT A FIRE MAY OCCUR, SO THE FIRE DEPT WAS NOTIFIED. THE FUEL FLOW DIVIDER WAS SUSPECTED TO BE THE FAULT, THE FLOW DIVIDER WAS Dec 4, 2009 · Cessna 208B · Engine Fuel DistributionSDR CA091215010Engine · unknown(CAN) PILOT REPORTED HEARING A GRINDING NOISE AND SHORTLY AFTERWARD NG WENT TO ZERO. ENGINE WILL BE TRANSPORTED TO MANUFACTURER FOR INVESTIGATION. MANUFACTURER WILL INVESTIGATE TO ESTABLISH ROOT CAUSE AND SUPPLEMENT THE REPORT ONCE THE INFORMATION IS AVAILABDec 3, 2009 · Cessna 208B · Engine (Turbine/Turboprop)SDR AXSA701FX120309Engine · failedDURING CLIMB THROUGH 7500FT WITHOUT WARNING THE ENGINE MADE A VERY LOUD GRINDING/SQUEALING NOISE FOR APPROX 3 SECONDS AND PWR WAS IMMEDIATELY LOST. THE PILOT WAS ABLE TO SUCCESSFULLY LAND IN A FIELD WITH NO DAMAGE TO THE ACFT. MX EXTERNAL EVALUATION OF THE ENDec 3, 2009 · N701FX · Cessna 208B · Engine (Turbine/Turboprop)SDR MTNA0911001Fire Warning · activatedFIRE WARNING LIGHT CAME ON AFTER TAKEOFF CLIMBING THRU 1500 FEET. EMERGENCY DECLARED AND RETURNED TO SJU.Nov 11, 2009 · N921FE · Cessna 208B · Fire DetectionSDR HSYA20091109Line · crackedDURING CLIMBOUT, CREW NOTICED TORQUE BEGIN FALLING. AFTER REACHING CRUISE ALTITUDE OF 3,500 MSL THE TORQUE STEADIED AT 975 FT LBS AND CREW DECLARED AN EMERGENCY DUE TO ENG LOSS OF POWER. FLIGHT LANDED AT 2250Z WITHOUT FURTHER INCIDENT. THE CREW REPORTED ITT Nov 6, 2009 · N916F · Cessna 208B · Fuel Controlling SystemSDR BSYA2009056Switch · burnedEN ROUTE FROM AVP TO MDT HAD SMOKE IN COCKPIT AFTER TURNING ON PROP HEAT SWITCH, THEN TURNED ON ALL ELECTRICAL POWER. AFTER A FEW MINUTES, TURNED POWER BACK ON, ALL WAS GOOD WITH PROP HEAT SWITCH LEFT OFF. AFTER LANDING IN MDT MAINTENANCE FOUND A BURNT SWITCNov 5, 2009 · N104AN · Cessna 208B · Propeller/Rotor Anti-Ice/De-Ice SystemSDR 2009F00094Bulkhead · damagedCUSTOMER SERVICE AGENT STEPPED ON BOTTOM STEP OF PASSENGER DOOR, WITHOUT THE A/C TAIL-STAND IN PLACE. A/C TAIL CONTACTED GROUND, DAMAGING AFT BULKHEAD AND TAIL TIE-DOWN ASSY.Oct 15, 2009 · N861MA · Cessna 208B · Fuselage Main, BulkheadSDR CA091022005Spar · corroded(CAN) DURING A VERTICAL STAB SPAR INSPECTION PER CESSNA CARAVAN 208B SUPPLEMENTAL INSPECTION NUMBER 55-30-01, PART OF A 20,000 HOUR INSPECTION, FRETTING DAMAGE WAS FOUND AT VERTICAL STABILIZER REAR SPAR WEB AT W.L. 134.00. THERE WAS NO CORROSION DETECTED WHEREOct 13, 2009 · Cessna 208B · Vertical Stabilizer, Spar/RibSDR CA091002005Wheel · cracked(CAN) RT WHEEL ASSY MAKING NOISE DURING TAKE-OFF ROLL AND LANDING. NEW BRAKE DISC HAD BEEN INSTALLED, NEW THICKNESS PERCEIVED TO BE THE CAUSE OF RUBBING ON THE BRAKE PADS. FURTHER INVESTIGATION SHOWED THE WHEEL WAS SPUN THE BRAKE DISC WOBBLED. WHEN DISASSEMBLESep 30, 2009 · Cessna 208B · Wheel/Ski/FloatSDR COEA2009092901983Chip Detector · contaminatedDURING TAXI, PILOT DISCOVERED THE CHIP DETECTOR LIGHT ILLUMINATED. PILOT RETURNED TO RAMP. MX TROUBLESHOT SYS, FOUND VERY SMALL PIECE OF FUZZ ON CHIP DETECTOR PROBES. TOOK SOAP SAMPLE, REPLACED OIL FILTER AND PERFORMED GROUND RUN. ACFT RETURNED TO SERVICESep 29, 2009 · N983FE · Cessna 208B · Engine Oil Indicating SystemSDR HSYA2009092209Float Switch · brokenDURING CLIMBOUT, THE CREW ADVISED AT 500 FEET AGL THE FUEL LOW LEVEL RESERVOIR LIGHT ILLUMINATED, THE CLIMB WAS CONTINUED TO 1500 FEET, AN EMERGENCY WAS DECLARED AND THE ACFT RETURNED WITHOUT INCIDENT TO DEPARTURE. MX TROUBLESHOOT THE PROBLEM AND FOUND FAULTSep 22, 2009 · N926FE · Cessna 208B · Fuel Indicating SystemSDR COEA2009081201965Connector · contaminatedTAXI BACK - GEG FLT 8777. DURING TAXI THE PILOT DISCOVERED THE NP INOP, READS ZERO AT ALL PROP SPEEDS. REMOVED NP CONNECTOR, CLEANED, DRIED AND REINSTALLED. AIRCRAFT RETURNED TO SERVICE.Aug 12, 2009 · N965FE · Cessna 208B · Propeller/Propulsor System WiringSDR DEM2009F00000Spring · brokenDURING GROUND PERFORMANCE RUN FOR MX THE OPERATOR HEARD A LOUD NOISE AND THE NOSE OF THE ACFT FELL BY 10 INCHES. ENG WAS BROUGHT TO IDLE AND SHUTDOWN. AFTER EXITING THE COCKPIT, THE OPERATOR FOUND NLG DRAG SPRING HAD SEPARATED 8 INCHES AFT OF THE LWR YOKE ATJul 29, 2009 · N745FX · Cessna 208B · Landing Gear Retraction/Extension SystemSDR AXSA783FE7/29/09Chip Detector · contaminatedFLIGHT 8414 PVD-ACK - JUST AFTER LEVELING OFF AT 3000FT THE CHIP DETECTOR LIGHT ILLUMINATED. THE PILOT DECLARED AN EMERGENCY AND ELECTED TO RETURN TO PVD. THE ENGINE CONTINUED TO OPERATE NORMALLY THROUGH THE FLIGHT AND THE FLIGHT LANDED WITHOUT INCIDENT. MAJul 29, 2009 · N783FE · Cessna 208B · Turbine Engine Accessory DriveSDR 2009FA0000657Spring · brokenNLG DRAG SPRING SEPARATED 6 INCHES AFT OF THE LOWER LUG ATTACHMENT HOLES DURING GROUND RUN AT POWER. VISUAL INSP SUGGESTED A LARGE CORROSION PIT IN LWR WALL NOT VISIBLE FROM THE EXTERIOR SURFACE AS THE STARTING POINT FOR THE BREAK.Jul 29, 2009 · N745FX · Cessna 208B · Nose/Tail Landing Gear Strut/AxleSDR COEA2009072202711Spar · crackedDURING PREFLIGHT; FLIGHT 7678 AT PDX PILOT NOTICED CRACK IN RIGHT HORIZONTAL STABILIZER AFT SPAR STA 55.00. MAINTENANCE REMOVED AND REPLACED RT ELEVATOR. AIRCRAFT RETURNED TO SERVICE.Jul 22, 2009 · N711FX · Cessna 208B · Horizontal Stabilizer, Spar/RibSDR CA090615009Aileron Sys · malfunctioned(CAN) FACTORY INSTALLED BELLCRANK WAS NOTED AS BEING VISUALLY DIFFERENT. WHEN COMPARED TO A SERVICABLE PART FROM STOCK, IT APPEARS THAT THE STOP LUG ON THE LT (ONLY) WAS WELDED INCORRECTLY AT MFG. THE AILERON RIGGING IS CORRECT, WITH THE STOP ADJUSTED TO GIVEJun 15, 2009 · Cessna 208B · Aileron Control SystemSDR COEA2009061901711Torque Tube · damagedMX NOTED PLAY BETWEEN THE LT AND RT ELEVATORS. FOUND LT ELEVATOR TORQUE TUBE RIVETS LOOSE. RIVETS REMOVED AND FLANGE AND TORQUE TUBE HOLES FOUND ELONGATED. TORQUE TUBE ASSY REPLACED WITH NEW UNIT.Jun 4, 2009 · N711FX · Cessna 208B · Elevator StructureSDR BSYA2009032Fuel Control · unknownAIRCRAFT EN ROUTE FROM DPA TO LUK AT 9,000FT WHEN ENGINE STARTED CUTTING BACK ON IT'S OWN TO 1200LBS TORQUE AND NG FROM 98 PERCENT TO 91 PERCENT. BORESCOPED ENGINE, GROUND PERFORMANCE RUN ALL OK. REMOVED AND REPLACED FUEL CONTROL AS PRECAUTIONARY MEASURE.May 22, 2009 · N102AN · Cessna 208B · Fuel Control/Turbine EnginesSDR HSYA200905292Skin · chafedWING STRUR FAIRING CHAFING ON THE FUSELAGE SKIN AFT OF THE RT WING STRUT LOWER FITTING. DAMAGE WAS SUBMITTED TO MFG FOR REPAIR APPROVAL. AREA WAS REPAIRED IAW MFG ER INSTRUCTIONS S-208B-0219/01RDA.May 20, 2009 · N890FE · Cessna 208B · Fuselage Main, Plate/SkinSDR HSYA20090529Skin · chafedWING STRUT FAIRING CHAFING ON FUSELAGE SKIN AFT OF RT WING STRUT LOWER FITTING. DAMAGE WAS SUBMITTED TO MFG FOR REPAIR APPROVAL. AREA WAS REPAIRED IAW MFG ENGINEERING REPAIR INSTRUCTIONS S-208B0060/01RDA.May 20, 2009 · N952FE · Cessna 208B · Fuselage Main, Plate/SkinSDR CA090508005Fcu · failed(CAN) DURING START FUEL FLOW CAME UP TO 120 PPH THEN BECAME ERRATIC FLUCTUATING BETWEEN 100 PPH AND 300 PPH THEN WENT TO 0 PPH. ENG SHUTDOWN NORMALLY. FCU INSTALLED AND DURING POST INSTALL GROUND RUNS THE ENGINE WAS HARD TO START AND WOULD FLAMEOUT. CHECKED May 7, 2009 · Cessna 208B · Fuel Controlling SystemSDR AXSA958FE5/1/2009Vertical Gyro · failedDURING CRUISE FLIGHT 8302 (EWR-PBG) THE PILOT NOTED THAT THE PRIMARY LEFT ATTITUDE INDICATOR IN A 5 DEGREE RIGHT BANK WITH AIRCRAFT ON CORRECT HEADING. WITHIN 15 MINUTES THE LEFT ATTITUDE INDICATOR WAS IN A 10 BANK AND HEADING INDICATOR WAS OFF BY 20 DEGREES.May 1, 2009 · N958FE · Cessna 208B · Attitude Gyro and Indicating SystemSDR 2009FA0000342Rod Bearing · defectiveDEFECT REPORT GENERATED BASED ON A FAILURE THAT THE MX FOUND BY CHANCE WHILE PERFORMING ANOTHER INSP. FWDING FOR YOUR REVIEW AND SUBMITTAL THROUGH THE QC DEPARTMENT.. MX FOUND ONE OF THESE FLAP CONTROL ROD ENDS TO BE DEFECTIVE WHILE PERFORMING OTHER MX AND UPApr 30, 2009 · N684SA · Cessna 208B · Trailing Edge Flap Control SystemSDR COEA2009041002728Wire · chafedFOUND FUEL SELECTOR WARNING CIRCUIT BREAKER TRIPPED AND FUEL SELECT OFF ENUNCIATOR LIGHT ILLUMINATED AND REMAINED ON. CAPTAIN ELECTED TO EXECUTE AN AIR TURNBACK AND DECLARED AN EMERGENCY. ACFT LANDED AND TAXIED TO RAMP WITHOUT INCIDENT. FOUND WD41 WIRE BETWEEApr 10, 2009 · N728FX · Cessna 208B · Fuel System WiringSDR BSYA2009023Circuit Breaker · poppedAIRCRAFT TAKEOFF OUT OF LCK, FLAPS WOULD NOT RETRACT. AIRCRAFT RETURNED TO LCK. MAINTENANCE FOUND CIRCUIT BREAKER POPPED. RESET BREAKER, OPS CHECKED GOOD.Apr 9, 2009 · N105AN · Cessna 208B · Trailing Edge Flap Control System
Back to Textron 208B