# U/A Canada PT6A-60 series - Type: Engine model (FAA registry) - Registry code: 61601 - Manufacturer (registry): U/A CANADA - Model: PT6A-60 - 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-60-series The registry names only the engine series, so ADs for every model in the series are matched. ## 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 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 (31) As reported by operators and repair stations, by the model named in the report. - [SDR CTYA2016040100000](https://openairdocs.org/sdr/CTYA2016040100000), Apr 1, 2016: ENGINE. POWER LOSS. PILOT REPORTED ENGINE RUNNING HOTTER THAN NORMAL, LACK OF POWER. - [SDR JVWA2016F00085](https://openairdocs.org/sdr/JVWA2016F00085), Feb 26, 2016: WINDSHIELD. CRACKED. RIGHT WINDSHIELD OUTER PANE CRACKED ABOUT 4" FROM THE INBD EDGE OF THE WINDSHIELD. - [SDR CA140630012](https://openairdocs.org/sdr/CA140630012), Jun 10, 2014: COMPRESSOR. MAKING METAL. (CAN) DURING APPROACH, PILOT FELT A STRONG VIBRATION AND AN EXCESSIVE TEMPERATURE RISE IN NR 1 ENGINE, REDUCED POWER. AFTER 2 MINUTES, THE TEMPERATURE INCREASED - [SDR CA140630020](https://openairdocs.org/sdr/CA140630020), Jun 10, 2014: COMPRESSOR WHEEL. SEIZED. (CAN) PILOTS EXPERIENCED STRONG VIBRATIONS ON ENGINE NR 1 FOLLOWED BY AN INCREASE IN INTER TURBINE TEMPERATURE (ITT). THEY ATTEMPTED TO REDUCE THE ITT TO NORMAL - [SDR CA140401013](https://openairdocs.org/sdr/CA140401013), Mar 29, 2014: FILTER. CONTAMINATED. (CAN) DURING REVENUE FLIGHT, ON APPROACH FOR LANDING, THE PILOT DID NOT HAVE ANY POWER RESPONSE FROM ENG NR 2. THE ENGINE POWER WAS LEFT AT IDLE DURING APPROACH - [SDR CA140306001](https://openairdocs.org/sdr/CA140306001), Mar 6, 2014: ENGINE. FIRE. (CAN) REPORTED THAT WHEN BEGINNING DESCENT AN ORANGE GLOW WAS SEEN COMING FROM THE ENGINE. THE ENGINE FIRE LIGHT ILLUMINATED AND THE ENGINE WAS SHUTDOWN. THE FI - [SDR CA121119014](https://openairdocs.org/sdr/CA121119014), Nov 8, 2012: FUEL CONTROL. MALFUNCTIONED. (CAN) REPORTING NO THROTTLE RESPONSE WHILE SPOOLING DOWN TO IDLE AT FL180. TROUBLESHOOTING IS ON-GOING AND FOCUSING ON THE FCU. - [SDR CA120905004](https://openairdocs.org/sdr/CA120905004), Jun 26, 2012: EXHAUST DUCT. DAMAGED. (CAN) WHEN PERFORMING A SCHEDULED FUEL NOZZLE REPLACEMENT, A TECH NOTICED WITH THE BORESCOPE A PART OF THE INNER LINER OF THE EXHAUST DUCT PROTRUDING. THE POWER - [SDR 2010FA0000888](https://openairdocs.org/sdr/2010FA0000888), Aug 25, 2010: STRAP. CRACKED. DURING A ROUTINE NR3 PHASE INSP, A CRACK WAS FOUND ON A CROSS TIE STRAP. THE STRAP LOCATION WAS ON THE RT SIDE OF THE CABIN INTERIOR AT SL 227.125. THE CRACK AP - [SDR S9BA20100003](https://openairdocs.org/sdr/S9BA20100003), Jul 13, 2010: BULKHEAD. CORRODED. LT BOTTOM SKIN ON AFT BULKHEAD HAS HOLE DUE TO CORROSION. REPAIRED HOLE IAW RD 53-387A AND RD53-387A 8110. - [SDR UVVR2010060700009](https://openairdocs.org/sdr/UVVR2010060700009), Jun 7, 2010: FITTING. CRACKED. RT ENGINE INBD ENGINE MOUNT FITTING WAS FOUND CRACKED APPROX .30 INCHES IN LENGTH DURING INSPECTION. - [SDR 2009FA0000710](https://openairdocs.org/sdr/2009FA0000710), Mar 3, 2009: BEARING. FAILED. FROM MFG: AN ELECTRICAL CURRENT FROM THE STARTER GEN OUT PUT SHAFT DISCHARGED INTO THE ENG ACCESSORY DRIVETRAIN CAUSE AN IN-FLIGHT SHUTDOWN. THE ELECTRICAL DISC - [SDR 2008F00028](https://openairdocs.org/sdr/2008F00028), Dec 3, 2008: COWLING. CRACKED. POSTFLIGHT RAMP INSP DISCLOSED THAT EACH ENG COWLING HAD SMALL CRACK FWD OF AND CONNECTING TO OTBD AFT LATCHING MECHANISM. CRACKS REPAIRED AND ACFT RETUNED TO S - [SDR CA080618003](https://openairdocs.org/sdr/CA080618003), Jun 2, 2008: SEAL. LEAKING. (CAN) DURING ENG COMPRESSOR RECOVERY WASH, ENGINE OIL LOSS FROM NR 1 BEARING SEAL. MULTIPLE ENGINE SPOOLS ARE REQUIRED TO COMPLETE AN ENG COMPRESSOR RECOVERY WA - [SDR UE5R02](https://openairdocs.org/sdr/UE5R02), Jul 5, 2007: GEARBOX. CORRODED. PT6A-60AG REDUCTION GEAR REAR HOUSING P/N 3106854-01 HAS SEVERE CORROSION ON OUTER SURFACE OF HOUSING. DEEP PITTING, SOME AREAS UP TO .125 INCH DEEP. CORRODED A - [SDR RU32005F00002](https://openairdocs.org/sdr/RU32005F00002), Jul 27, 2005: TRANSDUCER. FAILED. RT ENGINE OIL PRESSURE INDICATION WAS ABOVE 200 PSI. CREW NOTICED SLIGHT OIL SMELL IN AC. PRECAUTIONARY SHUTDOWN OF RT ENGINE IN FLIGHT. ALL OTHER INDICATIONS W - [SDR 2004FA0000805](https://openairdocs.org/sdr/2004FA0000805), Oct 1, 2004: BLOWER. OVERHEATED. SMOKE COMING FROM UNDER PILOTS FLOORBOARDS. UPON INVESTIGATION FOUND ENVIRONMENTAL BLOWER MOTOR TOO HOT TO TOUCH. AIRCRAFT LANDED SAFE WITH FIRE DEPARTMENT FOLL - [SDR AUS20040284](https://openairdocs.org/sdr/AUS20040284), Mar 19, 2004: CASE. CORRODED. (AUS) RT ENGINE AIR INLET CASE CORRODED. - [SDR I5W2003F00000](https://openairdocs.org/sdr/I5W2003F00000), Nov 5, 2003: CLEVIS. FAILED. PILOT REPORTS DURING TAKE OFF LANDING GEAR RETRACTED HARD AND MADE LOUD NOISE, AFTER LANDING A VISUAL INSPECTION WAS PERFORMED. THE NOSE ACTUATOR CLEVIS PN 2570 - [SDR ACE091103](https://openairdocs.org/sdr/ACE091103), Sep 11, 2003: PUMP. LEAKING. PILOT NOTICED FUEL LEAKING FROM ENGINE DRAIN ON PRE-FLIGHT. MAINTENANCE REPLACED THE DEFECTIVE PUMP. - [SDR GMZ2003F00000](https://openairdocs.org/sdr/GMZ2003F00000), Aug 11, 2003: BLOWER. FAILED. BLOWER MOTOR WEARS OUT CAUSING BLOWER MOTOR TO START SMOKING FILLING THE AIRCRAFT WITH SMOKE. WHEN THE BLOWER MOTOR IS REMOVED AND INSPECTED. IT IS FOUND THAT T - [SDR AW42003F00000](https://openairdocs.org/sdr/AW42003F00000), Apr 28, 2003: WINDSHIELD. CRACKED. FOLLOWING DEPARTURE, PILOT`S WINDSHIELD INNER GLASS PANE CRACKED. AIRCRAFT RETURNED TO DEPARTURE WHERE WINDSHIELD WAS REPLACED. - [SDR 0020](https://openairdocs.org/sdr/0020), Mar 3, 2003: TORQUE KNEE. CRACKED. DURING COMPLIANCE OF SB 32-3134 AND AD 2002-01-10, RIGHT LANDING GEAR UPPER TORQUE KNEE WAS FOUND TO BE CRACKED AT PROTRUSION OF CENTER LUG. THIS UNIT HAD BEEN - [SDR RU92003F00000](https://openairdocs.org/sdr/RU92003F00000), Nov 13, 2002: SQUAT SWITCH. FAILED. ON NOV. 13, 2002 GEAR FAILED TO RETRACT, SQUAT SWITCH FAILED. REPLACED SQUAT SWITCH. OPS CHECK, OK. - [SDR CA020828006](https://openairdocs.org/sdr/CA020828006), Aug 9, 2002: MOTOR. FAILED. (CAN) ELECTRIC MOTOR ON HYDRAULIC PACK - DRAWS TOO MUCH AMPENAGE. THE SYSTEM IS PROTECTED BY A 60 AMP CIRCUIT BREAKER. THIS ASSY IS OPERATING AT BELOW OR AT THE - [SDR AUS20020715](https://openairdocs.org/sdr/AUS20020715), Jun 20, 2002: BOLT. CRACKED. (AUS) LT AND RT WING UPPER REAR AND LOWER REAR ATTACHMENT BOLTS EXHIBIT SIGNS OF CRACKING IN RADIUS. FOUND DURING INSPECTION IAW AD/BEECH 300/8 AND RAYTHEON S.I - [SDR DBC2002F00002](https://openairdocs.org/sdr/DBC2002F00002), Apr 10, 2002: PRESSURE SWITCH. FAILED. SHORTLY AFTER TAKEOFF, PILOT NOTED LOW PRESSURE FUEL LIGHT ILLUMINATED. PILOT LANDED WITHOUT INCIDENT. TROUBLESHOT TO FAILED FUEL PRESSURE SWITCH. REMOVED (PN 1 - [SDR 2002FA0000364](https://openairdocs.org/sdr/2002FA0000364), Feb 28, 2002: WINDOW. CRACKED. WINDOW, LOCATED IN UPPER CABIN DOOR, WAS FOUND TO HAVE 4 CONSECUTIVE MOUNTING HOLES BROKEN ALONG LOWER EDGE. A RETAINING RING, CALLED OUT IN PARTS BOOK, WAS NOT - [SDR 20010425CW006](https://openairdocs.org/sdr/20010425CW006), Mar 15, 2001: HOSE. BURST. IN FLIGHT THE LEFT ENGINE OIL COOLER HOSE BURST CAUSING A LOSS OF OIL AND A PRECAUTIONARY ENGINE SHUTDOWN. THE PILOT MADE AN UNEVENTFUL LANDING. BEIN THAT THIS - [SDR 97ZZZX4217](https://openairdocs.org/sdr/97ZZZX4217), Aug 13, 1997: VALVE. BROKEN. DISCOVERED ON POST-FLIGHT INSPECTION, NR 1 ENGINE BLEED AIR FLOW CONTROL VALVE HAS A BROKEN CONTROL LINKAGE ARM. APPEARS LIKE BALL SOCKET WORN OUT. REPLACED BLE - [SDR AU961107](https://openairdocs.org/sdr/AU961107), Aug 9, 1996: COWLING. DOOR FAILED. (AUS) LH INBOARD ENGINE COWL DOOR SEPARATED ALONG HINGE LINE - DAMAGE TO ONE WINDOW AND MINOR SCRATCHES AND DENTS TO FUSELAGE ## STCs that may be installed (OpenAirDocs) (8) 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. Lists PT6A-60A - [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. Lists PT6A-60AG - [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. Lists PT6A-60A - [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) (464, 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 - [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 All of them: https://openairdocs.org/engine/u-a-canada-pt6a-60-series/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.