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Aircraft record

N989TA2011 Embraer ERJ 190-100 IGW

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Mar 25, 2023.

Safety record in brief:No NTSB accidents or incidents since 198220 ADs may apply25 service difficulty reports

Registration
Deregistered
Last based in
Salt Lake City, UT
owner city / state
Owners
1
since 2011
NTSB events
None
since 1982
ADs may apply
20
confirm with A&P
Service reports
25
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Wells Fargo Trust Co NA Trustee
Owner type
Corporation
City, state
Salt Lake City, UT
Certificate issued
Oct 25, 2011
Canceled
Mar 25, 2023
Airworthiness
Standard · Transport
Airworthiness date
Oct 26, 2011

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 data

Airframe

Manufacturer
Embraer
Model
ERJ 190-100 IGW
Year
2011
Serial number
19000482
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
ADCE3D

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
  1. 2011 – 2023Wells Fargo Trust Co NA TrusteeSalt Lake City, UT

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs 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.

ADSubjectEffectiveApplies to
2023-21-11Embraer S.A. (Type Certificate Previously Held by Yaborã Indústria Aeronáutica S.A.…Dec 26, 2023Airframe (ERJ 190-100 IGW)
2022-16-01WindowsAug 15, 2022Airframe (ERJ 190-100 IGW)Only with: Equipped with any NORDAM passenger window having PMA P/N NP00038-3.
2022-05-08Turbine Engine Oil SystemApr 11, 2022Engine (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.
2021-25-02Nacelles/ pylonsJan 20, 2022Airframe (ERJ 190-100 IGW)
2020-25-08Flight controlsJan 21, 2021Airframe (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 ADs
ADSubjectEffectiveApplies to
2020-12-12Nacelles/ pylonsAug 13, 2020Airframe (ERJ 190-100 IGW)
2020-05-21Indicating/ recording systemsApr 24, 2020Airframe (ERJ 190-100 IGW)Serial numbers per ANAC Brazilian AD 2019-10-01
2019-24-16Embraer S.A. AirplanesFeb 3, 2020Airframe (ERJ 190-100 IGW)Certain serial numbers: 19000002; 19000004; 19000006–19000213; 19000215–19000276; 19000278–19000466; 19000468–19000525; …
2019-19-03FuselageOct 31, 2019Airframe (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
2019-03-21Landing GearApr 2, 2019Airframe (ERJ 190-100 IGW)
2017-21-09FuselageNov 27, 2017Airframe (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)
2016-12-14PneumaticJul 27, 2016Airframe (ERJ 190-100 IGW)
2013-25-04Embraer S.A. AirplanesFeb 10, 2014Airframe (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.
2013-16-22FuselageSep 27, 2013Airframe (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
2013-11-17PneumaticAug 6, 2013Airframe (ERJ 190-100 IGW)Only with: Having Hamilton Sundstrand low pressure check valve (LPCV) P/N 1001447-3 or 1001447-4 installed.
2013-11-07Landing gearJul 9, 2013Airframe (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
2013-05-12Fire ProtectionMay 3, 2013Airframe (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
2013-03-13DoorsMar 19, 2013Airframe (ERJ 190-100 IGW)Serial numbers per EMBRAER Service Bulletins 170-52-0055 Rev 01, 190-52-0038 Rev 01, and 190LIN-52-0020
2012-16-09Air ConditioningSep 21, 2012Airframe (ERJ 190-100 IGW)
2012-15-03Landing GearSep 4, 2012Airframe (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 (25)

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.

  • Air conditioning and pressurization · warning system · false activationJan 21, 2019

    DURING PUSHBACK OF FLIGHT TAI367 FROM IAH TO SAL, THE AIRCRAFT HAD EICAS FAILURE MESSAGE OF RAM AIR VALVE FAULT, DUE THAT REASON RETURNED TO THE GATE FOR MAINTENANCE. MAINTENANCE PERSONNEL PERFORMED FAULT ANALYSIS AND RESET THE SYSTEM IN ACCORDANCE WITH FIM 21-25-00-810-804-A SUB TASK 810-813-A…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Windows · windshield · crackedDec 10, 2018

    DURING CRUISE OF FLIGHT TA441 FROM DFW TO SAL THE LH WINDSHIELD PRESENTED CRACKING, DUE THAT SITUATION THE AIRCRAFT DIVERTED TO IAH. AFTER AN UNEVENTFUL LANDING THE PILOT REPORTED THE FOLLOWING TWO ITEMS: 1) "LEFT WINDSHIELD CRACKED DURING CRUISE LEVEL FL370"; 2) "NO OVERWEIGHT DURING LANDING, MAX…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Exhaust · clevis · wornNov 2, 2017

    THRUST REVERSER PRESSURE RELIEF DOOR HINGE CLEVIS WORN. REPLACED THE DAMAGED CLEVIS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Equipment and furnishings · web · crackedNov 2, 2017

    PAX CABIN SEAT WEB CRACKED OUT OF LIMITS. THE WEB WAS REPLACED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · floor support · corrodedNov 2, 2017

    FWD FUSELAGE, PAX CABIN BETWEEN FRAMES 17 AND 20, AT -X49 FLOOR SUPPORT CORRODED. REPLACED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · dentedOct 31, 2017

    FWD FUSELAGE SKIN WITH SEVERAL DAMAGED (DENTS, EXISTING REWORK, CREASE, BLIND RIVET INSTALLED) IN THE ADJACENT BAY BETWEEN FR9 AND FR11, BETWEEN STR15L AND STR19L. THE CORRECTIVE ACTION WAS HANDLE UNDER THE OEM DISPOSITION ETD2017-190-089131.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · skin · corrodedOct 31, 2017

    RT WING UPPER SKIN T/E AREA BETWEEN RIB 11 AND RIB 20 SKIN WITH CORROSION AND THERE IS NOT ALLOWABLE DAMAGE TO EVALUATE THE DAMAGED AREA. THE CORRECTIVE ACTION WAS HANDLE UNDER THE OEM DISPOSITION ETD2017-190-091058.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · actuator · faultySep 29, 2017

    AFTER TAKE OFF, THE SLAT FAILED TO RETRACT, RETURNED TO DEPARTURE. AFTER AN UNEVENTFUL LANDING THE PILOT REPORTED THE SLAT FAILED DURING RETRACTION AFTER TAKE OFF. MAINTENANCE PERFORMED FAULT ANALYSIS IAW FIM 27-81-00-810-805-A, FOUND ONE ATTACHMENT BOLT OF THE SKEW SENSOR OF THE OUTBOARD SLAT…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · stringer · corrodedNov 25, 2015

    LOWER FUSELAGE AFT CARGO COMPARTMENT,STR 27 RT, BETWEEN FRAME 87 AND FRAME 88 WITH CORROSION. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER NON ROUTINE ITEM A1D208,1-83. REPAIR NAS BEEN ACCOMPLISHED UNDER ETD2015-190-105185 REV A, INSTRUCTIONS AND APPROVED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Nacelles and pylons · skin · crackedNov 25, 2015

    NR 2 ENGINE PYLON FWD PANEL SKIN WITH CRACKS. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER NON-ROUTINE ITEM A1D208,4-56. THE PART WAS REPLACED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Showing the 10 most recent of 25 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

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