U/A Canada PT6A-45

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 = 'PT6A45'
  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 2011F00057Display · failedTHE COPILOTS EHSI WOULD NOT POWER UP, SCREEN REMAINED BLANK.Mar 3, 2011 · N17WC · Beech B300 · Central DisplaySDR 9CC2011F00000Blower · failedENVIROMENTAL BLOWER FAILED, SMOKE IN CABIN.Feb 9, 2011 · N60VP · Beech C90A · Air Distribution FanSDR 2011FA0000072Brake Assy · leakingDURING LANDING ROLL-OUT AND AFTER UTILIZING BETA OR DISCING TO SLOW THE ACFT DOWN TO TAXI SPEEDS, I SWITCHED TO WHEEL BRAKING AND THERE WAS NO PRESSURE ON THE LT SIDE. GROUND CONTROL WAS ABLE TO CLEAR ME TO THE SIGNATURE RAMP AREA WITHOUT REQUIRING A FULL-STOJan 22, 2011 · N911RX · Beech B200 · Landing Gear Brake SystemSDR GUUA95452122910ACable · brokenDURING SCHEDULED ROUTINE MX, DISCOVERED AIRSTAIR DOOR FWD CABLES BROKEN, FWD CAMS WILL NOT ROTATE. REPLACED AIRSTAIR DOOR CABLE ASSY.Dec 29, 2010 · N87554 · Beech 1900D · Passenger/Crew DoorsSDR GUUA95457112510AStringer · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED CORROSION ON THE RT WING LOWER SKIN BONDED STRINGER AT WS 114.25 TO WS 124.25 CUT OUT 4.5 INCH SECTION ON CORRODED STRINGER. FABRICATED AND INSTALLED FROWARD REPAIR ANGLE AND AFT REPAIR ANGLE ON RIGHT WING LOWER BONDENov 25, 2010 · N87554 · Beech 1900D · Wing, Longeron/StringerSDR GUUA95453102810ASkin · chafedDURING SCHEDULED ROUTINE INSP DISCOVERED SKIN CHAFE LT PRESSURE PLATE AREA APPROX FS 258 AT WS 305. REPAIRED SKIN CHAFE INSTALLED DOUBLER 2.5 X 10.5 INCHES ON LT PRESSURE PLATE AREA AT FS 258, WS 305.Oct 28, 2010 · N87554 · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA95453102510CAngle · crackedDURING SCHEDULED ROUTINE INSP DISCOVERED AIRSTAIR DOOR FWD ANGLE CRACKED AT LOWER SNUBBER ATTACH POINTS APPROX FS 150 AT STR 9L. REMOVED 28 INCH SECTION OF -3 ANGLE AND INSTALLED -3 FILLER ANGLE AND 8.5 INCH UPPER SPLICE AND 6.5 INCH LOWER -11 SPLICE ANGLE.Oct 25, 2010 · N87554 · Beech 1900D · Fuselage Miscellaneous StructureSDR GUUA95457032010ASpar · damagedCOMPLIED WITH COLD EXPANSION OF FASTENER HOLES IN THE WING REAR SPAR LOWER CAP IAW FAA APPROVED DATA CONTAINED IN THE ACFT COMPANY KIT 118-4014-0003. NOTE: ACFT DOWN FOR KIT WING REAR SPAR INSTALLATION.Mar 20, 2010 · N87554 · Beech 1900D · Wing SparSDR COEA0701756Tire · failedAFTER LANDING, DURING ROLLOUT PILOT OBSERVED A STRONG VIBRATION THAT SUBSIDED AS THE AC SLOWED. GROUND PERSONAL CONFIRMED THE RT MAIN TIRE WAS FLAT. REPLACED RT MAIN TIRE AND WHEEL ASSY. (K)Dec 27, 2007 · N756FX · Cessna 208B · TireSDR MT92007F00000Tube · splitAIRCRAFT LANDED ON ITS SCHEDULED ROUTE, WHEN IT EXPERIENCED A FLAT TIRE ON ROLL OUT. THIS CAUSED THE CLOSURE OF THE ACTIVE RUNWAY. MAINTENANCE PERSONNEL REPLACED THE TIRE AND TOWED THE PLANE BACK TO THE RAMP. THE TIRE WAS DISASSEMBLED AND IT WAS FOUND THAT Jul 16, 2007 · N162SA · Cessna 208B · Tire TubeSDR 2005FA0001059Antenna · inoperativeFOUND UPPER UAT ANTENNA UNSERVICEABLE DURING UAT UPGRADE. (K)Apr 29, 2005 · N302EH · Dhav DHC6300 · Central DisplaySDR RU32005F00001Warning Light · false indicationON FINAL APPROACH, LOWERED GEAR AT FAF - NO LEFT MAIN GEAR LIGHT. CYCLED GEAR ONCE INSIDE FAF - STILL NO LIGHTS, EXECUTED FLY BY RWY 4R. 2 AIRLINE CREWS ADVISED ALL 3 GEARS APPEAR DOWN. FLEW LT TRAFFIC, CYCLED GEAR 3RD TIME, OBSERVED GEAR RETRACT AND EXTENDMar 24, 2005 · N76 · Beech 300BEECH · Landing Gear Position and WarningSDR 2003FA0000915Indicator · failedPROPELLER RPM INDICATED 300 RPM HIGH DURING FLIGHT. PILOT PERFORMED PRECAUTIONARY LANDING. NO OTHER PERIMETER FLUCTUATIONS. REPLACED INDICATOR WITH NEW PART. OPERATIONAL CHECK GOOD.Aug 25, 2003 · N64BP · Cessna 208B · Propeller Indication SystemSDR 2003FA0000893Indicator · malfunctionedPROPELLER RPM GAUGE INDICATED 300 RPM OVER REDLINE DURING FLIGHT. PILOT PERFORMED PRECAUTIONARY LANDING AT FIELD OTHER THAN PLANNED. FURTHER INVESTIGATION OF ENGINE AND SYSTEM: NOR TORQUE FLUCTUATUON, NO ITT FLUCTUATION, NO N FLUCTUATION, INDICATOR FAILURE OAug 11, 2003 · N64BP · Cessna 208B · Propeller Indication SystemSDR J7B2003F00000Rivet · looseLOOSE AND WORKING RIVETS IN INBOARD LEADING EDGE ATTACHMENT TO FORWARD SPAR RT AND LT WING.Dec 16, 2002 · N64BP · Cessna 208B · Wing, Plate/SkinSDR D5H2002F00000Pin · loosePILOT REPORTED SMOKE IN COCKPIT 30 MINUTES INTO FLIGHT. CONNECTOR FROM PROPELLER HEAT CIRCUIT BREAKER (P-186/J-186). CONNECTOR, 12 GAUGE WIRE(HA-36). MAINTENANCE CREW FOUND CONNECTOR FULLY ENGAGED AND STILL ATTACHED TO WIRE BUNDLE. MAINTENANCE FOUND TERMINSep 10, 2002 · N64BP · Cessna 208B · Propeller/Propulsor System WiringSDR DAT2002F00001Blade · brokenLT ENGINE STARTED TO SHAKE AFTER START UP. THE CREW SHUTDOWN THE ENGINE AND EXITED THE AIRCRAFT. MAINTENANCE INSPECTED THE LT ENGINE AND FOUND 2 BROKEN PT BLADES WHICH CAUSED BINDING OF THE POWER SECTION. THE POWER SECTION IS BEING REMOVED AND REPLACED.Jun 26, 2002 · N167RC · Stbros SD330 · Turbine SectionSDR 98ZZZX4303Gas Generator · failedAIRCRAFT DEPARTED, ABOUT 5 MINUTES AFTER LEVELING OFF, RT ENGINE SPUN DOWN. LANDED BACK AT BASE WITH SINGLE ENGINE, WITHOUT TRYING TO RESTART IT. NOTICED THE RIGHT TORQUE GAUGE DROPPED, BUT DISREGARDED IT BECAUSE ALL OTHER GAUGES WERE NORMAL. MECHANIC DISPAOct 23, 1998 · N55AN · Stbros SD330 · Turbine Engine Compressor SectionSDR 99ZZZX606Turbine Section · leakingA RECURRENCE OF THE LEAKING OIL ON THE LEFT POWER SECTION, PAGE 84101. THE REPAIR DID NOT HOLD. THE POWER SECTION WAS REMOVED AND REPLACED. RUN AND LEAK CHECKED GOOD.Mar 13, 1998 · N938MA · Stbros SD330 · Turbine SectionSDR 97ZZZX2005Gas Generator · seal failedPILOTS REPORTED SMOKE IN COCKPIT AND CLOSED PRSOV VALVE STOPPING THE SMOKE. SEVERAL MINUTES LATER, THE PILOTS NOTICED TORQUE AND OIL PRESSURE FLUCTUATING. FEATHERED AND SHUT DOWN ENGINE AND LANDED WITHOUT INCIDENCE. ENGINE WAS LEAKING OIL FROM THE COMPRESSOApr 25, 1997 · N936MA · Stbros SD330 · Turbine Section
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