# Service difficulty reports: U/A Canada PT6A-34

A list on [U/A Canada PT6A-34](https://openairdocs.org/engine/u-a-canada-pt6a-34.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 10 · 465 reports

- [SDR 2025F00092](https://openairdocs.org/sdr/2025F00092.md): Rivet · loose · Apr 13, 2025 · Quest KODIAK100 · Fuselage Main, Structure
  > THERE ARE FOUR RIVETS AROUND THE MLG FRAMES (INSIDE THE FUSELAGE, ALONG THE SEAT TRACKS) THAT ARE SMOKING (TWO ON THE RIGHT SIDE OF THE FUSELAGE, TWO ON THE LEFT SIDE). ON ANOTHER KODIAK 100 OUR ORGANIZATION OPERATES IN KALIMANTAN, INDONESIA, ONE OF THESE RIV
- [SDR 2024FA0000334](https://openairdocs.org/sdr/2024FA0000334.md): Lock Fastener · loose · Jan 11, 2024 · N423JT · Piper PA46350P · Fuselage, Wing Attach Fittings
  > AFT WING FITTING LOCK FASTENERS FOUND LOOSE ON LEFT AND RIGHT WING. ADDRESSED IN PIPPER SB820A BUT NOT APPLICABLE TO THIS MODEL AIRCRAFT AND SHOULD BE.
- [SDR 2022F00200](https://openairdocs.org/sdr/2022F00200.md): Lamp · broken · Apr 7, 2022 · N117WA · Emb EMB110P1 · Flight Compartment Lighting
  > THE PILOT REPORTED A VISIBLE PUFF OF SMOKE FROM THE OVERHEAD PANEL AREA TO MAINTENANCE. MAINTENANCE FOUND TWO WHEAT BULBS BROKEN AND POSSIBLY SHORTED TOGETHER IN DE-ICE PANEL BACK LIGHTING. NO OTHER ELECTRICAL ISSUES WERE FOUND. ALL SYSTEMS WERE FUNCTIONAL.
- [SDR CA190807008](https://openairdocs.org/sdr/CA190807008.md): Rod End · corroded · Aug 6, 2019 · Vikair DHC6400 · Fuel Control/Reciprocating Engines
  > (CAN) MSN 974 LEFT ENGINE FAILED TO RETURN TO LOWER POWER SETTING DURING TAXI THIS MORNING. WHEN L/H POWER LEVER RETURN TO IDLE POSITION THE NG STILL 68%, R/H IS NORMAL. AFTER REMOVE THE FCU CONTROL ROD, CORROSION IS FOUND ON ROD END BEARING. THEN WE HAVE RE
- [SDR AXSA2019061400019](https://openairdocs.org/sdr/AXSA2019061400019.md): Blades · cracked · Jun 14, 2019 · N116WA · Emb EMB110P1 · Turbine Section
  > DURING A HOT SECTION 3 CT BLADES WERE FOUND TO BE CRACKED AT THE FIR TREE.
- [SDR CA190709014](https://openairdocs.org/sdr/CA190709014.md): Fuel Control · malfunctioned · Jun 11, 2019 · Dhav DHC3 · Fuel Control/Turbine Engines
  > (CAN) PILOT APPLIED REVERSE POWER TO BACK AWAY FROM THE DOCK. WHEN THE POWER LEVER WAS MOVED BACK TO THE IDLE POSITION, THE ENGINE ACCELERATED UNCONTROLLED. PILOT TRIED TO SLOW THE AIRCRAFT DOWN BY PLACING POWER LEVER BACK INTO BETA RANGE, THE ENGINE DECELERAT
- [SDR CA190412007](https://openairdocs.org/sdr/CA190412007.md): Engine · damaged · Apr 10, 2019 · Dhav DHC3 · Turbine Engine Combustion Section
  > (CAN) DURING A NON-SCHEDULED HOT SECTION INSPECTION, THE BOLTS (PART NUMBER MS9574-06) SECURING THE CONTAINMENT RING TO POWER TURBINE VANE RING AT FLANGE D WERE FOUND LOOSE. THE LOCKWIRE WAS INTACT, BUT THERE WAS EVIDENCE OF FRETTING FOUND UNDERNEATH THE HEADS
- [SDR CA190412006](https://openairdocs.org/sdr/CA190412006.md): Duct · cracked · Apr 10, 2019 · Dhav DHC3 · Turbine Engine Combustion Section
  > (CAN) DURING A REGULARLY SCHEDULED BORESCOPE INSPECTION, DAMAGE WAS NOTED ON THE LARGE EXIT DUCT (LED). UPON FURTHER INSPECTION, A CRACK WAS FOUND ON THE INNER LINING AND NUMEROUS CRACKS WERE FOUND ON THE OUTER LINING ALONG THE WELD SEAM. (TC# 20190412006)
- [SDR CA190227016](https://openairdocs.org/sdr/CA190227016.md): Fuel Control · failed · Feb 24, 2019 · Dhav DHC3 · Fuel Control/Turbine Engines
  > (CAN) TO INITIATE DESCENT FOR LANDING, THE PILOT BROUGHT BACK THE POWER. AS THE POWER LEVER WAS BROUGHT BACK, POWER (INDICATED AND ACTUAL) STOPPED REDUCING AROUND 40 PSI, THE THROTTLE LEVER WAS ULTIMATELY BROUGHT TO THE IDLE STOP (GATE) WITH THE POWER (INDICAT
- [SDR CA190307019](https://openairdocs.org/sdr/CA190307019.md): Fuel Control · malfunctioned · Feb 16, 2019 · Dhav DHC3 · Fuel Control/Turbine Engines
  > (CAN) PILOT REPORTED THAT THE AIRCRAFT WAS NOT MAKING MAX POWER. ENGINE GROUND RUNS WERE CARRIED OUT AND WAS UNABLE TO OBTAIN MAX NG. ALSO, THE NG WAS NOT STABLE, IT WAS SLOWLY DECELERATING. THE FCU, PART NUMBER 3244786-8-7, WAS CHANGED AND MAX POWER WAS OBTAI
- [SDR CA190424021](https://openairdocs.org/sdr/CA190424021.md): Hose · leaking · Nov 18, 2018 · Vikair DHC6400 · Engine Air Intake System
  > (CAN) HOSE SPLIT AND LEAKING.
- [SDR AXSA2018082700001](https://openairdocs.org/sdr/AXSA2018082700001.md): Engine · unknown · Aug 25, 2018 · N118WA · Emb EMB110P1 · Engine (Turbine/Turboprop)
  > DURING CLIMB OUT, LEAVING 3500 FEET, A MUFFLED BANG WAS HEARD, FOLLOWED BY A YAW. THE ENGINE FAILURE DRILL WAS CARRIED OUT FOLLOWED BY THE CHECKLIST AFTER AN EMERGENCY WAS DECLARED. AN UNEVENTFUL LANDING WAS CARRIED OUT, AN ASSESSMENT OF NO FIRE WAS MADE B
- [SDR CA180822003](https://openairdocs.org/sdr/CA180822003.md): Line · leaking · Aug 13, 2018 · Quest KODIAK100 · Hydraulic System, Main
  > (CAN) THE PILOT REPORTED WHILE RETRACTING THE LANDING GEAR AFTER TAKEOFF, THE LANDING GEAR CIRCUIT BREAKER TRIPPED WITH THE LANDING GEAR AT MID RETRACTION. THE LANDING GEAR WAS PUMPED DOWN MANUALLY, AND A PRECAUTIONARY LANDING WAS MADE TO A REMOTE MAINTENANCE
- [SDR CA180616004](https://openairdocs.org/sdr/CA180616004.md): Pressure Switch · broken · May 28, 2018 · Vikair DHC6400 · Aircraft Fuel Distribution System
  > (CAN) FALSE INDICATION OF AMOUNT OF FUEL ATA 28-00. (TC# 20180616004)
- [SDR CA180616005](https://openairdocs.org/sdr/CA180616005.md): Probe · false indication · May 28, 2018 · Vikair DHC6400 · Fuel Indicating System
  > (CAN) FALSE INDICATION OF AMOUNT OF FUEL ATA 28-00. (TC# 20180616005)
- [SDR FAA2018052500164](https://openairdocs.org/sdr/FAA2018052500164.md): Pressure Switch · intermittent · May 25, 2018 · N153QS · Dhav DHC6 · Propeller Controlling System
  > AFTER TAKE OFF, AT 300 FT, THE NR 2 PROPELLER AUTOFEATHERED, THE AUTOFEATHER WAS SELECTED OFF AND THE PROPELLER UNFEATHERED AND RETURNED TO NORMAL OPS. TORQUE WAS OBSERVED BY THE CREW DURING THE AUTOFEATHER AND THE THROTTLE WAS RETARDED TO PREVENT AN OVER TOR
- [SDR CA180616003](https://openairdocs.org/sdr/CA180616003.md): Pressure Switch · fluctuates · May 12, 2018 · Vikair DHC6400 · Hydraulic Pressure Regulator, Auxiliary
  > (CAN) HYDRAULIC PRESSURE SWITCH PRE MOD 6/2313 DROPS TO 1220 PSI. OUTSIDE THE PERMISSIBLE LIMIT, SWITCH OPENS AT INCONSISTENT PRESSURES IN 1480, 1520,1500 PSI`S ATA 29-00. (TC# 20180616003)
- [SDR CA180510013](https://openairdocs.org/sdr/CA180510013.md): Duct · damaged · May 10, 2018 · Turbine Engine Combustion Section
  > (CAN) DURING ENGINE REPAIR, DAMAGE WAS NOTED ON THE LARGE EXIT DUCT (LED). THE LED HAD 818.5 HOURS AND 1806 CYCLES SINCE REPAIR. THE FOLLOWING WAS REPORTED BY THE REPAIR SHOP: SYMPTOMS: INSPECTION FINDING CRACKING AT OUTER SEAM WELD. CRACKING/BURNING AT SM
- [SDR CA180404016](https://openairdocs.org/sdr/CA180404016.md): Control Cable · chafed · Apr 2, 2018 · Vikair DHC6400 · Aileron Control System
  > (CAN) DURING THE EMMA 2 INSPECTION IT WAS DISCOVERED THAT THE LEFT HAND AILERON CABLE WAS CHAFING ON THE STEERING CABLE AT THE BASE OF THE YOKE. THE CHAFING OCCURRED AS THE YOKE WAS PULLED BACK PAST LEVEL FLIGHT. CABLES WERE INSPECTED AND FOUND TO BE UNDAMA
- [SDR CA180222018](https://openairdocs.org/sdr/CA180222018.md): Pump · failed · Jan 24, 2018 · Vikair DHC6400 · Fuel Boost Pump
  > (CAN) FORWARD BOOT PUMP 1 FAILURE ON TAXI IN AT GLA. (TC NR 20180222018).
- [SDR 4P1A2017042400001](https://openairdocs.org/sdr/4P1A2017042400001.md): Igniter · broken · Apr 24, 2017 · N120KQ · Quest KODIAK100 · Spark Plug/Igniter
  > WHEN PERFORMING A PROGRESSIVE ROUTINE 300 HOUR INSPECTION ON THE ENGINE, FOUND PART OF THE RIGHT IGNITER MISSING. PERFORMED A BORESCOPE INSPECTION AND FOUND MELTED PIECES ON THE POWER TURBINE BLADES AND IN THE RIGHT EXHAUST DUCT. THERE WAS ALSO DENTS IN A CO
- [SDR 4P1A2017021500001](https://openairdocs.org/sdr/4P1A2017021500001.md): Battery Cable · chafed · Feb 15, 2017 · N120KQ · Quest KODIAK100 · Electrical Power System Wiring
  > PILOT REPORTED THAT THE ALTERNATOR FAIL LIGHT CAME ON BUT THE ALTERNATOR CONTINUED TO WORK. WHEN THE AIRCRAFT RETURNED TO HOME BASE, REPLACED THE ALTERNATOR CONTROL UNIT. ON THE RETURN TO SERVICE FLIGHT THE ALTERNATOR FAIL LIGHT CAME ON AGAIN. DECIDED TO REPLA
- [SDR CA160301016](https://openairdocs.org/sdr/CA160301016.md): Ignition Lead · worn · Feb 23, 2016 · Dhav DHC3 · Ignition Harness (Distribution)
  > (CAN) DURING A REGULARLY SCHEDULED INSPECTION, THE LEFT HAND IGNITION LEAD, P/N CH53399-04, WAS FOUND TO BE WORN AT THE IGNITER ATTACHMENT END. THE LEAD HAD 509.2 HOURS SINCE INSTALLATION. THIS OPERATOR HAS HAD NUMEROUS PROBLEMS WITH IGNITION LEADS FAILING.
- [SDR CA160225005](https://openairdocs.org/sdr/CA160225005.md): Ignition Lead · failed · Feb 21, 2016 · Dhav DHC3 · Ignition Harness (Distribution)
  > (CAN) DURING A REGULARLY SCHEDULED INSPECTION, THE LEFT HAND IGNITION LEAD, WAS FOUND TO BE WORN AT THE IGNITER ATTACHMENT END. THIS OPERATOR HAS HAD NUMEROUS PROBLEMS WITH IGNITION LEADS FAILING.
- [SDR CA160125010](https://openairdocs.org/sdr/CA160125010.md): Door · mismanufactured · Jan 15, 2016 · Dhav DHC6* · Fixed Inner Doors
  > (CAN) DURING ROUTINE MAINTENCE, FOUND 2 PROBLEMS WITH THE ICA`S. ON AN EMMA, EQUALIZED MAINTENANCE MAXIMUM AVAILABILITY, INSPECTION CARD 15, SECTION 3B, THE FLIGHT COMPARTMENT DOORS ARE TO BE INSPECTED FOR HIRF BONDING WITH A SPECIFICATION OF 10 MILLIOHMS. T
- [SDR CA160111012](https://openairdocs.org/sdr/CA160111012.md): Seal · defective · Jan 11, 2016 · Dhav DHC6* · Aircraft Fuel Distribution System
  > (CAN) FUEL MOTIVE LINE STRAINER, CHECK VALVE FOUND TO HAVE A SWOLLEN RUBBER SEAL WHICH PREVENTED THE FLAPPER FROM SEALING. SPRING UNABLE TO RETURN VALVE TO CLOSED POSITION.
- [SDR AXSA20150107001](https://openairdocs.org/sdr/AXSA20150107001.md): Link · detached · Jan 6, 2016 · N830AC · Emb EMB110P1 · Landing Gear Door Retract Section
  > MORNING FLIGHT 1050, DEPARTED AT 0735 LOCAL TIME, BUT PERFORMED AN AIR RETURN TO ITS STARTING POINT AT 0752 DUE TO A GEAR NOT RETRACTED INDICATION. MX TECHNICIAN DETERMINED THAT A QUICK RELEASE DOOR LINK HAD COME OFF, ALLOWING THE LT MLG TO CONTACT ITS BELL C
- [SDR CA151205001](https://openairdocs.org/sdr/CA151205001.md): Axle · cracked · Dec 3, 2015 · Dhav DHC6300 · Main Landing Gear Strut/Axle/Truck
  > (CAN) DURING ROUTINE EMMA INSPECTION AXLE P/N C6UM1134-27 WAS FOUND TO HAVE A SUSPECTED CRACK AROUND BARREL APPROXIMATELY 3" LONG. PART WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE.
- [SDR CA151216008](https://openairdocs.org/sdr/CA151216008.md): Engine · malfunctioned · Dec 3, 2015 · Pac 750XL · Engine (Turbine/Turboprop)
  > (CAN) JUST AFTER DROPPING SKYDIVERS, THE PILOT FELT A VIBRATION AND SAW THAT THE ENGINE TORQUE READING WAS IN THE RED ARC. HE ELECTED TO PERFORM AN ENGINE SHUT DOWN AND GLIDE BACK TO THE AIRPORT. THE AIRCRAFT HOWEVER LANDED SHORT OF THE INTENDED RUNWAY CAUSIN
- [SDR AXSA2015112590038](https://openairdocs.org/sdr/AXSA2015112590038.md): Turbine Wheel · disintegrated · Nov 24, 2015 · N117WA · Emb EMB110P1 · Turbine Section
  > THE PILOT REPORTED THAT IN CRUISE, APPROX 20 MINUTES AFTER TAKEOFF, THE RT ENG SURGED MORE THAN ONCE & HE ELECTED TO SHUT IT DOWN. HE THEN DECLARED AN EMER & DIVERTED, MAKING A SUCCESSFUL LANDING. A VISUAL INSPECTION WITH BORESCOPE BY MX PERSONNEL REVEALED M
- [SDR CA151110010](https://openairdocs.org/sdr/CA151110010.md): Ignition Lead · damaged · Nov 8, 2015 · Dhav DHC3 · Ignition Harness (Distribution)
  > (CAN) DURING A REGULARLY SCHEDULED INSPECTION, THE LEFT HAND IGNITION LEAD, P/N CH53399-04, WAS FOUND TO BE WORN AT THE IGNITER ATTACHMENT END. THE LEAD HAD 389.5 HOURS SINCE INSTALLATION. THIS OPERATOR HAS HAD NUMEROUS PROBLEMS WITH IGNITION LEADS FAILING.
- [SDR CA151102015](https://openairdocs.org/sdr/CA151102015.md): Aileron · mismanufactured · Nov 2, 2015 · Dhav DHC6* · Aileron Control System
  > (CAN) PRODUCTION HAS REPORTED THAT THE HUB, FORK, AILERON OUTER WING, HAS BEEN MFG INCORRECTLY. IT HAS BEEN FOUND THAT HUBS WERE MISSING THE.03" X 45 CHAMFER AROUND THE.2495-.2505" DIAMETER HOLE. THE SHARP EDGE IS BROKEN, 0.005" TO 0.010", BUT THE CHAMFER
- [SDR CA151022007](https://openairdocs.org/sdr/CA151022007.md): Ignition Lead · worn · Oct 21, 2015 · Dhav DHC3 · Ignition Harness (Distribution)
  > (CAN) DURING A REGULARLY SCHEDULED INSPECTION, THE RIGHT HAND IGNITION LEAD, P/N CH53399-04, WAS FOUND TO BE WORN AT THE IGNITER ATTACHMENT END. THE TIP WAS BENT. THIS OPERATOR HAS HAD NUMEROUS PROBLEMS WITH IGNITION LEADS FAILING.
- [SDR CA151029025](https://openairdocs.org/sdr/CA151029025.md): Rod End · seized · Oct 14, 2015 · Dhav DHC6* · Fuel Control/Turbine Engines
  > (CAN) DURING GROUND RUN-UP FCU CONTROL ROD, PN C6CE1398-3 HAD STIFF/SEIZED END BEARINGS, PN DSC4-3A ON NR 2 ENGINE. FCU ROD AND END BEARINGS REPLACED.
- [SDR CA151014009](https://openairdocs.org/sdr/CA151014009.md): G Switch · failed · Oct 9, 2015 · Dhav DHC3 · Emergency Locator Beacon
  > (CAN) DURING THE ELT ANNUAL RECERTIFICATION, BENCH TESTING FOUND THAT THE G-SWITCH FAILED. THERE WERE ALSO TWO SCREWS WITH O - RINGS MISSING AND THE H-SHIELD WAS CRACKED. THIS OPERATOR HAS HAD SEVERAL OTHER ELT G-SWITCHES FAIL BENCH TESTING AND REQUIRED REPLA
- [SDR CA150924009](https://openairdocs.org/sdr/CA150924009.md): Altimeter · malfunctioned · Sep 21, 2015 · Beech A100 · Altimeter, Barometric/Encoder
  > (CAN) IMMEDIATELY UPON BECOMING AIRBORNE, FLIGHT CREW NOTICED THE CAPTAIN`S ALTIMETER HAD FLAGGED AND CONTINUED TO INDICATE FIELD ELEVATION THROUGHOUT THE CLIMB. ATC REPORTED THAT TRANSPONDER MODE C WAS NOT RECEIVED. THE CO-PILOT`S INSTRUMENTS FUNCTIONED NOR
- [SDR CA150923007](https://openairdocs.org/sdr/CA150923007.md): Lock · bent · Sep 18, 2015 · Quest KODIAK100 · Flight Compartment Equipment
  > (CAN) AIRCRAFT WAS INSPECTED FOLLOWING RECEIPT OF MFG SAFETY COMMUNIQUE QSC-008. CO-PILOT SEAT FOUND WITH DAMAGE EXACTLY AS DESCRIBED IN THE COMMUNIQUE. NO SEAT LOCKING DIFFICULTY WAS NOTED BY CREW PRIOR TO NOTICING DEFECT.
- [SDR CA150831008](https://openairdocs.org/sdr/CA150831008.md): Ignition Lead · broken · Aug 26, 2015 · Dhav DHC3 · Ignition Harness (Distribution)
  > (CAN) DURING A REGULARLY SCHEDULED INSPECTION, THE RIGHT HAND IGNITION LEAD WAS FOUND TO BE BROKEN AT THE IGNITER ATTACHMENT END. THE LEAD HAD A TSN OF 833.9 HOURS. THIS OPERATOR HAS HAD NUMEROUS PROBLEMS WITH IGNITION LEADS FAILING. IT SEEMS TO BE MOSTLY THE
- [SDR CA150828003](https://openairdocs.org/sdr/CA150828003.md): Engine · power loss · Aug 16, 2015 · Dhav DHC2MK3 · Engine (Turbine/Turboprop)
  > (CAN) ON TAKEOFF ALL ENGINE PARAMETERS ARE NORMAL AND WITHIN 5 SECONDS PROP RPM ONLY STARTS TO ROLLBACK TOWARDS FEATHER NO OTHER PARAMETERS FOLLOW. USE OF STANDBY THROTTLE THEN INCREASES PROP RPM TO MAINTAIN FLIGHT. BOTH THE PROP GOVERNOR AND PROP OVER-SPEED G
- [SDR CA150818009](https://openairdocs.org/sdr/CA150818009.md): Ignition Lead · worn · Aug 12, 2015 · Dhav DHC3 · Ignition Harness (Distribution)
  > (CAN) DURING A REGULARLY SCHEDULED INSPECTION, BOTH LEFT AND RIGHT HAND IGNITION LEADS WERE FOUND TO BE WORN AT THE IGNITER ATTACHMENT ENDS.
- [SDR CA150831010](https://openairdocs.org/sdr/CA150831010.md): Duct · cracked · Aug 10, 2015 · Dhav DHC3 · Turbine Engine Combustion Section
  > (CAN) DURING A SCHEDULED HOT SECTION INSPECTION, THE LARGE EXIT DUCT (LED) WAS FOUND CRACKED IN MULTIPLE LOCATIONS ALONG THE OUTER SEAM WELD. THE TSO OF THE LED IS 1687.8 HOURS. THIS OPERATOR HAS HAD NUMEROUS PREVIOUS INSTANCES OF CRACKED LED`S.
- [SDR CA150721005](https://openairdocs.org/sdr/CA150721005.md): Door · open · Jul 10, 2015 · Dhav DHC6* · Passenger/Crew Doors
  > (CAN) AN AIR OPERATOR RECENTLY EXPERIENCED AN EVENT WHERE THE MAIN CABIN PASSENGER DOOR OPENED IN FLIGHT. THIS HAPPENED ON APPROACH IN TURBULENT WEATHER CONDITIONS. THE OPERATOR CONCLUDED THAT THERE WAS NO FAULT IN THE DOOR LOCKING MECHANISM BUT NOTED THAT THE
- [SDR CA150727002](https://openairdocs.org/sdr/CA150727002.md): Engine · shutdown · Jul 10, 2015 · Pac 750XL · Engine (Turbine/Turboprop)
  > (CAN) DURING FLIGHT, THE ACFT EXPERIENCED POWER LOSS RESULTING IN THE UNCOMMANDED SHUTDOWN OF THE ENGINE. THE PILOT MADE AN EMERGENCY LANDING. ENGINE WILL BE REMOVED AND SENT FOR INVESTIGATION.
- [SDR 2015FA0000397](https://openairdocs.org/sdr/2015FA0000397.md): Blade · failed · Jul 9, 2015 · N820AB · Pac 750XL · Turbine Section
  > ENGINE EXPERIENCED TOTAL POWER LOSS JUST AFTER TAKEOFF DURING INITIAL CLIMB. PILOT EXECUTED A POWER OFF LANDING ON AN AIRPORT TAXIWAY WITH NO DAMAGE TO THE ACFT OR INJURY TO THE OCCUPANTS. THE COWLING WAS REMOVED AND THERE WAS NO OBSERVED EXTERNAL DAMAGE TO
- [SDR CA150728004](https://openairdocs.org/sdr/CA150728004.md): Engine · power loss · Jul 9, 2015 · Ayres S2RT34NORMAL · Engine (Turbine/Turboprop)
  > (CAN) DURING TAKEOFF, THE PILOT REPORTED LOSING POWER FORCING A LANDING IN A CORN FIELD. ENGINE KEPT RUNNING FOR SOME 40 SECONDS AFTER THE FORCED LANDING. NTSB IS IN CHARGE OF THE INVESTIGATION AND ASSISTANCE WAS REQUIRED.
- [SDR 2016FA0000277](https://openairdocs.org/sdr/2016FA0000277.md): Compressor · damaged · Jul 9, 2015 · N820AB · Pac 750XL · Turbine Engine Compressor Section
  > ENGINE EXPERIENCED TOTAL POWER LOSS JUST AFTER TAKEOFF, DURING INITIAL CLIMB. PILOT EXECUTED A POWER OFF LANDING ON AN AIRPORT TAXIWAY WITH NO DAMAGE TO THE AIRCRAFT OR INJURY TO THE OCCUPANTS. THE COWLING WAS REMOVED AND THERE WAS NO OBSERVED EXTERNAL DAMAG
- [SDR AXSA20150722001](https://openairdocs.org/sdr/AXSA20150722001.md): Transponder · smoke · Jun 30, 2015 · N119WA · Emb EMB110P1 · ATC Transponder System
  > PILOT REPORTED SMOKE COMING FROM BEHIND TRANSPONDER.
- [SDR CA150713005](https://openairdocs.org/sdr/CA150713005.md): Engine · malfunctioned · Jun 30, 2015 · Quest KODIAK100 · Engine (Turbine/Turboprop)
  > (CAN) THE PILOT REPORTED THAT DURING DESCEND AT APPROX 1000 FT ITT STARTED TO CLIMB, ALL OTHER PARAMETERS REMAINED NORMAL. AFTER LANDING THE PILOT DECIDED TO SHUT DOWN THE ENG & REQUIRED ASSISTANCE TO TAXI THE ACFT. NO INJURIES WERE REPORTED MFG WILL INVESTI
- [SDR CA150629022](https://openairdocs.org/sdr/CA150629022.md): Motor · failed · Jun 28, 2015 · Dhav DHC3 · Fuel Boost Pump
  > (CAN) WHEN NR 2 BOOST PUMP WAS SELECTED, PUMP SOUNDED VERY ROUGH & LABORED. OVERHAULED MOTOR WAS INSTALLED & DEFECT WAS CLEARED.
- [SDR CA150622004](https://openairdocs.org/sdr/CA150622004.md): Wire · corroded · Jun 19, 2015 · Dhav DHC6* · Communications System Wiring
  > (CAN) HF ANTENNA WIRE FAILED DUE TO CORROSION, RESULTING FROM WATER INGRESS INTO THE FEED THROUGH IPC REFERENCE 23-10-00 FIG 1.

Next page: https://openairdocs.org/engine/u-a-canada-pt6a-34/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 = 'PT6A34'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/u-a-canada-pt6a-34/reports

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