# U/A Canada PT6A-65AG - Type: Engine model (FAA registry) - Registry code: 61609 - Manufacturer (registry): U/A CANADA - Model: PT6A-65AG - Engine type: Turbo-prop - Power: 1,300 hp - Data sheet: [TCDS E4EA](https://openairdocs.org/tcds/E4EA) (OpenAirDocs) - Holder: Pratt & Whitney Canada Corp. - Installed in: 2 registered aircraft - Page: https://openairdocs.org/engine/u-a-canada-pt6a-65ag 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 2016-05-13](https://openairdocs.org/ad/2016-05-13): Corrosion and perforation of the two-ply Cu-Be bellows in Woodward FCUs. · Pratt & Whitney Canada PT6A-60AG, PT6A-65AG, PT6A-67AF and 1 more. Effective Apr 22, 2016 - [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) (1) - [SAIB NE-15-21](https://openairdocs.org/saib/NE-15-21): Fuel Injector Nozzle. Issued Aug 19, 2015 ## Registered aircraft (2) - [N159LA](https://openairdocs.org/aircraft/N159LA): [Wilmot Airplane Ventures LLC](https://openairdocs.org/faa-owner/WILMOT%20AIRPLANE%20VENTURES%20LLC), [Dover, DE](https://openairdocs.org/faa-place/DE/Dover), S/N 602-1159 - [N194BM](https://openairdocs.org/aircraft/N194BM): [Bombero Aviation LLC](https://openairdocs.org/faa-owner/BOMBERO%20AVIATION%20LLC), [Childress, TX](https://openairdocs.org/faa-place/TX/Childress), built 2008, S/N 802A-0283 ## NTSB investigations (1) 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 GAA17CA342](https://openairdocs.org/ntsb/GAA17CA342), Jun 15, 2017: Air Tractor AT 802 (N915AJ), Pocahontas, AR, substantial damage. Probable cause: The pilot's failure to maintain lateral/bank control during the initial climb in turbulent conditions. ## FAA accident and incident reports (1) 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. - [Accident 20170615008339A](https://openairdocs.org/incident/20170615008339A), Jun 15, 2017: Air Tractor Inc AT-802A (N915AJ), Pocahontas, AR, Substantial damage. On June 12, 2017, at approximately 13:00 central time, an Air tractor AT-802A, registered as N915AJ to c&c flying service took off from a private dirt runway… ## Service difficulty reports (35) As reported by operators and repair stations, by the model named in the report. - [SDR CA150710014](https://openairdocs.org/sdr/CA150710014), Jun 29, 2015: LINE. FRACTURED. (CAN) DURING SPRAYING OPERATION, PILOT INCREASED THE ENGINE POWER AND THE FUEL FLOW WENT TO MINIMUM FLOW WITH NO RESPONSE FROM THE ENGINE. PILOT THEN IMMEDIATEL - [SDR CA150224005](https://openairdocs.org/sdr/CA150224005), Feb 5, 2015: ENGINE. SEPARATED. (CAN) THE ENGINE LOST POWER ON TAKEOFF. THE ENGINE WAS RIPPED FROM THE FUSELAGE AND THERE WAS TAIL AND WING DAMAGE. - [SDR CA141006008](https://openairdocs.org/sdr/CA141006008), Sep 9, 2014: ENGINE. POWER LOSS. (CAN) DURING TAKEOFF, THE ENGINE LOST POWER FORCING TO PILOT TO MAKE AN EMERGENCY LANDING IN A FIELD. THE ACFT SUSTAINED DAMAGE TO THE LOWER FUSELAGE AND WINGS. - [SDR CA140826001](https://openairdocs.org/sdr/CA140826001), Jul 25, 2014: ENGINE. SURGES. (CAN) THE ACCIDENT WAS REPORTED BY THE NTSB AND SPECIFIED THAT THE ENGINE SUSTAINED A POWER SURGE THEN A LOSS OF THRUST ON APPROACH. THE AIRPLANE LANDED IN TREE - [SDR CA140630013](https://openairdocs.org/sdr/CA140630013), Jun 13, 2014: UNKNOWN. UNKNOWN. (CAN) AFTER TAKEOFF FROM A DIRT STRIP, THE PILOT INITIATED AN EARLY TURN AT APPROX. 10 FT ABOVE THE GROUND. SHORTLY AFTER, THE ACFT FELT LIKE IT WAS SETTLING AN - [SDR CA140619019](https://openairdocs.org/sdr/CA140619019), Jun 5, 2014: ENGINE. POWER LOSS. (CAN) DURING FLIGHT, THE PILOT HEARD A LOUD NOISE FOLLOWED BY LOSS OF POWER. A FORCED LANDING WAS MADE IN A FIELD DURING WHICH THE AIRCRAFT WAS DAMAGED (EXTENT - [SDR CA131113008](https://openairdocs.org/sdr/CA131113008), Nov 13, 2013: STRUT. CORRODED. (CAN) DURING ANNUAL INSPECTION, IT WAS FOUND THAT THE LT STABILIZER STRUT ASSY. LOWER ATTACH FORK AND BUSHINGS WERE HEAVILY CORRODED. - [SDR CA130822003](https://openairdocs.org/sdr/CA130822003), Aug 16, 2013: ENGINE. POWER LOSS. (CAN) ACFT WAS FLYING A FIRE SUPPRESSION FLIGHT WHEN THE PILOT EXPERIENCED A LOSS OF POWER. DROPPED THE LOAD OF RETARDANT AND WAS FORCED TO LAND AT A PRIVATE AI - [SDR CA130614002](https://openairdocs.org/sdr/CA130614002), May 18, 2013: BLADE. FAILED. (CAN) DURING T/O ROLL, THE ENGINE LOST POWER. THE T/O WAS ABORTED. POST EVENT ENGINE EXAMINATION FOUND FRACTURED 2ND STAGE POWER TURBINE BLADES. THE ENGINE WAS - [SDR CA120227009](https://openairdocs.org/sdr/CA120227009), Feb 27, 2012: GUSSET. CRACKED. (CAN) CRACKED FUSELAGE FRAME AT LT AFT, FLOAT/AFT WING SPAR ATTACHMENT AREA. CRACK IS IN AREA "C" OF WIPAIRE SL REV D. AREA ALREADY REPLACED WITH THE NEWEST VER - [SDR CA120130002](https://openairdocs.org/sdr/CA120130002), Nov 8, 2011: ENGINE. POWER LOSS. (CAN) SHORTLY AFTER T/O FROM A PRIVATE STRIP AT 150 FT ALTITUDE, THE ENGINE STARTED TO SURGE ACCOMPANIED BY ERRATIC PROPELLER SPEED AND TORQUE FLUCTUATIONS. THE - [SDR CA111226002](https://openairdocs.org/sdr/CA111226002), Jul 22, 2011: ENGINE. POWER LOSS. (CAN) FOLLOWING THE COMPLETION OF A SPRAY RUN, THE ENGINE LOST POWER AND THE PILOT EXECUTED A FORCED LANDING IN A FIELD ADJACENT TO THE ONE HE WAS SPRAYING. THE - [SDR CA110615008](https://openairdocs.org/sdr/CA110615008), Jun 12, 2011: PACKING. SPLIT. ON WALK AROUND, HYD FLUID WAS NOTICED ON RAMP AND ON LT MLG WHEELS. AC POWER WAS TURNED ON AND HYD PUMPS CYCLED AND IT WAS DETERMINED THAT HYD FLUID WAS LEAKING - [SDR CA100729006](https://openairdocs.org/sdr/CA100729006), Jul 28, 2010: LINER. MISREPAIRED. WHILE REMOVING THE LED PORTION OF CC OUTER LINER IAW PWC 724002-SRR-05 INCOMPLETE RESISTANCE WELD HOLDING LED PORTION IN PLACE WAS FOUND. CIRCUMFERENTIAL RESIST - [SDR CA100608009](https://openairdocs.org/sdr/CA100608009), Jun 3, 2010: SPAR. CRACKED. AFT ATTACH POINT SPAR RADIUS FOUND CRACKED ON A WALK AROUND - VERTICAL FIN. - [SDR CA100223004](https://openairdocs.org/sdr/CA100223004), Feb 22, 2010: PISTON. WRONG PART. (CAN) WRONG PISTON INSTALLED INTO BRAKE ASSY, PISTON PN 092-02100 FOR BRAKE ASSY 30-67B, WAS INSTALLED IN BRAKE ASSY 30-67C BRAKE ASSY 30-67C REQUIRES NO FRICTI - [SDR CA091207002](https://openairdocs.org/sdr/CA091207002), Nov 24, 2009: FRAME. CRACKED. (CAN) A REPAIR INVOLING WELDING A CRACK APPROX 1 INCH LONG LOCATED JUST ABOVE THE LT REAR FLOAT ATTACHMENT PLATE, WITHIN THE CIRCLE OF C. FIG 2 OF SL NR 71 WAS - [SDR CA090728004](https://openairdocs.org/sdr/CA090728004), Jul 26, 2009: O-RING. CUT. MLG ACTUATOR LEAKING, O-RING FOUND TO HAVE CUT IN IT. ACTUATOR SEALS REPLACED. O-RING INTERNAL IN BULKHEAD SUPPORT BLOCK WHERE ACTUATOR RAM PASSES THROUGH. - [SDR CA081118010](https://openairdocs.org/sdr/CA081118010), Nov 18, 2008: MOUNT. CRACKED. (CAN) DURING THE 300HR/ANNUAL INSP, ENGINE MOUNT WAS BEING INSPECTED IAW AD2008-10-12 AND AIR TRACTOR`S SL NR 253C, A CRACK WAS FOUND ON THE LT LOWER ENGINE ATT - [SDR CA071016015](https://openairdocs.org/sdr/CA071016015), Sep 17, 2007: ENGINE. POWER LOSS. (CAN) THE ENGINE LOST POWER DURING FIREFIGHTING OPERATIONS RESULTING IN A FORCED LANDING. - [SDR CA071016013](https://openairdocs.org/sdr/CA071016013), Sep 14, 2007: ENGINE. POWER LOSS. (CAN) THE ENGINE LOST POWER IN FLIGHT AND THE AIRCRAFT WAS DAMAGED IN THE RESULTING FORCED LANDING. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE - [SDR CA070313009](https://openairdocs.org/sdr/CA070313009), Mar 13, 2007: FRAME. CRACKED. (CAN) DURING ANNUAL INSPECTION, THE LOWER LONGITUDINAL FRAME OF THE STAINLESS STEEL FIREGATE P/N 80450-1 WAS NOTED TO BE CRACKED AT THE FWD END AND BULGED AT TH - [SDR CA070314022](https://openairdocs.org/sdr/CA070314022), Feb 22, 2007: ENGINE. FLAMED OUT. (CAN) THE ENGINE WAS REPORTED TO HAVE FLAMED OUT IN FLIGHT. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE DETERMINED. (TC NR 20070314022) - [SDR CA051006003](https://openairdocs.org/sdr/CA051006003), Sep 5, 2005: ENGINE. FLAMED OUT. (CAN) THE ENGINE WAS REPORTED TO HAVE FLAMED OUT ON FINAL APPROACH RESULTING IN THE AIRCRAFT LANDING SHORT OF THE RUNWAY. MFG WILL INVESTIGATE THE INCIDENT AND - [SDR 2005FA0001114](https://openairdocs.org/sdr/2005FA0001114), Aug 4, 2005: SPAR. BROKEN. THE UPPER RUDDER SPAR WAS BROKEN 12.5 INCHES ABOVE THE UPPER HINGE. IN ADDITION, THE SPAR CRACKED UNDER THE UPPER HINGE FITTINGS. THIS CAUSED THE RUDDER COUNTER - [SDR CA050708005](https://openairdocs.org/sdr/CA050708005), Jul 5, 2005: PROXIMITY SWITCH. LOOSE. DURING CRUISE, THE PILOT NOTED A GEAR UNSAFE LIGHT FOR THE NLG. THE AIRCRAFT DID A LOW PASS AT THE AIRPORT. IT WAS DETERMINED THAT THE GEAR WAS DOWN AND IT APPE - [SDR CA050614008](https://openairdocs.org/sdr/CA050614008), May 18, 2005: TORQUE TUBE. CRACKED. (CAN) DURING ANNUAL INSPECTION, RUDDER TUBE ASSY WAS FOUND TO BE UNAIRWORTHY DUE TO CRACKS. - [SDR CA041118004](https://openairdocs.org/sdr/CA041118004), Nov 18, 2004: FAIRING. MISLOCATED. (CAN) DURING ANNUAL INSPECTION THE HORIZONTAL STAB FAIRING SCREW HOLES FOUND TO BE DRILLED THROUGH THE RIVETS ATTCHING THE SKIN TO THE CLOSING RIBS OF BOTH HORI - [SDR CA030909002](https://openairdocs.org/sdr/CA030909002), Sep 7, 2003: O-RING. TORN. (CAN) DURING FLIGHT 1 HYDRAULIC PUMP LIGHT ILLUMINATED INDICATING LOW HYDRAULIC FLUID LEVEL. THE LANDING GEAR WAS EXTENDED NORMALLY AND THE AIRCRAFT RETURNED TO - [SDR AUS20020022](https://openairdocs.org/sdr/AUS20020022), Jan 11, 2002: PIPE. CRACKED. (AUS) P3 PIPE TO FUEL CONTROL UNIT CRACKED. - [SDR AU010248](https://openairdocs.org/sdr/AU010248), Mar 21, 2001: STRUCTURE. DAMAGED. (AUS) RUDDER CRACKED AND SKIN DEFORMED IN UPPER AREA WHERE THE BALANCEHORN ATTACHES TO THE RUDDER STRUCTURE. - [SDR AU010249](https://openairdocs.org/sdr/AU010249), Mar 19, 2001: MOUNT. FAILED. (AUS) LT SIDE ENGINE MOUNT RUBBER ISOLATION MOUNTS FAILED. ENGINE LOW ON LT SIDE CAUSING CHAFING OF THE FIRE SEALS ON THE BEARER. - [SDR AU981393](https://openairdocs.org/sdr/AU981393), Oct 22, 1998: BOLT. FAILED. (AUS) BRAKE MASTER CYLINDER EYEBOLT FAILED AT THE LOWER END OF THE LOCKNUT CAUSING THE AIRCRAFT TO SWERVE OFF THE RUNWAY. PART TC: 800. - [SDR AU970738](https://openairdocs.org/sdr/AU970738), Jun 27, 1997: SPAR CAP. CRACKED. (AUS) RH WING LOWER SPAR CAP CRACKED FROM BOLT HOLE - CRACK LENGTH 3.048MM (0.120IN) - FOUND DURING MAGNETIC PARTICLE INSPECTION - [SDR 97ZZZM156](https://openairdocs.org/sdr/97ZZZM156), Nov 21, 1996: COMPRESSOR BLADE. SPLIT. FLT - 759 - MIA-PID - PILOT REPORTED NR 1 TORQUE 3000 AT 11,000 FEET AND T5 AT 770 DEG, NG 93 PERCENT. OTHER ENGINES RUNNING NORMAL WITH 3700 TORQUE. A/C RETURN ## STCs that may be installed (OpenAirDocs) (7) 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 SE615GL](https://openairdocs.org/stc/SE615GL): Incorporation of a fuel flow transducer. Shadin Avionics - [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) (437, 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 - [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 All of them: https://openairdocs.org/engine/u-a-canada-pt6a-65ag/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.