# Service difficulty reports: Pratt & Whitney Canada PW610F-A

A list on [Pratt & Whitney Canada PW610F-A](https://openairdocs.org/engine/pratt-whitney-canada-pw610f-a.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 144 reports

- [SDR 2020FA0000323](https://openairdocs.org/sdr/2020FA0000323.md): Processor · failed · Jul 6, 2020 · Eclips ECLIPSEEA500 · Engine Fuel and Control
  > PROCESSING CENTER (P/N 2536-6) CONTROLS A MULTITUDE OF FUNCTIONS WITHIN THE AIRCRAFT, INCLUDING FLIGHT CONTROLS, PRESSURIZATION, FUEL, AND THE ENGINES THEMSELVES. IN THE LAST WEEK ALONE, HAVE SEEN TWO OCCURRENCES OF THE LEFT ACS FADEC CHANNEL B FAILING, CAU
- [SDR CA150817008](https://openairdocs.org/sdr/CA150817008.md): Engine · warning message · Aug 6, 2015 · Eclips ECLIPSEEA500 · Engine (Turbine/Turboprop)
  > (CAN) ON TAKE-OFF, HAD LEFT ENGINE CONTROL CAS MESSAGE, AND LEFT ENGINE SPD CAS MESSAGES, LEFT ENGINE DID NOT THROTTLE-UP. PILOT ABORTED TAKE-OFF, AND RETURNED TO THE FLIGHT LINE.
- [SDR 3BOR2015012715001](https://openairdocs.org/sdr/3BOR2015012715001.md): Duct · cracked · Jan 26, 2015 · N256DP · Eclips ECLIPSEEA500 · Engine Collector/Tailpipe/Nozzle
  > DURING THE 12 MONTH/300 HOUR ENGINE INSPECTION ON THE LT AND RT ENGINES ON THE ACFT, A VISUAL INSPECTION OF THE LT ENGINE EXHAUST AREA NOTED A PIECE OF THE ENGINE OUTER BYPASS DUCT MISSING. APPROXIMATELY 6" SECTION MISSING, BETWEEN 10 O'CLOCK AND 1 O'CLOCK AS
- [SDR CA141103010](https://openairdocs.org/sdr/CA141103010.md): Oil System · low pressure · Oct 27, 2014 · Eclips ECLIPSEEA500 · Engine Oil Indicating System
  > (CAN) THE ENGINE SUSTAINED A HIGH OIL PRESSURE. THE PILOT ELECTED TO SHUT DOWN THE ENGINE. THIS IS THE 2ND OCCURRENCE. THE FIRST OCCURRENCE WAS REPORTED ON 16 OCT. 2014. PRATT AND WHITNEY WILL INVESTIGATE TO ESTABLISH ROOT CAUSE AND PROVIDE INFORMATION TO TRA
- [SDR CA141103003](https://openairdocs.org/sdr/CA141103003.md): Oil System · low pressure · Oct 16, 2014 · Eclips ECLIPSEEA500 · Engine Oil Indicating System
  > (CAN) FOLLOWING AN UNEVENTFUL TAKEOFF AND CLIMB THE PILOT OBSERVED MAIN OIL PRESSURE (MOP) EXCEEDING OPERATIONAL LIMITS INTO RED ZONE WHILE IN CRUISE. AFTER UNSUCCESSFUL ATTEMPT TO REDUCE MOP, THE PILOT ELECTED TO ACCOMPLISH AN IFSD AND RETURNED THE ORIGIN AIR
- [SDR CA141103002](https://openairdocs.org/sdr/CA141103002.md): Engine · vibration · Oct 13, 2014 · Eclips ECLIPSEEA500 · Engine (Turbine/Turboprop)
  > (CAN) THE LEFT HAND ENGINE MADE NOISE AND VIBRATION PRIOR TO TAKE OFF. THE PILOT RETURNED TO FBO. IT WAS SUGGESTED TO BORESCOPE BOTH ENGINES FOR CARBON BUILD UP AND HPT VANE CARBON BLOCKAGE.
- [SDR CA140908006](https://openairdocs.org/sdr/CA140908006.md): Oil System · reads high · Aug 25, 2014 · Eclips ECLIPSEEA500 · Engine Oil Indicating System
  > (CAN) THE PILOT REPORTED AN HIGH OIL PRESSURE WARNING. REDUCED ENGINE THRUST TO IDLE IAW QRH INSTRUCTIONS AND LANDED. TROUBLESHOOTING ON-GOING.
- [SDR CA140602006](https://openairdocs.org/sdr/CA140602006.md): Indication Sys · malfunctioned · May 10, 2014 · Eclips ECLIPSEEA500 · Engine Fuel Indicating System
  > (CAN) DURING FLIGHT, 5 MINUTES AFTER DEPARTURE, THE PILOT REPORTED A FUEL FILTER AND A FUEL BYPASS MESSAGE INDICATION. THE PILOT ELECTED TO RETURN TO DEPARTURE WHERE AN UNEVENTFUL LANDING WAS PERFORMED. TROUBLESHOOTING IS ONGOING.
- [SDR CA130513001](https://openairdocs.org/sdr/CA130513001.md): Engine · power loss · Apr 27, 2013 · Eclips ECLIPSEEA500 · Engine (Turbine/Turboprop)
  > (CAN) DURING FLIGHT, THE CREW RECEIVED AN ENGINE CONTROL FAIL CAUTION WARNING. DURING ACCOMPLISHMENT OF THE CHECKLIST FOR THIS MESSAGE THEY DISCOVERED THAT THEY HAD NO THROTTLE RESPONSE OR CONTROL OVER THE RT ENGINE. THE CREW SHUT THE ENGINE DOWN AND LANDED
- [SDR 2012FA0000604](https://openairdocs.org/sdr/2012FA0000604.md): Actuator · false activation · Aug 8, 2012 · N218JT · Eclips ECLIPSEEA500 · Landing Gear Actuator
  > ACFT STARTED TO GET AN INTERMITTENT CAS MESSAGE FOR LANDING GEAR FAIL DURING MX TAXI /ENGINE RUN. ACFT WAS SHUTDOWN AND PULLED INTO THE HANGER TO TROUBLESHOT ACFT. WHEN ACFT POWER WAS REAPPLIED DURING A WALK AROUND TO INSPECT LANDING GEAR ACTUATORS WHILE UND
- [SDR 2012FA0000606](https://openairdocs.org/sdr/2012FA0000606.md): Fire Bottle · failed · May 23, 2012 · N218JT · Eclips ECLIPSEEA500 · Extinguishing System
  > RT ENGINE FIRE BOTTLE DISCHARGED INSIDE ENGINE PYLON. THIS IS THE SECOND BOTTLE FAILURE OF THE NEW DESIGN IN LESS THAN 6 MONTHS ON THIS ACFT. THE FIRE BOTTLE AGENT IS HIGHLY CORROSIVE AND CAN CAUSE STRUCTURAL DAMAGES TO ENGINE STRUCTURE IF NOT FOUND QUICKLY.
- [SDR CA110224001](https://openairdocs.org/sdr/CA110224001.md): Blades · failed · Feb 22, 2011 · Turbine Section
  > ENGINEERING INVESTIGATION REPORT EIR PW100 2011-009. DISASSEMBLY OF THE ENGINE TO INVESTIGATE PERFORMANCE DETERIORATION REVEALED EIGHT LP BLADES WERE FRACTURED. FURTHER INVESTIGATION REVEALED THE ENGINE SUSTAINED AN OVERTEMP. THE CAUSE OF THE FRACTURED LP BL
- [SDR CA110225001](https://openairdocs.org/sdr/CA110225001.md): O-Ring · leaking · Feb 16, 2011 · Pilats PC1245 · Landing Gear Brake System
  > NEW BRAKE UNIT ASSY LEAKING FLUID FROM THE 1 OR MORE PISTONS. UNIT REPLACED WITH SERVICEABLE UNIT. NO FUTHER ACTION WAS REQUIRED.
- [SDR CA110214003](https://openairdocs.org/sdr/CA110214003.md): Engine · power loss · Feb 1, 2011 · Engine (Turbine/Turboprop)
  > POWER ROLLBACK THE RT SIDE ENGINE ROLLED BACK 7 PERCENT ON 2 DIFFERENT FLIGHTS. 1ST OCCURRENCE HAPPENED AT 20,000 FT, THE 2ND WAS AT 32,000 FT, BOTH WHILE IN LEVEL FLIGHT AT CRUISE POWER. ON BOTH FLIGHTS, THE CREW REPORTED THAT THE ENGINE RETURNED TO NORMAL P
- [SDR CA110208009](https://openairdocs.org/sdr/CA110208009.md): Engine · failed · Jan 28, 2011 · Engine (Turbine/Turboprop)
  > (CAN) ABORTED TAKEOFF (SINGLE ENGINE) THE CUSTOMER REPORTED THAT THE ENGINE WOULD NOT MAKE POWER AND TAKE-OFF WAS ABORTED. DURING A SUBSEQUENT START THE ENGINE WOULD HANG AND THE EMERGENCY POWER LEVER WAS REQUIRED TO ACHIEVE IDLE POWER. TROUBLESHOOTING ONGOIN
- [SDR CA110124001](https://openairdocs.org/sdr/CA110124001.md): Wire · chafed · Jan 24, 2011 · Dhav DHC8301 · Electrical Power System Wiring
  > WHEN WING DEICE BOOTS ACTIVATED IN AUTO THEY FAILED TO INFLATE AND CB P8 WAS FOUND TO HAVE TRIPPED. RESET AND BOOTS OPERATED UNTIL L3 & R4 WHEN CB TRIPPED AGAIN. MANUAL BOOTS TRIED BUT MANUAL CONTROL CB, E8 TRIPPED. FOUND DEICE TIMER EMITTING ELECTRICAL BUR
- [SDR CA110120007](https://openairdocs.org/sdr/CA110120007.md): Control Cable · chafed · Jan 20, 2011 · Airtrc AT802 · Rudder Control System
  > DURING THE ANNUAL INSP, THE RUDDER CABLE ASSY PN 70524-10-500 WAS FOUND TO BE CHAFED WHERE THE CABLE PASSES THROUGH THE COCKPIT LOWER SKIN ASSY PN 11124-1. THE CABLE REQUIRED REPLACEMENT.
- [SDR CA110124003](https://openairdocs.org/sdr/CA110124003.md): Windshield · unserviceable · Jan 20, 2011 · Lear 60LEAR · Flight Compartment Windows
  > REMOVED LT WINDSHIELD, CTR POST LOWER ATTACHEMENT HOLES FOUND IMPROPER MACHINE. LOWER HOLES SHOULD BE COUNTERSUNK TO RECEIVED SCREWS AND NO COUNTERSUNK WERE FOUND ON PARTS.
- [SDR CA110119005](https://openairdocs.org/sdr/CA110119005.md): Filter · failed · Jan 18, 2011 · Airtrc AT802A · Hydraulic System, Main
  > BOTH OF THE SCOOP (UP AND DOWN), HYD PRESSURE FILTERS WERE FOUND DURING INSP WITH THE ENDS OF THEM BLOWN OUT AND MISSING PIECES. BOTH FILTERS WERE FOUND TO HAVE BEEN INSTALLED CORRECTLY IAW MM AND DWGS. HOWEVER, THIS APPEARS TO BE CONTRADICTORY TO THE INSTRUC
- [SDR CA110125016](https://openairdocs.org/sdr/CA110125016.md): Engine · failed · Jan 18, 2011 · Engine (Turbine/Turboprop)
  > (CAN) ON GROUND EVENT DURING OVERSPEED GOVERNOR CHECK PRIOR TO T/O, THE PILOT HEARD A LOUD NOISE AND SAW MATERIAL COMING OUT OF THE EXHAUST. THE ENGINE WAS SHUT DOWN. POST EVENT INSPECTION FOUND PUNCTURE DAMAGE FROM DEBRIS ON THE WINGS. THE ENGINE WILL BE SENT
- [SDR CA110117008](https://openairdocs.org/sdr/CA110117008.md): Window · cracked · Jan 17, 2011 · Cessna 550 · Flight Compartment Windows
  > THIS WINDOW IS NOT LAMINATED BUT THE CRACK RUNS ABOUT 75 PERCENT OF THE WAY AROUND THE CIRCUMFERENCE, LIKE IT IS LAMINATED AND SEPARATING. THE CRACK VARIES IN WIDTH GOING SOMETIMES INBD OF THE MOUNTING HOLES BUT NEVER IS DEEP ENOUGH TO BE IN THE VISIBLE AREA W
- [SDR CA110118001](https://openairdocs.org/sdr/CA110118001.md): Stator · cracked · Jan 17, 2011 · Beech B200 · Turbine Section
  > DURING SCHEDULED HSI THE PT STATOR 1ST STAGE WAS FOUND TO BE CRACKED BEYOND LIMITS, THE INNER RING WAS CRACKED COMPLETELY THROUGH AND THE OUTER RING WAS CRACKED COMPLETELY THROUGH EXTENDING INTO A VANE. INSP OF THE OPPOSITE ENGINE REVEALED CRACKING OF THE SAME
- [SDR CA110120006](https://openairdocs.org/sdr/CA110120006.md): Dump Valve · leaking · Jan 16, 2011 · Dhav DHC8311 · Aircraft Fuel Distribution System
  > ON ACFT 324, CREW REPORT A FUEL LEAK ON RT SIDE VENT TANK OF ACFT WHILE IN DE-ICE FACILITY. MFG WAS REQUESTED TO RESPOND. ACFT WAS BRINGING TO THE HANGAR FOR TROUBLESHOOTING AND DEFECT 963025 WAS OPEN. RT DUMP VALVE REPLACED, RT ARMING VALVE PN: 7SC0299, SN:
- [SDR CA110119004](https://openairdocs.org/sdr/CA110119004.md): Governor · failed · Jan 14, 2011 · Raythn B300RAYTHEON · Propeller Governor
  > ACFT CARRIED OUT A NORMAL TAKEOFF ON FIRST FLIGHT OF THE DAY. AFTER TAKEOFF, THE PROPELLER WENT TO 104 PERCENT NP AND THE CREW NOTED THAT THE PROPELLER COULD NOT BE SLOWED DOWN WITH THE PROP LEVER. THEY TURNED BACK AND CARRIED OUT A NORMAL LANDING, GROUND RUN
- [SDR CA110118004](https://openairdocs.org/sdr/CA110118004.md): Actuator · malfunctioned · Jan 12, 2011 · Cessna 550 · Rudder Tab Control System
  > DURING A BASE INSP, IT WAS DISCOVERED THAT THE RUDDER TRIM WHEEL WAS EXTREMELY DIFFICULT TO OPERATE. ON EXAMINATION, IT WAS FOUND THAT 1 OF THE ACTUATOR SCREWS SEEMS TO HAVE JUMPED A THREAD. THE TRIM ACTUATOR WAS REPLACED WITH A NEW PN 55654-102.
- [SDR CA110111005](https://openairdocs.org/sdr/CA110111005.md): Line · leaking · Jan 11, 2011 · Bombdr DHC8400 · Landing Gear Brake System
  > ENG 2 WITH REPORTED THICK SMOKE, AND HYDRAULIC QUANTITY ON SYS 2 ZEROED OUT. POSSIBLE WITH HYDRAULIC LEAK ON ENGINE. CREW DECIDED TO SHUTDOWN BOTH ENGINES FOR SAFETY PRECAUTION. ACFT NOW AWAITING TOW TRUCK. IDENTIFIED HYDRAULIC LEAK ON LT MLG HYDRAULIC HOSE
- [SDR CA110110009](https://openairdocs.org/sdr/CA110110009.md): Display · inoperative · Jan 10, 2011 · Bombdr DHC8400 · Propeller/Rotor Anti-Ice/De-Ice System
  > ON APPROACH, SMOKE STARTED FILLING THE FLIGHT DECK AND THE CREW DONNED THEIR SMOKE MASKS, NO EMERGENCY DECLARATION WAS MADE TO ATC. THE LANDING WAS NORMAL WITHOUT FURTHER ISSUE AND THE AIRCRAFT CONTINUED ON TO THE GATE. FLIGHT CREW NOTED THAT THE SMOKE APPEA
- [SDR CA110112001](https://openairdocs.org/sdr/CA110112001.md): Hose · ruptured · Jan 10, 2011 · Dhav DHC8* · Hydraulic System, Main
  > NR 2 HYD ISO VALVE AND ROLL SPOILER OUTBOARD HYD CAUTION LIGHT CAME ON DURING APPROACH. ALTERNATE NOSE GEAR EXTENSION PERFORMED. REPLACED HOSE TO DRAG STRUT ACTUATOR IN NOSE WHEEL WELL. DUE TO THE INCREASED FAILURE RATE OF PN DSC252B4-0124 OPERATOR WILL STA
- [SDR CA110110004](https://openairdocs.org/sdr/CA110110004.md): Selector · broken · Jan 8, 2011 · Bombdr DHC8400 · Landing Gear Selector
  > SHORTLY AFTER TAKEOFF FROM, FLIGHT CREW SELECTED GEAR UP AND THE SELECT HANDLE BROKE OFF. FLIGHT CREW PERFORMED ALTERNATE RELEASE AND RETURNED TO DEPARTURE AIRPORT. AIRCRAFT LANDED WITHOUT ISSUE. EVENT IS UNDER INVESTIGATION BY ZODIAC (ECE) AND BOMBARDIER.
- [SDR CA110110010](https://openairdocs.org/sdr/CA110110010.md): Socket · burned · Jan 8, 2011 · Dhav DHC8101 · Passenger Compartment Lighting
  > A CABIN SIDEWALL LIGHT WAS REPORTED AS BEING UNSERVICEABLE. THE FLUORESCENT TUBE LAMP HOLDER WAS FOUND BURNT AND PARTIALLY MELTED AT ONE OF THE RECEPTACLES ENDS.
- [SDR CA110110008](https://openairdocs.org/sdr/CA110110008.md): Timer · failed · Jan 7, 2011 · Pilats PC1245 · Propeller/Rotor Anti-Ice/De-Ice System
  > AFTER TURNING ON THE PROP DE-ICE, A PROP DE-ICE CAUTION WAS NOTED. MAINTENANCE FOUND THAT THE PROP DE-ICE TIMER WAS STUCK IN ONE CYCLE AND TWO OF THE PROP DE-ICE BOOTS WERE HEATING ALL OF THE TIME, EVEN WITH THE PROP DE-ICE OFF. A REPAIRED DE-ICE TIMER WAS I
- [SDR CA110110015](https://openairdocs.org/sdr/CA110110015.md): Door Frame · cracked · Jan 7, 2011 · Beech 100BEECH · Fuselage Main, Structure
  > DURING SCHEDULED REPLACEMENT OF CABIN AIR STAIR DOOR LATCH BOLTS THE HOLES CUT OUT FOR THE LATCHES TO EXTEND THROUGH THE DOOR FRAME WERE FOUND CRACKED ON THE FORWARD FRAME ASSY P/N 50-430043-867. THE HOLES CUT IN THE FRAME ASSY ARE APPROX 0.8 INCH IN DIAMETER
- [SDR CA110125005](https://openairdocs.org/sdr/CA110125005.md): Engine · failed · Jan 7, 2011 · Eclips ECLIPSEEA500 · Engine (Turbine/Turboprop)
  > (CAN) IFSD DURING REVENUE FLIGHT THE PILOT HEARD POPPING NOISE FROM ONE ENGINE FOLLOWED WITH RISING ITT INDICATION ON GAUGE. ENGINE WAS SHUTDOWN BY PILOT. AIRCRAFT DIVERTED WHERE IT LANDED UNEVENTFULLY. TROUBLESHOOTING ONGOING. (TC# 20110125005)
- [SDR CA110110001](https://openairdocs.org/sdr/CA110110001.md): Impeller · eroded · Jan 6, 2011 · Turbine Engine Compressor Section
  > HP IMPELLER WITH HEAVY EROSION, THINNING AND CRACKING AT THE BACKPLATE. THE TOTAL TIME ON THE ENGINE IS QUITE LOW. WE RECOMMEND ADDITIONAL INSPECTIONS ARE WARRANTED FOR THIS OPERATOR/ENVIRONMENT.
- [SDR CA110106011](https://openairdocs.org/sdr/CA110106011.md): Smoke Detector · failed · Jan 5, 2011 · Agusta AW139 · Smoke Detection
  > DURING UNSCHEDULED MAINTENANCE, THE SMOKE DETECTOR HAD TO BE DISCONNECTED FOR ACCESS. AN HIGHER THAN NORMAL FORCE WAS REQUIRED TO DISCONNECT THE CONNECTOR FROM THE UNIT. ONCE THE CONNECTOR WAS REMOVED, PIN NR 7 ON SMOKE DETECTOR UNIT WAS NOTICED TO BE BENT 9
- [SDR CA110110006](https://openairdocs.org/sdr/CA110110006.md): Seal · worn · Jan 5, 2011 · Pilats PC1245 · Propeller Assembly
  > AFTER TAKEOFF, THE PILOT NOTICED OIL ON THE WINDSHIELD. HE RETURNED AND LANDED. MAINTENANCE FOUND THE PROP SHAFT OIL SEAL LEAKING, AND REPLACED IT WITH NEW.
- [SDR CA110117003](https://openairdocs.org/sdr/CA110117003.md): Actuator · broken · Jan 5, 2011 · Bombdr DHC8400 · Landing Gear Door Retract Section
  > MX WAS UNABLE TO OPEN RT MLG DOORS FOR SCHEDULED MX. FURTHER TROUBLESHOOTING REVEALED A BROKEN ALTERNATE RELEASE CAM ASSY, BENT CLEVIS, AND HALF OF A BRG OUTER RACE FROM THE DOOR LINKAGE OVER CTR ALTERNATE RELEASE ARM. RT ALTERNATE EXTENSION CAM MECHANISIM
- [SDR CA110208005](https://openairdocs.org/sdr/CA110208005.md): Vent · disconnected · Jan 5, 2011 · Turbine Engine Oil System
  > (CAN) PILOT INDUCED IFSD THERE WAS A PILOT INDUCED IFSD DUE TO LOP. THE A/C PERFORMED AN UNEVENTFUL LANDING. INSPECTION SHOWED SIGNIFICANT INTERNAL DAMAGE OF ENGINE`S HOT SECTION. NR 6, 7 BEARING VENT TUBE WAS DISCONNECTED FROM THE CASE AND HELD IN PLACE ONLY
- [SDR CA110112011](https://openairdocs.org/sdr/CA110112011.md): Actuator · inoperative · Jan 4, 2011 · Cessna 560XL · Flight Control System
  > WHEN FLAPS WERE SELECTED ON APPROACH, THE CREW RECEIVED A "STAB MIS COMP". THE HORIZONTAL STAB ACTUATOR WAS NOT ACTUATING TO MOVE THE HORIZONTAL STABILIZER FROM +1 TO -2 DEGREES WITH FLAPS SELECTED.
- [SDR CA110125006](https://openairdocs.org/sdr/CA110125006.md): Engine · failed · Jan 4, 2011 · Engine (Turbine/Turboprop)
  > (CAN) POWER LOSS THE PILOT REPORTED THAT NR 1 ENGINE CHIP LIGHT CAME ON ACCOMPANIED BY A LOUD UNUSUAL SOUND WHILE HOVERING AT 4 FT. DURING TAKE OFF FROM RAS SHOUKER BASE HELIPAD AND NR 1 ENGINE TORQUE DROPPED TO ZERO. ENGINE AND RGB TO BE REMOVED FOR FURTHER I
- [SDR 2011FA0000063](https://openairdocs.org/sdr/2011FA0000063.md): Turbine · coked · Jan 3, 2011 · N214MS · Eclips ECLIPSEEA500 · Turbine Section
  > ON 1/3/11, ACFT DEPARTED AIRPORT. ACFT DEVELOPED A PROBLEM WITH THE LT ENGINE TEMP RUNNING HIGH, FOLLOWED BY A "LT ENGINE EXCEEDANCE" CREW ALTERTING SYS MESSAGE. PILOT REDUCED POWER ON ENGINE HOPING TO REDUCE TEMP, TEMP CONTINUED TO CLIMB, PILOT DECIDED TO S
- [SDR CA110124017](https://openairdocs.org/sdr/CA110124017.md): Powerplant · failed · Jan 3, 2011 · Engine (Turbine/Turboprop)
  > INABILITY TO ACHIEVE THRUST DURING REPOSITIONING FLIGHT, ON DESCENT AT 37K THE PILOT HEARD RUMBLING NOISE FROM THE RENTAL ENGINE. POWER WAS REDUCED TO STOP THE REPORTED NOISE GOING DOWN TO 30K. PILOT REPORTED AN OVERTEMP AND ELECTED TO SHUTDOWN THE ENGINE. AC
- [SDR CA110106013](https://openairdocs.org/sdr/CA110106013.md): Apu · failed · Jan 1, 2011 · Bombdr DHC8400 · APU Core Engine
  > WHEN THE APU WAS STARTED BEFORE THE FIRST FLIGHT IT FAILED TO START, AND THERE WAS A "BIG BANG" HEARD (SIMILAR TO A SMALL EXPLOSION) AND SOME SMOKE CAME OUT OF THE TAIL SECTION. A SECOND ATTEMPT FAILED. AFTER THE LAST FLIGHT WHEN WE INSPECTED THE APU AREA, T
- [SDR CA110124013](https://openairdocs.org/sdr/CA110124013.md): Engine · stalled · Jan 1, 2011 · Engine (Turbine/Turboprop)
  > ABORTED T/O IFSD DURING EARLY T/O ROLL CLOSE TO FULL POWER, LOUD NOISES (SUSPECTED COMPRESSOR STALLS) WERE HEARD FROM 1 (OR BOTH) ENGINES. THE T/O WAS ABORTED. POST FLIGHT INSP FOUND NO DAMAGE ON THE ENGINES AND NO CAUSES WERE IDENTIFIED FOR THE NOISES. GROUN
- [SDR CA110105019](https://openairdocs.org/sdr/CA110105019.md): Windshield · cracked · Dec 31, 2010 · Raythn B300RAYTHEON · Flight Compartment Windows
  > IN CRUISE RT SIDE WINDOW OUTER PANE CRACKED. CREW CONTINUED TO DESTINATION (HOME BASE) AND LANDED NORMAL.
- [SDR CA110107004](https://openairdocs.org/sdr/CA110107004.md): Harness · failed · Dec 31, 2010 · Bombdr DHC8400 · Landing Gear System Wiring
  > AFTER GEAR SELECTED UP, ALL THREE UNSAFE LIGHTS REMAINED ILLUMINATED, GEAR DOOR LIGHTS DID NOT ILLUMINATE. FLIGHT ATTENDANT REPORTED GEAR REMAINED DOWN. ATB TO BASE. MAINTENANCE REPLACED THE NW CENTERING HARNESS, THEN FOUND NOSE WHEEL NOT CENTERING AFTER WO
- [SDR CA110124016](https://openairdocs.org/sdr/CA110124016.md): Pressure Switch · failed · Dec 30, 2010 · Engine Oil Indicating System
  > OIL PRESSURE WARNING/IFSD DURING FLIGHT, THE CREW REPORTED AN OIL PRESSURE WARNING AND ELECTED TO SHUTDOWN THE ENGINE. THE ACFT DIVERTED FROM THE INTENDED DESTINATION AND LANDED SAFELY. THE PROBLEM WAS TRACED BACK TO A FAULTY OIL PRESSURE SWITCH WHICH WILL B
- [SDR CA110125002](https://openairdocs.org/sdr/CA110125002.md): Control Unit · failed · Dec 26, 2010 · Fuel Controlling System
  > UNCONTROLLED ACCELERATION ENGINE RPM ESCAPED RT AFTER START UP. TORQUE EXCEEDANCE WAS TO 123PERCENT AND 1-2 SECONDS ( LIMIT IS 137 PERCENT AND 20 SECONDS). THE MFCU WILL BE SENT FOR INVESTIGATION.
- [SDR CA101230001](https://openairdocs.org/sdr/CA101230001.md): Unknown · odor · Dec 25, 2010 · Dhav DHC8301 · Air Distribution System
  > 160 NAUTICAL MILES NORTH, FLIGHT CREW REPORTED A MIST AND AN ACRID SMELL IN THE CABIN. FLIGHT WAS THEN DECLARED AN EMERGENCY AND IS DIVERTING. ENGINE INSTALL IN PROGRESS IAW SHEETS. ON ENGINE INSTALL CONNECTED SPRING STRUT TO ENGINE TORQUED AND SAFTIED. COM
- [SDR CA110103001](https://openairdocs.org/sdr/CA110103001.md): Buss Bar · arced · Dec 24, 2010 · Bombdr DHC8400 · Propeller/Propulsor System Wiring
  > PROP DEICE CAUTION LIGHT ILLUMINATED. WHEN RESET NR 1 GREEN ADVISORY ILLUMINATED, GOT DUAL AC GEN CAUTION LIGHTS. AC GENS SUCCESSFULLY RESET. MAINTENANCE FOUND NR 1 PROP BUSS BAR "ARCING" DAMAGE DUE TO CONTACT WITH MAGNETIC PICKUP (MPU). BACK PLATE REPLACE

Next page: https://openairdocs.org/engine/pratt-whitney-canada-pw610f-a/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 = 'PW610FA'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/pratt-whitney-canada-pw610f-a/reports

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