# Service difficulty reports: N419YX A list on [N419YX](https://openairdocs.org/aircraft/N419YX.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR R61A2024100500456](https://openairdocs.org/sdr/R61A2024100500456.md): Power Supply · no test · Oct 5, 2024 · N419YX · Emb ERJ170200LR · Emergency Lighting > FWD LH EMERGENCY LIGHT POWER UNIT REQUIRES REPLACEMENT. R&R FWD LH EMERGENCY LIGHT POWER SUPPLY UNIT. - [SDR R61A2023021900157](https://openairdocs.org/sdr/R61A2023021900157.md): None · corroded · Feb 7, 2023 · N419YX · Emb ERJ170200LR · Fuselage Main, Floor Beam > WHILE IN HEAVY CHECK - FWD WET AREA RH SIDE OF CROSSBEAM 14 HAS CORROSION. PERFORMED PERMANENT REPAIR ON FWD WET AREA CROSSBEAM 14 RH SIDE. REF EMB SRM 53-00-10/REPAIR03. - [SDR R61A2023011000059](https://openairdocs.org/sdr/R61A2023011000059.md): Fmu · faulted · Jan 5, 2023 · N419YX · Emb ERJ170200LR · Fuel Controlling System > ENGINE 1 SHUTDOWN IN FLIGHT WITH ENG 1 FAIL. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R E1 FADEC AND FMU. - [SDR R61A2021101500801](https://openairdocs.org/sdr/R61A2021101500801.md): Power Unit · inoperative · Oct 14, 2021 · N419YX · Emb ERJ170200LR · Emergency Lighting > EMERGENCY LIGHTS NOT ILLUMINATED ABOVE R2 DOOR. R&R EMERGENCY LIGHT POWER UNIT #4. - [SDR R61A2020022420251](https://openairdocs.org/sdr/R61A2020022420251.md): Seat Track · corroded · Feb 24, 2020 · N419YX · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > WHILE IN HEAVY CHECK- CF 3 CABIN FLOOR STRUCTURE RH INBD LONGITUDINAL SEAT TRACK HAS CORROSION AT FR82. CUT AND REMOVED SECTION OF FLOOR BEAM DUE TO CORROSION OUT OF LIMITS REF SRM 53-23-10/AD01. APPLIED SURFACE PROTECTION TO R/H INBD SEAT TRACK BETWEEN FR 81- - [SDR R61A2020022420250](https://openairdocs.org/sdr/R61A2020022420250.md): Gusset · corroded · Feb 24, 2020 · N419YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure > WHILE IN HEAVY CHECK- CF 3 CABIN FLOOR STRUCTURE CORROSION RH GUSSET AT FR84. REMOVED CORROSION ON CF 3 CABIN FLOOR STRUCTURE RH GUSSET AT FR84 BY BLENDING. REMOVED 0.009" MATERIAL TO REMOVE DAMAGED AREA WHERE MATERIAL WAS REMOVED IS "OUT" OF LIMITS OF SRM REF - [SDR R61A2020022420249](https://openairdocs.org/sdr/R61A2020022420249.md): Web · corroded · Feb 24, 2020 · N419YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure > WHILE IN HEAVY CHECK- CF 3 CABIN FLOOR STRUCTURE CORROSION LH UPPER SHEET AT FR85-86. REMOVED CORROSION ON CF 3 CABIN FLOOR STRUCTURE LH UPPER SHEET AT FR85-86 BY BLENDING. REMOVED 0.008" MATERIAL FROM DAMAGED AREA TO REMOVE DAMAGE. REMAINING MATERIAL MEASURES - [SDR R61A2020022420248](https://openairdocs.org/sdr/R61A2020022420248.md): Web · corroded · Feb 24, 2020 · N419YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure > WHILE IN HEAVY CHECK- CF 3 CABIN FLOOR STRUCTURE CORROSION RH UPPER SHEET AT FR85-86. REMOVED CORROSION ON CF 3 CABIN FLOOR STRUCTURE RH UPPER SHEET AT FR85-86 BY BLENDING. REMOVED 0.008" MATERIAL FROM DAMAGED AREA TO REMOVE DAMAGE. REMAINING MATERIAL MEASURES - [SDR R61A2020022420247](https://openairdocs.org/sdr/R61A2020022420247.md): Floor Support · corroded · Feb 24, 2020 · N419YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure > WHILE IN HEAVY CHECK- CF 3 CABIN FLOOR STRUCTURE CORROSION LH SILL AT FR84. REMOVED CORROSION ON CF 3 CABIN FLOOR STRUCTURE L/H SILL AT FR84 BY BLENDING. REMOVED 0.011" MATERIAL TO REMOVE DAMAGED AREA WHERE MATERIAL WAS REMOVED IS REF: SRM 51-75-16 "OUT" OF LI - [SDR R61A2020022420246](https://openairdocs.org/sdr/R61A2020022420246.md): Seat Track · corroded · Feb 24, 2020 · N419YX · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > WHILE IN HEAVY CHECK- CF 3 CABIN FLOOR STRUCTURE RH INBD LONGITUDINAL SEAT TRACK HAS CORROSION AT FR82. CUT AND REMOVED SECTION OF FLOOR BEAM DUE TO CORROSION OUT OF LIMITS REF. SRM 53-23-10/AD01. INSTALLED NEW R/H I/B SEAT TRACK FROM BETWEEN FRAME 81-82 TO FR - [SDR R61A2020022420245](https://openairdocs.org/sdr/R61A2020022420245.md): Seat Track · corroded · Feb 24, 2020 · N419YX · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > WHILE IN HEAVY CHECK- CF 3 CABIN FLOOR STRUCTURE RH INBD LONGITUDINAL SEAT TRACK HAS CORROSION AND GOUGES FR83. REMOVED AND REPLACED SEAT TRACK PN: 170-86082-003 FROM FR 81 TO FR 84 REF EMB ETD2020-170-005453. - [SDR R61A2020022420244](https://openairdocs.org/sdr/R61A2020022420244.md): Seat Track · corroded · Feb 24, 2020 · N419YX · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > WHILE IN HEAVY CHECK- CF 3 CABIN FLOOR STRUCTURE RH INBD LONGITUDINAL SEAT TRACK HAS CORROSION FWD OF FR84. REMOVED AND REPLACED SEAT TRACK PN: 170-86082-003 FROM FR 81 TO FR 84 REF EMB ETD2020-170-005453. - [SDR R61A2020022420243](https://openairdocs.org/sdr/R61A2020022420243.md): Seat Track · corroded · Feb 24, 2020 · N419YX · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > WHILE IN HEAVY CHECK- LH SEAT TRACK INBD FLANGE HAS CORROSION ON TOP OF FLANGE AT FR 84; Y=(-10.78") REMOVED CORRODED SECTION REF ETD2020-170-005377. FABRICATED 3 EA REPAIR ANGLES REF ETD2020-170-005377. INSTALLED LH INBD SEAT TRACK REPAIR AT FRAME 84 REF ETD2 - [SDR R61A202002240242](https://openairdocs.org/sdr/R61A202002240242.md): Crossbeam · corroded · Feb 24, 2020 · N419YX · Emb ERJ170200LR · Fuselage Main, Structure > WHILE IN HEAVY CHECK- FLOOR STRUCTURE FR 84 CROSSBEAM HAS CORROSION ON TOP OF CROSSBEAM ADJACENT TO LH SEAT TRACK INBD FLANGE; Y=(-10.78"). CUT AND REMOVED 2 SECTIONS OF TOP OF CROSSBEAM ADJACENT TO LH SEAT TRACK AT FR84 DUE TO CORROSION OUT OF LIMITS REF. SRM - [SDR R61A202003050353](https://openairdocs.org/sdr/R61A202003050353.md): Spar · cracked · Feb 21, 2020 · N419YX · Emb ERJ170200LR · Wing Spar > WHILE IN HEAVY CHECK RH WINGTIP SPAR 1 HAS CRACK AT LOWER SIDE OF SPAR VERIFY BY NDT REMOVED AND REPLACED SPAR 1 EXTENSION. REF E175 SRM 51-40-08. - [SDR R61A202003020313](https://openairdocs.org/sdr/R61A202003020313.md): Attach Angle · corroded · Feb 19, 2020 · N419YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure > WHILE IN HEAVY CHECK FOUND BURST PANEL 1431DL HAS CORROSION ON 2EA LOWER ATTACH ANGLES REMOVED AND REPLACED ANGLES ONTO PANEL 1431DL. REF EMB SRM 51-40-02, 51-40-08, 51-45-00 AND EMB AMM 20-10-01/200 RESTORED FINISH REF. SRM 51-23-04, 51-23-05. - [SDR R61A202003020314](https://openairdocs.org/sdr/R61A202003020314.md): Attach Angle · corroded · Feb 12, 2020 · N419YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure > WHILE IN HEAVY CHECK FOUND BURST PANEL 1441FR HAS CORROSION ON 2EA LOWER ATTACH ANGLES REMOVED AND REPLACED LOWER ATTACH ANGLES AT PANEL 1441FR REF EMB SRM 51-40-08. - [SDR R61A2019120641353](https://openairdocs.org/sdr/R61A2019120641353.md): Light · worn · Dec 4, 2019 · N419YX · Emb ERJ170200LR · Emergency Lighting > PHOTOLUMINESCENT STRIP WORN IN FRONT OF FWD WARDROBE. R&R PHOTOLUMINESCENT STRIPS PER AMM 33-50-21. - [SDR R61A201901170065](https://openairdocs.org/sdr/R61A201901170065.md): Track · obstructed · Jan 17, 2019 · N419YX · Emb ERJ170200LR · Passenger/Crew Doors > MAIN CABIN DOOR DIFFICULT TO OPEN. CLEANED L1 DOOR TRACKS. C/W OPS CHECK PER AMM 52-11-00. NO DEFECTS NOTED. - [SDR R61A2018103061100](https://openairdocs.org/sdr/R61A2018103061100.md): Pressure Switch · defective · Oct 26, 2018 · N419YX · Emb ERJ170200LR · Landing Gear Brake System > PARKING BRAKE NOT RELEASED EICAS MESSAGE KEPT POPULATING EN ROUTE. QRH PROCEDURE WAS ACCOMPLISHED, MESSAGE CONTINUED TO POPULATE AND GO AWAY. DECLARED EMERGENCY, RETURNED TO FIELD, LANDED WITHOUT INCIDENT. R&R EMERGENCY BRAKE PRESSURE SWITCH SYSTEM 1 IAW AMM 3 - [SDR R61A2018090760926](https://openairdocs.org/sdr/R61A2018090760926.md): Door · lack of lube · Sep 6, 2018 · N419YX · Emb ERJ170200LR · Passenger/Crew Doors > MAIN CABIN DOOR L1 DIFFICULT TO OPEN FROM OUTSIDE. REMOVED FOD AND LUBRICATED DOOR IAW AMM 52-10-03. - [SDR R61A201806080711](https://openairdocs.org/sdr/R61A201806080711.md): Floor Support · corroded · Jun 8, 2018 · N419YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure > WHILE AIRCRAFT WAS IN FOR HEAVY MAINTENANCE VISIT, MAINT FOUND FWD FUSELAGE FLOOR FR19 LT OUTBOARD WINDSCREEN MOUNT CORRODED BEYOND ALLOWABLE LIMITS. LOCATED, DRILLED, AND INSTALLED NEW WINDSCREEN MOUNT IAW SRM 51-40-02, 51-40-03, AND 51-43-03. - [SDR R61A201806080710](https://openairdocs.org/sdr/R61A201806080710.md): Seat Track · corroded · Jun 8, 2018 · N419YX · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > WHILE AIRCRAFT WAS IN FOR HEAVY MAINTENANCE VISIT, LT SEAT TRACK HAS CORROSION BETWEEN FR19-FR20 ON VERY FWD END OF CROWN TEETH AREA. REPAIRED LT INBOARD SEAT TRACK PER ETD2018-170-065116. - [SDR R61A201806080709](https://openairdocs.org/sdr/R61A201806080709.md): Door Sill · corroded · Jun 8, 2018 · N419YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure > WHILE AIRCRAFT WAS IN FOR HEAVY MAINTENANCE VISIT, FOUND FWD WET AREA RT WEB AT FR12-FR14 HAS CORROSION. REMOVED AND INSTALLED NEW FLOOR SILL IAW SRM 51-41-02 AND 51-43-04. - [SDR R61A201806080714](https://openairdocs.org/sdr/R61A201806080714.md): Floor Support · corroded · Jun 8, 2018 · N419YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure > AFT WINDSCREEN I/B FLOOR MOUNT CORRODED. REMOVED AND REPLACED FLOOR MOUNT. - [SDR R61A201806080713](https://openairdocs.org/sdr/R61A201806080713.md): Shear Panel · corroded · Jun 8, 2018 · N419YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure > CENTER SHEAR PANEL CORRODED. REMOVED AND REPLACED SHEER PANEL. - [SDR R61A201806080708](https://openairdocs.org/sdr/R61A201806080708.md): Web · corroded · Jun 8, 2018 · N419YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure > WHILE AIRCRAFT WAS IN FOR HEAVY MAINTENANCE VISIT, MAINTENANCE FOUND FWD WET AREA LT WEB AT FR16 INBOARD LAV MOUNT HOLE CORRODED BEYOND ALLOWABLE LIMITS. REMOVED, LOCATED, DRILLED, AND INSTALLED NEW WEB IAW SRM 51-40-02, 51-40-03, AND 51-41-02. - [SDR R61A201806080712](https://openairdocs.org/sdr/R61A201806080712.md): Shear Panel · corroded · Jun 8, 2018 · N419YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure > SHEAR PANEL CORRODED. REMOVED AND REPLACED SHEER PANEL. - [SDR R61A201806010624](https://openairdocs.org/sdr/R61A201806010624.md): Rod End · out of adjust · May 31, 2018 · N419YX · Emb ERJ170200LR · Passenger/Crew Doors > L1 DOOR DIFFICULT TO OPEN AND CLOSE. ADJUSTED L1 DOOR LOWER HOIST BELLCRANK ROD ENDS IAW AMM 52-11-00. - [SDR R61A201712160979](https://openairdocs.org/sdr/R61A201712160979.md): Diaphragm · leaking · Dec 16, 2017 · N419YX · Emb ERJ170200LR · Passenger/Crew Doors > L1 DOOR ASSIST DIAPHRAGM APPEARS TO BE LEAKING. R&R L1 DOOR OPEN ASSIST DIAPHRAGM IAW AMM 52-11-51. - [SDR R61A201708210633](https://openairdocs.org/sdr/R61A201708210633.md): Handle · dirty · Aug 21, 2017 · N419YX · Emb ERJ170200LR · Passenger/Crew Doors > L1 DOOR DIFFICULT TO OPEN FROM OUTSIDE. CLEANED DEBRIS FROM DOOR OUTSIDE HANDLE AND OPS CHECK GOOD IAW AMM 52-11-52. - [SDR R61A201707160535](https://openairdocs.org/sdr/R61A201707160535.md): Door · out of adjust · Jul 16, 2017 · N419YX · Emb ERJ170200LR · Passenger/Crew Doors > MAIN CABIN DOOR IS DIFFICULT TO CLOSE. IT APPEARED TO NOT BE LINING UP CORRECTLY. ADJUSTED MAIN CABIN DOOR CLOSING ACTION IAW AMM 52-11-00-500. L1 DOOR OPS CHECKS OK. - [SDR R61A201607180417](https://openairdocs.org/sdr/R61A201607180417.md): Indicator · inoperative · Jul 18, 2016 · N419YX · Emb ERJ170200LR · Door Warning System > CREW REPORTED THAT THE L1 DOOR LATCHED INDICATOR WAS INOPERATIVE. REMOVED AND REPLACED POSITION INDICATOR IAW AMM AND OPS CHECKED GOOD. - [SDR R61A201606070386](https://openairdocs.org/sdr/R61A201606070386.md): Valve · faulted · Jun 7, 2016 · N419YX · Emb ERJ170200LR · Pneumatic Distribution System > THE CREW REPORTED THAT THEY RECEIVED BLEED 1 AND BLEED 2 OVERPRESSURE MESSAGES AFTER TAKEOFF. THE CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. AFTER LANDING, A BLEED 1 FAIL MESSAGE WAS ALSO REPORTED. MAINTENANCE REPLACED THE ENGINE 1 NAPRSOV. OPS CH - [SDR R61A201602040083](https://openairdocs.org/sdr/R61A201602040083.md): Actuator · inoperative · Feb 4, 2016 · N419YX · Emb ERJ170200LR · Landing Gear Retraction/Extension System > CREW REPORTED THAT THE RT MAIN GEAR FAILED TO RETRACT. CREW RAN QRH, DECLARED AN EMERGENCY AND WITH EMERGENCY VEHICLES ROLLING, LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R RT MLG DOWNLOCK RELASE ACTUATOR AND LANDING GEAR SELECT VALVE, PERFORMED S - [SDR R61A201510270764](https://openairdocs.org/sdr/R61A201510270764.md): Warning Message · illuminated · Oct 27, 2015 · N419YX · Emb ERJ170200LR · Landing Gear Brake System > CREW REPORTED LT AND RT BRAKE FAIL AND BRAKE CONTROL FAULT. MAINTENANCE PERFORMED SNL 170-32-0025 AND POWER RESET IAW AMM AND MESSAGES CLEARED. ACFT IS GOOD FOR SERVICE. - [SDR R61A201408211007](https://openairdocs.org/sdr/R61A201408211007.md): Skin · dented · Aug 21, 2014 · N419YX · Emb ERJ170200LR · Fuselage Main, Plate/Skin > DENT ON AFT OF REAR CARGO. REPAIRED IAW ETD2014-170-069017. ACFT RETURNED TO SERVICE. ## 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 = 'N419YX' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N419YX/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.