# N323JB: 2010 Embraer ERJ 190-100 IGW, registration cancelled 2026-06-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 3, 2026
- 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: 19000384
- Year built: 2010
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 30, 2010
- Certificate issued: September 29, 2010
- Last registry action: May 5, 2023
- Mode S code: A37A3F
- Owner when cancelled: [Jetblue Airways Corp](https://openairdocs.org/faa-owner/JETBLUE%20AIRWAYS%20CORP)
- Location: [Long Island City, NY](https://openairdocs.org/faa-place/NY/Long%20Island%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7476° N, 73.9388° W: Placed by OpenAirDocs at the center of ZIP code 11101, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N323JB
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=323JB
- Page: https://openairdocs.org/deregistered/N323JB-2026-06-03

From the FAA registry file of November 3, 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 (89, newest 50)

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

- [SDR YENA2025021100146](https://openairdocs.org/sdr/YENA2025021100146), Feb 6, 2025: PSU. OUT OF ADJUST. FLT#760, PHL-BOS.' (AIRCRAFT DIVERTED TO JFK AND DECLARED AN EMERGENCY) FLAP FAIL EICAS MSG WHILE RETRACTING 1 TO 0 ORH C/W. MSG DID NOT CLEAR; FLAPS INDICATED 
- [SDR YEN2024F00000](https://openairdocs.org/sdr/YEN2024F00000), Jun 17, 2024: WINDOW FRAME. CRACKED. DURING HEAVY MAINTENANCE: FUSELAGE / NOSE FORWARD FUSELAGE / WINDSHIELD FRAME / CENTER POST LH UPPER FASTENERS AREA / CRACK - PERMANENT REPAIR; REFERENCE: /1/ A
- [SDR YENA2024061800890](https://openairdocs.org/sdr/YENA2024061800890), Jun 17, 2024: PRESSURE BLKHD. CRACKED. DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / PRESSURE BULKHEAD @ FR 35 & STR 30L CRACKS AT FASTENER HOLES – TIME LIMITED REPAIR; AEM EA 53-9002-24 REV
- [SDR YENA2024061800873](https://openairdocs.org/sdr/YENA2024061800873), Jun 17, 2024: SKIN. DENTED. DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / PRESSURE BULKHEAD @ FR 35 & STR 30L / CRACKS AT FASTENER HOLES – TIME LIMITED REPAIR; REFERENCES: /1/ AEM
- [SDR YENA2024061800872](https://openairdocs.org/sdr/YENA2024061800872), Jun 17, 2024: SKIN. DENTED. DURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / SKIN BETWEEN FR 11-12 & STGR 17L-19L / DENTS & CRACK - TEMPORARY REPAIR; /1/ STS EA 125-2024-048 REV. IR /2/
- [SDR YENA2024062100890](https://openairdocs.org/sdr/YENA2024062100890), Jun 17, 2024: SKIN. CRACKED. DURING CURRENT DROP-IN CHECK, 2 DENTS, ONE OF WHICH HAS A CRACK DAMAGE, ON THE FWD SKIN BETWEEN FR 11-12 & STGR 17L-19L, WAS EVALUATED AFTER THE A/C WAS FERRIED
- [SDR YENA2024052100769](https://openairdocs.org/sdr/YENA2024052100769), May 19, 2024: SENSOR. FAILED. FLT#984, RDU-BOS. 'STEER FAIL; REMOVED AND REPLACED STEERING FEEDBACK SENSOR #2 IAW AMM 32-53-09. FAULT CLEARED. FUNCTIONAL TEST GOOD IAW AMM 32-53-09. A/C OK F
- [SDR YENA2024031200397](https://openairdocs.org/sdr/YENA2024031200397), Mar 9, 2024: SHEAR TIE. CORRODED. DURING HEAVY MAINTENANCE: CPCP CORROSION ON SHARE CLIP BTW FR88 STGR 28RH-29RH AT AFT CARGO COMPARTMENT; (RESOLVED ON W/O: 1288392 TASKCARD: NR-00007) REF: TOMX
- [SDR YENA2024031200396](https://openairdocs.org/sdr/YENA2024031200396), Mar 9, 2024: SHEAR TIE. CORRODED. DURING HEAVY MAINTENANCE: CPCP- CORROSION ON SHARE CLIP BTW FR87 STGR 28RH-29RH AFT CARGO; (RESOLVED ON W/O: 1288392 TASKCARD: NR-00013) REF: TOMX W/O 2482 N/R 
- [SDR YENA2024031200395](https://openairdocs.org/sdr/YENA2024031200395), Mar 9, 2024: SHEAR TIE. CORRODED. DURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON SHEAR CLIP BTW FR75 AND STRG28/27 RH ON AFT CARGO COMPARTMENT STRUCTURE; REMOVE CORROS
- [SDR YENA2024031200394](https://openairdocs.org/sdr/YENA2024031200394), Mar 9, 2024: SHEAR TIE. CORRODED. DURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON SHEAR CLIP BTW FR82 AND STRG28/27 RH ON AFT CARGO COMPARTMENT STRUCTURE; REMOVE CORROS
- [SDR YENA2024031200393](https://openairdocs.org/sdr/YENA2024031200393), Mar 9, 2024: SHEAR TIE. CORRODED. DURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON SHEAR CLIP BTW FR76 AND STRG28/29 LH ON AFT CARGO COMPARTMENT STRUCTURE; REMOVE CORROS
- [SDR YENA2024031200392](https://openairdocs.org/sdr/YENA2024031200392), Mar 9, 2024: SHEAR TIE. CORRODED. DURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON SHEAR CLIP BTW FR76 AND STRG28/27 LH ON AFT CARGO COMPARTMENT STRUCTURE; REMOVE CORROS
- [SDR YENA2024031200391](https://openairdocs.org/sdr/YENA2024031200391), Mar 9, 2024: SKIN. GOUGED. DURING HEAVY MAINTENANCE: GOUGES ON EXTERNAL FORWARD FUSELAGE LOWER SKIN PANEL BTW FR 20 TO X=6232.5 AND STGR 28L-27L; (RESOLVED ON W/O: 1288392 TASKCARD: NR-00
- [SDR YENA2024031200390](https://openairdocs.org/sdr/YENA2024031200390), Mar 9, 2024: SPAR. UNKNOWN. DURING HEAVY MAINTENANCE: IN REF NRC 00365:REPLACE INBD UPPER SPAR AT RH PYLON; (RESOLVED ON W/O: 1288392 TASKCARD: NR-00039) REF TOMEX WO 8619, NRC 00394, INBD
- [SDR YENA2024031200389](https://openairdocs.org/sdr/YENA2024031200389), Mar 9, 2024: SKIN. UNKNOWN. DURING HEAVY MAINTENANCE: DENT ON EXTERNAL DOUBLER OF PREVIOUS REPAIR AND FUSELAGE SKIN BTW FR 23-24 AND STGR 15L-16L AT CENTER FUSELAGE I EXTERNAL SIDE SKIN; (
- [SDR YENA2024031200388](https://openairdocs.org/sdr/YENA2024031200388), Mar 9, 2024: FLOOR SUPPORT. CORRODED. DURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON FLOOR STRUCTURE LONGITUDINAL BEAM BTW FR13 AND FR 14, Y= 280RH (W1); CMOR: REMOVE CORR
- [SDR YENA2024031200387](https://openairdocs.org/sdr/YENA2024031200387), Mar 9, 2024: STRINGER. CORRODED. DURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON STRINGER BTW FR76/78 AND STRG 29 RH ON AFT CARGO COMPARTMENT STRUCTURE; REMOVE CORROSI
- [SDR YENA2024031200386](https://openairdocs.org/sdr/YENA2024031200386), Mar 9, 2024: FRAME. CORRODED. DURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON FRAME 80 BTW STRG28/27 RH ON AFT CARGO COMPARTMENT STRUCTURE; CMOR:REMOVE CORROSION, E
- [SDR YENA2024031200385](https://openairdocs.org/sdr/YENA2024031200385), Mar 9, 2024: SHEAR TIE. CORRODED. DURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON SHEAR CLIP BTW FR76 AND STRG28/27 LH ON AFT CARGO COMPARTMENT STRUCTURE; REMOVE CORROS
- [SDR YENA2024031200384](https://openairdocs.org/sdr/YENA2024031200384), Mar 9, 2024: SHEAR TIE. CORRODED. DURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON SHEAR CLIP BTW FR76 AND STRG28/29 LH ON AFT CARGO COMPARTMENT STRUCTURE; REMOVE CORROS
- [SDR YENA2024031200383](https://openairdocs.org/sdr/YENA2024031200383), Mar 9, 2024: SHEAR TIE. CORRODED. DURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON SHEAR CLIP BTW FR77 AND STRG28/29 LH ON AFT CARGO COMPARTMENT STRUCTURE; REMOVE CORROS
- [SDR YENA2024031200382](https://openairdocs.org/sdr/YENA2024031200382), Mar 9, 2024: SHEAR TIE. CORRODED. DURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON SHEAR CLIP BTW FR79 AND STRG28/29 LH ON AFT CARGO COMPARTMENT STRUCTURE; REMOVE CORROS
- [SDR YENA2024031200381](https://openairdocs.org/sdr/YENA2024031200381), Mar 9, 2024: SHEAR TIE. CORRODED. DURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON SHEAR CLIP BTW FR82 AND STRG28/29 LH ON AFT CARGO COMPARTMENT STRUCTURE; REF: TOMX W/O
- [SDR YENA2024031200380](https://openairdocs.org/sdr/YENA2024031200380), Mar 9, 2024: SHEAR TIE. CORRODED. DURING HEAVY MAINTENANCE: CPCP- CORROSION ON SHARE CLIP BTW FR87 STGR 28RH-29RH AFT CARGO; REF: TOMX W/O 2482 N/R 00272 REPLACED PER EMB 190 SRM 51-41-02 AND SR
- [SDR YENA2024031200379](https://openairdocs.org/sdr/YENA2024031200379), Mar 9, 2024: SHEAR TIE. CORRODED. DURING HEAVY MAINTENANCE: CPCP- CORROSION ON SHARE CLIP BTW FR87 STGR 27RH-28RH AFT CARGO; REF: TOMX W/O 2482 N/R 00272 REPLACED PER EMB 190 SRM 51-41-02 AND SR
- [SDR YENA2024031200378](https://openairdocs.org/sdr/YENA2024031200378), Mar 9, 2024: SHEAR TIE. CORRODED. DURING HEAVY MAINTENANCE: CPCP CORROSION ON SHARE CLIP BTW FR85 STGR 27RH - 28RH AFT CARGO; REF: TOMX W/O 2482 N/R 00278 REPLACED PER EMB 190 SRM 51-41-01 AND 5
- [SDR YENA2024031200377](https://openairdocs.org/sdr/YENA2024031200377), Mar 9, 2024: SHEAR TIE. CORRODED. DURING HEAVY MAINTENANCE: CPCP- CORROSION ON SHARE CLIP BTW FR86 STGR 27RH-28RH AFT CARGO; REF: TOMX W/O 2482 N/R -00275 REPLACED PER EMB 190- SRM 51-41-01 AND 
- [SDR YENA2024031200376](https://openairdocs.org/sdr/YENA2024031200376), Mar 9, 2024: SHEAR TIE. CORRODED. DURING HEAVY MAINTENANCE: CPCP CORROSION ON SHARE CLIP BTW FR88 STGR 27RH-STGR 28RH AFT CARGO COMPARTMENT STRUCTURE; REF: TOMX W/O 2482 N/R 00271 SHARE CLIP REP
- [SDR YENA2024031200375](https://openairdocs.org/sdr/YENA2024031200375), Mar 9, 2024: SEAT TRACK. CORRODED. DURING HEAVY MAINTENANCE: CPCP CORROSION ON FLOOR STRUCTURE SEAT TRACK BEAM FR17 AND FR18 AND Y=300RH (W1); REF: TOMX W/O 2482 N/R 00182 REPAIRED PER EMB 190 SR
- [SDR YENA2024031200374](https://openairdocs.org/sdr/YENA2024031200374), Mar 9, 2024: SEAT TRACK. CORRODED. DURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / FLOOR STRUCTURE / RH FLOOR TRACK / BTWN FR13-14 & Y=273 / CORROSION - PERMANENT REPAIR (CONSIDERED A MAJOR R
- [SDR YENA2024031200373](https://openairdocs.org/sdr/YENA2024031200373), Mar 9, 2024: SKIN. DENTED. DURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / SKIN / BTW FR 23-24 & STGR 15L-16L / PREVIOUS DOUBLER / DENT - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2024031200372](https://openairdocs.org/sdr/YENA2024031200372), Mar 9, 2024: FRAME. CORRODED. DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE III / FRAME 80 / BTWN STR 27R-28R / CORROSION - TIME-LIMITED REPAIR (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2024031200371](https://openairdocs.org/sdr/YENA2024031200371), Mar 9, 2024: SKIN. GOUGED. DURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / LOWER SKIN / BTWN FR20-21 & STR 27LH-28LH / GOUGES - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2023061900673](https://openairdocs.org/sdr/YENA2023061900673), Jun 17, 2023: SHUTOFF VALVE. FAILED. FLT#1082, RIC-BOS. (AIRCRAFT PERFORMED AN AIR TURN BACK TO RIC) 'BLEED (1) ONE FAIL ON CLIMBOUT; REMOVED AND REPLACED #1 NAPRSOV IN REF AMM 36-11-03. OPS CHECK 
- [SDR YENA2022121601259](https://openairdocs.org/sdr/YENA2022121601259), Dec 13, 2022: CONNECTOR. DAMAGED. FLT#2324, MCO-DCA. (AIRCRAFT DECLARED AN EMERGENCY AND PERFORMED AN AIR TURN BACK TO MCO) ' SLAT FAIL MSG AFTER BIRD STRIKE. THE FLAP HANDLE WAS NOT MOVED. RETU
- [SDR YENA2022120901235](https://openairdocs.org/sdr/YENA2022120901235), Dec 5, 2022: LEVER. OUT OF ADJUST. FLT#1132, LGA-BOS. L1 DOOR ARMING LEVER RAISES APPROX 1/2 INCH IN-FLIGHT, RESULTING IN ARMING INDICATION TO NOT BEING VISIBLE; ADJUSTED ARMED/DISARMED VISUAL IN
- [SDR YENA2022090100848](https://openairdocs.org/sdr/YENA2022090100848), Aug 26, 2022: SLIDE. FAILED. FLT#8583, JFK-MCN. 'WHILE WORKING L2 DOOR INDICATION MDDR FOUND DOOR SLIDE BUSTLE PIN LANYARD DISCONNECTED (TOO SHORT TO REATTACH); REF EAMS N/R 00007, REMOVED 
- [SDR YENA2022090100849](https://openairdocs.org/sdr/YENA2022090100849), Aug 23, 2022: SKIN. DENTED. FLT#8583, JFK-MCN. 'W/O 1198428 ASSIGNED, AFT JACK PAD AREA DAMAGE REPAIR, W/O 1198975. ENCOMPASSED IN EAMS WO H8790; ACFT REG:323JB ACFT SN: 19000384, ACFT TAT
- [SDR YENA2022022500092](https://openairdocs.org/sdr/YENA2022022500092), Feb 24, 2022: NONE. NONE. FLT # 1899, FLL-HAV(AIR TURNBACK TO FLL). DURING ALL PHASES OF FLIGHT AN ABNORMAL AMOUNT OF RUDDER PRESSURE AND TRIM WAS REQUIRED TO KEEP AIRCRAFT IN COORDINATE
- [SDR YENA2021062900408](https://openairdocs.org/sdr/YENA2021062900408), Jun 23, 2021: SKIN. GOUGED. FLT 6102, BNA-BOS. FUSELAGE / CENTER FUSELAGE I / EXTERNAL SKIN FR23-24 & STGR15L-16L / DENT & GOUGE - PERMANENT REPAIR (EC E21-714-01); CLASSIFIED AS MAJOR REP
- [SDR YENA2020081700428](https://openairdocs.org/sdr/YENA2020081700428), Aug 9, 2020: PINTLE PIN. CORRODED. DURING HEAVY MAINTENANCE, CORROSION ON HOLES SHOCK STRUT REAR PINTLE PINS ON RH MAIN LANDING GEAR; REMOVED AND REPLACED SHOCK STRUT REAR PINTLE PIN ON RH MLG 28
- [SDR YENA2020081700427](https://openairdocs.org/sdr/YENA2020081700427), Aug 9, 2020: PINTLE PIN. CORRODED. DURING HEAVY MAINTENANCE, CORROSION ON HOLES LEG FWD PINTLE PIN ON LH MAIN LANDING GEAR; REMOVED AND REPLACED FWD PINTLE PIN ON LH MLG 2821-0067 SN L1413 FOR A 
- [SDR YENA2020081700426](https://openairdocs.org/sdr/YENA2020081700426), Aug 9, 2020: PINTLE PIN. CORRODED. DURING HEAVY MAINTENANCE, CORROSION ON HOLES LEG FWD PINTLE PINS ON LH MAIN LANDING GEAR; REMOVED AND REPLACED REAR PINTLE PIN ON LH MAIN LANDING GEAR PN 2821-0
- [SDR YENA2020081700425](https://openairdocs.org/sdr/YENA2020081700425), Aug 9, 2020: PINTLE PIN. CORRODED. DURING HEAVY MAINTENANCE, CORROSION ON HOLES LEG FWD PINTLE PINS ON TH MAIN LANDING GEAR; REMOVED SHOCK STRUT FWD PINTLE PIN PN 2821-0067 SN L1390 AND INSTALLED
- [SDR YENA201909020497](https://openairdocs.org/sdr/YENA201909020497), Sep 2, 2019: WIRE HARNESS. DAMAGED. SUPPLEMENTAL INFORMATION: FLT 860, PHL-BOS. EMERGENCY DECLARED. RETURNED TO FIELD. ENG 2 FIRE INDICATION IN FLIGHT; REF LOG PAGE 2702474 ITEM #1, FOUND W8C HARN
- [SDR YENA2018121840856](https://openairdocs.org/sdr/YENA2018121840856), Dec 14, 2018: BATTERY PACK. FAILED. FT # 112, ORD-BOS. EMERGENCY LIGHT POWER UNIT #6 FAILED FUNCTIONAL TEST; REPLACED ELPU #6 IAW AMM 33-50-01. ACFT OK FOR SERVICE
- [SDR YENA2018121840855](https://openairdocs.org/sdr/YENA2018121840855), Dec 14, 2018: BATTERY PACK. FAILED. FT # 112, ORD-BOS. EMERGENCY LIGHT POWER UNIT #1 FAILED FUNCTIONAL TEST; REPLACED ELPU #1 IAW AMM 33-50-01. ACFT OK FOR SERVICE
- [SDR YENA201709220781](https://openairdocs.org/sdr/YENA201709220781), Sep 22, 2017: POWER SUPPLY. NO TEST. FOUND THE MID, RT FAIRING EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R THE POWER SUPPLY IAW AMM 33-50-01.
- [SDR YENA20161022943](https://openairdocs.org/sdr/YENA20161022943), Oct 22, 2016: WINDSHIELD. FAILED. DURING CLIMB OUT THROUGH 16,500 FT, PILOT REPORTED HEARING A POP ON F/O SIDE. IMMEDIATELY AFTER HEARING THE POP, A RUSH OF AIR WAS HEARD, WHICH CONTINUED THROUG

All 89: https://openairdocs.org/deregistered/N323JB-2026-06-03/reports.md

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