N397NC2008 Embraer Empresa Brasileira De ERJ 190-100 IGW
Safety record in brief:No NTSB accidents or incidents since 19821 AD may apply5 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Wilmington Trust Company Trustee
- Owner type
- Corporation
- City, state
- Wilmington, DE
- Certificate issued
- Feb 4, 2025
- Expires
- Feb 29, 2032
- Airworthiness
- Standard · Transport
- Airworthiness date
- Feb 18, 2025
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Embraer Empresa Brasileira De
- Model
- ERJ 190-100 IGW
- Year
- 2008
- Serial number
- 19000151
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 112
- Engines
- 2
- Max takeoff weight
- 20,000 and over lb
- Type certificate data sheet
- A57NM
- Mode S code
- A49DF9
Engine
- Make and model
- Ge Cf34-10e5a1
- Type
- Turbo-fan
- Power
- 18,820 lb thrust
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2025 – nowWilmington Trust Company TrusteeWilmington, DE · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (1)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2022-05-08 | Turbine Engine Oil System | Apr 11, 2022 | Engine (CF34-10E5A1)Only with: Stationary oil seal P/N B1316-00453 or B1316-01274 installed at No. 1 forward bearing that was repaired, overhauled, or entered service after August 2014 and has used high thermal stability or high performance capability oil for 56 FHs or more. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (5)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Fuselage · skin · corrodedJan 15, 2026
CORROSION 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 CONDITION REPORTED WAS REPAIRED IAW…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · nickedJan 3, 2026
PER 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, SHEET 4 (DAMAGE IN ZONE NOT ALLOWED). THE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · nickedJan 3, 2026
DURING 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 THE BLEND-OUT WITH CLAD LAYER…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 5 reportsShow fewer reports
- Fuselage · skin · dentedJan 3, 2026
DURING 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 IN THE FORWARD FUSELAGE SKIN PER…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · corrodedJan 3, 2026
CUSTOMER 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), TABLE 102, FIG. 104 SHEET 4. THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026