U/A Canada PT6A-25

Service difficulty reports · 20

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "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 = 'PT6A25'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CA151117014Fuel Control · malfunctioned(CAN) FIELD SERVICE REPRESENTATIVE WAS JUST INFORMED OF TWO EVENTS ON THE SAME AIRCRAFT THIS IS THE SECOND EVENT, OCCURRED JUST AFTER TAKE-OFF FOR A TRAINING MISSION. IN THE FIRST CIRCUIT, THE CREW REALIZED THAT THE ENGINE PARAMETERS WERE STABILIZED ON FULL PJun 9, 2015 · Emb EMB312 · Fuel Control/Turbine EnginesSDR CA150927001Engine · malfunctioned(CAN) THIS EVENT WAS RE-CLASSIFIED FROM CAT 3 TO CAT 2. PILOT REPORTED THE FOLLOWING: "THE PILOT NOTICED THAT THE PCL WAS NOT MOVING FREELY ON THE PRE-FLIGHT. IT WAS MENTIONED TO THE GROUND CREW AND THEY CLASSIFY IT WAS NORMAL. 45 MIN INTO THE FLIGHT THE PILOMay 4, 2015 · Pilats PC7 · Engine (Turbine/Turboprop)SDR CA150519015Line · leaking(CAN) AFTER LANDING WITH THE POWER LEVER AT IDLE, THE NG DROPPED TO 44 PERCENT WITH AMBER CAUTION AND NP DROPPED TO APPROXIMATELY 700. TROUBLESHOOTING FOUND A LEAKING P3 LINE. THE TUBE WILL BE FORWARDED TO MFG SERVICE INVESTIGATION FOR FURTHER ANALYSIS.Apr 7, 2015 · Pilats PC7 · Engine (Turbine/Turboprop)SDR CA151117005Engine · power loss(CAN) ENGINE HAD 2 SEPARATE EVENTS ON THE SAME ACFT, THE 1ST EVENT WHICH OCCURRED DURING A MISSED APPROACH, THE STUDENT PILOT APPLIED FULL POWER BUT ONLY GOT 800 LB/FT OF TORQUE, FULL POWER SHOULD HAVE BEEN 1970 LB/FT. HE THEN REQUESTED EMERGENCY LANDING IN Mar 17, 2015 · Engine (Turbine/Turboprop)SDR CA150306001Engine · flamed out(CAN) THE ENGINE EXPERIENCED A FLAME OUT AT 8000 FEET DURING MANEUVERS FOLLOWED BY A SUCCESSFUL AUTO RELIGHT & ENGINE RESTART. THE AIRCRAFT LANDED UNEVENTFULLY. THE FIELD SERVICE REPRESENTATIVE IS EN ROUTE TO THE CUSTOMER. FAULT ISOLATION IS IN PROGRESS.Feb 23, 2015 · Engine (Turbine/Turboprop)SDR CA120813017Engine · fire(CAN) DURING TAXIING, THE PILOT NOTED THE ENGINE PERFORMANCE PARAMETERS DECAYING FOLLOWED BY FIRE AND SMOKE EXITING THE EXHAUST STUBS. THE PILOT IMMEDIATELY SHUTDOWN THE ENGINE AS PRECAUTION. ACFT WAS TOWED TO THE HANGAR. THE ENGINE WAS REMOVED FROM THE ACFJul 8, 2012 · Engine (Turbine/Turboprop)SDR CA110614001Engine · power loss(CAN) ACCIDENT DURING A TRAINING MISSION, THE ACFT LOST ENGINE POWER AND THE CREW MADE A CRASH LANDING IN A FIELD. THEY WERE NOT INJURED BUT THE ACFT WAS SUBTANTIALLY DAMAGED.Jun 3, 2011 · Emb EMB312 · Engine (Turbine/Turboprop)SDR CA110214007Engine · failedIFSD (SINGLE ENGINE) WHILE AT T/O FOR A NIGHT FLIGHT, AS THE POWER WAS INCREASED TO MAXIMUM, A LOUD NOISE WAS HEARD AND FIRE/SPARKS WERE SEEN COMING OUT OF THE ENGINE FOLLOWED BY WIND DOWN. THE T/O WAS ABORTED AND EMERGENCY DECLARED. FIRE CREWS EXTINGUISHED TFeb 7, 2011 · Pilats PC7 · Engine (Turbine/Turboprop)SDR CA070514041Drive Shaft · sheared(CAN) THE ENGINE WAS FOUND NOT TO RESPOND TO THROTTLE INPUT AND SUBSEQUENTLY ACCELERATED UNCOMMANDED. THE ENGINE WAS SHUTDOWN ON APPROACH. SUBSEQUENT INSPECTION REVEALED A SHEARED FUEL CONTROL UNIT DRIVE SHAFT. (TC NR 20070514041)Mar 27, 2007 · Pilats PC7 · Fuel Control/Turbine EnginesSDR CA060531011Engine · power loss(CAN) THE ENGINE WAS REPORTED TO HAVE LOST POWER FOLLOWING TAKE-OFF, RESULTING IN A FORCED LANDING.May 11, 2006 · Pilats PC7 · Engine (Turbine/Turboprop)SDR CA060425011Turbine Blades · damagedDURING A TRAINING FLIGHT, THE ENGINE WAS REPORTED TO EMIT NOISES AND SMOKE FOLLOWED BY AN UNCOMMANDED POWER REDUCTION AND FLAME OUT. SUBSEQUENT INSPECTION REVEALED FRACTURED POWER TURBINE BLADES. P&WC WILL INVESTIGATE THE EVENT AND WILL ADVISE OF ROOT CAUSE Apr 7, 2006 · Beech T34C1 · Turbine SectionSDR CA060403008Spline · wornTHE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION WHICH RESULTED IN THE AIRCRAFT CRASHING. INVESTIGATION DETERMINED THE FUEL PUMP SPLINE TO BE SUFFICIENTLY WORN TO RESULT IN THE LOSS OF ENGINE FUEL FLOW.Jan 12, 2006 · Beech T34C · Engine Fuel PumpSDR CA051006014Bleed Valve · out of limits(CAN) ON TAKE-OFF ROLL, THE ENGINE SURGED, ACCOMPANIED BY FLAMES EMITTED FROM THE EXHAUST. SUBSEQUENT INVESTIGATION DETERMINED THE COMPRESSOR BLEED VALVE CLOSING POINT TO BE OUT OF LIMITS. THE BOV WAS REPLACED.Sep 22, 2005 · Pilats PC7 · Compressor Bleed ValveSDR CA050429006Engine · shutdownDURING CRUISE, THE PILOT NOTICED OIL SMELL IN THE CABIN ACCOMPANIED BY DECREASING ENGINE OIL PRESSURE. THE PILOT DECLARED AN EMERGENCY AND COMPLETED AN UNSCHEDULED LANDING. FOLLOWING LANDING POWER COULD NOT BE MODULATED AND THE ENGINE WAS SHUT DOWN. SUBSEQUApr 14, 2005 · Engine (Turbine/Turboprop)SDR CA050419007Engine · malfunctioned(CAN) DURING A MAINTENANCE FLIGHT, THE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION. THE PILOT WAS UNABLE TO MODULATE POWER AND SUBSEQUENTLY SUCCESSFULLY EJECTED FROM THE AIRCRAFT. MFG WILL MONITOR THE INVESTIGATION OF THIS INCIDENT AND WILL ADVISE OF RApr 2, 2005 · Engine (Turbine/Turboprop)SDR CA050401005Engine · making metal(CAN) THE ENGINE EXPERIENCED AN UNCOMMANDED REDUCTION IN POWER FOLLOWING TAKE-OFF. THE FLIGHT DIVERTED TO POINT OF ORIGIN. DURING SUBSEQUENT TROUBLESHOOTING, THE CHIP DETECTOR WARNING ANNUNCIATED AND METAL PARTICLES WERE FOUND ON THE DETECTOR. MFG WILL MONIMar 29, 2005 · Engine (Turbine/Turboprop)SDR CA041117003Engine · flamed out(CAN) DURING CRUISE (10,000 FT) THE PILOT REPORTED A LOUD NOISE FOLLOWED BY ENGINE FLAMEOUT. AN ATTEMPTED RELIGHT WAS UNSUCCESSFUL AND AN EMERGENCY LANDING WAS PERFORMED. THE ENGINE IS UNDER INVESTIGATION. MFG WILL MONITOR THE PROGRESS AND FINDINGS OF THE Oct 15, 2004 · Engine (Turbine/Turboprop)SDR 97ZZZX1903Bearing · misassemblyNEW WOODWARD BEARING P/N 1412-654. RECEIVING IN INSPECTION REVEALED THAT INNER BEARING RACE, ROLLER BALLS, AND BALL CAGE WERE NOT SEATED CORRECTLY INTO THE OUTER RACE. BEARING WOULD SPIN, HOWEVER, THE OUTER RACE WOULD 'WOBBLE' WHEN ROTATED.Mar 1, 1997 · Turbine GovernorSDR CA960521010Blade · fractured(CAN)FOLLOWING A STALL EXERCISE DURING FLIGHT TRAINING, ON POWER APPLICATION, THERE WAS AN EXPLOSION FROM THE ENGINE. ENGINE WAS SECURED AND A LANDING MADE. AFTER ENGINE SPLIT AT THE "C" FLANGE, A FRACTURE D POWER TURBINE BLADE WAS EVIDENT.May 9, 1996 · Turbine SectionSDR CA960212037Fcu · damaged(CAN) DURING A FLIGHT, ENGINE PARAMETERS SUDDENLY INCREASED WHILE IN CRUISE. THE ENGINE DID NOT RESPOND TO POWER LEVER INPUTS. THE PILOT DIVERTED FLIGHT TO THE POINT OF ORIGIN AND SECURED THE ENGINE BEFORE DESCENDING. INSPECTION REVEALED A DAMAGED FUEL CONTROLFeb 5, 1996 · Fuel Control/Reciprocating Engines
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