# Service difficulty reports: U/A Canada PT6A-42

A list on [U/A Canada PT6A-42](https://openairdocs.org/engine/u-a-canada-pt6a-42.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 8 · 396 reports

- [SDR 2025FA0000454](https://openairdocs.org/sdr/2025FA0000454.md): Arm · broken · Jun 20, 2025 · N42J · Beech A200 · Landing Gear Steering System
  > AIRCRAFT BEING OPERATED BY TWO PILOT CREW. SIC WAS BACK TAXIING ON RUNWAY IN PREP FOR TAKEOFF. SIC MANEUVERED FOR A RIGHT 180 ON THE RUNWAY AND MADE THE RIGHT TURN. ABOUT HALF WAY THROUGH THE 180, CREW HEARD AND FELT A LOUD THUMP COMING FROM THE FLOOR. AFTER T
- [SDR CVUA2024112100004](https://openairdocs.org/sdr/CVUA2024112100004.md): Bleed Valve · stuck · Nov 19, 2024 · N875SP · Beech 200BEECH · Engine (Turbine/Turboprop)
  > RIGHT AFTER LIFTOFF, THERE WAS A LOUD POPPING SOUND COMING FROM THE LEFT ENGINE WITH FLAMES EMITTING FROM THE EXHAUST. COMMENCED A PRECAUTIONARY ENGINE SHUTDOWN, FEATHERED THE PROPELLER AND RETURNED TO THE FIELD FOR A SINGLE ENGINE LANDING. TAXIED BACK TO TH
- [SDR QMLA2024072920093](https://openairdocs.org/sdr/QMLA2024072920093.md): Spacer · out of limits · Jul 25, 2024 · N969MA · Gulstm 200 · Power Lever
  > THROTTLE LINKAGE SPACER OUT OF POSITION CAUSED THE PROPELLER TO TRY TO GO INTO BETO RANGE EARLY DURING FINAL APPROACH TO RWY 18R AT KLRD. SPACER WAS LATER ADJUSTED PROPERLY, GROUND ENGINE RUN WAS NORMAL. ACFT RETURNED TO SERVICE 26 JULY 24.
- [SDR TIMA20240716008](https://openairdocs.org/sdr/TIMA20240716008.md): Engine · faulted · Jul 16, 2024 · N125K · Beech B200C · Engine (Turbine/Turboprop)
  > ON FIANL APPROACH TO LANDING PILOT GOAT A NUMBER 1 ENGINE FUEL PRESSURE LIGHT ON QUICKLY FOLLOWED BY THE SAME ENGINE RILLING BACK AND SHUTTING OFF. AT THIS POINT THE PILOT WAS ON FINAL SO THE PILOT CONTINUED TO LAND AND WAS ABLE TO TAXI BACK.
- [SDR 9LMR202206080001](https://openairdocs.org/sdr/9LMR202206080001.md): Filter · dirty · Jun 8, 2022 · N996LM · Beech 200BEECH · Nacelle/Pylon, Main Frame
  > LH ENG NACELLE VISUAL INSPECTION COMPLIED WITH, LH DRAIN MANIFOLD HAS A LEAK CORRECTIVE ACTION:REMOVED CLEANED AND SERVICED LH ENGINE FUEL COLLECTOR FILTER, IAW BEECHCRAFT KING AIR 200 AMM 71-70-01. NO DISCREPANCIES NOTED AT THIS TIME.ENGINE RUN
- [SDR G1IA20210625012](https://openairdocs.org/sdr/G1IA20210625012.md): Pump · leaking · Jun 25, 2021 · N6728H · Beech 200BEECH · Fuel Boost Pump
  > WHILE ON THE LOADED LEG OF A MEDEVC WITH PILOT, MEDICAL CREW, PATIENT AND FAMILY ESCORT ON BOARD. DURING THE FINAL APPROACH SEGMENT WITH FLAPS SET TO APPROACH, LANDING GEAR RETRACTED, AND VERY SHORTLY AFTER AN ENGINE POWER REDUCTION, AN ODOR OF RAW FUEL WAS DE
- [SDR G1IA20210519008](https://openairdocs.org/sdr/G1IA20210519008.md): Line · leaking · May 19, 2021 · N6728H · Beech C90A · Fuel Controlling System
  > WHILE ON THE RETUEN LEG FROM A MEDEVC WITH ONLY PILOT AND MEDICAL CREW ON BOARD. DURING THE FINAL APPROACH SEGMENT WITH LANDING GEAR EXTENDED, AND VERY SHORTLY AFTER AN ENGINE POWER REDUCTION, A FAINT ODOR OF RAW FUEL WAS DETECTED IN THE CABIN. THE ODOR WENT A
- [SDR 1EAA2021052700158](https://openairdocs.org/sdr/1EAA2021052700158.md): Coupling · failed · Apr 12, 2021 · N389RA · Beech B200C · Engine Fuel Pump
  > FAILURE OF THE #1 ENGINE HP FUEL PUMP DRIVE COUPLING
- [SDR CA190808003](https://openairdocs.org/sdr/CA190808003.md): Heater · malfunctioned · Jul 24, 2019 · Fuel Heater
  > (CAN) DURING TAXI BEFORE TAKEOFF, THE PILOT ELECTED TO SHUT DOWN THE ENGINE DUE TO LACK OF THROTTLE RESPONSE, FOLLOWED BY INCREASING INTER TURBINE TEMPERATURE AND DECREASING RPM. THE AIRCRAFT RETURNED BACK TO AIRPORT UNEVENTFULLY. DURING TROUBLESHOOTING, IT WA
- [SDR TY2A20190712001](https://openairdocs.org/sdr/TY2A20190712001.md): O-Ring · failed · Jul 12, 2019 · N786DD · Beech B200 · Turbine Engine Oil System
  > AIRCRAFT TOOK OFF AND WAS IN CLIMB WHEN PILOT NOTICED A FLUID COMING OUT OF RT COWLING NEAR THE INBOARD EXHAUST STACK. PILOT BEGAN TO RETURN TO AIRPORT. ALL ENGINE INSTRUMENT GAUGES WERE IN GREEN BUT THE FLUID WAS CONTINUING TO COME OUT OF THE COWLING. THE
- [SDR CA190809010](https://openairdocs.org/sdr/CA190809010.md): Sun Gear · distressed · Jul 1, 2019 · Turbine Engine Reduction Gear
  > (CAN) DURING CLIMB AT FL1080, THE RIGHT ENGINE CHIP DETECTOR LIGHT ILLUMINATED. THE PILOT REDUCED ENGINE POWER, AND APPLIED EMERGENCY PROCEDURES AND SHUT-DOWN THE ENGINE AND LANDED UNEVENTFULLY. THE TEARDOWN SHOWED A 1ST STAGE SUN GEAR DISTRESS.. (TC# 20190
- [SDR CA190613006](https://openairdocs.org/sdr/CA190613006.md): Compressor Wheel · distressed · Jun 12, 2019 · Turbine Engine Compressor Section
  > (CAN) KEEWATIN AIR LP, ENGINE WAS SENT TO STANDARDAERO WITH THE OPERATOR REPORTING COMPRESSOR ROTOR DISTRESS. THE OPERATOR ALSO ELECTED TO OVERHAUL THE ENGINE DURING THIS SHOP VISIT. THIS REPORT IS ISSUED TO DISCUSS THE INVESTIGATION FINDINGS RELATING TO THE R
- [SDR CA190624011](https://openairdocs.org/sdr/CA190624011.md): Pump · seized · May 27, 2019 · Beech B200 · Engine Fuel Pump
  > (CAN) `DURING DESCENT THE RIGHT HAND ENGINE EXPERIENCED A FLAMEOUT RESULTING IN AN UN-COMMANDED IN-FLIGHT SHUTDOWN. IT HAD BEEN OBSERVED THAT DURING THIS TIME, THE FUEL FLOW DROPPED TO ZERO PPM. THE CREW CONTINUED TO DESTINED AIRPORT AND LANDED ON A SINGLE ENG
- [SDR CA190415019](https://openairdocs.org/sdr/CA190415019.md): Blade · broken · Apr 14, 2019 · Beech B200 · Turbine Engine Compressor Section
  > (CAN) KING AIR 200 AIRCRAFT WAS ON CLIMB THROUGH APPROXIMATELY FL200, THE RIGHT HAND ENGINE MADE A SINGLE LOUD BANG, A FLAME WAS OBSERVED TO BE EMITTED OUT OF THE EXHAUST, FOLLOWED BY SPARKS. THE FLIGHT CREW CONDUCTED A PRECAUTIONARY ENGINE SHUTDOWN, DECLARED
- [SDR CA190319023](https://openairdocs.org/sdr/CA190319023.md): Gear · failed · Feb 25, 2019 · Turbine Engine Combustion Section
  > (CAN) ENGINE WAS SENT FOR REPAIR WITH THE OPERATOR REPORTING OIL SYSTEM CONTAMINATION.
- [SDR CA190211001](https://openairdocs.org/sdr/CA190211001.md): Fcu · malfunctioned · Jan 31, 2019 · Fuel Control/Turbine Engines
  > (CAN) CUSTOMER REPORTED THAT LEFT ENGINE EXHIBITED UNCONTROLLED ACCELERATION AND THEN OVERTEMP ON THE CLIMB-OUT, AT ABOUT 300FT. DURING THE EVENT THE PILOT ALSO FOUND PILOT COULD NOT CONTROL THE ENGINE WITH THE LEVER, AND PROCEEDED TO DO AN EMERGENCY SHUTDOWN
- [SDR 2020FA0000075](https://openairdocs.org/sdr/2020FA0000075.md): Tube · broken · Nov 12, 2018 · N19CX · Piper PA46500TP · Trailing Edge Flap Control System
  > ON TAKEOFF FROM KEDC, SELECTED GEAR AND FLAPS UP. AIRCRAFT STARTED ROLLING TO THE LEFT HAVING TO USE FULL AILERON TO KEEP IT STRAIGHT, AT THIS POINT PILOT NOTICED RIGHT FLAP WAS DEPLOYED AND LEFT FLAP UP. SELECTED FLAPS DOWN AND WAS ABLE TO REGAIN CONTROL ON
- [SDR CA180314002](https://openairdocs.org/sdr/CA180314002.md): Filler · leaking · Mar 6, 2018 · Beech B200 · Turbine Engine Oil System
  > (CAN) AFTER STARTING THE RIGHT HAND ENGINE, THE PILOT OBSERVED THE ENGINE OIL PRESSURE WAS LOW (80PSI) AND FLUCTUATING +/- 5 PSI. THE PILOT PROCEEDED TO SHUT DOWN THE ENGINE AND OBSERVED THE OIL LEVEL WAS VERY LOW AND APPEARED TO HAVE LEAKED OUT THROUGH THE O
- [SDR CA180207023](https://openairdocs.org/sdr/CA180207023.md): Solenoid Valve · failed · Feb 2, 2018 · Beech B200 · Rudder Control System
  > (CAN) AIRCRAFT REQUIRED LEFT RUDDER INPUT IN FLIGHT AND ON GROUND. MORE THAN NORMAL RUDDER TRIM REQUIRED IN FLIGHT. CORRESPONDING RUDDER BOOST SOLENOID VALVE FOUND FAILED IN OPEN POSITION CAUSING RUDDER BOOST TO ACTUATE SLIGHTLY DURING ALL PHASES OF OPERATIO
- [SDR G1IA2016080260701](https://openairdocs.org/sdr/G1IA2016080260701.md): Wire · separated · Aug 2, 2016 · N607FJ · Beech B200 · Landing Gear System Wiring
  > CAPTAIN AND CO-PILOT HAD FLOWN UNEVENTFULLY AND JOINED THE DOWNWIND WITH THE INTENTION OF LANDING AT APPROXIMATELY 22:15, WHEN SELECTED THE DOWN POSITION WITH THE LANDING GEAR HANDLE AND THE LANDING GEAR REMAINED UP. NO GEAR HANDLE LIGHTS OR GEAR POSITION LIG
- [SDR CA160216012](https://openairdocs.org/sdr/CA160216012.md): Engine · power loss · Feb 12, 2016 · Piper PA46500TP · Engine (Turbine/Turboprop)
  > (CAN) CUSTOMER REPORTS ON TAKE-OFF ENGINE ROLLED BACK ON POWER. CUSTOMER INSTANTLY REDUCED POWER AND ABORTED TAKEOFF AND DID NOT SEE WHAT INSTRUMENTATION WAS READING. NO DAMAGE, INJURIES OR INCIDENT REPORTED.
- [SDR 2016F00045](https://openairdocs.org/sdr/2016F00045.md): Tube · chafed · Jan 19, 2016 · N383JP · Beech 200BEECH · Engine Bleed Air System
  > AFTER TAKEOFF AT 3000 FT AGL, LT BLEED FAIL, LIGHT ILLUMINATED. LT BLEED SWITCH WAS SELECTED "OFF" AND RTB WITH OUT INCIDENT. OVERHEAT DETECTION TUBING UNDER CO-PILOTS FLOOR WAS FOUND CHAFED AND PREVIOUSLY REPAIRED, TUBING WAS REPLACED WITH NEW. LT FIREWALL
- [SDR 5DLA2016F00040](https://openairdocs.org/sdr/5DLA2016F00040.md): Skin · wrinkled · Dec 30, 2015 · N622KM · Beech 200BEECH · Wing, Plate/Skin
  > DURING CRUISE, PILOT ENCOUNTERED SEVERE TURBULENCE WHICH INCLUDED A DESCENT OF ROUGHLY 400 FT IN 2 SECONDS. THE PLANE LANDED SAFELY AT THE INTENDED DESTINATION AIRPORT. GOT A TECH TO INSPECT THE PLANE IAW CH.5-5-00, FIRST LEVEL INSPECTION. SEVERAL SPOTS ON TH
- [SDR CA151215014](https://openairdocs.org/sdr/CA151215014.md): Fuel Control · malfunctioned · Nov 30, 2015 · Cessna 208B · Fuel Control/Turbine Engines
  > (CAN) IN JULY OF THIS YEAR (ENGINE TSN 909), A FCU MALFUNCTION WAS REPORTED BY THE OPERATOR. AN ACCESSORIES SHOP REPLACED THE FUEL CONTROL UNIT (FCU) BELLOWS, AND THE ENGINE WAS RETURNED TO SERVICE. IN OCTOBER, THE ENGINE IS REPORTED TO HAVE HAD A LOSS OF POWE
- [SDR CA150728006](https://openairdocs.org/sdr/CA150728006.md): Horn · dented · Jul 8, 2015 · Piper PA46500TP · Landing Gear Steering System
  > (CAN) DURING A ROUTINE 100 HRS INSPECTION, WE FOUND THAT THE NOSE GEAR STEERING HORN WAS RUBBING WITH THE FRONT ENGINE MOUNT. HORN AND RUB BLOCK WERE REMOVED AND TRIMMED TO ENSURE CLEARANCE BETWEEN ENGINE MOUNT AND STEERING HORN. ENGINE MOUNT DAMAGE INSPECTE
- [SDR CA150518007](https://openairdocs.org/sdr/CA150518007.md): Engine · malfunctioned · Apr 23, 2015 · Piper PA46500TP · Engine (Turbine/Turboprop)
  > (CAN) THE PILOT REPORTED AN OIL CHIP DETECTOR LIGHT, LOW MOP & HIGH MOT. THE EVENT OCCURRED WHILE PERFORMING NEGATIVE ACCELERATION FLIGHT TESTING. THIS IS A PRODUCTION ENG OFF M600 PROTOTYPE ACFT. TROUBLESHOOTING REVEALED RBG METALLIC DEBRIS IN OIL, BRONZE.
- [SDR WF1R2015022600073](https://openairdocs.org/sdr/WF1R2015022600073.md): Duct · cracked · Jan 28, 2015 · N555FW · Beech 200BEECH · Engine Anti-Icing System
  > THE WELDED ASSEMBLY HAD TO BE REMOVED FROM BOTH FORWARD LOWER ENGINE NACELLES DUE TO CRACKING AROUND THE MOUNT FLANGES. WE DRILLED THE WELD ASSY AWAY FROM THE COWLING STRUCTURES. ONLY THEN COULD WE SEE THE INTERNAL CRACKING THROUGH THE STEEL DUCK. THIS PORT
- [SDR CA150120002](https://openairdocs.org/sdr/CA150120002.md): Engine · making metal · Jan 7, 2015 · Piper PA46500TP · Engine (Turbine/Turboprop)
  > (CAN) DURING TAKE OFF, THE AIRCRAFT HAD AN OIL PRESSURE DROP FROM 48 PSI TO 28 PSI. THE PILOT DECLARED AN IFSD AND LANDED WITHOUT INCIDENT. UPON LANDING, THE OIL PRESSURE RETURNED TO NORMAL. THE TROUBLESHOOTING REVEALED METALLIC DEBRIS IN THE OIL FILTER.
- [SDR CA141210007](https://openairdocs.org/sdr/CA141210007.md): Elevator System · binding · Dec 8, 2014 · Cessna 208B · Elevator Tab Control System
  > (CAN) DURING A TRAINING FLIGHT, ON A RECOVERY FROM A SIMULATED FORCED APPROACH ELEVATOR TRIM BECAME JAMMED IN THE FULL NOSE UP POSITION. ATTEMPTS WERE MADE TO TRIM THE AIRCRAFT MANUALLY & ELECTRICALLY BUT TRIM WHEEL WAS JAMMED SOLID. SIGNIFICANT PRESSURE ON
- [SDR CA140826017](https://openairdocs.org/sdr/CA140826017.md): Engine · power loss · Aug 25, 2014 · Piper PA46500TP · Engine (Turbine/Turboprop)
  > (CAN) DURING TAKE-OFF ROLL ENGINE SUFFERED A POWER ROLLBACK. AWAITING FURTHER DETAILS FROM FSR. SERVICE INVESTIGATION PROPOSED TO RETURN THE FCU TO THE MANUFACTURER FOR FURTHER INVESTIGATION.
- [SDR CA140721005](https://openairdocs.org/sdr/CA140721005.md): Engine · power loss · Jul 7, 2014 · Piper PA46500TP · Engine (Turbine/Turboprop)
  > (CAN) PRIOR TO TAKEOFF, THE PILOT OBSERVED A LOW PROPELLER SPEED FOLLOWED BY A LOSS OF POWER. FIRE IN THE ENGINE COMPARTMENT WAS REPORTED WHICH HAD EXTINGUISHED BEFORE THE FIRE DEPT ARRIVED.
- [SDR CA140619016](https://openairdocs.org/sdr/CA140619016.md): Engine · malfunctioned · Jun 4, 2014 · Piper PA46500TP · Engine (Turbine/Turboprop)
  > (CAN) PILOT STARTED THE ENGINE AND NOTICED THAT THE ENGINE DID NOT RESPOND TO POWER LEVER INPUT. PILOT ELECTED TO USE EMERGENCY MANUAL OVERRIDE LEVER TO TAXI FOR TAKE OFF. PILOT APPLIED EMERGENCY MANUAL OVERRIDE LEVER FOR TAKEOFF AND DURING TAKEOFF ROLL HE NOT
- [SDR CA140505008](https://openairdocs.org/sdr/CA140505008.md): Engine · warning light · Apr 11, 2014 · Beech 200BEECH · Engine (Turbine/Turboprop)
  > (CAN) THE CREW OBSERVED THE CHIP LIGHT ON THE LT ENGINE. THEY PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN AND DECLARED AN EMERGENCY. CONTINUED TO DESTINATION AND LANDED. A POST FLIGHT INSPECTION REVEALED SIGNS OF METAL IN THE ENGINE OIL. THE ENGINE WAS REMOVE
- [SDR CA140224027](https://openairdocs.org/sdr/CA140224027.md): Bolt · broken · Feb 23, 2014 · Cessna 208B · Landing Gear Brake System
  > (CAN) ON LANDING, PILOT COMPLAINED ABOUT RT WHEEL BEING LOCKED UP, THEN LETTING LOOSE AGAIN. ON INSPECTION, FOUND BRAKE CYLINDER ASSY, CALIPER LOOSE ON DISK. BOTTOM RETAINING PIN, ANCHOR BOLT WAS MISSING, WITH THE THREAD AND LOCKNUT MISSING AS WELL. THE TOP
- [SDR EPUA20131011002](https://openairdocs.org/sdr/EPUA20131011002.md): Fuel Control · defective · Oct 9, 2013 · N215MC · Cessna 208B · Fuel Control/Reciprocating Engines
  > ENGINE STUCK AT HIGH POWER. POWER LEVER NON-RESPONSIVE, MADE EMERGENCY IDLE CUT-OFF LANDING. NO CONTAMINATION OF FCU INLET OR OUTLET FILTERS FOUND. NO CONTAMINATION OF P3 FILTER ASSY. DISCREPANCY DISCOVERED DURING LANDING. LANDING WAS ABORTED AND ACFT RETURNE
- [SDR CA131021012](https://openairdocs.org/sdr/CA131021012.md): Fuel Control · faulted · Oct 9, 2013 · Cessna 208B · Fuel Control/Reciprocating Engines
  > (CAN) UPON REDUCING POWER FOR INITIAL DESCENT TO DESTINATION, THE ENGINE DID NOT REACT. THE PILOT REDUCED THE POWER LEVER TO FLIGHT IDLE AND STILL NO RESPONSE. HE THEN ELECTED TO RETURN TO THEIR MAINTENANCE BASE. ON SHORT FINAL, THE ENGINE WAS SHUTDOWN USI
- [SDR CA130822002](https://openairdocs.org/sdr/CA130822002.md): Engine · flamed out · Aug 16, 2013 · Cessna 208B · Engine (Turbine/Turboprop)
  > (CAN) AFTER THE SEAL REPLACEMENT ACFT WAS TAXING TO THE TARMAC FOR GROUND RUN. DURING TAXIING, THE ENGINE HAD AN UNCOMMANDED SHUTDOWN WHEN ENGINE WAS AT LOW IDLE. A WHITE SMOKE WAS NOTICED THROUGH THE EXHAUST. A START WAS DONE AFTER THE EVENT AND WAS NORMAL.
- [SDR CA130717003](https://openairdocs.org/sdr/CA130717003.md): Blades · damaged · Jun 28, 2013 · Cessna 208B · Turbine Engine Compressor Section
  > (CAN) DURING ROUTINE FUEL NOZZLE CHANGE, A BOROSCOPE INSPECTION OF THE HOT SECTION WAS CONDUCTED. IT WAS DISCOVERED THAT ALL THE CT BLADES HAD DAMAGE ON THE OUTER TIP OF THE BLADES. IT IS UNCLEAR IF THIS WAS CAUSED BY FOD, ITT OVERTEMP OR MATERIAL FAILURE. THE
- [SDR 2013FA0000276](https://openairdocs.org/sdr/2013FA0000276.md): Windshield · failed · May 13, 2013 · N60AR · Beech B200 · Flight Compartment Windows
  > IN LEVEL CRUISE FLIGHT, WITH WINDSHIELD HEAT ON. THE CO PILOT WINDSHIELD INNER PLY CRACKED/SHATTERED. A NORMAL LANDING WAS MADE FOLLOWING THE ABNORMAL CHECKLIST FOR A FAILED WINDSHIELD. NO INJURIES AND NO OTHER DAMAGE OR PRESSURIZATION LOSS WAS EXPERIENCED.
- [SDR ZESA2013F00107](https://openairdocs.org/sdr/ZESA2013F00107.md): Fcu · malfunctioned · Apr 24, 2013 · N5AE · Beech 200BEECH · Fuel Control/Turbine Engines
  > AIRCRAFT WAS REPORTED AS HAVING A YAW ON APPROACH WHEN REDUCING POWER ON THE ENGINES. THE ROOT CAUSE WAS THE RT ENGINE FUEL CONTROL UNIT (FCU). THE FCU WOULD FLUCTUATE WHEN THE ACFT WAS ON APPROACH WHEN THE ENGINE POWER WAS BEING REDUCED. FCU REPLACED AND A
- [SDR CA130430012](https://openairdocs.org/sdr/CA130430012.md): Engine · power loss · Mar 13, 2013 · Piper PA46500TP · Engine (Turbine/Turboprop)
  > (CAN) DURING A SIMULATED FORCED LANDING, THE PILOT STATED THAT HE CLIMBED TO FL35 AND INITIATED SPIRAL TURNS FOR A LT TRAFFIC APPROACH TO THE RUNWAY. DURING FINAL APPROACH, THE ACFT STARTED DESCENDING AT A HIGHER RATE THAN EXPECTED. THE PILOT ATTEMPTED TO IN
- [SDR CA130118008](https://openairdocs.org/sdr/CA130118008.md): Check Valve · failed · Jan 17, 2013 · Piper PA46500TP · Fuel Controlling System
  > (CAN) FUEL PURGE TANK CHECK VALVE FOUND TO BE UNSERVICEABLE DURING ROUTINE INSPECTION/FUNCTION CHECK.
- [SDR CA121125003](https://openairdocs.org/sdr/CA121125003.md): Fuel Control · malfunctioned · Nov 7, 2012 · Fuel Control/Turbine Engines
  > (CAN) DURING TAXI, THE ENGINE POWER COULD NOT BE ADVANCED PAST 47 PERCENT NG NO OTHER DETAILS ARE AVAILABLE. TROUBLESHOOTING LED TO THE REPLACEMENT OF THE FUEL CONTROL, WHICH WILL BE SENT FOR INVESTIGATION.
- [SDR CA121228008](https://openairdocs.org/sdr/CA121228008.md): Fuel Control · power loss · Nov 7, 2012 · Fuel Control/Turbine Engines
  > (CAN) DURING TAXI, THE ENGINE POWER COULD NOT BE ADVANCED PAST 47 PERCENT NG. NO OTHER DETAILS ARE AVAILABLE. TROUBLESHOOTING LED TO THE REPLACEMENT OF THE FUEL CONTROL, WHICH WILL BE SENT FOR INVESTIGATION.
- [SDR G1IA20120914001](https://openairdocs.org/sdr/G1IA20120914001.md): Transistor · shorted · Sep 13, 2012 · N983C · Beech 200BEECH · Flight Compartment Lighting
  > ON APPROACH THE PILOT NOTICED SMOKE IN THE COCKPIT. PILOT PUT ON OXYGEN MASK AND LANDED WITHIN FIVE MINUTES WITHOUT FURTHER PROBLEMS. MAINTENANCE FOUND RESISTOR R19, A 100 OHKM 2 WATT RESISTOR, CRACKED FROM HEAT. TRANSISTOR Q7 WAS SHORTED FROM BASE TO EMITT
- [SDR CA120917003](https://openairdocs.org/sdr/CA120917003.md): Engine · malfunctioned · Sep 1, 2012 · Piper PA46500TP · Engine (Turbine/Turboprop)
  > (CAN) DURING DESCENT, AFTER THE PILOT RETARDED THE THROTTLE TO IDLE, REALIZED THAT THE TORQUE INDICATION WAS AT ZERO. THE PILOT CLOSED THE BLEED AIR AND THE AIR CONDITIONING SYSTEM AND PUSHED THE THROTTLE LEVER TO MAX. POSITION WITH NO RESPONSE FROM THE ENG
- [SDR 7EMA20120808429](https://openairdocs.org/sdr/7EMA20120808429.md): Fuel Control · inoperative · Aug 8, 2012 · N429EM · Beech 200BEECH · Fuel Control/Turbine Engines
  > ON DECENT, THE RT ENGINE FAILED TO RESPOND TO POWER LEVER MOVEMENT, TORQUE REMAINED AT 2000 LBS. AFTER TRYING SEVERAL TIMES TO GET RT ENGINE TO RESPOND BY MOVING POWER LEVER FORWARD AND AFT, ENGINE WAS SECURED, DECLARED EMERGENCY AND MADE SAFE LANDING. REMOV
- [SDR 7EMA20120806429](https://openairdocs.org/sdr/7EMA20120806429.md): Linkage · dirty · Aug 6, 2012 · N429EM · Beech 200BEECH · Power Lever
  > ON DESCENT, THE RT ENGINE FAILED TO RESPOND TO POWER-LEVER MOVEMENT, TORQUE REMAINED AT 2000 LBS. AFTER TRYING SEVERAL TIMES TO GET RT ENGINE TO RESPOND BY MOVING POWER LEVER FORWARD AND AFT, ENGINE WAS SECURED, DECLARED EMERGENCY AND MADE SAFE LANDING. MX C
- [SDR 2012FA0000590](https://openairdocs.org/sdr/2012FA0000590.md): Compressor Blade · damaged · Jul 17, 2012 · N248PA · Cessna 208B · Turbine Engine Compressor Section
  > PILOT REPORTED A BANGING NOISE DURING TAXI COMING FROM THE ENGINE. PILOT THEN TAXIIED TO THE HANGAR AND BROUGHT IT TO MECHANIC ON DUTY THAT DAY. MECHANIC THEN BOROSCOPE ENGINE AND FOUND FIRST STAGE COMPRESSOR HAS MINOR NORMAL WEAR AND TEAR, FIRST STAGE COMPR
- [SDR CA120802001](https://openairdocs.org/sdr/CA120802001.md): Blades · damaged · Jul 17, 2012 · Turbine Engine Compressor Section
  > (CAN) DURING TAXI FOR T/O, THE PASSENGERS ON BOARD HEARD A CHANGE IN ENGINE PITCH NOISE AND ALERTED THE PILOT WHO IMMEDIATELY ABORTED HIS T/O PROCEDURES. THE ACFT WAS RETURNED TO THE BASE WHERE GROUND TEST REVEALED THAT THE ENGINE COULD NOT REACH T/O POWER DUE

Next page: https://openairdocs.org/engine/u-a-canada-pt6a-42/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 = 'PT6A42'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/u-a-canada-pt6a-42/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.