U/A Canada PT6A-114

Service difficulty reports · 164

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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 engine_model_key = 'PT6A114'
  ORDER BY difficulty_date DESC"

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SDR 141A2026062900001Engine · faultedDURING CLIMB TO CRUISE, PASSING THROUGH 6000 TO 8000 FT THE ENGINE ITT WAS AT 740, WITH THE POWER BEING SET AT ONLY 1200LBS OF TORQUE. WE WERE ONLY ABLE TO MAINTAIN CLIMB RATE OF 200-300 FPM WITH AIRSPEED AT 95-100 INDICATED KNOTS. AT CRUISE ALTITUDE OF 8000FTJun 29, 2026 · N9481F · Cessna 208 · Engine (Reciprocating)SDR ENHA202208150001Engine · unknownAFTER BEING CLEARED FOR TAKEOFF, PILOT LINED UP ON RUNWAY 20R IN KENAI AND ADVANCED POWER AND THEN PILOT NOTICED AN UNUSUAL SOUND COMING FROM THE ENGINE COMPARTMENT. PILOT THEN REDUCED POWER AND ABORTED THE TAKEOFF AND PROCEEDED TO TAXI BACK TO THE HANGER. MAug 13, 2022 · N9536P · Cessna 208 · Engine (Turbine/Turboprop)SDR ENHA202202110001Engine · flamed outDURING CRUISE FLIGHT, ENGINE SURGED, FLAMED OUT AND RESTARTED ON ITS OWN. TORQUE WENT FROM 1600 FT/LBS DOWN TO APPROXIMATELY 800 FT/LBS, AND JUMPED BACK UP TO 1600 FT/LBS. PILOT RETURNED TO BASE. NO TROUBLESHOOTING WAS BEEN PERFORMED AT TIME OF SUBMISSION.Feb 10, 2022 · N9536P · Cessna 208 · Engine (Turbine/Turboprop)SDR 2017F00000O-Ring · cutLEFT BRAKE CALIPER, BRAKE PUCK O-RING FAILED, CUT. AIRCRAFT LOST BRAKING CONTROL TO THE LEFTOct 29, 2016 · N9539F · Cessna 208 · Landing Gear Brake SystemSDR EPUA20160422001Drive Assy · separatedSTANDBY POWER ANNUNCIATOR LIGHT WON’T GO OUT. INSPECTED ACFT & FOUND THAT THE RETAINING RING FOR THE STANDBY ALTERNATOR DRIVE PULLEY HAD FAILED. DUE TO THIS FAILURE THE DRIVE PULLEY HAD MIGRATED OUT OF THE HOUSING ASSEMBLY & WAS LYING IN THE ENG COWLING ASSEApr 22, 2016 · N750RV · Cessna 208B · Turbine Engine Accessory DriveSDR CA160115007Regulator · stuck(CAN) O2 LEVER INOPERATIVE, STUCK IN ON POSITION.Jan 13, 2016 · Cessna 208B · Crew Oxygen SystemSDR CA151026006Bracket · worn(CAN) RUDDER PEDAL BRACKET FOUND WITH ELONGATED HOLES WHERE BRAKE MASTER CYLINDER ATTACHES AND SPACER FASTENER SHEARED.Oct 23, 2015 · Cessna 208B · Rudder Control SystemSDR MTNA081220150001Engine · unknownSUSPECTED ENGINE FAILURE IN FLIGHT, RESULTING IN ACFT DITCHING.Aug 12, 2015 · N924FE · Cessna 208B · Engine (Turbine/Turboprop)SDR 2015F00099Boot · debondedALL 3 PROPELLER DE-ICE BOOTS DEBONDED FROM BLADE IN FLIGHT CAUSING A SEVERE VIBRATION. LANDED AT NEAREST AIRPORT WITH OUT INCIDENT. VISUAL INSPECTION REVEALED DEBONDING OF MOST OF THE BOOTS APPEARS TO BE A POORLY APPLIED BONDING APPLICATION.Jun 22, 2015 · N9481F · Cessna 208 · Propeller/Rotor Anti-Ice/De-Ice SystemSDR MTNA05152015001Engine · smokeON CLIMBOUT, AT APPROXIMATELY 2600 FT OF FLIGHT, THE PILOT REPORTED SMOKE COMING INTO THE COCKPIT FROM THE RT SIDE VENT. ALSO NOTICED AN ODOR OF BURNING OIL. ALL ENGIME INSTRUMENTS INDICATION WERE NORMAL. THE PILOT ELECTED TO RETURN TO AIRPORT. THE ACFT LANMay 15, 2015 · N924FE · Cessna 208B · Engine (Turbine/Turboprop)SDR CA141029012Transmission · failed(CAN) FLAP MOTOR CIRCUIT BREAKER TRIPPED ON ARRIVAL, FLAPS FAILED AT 10 DEGREE POSITION. FLAP TRANSMISSION REPLACED IAW 27-50-01. OPS CHECK C/O.Oct 28, 2014 · Cessna 208B · Trailing Edge Flap Control SystemSDR CA140905003Skin · cracked(CAN) DURING A SCHEDULED MAINTENANCE INSPECTION THE HORIZONTAL STABILIZER WAS NOTED TO HAVE A VERY LOUD OIL CANNING NOISE COMING FROM INSIDE THE TAIL SECTION WITH LIGHT PRESSURE APPLIED UP OR DOWN ON THE STABILIZER TIPS. UPON FURTHER INVESTIGATION THE AME FOUSep 4, 2014 · Cessna 208B · Horizontal Stabilizer, Plate/SkinSDR DEMA2014063000002Engine · failedDURING CRUISE, THE PILOT NOTICED A FLUCTUATION OF THE ENGINE TORQUE INDICATOR. THE FLUCTUATION WAS BETWEEN 50-100 FT/LBS. IMMEDIATELY FOLLOWING THE TORQUE FLUCTUATION, THE OIL PRESSURE DROPPED AND THE OIL TEMPERATURE ROSE. AN EMERGENCY WAS DECLARED AND THE Jun 27, 2014 · N929FE · Cessna 208B · Engine (Turbine/Turboprop)SDR CA140512002Bulkhead · cracked(CAN) DISCOVERED ON PRESEASON INSPECTION, WHILE COMPLETING THE ANNUAL COMPLETE FLOAT INSPECTION. RIGHT FLOAT BULKHEAD NR 9, DISCOVERED MULTIPLE CRACKS RADIATING FROM CORNERS. CURRENTLY CONSULTING WITH ENGINEERING REPAIR AND LOGISTICS ON REPAIR .May 7, 2014 · Cessna 208B · Wheel/Ski/FloatSDR CA140128016Bolt · wrong part(CAN) INCORRECT BOLTS FOUND INSTALLED IN LT & RT AILERON OUTER, WING, PUSHROD AFT ATTACH LOCATION. PN AN4H13A, DRILLED HEAD FOR LOCKWIRE, FOUND NOT INSTALLED.Jan 26, 2014 · Cessna 208B · AileronsSDR MK9A201401170001Engine · smokeAFTER SHUTDOWN SMOKE WAS OBSERVED COMING FROM THE ENGINE.Jan 16, 2014 · N825MA · Cessna 208B · Engine (Turbine/Turboprop)SDR CA131230003Indicator · failed(CAN) DURING CRUISE OIL PRESSURE FLICKERED ABOUT 5 PSI AND REDUCED TO JUST ABOVE 85 PSI AND STAYED THERE THROUGHOUT ALL POWER RANGES.Dec 27, 2013 · Cessna 208B · Engine Oil PressureSDR CA131201003Engine · distressed(CAN) THE PILOT REPORTED ENGINE DISTRESS AFTER JUST LEVELING OFF AT CRUISE, 6000 FT. THE PILOT HEARD A LOUD NOISE, THEN HEARD THE ENGINE WINDING DOWN WHILE EXPERIENCING LOSS OF POWER. THE PILOT TRIED TO RE-START THE ENGINE WITHOUT SUCCESS. THE PILOT PERFORMENov 15, 2013 · Cessna 208B · Engine (Turbine/Turboprop)SDR CA130703001Indicator · malfunctioned(CAN) DURING ENGINE START, ENGINE SLOW TO ACCELERATE. REPLACED NG INDICATOR.Jun 28, 2013 · Cessna 208B · Engine RPM Indicating SystemSDR CA131102004Actuator · failed(CAN) DURING A PREFLIGHT WALK AROUND, IT WAS FOUND THAT THE FLAP SYS WAS MAKING A GRINDING NOISE WHEN THE FLAPS WHERE SELECTED UP. MAINTENANCE DISCOVERED THAT THE FLAP SYS ACTUATOR HAD FAILED DUE TO HIGH CYCLES. THERE IS NO AIRWORTHINESS LIMITATIONS TO REPLAJun 19, 2013 · Cessna 208B · Trailing Edge Flap ActuatorSDR CA130614005Engine · malfunctioned(CAN) AFTER DROPPING OFF SKYDIVERS, AS THE ACFT WAS RETURNING TO BASE, THE ENGINE LOST POWER. UNABLE TO CLEAR TREES ON APPROACH, THE PILOT ELECTED TO SET THE ACFT DOWN IN A FIELD. THE PILOT, ONLY 1 ONBOARD, WAS SERIOUSLY INJURED. THE ACFT SUFFERED SUBSTANTIJun 9, 2013 · Cessna 208B · Engine (Turbine/Turboprop)SDR AWHA20130530001Drive Shaft · detachedDURING ROUTINE FUEL PUMP GARLOC SEAL REPLACEMENT FOR LEAKAGE, THE MECHANIC INSPECTED THE FUEL PUMP DRIVE GEAR AND IT BECAME DECOUPLED FROM THE FUEL PUMP. THIS IS NOT NORMAL FOR THIS MODEL PUMP. THE ACCESSORY DRIVE GEAR IS HOLLOW AND HAD THE FUEL PUMP DRIVE MMay 29, 2013 · N897FE · Cessna 208B · Engine Fuel PumpSDR CA130516011Support Bracket · cracked(CAN) FLAP ACTUATOR BRACKET ASSY FOUND CRACKED AT LIGHTING RELIEF HOLES AND ACROSS DOUBLER, PN 2611144-5 FROM FLANGE TO LIGHTING HOLE DURING PHASE INSPECTION. SERVICE KIT 208-158 INSTALLED TO RECTIFY PROBLEM.Apr 4, 2013 · Cessna 208 · Trailing Edge FlapsSDR CA130325023Clamp · broken(CAN) HANDLE FOR ACTIVATING CREW OXYGEN SYSTEM NOT ACTIVATING BOTTLE, SEEMS LIKE LINKAGE IS JAMMED. CLAMPING BOLT, PN S2323-8 FOUND BROKEN AND REPLACED.Mar 22, 2013 · Cessna 208B · Crew Oxygen SystemSDR CA121109004Mount · cracked(CAN) RT ENGINE MOUNT BRACKET FOUND TO BE CRACKED AT THE FWD ENDS OF REINFORCEMENT GUSSETS ACROSS WELD AREAS.Nov 8, 2012 · Cessna 208 · Engine Mount SectionSDR CA121106010Fcu · power loss(CAN) POWER LOSS DURING CRUISE FLIGHT, TWO TIMES. POWER DROPPED FROM 1600 TORQUE TO 1350. FUEL FLOW DROPPED FROM 350 TO 320. THIS LASTED APPROXIMATELY 20 SECONDS EACH.Nov 5, 2012 · Cessna 208B · Fuel Control/Turbine EnginesSDR CA121102007Pressure Switch · unknown(CAN) CAUTION ANNUNCIATOR LIGHT FLASHING ON & OFF WITH SYSTEM SELECTED OFF.Oct 31, 2012 · Cessna 208B · Standard Practices/StructuresSDR CA121031004Pump · leaking(CAN) NAVY BLUE DYE FLUID FOUND ON AFTERNOON WALK AROUND. BLUE FLUID COULD BE SEEN ON LT SIDE OF FCU. STARTER GENERATOR HAS A LINE WITH BLUE ON IT. LOWER COWLING HAS BLUE FLUID ON IT. ON MORNING WALK AROUND ALL ENGINE COWLINGS & ENGINE COMPONENTS WHERE CLEAOct 26, 2012 · Cessna 208B · Engine Fuel PumpSDR CA121022017Shimmy Dampener · malfunctioned(CAN) DURING TAKEOFF ROLL, RT RUDDER PEDAL BEGAN VIBRATING THROUGH 40 KIAS AND VIOLENTLY INTENSIFIED UP TO 65 KIAS.Oct 19, 2012 · Cessna 208B · Landing Gear Steering SystemSDR 2012FA0000703Sleeve · deformedENGINE LOST ABILITY TO GOVERN THE PROPELLER RPM DRIVING THE PROPELLER TO FEATHER. LOSS OF PROPELLER RPM LED TO A NO-POWER SITUATION REQUIRING A NO POWER GLIDING APPROACH BACK TO DEPARTURE AIRFIELD. TROUBLESHOOTING FOUND THE PROBLEM TO BE A ROTATED PROPELLER SOct 17, 2012 · N208JW · Cessna 208 · Turbine Engine Reduction GearSDR CA120823002Fuel Control · inoperative(CAN) P3 FAILURE AFTER LANDING. PILOT WENT TO TAXI INTO FBO AND ENGINE WAS NOT RESPONDING TO POWER LEVER MOVEMENT. ENGINE NG ROLLED BACK TO AT 50 PERCENT, VACUUM LOW LIGHT CAME ON AND STANDBY POWER CAME ON. PILOT USED EMERGENCY POWER LEVER TO TAXI AIRCRAFT.Aug 18, 2012 · Cessna 208B · Fuel Control/Turbine EnginesSDR CA120822016Panel · bulged(CAN) LEFT INBD TKS PANEL BULGED.Jun 5, 2012 · Cessna 208B · Standard Practices/StructuresSDR 2012FA0000421Hose · unserviceable12.5" LONG HOSE TO THE SECONDARY EXHAUST WAS FOUND TO HAVE SWOLLEN UP INTERNALLY.Jun 1, 2012 · N4687B · Cessna 208B · Turbine Engine Oil SystemSDR 2012FA0000359Vent Line · collapsedTHE PILOT REPORTED AN UNUSUAL AMOUNT OF OIL WAS BEING CONSUMED, AND ON HIS INBD FLIGHT THE OIL PRESSURE GAUGE WAS FLUCTUATING. THERE WERE NO VISIBLE SIGNS OF AN EXTERNAL OIL LEAK. ON THE GROUND RUN MX ALSO NOTED THE TORQUE WAS FLUCTUATING. WHEN BLEED AIR WAMay 18, 2012 · N4625B · Cessna 208B · Turbine Engine Oil SystemSDR HSYA2012022312412Engine · contaminatedPILOT REPORTED DURING TAXI, A STRONG CHEMICAL ODOR IN COCKPIT. TAXIED ACFT BACK TO THE BLOCKS. FREIGHT INSPECTED AND NO DISCREPANCIES FOUND. MX TROUBLESHOT AND FOUND THAT THE APPARENT CAUSE TO BE RESIDUAL RECOVERY WASH FLUID FROM A COMPLETED COMPRESSOR TURFeb 23, 2012 · N904FE · Cessna 208B · Engine (Turbine/Turboprop)SDR CA120222003Plate · cracked(CAN) RT WING PITOT TUBE FOUND TO BE CRACKED FORWARD OF ITS MOUNTING PLATE.Feb 21, 2012 · Cessna 208 · Pitot/Static SystemSDR MT9A2012F00000Engine · failedSHORTLY AFTER TAKEOFF, ENROUTE, ACFT EXPERIENCED AN ENGINE FLAMEOUT ACCOMPANIED BY A LOUD BANG. THE PILOT WAS ABLE TO SAFELY LAND WITH NO FURTHER INCIDENTS. MX INVESTIGATED AND FOUND THAT THE ENGINE HAD SUFFERED A CATASTROPHIC FAILURE, DESTROYING ALL ROTATINDec 12, 2011 · N208N · Cessna 208B · Engine (Turbine/Turboprop)SDR CA111129001Engine · malfunctioned(CAN) TEN MINUTES AFTER TAKEOFF, THE PILOT REPORTED THAT THE ENG HAD AN UNUSUAL NOISE & HE DECIDED TO RETURN TO THE AIRPORT. THE ACFT DID NOT MAKE IT BACK & CRASHED ON A ROAD. THE TWO PEOPLE INJURED, OFFER OF ASSISTANCE WILL BE MADE TO THE CHINESE AUTHORITIENov 11, 2011 · Engine (Turbine/Turboprop)SDR CA111030002Engine · malfunctioned(CAN) DURING LANDING ROLL, THE ACFT DEPARTED THE SIDE OF THE RUNWAY RT AND CAME TO A STOP 10 METERS FROM THE RUNWAY EDGE WITH THE NOSE GEAR COLLAPSED. THERE WERE NO INJURIES, AND THE ENGINE WAS ORIGINALLY BELIEVED TO BE A NON CONTRIBUTOR TO THIS EVENT. HOWEVESep 7, 2011 · Cessna 208 · Engine (Turbine/Turboprop)SDR CA110611001B-Nut · brokenTHE ACFT LANDED AND WAS PROCEEDING DOWN THE RUNWAY NORMALLY UNTIL THE PILOT APPLIED THE BRAKES IN PREPARATION FOR LT TURN ONTO TAXIWAY, THE ACFT STARTED TURNING TO THE LT AND PROCEEDED OFF THE RUNWAY AND DOWN AN EMBANKMENT JUST BEFORE THE TAXIWAY TURNOFF. THEJun 8, 2011 · Cessna 208 · Hydraulic System, MainSDR MTNA02231100002Engine · malfunctionedDURING CLIMB AT 10000 FT THE PILOT HEARD A LOUD BANG AND HAD A SEVERE VIBRATION. THE OIL PRESSURE DROPPED THE PILOT SHUT THE ENGINE DOWN AND FEATHERED THE PROP. THE PILOT MADE A SUCCESSFUL LANDING AT (MBAC) AT THE DIRECTION OF MIA. ATC,Feb 23, 2011 · N962FE · Cessna 208B · Engine (Turbine/Turboprop)SDR CA110208001Engine · flamed out(CAN) ACCIDENT ON A CARGO FLIGHT, DURING APPROACH, THE PILOT COULD NOT REDUCE POWER BELOW 1400 FT-LB AND THE THROTTLE LEVER WAS UNRESPONSIVE. DECIDED TO RETURN. TWO UNSUCCESSFUL LANDING ATTEMPTS WERE MADE AND ON THE 3RD ATTEMPT, THE ENGINE FLAMED OUT. THE ACFTJan 21, 2011 · Cessna 208B · Engine (Turbine/Turboprop)SDR CA110208002Engine · failed(CAN) IFSD/FORCED LANDING SHORTLY AFTER T/O, THE PILOT FELT VIBRATIONS IN HIS CONTROL COLUMN FOLLOWED BY A LOSS OF POWER. THE THROTTLE WAS RETARDED AND THE VIBRATION REDUCED. RE-ADVANCING THE THROTTLE RESULTED IN A MOMENTARY INCREASE OF POWER BEFORE EVERYTHINGJan 20, 2011 · Cessna 208B · Engine (Turbine/Turboprop)SDR HSYA2010122110Controller · failedPRIOR TO STARTING AN ILS APPROACH, STBY PWR LIGHT ILLUMINATED. NOTED 3 OF BUSS 1 C/B'S HAD POPPED, ALL SYSTEMS FUCTIONED NORMAL. TURNED LIGHTS OFF & ANTI-ICE SYSTEM LEFT ON DUE TO ICING CONDITIONS. TURNED ON TAXI & LANDING LIGHTS BEFORE LANDING & SEVERAL ANNUNDec 21, 2010 · N952FE · Cessna 208B · Electrical Power SystemSDR 2010FA0001063Case · brokenPILOT REPORTED TO MX THAT WITH THE THROTTLE LEVER AT THE GATE (FWD SIDE OF GATE) THE ENGINE WAS GOING INTO REVERSE. THE SUBSEQUENT INSP FOUND THE REVERSE ROPE CASING HAD BROKEN AT THE SWIVEL JOINT. THE REVERSE ROPE ITSELF WAS STILL ATTACHED.Sep 4, 2010 · N4687B · Cessna 208B · Propeller Feathering/ReversingSDR 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 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 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 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 Fittings
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