# N294JB: 2008 Embraer ERJ 190-100 IGW, registration cancelled 2025-12-09

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 9, 2025
- 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: 19000185
- Year built: 2008
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 25, 2008
- Certificate issued: October 8, 2025
- Last registry action: October 8, 2025
- Mode S code: A30520
- 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/N294JB
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=294JB
- Page: https://openairdocs.org/deregistered/N294JB-2025-12-09

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 (54, newest 50)

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

- [SDR YENA2021021900121](https://openairdocs.org/sdr/YENA2021021900121), Feb 15, 2021: FLOOR SUPPORT. CORRODED. DURING HMV, REF. TOMX N/R N294JB/1495/E2190/B6 CHECK N/R 00391- CORROSION ON FLOOR SILL BTW FR88/FR90 AND LBL 35" AT INTERNAL FLOOR STRUCTURE ; PER TOMX N/R N29
- [SDR YENA2021021900120](https://openairdocs.org/sdr/YENA2021021900120), Feb 15, 2021: SHEAR TIE. CORRODED. DURING HMV, REF. TOMX N/R N294JB/1495/E190/B6 CHECK N/R 00482-CPCP FINDING: CORROSION ON SHEAR CLIP OF FR67 BETWEEN STGR 29R AND 28R. ; PER TOMX N/R N294JB/1495
- [SDR YENA2021021900119](https://openairdocs.org/sdr/YENA2021021900119), Feb 15, 2021: SHEAR TIE. CORRODED. DURING HMV, REF. TOMX N/R N294JB/1495/E190/B6 CHECK N/R 00506 - CORROSION ON SHEAR CLIP OF FR89 BETWEEN STGR23L AND STGR25L ; PER TOMX N/R N294JB/1495/E190/B6 C
- [SDR YENA2021021900118](https://openairdocs.org/sdr/YENA2021021900118), Feb 15, 2021: SEAL REST. CORRODED. DURING HMV, REF. TOMX N/R N249JB/1495/E190/B6 CHECK N/R 00412 - CPCP FINDING CORROSION ON SEAL REST 3 EA ON AFT DOOR CUTOUT STRUCTURE ; PER TOMX N/R N294JB/1495
- [SDR YENA2021021900117](https://openairdocs.org/sdr/YENA2021021900117), Feb 15, 2021: DOUBLER. CORRODED. DURING HMV, REF. TOMX N/R N294JB/1495/E190/B6 CHECK N/R 00429 - CORROSION ON DOUBLER ON FLOOR STRUCTURE BTW FR87 AND FR88 LBL 42. ; PER TOMX N/R N294JB/1495/E19
- [SDR YENA2021021900116](https://openairdocs.org/sdr/YENA2021021900116), Feb 15, 2021: DOUBLER. CORRODED. DURING HMV, REF. TOMX N/R N294JB/1495/E190/B6 CHECK N/R 00430-CORROSION ON DOUBLER ON FLOOR STRUCTURE BTW FR87 AND FR88 RBL42 ; PER TOMX N/R N294JB/1495/E190/B6
- [SDR YENA2021021900115](https://openairdocs.org/sdr/YENA2021021900115), Feb 15, 2021: WEB. CORRODED. DURING HMV, REF. TOMX N/R N294JB/1495/E190/B6 CHECK N/R 00458-CORROSION ON WEB BTW FR84 AND FR85 Y=+340 TO Y=+1200. ; PER TOMX N/R N294JB/1495/E190/B6 CHECK N/R
- [SDR YENA2021021900114](https://openairdocs.org/sdr/YENA2021021900114), Feb 15, 2021: SKIN. CORRODED. DURING HMV, REF. TOMX N/R N294JB/1495/E190/B6 CHECK N/R 00624 - AFTER REMOVAL OF FIRE SEALANT AT APU COMPARTMENT, FWD EDGE CORROSION ON STRUCTURE. ; PER TOMX N/
- [SDR YENA2021021900113](https://openairdocs.org/sdr/YENA2021021900113), Feb 15, 2021: PLATE. CORRODED. DURING HMV, REF. TOMX N/R N294JB/1495/E190/B6 CHECK N/R 00460-CORROSION ON PLATE BETWEEN FR84 AND FR85 Y=-670 ; PER TOMX N/R N294JB/1495/E190/B6 CHECK N/R 00460
- [SDR YENA2021021900112](https://openairdocs.org/sdr/YENA2021021900112), Feb 15, 2021: STRUCTURE. CORRODED. DURING HMV, REF. TOMX N/R N294JB/1495/E190/B6 CHECK N/R 00561 - AFTER CLEAN AREA FUSELAGE 3 FINDINGS CORROSION BTW FR86 AND FR87 STGR27 AND STGR28 BELOW WATER T
- [SDR YENA2021021900111](https://openairdocs.org/sdr/YENA2021021900111), Feb 15, 2021: PLATE. CORRODED. DURING HMV, REF. TOMX N/R N294JB/1495/E90/B6 CHECK N/R 00490 - CORROSION ON PLATE CLOSING OF FWD CARGO DOOR SURROUNDING STRUCTURE CENTER FUSELAGE I ; PER TOMX N
- [SDR YENA2021021900110](https://openairdocs.org/sdr/YENA2021021900110), Feb 15, 2021: DOUBLER. CORRODED. DURING HMV, EC E21-098-01 FUSELAGE/CENTER FUSELAGE III - DOUBLER BETWEEN FRAMES 74- 75 AND STRINGERS 29L- 29R /CORROSION /PERMANENT REPAIR
- [SDR YENA2021021900109](https://openairdocs.org/sdr/YENA2021021900109), Feb 15, 2021: STRINGER. CORRODED. DURING HMV, EC E21-072-01 FUSELAGE / CENTER FUSELAGE III / STRINGER 23L BTWN FR 89-90 / CORROSION - PERMANENT REPAIR /// THIS IS CONSIDERED A MAJOR REPAIR.
- [SDR YENA2021021900108](https://openairdocs.org/sdr/YENA2021021900108), Feb 15, 2021: RIB. CRACKED. DURING HMV, EC E21-021-01 FUSELAGE / CENTER FUSELAGE II / WING TO FUSELAGE FAIRING CENTER PANEL REAR RIB @ FR45 RH / CRACK - PERMANENT REPAIR. MAJOR REPAIR.
- [SDR YENA2021021900107](https://openairdocs.org/sdr/YENA2021021900107), Feb 15, 2021: FLOORBEAM. CORRODED. DURING HMV, EC E21-042-01 FUSELAGE / CENTER FUSELAGE III / FLOOR STRUCTURE BEAMS AT FR85 AND Y-273 & Y+273 / CORROSION - PERMANENT REPAIR /// THIS IS CONSIDERED
- [SDR YENA2021021900106](https://openairdocs.org/sdr/YENA2021021900106), Feb 15, 2021: STRUCTURE. CORRODED. DURING HMV, EC E21-046-01 PYLONS / LH PYLON / UPPER SPARS AND REINFORCEMENTS / FWD & AFT LUGS / CORROSION DAMAGE – TIME LIMITED REPAIR /// THIS IS CONSIDERED A 
- [SDR YENA2021021900105](https://openairdocs.org/sdr/YENA2021021900105), Feb 15, 2021: FRAME. CRACKED. DURING HMV, EC E21-030-01 FUSELAGE/ CFII RH WFF FR52/ CRACK- PERMANENT REPAIR. MAJOR REPAIR.
- [SDR YENA2021021900104](https://openairdocs.org/sdr/YENA2021021900104), Feb 15, 2021: STRINGER. CORRODED. DURING HMV, EC E21-063-01 FUSELAGE/CENTER FUSELAGE III/ CORROSION ON STRINGER 14L BETWEEN FRAMES 89-90/ PERMANENT REPAIR /// THIS IS CONSIDERED A MAJOR REPAIR.
- [SDR YENA2021021900103](https://openairdocs.org/sdr/YENA2021021900103), Feb 15, 2021: STRUCTURE. CORRODED. DURING HMV, PYLONS / RH PYLON / UPPER SPARS AND REINFORCEMENTS / FWD & AFT LUGS / CORROSION DAMAGE - PERMANENT REPAIR. THIS IS CONSIDERED A MAJOR REPAIR.
- [SDR YENA2020051830344](https://openairdocs.org/sdr/YENA2020051830344), May 13, 2020: SKIN PANEL. CRACKED. DURING HEAVY MAINTENANCE, CRACK LOWER SKIN PANEL RH WING RIB 4; (REF AEROMAN NR 164208) ACCOMPLISHED REPAIR IAW AEROMAN EA57-0355-20 REV. O (COVER & PARTS 1-3),
- [SDR YENA2020051830343](https://openairdocs.org/sdr/YENA2020051830343), May 13, 2020: SKIN PANEL. CRACKED. DURING HEAVY MAINTENANCE, CRACK LOWER SKIN PANEL RH WING RIB 10; (REF AEROMAN NR 2020-164211) PERFORMED PERMANENT REPAIR IAW SRM 57-10-01 REPAIR 54P ITEM #9 FIG
- [SDR YENA201901230041](https://openairdocs.org/sdr/YENA201901230041), Jan 23, 2019: UNKNOWN. ODOR. FLT 1887, ORH-MCO. LEVEL 1 TRANSIENT ODOR FLIGHT DECK ONLY, DURING LEVEL OFF AT 6,000FT N1 APPROX 33% LASTED APPROX 30 SEC. BURNING SMELL AND FO HAD MINOR EYE I
- [SDR YENA201805270921](https://openairdocs.org/sdr/YENA201805270921), May 27, 2018: DOOR SILL. DAMAGED. DURING HEAVY MAINTENANCE, AN ELONGATED HOLE WAS DISCOVERED. REFER TO EC E18-425-01. FUSELAGE / CENTER FUSELAGE II / FLOOR STRUCTURE SILL FR42-43 & STR 17R / ELO
- [SDR YENA201705230386](https://openairdocs.org/sdr/YENA201705230386), May 23, 2017: WIRE HARNESS. DEFECTIVE. THE FLIGHT CREW REPORTED VIA ARINC THAT THEY WERE GETTING AN INTERMITTENT AURAL WARNING IN FLIGHT. THE R1 DOOR INDICATION WAS ON MEL AND THE WARNINGS THAT THE D
- [SDR YENA201701090024](https://openairdocs.org/sdr/YENA201701090024), Jan 9, 2017: GIRT BAR. DIRTY. L1 DOOR IS UNABLE TO BE DISARMED AFTER LANDING. HANDLES ARE FROZEN IN DOWN POSITION. REMOVED AND INSTALLED THE DOOR EVACUATION SLIDE IAW AMM 52-11-40. FOUND DEB
- [SDR YENA20151115565](https://openairdocs.org/sdr/YENA20151115565), Nov 15, 2015: STRINGER. CORRODED. CORROSION, STR 21L HAS CORROSION FRAME 89-90. COMPLIED WITH E15-1067-01 BY CUTTING OUT DAMAGED STR SECTION, FABRICATING NEW STR SECTION, HFEC, INSTALLED NEW STR
- [SDR YENA20151115564](https://openairdocs.org/sdr/YENA20151115564), Nov 15, 2015: SHEAR TIE. CORRODED. LT SHEAR CLIP IS CORRODED AT FRAME 89, AT STRINGER 19L. REMOVED CORRODED SHEAR CLIP, FABRICATED NEW SHEAR CLIP IAW JB EA E15-1076-01, INSTALLED NEW FABRICATED S
- [SDR YENA20151115563](https://openairdocs.org/sdr/YENA20151115563), Nov 15, 2015: STRINGER. CORRODED. CORROSION ON STRINGER 23L AT FRAME 91. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS, R & R STRINGER.
- [SDR YENA20151115562](https://openairdocs.org/sdr/YENA20151115562), Nov 15, 2015: STRINGER. CORRODED. STR 23L CORRODED AROUND FASTENERS AT FRAME 90-91 AS MARKED. BLENDED CORROSION , HFEC, NO DEFECTS NOTED, FABRICATED L-ANGLE DOUBLER, INSTALLED DOUBLER, ALODINED,
- [SDR YENA20151115561](https://openairdocs.org/sdr/YENA20151115561), Nov 15, 2015: SHEAR TIE. CORRODED. LT SHEAR CLIP CORRODED AT FRAME 89 BETWEEN STR 29L AND STR 29R. REMOVED CORRODED SHEAR CLIP. LOCATED, DRILLED, AND TREATED NEW SHEAR CLIP. INSTALLED AND TOP-COA
- [SDR YENA20151115560](https://openairdocs.org/sdr/YENA20151115560), Nov 15, 2015: STRINGER. CORRODED. STR 17L CORRODED, 14" AFT OF FRAME 88. CUT OUT DAMAGE. FABRICATED AND INSTALLED REPAIRED DOUBLER. COMPLIED WITH E15-1067-01.
- [SDR YENA20151115559](https://openairdocs.org/sdr/YENA20151115559), Nov 15, 2015: SHEAR TIE. CORRODED. SHEAR CLIP CORRODED AT FRAME 85 BETWEEN STR 27L AND STR 28L. REMOVED CORRODED SHEAR CLIP, FABRICATED NEW SHEAR CLIP, HFEC FABBED SHEAR CLIP, ALODINED, PRIMED, T
- [SDR YENA20151115558](https://openairdocs.org/sdr/YENA20151115558), Nov 15, 2015: SHEAR TIE. CORRODED. LT SHEAR CLIP IS CORRODED AT FRAME 89, AT STR 19L. REMOVED CORRODED SHEAR CLIP. FABRICATED NEW SHEAR CLIP IAW TASK CARD NR E15-1076-01. INSTALLED FABRICATED SHE
- [SDR YENA20151115557](https://openairdocs.org/sdr/YENA20151115557), Nov 15, 2015: SHEAR TIE. CORRODED. SHEAR CLIP CORRODED AT FRAME 87 BETWEEN STR 26L AND STR 27L. REMOVED SHEAR CLIP. FABRICATED NEW SHEAR CLIP IN COMPLIANCE WITH E15-1085-01. INSTALLED FABRICATED 
- [SDR YENA20151115556](https://openairdocs.org/sdr/YENA20151115556), Nov 15, 2015: STRINGER. CORRODED. STR 19L CORRODED AT FRAME 91. R & R CORRODED STRINGER JUNCTION. RESTORED TOPCOAT.
- [SDR YENA20151115555](https://openairdocs.org/sdr/YENA20151115555), Nov 15, 2015: SHEAR TIE. CORRODED. SHEAR CLIP CORRODED AT FRAME 88 BETWEEN STR 29L AND STR 29R. REMOVED CORRODED SHEAR CLIP, LOCATED, DRILLED, AND TREATED NEW CLIP. INSTALLED AND TOPCOATED NEW CL
- [SDR YENA20150911420](https://openairdocs.org/sdr/YENA20150911420), Sep 11, 2015: BATTERY PACK. NO TEST. DURING MAINTENANCE WHILE PERFORMING EMERGENCY, BATTERY PACKS FAILED TEST. R & R IAW AMM 33-50-01.
- [SDR YENA20150911419](https://openairdocs.org/sdr/YENA20150911419), Sep 11, 2015: BATTERY PACK. NO TEST. DURING MAINTENANCE WHILE PERFORMING EMERGENCY, LIGHT POWER UNITS FAILED TEST. R & R BATTERY PACK IAW AMM 33-50-01.
- [SDR YENA20150911418](https://openairdocs.org/sdr/YENA20150911418), Sep 11, 2015: BATTERY PACK. INOPERATIVE. DURING MAINTENANCE, WHILE PERFORMING EMERGENCY. POWER UNITS FUNCTIONAL TEST FAILED. R & R BATTERY PACK & FUNCTION TEST IAW AMM 33-50-01.
- [SDR YENA20150823378](https://openairdocs.org/sdr/YENA20150823378), Aug 23, 2015: ACM. FAILED. RETURNED TO DEPARTURE SHORTLY AFTER TAKEOFF, LAVATORY SMOKE INDICATION, R & R ACM IAW AMM 21-51-05, OPS AND LEAK CHECKED GOOD.
- [SDR YENA20150708258](https://openairdocs.org/sdr/YENA20150708258), Jul 8, 2015: HEAT EXCHANGER. CONTAMINATED. RETURNED TO DEPARTURE, LAV SMOKE EICAS WARNING AT 500AGL CABIN CREW REPORTED SMOKE IN AFT CABIN. ACCOMPLISHED INSPECTION FOR SMOKE IN CABIN. FOUND EVIDENCE OF C
- [SDR YENA20150708257](https://openairdocs.org/sdr/YENA20150708257), Jul 8, 2015: ACM. CONTAMINATED. RETURNED TO DEPARTURE, LAV SMOKE EICAS WARNING AT 500 AGL CABIN CREW REPORTED SMOKE IN AFT CABIN. ACCOMPLISHED INSPECTION FOR SMOKE IN CABIN. FOUND EVIDENCE OF 
- [SDR YENA20130803170](https://openairdocs.org/sdr/YENA20130803170), Aug 3, 2013: LOOP. OUT OF POSITION. ACFT DIVERTED DUE TO BLEED 2 LEAK EICAS MESSAGE DURING CLIMB OUT. RUN QRH PROCEDURES AND MESSAGE EXTINGUISHED. PERFORMED FIM TASK 36-21-00-810-803-A, FOLLOW CH 
- [SDR YENA20130502095](https://openairdocs.org/sdr/YENA20130502095), May 2, 2013: WINDSHIELD. CRACKED. FLT 1706 SDQ-MCO, AFTER LANDING THE FLIGHT CREW DECLARED AN EMERGENCY DUE TO CAPT WINDSCREEN CRACKED AND CAUGHT ON FIRE. REMOVED AND REPLACED CAPT'S SIDE LEFT W
- [SDR YENA20130110008](https://openairdocs.org/sdr/YENA20130110008), Jan 10, 2013: PRESSURE SENSOR. FAILED. FLT 663 SYR-MCO, AIRCRAFT DIVERTED TO IAD DUE TO NR 1 ENGINE BLEED OVER PRESSURE MESSAGE AT 129 PSI. UNABLE TO RESET PER THE QRH. REFERENCE FIM 36-14-00-810-804
- [SDR YENA20120209438](https://openairdocs.org/sdr/YENA20120209438), Feb 9, 2012: ELECTRICAL BOX. DEFECTIVE. FLT 1258 IAD-BOS, WHILE AIRCRAFT WAS SLOWING AND BEING VECTORED ON APPROACH, THE FLIGHT ATTENDANTS CALLED TO SAY A BURNING SMELL LIKE BURNING RUBBER WAS AROUND 
- [SDR YENA20111220398](https://openairdocs.org/sdr/YENA20111220398), Dec 20, 2011: POWER UNIT. FAILED. FLT 1712 SDQ-MCO, ON GROUND MAINTENANCE CHECK FOUND FWD LT DOOR EMERGENCY EXIT IDENTIFIER SIGN INOP. REMOVED AND REPLACED POWER UNIT IAW AMM 33-50-01. OPS CHECK
- [SDR YENA20110725308](https://openairdocs.org/sdr/YENA20110725308), Jul 25, 2011: SHUTOFF VALVE. STUCK. FLT 335 IAD-MCO, UPON DEP AT 1500 AGL - REQ'D BLEED 1 OVERPRESS EICAS WHILE RUNNING QRH. BLEED 2 IS FLUCTUATING FROM 2-98 PSI WITH BLEED 1 ALREADY ON MEL, ELECT
- [SDR YENA20110721304](https://openairdocs.org/sdr/YENA20110721304), Jul 21, 2011: ACM. FAILED. FLT 1791, AIR TURNBACK & EMERGENCY DECLARED - AFTER TAKEOFF CLIMBING THROUGH 500 FT, RECEIVED "LAV SMOKE" MESSAGE & ALARM. AFT F/A REPORTED SMOKE STARTED IN FWD
- [SDR YENA20110424241](https://openairdocs.org/sdr/YENA20110424241), Apr 24, 2011: SLIDE. FAILED. PRIOR TO DEPARTURE WITH L1 DOOR CLOSED, THE F/A REPORTED L1 DOOR SLIDE TOUGH TO ARM. TECH HAD TO REMOVE THE SLIDE IN ORDER TO OPEN DOOR. REPLACED L1 DOOR SLIDE 

All 54: https://openairdocs.org/deregistered/N294JB-2025-12-09/reports.md

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