# Service difficulty reports: U/A Canada PT6A-114

A list on [U/A Canada PT6A-114](https://openairdocs.org/engine/u-a-canada-pt6a-114.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 164 reports

- [SDR 141A2026062900001](https://openairdocs.org/sdr/141A2026062900001.md): Engine · faulted · Jun 29, 2026 · N9481F · Cessna 208 · Engine (Reciprocating)
  > DURING 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 8000FT
- [SDR ENHA202208150001](https://openairdocs.org/sdr/ENHA202208150001.md): Engine · unknown · Aug 13, 2022 · N9536P · Cessna 208 · Engine (Turbine/Turboprop)
  > AFTER 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. M
- [SDR ENHA202202110001](https://openairdocs.org/sdr/ENHA202202110001.md): Engine · flamed out · Feb 10, 2022 · N9536P · Cessna 208 · Engine (Turbine/Turboprop)
  > DURING 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.
- [SDR 2017F00000](https://openairdocs.org/sdr/2017F00000.md): O-Ring · cut · Oct 29, 2016 · N9539F · Cessna 208 · Landing Gear Brake System
  > LEFT BRAKE CALIPER, BRAKE PUCK O-RING FAILED, CUT. AIRCRAFT LOST BRAKING CONTROL TO THE LEFT
- [SDR EPUA20160422001](https://openairdocs.org/sdr/EPUA20160422001.md): Drive Assy · separated · Apr 22, 2016 · N750RV · Cessna 208B · Turbine Engine Accessory Drive
  > STANDBY 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 ASSE
- [SDR CA160115007](https://openairdocs.org/sdr/CA160115007.md): Regulator · stuck · Jan 13, 2016 · Cessna 208B · Crew Oxygen System
  > (CAN) O2 LEVER INOPERATIVE, STUCK IN ON POSITION.
- [SDR CA151026006](https://openairdocs.org/sdr/CA151026006.md): Bracket · worn · Oct 23, 2015 · Cessna 208B · Rudder Control System
  > (CAN) RUDDER PEDAL BRACKET FOUND WITH ELONGATED HOLES WHERE BRAKE MASTER CYLINDER ATTACHES AND SPACER FASTENER SHEARED.
- [SDR MTNA081220150001](https://openairdocs.org/sdr/MTNA081220150001.md): Engine · unknown · Aug 12, 2015 · N924FE · Cessna 208B · Engine (Turbine/Turboprop)
  > SUSPECTED ENGINE FAILURE IN FLIGHT, RESULTING IN ACFT DITCHING.
- [SDR 2015F00099](https://openairdocs.org/sdr/2015F00099.md): Boot · debonded · Jun 22, 2015 · N9481F · Cessna 208 · Propeller/Rotor Anti-Ice/De-Ice System
  > ALL 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.
- [SDR MTNA05152015001](https://openairdocs.org/sdr/MTNA05152015001.md): Engine · smoke · May 15, 2015 · N924FE · Cessna 208B · Engine (Turbine/Turboprop)
  > ON 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 LAN
- [SDR CA141029012](https://openairdocs.org/sdr/CA141029012.md): Transmission · failed · Oct 28, 2014 · Cessna 208B · Trailing Edge Flap Control System
  > (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.
- [SDR CA140905003](https://openairdocs.org/sdr/CA140905003.md): Skin · cracked · Sep 4, 2014 · Cessna 208B · Horizontal Stabilizer, Plate/Skin
  > (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 FOU
- [SDR DEMA2014063000002](https://openairdocs.org/sdr/DEMA2014063000002.md): Engine · failed · Jun 27, 2014 · N929FE · Cessna 208B · Engine (Turbine/Turboprop)
  > DURING 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
- [SDR CA140512002](https://openairdocs.org/sdr/CA140512002.md): Bulkhead · cracked · May 7, 2014 · Cessna 208B · Wheel/Ski/Float
  > (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.
- [SDR CA140128016](https://openairdocs.org/sdr/CA140128016.md): Bolt · wrong part · Jan 26, 2014 · Cessna 208B · Ailerons
  > (CAN) INCORRECT BOLTS FOUND INSTALLED IN LT & RT AILERON OUTER, WING, PUSHROD AFT ATTACH LOCATION. PN AN4H13A, DRILLED HEAD FOR LOCKWIRE, FOUND NOT INSTALLED.
- [SDR MK9A201401170001](https://openairdocs.org/sdr/MK9A201401170001.md): Engine · smoke · Jan 16, 2014 · N825MA · Cessna 208B · Engine (Turbine/Turboprop)
  > AFTER SHUTDOWN SMOKE WAS OBSERVED COMING FROM THE ENGINE.
- [SDR CA131230003](https://openairdocs.org/sdr/CA131230003.md): Indicator · failed · Dec 27, 2013 · Cessna 208B · Engine Oil Pressure
  > (CAN) DURING CRUISE OIL PRESSURE FLICKERED ABOUT 5 PSI AND REDUCED TO JUST ABOVE 85 PSI AND STAYED THERE THROUGHOUT ALL POWER RANGES.
- [SDR CA131201003](https://openairdocs.org/sdr/CA131201003.md): Engine · distressed · Nov 15, 2013 · Cessna 208B · Engine (Turbine/Turboprop)
  > (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 PERFORME
- [SDR CA130703001](https://openairdocs.org/sdr/CA130703001.md): Indicator · malfunctioned · Jun 28, 2013 · Cessna 208B · Engine RPM Indicating System
  > (CAN) DURING ENGINE START, ENGINE SLOW TO ACCELERATE. REPLACED NG INDICATOR.
- [SDR CA131102004](https://openairdocs.org/sdr/CA131102004.md): Actuator · failed · Jun 19, 2013 · Cessna 208B · Trailing Edge Flap Actuator
  > (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 REPLA
- [SDR CA130614005](https://openairdocs.org/sdr/CA130614005.md): Engine · malfunctioned · Jun 9, 2013 · Cessna 208B · Engine (Turbine/Turboprop)
  > (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 SUBSTANTI
- [SDR AWHA20130530001](https://openairdocs.org/sdr/AWHA20130530001.md): Drive Shaft · detached · May 29, 2013 · N897FE · Cessna 208B · Engine Fuel Pump
  > DURING 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 M
- [SDR CA130516011](https://openairdocs.org/sdr/CA130516011.md): Support Bracket · cracked · Apr 4, 2013 · Cessna 208 · Trailing Edge Flaps
  > (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.
- [SDR CA130325023](https://openairdocs.org/sdr/CA130325023.md): Clamp · broken · Mar 22, 2013 · Cessna 208B · Crew Oxygen System
  > (CAN) HANDLE FOR ACTIVATING CREW OXYGEN SYSTEM NOT ACTIVATING BOTTLE, SEEMS LIKE LINKAGE IS JAMMED. CLAMPING BOLT, PN S2323-8 FOUND BROKEN AND REPLACED.
- [SDR CA121109004](https://openairdocs.org/sdr/CA121109004.md): Mount · cracked · Nov 8, 2012 · Cessna 208 · Engine Mount Section
  > (CAN) RT ENGINE MOUNT BRACKET FOUND TO BE CRACKED AT THE FWD ENDS OF REINFORCEMENT GUSSETS ACROSS WELD AREAS.
- [SDR CA121106010](https://openairdocs.org/sdr/CA121106010.md): Fcu · power loss · Nov 5, 2012 · Cessna 208B · Fuel Control/Turbine Engines
  > (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.
- [SDR CA121102007](https://openairdocs.org/sdr/CA121102007.md): Pressure Switch · unknown · Oct 31, 2012 · Cessna 208B · Standard Practices/Structures
  > (CAN) CAUTION ANNUNCIATOR LIGHT FLASHING ON & OFF WITH SYSTEM SELECTED OFF.
- [SDR CA121031004](https://openairdocs.org/sdr/CA121031004.md): Pump · leaking · Oct 26, 2012 · Cessna 208B · Engine Fuel Pump
  > (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 CLEA
- [SDR CA121022017](https://openairdocs.org/sdr/CA121022017.md): Shimmy Dampener · malfunctioned · Oct 19, 2012 · Cessna 208B · Landing Gear Steering System
  > (CAN) DURING TAKEOFF ROLL, RT RUDDER PEDAL BEGAN VIBRATING THROUGH 40 KIAS AND VIOLENTLY INTENSIFIED UP TO 65 KIAS.
- [SDR 2012FA0000703](https://openairdocs.org/sdr/2012FA0000703.md): Sleeve · deformed · Oct 17, 2012 · N208JW · Cessna 208 · Turbine Engine Reduction Gear
  > ENGINE 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 S
- [SDR CA120823002](https://openairdocs.org/sdr/CA120823002.md): Fuel Control · inoperative · Aug 18, 2012 · Cessna 208B · Fuel Control/Turbine Engines
  > (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.
- [SDR CA120822016](https://openairdocs.org/sdr/CA120822016.md): Panel · bulged · Jun 5, 2012 · Cessna 208B · Standard Practices/Structures
  > (CAN) LEFT INBD TKS PANEL BULGED.
- [SDR 2012FA0000421](https://openairdocs.org/sdr/2012FA0000421.md): Hose · unserviceable · Jun 1, 2012 · N4687B · Cessna 208B · Turbine Engine Oil System
  > 12.5" LONG HOSE TO THE SECONDARY EXHAUST WAS FOUND TO HAVE SWOLLEN UP INTERNALLY.
- [SDR 2012FA0000359](https://openairdocs.org/sdr/2012FA0000359.md): Vent Line · collapsed · May 18, 2012 · N4625B · Cessna 208B · Turbine Engine Oil System
  > THE 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 WA
- [SDR HSYA2012022312412](https://openairdocs.org/sdr/HSYA2012022312412.md): Engine · contaminated · Feb 23, 2012 · N904FE · Cessna 208B · Engine (Turbine/Turboprop)
  > PILOT 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 TUR
- [SDR CA120222003](https://openairdocs.org/sdr/CA120222003.md): Plate · cracked · Feb 21, 2012 · Cessna 208 · Pitot/Static System
  > (CAN) RT WING PITOT TUBE FOUND TO BE CRACKED FORWARD OF ITS MOUNTING PLATE.
- [SDR MT9A2012F00000](https://openairdocs.org/sdr/MT9A2012F00000.md): Engine · failed · Dec 12, 2011 · N208N · Cessna 208B · Engine (Turbine/Turboprop)
  > SHORTLY 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 ROTATIN
- [SDR CA111129001](https://openairdocs.org/sdr/CA111129001.md): Engine · malfunctioned · Nov 11, 2011 · Engine (Turbine/Turboprop)
  > (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 AUTHORITIE
- [SDR CA111030002](https://openairdocs.org/sdr/CA111030002.md): Engine · malfunctioned · Sep 7, 2011 · Cessna 208 · Engine (Turbine/Turboprop)
  > (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. HOWEVE
- [SDR CA110611001](https://openairdocs.org/sdr/CA110611001.md): B-Nut · broken · Jun 8, 2011 · Cessna 208 · Hydraulic System, Main
  > THE 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. THE
- [SDR MTNA02231100002](https://openairdocs.org/sdr/MTNA02231100002.md): Engine · malfunctioned · Feb 23, 2011 · N962FE · Cessna 208B · Engine (Turbine/Turboprop)
  > DURING 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,
- [SDR CA110208001](https://openairdocs.org/sdr/CA110208001.md): Engine · flamed out · Jan 21, 2011 · Cessna 208B · Engine (Turbine/Turboprop)
  > (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 ACFT
- [SDR CA110208002](https://openairdocs.org/sdr/CA110208002.md): Engine · failed · Jan 20, 2011 · Cessna 208B · Engine (Turbine/Turboprop)
  > (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 EVERYTHING
- [SDR HSYA2010122110](https://openairdocs.org/sdr/HSYA2010122110.md): Controller · failed · Dec 21, 2010 · N952FE · Cessna 208B · Electrical Power System
  > PRIOR 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 ANNUN
- [SDR 2010FA0001063](https://openairdocs.org/sdr/2010FA0001063.md): Case · broken · Sep 4, 2010 · N4687B · Cessna 208B · Propeller Feathering/Reversing
  > PILOT 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.
- [SDR BSYA2010021](https://openairdocs.org/sdr/BSYA2010021.md): Chip Detector · contaminated · Apr 1, 2010 · N9448B · Cessna 208B · Turbine Engine Accessory Drive
  > EN 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 MIN
- [SDR HSYA2010022510](https://openairdocs.org/sdr/HSYA2010022510.md): Fuel Control · failed · Feb 25, 2010 · N997FE · Cessna 208B · Fuel Control/Turbine Engines
  > DURING 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
- [SDR MTNA0110001](https://openairdocs.org/sdr/MTNA0110001.md): Unknown · smoke · Jan 22, 2010 · N924FE · Cessna 208B · Air Distribution System
  > THE 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
- [SDR 2010FA0000020](https://openairdocs.org/sdr/2010FA0000020.md): Tube · corroded · Jan 5, 2010 · N4655B · Cessna 208B · Fuel Heater
  > THE 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 LEAKS
- [SDR CA100127007](https://openairdocs.org/sdr/CA100127007.md): Attach Fitting · damaged · Dec 25, 2009 · Cessna 208B · Wing, Attach Fittings
  > (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.

Next page: https://openairdocs.org/engine/u-a-canada-pt6a-114/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/engine/u-a-canada-pt6a-114/reports

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