- Registered owner
- Sidlinger Computer Corp
- Location
- Flagstaff, AZ
- Owner type
- Corporation
- Serial number
- 200.152
- Year built
- 2003
- Type
- Glider
- Engine
- 4 cycle
- Airworthiness
- Standard, utility
- Airworthiness date
- December 3, 2003
- Certificate issued
- December 1, 2003
- Expires
- July 31, 2029
- Mode S code
- A3686A
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 5
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1997 | 1 |
|---|---|
| 1998 | 2 |
| 2007 | 1 |
| 2009 | 1 |
Information bulletins that may apply · 1
Advisory, not mandatory.
Airframe · Aeromot AMT-200S
SAIB CE-06-16NTSB investigations
No NTSB investigations matched to N319BSMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Aeromot AMT-200S aircraft
FAA incident reports
No FAA accident or incident reports matched to N319BSMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Aeromot AMT-200S aircraft
Service difficulty reports
No reports matched to N319BSGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Aeromot AMT-200S aircraft
STCs that may be installed · 5
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Aeromot AMT-200S
STC SA02283SE PAGE 1Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30PSTC SA02402SE PAGE 1Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30CSTC SA00068SEInstallation of fuel flow/pressure instruments. (W/TSIO-360-MB1)STC SA01988SEInstallation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.STC SA01157LAInstallation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument.