# Service difficulty reports: Pratt & Whitney Canada PW615F-A

A list on [Pratt & Whitney Canada PW615F-A](https://openairdocs.org/engine/pratt-whitney-canada-pw615f-a.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 73 reports

- [SDR O9IA20260730167](https://openairdocs.org/sdr/O9IA20260730167.md): Oil System · malfunctioned · Jul 30, 2026 · N171AA · Cessna 510 · Engine Oil Indicating System
  > RT ENG OIL PRESSURE DROPPED TO 0 ON APPROACH INTO HIO FROM PAE. PRESSURE JUMPED UP INTO GREEN & SPIKED INTO RED & STAYED THERE. ENG THEN SHUTDOWN INFLT ON APPROACH. PILOT DECLARED AN EMERGENCY & LANDED WITHOUT INCIDENT. MAINT CHKD OIL LEVEL ON ENGS & BOTH W
- [SDR 2026FA0000133](https://openairdocs.org/sdr/2026FA0000133.md): Pressure Switch · leaking · Feb 18, 2026 · N79SG · Cessna 510 · Aircraft Fuel Distribution System
  > REPEATED FAILURE OF FUEL PRESSURE SWITCH P/N: 9912033-2 CAUSING FUEL TO LEAK FROM THE WEEP HOLE OF THE SWITCH BODY. FUEL THEN LEAKS INTO THE COWLING. FAILURES INCLUDE SWITCH S/N'S: 13646, 13661, 13262 ALL FAILURES HAVE OCCURRED WITHIN A 12-MONTH PERIOD OF 01/2
- [SDR 2023FA0000284](https://openairdocs.org/sdr/2023FA0000284.md): Sensor · failed · Apr 20, 2023 · N510PX · Cessna 510 · Engine Oil Indicating System
  > LOSS OF OIL PRESSURE INDICATION ON LEFT ENGINE. ACTUAL PROBLEM WAS A BAD PRESSURE SENSOR. SINGLE POINT OF FAILURE. THERE IS NO BACK UP TO THIS INDICATION.
- [SDR 11FA2019070100001](https://openairdocs.org/sdr/11FA2019070100001.md): Engine · malfunctioned · May 23, 2019 · N820UT · Cessna 510 · Engine (Turbine/Turboprop)
  > ITT SPIKE NR 2 ENGINE EXCEEDED REDLINE. ENGINE AND FADEC REMOVED AND SENT TO PWC FOR TEARDOWN INSPECTION.
- [SDR CA190604007](https://openairdocs.org/sdr/CA190604007.md): Warning Message · illuminated · May 23, 2019 · Cessna 510 · Engine (Turbine/Turboprop)
  > (CAN) PILOT REPORTED ITT SPIKE INTO THE YELLOW RANGE DURING TAKE-OFF ON THE RIGHT HAND ENGINE. THE TAKE-OFF WAS ABORTED BEFORE AIRCRAFT LEAVE THE GROUND AND RETURNED TO BACK RAMP FOR TROUBLESHOOTING.
- [SDR GQRA2019052400001](https://openairdocs.org/sdr/GQRA2019052400001.md): Engine · overtemp · May 20, 2019 · N452AR · Emb EMB500 · Engine (Turbine/Turboprop)
  > AIRCRAFT WAS ENROUTE DTN -ABQ. IN LEVEL FLIGHT AT FL400 CREW EXPERIENCED A LOUD VIBRATION IN ONE OF THE ENGINES THAT LASTED FOR APPROXIMATELY 10-20 SECONDS. CREW COULD NOT TELL WHICH ENGINE. IT HAPPENED AGAIN WITH A CORRESPONDING RED ITT GAUGE INDICATING 881 D
- [SDR 11FA2019070100002](https://openairdocs.org/sdr/11FA2019070100002.md): Unknown · malfunctioned · May 20, 2019 · N820UT · Cessna 510 · Engine EGT/TIT Indicating System
  > ITT SPIKE IN THE CLIMB FOR UNKNOWN REASONS. MANUALLY ADJUSTED POWER SETTING AND NORMAL OPERATIONS RESUMED.
- [SDR CA190524003](https://openairdocs.org/sdr/CA190524003.md): Housing · damaged · May 13, 2019 · Cessna 510 · Turbine Engine Compressor Section
  > (CAN) DURING TAKE-OFF ROLL CREW NOTICED ENGINE HIGH ITT AT RED BAND. AIRCRAFT RETURNED TO ITS ORIGINAL DEPARTURE AND LANDED UNEVENTFULLY. TROUBLESHOOTING IS ONGOING. (TC# 20190524003)
- [SDR CNQ4N510BK052017](https://openairdocs.org/sdr/CNQ4N510BK052017.md): Precooler · ruptured · May 15, 2017 · N510BK · Cessna 510 · Pneumatic Distribution System
  > AFTER TAKE OFF, OPERATOR REPORTED THE LEFT ENGINE DUCT OVERHEAT ANNUNCIATOR ILLUMINATED. THE OPERATOR REDUCED THE ENGINE POWER SETTINGS, LANDED BACK TO DEPARTURE. INVESTIGATION REVEALED THE LEFT ENGINE BLEED AIR PRE-COOLER HAD RUPTURED CAUSING THE DUCT OVER
- [SDR 2016FA0000244](https://openairdocs.org/sdr/2016FA0000244.md): Regulator · leaking · Mar 15, 2016 · N397CM · Cessna 510 · Crew Oxygen System
  > OXYGEN BOTTLE RECEIVED FROM REPAIR SHOP FOR FITMENT TO AIRCRAFT. ON FITMENT OF OXYGEN BOTTLE ASSY DURING 30 MINUTE LEAK TEST IAW MM, REV 12, 35-10-00, REV 8, 6, B 11A. LEAK DETECTED FROM PRESSURE REGULATOR ON/OFF VALVE. PART REMOVED FROM AIRCRAFT AND RETURN
- [SDR CA160216013](https://openairdocs.org/sdr/CA160216013.md): Oil System · low pressure · Feb 12, 2016 · Cessna 510 · Turbine Engine Oil System
  > (CAN) THE FLIGHT CREW OBSERVED A RED INDICATION ON THE NR 2 ENGINE OIL PRESSURE DISPLAY. THE FLIGHT CREW ACTIONED THE ABNORMAL PROCEDURES CHECKLIST, DETERMINED IT WAS A FAULTY INDICATION AND CONTINUED WITH THE DESCENT. WHILE ON LEFT BASE TO RUNWAY 35, THE MAST
- [SDR CA160204007](https://openairdocs.org/sdr/CA160204007.md): Transducer · failed · Feb 2, 2016 · Cessna 510 · Engine Oil Indicating System
  > (CAN) TRANSDUCERS SEEM TO HAVE A SHORT LIFE LIMIT AND GIVE IRRATIC, FALSE INDICATIONS WHEN THEY FAIL IN FLIGHT.
- [SDR CA151030010](https://openairdocs.org/sdr/CA151030010.md): Oil System · pressure loss · Oct 25, 2015 · Cessna 510 · Engine Oil Indicating System
  > (CAN) DURING TAXI BEFORE TAKEOFF FOR A TEST FLIGHT AFTER MAINTENANCE, THE PILOT RECEIVED A NR 2 ENGINE OIL PRESSURE LOW WARNING. TAKEOFF WAS ABORTED AND THE ACFT TAXIED BACK TO SERVICE CENTER. TROUBLESHOOTING IS ON-GOING.
- [SDR ON0A2015FA0000542](https://openairdocs.org/sdr/ON0A2015FA0000542.md): Starter Gen · failed · Oct 9, 2015 · N30NF · Cessna 510 · Starter-Generator
  > LEFT ENGINE GENERATOR FAILED IN FLIGHT, CREW RECEIVED GENERATOR FAIL CAS AND FELT VIBRATION THROUGH THE AIRFRAME.
- [SDR CA150925003](https://openairdocs.org/sdr/CA150925003.md): Engine · power loss · Sep 4, 2015 · Cessna 510 · Engine (Turbine/Turboprop)
  > (CAN) THE PILOT REPORTED THAT AFTER NOTICING AN INCREASING IN RAT INDICATION AND A DECREASING IN THE RATE OF CLIMB,BOTH ENGINES ROLLED BACK. "NORMALLY THE ENGINE ROLL BACK IS PREDATED BY A T2 HEATER FAIL L/R. BUT WAS NOT THE CASE. SINCE THE RATE OF CLIMB WAS V
- [SDR CA150911006](https://openairdocs.org/sdr/CA150911006.md): Engine · power loss · Sep 3, 2015 · Cessna 510 · Engine (Turbine/Turboprop)
  > (CAN) THE LT ENGINE HAD A UNCOMMANDED POWER ROLL BACK. NO T2 HTR CAS MESSAGE APPEARED. IT OCCURRED DURING CLIMB IN IMC, SUPER MOIST, LIGHT ICE, AROUND FL270.
- [SDR 2015FA0000325](https://openairdocs.org/sdr/2015FA0000325.md): Circuit Board · failed · Jul 16, 2015 · N511TP · Cessna 510 · Landing Gear System Wiring
  > PILOT FOR ACFT INFORMED THE TOWER THAT HE HAD NO POSITIVE GEAR DOWN AND LOCKED INDICATION, THE TOWER DECLARED AN EMEMERGENCY LANDING. PILOT SELECTED GEAR DOWN AND HAD NO GREEN LIGHT INDICATION FOR DOWN AND LOCKED. HE BLEW GEAR AND STILL HAD NO LIGHT DOWN AND
- [SDR CA150205007](https://openairdocs.org/sdr/CA150205007.md): Carbon Seal · leaking · Jan 26, 2015 · Cessna 510 · Turbine Engine Oil System
  > (CAN) DURING FLIGHT, THE OIL PRESSURE DROPPED TO THE LOW SIDE, AND THE PILOT REDUCED POWER TO IDLE, BUT DID NOT SHUT IT DOWN. THE TROUBLESHOOTING REVEALED THE SIGHT GLASS WAS EMPTY UPON CHECKING, AND THE OIL FILTER BYPASS INDICATOR WAS POPPED. THE CARBON PARTI
- [SDR CA150205003](https://openairdocs.org/sdr/CA150205003.md): Engine · malfunctioned · Jan 22, 2015 · Cessna 510 · Engine (Turbine/Turboprop)
  > (CAN) PILOT REPORTED THAT DURING THE DESCENT, WHEN PASSING FL250, THEY HEARD A NOISE ON THE ENGINE NR 2, WHILE BOTH ENGINES WHERE BELOW CRUISE POWER. THE AIRCRAFT DIVERTED. DURING THE TROUBLESHOOTING, BOTH ENGINE SPOOLS (LOW AND HIGH POWER) ROTATED NORMALLY. A
- [SDR CA141202020](https://openairdocs.org/sdr/CA141202020.md): Oil System · empty · Nov 20, 2014 · Cessna 510 · Turbine Engine Oil System
  > (CAN) DURING FLIGHT THE PILOT NOTICED OIL PRESSURE FLUCTUATING. THE PILOT ELECTED TO START DESCENT AND THE PRESSURE CONTINUED DECREASING INTO THE RED BAND. THE PILOT THEN SHUT THE ENGINE DOWN, AND DECLARED AN EMERGENCY WHERE HE PERFORMED AN UNEVENTFUL SINGLE E
- [SDR CA141202014](https://openairdocs.org/sdr/CA141202014.md): Warning Message · illuminated · Nov 15, 2014 · Cessna 510 · Engine Indicating System
  > (CAN) LEFT ENGINE CONTROL AMBER MESSAGE ILLUMINATED IN THE DECENT. THROTTLE RETARDED TO IDLE BUT ENGINE REMAINED AT 55% UNTIL PASSING THROUGH 4,000FT. WARNING REMAINED UNTIL POWER CYCLED ON THE GROUND. THE AIRCRAFT IS AWAITING DOWNLOAD ANALYSIS.
- [SDR 2014FA0000587](https://openairdocs.org/sdr/2014FA0000587.md): Engine · malfunctioned · Oct 3, 2014 · N510BK · Cessna 510 · Engine (Turbine/Turboprop)
  > RT ENGINE SHUTDOWN AT FL370 FOR AN HOUR AT CRUISE WITH NO ISSUE. STARTED TO CLIMB, AND ABOUT 2-3 MINUTES LATER AT ABOUT 39,500" HAD THE RT ENGINE OIL TEMPERATURE CLIMB HIGH, REDUCED POWER. IT KEPT CLIMBING AFTER STABILIZING FOR A SHORT BIT EACH TIME THE P
- [SDR CA140915014](https://openairdocs.org/sdr/CA140915014.md): Starter Gen · failed · Sep 6, 2014 · Cessna 510 · Starter-Generator
  > (CAN) NR 2 ENGINE STARTER GENERATOR FAILED DURING FLIGHT AND WAS CASUING ENGINE VIBRATION. UPON INSPECTION FOLLOWING REMOVAL THE STARTER GENERATOR WAS FOUND TO HAVE INTERNAL BEARING FAILURE CAUSING THE VIBRATION.
- [SDR CA140908011](https://openairdocs.org/sdr/CA140908011.md): Engine · vibration · Aug 27, 2014 · Engine (Turbine/Turboprop)
  > (CAN) DURING REVENUE FLIGHT, AT FL400, THE PILOT ELECTED TO SHUTDOWN THE LT ENGINE DUE TO HIGH VIBRATION. THE ACFT LANDED UNEVENTFULLY. THE INVESTIGATION IS ON-GOING.
- [SDR CA140630003](https://openairdocs.org/sdr/CA140630003.md): Engine · failed · Jun 13, 2014 · Cessna 510 · Engine (Turbine/Turboprop)
  > (CAN) THE PILOT HEARD A LOUD NOISE FOLLOWED BY ENGINE PARAMETERS GOING INTO THE RED BAND. UPON INITIATING ENGINE SHUTDOWN, HEARD ANOTHER LOUD NOISE FOLLOWED BY SMOKE IN THE COCKPIT. AN EMERGENCY WAS DECLARED AND AN UNEVENTFUL SINGLE ENGINE LANDING WAS ACCOMPL
- [SDR CA130408009](https://openairdocs.org/sdr/CA130408009.md): Wire · damaged · Apr 3, 2013 · Cessna 510 · Window System Wiring
  > (CAN) ON A RECENT TRIP, THE PILOT NOTED PRIOR TO TAKEOFF A CAS MESSAGE DISPLAYING LT WINDSHIELD HEAT FAILURE. ACFT RETURNED TO THE RAMP AND FURTHER INVESTIGATION WAS CARRIED OUT SUSPECTING A BAD WINDSHIELD HEAT CONTROLLER. PLANS WERE TO SWAP THE 2 CONTROLLER
- [SDR CA121105015](https://openairdocs.org/sdr/CA121105015.md): Engine · odor · Oct 23, 2012 · Cessna 510 · Turbine Engine Oil System
  > (CAN) FOLLOWING T/O, THE CREW REPORTED A STRONG BURNING SMELL FOLLOWED BY BLUE TINGED SMOKE. ENGINES INDICATIONS WERE FOUND NORMAL. THE PILOT REQUESTED A PRIORITY RETURN TO THE DEPARTURE AIRPORT AND THE A/C LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTIONS SHOW
- [SDR CA121022001](https://openairdocs.org/sdr/CA121022001.md): Engine · malfunctioned · Oct 5, 2012 · Engine (Turbine/Turboprop)
  > (CAN) PILOT REPORTED HEARING A LOUD BANG FROM THE LT ENGINE FOLLOWED BY OIL ODOR IN THE CABIN. PILOT ELECTED TO SHUTDOWN THE ENGINE DUE TO THE OIL ODOR. PILOT ALSO SAW A WARNING LIGHT FLASH BUT IS NOT CERTAIN IF IT WAS A CAUTION LIGHT OR THE FIRE WARNING LIGH
- [SDR 2012FA0000647](https://openairdocs.org/sdr/2012FA0000647.md): Duct · delaminated · Sep 26, 2012 · N949JB · Cessna 510 · Turbine Engine Bypass Section
  > AFT BYPASS DUCT WAS FOUND DELAMINATED DURING A SCHEDULED INSPECTION.
- [SDR 2012FA0000652](https://openairdocs.org/sdr/2012FA0000652.md): Ferrule · cracked · Sep 26, 2012 · N949JB · Cessna 510 · Trailing Edge Flap Control System
  > DURING A SCHEDULED INSPECTION, THE FERRULE ON THE RT FLAP FLEX SHAFT OUTER HOUSING WAS FOUND CRACKED. CRACK WAS ON THE END WHERE THE CABLE ATTACHES TO THE FLAP ACTUATOR.
- [SDR CA120903005](https://openairdocs.org/sdr/CA120903005.md): Engine · vibration · Aug 28, 2012 · Cessna 510 · Engine (Turbine/Turboprop)
  > (CAN) DURING FLIGHT, THE PILOT FELT SUDDEN HEAVY VIBRATIONS WITH A RISING ENGINE TEMPERATURE. THE ENGINE WAS SHUTDOWN AND SECURED BEFORE AN UNEVENTFUL SINGLE ENGINE LANDING WAS ACCOMPLISHED. POST FLIGHT INSPECTION FOUND SEIZED TURBINES. THE ENGINE WILL BE R
- [SDR CA120821003](https://openairdocs.org/sdr/CA120821003.md): Engine · vibration · Aug 12, 2012 · Cessna 510 · Engine (Turbine/Turboprop)
  > (CAN) APPROXIMATELY 30 MIN AFTER DEPARTURE, THE PILOT FELT A SMALL VIBRATION. 10 MINUTES LATER, THE FOLLOWING CAS MESSAGE WAS SEEN: GEN OFF L. AFTER ANOTHER 45 MIN, DURING APPROACH TO LFPB, OIL PRESSURE RAISED AND THEN DECREASED TO 0 PSI. ENGINE WAS SHUTDOWN
- [SDR CA120814003](https://openairdocs.org/sdr/CA120814003.md): Fuel Tank · fod · Aug 10, 2012 · Cessna 510 · Fuel Storage
  > (CAN) DURING SCHEDULED INSPECTION OF THE INTERNAL FUEL TANK A 24" BY 29" CLOTH RAG WAS DISCOVERED IN THE FUEL BAY COVERED BY ACCESS PANEL 147EB. THIS WAS THE FIRST TIME ACCESSING THIS AREA SINCE THE ACFT WAS BUILT IN 2009. ON A PREVIOUS FLIGHT A LOW FUEL PRE
- [SDR CA120814006](https://openairdocs.org/sdr/CA120814006.md): Pushrod · undertorqued · Aug 10, 2012 · Cessna 510 · Elevator Control System
  > (CAN) DURING THE 36 MONTH CHECK THE AREA OF THE ELEVATOR CONTROL SYS SECTOR AND HORN WAS ACCESSED FOR THE FIRST TIME SINCE THE ACFT WAS NEW AND IT WAS FOUND THE BOLTS WERE NOT TORQUED CORRECTLY AND THAT BOTH THE BOLTS COULD BE SLID BACK AND FORTH IN THE ROD AN
- [SDR CA120716003](https://openairdocs.org/sdr/CA120716003.md): Oil System · low pressure · Jul 2, 2012 · Cessna 510 · Engine Oil Indicating System
  > (CAN) 20 MINUTES INTO THE FLIGHT, NOISE HEARD FROM THE LT ENGINE AND MASTER WARNING WITH LOW OIL PRESSURE AND ITT EXCEEDING LIMITS OCCURRED. THE CREW REDUCED POWER TO IDLE, N1 AT 15 PERCENT, AND SHUTDOWN THE ENGINE AFTER 2 MINUTES. A SINGLE ENGINE LANDING WA
- [SDR CNQR2012052286445](https://openairdocs.org/sdr/CNQR2012052286445.md): Gearbox · cracked · May 22, 2012 · N1EL · Cessna 510 · Accessory Gearboxes
  > A CRACK WAS DISCOVERED IN THE ENGINE ACCESSORY GEARBOX NEAR THE STARTER/GENERATOR MOUNTING FLANGE. DURING THE AIRCRAFT`S LAST FLIGHT IT EXPERIENCED A GENERATOR BEARING FAILURE. DURING THE POST RUNS, AFTER PART REPLACEMENT AN OIL LEAK WAS DISCOVERED COMING FRO
- [SDR A8JA201204100013](https://openairdocs.org/sdr/A8JA201204100013.md): Transmitter · failed · Apr 10, 2012 · N510GJ · Cessna 510 · Engine Oil Indicating System
  > WHILE PERFORMING A CHECK FLIGHT AFTER MX, PILOT AND MECHANIC NOTICED AN ERRATIC OIL PRESSURE INDICATION ON THE NR 2 ENGINE. OIL PRESSURE WOULD GO FROM ZERO TO NORMAL, WITH RAPID FLUCTUATIONS. NO OTHER ENGINE PARAMETERS WERE AFFECTED. PILOT ELECTED TO RETURN
- [SDR A8JA201204060012](https://openairdocs.org/sdr/A8JA201204060012.md): Connector · damaged · Apr 6, 2012 · N510CJ · Cessna 510 · Engine Oil System Wiring
  > ACFT DEPARTED, IN CRUISE AT FL360, CREW NOTICED "OIL PRESS LO L" CAS MESSAGE ON THE CENTER MFD. THE CREW REFERRED TO THE ACFT CHECKLIST, WHICH INSTRUCTED THE CREW TO PERFORM A PRECAUTIONARY SHUTDOWN TO AVOID DAMAGE TO THE ENGINE. THE CREW PERFORMED THE RECO
- [SDR CA120409001](https://openairdocs.org/sdr/CA120409001.md): Bearing · failed · Apr 5, 2012 · Cessna 510 · Turbine Section
  > (CAN) IN LEVEL FLIGHT AT FL 360. LEFT ENGINE BEGAN MAKING POPPING SOUNDS ACCOMPANIED BY METALLIC CLUNKING/GRINDING NOISES. POWER LOSS AND NOTICEABLE ODOR AND MINOR VISIBLE SMOKE WAS NOTED, ALONG WITH IMMEDIATE MASTER WARNING ANNUNCIATOR LT. LT ENGINE INTERN
- [SDR CA120411003](https://openairdocs.org/sdr/CA120411003.md): Engine · making metal · Apr 4, 2012 · Cessna 510 · Engine (Turbine/Turboprop)
  > (CAN) WHILE CRUISING AT 36,000 FT, THE PILOT HEARD A LOUD NOISE FROM THE LT ENGINE. SHORTLY AFTER, ITT WAS INCREASING AND THE ENGINE WAS LOSING POWER. THE PILOT ELECTED TO SHUTDOWN THE ENGINE AND MADE AN UNEVENTFUL SINGLE ENGINE LANDING. POST-FLIGHT INSPECTI
- [SDR CA120228011](https://openairdocs.org/sdr/CA120228011.md): Transducer · failed · Feb 24, 2012 · Cessna 510 · Engine Oil Indicating System
  > (CAN) RIGHT ENGINE OIL PRESSURE INDICATION WENT TO PSI 12 MINUTES INTO FLIGHT. ENGINE WAS SHUTDOWN AND ACFT LANDED WITHOUT INCIDENT. OIL PRESSURE TRANSDUCER WAS PRESSURE TESTED TO 80 PSI AND TRANSDUCER SUBJECTED TO VIBRATION. WIRING WAS CHECKED. ALL INDICAT
- [SDR CA120213015](https://openairdocs.org/sdr/CA120213015.md): Oil System · high pressure · Feb 8, 2012 · Cessna 510 · Engine Oil Indicating System
  > (CAN) THE PILOT SAW INCREASING OIL PRESSURE ON ONE ENGINE. THE PRESSURE WENT INTO THE AMBER AND THEN INTO THE RED. THE THROTTLE WAS PULLED BACK TO IDLE AND THE OIL PRESSURE WENT INTO THE GREEN. THE OIL PRESSURE DROPPED AGAIN INTO THE AMBER AND THEN RED. TH
- [SDR CA120213013](https://openairdocs.org/sdr/CA120213013.md): Bleed Valve · out of rig · Jan 9, 2012 · Compressor Bleed Valve
  > (CAN) AS THE TLA WAS REDUCED TO INITIATE DESCENT FROM AN ALTITUDE OF APPROXIMATELY 39,000 FT, A POPPING NOISE WAS HEARD, FOLLOWED BY A FLAMEOUT, ENGINE FAIL MESSAGE, WHICH IMMEDIATELY WAS RECOVERED BY THE AUTO-RELIGHT CAPABILITY. ACFT HAS BEEN RETURNED TO SE
- [SDR CA110928006](https://openairdocs.org/sdr/CA110928006.md): Engine · power loss · Sep 13, 2011 · Engine (Turbine/Turboprop)
  > (CAN) DURING LEVEL CRUISE FLIGHT AT FL370, THE RT ENGINE POWER ROLLED BACK AND SHUTDOWN. IT WAS NOT SUDDEN, AND THE TIMING WAS SIMILAR TO A NORMAL SHUTDOWN. THE PILOT DID NOT NOTICE ANY VIBRATIONS OR NOISE. THERE WERE NO CAS MESSAGES BEFORE THE SHUTDOWN. T
- [SDR CA110810002](https://openairdocs.org/sdr/CA110810002.md): Transmitter · faulty · Aug 4, 2011 · Cessna 510 · Engine Oil Pressure
  > IFSD, CLIMBING THROUGH 14,000 FT THE PILOT NOTED THE RT ENGINE OIL PRESSURE DROPPING LOWER INTO THE AMBER, THEN RED ZONE. THE LOW OIL PRESS R CAS MESSAGE CAME ON AND PILOT SHUT DOWN THE ENGINE AND LANDED SAFELY. THE OIL PRESSURE TRANSMITTER WAS BENCH CHECKED A
- [SDR CA110602008](https://openairdocs.org/sdr/CA110602008.md): Controller · failed · May 31, 2011 · Cessna 510 · Cabin Pressure Controller
  > THE CREW REPORTED THAT AFTER TAKEOFF AND DURING CLIMB THAT THE ACFT WOULD NOT PRESSURIZE. THE ACFT RETURNED TO BASE WHERE MX INVESTIGATED THE PROBLEM. IT WAS FOUND THAT THE PRESSURIZATION CONTROLLER HAD FAILED. THE PART WAS CHANGED WITH A SERVICEABLE REPAIR
- [SDR CA110616007](https://openairdocs.org/sdr/CA110616007.md): Manifold · leaking · May 25, 2011 · Cessna 510 · Engine Fuel Distribution
  > (CAN) THE ENGINE EXHIBITED A LOSS OF PERFORMANCE MARGIN AND A BORESCOPE INSPECTION OF THE HOT SECTION WAS CARRIED OUT. THE INTERNAL FUEL MANIFOLD WAS DETERMINED TO BE LEAKING WITH ASSOCIATED DAMAGE, BURNING, OF THE MANIFOLD OUTER SHIELD AND THE COMBUSTION LIN
- [SDR A8JA20110504001](https://openairdocs.org/sdr/A8JA20110504001.md): Connector · dirty · May 4, 2011 · N510CJ · Cessna 510 · Fuel System Wiring
  > ACFT DEPARTED. WHILE CLIMBING THROUGH, CREW NOTED AN AMBER CAS MESSAGE OF "RT FUEL BOOST". THIS INDICATES A LOW FUEL PRESSURE DETECTION AND ALERTS THE CREW THAT THE BOOST PUMP WAS AUTOMATICALLY ACTIVATED. THE CREW PERFORMED THE ACTIONS FROM THE EMERGENCY CH
- [SDR CA110427002](https://openairdocs.org/sdr/CA110427002.md): Engine · shutdown · Apr 7, 2011 · Engine (Turbine/Turboprop)
  > (CAN) UNCOMMANDED SHUT DOWN DURING FLIGHT, AN UNCOMMANDED SHUTDOWN OF THE ENGINE OCCURRED. THE FLIGHT WAS DIVERTED AND AN UNEVENTFUL SINGLE ENGINE LANDING WAS PERFORMED. NO OTHER INFO IS AVAILABLE AT THIS TIME HOWEVER PREPARATIONS ARE BEING MADE TO REMOVE THE
- [SDR CA110316007](https://openairdocs.org/sdr/CA110316007.md): Bolt · defective · Mar 16, 2011 · Cessna 510 · Landing Gear Brake System
  > (CAN) DURING MA INSPECTION FOUND PILOT & COPILOT BRAKE ROD LINK BOLT CHAFING COCKPIT FLOORBOARD MFG ADMITTED TO A PN CHANGE DURING PRODUCTION TO SPEED UP INSTALLATION. RECEIVED AUTHORIZATION TO USE THE ORIGINAL PN VIA EMAIL. NO MENTION WAS MADE OF ANY KIND O

Next page: https://openairdocs.org/engine/pratt-whitney-canada-pw615f-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 = 'PW615FA'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/pratt-whitney-canada-pw615f-a/reports

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