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Aircraft record

N304JB2009 Embraer ERJ 190-100 IGW

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Jun 8, 2026.

Safety record in brief:No NTSB accidents or incidents since 198220 ADs may apply77 service difficulty reports

Registration
Deregistered
Last based in
Wilmington, DE
owner city / state
Engine
CF34-10E6 · 18,820 lb thrust
Ge
Owners
1
since 2025
NTSB events
None
since 1982
ADs may apply
20
confirm with A&P
Service reports
77
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Wilmington Trust Co Trustee
Owner type
Corporation
City, state
Wilmington, DE
Certificate issued
Dec 16, 2025
Canceled
Jun 8, 2026
Airworthiness
Standard · Transport
Airworthiness date
Mar 17, 2009

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 data

Airframe

Manufacturer
Embraer
Model
ERJ 190-100 IGW
Year
2009
Serial number
19000257
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
20
Engines
2
Max takeoff weight
12,500 - 19,999 lb
Type certificate data sheet
A57NM
Mode S code
A32EF8

Engine

Make and model
Ge Cf34-10e6
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
  1. 2025 – 2026Wilmington Trust Co TrusteeWilmington, DE

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (20)

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.

ADSubjectEffectiveApplies to
2023-21-11Embraer S.A. (Type Certificate Previously Held by Yaborã Indústria Aeronáutica S.A.…Dec 26, 2023Airframe (ERJ 190-100 IGW)
2022-16-01WindowsAug 15, 2022Airframe (ERJ 190-100 IGW)Only with: Equipped with any NORDAM passenger window having PMA P/N NP00038-3.
2022-05-08Turbine Engine Oil SystemApr 11, 2022Engine (CF34-10E6)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.
2021-25-02Nacelles/ pylonsJan 20, 2022Airframe (ERJ 190-100 IGW)
2020-25-08Flight controlsJan 21, 2021Airframe (ERJ 190-100 IGW)Serial numbers per ANAC AD 2020-05-01 (ERJ 170) and ANAC AD 2020-05-02 (ERJ 190)
Show all 20 ADs
ADSubjectEffectiveApplies to
2020-12-12Nacelles/ pylonsAug 13, 2020Airframe (ERJ 190-100 IGW)
2020-05-21Indicating/ recording systemsApr 24, 2020Airframe (ERJ 190-100 IGW)Serial numbers per ANAC Brazilian AD 2019-10-01
2019-24-16Embraer S.A. AirplanesFeb 3, 2020Airframe (ERJ 190-100 IGW)Certain serial numbers: 19000002; 19000004; 19000006–19000213; 19000215–19000276; 19000278–19000466; 19000468–19000525; …
2019-19-03FuselageOct 31, 2019Airframe (ERJ 190-100 IGW)Serial numbers per Embraer Service Bulletins SB170-53-0142 Rev 01, SB190-53-0098 Rev 01, and SB190LIN-53-0072 Rev 01
2019-03-21Landing GearApr 2, 2019Airframe (ERJ 190-100 IGW)
2017-21-09FuselageNov 27, 2017Airframe (ERJ 190-100 IGW)Serial numbers per Embraer Service Bulletin 170-53-0051, Revision 03 (ERJ 170); Embraer Service Bulletin 190-53-0019, Revision 03 (ERJ 190)
2016-12-14PneumaticJul 27, 2016Airframe (ERJ 190-100 IGW)
2013-25-04Embraer S.A. AirplanesFeb 10, 2014Airframe (ERJ 190-100 IGW)Only with: ERJ 170 airplanes equipped with Goodrich escape slides P/N 4A4030-5; ERJ 190 airplanes equipped with Goodrich escape slides P/N 104003-2.
2013-16-22FuselageSep 27, 2013Airframe (ERJ 190-100 IGW)Serial numbers per Embraer Service Bulletins 170-53-0093 Rev 01, 190-53-0054 Rev 01, and 190LIN-53-0059 Rev 01, dated March 16, 2012
2013-11-17PneumaticAug 6, 2013Airframe (ERJ 190-100 IGW)Only with: Having Hamilton Sundstrand low pressure check valve (LPCV) P/N 1001447-3 or 1001447-4 installed.
2013-11-07Landing gearJul 9, 2013Airframe (ERJ 190-100 IGW)Serial numbers per EMBRAER Service Bulletin 190-57-0036, Revision 02, dated August 12, 2011; EMBRAER Service Bulletin 190LIN-57-0016, dated June 10, 2011
2013-05-12Fire ProtectionMay 3, 2013Airframe (ERJ 190-100 IGW)Serial numbers per Embraer Service Bulletins 170-26-0011 Rev 02, 190-26-0011 Rev 02, and 190LIN-26-0006 Rev 02
2013-03-13DoorsMar 19, 2013Airframe (ERJ 190-100 IGW)Serial numbers per EMBRAER Service Bulletins 170-52-0055 Rev 01, 190-52-0038 Rev 01, and 190LIN-52-0020
2012-16-09Air ConditioningSep 21, 2012Airframe (ERJ 190-100 IGW)
2012-15-03Landing GearSep 4, 2012Airframe (ERJ 190-100 IGW)

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (77)

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 · damagedMar 9, 2026

    CUSTOMER REPORTS LIGHTNING STRIKE DAMAGE AFFECTING THE CENTER FUSELAGE III SKIN, LOCATED AT FR74 AND STR 28L. THE DAMAGE WAS REMOVED BY BLENDING THE AFFECTED AREA IN ACCORDANCE WITH SRM 51-10-03, BLEND-OUT TYPE D. AFTER EVALUATION, IT WAS DETERMINED THAT THE BLEND-OUT IS OUTSIDE THE LIMITS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · damagedMar 9, 2026

    DURING THE STRUCTURAL INSPECTION, AN EXISTING BLEND-OUT WAS FOUND IN THE CENTER FUSELAGE III LOWER SKIN BETWEEN FRAMES 86-87 AND STRINGERS 27R-28R. SINCE NO PREVIOUS RECORD OF THIS BLEND-OUT EXISTS, IT WAS INSPECTED AND EVALUATED. THE CONDITION WAS FOUND TO BE OUTSIDE THE LIMITS DEFINED IN SRM…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · damagedMar 9, 2026

    WAS REPORTED THAT DURING A STRUCTURAL INSPECTION, LIGHTNING STRIKE DAMAGE (LSD) WAS IDENTIFIED AT FR32 AND JUST ABOVE STR-26LH. THE DAMAGE WAS REMOVED BY BLENDING THE AFFECTED AREA IN ACCORDANCE WITH SRM 51-10-03, BLEND-OUT TYPE D. AFTER EVALUATION, IT WAS DETERMINED THAT THE BLEND-OUT EXCEEDS THE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fuselage · doubler · misinstalledMar 9, 2026

    DURING STRUCTURAL INSPECTION, THE CUSTOMER FOUND AN EXTERNAL REPAIR DOUBLER AT FR74 + 105 MM AND STR 24L + 85 MM, REPORTEDLY INSTALLED IN ACCORDANCE WITH EMB IC2009-190/05358C DATED 09-JUL-2009. ONCE THE AVAILABLE DOCUMENTATION LACKED ESSENTIAL INFORMATION, THE REPAIR WAS REMOVED, EXPOSING AN…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · skin · crackedMar 9, 2026

    CRACKS (2EA) AND ONE ELONGATED HOE WERE FOUND AFFECTING THE LH WING LOWER SKIN AFT SPAR 2 BTWN RIB 10/11. SRM PART II 57-10-01 REP. 54 WAS EVALUATED. THE CRACK #1 IS NOT REPAIRABLE DUE TO THE LOCATION OF THE CRACK AND CRACK #2 IS REPAIRABLE PER SRM AND THE ELONGATED IS REPAIRABLE PER SRM (FREEZE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · damagedMar 9, 2026

    DURING THE STRUCTURAL INSPECTION, DAMAGE CAUSED BY A LIGHTNING STRIKE WAS FOUND ON THE EXTERNAL SKIN OF THE CENTER FUSELAGE I, AT FR24 + 327MM, STR-27LH + 8MM. AFTER PERFORMING A LIGHT BLEND-OUT, IT WAS DETERMINED THAT IN A POINT, THE DAMAGE EXCEEDED 50% OF THE SKIN THICKNESS. THE AFFECTED AREA…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · damagedMar 9, 2026

    CUSTOMER REPORTS TWO LIGHTNING STRIKE DAMAGES AFFECTING THE CENTER FUSELAGE I SKIN, LOCATED AT FR33 + 242 MM (DAMAGE #1) AND FR33 + 394 MM (DAMAGE #2) ON STR 26L. DAMAGE #1 WAS COMPLETELY REMOVED BY BLEND-OUT. DAMAGE #2, DEPTH EXCEEDED 50% OF THE SKIN THICKNESS, SO IT WAS REMOVED BY DRILLING A…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · rib · corrodedMar 9, 2026

    DURING A STRUCTURAL INSPECTION, CORROSION WAS FOUND AT A FASTENER HOLE LOCATED ON THE LH WINGLET LOWER SURFACE, AT THE SUPPORT STRUCTURE OF ACCESS PANEL 551AB, SEE FIGURE 1 FOR DAMAGE OVERVIEW. THE AFFECTED FASTENER HOLE INVOLVES BOTH THE WING SPAR II AND WINGLET RIB 1 FLANGES. ALL CORROSION WAS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · unknown · unknownApr 11, 2023

    DURING HEAVY MAINTENANCE: WINGS/ LH WING MAIN BOX / TRAILING EDGE LOWER SKIN AT AFT SPAR 2 BETWEEN RIB 10 AND RIB 11/ CRACK AND ELONGATED HOLES - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · unknown · unknownApr 11, 2023

    DURING HEAVY MAINTENANCE: LH WING TE AREA, LOWER SKIN HAS 2 EACH CRACK O/B PYLON; REF: TOMX W/O 2191 NR-00014 REPAIRED PER ETI-190-23-535 REV 3 AND ETD-2023-190-008554 REV B. NO SPECIFIC OR ADDITIONAL INSPECTIONS ARE NECESSARY. TOMX MECH 10000726 INSP 325718.

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Showing the 10 most recent of 77 reports.

Related aircraft

Show all 8 related aircraft
All 27 registered Embraer ERJ 190-100 IGW aircraft

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

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