# Service difficulty reports: U/A Canada PT6A-65AG

A list on [U/A Canada PT6A-65AG](https://openairdocs.org/engine/u-a-canada-pt6a-65ag.md).

Newest first. General aviation reporting is voluntary.

- [SDR CA150710014](https://openairdocs.org/sdr/CA150710014.md): Line · fractured · Jun 29, 2015 · Fuel Controlling System
  > (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
- [SDR CA150224005](https://openairdocs.org/sdr/CA150224005.md): Engine · separated · Feb 5, 2015 · Airtrc AT602 · Engine (Turbine/Turboprop)
  > (CAN) THE ENGINE LOST POWER ON TAKEOFF. THE ENGINE WAS RIPPED FROM THE FUSELAGE AND THERE WAS TAIL AND WING DAMAGE.
- [SDR CA141006008](https://openairdocs.org/sdr/CA141006008.md): Engine · power loss · Sep 9, 2014 · Hughes 369HM · Engine (Turbine/Turboprop)
  > (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.
- [SDR CA140826001](https://openairdocs.org/sdr/CA140826001.md): Engine · surges · Jul 25, 2014 · Engine (Turbine/Turboprop)
  > (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.
- [SDR CA140630013](https://openairdocs.org/sdr/CA140630013.md): Unknown · unknown · Jun 13, 2014 · Airtrc AT502B · Standard Practices/Structures
  > (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.
- [SDR CA140619019](https://openairdocs.org/sdr/CA140619019.md): Engine · power loss · Jun 5, 2014 · Airtrc AT602 · Engine (Turbine/Turboprop)
  > (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.
- [SDR CA131113008](https://openairdocs.org/sdr/CA131113008.md): Strut · corroded · Nov 13, 2013 · Airtrc AT602 · Fuselage, Stabilizer Attach Fittings
  > (CAN) DURING ANNUAL INSPECTION, IT WAS FOUND THAT THE LT STABILIZER STRUT ASSY. LOWER ATTACH FORK AND BUSHINGS WERE HEAVILY CORRODED.
- [SDR CA130822003](https://openairdocs.org/sdr/CA130822003.md): Engine · power loss · Aug 16, 2013 · Airtrc AT802A · Engine (Turbine/Turboprop)
  > (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.
- [SDR CA130614002](https://openairdocs.org/sdr/CA130614002.md): Blade · failed · May 18, 2013 · Airtrc AT802A · Turbine Section
  > (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 REPA
- [SDR CA120227009](https://openairdocs.org/sdr/CA120227009.md): Gusset · cracked · Feb 27, 2012 · Airtrc AT802A · Fuselage Main, Frame
  > (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.
- [SDR CA120130002](https://openairdocs.org/sdr/CA120130002.md): Engine · power loss · Nov 8, 2011 · Airtrc AT602 · Engine (Turbine/Turboprop)
  > (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 LAND
- [SDR CA111226002](https://openairdocs.org/sdr/CA111226002.md): Engine · power loss · Jul 22, 2011 · Hughes 369A · Engine (Turbine/Turboprop)
  > (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 WI
- [SDR CA110615008](https://openairdocs.org/sdr/CA110615008.md): Packing · split · Jun 12, 2011 · Airtrc AT802A · Landing Gear Actuator
  > ON 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 S
- [SDR CA100729006](https://openairdocs.org/sdr/CA100729006.md): Liner · misrepaired · Jul 28, 2010 · Beech 1900C · Turbine Engine Combustion Section
  > WHILE 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 CO
- [SDR CA100608009](https://openairdocs.org/sdr/CA100608009.md): Spar · cracked · Jun 3, 2010 · Airtrc AT802A · Vertical Stabilizer, Spar/Rib
  > AFT ATTACH POINT SPAR RADIUS FOUND CRACKED ON A WALK AROUND - VERTICAL FIN.
- [SDR CA100223004](https://openairdocs.org/sdr/CA100223004.md): Piston · wrong part · Feb 22, 2010 · Airtrc AT802A · Brake
  > (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 2
- [SDR CA091207002](https://openairdocs.org/sdr/CA091207002.md): Frame · cracked · Nov 24, 2009 · Airtrc AT802A · Wing Spar
  > (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 AR
- [SDR CA090728004](https://openairdocs.org/sdr/CA090728004.md): O-Ring · cut · Jul 26, 2009 · Airtrc AT802A · Landing Gear Actuator
  > MLG 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.
- [SDR CA081118010](https://openairdocs.org/sdr/CA081118010.md): Mount · cracked · Nov 18, 2008 · Airtrc AT602 · Engine Mount Section
  > (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
- [SDR CA071016015](https://openairdocs.org/sdr/CA071016015.md): Engine · power loss · Sep 17, 2007 · Airtrc AT802A · Engine (Turbine/Turboprop)
  > (CAN) THE ENGINE LOST POWER DURING FIREFIGHTING OPERATIONS RESULTING IN A FORCED LANDING.
- [SDR CA071016013](https://openairdocs.org/sdr/CA071016013.md): Engine · power loss · Sep 14, 2007 · Airtrc AT602 · Engine (Turbine/Turboprop)
  > (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)
- [SDR CA070313009](https://openairdocs.org/sdr/CA070313009.md): Frame · cracked · Mar 13, 2007 · Airtrc AT802A · Nacelle/Pylon, Frame/Spar/Rib
  > (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
- [SDR CA070314022](https://openairdocs.org/sdr/CA070314022.md): Engine · flamed out · Feb 22, 2007 · Ayres S2RHGT65 · Engine (Turbine/Turboprop)
  > (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)
- [SDR CA051006003](https://openairdocs.org/sdr/CA051006003.md): Engine · flamed out · Sep 5, 2005 · Ayres S2RT660 · Engine (Turbine/Turboprop)
  > (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.
- [SDR 2005FA0001114](https://openairdocs.org/sdr/2005FA0001114.md): Spar · broken · Aug 4, 2005 · N4121G · Ayres S2RT660 · Rudder, Spar/Rib
  > THE 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 R
- [SDR CA050708005](https://openairdocs.org/sdr/CA050708005.md): Proximity Switch · loose · Jul 5, 2005 · Airtrc AT802A · Landing Gear Position and Warning
  > DURING 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
- [SDR CA050614008](https://openairdocs.org/sdr/CA050614008.md): Torque Tube · cracked · May 18, 2005 · Airtrc AT802A · Rudder Control System
  > (CAN) DURING ANNUAL INSPECTION, RUDDER TUBE ASSY WAS FOUND TO BE UNAIRWORTHY DUE TO CRACKS.
- [SDR CA041118004](https://openairdocs.org/sdr/CA041118004.md): Fairing · mislocated · Nov 18, 2004 · Airtrc AT802A · Horizontal Stabilizer Miscellaneous Structure
  > (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 PORT
- [SDR CA030909002](https://openairdocs.org/sdr/CA030909002.md): O-Ring · torn · Sep 7, 2003 · Airtrc AT802A · Hydraulic Pump (Electric/Engine), Main
  > (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
- [SDR AUS20020022](https://openairdocs.org/sdr/AUS20020022.md): Pipe · cracked · Jan 11, 2002 · Airtrc AT802A · Fuel Controlling System
  > (AUS) P3 PIPE TO FUEL CONTROL UNIT CRACKED.
- [SDR AU010248](https://openairdocs.org/sdr/AU010248.md): Structure · damaged · Mar 21, 2001 · Airtrc AT802A · Rudder Structure
  > (AUS) RUDDER CRACKED AND SKIN DEFORMED IN UPPER AREA WHERE THE BALANCEHORN ATTACHES TO THE RUDDER STRUCTURE.
- [SDR AU010249](https://openairdocs.org/sdr/AU010249.md): Mount · failed · Mar 19, 2001 · Airtrc AT802A · Engine Mount Section
  > (AUS) LT SIDE ENGINE MOUNT RUBBER ISOLATION MOUNTS FAILED. ENGINE LOW ON LT SIDE CAUSING CHAFING OF THE FIRE SEALS ON THE BEARER.
- [SDR AU981393](https://openairdocs.org/sdr/AU981393.md): Bolt · failed · Oct 22, 1998 · Airtrc AT802 · Master Cylinder/Brake Valve
  > (AUS) BRAKE MASTER CYLINDER EYEBOLT FAILED AT THE LOWER END OF THE LOCKNUT CAUSING THE AIRCRAFT TO SWERVE OFF THE RUNWAY. PART TC: 800.
- [SDR AU970738](https://openairdocs.org/sdr/AU970738.md): Spar Cap · cracked · Jun 27, 1997 · Ayres S2RT65 · Wing Spar
  > (AUS) RH WING LOWER SPAR CAP CRACKED FROM BOLT HOLE - CRACK LENGTH 3.048MM (0.120IN) - FOUND DURING MAGNETIC PARTICLE INSPECTION
- [SDR 97ZZZM156](https://openairdocs.org/sdr/97ZZZM156.md): Compressor Blade · split · Nov 21, 1996 · N8041D · Dhav DHC7102 · Turbine Engine Compressor Section
  > FLT - 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 REP

## 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 = 'PT6A65AG'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/u-a-canada-pt6a-65ag/reports

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