N265JB2006 Embraer ERJ 190-100 IGW
This N-number isn't registered right now. Below is its last known registration, canceled Aug 4, 2025.
Safety record in brief:No NTSB accidents or incidents since 198220 ADs may apply51 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- Tvpx Aircraft Solutions INC Trustee
- Owner type
- Corporation
- City, state
- North Salt Lake, UT
- Certificate issued
- Jul 9, 2025
- Canceled
- Aug 4, 2025
- Airworthiness
- Standard · Transport
- Airworthiness date
- Nov 10, 2006
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Embraer
- Model
- ERJ 190-100 IGW
- Year
- 2006
- Serial number
- 19000049
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 20
- Engines
- 2
- Max takeoff weight
- 12,500 - 19,999 lb
- Type certificate data sheet
- A57NM
- Mode S code
- A2925A
Engine
- Make and model
- Ge Cf34-10e6
- Type
- Turbo-fan
- Power
- 18,820 lb thrust
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2025Tvpx Aircraft Solutions INC TrusteeNorth Salt Lake, UT
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (20)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2023-21-11 | Embraer S.A. (Type Certificate Previously Held by Yaborã Indústria Aeronáutica S.A.… | Dec 26, 2023 | Airframe (ERJ 190-100 IGW) |
| 2022-16-01 | Windows | Aug 15, 2022 | Airframe (ERJ 190-100 IGW)Only with: Equipped with any NORDAM passenger window having PMA P/N NP00038-3. |
| 2022-05-08 | Turbine Engine Oil System | Apr 11, 2022 | Engine (CF34-10E6)Only with: Stationary oil seal P/N B1316-00453 or B1316-01274 installed at No. 1 forward bearing that was repaired, overhauled, or entered service after August 2014 and has used high thermal stability or high performance capability oil for 56 FHs or more. |
| 2021-25-02 | Nacelles/ pylons | Jan 20, 2022 | Airframe (ERJ 190-100 IGW) |
| 2020-25-08 | Flight controls | Jan 21, 2021 | Airframe (ERJ 190-100 IGW)Serial numbers per ANAC AD 2020-05-01 (ERJ 170) and ANAC AD 2020-05-02 (ERJ 190) |
Show all 20 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2020-12-12 | Nacelles/ pylons | Aug 13, 2020 | Airframe (ERJ 190-100 IGW) |
| 2020-05-21 | Indicating/ recording systems | Apr 24, 2020 | Airframe (ERJ 190-100 IGW)Serial numbers per ANAC Brazilian AD 2019-10-01 |
| 2019-24-16 | Embraer S.A. Airplanes | Feb 3, 2020 | Airframe (ERJ 190-100 IGW)Certain serial numbers: 19000002; 19000004; 19000006–19000213; 19000215–19000276; 19000278–19000466; 19000468–19000525; … |
| 2019-19-03 | Fuselage | Oct 31, 2019 | Airframe (ERJ 190-100 IGW)Serial numbers per Embraer Service Bulletins SB170-53-0142 Rev 01, SB190-53-0098 Rev 01, and SB190LIN-53-0072 Rev 01 |
| 2019-03-21 | Landing Gear | Apr 2, 2019 | Airframe (ERJ 190-100 IGW) |
| 2017-21-09 | Fuselage | Nov 27, 2017 | Airframe (ERJ 190-100 IGW)Serial numbers per Embraer Service Bulletin 170-53-0051, Revision 03 (ERJ 170); Embraer Service Bulletin 190-53-0019, Revision 03 (ERJ 190) |
| 2016-12-14 | Pneumatic | Jul 27, 2016 | Airframe (ERJ 190-100 IGW) |
| 2013-25-04 | Embraer S.A. Airplanes | Feb 10, 2014 | Airframe (ERJ 190-100 IGW)Only with: ERJ 170 airplanes equipped with Goodrich escape slides P/N 4A4030-5; ERJ 190 airplanes equipped with Goodrich escape slides P/N 104003-2. |
| 2013-16-22 | Fuselage | Sep 27, 2013 | Airframe (ERJ 190-100 IGW)Serial numbers per Embraer Service Bulletins 170-53-0093 Rev 01, 190-53-0054 Rev 01, and 190LIN-53-0059 Rev 01, dated March 16, 2012 |
| 2013-11-17 | Pneumatic | Aug 6, 2013 | Airframe (ERJ 190-100 IGW)Only with: Having Hamilton Sundstrand low pressure check valve (LPCV) P/N 1001447-3 or 1001447-4 installed. |
| 2013-11-07 | Landing gear | Jul 9, 2013 | Airframe (ERJ 190-100 IGW)Serial numbers per EMBRAER Service Bulletin 190-57-0036, Revision 02, dated August 12, 2011; EMBRAER Service Bulletin 190LIN-57-0016, dated June 10, 2011 |
| 2013-05-12 | Fire Protection | May 3, 2013 | Airframe (ERJ 190-100 IGW)Serial numbers per Embraer Service Bulletins 170-26-0011 Rev 02, 190-26-0011 Rev 02, and 190LIN-26-0006 Rev 02 |
| 2013-03-13 | Doors | Mar 19, 2013 | Airframe (ERJ 190-100 IGW)Serial numbers per EMBRAER Service Bulletins 170-52-0055 Rev 01, 190-52-0038 Rev 01, and 190LIN-52-0020 |
| 2012-16-09 | Air Conditioning | Sep 21, 2012 | Airframe (ERJ 190-100 IGW) |
| 2012-15-03 | Landing Gear | Sep 4, 2012 | Airframe (ERJ 190-100 IGW) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (51)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Lights · power unit · failedMar 23, 2019
FLT 1736, MSP-BOS. BOTH AFT EMERGENCY LIGHT POWER UNIT FAILED FUNCTIONAL TEST; R & R BOTH AFT EMERGENCY LIGHT POWER UNITS REF AMM CH 33-50-01. OPS CHECK OK.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · power unit · failedMar 23, 2019
FLT 1736, MSP-BOS. BOTH AFT EMERGENCY LIGHT POWER UNIT FAILED FUNCTIONAL TEST; R & R BOTH AFT EMERGENCY LIGHT POWER UNITS REF AMM CH 33-50-01. OPS CHECK OK.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · power unit · failedMar 23, 2019
FLT 1736, MSP-BOS. MID LT EMERGENCY POWER UNIT FOR LIGHT FAILED FUNCTIONAL CHECK; R & R MID LT EMERGENCY LIGHT POWER UNIT. REF AMM CH 33-50-01.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Lights · power unit · failedMar 23, 2019
FLT 1736, MSP-BOS. FWD RT EMERGENCY LIGHT POWER UNIT FAILED FUNCTIONAL CHECK; R & R FWD RT EMERGENCY LIGHT POWER UNIT REF AMM CH 33-50-01 OPS CHECK OK.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · shear panel · corrodedSep 27, 2018
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON CABIN FLOOR STRUCTURE, AT STR 17R, AND BTW FR 84 AND FR 85, CORROSION FOUND ON SHEAR PANEL. REF P/N: 190-65293-001, REF SRMI 53-1-10, FIG 78. NO SPECIFIED LIMITS NOTED IN THE SRM, THEREFORE THE SHEAR PANEL WAS REPLACED PER SRM 51-42-04.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · splice · corrodedSep 27, 2018
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD FUSELAGE FLOOR STRUCTURE, BTW FR18-19 AND BTW RBL 11-36, CORROSION MEAS 2.75"L X .700" W X .038" D. MATERIAL LOSS IS BEYOND 60%. REMOVED AND REPLACED FLOOR SPLICE IAW 51-43-03. REF P/N: 170-12114-001. CROSS REF SRMI 53-10-10, FIG 51A, ITEM…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · plate · corrodedSep 27, 2018
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD FUSELAGE FLOOR STRUCTURE, SILL FLOOR PLATE, LOCATED BTW FR12-14 AND RBL 36 TO RBL 46, CORROSION IS BEYOND LIMITS. CORROSION MEAS 2.00" L X 1.00" W X .030" D. MATERIAL LOSS IS 60%. REMOVED AND REPLACED FLOOR SILL PLATE IAW 51-41-02 AND…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · plate · corrodedSep 27, 2018
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CARGO DOOR SURROUND, CLOSING-PLATE. CORRODED BEYOND LIMITS. CORROSION MEASURES 2.00" X .250"W X .045" D. MATERIAL LOSS = 16.36%. CORROSION IS BEYOND ALLOWABLE LIMITS. NOTE NO SPECIFIED LIMITS IN THE AMM OR SRM, THEREFORE THE PART WAS…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · shear tie · corrodedSep 27, 2018
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD. FUSELAGE AREA, LOCATED AT FR 16 AND BTW STR 28L & STR 28R, SHEAR-TIE. MAT LOSS WAS 50%; L= .90" X W=.150"W X .D= .020". NO SPECIFIC DAMAGE LIMITS IN THE SRM OR AMM FOR THIS PART, MAT LOSS WAS 50%. THEREFORE, THE PART WAS DEEMED…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · beam · corrodedSep 27, 2018
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CARGO DOOR SURROUND, SILL BEAM FOUND WITH CORROSION (FR 25, +10.00", RBL 46). MATERIAL LOSS IS 67%. CORROSION MEASURES: 2.50" L X .650" W X .080" D. CORROSION WAS BEYOND LIMITS, THEREFORE THE SILL BEAM WAS REPLACED PER SRM 51-43-04. P/N:…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 51 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026