# N321XS: 2002 Aeromot AMT-200S - Status: Valid registration - Airframe: [Aeromot AMT-200S](https://openairdocs.org/model/aeromot-amt-200s) (registry code 0160001, 2 seats) - Engine: [Bombardier ROTAX (ALL)](https://openairdocs.org/engine/bombardier-rotax-all) (registry code 09050) - Data sheets: [TCDS TG00004AT](https://openairdocs.org/tcds/TG00004AT) (Aeromot-Industria Mecanico Metalurgica Ltda.) (OpenAirDocs) - Serial number: 200.150 - Year built: 2002 - Type: Glider - Engine type: 4 cycle - Airworthiness: Standard, utility - Airworthiness date: October 31, 2002 - Certificate issued: September 27, 2022 - Expires: September 30, 2029 - Mode S code: A37425 - Registered owners: [Snyder Christopher L](https://openairdocs.org/faa-owner/SNYDER%20CHRISTOPHER%20L), [Appleby Peter B](https://openairdocs.org/faa-owner/APPLEBY%20PETER%20B) - Location: [Moseley, VA](https://openairdocs.org/faa-place/VA/Moseley) - Owner type: Co-owned - Owner's area on the map: 37.4221° N, 77.7814° W: Placed by OpenAirDocs at the center of ZIP code 23120, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=321XS - Page: https://openairdocs.org/aircraft/N321XS 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): 5 in force ### Matched by airframe (Aeromot AMT-200S) - [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 - [AD 98-15-19](https://openairdocs.org/ad/98-15-19): Flexible Hoses Of Engine Lubricating System · Aeromot-Industria Mecanico Metalurgica Ltda. AMT-200 (Super Ximango) and AMT-200S (Super Ximango). Effective Sep 7, 1998 - [AD 98-05-05](https://openairdocs.org/ad/98-05-05): Main Landing Gear Attaching Bolts, Nuts · Aeromot-Industria Mecanico Metalurgica Ltda. AMT-100 (Ximango), AMT-200 (Super Ximango) and AMT-200S (Super Ximango). Effective Apr 17, 1998 - [AD 97-15-07](https://openairdocs.org/ad/97-15-07): Forward Horizontal Stabilizer Front Bolt · Aeromot-Industria Mecanico Metalurgica Ltda. AMT-200 (Super Ximango) and AMT-200S (Super Ximango). Effective Aug 15, 1997 ### Matched by engine (Bombardier ROTAX (ALL)) None in force. ## 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 N321XS. ## 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. - [Incident 20030504028169I](https://openairdocs.org/incident/20030504028169I), May 4, 2003: Aimm AMT200S (N321XS), Prescott, AZ, Minor damage. (-23) Following landing right brake locked up causing the glider to veer right and strike a runway sign. ## 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) (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-200S) - [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-200S aircraft: https://openairdocs.org/model/aeromot-amt-200s/aircraft.md - The Bombardier ROTAX (ALL) engine: https://openairdocs.org/engine/bombardier-rotax-all.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.