# U/A Canada PT6A-60A - Type: Engine model (FAA registry) - Registry code: 61602 - Manufacturer (registry): U/A CANADA - Model: PT6A-60A - Engine type: Turbo-prop - Power: 1,050 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-60a 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 2004-25-18](https://openairdocs.org/ad/2004-25-18): Propeller governor assemblies · Pratt & Whitney Canada PT6A-60A and PT6A-65B. Effective Jan 18, 2005 - [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 (596, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR RU3A2025102800001](https://openairdocs.org/sdr/RU3A2025102800001), Oct 24, 2025: BRAKE. OVERTEMP. DURING ROLLOUT INSPECTION, CREW RETURNED TO GATE DUE TO AIRCRAFT'S BRAKES BECAME EXCESSIVELY HOT PRODUCING VISIBLE SMOKE. FIRE TRUCKS WERE ROLLED OUT AND SPRAYE - [SDR CTUR20250528001](https://openairdocs.org/sdr/CTUR20250528001), May 7, 2025: LEVER. MISSING. TRIED FLYING N817PA MORNING OF MAY 7TH AND THE RIGHT SIDE DOESN'T COME OUT OF THE GROUND PITCH. DOING THE AUTO FEATHER TEST, THE RIGHT PROP WAS AT 1700 RPM. TRI - [SDR NOZR72024B](https://openairdocs.org/sdr/NOZR72024B), Jul 3, 2024: BLEED VALVE. FAILED. THE FLIGHT CREW REPORTED THE NO:1 ENGINE BEGAN POPPING AND LOST 50% OF ITS POWER 11 MINUTES AFTER TAKEOFF. AN UNSCHEDULED LANDING WAS PERFORMED AT THE DEPARTURE - [SDR GRTA20240307001](https://openairdocs.org/sdr/GRTA20240307001), Mar 6, 2024: HEAT EXCHANGER. LEAKING. WHILE FLYING AT FL 320 #2 RIGHT SIDE ENGINE LOST OIL PRESSURE INSTANTLY. REQUESTED DIVERT TO KHSV. ON LANDING NOTED OIL DRIPPING FROM BOTTOM OF COWLING. MX FOUN - [SDR 2023FA0000838](https://openairdocs.org/sdr/2023FA0000838), Dec 18, 2023: STARTER GEN. FAILED. WHEN STARTING LEFT ENGINE AND BRINGING LEFT GENERATOR ON LINE IT WOULD NOT COME ON LINE. I CHECKED TO MAKE SURE IGNITION STARTER WAS OFF AND IT WAS. I SHUT DOWN - [SDR YADA20230603001](https://openairdocs.org/sdr/YADA20230603001), Jun 1, 2023: UNKNOWN. UNKNOWN. DURING DESCENT THE RIGHT HAND ENGINE OIL PRESSURE WARNING INDICATOR ALERTED, PIC PERFORMED PRECAUTIONARY ENGINE SHUTDOWN AND LANDED SAFELY WITHOUT FURTHER INCID - [SDR O2GA2023032782001](https://openairdocs.org/sdr/O2GA2023032782001), Mar 19, 2023: VALVE. INTERMITTENT. AT FL310 RIGHT ENGINE OIL TEMPERATURE EXCEEDED 99* CELSIUS FOR MORE THAN 10 MINUTES. PEAKED AT 102* CELSIUS AND WAS STABLE AT 101* CELSIUS WHEN THE RIGHT THROTT - [SDR O2GA2022110783901](https://openairdocs.org/sdr/O2GA2022110783901), Oct 25, 2022: ENGINE. FAILED. DURING CLIMB LEFT ENGINE PROP CAME OUT OF SYNC FOLLOWED BY A LEFT SEVERE ENGINE VIBRATION (TORQUE JUMPED TO 130%). LEFT ENGINE ITT WENT INTO THE RED. POWER WAS - [SDR QMLA2022082620057](https://openairdocs.org/sdr/QMLA2022082620057), Aug 24, 2022: RELAY. FAILED. ON APPROACH TO KGCK WHEN IT WAS TIME TO PUT FLAPS TO APPROACH SETTING THE FLAPS DID NOT COME DOWN OR INDICATE IN THE DOWN POSITION. DECIDED TO RETURN TO KAAO AN - [SDR O2GA2022082182501](https://openairdocs.org/sdr/O2GA2022082182501), Aug 14, 2022: VALVE. INTERMITTENT. ON TAKE OFF JUST AFTER ROTATION R ENG OIL TEMP WENT YELLOW @ 105* C. THEN 109* C. DURING THE COURSE CHANGE TURN THE R ENG OIL TEMP TURNED RED @ 117*C. STAYED TH - [SDR 2022FA0000355](https://openairdocs.org/sdr/2022FA0000355), Jul 18, 2022: GOVERNOR. INOPERATIVE. DURING ENGINE PRE-TAKEOFF PERFORMANCE RUNS, THE #2 PROP WOULD NOT COME OUT OF FEATHER. MAINTENANCE TEAM INSPECTED THE ENGINE &PERFORMED ENGINE RUNS AND COULD NO - [SDR T4OR2022082400001](https://openairdocs.org/sdr/T4OR2022082400001), Apr 4, 2022: PITCH LINK. GALLED. NEWLY OVERHAULED PROPS, HARTZELL PN HC-B4MP-3C, ON KING AIR B300. INFLIGHT, WHEN POWER WAS REDUCED FOR LANDING, THE PROPS S/N FWA4217 AND FWA4213 WENT FLATTER T - [SDR 2022FA0000251](https://openairdocs.org/sdr/2022FA0000251), Mar 21, 2022: PRESSURE SWITCH. FAILED. AIR CONDITIONING SYSTEM WOULD NOT COOL. RECOVERED FREON AND PERFORMED FUNCTIONAL TEST ON BINARY PRESSURE SWITCH. SWITCH WAS FOUND TO REMAIN IN AN "OPEN" CONDITI - [SDR 2022FA0000155](https://openairdocs.org/sdr/2022FA0000155), Mar 16, 2022: NONE. NONE. ON PREFLIGHT RIGHT ENGINE WAS SHOWING 3.5QTS LOW. I PUT APPROX 1.75 QTS OF OIL IN RIGHT ENGINE TO BRING IT UP TO 1.75 LOW ON DIPSTICK. THE R ENG TEMP WAS A BIT - [SDR GSPA202112160001](https://openairdocs.org/sdr/GSPA202112160001), Dec 9, 2021: LANDING GEAR. FAULTED. EMPTY LEG MMSL TO KSDM IN ORDER TO CLEAR CUSTOMS. FLEW APPROACH INTO KSDM AT APPROXIMATELY1800L, LOST AIRPORT ENVIRONMENT WHILE CIRCLING, EXECUTED MISSED APPROA - [SDR GSPA20211207](https://openairdocs.org/sdr/GSPA20211207), Nov 21, 2021: ACTUATOR. INTERMITTENT. ON DEPARTURE WE RETRACTED THE GEAR AS NORMAL WITH NO ABNORMAL CONDITIONS EXCEPT A RED GEAR HANDLE. WE FOUND THE LANDING GEAR RELAY CIRCUIT BREAKER POPPED. PER C - [SDR O2GA2021101383901](https://openairdocs.org/sdr/O2GA2021101383901), Oct 7, 2021: FUEL CONTROL. INOPERATIVE. DURING CRUISE FLIGHT THE RIGHT ENGINE ROLLED BACK UN-COMMANDED. RIGHT ENGINE FUEL FLOW DROPPED TO 90. FLIGHT CREW SHUTDOWN THE ENGINE, DECLARED AN EMERGENCY AND - [SDR O2GA2021051782701](https://openairdocs.org/sdr/O2GA2021051782701), May 12, 2021: OIL SYSTEM. LEAKING. DURING FLIGHT FL290 RIGHT ENGINE OIL PRESSURE DROPPED AND WENT INTO THE RED. OIL WAS OBSERVED STREAKING ALONG ENGINE COWL. AN INFLIGHT ENGINE SHUTDOWN WAS PERFO - [SDR O2GA2021040680001](https://openairdocs.org/sdr/O2GA2021040680001), Apr 1, 2021: ARMATURE. FAILED. ENROUTE KHVN TO KRDU AT FL260 AN EICAS “R GEN TIE OPEN” ILLUMINATED. FOLLOWED THE CHECKLIST AND CLEARED EICAS. AFTER ABOUT 4 MINUTES “R GEN TIE OPEN” AGAIN ILLU - [SDR CGHR2021011801001](https://openairdocs.org/sdr/CGHR2021011801001), Jan 18, 2021: MOUNT. CRACKED. CRACKS HAVE BEEN FOUND IN THE FIELD DURING ROUTINE VISUAL INSPECTIONS OF ENGINE MOUNT TRUSS/COWLING MOUNT ATTACH BRACKETS. THE CRACKS FOUND ARE ALMOST ALWAYS EX - [SDR CGHR2021011801002](https://openairdocs.org/sdr/CGHR2021011801002), Jan 18, 2021: MOUNT. CRACKED. CRACKS HAVE BEEN FOUND IN THE FIELD DURING ROUTINE VISUAL INSPECTIONS OF ENGINE MOUNT TRUSS/COWLING MOUNT ATTACH BRACKETS. THE CRACKS FOUND ARE ALMOST ALWAYS EX - [SDR CGHR2021011801003](https://openairdocs.org/sdr/CGHR2021011801003), Jan 18, 2021: MOUNT. CRACKED. CRACKS HAVE BEEN FOUND IN THE FIELD DURING ROUTINE VISUAL INSPECTIONS OF ENGINE MOUNT TRUSS/COWLING MOUNT ATTACH BRACKETS. THE CRACKS FOUND ARE ALMOST ALWAYS EX - [SDR CGHR2021011801004](https://openairdocs.org/sdr/CGHR2021011801004), Jan 18, 2021: MOUNT. CRACKED. CRACKS HAVE BEEN FOUND IN THE FIELD DURING ROUTINE VISUAL INSPECTIONS OF ENGINE MOUNT TRUSS/COWLING MOUNT ATTACH BRACKETS. THE CRACKS FOUND ARE ALMOST ALWAYS EX - [SDR 2020FA0000561](https://openairdocs.org/sdr/2020FA0000561), Dec 22, 2020: ACTUATOR. CORRODED. LT MAIN GEAR RETRACT ACTUATOR FOUND CORRODED THRU CHROME COATING NEAR ATTACH END WERE EXPOSED WITH GEAR IN THE RETRACTED POSITION. NEW VERSION OF ACTUATOR HAS C - [SDR 2020FA0000529](https://openairdocs.org/sdr/2020FA0000529), Dec 9, 2020: POWERPACK. FAULTED. PILOT REPORTED AFTER TAKE OFF, THE GEAR WAS RETRACTED NORMALLY. UPON APPROACH, THE GEAR HANDLE WAS SELECTED DOWN, BUT THERE WAS NO GEAR MOVEMENT AND NO LIGHT IN - [SDR O2GA2020092186501](https://openairdocs.org/sdr/O2GA2020092186501), Sep 18, 2020: B-NUT. UNSECURE. LEFT ENGINE IN-FLIGHT SHUTDOWN BY THE CREW DURING CRUISE FLIGHT DUE TO LOSS OF OIL PRESSURE. EMERGENCY WAS DECLARED AND AIRCRAFT DIVERTED TO KGSO. SINGLE ENGINE - [SDR YEWA20200910002](https://openairdocs.org/sdr/YEWA20200910002), Aug 31, 2020: EXHAUST DUCT. TORN. PILOT REPORTED HEARING A POP UPON ADVANCING PROP LEVERS ON MID-FINAL APPROACH INTO KAAO. PILOT NOTICED NR 1 ENGINE TORQUE INDICATION EXTREMELY LOW, LANDING WAS - [SDR RU3A20200430019](https://openairdocs.org/sdr/RU3A20200430019), Apr 30, 2020: UNKNOWN. MALFUNCTIONED. LEFT ENGINE OIL TEMP HIGH. RAPID RISE IN OIL TEMP, TEMP FOLLOWS POWER LEVER. ENGINE AT IDLE TO MAINTAIN ACCEPTABLE TEMPERATURE - [SDR RU3A20200421018](https://openairdocs.org/sdr/RU3A20200421018), Apr 21, 2020: UNKNOWN. MALFUNCTIONED. LEFT ENGINE OIL TEMP EXCEEDED 99 DEG. W/YELLOW INDICATOR. TEMP REACHED 107 DEG. W/NORMAL OIL PRESSURE. TEMP RETURNED TO NORM RANGE DESCENDING FOR CAUTIONARY LAN - [SDR DATA20181217001](https://openairdocs.org/sdr/DATA20181217001), Dec 15, 2019: AMPLIFIER. FAILED. DURING CRUISE AT 6000 FT FROM SJU TO STT THE LEFT FUEL PRESSURE WARNING ILLUMINATED. RAN MEMORY ITEMS AND ENGINE SHUTDOWN CHECKLIST FROM QRH AND DECLARED AN EME - [SDR AXSA2019121200001](https://openairdocs.org/sdr/AXSA2019121200001), Dec 11, 2019: LINE. LEAKING. RIGHT ENGINE SHUT DOWN IN FLIGHT. INSPECTED RH ENGINE CONTROLS, FOUND TO BE SATISFACTORY. FOUND P3 LOOSE ON FCU. TIGHTENED AND SAFETIED, RAN ENGINE TWICE WITH H - [SDR COEA2019112601797](https://openairdocs.org/sdr/COEA2019112601797), Nov 26, 2019: INDICATOR. ERRATIC. FLIGHT 8775 ROUTE: PHX-FLG DISCREPANCY: DURING TAKEOFF, THE TORQUE GAUGE BEGAN TO GIVE ERRATIC READINGS. PILOT ELECTED TO DECLARE AN EMERGENCY AND RETURN TO PHX - [SDR RU3A20191029056](https://openairdocs.org/sdr/RU3A20191029056), Oct 29, 2019: WARNING MESSAGE. ILLUMINATED. RT BL AIR FAIL ANNUNCIATOR ILLUMINATED. ENGINE INDICATIONS ALL NORMAL. - [SDR NOZR201908080001](https://openairdocs.org/sdr/NOZR201908080001), Jul 30, 2019: FCU. FAILED. CREW NOTED THAT THE NR 1 ENGINE POWER LEVER AND CONDITION LEVER WERE BINDING DURING THEIR MORNING CHECKS. THE PRIOR DAY, THE SAME CREW NOTICED A "HIGH FREQUENCY - [SDR GSPA2019072400001](https://openairdocs.org/sdr/GSPA2019072400001), Jul 21, 2019: CONTROL VALVE. INOPERATIVE. WHILE CLIMBING TO OUR CRUZE ALTITUDE OF 26000 THE WHITE CABIN ALTITUDE LIGHT ILLUMINATED AND THE HORN SOUNDED WHILE CLIMBING THROUGH 23500. THE CABIN ALTITUDE W - [SDR GSPA201904040001](https://openairdocs.org/sdr/GSPA201904040001), Mar 18, 2019: FUEL CONTROL. FAULTY. THE START UP WAS UNEVENTFUL, AND THE RUN UP CHECKS WERE COMPLETED WITHOUT ANY DISCREPANCIES. CLEARED FOR TAKEOFF, TAXIED OUT, AND CAME TO A FULL STOP. PERFORMED - [SDR O2GA2019031284901](https://openairdocs.org/sdr/O2GA2019031284901), Mar 10, 2019: ROD. DISCONNECTED. ON DESCENT NOTICED THE RIGHT ENGINE ITT STARTING TO RISE. ATTEMPTED TO CONTROL WITH THROTTLE WAS NOT POSSIBLE AND SPLIT OF THROTTLES WAS MORE THEN ONE INCH. COM - [SDR CA190329002](https://openairdocs.org/sdr/CA190329002), Mar 10, 2019: ENGINE. UNRESPONSIVE. (CAN) DURING FLIGHT ENGINE #2 HAD NO RESPONSE TO POWER LEVER MOVEMENT AND HIGH ITT. THE CREW ELECTED TO SHUT DOWN THE ENGINE AND DIVERT. THE LANDING WAS UNEVENT - [SDR 2020FA0000089](https://openairdocs.org/sdr/2020FA0000089), Feb 14, 2019: PLATE. DAMAGED. UPPER FORWARD HOLE FOR THE UPPER ANCHOR BOLT FOR THE FORWARD BRAKE CALIPER BROKE OUT JAMMING THE FORWARD CALIPER ON THE BRAKE DISK ROTATING WITH THE TIRE AND BR - [SDR CA190213013](https://openairdocs.org/sdr/CA190213013), Feb 12, 2019: STARTER GEN. DAMAGED. (CAN) ABOUT AN HOUR INTO FLIGHT THE R/H DC GEN FAIL ANNUNCIATOR CAME ON, LOSS OF R/H DC GEN WAS CONFIRMED ON AMMETER. AIRCRAFT RETURNED TO BASE WITH NO FURTHER - [SDR O2GA2019020188901](https://openairdocs.org/sdr/O2GA2019020188901), Jan 21, 2019: BLADE. BENT. CREW REPORTED AFTER POST FLIGHT NOTED ALL 4 RIGHT PROPELLER BLADES TIPS BENT. CREW WRITE UP STATES UPON LANDING RIGHT PROP STRUCK RUNWAY. THE RIGHT ENGINE AND P - [SDR CA190816007](https://openairdocs.org/sdr/CA190816007), Jan 2, 2019: CONTROL VALVE. INTERMITTENT. (CAN) 1. AN INTERMITTENT FAULTY BLEED AIR SYSTEM FLOW CONTROL VALVE P/N 1H98-2 (TC# 20190816007) - [SDR JIKA2018111301](https://openairdocs.org/sdr/JIKA2018111301), Nov 13, 2018: CAP. UNSECURE. MAINTENANCE DISCREPANCY: THE PILOT REPORTED WHILE IN CRUISE FLIGHT THAT THE LEFT ENGINE OIL PRESSURE WAS INDICATING 50 PSI (NORMAL OPERATING RANGE 70-90 PSI). T - [SDR GSPA2018FA0000383](https://openairdocs.org/sdr/GSPA2018FA0000383), Sep 19, 2018: LANDING GEAR. MALFUNCTIONED. ON APPROACH TO AIRPORT, WE WENT TO PUT THE LANDING GEAR DOWN. MOVED THE LANDING GEAR LEVER TO THE DOWN POSITION BUT NOTHING HAPPENED. THERE WAS NO SOUND OF THE - [SDR O2GA2018080684701](https://openairdocs.org/sdr/O2GA2018080684701), Jul 25, 2018: FCU. DEFECTIVE. RIGHT ENGINE ROLL BACK DURING TAKEOFF WITH ACCOMPANYING YAW. TAKEOFF ABORTED. MAINTENANCE REPLACED THE RIGHT ENGINE FUEL CONTROL UNIT AND STARTER GENERATOR. SUC - [SDR CA180808025](https://openairdocs.org/sdr/CA180808025), Jul 25, 2018: COMPRESSOR. FAILED. (CAN) AIR CONDITIONING COMPRESSOR P/N 201-0450-3 FAILURE, 73.5 HRS FROM INSTALLATION. DEFECT REPORTED: `AIR CONDITIONING NOT COOLING` AIR CONDITIONING COMPRESSO - [SDR O2GA20180713001](https://openairdocs.org/sdr/O2GA20180713001), Jul 8, 2018: B-NUT. LOOSE. DURING CRUISE FLIGHT RIGHT ENGINE OIL PRESSURE DROPPED TO 60PSI. DECREASED POWER SETTING, DECLARED AN EMERGENCY AND DIVERTED TO KMSV. TWO ENGINE LANDING WAS UNE - [SDR CA180808024](https://openairdocs.org/sdr/CA180808024), Jun 27, 2018: COMPRESSOR. FAILED. (CAN) AIR CONDITIONING COMPRESSOR P/N 201-0450-3 FAILURE, 15.7 HRS FROM INSTALLATION. DEFECT REPORTED: `AIR CONDITIONING NOT WORKING` AIR CONDITIONING COMPRESSO - [SDR CA180808020](https://openairdocs.org/sdr/CA180808020), Jun 17, 2018: DISPLAY. FAILED. (CAN) ROCKWELL COLLINS PROLINE FUSION EQUIPPED AIRCRAFT, ADAPTIVE FLIGHT DISPLAY AFD-3700. DEFECT REPORTED AS `NUMEROUS ERRONEOUS CAS MESSAGES SHOWING UP ON RET - [SDR CA180808023](https://openairdocs.org/sdr/CA180808023), Jun 5, 2018: COMPRESSOR. FAILED. (CAN) AIR CONDITIONING COMPRESSOR P/N 201-0450-3 FAILURE ON AN AIRCRAFT WITH UNDER 400 HRS FROM NEW. DEFECT REPORTED: `AIR CONDITIONING FOUND TO NOT BE BLOWING All 596: https://openairdocs.org/engine/u-a-canada-pt6a-60a/reports.md ## 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 SE01624WI](https://openairdocs.org/stc/SE01624WI): Conversion of Pratt & Whitney Canada, Model PT6A-60A to a North Star Aviation PT6A-60AG turboprop engine. Data required: 1. A copy of this certificate 2. North Star Aviation document, NSA No. 1200, Turboprop Engine Conversion of PT6A-60A Model to PT6A-60AG Configuration per FAA Approved STC , dated March 15, 2011, or later FAA approved revision 3. The ICA supplement for North Star Aviation PT6A-60AG models, Instructions for Continued Airworthiness, NSA No. 1200-ICA, Rev NC, dated March 9, 2011 or later applicable revision. North Star Aviation Inc - [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 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) (449, 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 - [3021848CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181188254020260217165221.0001): Spacer, Oil Slinger. Core Parts LLC · PMA PQ05326NM · Replaces 3021848 · Feb 11, 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 - [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 - [3100920-04ANB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178742718720240917173637.0001): Piston Assy. ANB Aviation Parts LLC · PMA PQ1730CE · Replaces 3100920-04 · Jun 25, 2024 - [3103173-01ANB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133435034120240917173637.0001): Piston. ANB Aviation Parts LLC · PMA PQ1730CE · Replaces 3103173-01 · Jun 25, 2024 - [3100918-05ANB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103138423920240917173638.0001): Spacer. ANB Aviation Parts LLC · PMA PQ1730CE · Replaces 3100918-05 · Jun 25, 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 - [3005290CLACP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171588224920250611143002.0001): Weight, Balance, Compressor. CORE PARTS LLC · PMA PQ05326NM · Replaces 3005290CLA · 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 - [CH92106-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182423481520231024191312.0001): Exciter-Ignition. Champion Aerospace LLC · PMA PQ1287CE · Replaces Pratt & Whitney Canada … · May 12, 2023 - [CH92106-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170076831020231024191315.0001): Exciter-Ignition. Champion Aerospace LLC · PMA PQ1287CE · Replaces Unison10-381550-110-381550-49047840-190… · May 12, 2023 All of them: https://openairdocs.org/engine/u-a-canada-pt6a-60a/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.