- Registered owner
- Skywest Airlines Inc
- Location
- St George, UT
- Owner type
- Corporation
- Serial number
- 17000401
- Year built
- 2014
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- November 23, 2024
- Certificate issued
- May 23, 2014
- Expires
- May 31, 2027
- Mode S code
- A02413
Embraer S A ERJ 170-200 LLTCDS A56NMAirframe · Embraer S A ERJ 170-200 LLTCDS E00063ENEngine · GE CF34-8E5
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 30
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2004 | 1 |
|---|---|
| 2005 | 1 |
| 2008 | 2 |
| 2009 | 1 |
| 2013 | 1 |
| 2017 | 2 |
| 2018 | 1 |
| 2019 | 1 |
| 2020 | 4 |
| 2021 | 3 |
| 2022 | 6 |
| 2023 | 5 |
| 2024 | 2 |
| 2025 | 3 |
| 2026 | 2 |
Airframe · Embraer S A ERJ 170-200 LL
AD 2026-13-02NavigationAD 2025-14-05Nacelles/PylonsAD 2025-01-05Time Limits/Maintenance ChecksInformation bulletins that may apply · 1
Advisory, not mandatory.
Airframe · Embraer S A ERJ 170-200 LL
SAIB NM-20-12Powerplant System - Operating in Icing ConditionsNTSB investigations
No NTSB investigations matched to N108SYMatched 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 Embraer S A ERJ 170-200 LL aircraft
FAA incident reports
No FAA accident or incident reports matched to N108SYMatched 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 Embraer S A ERJ 170-200 LL aircraft
Service difficulty reports · 46
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR SWIA20241017926Shear Panel · damagedELONGATED HOLE FOUND AFTER REMOVAL OF PANEL R/H END OF FR88 FOR R/H SHEAR PANEL ATTACHMENT (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED ELONGATED HOLE BY DRILLING TO SPECIFIC DIAMETER TO REMOVE DAMAGE. INSTALLED BUSHING.SEE CONTINUATION CARD FOR WORK PERFORMED.SDR SWI2024F01126Floorbeam · corrodedAFTER REMOVAL OF R/H INBOARD BEAM FR12-20 FOUND CORROSION AT FR17 CROSSBEAM (C-CHECK RO 10/15/2024) (FILED CLOSED)WEIGHT OF FR 17 CROSSBEAM REPAIR PARTS AND FASTENERS MEASURE 253.5 G. (TOOLING I.D# HG3-61241 DUE: 08/21/25) PERFORMED CROSSBEAM REPAIR AT FR17 RESDR SWIA20241017925Beam · corrodedAFTER REMOVAL OF R/H INBOARD BEAM FR12-20 FOUND CORROSION AT FR17 CROSSBEAM (C-CHECK RO 10/15/2024) (FILED OPEN)WEIGHT OF FR 17 CROSSBEAM REPAIR PARTS AND FASTENERS MEASURE 253.5 G. (TOOLING I.D# HG3-61241 DUE: 08/21/25) PERFORMED CROSSBEAM REPAIR AT FR17 REF:
See all 46 reportsSTCs that may be installed · 20
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 20 STCs