# Service difficulty reports: Pratt & Whitney Canada PT6A-67AG

A list on [Pratt & Whitney Canada PT6A-67AG](https://openairdocs.org/engine/pratt-whitney-canada-pt6a-67ag.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 87 reports

- [SDR 2024F00294](https://openairdocs.org/sdr/2024F00294.md): Breather Tube · misrouted · Nov 19, 2024 · N3324T · Dhav DHC3 · Engine (Turbine/Turboprop)
  > SMOKE IN CABIN. CORRECTIVE ACTION: FOUND ENGINE BREATHER TUBE MIS-ROUTED CAUSING BREATHER VAPORS TO ENTER THE LOWER FUSELAGE.
- [SDR 2021FA0000043](https://openairdocs.org/sdr/2021FA0000043.md): Shaft · flaking · Feb 11, 2021 · N512LA · Propeller System
  > DURING RE-INSTALLATION OF POWER SECTION AFTER WIRE STRIKE, WHILE INSTALLING PROPELLER, THE COATING ON THE FRESHLY OVERHAULED PROPELLER SHAFT WAS FLAKING OFF UNDERNEATH THE WASHERS ON THE PROPELLER RETENTION BOLTS. THE TORQUE SETTING WAS INACCURATE. YOU COULD A
- [SDR 2019FA0000175](https://openairdocs.org/sdr/2019FA0000175.md): Adapter · broken · May 29, 2019 · N870LA · Airtrc AT802 · Trailing Flap Position Indicating System
  > WHILE COMPLYING WITH AIR TRACTOR SL 375, A FLAP MOTOR MOUNTING ADAPTER WAS FOUND WITH A BROKEN MOUNTING STUD. IF THE SECOND STUD HAD BROKE THE FLAP MOTOR WOULD FALL DOWN ON THE AILERON PUSH PULL TUBE.
- [SDR CA180709004](https://openairdocs.org/sdr/CA180709004.md): Switch · failed · Jul 6, 2018 · Airtrc AT802A · Agricultural Spray System
  > (CAN) EMERGENCY DUMP LEVER FAILED TO OPERATE E-DUMP SYSTEM. (TC# 20180709004)
- [SDR 3S4A2018051500055](https://openairdocs.org/sdr/3S4A2018051500055.md): Warning System · activated · May 13, 2018 · N829SA · Pilats PC1247E · Engine Oil Pressure
  > RED CAS MESSAGE "HIGH OIL PRESSURE" DURING CLIMB AIRCRAFT DIVERTED TO SJC FROM SQL.
- [SDR 2017FA0000535](https://openairdocs.org/sdr/2017FA0000535.md): Pressure Sensor · inaccurate · Nov 1, 2017 · N896WP · Airtrc AT802 · Engine Oil Pressure
  > ON FINAL APPROACH, PILOT NOTICED OIL PRESSURE DROPPING AND JUST AT TOUCHDOWN, OIL PRESSURE DROPPED TO ZERO AND RED WARNING LIGHT ON GLASS DISPLAY CAME ON. PILOT SHUT ENGINE DOWN AND ROLLED TO STOP ON TAXIWAY. AFTER TROUBLESHOOTING, FAILURE OF THE ENGINE OIL PR
- [SDR Q5QA2017011607](https://openairdocs.org/sdr/Q5QA2017011607.md): Transmitter · faulty · Dec 3, 2016 · N432CV · Pilats PC1245 · Trailing Flap Position Indicating System
  > PILOT REPORTED A FLAPS FAILED INDICATION. INVESTIGATION DISCLOSED THE RT FLAP POSITION TRANSMITTER WAS FAULTY. INSTALLED A NEW TRANSMITTER. SUBSEQUENT FLAP OPERATIONAL CHECKS WERE SATISFACTORY. NO FURTHER ACTION WAS REQUIRED.
- [SDR QMLA2016052216053](https://openairdocs.org/sdr/QMLA2016052216053.md): Bolt · loose · May 22, 2016 · N316PM · Pilats PC1245 · Wheel/Ski/Float
  > AFTER TAXIING INTO THE RAMP, THE PILOT DISCOVERED THAT THE LT MAIN TIRE WAS FLAT, TRIED TO AIR THE TIRE TO MOVE THE PLANE INTO THE HANGAR. IT WOULD NOT HOLD PRESS. THE WHEEL HALF BOLTS HAD LOST ALL TORQUE. THE BOLT HEADS HAD CONTACTED THE BRAKE TORQUE TUBE
- [SDR CA160224008](https://openairdocs.org/sdr/CA160224008.md): Windshield · cracked · Feb 24, 2016 · Airtrc AT802 · Flight Compartment Windows
  > (CAN) UPON INSPECTION A 4" CRACK WAS DISCOVER ON LT SIDE WINDSHIELD.
- [SDR 2016FA0000201](https://openairdocs.org/sdr/2016FA0000201.md): Valve · out of limits · Feb 17, 2016 · Beech B300B350C · Propeller Controlling System
  > (B-00101) DURING CRUISE, RT ENGINE PROPELLER RPM DROP TO 1340, TORQUE INDICATION RISE TO RED LINE. DURING DESCENT, WHEN ADJUSTING THE PROP LEVER, THE ENGINE PROPELLER RPM SOMETIMES NORMAL, SOMETIMES UNABLE TO CONTROL. PRIOR TO LANDING, ENGINE PROPELLER RPM DRO
- [SDR HDNA20160123089](https://openairdocs.org/sdr/HDNA20160123089.md): Governor · fluctuates · Jan 22, 2016 · N705MS · Pilats PC1247E · Propeller Governor
  > ON THE INITIAL LEG, FOR PATIENT PICK UP THE PLANE PERFORMED FLAWLESSLY. ON THE DEPARTURE & CLIMB TO CRUISE WITH PATIENT ONBOARD THE ACFT PERFORMED FLAWLESSLY. DURING CRUISE EN-ROUTE AT FL180 & APPROX 50 MILES NE OF THE AREA THE NP RPM, PROP RPM, BEGAN TO BEH
- [SDR CA151102011](https://openairdocs.org/sdr/CA151102011.md): Tube · cracked · Oct 30, 2015 · Airtrc AT802A · Elevator Structure
  > (CAN) CRACK NOTED ON ELEVATOR DOWN STOP TUBE, BS 268.3125", TOP FWD RT SIDE. CRACK APPROXIMATELY.7500" IN LENGTH.
- [SDR CA150908017](https://openairdocs.org/sdr/CA150908017.md): Proximity Sensor · faulty · Sep 5, 2015 · Airtrc AT802A · Landing Gear Position and Warning
  > (CAN) RT MAIN GEAR DID NOT IND DOWN, A/C DID FLY BY TO CONFIRM GEAR DOWN. CONFIG AND LANDED SAFELY. FAULTY GROUND AT DOWN PROXIMITY SENSOR DETERMINED TO BE AT FAULT.
- [SDR CA150819006](https://openairdocs.org/sdr/CA150819006.md): Float · cracked · Aug 17, 2015 · Airtrc AT802A · Wheel/Ski/Float
  > (CAN) RT FLOAT FOAM TANK FOUND TO BE CRACKED. CRACK WAS FOUND ON LT FWD LOWER CORNER OF THE TANK.
- [SDR CA150819007](https://openairdocs.org/sdr/CA150819007.md): Rivet · broken · Aug 17, 2015 · Airtrc AT802A · Wheel/Ski/Float
  > (CAN) RIGHT FLOAT BAGGAGE LIP, PN 13A01162-052 PARTS MANUAL, REV F, PAGE 24 - 26, ITEM NR 17, HAD 5 BROKEN RIVETS.
- [SDR CA150713016](https://openairdocs.org/sdr/CA150713016.md): Window · blew out · Jul 2, 2015 · Airtrc AT802A · Flight Compartment Windows
  > (CAN) LEFT COCKPIT WINDOW BLOWN OUT.
- [SDR CA150702006](https://openairdocs.org/sdr/CA150702006.md): Clamp · broken · Jun 30, 2015 · Airtrc AT802A · Wheel/Ski/Float
  > (CAN) BAND CLAMP HOLDING PULLEY FOR WATER RUDDER STEERING CABLES FOUND BROKEN RT SIDE. MOUNT ROTATED AND ENGAGED FLAP UP SW CAUSING FLAPS TO NOT OPERATE. CLAMP INSTALLED. FLIGHT CONTROLS/FLAPS CYCLED. NO FURTHER DEFECTS.
- [SDR CA150603004](https://openairdocs.org/sdr/CA150603004.md): Gearbox · making metal · May 20, 2015 · Accessory Gearboxes
  > (CAN) PILOT OBSERVED AGB CHIP DETECTOR ANNUNCIATE ON MFD DISPLAY WITH LOW OIL PRESSURE CAUTION LIGHT ILLUMINATED. SUBSEQUENT LOUD NOISE WAS HEARD WITH PROPELLER GOING INTO FEATHER. PILOT ELECTED TO PUT ENGINE IN FLIGHT IDLE AND LANDED. SUBSEQUENT INSPECTION
- [SDR JWQG2015FA0000124](https://openairdocs.org/sdr/JWQG2015FA0000124.md): Check Valve · obstructed · Apr 7, 2015 · N512LA · Airtrc AT802A · Aircraft Fuel Distribution System
  > WHILE FIXING A LEAK ON THE INTEGRAL FUEL TANK IN THE LT WING, THE OUTLET IN THE TANK FOR THE FUEL VENT CHECK VALVE WAS DISCOVERED TO BE PLUGGED WITH FUEL TANK SEALANT. THIS WAS SEALANT APPLIED AT THE FACTORY AS WE HAVE OWNED THIS AIRCRAFT SINCE NEW. THIS FUEL
- [SDR ESMR20150323001](https://openairdocs.org/sdr/ESMR20150323001.md): Position Sensor · malfunctioned · Mar 18, 2015 · N539PE · Pilats PC1245 · Trailing Flap Position Indicating System
  > TWO CREW & TWO PAXS, CLEARED TO LAND ON RUNWAY 3L, AT APPROX 800 FEET AGL. CALLED FOR FLAPS TO BE MOVED FROM 30 DEGREES TO 40 DEGREES. A FEW SECONDS LATER WE RECEIVED A FLAPS & PUSHER ANNUNCIATOR FOLLOWED BY AN AURAL, FLAP ASYMMETRY, WARNING. AT THAT POINT
- [SDR CA141223007](https://openairdocs.org/sdr/CA141223007.md): Governor · failed · Nov 11, 2014 · Piagio P180 · Propeller Governor
  > (CAN) CREW DETERMINED PROPELLER CONTROLS NOT FUNCTIONING. IAW JLB ENTRY RT PROPELLER LOSS OF RPM. ENGINE SHUTDOWN PERFORMED IAW CHECKLIST. LANDED AIRCRAFT SAFELY. PROPELLER GOVERNOR REPLACED, AIRCRAFT RETURNED TO SERVICE WITHOUT FURTHER INCIDENT.
- [SDR TXHA20140630001](https://openairdocs.org/sdr/TXHA20140630001.md): Transmitter · false indication · Jun 30, 2014 · N729PC · Stbros SD360 · Engine BMEP/Torque Indicating
  > PILOT REPORTED FAULTY TORQUE INDICATION ON RT ENG.
- [SDR CALA2014060291178](https://openairdocs.org/sdr/CALA2014060291178.md): Hydraulic Line · frayed · May 28, 2014 · N213UA · Boeing 777222 · Hydraulic System, Main
  > HYD HOSE ON FWD PART OF RT LG TRUCK OUTER LAYER FRAYED. LINE WRAPPED WITH SELF-FUSING SILICONE TAPE AS A TEMPORARY REPAIR IAW MM 20-10-10 PG 203. REPLACED HOSE ASSEMBLY.
- [SDR CA140303001](https://openairdocs.org/sdr/CA140303001.md): Line · damaged · Feb 21, 2014 · Engine (Turbine/Turboprop)
  > (CAN) AFTER TAKING OFF, THE ACFT SUFFERED ENGINE PROBLEMS. THE PILOT DROPPED THE LOADED WATER AND LANDED IN A MARSH. THE CAUSE FOR THIS ACCIDENT WAS ATTRIBUTED TO DAMAGE ON A FLEXIBLE PY LINE. IAW RECORDS, A LARGE NUMBER OF MFG POWERED AIR TRACTORS INCORP
- [SDR CA130726013](https://openairdocs.org/sdr/CA130726013.md): Gearbox · making metal · Jul 25, 2013 · Airtrc AT802A · Accessory Gearboxes
  > (CAN) CHIP LIGHT ILLUMINATED IN FLIGHT, PILOT RETURNED AND UPON TROUBLESHOOTING IT WAS FOUND THAT AGB CHIP WAS THE PROBLEM. 1 SMALL METAL SILVER AND BLACK MAGNETIC FUZZ FOUND ON CHIP. RGB AND OIL FILTER ALSO CHECKED FOR CONTAMINENTS. NONE FOUND. ACFT RETUR
- [SDR CA130718001](https://openairdocs.org/sdr/CA130718001.md): Shaft · worn · Jul 17, 2013 · Airtrc AT802A · Cabin Cooling System
  > (CAN) AIR CONDITIONING DRIVE PAD ASSY, PULLY FOUND LOOSE WITH RADIAL PLAY ON REAR BEARING SHAFT SUPPORT. BEARING NOT SEIZED AND WEAR RESTRICTED TO SHAFT OUTSIDE DIAMETER ONLY.
- [SDR CA130702009](https://openairdocs.org/sdr/CA130702009.md): Attach Bracket · cracked · Jun 28, 2013 · Airtrc AT802A · Vertical Stabilizer Miscellaneous Structure
  > (CAN) DURING THE POST FLIGHT INSPECTION, IT WAS NOTED THAT THE RT LOWER AUXILAIRY VERTICAL FIN FWD OTBD ATTACH BRACKET WAS CRACKED.
- [SDR CA130702003](https://openairdocs.org/sdr/CA130702003.md): Gearbox · making metal · Jun 24, 2013 · Airtrc AT802 · Accessory Gearboxes
  > (CAN) ENGINE CHIP LIGHT AFTER TAKEOFF. LOAD ABORTED RETURNED TO DEPARTURE. ACFT REQUIRED ENGINE CHANGE. AGB CHIP.
- [SDR CA130530007](https://openairdocs.org/sdr/CA130530007.md): Actuator · damaged · May 28, 2013 · Airtrc AT802A · Trailing Edge Flap Actuator
  > (CAN) FLAPS MADE EXCESSIVE NOISE WHEN LOWERING FOUND ACTUATOR END CAP WORN AND BALL BEARINGS ENTERING GEARS.
- [SDR CA130522009](https://openairdocs.org/sdr/CA130522009.md): Warning Light · false activation · May 13, 2013 · Airtrc AT802A · Central Warning
  > (CAN) FUEL FILTER LIGHT CAME ON IN FLIGHT.
- [SDR CA130214001](https://openairdocs.org/sdr/CA130214001.md): Bearing · separated · Feb 13, 2013 · Airtrc AT802 · Rudder Structure
  > (CAN) RUDDER ASSEMBLY IS ATTACHED TO VERTICAL FIN BY 3 POINTS TOP, MIDDLE AND BOTTOM. UPON INSPECTION, IT WAS DISCOVERED THAT THE MIDDLE BEARING HAD PARTED FROM THE RUDDER AND THAT THE BOTTOM BEARING SHOWED SIGNS OF WEAR.
- [SDR CA130206009](https://openairdocs.org/sdr/CA130206009.md): Probe · cracked · Feb 6, 2013 · Airtrc AT802A · Fuselage Structure (General)
  > (CAN) WELDS AT FRONT END OF SCOOPS AT DEFLECTORS CRACKING,BREAKING, 2 FINDINGS.
- [SDR CA130214006](https://openairdocs.org/sdr/CA130214006.md): Muffler · cracked · Feb 5, 2013 · Airtrc AT802A · Engine Noise Suppressor
  > (CAN) PILOTS COMPLAIN OF LACK OF HEAT. BLEED AIR SYS INSPECTED AND FOUND THIS UNIT CRACKED. ALONG WITH WORN SCEET TUBING.7500". NEW MUFFLER INSTALLED WITH NEW SCEET ATTACHING TUBING. SYSTEM CHECKED SERVICABLE. FLEET INSPECTION COMPLETED AND FOUND 2 OTHER
- [SDR CA130214010](https://openairdocs.org/sdr/CA130214010.md): Valve · failed · Jan 22, 2013 · Airtrc AT802A · Engine Fuel Distribution
  > (CAN) SEVERAL MINUTES AFTER START, FUEL WOULD EMIT FROM EPA CAN OVERFLOW LINE. SYSTEM CHECKED AND FOUND THAT PURGE VALVE WAS LEAKED INTO DUMP SYS AFTER ENGINE START. NEW VALVE INSTALLED AND SYSTEM CHECKED SERVICEABLE.
- [SDR CA130123007](https://openairdocs.org/sdr/CA130123007.md): Washer · loose · Jan 16, 2013 · Airtrc AT802A · Wheel/Ski/Float
  > (CAN) AFT FLOAT ATTACH PLYON, AFT PYLON TO FLOAT ATTACH BOLT HAS BEEN FOUND LOOSE ON SEVERAL ACFT. WASHERS UNDER NUT AND BOLT HEAD SHOW WEAR THRU 1/3 THICKNESS OF WASHER. BOLT AND NUT ARE RUSTY AND WORKING IS EVIDENT ON ATTACH FITTING. FLEET CAMPAIGN TO ADDR
- [SDR CA121213005](https://openairdocs.org/sdr/CA121213005.md): Pitot Head · leaking · Dec 13, 2012 · Airtrc AT802A · Pitot/Static System
  > (CAN) RECERTIFICATION OF PITOT AND STATIC SYS, AN ABNORMAL LEAK WAS FOUND, ON CLOSE INSPECTION THE ALUMINUM LINE BETWEEN PITOT TUBE AND DRAIN COCK FOR THE PITOT SYSTEM WAS FOUND TO HAVE A PIN HOLE DUE TO BUILD UP OF FIRE RETARDANT THAT CAUSED CORROSION TO SET
- [SDR CA121130012](https://openairdocs.org/sdr/CA121130012.md): Pedal · damaged · Nov 30, 2012 · Airtrc AT802 · Rudder Control System
  > (CAN) RUDDER PEDALS HIT STRUCTURE WHEN ADJUSTED TO FULL AFT POSITION WELL BEFORE FULL TRAVEL LIMITS REACHED. THIS SEEMS TO BE A DESIGN FLAW IN THE RUDDER PEDAL, NOT EASILY FIXED WITHOUT RE-ENGINEERING.
- [SDR CA121213007](https://openairdocs.org/sdr/CA121213007.md): Fuel Cell · contaminated · Nov 19, 2012 · Airtrc AT802A · Fuel Storage
  > (CAN) EXCESSIVE AMOUNTS OF WATER FOUND IN LT FUEL CELL. PILOT REPORTED TO MAINTENANCE FUEL CAP WAS LEFT OFF AFTER REFUELING WHEN HEAVY RAINS WERE REPORTED. FUEL CELL AND SYSTEM FLUSHED/CLEANED AND ACFT RETURNED TO SERVICE.
- [SDR CA121213008](https://openairdocs.org/sdr/CA121213008.md): Coupling · twisted · Nov 19, 2012 · Airtrc AT802 · Trailing Edge Flap Actuator
  > (CAN) RUBBER FLAP ACTUATOR COUPLING FOUND EXCESSIVELY TWISTED DURING FLAP ACTUATOR INSPECTION. RUBBER COUPLING REPLACED AND ACFT RETURNED TO SERVICE.
- [SDR CA121023005](https://openairdocs.org/sdr/CA121023005.md): Longeron · cracked · Sep 21, 2012 · Airtrc AT802A · Fuselage Main, Longeron/Stringer
  > (CAN) LONGITUDINAL CRACK FOUND ON UPPER RT AFT TAIL TOP TUBE LONGERON, PN 11029-8.
- [SDR CA120917025](https://openairdocs.org/sdr/CA120917025.md): Float · cracked · Sep 17, 2012 · Airtrc AT802A · Wheel/Ski/Float
  > (CAN) CRACKS FOUND ON LT AND RT FLOAT NOSE GEAR ACTUATOR ATTACH BULKHEAD EMINATING FROM ACTUATOR ATTACH BOLT HOLES.
- [SDR CA120917026](https://openairdocs.org/sdr/CA120917026.md): Float · cracked · Sep 17, 2012 · Airtrc AT802A · Wheel/Ski/Float
  > (CAN) CRACKS FOUND ON LT AND RT FLOAT HOSE GEAR ACTUATOR ATTACH BULKHEAD EMINATING FROM ACTUATOR ATTACH BOLT HOLES.
- [SDR CA120917021](https://openairdocs.org/sdr/CA120917021.md): Float · damaged · Sep 16, 2012 · Airtrc AT802A · Wheel/Ski/Float
  > (CAN) RT NOSE GEAR COLLAPSED ON LANDING ROLL OUT. NOSE GEAR ACTUATOR MOUNTING FLANGE FROM FLOAT NOSE BOX END CAP. THE END CAP THAT THE NOSE GEAR ACTUATOR HARD MOUNTS TO EXPERIENCED STRUCTURAL FAILURE.
- [SDR CA120924004](https://openairdocs.org/sdr/CA120924004.md): Engine · failed · Sep 15, 2012 · Airtrc AT802A · Engine (Turbine/Turboprop)
  > (CAN) THE ENGINE EXPERIENCED A FAILURE DURING TAKEOFF. INVESTIGATION FOUND THAT 3 OF THE P/T BLADES ON THE 2ND STAGE DISK WERE BROKEN IN THE FIR TREE AREA AND THE REST BROKEN OFF ABOVE THE PLATFORM AREA. THE DAMAGE WAS CONFINED TO THE POWER SECTION AND IS UN
- [SDR CA120917004](https://openairdocs.org/sdr/CA120917004.md): Engine · power loss · Sep 3, 2012 · Airtrc AT802A · Engine (Turbine/Turboprop)
  > (CAN) THE PILOT HAD TO ABORT A TAKEOFF DUE TO ENGINE NOT MAKING TORQUE. ENGINE PARAMETERS SHOWED NG 91 PERCENT, TORQUE 2500 FT-LB, FUEL FLOW: 96 GALS/HOUR. THE P3 AND PY AND FUEL FILTER WERE CHECKED, TROUBLESHOOTING IS POINTING TOWARDS A FAULTY FUEL CONTROL.
- [SDR CA120816003](https://openairdocs.org/sdr/CA120816003.md): Adapter · broken · Aug 13, 2012 · Airtrc AT802 · Trailing Edge Flap Actuator
  > (CAN) FLAP MOTOR ACTUATOR ADAPTER PLATE STUD FOUND TO HAVE BROKEN OFF.
- [SDR CA120724004](https://openairdocs.org/sdr/CA120724004.md): Exciter · failed · Jul 23, 2012 · Airtrc AT802A · Exciter
  > (CAN) WHEN IGNITION SELECTED ON DURING START OR IN CONTINUOUS MODE, THE 5 AMP START CONTROL C/B WOULD TRIP. IT WAS DETERMINED THAT THE IGNITION EXCITER BOX IS UNSERVICEABLE. IGNITOR EXCITER BOX REPLACED FUNTION CHECKED SERVICEABLE.
- [SDR CA120723008](https://openairdocs.org/sdr/CA120723008.md): Engine · malfunctioned · Jul 16, 2012 · Airtrc AT802 · Engine (Turbine/Turboprop)
  > (CAN) WHILE THE ACFT WAS ON CRUISE FLIGHT AT 1000 FT. WITHOUT ANY WARNING OR ABNORMAL BEHAVIOUR THE ENGINE SHUTDOWN. A RE-START WAS ATTEMPTED WITHOUT SUCCESS AND THE PILOT PERFORMED A DEAD STICK LANDING ON A FLAT FIELD. PILOT UNINJURED BUT THE ACFT SUSTAI
- [SDR CA120718008](https://openairdocs.org/sdr/CA120718008.md): Pressure Switch · faulted · Jul 14, 2012 · Airtrc AT802A · Aircraft Fuel Distribution System
  > (CAN) FUEL FILTER LIGHT ILLUMINATED, FUEL FILTER REMOVED, CLEANED, INSPECTED AND REPLACED. NO MAJOR CONTAMINATION FOUND. FAULTY SWITCH FOUND TO BE SOURCE OF ILLUMINATION, SWITCH REPLACED.
- [SDR CA120723004](https://openairdocs.org/sdr/CA120723004.md): Indication Sys · malfunctioned · Jul 11, 2012 · Airtrc AT802A · Engine BMEP/Torque Indicating
  > (CAN) PILOT IS REPORTING TORQUE IS DROPPING FROM 3600 TO 3200 WHILE MAKING TURNS WHEN SPRAYING WITH THE ACFT. TORQUE IS HAVING TO BE MONITORED AND INCREASED TO CARRY THE ACFT THROUGH A TURN. WORK PERFORMED ON ACFT TO DATE: CLOSING CHECK, FCU REPLACED, TRIM ST

Next page: https://openairdocs.org/engine/pratt-whitney-canada-pt6a-67ag/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 = 'PT6A67AG'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/pratt-whitney-canada-pt6a-67ag/reports

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