# N304JB: 2009 Embraer ERJ 190-100 IGW, registration cancelled 2026-06-08

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 8, 2026
- Exported to: Spain
- Status when cancelled: Valid registration
- Airframe: [Embraer ERJ 190-100 IGW](https://openairdocs.org/model/embraer-erj-190-100-igw) (registry code 3260408)
- Engine: [GE CF34-10E6](https://openairdocs.org/engine/ge-cf34-10e6) (registry code 30023)
- Data sheets: [TCDS A57NM](https://openairdocs.org/tcds/A57NM), [TCDS E00070EN](https://openairdocs.org/tcds/E00070EN) (OpenAirDocs)
- Serial number: 19000257
- Year built: 2009
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 17, 2009
- Certificate issued: December 16, 2025
- Last registry action: December 16, 2025
- Mode S code: A32EF8
- Owner when cancelled: [Wilmington Trust Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20TRUSTEE)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N304JB
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=304JB
- Page: https://openairdocs.org/deregistered/N304JB-2026-06-08

From the FAA registry file of November 7, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Embraer ERJ 190-100 IGW: https://openairdocs.org/model/embraer-erj-190-100-igw.md

## Service difficulty reports (77, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR EE4Y2026030924077](https://openairdocs.org/sdr/EE4Y2026030924077), Mar 9, 2026: RIB. CORRODED. 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, 
- [SDR EE4Y2026030924076](https://openairdocs.org/sdr/EE4Y2026030924076), Mar 9, 2026: SKIN. DAMAGED. 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 26
- [SDR EE4Y2026030924075](https://openairdocs.org/sdr/EE4Y2026030924075), Mar 9, 2026: SKIN. DAMAGED. 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. 
- [SDR EE4Y2026030924074](https://openairdocs.org/sdr/EE4Y2026030924074), Mar 9, 2026: SKIN. CRACKED. 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 
- [SDR EE4Y2026030924073](https://openairdocs.org/sdr/EE4Y2026030924073), Mar 9, 2026: DOUBLER. MISINSTALLED. 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 IC
- [SDR EE4Y2026030924072](https://openairdocs.org/sdr/EE4Y2026030924072), Mar 9, 2026: SKIN. DAMAGED. 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 BLENDI
- [SDR EE4Y2026030924071](https://openairdocs.org/sdr/EE4Y2026030924071), Mar 9, 2026: SKIN. DAMAGED. 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 PRE
- [SDR EE4Y2026030924069](https://openairdocs.org/sdr/EE4Y2026030924069), Mar 9, 2026: SKIN. DAMAGED. 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 AR
- [SDR YENA2023041300352](https://openairdocs.org/sdr/YENA2023041300352), Apr 11, 2023: UNKNOWN. UNKNOWN. 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
- [SDR YENA2023041300351](https://openairdocs.org/sdr/YENA2023041300351), Apr 11, 2023: UNKNOWN. UNKNOWN. 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 REPA
- [SDR YENA2022051700493](https://openairdocs.org/sdr/YENA2022051700493), May 16, 2022: SKIN. DAMAGED. DURING HEAVY MAINTENANCE, PROTUBERANCE EXTERNAL SKIN FR 30-31 STR 26-27; MAJOR REPAIR REF TOMX NR 1894-00330 - EVALUATED AND REPAIRED PROTUBERANCE IAW EMB 190 S
- [SDR YENA2022051700491](https://openairdocs.org/sdr/YENA2022051700491), May 16, 2022: SKIN. CORRODED. DURING HEAVY MAINTENANCE, CORROSION ON INTERNAL SKIN BTW FR86/FR87 AND STGR 29L/28L; REMOVED CORROSION AND EVALUATED. FOUND OUT OF LIMITS. PER EMB 190 SRM 53-23
- [SDR YENA2022051700489](https://openairdocs.org/sdr/YENA2022051700489), May 16, 2022: FINGER DOUBLER. CORRODED. DURING HEAVY MAINTENANCE, CORROSION ON FINGER PLATE AT AFT CARGO DOOR CUTOUT BTW FR77/78, STGR 27R/28R; REMOVED CORROSION AND EVALUATED. FOUND OUT OF LIMITS. RE
- [SDR YENA2022051700490](https://openairdocs.org/sdr/YENA2022051700490), May 16, 2022: FINGER DOUBLER. CORRODED. DURING HEAVY MAINTENANCE, CORROSION ON FINGER PLATE AT AFT CARGO DOOR CUTOUT BTW FR79/80, STGR 27R/28R; REMOVED CORROSION AND EVALUATED. FOUND OUT OF LIMITS. RE
- [SDR YENA2022051700488](https://openairdocs.org/sdr/YENA2022051700488), May 16, 2022: SEAL REST. CORRODED. DURING HEAVY MAINTENANCE, CORROSION ON LWR CENTRAL SEAL REST AT AFT CARGO DOOR CUTOUT; REMOVED CORROSION, EVALUATED AND FOUND OUT OF LIMITS. REMOVED AND REPLACE
- [SDR YENA2022051700487](https://openairdocs.org/sdr/YENA2022051700487), May 16, 2022: SEAL REST. CORRODED. DURING HEAVY MAINTENANCE, CORROSION ON LOWER FORWARD SEAL REST AT AFT CARGO DOOR CUTOUT; REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED F
- [SDR YENA2022051700486](https://openairdocs.org/sdr/YENA2022051700486), May 16, 2022: SKIN. CORRODED. DURING HEAVY MAINTENANCE, FUSELAGE / CENTER FUSELAGE III / LOWER SKIN / BTW FR86 - FR87 AND STGR 29LH - 29RH / CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MA
- [SDR YENA2022030900132](https://openairdocs.org/sdr/YENA2022030900132), Mar 7, 2022: CONTROLLER. FAILED. FLT#384, MCO-MCO.'BLEED 2 LEAK CLIMBING THROUGH FL 290; PER FIM 36-21-00-810-804-A PERFORMED BLEED LEAK CHECK ON ENG #2 NO LEAK NOTED INSPECTION ODS LOOP ELECTR
- [SDR YENA2021121300837](https://openairdocs.org/sdr/YENA2021121300837), Dec 11, 2021: CLAMP. MIGRATED. FLT 940, SRQ-BOS(DIVERTED TO MCO). BLEED 2 LEAK QRH COMPLETED; T/S PER FIM 36-11-10 FOUND MIGRATED SUPPORT CLAMP ALLOWING PIGTAIL J2148 OF LOOP 5 TO MAKE CONTAC
- [SDR YENA2021121300836](https://openairdocs.org/sdr/YENA2021121300836), Dec 11, 2021: CLAMP. MIGRATED. FLT 940, SRQ-BOS(DIVERTED TO MCO). BLEED 2 LEAK QRH COMPLETED; T/S PER FIM 36-11-10 FOUND MIGRATED SUPPORT CLAMP ALLOWING PIGTAIL J2148 OF LOOP 5 TO MAKE CONTAC
- [SDR YENA2021010700010](https://openairdocs.org/sdr/YENA2021010700010), Jan 3, 2021: POWER SUPPLY. NO TEST. DURING HEAVY MAINTENANCE, ELPU NR 2 FAILED OPERATIONS CHECK. R & R ELPU NR 2, IAW AMM 33-50-01-000-801-A AND 33-50-01-801-A. REF TO MX NR 00033.
- [SDR YENA2019062720344](https://openairdocs.org/sdr/YENA2019062720344), Jun 22, 2019: POWER SUPPLY. FAILED. FT # 2167, RH AFT OVERWING EMERGENCY LIGHT INOP; REMOVED AND REPLACED ELPSU # 4 IAW AMM 33-50-01 OPS CHECK NORMAL.
- [SDR YENA201901050012](https://openairdocs.org/sdr/YENA201901050012), Jan 5, 2019: REPAIR. CORRODED. DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON (141-57) CENTER FUSELAGE III FLOOR STRUCTURE, CORROSION FOUND ON PREVIOUS SEAT TRACK REPAIR BTW FR 84-85 A
- [SDR YENA201803240150](https://openairdocs.org/sdr/YENA201803240150), Mar 24, 2018: SHEAR PANEL. CORRODED. DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT WET AREA MIDDLE SHEAR PANEL AT FRAME 87 - 88. REPLACED THE SHEAR PANEL IAW SRM IAW 51-42-01, AND 51-42
- [SDR YENA201803240149](https://openairdocs.org/sdr/YENA201803240149), Mar 24, 2018: FLOOR PANEL. CORRODED. DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT WET AREA FLOOR PANEL CORRODED AT FRAME 78. REPLACED THE FLOOR PANEL IAW SRM 51-42-01, AND 51-42-03.
- [SDR YENA201702020057](https://openairdocs.org/sdr/YENA201702020057), Feb 2, 2017: PUMP. FAILED. FLIGHT CREW REPORTED EDP 2 FAIL FOLLOWED BY COMPLETE LOSS OF NR 2 HYDRAULIC SYSTEM. DIVERTED. EMERGENCY DECLARED. REPLACED NR 2 ENGINE EDP HYDRAULIC PUMP IAW AM
- [SDR YENA20160510445](https://openairdocs.org/sdr/YENA20160510445), May 10, 2016: FRAME. CORRODED. DURING MAINTENANCE AT HEAVY CHECK STATION, CORROSION WAS FOUND ON FRAME 17, RBL 8.5"; CORROSION WAS REMOVED AND 2 L SHAPED REINFORCEMENT ANGLES WERE INSTALLED, 
- [SDR YENA20160510444](https://openairdocs.org/sdr/YENA20160510444), May 10, 2016: FRAME. CORRODED. DURING MAINTENANCE AT HEAVY CHECK BS, CORROSION WAS FOUND ON FRAME 14 RBL 23"; CORROSION WAS R & R DOUBLERS WERE INSTALLED.
- [SDR YENA20160510443](https://openairdocs.org/sdr/YENA20160510443), May 10, 2016: FRAME. CORRODED. DURING MAINTENANCE AT HEAVY CHECK STATION, CORROSION WAS FOUND ON FRAME 14 RBL 15.5; CORROSION WAS REMOVED AND REPAIRED DOUBLERS WERE INSTALLED.
- [SDR YENA20160510442](https://openairdocs.org/sdr/YENA20160510442), May 10, 2016: SEAT TRACK. CORRODED. DURING MAINTENANCE AT HEAVY CHECK STATION, CORROSION WAS FOUND ON AFT WET AREA RT SEAT TRACK BEAM FR84, RBL 10". REFERENCE EAMS NR 00187, CORROSION WAS REMOVED.
- [SDR YENA20160510441](https://openairdocs.org/sdr/YENA20160510441), May 10, 2016: SEAT TRACK. CORRODED. DURING MAINTENANCE AT HEAVY CHECK STATION, CORROSION WAS FOUND ON AFT WET AREA RT SEAT TRACK BEAM FRAME 84, RBL 12", CORROSION WAS REMOVED. NEW DOUBLER WAS FABR
- [SDR YENA20160510440](https://openairdocs.org/sdr/YENA20160510440), May 10, 2016: SEAT TRACK. CORRODED. DURING MAINTENANCE AT HEAVY CHECK STATION, CORROSION WAS FOUND ON RT SEAT TRACK AT THE GALLEY MOUNT BETWEEN FRAMES 13-14 IN THE FWD CABIN. CORROSION WAS R & R W
- [SDR YENA20160510439](https://openairdocs.org/sdr/YENA20160510439), May 10, 2016: FRAME. CORRODED. DURING MAINTENANCE, CORROSION WAS FOUND ON FRAME 17, 8" LBL; REMOVED ALL CORROSION BY BLENDING AND CUTTING ALL AREAS. INSTALLED 2 L SHAPED REINFORCEMENT ANGLES,
- [SDR YENA20160510438](https://openairdocs.org/sdr/YENA20160510438), May 10, 2016: FRAME. CORRODED. DURING MAINTENANCE, CORROSION WAS FOUND ON FR 17, 7" LBL; REMOVED ALL CORROSION BY BLENDING AND CUTTING ALL AREAS. INSTALLED 2 L SHAPED REINFORCEMENT ANGLES REF
- [SDR YENA20160510437](https://openairdocs.org/sdr/YENA20160510437), May 10, 2016: SUPPORT. CORRODED. DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA LT PANEL SUPPORT FR87, LBL 44". REF EAMS NR 00179; REMOVED CORROSION AND REPLACED LT SUPPORT PANEL, REF 
- [SDR YENA20160510436](https://openairdocs.org/sdr/YENA20160510436), May 10, 2016: FLOOR SUPPORT. CORRODED. DURING MAINTENANCE, CORROSION WAS FOUND ON FLOOR SUPPORT 6" AFT FRAME 15, 45" LBL. REF EAMS NR 00199. REPLACED FLOOR SUPPORT. REF SRM 51-43-03.
- [SDR YENA20160510435](https://openairdocs.org/sdr/YENA20160510435), May 10, 2016: SHEAR PLATE. CORRODED. DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA CENTER SHEAR PANEL 5" AFT FR87, LBL 4"; REPLACED CENTER SHEAR PANEL. REF SRM 51-42-01, 51-23-06.
- [SDR YENA20160510434](https://openairdocs.org/sdr/YENA20160510434), May 10, 2016: GUSSET. CORRODED. DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA RT GUSSET PLATE FR 90, RBL 24, REPLACED GUSSET IAW SRM 51-41-02.
- [SDR YENA20160510433](https://openairdocs.org/sdr/YENA20160510433), May 10, 2016: SEAT TRACK. CORRODED. DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA RT SEAT TRACK FR 87, RBL 12. SEAT TRACK REPLACED IAW SRM 51-41-01, 51-42-01, AND 51-43-03.
- [SDR YENA20160510432](https://openairdocs.org/sdr/YENA20160510432), May 10, 2016: SUPPORT. CORRODED. DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA RT PANEL SUPPORT FR 89, RBL 43"; REPLACED PANEL SUPPORT. REF SRM 51-41-02, 51-43-01.
- [SDR YENA20160510431](https://openairdocs.org/sdr/YENA20160510431), May 10, 2016: SUPPORT. CORRODED. DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA LT PANEL SUPPORT FR90, LBL 42". REPLACED PANEL SUPPORT REF SRM 51-41-01, 5141-02, 51-42-02, 51-43-03.
- [SDR YENA20160510430](https://openairdocs.org/sdr/YENA20160510430), May 10, 2016: SUPPORT. CORRODED. DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA RT PANEL SUPPORT FRAME 84, RBL 24", REPLACED PANEL REF SRM 51-41-02, 51-43-04.
- [SDR YENA20160510429](https://openairdocs.org/sdr/YENA20160510429), May 10, 2016: SUPPORT. CORRODED. DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA RT PANEL SUPPORT FR 84, RBL 42". REF EAMS NR 00193. REPLACED PANEL REF SRM 51-41-02, 51-43-04.
- [SDR YENA20160510428](https://openairdocs.org/sdr/YENA20160510428), May 10, 2016: SUPPORT. CORRODED. DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA RT SUPPORT PANEL FR 84, RBL 24". REF EAMS NR 00192, REPLACED PANEL. REF SRM 51-41-02, 51-42-02, 51-43-04
- [SDR YENA20160510427](https://openairdocs.org/sdr/YENA20160510427), May 10, 2016: STRUCTURE. CORRODED. DURING MAINTENANCE, CORROSION WAS FOUND ON AFT RT SILL 1.5" AFT FR 20 49" RBL. UAW EAMS NR 00221. REPLACED SILL REF SRM 51-41-02.
- [SDR YENA20160510426](https://openairdocs.org/sdr/YENA20160510426), May 10, 2016: STRUCTURE. CORRODED. DURING MAINTENANCE, CORROSION WAS FOUND ON AFT RT SILL 13.5" AFT, FR19, 49" RBL. REF EAMS NR 00220. REPLACED SILL REF SRM 51-41-02.
- [SDR YENA20160510425](https://openairdocs.org/sdr/YENA20160510425), May 10, 2016: STRUCTURE. CORRODED. DURING MAINTENANCE, CORROSION WAS FOUND ON AFT RT SILL 11" AFT FRAME 18, RBL 49". REF EAMS NR 00219, REPLACED SILL, REF SRM 51-41-02.
- [SDR YENA20160510424](https://openairdocs.org/sdr/YENA20160510424), May 10, 2016: STRUCTURE. CORRODED. DURING MAINTENANCE, CORROSION WAS FOUND ON FWD RT SILL 8" AFT FR13, 49" RBL. REF EAMS NR 00209. REPLACED SILL. REF SRM 51-41-02.
- [SDR YENA20160510423](https://openairdocs.org/sdr/YENA20160510423), May 10, 2016: STRUCTURE. CORRODED. DURING MAINTENANCE, CORROSION WAS FOUND ON AFT RT SILL FRAME 17, 42.5" RBL. REF EAMS NR 00215, REPLACED SILL. REF SRM 51-42-01.
- [SDR YENA20160510422](https://openairdocs.org/sdr/YENA20160510422), May 10, 2016: STRUCTURE. CORRODED. DURING MAINTENANCE, CORROSION WAS FOUND ON AFT RT SILL 1.5" AFT FR 17, 48" RBL. REF EAMS NR 00216, REPLACED AFT RT SILL REF SRM 51-41-02.

All 77: https://openairdocs.org/deregistered/N304JB-2026-06-08/reports.md

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