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Aircraft record

N985TA2009 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 Aug 23, 2016.

Safety record in brief:No NTSB accidents or incidents since 198220 ADs may apply10 service difficulty reports

Registration
Deregistered
Last based in
Salt Lake City, UT
owner city / state
Owners
1
since 2009
NTSB events
None
since 1982
ADs may apply
20
confirm with A&P
Service reports
10
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Wells Fargo Bank Northwest NA Trustee
Owner type
Corporation
City, state
Salt Lake City, UT
Certificate issued
Dec 4, 2009
Canceled
Aug 23, 2016
Airworthiness
Standard · Transport
Airworthiness date
Dec 7, 2009

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
2009
Serial number
19000287
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
ADBF61

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. 2009 – 2016Wells Fargo Bank Northwest 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 (10)

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 · support · crackedDec 17, 2015

    NOSE WW SUPPORT ASSEMBLY WITH CRACK. DAMAGE HAS BEEN REPORTED & MANAGED UNDER NON-ROUTINE ITEM A1D207 1 - 55. THE SUPPORT WAS REPLACED UNDER ETD 2015-190-114292, INSTRUCTIONS & APPROVED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · stringer · corrodedDec 15, 2015

    LOWER FUSELAGE AFT CARGO COMPARTMENT, STRINGER 29R CORRODED, BETWEEN FRAME 76 & FRAME 81. DAMAGE HAS BEEN REPORTED & MANAGED UNDER NON-ROUTINE ITEM A1D207 1-33.CORRECTIVE ACTION: REPAIR HAS BEEN ACCOMPLISHED UNDER ETD2015-190-2015-112854, INSTRUCTIONS & APPROVED/. .

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · doubler · corrodedDec 15, 2015

    CENTER FUSELAGE III, AFT CARGO COMPARTMENT FROM FRAME 80 TO 81, BETWEEN STRINGER 27R & 28R, INTERNAL DOUBLER WITH CORROSION. DAMAGE HAS BEEN REPORTED & MANAGED UNDER NON-ROUTINE ITEM A1D207 1-32. REPAIR HAS BEEN ACCOMPLISHED UNDER ETD2015-190.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Wings · skin · crackedDec 15, 2015

    RT WING CRACK LE EDGE UPPER SKIN AT RIB 14. DAMAGE HAS BEEN REPORTED & MANAGED UNDER NON-ROUTINE ITEM A1D207, 6 - 15. REPAIR HAS BEEN ACCOMPLISHED UNDER ETD 2015-190-113543, INSTRUCTIONS & APPROVED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · doubler · corrodedDec 15, 2015

    CENTER FUSELAGE III, AFT CARGO COMPARTMENT FROM FRAME 77 - 78, BETWEEN STRINGER 28R & 29R, INTERNAL DOUBLER WITH CORROSION. DAMAGE HAS BEEN REPORTED & MANAGED UNDER NON-ROUTINE ITEM A1D207 1-31. REPAIR HAS BEEN ACCOMPLISHED UNDER ETD2015-112027, INSTRUCTIONS & APPROVED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Power plant · module · damagedNov 22, 2015

    AFTER ARRIVAL, THE PILOT REPORTED BIRD STRIKE ON ENGINE 2 NACELLE. IT WAS PERFORMED INSPECTION AFTER BIRD STRIKE IAW AMM 05-50-02-200-801-A, FOUND A DENT OUT OF LIMITS FOR ACFT OPERATION ON THE AIR INLET MODULE 2, THE AIR INLET MODULE WAS REPLACED IAW AMM 71-61-00/400, PERFORMED ENGINE RUN UP IAW…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Electrical power · gcu · inoperativeMay 13, 2015

    AFTER LANDING AS FLIGHT TAI 536, THE PILOT REPORTED DC BUS 2 OFF DUE TO TR 2 FAILURE. IAW FIM 24-31-00-810-806-A & AMM 24-21-19-000 400-801-A THE GCU NR 2 WAS REPLACED. THE APPLICABLE OPERATIONAL TEST PERFORMED WITH NO FAILURE MSGS. ONCE THE CORRECTIVE MX ACTIONS WERE COMPLETED, THE ACFT WAS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine air · line · leakingJun 27, 2014

    DURING CLIMB, PILOT REPORTED NR 2 BLEED OSCILLATING DURING CLIMB +/-30 PSI. RETURNED & PERFORMED AN UNEVENTFUL LANDING. PERFORMED FAULT ANALYSIS IAW FIM 36-14-00-810-811-A, LEAK TESTED THE SERVO LINES OF THE RT TORQUE MOTOR CONTROLLER IAW AMM 36-11-06-790-801-A. FOUND A LEAK ON THE RT NAPRSOV…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine · engine · vibrationDec 4, 2012

    DURING CLIMB OF THE AIRCRAFT AS FLIGHT TP-831 FROM LIM TO CUZ, THE PILOT IN COMMAND REPORTED: "ENGINE NR 1 ABNORMAL VIBRATION 4.2 LP WITH SOUND DURING CLIMB", THEREFORE, THE AIRCRAFT WAS RETURNED TO LIM AIRPORT (ATB). ADDITIONAL THE PILOT REPORTED: "LANDING WEIGHT 39200 KGS AND VERTICAL SPEED 100…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · actuator · malfunctionedOct 24, 2012

    DURING FLIGHT, PILOT REPORTED "SLATS FAILURE"; AIRCRAFT RETURNED TO AIRPORT AND LANDED WITH 45,000 KGS OVERWEIGHT AND 300 FPM SINK RATE. ONCE THE AIRCRAFT WAS POSITIONED AT THE MAINTENANCE RAMP, FIM 27-83-00-810-818-A AND FIM 27-81-00-810-805-A WAS PERFORMED AND FOUND LEFT SLAT ACTUATOR NR 7…

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

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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