# U/A Canada PT6A-114A - Type: Engine model (FAA registry) - Registry code: 61584 - Manufacturer (registry): U/A CANADA - Model: PT6A-114A - Engine type: Turbo-prop - Power: 675 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-114a 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 2022-08-13](https://openairdocs.org/ad/2022-08-13): Turbine Section · Pratt & Whitney Canada PT6A-34, PT6A-34B, PT6A-34AG and 2 more. Effective May 27, 2022 - [AD 2014-17-08 R1](https://openairdocs.org/ad/2014-17-08-R1): Compressor turbine (CT) blades · Pratt & Whitney Canada PT6A-114 and PT6A-114A. Effective Jun 5, 2015 - [AD 2012-09-10](https://openairdocs.org/ad/2012-09-10): First stage sun gears · Pratt & Whitney Canada PT6A-110, PT6A-112, PT6A-114 and 12 more. Effective May 23, 2012 - [AD 2001-20-01](https://openairdocs.org/ad/2001-20-01): Compressor Bleed Valve Assembly · Pratt & Whitney Canada PT6A-114A and PT6A-25C. Effective Nov 5, 2001 - [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 Effective Mar 14, 1997 Historical (superseded or no longer in force): - [AD 2014-17-08](https://openairdocs.org/ad/2014-17-08) (historical): Compressor turbine (CT) blades · Pratt & Whitney Canada PT6A-114 and PT6A-114A. Effective Oct 8, 2014 ## Information bulletins (advisory) (2) - [SAIB NE-12-04](https://openairdocs.org/saib/NE-12-04): Turbine/ Turboprop Engine: Reduction Gearbox. Issued Nov 1, 2011 - [SAIB NE-10-47](https://openairdocs.org/saib/NE-10-47): Turbine Engine Compressor Section. Issued Aug 30, 2010 ## 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 (705, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR GAJA202610070223](https://openairdocs.org/sdr/GAJA202610070223), Oct 1, 2026: ENGINE. SURGES. DURING CRUISE AT 13,000FT, THE PILOT EXPERIENCED A TEMPORARY UNCOMMANDED POWER SURGE BUT THE AIRCRAFT SETTLED BACK INTO NORMAL CRUISE PERFORMANCE SETTING. WITHI - [SDR DEMA202605270001](https://openairdocs.org/sdr/DEMA202605270001), May 19, 2026: FUEL CONTROL. UNCONTROLLABLE. LOSS OF ENGINE THROTTLE RESPONSE FOLLOWED BY AN UNCOMMANDED ENGINE SHUTDOWN ON THE TAXIWAY PRIOR TO TAKEOFF. THE AIRCRAFT FUEL SYSTEM WAS CHECK FOR CONTAMINATIO - [SDR 2026FA0000334](https://openairdocs.org/sdr/2026FA0000334), May 4, 2026: BELLOWS. FAULTED. PILOT NOTICED AFTER DESCENT TO FLIGHT LEVEL 1500 FEET, LEVELING OFF AND ADDING POWER, TORQUE INDICATION DROPPED 200 AND RECOVERED ON ITS OWN WITH NO INPUT TO TH - [SDR ENHA 20250521862](https://openairdocs.org/sdr/ENHA%2020250521862), May 20, 2025: REGULATOR. STICKING. PILOT OBSERVED THE PILOT DOOR POST GETTING HOT. MECHANICS REPLACED THE BLEED AIR PRESSURE REGULATOR AND PROBLEM WAS RESOLVED. - [SDR 1AZA2025F00117](https://openairdocs.org/sdr/1AZA2025F00117), May 6, 2025: ENGINE. ABNORMAL. ENGINE CHIP DETECTOR LIGHT ILLUMINATED IN FLIGHT,. LOW OIL PRESSURE LIGHT ILLUMINATED, LOW OIL PRESSURE INDICATED. POST-FLIGHT, REMOVED OIL SCREEN AND FOUND MET - [SDR 2025FA0000339](https://openairdocs.org/sdr/2025FA0000339), Apr 22, 2025: ENGINE. FAILED. PILOT REPORTED A CHIP LIGHT ILLUMINATED DURING APPROACH INTO ONT. BEGAN MONITORING PARAMETERS, AND HEARD A POP. OIL PRESSURE DROPPED FROM 101 TO 94 PSI. A FEW M - [SDR ENHA2025013008](https://openairdocs.org/sdr/ENHA2025013008), Jan 29, 2025: BRAKE PADS. LOCKED. BRAKES LOCKED. MECHANICS LOOSENED THE PADS AND RETORQUED IAW C208MM 32-40-00. OPS CHECK WAS GOOD. - [SDR ENHA 202410040001](https://openairdocs.org/sdr/ENHA%20202410040001), Sep 30, 2024: TUBE. LOOSE. BLEED AIR HEAT INOP, NO AIRFLOW AND HOT SMELL WHEN BLEED AIR HEAT IS TURNED ON. MECHANICS FOUND SCAT TUBE AT CABIN AIR VALVE HAD COME LOOSE. RE-SECURED IAW 208M - [SDR K2AA2024092300730](https://openairdocs.org/sdr/K2AA2024092300730), Sep 23, 2024: SKIN. CORRODED. LEFT HAND WING LEADING EDGE SKIN FOUND WITH CORROSION BEYOND LIMITS. RE-SKIN OF THE LH LEADING EDGE IS WORKABLE FROM THE MM AND SRM. HOWEVER THE REPAIR WILL PUT - [SDR 141A2024050700003](https://openairdocs.org/sdr/141A2024050700003), May 7, 2024: UNKNOWN. ODOR. DURING CRUISE FLIGHT, CA AND FO NOTICED A STRONG BURNING SMELL, LIKE BURNING RUBBER AND PLASTIC. FLIGHT WAS DIVERTED AND MADE AN UNSCHEDULED LANDING. MAINTENANC - [SDR ENHA2024040800088](https://openairdocs.org/sdr/ENHA2024040800088), Apr 5, 2024: UNKNOWN. ODOR. HOT ELECTRICAL SMELL. SMELL DISAPEARED ON TAXI BACK TO RAMP. SUSPECTED THAT DEICE FLUID WAS SPRAYED ON EXHAUST, MECHANICS INSPECTEDT ENGINE BAY, JUNCTION BOX, C - [SDR 141A2024040200002](https://openairdocs.org/sdr/141A2024040200002), Mar 29, 2024: MASTER CYLINDER. DEFECTIVE. LEFT HAND BRAKE INEFFECTIVE. MAINTENANCE REPLACED LEFT HAND MASTER CYLINDER. PERFORMED HIGH SPEED TAXI. OPS CHECKED GOOD - [SDR 2024F00088](https://openairdocs.org/sdr/2024F00088), Mar 20, 2024: WIRE. CHAFED. SMOKE IN COCKPIT. DURING DESCENT THE FO NOTICED A BURNING SMELL FOLLOWED BY SMOKE COMING OUT OF THE AREA LOCATED BY THE RIGHT KNEE. ALL SYSTEMS AND INDICATIONS - [SDR 2024FA0000189](https://openairdocs.org/sdr/2024FA0000189), Feb 26, 2024: FIRE LOOP. BROKEN. DURING CRUISE, ENGINE FIRE ANNUNCIATOR ILLUMINATED FOR APPROX 3 SECONDS WITH WARNING HORN THEN EXTINGUISHED. THEN APPROX 10 SECONDS LATER IT OCCURRED AGAIN AND - [SDR 2024F00028](https://openairdocs.org/sdr/2024F00028), Feb 8, 2024: BELT. BROKEN. SMELL OF SMOKE IN THE COCKPIT DUE AC BELT BREAKING - [SDR 2024FA0000013](https://openairdocs.org/sdr/2024FA0000013), Jan 9, 2024: LINE. CRACKED. SMOKE IN COCKPIT ON TAKEOFF. - [SDR 2023F00337](https://openairdocs.org/sdr/2023F00337), Nov 25, 2023: V-BELT. BROKEN. SMOKE IN THE COCKPIT AFTER TAKEOFF. MAINTENANCE FOUND AIR CONDITIONING BELT BROKEN. SYSTEM PLACED ON MEL - [SDR 2023FA0000616](https://openairdocs.org/sdr/2023FA0000616), Oct 20, 2023: CONNECTOR. FAILED. PILOT DEPARTED THE MORNING OR MARCH 31 2023 AND SHORTLY INTO HIS FLIGHT, REPORTED AN ELECTRICAL BURNING SMELL. TURN BACK WAS PREFORMED AND FLIGHT RETURNED TO AI - [SDR ENHA202310160002](https://openairdocs.org/sdr/ENHA202310160002), Oct 13, 2023: UNKNOWN. UNKNOWN. PILOT NOTED "I OBSERVED A RUNAWAY ENGINE CONDITION, MY TORQUE AND NG GUAGES CLIMBED TO REDLINE WITH MY POWER LEVER IN IDLE POSITION. I DECIDED TO CLIMB TO 9500 - [SDR ENHA2023090800691](https://openairdocs.org/sdr/ENHA2023090800691), Sep 5, 2023: CALIPER. BROKEN. THE RIGHT WHEEL LOCKED UP ON LANDING, AFTER ABOUT 200' IT BROKE LOOSE AND WAS ROLLING AGAIN HOWEVER I HAD NO BRAKE ON THE RIGHT. I TAXIED TO THE RAMP AND FOUND - [SDR 2023F00267](https://openairdocs.org/sdr/2023F00267), Sep 4, 2023: BRAKE PADS. GLAZED. LOST BRAKING AUTHORITY ON BOTH PILOT AND COPILOT SIDE AFTER LANDING - [SDR 2023FA0000320](https://openairdocs.org/sdr/2023FA0000320), Jun 19, 2023: COMPRESSOR. SEIZED. DURING LANDING SMELLED THE ODOR OF SMOKE. TURNED OF AIR CONDITIONING SYSTEM AND SMELL DISSIPATED. FOUND AC BELT BROKEN AND COMPRESSOR SEIZED - [SDR 2023F00206](https://openairdocs.org/sdr/2023F00206), Jun 17, 2023: BRAKE. UNKNOWN. RIGHT BRAKE FAILURE ON TAXI ON BOTH PIC AND SIC'S SIDE. - [SDR 2023FA0000300](https://openairdocs.org/sdr/2023FA0000300), Jun 2, 2023: UNKNOWN. UNKNOWN. BURNT SMELL NOTICED BY CREW ON CLIMB OUT. ALL INSTRUMENTS INDICATED GREEN, NO SMOKE OR FLAMES NOTICED. FIRST OFFICER COMMENTED HE MAY NOT HAVE SECURED THE OIL F - [SDR 2023F00105](https://openairdocs.org/sdr/2023F00105), Apr 4, 2023: BOLT. MISSING. LOSS OF OIL PRESSURE ON DEPARTURE CLIMB OUT - [SDR 2023F00040](https://openairdocs.org/sdr/2023F00040), Feb 1, 2023: NONE. WORN. CREW REPORTED PROPELLER HEAT INOP-SHOWS 8-9 AMPS IN BOTH AUTO AND MANUAL. MODES. CORRECTIVE ACTION: REMOVED PROPELLER ANTI-ICE LEADS. INSTALLED THREE NEW PROPEL - [SDR 2022FA0000731](https://openairdocs.org/sdr/2022FA0000731), Nov 22, 2022: LINE. LEAKING. SMOKE COMING OUT OF PILOTS SIDE VENT IN FLIGHT. UPON INVESTIGATION AFTER LANDING, IT WAS DISCOVERED THAT THE LINES GOING TO THE COMPRESSOR WERE LEAKING FREON. - [SDR 2022F00023](https://openairdocs.org/sdr/2022F00023), Dec 8, 2021: FUEL CONTROL. FLUCTUATES. WHILE IN ROUTE FROM KONT TO KSMX THE PILOT EXPERIENCED ABNORMAL POWER SURGES AND ABNORMAL FLUCTUATIONS IN THE TORQUE GAGE. A REQUEST TO RETURN TO KONT WAS MADE - [SDR MTNA20210809001](https://openairdocs.org/sdr/MTNA20210809001), Aug 7, 2021: CHIP DETECTOR. CONTAMINATED. CHIP DETECTOR LIGHT CAME ON IN FLIGHT. MAINTENANCE INSPECTED BOTH CHIP DETECTORS. DEBRIS FOUND ON AGB CHIP DETECTOR. PERFORMED INSPECTION OF OIL FILTER, NO CONT - [SDR ENHA202012180001](https://openairdocs.org/sdr/ENHA202012180001), Dec 14, 2020: BOLT. FAILED. LEFT HAND BRAKE CALIPER LOWER ANCHOR BOLT FAILED, BOLT DEPARTED AIRCRAFT. BRAKE LOCKED UP. - [SDR 2020F00487](https://openairdocs.org/sdr/2020F00487), Dec 5, 2020: FUEL CONTROL. MALFUNCTIONED. JUST AFTER SHUTDOWN THE PILOT NOTICED SMOKE COMING FROM THE THE RIGHT SIDE OF THE AIRCRAFT, FOLLOWED BY FLAME ABOVE THE COPILOT WINDOW. THE PILOT EXITED THE COC - [SDR 2020F00423](https://openairdocs.org/sdr/2020F00423), Oct 5, 2020: BOOT. DEBONDED. ON CLIMB OUT FROM FAT THE PILOT HEARD A "POP" AND THEN FELT A VIBRATION IN THE AIRFRAME. HE NOTIFIED ATC OF HIS NEED TO RETURN ASAP AND LANDED WITH OUT INCIDENT - [SDR MTNA20200721001](https://openairdocs.org/sdr/MTNA20200721001), Jul 21, 2020: ENGINE. MALFUNCTIONED. IN CRUISE WITH ENGINE PARAMETERS NORMAL A SERIES OF BANGS WITH ASSOCIATED DROPS IN TORQUE, RISES IN ITT AND DROPS IN FUEL FLOW. RATE OF BANGS AND FLUCTUATIONS D - [SDR M36R201911260018](https://openairdocs.org/sdr/M36R201911260018), Nov 18, 2019: TURBINE BLADES. CORRODED. A STANDARD BORESCOPE INSPECTION OF THE COMPRESSOR TURBINE BLADES WAS CONDUCTED WITH NO DEFECTS NOTED IN ACCORDANCE WITH THE PRATT AND WHITNEY CANADA MAINTENANCE - [SDR AXSA201910030001](https://openairdocs.org/sdr/AXSA201910030001), Oct 2, 2019: FIRE DETECTOR. SHORTED. ENGING FIRE WARNING AND ANNUCIATOR ACTIVATED AFTER TAKE OFF, STAYED ON DURING LANDING AND TAXI. NO VISIBLE SIGNS OF FIRE NOTED. - [SDR ENHA2019090600000](https://openairdocs.org/sdr/ENHA2019090600000), Sep 5, 2019: O-RING. WORN. FROM PILOT IRREGULARITY REPORT: "1115M HAD A LEFT BRAKE FAILURE AFTER LANDING RWY 19R. AS I WAS TAXING DOWN C I WAS USING A COMBINATION OF THE RIGHT BRAKE AND P - [SDR AWHA2019073100000](https://openairdocs.org/sdr/AWHA2019073100000), Jul 22, 2019: POWER LEVER. OUT OF RIG. DURING POST COMPRESSOR WASH ENGINE RUN MAINTENANCE FOUND PROP STARTING TO GO INTO BETA WHEN THE POWER LEVER WAS AT THE GATE. THE MECHANIC DETERMINED THE ENGINE - [SDR EPUA20190716001](https://openairdocs.org/sdr/EPUA20190716001), Jul 15, 2019: FUEL CONTROL. LEAKING. PILOT REPORTS " UPON DEPARTING A STRONG ODOR OF POLISH OR FUEL BEGAN FILLING THE CABIN. AT FIRST WE BELIEVED IT WAS FUEL ON GLOVES OR A RAG. AS WE FLEW THE SMEL - [SDR AWHA201906184001](https://openairdocs.org/sdr/AWHA201906184001), Jun 14, 2019: MASTER CYLINDER. FAILED. UPON TAXI TO RWY 20 FOR DEPARTURE FROM KPWT AT IDLE RPM (A TWY NE BOUND) LOSS OF BRAKING/STEERING CONTROL, RESULTED IN ACFT VEERING OFF PAVED SURFACE AND INTO T - [SDR MUIA20190518001](https://openairdocs.org/sdr/MUIA20190518001), May 8, 2019: STATIC SYSTEM. CONTAMINATED. CREW REPORTED PIC AND SIC AIRSPEED INDICATORS AND PIC AND SIC VERTICAL SPEED INDICATORS GAVE ERRONEOUS READING IN HEAVY PRECIPITATION AND TURBULENCE. MAINTENANC - [SDR 2019FA0000268](https://openairdocs.org/sdr/2019FA0000268), Apr 23, 2019: DOOR FRAME. CORRODED. LOWER CARGO DOOR THRESHOLD AIRFRAME SKIN CORRODED - [SDR 2019FA0000269](https://openairdocs.org/sdr/2019FA0000269), Apr 23, 2019: SKIN. CHAFED. CHAFE DAMAGE ON LOWER COWLING - [SDR 2019FA0000270](https://openairdocs.org/sdr/2019FA0000270), Apr 23, 2019: SUPPORT BRACKET. CHAFED. FLAP LEADING EDGE CHAFING AND SUPPORT BRACKET WEAR - [SDR 2019FA0000271](https://openairdocs.org/sdr/2019FA0000271), Apr 23, 2019: STRUCTURE. DENTED. DENTED ELEVATOR - [SDR 2019FA0000272](https://openairdocs.org/sdr/2019FA0000272), Apr 23, 2019: TORQUE TUBE. CORRODED. RUDDER TORQUE TUBE REQUIRES REPLACEMENT - [SDR 2019FA0000273](https://openairdocs.org/sdr/2019FA0000273), Apr 23, 2019: FLAP TRACK. WORN. FLAP TRACKS WORN - [SDR 2019FA0000274](https://openairdocs.org/sdr/2019FA0000274), Apr 23, 2019: FLAP TRACK. WORN. FLAP TRACKS WORN - [SDR ENHA2019F00156](https://openairdocs.org/sdr/ENHA2019F00156), Mar 18, 2019: CANISTER. FULL. FUEL SMELL IN COCKPIT. EPA CAN FULL. - [SDR MUIA20190212001](https://openairdocs.org/sdr/MUIA20190212001), Feb 12, 2019: CONNECTOR. CONTAMINATED. CREW PERFORMED AIR RETURN AFTER RESERVOIR LOW FUEL LIGHT ILLUMINATED ON ANNUNCIATOR PANEL WITH LH & RH WING LOW FUEL LIGHTS ILLUMINATED ON ANNUNCIATOR PANEL WHE - [SDR AWHA20190204001](https://openairdocs.org/sdr/AWHA20190204001), Dec 18, 2018: BLEED VALVE. MALFUNCTIONED. WHEN THE PILOT PUSHED THE POWER LEVER UP ON THE TAKEOFF ROLL HE HEARD TWO LOUD BANGS COMING FROM THE ENGINE COMPARTMENT. HE ABORTED TAKEOFF AND RETURNED TO THE All 705: https://openairdocs.org/engine/u-a-canada-pt6a-114a/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 SE00002EN](https://openairdocs.org/stc/SE00002EN): Instructions for Continued Airworthiness for the PT6A-34, -34AG, -34B, -36, -114, -114A, -116, -135, and -135A engine models that define specific maintenance tasks and their associated maintenance schedules, and that are used as a supplement to the applicable Pratt & Whitney Canada manuals. MORE Company Inc - [STC SE00482SE](https://openairdocs.org/stc/SE00482SE): Incorporation of turbine engine into a twin power section turboprop assembly. Fifty-Ten-Yankee LLC - [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 SE09286SC](https://openairdocs.org/stc/SE09286SC): Installation of an alternate gas generator case. Airforce Turbine Service - [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 ## PMA parts (OpenAirDocs) (471, 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 - [3045951-02AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135029382220260722151307.0001): Detector, Chip, Magnetic. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3045951-02 · May 27, 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 - [3028815CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119353433120260311145425.0001): Sleeve, Propeller Shaft, Oil Transfer. Core Parts LLC · PMA PQ05326NM · Replaces 3028815 · 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 - [3007355CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID150958507420260217165221.0001): Spacer, Adjusting. Core Parts LLC · PMA PQ05326NM · Replaces 3007355 · Feb 11, 2026 - [3010671RM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180066927420260204181356.0001): Washer, Flat. Rimark Manufacturing · PMA PQ10018NE · Replaces 3010671 · Jan 28, 2026 - [3010880CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111084696520260108163216.0001): Gasket, Igniter. CORE PARTS LLC · PMA PQ05326NM · Replaces 3010880 · Oct 16, 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 - [WF344763](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115254655320250602133049.0001): Nozzle Cover, Machined. Donaldson Company Inc · PMA PQ2432CE · Replaces 3120869-01, Alternate: 3019491… · May 23, 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 - [3049873-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193736418720260108162918.0001): Washer, Key. CORE PARTS LLC · PMA PQ05326NM · Replaces 3049873-01 · Jan 17, 2025 - [3116033-01ACD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183380911920250127211157.0001): Gasket, Eight-Hole. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 3116033-01 · Dec 18, 2024 - [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 - [3110741-02CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169885030720250605164146.0001): Ring, Retaining, Compressor Turbine. CORE PARTS LLC · PMA PQ05326NM · Replaces 3110741-02 · Oct 31, 2024 - [218794ACD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136891010120241022133827.0001): Washer, CRES. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 218794 · Oct 3, 2024 - [3010671CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189963175420241202221129.0001): Washer, Flat. CORE PARTS LLC · PMA PQ05326NM · Replaces 3010671 · 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 - [3006523CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132375139220240509162259.0001): Bearing, Sleeve, Flanged. CORE PARTS LLC · PMA PQ05326NM · Replaces 3006523 · Mar 25, 2024 - [3008676CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID120421035120240509162301.0001): Bearing, Sleeve, Flanged. CORE PARTS LLC · PMA PQ05326NM · Replaces 3008676 · 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 - [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 - [3005290CLECP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID142064254420250611143003.0001): Weight, Balance, Compressor. CORE PARTS LLC · PMA PQ05326NM · Replaces 3005290CLE · May 19, 2023 - [3005290CLDCP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141205886020250611143003.0001): Weight, Balance, Compressor. CORE PARTS LLC · PMA PQ05326NM · Replaces 3005290CLD · May 19, 2023 - [3005290CLBCP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118455233520250611143003.0001): Weight, Balance, Compressor. CORE PARTS LLC · PMA PQ05326NM · Replaces 3005290CLB · May 19, 2023 - [3005290CLCCP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103292467820250611143003.0001): Weight, Balance, Compressor. CORE PARTS LLC · PMA PQ05326NM · Replaces 3005290CLC · 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 - [TA3057-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161272206620230515183738.0001): Turbine Engine Preheat Kit. Hartzell Propeller LLC · PMA PQ2040CE · Modification part · May 5, 2023 - [TA3057-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID146529815220230515183804.0001): Turbine Engine Preheat Kit. Hartzell Propeller LLC · PMA PQ2040CE · Modification part · May 5, 2023 - [540-1407-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195148956920241024194516.0001): Valve Compressor Bleed. Honeywell International Inc. · PMA PQ1222NM · Replaces 540-1407-4 · May 2, 2023 - [3244897-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID138879401020241024194519.0001): Fuel Control Turboprop. Honeywell International Inc. · PMA PQ1222NM · Replaces 3244897-4 · May 2, 2023 - [RM3022375](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197353719220230503123945.0001): Seal, Plain. Rimark Manufacturing · PMA PQ10018NE · Replaces 3022375 · Apr 19, 2023 - [RM3022374](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID109994811820230503123941.0001): Seal, Plain. Rimark Manufacturing · PMA PQ10018NE · Replaces 3022374 · Apr 19, 2023 - [540-1407-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149574330120240306163319.0001): Valve, Bleed (Small PT6). Honeywell International Inc. · PMA PQ1222NM · Replaces 3049038-02 · Apr 14, 2023 - [206684ACD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193915393720230321122918.0001): Gasket, Propeller Governor Mounting. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 206684 · Mar 16, 2023 All of them: https://openairdocs.org/engine/u-a-canada-pt6a-114a/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.