# N258JB: 2006 Embraer ERJ 190-100 IGW, registration cancelled 2025-12-22

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 22, 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: 19000047
- Year built: 2006
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 5, 2006
- Certificate issued: July 22, 2025
- Last registry action: July 22, 2025
- Mode S code: A27600
- 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/N258JB
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=258JB
- Page: https://openairdocs.org/deregistered/N258JB-2025-12-22

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 (101, newest 50)

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

- [SDR EE4Y2025111423461](https://openairdocs.org/sdr/EE4Y2025111423461), Nov 14, 2025: SKIN. NICKED. DURING STRUCTURAL INSPECTION, SKIN WITH NICKS WERE FOUND AT FWD FUSELAGE FROM FR18+85MM / FR19+150MM, BTWN STR26L / 27L+80MM. THE NICKS REPORTED EXCEED THE LIMI
- [SDR EE4Y2025111423448](https://openairdocs.org/sdr/EE4Y2025111423448), Nov 14, 2025: SKIN. DAMAGED. DURING STRUCTURAL INSPECTION, LIGHTNING STRIKE DAMAGES (LSD) WERE FOUND ON THE FUSELAGESKIN. THE LSDS WERE REMOVED BY BLENDING THE AFFECTED AREAS IN ACCORDANCE 
- [SDR EE4Y2025111423446](https://openairdocs.org/sdr/EE4Y2025111423446), Nov 14, 2025: SKIN. DAMAGED. DURING STRUCTURAL INSPECTION, SMALL NICKS AND LIGHTNING STRIKE DAMAGES WERE FOUND ONTHE FUSELAGE SKIN. MOST NICKS WERE REMOVED VIA BLEND-OUTS. 3 LSDS WERE REMOV
- [SDR EE4Y2025111323455](https://openairdocs.org/sdr/EE4Y2025111323455), Nov 13, 2025: SKIN. DENTED. DURING A STRUCTURAL INSPECTION, A DENT WAS IDENTIFIED ON THE CENTER FUSELAGE LOWER SKIN AT FRAME 27 AND BETWEEN STRINGERS 27LH-28RH. ACCORDING TO DOCUMENTATION 
- [SDR EE4Y2025111323452](https://openairdocs.org/sdr/EE4Y2025111323452), Nov 13, 2025: INLET. DENTED. DURING THE STRUCTURE INSPECTION, WAS IDENTIFIED AN EXISTING DENTS REPAIR LOCATED ON THE ENGINE NR 2, INLET COWL, INNER BARREL. ACCORDING TO DOCUMENTATION PROVID
- [SDR EE4Y2025111323451](https://openairdocs.org/sdr/EE4Y2025111323451), Nov 13, 2025: INLET. DENTED. DURING THE STRUCTURE INSPECTION, WAS IDENTIFIED AN EXISTING DENTS REPAIR LOCATED ON THE ENGINE NR 1, INLET COWL, INNER BARREL. ACCORDING TO DOCUMENTATION PROVID
- [SDR EE4Y2025111323457](https://openairdocs.org/sdr/EE4Y2025111323457), Nov 13, 2025: SKIN. DAMAGED. DURING A STRUCTURAL INSPECTION, NICKS WERE FOUND ON THE FUSELAGE SKIN AT FR 26 AND STRINGER 27L. THE DAMAGE WAS REMOVED VIA BLEND-OUT IN ACCORDANCE WITH SRM 51-
- [SDR EE4Y2025111323456](https://openairdocs.org/sdr/EE4Y2025111323456), Nov 13, 2025: SKIN. NICKED. DURING A STRUCTURAL INSPECTION, NICKS WERE IDENTIFIED ON THE FUSELAGE SKIN FROM FR 32 TO FR 32 + 175 MM, BETWEEN STRINGERS 27R AND 28R. THE DAMAGE WAS REMOVED V
- [SDR EE4Y2025111323450](https://openairdocs.org/sdr/EE4Y2025111323450), Nov 13, 2025: SKIN. CRACKED. DURING INSPECTION, A CRACK WAS FOUND ON THE LH SKIN PANEL OF THE VERTICAL STABILIZER, LOCATED NEAR THE AFT EDGE JUST BELOW RIB 06. THE AFFECTED AREA FALLS WITHI
- [SDR EE4Y2025111323449](https://openairdocs.org/sdr/EE4Y2025111323449), Nov 13, 2025: SKIN. DAMAGED. DURING A STRUCTURAL INSPECTION, LIGHTNING STRIKE DAMAGE (LSD) WAS FOUND ON THE FUSELAGE SKIN AT FR 97 + 25 MM, STR-27LH, DUE TO ITS PROXIMITY TO THE STRINGER 27
- [SDR EE4Y2025111323447](https://openairdocs.org/sdr/EE4Y2025111323447), Nov 13, 2025: SKIN. DAMAGED. DURING STRUCTURAL INSPECTION, LIGHTNING STRIKE DAMAGES (LSD) WERE FOUND ON THE FUSELAGE SKIN. THE LSDS WERE REMOVED BY BLENDING THE AFFECTED AREAS IN ACCORDANCE
- [SDR EE4Y2025111323445](https://openairdocs.org/sdr/EE4Y2025111323445), Nov 13, 2025: SKIN. DAMAGED. DURING STRUCTURAL INSPECTION, SMALL NICKS AND LIGHTNING STRIKE DAMAGES (LSD) WERE FOUND ON THE FUSELAGE SKIN. MOST NICKS WERE REMOVED VIA BLEND-OUTS. SIX (6) LS
- [SDR EE4Y2025111323444](https://openairdocs.org/sdr/EE4Y2025111323444), Nov 13, 2025: SKIN. CRACKED. DURING A STRUCTURAL INSPECTION, A CRACK WAS FOUND IN THE RH WING LEADING EDGE SKIN CUTOUTBETWEEN RIBS 19 AND 20. THE AFFECTED AREAWAS TRIMMED IN ACCORDANCE WITH
- [SDR EE4Y2025111323443](https://openairdocs.org/sdr/EE4Y2025111323443), Nov 13, 2025: SKIN. CRACKED. DURING A STRUCTURAL INSPECTION, A CRACK WAS FOUND IN THE LH WING LEADING EDGE SKIN CUTOUT BETWEEN RIBS 19 AND 20. THE AFFECTED AREA WAS TRIMMED IN ACCORDANCE WI
- [SDR EE4Y2025111323442](https://openairdocs.org/sdr/EE4Y2025111323442), Nov 13, 2025: SKIN. DAMAGED. DURING A STRUCTURAL INSPECTION, CUSTOMER IDENTIFIED AN EXISTING SKIN REPAIR LOCATED BETWEEN FR23 AND FR24, AND BETWEEN STRINGERS 16L AND 17L. ACCORDING TO DOCUM
- [SDR YENA2024103101420](https://openairdocs.org/sdr/YENA2024103101420), Oct 30, 2024: BATTERY PACK. NO TEST. DURING HEAVY MAINTENANCE: EMERGENCY LIGHT BATTERY PACK #5 FAILED OPERATIONAL CHECK; REF EAMS WO H9782, NR00001 REPLACED LIGHT BATTERY PACK #5 PER E190 AMM 33-50
- [SDR YENA2023091801107](https://openairdocs.org/sdr/YENA2023091801107), Sep 13, 2023: UNKNOWN. UNKNOWN. DURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON FLOOR STRUCTURE LONGITUDINAL BEAM BTW FR 86 TO FR 89 AND Y=250 LH (W2); (RESOLVED ON W
- [SDR YENA2023091801106](https://openairdocs.org/sdr/YENA2023091801106), Sep 13, 2023: UNKNOWN. UNKNOWN. DURING HEAVY MAINTENANCE: CORROSION ON FLOOR BEAM BTW FR12 TO FR13 AND Y = 460 LH (W1); (RESOLVED ON W/O: 1228947 TASKCARD: NR-00003 ) CORROSION ON FLOOR BEAM B
- [SDR YENA2023091801105](https://openairdocs.org/sdr/YENA2023091801105), Sep 13, 2023: UNKNOWN. UNKNOWN. DURING HEAVY MAINTENANCE: CORROSION ON FLOOR STRUCTURE LONGITUDINAL BEAM AT FR 16 AND Y= 280 LH (W1); (RESOLVED ON W/O: 1228947 TASKCARD: NR-00004 ) CORROSION O
- [SDR YENA2023091801104](https://openairdocs.org/sdr/YENA2023091801104), Sep 13, 2023: UNKNOWN. UNKNOWN. DURING HEAVY MAINTENANCE: AFTER FASTENERS REMOVAL: CORROSION ON STGR 25LH BTW FR82/83 WAS FOUND; REF TOMX WO 2265 NR# 00234 STRINGER 25LH FROM FR74 TO FR90 WAS 
- [SDR YENA2023091801103](https://openairdocs.org/sdr/YENA2023091801103), Sep 13, 2023: UNKNOWN. UNKNOWN. DURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON FLOOR STRUCTURE LONGITUDINAL BEAM, LOCATED BTW FR12 TO FR19 AND Y= 280 RH (W1); EF TOM
- [SDR YENA2023091801102](https://openairdocs.org/sdr/YENA2023091801102), Sep 13, 2023: UNKNOWN. UNKNOWN. DURING HEAVY MAINTENANCE: JETBLUE CUSTOMER N/R: LAV SERVICE PANEL CUTOUT, FUSELAGE SKIN HAS CORROSION; (RESOLVED ON W/O: 1206076 TASKCARD: NR-00013 ) SKIN AND D
- [SDR YENA2023091801101](https://openairdocs.org/sdr/YENA2023091801101), Sep 13, 2023: UNKNOWN. UNKNOWN. DURING HEAVY MAINTENANCE: AFTER RH ELEVATOR BEARING REMOVAL FROM HINGE, FITTING #2 WAS FOUND CORROSION IN HOUSING; REPLACED HOUSING AT RH ELEVATOR HINGE FITTING
- [SDR YENA2023091801100](https://openairdocs.org/sdr/YENA2023091801100), Sep 13, 2023: UNKNOWN. UNKNOWN. DURING HEAVY MAINTENANCE: REPLACE THE INBOARD AND OUTBOARD SPAR AT THE RH PYLON DUE TO AFT LUG CORROSION; REF TOMX W/O 2265 NR00306: INBD AND OUTBD SPARS AT RH 
- [SDR YENA2023091801099](https://openairdocs.org/sdr/YENA2023091801099), Sep 13, 2023: UNKNOWN. UNKNOWN. DURING HEAVY MAINTENANCE: REPLACE THE INBOARD AND OUTBOARD SPAR AT THE LH PYLON DUE TO AFT LUG CORROSION; REF TOMX W/O 2265 NR00305: INBD AND OUTBD SPARS AT LH 
- [SDR YENA2023091801098](https://openairdocs.org/sdr/YENA2023091801098), Sep 13, 2023: UNKNOWN. UNKNOWN. DURING HEAVY MAINTENANCE: MAJOR REPAIR: REPLACE THE EXISTING REPAIR DOUBLER IN LH WING THAT INTERFERES WITH THE INSTALLATION OF SB190-57-0056, LH WING REAR LOWE
- [SDR YENA2023091801097](https://openairdocs.org/sdr/YENA2023091801097), Sep 13, 2023: UNKNOWN. UNKNOWN. DURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON FLOOR STRUCTURE LONGITUDINAL BEAM, LOCATED BTW FR12 TO FR19 AND Y= 280 RH (W1); REF TO
- [SDR YENA2023091801096](https://openairdocs.org/sdr/YENA2023091801096), Sep 13, 2023: UNKNOWN. UNKNOWN. DURING HEAVY MAINTENANCE: WINGS / RH & LH WING / FWD LWR SKINS / SB IMPLEMENTATION / FWD FITTINGS / BOLT INSTALLATION / WASHER DEVIATION - PERMANENT REPAIR. (CO
- [SDR YENA2023091801095](https://openairdocs.org/sdr/YENA2023091801095), Sep 13, 2023: UNKNOWN. UNKNOWN. DURING HEAVY MAINTENANCE: WINGS / RH WING / WING MAIN BOX / LOWER SKIN PANEL SB APPLICATION / DISCREPANT FASTENER - TEMPORARY REPAIR. (CONSIDERED AS A MAJOR REP
- [SDR YENA2023091801094](https://openairdocs.org/sdr/YENA2023091801094), Sep 13, 2023: UNKNOWN. UNKNOWN. DURING HEAVY MAINTENANCE: WINGS / LH WING / LOWER SKIN PANEL BETWEEN RIB 9-10 / EXISTING REPAIR & SB 57-0056 DOUBLER INTERFERENCE - TEMPORARY REPAIR. (CONSIDERE
- [SDR YENA2023091801093](https://openairdocs.org/sdr/YENA2023091801093), Sep 13, 2023: UNKNOWN. UNKNOWN. DURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / FLOOR STRUCTURE AT FR 13-14 AND Y= 280 RH / CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023091801092](https://openairdocs.org/sdr/YENA2023091801092), Sep 13, 2023: UNKNOWN. UNKNOWN. DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE III / FRAME 88 / BETWEEN STRINGER 27R AND 28R / EXISTING MISDRILLED HOLE - PERMANENT REPAIR. (CONSIDERED AS
- [SDR YENA2023091801091](https://openairdocs.org/sdr/YENA2023091801091), Sep 13, 2023: UNKNOWN. UNKNOWN. DURING HEAVY MAINTENANCE: WINGS / LH AND RH WING / REAR LOWER SKINS / SB 190-57-0056 / REPAIR WASHER INSTALLATION - TEMPORARY REPAIR. (CONSIDERED AS A MAJOR REP
- [SDR YENA2023091801090](https://openairdocs.org/sdr/YENA2023091801090), Sep 13, 2023: UNKNOWN. UNKNOWN. DURING HEAVY MAINTENANCE: WINGS / RH WING / WING MAIN BOX / LOWER SKIN PANEL SB APPLICATION / DISCREPANT FASTENER - TEMPORARY REPAIR. (CONSIDERED AS A MAJOR REP
- [SDR YENA2023011300039](https://openairdocs.org/sdr/YENA2023011300039), Jan 10, 2023: HINGE PIN. OUT OF POSITION. FLT#23, DCA-MCO. 'COCKPIT DOOR HINGE PIN POPPED OUT OF POSITION; REPLACED COCKPIT DOOR LOWER HINGE AND ADJUSTED COCKPIT DOOR IAW AMM 52-51-01. A/C OK FOR SERVIC
- [SDR YENA202301040011](https://openairdocs.org/sdr/YENA202301040011), Dec 26, 2022: PRESSURE SWITCH. FAULTED. FLT 726, BWI - BOS. AIRCRAFT PERFORMED AN AIR TURN BACK TO BWI, BLEED 1 OVERPRESSURE MSG APPEARED ON CLIMB AFTER TAKEOFF. RAN QRH PROCD, MSG RETURNED. DISPATCH 
- [SDR YENA2022121901269](https://openairdocs.org/sdr/YENA2022121901269), Dec 16, 2022: A/C PACK. ODOR. FLT 1182, RIC-BOS. ODOR OF EXHAUST IN FLIGHT DECK ONLY. DURING THE LAST PART OF THE CLIMB, CRUISE, AND DESCENT. MILD, EXHAUST SMELL THROUGH FLIGHT DECK VENTS WO
- [SDR YENA2022081200793](https://openairdocs.org/sdr/YENA2022081200793), Aug 8, 2022: A/C PACK. DIRTY. FLT#2028, MCO-EWR. 'ODOR DIRTY SOCKS DETECTED ON TAKE-OFF ROLL LEVEL 1 DURATION OF 5 MINUTES MODERATE INTENSITY DETECTED IN COCKPIT ONLY NO REPORT OF ODOR FROM 
- [SDR YENA2022021400062](https://openairdocs.org/sdr/YENA2022021400062), Feb 13, 2022: NONE. FAILED. FLT # 733, MCO-SJU (AIRTURN BACK TO MCO). CLIMBING THROUGH FL230 ENG 2 LP VIBRATION WAS 4.1 FOLLOWED QRH PROCEDURE; PER FIM 77-31-00-810-816A R/R EVM MODULE PER
- [SDR YENA2020120700565](https://openairdocs.org/sdr/YENA2020120700565), Dec 1, 2020: POWER SUPPLY. FAILED. FLT 932, IAH-BOS. EMERGENCY LIGHT AT CEILING PANEL 11 INOPERABLE. R & R EMERGENCY LIGHT POWER UNIT NR 6, IAW AMM 33-50-01. OPERATIONS CHECK GOOD. A/C OK FOR SER
- [SDR YENA2020090800453](https://openairdocs.org/sdr/YENA2020090800453), Sep 4, 2020: BATTERY. FAILED. DURING HEAVY MAINTENANCE, INOPERABLE EMERGENCY LIGHT POWER UNIT AT MID CABIN P/N 3400-22-10 S/N 001995 IN PASSENGER CABIN. RESOLVED ON W/O: 1050580 TASKCARD: NR
- [SDR YENA2020090800452](https://openairdocs.org/sdr/YENA2020090800452), Sep 4, 2020: LIGHT. INOPERATIVE. DURING HEAVY MAINTENANCE, INOPERABLE EXTERNAL SKIN LT FWD EMERGENCY LIGHT ON UPPER FUSELAGE (1EA). R & R FWD EXTERNAL EMERGENCY LIGHT ASSEMBLY LT SIDE, IAW E190
- [SDR YENA2020090800451](https://openairdocs.org/sdr/YENA2020090800451), Sep 4, 2020: SKIN. CORRODED. DURING HEAVY MAINTENANCE, CORROSION INTERNAL SKIN ON ACCESS PANEL 351GL IN TAIL COMPARTMENT. ACCOMPLISHED REPAIR OF CORROSION DAMAGE FOUND ON THE TAIL CONE ( S/
- [SDR YENA2020090800450](https://openairdocs.org/sdr/YENA2020090800450), Sep 4, 2020: SKIN. DAMAGED. DURING HEAVY MAINTENANCE, PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN BETWEEN FR 96 TO FR 97 AT STGR 23R LOWER FUSELAGE. PERFORMED PERMANENT REPAIR ON EXTERNAL 
- [SDR YENA2020090800449](https://openairdocs.org/sdr/YENA2020090800449), Sep 4, 2020: SKIN. DENTED. DURING HEAVY MAINTENANCE DENT EXTERNAL SKIN FR 96 TO FR 97 AT LEVEL STR23L LOWER FUSELAGE. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN BETWEEN FR96 TO FR97 AT L
- [SDR YENA2020090800448](https://openairdocs.org/sdr/YENA2020090800448), Sep 4, 2020: RIB. CRACKED. DURING HEAVY MAINTENANCE, CRACK RIB 10 WING MAIN BOX LOWER SKIN SPAR 2 TRAILING EDGE RT WING. PERFORMED PERMANENT REPAIR ON RIB 10 WING MAIN BOX LOWER SKIN SPAR
- [SDR YENA201809220942](https://openairdocs.org/sdr/YENA201809220942), Sep 22, 2018: SKIN. CRACKED. DURING HEAVY MAINTENANCE, B6 CHECK AT (SAL), A CRACK (LENGTH: 2.627 INCHES) WAS FOUND ON LT WING REAR LOWER SKIN (P/N 190-33065-013) AT RIB 10+1". SEE THE REF /
- [SDR YENA2018092620359](https://openairdocs.org/sdr/YENA2018092620359), Sep 22, 2018: STRUCTURE. CORRODED. DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON SHEAR TIE FLOOR STRUCTURE AT FR 76 BTWN STR 28R TO STR 29R ON AFT CARGO COMPARTMENT; REPLACED SHEAR TIE FL
- [SDR YENA201708260704](https://openairdocs.org/sdr/YENA201708260704), Aug 26, 2017: MOUNT. DAMAGED. FLT 1479, DCA-FLL. FOUND AFT ESCAPE DOOR SLIDE BUSTLE BRACKET DAMAGED(AFT). REMOVE SLIDE FOR REPAIR, REPLACED SHOCK MOUNT ON SLIDE AND REINSTALLED SLIDE ASSY IA
- [SDR YENA20160620569](https://openairdocs.org/sdr/YENA20160620569), Jun 20, 2016: PANEL SUPPORT. CORRODED. DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA RT PANEL SUPPORT AT FRAME 90, RBL 42". R & R RT PANEL SUPPORT IAW SRM 51-42-01 & 51-43-03.

All 101: https://openairdocs.org/deregistered/N258JB-2025-12-22/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ENG09IA017](https://openairdocs.org/ntsb/ENG09IA017), Sep 3, 2009: Embraer ERJ 190-100 IGW (N258JB), Nassau, Bahamas, incident, minor damage. Probable cause: failure of the engine high pressure turbine active clearance control valve fuel rod supply tube coupling seal due to a cross-threaded B-nut as installed during original manufacture.

## 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 20130404006909I](https://openairdocs.org/incident/20130404006909I), Apr 4, 2013: Embraer ERJ 190-100 IGW (N258JB), Allentown, PA, No damage. Washington FSDO aviation safety inspectors pete popsuy and michele johnson arrived iad, gate B66 at approximately 1045 on 4/4/13. Jetblue flt. # 1251 bos iad,…

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