# N125TX: 2000 Aeromot AMT-300 - Status: Valid registration - Airframe: [Aeromot AMT-300](https://openairdocs.org/model/aeromot-amt-300) (registry code 0160002, 2 seats) - Engine: [NONE](https://openairdocs.org/engine/none) (registry code 00000) - Data sheets: [TCDS TG00004AT](https://openairdocs.org/tcds/TG00004AT) (Aeromot-Industria Mecanico Metalurgica Ltda.) (OpenAirDocs) - Serial number: 300.125 - Year built: 2000 - Type: Glider - Engine type: None - Airworthiness: Standard, utility - Airworthiness date: November 25, 2000 - Certificate issued: August 7, 2015 - Expires: August 31, 2028 - Mode S code: A06804 - Registered owner: [Airborne Engineering Dynamics LLC](https://openairdocs.org/faa-owner/AIRBORNE%20ENGINEERING%20DYNAMICS%20LLC) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: LLC - Owner's area on the map: 39.7236° N, 75.5412° W: Placed by OpenAirDocs at the center of ZIP code 19801, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=125TX - Page: https://openairdocs.org/aircraft/N125TX 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): 2 in force ### Matched by airframe (Aeromot AMT-300) - [AD 2009-12-14](https://openairdocs.org/ad/2009-12-14): Engine fuel & control · Aeromot-Industria Mecanico Metalurgica Ltda. AMT-100 (Ximango), AMT-200 (Super Ximango), AMT-200S (Super Ximango) and 1 more. Effective Jul 17, 2009 - [AD 2007-23-15](https://openairdocs.org/ad/2007-23-15): Self-locking nuts · Aeromot-Industria Mecanico Metalurgica Ltda. AMT-100 (Ximango), AMT-200 (Super Ximango), AMT-200S (Super Ximango) and 1 more. Effective Dec 26, 2007 ### Matched by engine (NONE) None in force. ### Historical (superseded or no longer in force) - [AD 2011-11-03](https://openairdocs.org/ad/2011-11-03) (historical): Ignition · Aeromot-Industria Mecanico Metalurgica Ltda. AMT-200 (Super Ximango), AMT-300 (Turbo Ximango Shark), H-36 DIMONA and 8 more. Effective Jun 16, 2011 ## Information bulletins (advisory) (1 in force) - [SAIB CE-06-16](https://openairdocs.org/saib/CE-06-16): . Issued Dec 16, 2005 ## NTSB investigations None matched to N125TX. ## FAA accident and incident reports None matched to N125TX. ## 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 N125TX not matched to an aircraft (6) They name N125TX, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR 2009FA0000170](https://openairdocs.org/sdr/2009FA0000170), Mar 3, 2009: ACTUATOR. CORRODED. REPORTED DURING SUPPLEMENTAL INSPECTIONS FOR CONTINUED AIRWORTHINESS FOR THE AIRPLANE. DURING INSPECTION OF ELEVATOR TRIM TAB ACUTATOR IAW MM 27-30-02 FOUND BAR - [SDR 2009FA0000151](https://openairdocs.org/sdr/2009FA0000151), Feb 27, 2009: TRUSS. CORRODED. DURING SUPPLEMENTAL INSPECTION 54-10-02 FOUND RT WING INBD TRUSS ASSY PN 5951051-38 SEVERELY PITTED. SENT OUT FOR REPAIR. - [SDR 2009FA0000150](https://openairdocs.org/sdr/2009FA0000150), Feb 27, 2009: TRUSS. CORRODED. DURING SUPPLEMENTAL INSPECTION 54-10-02 FOUND LT WING INBD TRUSS ASSY PN 5951051-37 SEVERELY PITTED. SENT OUT FOR REPAIR. - [SDR 2009FA0000128](https://openairdocs.org/sdr/2009FA0000128), Feb 25, 2009: MAST. RUSTED. PREVIOUSLY REPORTED TO MFG IAW INSTRUCTIONS STIPULATED IN THE SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. FOUND RUDDER TORQUE - [SDR 2009FA0000118](https://openairdocs.org/sdr/2009FA0000118), Feb 25, 2009: FITTING. MISREPAIRED. PREVIOUSLY REPORTED IAW INSTRUCTIONS BY MFG SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. THE RT WING UPPER FWD ATTACH FITTING - [SDR 2009FA0000117](https://openairdocs.org/sdr/2009FA0000117), Feb 25, 2009: ATTACH FITTING. MISREPAIRED. PREVIOUSLY REPORTED IAW INSTRUCTIONS BY MFG SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. THE RT WING LWR FWD ATTACH FITTING PN ## STCs that may be installed (OpenAirDocs) (5) 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 airframe (Aeromot AMT-300) - [STC SA02283SE PAGE 1](https://openairdocs.org/stc/SA02283SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P. Electronics International Inc - [STC SA02402SE PAGE 1](https://openairdocs.org/stc/SA02402SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30C. Electronics International Inc - [STC SA00068SE](https://openairdocs.org/stc/SA00068SE): Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1). Electronics International Inc - [STC SA01988SE](https://openairdocs.org/stc/SA01988SE): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P. Electronics International Inc - [STC SA01157LA](https://openairdocs.org/stc/SA01157LA): Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. Electronics International Inc ## Related - Other Aeromot AMT-300 aircraft: https://openairdocs.org/model/aeromot-amt-300/aircraft.md - The NONE engine: https://openairdocs.org/engine/none.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.