# Pratt & Whitney Canada PT6A-67D

- Type: Engine model (FAA registry)
- Registry code: 52210
- Manufacturer (registry): P&W CANADA
- Model: PT6A-67D
- Engine type: Turbo-prop
- Power: 1,279 hp
- Data sheet: [TCDS E26NE](https://openairdocs.org/tcds/E26NE) (OpenAirDocs)
- Holder: Pratt & Whitney Canada Corp.
- Installed in: 10 registered aircraft
- Page: https://openairdocs.org/engine/pratt-whitney-canada-pt6a-67d

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 2024-04-51](https://openairdocs.org/ad/2024-04-51): Turbine Section · Pratt & Whitney Canada PT6A-64, PT6A-66, PT6A-66A and 17 more. Effective Mar 28, 2024
- [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
- [AD 95-13-08](https://openairdocs.org/ad/95-13-08): Compressor Turbine Disk · Pratt & Whitney Canada PT6A-67D. Effective Jul 12, 1995

## Information bulletins (advisory) (1)

- [SAIB NE-15-21](https://openairdocs.org/saib/NE-15-21): Fuel Injector Nozzle. Issued Aug 19, 2015

## Registered aircraft (10)

- [N157CK](https://openairdocs.org/aircraft/N157CK): [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE), [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake), built 1995, S/N UE157
- [N1902D](https://openairdocs.org/aircraft/N1902D): [Boeing Co](https://openairdocs.org/faa-owner/BOEING%20CO), [Berkeley, MO](https://openairdocs.org/faa-place/MO/Berkeley), built 1998, S/N UE327
- [N190AW](https://openairdocs.org/aircraft/N190AW): [Csi 135 Division LLC](https://openairdocs.org/faa-owner/CSI%20135%20DIVISION%20LLC), [Albuquerque, NM](https://openairdocs.org/faa-place/NM/Albuquerque), built 1999, S/N UE-382
- [N195AW](https://openairdocs.org/aircraft/N195AW): [Csi 135 Division LLC](https://openairdocs.org/faa-owner/CSI%20135%20DIVISION%20LLC), [Albuquerque, NM](https://openairdocs.org/faa-place/NM/Albuquerque), built 1993, S/N UE-128
- [N418LC](https://openairdocs.org/aircraft/N418LC): [Alpine Aviation Inc](https://openairdocs.org/faa-owner/ALPINE%20AVIATION%20INC), [Provo, UT](https://openairdocs.org/faa-place/UT/Provo), built 1993, S/N UE-118
- [N60MJ](https://openairdocs.org/aircraft/N60MJ): [Alpine Aviation Inc](https://openairdocs.org/faa-owner/ALPINE%20AVIATION%20INC), [Provo, UT](https://openairdocs.org/faa-place/UT/Provo), built 1993, S/N UE-60
- [N660MW](https://openairdocs.org/aircraft/N660MW): [Marvin Lumber And Cedar Co](https://openairdocs.org/faa-owner/MARVIN%20LUMBER%20AND%20CEDAR%20CO), [Warroad, MN](https://openairdocs.org/faa-place/MN/Warroad), built 1996, S/N UE-215
- [N680MW](https://openairdocs.org/aircraft/N680MW): [Marvin Lumber And Cedar Co](https://openairdocs.org/faa-owner/MARVIN%20LUMBER%20AND%20CEDAR%20CO), [Warroad, MN](https://openairdocs.org/faa-place/MN/Warroad), built 1999, S/N UE-362
- [N716MJ](https://openairdocs.org/aircraft/N716MJ): [Alpine Aviation Inc](https://openairdocs.org/faa-owner/ALPINE%20AVIATION%20INC), [Provo, UT](https://openairdocs.org/faa-place/UT/Provo), built 1992, S/N UE-16
- [N717LC](https://openairdocs.org/aircraft/N717LC): [Aircraft Capital Partners LLC](https://openairdocs.org/faa-owner/AIRCRAFT%20CAPITAL%20PARTNERS%20LLC), [Bozeman, MT](https://openairdocs.org/faa-place/MT/Bozeman), built 1992, S/N UE-17

## NTSB investigations

None matched to aircraft with this engine model.

## FAA accident and incident reports (2)

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.

- [Incident 20200608007919I](https://openairdocs.org/incident/20200608007919I), Jun 8, 2020: Beech 1900D (N60MJ), Minot, ND, No damage. While starting his descent, the pilot noticed the rudder pedals seemed very loose and went to max travel in each direction with no apparent rudder movement.…
- [Incident 20191104022619I](https://openairdocs.org/incident/20191104022619I), Nov 4, 2019: Beech 1900D (N716MJ), Sioux Falls, SD, Minor damage. On November 4, 2019 at approximately 8:45 pm CST a Beech 1900D registration number N716MJ registered to alpine aviation express LLC had an incident (struck a…

## Service difficulty reports (1,812, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR TIMA20250603003](https://openairdocs.org/sdr/TIMA20250603003), Jun 3, 2025: ENGINE. POWER LOSS. AFTER LEVELING OFF AT 14000' LEFT FUEL PRESSURE ANNUNCIATION CAME ON, STNADBY PUMP TURNED ON, FUEL PRESSURE ANNUMC REMAINED ON, FLOW DROPPED, ENGINE ROLLED BACK
- [SDR TIMA2024071105007](https://openairdocs.org/sdr/TIMA2024071105007), Jul 5, 2024: ENGINE. POWER LOSS. AFTER DESCENDING AND LEVELING OFF LEFT ENGINE TORQUE NOT RISISNG PROPERLY AND INCORRECT ENGINE CONTROL/FEEL, PILOT NOTICED IMPROPER PWOER OUT OF LEFT ENGINE AND
- [SDR TIMA20240705007](https://openairdocs.org/sdr/TIMA20240705007), Jul 5, 2024: ENGINE. LOW TORQUE. AFTER DESCENDING AND LEVELING OFF LEFT ENGINE TORQUE NOT RISING PROPERLY AND INCORRECT ENGINE CONTROL / FEEL, PILOT NOTICED IMPROPER POWER OUT OF LEFT ENGINE AN
- [SDR CA190621007](https://openairdocs.org/sdr/CA190621007), Jun 20, 2019: TORQUE TUBE. CRACKED. (CAN) DURING HEAVY CHECK 3RD PARTY MRO IDENTIFED RUDDER TORQUE SHAFT LOOSE AND A CIRCUMFERENTIAL CRACK.
- [SDR CA190513002](https://openairdocs.org/sdr/CA190513002), May 11, 2019: PRESSURE SWITCH. LEAKING. (CAN) AFTER DEPARTING OUT OF XXX WE HAD THE #2 ENGINE BOUNCING BETWEEN 4000-2500 TORQUE, AT 400 FEET WE BROUGHT POWER BACK TO CLIMB POWER AND THE TORQUE WAS STE
- [SDR CA190501023](https://openairdocs.org/sdr/CA190501023), May 1, 2019: SCREW. DAMAGED. (CAN) UPON APPROCH INTO XXXX, FLIGHT CREW OF C-XXXX ATTEMPTED TO SELECT GEAR DOWN. `LANDING GEAR CONTROL` CIRCUIT BREAKER FOUND TO BE `POPPED`. BREAKER RESET & 
- [SDR CA190415001](https://openairdocs.org/sdr/CA190415001), Apr 13, 2019: GOVERNOR. WEAK. (CAN) LEFT ENGINE AUTO FEATHER ENGAGED ON APPROACH PILOT REPORTED PROP FEATHERED FOR ABOUT 3 SEC WHEN POWER WAS REDUCED BEFORE SELECTING FLAP 35. IT CAUSED THE 
- [SDR CA190403020](https://openairdocs.org/sdr/CA190403020), Apr 3, 2019: PUSHROD. WORN. (CAN) DURING INSPECTION IT WAS DISCOVERED THAT THERE WAS WEAR ON THE RH POWER LEVER PEDESTAL PUSH ROD. IT WAS DETERMINED TO ORIGINATE FROM INTERFERENCE WITH THE
- [SDR CA181015014](https://openairdocs.org/sdr/CA181015014), Oct 12, 2018: BUSS BAR. CORRODED. (CAN) DURING TROUBLE SHOOTING FOUND OUT THAT BUS BAR WAS CORRODED AND NOT MAKING PROPER CONTACTS WHEN GPU IS ATTACHED. BUS BAR WAS REPLACED ALONG WITH RECEPTACL
- [SDR CA180707001](https://openairdocs.org/sdr/CA180707001), Jul 4, 2018: TRANSDUCER. DISCONNECTED. (CAN) ATTACH SCREWS P/N MS24693-S24 BECAME FREE OF WHEEL SPEED TRANSDUCER P/N 140-04715. TRANSDUCER WAS ABLE TO SHIFT INSIDE THE AXLE ALLOWING FOR THE TRANSDUCE
- [SDR CA180222015](https://openairdocs.org/sdr/CA180222015), Feb 16, 2018: LANDING GEAR. DAMAGED. (CAN) DURING PUSH BACK IN YUL, DUE TO ICY CONDITION NOSE STEERING EXCEEDED NOSE GEAR STEERING LIMIT AND DAMAGE TO STEERING BUNGEE, SHIMMY DAMPER, GUIDE AND ALIG
- [SDR GLBA2016042500583](https://openairdocs.org/sdr/GLBA2016042500583), Apr 24, 2016: PCB. FAULTY. PILOT REPORTED THAT THE AUTOFEATHER ARMED WITH N1 ABOUT 95%, AFX DISABLE ILLUMINATED & RT AUTOFEATHER FAILED TO ARM. REPLACED PCB A123, PN ON & OFF 129-364091-9
- [SDR GLBA2016041400580](https://openairdocs.org/sdr/GLBA2016041400580), Apr 14, 2016: UNKNOWN. MALFUNCTIONED. PILOT REPORTED THAT THEY HAD UNSCHEDULED AUTOFEATHER CYCLING ON FINAL. PERFORMED AUTOFEATHER OPERATIONAL CHECKS & COULD NOT DUPLICATE DISCREPANCY SIGNED OFF USI
- [SDR GLBA2016040800579](https://openairdocs.org/sdr/GLBA2016040800579), Apr 5, 2016: AUTOFEATHER SYS. UNKNOWN. PILOT REPORTED THAT THE LT ENG AUTO FEATHER CYCLED SEVERAL TIMES ON APPROACH. COMPLIED WITH FCD 1900-08-61-01, NO DEFECTS NOTED.
- [SDR CA160229004](https://openairdocs.org/sdr/CA160229004), Feb 26, 2016: HOSE. LEAKING. (CAN) ON APPROACH WITH GEAR SELECTED TO THE DOWN POSITION THE CREW NOTICED THERE WERE NO THREE GREEN OR RED GEAR HANDLE LIGHTS ILLUMINATED. THE GEAR WAS CYCLED 
- [SDR CA160209004](https://openairdocs.org/sdr/CA160209004), Feb 4, 2016: ANGLE. CRACKED. (CAN) DURING A STRUCTURAL INSPECTION MAINTENANCE FOUND THE RH CLOSING ANGLE CRACKED 1.5 INCHES RFS 303. CLOSING ANGLE CRACK WAS REPAIRED IAW CAS ENGINEERING EA 
- [SDR CA160202006](https://openairdocs.org/sdr/CA160202006), Feb 2, 2016: LINE. MELTED. (CAN) DURING INSPECTION FOUND RT TAILET DE-ICE BOOT NOT INFLATING. HAD POSITIVE INDICATION, DE-ICE BOOT SHOULD BE INFLATED. FOUND DE-ICE LINE TO TAILET MELTED B
- [SDR CA160203021](https://openairdocs.org/sdr/CA160203021), Feb 1, 2016: CONNECTOR. BROKEN. (CAN) ON DEPARTURE, THE CREW REPORTED THAT THE GEAR WOULD NOT RETRACT AFTER DEPARTURE WHEN THE HANDLE WAS SELECTED TO THE UP POSITION. 3 GREEN LIGHT EXTINGUISHE
- [SDR CA160202001](https://openairdocs.org/sdr/CA160202001), Jan 25, 2016: ACTUATOR. CRACKED. (CAN) LEFT MLG END CAP INSPECTION CARRIED OUT INDICATION OF CRACK FOUND BY NDI. LEFT MLG ACTUATOR REPLACED.
- [SDR CA160118009](https://openairdocs.org/sdr/CA160118009), Jan 18, 2016: SWITCH. FAULTY. (CAN) MAINTENANCE WERE UNABLE TO SILENCE LANDING GEAR WARNING HORN ONCE ACTIVATED. TROUBLESHOOTING REVEALED THAT THE RT MLG SWITCH ASSY, A108 WAS AT FAULT. THE 
- [SDR CA160118013](https://openairdocs.org/sdr/CA160118013), Jan 15, 2016: SPAR CAP. CORRODED. (CAN) DURING PLATE NUT INSPECTION AT OTBD LT HORIZONTAL STABILIZER, CORROSION WAS FOUND ON LOWER SPAR CAP AT PLATE NUTS AND 2 FASTENERS JUST INBD OF CENTER ELEV
- [SDR CA160120010](https://openairdocs.org/sdr/CA160120010), Jan 14, 2016: TRUSS. CRACKED. (CAN) DURING A H-CHECK NDT INSPECTION OF AN ENGINE MOUNT IAW MFG RECOMMENDATIONS A SUSPECT CRACK WAS INDICATED IN 1 OF THE WELDED AREAS. THE SUBJECT ENGINE TRUS
- [SDR CA160118004](https://openairdocs.org/sdr/CA160118004), Jan 7, 2016: ACTUATOR. WORN. (CAN) DURING A DAILY INSPECTION, THE RT FLAP WAS FOUND TO HAVE EXCESSIVE PLAY. UPON INSPECTION FOUND INBD FLAP ACTUATOR HAD EXCESSIVE END PLAY AND WAS REMOVED F
- [SDR CA160106007](https://openairdocs.org/sdr/CA160106007), Jan 5, 2016: SUPPORT BRACKET. DAMAGED. (CAN) GPU POWER PLUG AND STRUCTURAL SUPPORT BRACKET FOUND DAMAGED DURING LINE INSPECTION. GROUND POWER STRUCTURAL BASE BRACKET REPAIRED. REPAIR PORTION OF BRACK
- [SDR CA160108008](https://openairdocs.org/sdr/CA160108008), Jan 4, 2016: SKIN. DAMAGED. (CAN) LT AND RT L/E SKINS FOUND DAMAGED AT HSS 5.00. LY L/E SKIN AND DOUBLER AT HSS 5.00 REPAIRED. DAMAGE SKIN AND DOUBLER TRIMMED AWAY. SKIN INSERTION MADE FRO
- [SDR CA151229020](https://openairdocs.org/sdr/CA151229020), Dec 27, 2015: SPAR CAP. CRACKED. (CAN) DURING COMPLETION OF AN I-CHECK AND AD2013-24-03, CRACKING IN VERTICAL STABILIZER. MAINTENANCE DISCOVERED THAT BOTH LT AND RT VERTICAL STABILIZER. SPAR CA
- [SDR CA151223007](https://openairdocs.org/sdr/CA151223007), Dec 20, 2015: PROXIMITY SWITCH. OUT OF ADJUST. (CAN) ON APPROACH CREW REPORTED RT MAIN GEAR WAS NOT INDICATING DOWN AND LOCKED WHEN IN THE AIR AND GEAR HANDLE IS IN THE DOWN POSITION. CHECKLIST PROCEDURES CA
- [SDR CA151221008](https://openairdocs.org/sdr/CA151221008), Dec 19, 2015: UPLOCK SWITCH. CORRODED. (CAN) CREW REPORTED LANDING GEAR INDICATION CIRCUIT BREAKER POPPED. LOST THREE (3) GREEN INDICATION. CREW FOLLOWED CHECKLIST, RESET CB, 3 GREEN INDICATION WAS E
- [SDR CA151218003](https://openairdocs.org/sdr/CA151218003), Dec 17, 2015: DISPLAY. MALFUNCTIONED. (CAN) ELECTRICAL BURNING ODOR WAS DETECTED DURING FLIGHT, ISAT SYS CONTROL PANEL WAS SUSPECTED THE SOURCE. ISAT CIRCUIT BREAKER PULLED. ISAT CONTROL HEAD INSPEC
- [SDR CA151221001](https://openairdocs.org/sdr/CA151221001), Dec 17, 2015: KEELBEAM. CRACKED. (CAN) INBD KEEL WEB FLANGE, PN: 114-980024 OF RT NACELLE FOUND CRACKED APPROXIMATELY 1.0 IN LENGTH. REPAIR CARRIED OUT. DAMAGED PORTION OF KEEL WEB FLANGE REMOV
- [SDR CA151207007](https://openairdocs.org/sdr/CA151207007), Dec 4, 2015: PACKING. LEAKING. (CAN) DURING REPLACEMENT OF AN ENGINE OIL FILTER MAINTENANCE FOUND A BATCH OF AS3209-224 RINGS, ENGINE OIL FILTER, THE ONE THAT GOES AROUND THE OUTSIDE OF THE F
- [SDR CA160208002](https://openairdocs.org/sdr/CA160208002), Dec 4, 2015: GAS GENERATOR. DAMAGED. (CAN) ENGINE WAS SENT TO O/H SHOP WITH THE OPERATOR REPORTING METAL IN OIL. DUE TO THE TSO OF THE POWER SECTION BEING 7597HRS, THE OPERATOR ELECTED TO REPAIR TH
- [SDR CA151201011](https://openairdocs.org/sdr/CA151201011), Nov 30, 2015: SWITCH. OUT OF ADJUST. (CAN) WHILE ENROUTE THE CREW NOTICED THE, CARGO DOOR, ANNUNCIATOR HAD ILLUMINATED. THE CREW ELECTED TO DIVERT TO AIRPORT AS MAINTENANCE PERSONNEL WERE AVAILABLE
- [SDR CA151130011](https://openairdocs.org/sdr/CA151130011), Nov 28, 2015: SWITCH. OUT OF ADJUST. (CAN) ON A FLIGHT THE CREW NOTICED THE, CABIN DOOR, WARNING LIGHT WAS ILLUMINATED. THE CREW ELECTED TO RETURN TO THE AIRPORT AS MAINTENANCE WAS AVAILABLE AT THI
- [SDR CA151202004](https://openairdocs.org/sdr/CA151202004), Nov 27, 2015: ENGINE. OVERTEMP. (CAN) ENGINE WAS SENT FOR REPAIR WITH THE OPERATOR REPORTING AN IN FLIGHT-SHUTDOWN IFSD, THE ENGINE TEMPERATURE CLIMBED BEYOND NORMAL OPERATING LEVELS. NO OVERT
- [SDR CA151210006](https://openairdocs.org/sdr/CA151210006), Nov 24, 2015: STRINGER. CORRODED. (CAN) DURING A SCHEDULED FUEL TANK INSPECTION UTILIZING X-RAY THE FOLLOWING DEFECTS WERE NOTED. LEFT LOWER STR CORRODED BETWEEN LT WING STA 114-124 AT 39.5 PERC
- [SDR CA151125009](https://openairdocs.org/sdr/CA151125009), Nov 23, 2015: DUCT. CRACKED. (CAN) BRAKE DEICE WARNING ILLUMINATED IN FLIGHT. FOUND CRACK ON BLEED AIR DUCT 129-550067-1 CAUSING EVA TUBE TO MELT AND TRIGGER LIGHT.
- [SDR CA160106002](https://openairdocs.org/sdr/CA160106002), Nov 22, 2015: SWITCH. OUT OF ADJUST. (CAN) CREW REPORTED A DOOR UNSAFE LIGHT ON DEPARTURE. THE CREW CANCELLED IFR AND RETURNED TO THE AIRPORT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISP
- [SDR CA151116009](https://openairdocs.org/sdr/CA151116009), Nov 13, 2015: FRAME. CRACKED. (CAN) DURING STRUCTURAL INSPECTION A-CHECK ITEM 37, WHICH STATES AT FS 288 CHECK FOR STRESSED AND MISSING FASTENERS ON THE LOWER FUSELAGE BULKHEAD, PN 114-43009
- [SDR CA151201010](https://openairdocs.org/sdr/CA151201010), Nov 13, 2015: OIL SYSTEM. PRESSURE LOSS. (CAN) THE AIRCRAFT WAS ON A FLIGHT AND WAS DIVERTED DUE TO LOSS OF OIL PRESSURE. THE PILOT NOTICED THE OIL PRESSURE DROPPING OFF LINE AND THE TQ WAS FLUCTUATING
- [SDR CA151120002](https://openairdocs.org/sdr/CA151120002), Nov 10, 2015: OIL SYSTEM. LOW PRESSURE. (CAN) AIRCRAFT LOST OIL PRESSURE ON RT ENGINE IN CRUISE FLIGHT. AS A RESULT, AUTOFEATHER ENGAGED AND RT PROPELLER FEATHERED. CREW DECLARED EMERGENCY AND LANDED 
- [SDR CA151106006](https://openairdocs.org/sdr/CA151106006), Nov 2, 2015: ACTUATOR. BINDING. (CAN) AFTER LANDING THE FLIGHT CREW PERFORMED THE AFTER LANDING CHECKLIST AND SELECTED THE FLAPS TO FULL UP POSITION THEY NOTICED THAT THE INDICATOR STOP AT THE
- [SDR CA151121002](https://openairdocs.org/sdr/CA151121002), Nov 2, 2015: WIRE HARNESS. BURNED. (CAN) PILOT REPORTED LT PROPELLER HEAT AMPERAGE INDICATING "LOW". UPON FURTHER EXAMINATION/TROUBLESHOOTING, MAINTENANCE DISCOVERED THE PROP HEAT WIRING HARNESS 
- [SDR CA151103008](https://openairdocs.org/sdr/CA151103008), Nov 1, 2015: ANGLE. OUT OF POSITION. (CAN) THE PILOT REPORTED THAT THE LT ENGINE WOULD ONLY STAY IN FEATHER IF THE PROP CONTROL LEVER IS HELD DOWN. IT WAS NOTED THAT THE AUTO FEATHER SYS TESTED SER
- [SDR CA151102008](https://openairdocs.org/sdr/CA151102008), Oct 31, 2015: SHAFT. SHEARED. (CAN) ELEVATOR TRIM ISSUE IN FLIGHT. TRIM ACTUATOR SHAFT FOUND SHEARED.
- [SDR CA151027001](https://openairdocs.org/sdr/CA151027001), Oct 25, 2015: ENGINE. POWER LOSS. (CAN) FLIGHT CREW NOTICED LT BLEED FAIL DURING TAKEOFF, JUST AFTER, THE LT TORQUE DECREASED ALONG WITH THE LT PROP RPM. THE ITT STARTED TO INCREASE BEFORE THE C
- [SDR CA151031004](https://openairdocs.org/sdr/CA151031004), Oct 25, 2015: GEARBOX. DAMAGED. (CAN) ON THE CLIMBOUT THE CREW OBSERVED ABNORMAL TORQUE AND ITT INDICATIONS. AS A PRECAUTION, THE CREW ELECTED TO SHUTDOWN THE LT ENGINE. THE ACFT RETURNED WHER
- [SDR CA151019007](https://openairdocs.org/sdr/CA151019007), Oct 19, 2015: LINE. CRACKED. (CAN) LINE CRACKED AT FLARED AREA.
- [SDR CA151022010](https://openairdocs.org/sdr/CA151022010), Oct 19, 2015: SENSOR. DIRTY. (CAN) AFTER TAKEOFF WHILE ENROUTE AND CLIMBING THROUGH 3500 ASL, THE CARGO DOOR LIGHT AND MASTER WARNING ILLUMINATED. A DECISION WAS MADE TO RETURN PROMPTLY SUS
- [SDR CA151016009](https://openairdocs.org/sdr/CA151016009), Oct 15, 2015: LINE. CRACKED. (CAN) BLEED AIR LINE CRACKED AND SEPARATED AROUND FLANGE AREA THAT MOUNTS TO LT ENGINE FIRE WALL CAUSING BLEED AIR FAIL INDICATION.

All 1,812: https://openairdocs.org/engine/pratt-whitney-canada-pt6a-67d/reports.md

## PMA parts (OpenAirDocs) (387, 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
- [3112608-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171267029020260217165222.0001): Spacer, Oil Slinger. Core Parts LLC · PMA PQ05326NM · Replaces 3112608-01 · 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
- [3120980-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118510848020260108163102.0001): Seal, Turbine Blade. CORE PARTS LLC · PMA PQ05326NM · Replaces 3120980-01 · Jul 14, 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
- [WF336238](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID112708987520250602133027.0001): Compressor Air Filter Element. Donaldson Company Inc · PMA PQ2432CE · Replaces 3038142, P-1139 · 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
- [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
- [3058-132ACD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID107388137220240926215417.0001): Seal. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 3058-132 · Sep 11, 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
- [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
- [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
- [3032255CL5CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134796264620250611143005.0001): Weight, Balance, Compressor. CORE PARTS LLC · PMA PQ05326NM · Replaces 3032255CL5 · 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
- [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/pratt-whitney-canada-pt6a-67d/pma.md

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