- Registered owner
- Wilmington Trust Company Trustee
- Location
- Wilmington, DE
- Owner type
- Corporation
- Serial number
- 19000151
- Year built
- 2008
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- February 18, 2025
- Certificate issued
- February 4, 2025
- Expires
- February 29, 2032
- Mode S code
- A49DF9
Embraer Empresa Brasileira De ERJ 190-100 IGWTCDS A57NMAirframe · Embraer Empresa Brasileira De ERJ 190-100 IGWTCDS E00070ENEngine · GE CF34-10E5A1
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 60
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2006 | 2 |
|---|---|
| 2007 | 8 |
| 2008 | 7 |
| 2009 | 3 |
| 2010 | 11 |
| 2011 | 6 |
| 2012 | 3 |
| 2013 | 6 |
| 2014 | 2 |
| 2016 | 1 |
| 2017 | 3 |
| 2018 | 2 |
| 2019 | 2 |
| 2020 | 5 |
| 2021 | 1 |
| 2022 | 4 |
| 2023 | 3 |
| 2024 | 2 |
| 2025 | 3 |
| 2026 | 1 |
Airframe · Embraer Empresa Brasileira De ERJ 190-100 IGW
AD 2026-13-02NavigationAD 2025-14-05Nacelles/PylonsAD 2024-20-06FuelInformation bulletins that may apply · 1
Advisory, not mandatory.
Airframe · Embraer Empresa Brasileira De ERJ 190-100 IGW
SAIB NM-20-12Powerplant System - Operating in Icing ConditionsNTSB investigations
No NTSB investigations matched to N397NCMatched 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 Empresa Brasileira De ERJ 190-100 IGW aircraft
FAA incident reports
No FAA accident or incident reports matched to N397NCMatched 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 Empresa Brasileira De ERJ 190-100 IGW aircraft
Service difficulty reports · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR EE4Y2026150123769Skin · corrodedCORROSION DAMAGE AFFECTING THE CENTER FUSELAGE II SKIN INNER FACE,LOCATED IN THE S29L LOCATION, AT FR73+235MM. VERIFIED BLEND OUT WITH CLAD LAYERPENETRATED AND FOUND OUT OF LIMITS IAW PART II SRM 53-22-01, AD51, PARAG. 5A (2),TABLE 102, FIG. 104 SHEET 2. THE CSDR EE4Y2026010323693Skin · corrodedCUSTOMER REPORTS CORROSION DAMAGE AFFECTING THE CENTER FUSELAGE II SKIN INNER FACE, LOCATED IN THE STRG-29LH LOCATION, AT FR73+130MM. VERIFIED BLEND OUT WITH CLAD LAYER PENETRATED AND FOUND OUT OF LIMITS IAW ERJ190 PART II SRM 53-22-01, AD51, PARAG. 5A (2), TASDR EE4Y2026010323692Skin · dentedDURING THE STRUCTURAL INSPECTION, THE FUSELAGE RH SKIN PANEL LOCATED BETWEEN FR01–FR05 AND STRG 08RH–15RH WAS FOUND WITH 32 DENTS. EVALUATED DENTED SKIN AGAINST LIMITS PER ERJ-190 PART II SRM 53-10-01, AD 52, PARAGRAPH 3F. ADDITIONALLY, 32 DENTS WERE RECORDED SDR EE4Y2026010323691Skin · nickedDURING THE STRUCTURAL INSPECTION, NICKS WERE FOUND ON THE FORWARD FUSELAGE BETWEEN FR17 +100MM AND FR20 + 165MM AND BETWEEN S-26L AND S-26R ON THE EXTERNAL SKIN. THE DAMAGE WAS BLENDED IN ACCORDANCE WITH ERJ-190 SRM PART II 51-10-03, TYPES A AND D. EVALUATED TSDR EE4Y2026010323690Skin · nickedPER CUSTOMER REQUEST MUST BE EVALUATED EXISTING NICKS LOCATED FROM FR15 TO FR17+100MM, BETWEEN STRG 26LH AND 26RH. 7. EVALUATED BLEND OUT WITH CLAD LAYER PENETRATED AND FOUND OUT LIMITS PER ERJ190 PART II SRM 53-10-01, AD 51, PARG. 4B, TABLE 102, FIG. 101, SHE
STCs that may be installed · 62
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.