# Service difficulty reports: Pratt & Whitney Canada PT6A-66

A list on [Pratt & Whitney Canada PT6A-66](https://openairdocs.org/engine/pratt-whitney-canada-pt6a-66.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 177 reports

- [SDR CA190428001](https://openairdocs.org/sdr/CA190428001.md): Seal · leaking · Apr 14, 2019 · Piagio P180 · Turbine Engine Compressor Section
  > (CAN) OIL ODOR NOTED IN CABIN DURING CLIMB, VISIBLE SMOKE/HAZE NOTED IN CABIN AT TOP OF CLIMB, ENGINE POWER REDUCED AND SMOKE/HAZE CLEARED AND OIL ODOR REDUCED. AIRCRAFT RETURNED TO BASE WITH NO FURTHER INCIDENT. POST FLIGHT INVESTIGATION REVEALED OIL CONTAMI
- [SDR 2016FA0000657](https://openairdocs.org/sdr/2016FA0000657.md): Fuel Control · malfunctioned · Dec 14, 2016 · N850VT · Socata TBM700 · Fuel Control/Turbine Engines
  > ENGINE SLOW TO START, HANGING AT 33 PERCENT 50+ SECONDS TO START. CHANGED ACFT BATTERY SAME RESULTS. CALIBRATED FCU STARTS AT 38 SECONDS.
- [SDR CA160301004](https://openairdocs.org/sdr/CA160301004.md): Heater · malfunctioned · Feb 17, 2016 · Piagio P180 · Fuel Heater
  > (CAN) AFTER LANDING, EXTERNAL FUEL LEAK WAS NOTICED. (THIS IS THE 3RD EVENT). THE FUEL WAS INSIDE THE RIGHT HAND ENGINE NACELLE, ON WING, FUSELAGE AND EVEN INSIDE THE LANDING GEAR VANE. PIAGGIO DID A GROUND RUN, AND REPORTED, ABOVE IDLE POWER, A FUEL SPRAY FRO
- [SDR CA160113002](https://openairdocs.org/sdr/CA160113002.md): Actuator · loose · Jan 11, 2016 · Piagio P180 · Rudder Tab Control System
  > (CAN) DURING INSPECTION, NOTICED ROD END JAM NUTS NOT SECURE ON RUDDER TRIM ACTUATOR.
- [SDR CA160119021](https://openairdocs.org/sdr/CA160119021.md): Engine · malfunctioned · Dec 30, 2015 · Piagio P180 · Engine (Turbine/Turboprop)
  > (CAN) THE OPERATOR REPORTED THAT 4 TIMES OUT OF 5, THE ENGINE WILL NOT GO IN REVERSE. CYCLING THE CONTROLS HAD NO EFFECT. TROUBLESHOOTING IS ON-GOING WITH RIGGING TESTING AND PROPELLER GOVERNOR SWAP.
- [SDR CA151125004](https://openairdocs.org/sdr/CA151125004.md): Hose · collapsed · Nov 23, 2015 · Piagio P180 · Engine Cooling System
  > (CAN) FOUND DURING A SCHEDULED INSPECTION RIGHT BLEED AIR PRE-COOLER OVERHEATED AND RT ENGINE BLEED AIR SUPPLY HOSE INTERIOR WALL COLLAPSED.
- [SDR CA151125005](https://openairdocs.org/sdr/CA151125005.md): Anti-Ice Valve · malfunctioned · Nov 20, 2015 · Piagio P180 · Airfoil Anti/De-ice System
  > (CAN) LEFT WING ANTI-ICE VALVE FAILED TO CLOSE WHEN SELECTED "OFF". INVESTIGATION FOUND "BUTTEFLY" TURNING ON SHAFT DUE TO STRIPPED SPLINES.
- [SDR 2016FA0000613](https://openairdocs.org/sdr/2016FA0000613.md): Fuel Control · malfunctioned · Jul 1, 2015 · N418A · Socata TBM700 · Fuel Control/Turbine Engines
  > ENGINE IS SLOW TO START AND DOES NOT MAKE MAX REVERSE CHECK. RECALIBRATED THE FCU.
- [SDR 2016FA0000612](https://openairdocs.org/sdr/2016FA0000612.md): Fuel Control · malfunctioned · May 28, 2015 · N900TK · Socata TBM700 · Fuel Control/Turbine Engines
  > ENGINE IS SLOW TO START. RECALIBRATED THE FCU.
- [SDR CA150414004](https://openairdocs.org/sdr/CA150414004.md): Hinge Pin · sheared · Apr 13, 2015 · Piagio P180 · Air Intake Anti/De-Ice System
  > (CAN) ENGINE ANTI-ICE DIVERTER DOOR HINGE PINS SHEARED. DOOR WAS FOUND LOOSE IN COWL. TECH SUPPORT HAS SEEN THIS IN THE PAST. DAMAGE POSSIBLY CAUSED BY ICE BUILD-UP.
- [SDR CA150323001](https://openairdocs.org/sdr/CA150323001.md): O-Ring · missing · Mar 19, 2015 · Turbine Engine Oil System
  > (CAN) 3 EVENTS WERE REPORTED BY MFG, FAULTY INDICATION ON THE FILLER CAP AND OIL LEVEL INDICATOR, PN 3075906-01. FOLLOWING AN INVESTIGATION AT THE SUPPLIER, THEY CONFIRMED THE ISSUE WAS CAUSED BY THE ABSENCE OF THE O-RING WHICH ALLOWS MOISTURE TO INFILTRATE T
- [SDR CA150325012](https://openairdocs.org/sdr/CA150325012.md): Engine · flamed out · Mar 11, 2015 · Piagio P180 · Engine (Turbine/Turboprop)
  > (CAN) FOLLOWING THROTTLE REDUCTION TO IDLE DURING DESCENT THE ENGINE FLAMED OUT. THE PILOT WAS ABLE TO RESTART THE ENGINE WHICH FLAMED OUT AGAIN TWICE WHILE BRINGING THROTTLE TO IDLE. ALL EVENTS OCCURRED IN EEC MODE.
- [SDR TWYA201502183241](https://openairdocs.org/sdr/TWYA201502183241.md): Screw · failed · Feb 11, 2015 · N590TW · Pilats PC1245 · Propeller Assembly
  > PITCH TRIM BRACKET SCREWS FAILED INTERNAL.
- [SDR GQRR2014FA0000673](https://openairdocs.org/sdr/GQRR2014FA0000673.md): Exhaust Stack · cracked · Nov 26, 2014 · N562NA · Pilats PC1245 · Engine Collector/Tailpipe/Nozzle
  > ENGINE DEICE HOT AIR OUTLET CRACKED.
- [SDR 2014FA0000536](https://openairdocs.org/sdr/2014FA0000536.md): Cabin Pressure · malfunctioned · Aug 11, 2014 · N331GL · Socata TBM700 · Cabin Pressure Control System
  > DURING CRUISE, WHILE AT FL310, CABIN PRESSURE BEGAN TO RISE AS CONFIRMED BY THE G1000 ELECTRONIC GAUGES FOR CABIN ALT, ROC AND DIFF PRESSURE. AT 10,300' CABIN ALTITUDE THE CABIN ALTITUDE CAS MESSAGE APPEARED. WHEN THE CABIN ALTITUDE REACHED APPROXIMATELY 10,5
- [SDR CA140721003](https://openairdocs.org/sdr/CA140721003.md): Engine · vibration · Jun 25, 2014 · Socata TBM700 · Engine (Turbine/Turboprop)
  > (CAN) AFTER TAKEOFF, THE PILOT NOTICED A VIBRATION HAD COME BACK AFTER THE ENGINE WAS REINSTALLED. THE PILOT MENTIONED THAT THIS VIBRATION HAD NOT BEEN FELT WHEN THE RENTAL ENGINE WAS INSTALLED.
- [SDR QMLA2014050114047](https://openairdocs.org/sdr/QMLA2014050114047.md): Unknown · malfunctioned · May 1, 2014 · N317NA · Pilats PC1245 · Propeller Controlling System
  > AFTER TOUCHING DOWN, REVERSE WAS SELECTED. THE PROPELLER INITIALLY WENT INTO REVERSE NORMALLY, AFTER A FEW SECONDS THE PROPELLER THEN WENT TO FLAT PITCH, RESULTING IN LOSS OF REVERSE EFFECTIVENESS.
- [SDR CA140130008](https://openairdocs.org/sdr/CA140130008.md): Valve · frozen · Jan 29, 2014 · Piagio P180 · Passenger/Crew Doors
  > (CAN) AFTER LIFTOFF, CABIN DOOR LIGHT ILLUMINATED. CREW MAINTAINED FL 10 AND COMPLETED TRIP WITHOUT INCIDENT. 3 WAY VALVES FROZEN, AIC SAT ON RAMP APPROXIMATELY 6 HOURS -30C - TIS OF AIC C/O NFF SYSTEM DRAINED IAW AMM, AIC DEPARTED NEXT MORNING. NO ISSUES WI
- [SDR 2013FA0000763](https://openairdocs.org/sdr/2013FA0000763.md): Actuator · inoperative · Dec 10, 2013 · N871AT · Piagio P180 · Stabilizer Control System
  > AFTER ROTATION, THE PRIMARY PITCH TRIM WAS NOT WORKING. TRIM CLACKER WAS CLACKING BUT, THERE WAS NO MOVEMENT OF THE STABILIZER. SWITCHED TO SECONDARY HORIZONTAL PITCH TRIM WHICH WAS OPERATIONAL. MADE AN UNEVENTFUL LANDING. TROUBLESHOOTING REVEALED THE MOT
- [SDR UALA2013061904269](https://openairdocs.org/sdr/UALA2013061904269.md): Coupling · broken · Jun 18, 2013 · N213UA · Boeing 777222 · Air Distribution System
  > BLEED LOSS WING LT EICAS CAME ON IN DESCENT. FOUND COUPLING BROKEN ON LT LOWER FLOW CONTROL VALVE. REPLACED BROKEN COUPLING, OPS CHECKED GOOD.
- [SDR PCPR2013061301](https://openairdocs.org/sdr/PCPR2013061301.md): Pump · leaking · Jun 13, 2013 · N25EP · Pilats PC1245 · Engine Fuel Pump
  > DURING UNSCHEDULED MX, FOUND ENGINE DRIVEN FUEL PUMP LEAKING AT RELIEF VALVE GASKET. ENGINE COMPARTMENT COVERED WITH FUEL RESIDUE.
- [SDR UALA2013060703959](https://openairdocs.org/sdr/UALA2013060703959.md): Sdu · failed · Jun 6, 2013 · N213UA · Boeing 777222 · Communications System
  > DURING TAXI OUT, RECEIVED A SATCOM EICAS MESSAGE. REPLACED SDU, FOUND CIRCUIT BREAKERS OPEN FOR SATCOM, CLOSED BREAKERS, TESTED OKAY PER MM.
- [SDR V2JA0602134154986](https://openairdocs.org/sdr/V2JA0602134154986.md): Display · failed · Jun 2, 2013 · N156SL · Piagio P180 · Flight Environment Data
  > IN FLIGHT, CAPTAINS PFD WENT BLANK, WITHIN A FEW SECONDS A STRONG BURNING ODOR FILLED THE COCKPIT.
- [SDR V2JA052313DEF130](https://openairdocs.org/sdr/V2JA052313DEF130.md): Seal · damaged · May 23, 2013 · N165SL · Piagio P180 · Passenger/Crew Doors
  > MASTER CAUTION (DOOR SEAL) AT 34,000. RAN CHECKLIST WITH F/O FOR DESCENT TO 30,000 FT. AT 30,000 FT AIRCRAFT WAS STABLE. AFTER ABOUT 5 TO 10 MINUTES A LOUD DOOR SEAL NOISE WAS NOTED AND CABIN BEGAN TO CLIMB RAPIDLY. AN EMERGENCY DESCENT WAS PERFORMED AS A
- [SDR V2JA0523134153420](https://openairdocs.org/sdr/V2JA0523134153420.md): Fitting · leaking · May 23, 2013 · N143SL · Piagio P180 · Hydraulic Pump (Electric/Engine), Main
  > HYDRAULIC PUMP FAILED ON APPROACH. FOLLOWED CHECKLIST HAND-PUMPED GEAR DOWN. "HYD PRESS" CAUTION LIGHT ILLUMINATED, ASSOCIATED PRESSURE BETWEEN 0-200 PSI, DIVERTED.
- [SDR CA130527011](https://openairdocs.org/sdr/CA130527011.md): Spring · weak · May 16, 2013 · Piagio P180 · Propeller Controlling System
  > (CAN) PROPELLER RPM DECAYED TO UNCOMMANDED FEATHER AT 1000` AGL AFTER TAKE OFF. PROPELLER FAILURE OCCURRED AFTER THE POST TAKE OFF POWER REDUCTION. UNABLE TO RECOVER PROPELLER TO NORMAL RPM. PRIOR TO THE FAILURE, THE PROPELLER GOVERNOR HAD BEEN REINSTALLED AF
- [SDR CA130603006](https://openairdocs.org/sdr/CA130603006.md): Control System · malfunctioned · May 16, 2013 · Piagio P180 · Propeller Controlling System
  > (CAN) THE LEFT PROPELLER RPM DECAYED UNCOMMANDED TO FEATHER AT 1000` AGL. THE FAILURE OCCURRED AS THE POST TAKE OFF POWER REDUCTION WAS PERFORMED. THE CREW WAS UNABLE TO RECOVER THE PROPELLER TO NORMAL RPM AND, THEREFORE, THE PILOT SHUT DOWN AND SECURED THE LH
- [SDR UALA2013051303312](https://openairdocs.org/sdr/UALA2013051303312.md): Converter · failed · May 12, 2013 · N213UA · Boeing 777222 · AC Generation System
  > ELEC BACKUP SYS A FAILURE IN THE BACKUP ELECTRICAL SYS HAS OCCURRED THAT CANNOT BE ATTRIBUTED TO A BACKUP GENERATOR. FOUND BACK UP CONVERTER FAULTY IAW FIM 24-25-TASK 802. 28V DC PCN PRESENT AT PIN 1 OF CONNECTOR 24008, REF WDM 24-25-31. REQUIRED 566-9012 N
- [SDR V2JA0504134151771](https://openairdocs.org/sdr/V2JA0504134151771.md): Autofeather Sys · malfunctioned · May 4, 2013 · N132SL · Piagio P180 · Propeller Feathering/Reversing
  > CREW REPORTS UNCOMMANDED AUTOFEATHER ON LEFT ENGINE.
- [SDR V2JA0504134142480](https://openairdocs.org/sdr/V2JA0504134142480.md): Adc · failed · May 4, 2013 · N165SL · Piagio P180 · Air Data Computer
  > BOTH ADC FAILED IN FLIGHT. ADC 1 FAILED FIRST, REVERTED TO ADC 2 WHICH FAILED 15 MINUTES LATER.
- [SDR V2JA2013043049004](https://openairdocs.org/sdr/V2JA2013043049004.md): Door · out of adjust · Apr 30, 2013 · N109SL · Piagio P180 · Cargo/Baggage Doors
  > CARGO DOOR LIGHT ON IN FLIGHT. ADJUSTED BAGGAGE DOOR IAW AMM 52-30-00. OPS CHECKED GOOD.
- [SDR 2013FA0000256](https://openairdocs.org/sdr/2013FA0000256.md): Wire Harness · misinstalled · Apr 26, 2013 · N79CN · Piagio P180 · Fuel System Wiring
  > RT FUEL QTY NOT DECREASING DURING RUN-UP. GROUND RUN-UP FINDING DATED 25-04, 2013. FOUND LT AND RT FUEL QUANTITY INDICATION SYSTEM CROSSED WITH EACH OTHER UNDERNEATH CENTER PEDESTAL FLOOR AT FS 500. WIRING BUNDLES REROUTED WITH THEIR RELATIVE INDICATORS TO T
- [SDR V2JA2013050447914](https://openairdocs.org/sdr/V2JA2013050447914.md): Landing Gear · failed · Apr 24, 2013 · N139SL · Piagio P180 · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF, WHEN GEAR SELECTED UP, HYD IN HIGH DUTY, 3 GREEN AND NO RED IN-TRANSIT. AFTER CYCLING THE LANDING GEAR HANDLE, LANDING GEAR RETRACTED NORMALLY. AFTER NOSE GEAR WAS LOWERED TO THE GROUND, FOLLOWING LANDING TOUCHDOWN, ACFT VEERED TO THE RT WITH
- [SDR V2JA2013033083417](https://openairdocs.org/sdr/V2JA2013033083417.md): Switch · out of adjust · Mar 30, 2013 · N132SL · Piagio P180 · Door Warning System
  > PILOT DISCREPANCY: BAG DOOR LIGHT IN FLIGHT. ADJUSTED AND OPS CHECKED BAGGAGE DOOR SWITCHES IAW P-180 LL MM 52-70-00, NO DEFECTS NOTED.
- [SDR V2JA20121218006](https://openairdocs.org/sdr/V2JA20121218006.md): Warning Light · illuminated · Mar 3, 2013 · N138SL · Piagio P180 · Door Warning System
  > CARGO DOOR LIGHT ILLUMINATED AFTER TAKEOFF, PERFORMED LT ENGINE SECURING CHECKLIST, LIGHT EXTINGUISHED AFTER THE ENGINE WAS SECURED, THEN ILLUMINATED AGAIN AND STAYED ON UNTILL SHORT FINAL, THEN EXTINGUISHED.
- [SDR V2JA201212180005](https://openairdocs.org/sdr/V2JA201212180005.md): Engine · failed · Feb 22, 2013 · N161SL · Piagio P180 · Engine (Turbine/Turboprop)
  > CLIMBING OUT OF FL260 TO FL310, RT TORQUE DROPPED 20 PERCENT AND IMMEDIATELY ROSE BACK TO 97 PERCENT. A SLIGHT HIGH FREQUENCY VIBRATION WAS THEN NOTICED BY CREW. CLIMB WAS CONTINUED TO FL310. AT FL310 OIL PRESSURE DROPPED BELOW 90PSI ON THE RT ENGINE WITH AU
- [SDR V2JA20121218004](https://openairdocs.org/sdr/V2JA20121218004.md): Autofeather Sys · activated · Feb 20, 2013 · N143SL · Piagio P180 · Propeller Feathering/Reversing
  > UNCOMMANDED AUTO FEATHER ON FINAL.
- [SDR V2JA0208134143337](https://openairdocs.org/sdr/V2JA0208134143337.md): Switch · dirty · Feb 8, 2013 · N143SL · Piagio P180 · Propeller Feathering/Reversing
  > UNCOMMANDED AUTOFEATHER IN FLIGHT ON LAST LEG. POWER LEVERS, AND ALL ENGINE PARAMETERS WERE EQUAL. FOUND SWITCH DIRTY.
- [SDR V2JA20121218003](https://openairdocs.org/sdr/V2JA20121218003.md): Propeller · faulty · Feb 7, 2013 · N143SL · Piagio P180 · Propeller Feathering/Reversing
  > UNCOMMANDED AUTO-FEATHER OF RT ENGINE ON FINAL.
- [SDR CA130212008](https://openairdocs.org/sdr/CA130212008.md): Oil System · low pressure · Jan 29, 2013 · Piagio P180 · Engine Oil Indicating System
  > (CAN) AFTER AN AIRCRAFT MAINTENANCE, DURING FLIGHT TESTING, 1 PROCEDURE CALLS FOR AN IN-FLIGHT SHUTDOWN AND RELIGHT. DURING THE RELIGHT ATTEMPT THE ENGINE NR 2 OIL PRESSURE WAS INDICATING 12 PSI. THE PILOT SHUTDOWN THE ENGINE AND LANDED SAFELY AT THE AIRPORT
- [SDR V2JA20121218002](https://openairdocs.org/sdr/V2JA20121218002.md): Warning Light · illuminated · Jan 28, 2013 · N138SL · Piagio P180 · Door Warning System
  > BAGGAGE DOOR LIGHT CAME ON IN FLIGHT. SECURED LEFT ENGINE.
- [SDR V2JA20121218001](https://openairdocs.org/sdr/V2JA20121218001.md): Connector · dirty · Dec 18, 2012 · N179SL · Piagio P180 · Fire Protection System Wiring
  > RT ENGINE FIRE LIGHT ON SHORT FINAL. AFTER LANDING, SHUTDOWN ENGINE AND DISCHARGED FIRE BOTTLE. CONNECTOR ON FIRE LOOP DIRTY.
- [SDR GQRR201306292920](https://openairdocs.org/sdr/GQRR201306292920.md): Manifold · failed · Oct 31, 2012 · N401WS · Piagio P180 · Landing Gear Steering System
  > ON LANDING ROLL OUT THE ACFT SUFFERED AN UNCOMMANDED STEERING INPUT, THE ACFT EXITED THE RUNWAY AND WAS HEAVILY DAMAGED. SUBSEQUENT TESTING POINTS TO A FAILURE OF THE RECENTLY O/H STEERING MANIFOLD.
- [SDR V2JA113110142012](https://openairdocs.org/sdr/V2JA113110142012.md): Fire Detector · false indication · Oct 14, 2012 · N163SL · Piagio P180 · Fire Detection
  > AIRCRAFT EXPERIENCED THE ILLUMINATION OF THE RT ENGINE FIRE LIGHT WHILE IN DESCENT. CREW DECLARED AN EMERGENCY, PERFORMED QRH, AND DIVERTED. THE ENGINE WAS SHUTDOWN AND THE LIGHT REMAINED ON. IAW THE QRH THE ENGINE FIRE EXTINGUISHER WAS DISCHARGED, THE LIG
- [SDR V2JA078L120792612](https://openairdocs.org/sdr/V2JA078L120792612.md): Transducer · malfunctioned · Sep 26, 2012 · N195SL · Piagio P180 · Engine Oil Indicating System
  > AFTER TAKEOFF, AT APPROX 600FT, THE RT ENG OIL PRESSURE INDICATION DROPPED TO 20 PSI FOR APPROX 8-9 SECONDS, THE OIL PRESSURE WARNING ANNUNCIATOR DID NOT ILLUMINATE. THE CREW SHUTDOWN NR 2 ENG AND RETURNED TO FIELD. EMERGENCY WAS NOT DECLARED. REMOVED & INS
- [SDR V2JA078L107392412](https://openairdocs.org/sdr/V2JA078L107392412.md): Rod · out of rig · Sep 24, 2012 · N107SL · Piagio P180 · Landing Gear Door Retract Section
  > AFTER TAKE OFF WITH GEAR RETRACTED HAD RT GEAR UNSAFE LIGHT COME ON AT 190 -200 KNOTS, SLOWED DOWN AND LIGHT STAYED ON, DIVERTED ACFT TO WITHOUT INCIDENT. FOUND RT MLG DOOR WITH BROKEN UPLOCK ROLLER ASSY, JAMMED UP INSIDE UPLOCK SPRING DAMPNER. REMOVED DOOR
- [SDR V2JA078L105492112](https://openairdocs.org/sdr/V2JA078L105492112.md): Fcu · unserviceable · Sep 21, 2012 · N153SL · Piagio P180 · Fuel Control/Turbine Engines
  > IN FLIGHT AND ON SHORT FINAL, THE AUTOFEATHER SYSTEM WAS ATTEMPTING AN UNCOMMANDED FEATHER. PERFORMED ENGINE GROUND RUNS AND NOTED RT ENGINE LAGS IN THE AUTOFEATHER RANGE. R & R RT ENGINE FCU IAW EMM CH: 73-20-00. PERFORMED STATIC RIGGING, OPS, LEAKS AND FI
- [SDR V2JA078L114691812](https://openairdocs.org/sdr/V2JA078L114691812.md): Motor · failed · Sep 18, 2012 · N173SL · Piagio P180 · Hydraulic Pump (Electric/Engine), Main
  > NOTICED 2 GEAR UNSAFE LIGHTS (NOSE AND RT) AND THE HYD PRESS LIGHT ILLUMINATED, HAND PUMPED GEAR DOWN. LANDED WITHOUT HYD PRESSURE. R & R HYD PUMP ELECTRIC MOTOR. PERFORMED OPS CHECK, OPS CHECKED GOOD AT THIS TIME ON GROUND IAW AMM 29-00-00 & 29-10-00.
- [SDR V2JA201209191512](https://openairdocs.org/sdr/V2JA201209191512.md): Switch · out of adjust · Sep 15, 2012 · N180HM · Piagio P180 · Door Warning System
  > BAGGAGE DOOR ILLUMINATED AFTER ROTATION. ADJUSTED BAGGAGE DOOR AFT SWITCH IAW AMM CH: 52-72-00. OPS CHECK GOOD IAW AMM CH: 52-70-00.
- [SDR V2JA201209100003](https://openairdocs.org/sdr/V2JA201209100003.md): Switch · out of adjust · Sep 9, 2012 · N145SL · Piagio P180 · Door Warning System
  > CREW REPORTED A BAGGAGE DOOR WARNING ANNUNCIATION AFTER TAKEOFF, SHUTDOWN THE NR 1 ENGINE AND DIVERTED SAFELY. ADJUSTED FORWARD BAGGAGE DOOR SWITCH IAW AMM 52-70-00. OP`S CHECKED NORMAL. NO DEFECTS NOTED.

Next page: https://openairdocs.org/engine/pratt-whitney-canada-pt6a-66/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 = 'PT6A66'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/pratt-whitney-canada-pt6a-66/reports

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