# Service difficulty reports: U/A Canada PT6A-65B

A list on [U/A Canada PT6A-65B](https://openairdocs.org/engine/u-a-canada-pt6a-65b.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 13 · 628 reports

- [SDR YADA2025051001](https://openairdocs.org/sdr/YADA2025051001.md): Housing · eroded · May 10, 2025 · N126AX · Beech 1900C · Turbine Engine Oil System
  > FLIGHT CREW REPORTED THE #1 ENGINE LEAKING OIL - MAINTENANCE LOCATED A PINHOLE ON THE ENGINE OIL SCAVENGE PUMP HOUSING AND REPLACED THE HOUSING DUE CAVITATION EROSION THROUGH THE PUMP BODY.
- [SDR YADA2025012701](https://openairdocs.org/sdr/YADA2025012701.md): Pump · eroded · Jan 27, 2025 · N125AX · Beech 1900C · Turbine Engine Oil System
  > MAINTENANCE DISCOVERED A LEAKING ENGINE OIL SCAVENGE PUMP - A PINHOLE WAS VERIFIED IN THE PUMP HOUSING OUTER WALL FROM INTERNAL EROSION - REPLACED SAME.
- [SDR YADA2025012201](https://openairdocs.org/sdr/YADA2025012201.md): Housing · eroded · Jan 22, 2025 · N117AX · Beech 1900C · Turbine Engine Oil System
  > MAINTENANCE NOTICED OIL LEAKING FROM #2 ENGINE COWLING. INSPECTION REVEALED OIL LEAKING FROM THE SCAVENGE OIL PUMP HOUSING PINHOLE AND REPLACED HOUSING. REMOVED UNIT WAS VERIFIED TO HAVE INTERNAL EROSION THROUGH BODY OF THE HOUSING. THIS HAS BECOME A COMMO
- [SDR TIMA20240920012](https://openairdocs.org/sdr/TIMA20240920012.md): Engine · power loss · Sep 20, 2024 · N131SF · Beech 1900C · Engine (Turbine/Turboprop)
  > ON DESCENT TO RWY 27, ON ABOUT AN 8 MILE FINAL I REDUCED POWER TO SLOW DOWN. WHEN I WENT TO ADD POWER ONCE AGAIN THE LH SIDE PRODUCED NO ADDITIONAL THRUST. UPON LOOKING AT THE ENGINE INDICATIONS I NOTICED N1 WAS AT 35%, AUTO IGNITION WAS ACTIVATED, AND AUTO FE
- [SDR TIMA20240917011](https://openairdocs.org/sdr/TIMA20240917011.md): Engine · low torque · Sep 17, 2024 · N422AX · Beech 1900C · Engine (Turbine/Turboprop)
  > TAXIED FROM THE RAMP INTO THE RUN UP AREA, DID RUN UPS AS NORMAL NOTHING ABNORMAL DETECTED. TOOK OFF 16L REACHED V1 AND ROTATED AS I NOTICED THE PLANE WAS A LITTLE SLUGGISH TO LEAVE THE GROUND AS I GOT AIRBORNE I NOTICED THE TORQUE FOR THE LEFT ENGINE STARTING
- [SDR YADA2024060351101](https://openairdocs.org/sdr/YADA2024060351101.md): Housing · eroded · May 11, 2024 · N117AX · Beech 1900C · Turbine Engine Oil System
  > PILOT REPORTED OIL LEAK ON #1 ENGINE AFTER FLIGHT - MAINTENANCE LOCATED LEAK AT #1 ENGINE SCAVENGE PUMP HOUSING AND REPLACED SAME.
- [SDR YADA2024042401](https://openairdocs.org/sdr/YADA2024042401.md): Housing · eroded · Apr 24, 2024 · N244AX · Beech 1900C · Turbine Engine Oil System
  > MAINTENANCE DISCOVERED A LEAKING ENGINE OIL SCAVENGE PUMP - A PINHOLE WAS VERIFIED IN THE PUMP HOUSING OUTER WALL FROM INTERNAL EROSION - REPLACED SAME.
- [SDR YADA2023110401](https://openairdocs.org/sdr/YADA2023110401.md): Housing · eroded · Nov 4, 2023 · N113AX · Beech 1900C · Turbine Engine Oil System
  > PILOT REPORTED SEEING OIL ON RH WING DURING PREFLIGHT. MAINTENANCE IDENTIFIED A LEAK FROM A HOLE IN THE RH ENGINE OIL SCAVENGE PUMP HOUSING AND REPLACED SAME. THIS IS A COMON ISSUE WITH THESE PUMP HOUSINGS.
- [SDR TIMA20231031008](https://openairdocs.org/sdr/TIMA20231031008.md): Unknown · unknown · Oct 31, 2023 · N124GP · Beech 1900C · Engine Fuel and Control
  > NORMAL TAXI/RUN UP/TAKEOFF / CLIMB. AS I WAS LEVELING OFF FUEL PRESSURE LOW ON RH ENG ILLUMINATED, SWITCHED ON STANDBY PUMP AND LIGHT EXTINGUISHED LOOKED FOR AND FOUND NO SECONDARY INDICATIONS OF IMPENDING FAILURE. REDUCED POWER TO CRUISE SETTING AND SCANNED
- [SDR YADA2023071301](https://openairdocs.org/sdr/YADA2023071301.md): Housing · eroded · Jun 22, 2023 · N119AX · Beech 1900C · Engine Fuel Pump
  > PILOT REPORTED OIL LEAKING OUT OF RIGHT ENGINE. MAINTENANCE DISCOVER #2 ENGINE OIL SCAVENGE PUMP HAVING A PINHOLE LEAK AND THE HOUSING WAS REPLACED. INSPECTION DETERMINED THAT CAVITATION EROSION OF THE PUMP BODY IN A CORNER OF THE CAVITY HAD CREATED A HOLE.
- [SDR JIKA20230116001](https://openairdocs.org/sdr/JIKA20230116001.md): Seal · leaking · Jan 10, 2023 · N7203C · Beech 1900C · Turbine Engine Oil System
  > PILOT REPORTED THAT UPON APPROACH TO KRDM THE RT ENGINE OIL PRESSURE ANNUNCIATOR ILLUMINATED. PILOT DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT SYSTEM TO A LEAK COMING FROM RH ENGINE OIL SCAVENGE PUMP. MAINTENANCE REMOVED AND RE
- [SDR YADA2022100301](https://openairdocs.org/sdr/YADA2022100301.md): None · eroded · Oct 15, 2022 · N125AX · Beech 1900C · Engine Oil Distribution (Airframe Furnished)
  > DURING UNRELATED MAINTENANCE, AN OIL LEAK WAS DISCOVERED FROM THE LEFT ENGINE. MAINTENANCE IDENTIFIED THE ENGINE OIL SCAVENGE PUMP AS HAVING A PINHOLE LEAK AND THE PUMP HOUSING WAS REPLACED. INSPECTION DETERMINED THAT CAVITATION EROSION OF THE PUMP BODY IN A
- [SDR YADA20211223201](https://openairdocs.org/sdr/YADA20211223201.md): Control Panel · shorted · Dec 22, 2021 · N110AX · Beech 1900C · Light System Wiring
  > STRONG SMELL OF SOMETHING BURNING SUB PANEL LIGHTS FLICKERING THEN COMPLETELY SHUT OFF. FOUND EEL PANEL A321 114-384007-15 SHORTING INTERNALLY.
- [SDR YADA2021081601](https://openairdocs.org/sdr/YADA2021081601.md): Engine · failed · Aug 13, 2021 · N247AX · Beech 1900C · Engine (Turbine/Turboprop)
  > INTERNAL ENGINE FAILURE OF RIGHT ENGINE WHILE AT CRUSIE 23000 FT.
- [SDR YADA20210817201](https://openairdocs.org/sdr/YADA20210817201.md): Housing · eroded · Aug 12, 2021 · N115AX · Beech 1900C · Turbine Engine Oil System
  > PILOT REPORTED "OIL LEAKING FROM RIGHT ENGINE" - MAINTENANCE FOUND OIL LEAK TO BE COMING FROM THE ENGINE OIL SCAVENGE PUMP HOUSING. REPLACED HOUSING. FOUND CAVITATION EROSION THROUGH CASTING.
- [SDR YADA20210510001](https://openairdocs.org/sdr/YADA20210510001.md): Housing · eroded · May 8, 2021 · N246AX · Beech 1900C · Turbine Engine Oil System
  > PILOT REPORTED "LEFT ENGINE OIL LEAK". MAINTENANCE OIL LEAK TO BE COMING FROM THE OIL SCAVENGE PUMP HOUSING. REPLACED SCAVENGE PUMP HOUSING. FOUND CAVITATION EROSION THROUGH CASTING.
- [SDR JIKA2021020501](https://openairdocs.org/sdr/JIKA2021020501.md): Drain Line · leaking · Feb 5, 2021 · N3071A · Beech 1900C · Turbine Engine Oil System
  > SMOKE IN COCKPIT. TURNED OFF BOTH BLEEDS. SMOKE FILTERED OUT. RIGHT BLEED CAUSED NO MORE SMOKE. LEFT BLEED BROUGHT SMOKE AGAIN. FINISHED WITH RIGHT BLEED ONLY. THE AIRCRAFT LANDED WITHOUT INCIDENT IN KOMA. OMA MX- CHECKED GAS GEN. BREATHER TUBE FOR OBSTRUCTION
- [SDR YADA2021062101](https://openairdocs.org/sdr/YADA2021062101.md): Engine · failed · Jan 25, 2021 · N575A · Beech 1900C · Engine (Turbine/Turboprop)
  > INTERNAL ENGINE FAILURE OF RIGHT ENGINE WHILE ON DECENT FOR LANDING - ENGINE REPLACED - O/H FACILITY DID NOT DETERMINE ORIGINAL FAILURE
- [SDR YADA20210107001](https://openairdocs.org/sdr/YADA20210107001.md): Scavenge Pump · cavitates · Dec 31, 2020 · N118AX · Beech 1900C · Turbine Engine Oil System
  > NR 2 ENGINE OIL LEAKING. MAINTENANCE FOUND OIL LEAK TO BE COMING FROM THE OIL SCAVENGE PUMP HOUSING. REMOVED AND REPLACED OIL SCAVENGE PUMP. UPON FURTHER INVESTIGATION OF REMOVED OIL SCAVENGE PUMP, THERE WAS CAVITATION INSIDE OF THE HOUSING ITSELF.
- [SDR JIKA2020092801](https://openairdocs.org/sdr/JIKA2020092801.md): Fuel Control · broken · Sep 28, 2020 · N7203C · Beech 1900C · Fuel Control/Turbine Engines
  > WHILE IN ROUTE TO KPDX, THE FLIGHT CREW REPORTED LEFT ENGINE TORQUE AND N1 INDICATIONS DROPPED. CHECKLIST ITEMS WERE FOLLOWED AND THE LEFT ENGINE WAS SHUT DOWN. THE CREW DECLARED AN EMERGENCY AND THE AIRCRAFT DIVERTED TO KDLS AND LANDED WITHOUT INCIDENT. PD
- [SDR YADA20200702001](https://openairdocs.org/sdr/YADA20200702001.md): Fcu · power loss · Jul 1, 2020 · N125AX · Beech 1900C · Fuel Control/Turbine Engines
  > PILOT REPORT: LEFT ENGINE FAILURE IN FLIGHT. TORQUE ROLLED BACK SLOWLY TO 0 NG INDICATED APPROX 55 FUEL FLOW 100 PPH. ATTEMPTED STARTER ASSIST AIRSTART. PROP FEATHERED AND UNFEATHERED NORMALLY. SAME INDICATIONS FOR RESTART. SECURED ENGINE. 1300 LBS OF FU
- [SDR TIMA20200613003](https://openairdocs.org/sdr/TIMA20200613003.md): Engine · malfunctioned · Jun 13, 2020 · N198GA · Beech 1900C · Engine (Turbine/Turboprop)
  > AIRCRAFT DEPARTED DEN AND SHORTLY AFTER CLIMBOUT, LEVELING OUT AT 10K', THE PILOT BEGAN PULLING BACK POWER AND EXPERIENCED THE RIGHT ENGINE PROPELLER BECAME "JERKY" AND SPORADIC WITHOUT ANT PROPELLER LEVER INPUTS. SOON AFTER, THE RIGHT ENGINE ITT CLIMBED TO 11
- [SDR JIKA2019112119](https://openairdocs.org/sdr/JIKA2019112119.md): Engine · oil consumption · Nov 16, 2019 · N718AF · Beech 1900C · Engine (Turbine/Turboprop)
  > ENROUTE TO KSDF THE CABIN SHOWED SIGNS OF SMOKE WHEN THE RIGHT BLEED AIR WAS TURNED ON. THE SMOKE DISSIPATED WHEN THE RIGHT BLEED WAS TURNED OFF. MAINTENANCE INSPECTED THE RIGHT BLEED AIR SYSTEM AND FOUND RESIDUAL OIL IN THE RIGHT NACELLE BLEED AIR PRE COOLER
- [SDR JIKA2019102301](https://openairdocs.org/sdr/JIKA2019102301.md): Oil System · leaking · Oct 19, 2019 · N718AF · Beech 1900C · Turbine Engine Oil System
  > ON APPROACH INTO KSDF THE PILOT REPORTED SMOKE COMING FROM THE BLEED AIR. THE PILOT TURNED OFF THE RIGHT BLEED AIR AND THE SMOKE DISSIPATED. THE PILOT LANDED AT KSDF WITHOUT INCIDENT. AN EMERGENCY WAS NOT DECLARED. MAINTENANCE TROUBLE SHOT THE RIGHT ENGINE
- [SDR JIKA2019101701](https://openairdocs.org/sdr/JIKA2019101701.md): Packing · leaking · Oct 15, 2019 · N718AF · Beech 1900 · Turbine Engine Oil System
  > APPROXIMATELY 1HR INTO FLIGHT, RIGHT ENGINE OIL PRESSURE DROPPED TO 40PSI ACCOMPANIED WITH LOW OIL PRESSURE WARNING ANNUNCIATOR LIGHT. CREW COMPLIED WITH CHECKLIST ACTION TO SECURE THE RIGHT ENGINE. THE FLIGHT WAS CONTINUED TO DESTINATION WITH SINGLE ENGINE A
- [SDR YADA2019060600214](https://openairdocs.org/sdr/YADA2019060600214.md): Cable · dragging · Jun 6, 2019 · N124AX · Beech 1900C · Engine Controls
  > LEFT HAND CONDITION CABLE ASSEMBLY SUFFERED AN INCREASE IN FRICTION TO POINT OF ROD END FAILURE AT THE CONTROL LEVER WITH IN 30 DAYS OF INSTALL.
- [SDR CA190219002](https://openairdocs.org/sdr/CA190219002.md): Engine · shutdown · Feb 7, 2019 · Beech 1900C · Engine (Turbine/Turboprop)
  > (CAN) CUSTOMER REPORTED SHORTLY AFTER TAKEOFF, THE LEFT HAND ENGINE SHUT DOWN UNEXPECTEDLY. THE FIGHT CREW CONTINUED THE CLIMB TO 2000 FEET ASL IN VFR CONDITIONS, DECLARED AN EMERGENCY, AND RETURNED TO AIRPORT. THE SUBSEQUENT LANDING WAS UNEVENTFUL. PRATT AND
- [SDR TIMA201902081024](https://openairdocs.org/sdr/TIMA201902081024.md): Seal · leaking · Feb 4, 2019 · N218SL · Beech 1900C · Turbine Engine Oil System
  > PILOT REDUCED RH ENGINE POWER AFTER THE OIL PSI LOW WARNING ANNUNCIATOR ALERTED. PILOT RETURNED TO DEPARTURE AIRPORT, LANDED WITHOUT INCIDENT, AND SHUTDOWN ENGINE WHEN CLEAR OF THE RUNWAY. MAINTENANCE FOUND FAULTY OIL SEAL AT PROP SHAFT AND REPLACED THE SE
- [SDR TIMA201902080004](https://openairdocs.org/sdr/TIMA201902080004.md): Seal · leaking · Feb 4, 2019 · N218SL · Beech 1900C · Turbine Engine Oil System
  > PILOT REDUCED RH ENGINE POWER AFTER OIL PSI LOW WARNING ANNUNCIATOR ALERTED. PILOT RETURNED TO DEPARTURE AIRPORT, LANDED WITHOUT INCIDENT, AND SHUTDOWN ENGINE WHEN CLEAR OF THE RUNWAY. MAINTENANCE FOUND LEAKING OIL SEAL AT PROP SHAFT AND REPLACED THE SEAL.
- [SDR YADA20180105001](https://openairdocs.org/sdr/YADA20180105001.md): Scavenge Pump · leaking · Jan 5, 2019 · N115AX · Beech 1900C · Turbine Engine Oil System
  > MAINTENANCE DISCOVERED THAT THE NR 1 ENGINE HAD AN OIL LEAK AT THE SCAVENGE PUMP HOUSING– THE PUMP WAS LEAKING THROUGH THE CASTING. THIS IS THE THIRD SUCH FAILURE OF THIS PART IN ONE YEAR FOR US.
- [SDR YADA20190103001](https://openairdocs.org/sdr/YADA20190103001.md): Scavenge Pump · leaking · Jan 3, 2019 · N113AX · Beech 1900C · Turbine Engine Oil System
  > AFTER LANDING, CREW NOTICED ENGINE OIL ON LT WING. MAINTENANCE LOCATED OIL LEAK AT NR 1 ENGINE OIL SCAVENGE PUMP HOUSING AND REPLACED SAME. REMOVED HOUSING VERIFIED TO HAVE CAVITATION CAVITY THROUGH WALL OF SCAVENGE PUMP BODY THAT WAS ALLOWING OIL TO ESCAPE T
- [SDR TIMA2018120400001](https://openairdocs.org/sdr/TIMA2018120400001.md): Vernatherm · failed · Dec 3, 2018 · N218SL · Beech 1900C · Engine Oil Temperature Regulator
  > PILOT SHUTDOWN RT ENGINE AFTER NOTICING OIL TEMP HIGH, PRESSURE LOW, AND OIL STREAKS ON COWL. INVESTIGATION FOUND OIL TEMPERATURE VERNATHERM WAS NOT PASSING OIL THRU THE OIL COOLER.
- [SDR TIMA2018103100001](https://openairdocs.org/sdr/TIMA2018103100001.md): Hose · chafed · Oct 30, 2018 · N197GA · Beech 1900C · Engine Oil Distribution (Airframe Furnished)
  > ENGINE WAS SHUTDOWN IN FLIGHT AFTER TORQUE AND OIL PRESSURE FLUCTUATIONS. INSPECTION REVEALED THAT THE OIL HOSE CONNECTED BETWEEN THE ENGINE AND OIL COOLER HAD CHAFED THROUGH THE INSULATION AND SHIELDING WHERE THE HOSE RESTED ON THE AFT NACELLE STRUCTURE TO T
- [SDR YADA2018103000179](https://openairdocs.org/sdr/YADA2018103000179.md): Control Cable · corroded · Oct 24, 2018 · N113A · Beech 1900C · Rudder Control System
  > RUDDER CABLE FOUND FRAYED AND SEVERELY CORRODED AT A ROUTINE INSPECTION.
- [SDR YADA2018082017001](https://openairdocs.org/sdr/YADA2018082017001.md): Filter · contaminated · Aug 17, 2018 · N124AX · Beech 1900C · Engine Oil Indicating System
  > PILOT REPORTED THE RT ENGINE OIL PRESSURE WAS OBSERVED TO BE SHOWING 65 PSI AFTER TAKEOFF. NO EMERGENCY WAS DECLARED, AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE NR 2 ENGINE MAIN OIL FILTER AND THEN CLEANED CONTAMINATION OUT OF THE OIL PRESSURE TRANSMITTER
- [SDR YADA20180518001](https://openairdocs.org/sdr/YADA20180518001.md): Bellows · faulty · May 18, 2018 · N110AX · Beech 1900C · Fuel Control/Turbine Engines
  > PILOT REPORTED WHILE TAXIING THE RIGHT HAND ENGINE HAD A HUNG START WHILE USING BATTERY POWER TO START THE ENGINE AND THAT THE ENGINE FAILED DURING THE TAXI, PILOT RETURNED TO HOME STATION. MAINTENANCE IS CURRENTLY TROUBLESHOOTING THE ISSUE BUT HAS FOUND THAT
- [SDR YADA20180426001](https://openairdocs.org/sdr/YADA20180426001.md): Lens · detached · Apr 25, 2018 · N111AX · Beech 1900C · Exterior Lighting
  > LEFT WING TIP NAV STROBE LENS COVER LOST INFLIGHT.
- [SDR JDWA201804190001](https://openairdocs.org/sdr/JDWA201804190001.md): Fuel Control · malfunctioned · Apr 17, 2018 · N130UE · Beech 1900C · Fuel Control/Turbine Engines
  > DURING APPROACH, THE NR 1 POWER OUTPUT REDUCED AND WOULD NOT RESPOND TO INPUT. THE ENGINE WAS SHUT DOWN AND AIRCRAFT LANDED WITHOUT INCIDENT. TROUBLESHOOTING REVEALED NO DAMAGED P3 OR PY LINES. REPLACED FUEL CONTROL UNIT.
- [SDR YADA2018022218001](https://openairdocs.org/sdr/YADA2018022218001.md): Gasket · failed · Feb 22, 2018 · N268SL · Beech 1900C · Pneumatic Indicating System
  > RIGHT BLEED AIR ANNUNCIATOR ILLUMINATED INFLIGHT. RIGHT OVERTEMP SENSOR GASKET FAILED MELTING THE EVA TUBING.
- [SDR TIMA20180214003](https://openairdocs.org/sdr/TIMA20180214003.md): Governor · open · Feb 7, 2018 · N192GA · Beech 1900C · Propeller Governor
  > PROPELLER DID NOT COME OUT OF FEATHER AFTER A PROPELLER CYCLE CHECK DURING RUN-UP. REPLACING THE OVERSPEED GOVERNOR ELIMINATED THE PROBLEM. THE DUMP VALVE OF THE OVERSPEED GOVERNOR STUCK IN THE OPEN POSITION.
- [SDR YADA20180118001](https://openairdocs.org/sdr/YADA20180118001.md): Scavenge Pump · leaking · Jan 18, 2018 · N113AX · Beech 1900C · Turbine Engine Oil System
  > MAINTENANCE DISCOVERED THAT THE NR 2 ENGINE OIL SCAVENGE PUMP HOUSING WAS LEAKING THROUGH THE CASTING. OIL SCAVENGE PUMP HOUSING WAS REMOVED AND REPLACED.
- [SDR JIKA2018011601](https://openairdocs.org/sdr/JIKA2018011601.md): Tube · collapsed · Jan 16, 2018 · N31704 · Beech 1900C · Turbine Engine Oil System
  > THE PILOT REPORTED THAT THE LEFT ENGINE OIL PRESSURE BEGAN FLUCTUATING NEAR THE LOW REDLINE. THE PILOT PERFORMED A PRECAUTIONARY INFLIGHT SHUT DOWN OF THE LEFT ENGINE AND DIVERTED. LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE LEFT ENGINE AND FOUND OIL
- [SDR TIMA20170811011](https://openairdocs.org/sdr/TIMA20170811011.md): Line · chafed · Aug 11, 2017 · N101UE · Beech 1900C · Engine Fuel Distribution
  > AFTER A NORMAL TAKEOFF, THE PILOT WAS UNABLE TO MAINTAIN CLIMB POWER AND TORQUE ON THE LT ENGINE. AS POWER CONTINUED TO DECREASE, THE PILOT SHUT DOWN THE LT ENGINE AND RETURNED TO DEPARTURE FOR AN UNEVENTFUL LANDING. INSPECTION REVEALED THAT THE PRIMARY FU
- [SDR YADA20170515001](https://openairdocs.org/sdr/YADA20170515001.md): Fcu · unresponsive · May 15, 2017 · N111AX · Beech 1900C · Fuel Control/Turbine Engines
  > PILOT REPORTED THAT THE LEFT HAND ENGINE WAS UNRESPONSIVE TO POWER LEVER INPUT AND WOULD NOT COME OUT OF IDLE. MAINTENANCE PERSONAL REMOVED AND REPLACED THE LEFT HAND ENGINE FUEL CONTROL UNIT, PERFORMED RIGGING, OPERATIONAL AND LEAK CHECKS OF THE LEFT HAND ENG
- [SDR JIKA2016050301](https://openairdocs.org/sdr/JIKA2016050301.md): Bleed Valve · sticking · May 3, 2016 · N338AF · Beech 1900C · Compressor Bleed Valve
  > THE TRAINING CAPTAIN REPORTED WHILE PERFORMING TRAINING STALL MANEUVERS, THE FIRST OFFICER REDUCED POWER, A MOMENTARY COMPRESSOR STALL OCCURRED, BETWEEN 500 - 1000 FT & LBS TORQUE ON THE LT ENG. TRAINING CAPTAIN REDUCED POWER, THIS RESULTED IN ANOTHER STALL.
- [SDR CA160216023](https://openairdocs.org/sdr/CA160216023.md): Motor · failed · Feb 11, 2016 · Beech 1900C · Trailing Edge Flap Actuator
  > (CAN) FLIGHT CREW REPORTED ELECTRICAL SMOKE ODOR IN FLIGHT DECK. FLAP MOTOR FOUND U/S AND CIRCUIT BREAKER TRIPPED.
- [SDR TIMA20160108001](https://openairdocs.org/sdr/TIMA20160108001.md): Pressure Switch · faulty · Jan 8, 2016 · N127BA · Beech 1900C · Propeller Feathering/Reversing
  > IMMEDIATELY AFTER ROTATION THE LT PROPELLER AUTO FEATHERED. PILOT REDUCED POWER & IMMEDIATELY LANDED, ABORTING THE TAKEOFF. THE PROBLEM WAS DISCOVERED TO BE A FAULTY AUTO FEATHER LOW PRESS SWITCH.
- [SDR CA160125006](https://openairdocs.org/sdr/CA160125006.md): Fuel Control · failed · Dec 22, 2015 · Beech 1900C · Fuel Control/Turbine Engines
  > (CAN) REJECTED TAKEOFF BY FLIGHT CREW WHO REPORTED NO POWER ON LT ENGINE. AS FLIGHT CREW TAXIED BACK POWER RETURNED AND ENGINE STABLE BUT SLOW RESPONSE TO POWER INPUT.
- [SDR JIKA201512081501](https://openairdocs.org/sdr/JIKA201512081501.md): Fuel Control · low pressure · Dec 3, 2015 · N3052K · Beech 1900 · Fuel Control/Turbine Engines
  > EN-ROUTE, THE PILOT REPORTED THAT THE RT ENG TORQUE STARTED TO DROP OFF. THE PILOT WAS ABLE TO MATCH TOQUE BY ADVANCING THE RT POWER LEVER. DURING APPROACH, THE RT ENG BEGAN TO SURGE. THE PILOT PERFORMED A PRECAUTIONARY IN FLIGHT SHUTDOWN OF THE RT ENG. DE
- [SDR CA151204005](https://openairdocs.org/sdr/CA151204005.md): Line · cracked · Dec 3, 2015 · Beech 1900C · Aircraft Fuel Distribution System
  > (CAN) DURING INSTALLATION OF THE FUEL MOTIVE LINE IN THE RT WING ROOT IT WAS NOTICED THAT THE B-NUT TUBE SLEEVE WAS CRACKED.

Next page: https://openairdocs.org/engine/u-a-canada-pt6a-65b/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 = 'PT6A65B'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/u-a-canada-pt6a-65b/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.