# N136XS: 2002 Aeromot AMT-200S - Status: Valid registration - Airframe: [Aeromot AMT-200S](https://openairdocs.org/model/aeromot-amt-200s) (registry code 0160001, 2 seats) - Engine: [Rotax SEE BOMBADIER](https://openairdocs.org/engine/rotax-see-bombadier) (registry code 55555) - Data sheets: [TCDS TG00004AT](https://openairdocs.org/tcds/TG00004AT) (Aeromot-Industria Mecanico Metalurgica Ltda.) (OpenAirDocs) - Serial number: 200.136 - Year built: 2002 - Type: Glider - Engine type: 4 cycle - Airworthiness: Standard, utility - Airworthiness date: June 19, 2002 - Certificate issued: November 18, 2021 - Expires: November 30, 2028 - Mode S code: A09399 - Registered owner: [Tuskegee Airmen National Historical Museum Inc](https://openairdocs.org/faa-owner/TUSKEGEE%20AIRMEN%20NATIONAL%20HISTORICAL%20MUSEUM%20INC) - Location: [Detroit, MI](https://openairdocs.org/faa-place/MI/Detroit) - Owner type: Corporation - Owner's area on the map: 42.3314° N, 83.0458° W: Placed by OpenAirDocs: center of Detroit, MI, 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=136XS - Page: https://openairdocs.org/aircraft/N136XS 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 (Rotax SEE BOMBADIER) 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 N136XS. ## 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 20031119036939I](https://openairdocs.org/incident/20031119036939I), Nov 19, 2003: Aimm AMT200S (N136XS), Colorado Spring, CO, Minor damage. (-23) Pilot called left base, gear down, and landed runway 30 experiencing a gear collapse. Minor damage to aircraft. Belly skin was scraped, as was the RH… ## Service difficulty reports (2) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 2004FA0000384](https://openairdocs.org/sdr/2004FA0000384), Apr 21, 2004: NUT. MISSING. UPON LANDING AIRCRAFT VEERED OFF THE RUNWAY. UPON INSPECTION IT WAS FOUND THAT THE NUT, (PN 5PA-108) HAD FALLEN OFF ALLOWING THE LINK (PN 32358) TO SEPARATE. - [SDR 2004FA0000368](https://openairdocs.org/sdr/2004FA0000368), Mar 29, 2004: CABLE. BROKEN. STARTER CABLE PN 52621 BROKE AT THE LUG CONNECTED TO THE STARTER. ## 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 Rotax SEE BOMBADIER engine: https://openairdocs.org/engine/rotax-see-bombadier.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.