# U/A Canada PT6A-65AR - Type: Engine model (FAA registry) - Registry code: 61608 - Manufacturer (registry): U/A CANADA - Model: PT6A-65AR - Engine type: Turbo-prop - Power: 1,424 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-65ar Model codes come from the FAA registry's reference file. ## ADs that may apply (OpenAirDocs) Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. - [AD 97-04-12](https://openairdocs.org/ad/97-04-12): Compressor Bleed-off Valve · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 52 more. Effective Mar 14, 1997 ## Information bulletins (advisory) (2) - [SAIB NE-15-21](https://openairdocs.org/saib/NE-15-21): Fuel Injector Nozzle. Issued Aug 19, 2015 - [SAIB CE-03-24](https://openairdocs.org/saib/CE-03-24): . Issued Feb 19, 2003 ## Registered aircraft None registered with this engine model now. ## NTSB investigations None matched to aircraft with this engine model. ## FAA accident and incident reports None matched to aircraft with this engine model. ## Service difficulty reports (55, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR 8WWA2026F00002](https://openairdocs.org/sdr/8WWA2026F00002), Aug 31, 2025: CONTROL CABLE. CHAFED. DURING INSPECTIONS WE HAVE DISCOVERED A TREND WHERE THE TELEFLEX CABLES THAT CONNECT TO THE FCU POWER CONTROL ARE SHOWING SIGNS OF WEAR CAUSED BY CHAFING AGAINS - [SDR DATA2016081601](https://openairdocs.org/sdr/DATA2016081601), Aug 16, 2016: INDICATION SYS. FALSE INDICATION. ON APPROACH, FOLLOWING APPROACH CHECKLIST AND SELECTING GEAR DOWN, F/O NOTED THE NOSE GEAR LIGHT ILLUMINATED RED, WHILE THE GEAR LEFT AND GEAR RIGHT WERE GREEN. - [SDR CA150604016](https://openairdocs.org/sdr/CA150604016), Jun 1, 2015: HOUSING. RESTRICTED. (CAN) AN AGB HOUSING LABELED AS PN 3105662-01 WAS REMOVED DURING AN UNSCHEDULED LIGHT OVERHAUL DUE TO IMPROPER PRESERVATION. THE HOUSING WAS FOUND WITH RESTRICT - [SDR DKEA2015F00031](https://openairdocs.org/sdr/DKEA2015F00031), Feb 5, 2015: HYDRAULIC SYSTEM. OVERHEATED. HYDRAULIC TEMPERATURE GAUGES IN THE RED-ZONE WHILE IN FLIGHT. - [SDR CA120312022](https://openairdocs.org/sdr/CA120312022), Mar 9, 2012: CONTROL CABLE. FRAYED. (CAN) DURING A SCHEDULED VISUAL INSPECTION OF THE FLAP CONTROL CABLES, A BADLY FRAYED CABLE WAS DISCOVERED, WHERE THE CABLE PASSES OVER A PULLEY THAT IS SOMEWHA - [SDR AVSA2011103100002](https://openairdocs.org/sdr/AVSA2011103100002), Nov 21, 2011: ENGINE. UNKNOWN. UNKNOWN, REMOVED FROM SERVICE. - [SDR 2011FA0000720](https://openairdocs.org/sdr/2011FA0000720), Nov 1, 2011: SLEEVE. SEIZED. AFTER TAKEOFF CLIMB AT 6000 FT, CREW PULLED BACK POWER TO CRUISE. SHORTLY AFTER, TORQUE ON THE NR 2 ENGINE DROPPED AND THE LOW OIL WARNING LIGHT ILLUMINATED. TH - [SDR CA111017006](https://openairdocs.org/sdr/CA111017006), Oct 14, 2011: CIRCUIT BREAKER. UNSERVICEABLE. (CAN) ACFT RETURNED TO BASE AFTER THE ODOR OF SMOKE WAS DISCOVERED IN THE COCKPIT. UPON INSPECTION, IT WAS DISCOVERED THAT THE PILOTS RMI INTERNAL LIGHTING HAD - [SDR G78R20111006002](https://openairdocs.org/sdr/G78R20111006002), Aug 9, 2011: ENGINE. SHUTDOWN. AFTER TAKEOFF CLIMB, AT 6,000 FT, THE CREW PULLED BACK THE POWER TO CRUISE. ON THE RT ENGINE, THE TORQUE DROPPED AND LOW OIL PRESSURE LIGHT ILLUMINATED. PROPELL - [SDR DATA200900002](https://openairdocs.org/sdr/DATA200900002), Jun 7, 2009: ENGINE. POWER LOSS. UPON POWER UP FOR TAKEOFF, LT ENGINE BUFFET AND POWER LOSS. SHUTDOWN LT ENGINE. SUSPECT POWER SECTION FAILURE. - [SDR CA081029005](https://openairdocs.org/sdr/CA081029005), Sep 15, 2008: OIL SYSTEM. LEAKING. (CAN) DURING CRUISE, THE PILOTS OBSERVED ENG TEMPERATURE RISING THRU 800°C AND PEAKING OVER 1000°C. FLAMES WERE NOTICED FROM THE EXHAUST. THE ENG WAS SHUTDOWN A - [SDR DATA200700005](https://openairdocs.org/sdr/DATA200700005), Jun 20, 2007: ENGINE. POWER LOSS. WHILE IN CRUISE, LEFT ENGINE LOST POWER WITH INCREASE OF ITT TO 1200 FOLLOWED BY LOUD NOISE. FOLLOWED PROCEDURES AND SHUT DOWN ENGINE. DIVERTED TO MWA. ENGINE R - [SDR CA070628003](https://openairdocs.org/sdr/CA070628003), May 16, 2007: BOLT. FAILED. (CAN) ENGINE S/N PCE 97543 WAS REMOVED SUBSEQUENT TO IN-FLIGHT SHUTDOWN AFTER THE ENGINE OIL PRESSURE DROPPED TO (0) IN FLIGHT. METAL WAS FOUND IN THE OIL FILTE - [SDR CA070704015](https://openairdocs.org/sdr/CA070704015), May 11, 2007: ENGINE. SEIZED. (CAN) IN CRUISE, SMOKE WAS OBSERVED IN THE CABIN AND ENGINE POWER REDUCED UNCOMMANDED. THE ENGINE WAS SHUTDOWN IN FLIGHT AND THE AIRCRAFT DIVERTED TO POINT OF D - [SDR CA070514037](https://openairdocs.org/sdr/CA070514037), Mar 21, 2007: ENGINE. NOISY. (CAN) THE ENGINE EMITTED A NOISE ON TAKEOFF ROLL ACCOMPANIED BY AN UNCOMMANDED REDUCTION IN POWER. TAKEOFF WAS ABORTED. MFG WILL MONITOR INVESTIGATION OF THE EV - [SDR CA060926005](https://openairdocs.org/sdr/CA060926005), Sep 13, 2006: BLADE. CORRODED. (CAN) UPON VISUAL INSPECTION , CORROSION WAS FOUND ON THE BLADE SHANK. AFTER REWORK TO MINIMUM DIMENSION DAMAGE STILL REMAINS. BLADE WIDTH AND THICKNESS IS WELL - [SDR CA060307004](https://openairdocs.org/sdr/CA060307004), Mar 3, 2006: BOLT. FAILED. (CAN) THE POWER SECTION OF ENGINE S/N PCE-PS 97533 WAS REMOVED DUE TO SEIZED CONDITION. THE REASON FOR REMOVAL AS DESCRIBED BY THE OPERATOR WAS FAILURE ON START - [SDR CA050414011](https://openairdocs.org/sdr/CA050414011), Apr 8, 2005: CIRCUIT BREAKER. FAILED. REMOTE C/B FOR INLET HEAT STAYED IN CLOSED POSITION AND WOULD NOT OPEN. ALLOWING THE RT ENGINE INTAKE HEAT TO OPERATE WHEN AIRCRAFT POWER WAS TURNED ON AND CAUS - [SDR CA041108008](https://openairdocs.org/sdr/CA041108008), Nov 1, 2004: BRACKET. CRACKED. (CAN) BOTH ELEVATOR TRIM TAB MASS BALANCE BRACKETS WERE FOUND CRACKED DURING 9600 HOUR STRUCTURAL INSPECTION. THESE BRACKETS WERE RECENTLY REPLACED TO COMPLY WI - [SDR CA041101009](https://openairdocs.org/sdr/CA041101009), Oct 26, 2004: BOLT. FRACTURED. (CAN) ENG SHUTDOWN IN FLT DUE TO TORQUE FLUCTS & LOW OIL PRESS. 6 BOLTS USED TO ASSEMBLE 1ST STAGE CARRIER ASSY. 2 OF 6 BOLTS FAILED DURING OPS. 1 BOLT HEAD FOR - [SDR CA040722005](https://openairdocs.org/sdr/CA040722005), Jul 13, 2004: BOLT. FAILED. (CAN) THE ENGINE WAS IN FLIGHT WHEN IT SUFFERED A FAILURE. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT LANDED. AN INVESTIGATION FOUND THAT THE BOLT HEAD OF A 1ST S - [SDR CA031117008](https://openairdocs.org/sdr/CA031117008), Nov 10, 2003: LAMP. SHORTED. (CAN) PILOT NOTED ELEC BURNING ODOR. CREW DISENGAGED AC ELEC MASTER. FOUND TRANS & WIRING WARM TO TOUCH. WIRES MELTING A PLASTIC ABRASION SHIELD. DAMAGE DETECTE - [SDR CA031117007](https://openairdocs.org/sdr/CA031117007), Nov 10, 2003: LAMP. SHORTED. (CAN) TRANSFORMER IS DESIGNED TO STEP DOWN 115 VAC SUPPLY VOLTAGE TO A MAX OF 5 VAC REQUIRED BY REST OF CIRCUITRY. OUTPUT WIRES FROM ABOVE MENTIONED TRANSFORMER - [SDR CA030619003](https://openairdocs.org/sdr/CA030619003), Jun 17, 2003: CIRCUIT BREAKER. FAILED. (CAN) PILOT TURNED ON MASTER SWITCH AT BEGINNING OF DAY AND GROUND HANDLERS NOTICED SMOKE COMING FROM THE RT ENGINE INTAKE LIP HEATER. THE MASTER WAS SHUT OFF B - [SDR CA030618005](https://openairdocs.org/sdr/CA030618005), Jun 13, 2003: SWITCH. JAMMED. (CAN) THIS SWITCH SWITCHES POWER FROM EXTERNAL TO OFF AND TO INTERNAL POWER. THE SWITCH JAMMED AND IT WAS PHYSICALLY IMPOSSIBLE TO MOVE THE SWITCH TO THE OFF PO - [SDR CA030618006](https://openairdocs.org/sdr/CA030618006), Jun 13, 2003: SPRING. BROKEN. (CAN) THIS PART IS THE STRUT THAT LOCKS THE MAIN CABIN DOOR IN THE OPEN POSITION. THE INTERNAL SPRING FAILED CAUSING THE DOOR TO COME TO A SUDDEN STOP WHEN FULL - [SDR CA030422002](https://openairdocs.org/sdr/CA030422002), Apr 17, 2003: CONTROL CABLE. BROKEN. (CAN) ON APPROACH THE PILOT COULD NOT GET RT ENGINE POWER LOW ENOUGH FOR APPROACH POWER SETTING. A/C LANDED AT HIGHER THAN NORMAL POWER SETTING AND AFTER LANDIN - [SDR CA030327008](https://openairdocs.org/sdr/CA030327008), Mar 24, 2003: HOSE. LEAKING. (CAN) ON LANDING ROLLOUT BOTH STEERING AND NORMAL BRAKES WERE LOST. BOTH HYDRAULIC CAUTION LIGHTS CAME ON.THE AIRCRAFT WAS MANEUVERED OFF THE RUNWAY USING DIFFE - [SDR CA030225002](https://openairdocs.org/sdr/CA030225002), Feb 20, 2003: BRACKET. CRACKED. (CAN) BRACKET WAS INSPECTED AS PART OF A FLEET CAMPAIGN INITIATED IN-HOUSE. BRACKET WAS FOUND TO HAVE A .7500 INCH CRACK AND A .2500 INCH CRACK FROM THE OUTSIDE - [SDR CA030220005](https://openairdocs.org/sdr/CA030220005), Feb 19, 2003: BALANCE WEIGHT. SEPARATED. (CAN) AIRPORT PERSONNEL APPROACHED MAINT WITH PIECE OF METAL THAT HAD BEEN FOUND ON RUNWAY. SUSPECTED IT WAS OURS DUE TO COLOR. IDENTIFIED AS A BALANCE WEIGHT A - [SDR CA030110002](https://openairdocs.org/sdr/CA030110002), Jan 8, 2003: CONTROL CABLE. BROKEN. (CAN) PILOT REPORTED THAT FLAPS WOULD NOT EXTEND TO SELECTED POSITION. THEY WOULD FALL 2-4 DEGREES SHORT OF SELECTED POSITION. RETRACTION WAS OKAY. INVESTIGATIO - [SDR CA020926003](https://openairdocs.org/sdr/CA020926003), Sep 24, 2002: CONTROL CABLE. BROKEN. (CAN) FLAP SELECTOR CONTROL CABLE WAS FOUND BROKEN AT THE POINT WHERE THE CABLE EXITS THE FUSELAGE AND CONTINUES ON TO THE FLAP SELECTOR. A SECOND SPOT ON THE C - [SDR CA020726013](https://openairdocs.org/sdr/CA020726013), Jul 16, 2002: ENGINE. FAILED. (CAN) DURING WALKAROUND PILOTS NOTICED GRINDING NOISE COMING FROM LT ENGINE. MAINTENANCE WAS CALLED TO INVESTIGATE. GRINDING NOISE WAS COMING FROM POWER SECTION - [SDR CA020604008](https://openairdocs.org/sdr/CA020604008), Jun 3, 2002: CONTROL CABLE. FAILED. (CAN) DURING UNSCHEDULED REMOVAL OF RT FCU IT OBSERVED THAT PROP CONTROL CABLE FRAYED AT PULLEY LOCATED IN RT WING CENTER SECTION. PROP CONTROL MOVED TO ASSIST - [SDR CA020403003](https://openairdocs.org/sdr/CA020403003), Mar 25, 2002: BOSS. CORRODED. (CAN) ROUTINE INSPECTION REVEALED EXTRA PLAY IN NOSE GEAR DOORS. FURTHER INVESTIGATION SHOWED THAT 4 BOLTS HAD SHEARED. THIS WAS LIKELY DUE TO THE FACT THAT THE - [SDR CA011101015](https://openairdocs.org/sdr/CA011101015), Oct 29, 2001: GEARBOX. LEAKING. (CAN) DURING LAST 2 MINUTES OF APPROACH THE RT HYDRAULIC PRESSURE DROPPED OFF. AIRCRAFT LANDED UNEVENTFULLY AND WAS TOWED TO HANGAR. RT HYDRAULIC PUMP WAS REPLA - [SDR JJB2001F00003](https://openairdocs.org/sdr/JJB2001F00003), Sep 8, 2001: STRAINER. MISSING. DURING SCHEDULED MAINTENANCE, (FUEL TANK INSPECTION) FOUND RIGHT AFT TRANSFER PUMP FUEL STRAINER AND HOSE NOT INSTALLED ON AIRCRAFT. NOTE: NOT INSTALLED BY MFG. - [SDR JJB2001F00004](https://openairdocs.org/sdr/JJB2001F00004), Sep 8, 2001: HOSE. MISSING. DURING SCHEDULED MAINTENANCE, (FUEL TANK INSPECTION) FOUND RIGHT AFT TRANSFER PUMP FUEL STRAINER AND HOSE NOT INSTALLED ON AIRCRAFT. NOTE: NOT INSTALLED BY MFG. - [SDR JRA2002F00000](https://openairdocs.org/sdr/JRA2002F00000), Jul 14, 2001: LINE. RUPTURED. PRIOR TO TAKEOFF, RUPTURED ITS LEFT-HAND MAIN WHEEL BRAKE EXPANDER TUBE. RUPTURE CAUSED HYDRAULIC FLUID LOSS AND LEFT BRAKE LOSS. AC WAS STOPPED WITH REVERSE TH - [SDR CA010504008](https://openairdocs.org/sdr/CA010504008), Apr 7, 2001: CIRCUIT BREAKER. SHORTED. (CAN) LT ENGINE INLET HEAT OVER HEATED AND RESULTED IN DAMAGING THE INLET HEAT ASSY. THE CAUSE WAS THE REMOTE CIRCUIT BREAKER FAILURE.PILOT REPORTED LEFT INTAKE - [SDR 20010419CW014](https://openairdocs.org/sdr/20010419CW014), Mar 29, 2001: VALVE. STUCK. LEFT BRAKE DEICE VALVE STUCK IN ON POSITION. - [SDR CA010405004](https://openairdocs.org/sdr/CA010405004), Mar 25, 2001: WIRE. CHAFED. (CAN) NR 1 ENGINE LIP HEAT HARNESS. BOTH OF THE 2 MAIN CONDUCTORS (6 GAUGE WIRE) THAT SUPPLY CURRENT TO THE INLET HEAT OF THE L/H ENGINE WERE FOUND CHAFED COMPL - [SDR CA001026013](https://openairdocs.org/sdr/CA001026013), Oct 4, 2000: SELECTOR VALVE. DEFECTIVE. (CAN) PILOT REPORTED THAT THE BRAKE PRESSURE WAS BETWEEN 175 TO 200 PSI PRIOR TO LANDING. DURING INVESTIGATION, THE STEERING SELECTOR VALVE WAS FOUND TO BE DEFE - [SDR CA000118029](https://openairdocs.org/sdr/CA000118029), Dec 29, 1999: FUEL CONTROL. FAILED. (CAN) TACH VALVE GUIDE PIN BACKED OUT WHICH DAMAGED THE BALLHEAD RETAINER AND THE BEARING SEIZED. THE FCU COUPLING WAS ALSO DAMAGED AS A RESULT. PIN HAS PRELOAD - [SDR CA000110035](https://openairdocs.org/sdr/CA000110035), Nov 24, 1999: BEARING. FAILED. (CAN) PRE SB 60034-73-1 BEARING FOUND TO BE FAILING DURING ROUTINE BENCH CHECK. POST SB BEARING AVAILABLE WHICH HAS LARGER RETAINER TYPE BALL BEARINGS. - [SDR CA990907009](https://openairdocs.org/sdr/CA990907009), Aug 14, 1999: BOLTS. SHEARED. (CAN) ONE BOLT FOUND SHEARED AND BETA ROD PN B-3475A-3 WAS PULLED OUT. ON REMOVAL OF THE PROP, ANOTHER BOLT SHEARED. - [SDR PIVA11079](https://openairdocs.org/sdr/PIVA11079), Apr 7, 1998: ENGINE. FAILED. SHUT DOWN OF ONE ENGINE IN-FLIGHT PER FOLLOWING PILOT REPORT IN PIVA AFML PAGE 102793, NR 1 ENGINE FAILED IN-FLIGHT. NOTED COMPRESSOR STALL FOLLOWED BY 3 LARGE - [SDR 98ZZZX868](https://openairdocs.org/sdr/98ZZZX868), Jan 22, 1998: PACKING. BROKEN. PRECAUTIONARY SHUT DOWN OF NR 2 ENGINE IN-FLIGHT. LOW TORQUE AND LOW OIL PRESSURE. FOUND OIL LEAK ON FRONT SCAVENGE OIL TRANSFER TUBE AREA. REPLACED AS 3209-117 - [SDR CA971110001](https://openairdocs.org/sdr/CA971110001), Nov 1, 1997: GUIDE LUG PIN. WORN. (CAN) PILOT REPORTED NR 1 PROPELLER WOULD NOT COME OUT OF FEATHER. INVESTIGATION FOUND THE SNAP RING (P/N 79-1210056) OF THE LOW PITCH STOP ROD ADRIFT. FURTHER - [SDR CA960724002](https://openairdocs.org/sdr/CA960724002), Jul 16, 1996: CABLE. FRAYED. (CAN) CABLE FRAYED AT PULLEY LOCATION STA 75.45 FOR LEFT ENGINE POWER CONTROL. CABLE WAS LAST INSPECTED PER SD360-76-08R1, 414 HOURS PREVIOUSLY. COULD NOT ACHIE All 55: https://openairdocs.org/engine/u-a-canada-pt6a-65ar/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 SE00014EN](https://openairdocs.org/stc/SE00014EN): Installation of the Pratt & Whitney Engine Services, Inc. CrossCheck Engine Monitor Kit P/N HUMS-K-071-1, Rev. A on the specified PT6A engine models and kit P/N HUMS-K-071-2 on the specified A250 engine models. Pratt & Whitney Engine Services Inc - [STC SE00020EN](https://openairdocs.org/stc/SE00020EN): Installation of the Pratt & Whitney Engine Services, Inc. TrendCheck/ TrendCheck Plus Engine Monitor Kit P/N TREND-K-010-1. Pratt & Whitney Engine Services Inc - [STC SE8652SW](https://openairdocs.org/stc/SE8652SW): Installation of a flexible hose from the Propeller Primary Governor to the Fuel Control Unit. Air Tractor Inc - [STC SE01805NY](https://openairdocs.org/stc/SE01805NY): Installation of Fuel Nozzle Adapters using studs and nuts. Atlantic Turbines International Inc - [STC SE09257SC](https://openairdocs.org/stc/SE09257SC): Convert P&W Engine Models PT6A-15AG, -27, and -28, into PT6A-34 configuration. Covington Aircraft Engines, Inc - [STC SE659NE](https://openairdocs.org/stc/SE659NE): Installation of oil tank filler neck check valve, P/N TSA-76A. Aviation Components Support ## PMA parts (OpenAirDocs) (438, first 50) Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this engine model on its data sheet, so check the FAA record before relying on it. Newest first. - [3005293CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122934446820260909150736.0001): Insert, Fuel Control Drive Shaft. Core Parts LLC · PMA PQ05326NM · Replaces 3005293 · Aug 17, 2026 - [3019136CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186981497620260728184309.0001): Ring, Plastic. Core Parts LLC · PMA PQ05326NM · Replaces 3019136 · Jul 10, 2026 - [3012928CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID185594574320260728184309.0001): Spacer, Stepped. Core Parts LLC · PMA PQ05326NM · Replaces 3012928 · Jul 10, 2026 - [3022834CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159372011320260528133243.0001): Sleeve, First Stage Reduction Carrier. Core Parts LLC · PMA PQ05326NM · Replaces 3022834 · Apr 17, 2026 - [ST3277-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199989902020260311145336.0001): Gasket, Starter Generator. Core Parts LLC · PMA PQ05326NM · Replaces ST3277-01 · Feb 26, 2026 - [ST3276-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101621452020260311145336.0001): Gasket, Four-Hole. Core Parts LLC · PMA PQ05326NM · Replaces ST3276-01 · Feb 26, 2026 - [3109585-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117456133120260217165221.0001): Spacer, Oil Slinger. Core Parts LLC · PMA PQ05326NM · Replaces 3109585-01 · Feb 11, 2026 - [3010880CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111084696520260108163216.0001): Gasket, Igniter. CORE PARTS LLC · PMA PQ05326NM · Replaces 3010880 · Oct 16, 2025 - [3018008CL3AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195594091320251113202147.0001): Weight, Turbine, Balance. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3018008CL3 · Sep 23, 2025 - [3031660CL3AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178817307620251113202148.0001): Weight, Turbine, Balance. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3031660CL3 · Sep 23, 2025 - [3018008CL5AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID176043530320251113202147.0001): Weight, Turbine, Balance. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3018008CL5 · Sep 23, 2025 - [3018008CL4AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID167757909020251113202147.0001): Weight, Turbine, Balance. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3018008CL4 · Sep 23, 2025 - [3018008CL2AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID160336366220251113202147.0001): Weight, Turbine, Balance. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3018008CL2 · Sep 23, 2025 - [3018008CL1AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143949810220251113202146.0001): Weight, Turbine, Balance. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3018008CL1 · Sep 23, 2025 - [3031660CL1AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132736100820251113202148.0001): Weight, Turbine, Balance. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3031660CL1 · Sep 23, 2025 - [3031660CL5AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID104430369720251113202149.0001): Weight, Turbine, Balance. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3031660CL5 · Sep 23, 2025 - [3031660CL2AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102794227220251113202148.0001): Weight, Turbine, Balance. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3031660CL2 · Sep 23, 2025 - [3031660CL4AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102269369120251113202148.0001): Weight, Turbine, Balance. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3031660CL4 · Sep 23, 2025 - [3034292WFC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166533215020250624152909.0001): Disposable Oil Filter Element. Donaldson Company Inc · PMA PQ2432CE · Replaces 3034292, 3034293, 3958257-01, 3028419… · Jun 2, 2025 - [3034507WFC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141045710620250624152910.0001): Cleanable Oil Filter Element. Donaldson Company Inc · PMA PQ2432CE · Replaces 3017383, 3020967, 3022069, 3022070… · Jun 2, 2025 - [3034393WFC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID100181403420250624152909.0001): Disposable Oil Filter Element. Donaldson Company Inc · PMA PQ2432CE · Replaces 3034393, 3033315, 3059257-01, 3028419… · Jun 2, 2025 - [WF334552](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID147857861520250602133017.0001): Compressor Air Filter. Donaldson Company Inc · PMA PQ2432CE · Replaces 3029268, Alternate: 3028856, 3029267… · May 23, 2025 - [WF337408](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125475616820250602133039.0001): Filter Element Assy, Fuel. Donaldson Company Inc · PMA PQ2432CE · Replaces 217384-1, 26281 · May 23, 2025 - [3109767-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180344174520260108163021.0001): Seal, Air, Power Turbine Rotor. CORE PARTS LLC · PMA PQ05326NM · Replaces 3109767-01 · May 15, 2025 - [3115091-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180857219920250923184724.0001): Ball, Plastic, 0.750. CORE PARTS LLC · PMA PQ05326NM · Replaces 3115091-01 · Feb 13, 2025 - [3058971-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110906306720250923184724.0001): Valve Assy, Oil Filler Tube. CORE PARTS LLC · PMA PQ05326NM · Replaces 3058971-01 · Feb 13, 2025 - [3049870-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID120826506620260108162918.0001): Washer, Key. CORE PARTS LLC · PMA PQ05326NM · Replaces 3049870-01 · Jan 17, 2025 - [3049869-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117447801820260108162917.0001): Washer, Key. CORE PARTS LLC · PMA PQ05326NM · Replaces 3049869-01 · Jan 17, 2025 - [3012414AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169774044220250106202801.0001): Nut, Self-Locking, 12 Point. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3012411 · Dec 10, 2024 - [3012414AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164469161820250106202800.0001): Nut, Self-Locking, 12 Point. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3012413 · Dec 10, 2024 - [3012414AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152753542620250106202759.0001): Nut, Self-Locking, 12 Point. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3012414 · Dec 10, 2024 - [3012414AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117377138920250106202801.0001): Nut, Self-Locking, 12 Point. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3012412 · Dec 10, 2024 - [3112397-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184407500420250605164147.0001): Ring, Retaining, Compressor Turbine. CORE PARTS LLC · PMA PQ05326NM · Replaces 3112397-01 · Oct 31, 2024 - [3112375-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180129798320250605164147.0001): Stop, Ring, Compressor Turbine. CORE PARTS LLC · PMA PQ05326NM · Replaces 3112375-01 · Oct 31, 2024 - [3105135-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182128581420241202221130.0001): Washer, Flat. CORE PARTS LLC · PMA PQ05326NM · Replaces 3105135-01 · Aug 22, 2024 - [3012675AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID196954661720240919140845.0001): Nut, Self-Locking, Hex. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3012675, 3005816, 3012674, 3028286… · Aug 7, 2024 - [3015234AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID130436253520240919140838.0001): Nut, Self-Locking, Shank. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3015234, 3015233, 3015232, 3016299… · Aug 7, 2024 - [3120298-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID146494060120241202220950.0001): Shroud, Power Turbine. CORE PARTS LLC · PMA PQ05326NM · Replaces 3120298-01 · Apr 30, 2024 - [3006523CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132375139220240509162259.0001): Bearing, Sleeve, Flanged. CORE PARTS LLC · PMA PQ05326NM · Replaces 3006523 · Mar 25, 2024 - [3003987CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125662034220231204145325.0001): Pin, Lock. CORE PARTS LLC · PMA PQ05326NM · Replaces 3003987 · Aug 1, 2023 - [3016598CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189342823620231204151230.0001): Washer, Key. CORE PARTS LLC · PMA PQ05326NM · Replaces 3016598 · Jul 26, 2023 - [3024146CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID175684471820231204151231.0001): Washer, Key. CORE PARTS LLC · PMA PQ05326NM · Replaces 3024146 · Jul 26, 2023 - [ST6202-011CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121242960820241204145238.0001): Packing, Preformed. CORE PARTS LLC · PMA PQ05326NM · Replaces ST6202-011 · Jun 15, 2023 - [3032255CL3CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID196126098120250611143004.0001): Weight, Balance, Compressor. CORE PARTS LLC · PMA PQ05326NM · Replaces 3032255CL3 · May 19, 2023 - [3036722CL1CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149331980920250611143005.0001): Weight, Balance, Compressor. CORE PARTS LLC · PMA PQ05326NM · Replaces 3036722CL1 · May 19, 2023 - [3032255CL4CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID148251690420250611143004.0001): Weight, Balance, Compressor. CORE PARTS LLC · PMA PQ05326NM · Replaces 3032255CL4 · May 19, 2023 - [3032255CL2CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134931261520250611143004.0001): Weight, Balance, Compressor. CORE PARTS LLC · PMA PQ05326NM · Replaces 3032255CL2 · May 19, 2023 - [3036722CL2CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128652215520250611143005.0001): Weight, Balance, Compressor. CORE PARTS LLC · PMA PQ05326NM · Replaces 3036722CL2 · May 19, 2023 - [3032255CL1CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115337523020250611143004.0001): Weight, Balance, Compressor. CORE PARTS LLC · PMA PQ05326NM · Replaces 3032255CL1 · May 19, 2023 - [CH92106-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182950761420231024191314.0001): Exciter-Ignition. Champion Aerospace LLC · PMA PQ1287CE · Replaces Champion… · May 12, 2023 All of them: https://openairdocs.org/engine/u-a-canada-pt6a-65ar/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.