# Thielert TAE125-02-114

- Type: Engine model (FAA registry)
- Registry code: 59303
- Manufacturer (registry): THIELERT
- Model: TAE125-02-114
- Engine type: Reciprocating
- Power: 152 hp
- Data sheet: [TCDS E00069EN](https://openairdocs.org/tcds/E00069EN) (OpenAirDocs)
- Holder: Continental Aerospace Technologies GmbH
- Installed in: 2 registered aircraft
- Page: https://openairdocs.org/engine/thielert-tae125-02-114

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.

- [AD 2023-01-08](https://openairdocs.org/ad/2023-01-08): Engine (Turbine/Turboprop) · Continental Aerospace Technologies TAE 125-02-99 and TAE 125-02-114. Effective Mar 9, 2023
- [AD 2020-26-06](https://openairdocs.org/ad/2020-26-06): Exhaust Turbine System (RECIP) · Technify Motors TAE 125-02-114 and TAE 125-02-99. Effective Dec 29, 2020
- [AD 2017-19-15](https://openairdocs.org/ad/2017-19-15): Reciprocating Engine Front Section · Technify Motors TAE 125-02-114 and TAE 125-02-99. Effective Oct 31, 2017
- [AD 2016-07-19](https://openairdocs.org/ad/2016-07-19): Fuel feed pumps · Technify Motors TAE 125-02-114 and TAE 125-02-99. Effective May 9, 2016
- [AD 2015-21-01](https://openairdocs.org/ad/2015-21-01): Dual mass flywheel · Technify Motors TAE 125-02-114 and TAE 125-02-99. Effective Nov 27, 2015
- [AD 2014-17-03](https://openairdocs.org/ad/2014-17-03): Fuel pump · Technify Motors TAE 125-02-114 and TAE 125-02-99. Effective Oct 2, 2014
- [AD 2012-26-13](https://openairdocs.org/ad/2012-26-13): Software mapping · Thielert Aircraft Engines TAE 125-01, TAE 125-02-114 and TAE 125-02-99. Effective Feb 13, 2013
- [AD 2012-26-12](https://openairdocs.org/ad/2012-26-12): Oil filler plug vent hole · Thielert Aircraft Engines TAE 125-02-114 and TAE 125-02-99. Effective Feb 13, 2013
- [AD 2012-02-05](https://openairdocs.org/ad/2012-02-05): Engine · Thielert Aircraft Engines TAE 125-02-114 and TAE 125-02-99. Effective Mar 2, 2012
- [AD 2011-05-06](https://openairdocs.org/ad/2011-05-06): Timing chain · Thielert Aircraft Engines TAE 125-02-114 and TAE 125-02-99. Effective Mar 30, 2011

Historical (superseded or no longer in force):

- [AD 2011-07-09](https://openairdocs.org/ad/2011-07-09) (historical): Full- authority digital electronic control (FADEC) software · Thielert Aircraft Engines TAE 125-01, TAE 125-02-114 and TAE 125-02-99. Effective May 5, 2011

## Registered aircraft (2)

- [N205TD](https://openairdocs.org/aircraft/N205TD): [B&R Mcclure Limited Family Partnership](https://openairdocs.org/faa-owner/B%26R%20MCCLURE%20LIMITED%20FAMILY%20PARTNERSHIP), [Panama City, FL](https://openairdocs.org/faa-place/FL/Panama%20City), built 2015, S/N 7429
- [N612TD](https://openairdocs.org/aircraft/N612TD): [Driftwood Aviation LLC](https://openairdocs.org/faa-owner/DRIFTWOOD%20AVIATION%20LLC), [Northport, MI](https://openairdocs.org/faa-place/MI/Northport), built 2014, S/N 7392

## NTSB investigations (1)

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 GAA17CA182](https://openairdocs.org/ntsb/GAA17CA182), Mar 9, 2017: Pedersen Bjarne Martin Sportsman GS-2 (N237PM), Robbinsville, NJ, substantial damage. Probable cause: The pilot’s failure to maintain directional control during the landing roll in gusting wind conditions.

## FAA accident and incident reports (1)

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 20170309003309A](https://openairdocs.org/incident/20170309003309A), Mar 9, 2017: Pedersen Bjarne Martin SPORTSMAN GS-2 (N237PM), Robbinsville, NJ, Destroyed. [privacy data omitted] Stated that he was flying into Trenton-Robbinsville Airport to pick up his friend who was dropping off an aircraft for an annual…

## Service difficulty reports (12)

As reported by operators and repair stations, by the model named in the report.

- [SDR CA151007022](https://openairdocs.org/sdr/CA151007022), Oct 1, 2015: GEARBOX. MAKING METAL. (CAN) UNCOMMANDED POWER LOSS IN DEPARTURE LEG OF FLIGHT. PILOT REDUCED POWER TO 55% BUT NOTICED IT ACTUALLY REDUCED TO 35%. PROPELLER RPM DROPPED, ALTHOUGH DROP
- [SDR CA121214004](https://openairdocs.org/sdr/CA121214004), Dec 12, 2012: TRAY. CRACKED. (CAN) DURING SCHEDULED INSPECTION, TECH DISCOVERED CRACKED BATTERY TRAY. TRAY IS CONSTRUCTED OF COMPOSITE, FIBERGLASS. THERE ARE 2 NUTPLATES INSTALLED ON THE SI
- [SDR CA121105018](https://openairdocs.org/sdr/CA121105018), Nov 5, 2012: STRUT. CRACKED. (CAN) CORROSION FOUND ON ALL COMPONENTS OF LT, RT AND NLG ASSEMBLIES DRAG STRUTS, LINKS AND ACTUATORS REQUIRED REPLACEMENT. CORROSION LEVEL III EXFOLIATION AND 
- [SDR CA110427001](https://openairdocs.org/sdr/CA110427001), Apr 26, 2011: BELLCRANK. WORN. (CAN) THE SPLIT FLAP BELLCRANK HAS A .006" DEEP WEAR MARK ON THE FLAP ACTUATOR LOWER ARM. THE MATERIAL THICKNESS IN THIS AREA IS .065". THE WEAR WAS CAUSED BY I
- [SDR CA100707003](https://openairdocs.org/sdr/CA100707003), Jul 2, 2010: CONTROL CABLE. FRAYED. RUDDER CONTROL CABLE WAS FOUND FRAYED WHERE IT EXITS TEFLON TUBE.
- [SDR CA100119009](https://openairdocs.org/sdr/CA100119009), Jan 18, 2010: SHIELD. CRACKED. (CAN) THE SHIELD PROTECTING THE ENGINE HEAD FROM THE TURBOCHARGER HEAT IS CRACKED AND ONE MOUNTING EAR IS BROKEN OFF. IT APPEARS THAT REPAIRS HAVE BEEN MADE BEF
- [SDR CA090922006](https://openairdocs.org/sdr/CA090922006), Sep 21, 2009: PITOT TUBE. DEFORMED. (CAN) PITOT TUBE BENT ON HORIZONTAL SHAFT NEAR ELBOW. SHOWS INDICATIONS OF OVERHEATING. BULGE IN METAL NEAR BEND DEFORMITY. (TC# 20090922006)
- [SDR CA090915008](https://openairdocs.org/sdr/CA090915008), Sep 13, 2009: ALTERNATOR. FAILED. (CAN) CHARGING SYSTEM WARNING LIGHT CAME ON IN FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE ALTERNATOR AND GROUND TESTED SERVICEABLE. THE 
- [SDR CA090619009](https://openairdocs.org/sdr/CA090619009), Jun 18, 2009: FIRE DETECTOR. MALFUNCTIONED. (CAN) THE LT ENGINE FIRE DETECTOR ILLUMINATED ON APPROACH. PILOT DECLARED AN EMERGENCY AND CONTINUED APPROACH TO LANDING. WARNING ANNUNCIATOR EXTINGUSHED ABOUT 
- [SDR CA080115005](https://openairdocs.org/sdr/CA080115005), Jan 14, 2008: PUSHROD. BENT. (CAN) AFTER RECEIVING A REPORT OF AN ANOMALY WITH THE CONTROL ROD FROM ANOTHER OPERATOR, INSPECTED THE ROD ENDS ON OUR AC. ALSO FOUND THE ROD ENDS ON BOTH LT AN
- [SDR CA080213013](https://openairdocs.org/sdr/CA080213013), Jan 4, 2008: SELECTOR. LEAKING. (CAN) AC WAS BEING RETRO-FITTED WITH A 2.0 TURBO DIESEL ENGINE IAW STC. THE FUEL SYS WAS COMPLETED, FUEL INSTALLED AND INSPECTED FOR LEAKS. A LEAK WAS DISCOVERE
- [SDR CA071220002](https://openairdocs.org/sdr/CA071220002), Nov 8, 2007: ECU. MALFUNCTIONED. (CAN) DURING FLIGHT TRAINING MANEUVERS, SIMULATED SINGLE ENG OPS AT 5000 FT ASL, THE LT ENGINE WAS THROTTLED BACK TO FLIGHT IDLE (5 PERCENT PWR, THROTTLE RETARD

## PMA parts (OpenAirDocs) (2)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this engine model on its data sheet, so check the FAA record before relying on it. Newest first.

- [TA3219-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID146495541720240531131058.0001): Engine Preheat Kit. Hartzell Propeller LLC · PMA PQ2040CE · Modification part · May 22, 2024
- [TA3219-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105252591820240531131058.0001): Engine Preheat Kit. Hartzell Propeller LLC · PMA PQ2040CE · Modification part · May 22, 2024

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