# Service difficulty reports: N989TA, cancelled Mar 25, 2023 A list on [N989TA, cancelled Mar 25, 2023](https://openairdocs.org/deregistered/N989TA-2023-03-25.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR RJEF20190123001](https://openairdocs.org/sdr/RJEF20190123001.md): Warning System · false activation · Jan 21, 2019 · N989TA · Emb ERJ190100IGW · Air Distribution System > 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 - [SDR RJEF201812121002](https://openairdocs.org/sdr/RJEF201812121002.md): Windshield · cracked · Dec 10, 2018 · N989TA · Emb ERJ190100IGW · Flight Compartment Windows > 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"; - [SDR EE4Y2017110205082](https://openairdocs.org/sdr/EE4Y2017110205082.md): Clevis · worn · Nov 2, 2017 · N989TA · Emb ERJ190100IGW · Engine Thrust Reverser > THRUST REVERSER PRESSURE RELIEF DOOR HINGE CLEVIS WORN. REPLACED THE DAMAGED CLEVIS. - [SDR EE4Y2017110205085](https://openairdocs.org/sdr/EE4Y2017110205085.md): Web · cracked · Nov 2, 2017 · N989TA · Emb ERJ190100IGW · Passenger Compartment Equipment > PAX CABIN SEAT WEB CRACKED OUT OF LIMITS. THE WEB WAS REPLACED. - [SDR EE4Y2017110205086](https://openairdocs.org/sdr/EE4Y2017110205086.md): Floor Support · corroded · Nov 2, 2017 · N989TA · Emb ERJ190100IGW · Fuselage Miscellaneous Structure > FWD FUSELAGE, PAX CABIN BETWEEN FRAMES 17 AND 20, AT -X49 FLOOR SUPPORT CORRODED. REPLACED. - [SDR EE4Y2017103105048](https://openairdocs.org/sdr/EE4Y2017103105048.md): Skin · corroded · Oct 31, 2017 · N989TA · Emb ERJ190100IGW · Wing, Plate/Skin > 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. - [SDR EE4Y2017103105047](https://openairdocs.org/sdr/EE4Y2017103105047.md): Skin · dented · Oct 31, 2017 · N989TA · Emb ERJ190100IGW · Fuselage Main, Plate/Skin > 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. - [SDR RJEF20171005001](https://openairdocs.org/sdr/RJEF20171005001.md): Actuator · faulty · Sep 29, 2017 · N989TA · Emb ERJ190100IGW · Leading Edge Slat Position Indicating System > 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 - [SDR EE4Y2015112500428](https://openairdocs.org/sdr/EE4Y2015112500428.md): Shear Tie · corroded · Nov 25, 2015 · N989TA · Emb ERJ190100IGW · Fuselage Internal Mounting Structure > 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 REPLACED UNDER DWG, PN 170-65180-447, INSTRUCTIONS. - [SDR EE4Y2015112500427](https://openairdocs.org/sdr/EE4Y2015112500427.md): Shear Tie · corroded · Nov 25, 2015 · N989TA · Emb ERJ190100IGW · Fuselage Internal Mounting Structure > 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.md): Shear Tie · corroded · Nov 25, 2015 · N989TA · Emb ERJ190100IGW · Fuselage Internal Mounting Structure > 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 REPLACED UNDER DWG, PN 170-65180-447, INSTRUCTIONS. - [SDR EE4Y2015112500425](https://openairdocs.org/sdr/EE4Y2015112500425.md): Frame · corroded · Nov 25, 2015 · N989TA · Emb ERJ190100IGW · Fuselage Main, Frame > 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 REPLACED UNDER DWG INSTRUCTIONS. - [SDR EE4Y2015112500423](https://openairdocs.org/sdr/EE4Y2015112500423.md): Skin · cracked · Nov 25, 2015 · N989TA · Emb ERJ190100IGW · Nacelle/Pylon, Plate/Skin > 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.md): Stringer · corroded · Nov 25, 2015 · N989TA · Emb ERJ190100IGW · Fuselage Main, Longeron/Stringer > 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. - [SDR EE4Y2015112400421](https://openairdocs.org/sdr/EE4Y2015112400421.md): Beam · corroded · Nov 24, 2015 · N989TA · Emb ERJ190100IGW · Fuselage Main, Structure > 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 BEEN ACCOMPLISHED UNDER ETD2015-190-104303,INSTRUCTIONS AND APPROVED. - [SDR EE4Y2015112400420](https://openairdocs.org/sdr/EE4Y2015112400420.md): Finger Doubler · corroded · Nov 24, 2015 · N989TA · Emb ERJ190100IGW · Fuselage Main, Structure > LOWER FUSELAGE AFT CARGO COMPARTMENT, CARGO DOOR CENTER FUSELAGE III, FINGER PLATE WITH CORROSION. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER NON ROUTINE ITEM A1D208,1-69. REPAIR NAS BEEN ACCOMPLISHED UNDER ETD2015-190-104335, INSTRUCTIONS AND APPROVED. - [SDR EE4Y2015112400419](https://openairdocs.org/sdr/EE4Y2015112400419.md): Skin · bulged · Nov 24, 2015 · N989TA · Emb ERJ190100IGW · Fuselage Main, Plate/Skin > 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 ETD2015-190-103976, INSTRUCTIONS AND APPROVED. - [SDR EE4Y2015112400418](https://openairdocs.org/sdr/EE4Y2015112400418.md): Skin · bulged · Nov 24, 2015 · N989TA · Emb ERJ190100IGW · Fuselage Main, Plate/Skin > 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 ETD2015-190-103976, INSTRUCTIONS AND APPROVED. - [SDR EE4Y2015112400417](https://openairdocs.org/sdr/EE4Y2015112400417.md): Housing · corroded · Nov 24, 2015 · N989TA · Emb ERJ190100IGW · Exterior Lighting > 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 TO CMM 33-42-77, INSTRUCTIONS AND APPROVED. - [SDR EE4Y2015112400416](https://openairdocs.org/sdr/EE4Y2015112400416.md): Housing · corroded · Nov 24, 2015 · N989TA · Emb ERJ190100IGW · Exterior Lighting > 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 ACCORDING CMM 33-42-77, INSTRUCTIONS AND APPROVED. - [SDR EE4Y2015112400415](https://openairdocs.org/sdr/EE4Y2015112400415.md): Seal Rest · corroded · Nov 24, 2015 · N989TA · Emb ERJ190100IGW · Cargo/Baggage Doors > 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 WAS REPLACED. - [SDR EE4Y2015111700414](https://openairdocs.org/sdr/EE4Y2015111700414.md): Structure · corroded · Nov 17, 2015 · N989TA · Emb ERJ190100IGW · Aerodynamic Fairings > TAIL CONE STATION X34737, LOWER SECTION CHORD WITH CORROSION. DAMAGE HAS BEEN REPORTED & MANAGED UNDER NON-ROUTINE ITEM A1D208 1-53. REPAIR HAS BEEN ACCOMPLISHED UNDER ETD2015-190-103992, INSTRUCTIONS & APPROVED. - [SDR RJEF20151028001](https://openairdocs.org/sdr/RJEF20151028001.md): Sensor · out of adjust · Oct 28, 2015 · N989TA · Emb ERJ190100IGW · Landing Gear Steering System > 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 SENSORS WERE ADJUSTED & FUNCTIONAL TEST PERFORMED IAW AMM 32-53-09 500 WITH NO EICAS FAILURE MSGS. - [SDR RJEF20150728001](https://openairdocs.org/sdr/RJEF20150728001.md): Warning System · false activation · Jul 28, 2015 · N989TA · Emb ERJ190100IGW · Navigation System > 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 34-02-01-810-804-A & REPLACED THE NIM 1 IAW AMM 34-02-000-801-A34-02-400-801-A. PERFORMED OPERATIONAL TEST WITH N - [SDR RJEF20150411001](https://openairdocs.org/sdr/RJEF20150411001.md): Circuit Card · unserviceable · Apr 11, 2015 · N989TA · Emb ERJ190100IGW · Cabin Pressure Control System > 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. REPLACED THE AMS CONTROLLER CHA 1 & CHA 2 IAW FIM 21-00-00-810-805-A & AMM 21-00-01-000 400-801- ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N989TA' AND deregistration_id = 'N989TA-2023-03-25' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N989TA-2023-03-25/reports --- 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.