# Service difficulty reports: Pratt & Whitney Canada PT6A-67R

A list on [Pratt & Whitney Canada PT6A-67R](https://openairdocs.org/engine/pratt-whitney-canada-pt6a-67r.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 95 reports

- [SDR DATA07092021001](https://openairdocs.org/sdr/DATA07092021001.md): Governor · inoperative · Jul 7, 2021 · N764JR · Stbros SD360300 · Propeller Governor
  > AT 10,000 MSL ON CLIMB THE NUMBER 2 PROPELLER RPM SLOWLY STARTED TO DECREASE. AN ATTEMPT TO FORWARD THE PROPELLER LEVER CAUSED THE RPM DECREASE TO CONTINUE. THE ENGINE WAS SHUT DOWN IN FLIGHT, AN EMERGENCY WAS DECLARED AND THE CREW RETURNED THE AIRCRAFT TO THE
- [SDR DATA2021030901](https://openairdocs.org/sdr/DATA2021030901.md): Gas Generator · low torque · Mar 8, 2021 · N972AA · Stbros SD360300 · Turbine Engine Combustion Section
  > DURING CLIMB CHECKS FLIGHT CREW OBSERVED THE RIGHT PROPELLER RPM DROPPED TO THE 800 RANGE. THE MOVED THE ENGINE CONTROL LEVERS FORWARDS AND BACKWARDS ON THE AFFECTED ENGINE AND OBSERVED NO CHANGE IN THE RPM. AT THIS TIME THE ENGINE TORQUE DECREASED. CREW DECLA
- [SDR EXDA2019092500000](https://openairdocs.org/sdr/EXDA2019092500000.md): Engine · flamed out · Sep 20, 2019 · N973AA · Stbros SD360 · Engine (Turbine/Turboprop)
  > WHILE ENROUTE FROM KSUS TO KDTO THE RIGHT ENGINE HAD AN UNCOMMANDED SHUT DOWN IN FLIGHT. THE FLIGHT CREW ASKED ACT TO LAND AT THE NEAREST AIRPORT. THE AIRCRAFT WAS CLEARED TO LAND AT KFSM WITHOUT ANY FURTHER PROBLEMS.
- [SDR CA190808009](https://openairdocs.org/sdr/CA190808009.md): Rod End · cracked · Jul 30, 2019 · Doug DC3C · Trailing Edge Flap Control System
  > (CAN) UPON INSPECTION OF FLAP OPERATING INSPECTION, IT WAS NOTED THAT THE FLAP ON THE L/H SIDE, PUSH/PULL ROD ON IIB SIDE, IIB ROD END WAS BENT A SIGNIFICANT AMOUNT TO CRACK, ALSO FOUND R/H IIB FLAP TURNBUCKLE ATTACHMENT POINTS ON FLAP CRACKED IN TWO SPOTS, MO
- [SDR UOIA2019071900001](https://openairdocs.org/sdr/UOIA2019071900001.md): Pump · inoperative · Jul 19, 2019 · N916GD · Stbros SD360200 · Hydraulic Pump (Electric/Engine), Main
  > LEFT HYDRAULIC PUMP OUT.
- [SDR 2018FA0000536](https://openairdocs.org/sdr/2018FA0000536.md): Lead · cut · Dec 18, 2018 · N272ZZ · Doug DC3 · Data Recorders (Flight/Maintenance)
  > THE POSITION TRANSDUCERS ARE BEING USED AS SENSORS FOR SOME FLIGHT DATA RECORDER (FDR) PARAMETERS AND ARE MANUALLY ATTACHED VIA A STEEL LEAD/LINE TO SENSE SURFACE MOVEMENT. OVER TIME, IT HAS BEEN NOTED THAT THE STEEL LEADS EXTENDING OUT OF THE SENSORS ARE CUT
- [SDR DATA20180604101](https://openairdocs.org/sdr/DATA20180604101.md): Engine · power loss · Jun 1, 2018 · N764JR · Stbros SD360300 · Engine (Turbine/Turboprop)
  > ON A 5 MILE FINAL WITH AN RJ IN TRAIL BY 3 MILES, PULLED POWER BACK TO IDLE. RIGHT ENGINE MADE A POPPING NOISE AND STARTED FLUCTUATING IN TORQUE. P USHED BOTH POWER LEVERS UP TO SEE IF THE TORQUE WOULD STABILIZE, THAT FAILED, DECIDED TO SECURE THE RIGHT ENGI
- [SDR DATA2017020301](https://openairdocs.org/sdr/DATA2017020301.md): Engine · overtemp · Feb 3, 2017 · N764JR · Stbros SD360300 · Engine (Turbine/Turboprop)
  > AFTER TAKE OFF, DURING NORMAL CLIMB, CLIMB CHECKLIST ACCOMPLISHED, NR 1 ENGINE ITT WAS NOTED TO BE HIGH AT 840°- OIL PSI 125 - OIL TEMP 110°. POWER WAS REDUCED ON AFFECTED ENGINE, BUT CONDITION PERSISTED DICTATING A PRECAUTIONARY NR 1 ENGINE SHUTDOWN AND RETUR
- [SDR 2016FA0000658](https://openairdocs.org/sdr/2016FA0000658.md): Bolt · sheared · Oct 31, 2016 · Turbine Engine Reduction Gear
  > THE ENGINE WAS REMOVED DUE TO METAL IN THE OIL SYSTEM. FOUND ONE BOLT WITH THE HEAD SHEARED OFF.
- [SDR DATA2016062201](https://openairdocs.org/sdr/DATA2016062201.md): Governor · malfunctioned · Jun 22, 2016 · N376AC · Stbros SD360 · Turbine Governor
  > CREW EXPERIENCED NR 1 ENGINE FLUCTUATIONS DURING CLIMB. NECESSARY CLIMB POWER SETTINGS DID NOT AFFECT THE INDICATIONS. AIRCREW DECIDED TO RETURN TO BLOCK IN ORDER TO BE SAFE AND HAVE MAINTENANCE LOOK INTO THE ISSUE. MAINTENANCE LOOKED INTO ISSUE, CHANGED OV
- [SDR DATA2015122101](https://openairdocs.org/sdr/DATA2015122101.md): Circuit Breaker · malfunctioned · Dec 21, 2015 · N733CH · Stbros SD360 · Propeller Feathering/Reversing
  > AFTER BEING CLEARED FOR TAKEOFF & APPLYING TAKEOFF POWER, FIRST OFFICER NOTICED, AUTO FEATHER, LIGHT FAILED TO ILLUMINATE & CALLED ABORT. ACFT PULLED OFF ACTIVE RUNWAY & PARKED ON TAXIWAY WHERE IT WAS FOUND THAT AUTO FEATHER CIRCUIT BREAKER WAS TRIPPED. CIRC
- [SDR CA151030001](https://openairdocs.org/sdr/CA151030001.md): Engine · malfunctioned · Oct 19, 2015 · Doug DC3C · Engine (Turbine/Turboprop)
  > (CAN) AN IFSD OCCURRED ON THE ABOVE AIRCRAFT. THE FLIGHT WAS DIVERTED AND IT LANDED SAFELY SINGLE ENGINE. NO OTHER DETAILS ARE AVAILABLE AT THIS TIME.
- [SDR CA151019005](https://openairdocs.org/sdr/CA151019005.md): Sensor · failed · Oct 16, 2015 · Doug DC3C · Aircraft Fuel Distribution System
  > (CAN) WHILE ON DOWNWIND LEG AND FINAL APPROACH FOR LANDING THE AIRCRAFT FLEW OVER A PORTION OF THE DESTINATION AIRPORT WHERE SEVERAL PERSONS ON THE GROUND NOTICED AN UNUSUAL VAPOR TRAIL STREAMING FROM THE TAIL SECTION OF THE AIRCRAFT. THE AIRCRAFT LANDED NORM
- [SDR CA150611008](https://openairdocs.org/sdr/CA150611008.md): Fork · cracked · Jun 10, 2015 · Doug DC3C · Nose/Tail Landing Gear Strut/Axle
  > (CAN) FOLLOWING COMPLETION OF AN UNRELATED SCHEDULED MX CHECK, THE ACFT WAS BEING TOW BACKWARDS AT THE TAIL WHEEL ATTACHMENT POINT & DURING A SLOW TURN TO THE RT THE TAIL WHEEL FORK FRACTURED AT THE LT FORK AXEL BORE IN THE LOCATION OF THE BONDED BUSHING PN 11
- [SDR EXDA2015F00061](https://openairdocs.org/sdr/EXDA2015F00061.md): Fuel Control · unknown · May 13, 2015 · N974AA · Stbros SD360 · Fuel Control/Turbine Engines
  > ON 5/13/2015 ACFT HAD AN UNSELECTED LT ENGINE SHUTDOWN IN FLIGHT, WHILE ENROUTE. THE FLIGHT CREW DECLARED AN EMERGENCY AND MADE AN UNSCHEDULED LANDING. ON 5/14/2015 THE ACFT WAS INSPECTED AND NO DEFECTS WERE FOUND. ALL GROUND PERFORMANCE CHECKS WERE SATISFAC
- [SDR DATA2015033101](https://openairdocs.org/sdr/DATA2015033101.md): Wire · broken · Mar 31, 2015 · N376AC · Stbros SD360300 · Powerplant System Wiring
  > ON TAKEOFF ROLL RT ENG RTOP SYS FAILED TO ACTIVATE. TAKEOFF WAS ABORTED IAW ACC SOP'S. ACFT RETURNED TO BLOCK. UPON TROUBLESHOOTING IT WAS FOUND THAT A BROKEN WIRE ON RTOP VLV CONNECTOR HAD BROKEN CAUSING THE RTOP SYS TO NOT ACTIVATE. WIRE WAS REPAIRED & S
- [SDR CA150408024](https://openairdocs.org/sdr/CA150408024.md): Engine · shutdown · Feb 23, 2015 · Engine (Turbine/Turboprop)
  > (CAN) THE RT ENGINE SHUTDOWN IN FLIGHT DURING DESCENT. THE ENGINE WAS REMOVED AND SENT FOR INVESTIGATION.
- [SDR TXHA2015012200688](https://openairdocs.org/sdr/TXHA2015012200688.md): Cable · lack of lube · Jan 21, 2015 · N351TA · Stbros SD360 · Power Lever
  > ON TAKEOFF LEFT ENGINE DEVELOPED ONLY 1400-1500LBS OF TORQUE WITH THROTTLES FULL FORWARD. REMOVED AND LUBRICATED POWER CONTROL CABLE AND PERFORMED A RIGGING CHECK AND POWER RUN UP. ALL PARAMETERS FOUND NORMAL AND WITHIN LIMITS.
- [SDR CA141031008](https://openairdocs.org/sdr/CA141031008.md): Elbow · damaged · Oct 26, 2014 · Doug DC3C · Control Column Section
  > (CAN) DURING A ROUTINE INSPECTION 2 OF THE 6 SCREWS SECURING CONTROL COLUMN UPPER ELBOW TO THE CONTROL COLUMN UPPER TUBE ASSY WERE FOUND LOOSE. FURTHER INVESTIGATION REVEALED THE THREADS IN THE CONTROL COLUMN UPPER ELBOW WHICH IS A MACHINED CASTING WERE STRIP
- [SDR DATA20140923002](https://openairdocs.org/sdr/DATA20140923002.md): Flex Hose · leaking · Sep 22, 2014 · N151CA · Stbros SD360 · Fuel Controlling System
  > AFTER TAKEOFF CREW EXPERIENCED LT ENG SURGE. RETURNED SAFELY TO POINT OF ORIGIN. FOUND TO BE CAUSED BY ENG P2.5 BLEED AIR LEAK. REPLACED P2.5 FLEXIBLE HOSE.
- [SDR 2014F00110](https://openairdocs.org/sdr/2014F00110.md): Wire · unsecure · Jun 9, 2014 · N972AA · Stbros SD360 · Landing Gear System Wiring
  > DURING APPROACH, CREW LOWERED THE LANDING GEAR AND ONLY THE LT MAIN GEAR SHOWED TO BE DOWN AND LOCKED. ABORTED THE LANDING. TOWER REPORTED THE GEAR APPEARED TO BE DOWN. RAN APPROPIATE CHECK LIST AND DETERMINED THE LANDING GEAR WAS DOWN & LOCKED. DECLARED A
- [SDR CA130709001](https://openairdocs.org/sdr/CA130709001.md): Blade · cracked · Jul 3, 2013 · Turbine Section
  > (CANENGINE WAS SENT FOR REPAIR AFTER THE CUSTOMER REPORTED A CRACK ON 1 EA 2ND STAGE POWER TURBINE BLADE.
- [SDR CA121203016](https://openairdocs.org/sdr/CA121203016.md): Engine · making metal · Dec 3, 2012 · Doug DC3CS1C3G · Engine (Turbine/Turboprop)
  > (CAN) ENGINE WAS SENT FOR INVESTIGATION AFTER THE CUSTOMER REPORTED AN IN FLIGHT SHUTDOWN WITH TORQUE AT ZERO AND T5 AT MAXIMUM OF THE GAGE. ALSO REPORTED PRESENCE OF OIL AND METAL FLAKES IN THE EXHAUST DUCT AND SCRAPPING NOISE WHEN TURNING THE PROPELLER.
- [SDR CA121003003](https://openairdocs.org/sdr/CA121003003.md): Engine · low torque · Sep 22, 2012 · Doug DC3CS1C3G · Engine BMEP/Torque Indicating
  > (CAN) THE CREW DEPARTED AND MADE A CLIMBING LT TURN AND CONTINUED ASCENT TO 8000. AT WHICH POINT THE POWER LEVER WAS SELECTED TO TRAINING POWER 40 PERCENT. ONCE THE POWER WAS SET TO 40 PERCNET THE TORQUE ON THE LT ENGINE DROPPED TO 0 PERCENT. CREW SECURED TH
- [SDR CA120417005](https://openairdocs.org/sdr/CA120417005.md): Pin · sheared · Apr 12, 2012 · Doug DC3C · Trailing Edge Flap Actuator
  > (CAN) AFTER LANDING, THE FLAPS WOULD NOT RETRACT. THE FLAP ACTUATOR WAS REPLACED AND THE FLAPS FUNCTION CHECKED. UPON DISASSEMBLY OF THE FLAP ACTUATOR THE PIN THAT SECURES THE PISTON TO THE SHAFT WAS FOUND SHEARED.
- [SDR DATR001632](https://openairdocs.org/sdr/DATR001632.md): Bolt · failed · Sep 17, 2011 · N764JR · Stbros SD360 · Engine (Turbine/Turboprop)
  > RT SIDE ENGINE EXPERIENCED A LOW OIL PRESSURE LIGHT 1.5 HOURS INTO MISSION AND SUBSEQUENT PRESSURE LOSS. ENGINE WAS SHUTDOWN IN FLIGHT AND ACFT DIVERTED. THE ENGINE WAS RECEIVED AT THIS FACILITY FOR INVESTIGATION. THE PROPELLER SHAFT WAS HARD TO TURN AND A
- [SDR TXHA20110818001](https://openairdocs.org/sdr/TXHA20110818001.md): Shaft · sheared · Aug 18, 2011 · N729PC · Stbros SD360 · Engine Fuel Pump
  > ON TAKEOFF ROLL THE LT ENGINE FLAMED OUT, PILOT ABORTED TAKEOFF NO FURTHER INCIDENT, RETURNED TO BLOCK. INVESTIGATION BY MX FOUND THE LT FUEL PUMP SHAFT SHEARED.
- [SDR 2011F00148](https://openairdocs.org/sdr/2011F00148.md): Probe · failed · Jun 14, 2011 · N729PC · Stbros SD360 · Engine EGT/TIT Indicating System
  > LT ENGINE ITT SPIKED TO 1150, THEY REDUCED POWER TO FLIGHT IDLE AND ITT REMAINED AT 830 DEG CENT. SHUTDOWN ENGINE AND CONTINUED TO DESTINATION, LANDED WITHOUT INCIDENT. INVESTIGATION, SPLIT ENG AND DID A HOT SECTION INSPECTION AND FOUND NO DEFECTS. TESTED THE
- [SDR 2011F00149](https://openairdocs.org/sdr/2011F00149.md): Probe · failed · Jun 14, 2011 · N729PC · Stbros SD360 · Engine EGT/TIT Indicating System
  > LT ENGINE ITT SPIKED TO 1150 THEY REDUCED POWER TO FLIGHT IDLE AND ITT REMAINED AT 830 DEG CENT. SHUTDOWN ENGINE AND CONTINUED TO DESTINATION, LANDED WITHOUT INCIDENT. INVESTIGATION, SPLIT ENG AND DID A HOT SECTION INSPECTION AND FOUND NO DEFECTS. TESTED THE
- [SDR CA110525010](https://openairdocs.org/sdr/CA110525010.md): Turbine Blades · failed · May 25, 2011 · Turbine Section
  > ENGINE WAS REMOVED SUBSEQUENT TO A CATASTROPHIC FAILURE DURING TAKEOFF ROLL. THE PILOT REPORTED "ENGINE FAILED ON TAKEOFF ROLL, AUDIBLE NOISE, METAL EXITING EXHAUST DUCT, ENGINE WENT TO MIN FLOW AND TAKEOFF ABORTED". DURING DISMANTLE INVESTIGATION, THE ENGINE
- [SDR TXHA 7152010](https://openairdocs.org/sdr/TXHA%207152010.md): Engine · making metal · Jul 14, 2010 · N808KR · Stbros SD360 · Engine (Turbine/Turboprop)
  > UPON BLOCKING, PROP WAS FOUND FROZEN AND UNABLE TO TURN. INSPECTED FWD SCREEN AND OIL FILTER, FOUND METAL SHAVINGS IN POWER SECTION SCAVENGE SCREEN AND OIL FILTER. ENGINE WAS REMOVED AND SENT TO MFG FOR FURHTER INVESTIGATION.
- [SDR CA100702006](https://openairdocs.org/sdr/CA100702006.md): Line · cracked · Jun 25, 2010 · Turbine Engine Compressor Section
  > UNCOMMANDED POWER CHANGE DURING CRUISE, THE ENGINE HAD AN UNCOMMANDED DECELERATION. THE FLIGHT WAS DIVERTED AND THE ACFT LANDED SAFELY. GROUND ENGINEERS FOUND A FRACTURED P3 LINE WHICH WAS REPLACED BEFORE THE ACFT WAS RETURNED TO SERVICE. MFG WILL INVESTIGA
- [SDR TXH2010F00002](https://openairdocs.org/sdr/TXH2010F00002.md): Fire Loop · loose · May 24, 2010 · N351TA · Stbros SD360 · Fire Detection
  > LT ENG HAD FIRE WARNING LIGHT ILLUMINATED, NO FIRE, FERRY PERMIT WAS ISSUED IAS GMM CHAP 5.18. NO PART WERE CHANGED. AFT FIRE LOOP FOUND LOOSE, CONNECTION RESECURED. OPS CK OK.
- [SDR TXH2010F00003](https://openairdocs.org/sdr/TXH2010F00003.md): Bolt · failed · May 21, 2010 · N808KR · Stbros SD360 · Engine (Turbine/Turboprop)
  > ENG SN PCE 106099 WAS REMOVED FOR METAL CONTAMINATION. IN FLIGHT, OIL PRESSURE FLUCTUATED 70-80 PSI, OIL TEMPERATURE IN CAUTION RANGE. POST FLIGHT INSP FOUND PROP BINDING WITH NOISE COMING FROM POWER SECTION GEAR BOX. REMOVED SCAVENGE PUMP OIL SCREEN AND FO
- [SDR TXH2010F00001](https://openairdocs.org/sdr/TXH2010F00001.md): Oil Cooler · leaking · Apr 26, 2010 · N808TR · Stbros SD360200 · Engine Oil Cooler
  > NR 1 ENGINE OIL PRESSURE DROPPED DOWN IN FLIGHT. CHANGED OIL COOLER AND LEAK CHECKED, OK.
- [SDR TXH2010F00000](https://openairdocs.org/sdr/TXH2010F00000.md): Oil Filter · clogged · Apr 24, 2010 · N808TR · Stbros SD360200 · Turbine Engine Oil System
  > DURING CLIMB PHASE OF FLIGHT, NR 1 ENGINE OIL PRESSURE BEGAN TO FLUCUTATE BETWEEN 90-50 PSI ALL OTHER INDICATIONS WERE NORMAL. RETURNED TO DEPARTURE, MX CHECKED FOR OIL LEAKS, NONE NOTED. REPLACED OIL FILTER, LEAK AND RUN CHECK, OK.
- [SDR UE5R052709](https://openairdocs.org/sdr/UE5R052709.md): Fuel Nozzle · leaking · May 27, 2009 · Fuel Injector Nozzle
  > DURING BENCH FLOW TEST OF DUPLEX FUEL NOZZLE ASSEMBLY, IT WAS NOTED THAT THERE WAS A LEAK COMING FROM THE WELD LOCATED ON THE FUEL NOZZLE ASSEMBLY BODY.
- [SDR CA081104002](https://openairdocs.org/sdr/CA081104002.md): Compressor · seized · Oct 31, 2008 · Doug DC3C · Turbine Engine Compressor Section
  > (CAN) DURING CRUISE, THE RT GENERATOR KICKED OFF-LINE. SHORTLY AFTER THAT TEMP INDICATIONS IN THE RT ENG CLIMBED CAUSING THE FLIGHT CREW TO SHUT DOWN THE ENGINE AND CONTINUE ON TO LAND AT THE SCHEDULED POINT OF LANDING. THE STARTER GEN WAS REMOVED AND THE COMP
- [SDR CA081112011](https://openairdocs.org/sdr/CA081112011.md): Generator · inoperative · Oct 31, 2008 · Doug DC3C · AC Generator-Alternator
  > (CAN) DURING CRUISE, THE CREW OBSERVED THE NR 2 GENERATOR GO OFF LINE WITH AN INCREASE IN ENG TEMP. IT WAS SHUTDOWN AND A SINGLE ENG LANDING FOLLOWED. POST FLIGHT INSP FOUND THE COMPRESSOR HARD TO ROTATE. THE ENGINE WILL BE REMOVED AND FORWARDED FOR INVESTIGA
- [SDR CA081124001](https://openairdocs.org/sdr/CA081124001.md): Bungee · mismarked · Oct 6, 2008 · Doug DC3CS4C4G · Wheel/Ski/Float
  > (CAN) DURING AERIAL WORK WITH SKIS INSTALLED THE RT MAIN GEAR DID NOT EXTEND FULLY. WITH THE ASSISTANCE OF A BELLY MOUNTED CAMERA THE CAUSE WAS DETERMINED TO BE THE SKI FWD LIMIT CABLE ASSY. THE LANDING GEAR WAS CYCLED AND EXTENDED SUCCESSFULLY. BOTH LT AND RT
- [SDR N973081107](https://openairdocs.org/sdr/N973081107.md): Indication Sys · malfunctioned · Aug 10, 2007 · N973AA · Stbros SD360 · Propeller Indication System
  > WHILE EN ROUTE TO MCI THE FLIGHT CREW ELECTED TO SHUT DOWN THE RIGHT ENGINE AS A PRECAUTIONARY MEASURE DUE TO ERRATIC PROPELLER SPEED INDICATION AND DIVERTED TO COU. EXDA MAINTENANCE WAS DISPATCHED TO COU AND INSPECTED THE PROPELLER RIGGING IAW SHORTS MAINTEN
- [SDR CA070803007](https://openairdocs.org/sdr/CA070803007.md): Engine · damaged · Jun 17, 2007 · Stbros SD360 · Engine (Turbine/Turboprop)
  > (CAN) ON SHORT FINAL, THE ENGINE LOST POWER AND SMOKE WAS SEEN EXITING THE ENGINE EXHAUST. POST-FLIGHT INSPECTION REVEALED INTERNAL ENGINE DAMAGE. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE COMPLETED. (TC NR 20070803007)
- [SDR CA070803011](https://openairdocs.org/sdr/CA070803011.md): Bolt · sheared · Jun 15, 2007 · Stbros SD360 · Turbine Engine Reduction Gear
  > (CAN) ON CLIMB, ENGINE OIL PRESSURE WAS SEEN TO FALL TO ZERO AND THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INVESTIGATION REVEALED A SHEARED 1ST STAGE REDUCTION GEAR CARRIER BOLT. (TC NR 20070803011)
- [SDR CA070418005](https://openairdocs.org/sdr/CA070418005.md): Wire · arced · Apr 16, 2007 · Doug DC3C · Navigation System Wiring
  > (CAN) THE AIRSPEED AURAL WARNING CIRCUIT BREAKER WAS FOUND TO BE (POPPED). WHEN THE UPPER PANEL WAS LOWERED EVIDENCE OF ARCING WAS FOUND ON AIRFRAME STRUCTURE. THE WIRE WAS REPAIRED THROUGH PARTIAL REPLACEMENT, CHAFE PROTECTOR WAS ADDED TO THE AIRFRAME STRUC
- [SDR DAT2006F00008](https://openairdocs.org/sdr/DAT2006F00008.md): Tire · failed · Sep 6, 2006 · N617FB · Stbros SD360 · Tire
  > THE LANDING WAS NORMAL AND UNDER CONTROL. SLOWING TO ABOUT 60-70 KNOTS THE LT MAIN TIRE BLEW. WHEN THE TIRE BLEW AIRCRAFT WAS MAINTAINED ON CENTERLINE AND STEERING AIRCRAFT OFF THE ACTIVE RUNWAY. UPON FURTHER EVALUATION THE LT TIRE SHOWED SIGNS THAT WAS NOT
- [SDR CA060403005](https://openairdocs.org/sdr/CA060403005.md): Engine · making metal · Mar 2, 2006 · Engine (Turbine/Turboprop)
  > (CAN) IN FLIGHT, THE ENGINE LOW OIL PRESSURE WARNING ANNUNCIATED AND THE ENGINE WAS SHUTDOWN. SUBSEQUENT INSPECTION REVEALED METALIC DEBRIS IN THE ENGINE OIL. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE EXTABLISHED. (TC NR 20060403005)
- [SDR DAT2005F00014](https://openairdocs.org/sdr/DAT2005F00014.md): Gas Generator · surges · Sep 15, 2005 · N136LR · Stbros SD360 · Turbine Engine Compressor Section
  > ABORTED THE TAKEOFF DUE TO THE LT RTOP INDICATOR DID NOT ILLUMINATE ON THE TAKEOFF. AC WAS RETURNED TO MAINTENANCE HANGAR. CHIEF INSPECTOR TESTED THE RTOP SYSTEM ON THE GROUND. OPS CHECK GOOD IAW MM. AC WAS RETURNED TO SERVICE. (K)
- [SDR DAT2005F00013](https://openairdocs.org/sdr/DAT2005F00013.md): Compressor · surges · Sep 14, 2005 · N136LR · Stbros SD360 · Turbine Engine Compressor Section
  > AS POWER WAS BROUGHT TO TAKEOFF SETTINGS, THE RT TORQUE INSTANTLY INCREASED FROM 1400 LBS. THE RISE IN TORQUE OF THE LT ENGINE WAS FOLLOWED BY 2 COMPRESSOR STALLS, AT WHICH POINT THE TAKEOFF WAS ABORTED. AFTER A RUNUP WAS PERFORMED BY MAINTENANCE, IT WAS FOU
- [SDR DAT2005F00008](https://openairdocs.org/sdr/DAT2005F00008.md): Blade · cracked · Jun 30, 2005 · N263GA · Stbros SD360 · Propeller Blade Section
  > DURING THE SCHEDULED COMPLIANCE OF AD ON THE LT PROPELLER IT WAS FOUND 1 OF 6 PROPELLER BLADES WERE CRACKED. MECHANIC REMOVED AND REPLACED THE PROPELLER IAW MM. OPS CHECK GOOD. AC WAS RETURNED TO SERVICE. (K)
- [SDR AUS20040378](https://openairdocs.org/sdr/AUS20040378.md): Connector · corroded · May 3, 2004 · Stbros SD360 · Electrical Connectors
  > (AUS) LT ENGINE FIRE WIRE CONNECTOR CORRODED. CONNECTOR IS LOCATED AT THE REAR FIREWALL POSITION.

Next page: https://openairdocs.org/engine/pratt-whitney-canada-pt6a-67r/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE engine_model_key = 'PT6A67R'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/pratt-whitney-canada-pt6a-67r/reports

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