N934QQ2006 Embraer ERJ 190-100 IGW
This N-number isn't registered right now. Below is its last known registration, canceled Jun 29, 2023.
Safety record in brief:No NTSB accidents or incidents since 198220 ADs may apply13 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 6, 2021
- Canceled
- Jun 29, 2023
- Airworthiness
- Standard · Transport
- Airworthiness date
- Jun 9, 2023
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
- 19000034
- 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
- ACF5F2
Engine
- Make and model
- Ge Cf34-10e5
- 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- 2021 – 2023Tvpx 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 (CF34-10E5)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 (13)
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.
- Fuselage · skin · damagedApr 11, 2023
DURING THE STRUCTURAL INSPECTION, IT WAS FOUND AN EXISTING REPAIR WITHOUT RECORDS IN THE FUSELAGE SKIN, LOCATED BETWEEN FRAMES 83-84 AND BETWEEN STRINGERS 13L-16L. WAS REPAIRED FOLOWING EMB REPAIR INSTRUCTIONS UNDER ETD2023-190-003976 REV / AND COOPESA EO# COO-EO-2023-17176-R00 AND APPROVED ON…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · skin · crackedApr 11, 2023
DURING THE STRUCTURE INSPECTION, A CRACK WAS FOUND IN THE LH WING LEADING EDGE SKIN BETWEEN RIBS 19 AND 20. THE CRACKED AREA HAS NOT BEEN TRIMMED, HOWEVER, THE FINAL MEASURE AFTER TRIM OUT WILL EXCEED THE MINIMUM ALLOWED IN E190- SRM 57-49-01 REPAIR 51. WAS REPAIRED FOLLOWING EMB REPAIR…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · damagedApr 11, 2023
DURING THE STRUCTURAL INSPECTION, IT WAS FOUND A BLEND OUT EXCEEDED 50 PERCENT OF THE SKIN THICKNESS. ALLIANCE INTENDS TO PERFORM A REPAIR FOLLOWING SRM II 53-22-01 REPAIR 63 GUIDELINES; HOWEVER, THE DAMAGED AREA IS LOCATED IN A NON-ALLOWED REPAIR AREA AS PER PARAGRAPH 3.B. AND FIGURE 204. WAS…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Fuselage · skin · corrodedApr 10, 2023
DURING THE STRUCTURE INSPECTION, THE FUSELAGE SKIN WAS FOUND WITH HEAVY CORROSION AT THE INTERNAL SURFACE BETWEEN FR73 AND X=23146.00 AND AT STRINGER 28L AND 29R, IN ORDER TO REMOVE ALL CORROSION, TWO CUTOUTS AT THE FORWARD SKIN PANEL (190-25004-001) WERE REQUIRED. WAS REPAIRED FOLLOWING REPAIR…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Nacelles and pylons · pylon · corrodedApr 10, 2023
DURING THE ACCOMPLISHMENT OF SB 190-57-0056, WAS FOUND THE LH PYLON, INBOARD AND OUTBOARD SPARS LUGS BUSHING WITH CORROSION. WAS REPAIRED FOLLOWING REPAIR INSTRUCTIONS UNDER EDT2023-190-004140 REV / AND COOPESA EO# COO-EO-2023-17181-R00 AND APPROVED ON ANAC F-200 PROVIDED BY EMB.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Nacelles and pylons · pylon · corrodedApr 10, 2023
DURING THE ACCOMPLISHMENT OF SB 190-57-0056, CUSTOMER FOUND THE RH PYLON, INBOARD AND OUTBOARD SPARS LUGS BUSHING WITH CORROSION. WAS REPAIRED FOLLOWING REPAIR INSTRUCTIONS UNDER ETD2023-190-004146 REV A AND COOPESA EO# COO-EO-2023-17184-R00 AND APPROVED ON ANAC F-200 PROVIDED BY EMB.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · web · corrodedApr 10, 2023
DURING THE STRUCTURAL INSPECTION PROCESS WE FOUND CORROSION AT RH WING, FRONT SPAR AT THE RIB 41 LEADING EDGE AREA. THE LEADING EDGE RIB 41 WAS REMOVED AND ALL THE CORROSION COMMON TO THE FRONT SPAR WEB WAS REMOVED BY BLEND OUT. WAS REPAIRED FOLLOWING EMB REPAIR INSTRUCTIONS UNDER…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · canningApr 10, 2023
DURING THE STRUCTURE INSPECTION, A DENT WITH "CREASE-LIKE DAMAGE" WAS FOUND AT FR2 + 145MM AND BELOW STRINGER 12R ON THE SKIN, BE INFORMED THAT THE DENT WAS RE-CONTOURED AS PER SRM II 53-00-00/AD52 ITEM 5, HOWEVER, OIL CANING IS PRESENT ON THE SKIN. WAS REPAIRED FOLLOWING EMB REPAIR INSTRUCTIONS…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · skin · crackedApr 10, 2023
DURING THE STRUCTURAL INSPECTION, IT WAS FOUND AN CRACK UNDER THE EXISTING REINFORCEMENT LOCATED IN THE LH WING UPPER SKIN AT SPAR II OVER RIB 10.WAS REPAIRED FOLLOWING EMB REPAIR INSTRUCTIONS UNDER ETD2023-190-004421 REV / AND COOPESA EO# COO-EO-2023-17209-R00 AND APPROVED ON ANAC F-200 PROVIDED…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Power plant · inlet · dentedApr 10, 2023
DURING THE STRUCTURAL INSPECTION, WERE FOUND 10 EA. DENTS INLET COWL INNER BARREL PERFORATED SKIN. THE LARGEST DENT MEASURS 2.051" (L) X 0.533" (W) X 0.012" (DEPTH). THE DEEPEST DENT MEASURES 0.445" (L) X 0.328" (W) X 0.017" (DEPTH). DENT CLOSEST TO AFT EDGE IS 3.573" FROM AFT EDGE. WERE REPAIRED…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 13 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