# N691TA: 2015 Costruzioni Aeronautiche Tecna P2008

- Status: Valid registration
- Airframe: [Costruzioni Aeronautiche Tecna P2008](https://openairdocs.org/model/costruzioni-aeronautiche-tecna-p2008) (registry code 060007Q, 2 seats)
- Engine: [Rotax 914 series](https://openairdocs.org/engine/rotax-914-series) (registry code 55575)
- Data sheets: [TCDS E00058NE](https://openairdocs.org/tcds/E00058NE) (BRP-Rotax GmbH & Co KG) (OpenAirDocs)
- Serial number: 091
- Year built: 2015
- Type: Fixed wing single engine
- Engine type: 4 cycle
- Airworthiness: Light sport, airplane
- Airworthiness date: September 21, 2015
- Certificate issued: January 7, 2025
- Expires: January 31, 2032
- Mode S code: A93017
- Registered owner: [Yukon Aviation LLC](https://openairdocs.org/faa-owner/YUKON%20AVIATION%20LLC)
- Location: [Colfax, WI](https://openairdocs.org/faa-place/WI/Colfax)
- Owner type: LLC
- Owner's area on the map: 45.0185° N, 91.7196° W: Placed by OpenAirDocs at the center of ZIP code 54730, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=691TA
- Page: https://openairdocs.org/aircraft/N691TA

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every Rotax 914 model are included.

## ADs that may apply (OpenAirDocs): 16 in force

### Matched by airframe (Costruzioni Aeronautiche Tecna P2008)

None in force.

### Matched by engine (Rotax 914 series)

- [AD 2026-16-11](https://openairdocs.org/ad/2026-16-11): Reciprocating Engine Front Section · BRP-Rotax 912 F2, 912 F3, 912 F4 and 16 more. Effective Aug 28, 2026
- [AD 2023-17-13](https://openairdocs.org/ad/2023-17-13): Reciprocating Engine Front Section · BRP-Rotax 912 F2, 912 F3, 912 F4 and 16 more. Effective Sep 20, 2023
- [AD 2019-21-12](https://openairdocs.org/ad/2019-21-12): Reciprocating Engine Cylinder Section · BRP-Rotax 914 F2, 914 F3 and 914 F4. Effective Nov 19, 2019
- [AD 2019-10-04](https://openairdocs.org/ad/2019-10-04): Reciprocating Engine Cylinder Section · BRP-Rotax 912 F2, 912 F3, 912 F4 and 6 more. Effective Jul 10, 2019
- [AD 2016-23-04](https://openairdocs.org/ad/2016-23-04): Carburetor floats · BRP-Rotax 912 F2, 912 F3, 912 F4 and 6 more. Effective Dec 7, 2016
- [AD 2016-13-04](https://openairdocs.org/ad/2016-13-04): Engine coolant temperature limit · BRP--POWERTRAIN 912 F2, 912 F3, 912 F4 and 6 more. Effective Jul 27, 2016
- [AD 2013-15-19](https://openairdocs.org/ad/2013-15-19): Excessive oil consumption · BRP--POWERTRAIN 912 F2, 912 F3, 912 F4 and 6 more. Effective Aug 27, 2013
- [AD 2012-04-03](https://openairdocs.org/ad/2012-04-03): Oil pump attachment bolts · BRP--POWERTRAIN 912 S2, 912 S3 and 914 F2. Effective Mar 16, 2012
- [AD 2012-01-07](https://openairdocs.org/ad/2012-01-07): Fuel pressure regulators · BRP--POWERTRAIN 914 F2, 914 F3 and 914 F4. Effective Feb 27, 2012
- [AD 2011-25-02](https://openairdocs.org/ad/2011-25-02): Crankshaft · BRP--POWERTRAIN 912 F2, 912 F3, 912 F4 and 6 more. Effective Dec 22, 2011
- [AD 2011-12-04](https://openairdocs.org/ad/2011-12-04): Washers · Bombardier-Rotax 912 F3, 912 S2, 912 S3 and 4 more. Effective Jun 27, 2011
- [AD 2010-20-23](https://openairdocs.org/ad/2010-20-23): Engine crankcase · Bombardier-Rotax 912 F2, 912 F3, 912 F4 and 6 more. Effective Nov 8, 2010
- [AD 2008-26-05](https://openairdocs.org/ad/2008-26-05): Exhaust muffler · BRP--POWERTRAIN 914 F2, 914 F3 and 914 F4. Effective Jan 26, 2009
- [AD 2005-01-14](https://openairdocs.org/ad/2005-01-14): Valve train on all engines · BRP--POWERTRAIN 912 F2, 912 F3, 912 F4 and 6 more. Effective Feb 15, 2005
- [AD 2002-16-07](https://openairdocs.org/ad/2002-16-07): Valve Spring Retainers · BRP--POWERTRAIN 912 F2, 912 F3, 912 F4 and 6 more. Effective Sep 3, 2002
- [AD 2002-10-14](https://openairdocs.org/ad/2002-10-14): Exhaust Bend Assemblies Located Between the Cylinder Heads and Exhaust Manifold Assembly · BRP--POWERTRAIN 914 F2, 914 F3 and 914 F4. Effective Jun 12, 2002

### Historical (superseded or no longer in force)

- [AD 2013-07-12](https://openairdocs.org/ad/2013-07-12) (historical): Cylinder heads · BRP--POWERTRAIN 912 F2, 912 F3, 912 F4 and 6 more. Effective Apr 30, 2013
- [AD 2002-21-16](https://openairdocs.org/ad/2002-21-16) (historical): Valve train · Bombardier-Rotax 912 F2, 912 F3, 912 F4 and 6 more. Effective Oct 28, 2002
- [AD 2002-16-26](https://openairdocs.org/ad/2002-16-26) (historical): Engine crankcase · Bombardier-Rotax 912 F2, 912 F3, 912 F4 and 3 more. Effective Sep 16, 2002

## Information bulletins (advisory) (2 in force)

- [SAIB NE-05-84R1](https://openairdocs.org/saib/NE-05-84R1): Reciprocating Engine Liquid Cooling: Bombardier-Rotax 912 & 914 Series Engines. Issued Sep 10, 2009
- [SAIB NE-08-36](https://openairdocs.org/saib/NE-08-36): BRP-Rotax 912 A, 912 F, 912 S, & 914 F Series Reciprocating Engines. Issued Jul 16, 2008
- [SAIB NE-05-84](https://openairdocs.org/saib/NE-05-84) (historical): . Issued Aug 30, 2005

## NTSB investigations

None matched to N691TA.

## NTSB investigations on N691TA not matched to an aircraft (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 DCA06IA007](https://openairdocs.org/ntsb/DCA06IA007), Nov 28, 2005: Raytheon Corporate Jets Beechjet 400 (N691TA), Jacksonville, FL, incident, minor damage. Probable cause: The dual-engine flameout due to high-altitude ice crystals that had accreted onto the JT15D-5 engines' compressor vanes and were ingested into the engine when the pilots retarded the power levers,…

## FAA accident and incident reports

None matched to N691TA.

## Reports on N691TA not matched to an aircraft (1)

They name N691TA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20051128031849I](https://openairdocs.org/incident/20051128031849I), Nov 28, 2005: Beech 400A (N691TA), Jacksonville, FL. (-23) N691TA was cleared by ATC to descend from 38000 to 33000 near gainesville FL. When crew reduced power to descend #2 engine followed by #1 engine flamed…

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N691TA not matched to an aircraft (1)

They name N691TA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DJFA2005168](https://openairdocs.org/sdr/DJFA2005168), Nov 28, 2005: ENGINE. POWER LOSS. EN ROUTE, SHORTLY AFTER POWER WAS REDUCED TO BEGIN DESCENT FROM CRUISE ALTITUDE, BOTH ENGINES EXPERIENCED A SUSTAINED POWER LOSS. UNABLE TO RESTART EITHER ENGIN

## STCs that may be installed (OpenAirDocs) (1)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the engine (Rotax 914 series)

- [STC SE01966WI](https://openairdocs.org/stc/SE01966WI): Use of GAMI G100UL High Octane Unleaded Avgas in spark ignition piston aircraft engines. General Aviation Modifications Inc. Lists 914 F2

## Related

- Other Costruzioni Aeronautiche Tecna P2008 aircraft: https://openairdocs.org/model/costruzioni-aeronautiche-tecna-p2008/aircraft.md
- The Rotax 914 series engine: https://openairdocs.org/engine/rotax-914-series.md

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