U/A Canada PT6A-65AG

Service difficulty reports · 35

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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 = 'PT6A65AG'
  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 CA150710014Line · fractured(CAN) DURING SPRAYING OPERATION, PILOT INCREASED THE ENGINE POWER AND THE FUEL FLOW WENT TO MINIMUM FLOW WITH NO RESPONSE FROM THE ENGINE. PILOT THEN IMMEDIATELY MADE AN EMERGENCY LANDING UNEVENTFULLY. DURING TROUBLESHOOTING, A P3 LINE FROM FCU TO P3 FILTER Jun 29, 2015 · Fuel Controlling SystemSDR CA150224005Engine · separated(CAN) THE ENGINE LOST POWER ON TAKEOFF. THE ENGINE WAS RIPPED FROM THE FUSELAGE AND THERE WAS TAIL AND WING DAMAGE.Feb 5, 2015 · Airtrc AT602 · Engine (Turbine/Turboprop)SDR CA141006008Engine · power loss(CAN) DURING TAKEOFF, THE ENGINE LOST POWER FORCING TO PILOT TO MAKE AN EMERGENCY LANDING IN A FIELD. THE ACFT SUSTAINED DAMAGE TO THE LOWER FUSELAGE AND WINGS. THE NTSB HAS REQUESTED ASSISTANCE FROM ENGINE MFG AND SUPPORT WILL BE PROVIDED ACCORDINGLY.Sep 9, 2014 · Hughes 369HM · Engine (Turbine/Turboprop)SDR CA140826001Engine · surges(CAN) THE ACCIDENT WAS REPORTED BY THE NTSB AND SPECIFIED THAT THE ENGINE SUSTAINED A POWER SURGE THEN A LOSS OF THRUST ON APPROACH. THE AIRPLANE LANDED IN TREES AND THE PILOT WAS NOT INJURED.Jul 25, 2014 · Engine (Turbine/Turboprop)SDR CA140630013Unknown · unknown(CAN) AFTER TAKEOFF FROM A DIRT STRIP, THE PILOT INITIATED AN EARLY TURN AT APPROX. 10 FT ABOVE THE GROUND. SHORTLY AFTER, THE ACFT FELT LIKE IT WAS SETTLING AND THE PILOT APPLIED FULL POWER AND NOTICED TORQUE DECREASING BEFORE THE ACFT IMPACTED THE GROUND. Jun 13, 2014 · Airtrc AT502B · Standard Practices/StructuresSDR CA140619019Engine · power loss(CAN) DURING FLIGHT, THE PILOT HEARD A LOUD NOISE FOLLOWED BY LOSS OF POWER. A FORCED LANDING WAS MADE IN A FIELD DURING WHICH THE AIRCRAFT WAS DAMAGED (EXTENT UNKNOWN). THE PILOT, ONLY ONE ON BOARD WAS NOT INJURED.Jun 5, 2014 · Airtrc AT602 · Engine (Turbine/Turboprop)SDR CA131113008Strut · corroded(CAN) DURING ANNUAL INSPECTION, IT WAS FOUND THAT THE LT STABILIZER STRUT ASSY. LOWER ATTACH FORK AND BUSHINGS WERE HEAVILY CORRODED.Nov 13, 2013 · Airtrc AT602 · Fuselage, Stabilizer Attach FittingsSDR CA130822003Engine · power loss(CAN) ACFT WAS FLYING A FIRE SUPPRESSION FLIGHT WHEN THE PILOT EXPERIENCED A LOSS OF POWER. DROPPED THE LOAD OF RETARDANT AND WAS FORCED TO LAND AT A PRIVATE AIR STRIP. ENGINE WILL BE REMOVED ON-SITE AND A RENTAL INSTALLED.Aug 16, 2013 · Airtrc AT802A · Engine (Turbine/Turboprop)SDR CA130614002Blade · failed(CAN) DURING T/O ROLL, THE ENGINE LOST POWER. THE T/O WAS ABORTED. POST EVENT ENGINE EXAMINATION FOUND FRACTURED 2ND STAGE POWER TURBINE BLADES. THE ENGINE WAS REMOVED AND FORWARDED, WHERE IT WAS LAST REPAIRED LESS THAN 1000 HRS AGO, FOR INVESTIGATION AND REPAMay 18, 2013 · Airtrc AT802A · Turbine SectionSDR CA120227009Gusset · cracked(CAN) CRACKED FUSELAGE FRAME AT LT AFT, FLOAT/AFT WING SPAR ATTACHMENT AREA. CRACK IS IN AREA "C" OF WIPAIRE SL REV D. AREA ALREADY REPLACED WITH THE NEWEST VERSION OF TUBING. SUGGEST DRILLING HOLE AT AREA C TO IMPROVE FLEXIBILITY.Feb 27, 2012 · Airtrc AT802A · Fuselage Main, FrameSDR CA120130002Engine · power loss(CAN) SHORTLY AFTER T/O FROM A PRIVATE STRIP AT 150 FT ALTITUDE, THE ENGINE STARTED TO SURGE ACCOMPANIED BY ERRATIC PROPELLER SPEED AND TORQUE FLUCTUATIONS. THE PILOT TURNED BACK TOWARDS THE LANDING STRIP AND AT THAT POINT, THE ENGINE LOST POWER. A FORCED LANDNov 8, 2011 · Airtrc AT602 · Engine (Turbine/Turboprop)SDR CA111226002Engine · power loss(CAN) FOLLOWING THE COMPLETION OF A SPRAY RUN, THE ENGINE LOST POWER AND THE PILOT EXECUTED A FORCED LANDING IN A FIELD ADJACENT TO THE ONE HE WAS SPRAYING. THE ACFT WAS SUBSTANTIALLY DAMAGED AND THE PILOT SUFFERED ONLY MINOR INJURIES. OFFER OF ASSISTANCE WIJul 22, 2011 · Hughes 369A · Engine (Turbine/Turboprop)SDR CA110615008Packing · splitON WALK AROUND, HYD FLUID WAS NOTICED ON RAMP AND ON LT MLG WHEELS. AC POWER WAS TURNED ON AND HYD PUMPS CYCLED AND IT WAS DETERMINED THAT HYD FLUID WAS LEAKING FROM FWD END OF MLG ACTUATOR SHAFT. LT MLG ACTUATOR DISSASSEMBLED AND FOUND PACKING ITEM 38 WAS SJun 12, 2011 · Airtrc AT802A · Landing Gear ActuatorSDR CA100729006Liner · misrepairedWHILE REMOVING THE LED PORTION OF CC OUTER LINER IAW PWC 724002-SRR-05 INCOMPLETE RESISTANCE WELD HOLDING LED PORTION IN PLACE WAS FOUND. CIRCUMFERENTIAL RESISTANCE WELD HAD SEVEN EQUALLY SPACED WELDING POINTS WHICH HELD IN PLACE THE LED PORTION INSTEAD OF COJul 28, 2010 · Beech 1900C · Turbine Engine Combustion SectionSDR CA100608009Spar · crackedAFT ATTACH POINT SPAR RADIUS FOUND CRACKED ON A WALK AROUND - VERTICAL FIN.Jun 3, 2010 · Airtrc AT802A · Vertical Stabilizer, Spar/RibSDR CA100223004Piston · wrong part(CAN) WRONG PISTON INSTALLED INTO BRAKE ASSY, PISTON PN 092-02100 FOR BRAKE ASSY 30-67B, WAS INSTALLED IN BRAKE ASSY 30-67C BRAKE ASSY 30-67C REQUIRES NO FRICTION SPRING AND SHOULD HAVE PISTON PN 092-01600 INSTALLED. REF IPC AWBPC0001-7 PAGE 4-50, 4-51. (TC 2Feb 22, 2010 · Airtrc AT802A · BrakeSDR CA091207002Frame · cracked(CAN) A REPAIR INVOLING WELDING A CRACK APPROX 1 INCH LONG LOCATED JUST ABOVE THE LT REAR FLOAT ATTACHMENT PLATE, WITHIN THE CIRCLE OF C. FIG 2 OF SL NR 71 WAS CARRIED OUT. THE FOLLOWING DAY, NOTICED A CRACK APPROX 3/4 TO 1 INCH LONG IN THE WELD THAT RUNS ARNov 24, 2009 · Airtrc AT802A · Wing SparSDR CA090728004O-Ring · cutMLG ACTUATOR LEAKING, O-RING FOUND TO HAVE CUT IN IT. ACTUATOR SEALS REPLACED. O-RING INTERNAL IN BULKHEAD SUPPORT BLOCK WHERE ACTUATOR RAM PASSES THROUGH.Jul 26, 2009 · Airtrc AT802A · Landing Gear ActuatorSDR CA081118010Mount · cracked(CAN) DURING THE 300HR/ANNUAL INSP, ENGINE MOUNT WAS BEING INSPECTED IAW AD2008-10-12 AND AIR TRACTOR`S SL NR 253C, A CRACK WAS FOUND ON THE LT LOWER ENGINE ATTACH POINT VIA 10X MAGNIFYING GLASS. ACFT HAS BEEN NOTIFIED ABOUT THE CRACK AND A NEW ENGINE MOUNT Nov 18, 2008 · Airtrc AT602 · Engine Mount SectionSDR CA071016015Engine · power loss(CAN) THE ENGINE LOST POWER DURING FIREFIGHTING OPERATIONS RESULTING IN A FORCED LANDING.Sep 17, 2007 · Airtrc AT802A · Engine (Turbine/Turboprop)SDR CA071016013Engine · power loss(CAN) THE ENGINE LOST POWER IN FLIGHT AND THE AIRCRAFT WAS DAMAGED IN THE RESULTING FORCED LANDING. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20071016013)Sep 14, 2007 · Airtrc AT602 · Engine (Turbine/Turboprop)SDR CA070313009Frame · cracked(CAN) DURING ANNUAL INSPECTION, THE LOWER LONGITUDINAL FRAME OF THE STAINLESS STEEL FIREGATE P/N 80450-1 WAS NOTED TO BE CRACKED AT THE FWD END AND BULGED AT THE AFT END. (2) OTHER AC HAVE SIMILAR DAMAGE. WATER WAS FOUND IN THE TUBE AND THE DAMAGE APPEARS TO Mar 13, 2007 · Airtrc AT802A · Nacelle/Pylon, Frame/Spar/RibSDR CA070314022Engine · flamed out(CAN) THE ENGINE WAS REPORTED TO HAVE FLAMED OUT IN FLIGHT. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE DETERMINED. (TC NR 20070314022)Feb 22, 2007 · Ayres S2RHGT65 · Engine (Turbine/Turboprop)SDR CA051006003Engine · flamed out(CAN) THE ENGINE WAS REPORTED TO HAVE FLAMED OUT ON FINAL APPROACH RESULTING IN THE AIRCRAFT LANDING SHORT OF THE RUNWAY. MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE DETERMINED.Sep 5, 2005 · Ayres S2RT660 · Engine (Turbine/Turboprop)SDR 2005FA0001114Spar · brokenTHE UPPER RUDDER SPAR WAS BROKEN 12.5 INCHES ABOVE THE UPPER HINGE. IN ADDITION, THE SPAR CRACKED UNDER THE UPPER HINGE FITTINGS. THIS CAUSED THE RUDDER COUNTER BALANCE TO BE LOOSE RESULTING IN RUDDER FLUTTER. FURTHER FLIGHT COULD HAVE RESULTED IN LOSS OF RAug 4, 2005 · N4121G · Ayres S2RT660 · Rudder, Spar/RibSDR CA050708005Proximity Switch · looseDURING CRUISE, THE PILOT NOTED A GEAR UNSAFE LIGHT FOR THE NLG. THE AIRCRAFT DID A LOW PASS AT THE AIRPORT. IT WAS DETERMINED THAT THE GEAR WAS DOWN AND IT APPEARED TO BE AN INDICATION PROBLEM. THE AIRCRAFT LANDED WITHOUT INCIDENT. DURING INVESTIGATION BY Jul 5, 2005 · Airtrc AT802A · Landing Gear Position and WarningSDR CA050614008Torque Tube · cracked(CAN) DURING ANNUAL INSPECTION, RUDDER TUBE ASSY WAS FOUND TO BE UNAIRWORTHY DUE TO CRACKS.May 18, 2005 · Airtrc AT802A · Rudder Control SystemSDR CA041118004Fairing · mislocated(CAN) DURING ANNUAL INSPECTION THE HORIZONTAL STAB FAIRING SCREW HOLES FOUND TO BE DRILLED THROUGH THE RIVETS ATTCHING THE SKIN TO THE CLOSING RIBS OF BOTH HORIZONTALSTABS. HOLES WERE LOCATED ON THE LOWER SURFACES ONLY. 7 OF 19 RIVETS WERE DRILL ED ON THE PORTNov 18, 2004 · Airtrc AT802A · Horizontal Stabilizer Miscellaneous StructureSDR CA030909002O-Ring · torn(CAN) DURING FLIGHT 1 HYDRAULIC PUMP LIGHT ILLUMINATED INDICATING LOW HYDRAULIC FLUID LEVEL. THE LANDING GEAR WAS EXTENDED NORMALLY AND THE AIRCRAFT RETURNED TO THE AIRPORT FOR A NORMAL LANDING. DURING INVESTIGATION THE MAINTENANCE CREW FOUND A HYDRAULIC LEAK Sep 7, 2003 · Airtrc AT802A · Hydraulic Pump (Electric/Engine), MainSDR AUS20020022Pipe · cracked(AUS) P3 PIPE TO FUEL CONTROL UNIT CRACKED.Jan 11, 2002 · Airtrc AT802A · Fuel Controlling SystemSDR AU010248Structure · damaged(AUS) RUDDER CRACKED AND SKIN DEFORMED IN UPPER AREA WHERE THE BALANCEHORN ATTACHES TO THE RUDDER STRUCTURE.Mar 21, 2001 · Airtrc AT802A · Rudder StructureSDR AU010249Mount · failed(AUS) LT SIDE ENGINE MOUNT RUBBER ISOLATION MOUNTS FAILED. ENGINE LOW ON LT SIDE CAUSING CHAFING OF THE FIRE SEALS ON THE BEARER.Mar 19, 2001 · Airtrc AT802A · Engine Mount SectionSDR AU981393Bolt · failed(AUS) BRAKE MASTER CYLINDER EYEBOLT FAILED AT THE LOWER END OF THE LOCKNUT CAUSING THE AIRCRAFT TO SWERVE OFF THE RUNWAY. PART TC: 800.Oct 22, 1998 · Airtrc AT802 · Master Cylinder/Brake ValveSDR AU970738Spar Cap · cracked(AUS) RH WING LOWER SPAR CAP CRACKED FROM BOLT HOLE - CRACK LENGTH 3.048MM (0.120IN) - FOUND DURING MAGNETIC PARTICLE INSPECTIONJun 27, 1997 · Ayres S2RT65 · Wing SparSDR 97ZZZM156Compressor Blade · splitFLT - 759 - MIA-PID - PILOT REPORTED NR 1 TORQUE 3000 AT 11,000 FEET AND T5 AT 770 DEG, NG 93 PERCENT. OTHER ENGINES RUNNING NORMAL WITH 3700 TORQUE. A/C RETURNED TO MIA. THE A/C WAS INSPECTED AND FOUND TO BE SAFE FOR 3 ENGINE FERRY TO FLL. MAINTENANCE REPNov 21, 1996 · N8041D · Dhav DHC7102 · Turbine Engine Compressor Section
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