# N989TA: 2011 Embraer ERJ 190-100 IGW, registration cancelled 2023-03-25 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 25, 2023 - 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: 19000482 - Year built: 2011 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 26, 2011 - Certificate issued: October 25, 2011 - Last registry action: March 24, 2023 - Mode S code: ADCE3D - Owner when cancelled: [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N989TA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=989TA - Page: https://openairdocs.org/deregistered/N989TA-2023-03-25 From the FAA registry file of November 5, 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 (25) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR RJEF20190123001](https://openairdocs.org/sdr/RJEF20190123001), Jan 21, 2019: WARNING SYSTEM. FALSE ACTIVATION. 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 MAINTE - [SDR RJEF201812121002](https://openairdocs.org/sdr/RJEF201812121002), Dec 10, 2018: WINDSHIELD. CRACKED. 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 - [SDR EE4Y2017110205082](https://openairdocs.org/sdr/EE4Y2017110205082), Nov 2, 2017: CLEVIS. WORN. THRUST REVERSER PRESSURE RELIEF DOOR HINGE CLEVIS WORN. REPLACED THE DAMAGED CLEVIS. - [SDR EE4Y2017110205085](https://openairdocs.org/sdr/EE4Y2017110205085), Nov 2, 2017: WEB. CRACKED. PAX CABIN SEAT WEB CRACKED OUT OF LIMITS. THE WEB WAS REPLACED. - [SDR EE4Y2017110205086](https://openairdocs.org/sdr/EE4Y2017110205086), Nov 2, 2017: FLOOR SUPPORT. CORRODED. FWD FUSELAGE, PAX CABIN BETWEEN FRAMES 17 AND 20, AT -X49 FLOOR SUPPORT CORRODED. REPLACED. - [SDR EE4Y2017103105048](https://openairdocs.org/sdr/EE4Y2017103105048), Oct 31, 2017: SKIN. CORRODED. 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 - [SDR EE4Y2017103105047](https://openairdocs.org/sdr/EE4Y2017103105047), Oct 31, 2017: SKIN. DENTED. FWD FUSELAGE SKIN WITH SEVERAL DAMAGED (DENTS, EXISTING REWORK, CREASE, BLIND RIVET INSTALLED) IN THE ADJACENT BAY BETWEEN FR9 AND FR11, BETWEEN STR15L AND STR1 - [SDR RJEF20171005001](https://openairdocs.org/sdr/RJEF20171005001), Sep 29, 2017: ACTUATOR. FAULTY. 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 O - [SDR EE4Y2015112500428](https://openairdocs.org/sdr/EE4Y2015112500428), Nov 25, 2015: SHEAR TIE. CORRODED. LOWER FUSELAGE FRAME 86, BETWEEN STR 27R AND STR 28R WITH CORROSION. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER NON ROUTINE ITEM A1D208,1-88. SHEAR TIE WAS REPL - [SDR EE4Y2015112500427](https://openairdocs.org/sdr/EE4Y2015112500427), Nov 25, 2015: SHEAR TIE. CORRODED. LOWER FUSELAGE FRAME 87 SHEAR TIE, BETWEEN STR 27R AND STR 28R CORRODED. SHEAR TIE WAS REPLACED UNDER DWG. - [SDR EE4Y2015112500426](https://openairdocs.org/sdr/EE4Y2015112500426), Nov 25, 2015: SHEAR TIE. CORRODED. LOWER FUSELAGE FRAME 85, BETWEEN STR 27R AND STR 28R WITH CORROSION. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER NON ROUTINE ITEM A1D208,1-89. SHEAR TIE WAS REPL - [SDR EE4Y2015112500425](https://openairdocs.org/sdr/EE4Y2015112500425), Nov 25, 2015: FRAME. CORRODED. LOWER FUSELAGE FR 88, BETWEEN STR 27 AND STR 29 WITH CORROSION. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER NON ROUTINE ITEM A1D208,1-71. FRAME SECTION WAS REPLA - [SDR EE4Y2015112500423](https://openairdocs.org/sdr/EE4Y2015112500423), Nov 25, 2015: SKIN. CRACKED. 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. - [SDR EE4Y2015112400422](https://openairdocs.org/sdr/EE4Y2015112400422), Nov 25, 2015: STRINGER. CORRODED. 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 - [SDR EE4Y2015112400421](https://openairdocs.org/sdr/EE4Y2015112400421), Nov 24, 2015: BEAM. CORRODED. LOWER FUSELAGE FWD CARGO COMPARTMENT DOOR CUTOUT, LOWER BEAM WITH CORROSION. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER NON ROUTINE ITEM A1D208,1-70. REPAIR NAS - [SDR EE4Y2015112400420](https://openairdocs.org/sdr/EE4Y2015112400420), Nov 24, 2015: FINGER DOUBLER. CORRODED. LOWER FUSELAGE AFT CARGO COMPARTMENT, CARGO DOOR CENTER FUSELAGE III, FINGER PLATE WITH CORROSION. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER NON ROUTINE ITEM A - [SDR EE4Y2015112400419](https://openairdocs.org/sdr/EE4Y2015112400419), Nov 24, 2015: SKIN. BULGED. TAIL CONE AT X34707 RT SIDE LOWER SKIN BULGED. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER A NON ROUTINE ITEM A1D208,1-40. REPAIR HAS BEEN ACCOMPLISHED UNDER ETD - [SDR EE4Y2015112400418](https://openairdocs.org/sdr/EE4Y2015112400418), Nov 24, 2015: SKIN. BULGED. TAIL CONE AT X34707 LT SIDE LOWER SKIN BULGED. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER NON ROUTINE ITEM A1D208,1-39. REPAIR HAS BEEN ACCOMPLISHED UNDER ETD20 - [SDR EE4Y2015112400417](https://openairdocs.org/sdr/EE4Y2015112400417), Nov 24, 2015: HOUSING. CORRODED. RT WING L/E TIP LENS ASSY WITH CORROSION. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER A NON ROUTINE ITEM A1D208,6-24. THE REPAIR HAS BEEN ACCOMPLISHED ACCORDING - [SDR EE4Y2015112400416](https://openairdocs.org/sdr/EE4Y2015112400416), Nov 24, 2015: HOUSING. CORRODED. LT WING L/E TIP LENS ASSEMBLY WITH CORROSION. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER NON ROUTINE ITEM A1D208,5-25. THE REPAIR HAS BEEN ACCOMPLISHED ACCORDIN - [SDR EE4Y2015112400415](https://openairdocs.org/sdr/EE4Y2015112400415), Nov 24, 2015: SEAL REST. CORRODED. LOWER FUSELAGE FWD CARGO COMPARTMENT DOOR CUT OUT SECTION LOWER SEAL REST CORRODED HAS BEEN REPORTED AND MANAGED UNDER NON ROUTINE ITEM A1D208,1-51. THE PART WA - [SDR EE4Y2015111700414](https://openairdocs.org/sdr/EE4Y2015111700414), Nov 17, 2015: STRUCTURE. CORRODED. TAIL CONE STATION X34737, LOWER SECTION CHORD WITH CORROSION. DAMAGE HAS BEEN REPORTED & MANAGED UNDER NON-ROUTINE ITEM A1D208 1-53. REPAIR HAS BEEN ACCOMPLISHE - [SDR RJEF20151028001](https://openairdocs.org/sdr/RJEF20151028001), Oct 28, 2015: SENSOR. OUT OF ADJUST. DURING TAXIING, AS FLIGHT TAI-311, THE PILOT REPORTED STEERING FAILURE, SO THE ACFT WAS RETURNED TO THE GATE. IAW FIM 32-53-00-810-817-A, THE STEERING FEEDBACK - [SDR RJEF20150728001](https://openairdocs.org/sdr/RJEF20150728001), Jul 28, 2015: WARNING SYSTEM. FALSE ACTIVATION. PREVIOUS TO DISPATCH OF FLIGHT TA-367, THE PILOT IN COMMAND REPORTED, EICAS MSG, NAV COM 1 WAS FAILED. IT WAS PERFORMED A FAULT ANALYSIS IAW FIM 34-02-01-810-80 - [SDR RJEF20150411001](https://openairdocs.org/sdr/RJEF20150411001), Apr 11, 2015: CIRCUIT CARD. UNSERVICEABLE. DURING FLIGHT TAI 425, THE PILOT REPORTED AMS CTRL FAIL MSG ON EICAS AT FL370. THEREFORE, THE FLIGHT WAS DIVERTED TO ITS ALTERNATE AIRPORT. NO OWL WAS REPORTED. ## 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 20181210023419I](https://openairdocs.org/incident/20181210023419I), Dec 10, 2018: Embraer ERJ 190-100 IGW (N989TA), Houston, TX, Minor damage. The aircraft while in straight and level flight @ approximately FL370 experienced a L-1 wind screen inner pane glass failure for no apparent reason. The… --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.