# Service difficulty reports: Pratt & Whitney Canada PW617F-E

A list on [Pratt & Whitney Canada PW617F-E](https://openairdocs.org/engine/pratt-whitney-canada-pw617f-e.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 63 reports

- [SDR 4NSA202607160001](https://openairdocs.org/sdr/4NSA202607160001.md): Unknown · odor · Jul 15, 2026 · N374N · Emb EMB500 · Air Distribution System
  > TOOK OFF FROM W22 ON A FERRY FLIGHT TO BNA WHEN SMOKE BEGAN TO APPEAR IN THE COCKPIT ACCOMPANIED BY AN ODOR OF SOMETHING BURNING (SMELLED ELECTRICAL INITIALLY). DIVERTED TO KCKB AND STATED TO ATC THAT A PRECAUTIONARY LANDING WAS NECESSARY DUE TO SMOKE IN THE C
- [SDR 2022FA0000638](https://openairdocs.org/sdr/2022FA0000638.md): Pressure Switch · defective · Oct 16, 2022 · N500XX · Gulstm GVSPG500 · Cabin Pressure Indicator
  > CREW DEPARTED OUT OF KMMU. OIL PRESSURE INDICATION ON #2 ENGINE INDICATING ZERO AFTER WARNING LIGHT CAME ON. CREW PERFORMED A PRECAUTIONARY SHUTDOWN AND FOLLOWED THE SHUTDOWN CHECKLIST. CREW LEVELED OFF AROUND FL200 AFTER NOTIFYING ATC AND CONTINUED WITH CHECK
- [SDR Q5QA2019092003](https://openairdocs.org/sdr/Q5QA2019092003.md): Powerpack · failed · Sep 20, 2019 · N649DX · Emb EMB500 · Hydraulic Pump (Electric/Engine), Main
  > PILOT POWERED UP THE AIRCRAFT AND IMMEDIATELY NOTED THE HYDRAULIC PUMP WAS CYCLING CONTINUOUSLY. PILOT PROCEEDED TO SHUT DOWN THE AIRCRAFT. CORRECTIVE ACTION INVOLVED INSTALLING AN OVERHAULED POWERPACK. OPERATIONAL CHECK WAS SATISFACTORY.
- [SDR CA190604002](https://openairdocs.org/sdr/CA190604002.md): Engine · malfunctioned · May 21, 2019 · Emb EMB500 · Engine (Turbine/Turboprop)
  > (CAN) DURING FLIGHT AT 40K FEET PILOT DETECTED FUEL/OIL SMELL IN THE CABIN FOLLOWED BY LEFT HAND ENGINE VIBRATION WHICH LED TO ENGINE OVER-TEMP EXCEEDANCE. N1 FAULT APPEARED AND PILOT ELECTED TO REDUCE ENGINE POWER. SAME THING HAPPENED TO RIGHT HAND ENGINE FOL
- [SDR E07A2018071000001](https://openairdocs.org/sdr/E07A2018071000001.md): Starter Gen · defective · Jul 9, 2018 · N665AS · Emb EMB500 · Starter-Generator
  > DURING CLIMB OUT CREW NOTICED VIBRATION COMING FROM LT ENGINE. CREW ELECTED TO SHUT DOWN LT ENGINE AND RETURN TO DEPARTURE AIRPORT.
- [SDR Q5QA2018043000001](https://openairdocs.org/sdr/Q5QA2018043000001.md): Pump · failed · Apr 27, 2018 · N649DX · Emb EMB500 · Hydraulic Pump (Electric/Engine), Main
  > PILOT EXPERIENCED A TOTAL HYDRAULIC FAILURE. WITHOUT HYDRAULIC PRESSURE, THE LANDING GEAR FELL OUT AND CYCLED TO DOWN AND LOCKED. THE PILOT DIVERTED AND LANDED WITHOUT INCIDENT UTILIZING EMERGENCY BRAKES. REPLACED THE HYDRAULIC PUMP ASSEMBLY. THIS IS THE
- [SDR 9SUA2017092601](https://openairdocs.org/sdr/9SUA2017092601.md): Warning Message · false activation · Sep 24, 2017 · N580JS · Emb EMB500 · Door Warning System
  > UPON REACHING AN ALTITUDE OF 30,000', PAX DOOR OPEN CAS WARNING MESSAGE ILLUMINATED. DECLARED AN EMERGENCY, STARTED AN EMERGENCY DESCENT AND RAN THE CHECKLIST IN THE QRH. RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTENANCE OPERATED THE DOOR SEVER
- [SDR 9SUA201707120001](https://openairdocs.org/sdr/9SUA201707120001.md): Warning System · activated · Jul 8, 2017 · N581JS · Emb EMB500 · Landing Gear Brake System
  > UPON ENTERING THE LEFT DOWNWIND AT KDRO, AND AFTER BRINGING THE GEAR DOWN AT APPROXIMATELY THE MIDFIELD POINT, WE RECEIVED A "BRK FAIL" CAS MESSAGE ILLUMINATION. AT THIS TIME, WE DECIDED TO BREAK OFF FROM THE PATTERN TO RUN OUR QRH. WE CIRCLED TO THE SOUTHWEST
- [SDR 9SUA2017070301](https://openairdocs.org/sdr/9SUA2017070301.md): Cable · kinked · Jun 30, 2017 · N580JS · Emb EMB500 · Passenger/Crew Doors
  > PAX DOOR OPEN CAS MESSAGE DISPLAYED IN FLIGHT. SIMULTANEOUS DECREASE IN CABIN PRESSURE. THE CREW EXECUTED AN EMERGENCY DESCENT AND DECLARED AN EMERGENCY. CABIN ALTITUDE NEVER INCREASED ENOUGH TO CAUSE THE OXYGEN MASKS TO DROP. THE CREW PERFORMED A STANDARD CO
- [SDR Q5QA20170612010](https://openairdocs.org/sdr/Q5QA20170612010.md): Pump · failed · Jun 12, 2017 · N649DX · Emb EMB500 · Hydraulic Pump (Electric/Engine), Main
  > HYDRAULIC PUMP FAILED IN FLIGHT.
- [SDR Q5QA20170404009](https://openairdocs.org/sdr/Q5QA20170404009.md): Hydraulic System · low pressure · Apr 4, 2017 · N649DX · Emb EMB500 · Hydraulic System, Main
  > LOW HYD CAS, HYDRAULIC PRESSURE DROPPED TO 800 PSI IN FLIGHT. HYDRAULIC POWER-PACK ASSEMBLY WAS FOUND TO BE FAILED.
- [SDR Q5QA2017030800067](https://openairdocs.org/sdr/Q5QA2017030800067.md): Pump · failed · Mar 7, 2017 · N288DX · Emb EMB500 · Hydraulic Pump (Electric/Engine), Main
  > BRAKE SYSTEM FAILURE CAUSED BY HYDRAULIC PUMP FAILURE.
- [SDR 2016FA0000662](https://openairdocs.org/sdr/2016FA0000662.md): Engine · flamed out · Dec 16, 2016 · N623DT · Emb EMB500 · Engine (Turbine/Turboprop)
  > DURING TAKE OFF, ENGINE FLAMED OUT WITH INFLIGHT. RESTARTED.
- [SDR Q5QA20161115006](https://openairdocs.org/sdr/Q5QA20161115006.md): Pump · failed · Nov 9, 2016 · N649DX · Emb EMB500 · Hydraulic Pump (Electric/Engine), Main
  > WHILE CRUISING AT 22,000 FT, PILOT EXPERIENCED HYD AUTO PRESSURE FLUCTUATION BETWEEN 1600/3200. HYD ON, PRESSURE FLUCTUATIONS AND SPIKES TO 3800. HYD OFF, PRESS 0 AND LANDING GEAR FALLS OUT. PILOT LANDED WITH HYD PRESSURE ON AND SEEING PRESSURE FLUCTUATIONS AN
- [SDR 9SUA2016073002](https://openairdocs.org/sdr/9SUA2016073002.md): Container · odor · Jul 26, 2016 · N583JS · Emb EMB500 · Air Distribution System
  > SMOKE IN THE CABIN AFTER TAKEOFF. DECLARED AN EMERGENCY. RETURNED TO THE FIELD WITH NO FURTHER INCIDENT. MAINTENANCE DEBRIEFED THE FLIGHT CREW, CREW REPORTED THERE WAS A SLIGHT FOG IN THE CABIN AND COCKPIT WITH A ACCOMPANYING ODOR OF HOT PLASTIC. VCS SYSTEM
- [SDR 9SUA2016072101](https://openairdocs.org/sdr/9SUA2016072101.md): Powerpack · failed · Jul 16, 2016 · N575JS · Emb EMB500 · Hydraulic System, Main
  > HYDRAULIC LOW PRESSURE CAS MESSAGE ILLUMINATED WHEN GEAR WAS LOWERED. BRAKE FAIL CAS MESSAGE ILLUMINATED 15 SECONDS AFTER THE GEAR WAS DOWN, CREW ABORTED LANDING, CREW USED THE EMERGENCY PARKING BRAKE TO STOP THE AIRCRAFT WITHOUT ISSUE. SYSTEM WAS TROUBLESHO
- [SDR E07A201606010001](https://openairdocs.org/sdr/E07A201606010001.md): Valve · sticking · Jun 1, 2016 · N639AS · Emb EMB500 · Engine Bleed Air System
  > BLEED 2 DUCT OVERTEMP. VALVE STICKS.
- [SDR Q5Q2016F00001](https://openairdocs.org/sdr/Q5Q2016F00001.md): Blade · failed · Mar 30, 2016 · N288DX · Emb EMB500 · Engine (Turbine/Turboprop)
  > THE REFERENCED ENGINE WAS REMOVED AND SENT TO MFG FOR O/H. MFG DETERMINED THAT A NUMBER OF HIGH PRESSURE TURBINE BLADES, PN 35C5521-01 WERE DEFECTIVE DUE TO CRACKS AT THE FILLET RADIUS. MFG MADE THE AIRWORTHINESS DETERMINATIONS BY HAVING THEIR O/H LINE PERSO
- [SDR CA160226006](https://openairdocs.org/sdr/CA160226006.md): Brake · cracked · Feb 26, 2016 · Emb EMB500 · Landing Gear Brake System
  > (CAN) DURING A GENERAL VISUAL INPECTION OF THE NOSE LANDING GEAR IT WAS DISCOVERED THAT A CRACK HAD DEVELOPED ACROSS THE SPIN BRAKE ASSEMBLY TWO LOWER MOUNTING HOLES. THIS AIRCRAFT HAS 3315.7 HRS AND 2898 CYCLES. NO OTHER DAMAGE WAS NOTED.
- [SDR CA160226007](https://openairdocs.org/sdr/CA160226007.md): Wire · broken · Feb 26, 2016 · Emb EMB500 · Engine Indicating System Wiring
  > (CAN) THERMOCOUPLE PROBES HAVE BROKEN WIRING AND ARE RENDERED UNSERVICABLE.
- [SDR CA160302017](https://openairdocs.org/sdr/CA160302017.md): Tire · failed · Feb 7, 2016 · Emb EMB500 · Tire
  > (CAN) LEFT HAND MLG TIRE TREAD SEPARATED ON TAKE OFF, CAUSING DAMAGE TO FLAP AND WING STRUCTURE. ON TAKE OFF VIBRATION WAS NOTED BUT GEAR RETRACTION AND ALL OTHER INDICATIONS WERE NORMAL. ON LANDING ADDITIONAL VIBRATION NOTED, AFTER COMING TO A STOP IT WAS NOT
- [SDR Q5QA2016F00042](https://openairdocs.org/sdr/Q5QA2016F00042.md): Oil System · low pressure · Jan 1, 2016 · N648DX · Emb EMB500 · Engine Oil Pressure
  > LOSS OF ENGINE OIL PRESSURE IN FLIGHT REQUIRING ENGINE SHUTDOWN.
- [SDR 9SUA2015122101](https://openairdocs.org/sdr/9SUA2015122101.md): Powerpack · failed · Dec 15, 2015 · N575JS · Emb EMB500 · Hydraulic Pump (Electric/Engine), Main
  > THE CREW WAS EXECUTING A VISUAL APPROACH. AFTER EXTENDING THE LG, THE HYD PRESS FAILED TO RECOVER. THE CREW RECEIVED HYD LO PRESS & BRK FAIL CAS MSGS. ABORTED THE APPROACH & ASKED FOR RADAR VECTORS ON THE SOUTH SIDE WHILE RUNNING THE QRH. THE QRH PROCEDURE
- [SDR E07A20151211001](https://openairdocs.org/sdr/E07A20151211001.md): Engine · contaminated · Dec 8, 2015 · N620AS · Emb EMB500 · Engine (Turbine/Turboprop)
  > ON TAKEOFF, CREW NOTED SLIGHT SMOKE IN CABIN & SMELL OF BURNING OIL. RETURNED WITHOUT INCIDENT. THIS WAS FIRST FLIGHT AFTER OVERHAULED ENGS WERE INSTALLED. OPENED BLEED SYS & USED BORESCOPE TO INSPECTED ENG & BLEED SYS UP TO THE PRESS AFT PRESS BULKHEAD. N
- [SDR CA150811007](https://openairdocs.org/sdr/CA150811007.md): Rivet · broken · Aug 7, 2015 · Emb EMB500 · Engine Air Intake System
  > (CAN) DURING AN AIRWORTHINESS CONDITION CHECK, IT WAS DISCOVERED THAT A RIVET HEAD FOR THE TTO SENSOR ATTACHMENT MOUNT IN THE #1 ENGINE INLET HAD DEPARTED. ONLY ONE OF THE FIVE TOTAL WAS FOUND MISSING THE HEAD, THE AIRFRAME AND ENGINE HAD A TOTAL OF 3029.3 HRS
- [SDR 2015FA0000348](https://openairdocs.org/sdr/2015FA0000348.md): Clamp · leaking · Jul 23, 2015 · N100NV · Emb EMB500 · Pneumatic Distribution System
  > DUCT NR 2 OVERTEMP. PERFORMED QRH PROCEDURE AND RETURNED TO DEPARTURE. INSPECTED ACFT AND FOUND RT TMV DUCT CONNECTOR LEAKING. ADJUSTED CLAMP ON TMV AND SECURED. ACCOMPLISHED FULL POWER ENGINE RUNS IAW AMM 71-00-00. NO BLEED LEAKS OR INDICATIONS DURING R
- [SDR CA150724003](https://openairdocs.org/sdr/CA150724003.md): Control Cable · worn · Jul 22, 2015 · Emb EMB500 · Aileron Control System
  > (CAN) DURING A SCHEDULED 333FH INSPECTION AN AILERON CONTROL CABLE IN THE R/H WING SHOWED WEAR BETWEEN RIBS 5 AND 6. THERE WAS NOT VISIBLE CONTACT ON ADJACENT STRUCTURE.
- [SDR CA150724004](https://openairdocs.org/sdr/CA150724004.md): Control Cable · worn · Jul 22, 2015 · Emb EMB500 · Aileron Control System
  > (CAN) DURING A SCHEDULED 3000 FH INSPECTION AN AILERON CONTROL CABLE IN THE L/H WING SHOWED WEAR BETWEEN RIBS 5 AND 6, THERE WAS NO VISIBLE CONTACT ON ADJACENT STRUCTURE.
- [SDR CA150615003](https://openairdocs.org/sdr/CA150615003.md): Engine · faulty · Jun 2, 2015 · Emb EMB500 · Engine (Turbine/Turboprop)
  > (CAN) PILOTS REPORTED SMOKE IN CABIN AFTER TAKEOFF, 1500 - 2000 FEET. CREW PUT MASK ON & LANDED. ENG HAD A RECENT HSI. THE TROUBLESHOOTING SHOWED OIL AROUND THE INNER DIAMETER OF THE FAN DISC & IN THE EXHAUST BREATHER OUT PORT & ON THE FMU DRAIN. OIL CONSU
- [SDR 9SUA2015FA0000221](https://openairdocs.org/sdr/9SUA2015FA0000221.md): Carbon Seal · failed · May 14, 2015 · N575JS · Emb EMB500 · Turbine Engine Oil System
  > SMOKE IN COCKPIT RIGHT AFTER TAKEOFF. SMOKE ENTERED FROM UNDER AVIONICS, POSSIBLY FLOOR/RUDDER AREA. ENTERED CABIN AS WELL. RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. RAN ACFT AT TAKEOFF POWER FOR 30 MIN. OPERATED BLEED SYSTEMS. PERFORMED CABIN/
- [SDR CA150306009](https://openairdocs.org/sdr/CA150306009.md): Indication Sys · stuck · Mar 2, 2015 · Emb EMB500 · Engine Oil Pressure
  > (CAN) THE AIRCRAFT TOOK OFF & AFTER CROSSING 1500 FT THE ENGINE 2 LOW OIL PRESS CAS CAME ON. WHEN THE PILOT CHECKED THE RIGHT HAND OIL PRESS IT WAS SHOWING 75 PSI, IN RED, WITH ENGINE EXCEEDANCE CAS MESSAGE. THE AIRCRAFT LANDED AT DEPARTURE AIRPORT, DURING A
- [SDR CA141203009](https://openairdocs.org/sdr/CA141203009.md): Bolt · damaged · Dec 2, 2014 · Emb EMB500 · Trailing Edge Flaps
  > (CAN) DURING FLAP REMOVAL IT WAS DISCOVERED THAT BOTH FLAP ACTUATOR ATTACHING BOLTS WERE DAMAGED. THE LT BOLT APPEARS TO HAVE BEEN OVER TORQUED ON INSTALL, WHILE THE RT BOLT HAS A COUPLE GOUGE MARKS AROUND THE CIRCUMFERENCE OF THE BOLT.
- [SDR CA141203008](https://openairdocs.org/sdr/CA141203008.md): Control Cable · worn · Nov 29, 2014 · Emb EMB500 · Aileron Control System
  > (CAN) DURING INSPECTION THE LT AND RT FWD AILERON CABLES LOCATED IN THE WING WERE DISCOVERED TO HAVE 40% BLENDING OF THE CABLE WHERE IT PASSES OVER THE PULLEYS.
- [SDR CA141203007](https://openairdocs.org/sdr/CA141203007.md): Torque Tube · worn · Nov 26, 2014 · Emb EMB500 · Elevator Structure
  > (CAN) DURING INSPECTION IT WAS NOTED THAT THERE WAS EXCESSIVE PLAY IN THE RT ELEVATOR FITTING AND ATTACHING TORQUE TUBE. UPON DISASSEMBLY SOME WEAR WAS NOTED ON BOTH THE TORQUE AND THE R/H ELEVATOR FITTING.
- [SDR CA141202013](https://openairdocs.org/sdr/CA141202013.md): Engine · power loss · Nov 14, 2014 · Cessna 510 · Engine (Turbine/Turboprop)
  > (CAN) WHILE ENROUTE AT ABOUT FL300 IN POOR WEATHER AND CONSTANT ICING CONDITIONS, BOTH ENGINES POWER ROLLBACK. THE LT ENGINE RECOVERED BUT SUFFERED SIGNIFICANT FLUCTUATIONS. THE PILOT WANTED TO CLIMB HIGHER BUT THE ACFT WOULD NOT RESPOND, CHOSE TO DESCEND AND
- [SDR RT5R2014101084123](https://openairdocs.org/sdr/RT5R2014101084123.md): Carbon Seal · failed · Oct 8, 2014 · N777JQ · Emb EMB500 · Turbine Engine Oil System
  > IT WAS REPORTED THAT THE ACFT MADE AN UNSCHEDULED LANDING AND A PILOT COMMANDED SHUTDOWN NR 1 ENGINE DUE TO LOW OR LOSS OF OIL PRESSURE INDICATION.
- [SDR CA141024012](https://openairdocs.org/sdr/CA141024012.md): Oil System · low pressure · Oct 6, 2014 · Emb EMB500 · Engine Oil Indicating System
  > (CAN) WHILE IN CLIMB, 25 MINUTES AFTER T/O, PILOT NOTED ENGINE 1 LOW OIL PRESSURE WARNING AND ENGINE EXCEEDANCE MESSAGE. OIL PRESSURE GRADUALLY DECREASING AND PILOT INITIATED ENGINE SHUTDOWN WHEN PRESSURE REACHED 60 PSI, LOWEST 47 PSI. EMERGENCY WAS DECLARED
- [SDR 9SUA201407180002](https://openairdocs.org/sdr/9SUA201407180002.md): Exhaust Duct · cracked · Jul 8, 2014 · N582JS · Emb EMB500 · Engine Collector/Tailpipe/Nozzle
  > TURBINE EXHAUST COWL ASSY CRACKED ON NR1 ENGINE. REMOVED TURBINE EXHAUST COWL ASSY, PN 35C4655-01, DUE TO CRACK. INSTALLED NEW TURBINE EXHAUST COWL ASSY, PN 35C4655-01. ALL WORK PERFORMED IAW MM PN 3072162, REV NR 11, DATED MAY 17, 2014. WORK PERFORMED BY
- [SDR 9SUA201407180001](https://openairdocs.org/sdr/9SUA201407180001.md): Control Valve · failed · Jul 2, 2014 · N580JS · Emb EMB500 · Landing Gear Brake System
  > BRAKE FAIL CAS MESSAGE OCCURRED AT 23,000 FT ENROUTE TO 36000 FT CLEARED TO LEVEL OFF AT 24,000. DIVERTED. CREW RAN CHECKLIST FOR THE BRAKE FAIL. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. PERFORMED BRAKE SYSTEM FUNCTIONAL TEST IAW 32-41-00-720-80
- [SDR CA140619014](https://openairdocs.org/sdr/CA140619014.md): Engine · power loss · Jun 4, 2014 · Emb EMB500 · Engine (Turbine/Turboprop)
  > (CAN) DURING CRUISE, THE ENGINE SUFFERED AN UNCOMMANDED POWER LOSS AND IMMEDIATELY RECOVERED. P&WCÏ¿½S LOCAL FIELD SUPPORT REPRESENTATIVE WILL ANALYSE THE POST FLIGHT DATA DOWNLOAD TO TROUBLESHOOT.
- [SDR CA131105004](https://openairdocs.org/sdr/CA131105004.md): Engine · unknown · Oct 29, 2013 · Emb EMB500 · Engine (Turbine/Turboprop)
  > (CAN) DURING FLIGHT, THE ACFT ENCOUNTERED LIGHT RIME ICE CONDITION. ONCE ABOVE FL260, THE PILOT NOTICED THE ACFT WAS CLIMBING AT AN ANEMIC OR ZERO RATE. AFTER CROSSING FL290, THE PILOT NOTICED THAT THERE WAS A SIGNIFICANT DISCREPANCY BETWEEN BOTH ENGINES, TO
- [SDR CA131007006](https://openairdocs.org/sdr/CA131007006.md): Oil System · low pressure · Sep 25, 2013 · Emb EMB500 · Engine Oil Pressure
  > DURING FLIGHT, THE ENGINE OIL PRESSURE DROPPED, FORCING THE PILOT TO SHUT THE ENGINE DOWN. AN UNEVENTFUL SINGLE ENGINE LANDING FOLLOWED. POST FLIGHT INSPECTION FOUND ENGINE EXTERNALS TO BE DRY BUT NO OIL ON THE SIGHT GLASS. THE ENGINE IS BEING REPLACED.
- [SDR CA130921001](https://openairdocs.org/sdr/CA130921001.md): Oil System · fluctuates · Sep 11, 2013 · Emb EMB500 · Engine Oil Pressure
  > (CAN) OIL PRESSURE FLUCTUATIONS WERE FOLLOWED BY LOW OIL PRESSURE LIGHT AFTER THROTTLE BACK OF THE ENGINE. THE CREW ELECTED TO SHUTDOWN THE ENGINE. AN UNEVENTFUL SINGLE-ENGINE LANDING WAS ACCOMPLISHED.
- [SDR CA130819003](https://openairdocs.org/sdr/CA130819003.md): Oil System · leaking · Aug 8, 2013 · Emb EMB500 · Turbine Engine Oil System
  > (CAN) AFTER FLYING FOR.5 HOUR THE ENGINE NR 2 LOST OIL PRESSURE. THE PILOTS ELECTED TO SHUTDOWN THE ENGINE AND LANDED SAFELY. JUST BEFORE THE FLIGHT THE ENGINE OIL LEVEL WAS RECORDED TO BE 75 PERCENT AT THE SIGHT GLASS. THE ON GROUND INVESTIGATION REVEALED
- [SDR CA130805014](https://openairdocs.org/sdr/CA130805014.md): Engine · faulted · Aug 1, 2013 · Emb EMB500 · Engine (Turbine/Turboprop)
  > (CAN) DURING TAKEOFF ROLL, THE PILOT REPORTED E2 CONTROL FAULT AND ENGINE 2 FADEC FMU TORQUE MOTOR FAULTS. THE CREW ELECTED TO ABORT TAKEOFF. NO INJURIES REPORTED. EDCU MEMORY DOWNLOAD WAS SEND TO CFIRST. TROUBLESHOOTING ONGOING.
- [SDR CA130716003](https://openairdocs.org/sdr/CA130716003.md): Tire · bulged · Jul 14, 2013 · Emb EMB500 · Tire
  > (CAN) IN THE PAST MONTH WE HAVE REMOVED 2 MAIN WHEEL TIRES FROM ACFT FOR SIDEWALL AND TREAD BULGES. THE TIRES ARE 21 X 6.5 X 10, PN 215K26-1. THE FIRST TIRE WAS REMOVED FROM THE LT POSITION OF ACFT. TIRE: PN 215K26-1, SN 22712476, TSN 292.7. THE SECOND TIR
- [SDR CA130705005](https://openairdocs.org/sdr/CA130705005.md): Heater · failed · Jul 5, 2013 · Emb EMB500 · Ice/Rain Protection System
  > (CAN) ON ENGINE START CAS MESSAGE, SWPS HTR 2 FAIL, APPEARED. TROUBLESHOOTING REVEALED THE NR 2 AOA VANE HEATER HAS FAILED. NR 2 AOA VANE BASE ASSEMBLY TO BE REPLACED.
- [SDR CA130628007](https://openairdocs.org/sdr/CA130628007.md): Hose · leaking · Jun 26, 2013 · Emb EMB500 · Hydraulic System, Main
  > (CAN) DURING POST FLIGHT INSPECTION FOUND LT MLG ACTUATOR RETRACTION LINE LEAKING. HOSE ASSEMBLY, PN A11011-1, REPLACED.
- [SDR CA130415004](https://openairdocs.org/sdr/CA130415004.md): Powerpack · failed · Apr 11, 2013 · Emb EMB500 · Hydraulic System, Main
  > (CAN) BRAKE FAIL CAS FOLLOWED BY HYD FAIL CAS DURING TAXI OUT. HYDRAULIC PRESSURE RETURNED, BUT BRAKE FAIL CAS REMAINED. ACFT TAXIED BACK TO CHOCKS. CMC/CVFDR DOWNLOADS PERFORMED. FORWARDED TO MFG ENGINEERS, SUGGEST REPLACEMENT OF HYDRAULIC POWER PACK.
- [SDR CA130328003](https://openairdocs.org/sdr/CA130328003.md): Pressure Switch · malfunctioned · Mar 24, 2013 · Emb EMB500 · Landing Gear Brake System
  > (CAN) DURING A TIGHT LT 180 DEGREE TURN, CREW NOTICED A REDUCTION IN LT BRAKE EFFECTIVENESS, ACFT ACCELERATED THEN EMERGENCY PARK BRAKE WAS ACTIONED TO STOP THE ACFT, THEN CREW WAS PRESENTED WITH A BRAKE FAIL CAS MESSAGE AND THE HYD PRESSURE WAS INDICATING ZER

Next page: https://openairdocs.org/engine/pratt-whitney-canada-pw617f-e/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 = 'PW617FE'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/pratt-whitney-canada-pw617f-e/reports

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