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

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

Newest first. General aviation reporting is voluntary.

Page 1 of 15 · 705 reports

- [SDR GAJA202610070223](https://openairdocs.org/sdr/GAJA202610070223.md): Engine · surges · Oct 1, 2026 · N984AC · Cessna 208B · Engine (Turbine/Turboprop)
  > DURING CRUISE AT 13,000FT, THE PILOT EXPERIENCED A TEMPORARY UNCOMMANDED POWER SURGE BUT THE AIRCRAFT SETTLED BACK INTO NORMAL CRUISE PERFORMANCE SETTING. WITHIN THE NEXT 2 MINUTES, THE UNCOMMANDED CONTROL COMMENCED AGAIN ONLY THIS TIME PROCEEDED TO REDLINE A
- [SDR DEMA202605270001](https://openairdocs.org/sdr/DEMA202605270001.md): Fuel Control · uncontrollable · May 19, 2026 · N774FE · Cessna 208B · Fuel Control/Turbine Engines
  > LOSS OF ENGINE THROTTLE RESPONSE FOLLOWED BY AN UNCOMMANDED ENGINE SHUTDOWN ON THE TAXIWAY PRIOR TO TAKEOFF. THE AIRCRAFT FUEL SYSTEM WAS CHECK FOR CONTAMINATION WITH NO APPRECIABLE WATER OR DEBRIS FOUND IN WING TANKS OR RESERVOIR. FIREWALL FUEL FILTER ASSEM
- [SDR 2026FA0000334](https://openairdocs.org/sdr/2026FA0000334.md): Bellows · faulted · May 4, 2026 · N347KA · Cessna 208B · Fuel Control/Turbine Engines
  > PILOT NOTICED AFTER DESCENT TO FLIGHT LEVEL 1500 FEET, LEVELING OFF AND ADDING POWER, TORQUE INDICATION DROPPED 200 AND RECOVERED ON ITS OWN WITH NO INPUT TO THE POWER LEVER. AFTER DISCUSSION WITH PRATT AND WHITTNEY, IT WAS DETERMINED THAT THE FUEL CONTROL DE
- [SDR ENHA 20250521862](https://openairdocs.org/sdr/ENHA%2020250521862.md): Regulator · sticking · May 20, 2025 · N410GV · Cessna 208B · Engine Bleed Air System
  > PILOT OBSERVED THE PILOT DOOR POST GETTING HOT. MECHANICS REPLACED THE BLEED AIR PRESSURE REGULATOR AND PROBLEM WAS RESOLVED.
- [SDR 1AZA2025F00117](https://openairdocs.org/sdr/1AZA2025F00117.md): Engine · abnormal · May 6, 2025 · N867HP · Cessna 208B · Powerplant System
  > ENGINE CHIP DETECTOR LIGHT ILLUMINATED IN FLIGHT,. LOW OIL PRESSURE LIGHT ILLUMINATED, LOW OIL PRESSURE INDICATED. POST-FLIGHT, REMOVED OIL SCREEN AND FOUND METAL CONTAMINATION
- [SDR 2025FA0000339](https://openairdocs.org/sdr/2025FA0000339.md): Engine · failed · Apr 22, 2025 · N781FE · Cessna 208B · Engine (Turbine/Turboprop)
  > PILOT REPORTED A CHIP LIGHT ILLUMINATED DURING APPROACH INTO ONT. BEGAN MONITORING PARAMETERS, AND HEARD A POP. OIL PRESSURE DROPPED FROM 101 TO 94 PSI. A FEW MOMENTS LATER SHE HEARD TO MORE POPS, THEN OIL PRESSURE WENT 0 AND ENGINE SHUT DOWN. PILOT DECLARED A
- [SDR ENHA2025013008](https://openairdocs.org/sdr/ENHA2025013008.md): Brake Pads · locked · Jan 29, 2025 · N1115M · Cessna 208B · Landing Gear Brake System
  > BRAKES LOCKED. MECHANICS LOOSENED THE PADS AND RETORQUED IAW C208MM 32-40-00. OPS CHECK WAS GOOD.
- [SDR ENHA 202410040001](https://openairdocs.org/sdr/ENHA%20202410040001.md): Tube · loose · Sep 30, 2024 · N411GV · Cessna 208B · Air Distribution System
  > BLEED AIR HEAT INOP, NO AIRFLOW AND HOT SMELL WHEN BLEED AIR HEAT IS TURNED ON. MECHANICS FOUND SCAT TUBE AT CABIN AIR VALVE HAD COME LOOSE. RE-SECURED IAW 208MM 21-41-00, OPS CHECK GOOD.
- [SDR K2AA2024092300730](https://openairdocs.org/sdr/K2AA2024092300730.md): Skin · corroded · Sep 23, 2024 · N347KA · Cessna 208B · Wing, Plate/Skin
  > LEFT HAND WING LEADING EDGE SKIN FOUND WITH CORROSION BEYOND LIMITS. RE-SKIN OF THE LH LEADING EDGE IS WORKABLE FROM THE MM AND SRM. HOWEVER THE REPAIR WILL PUT US OVER THE $25000 LIMIT WITH PARTS AND LABOR.
- [SDR 141A2024050700003](https://openairdocs.org/sdr/141A2024050700003.md): Unknown · odor · May 7, 2024 · N9481F · Cessna 208 · Air Distribution System
  > DURING CRUISE FLIGHT, CA AND FO NOTICED A STRONG BURNING SMELL, LIKE BURNING RUBBER AND PLASTIC. FLIGHT WAS DIVERTED AND MADE AN UNSCHEDULED LANDING. MAINTENANCE WAS DISPATCH AND PERFORMED THE INSPECTION WITH NO DEFECTS NOTED AND A GROUND PERFORMANCE RUN. NO S
- [SDR ENHA2024040800088](https://openairdocs.org/sdr/ENHA2024040800088.md): Unknown · odor · Apr 5, 2024 · N411GV · Cessna 208B · Air Distribution System
  > HOT ELECTRICAL SMELL. SMELL DISAPEARED ON TAXI BACK TO RAMP. SUSPECTED THAT DEICE FLUID WAS SPRAYED ON EXHAUST, MECHANICS INSPECTEDT ENGINE BAY, JUNCTION BOX, CIRCUIT BREAKER PANELS AND ALL WIRES BEHIND INSTRUMEENT PANEL, NO DEFECTS DETECTED.. PERFORMED RUNU
- [SDR 141A2024040200002](https://openairdocs.org/sdr/141A2024040200002.md): Master Cylinder · defective · Mar 29, 2024 · N1258B · Cessna 208B · Master Cylinder/Brake Valve
  > LEFT HAND BRAKE INEFFECTIVE. MAINTENANCE REPLACED LEFT HAND MASTER CYLINDER. PERFORMED HIGH SPEED TAXI. OPS CHECKED GOOD
- [SDR 2024F00088](https://openairdocs.org/sdr/2024F00088.md): Wire · chafed · Mar 20, 2024 · N750Z · Cessna 208B · Electrical Power System Wiring
  > SMOKE IN COCKPIT. DURING DESCENT THE FO NOTICED A BURNING SMELL FOLLOWED BY SMOKE COMING OUT OF THE AREA LOCATED BY THE RIGHT KNEE. ALL SYSTEMS AND INDICATIONS WERE NORMAL. MAINTENANCE FOUND A CHAFFED WIRING TO THE LAV CIRCUIT BREAKER BEHIND THE FO'S SIDE KICK
- [SDR 2024FA0000189](https://openairdocs.org/sdr/2024FA0000189.md): Fire Loop · broken · Feb 26, 2024 · N937CK · Cessna 208B · Fire Detection
  > DURING CRUISE, ENGINE FIRE ANNUNCIATOR ILLUMINATED FOR APPROX 3 SECONDS WITH WARNING HORN THEN EXTINGUISHED. THEN APPROX 10 SECONDS LATER IT OCCURRED AGAIN AND REPEATED THIS ABOUT EVERY 10-15 SECONDS. AFTER THE THIRD EVENT THE ANNUNCIATOR REMAINED ON. ALL ENGI
- [SDR 2024F00028](https://openairdocs.org/sdr/2024F00028.md): Belt · broken · Feb 8, 2024 · N857MA · Cessna 208B · Cabin Cooling System
  > SMELL OF SMOKE IN THE COCKPIT DUE AC BELT BREAKING
- [SDR 2024FA0000013](https://openairdocs.org/sdr/2024FA0000013.md): Line · cracked · Jan 9, 2024 · N864FE · Cessna 208B · Engine (Turbine/Turboprop)
  > SMOKE IN COCKPIT ON TAKEOFF.
- [SDR 2023F00337](https://openairdocs.org/sdr/2023F00337.md): V-Belt · broken · Nov 25, 2023 · N31SA · Cessna 208B · Air Conditioning System
  > SMOKE IN THE COCKPIT AFTER TAKEOFF. MAINTENANCE FOUND AIR CONDITIONING BELT BROKEN. SYSTEM PLACED ON MEL
- [SDR 2023FA0000616](https://openairdocs.org/sdr/2023FA0000616.md): Connector · failed · Oct 20, 2023 · N661WA · Cessna 208B · Ice/Rain Protection System Wiring
  > PILOT DEPARTED THE MORNING OR MARCH 31 2023 AND SHORTLY INTO HIS FLIGHT, REPORTED AN ELECTRICAL BURNING SMELL. TURN BACK WAS PREFORMED AND FLIGHT RETURNED TO AIRPORT WHERE MAINTENANCE WAS READILY AVALLABLE. AFTER INVESTIGATION FOUND THO ELECTRICAL CONNECTOR
- [SDR ENHA202310160002](https://openairdocs.org/sdr/ENHA202310160002.md): Unknown · unknown · Oct 13, 2023 · N410GV · Cessna 208B · Engine (Turbine/Turboprop)
  > PILOT NOTED "I OBSERVED A RUNAWAY ENGINE CONDITION, MY TORQUE AND NG GUAGES CLIMBED TO REDLINE WITH MY POWER LEVER IN IDLE POSITION. I DECIDED TO CLIMB TO 9500 FT AND CONTINUE TOWARDS KING SALMON ALASKA. MY ITT GUAGE SLOWLY CLIMBED TO A MAXIMUM OF 900C. ON
- [SDR ENHA2023090800691](https://openairdocs.org/sdr/ENHA2023090800691.md): Caliper · broken · Sep 5, 2023 · N804TH · Cessna 208B · Brake
  > THE RIGHT WHEEL LOCKED UP ON LANDING, AFTER ABOUT 200' IT BROKE LOOSE AND WAS ROLLING AGAIN HOWEVER I HAD NO BRAKE ON THE RIGHT. I TAXIED TO THE RAMP AND FOUND THE TOP BOLT ON THE BRAKE CALIPER BROKE AND THE BRAKE CALIPER WAS JAMMED INTO THE TIRE.
- [SDR 2023F00267](https://openairdocs.org/sdr/2023F00267.md): Brake Pads · glazed · Sep 4, 2023 · N937CK · Cessna 208B · Brake
  > LOST BRAKING AUTHORITY ON BOTH PILOT AND COPILOT SIDE AFTER LANDING
- [SDR 2023FA0000320](https://openairdocs.org/sdr/2023FA0000320.md): Compressor · seized · Jun 19, 2023 · N9642F · Cessna 208B · Air Conditioning System
  > DURING LANDING SMELLED THE ODOR OF SMOKE. TURNED OF AIR CONDITIONING SYSTEM AND SMELL DISSIPATED. FOUND AC BELT BROKEN AND COMPRESSOR SEIZED
- [SDR 2023F00206](https://openairdocs.org/sdr/2023F00206.md): Brake · unknown · Jun 17, 2023 · N29MG · Cessna 208B · Brake
  > RIGHT BRAKE FAILURE ON TAXI ON BOTH PIC AND SIC'S SIDE.
- [SDR 2023FA0000300](https://openairdocs.org/sdr/2023FA0000300.md): Unknown · unknown · Jun 2, 2023 · N859MA · Cessna 208B · Engine Oil System (Airframe Furnished)
  > BURNT SMELL NOTICED BY CREW ON CLIMB OUT. ALL INSTRUMENTS INDICATED GREEN, NO SMOKE OR FLAMES NOTICED. FIRST OFFICER COMMENTED HE MAY NOT HAVE SECURED THE OIL FILLER CAP. OIL PRESSURE STARTED TO FLUCTUATE AND THE DECISION WAS MADE TO RETURN TO THE DEPARTING ST
- [SDR 2023F00105](https://openairdocs.org/sdr/2023F00105.md): Bolt · missing · Apr 4, 2023 · N9481F · Cessna 208A · Engine (Turbine/Turboprop)
  > LOSS OF OIL PRESSURE ON DEPARTURE CLIMB OUT
- [SDR 2023F00040](https://openairdocs.org/sdr/2023F00040.md): None · worn · Feb 1, 2023 · N208EE · Cessna 208B · Propeller/Rotor Anti-Ice/De-Ice System
  > CREW REPORTED PROPELLER HEAT INOP-SHOWS 8-9 AMPS IN BOTH AUTO AND MANUAL. MODES. CORRECTIVE ACTION: REMOVED PROPELLER ANTI-ICE LEADS. INSTALLED THREE NEW PROPELLER DE-ICE LEADS. PROPELLER ANTI-ICE SYSTEMS CHECK GOOD ON ENGINE GROUND RUN. SUBSEQUENT FLIGHT WAS
- [SDR 2022FA0000731](https://openairdocs.org/sdr/2022FA0000731.md): Line · leaking · Nov 22, 2022 · N865MA · Cessna 208B · Accessory Gearboxes
  > SMOKE COMING OUT OF PILOTS SIDE VENT IN FLIGHT. UPON INVESTIGATION AFTER LANDING, IT WAS DISCOVERED THAT THE LINES GOING TO THE COMPRESSOR WERE LEAKING FREON.
- [SDR 2022F00023](https://openairdocs.org/sdr/2022F00023.md): Fuel Control · fluctuates · Dec 8, 2021 · N722FX · Cessna 208B · Engine Fuel and Control
  > WHILE IN ROUTE FROM KONT TO KSMX THE PILOT EXPERIENCED ABNORMAL POWER SURGES AND ABNORMAL FLUCTUATIONS IN THE TORQUE GAGE. A REQUEST TO RETURN TO KONT WAS MADE BUT WEATHER WAS CLOSING IN. THE PILOT DECLARED AN EMERGENCY AND REQUESTED TO DIVERT TO KBUR AND LAND
- [SDR MTNA20210809001](https://openairdocs.org/sdr/MTNA20210809001.md): Chip Detector · contaminated · Aug 7, 2021 · N851FE · Cessna 208B · Accessory Gearboxes
  > CHIP DETECTOR LIGHT CAME ON IN FLIGHT. MAINTENANCE INSPECTED BOTH CHIP DETECTORS. DEBRIS FOUND ON AGB CHIP DETECTOR. PERFORMED INSPECTION OF OIL FILTER, NO CONTAMINATION FOUND. CLEANED CHIP DETECTOR AND REINSTALLED. PERFORMED ENGINE GROUND RUNS AND REINSPECTED
- [SDR ENHA202012180001](https://openairdocs.org/sdr/ENHA202012180001.md): Bolt · failed · Dec 14, 2020 · N25JA · Cessna 208B · Landing Gear Brake System
  > LEFT HAND BRAKE CALIPER LOWER ANCHOR BOLT FAILED, BOLT DEPARTED AIRCRAFT. BRAKE LOCKED UP.
- [SDR 2020F00487](https://openairdocs.org/sdr/2020F00487.md): Fuel Control · malfunctioned · Dec 5, 2020 · N984FE · Cessna 208B · Fuel Control/Turbine Engines
  > JUST AFTER SHUTDOWN THE PILOT NOTICED SMOKE COMING FROM THE THE RIGHT SIDE OF THE AIRCRAFT, FOLLOWED BY FLAME ABOVE THE COPILOT WINDOW. THE PILOT EXITED THE COCKPIT AND CONTACTED EMERGENCY SERVICES. THE PILOT CALLED DISPATCH AND WAS TRANSFERRED TO MAINTENANC
- [SDR 2020F00423](https://openairdocs.org/sdr/2020F00423.md): Boot · debonded · Oct 5, 2020 · N863MA · Cessna 208B · Propeller/Rotor Anti-Ice/De-Ice System
  > ON CLIMB OUT FROM FAT THE PILOT HEARD A "POP" AND THEN FELT A VIBRATION IN THE AIRFRAME. HE NOTIFIED ATC OF HIS NEED TO RETURN ASAP AND LANDED WITH OUT INCIDENT. UPON INSPECTION MAINTENANCE FOUND APPROXIMATELY 4" OF THE NR 3 BLADE DEICE BOOT MISSING. ALL TH
- [SDR MTNA20200721001](https://openairdocs.org/sdr/MTNA20200721001.md): Engine · malfunctioned · Jul 21, 2020 · N874FE · Cessna 208B · Engine (Turbine/Turboprop)
  > IN CRUISE WITH ENGINE PARAMETERS NORMAL A SERIES OF BANGS WITH ASSOCIATED DROPS IN TORQUE, RISES IN ITT AND DROPS IN FUEL FLOW. RATE OF BANGS AND FLUCTUATIONS DECREASED WHEN TORQUE REDUCED TO 1100 LBS AND STOPPED WHEN TORQUE REDUCED BELOW 800LBS. REPLACED EN
- [SDR M36R201911260018](https://openairdocs.org/sdr/M36R201911260018.md): Turbine Blades · corroded · Nov 18, 2019 · N78SA · Cessna 208B · Turbine Section
  > A STANDARD BORESCOPE INSPECTION OF THE COMPRESSOR TURBINE BLADES WAS CONDUCTED WITH NO DEFECTS NOTED IN ACCORDANCE WITH THE PRATT AND WHITNEY CANADA MAINTENANCE MANUAL. THE TECHNICIAN ELECTED TO DO AN ADDITIONAL INSPECTION OF THE BLADES THROUGH THE EXHAUST DUC
- [SDR AXSA201910030001](https://openairdocs.org/sdr/AXSA201910030001.md): Fire Detector · shorted · Oct 2, 2019 · N898FE · Cessna 208B · Fire Detection
  > ENGING FIRE WARNING AND ANNUCIATOR ACTIVATED AFTER TAKE OFF, STAYED ON DURING LANDING AND TAXI. NO VISIBLE SIGNS OF FIRE NOTED.
- [SDR ENHA2019090600000](https://openairdocs.org/sdr/ENHA2019090600000.md): O-Ring · worn · Sep 5, 2019 · N1115M · Cessna 208B · Brake
  > FROM PILOT IRREGULARITY REPORT: "1115M HAD A LEFT BRAKE FAILURE AFTER LANDING RWY 19R. AS I WAS TAXING DOWN C I WAS USING A COMBINATION OF THE RIGHT BRAKE AND PROP REVERSE TO SLOW DOWN. EVERY TIME I CAME OUT OF PROP REVERSE THE PLANE VEERED MORE TO THE RIGHT
- [SDR AWHA2019073100000](https://openairdocs.org/sdr/AWHA2019073100000.md): Power Lever · out of rig · Jul 22, 2019 · N920FE · Cessna 208B · Power Lever
  > DURING POST COMPRESSOR WASH ENGINE RUN MAINTENANCE FOUND PROP STARTING TO GO INTO BETA WHEN THE POWER LEVER WAS AT THE GATE. THE MECHANIC DETERMINED THE ENGINE CONTROLS WERE OUT OF RIG AND ADJUSTED REAR CLEVIS AND 11" ROD AS NEEDED AND SAFETIED. OPERATIONAL
- [SDR EPUA20190716001](https://openairdocs.org/sdr/EPUA20190716001.md): Fuel Control · leaking · Jul 15, 2019 · N1296Y · Cessna 208B · Fuel Control/Turbine Engines
  > PILOT REPORTS " UPON DEPARTING A STRONG ODOR OF POLISH OR FUEL BEGAN FILLING THE CABIN. AT FIRST WE BELIEVED IT WAS FUEL ON GLOVES OR A RAG. AS WE FLEW THE SMELL BE GREW IN STRENGTH AND THE PASSENGERS NOTED IT AS WELL. WE RETURNED TO BASE. MAINTENANCE INSP
- [SDR AWHA201906184001](https://openairdocs.org/sdr/AWHA201906184001.md): Master Cylinder · failed · Jun 14, 2019 · N661WA · Cessna 208B · Master Cylinder/Brake Valve
  > UPON TAXI TO RWY 20 FOR DEPARTURE FROM KPWT AT IDLE RPM (A TWY NE BOUND) LOSS OF BRAKING/STEERING CONTROL, RESULTED IN ACFT VEERING OFF PAVED SURFACE AND INTO THE GRASS ADJACENT TO TWY. ACFT WAS IMMEDIATELY SHUTDOWN AND SECURED. NO CONTACT WITH ANY OBJECT AND
- [SDR MUIA20190518001](https://openairdocs.org/sdr/MUIA20190518001.md): Static System · contaminated · May 8, 2019 · N1983X · Cessna 208B · Pitot/Static System
  > CREW REPORTED PIC AND SIC AIRSPEED INDICATORS AND PIC AND SIC VERTICAL SPEED INDICATORS GAVE ERRONEOUS READING IN HEAVY PRECIPITATION AND TURBULENCE. MAINTENANCE DRAINED WATER FROM BOTH STATIC SYSTEMS AND VERIFIED LT AND RT PITOT/STATIC MAST HEATERS ARE OPERAT
- [SDR 2019FA0000268](https://openairdocs.org/sdr/2019FA0000268.md): Door Frame · corroded · Apr 23, 2019 · N9820F · Cessna 208B · Fuselage Main, Structure
  > LOWER CARGO DOOR THRESHOLD AIRFRAME SKIN CORRODED
- [SDR 2019FA0000269](https://openairdocs.org/sdr/2019FA0000269.md): Skin · chafed · Apr 23, 2019 · N9820F · Cessna 208B · Fuselage Main, Plate/Skin
  > CHAFE DAMAGE ON LOWER COWLING
- [SDR 2019FA0000270](https://openairdocs.org/sdr/2019FA0000270.md): Support Bracket · chafed · Apr 23, 2019 · N9820F · Cessna 208B · Trailing Edge Flaps
  > FLAP LEADING EDGE CHAFING AND SUPPORT BRACKET WEAR
- [SDR 2019FA0000271](https://openairdocs.org/sdr/2019FA0000271.md): Structure · dented · Apr 23, 2019 · N9820F · Cessna 208B · Elevator, Plate/Skin
  > DENTED ELEVATOR
- [SDR 2019FA0000272](https://openairdocs.org/sdr/2019FA0000272.md): Torque Tube · corroded · Apr 23, 2019 · N9820F · Cessna 208B · Rudder Control System
  > RUDDER TORQUE TUBE REQUIRES REPLACEMENT
- [SDR 2019FA0000273](https://openairdocs.org/sdr/2019FA0000273.md): Flap Track · worn · Apr 23, 2019 · N9820F · Cessna 208B · Trailing Edge Flaps
  > FLAP TRACKS WORN
- [SDR 2019FA0000274](https://openairdocs.org/sdr/2019FA0000274.md): Flap Track · worn · Apr 23, 2019 · N9820F · Cessna 208B · Trailing Edge Flaps
  > FLAP TRACKS WORN
- [SDR ENHA2019F00156](https://openairdocs.org/sdr/ENHA2019F00156.md): Canister · full · Mar 18, 2019 · N929TG · Cessna 208B · Fuel Dump System
  > FUEL SMELL IN COCKPIT. EPA CAN FULL.
- [SDR MUIA20190212001](https://openairdocs.org/sdr/MUIA20190212001.md): Connector · contaminated · Feb 12, 2019 · N208EE · Cessna 208B · Instrument System Wiring
  > CREW PERFORMED AIR RETURN AFTER RESERVOIR LOW FUEL LIGHT ILLUMINATED ON ANNUNCIATOR PANEL WITH LH & RH WING LOW FUEL LIGHTS ILLUMINATED ON ANNUNCIATOR PANEL WHEN DAY-NIGHT SWITCH MOVED TO "DAY" MODE. FOUND MOISTURE ACCUMULATION UNDER FLOOR IN AREA OF FUEL RESE
- [SDR AWHA20190204001](https://openairdocs.org/sdr/AWHA20190204001.md): Bleed Valve · malfunctioned · Dec 18, 2018 · N846FE · Cessna 208B · Compressor Bleed Valve
  > WHEN THE PILOT PUSHED THE POWER LEVER UP ON THE TAKEOFF ROLL HE HEARD TWO LOUD BANGS COMING FROM THE ENGINE COMPARTMENT. HE ABORTED TAKEOFF AND RETURNED TO THE RAMP. THE PRE-TAKEOFF RUN UP WAS UNEVENTFUL. MECHANIC RAN THE ENGINE AND HEARD THE SAME LOUD BANG. I

Next page: https://openairdocs.org/engine/u-a-canada-pt6a-114a/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 = 'PT6A114A'
ORDER BY difficulty_date DESC
```

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

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