# N155EA: Eagle EAGLE 150B

- Status: Valid registration
- Airframe: [Eagle EAGLE 150B](https://openairdocs.org/model/eagle-eagle-150b) (registry code 05607TE, 2 seats)
- Data sheets: [TCDS A00005LA](https://openairdocs.org/tcds/A00005LA) (CTRM Aviation Sdn. Bhd.) (OpenAirDocs)
- Serial number: 025
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Certificate issued: March 6, 2017
- Expires: March 31, 2030
- Mode S code: A0DD27
- Registered owner: [Strato Air LLC](https://openairdocs.org/faa-owner/STRATO%20AIR%20LLC)
- Location: [Shady Shores, TX](https://openairdocs.org/faa-place/TX/Shady%20Shores)
- Owner type: LLC
- Owner's area on the map: 33.2038° N, 97.0553° W: Placed by OpenAirDocs at the center of ZIP code 76208, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=155EA
- Page: https://openairdocs.org/aircraft/N155EA

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.

## ADs that may apply (OpenAirDocs): 7 in force

### Matched by airframe (Eagle EAGLE 150B)

- [AD 2007-23-06](https://openairdocs.org/ad/2007-23-06): Severe exfoliation corrosion on Wing/ Canard Flap Hinges · CTRM Aviation Sdn. Bhd. 150B. Effective Dec 11, 2007
- [AD 2007-04-02](https://openairdocs.org/ad/2007-04-02): Canard inboard flap hinge support brackets · CTRM Aviation Sdn. Bhd. 150B. Effective Mar 21, 2007
- [AD 2005-05-14](https://openairdocs.org/ad/2005-05-14): Co-pilot rudder pedal assembly · CTRM Aviation Sdn. Bhd. 150B. Effective Apr 22, 2005
- [AD 2004-26-01](https://openairdocs.org/ad/2004-26-01): Inspect the port and starboard undercarriage attach bracket · CTRM Aviation Sdn. Bhd. 150B. Effective Jan 31, 2005
- [AD 2003-19-07](https://openairdocs.org/ad/2003-19-07): Canard rear spar · CTRM Aviation Sdn. Bhd. 150B. Effective Nov 3, 2003
- [AD 2002-02-01](https://openairdocs.org/ad/2002-02-01): Throttle Control Assembly · CTRM Aviation Sdn. Bhd. 150B. Effective Mar 21, 2002
- [AD 2001-09-16](https://openairdocs.org/ad/2001-09-16): Rudder Cables · CTRM Aviation Sdn. Bhd. 150B. Effective Jun 29, 2001

### Historical (superseded or no longer in force)

- [AD 2004-11-04](https://openairdocs.org/ad/2004-11-04) (historical): Canard inboard flap hinge support brackets · CTRM Aviation Sdn. Bhd. 150B. Effective Jun 4, 2004

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N155EA.

## FAA accident and incident reports

None matched to N155EA.

## 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.

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Eagle EAGLE 150B aircraft: https://openairdocs.org/model/eagle-eagle-150b/aircraft.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.