# U/A Canada PT6A-34 - Type: Engine model (FAA registry) - Registry code: 61534 - Manufacturer (registry): U/A CANADA - Model: PT6A-34 - Engine type: Turbo-prop - Power: 750 hp - Installed in: 3 registered aircraft - Page: https://openairdocs.org/engine/u-a-canada-pt6a-34 Model codes come from the FAA registry's reference file. ## ADs that may apply (OpenAirDocs) Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. None matched. ## Registered aircraft (3) - [N118WA](https://openairdocs.org/aircraft/N118WA): [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE), [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake), built 1980, S/N 110.250 - [N147MV](https://openairdocs.org/aircraft/N147MV): [Air Legends Foundation](https://openairdocs.org/faa-owner/AIR%20LEGENDS%20FOUNDATION), [San Antonio, TX](https://openairdocs.org/faa-place/TX/San%20Antonio), S/N J-50 - [N40214](https://openairdocs.org/aircraft/N40214): [American Ag Aviation Inc DBA](https://openairdocs.org/faa-owner/AMERICAN%20AG%20AVIATION%20INC%20DBA), [Five Points, CA](https://openairdocs.org/faa-place/CA/Five%20Points), built 1980, S/N T34-032 ## NTSB investigations (8) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB GAA20CA020](https://openairdocs.org/ntsb/GAA20CA020), Oct 11, 2019: Ayres S2R (N3090C), Willacoochee, GA, substantial damage. Probable cause: The pilot's failure to maintain clearance from power lines while maneuvering at low altitude. - [NTSB NYC05FA042](https://openairdocs.org/ntsb/NYC05FA042), Jan 14, 2005: Embraer EMB-110P1 (N49BA), Swanzey, NH, destroyed, 1 fatal. Probable cause: The pilot's improper decision to attempt a single-engine missed approach with the airplane in a slow airspeed, full flap configuration, which resulted in a minimum control speed (Vmc) roll.… - [NTSB MIA01IA144](https://openairdocs.org/ntsb/MIA01IA144), May 22, 2001: Grumman G-73 (N142PA), Fort Lauderdale, FL, incident, minor damage. Probable cause: The improper review of component records by company maintenance personnel of returned landing gear components from a laboratory for magnaflux and x-ray. This resulted in unserviceable components… - [NTSB MIA00IA186](https://openairdocs.org/ntsb/MIA00IA186), Jun 11, 2000: Grumman G-73T (N142PA), Watson Island, FL, incident, minor damage. Probable cause: the overload separations of the control yoke on the captain's side. - [NTSB FTW96LA069](https://openairdocs.org/ntsb/FTW96LA069), Dec 13, 1995: Ayres S2R-T34 (N3090C), West Helena, AR, substantial damage. Probable cause: Binding of the power lever linkage, due to corrosion, which resulted in a situation that led to an inadvertent shut-down of the engine at a critical point on the approach to land. A factor relating… - [NTSB DCA86AA021](https://openairdocs.org/ntsb/DCA86AA021), Mar 14, 1986: Embraer EMB-110P1 (N1356P), Alpena, MI, destroyed, 3 fatal - [NTSB CHI83IA103](https://openairdocs.org/ntsb/CHI83IA103), Feb 4, 1983: Embraer EMB-110 (N1356P), Milwaukee, WI, incident, minor damage - [NTSB SEA82IA029](https://openairdocs.org/ntsb/SEA82IA029), Feb 18, 1982: Embraer EMB-11OP1 (N101RA), Boise, ID, incident, minor damage ## FAA accident and incident reports (15) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Accident 20191011021119A](https://openairdocs.org/incident/20191011021119A), Oct 11, 2019: Ayres Corporation S2R-T34 (N3090C), Willacoichee, GA, Destroyed. I arrived at the accident site Saturday 10/12/2019 @ 1230 eastern time. I spoke with the land owner who was on site when the accident occurred. He stated the… - [Incident 20180825018529I](https://openairdocs.org/incident/20180825018529I), Aug 25, 2018: Embraer EMB-110P1 (N118WA), Syracuse, NY, No damage. On 08/25/2018, wiggins airways EMB-110, N118WA was departing from syr on flight number 1346 to kptd. As the aircraft was leaving 3500?, the pilot stated they… - [Incident 20050422008279I](https://openairdocs.org/incident/20050422008279I), Apr 22, 2005: Gulstm G73 (N142PA), Ft Lauderdale, FL, Minor damage. (-23) Flight was conducting an operational flight after control surface maintenance. Operational flight completed with no problems. Upon returning to fll gear… - [Accident 20050113000719A](https://openairdocs.org/incident/20050113000719A), Jan 13, 2005: Emb EMB110P1 (N49BA), Keene, NH, Destroyed, 1 fatal. (-23) The aircraft crashed during an ILS to runway 02 at the Keene/Dillant-Hopkins Airport (een). The aircraft was in IMC conditions during the approach. The… - [Incident 20010522012019I](https://openairdocs.org/incident/20010522012019I), May 22, 2001: Gulstm G73 (N142PA), Ft Lauderdale, FL, Minor damage. (.4) On may 22, 2001, at about 1746 eastern daylight time, a Grumman G-73, N142PA, registered to seaplane leasing ii LLC, operated by flying boat inc, doing… - [Incident 20000611035039I](https://openairdocs.org/incident/20000611035039I), Jun 11, 2000: Gulstm G73 (N142PA), Watson Island, FL, Minor damage. (-23)On June 11, 2000, at 1130 am, a Grumman G73T, N142PA landed at Watson Island. As the aircraft was water taxing, the pilot applied rearward movement to the… - [Accident 19951213040459A](https://openairdocs.org/incident/19951213040459A), Dec 13, 1995: Ayres S2RT34NORMAL (N3090C), Helena/West Hel, AR, Substantial damage. Ferrying to airport for annual. Throttle jammed at cruise. Tried land. Condition lever idle cut off. Landed short. - [Incident 19910826047609I](https://openairdocs.org/incident/19910826047609I), Aug 26, 1991: Gulstm G73 (N609SS), San Juan, Puerto Rico, Minor damage. While taxiing to gate the left top engine cowling departed aircraft. Hit propeller. - [Incident 19880803057889I](https://openairdocs.org/incident/19880803057889I), Aug 3, 1988: Ayres S2RT34RESTD (N40214), Champion, NE. An agricultural chemical was erroneously dispensed on person and of mr carter. Trying to locate pilot. - [Incident 19870803051259I](https://openairdocs.org/incident/19870803051259I), Aug 3, 1987: Emb EMB110P1 (N101RA), Fresno, CA, Minor damage. Takeoff aborted due to caution indication. Nose steering ineffective. Faulty circuit breaker on gear control. - [Accident 19860313013319A](https://openairdocs.org/incident/19860313013319A), Mar 13, 1986: Emb EMB110P1 (N1356P), Alpena, MI, Destroyed, 2 fatal. The aircraft descended below glideslope and struck trees. Inefficient weather dissemination contributed to accident - [Incident 19840227012289I](https://openairdocs.org/incident/19840227012289I), Feb 27, 1984: Emb EMB110P1 (N102EB), Erie, PA. Unsafe gear indication but gear was down and locked. Snow had blown onto nose gear downlock switch and froze. - [Incident 19830204007749I](https://openairdocs.org/incident/19830204007749I), Feb 4, 1983: Emb EMB110P1 (N1356P), Milwaukee, WI. Pilot experienced elevator osillations. No airframe ice. Installed a new trim tab hinge assembly. - [Incident 19820218011799I](https://openairdocs.org/incident/19820218011799I), Feb 18, 1982: Emb EMB110P1 (N101RA), Boise, ID, Minor damage. Cabin emergency exit door blew off on takeoff roll. Aborted. Plastic shield over t handle was broken. Pins normal. - [Incident 19810417024279I](https://openairdocs.org/incident/19810417024279I), Apr 17, 1981: Emb EMB110P1 (N101RA), Twin Falls, ID. Failed to get down and locked indication on right gear. Landed ok and found sticking down lock cylinder. ## Service difficulty reports (465, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR 2025F00092](https://openairdocs.org/sdr/2025F00092), Apr 13, 2025: RIVET. LOOSE. 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 LEF - [SDR 2024FA0000334](https://openairdocs.org/sdr/2024FA0000334), Jan 11, 2024: LOCK FASTENER. LOOSE. 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), Apr 7, 2022: LAMP. BROKEN. 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 I - [SDR CA190807008](https://openairdocs.org/sdr/CA190807008), Aug 6, 2019: ROD END. CORRODED. (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 I - [SDR AXSA2019061400019](https://openairdocs.org/sdr/AXSA2019061400019), Jun 14, 2019: BLADES. CRACKED. DURING A HOT SECTION 3 CT BLADES WERE FOUND TO BE CRACKED AT THE FIR TREE. - [SDR CA190709014](https://openairdocs.org/sdr/CA190709014), Jun 11, 2019: FUEL CONTROL. MALFUNCTIONED. (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. PIL - [SDR CA190412007](https://openairdocs.org/sdr/CA190412007), Apr 10, 2019: ENGINE. DAMAGED. (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 - [SDR CA190412006](https://openairdocs.org/sdr/CA190412006), Apr 10, 2019: DUCT. CRACKED. (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 - [SDR CA190227016](https://openairdocs.org/sdr/CA190227016), Feb 24, 2019: FUEL CONTROL. FAILED. (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 AROU - [SDR CA190307019](https://openairdocs.org/sdr/CA190307019), Feb 16, 2019: FUEL CONTROL. MALFUNCTIONED. (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 STABL - [SDR CA190424021](https://openairdocs.org/sdr/CA190424021), Nov 18, 2018: HOSE. LEAKING. (CAN) HOSE SPLIT AND LEAKING. - [SDR AXSA2018082700001](https://openairdocs.org/sdr/AXSA2018082700001), Aug 25, 2018: ENGINE. UNKNOWN. 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 EM - [SDR CA180822003](https://openairdocs.org/sdr/CA180822003), Aug 13, 2018: LINE. LEAKING. (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 - [SDR CA180616004](https://openairdocs.org/sdr/CA180616004), May 28, 2018: PRESSURE SWITCH. BROKEN. (CAN) FALSE INDICATION OF AMOUNT OF FUEL ATA 28-00. (TC# 20180616004) - [SDR CA180616005](https://openairdocs.org/sdr/CA180616005), May 28, 2018: PROBE. FALSE INDICATION. (CAN) FALSE INDICATION OF AMOUNT OF FUEL ATA 28-00. (TC# 20180616005) - [SDR FAA2018052500164](https://openairdocs.org/sdr/FAA2018052500164), May 25, 2018: PRESSURE SWITCH. INTERMITTENT. 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 W - [SDR CA180616003](https://openairdocs.org/sdr/CA180616003), May 12, 2018: PRESSURE SWITCH. FLUCTUATES. (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 - [SDR CA180510013](https://openairdocs.org/sdr/CA180510013), May 10, 2018: DUCT. DAMAGED. (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 T - [SDR CA180404016](https://openairdocs.org/sdr/CA180404016), Apr 2, 2018: CONTROL CABLE. CHAFED. (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 OCC - [SDR CA180222018](https://openairdocs.org/sdr/CA180222018), Jan 24, 2018: PUMP. FAILED. (CAN) FORWARD BOOT PUMP 1 FAILURE ON TAXI IN AT GLA. (TC NR 20180222018). - [SDR 4P1A2017042400001](https://openairdocs.org/sdr/4P1A2017042400001), Apr 24, 2017: IGNITER. BROKEN. WHEN PERFORMING A PROGRESSIVE ROUTINE 300 HOUR INSPECTION ON THE ENGINE, FOUND PART OF THE RIGHT IGNITER MISSING. PERFORMED A BORESCOPE INSPECTION AND FOUND MEL - [SDR 4P1A2017021500001](https://openairdocs.org/sdr/4P1A2017021500001), Feb 15, 2017: BATTERY CABLE. CHAFED. 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 CON - [SDR CA160301016](https://openairdocs.org/sdr/CA160301016), Feb 23, 2016: IGNITION LEAD. WORN. (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 - [SDR CA160225005](https://openairdocs.org/sdr/CA160225005), Feb 21, 2016: IGNITION LEAD. FAILED. (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 P - [SDR CA160125010](https://openairdocs.org/sdr/CA160125010), Jan 15, 2016: DOOR. MISMANUFACTURED. (CAN) DURING ROUTINE MAINTENCE, FOUND 2 PROBLEMS WITH THE ICA`S. ON AN EMMA, EQUALIZED MAINTENANCE MAXIMUM AVAILABILITY, INSPECTION CARD 15, SECTION 3B, THE FLI - [SDR CA160111012](https://openairdocs.org/sdr/CA160111012), Jan 11, 2016: SEAL. DEFECTIVE. (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 CLOS - [SDR AXSA20150107001](https://openairdocs.org/sdr/AXSA20150107001), Jan 6, 2016: LINK. DETACHED. 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 TECHNICIA - [SDR CA151205001](https://openairdocs.org/sdr/CA151205001), Dec 3, 2015: AXLE. CRACKED. (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 AIRCRAF - [SDR CA151216008](https://openairdocs.org/sdr/CA151216008), Dec 3, 2015: ENGINE. MALFUNCTIONED. (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 - [SDR AXSA2015112590038](https://openairdocs.org/sdr/AXSA2015112590038), Nov 24, 2015: TURBINE WHEEL. DISINTEGRATED. 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 & DI - [SDR CA151110010](https://openairdocs.org/sdr/CA151110010), Nov 8, 2015: IGNITION LEAD. DAMAGED. (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 - [SDR CA151102015](https://openairdocs.org/sdr/CA151102015), Nov 2, 2015: AILERON. MISMANUFACTURED. (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 A - [SDR CA151022007](https://openairdocs.org/sdr/CA151022007), Oct 21, 2015: IGNITION LEAD. WORN. (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 BEN - [SDR CA151029025](https://openairdocs.org/sdr/CA151029025), Oct 14, 2015: ROD END. SEIZED. (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), Oct 9, 2015: G SWITCH. FAILED. (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 WA - [SDR CA150924009](https://openairdocs.org/sdr/CA150924009), Sep 21, 2015: ALTIMETER. MALFUNCTIONED. (CAN) IMMEDIATELY UPON BECOMING AIRBORNE, FLIGHT CREW NOTICED THE CAPTAIN`S ALTIMETER HAD FLAGGED AND CONTINUED TO INDICATE FIELD ELEVATION THROUGHOUT THE CLIMB - [SDR CA150923007](https://openairdocs.org/sdr/CA150923007), Sep 18, 2015: LOCK. BENT. (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 - [SDR CA150831008](https://openairdocs.org/sdr/CA150831008), Aug 26, 2015: IGNITION LEAD. BROKEN. (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 HO - [SDR CA150828003](https://openairdocs.org/sdr/CA150828003), Aug 16, 2015: ENGINE. POWER LOSS. (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 STAND - [SDR CA150818009](https://openairdocs.org/sdr/CA150818009), Aug 12, 2015: IGNITION LEAD. WORN. (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), Aug 10, 2015: DUCT. CRACKED. (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 - [SDR CA150721005](https://openairdocs.org/sdr/CA150721005), Jul 10, 2015: DOOR. OPEN. (CAN) AN AIR OPERATOR RECENTLY EXPERIENCED AN EVENT WHERE THE MAIN CABIN PASSENGER DOOR OPENED IN FLIGHT. THIS HAPPENED ON APPROACH IN TURBULENT WEATHER CONDITI - [SDR CA150727002](https://openairdocs.org/sdr/CA150727002), Jul 10, 2015: ENGINE. SHUTDOWN. (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 RE - [SDR 2015FA0000397](https://openairdocs.org/sdr/2015FA0000397), Jul 9, 2015: BLADE. FAILED. 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 - [SDR CA150728004](https://openairdocs.org/sdr/CA150728004), Jul 9, 2015: ENGINE. POWER LOSS. (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 - [SDR 2016FA0000277](https://openairdocs.org/sdr/2016FA0000277), Jul 9, 2015: COMPRESSOR. DAMAGED. 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 AIR - [SDR AXSA20150722001](https://openairdocs.org/sdr/AXSA20150722001), Jun 30, 2015: TRANSPONDER. SMOKE. PILOT REPORTED SMOKE COMING FROM BEHIND TRANSPONDER. - [SDR CA150713005](https://openairdocs.org/sdr/CA150713005), Jun 30, 2015: ENGINE. MALFUNCTIONED. (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 SH - [SDR CA150629022](https://openairdocs.org/sdr/CA150629022), Jun 28, 2015: MOTOR. FAILED. (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), Jun 19, 2015: WIRE. CORRODED. (CAN) HF ANTENNA WIRE FAILED DUE TO CORROSION, RESULTING FROM WATER INGRESS INTO THE FEED THROUGH IPC REFERENCE 23-10-00 FIG 1. All 465: https://openairdocs.org/engine/u-a-canada-pt6a-34/reports.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.