# Pratt & Whitney Canada PW119C

- Type: Engine model (FAA registry)
- Registry code: 52163
- Manufacturer (registry): P&W CANADA
- Model: PW119C
- Engine type: Turbo-prop
- Power: 1,851 hp
- Data sheet: [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs)
- Holder: Pratt & Whitney Canada Corp.
- Installed in: 20 registered aircraft
- Page: https://openairdocs.org/engine/pratt-whitney-canada-pw119c

Model codes come from the FAA registry's reference file.

## ADs that may apply (OpenAirDocs)

Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2013-15-08](https://openairdocs.org/ad/2013-15-08): First-stage PT blades · Pratt & Whitney Canada PW118A, PW118B, PW119B and 15 more. Effective Sep 17, 2013
- [AD 2012-26-08](https://openairdocs.org/ad/2012-26-08): Propeller shafts · Pratt & Whitney Canada PW118, PW118A, PW118B and 20 more. Effective Feb 15, 2013
- [AD 2006-19-06](https://openairdocs.org/ad/2006-19-06): Propeller shaft · Pratt & Whitney Canada PW118, PW118A, PW118B and 14 more. Effective Sep 29, 2006
- [AD 2003-16-04](https://openairdocs.org/ad/2003-16-04): Fuel heaters · Pratt & Whitney Canada PW118, PW118A, PW118B and 19 more. Effective Sep 10, 2003
- [AD 98-14-02](https://openairdocs.org/ad/98-14-02): Fuel Manifold Transfer Tubes · Pratt & Whitney Canada PW118, PW118A, PW118B and 17 more. Effective Aug 31, 1998
- [AD 97-17-05](https://openairdocs.org/ad/97-17-05): Gas Generator Case Drain Ports · Pratt & Whitney Canada PW118, PW118A, PW118B and 17 more. Effective Sep 9, 1997

Historical (superseded or no longer in force):

- [AD 2012-11-14](https://openairdocs.org/ad/2012-11-14) (historical): Propeller shafts · Pratt & Whitney Canada PW118, PW118A, PW118B and 20 more. Effective Jul 20, 2012

## Registered aircraft (20)

- [N250BG](https://openairdocs.org/aircraft/N250BG): [Kilburn Brian](https://openairdocs.org/faa-owner/KILBURN%20BRIAN), [Parker, CO](https://openairdocs.org/faa-place/CO/Parker), built 1994, S/N 3025
- [N307EF](https://openairdocs.org/aircraft/N307EF): [U S Air Force Special Operations Command](https://openairdocs.org/faa-owner/U%20S%20AIR%20FORCE%20SPECIAL%20OPERATIONS%20COMMAND), [Hurlburt Field, FL](https://openairdocs.org/faa-place/FL/Hurlburt%20Field), built 1998, S/N 3097
- [N340LS](https://openairdocs.org/aircraft/N340LS): [US Air Force Special Operations Command](https://openairdocs.org/faa-owner/US%20AIR%20FORCE%20SPECIAL%20OPERATIONS%20COMMAND), [Hurlburt Field, FL](https://openairdocs.org/faa-place/FL/Hurlburt%20Field), built 1995, S/N 3040
- [N347EF](https://openairdocs.org/aircraft/N347EF): [U S Air Force Special Operations Command](https://openairdocs.org/faa-owner/U%20S%20AIR%20FORCE%20SPECIAL%20OPERATIONS%20COMMAND), [Hurlburt Field, FL](https://openairdocs.org/faa-place/FL/Hurlburt%20Field), built 1995, S/N 3047
- [N355EF](https://openairdocs.org/aircraft/N355EF): [U S Air Force Special Operations Command](https://openairdocs.org/faa-owner/U%20S%20AIR%20FORCE%20SPECIAL%20OPERATIONS%20COMMAND), [Hurlburt Field, FL](https://openairdocs.org/faa-place/FL/Hurlburt%20Field), built 1995, S/N 3050
- [N360EF](https://openairdocs.org/aircraft/N360EF): [US Airforce Special Operations Command](https://openairdocs.org/faa-owner/US%20AIRFORCE%20SPECIAL%20OPERATIONS%20COMMAND), [Hurlburt Field, FL](https://openairdocs.org/faa-place/FL/Hurlburt%20Field), built 1995, S/N 3060
- [N385EF](https://openairdocs.org/aircraft/N385EF): [U S Air Force Special Operations Command](https://openairdocs.org/faa-owner/U%20S%20AIR%20FORCE%20SPECIAL%20OPERATIONS%20COMMAND), [Hurlburt Field, FL](https://openairdocs.org/faa-place/FL/Hurlburt%20Field), built 1997, S/N 3085
- [N391EF](https://openairdocs.org/aircraft/N391EF): [U S Air Force Special Operations Command](https://openairdocs.org/faa-owner/U%20S%20AIR%20FORCE%20SPECIAL%20OPERATIONS%20COMMAND), [Hurlburt Field, FL](https://openairdocs.org/faa-place/FL/Hurlburt%20Field), built 1997, S/N 3091
- [N524AW](https://openairdocs.org/aircraft/N524AW): [US Air Force Special Operations Command](https://openairdocs.org/faa-owner/US%20AIR%20FORCE%20SPECIAL%20OPERATIONS%20COMMAND), [Hurlburt Field, FL](https://openairdocs.org/faa-place/FL/Hurlburt%20Field), built 1994, S/N 3020
- [N525EF](https://openairdocs.org/aircraft/N525EF): [U S Air Force Special Operations Command](https://openairdocs.org/faa-owner/U%20S%20AIR%20FORCE%20SPECIAL%20OPERATIONS%20COMMAND), [Hurlburt Field, FL](https://openairdocs.org/faa-place/FL/Hurlburt%20Field), built 1999, S/N 3106
- [N545EF](https://openairdocs.org/aircraft/N545EF): [US Air Force Special Operations Command](https://openairdocs.org/faa-owner/US%20AIR%20FORCE%20SPECIAL%20OPERATIONS%20COMMAND), [Hurlburt Field, FL](https://openairdocs.org/faa-place/FL/Hurlburt%20Field), built 1997, S/N 3093
- [N565EF](https://openairdocs.org/aircraft/N565EF): [US Air Force Special Operations Command](https://openairdocs.org/faa-owner/US%20AIR%20FORCE%20SPECIAL%20OPERATIONS%20COMMAND), [Hurlburt Field, FL](https://openairdocs.org/faa-place/FL/Hurlburt%20Field), built 1998, S/N 3068
- [N570EF](https://openairdocs.org/aircraft/N570EF): [Prattville Turbine Engines LLC](https://openairdocs.org/faa-owner/PRATTVILLE%20TURBINE%20ENGINES%20LLC), [Prattville, AL](https://openairdocs.org/faa-place/AL/Prattville), built 1995, S/N 3058
- [N577EF](https://openairdocs.org/aircraft/N577EF): [U S Air Force Special Operations Command](https://openairdocs.org/faa-owner/U%20S%20AIR%20FORCE%20SPECIAL%20OPERATIONS%20COMMAND), [Hurlburt Field, FL](https://openairdocs.org/faa-place/FL/Hurlburt%20Field), built 1997, S/N 3077
- [N645HM](https://openairdocs.org/aircraft/N645HM): [645th Aeronautical Engineering Group (Aesg)](https://openairdocs.org/faa-owner/645TH%20AERONAUTICAL%20ENGINEERING%20GROUP%20(AESG)), [Wright Pat, OH](https://openairdocs.org/faa-place/OH/Wright%20Pat), built 1994, S/N 3013
- [N907EF](https://openairdocs.org/aircraft/N907EF): [US Air Force Special Operations Command](https://openairdocs.org/faa-owner/US%20AIR%20FORCE%20SPECIAL%20OPERATIONS%20COMMAND), [Hurlburt Field, FL](https://openairdocs.org/faa-place/FL/Hurlburt%20Field), built 1998, S/N 3104
- [N929EF](https://openairdocs.org/aircraft/N929EF): [US Air Force Special Operations Command](https://openairdocs.org/faa-owner/US%20AIR%20FORCE%20SPECIAL%20OPERATIONS%20COMMAND), [Hurlburt Field, FL](https://openairdocs.org/faa-place/FL/Hurlburt%20Field), built 1994, S/N 3026
- [N941EF](https://openairdocs.org/aircraft/N941EF): [US Air Force Special Operations Command](https://openairdocs.org/faa-owner/US%20AIR%20FORCE%20SPECIAL%20OPERATIONS%20COMMAND), [Hurlburt Field, FL](https://openairdocs.org/faa-place/FL/Hurlburt%20Field), built 1994, S/N 3016
- [N953EF](https://openairdocs.org/aircraft/N953EF): [US Air Force Special Operations Command](https://openairdocs.org/faa-owner/US%20AIR%20FORCE%20SPECIAL%20OPERATIONS%20COMMAND), [Hurlburt Field, FL](https://openairdocs.org/faa-place/FL/Hurlburt%20Field), built 1995, S/N 3075
- [N975EF](https://openairdocs.org/aircraft/N975EF): [U S Air Force Special Operations Command](https://openairdocs.org/faa-owner/U%20S%20AIR%20FORCE%20SPECIAL%20OPERATIONS%20COMMAND), [Hurlburt Field, FL](https://openairdocs.org/faa-place/FL/Hurlburt%20Field), built 1995, S/N 3031

## NTSB investigations (2)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA12WA040](https://openairdocs.org/ntsb/DCA12WA040), Feb 20, 2012: Dornier 328 (N953EF), Reykjavik, Iceland, incident, minor damage
- [NTSB SEA96IA074](https://openairdocs.org/ntsb/SEA96IA074), Mar 31, 1996: Dornier DO 328-100 (N334PH), Eugene, OR, incident, minor damage. Probable cause: delamination of the wing de-icing boot, due to the boot reaching its life limit.

## FAA accident and incident reports (3)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20000911029249I](https://openairdocs.org/incident/20000911029249I), Sep 11, 2000: Dorner DO328100 (N340LS), Chicago, IL. (-23)While holding and waiting for take-off clearance at the 27L run up pad, a fire warning (later confirmed false) was indicated in the #2 engine. The warning…
- [Incident 19960331044229I](https://openairdocs.org/incident/19960331044229I), Mar 31, 1996: Dorner DO328100 (N334PH), Eugene, OR, Minor damage. (-5)The flight crew reported that as the airplane was climbing between 14,000 feet and 16,000 feet in light icing conditions, they felt a moderate shudder. The…
- [Incident 19951214045299I](https://openairdocs.org/incident/19951214045299I), Dec 14, 1995: Dorner DO328100 (N334PH), Seattle, WA, Minor damage. Lightning strike during approach. Damaged left wing tip. Nav light assembly missing. Burn marks on rivets.

## Service difficulty reports (49)

As reported by operators and repair stations, by the model named in the report.

- [SDR 2016FA0000002](https://openairdocs.org/sdr/2016FA0000002), Dec 30, 2015: CONTROL WHEEL. CRACKED. AFTER INITIAL CLIMB THE CO-PILOT ATTEMPTED TO LOWER THE NOSE OF THE ACFT FOR CRUISE CLIMB. AS SOON AS FORWARD FORCE WAS APPLIED TO THE CONTROL WHEEL THE RT HORN
- [SDR J8UR2015FA0000515](https://openairdocs.org/sdr/J8UR2015FA0000515), Oct 28, 2015: ACTUATOR. ACTIVATED. AIRCRAFT STICK PUSHER FAILED IN THE RETRACTED POSITION, ELEVATORS BEING HELD IN FULL NOSE DOWN DEFLECTION, AFTER BEING TESTED BY THE AIRCREW ON PREFLIGHT CHECKS
- [SDR 2014F00085](https://openairdocs.org/sdr/2014F00085), Apr 23, 2014: ALTERNATOR. CRACKED. WHILE CLIMBING THROUGH, FL 140, THE FLIGHT CREW REPORTED LOSS OF OIL PRESSURE ON THE RT ENGINE. THEY IMMEDIATELY FEATHERED THEN SHUTDOWN THE ENGINE AND RETURNED
- [SDR CA121105006](https://openairdocs.org/sdr/CA121105006), Oct 26, 2012: ENGINE. MALFUNCTIONED. (CAN) ON START UP FOR A RE-POSITIONING FLIGHT, THE CAPTAIN WAS ADVISED BY GROUND HANDLERS OF A PROBLEM WITH THE LT ENGINE. THE ENGINE WAS SHUTDOWN AND INSPECTIO
- [SDR CA120815001](https://openairdocs.org/sdr/CA120815001), Aug 15, 2012: TURBINE. DAMAGED. (CAN) FRONT INLET CASE REPLACEMENT REPLACEMENT AND LATER DURING TEST CELL PERFORMANCE CHECKS, THE HOT SECTION HAD A MAJOR FAILURE.
- [SDR XV6A201109010013](https://openairdocs.org/sdr/XV6A201109010013), Sep 1, 2011: SHUTOFF VALVE. DEFECTIVE. BLEED SOV FAIL MSG. TIME ON UNIT NOT TRACKED.
- [SDR CA110330008](https://openairdocs.org/sdr/CA110330008), Mar 28, 2011: WHEEL. DAMAGED. (CAN) LT I/B MAIN WHEEL ASSY WAS REPLACED ON 28-MAR-11 DUE TO A VERY BAD LEAK. THIS MAIN WHEEL ASSYÏ¿½S TIRE PRESSURE WAS ADJUSTED TO THE CORRECT SETTING ON 25-
- [SDR CA110331013](https://openairdocs.org/sdr/CA110331013), Mar 24, 2011: COMPUTER. MALFUNCTIONED. (CAN) FLIGHT MANAGEMENT SYSTEM DATA BASE CAUSES THE FMS TO RESET ON APPROACH INTO AIRPORT. MFG ENGINEERS ARE WORKING ON A SOFTWARE FIX. FMS DATA BASE IS FUNCTIO
- [SDR CA100726017](https://openairdocs.org/sdr/CA100726017), Jul 23, 2010: STARTER GEN. FAILED. (CAN) LT STATER-GENERATOR FAILED PRIOR TO DESCENT. PILOTS FOLLOWED QRH CHECKLIST AND ATTEMPTED TO RESET IT. STARTER-GEN WOULD NOT RESET. REMAINDER OF THE FLIGHT
- [SDR XV6A2010042400006](https://openairdocs.org/sdr/XV6A2010042400006), Apr 24, 2010: LIGHT. INOPERATIVE. LT REAR EMERGENCY EXTERNAL EXIT LIGHT INOP.
- [SDR CA090806012](https://openairdocs.org/sdr/CA090806012), Aug 5, 2009: CONTROL UNIT. MALFUNCTIONED. FLIGHT CREW WAS TAXING OUT FOR ITS FIRST FLIGHT OF THE DAY WHEN THEY STARTED TO SMELL SMOKE IN THE COCKPIT. FA INFORMED THE CREW THAT THERE WAS ALSO SMOKE IT TH
- [SDR XV6A2009030600001](https://openairdocs.org/sdr/XV6A2009030600001), Mar 6, 2009: STRUCTURE. CRACKED. REPETITIVE EDDY CURRENT INSPECTION IAW RAS-328-57-3051 AND AD 2008-10-15.
- [SDR XV62008F00000](https://openairdocs.org/sdr/XV62008F00000), Jun 3, 2008: CONTROL CABLE. OBSTRUCTED. R/S POWER LEVER WOULD NOT GO INTO GROUND IDLE AFTER LANDING. FOUND HINGE FROM COCKPIT DOOR INTERFERING WITH CABLES/ PULLEYS TRAVEL AT RT AVIONICS AFT SIDE. REMO
- [SDR CA080207007](https://openairdocs.org/sdr/CA080207007), Jan 30, 2008: ELT. FAILED. (CAN) NUMEROUS UNCOMMANDED ELT ACTIVATIONS WITH ELT97. HAVE HAD ACTIVATIONS WITH THE AC INFLIGHT AND PARKED ON THE APRON. THE LASTEST WAS WITH ELT S/N-4584 ON J
- [SDR CA071121004](https://openairdocs.org/sdr/CA071121004), Nov 20, 2007: TURBINE. SEIZED. (CAN) AIRCRAFT DEVELOPED WHITE SMOKE IN CABIN WHILE TAXING FOR TAKEOFF. PILOTS NOTICED A CAS LT PACK FAIL LIGHT AND AN AFT LAV SMOKE DETECT CAS MESSAGE. AIRCRAF
- [SDR CA070725004](https://openairdocs.org/sdr/CA070725004), May 4, 2007: BOOT. LOOSE. (CAN) PILOTS REPORTED LT HORIZONTAL STAB. DE-ICER BOOT APPEARS LOOSE. MAINTENANCE INSPECTED THE DE-ICER BOOT AND FOUND THE BOOT HAD COME LOOSE FROM THE AIRCRAFT
- [SDR CA061107008](https://openairdocs.org/sdr/CA061107008), Nov 1, 2006: TRIM PANEL. SHORTED. (CAN) ENROUTE THE PILOT REPORTED A STRONG SMELL AND A FLASH OF LIGHT FROM CENTER CONSOLE AREA. THEY TURNED THE INTERIOR DOME LIGHT ON A CONFIRMED THAT A PLASTIC
- [SDR CA060906022](https://openairdocs.org/sdr/CA060906022), Sep 7, 2006: SEAL. LEAKING. (CAN) FOLLOWING TAKEOFF ENGINE OIL PRESSURE WAS SEEN TO FLUCTUATE AND DECAY TO ZERO. THE ENGINE WAS SHUTDOWN IN FLIGHT AND THE AIRCRAFT DIVERTED TO POINT OF DEP
- [SDR CA060831006](https://openairdocs.org/sdr/CA060831006), Jul 7, 2006: HYDRAULIC SYSTEM. FAILED. (CAN) AIRCRAFT READIED AND RT ENGINE START PARAMETERS NORMAL. RT CONDITION LEVER ADVANCED TO MIN. RT PROP DOES NOT UNFEATHER. RT CONDITION LEVER RETARDED TO FEA
- [SDR CA051223016](https://openairdocs.org/sdr/CA051223016), Nov 8, 2005: BOOT. SPLIT. CREW REPORTED A FAIL INDICATION FOR THE RT HORIZONTAL STAB DEICE BOOT. UPON INSPECTION BY MAINTENANCE THE BOOT HAD A 12 INCH SPLIT AND WAS REPLACED. NO IN FLIGH
- [SDR CA050901005](https://openairdocs.org/sdr/CA050901005), Aug 29, 2005: WIRE HARNESS. SHORTED. A/C DEPARTED YYC, DURING CLIMB-OUT LIGHTS FLICKERED LT GEN KICKED OFFLINE AND CREW LOST FMS SCREEN AND PROP SYNC CB POPPED. AS DEPARTING MX BASES, ELECTED TO RE
- [SDR A6WA200330006](https://openairdocs.org/sdr/A6WA200330006), Mar 9, 2003: OIL SYSTEM. OVERSERVICED. IN CRUISE AT 29,000 FEET, NR 2 ENGINE OIL PRESSURE FLUCTUATED BETWEEN 51-55. INSPECTED AND FOUND OIL OVERSERVICED. REMOVED ONE QUART OF OIL. INSPECTED AND CLEAN
- [SDR CA020606006](https://openairdocs.org/sdr/CA020606006), May 27, 2002: RESTRICTOR VALVE. FAILED. (CAN) LEFT OUTBOARD GROUND SPOILER FAILED TO DEPLOY ON LANDING. REPACED R/H RESTRICTOR VALVE P/N ZRV 87-3, S/N 90213160 AND CHECK VALVE P/N ZCV 157-1, S/N 80356
- [SDR A6WA200100069](https://openairdocs.org/sdr/A6WA200100069), Dec 13, 2001: BOOT. DEFECTIVE. RIGHT ENGINE HAD FLUCTUATING TORQUE INDICATION OF 10 - 25 PERCENT IN FLIGHT. MAINTENANCE FOUND INTAKE DE-ICE BOOT INFLATING AND CHOKING OFF ENGINE AIR INLET SUP
- [SDR A6WA200100066](https://openairdocs.org/sdr/A6WA200100066), Dec 7, 2001: OIL FILTER. OBSTRUCTED. LEFT ENGINE OIL PSI HIGH IN CRUISE. MAINTENANCE FOUND LT BYPASS FILTER CAS MESSAGE. REMOVED AND REPLACED NR 1 OIL FILTER AND SCAVENGE FILTERS.
- [SDR A6WA200100055](https://openairdocs.org/sdr/A6WA200100055), Sep 10, 2001: TRANSDUCER. FAULTY. RIGHT OIL PRESSURE HIGH. MAINTENANCE REMOVED AND REPLACED ENG PSI TRANSDUCER, MAIN ENGINE SCAVENGE FILTERS, OIL PUMP REGULATOR VALVE, AND NR 2 ENG KB HARNESS.
- [SDR A6WA200100028](https://openairdocs.org/sdr/A6WA200100028), Apr 27, 2001: GEARBOX. DEFECTIVE. DESCENT OUT OF FL240, LT ENGINE SURGED FROM 0 PERCENT TO 30 PERCENT TORQUE AND LT PROP IMMEDIATELY WENT TO 103 PERCENT NP. FLEW FOR 4 MINUTES WITH ENGINE AT FLT
- [SDR A6WA200000081](https://openairdocs.org/sdr/A6WA200000081), Dec 26, 2000: HMU. FAILED. LEFT ENGINE UNCOMMANDED POWER LOSS. POWER LEVER MOVEMENT HAS NO EFFECT. ENGINE SHUTDOWN. MAINTENANCE REMOVED AND REPLACED ENGINE HMU.
- [SDR A6WA200000069](https://openairdocs.org/sdr/A6WA200000069), Dec 12, 2000: IMPELLER. DAMAGED. LT ENGINE POWER LOSS AND STOPPAGE ON TAKE-OFF AFTER TAKE-OFF POWER WAS SET. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE. LP IMPELLER BLADE WAS FOUND DAMAGED CA
- [SDR 99ZZZX1140](https://openairdocs.org/sdr/99ZZZX1140), Feb 12, 1999: FUEL PUMP. FAILED. PILOT REPORTED ON 10 MILE FINAL AT 3,000 FEET MSL, THE LEFT ENGINE ROLLED BACK WITH THE POWER LEVER PULLED BACK TO FLIGHT IDLE. REPLACED LT HMU AND FUEL PUMP WI
- [SDR 99ZZZX1141](https://openairdocs.org/sdr/99ZZZX1141), Feb 12, 1999: HMU. FAILED. PILOT REPORTED ON 10 MILE FINAL AT 3,000 FEET MSL, THE LEFT ENGINE ROLLED BACK WITH THE POWER LEVER PULLED BACK TO FLIGHT IDLE. REPLACED LT HMU AND FUEL PUMP WI
- [SDR M8XA9800014](https://openairdocs.org/sdr/M8XA9800014), Jun 23, 1998: DAU. DEFECTIVE. SHORTLY AFTER TAKEOFF, THE FLIGHT CREW REPORTED A PROBLEM WITH THE NR 1 ALTERNATOR. THEY WERE ALERTED BY AC VOLT FAIL MESSAGE ON THE EICAS SCREEN. AIRCRAFT RETU
- [SDR M8XA9800013](https://openairdocs.org/sdr/M8XA9800013), Jun 22, 1998: WINDSHIELD. DEFECTIVE. AIRCRAFT RETURNED TO DEN BECAUSE OF A CRACKED RIGHT FRONT WINDSHIELD AS A RESULT OF ENCOUNTERING A HAIL STORM SHORTLY AFTER TAKEOFF. AIRCRAFT LANDED IN DEN WITH
- [SDR M8XA9800010](https://openairdocs.org/sdr/M8XA9800010), Jun 3, 1998: FLAP CONTROL. MALFUNCTIONED. SHORTLY AFTER TAKE-OFF, THE FLIGHT CREW REPORTED A FLAP CONTROL FAULT AND ASYMMETRY WARNING MESSAGE. AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT FURTHER I
- [SDR M8XA9800009](https://openairdocs.org/sdr/M8XA9800009), May 26, 1998: AIR DISTR. ODOR. CREW REPORTED RECEIVING AN EICAS. LEFT PACK FAIL MESSAGE DURING TAXI. PILOT CYCLED THE LT PACK SWITCH,THE FAIL MESSAGE THEN CLEARED ITSELF. FAIL MESSAGE ILLUMIN
- [SDR M8XA9800012](https://openairdocs.org/sdr/M8XA9800012), May 22, 1998: CONTROLLER. DEFECTIVE. SHORTLY AFTER T/O, THE FLIGHT CREW REPORTED A PROBLEM WITH THE AIRCRAFT PRESSURIZATION SYSTEM. AIRCRAFT WOULD NOT PRESSURIZE IN AUTO OR MANUAL MODE. AIRCRAFT RE
- [SDR M8XA9800008](https://openairdocs.org/sdr/M8XA9800008), May 18, 1998: INDICATION. MALFUNCTIONED. EN ROUTE FROM DEN TO DRO, THE FLIGHT CREW NOTICED ON THE FLAP POSITION INDICATION PORTION OF THE EICAS. SCREEN THAT THE RIGHT FLAP INDICATED A ONE DEGREE DEFLEC
- [SDR M8XA9800007](https://openairdocs.org/sdr/M8XA9800007), May 12, 1998: PITOT HEAT. FAILED. EN ROUTE FROM DEN TO CYS, AIRCRAFT ENCOUNTERED ICING CONDITIONS. SINCE THE PITOT HEAT SYSTEM WAS MEL'D, AIRCRAFT WAS FORCED TO RETURN TO DEN. AIRCRAFT LANDED IN
- [SDR M8XA9800005](https://openairdocs.org/sdr/M8XA9800005), May 8, 1998: SEAL. FAILED. DURING CLIMBOUT, THE CREW REPORTED A PROBLEM WITH AIR LEAKING AROUND THE DOCUMENT DOOR. CREW THEN ELECTED TO RETURN TO DEN. AIRCRAFT LANDED IN DEN WITH NO FURTH
- [SDR M8XA9800004](https://openairdocs.org/sdr/M8XA9800004), Apr 7, 1998: RADAR UNIT. DEFECTIVE. CREW REPORTED THAT THE RADAR APPEARED TO BE INOPERATIVE, NO GROUND PAINT. CREW ELECTED TO RETURN TO DENVER. AIRCRAFT LANDED IN DEN WITH NO FURTHER INCIDENTS. MX
- [SDR M8XA9800002](https://openairdocs.org/sdr/M8XA9800002), Feb 7, 1998: INDICATION. MALFUNCTIONED. CREW REPORTED THAT THEY RECEIVED NO VISUAL EICAS INDICATION THAT THE GROUND SPOILERS WERE ARMED AFTER THE CONDITION LEVERS WERE ADVANCED TO THE TAKEOFF POSITION
- [SDR M8XA9700022](https://openairdocs.org/sdr/M8XA9700022), Dec 26, 1997: BRACKET. FAILED. EN ROUTE, THE CREW RECEIVED A DOOR WARNING INDICATION. ACFT RETURNED, LANDED WITHOUT FURTHER INCIDENT. MX DISCOVERED THE PAX DOOR PROXIMITY SENSOR TARGET WAS MI
- [SDR M8XA9700020](https://openairdocs.org/sdr/M8XA9700020), Dec 18, 1997: HINGE. DEFECTIVE. SHORTLY AFTER THE A/C ARRIVED IN (DIA) MX WAS REQUESTED TO INSPECT THE PAX DOOR AS A RESULT OF DOOR BEING DIFFICULT TO CLOSE FROM TUL. MX INSPECT DOOR AND DISCO
- [SDR M8XA9700018](https://openairdocs.org/sdr/M8XA9700018), Dec 17, 1997: PRESS SWITCH. DEFECTIVE. EN ROUTE, RECEIVED A CAS MESSAGE EMERGENCY/PARKING BRAKE ACCUMULATOR PRESSURE ALERT. DIVERTED TO COS WHERE MX WAS AVAILABLE. ACFT LANDED WITH NO FURTHER INCIDEN
- [SDR M8XA9700019](https://openairdocs.org/sdr/M8XA9700019), Dec 17, 1997: VALVE. DEFECTIVE. EN ROUTE, THE FLIGHT CREW REPORTED A PROBLEM WITH THE EMERGENCY/ PARKING BRAKE ACCUMULATOR PRESSURE INDICATION. THIS IS A REPEAT OF SAME PROBLEM EXPERIENCED EAR
- [SDR M8XA9700017](https://openairdocs.org/sdr/M8XA9700017), Oct 30, 1997: WARNING. ACTIVATED. DURING THE TAKEOFF ROLL, THE FLIGHT CREW WAS ALERTED BY A GROUND SPOILERS NOT STOWED CAS MESSAGE. CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MX CONDUCTE
- [SDR M8XA9700015](https://openairdocs.org/sdr/M8XA9700015), Sep 29, 1997: BEARING. DEFECTIVE. PROPELLER SERIAL NUMBER HL-146, WAS REMOVED FROM AIRCRAFT N331MX (S/N 3067) FOR SCHEDULED MAINTENANCE. WHEN THE PROPELLER WAS BEING DISASSEMBLED IN PREPARATION 
- [SDR M8XA9700014](https://openairdocs.org/sdr/M8XA9700014), Sep 16, 1997: CAS WARNING. ACTIVATED. DURING THE TAKEOFF ROLL PRIOR TO REACHING V1, THE CREW WAS ALERTED BY THE CAS SYSTEM THAT THEY HAD ENCOUNTERED AN INVERTER BUS FAIL. THIS WAS ACCOMPANIED BY AN 
- [SDR M8XA9700012](https://openairdocs.org/sdr/M8XA9700012), Aug 22, 1997: BOOST PUMP. FAILED. DURING THE TAKEOFF ROLL, THE FLT WAS ALERTED BY A ELPMP AUTO FAIL CAS MESSAGE. THE FLT CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. DENVER MX INSPECTED TH

## STCs that may be installed (OpenAirDocs) (1)

Approved for this engine model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC SE2805SO](https://openairdocs.org/stc/SE2805SO): Installation of an oil tank safety cap adapter which is intended to prevent loss of oil in the event of loss or damage to the oil filler cap. Jet Avion Corporation

## PMA parts (OpenAirDocs) (245, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this engine model on its data sheet, so check the FAA record before relying on it. Newest first.

- [3032255CL2CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191902940220260217155849.0001): Weight Balance Compressor. Core Parts LLC · PMA PQ05326NM · Replaces 3032255CL2 · Jan 6, 2026
- [3024146CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182686186420260217160347.0001): Washer Key. Core Parts LLC · PMA PQ05326NM · Replaces 3024146 · Jan 6, 2026
- [3032255CL4CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181545932020260217155850.0001): Weight Balance Compressor. Core Parts LLC · PMA PQ05326NM · Replaces 3032255CL4 · Jan 6, 2026
- [3032255CL5CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168234696220260217155850.0001): Weight Balance Compressor. Core Parts LLC · PMA PQ05326NM · Replaces 3032255CL5 · Jan 6, 2026
- [3032255CL3CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152118224920260217155849.0001): Weight Balance Compressor. Core Parts LLC · PMA PQ05326NM · Replaces 3032255CL3 · Jan 6, 2026
- [ST3086-013CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139847229320260217160512.0001): Packing Preformed. Core Parts LLC · PMA PQ05326NM · Replaces ST3086-013 · Jan 6, 2026
- [3032255CL1CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137001436220260217155848.0001): Weight Balance Compressor. Core Parts LLC · PMA PQ05326NM · Replaces 3032255CL1 · Jan 6, 2026
- [3015234CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190658425320260217153955.0001): Nut Self-Locking Shank. Core Parts LLC · PMA PQ05326NM · Replaces 3015234 · Jan 5, 2026
- [3010880CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117245394120260217153009.0001): Gasket Igniter. Core Parts LLC · PMA PQ05326NM · Replaces 3010880 · Jan 5, 2026
- [3003987CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110231097220260217153647.0001): Pin Lock. Core Parts LLC · PMA PQ05326NM · Replaces 3003987 · Jan 5, 2026
- [3018344CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103008963120260217153140.0001): Rivet Tubular Countersunk. Core Parts LLC · PMA PQ05326NM · Replaces 3018344 · Jan 5, 2026
- [WF329398](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173837820120250624152917.0001): Filter Element. Donaldson Company Inc · PMA PQ2432CE · Replaces 3035681, 5905587, Alternate… · Jun 2, 2025
- [WF429940](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168842044420250624152911.0001): Switch, Differential Pressure Indicator. Donaldson Company Inc · PMA PQ2432CE · Replaces 5905588, 3035683 · Jun 2, 2025
- [3034508WFC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168792409620250624152910.0001): Oil Filter Element. Donaldson Company Inc · PMA PQ2432CE · Replaces 3034508 3036376, Alternate: 11-11064… · Jun 2, 2025
- [WF334638](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197682983220250602133018.0001): Cleanable Oil Filter Element. Donaldson Company Inc · PMA PQ2432CE · Replaces 3112895-01, 3059255-01, 3059254-01… · May 23, 2025
- [WF331451](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192483939520250602133018.0001): Non-Cleanable Oil Filter Element. Donaldson Company Inc · PMA PQ2432CE · Replaces 3034190, Alternate: 3059253-01… · May 23, 2025
- [WF334591](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121150890220250602133018.0001): Filter Element. Donaldson Company Inc · PMA PQ2432CE · Replaces 3038454, Alternate: 11-11102… · May 23, 2025
- [3014422AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157889633320250310190842.0001): Packing with Retainer. Aero Attitude, LLC · PMA PQ00001CB · Replaces PWC 3014422 · Feb 25, 2025
- [3015234AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID130436253520240919140838.0001): Nut, Self-Locking, Shank. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3015234, 3015233, 3015232, 3016299… · Aug 7, 2024
- [7590526AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184790841820240129140716.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 3059777-01 · Dec 11, 2023
- [7587923AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178335771520240129140707.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 3059255-01 · Dec 11, 2023
- [7587923AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID176073949320240129140706.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 3059252-01 · Dec 11, 2023
- [7578659AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173270088920240129140709.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 3020291 · Dec 11, 2023
- [7590526AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171676279420240129140714.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 3038454 · Dec 11, 2023
- [7587923AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168806079720240129140707.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 3112895-01 · Dec 11, 2023
- [7590526AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168658722420240129140716.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 725825 · Dec 11, 2023
- [7587923AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID167757756320240129140706.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 3059253-01 · Dec 11, 2023
- [7578659AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165226990020240129140710.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 3015330 · Dec 11, 2023
- [7590526AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161839470920240129140715.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 3035729 · Dec 11, 2023
- [7578659AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159127581320240129140711.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 3034742 · Dec 11, 2023
- [7578659AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID155717735120240129140711.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 3034743 · Dec 11, 2023
- [7590526AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID154138367520240129140715.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 3035728 · Dec 11, 2023
- [7578659AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID153308215920240129140710.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 3014635 · Dec 11, 2023
- [7578659AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152901791720240129140712.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 3059256-01 · Dec 11, 2023
- [7587923AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID146767814120240129140705.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 3034190 · Dec 11, 2023
- [7590526AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145978549120240129140715.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 3059775-01 · Dec 11, 2023
- [7578659AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145669272020240129140709.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 3036376 · Dec 11, 2023
- [7590526AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145509498920240129140717.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 7590048AM · Dec 11, 2023
- [7590526AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139656555320240129140715.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 3059776-01 · Dec 11, 2023
- [7578659AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135679117420240129140714.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 3111843-01 · Dec 11, 2023
- [7578659AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID130080262720240129140709.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 3034508 · Dec 11, 2023
- [7587923AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128560613620240129140707.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 3059254-01 · Dec 11, 2023
- [7578659AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128292367220240129140713.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 3059414-01 · Dec 11, 2023
- [7590526AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123642627020240129140715.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 3035317 · Dec 11, 2023
- [7578659AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117230667420240129140713.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 3073301-01 · Dec 11, 2023
- [7578659AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID116433161920240129140708.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 3029316 · Dec 11, 2023
- [7590526AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID113632618020240129140716.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 7587615AM · Dec 11, 2023
- [7587923AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID113611469520240129140707.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 7590047-101AM · Dec 11, 2023
- [7578659AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105468072420240129140712.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 3054626-01 · Dec 11, 2023
- [7578659AM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105269689420240129140708.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 3029315 · Dec 11, 2023

All of them: https://openairdocs.org/engine/pratt-whitney-canada-pw119c/pma.md

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