# U/A Canada PT6A-65R

- Type: Engine model (FAA registry)
- Registry code: 61607
- Manufacturer (registry): U/A CANADA
- Model: PT6A-65R
- Engine type: Turbo-prop
- Power: 1,376 hp
- Data sheet: [TCDS E4EA](https://openairdocs.org/tcds/E4EA) (OpenAirDocs)
- Holder: Pratt & Whitney Canada Corp.
- Installed in: 0 registered aircraft
- Page: https://openairdocs.org/engine/u-a-canada-pt6a-65r

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 97-04-12](https://openairdocs.org/ad/97-04-12): Compressor Bleed-off Valve · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 52 more. Effective Mar 14, 1997

## Information bulletins (advisory) (2)

- [SAIB NE-15-21](https://openairdocs.org/saib/NE-15-21): Fuel Injector Nozzle. Issued Aug 19, 2015
- [SAIB CE-03-24](https://openairdocs.org/saib/CE-03-24): . Issued Feb 19, 2003

## Registered aircraft

None registered with this engine model now.

## NTSB investigations

None matched to aircraft with this engine model.

## FAA accident and incident reports

None matched to aircraft with this engine model.

## Service difficulty reports (32)

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

- [SDR DATA2020022701](https://openairdocs.org/sdr/DATA2020022701), Feb 25, 2020: UNKNOWN. ODOR. ON CLIMB OUT FROM TUPJ CAPTAIN STATED HE SAW AND SMELLED SMOKE. EMERGENCY WAS DECLARED AND RETURNED TO NEAREST AIRPORT WHICH WAS TUPJ AND LANDED SAFELY. MAINTEN
- [SDR DATA20191220001](https://openairdocs.org/sdr/DATA20191220001), Dec 18, 2019: HYDRAULIC SYSTEM. LOW PRESSURE. ON APPROACH TO LAND THE BRAKES WERE FOUND TO BE INDICATING NO PRESSURE WHEN TESTED AFTER COMPLETION OF APPROACH CHECKS. APPROACH WAS TERMINATED TO DIAGNOSE THE 
- [SDR DATA201803210002](https://openairdocs.org/sdr/DATA201803210002), Mar 17, 2018: CONNECTOR. CORRODED. AFTER TAKEOFF, ON CLIMB OUT, TORQUE INDICATION DROPPED BELOW 1000 AIRCREW DECIDED TO RETURN TO BASE FOR MAINTENANCE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENAN
- [SDR DATA2018032100001](https://openairdocs.org/sdr/DATA2018032100001), Mar 8, 2018: CHECK VALVE. STICKING. DURING CRUISE FLIGHT, THE LEFT ENGINE FUEL INDICATION ON CWP ILLUMINATED. WHILE LOOKING IN QRH, RECEIVED LOW OIL, LEFT GENERATOR AND LEFT AUTOFEATHER INDICATION
- [SDR DATA20130307001](https://openairdocs.org/sdr/DATA20130307001), Mar 5, 2013: BLEED VALVE. STICKING. ON APPROACH, THE CREW INITIATED A GO-AROUND. UPON INCREASING THRUST, THE CREW EXPERIENCED SURGING AND TORQUE FLUCTUATION ON THE RIGHT ENGINE. FOLLOWING QRH PROC
- [SDR DATA2011000004](https://openairdocs.org/sdr/DATA2011000004), Dec 7, 2011: ENGINE. BIRD INGESTION. FLIGHT 1465 ASW TO SDF IN LEVEL CRUISE APPROX 9000FT, FLIGHT CREW NOTICED SEVERE LOSS OF POWER FROM THE LEFT ENGINE. OBSERVED APPROX 45 PERCENT NG, LOW FUEL FLO
- [SDR DATA2010000001](https://openairdocs.org/sdr/DATA2010000001), Oct 19, 2010: SMOKE DETECTOR. FALSE ACTIVATION. DURING APPROACH ERRONEOUS SMOKE INDICATION FROM SMOKE DETECTOR IN NOSE COMPARTMENT OF AIRCRAFT. SMOKE DETECTOR IS A SINGLE DETECTOR SINGLE OPERATING SYSTEM.
- [SDR DATA2010FA0000252](https://openairdocs.org/sdr/DATA2010FA0000252), Mar 19, 2010: CABLE. BROKEN. AFTER T/O, LT ENGINE THROTTLE WAS UNRESPONSIVE. ENG WAS SHUTDOWN. ACFT RETURNED BACK TO STATION. POWER CABLE WAS FOUND BROKEN IN FUSELAGE. UNKNOWN THE TRUE AGE 
- [SDR DATA200700009](https://openairdocs.org/sdr/DATA200700009), Nov 17, 2007: LINE. BROKEN. WITH ABOUT 500' TO TOUCHDOWN THE LEFT ENGINE WENT INTO FEATHER (NO INDICATION ON CWP). ALL ENGINE INSTRUMENTS WERE NORMAL EXCEPT TORQUE AT 0 LBS. TORQUE WAS SET
- [SDR DATA200700007](https://openairdocs.org/sdr/DATA200700007), Aug 2, 2007: ENGINE. FAILED. N151CA DEPARTED MKE AT 00:00 ON A REPOSITION FLIGHT TO DNV. UPON REACHING CRUISE (5000FT) ALTITUDE, CRUISE POWER WAS SET BY THE FIRST OFFICER AS THE CAPTAIN WAS
- [SDR DATA200700006](https://openairdocs.org/sdr/DATA200700006), Jul 11, 2007: ENGINE. SURGES. THE CREW WAS DEPARTING CHARLESTON, SC, THE PILOT SMOOTHLY ADVANCED THE THROTTLES TO ALLOW THE PROPS TO SPIN UP TO MAX RPM, BEFORE SETTING TAKEOFF POWER. THE LEF
- [SDR DAT2006F00009](https://openairdocs.org/sdr/DAT2006F00009), Sep 15, 2006: ATTACH BOLT. BROKEN. DURING THE SCHEDULED MAINTENANCE, THE PROP TORQUE WAS COMPLIED WITH ON THE RT SIDE, AT 30311.5 TAT AND 37942 TAC. THE INSPECTION FOUND (1) BROKEN PROP ATTACHMEN
- [SDR DAT2006F00002](https://openairdocs.org/sdr/DAT2006F00002), Mar 28, 2006: CONTROL CABLE. BROKEN. DURING THE TAKEOFF ROLL, A LT TURN TENDENCY WAS NOTICED AND THE TORQUE GAUGES WERE CHECKED. THE LT PROP GAUGE WAS INDICATING 12 RPM. DUE TO THE UNEXPECTED BEHAV
- [SDR DAT2005F00010](https://openairdocs.org/sdr/DAT2005F00010), Aug 3, 2005: ENGINE. SHUTDOWN. DEPARTING, CAPTAIN NOTICED THE LT ENGINE TORQUE DROPPING AND THE ITT RISE TO APPROX 850 DEGREES. THE CAPTAIN PUSHED THE LT POWER LEVEL UP SLIGHTLY TO VERIFY THA
- [SDR DAT2005F00007](https://openairdocs.org/sdr/DAT2005F00007), Jul 7, 2005: TIRE. FAILED. AC HAD NORMAL STARTUP, TAXI OUT AND WAS CLEARED FOR TAKEOFF. FO WAS FLYING, CAPTAIN SET THE POWER, MADE THE CALLOUTS AND HAD JUST FINISHED SAYING (AIRSPEED ALIV
- [SDR DAT2005F00006](https://openairdocs.org/sdr/DAT2005F00006), Jun 15, 2005: LINE. CONTAMINATED. DURING FINAL APPROACH AND FINAL CHECKS, THE PROPS FWD THE RT ENGINE STARTED TO SURGE. POWER BROUGHT BACK ON RT ENGINE TO SLOW UP SURGE AND IT STOPPED SURGING MO
- [SDR DAT2005F00005](https://openairdocs.org/sdr/DAT2005F00005), Jun 9, 2005: TIRE. FAILED. DURING DEPARTURE ON TAKEOFF ROLL, ACCELERATION WAS NORMAL THROUGH 85 KNOTS, FLIGHT CREW HEARD A NOISE OUTSIDE OF THE AIRCRAFT. AC STARTED TO PULL TO LT AND THER
- [SDR 2001F00263](https://openairdocs.org/sdr/2001F00263), Aug 17, 2001: BLEED VALVE. MALFUNCTIONED. A/C DEPARTED CHEYENNE, WY, AFTER FUEL TOP OFF AND CLIMBING OUT THE LT ENGINE TORQUE DROPPED TO 2500 NR AND NG DROPPED 3 PERCENT. THE PILOT INCREASED THE POWER L
- [SDR CA010504007](https://openairdocs.org/sdr/CA010504007), Mar 23, 2001: FITTING. CORRODED. (CAN) DURING MID-LIFE STRUCTURAL INSPECTION THE ABOVE CLEAT WAS FOUND TO BE EXFOLIATED IN VARIOUS SPOTS BETWEEN THE WEBS. IT IS LIKELY THAT STANDING WATER COULD
- [SDR AU001244](https://openairdocs.org/sdr/AU001244), Dec 26, 2000: GEAR. WORN. (AUS) FLAP ACTUATOR FAULTY. INVESTIGATION FOUND THE WORM GEAR AND DRIVE GEAR WORN.
- [SDR CA001214017](https://openairdocs.org/sdr/CA001214017), Sep 9, 2000: BLADE. DAMAGED. (CAN) PILOT REPORTED THAT BLADE RUBBING NOISE WAS COMING FROM POWER TURBINE SECTION WHEN THE PROPELLER WAS TURNED BY HAND ON THE LEFT HAND ENGINE. LEFT HAND POW
- [SDR AU990099](https://openairdocs.org/sdr/AU990099), Feb 3, 1999: OIL COOLER. FAULTY. (AUS) RT ENGINE OIL COOLER FAULTY.
- [SDR AU981037](https://openairdocs.org/sdr/AU981037), Aug 11, 1998: WHEEL. DAMAGED. (AUS) RIGHT MAIN LANDING GEAR WHEEL OUTER RIM GROUND AWAY WHEN TIRE FAILED FOLLOWING BRAKE LOCK-UP.
- [SDR AU981038](https://openairdocs.org/sdr/AU981038), Aug 10, 1998: WHEEL. FAILED. (AUS) RIGHT MAIN WHEEL OUTER RIM SECTION MISSING.
- [SDR 99ZZZX551](https://openairdocs.org/sdr/99ZZZX551), Jun 25, 1998: VALVE. BROKEN. ON DESCENT, RIGHT ENGINE BEGAN TO SURGE WITH POWER LEVER MOVEMENTS. SHUT DOWN ENGINE FOR PRECAUTIONARY MEASURES AND LANDED ON ONE ENGINE. REMOVED AND REPLACED B
- [SDR AU980050](https://openairdocs.org/sdr/AU980050), Jan 1, 1998: SEAL. FAILED. (AUS) LH ENGINE GAS GENERATOR TACHO GENERATOR SHAFT SEAL FAILED.
- [SDR AU961087](https://openairdocs.org/sdr/AU961087), Aug 2, 1996: OIL SYSTEM. LOW PRESSURE. (AUS) RH ENGINE OIL PRESSURE LOSS
- [SDR AU961031](https://openairdocs.org/sdr/AU961031), Jul 17, 1996: RELAY. FAULTY. (AUS) NOSE LANDING GEAR RELAY FAULTY
- [SDR AU960866](https://openairdocs.org/sdr/AU960866), Jun 21, 1996: WINDOW. SEPARATED. (AUS) PASSENGER OUTER WINDOW AT SEAT POSITION 7A SEPARATED DURING FLIGHT - INSPECTION FOUND THAT THE WINDOW PANE AND THE RUBBER SEAL WERE MISSING - THIS WINDOW 
- [SDR AU960794](https://openairdocs.org/sdr/AU960794), Jun 4, 1996: TRIM SYSTEM. STUCK. (AUS) ELEVATOR TRIM SYSTEM JAMMED - INVESTIGATION FOUND THE METAL PORTION OF A SMALL GLOBE IN THE CONSOLE WHICH MAY HAVE BEENCAUGHT IN THE CHAIN CAUSING THE PRO
- [SDR AU960592](https://openairdocs.org/sdr/AU960592), May 7, 1996: SCREW. LOOSE. (AUS) NOSE LANDING GEAR ABUTTMENT PLATE OUT OF ADJUSTMENT
- [SDR CA960311007](https://openairdocs.org/sdr/CA960311007), Feb 20, 1996: BLADES. FAILED. (CAN) ON TAKEOFF ROLL AT 2000 LBS TORQUE, A LARGE POPPING SOUND CAME FROM THE #2 ENGINE, FOLLOWED BY VIBRATION. TAKEOFF ABORTED AND ENGINE SHUT DOWN ON TAXI IN.

## STCs that may be installed (OpenAirDocs) (6)

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 SE00014EN](https://openairdocs.org/stc/SE00014EN): Installation of the Pratt & Whitney Engine Services, Inc. CrossCheck Engine Monitor Kit P/N HUMS-K-071-1, Rev. A on the specified PT6A engine models and kit P/N HUMS-K-071-2 on the specified A250 engine models. Pratt & Whitney Engine Services Inc
- [STC SE00020EN](https://openairdocs.org/stc/SE00020EN): Installation of the Pratt & Whitney Engine Services, Inc. TrendCheck/ TrendCheck Plus Engine Monitor Kit P/N TREND-K-010-1. Pratt & Whitney Engine Services Inc
- [STC SE8652SW](https://openairdocs.org/stc/SE8652SW): Installation of a flexible hose from the Propeller Primary Governor to the Fuel Control Unit. Air Tractor Inc
- [STC SE01805NY](https://openairdocs.org/stc/SE01805NY): Installation of Fuel Nozzle Adapters using studs and nuts. Atlantic Turbines International Inc
- [STC SE09257SC](https://openairdocs.org/stc/SE09257SC): Convert P&W Engine Models PT6A-15AG, -27, and -28, into PT6A-34 configuration. Covington Aircraft Engines, Inc
- [STC SE659NE](https://openairdocs.org/stc/SE659NE): Installation of oil tank filler neck check valve, P/N TSA-76A. Aviation Components Support

## PMA parts (OpenAirDocs) (450, 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.

- [3005293CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122934446820260909150736.0001): Insert, Fuel Control Drive Shaft. Core Parts LLC · PMA PQ05326NM · Replaces 3005293 · Aug 17, 2026
- [3019136CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186981497620260728184309.0001): Ring, Plastic. Core Parts LLC · PMA PQ05326NM · Replaces 3019136 · Jul 10, 2026
- [3012928CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID185594574320260728184309.0001): Spacer, Stepped. Core Parts LLC · PMA PQ05326NM · Replaces 3012928 · Jul 10, 2026
- [3022834CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159372011320260528133243.0001): Sleeve, First Stage Reduction Carrier. Core Parts LLC · PMA PQ05326NM · Replaces 3022834 · Apr 17, 2026
- [ST3277-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199989902020260311145336.0001): Gasket, Starter Generator. Core Parts LLC · PMA PQ05326NM · Replaces ST3277-01 · Feb 26, 2026
- [ST3276-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101621452020260311145336.0001): Gasket, Four-Hole. Core Parts LLC · PMA PQ05326NM · Replaces ST3276-01 · Feb 26, 2026
- [3109585-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117456133120260217165221.0001): Spacer, Oil Slinger. Core Parts LLC · PMA PQ05326NM · Replaces 3109585-01 · Feb 11, 2026
- [3010880CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111084696520260108163216.0001): Gasket, Igniter. CORE PARTS LLC · PMA PQ05326NM · Replaces 3010880 · Oct 16, 2025
- [3018008CL3AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195594091320251113202147.0001): Weight, Turbine, Balance. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3018008CL3 · Sep 23, 2025
- [3031660CL3AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178817307620251113202148.0001): Weight, Turbine, Balance. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3031660CL3 · Sep 23, 2025
- [3018008CL5AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID176043530320251113202147.0001): Weight, Turbine, Balance. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3018008CL5 · Sep 23, 2025
- [3018008CL4AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID167757909020251113202147.0001): Weight, Turbine, Balance. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3018008CL4 · Sep 23, 2025
- [3018008CL2AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID160336366220251113202147.0001): Weight, Turbine, Balance. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3018008CL2 · Sep 23, 2025
- [3018008CL1AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143949810220251113202146.0001): Weight, Turbine, Balance. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3018008CL1 · Sep 23, 2025
- [3031660CL1AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132736100820251113202148.0001): Weight, Turbine, Balance. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3031660CL1 · Sep 23, 2025
- [3031660CL5AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID104430369720251113202149.0001): Weight, Turbine, Balance. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3031660CL5 · Sep 23, 2025
- [3031660CL2AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102794227220251113202148.0001): Weight, Turbine, Balance. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3031660CL2 · Sep 23, 2025
- [3031660CL4AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102269369120251113202148.0001): Weight, Turbine, Balance. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3031660CL4 · Sep 23, 2025
- [3034292WFC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166533215020250624152909.0001): Disposable Oil Filter Element. Donaldson Company Inc · PMA PQ2432CE · Replaces 3034292, 3034293, 3958257-01, 3028419… · Jun 2, 2025
- [3034507WFC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141045710620250624152910.0001): Cleanable Oil Filter Element. Donaldson Company Inc · PMA PQ2432CE · Replaces 3017383, 3020967, 3022069, 3022070… · Jun 2, 2025
- [3034393WFC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID100181403420250624152909.0001): Disposable Oil Filter Element. Donaldson Company Inc · PMA PQ2432CE · Replaces 3034393, 3033315, 3059257-01, 3028419… · Jun 2, 2025
- [WF334552](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID147857861520250602133017.0001): Compressor Air Filter. Donaldson Company Inc · PMA PQ2432CE · Replaces 3029268, Alternate: 3028856, 3029267… · May 23, 2025
- [WF337408](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125475616820250602133039.0001): Filter Element Assy, Fuel. Donaldson Company Inc · PMA PQ2432CE · Replaces 217384-1, 26281 · May 23, 2025
- [3109767-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180344174520260108163021.0001): Seal, Air, Power Turbine Rotor. CORE PARTS LLC · PMA PQ05326NM · Replaces 3109767-01 · May 15, 2025
- [3115091-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180857219920250923184724.0001): Ball, Plastic, 0.750. CORE PARTS LLC · PMA PQ05326NM · Replaces 3115091-01 · Feb 13, 2025
- [3058971-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110906306720250923184724.0001): Valve Assy, Oil Filler Tube. CORE PARTS LLC · PMA PQ05326NM · Replaces 3058971-01 · Feb 13, 2025
- [3049870-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID120826506620260108162918.0001): Washer, Key. CORE PARTS LLC · PMA PQ05326NM · Replaces 3049870-01 · Jan 17, 2025
- [3049869-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117447801820260108162917.0001): Washer, Key. CORE PARTS LLC · PMA PQ05326NM · Replaces 3049869-01 · Jan 17, 2025
- [3012414AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169774044220250106202801.0001): Nut, Self-Locking, 12 Point. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3012411 · Dec 10, 2024
- [3012414AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164469161820250106202800.0001): Nut, Self-Locking, 12 Point. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3012413 · Dec 10, 2024
- [3012414AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152753542620250106202759.0001): Nut, Self-Locking, 12 Point. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3012414 · Dec 10, 2024
- [3012414AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117377138920250106202801.0001): Nut, Self-Locking, 12 Point. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3012412 · Dec 10, 2024
- [3112397-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184407500420250605164147.0001): Ring, Retaining, Compressor Turbine. CORE PARTS LLC · PMA PQ05326NM · Replaces 3112397-01 · Oct 31, 2024
- [3112375-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180129798320250605164147.0001): Stop, Ring, Compressor Turbine. CORE PARTS LLC · PMA PQ05326NM · Replaces 3112375-01 · Oct 31, 2024
- [3105135-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182128581420241202221130.0001): Washer, Flat. CORE PARTS LLC · PMA PQ05326NM · Replaces 3105135-01 · Aug 22, 2024
- [3012675AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID196954661720240919140845.0001): Nut, Self-Locking, Hex. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3012675, 3005816, 3012674, 3028286… · Aug 7, 2024
- [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
- [3120298-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID146494060120241202220950.0001): Shroud, Power Turbine. CORE PARTS LLC · PMA PQ05326NM · Replaces 3120298-01 · Apr 30, 2024
- [3006523CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132375139220240509162259.0001): Bearing, Sleeve, Flanged. CORE PARTS LLC · PMA PQ05326NM · Replaces 3006523 · Mar 25, 2024
- [3003987CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125662034220231204145325.0001): Pin, Lock. CORE PARTS LLC · PMA PQ05326NM · Replaces 3003987 · Aug 1, 2023
- [3016598CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189342823620231204151230.0001): Washer, Key. CORE PARTS LLC · PMA PQ05326NM · Replaces 3016598 · Jul 26, 2023
- [3024146CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID175684471820231204151231.0001): Washer, Key. CORE PARTS LLC · PMA PQ05326NM · Replaces 3024146 · Jul 26, 2023
- [ST6202-011CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121242960820241204145238.0001): Packing, Preformed. CORE PARTS LLC · PMA PQ05326NM · Replaces ST6202-011 · Jun 15, 2023
- [3032255CL3CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID196126098120250611143004.0001): Weight, Balance, Compressor. CORE PARTS LLC · PMA PQ05326NM · Replaces 3032255CL3 · May 19, 2023
- [3036722CL1CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149331980920250611143005.0001): Weight, Balance, Compressor. CORE PARTS LLC · PMA PQ05326NM · Replaces 3036722CL1 · May 19, 2023
- [3032255CL4CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID148251690420250611143004.0001): Weight, Balance, Compressor. CORE PARTS LLC · PMA PQ05326NM · Replaces 3032255CL4 · May 19, 2023
- [3032255CL2CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134931261520250611143004.0001): Weight, Balance, Compressor. CORE PARTS LLC · PMA PQ05326NM · Replaces 3032255CL2 · May 19, 2023
- [3036722CL2CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128652215520250611143005.0001): Weight, Balance, Compressor. CORE PARTS LLC · PMA PQ05326NM · Replaces 3036722CL2 · May 19, 2023
- [3032255CL1CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115337523020250611143004.0001): Weight, Balance, Compressor. CORE PARTS LLC · PMA PQ05326NM · Replaces 3032255CL1 · May 19, 2023
- [CH92106-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182950761420231024191314.0001): Exciter-Ignition. Champion Aerospace LLC · PMA PQ1287CE · Replaces Champion… · May 12, 2023

All of them: https://openairdocs.org/engine/u-a-canada-pt6a-65r/pma.md

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.