# Service difficulty reports: Pratt & Whitney Canada PT6A-64

A list on [Pratt & Whitney Canada PT6A-64](https://openairdocs.org/engine/pratt-whitney-canada-pt6a-64.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 59 reports

- [SDR 2016FA0000608](https://openairdocs.org/sdr/2016FA0000608.md): Fuel Control · malfunctioned · Dec 10, 2016 · N8EG · Socata TBM700 · Fuel Control/Turbine Engines
  > ENGINE HANGS DURING START BELOW 40%. SEND FOR RE-CALIBRATION.
- [SDR 2016FA0000609](https://openairdocs.org/sdr/2016FA0000609.md): Fuel Control · malfunctioned · Dec 10, 2016 · N8EG · Socata TBM700 · Fuel Control/Turbine Engines
  > AFTER RECEIPT OF FCU AFTER RE-CALIBRATION ENGINE WILL START NORMALLY BUT WILL NOT MAKE MAX REVERSE CHECK. SEND OUT FOR RE-CAL.
- [SDR 2016FA0000610](https://openairdocs.org/sdr/2016FA0000610.md): Fuel Control · malfunctioned · Dec 10, 2016 · N213RE · Socata TBM700 · Fuel Control/Turbine Engines
  > MAX REVERSE FAILED CHECK. RE-CALIBRATE FCU.
- [SDR 2016FA0000611](https://openairdocs.org/sdr/2016FA0000611.md): Fuel Control · malfunctioned · Dec 10, 2016 · N213RE · Socata TBM700 · Fuel Control/Turbine Engines
  > ENGINE SURGES IN MAX REVERSE. FCU TO RECALIBRATE.
- [SDR 2016FA0000625](https://openairdocs.org/sdr/2016FA0000625.md): Fuel Control · malfunctioned · Nov 19, 2016 · N700GQ · Socata TBM700 · Fuel Control/Turbine Engines
  > ITT LIGHT WHEN GOING INTO MAX REVERSE. RECALIBRATE FCU.
- [SDR 2016FA0000623](https://openairdocs.org/sdr/2016FA0000623.md): Fuel Control · abnormal · Oct 17, 2016 · N700G · Socata TBM700 · Fuel Control/Turbine Engines
  > MAX ITT LIGHT WHEN GOING INTO MAX REVERSE. RE-CALIBRATE FCU.
- [SDR 2016FA0000622](https://openairdocs.org/sdr/2016FA0000622.md): Fuel Control · malfunctioned · Aug 16, 2016 · Socata TBM700 · Fuel Control/Turbine Engines
  > ENGINE STARTING WARM. RE-CALIBRATE FCU.
- [SDR 2016FA0000621](https://openairdocs.org/sdr/2016FA0000621.md): Fuel Control · malfunctioned · Jul 26, 2016 · Socata TBM700 · Fuel Control/Turbine Engines
  > ENGINE STATING WARM. RE-CALIBRATE FCU.
- [SDR 2016FA0000620](https://openairdocs.org/sdr/2016FA0000620.md): Fuel Control · malfunctioned · Mar 25, 2016 · Socata TBM700 · Fuel Control/Turbine Engines
  > ENGINE STARTS WARM. RE-CALIBRATE FCU.
- [SDR 2016FA0000624](https://openairdocs.org/sdr/2016FA0000624.md): Fuel Control · malfunctioned · Jan 24, 2016 · N220NA · Socata TBM700 · Fuel Control/Turbine Engines
  > ENGINE STARTING WARM AND SLOW STARTS. RE-CALIBRATE FCU.
- [SDR CA160120012](https://openairdocs.org/sdr/CA160120012.md): Governor · faulted · Jan 3, 2016 · Propeller Governor
  > (CAN) DURING CRUISE, WITH THE POWER SETTING ABOVE 80 PERCENT, THE PILOT REPORTED 5 PERCENT TO 15 PERCENT TORQUE FLUCTUATIONS, WITH ASSOCIATED TEMP VARIATIONS, UNSPECIFIED VALUE. HE ELECTED TO DIVERT. TROUBLESHOOTING IDENTIFIED A POSSIBLE FAULTY PROPELLER GOV
- [SDR 2016FA0000617](https://openairdocs.org/sdr/2016FA0000617.md): Fcu · malfunctioned · Sep 21, 2015 · N777FX · Socata TBM700 · Fuel Control/Turbine Engines
  > HIGH TEMPS DURING START. RE-CLAIBRATE FCU.
- [SDR 2016FA0000615](https://openairdocs.org/sdr/2016FA0000615.md): Fuel Control · malfunctioned · Sep 9, 2015 · N622PK · Socata TBM700 · Fuel Control/Turbine Engines
  > MAX ITT LIGHT COMES ON WHEN PULLING INTO MAX REVERSE. RE-CALIBRATE FCU.
- [SDR 2016FA0000616](https://openairdocs.org/sdr/2016FA0000616.md): Fcu · malfunctioned · Aug 18, 2015 · N773TC · Socata TBM700 · Fuel Control/Turbine Engines
  > ENGINE START TEMPS EXCESSIVE. RECALIBRATE FCU.
- [SDR 2016FA0000614](https://openairdocs.org/sdr/2016FA0000614.md): Fuel Control · malfunctioned · Aug 7, 2015 · N773TC · Socata TBM700 · Fuel Control/Turbine Engines
  > FAILED MAX REVERSE CHECK. RE-CALIBRATED FCU.
- [SDR 2016FA0000595](https://openairdocs.org/sdr/2016FA0000595.md): Fuel Control · out of limits · May 5, 2015 · N753BD · Socata TBM700 · Fuel Control/Turbine Engines
  > MANUAL OVER RIDE LOWER THAN 40 PERCENT AND FUEL FLOW LOWER THAN 60 PERCENT. FUEL CONTROL UNIT CONTACTING STOPS.
- [SDR 2016FA0000597](https://openairdocs.org/sdr/2016FA0000597.md): Fuel Control · abnormal · Dec 8, 2014 · N700HK · Socata TBM700 · Fuel Control/Turbine Engines
  > ENGINE IS SLOW TO START AND NOT MAKING MAX REVERSE. CALIBRATED FUEL CONTROL UNIT.
- [SDR CA141024008](https://openairdocs.org/sdr/CA141024008.md): Oil System · low pressure · Oct 5, 2014 · Socata TBM700 · Engine Oil Indicating System
  > (CAN) WHILE ENROUTE, HAD AN INDICATION OF LOW OIL PRESSURE. THE PILOT WAS UNABLE TO LAND. WHILE MANEUVERING FOR A FORCED LANDING ON A FOOTBALL FIELD THE AIRPLANE COLLIDED WITH TREES THAT SEPARATED THE RT WING. THE AIRPLANE CAME TO REST UPRIGHT ON THE FO
- [SDR 2016FA0000596](https://openairdocs.org/sdr/2016FA0000596.md): Fuel Control · abnormal · Aug 9, 2014 · N327MM · Socata TBM700 · Fuel Control/Turbine Engines
  > ENGINE IS SLOW TO START. FUEL CONTROL UNIT HAD TO BE RE-CALIBRATED.
- [SDR 2014FA0000294](https://openairdocs.org/sdr/2014FA0000294.md): Structure · contaminated · Apr 10, 2014 · N356F · Socata TBM700 · Horizontal Stabilizer Structure
  > HORIZONTAL STABILIZER STRUCTURE COMPROMISED BY APPARENT WATER DAMAGE CREATING CRACKS AND CORROSION. DEFECTS WITHIN THE PRIMARY STRUCTURE OF THE HORIZONTAL STABILIZER. HONEYCOMB CORE CONTAMINATED WITH WATER INTRUSION.
- [SDR CA131007007](https://openairdocs.org/sdr/CA131007007.md): Fuel Control · malfunctioned · Sep 22, 2013 · Socata TBM700 · Fuel Control/Turbine Engines
  > (CAN) DURING FLIGHT, THE ENGINE TQ STAYED AT 72.7 PERCENT AND THE ENGINE ITT WAS 752. IT REMAINED BELOW 72.7 PERCENT EVEN WHEN THE MANUAL OVERRIDE USED TO 100 PERCENT TORQUE. THE FCU WAS REMOVED FOR INVESTIGATION.
- [SDR RL8R2013FA0000541](https://openairdocs.org/sdr/RL8R2013FA0000541.md): Roll Pin · loose · Aug 28, 2013 · N144JT · Socata TBM700 · Ailerons
  > DURING A ROUTINE ANNUAL INSPECTION, THE LT AND RT AILERON MOUNTING PIVOT POINT ROLL PINS WERE FOUND TO BE LOOSE AND WORKING.
- [SDR RL8R2013FA0000542](https://openairdocs.org/sdr/RL8R2013FA0000542.md): Roll Pin · loose · Aug 28, 2013 · N700ZZ · Socata TBM700 · Ailerons
  > DURING A ROUTINE ANNUAL INSPECTION, THE LT & RT INBD AILERON MOUNTING PIVOT POINTS ROLL PINS WERE FOUND TO BE LOOSE AND WORKING.
- [SDR RL8R2013FA0000543](https://openairdocs.org/sdr/RL8R2013FA0000543.md): Roll Pin · loose · Aug 28, 2013 · N702GS · Socata TBM700 · Ailerons
  > DURING A ROUTINE ANNUAL INSPECTION, THE LT & RT INBD AILERON MOUNTING PIVOT POINT ROLL PINS WERE FOUND TO BE LOOSE AND WORKING.
- [SDR RL8R2013FA0000544](https://openairdocs.org/sdr/RL8R2013FA0000544.md): Roll Pin · loose · Aug 28, 2013 · N700MX · Socata TBM700 · Ailerons
  > DURING A ROUTINE ANNUAL INSPECTION, THE LT INBD AILERON MOUNTING PIVOT POINT ROLL PIN WAS FOUND TO BE LOOSE AND WORKING.
- [SDR CA130610001](https://openairdocs.org/sdr/CA130610001.md): Engine · malfunctioned · Jun 10, 2013 · Engine (Turbine/Turboprop)
  > (CAN) EIR PT6A 2013-039, ENGINE WAS SENT FOR INVESTIGATION AFTER THE CUSTOMER REPORTED A LOSS OF OIL PRESSURE FOLLOWED BY AN IN-FLIGHT SHUTDOWN. ACCORDING TO INFORMATION RECEIVED FROM THE CUSTOMER, SOON AFTER TAKEOFF, A SLIGHT VIBRATION WAS FELT FROM THE ENGI
- [SDR CA130603004](https://openairdocs.org/sdr/CA130603004.md): Engine · making metal · May 15, 2013 · Socata TBM700 · Engine (Turbine/Turboprop)
  > (CAN) THE PILOT REPORTED THAT 5 MINUTES AFTER TAKEOFF DURING CLIMB HE FELT A SLIGHT VIBRATION AND THE OIL PRESSURE WENT MOMENTARILY IN TO THE YELLOW RANGE. THE PILOT MADE RIGHT TURN TO RETURN TO HOME BASE WITH THE LOP WARNING LLUMINATED AND A GROWL NOISE BEING
- [SDR CA130502001](https://openairdocs.org/sdr/CA130502001.md): Engine · power loss · Apr 28, 2013 · Socata TBM700 · Engine (Turbine/Turboprop)
  > (CAN) SHORTLY AFTER T/O, A LOSS OF ENGINE POWER OCCURRED AND THE A/C MADE A FORCED WHEELS UP LANDING IN AN OPEN FIELD. NO ONE ON BOARD WAS SERIOUSLY INJURED. THE A/C SUFFERED DAMAGE TO THE PROPELLER AND LOWER FUSELAGE. OFFER OF ASSISTANCE WILL BE MADE TO THE D
- [SDR CA130401008](https://openairdocs.org/sdr/CA130401008.md): Oil System · overheated · Mar 25, 2013 · Engine Oil Temperature
  > (CAN) DURING CRUISE FLIGHT AT FL260, THE OIL TEMPERATURE WAS OBSERVED TO EXCEED THE RED LINE. THE PILOT PERFORMED AN EMERGENCY DESCENT TO FL20 AND DECLARED AN EMERGENCY. THE ENGINE WAS REDUCED TO IDLE POWER DURING DESCENT AND THE ACFT WAS LANDED UNEVENTFULLY
- [SDR 2013FA0000281](https://openairdocs.org/sdr/2013FA0000281.md): Insert · loose · Mar 13, 2013 · N700WK · Socata TBM700 · Trailing Edge Flaps
  > INBD FLAP CARRIAGE INSERTS HAVE LOOSENED UP UNDER NORMAL USE. COULD POSSIBLY LEAD TO FLAP CARRIAGE ATTACHMENT FAILURE DURING FLAP DEPLOYMENT WITH SUBSEQUENT LOSS OF FLAP OR WORSE. REQUIRES REPAIR TO FLAP END AND INSTALLATION OF NEW FLAP CARRIAGE INSERTS. TH
- [SDR 2013FA0000282](https://openairdocs.org/sdr/2013FA0000282.md): Insert · loose · Mar 13, 2013 · N700WK · Socata TBM700 · Trailing Edge Flaps
  > INBD FLAP CARRIAGE INSERTS HAVE LOOSENED UP UNDER NORMAL USE. COULD POSSIBLY LEAD TO FAP CARRIAGE ATTACHMENT FAILURE DURING FLAP DEPLOYMENT WITH SUBSEQUENT LOSS OF FLAP OR WORSE. REQUIRES REPAIR TO FLAP END AND INSTALLATION OF NEW FLAP CARRIAGE INSERTS. THI
- [SDR 2013FA0000283](https://openairdocs.org/sdr/2013FA0000283.md): Insert · loose · Mar 13, 2013 · N702AV · Socata TBM700 · Trailing Edge Flaps
  > INBOARD FLAP CARRIAGE INSERTS HAVE LOOSENED UP UNDER NORMAL USE. COULD POSSIBLY LEAD TO FAP CARRIAGE ATTACHMENT FAILURE DURING FLAP DEPLOYMENT WITH SUBSEQUENT LOSS OF FLAP OR WORSE. REQUIRES REPAIR TO FLAP END AND INSTALLATION OF NEW FLAP CARRIAGE INSERTS.
- [SDR 2014FA0000149](https://openairdocs.org/sdr/2014FA0000149.md): Insert · loose · Mar 13, 2013 · N700WK · Socata TBM700 · Trailing Edge Flaps
  > INBD FLAP CARRIAGE INSERTS HAVE LOOSENED UP UNDER NORMAL USE. COULD POSSIBLY LEAD TO FLAP CARRIAGE ATTACHMENT FAILURE DURING FLAP DEPLOYMENT WITH SUBSEQUENT LOSS OF FLAP OR WORSE. REQUIRES REPAIR TO FLAP END AND INSTALLATION OF NEW FLAP CARRIAGE INSERTS. TH
- [SDR RL8R2014030700150](https://openairdocs.org/sdr/RL8R2014030700150.md): Carriage · damaged · Mar 13, 2013 · N700WK · Socata TBM700 · Trailing Edge Flaps
  > INBD FLAP CARRIAGE INSERTS HAVE LOOSENED UP UNDER NORMAL USE. COULD POSSIBLY LEAD TO FLAP CARRIAGE ATTACHMENT FAILURE DURING FLAP DEPLOYMENT WITH SUBSEQUENT LOSS OF FLAP OR WORSE. REQUIRES REPAIR TO FLAP END AND INSTALLATION OF NEW FLAP CARRIAGE INSERTS. TH
- [SDR CA130116005](https://openairdocs.org/sdr/CA130116005.md): Fuel Nozzle · malfunctioned · Dec 18, 2012 · Fuel Injector Nozzle
  > (CAN) FOLLOWING AN ENGINE CHANGE, THE CREW PERFORMED A FLIGHT TO PERFORM CUTOFF AND RELIGHT TEST. THE ENGINE DID NOT RELIGHT AFTER 2 ATTEMPTS. A SINGLE ENGINE UNEVENTFUL LANDING WAS PERFORMED. THE ENGINE DID NOT RELIGHT DURING THE ON GROUND INVESTIGATION. T
- [SDR CA120821002](https://openairdocs.org/sdr/CA120821002.md): Engine · power loss · Aug 8, 2012 · Engine (Turbine/Turboprop)
  > (CAN) DURING CLIMB AT 1900 FT, THE PILOT HEARD ABNORMAL NOISES FROM THE ENGINE FOLLOWED BY EXHAUST SMOKE AND POWER LOSS. THE PILOT SECURED THE ENGINE INTO FEATHER MODE. THE ACFT LANDED SAFELY. PRELIMINARY INSPECTION REVEALED SEIZED PROPELLER SHAFT.
- [SDR CA120723001](https://openairdocs.org/sdr/CA120723001.md): Oil System · malfunctioned · Jul 10, 2012 · Socata TBM700 · Engine Oil Pressure
  > (CAN) THE PILOT REPORTED THAT THE OIL PRESSURE HAS DECREASED STEADILY FOR THE PAST 4 FLIGHTS, ENDING VERY CLOSE TO THE YELLOW BAND IN CRUISE ON THE LAST FLIGHT. THE TORQUE ALSO WENT DOWN ON THE LAST FLIGHT, THE PILOT COULD ACTUALLY FEEL IT. AFTER LANDING, TH
- [SDR 2012FA0000081](https://openairdocs.org/sdr/2012FA0000081.md): Fuel Control · failed · Jan 31, 2012 · N701QD · Socata TBM700 · Fuel Control/Turbine Engines
  > DURING RUNUP, PROP FEATHER CHECK CONDUCTED NORMALLY. WHEN ADVANCING POWER LEVER TO DO A PROP OVERSPEED TEST, COULD NOT REACH 1900 RPM WITH POWER LEVER FORWARD. HIGHEST RPM ACHIEVED WAS 1700. SHUTDOWN AND RESTART. DURING THE START, AT LOW IDLE, FLAMES SHOT
- [SDR CA120129001](https://openairdocs.org/sdr/CA120129001.md): Fuel Control · failed · Jan 13, 2012 · Socata TBM700 · Fuel Control/Turbine Engines
  > (CAN) WHILE PREPARING FOR THE SCHEDULED NIGHT FLIGHTS, AFTER NORMAL ENGINE START, WHILE RUNNING UP TO PERFORM THE FEATHERING CHECK, THE ENGINE COULD ONLY ACHIEVE 1700 RPM ON THE PROPELLER WHERE 1900 RPM SHOULD HAVE BEEN AVAILABLE WITH THROTTLE FULL FORWARD. FL
- [SDR 2011FA0000329](https://openairdocs.org/sdr/2011FA0000329.md): Gasket · separated · May 26, 2011 · N175JB · Socata TBM700 · Propeller Governor
  > PROPELLER OVERSPEED GOVERNOR TO ENGINE PAD GASKET FAILED CAUSING LOSS OF OIL.
- [SDR CA110516016](https://openairdocs.org/sdr/CA110516016.md): Gasket · leaking · May 9, 2011 · Turbine Engine Oil System
  > (CAN) OIL LEAK 5 MILES OUT, THE ENGINE HAD A MAJOR OIL LOSS. THE PILOT ELECTED TO RETURN TO THE DEPARTURE AIRPORT WITHOUT SHUTTING THE ENGINE DOWN. AN UNEVENTFUL LANDING WAS MADE. GROUND INSP FOUND NO OIL LEFT IN THE ENGINE. THE PROBLEM WAS TRACED BACK TO A L
- [SDR 2010FA0000931](https://openairdocs.org/sdr/2010FA0000931.md): Control Cable · broken · Sep 1, 2010 · N843BH · Socata TBM700 · Engine Controls
  > PERFORMED NORMAL START, NOTED LOW IDLE LOW, MOVED CONDITION LEVER TO HIGH IDLE WITH NO RESPONSE FROM ENGINE, TRIED SEVERAL TIMES & HAD NO RESPONSE. PERFORMED ENGINE SHUTDOWN. MOVED CONDITION LEVER IN COCKPIT WHILE 2ND PERSON WATCHED MOVEMENT ON FCU. MOVEMENT
- [SDR CA100608001](https://openairdocs.org/sdr/CA100608001.md): Electrical Sys · unknown · May 23, 2010 · Electrical Power System
  > ACCIDENT DURING CRUISE AT FL130, THE ACFT RUDDER STOPPED RESPONDING, GETTING STUCK FULL LT. PILOT MANAGED TO MAINTAIN CONTROL BUT HE THEN SAW THAT BOTH GPS`S WENT OUT FOLLOWED BY LOW FUEL PRESSURE WARNING AND ENGINE SPOOL DOWN. FEATHERED THE PROPELLER AND ASK
- [SDR GLBA200911301](https://openairdocs.org/sdr/GLBA200911301.md): Linkage · out of adjust · Nov 28, 2009 · N253GL · Beech 1900D · Propeller Feathering/Reversing
  > RT AUTO FEATHER ENGAGED ON APPROACH TO LANDING AT 780 FT AGL AS PWR WAS INCREASED FROM IDLE THROUGH 600LBS OF TORQUE. WHEN THE AUTO FEATHER ENGAGED IT WENT IN AND OUT OF FEATHER SEVERAL TIMES BEFORE MORE PWR WAS APPLIED AND THE AUTO FEATHERING CYCLE STOPPED O
- [SDR 2009FA0000623](https://openairdocs.org/sdr/2009FA0000623.md): Shaft · fractured · Jul 10, 2009 · N708PW · Socata TBM700 · Turbine Section
  > DURING START ATTEMPT, THE POWER SECTION DID NOT ROTATE WHEN THE NG REACHED 13 PERCENT. START WAS ABORTED AND PROPELLER TURNED BY HAND. A NOISE WAS HEARD FROM THE EXHAUST STACK AND DRAGGING/BINDING WAS FELT. POWER SECTION WAS REMOVED AND SENT FOR TROUBLESHO
- [SDR 2007FA0000328](https://openairdocs.org/sdr/2007FA0000328.md): Fitting · cracked · Apr 6, 2007 · N704QD · Socata TBM700 · Rudder/Tab, Attach Fittings
  > DURING A 6000HR/10 YEAR CORROSION INSPECTION AD2007-06-11 WAS BEING COMPLIED IAW AD AND MANDATORY SB70-=104, AMENDMENT 2. AFTER COMPLETING THE PENETRANT INSPECTION NO CRACKS WERE DETECTED IN THE SPECIFIED AREAS HOWEVER THE FITTINGS LISTED IN BLOCK 5 WERE REMO
- [SDR 2007FA0000329](https://openairdocs.org/sdr/2007FA0000329.md): Fitting · corroded · Apr 6, 2007 · N704QD · Socata TBM700 · Horizontal Stabilizer Structure
  > DURING A 6000HR/10 YEAR CORROSION INSPECTION AD2007-06-11 WAS BEING COMPLIED IAW AD AND MANDATORY SB70-104, AMENDMENT 2. AFTER COMPLETING THE PENETRANT INSPECTION, NO CRACKS WERE DETECTED IN THE SPECIFIED AREAS HOWEVER THE FITTINGS LISTED IN BLOCK 5 WERE REMO
- [SDR CA061006020](https://openairdocs.org/sdr/CA061006020.md): Engine · seized · Sep 25, 2006 · Socata TBM700 · Engine (Turbine/Turboprop)
  > (CAN) ENGINE OIL TEMPERATURE WAS SEEN TO INCREASE IN FLIGHT ACCOMPANIED BY A LOSS OF OIL PRESSURE. THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED OIL IN THE ENGINE DRAINS AND SEIZURE OF THE POWER SECTION. MFG WILL INVESTIGATE THE EVENT AN
- [SDR CA061103004](https://openairdocs.org/sdr/CA061103004.md): Oil System · overtemp · Sep 25, 2006 · Socata TBM700 · Turbine Engine Oil System
  > (CAN) IN FLIGHT ENGINE OIL TEMPERATURE WAS SEEN TO INCREASE ACCOMPANIED BY A DROP IN OIL PRESSURE. THE ENGINE WAS SHUTDOWN IN FLIGHT. POST FLIGHT INSPECTION REVEALED DEBRIS IN THE ENGINE OIL SYSTEM AND EVIDENSE OF OIL LEAKAGE FROM THE ENGINE DRAIN. MFG WILL
- [SDR CA061219022](https://openairdocs.org/sdr/CA061219022.md): Engine · leaking · Sep 25, 2006 · Socata TBM700 · Turbine Engine Oil System
  > (CAN) IN FLIGHT THE ENGINE OIL TEMPERATURE INCREASED ACCOMPANIED BY A LOSS OF OIL PRESSURE. THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED METAL CONTAMINATION OF THE OIL SYSTEM, INTERNAL OIL LEAKAGE AND SEIZURE OF THE REDUCTION GEAR BOX.

Next page: https://openairdocs.org/engine/pratt-whitney-canada-pt6a-64/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 = 'PT6A64'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/pratt-whitney-canada-pt6a-64/reports

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