# N247JB: 2006 Embraer ERJ 190-100 IGW, registration cancelled 2025-10-23

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 23, 2025
- Exported to: Australia
- 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: 19000042
- Year built: 2006
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 22, 2006
- Certificate issued: February 20, 2025
- Last registry action: February 20, 2025
- Mode S code: A24ACA
- Owner when cancelled: [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE)
- Location: [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake)
- Owner type: Corporation
- Owner's area on the map: 40.8386° N, 111.9179° W: Placed by OpenAirDocs at the center of ZIP code 84054, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N247JB
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=247JB
- Page: https://openairdocs.org/deregistered/N247JB-2025-10-23

From the FAA registry file of October 29, 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 (68, newest 50)

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

- [SDR EE4Y2025092723176](https://openairdocs.org/sdr/EE4Y2025092723176), Sep 27, 2025: SKIN. DAMAGED. DURING THE ACCOMPLISHMENT OF SB 190-57-0056 AT RH WING AFT REINFORCEMENT AREA, WAS FOUND FIVE OVERSIZED FASTENER HOLES LOCATED AT THE AREA AFFECTED BY THE REINF
- [SDR EE4Y2025092723175](https://openairdocs.org/sdr/EE4Y2025092723175), Sep 27, 2025: SKIN. DAMAGED. DURING THE ACCOMPLISHMENT OF SB 190-57-0056 AT THE LH WING FORWARD REINFORCEMENT AREA, ALLIANCE AIRLINES FOUND TWO OVERSIZED FASTENER HOLES LOCATED IN THE AREA 
- [SDR EE4Y2025092723174](https://openairdocs.org/sdr/EE4Y2025092723174), Sep 27, 2025: SKIN. DELAMINATED. CUSTOMER REPORTS DELAMINATION DAMAGE AFFECTING THE LH INBOARD AFT FLAP LOWER SKIN. THE DAMAGE IS LOCATED AT SPAR 2 AND RIB 5A +50MM. THE DAMAGE AREA WAS EVALUAT
- [SDR EE4Y2025FA0000667](https://openairdocs.org/sdr/EE4Y2025FA0000667), Sep 27, 2025: SKIN. WORN. DURING THE INSPECTION WAS FOUND ON ENGINE NR 2 OUTBD THRUST REVERSER TRANSLATING COWL, EXTERNAL SKIN WITH WORN AT 1 O’CLOCK POSITION. DUE TI THIS, WAS REPORTED 
- [SDR EE4Y2025092723172](https://openairdocs.org/sdr/EE4Y2025092723172), Sep 27, 2025: REPAIR. MISINSTALLED. DURING STRUCTURAL INSPECTION, AN EXISTING REPAIR WAS FOUND ON THE FUSELAGE SKIN AT FR19 BETWEEN STR-27R. ACCORDING TO PREVIOUS OPERATOR DOCUMENTATION, THE REPAI
- [SDR 2025FA0000651](https://openairdocs.org/sdr/2025FA0000651), Sep 17, 2025: SKIN. DAMAGED. DURING THE STRUCTURE INSPECTION IT WAS FOUND THE FORWARD FUSELAGE, AT FR18+50MM, AND S27LH + 155MM (JUST 8.0MM FROM THESTR 28L FASTENER ROW), THE EXTERNAL SKIN 
- [SDR EE4Y2025091723171](https://openairdocs.org/sdr/EE4Y2025091723171), Sep 17, 2025: SKIN. DAMAGED. CUSTOMER REPORTS A LIGHTNING STRIKE DAMAGE AFFECTING THE EXTERNAL SKIN OF THE FWD FUSELAGE, LOCATED AT FRAME 20+85MM, STRINGER 27RH+115MM. THE DAMAGE EXCEEDS 50
- [SDR YENA2024061300868](https://openairdocs.org/sdr/YENA2024061300868), Jun 11, 2024: POWER SUPPLY. FAILED. FLT#2254, DCA-BOS.' WHILE PERFORMING TASK CARD E190-33-50-25-710-801 FWD RH EXT EMERG LIGHT WILL NOT ILLUMINATE. ( EXTERNAL EMERGENCY-OPS NOT CONDUCTED AT NIGHT
- [SDR YENA2023122101639](https://openairdocs.org/sdr/YENA2023122101639), Dec 20, 2023: UNKNOWN. UNKNOWN. DURING HEAVY MAINTENANCE: AFTER LATCH FITTINGS REMOVAL IN REF WITH NRC 071,CORROSION ON LOWER BEAM IN CUTOUT AT FWD CARGO DOOR; REF TOMX WO # 2404 NR # 00144 CO
- [SDR YENA2023122101638](https://openairdocs.org/sdr/YENA2023122101638), Dec 20, 2023: UNKNOWN. UNKNOWN. DURING HEAVY MAINTENANCE: CRACK AT END OF STRG 9R IN FR 73, LOCATED AT INTERNAL STRUCTURE OF CF II; REF TOMX WO #2404 TOMX NR # 00051Y:STRG 9R IN FR 73, LOCATED
- [SDR YENA2023122101637](https://openairdocs.org/sdr/YENA2023122101637), Dec 20, 2023: UNKNOWN. UNKNOWN. DURING HEAVY MAINTENANCE: AFTER STRG 29R REMOVAL, FOUND CORROSION AT INNER FUSELAGE SKIN LOCATED BETWEEN FR73/74 IN AFT CARGO COMPARTMENT; REF TOMX WO # 2404 NR
- [SDR YENA2023122101636](https://openairdocs.org/sdr/YENA2023122101636), Dec 20, 2023: UNKNOWN. UNKNOWN. DURING HEAVY MAINTENANCE: DURING AFT FUS FAIRING 199ML INSTALLATION, UPPER EMERGENCY LIGHT WAS FOUND INNOPERATIVE; REF TOMX WO #2404 NR # 00176 UPPER EMERGENCY 
- [SDR YENA2023122101635](https://openairdocs.org/sdr/YENA2023122101635), Dec 20, 2023: NONE. NONE. DURING HEAVY MAINTENANCE: # 2 ENGINE REMOVED TO FOM; # 2 ENGINE REINSTALLED IAW E190 AMM 71-00-01.
- [SDR YENA2023122101634](https://openairdocs.org/sdr/YENA2023122101634), Dec 20, 2023: UNKNOWN. UNKNOWN. DURING HEAVY MAINTENANCE: CPCP FINDING CORROSION ON STRINGER ON AFT COMPARTMENT STRUCTURE BTW FR 76/78 AND STRG 29R; "REF TOMX WO # 2404 NR # 00091 CORROSION ON
- [SDR YENA2023122101633](https://openairdocs.org/sdr/YENA2023122101633), Dec 20, 2023: SHEAR TIE. CORRODED. DURING HEAVY MAINTENANCE: CORROSION ON SHEAR CLIP ON AFT COMPARTMENT STRUCTURE BTW FR87 AND STRG 28R/27R; "REF: TOMX W/O 2404 N/R 00097 REPLACED SHEAR CLIP PER 
- [SDR YENA2023122101632](https://openairdocs.org/sdr/YENA2023122101632), Dec 20, 2023: SHEAR TIE. CORRODED. DURING HEAVY MAINTENANCE: CORROSION ON SHEAR CLPI ON AFT COMPARTMENT STRUCTURE BTW FR88 AND STRG 28R/27R; "REF: TOMX W/O 2404 N/R 00096 REPLACED SHEAR CLIP PER 
- [SDR YENA2023122101631](https://openairdocs.org/sdr/YENA2023122101631), Dec 20, 2023: SHEAR TIE. CORRODED. DURING HEAVY MAINTENANCE: CORROSION ON SHEAR CLIP ON AFT COMPARTMENT STRUCTURE BTW FR83 AND STRINGER 28L/29L; "REF: TOMX W/O 2404 N/R 00090 STRINGER CLIP WAS RE
- [SDR YENA2023122101630](https://openairdocs.org/sdr/YENA2023122101630), Dec 20, 2023: SHEAR TIE. CORRODED. DURING HEAVY MAINTENANCE: CORROSTION ON SHEAR CLIP IN AFT COMPARTMENT STRUCTURE BTW FR82 AND STRINGER 28R/29R; "REF: TOMX W/O 2404 N/R 00089SHEAR CLIP WAS REPLA
- [SDR YENA2023122101629](https://openairdocs.org/sdr/YENA2023122101629), Dec 20, 2023: UNKNOWN. UNKNOWN. DURING HEAVY MAINTENANCE: CORROSION ON RH SEAT TRACK LOCATED BTW RE 17/18 AND Y:300RH AT CABIN FLOOR STRUCTURE (W1); REF: TOMX W/O 2404 N/R - 00060 SEAT TRACK W
- [SDR YENA2023122101628](https://openairdocs.org/sdr/YENA2023122101628), Dec 20, 2023: UNKNOWN. UNKNOWN. DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE III / FLOOR STRUCTURE / RH SEAT TRACK / FR84 / CORROSION - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2023122101627](https://openairdocs.org/sdr/YENA2023122101627), Dec 20, 2023: UNKNOWN. UNKNOWN. DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE II / LOWER SKIN / AT STR 29R BETWEEN FR73 – FR74 / CORROSION - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2023092601127](https://openairdocs.org/sdr/YENA2023092601127), Sep 24, 2023: BATTERY. DAMAGED. FLT#2754, DCA-BOS. 'ELT BATTERY ??? AND FOUND ELT WIRES DAMAGED; REPLACED ELT BATTERY REPAIRED C/P PER 25-61-01. CHECK SYSTEM OK.PER 25-61-00.'
- [SDR YENA2022121901271](https://openairdocs.org/sdr/YENA2022121901271), Dec 17, 2022: LINK. MALFUNCTIONED. FLT 1340, NAS-MCO. AFTER LIFT OFF LANDING GEAR UP LOCK SELOIND CYCLE REPEATEDLY. GEAR HAND WOULD NOT GO UP MOMENTARILY. OCCURRED ON BOTH LEGS. THE GEAR EXTENDED
- [SDR YENA2022031500212](https://openairdocs.org/sdr/YENA2022031500212), Dec 21, 2021: SKIN. CRACKED. DURING HEAVY MAINTENANCE, CRACK: LOWER SKIN RH WING AT WING SPAR 2 AND RIB 9A +3.00"; REF TOMX NR 00373:ACCOMPLISHED REPAIR IAW EMBRAER SRM 57-10-01 PAR 11(P)(Q
- [SDR YENA2022031500211](https://openairdocs.org/sdr/YENA2022031500211), Dec 21, 2021: NONE. NONE. DURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING CORROSION IN FWD SEAL REST IN LOWER EDGE OF AFT CARGO DOOR CUTOUT STRUCTURE; ALL WORK ACCOMPLISHED REF
- [SDR YENA2022031500210](https://openairdocs.org/sdr/YENA2022031500210), Dec 21, 2021: NONE. NONE. DURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING CORROSION IN AFT SEAL REST IN LOWER EDGE OF AFT CARGO; ALL WORK ACCOMPLISHED REF TOMX NR 00301 AFT SEA
- [SDR YENA2022031500209](https://openairdocs.org/sdr/YENA2022031500209), Dec 21, 2021: NONE. NONE. DURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING CORROSION IN MIDDLE SEAL REST IN LOWER EDGE OF AFT CARGO DOOR CUTOUT STRUCTURE; ALL WORK ACCOMPLISHED 
- [SDR YENA2022021600071](https://openairdocs.org/sdr/YENA2022021600071), Dec 21, 2021: NONE. NONE. DURING HEAVY MAINTENANCE, CRACK: LOWER SKIN RH WING AT WING SPAR 2 AND RIB 9A +3.00"; REF TOMX NR 00373:ACCOMPLISHED REPAIR IAW EMBRAER SRM 57-10-01 PAR 11(P)(Q
- [SDR YENA2022021600070](https://openairdocs.org/sdr/YENA2022021600070), Dec 21, 2021: NONE. NONE. DURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING CORROSION IN FWD SEAL REST IN LOWER EDGE OF AFT CARGO DOOR CUTOUT STRUCTURE; ALL WORK ACCOMPLISHED REF
- [SDR YENA2022021600069](https://openairdocs.org/sdr/YENA2022021600069), Dec 21, 2021: NONE. NONE. DURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING CORROSION IN MIDDLE SEAL REST IN LOWER EDGE OF AFT CARGO DOOR CUTOUT STRUCTURE; ALL WORK ACCOMPLISHED 
- [SDR YENA2022021600068](https://openairdocs.org/sdr/YENA2022021600068), Dec 21, 2021: NONE. NONE. DURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING CORROSION IN AFT SEAL REST IN LOWER EDGE OF AFT CARGO; ALL WORK ACCOMPLISHED REF TOMX NR 00301 AFT SEA
- [SDR YENA2022021600067](https://openairdocs.org/sdr/YENA2022021600067), Dec 21, 2021: SEAL REST. CORRODED. DURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING CORROSION IN FWD SEAL REST IN LOWER EDGE OF AFT CARGO DOOR CUTOUT STRUCTURE; "ALL WORK ACCOMPLISHED RE
- [SDR YENA2022021600066](https://openairdocs.org/sdr/YENA2022021600066), Dec 21, 2021: SEAL REST. CORRODED. DURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING CORROSION IN AFT SEAL REST IN LOWER EDGE OF AFT CARGO; "ALL WORK ACCOMPLISHED REF TOMX NR 00301 AFT SE
- [SDR YENA2022021600065](https://openairdocs.org/sdr/YENA2022021600065), Dec 21, 2021: DOOR FRAME. CORRODED. DURING HEAVY MAINTENANCE, "FROM TOMX NR 00300, INITIAL INSPECTION: ""CPCP FINDING"" CORROSION IN FASTENER PERIPHERY LOCATED OVER MACHINED BEAM BETWEEN STRG 27R/
- [SDR YENA2022021600064](https://openairdocs.org/sdr/YENA2022021600064), Dec 21, 2021: DOOR FRAME. CORRODED. DURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING CORROSION IN MIDDLE SEAL REST IN LOWER EDGE OF AFT CARGO DOOR CUTOUT STRUCTURE; "ALL WORK ACCOMPLISHED
- [SDR YENA2021102100707](https://openairdocs.org/sdr/YENA2021102100707), Oct 20, 2021: DIAPHRAGM. BLOWN. FLT # 628, CHS-EWR. R1 DOOR REQ. SERVICING AND DOOR DIAPHRAM BLOWN. ; REPLACED R-1 SERVICE DOOR PNEUMATIC ASSY DIAPHRAM AND SHEAR PIN IAW AMM 52-41-53/400. SERV
- [SDR YENA2021102100706](https://openairdocs.org/sdr/YENA2021102100706), Oct 20, 2021: SLIDE. DEPLOYED. FLT # 628, CHS-EWR. A/C OOS DUE TO R1 DOOR SLIDE BLOWN ; R/R OF R1 DOOR SLIDE IAW AMM 52-11-40. OPS CHECK GOOD A/C OK FOR SVC.
- [SDR YENA2021072900489](https://openairdocs.org/sdr/YENA2021072900489), Jul 25, 2021: CONTROL MODULE. FAILED. FLT 2155, JFK-FLL. IN CRUISE, GOT "BRK FH FAULT" AND "BRK LH FAULT". AFTER LANDING, GOT "LG NO DISPATCH" WITH BRK FAULT MESSAGES. NOTICED HYDRAULIC SYSTEM 1 QUA
- [SDR YENA2021020400083](https://openairdocs.org/sdr/YENA2021020400083), Jan 31, 2021: WARNING MESSAGE. FALSE ACTIVATION. FLIGHT 663, EWR-JAX. AILERON RT HAND FAIL MSG APPEARED AT CRUISE; TROUBLESHOT IAW FIM REFERENCE 27-03-00-810-926-A . PERFORMED RETURN TO SERVICE TEST IAW AMM 27
- [SDR YENA201909120525](https://openairdocs.org/sdr/YENA201909120525), Sep 12, 2019: POWER UNIT. FAILED. FLT 1979, DCA-FLL. WHILE PERFORMING T/C E190-33-50-01-720-801-AFT. FOUND AFT ELPU 5+6 FAILS FUNCTIONAL TEST; R & R ELPU 5 + 6 IAW AMM 33-50-01. OPS CK OK. A/C O
- [SDR YENA201902259090](https://openairdocs.org/sdr/YENA201902259090), Feb 19, 2019: UNKNOWN. ODOR. FT # 2133, DESCENDING THRU 12K, GOT STRONG JET EXHAUST SMELLING FUMES IN COCKPIT. GOT VERY STRONG SMELLING BOTH PILOTS WENT ON O2. TURNING RECIRCS OFF BRIEFLY H
- [SDR YENA2018092090352](https://openairdocs.org/sdr/YENA2018092090352), Sep 19, 2018: BATTERY. DISCHARGED. FLT 2680, EWR-BOS. 2 EACH EMERGENCY LIGHT POWER UNITS FAILED OPERATIONAL TEST. REPLACED 2 EACH EMERGENCY POWER UNITS IAW AMM 33-50-01.
- [SDR YENA2018092090351](https://openairdocs.org/sdr/YENA2018092090351), Sep 19, 2018: BATTERY. DISCHARGED. FLT 2680, EWR-BOS. 2 EACH EMERGENCY LIGHT POWER UNITS FAILED OPERATIONAL TEST. REPLACED 2 EACH EMERGENCY POWER UNITS IAW AMM 33-50-01.
- [SDR YENA201807270935](https://openairdocs.org/sdr/YENA201807270935), Jul 27, 2018: SKIN. DAMAGED. DURING HEAVY MAINTENANCE ( BASIC 6 CHECK AT SAL) FOR A/C N247JB, WHILE ACCOMPLISHING JACKING PROCEDURES, CREASE DAMAGE WAS A RESULT OF IMPROPERLY FOLLOWING PROC
- [SDR YENA2018100970579](https://openairdocs.org/sdr/YENA2018100970579), Jul 27, 2018: SUPPORT BRACKET. CORRODED. DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF NR 2018-222180 SUPPORT BRACKET FLOOR STRUCTURE LOCATED AT FR76 AND BETWEEN S29R TO S-29L (2EA) ON AFT 
- [SDR YENA2018100970578](https://openairdocs.org/sdr/YENA2018100970578), Jul 27, 2018: SUPPORT BRACKET. CORRODED. DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF NR 2018-222179 SUPPORT BRACKET FLOOR STRUCTURE LOCATED AT FR74 AND S-29L ON AFT CARGO COMPARTMENT; REP
- [SDR YENA2018100970577](https://openairdocs.org/sdr/YENA2018100970577), Jul 27, 2018: SUPPORT BRACKET. CORRODED. DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF NR 2018-222184 SUPPORT BRACKET FLOOR STRUCTURE AT FR81 ANFD SR-29R ON AFT CARGO COMPARTMENT; REPLACED 
- [SDR YENA2018100970576](https://openairdocs.org/sdr/YENA2018100970576), Jul 27, 2018: SUPPORT BRACKET. CORRODED. DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF NR 2018-222183 SUPPORT BRACKET FLOOR STRUCTURE LOCATED AT FR80 BETWEEN S29L-S29R (2EA) ON AFT CARGO CO
- [SDR YENA2018100970575](https://openairdocs.org/sdr/YENA2018100970575), Jul 27, 2018: SUPPORT BRACKET. CORRODED. DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF NR 2018-222183 SUPPORT BRACKET FLOOR STRUCTURE LOCATED AT FR80 BETWEEN S29L TO S29R (2EA) ON AFT CARGO
- [SDR YENA201712131000](https://openairdocs.org/sdr/YENA201712131000), Dec 13, 2017: BATTERY PACK. FAILED. FT # 1282, RIC-BOS. EMERGENCY LIGHT OVER L1 DOOR INOP; R & R #1 EMERGENCY POWER UNIT PER AMM 33-50-01. OPS CHECK GOOD.

All 68: https://openairdocs.org/deregistered/N247JB-2025-10-23/reports.md

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20070905830039I](https://openairdocs.org/incident/20070905830039I), Sep 5, 2007: Emb ERJ190100IGW (N247JB), Buffalo, NY, No damage. (-23) Jet blue flight 1211, boston, ma to Buffalo, NY, 1441 zulu time. During configuration for final approach into buf, the captain [privacy data omitted]…

## Other aircraft with N247JB

- [Cancelled 1990-11-02](https://openairdocs.org/deregistered/N247JB-1990-11-02): Barnett James S DRIFTER XP503, S/N DR0247. N-number assigned, not yet registered

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