# Service difficulty reports: N405YX

A list on [N405YX](https://openairdocs.org/aircraft/N405YX.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR R612026F00002](https://openairdocs.org/sdr/R612026F00002.md): Skin · dented · Sep 5, 2026 · N405YX · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > REPAIRED DENT UNDER CA DV WINDOW BY INSTALLING DOUBLER AND FILLER REPAIR ON FUSELAGE SKIN BETWEEN FR10-FR-11 STGR 15L-17L. REF: ETD2025-170-928451 AND EMB SRM 53-10-01/REPAIR 12P AND SRIIM CHAPTER 51
- [SDR R61A2026090500249](https://openairdocs.org/sdr/R61A2026090500249.md): Skin · corroded · Sep 5, 2026 · N405YX · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > AFT CARGO SKIN AT FR 85/86 STRG 23L RIVET HAS CORROSION. PERFORMED PERMANENT REPAIR,STRINGER 23L REPLACEMENT AND SPLICE, AT AFT CARGO SKIN FR 85/86 STRINGER 23L REF. ETD2026-170-014561 AND SRIIM CHAPTER 51.
- [SDR R61A2024082700367](https://openairdocs.org/sdr/R61A2024082700367.md): Windshield · cracked · Aug 24, 2024 · N405YX · Emb ERJ170200LR · Flight Compartment Windows
  > CA WINDSHIELD CRACKED IN FLIGHT AT 27000 FT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R CA WINDSHIELD.
- [SDR R61A2024061700273](https://openairdocs.org/sdr/R61A2024061700273.md): Glowstrip · unsecure · Jun 15, 2024 · N405YX · Emb ERJ170200LR · Emergency Equipment
  > PHOTOLUMINESCENT STRIP DETACHED FROM FLOORING IN FIRST CLASS/GALLEY AREA. RESECURED PHOTOLUMINESCENT STRIP.
- [SDR R61A2024060500247](https://openairdocs.org/sdr/R61A2024060500247.md): Floorbeam · chafed · May 15, 2024 · N405YX · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > WHILE IN HEAVY CHECK - INTERNAL FLOOR STRUCTURE CENTER CROSSBEAM AT FR 78 HAS 2EA SPOTS OF CHAFFING DAMAGE ON BOTTOM EDGE AS SEEN THROUGH AFT CARGO. COMPLIED WITH ETD2024-170-013947 BY FABRICATING AND INSTALLED AN ''L'' ANGLE REPAIR DOUBLER TO CROSSBEAM FRAME
- [SDR R61A2023110200603](https://openairdocs.org/sdr/R61A2023110200603.md): Unknown · unknown · Nov 3, 2023 · N405YX · Emb ERJ170200LR · Emergency Lighting
  > R2 DOOR EMERGENCY LIGHT AND FLIGHT LIGHT INOPERATIVE, REPLACED NUMBER 4 EMERGENCY BATTERY, OPS CHECK GOOD.
- [SDR R61A2021061000480](https://openairdocs.org/sdr/R61A2021061000480.md): Shear Tie · corroded · May 19, 2021 · N405YX · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORRODED SHEAR CLIP AT FR 85, STRINGER 28R. REMOVED AND REPLACED SHEAR CLIP PN 170-66064-001 IAW EMB SRM 51-40-08, 51-40-02, AND 51-23-06.
- [SDR R61A2020120100827](https://openairdocs.org/sdr/R61A2020120100827.md): Power Supply · inoperative · Nov 26, 2020 · N405YX · Emb ERJ170200LR · Emergency Lighting
  > AFT GALLEY EMERGENCY EXIT SIGN FOR CENTER AISLE WILL NOT ILLUMINATE. R & R EMERGENCY LIGHT POWER UNIT NR 3, IAW AMM 33-50-01.
- [SDR R61A2020060500520](https://openairdocs.org/sdr/R61A2020060500520.md): Slide · inoperative · Jun 2, 2020 · N405YX · Emb ERJ170200LR · Escape Slide
  > GIRT BAR STUCK L1. FOUND L1 DOOR EMERGENCY EVACUATION SLIDE TO BE INOP, SEPARATED FROM THE BACKBOARD. R & R L1 DOOR EMERGENCY EVACUATION SLIDE IAW AMM 25-65-01.
- [SDR R61A2020022520255](https://openairdocs.org/sdr/R61A2020022520255.md): Power Supply · inoperative · Feb 22, 2020 · N405YX · Emb ERJ170200LR · Emergency Lighting
  > EMERGENCY LIGHT BATTERY FAULT ON EICAS, SOME EMERGENCY LIGHTS INTERMITTENT ON CEILING AND R2 EXIT. R&R AFT RH INBOARD EMERGENCY LIGHT POWER UNIT IAW AMM 33-50-01.
- [SDR R61A201905250550](https://openairdocs.org/sdr/R61A201905250550.md): Power Unit · inoperative · May 25, 2019 · N405YX · Emb ERJ170200LR · Emergency Lighting
  > COCKPIT EMERGENCY LIGHT DOES NOT ILLUMINATE. R&R EMERGENCY LIGHT POWER UNIT IN FWD RT GALLEY BY R1 PANEL IAW AMM 33-50-01. OPS CHECK GOOD.
- [SDR R61A201901050008](https://openairdocs.org/sdr/R61A201901050008.md): Floorbeam · corroded · Jan 4, 2019 · N405YX · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > CORROSION RT INBD BEAM AT FR 84.
- [SDR R61A201901050007](https://openairdocs.org/sdr/R61A201901050007.md): Beam · corroded · Jan 4, 2019 · N405YX · Emb ERJ170200LR · Fuselage Main, Structure
  > CORROSION AT THE FWD CARGO HORIZONTAL BEAM BETWEEN FR 24-27.
- [SDR R61A201812301263](https://openairdocs.org/sdr/R61A201812301263.md): Beam · corroded · Dec 30, 2018 · N405YX · Emb ERJ170200LR · Fuselage Main, Structure
  > WHILE ACFT IN HEAVY CHECK MAINT FOUND INBD BEAM IS CORRODED BETWEEN FR 86-89,REMOVED AND REPLACED RH INBD BEAM BETWEEN FR 86-89 REF. E175 SRM 51-40-08,RESTORED SURFACE PROTECTION REF SRM 51-23-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.
- [SDR R61A201812301262](https://openairdocs.org/sdr/R61A201812301262.md): Seat Track · corroded · Dec 30, 2018 · N405YX · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > WHILE ACFT IN HEAVY CHECK MAINT FOUND CORROSION FWD WET AREA L.HAND SEAT TRACK BETWEEN FR.19 AND FR.20,REMOVED AND REPLACED WITH NEW FWD WET AREA L.HAND SEAT TRACK PER SRM51-40-08.APPLIED SURFACE PROTECTION FOR FASTENERS. ACFT REMAINS IN HEAVY CHECK UNTIL COMP
- [SDR R61A201812301261](https://openairdocs.org/sdr/R61A201812301261.md): Support · corroded · Dec 30, 2018 · N405YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE ACFT IN HEAVY CHECK MAINT FOUND CORROSION FWD WET AREA FWD R.HAND SILL BETWEEN FR.13 AND FR.14,REMOVED AND REPLACED RH SILLBETWEEN FR.13-14 REF. E175 SRM 51-40-08,RESTORED SURFACE PROTECTION REF SRM 51-23-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.
- [SDR R61A201812301260](https://openairdocs.org/sdr/R61A201812301260.md): Splice · corroded · Dec 30, 2018 · N405YX · Emb ERJ170200LR · Fuselage Main, Structure
  > WHILE ACFT IN HEAVY CHECK FOUND CORROSION_R.HAND I/B SPLICE FR.90,REMOVED AND REPLACED R.HAND I/B BEAM SPLICE REF:SRM 51-21-01, SRM 51-40-08. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.
- [SDR R61A201812301259](https://openairdocs.org/sdr/R61A201812301259.md): Gusset · corroded · Dec 30, 2018 · N405YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE ACFT IN HEAVY CHECK FOUND CORROSION AT RH OB GUSSET AT FR90, REMOVED AND REPLACED RH OB GUSSET AT FR 90 REF. E175 SRM 51-40-08, 51-23-01. RESTORED SURFACE PROTECTION REF SRM 51-23-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.
- [SDR R61A201812301258](https://openairdocs.org/sdr/R61A201812301258.md): Shear Panel · corroded · Dec 30, 2018 · N405YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE ACFT IN HEAVY CHECK FOUND CORROSION CENTER SHEAR PANEL AT FR 87-88 REMOVED AND REPLACED RH SHEAR PANEL REF SRM 51-23-04. APPLIED SURFACE PROTECTION ON RH SHEAR PANEL REF EMB SRM 51-40-08. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION
- [SDR R61A201812301257](https://openairdocs.org/sdr/R61A201812301257.md): Shear Panel · corroded · Dec 30, 2018 · N405YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE ACFT IN HEAVY CHECK FOUND CORROSION AT RH SHEAR PANEL AT FR 87-88. REMOVED AND REPLACED RH SHEAR PANEL REF SRM 51-23-04. APPLIED SURFACE PROTECTION ON RH SHEAR PANEL REF EMB SRM 51-40-08. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.
- [SDR R61A201901020004](https://openairdocs.org/sdr/R61A201901020004.md): Intercostal · corroded · Dec 15, 2018 · N405YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > RT INBD INTERCOSTAL IS CORRODED BETWEEN FR 90-91. BLENDED RT INBD INTERCOSTAL BETWEEN FR 90-91. 0.034" REMAINING ON INTERCOSTAL, 0.036" ON ADJACENT L ANGLE. PER SRM 51-75-16 REMAINING THICKNESS IS GREATER THAN ACCEPTABLE; THEREFORE OUT OF LIMITS. POINT MIC HG3
- [SDR R61A201901020005](https://openairdocs.org/sdr/R61A201901020005.md): Threshold · corroded · Dec 14, 2018 · N405YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > MAJOR REPAIR: CORROSION FOUND, AT FWD AND AFT GIRT BAR FITTINGS, WHILE PERFORMING L1 DOOR LOWER BEAM REWORK. REMOVED CORROSION BY BLENDING AT FWD AND AFT GIRT BAR FITTINGS L1 DOOR LOWER BEAM MATERIAL REMOVED (.085") FOUND TO BE OUT OF LIMITS. REF: SRM 53-10-11
- [SDR R61A201901020003](https://openairdocs.org/sdr/R61A201901020003.md): Doubler · corroded · Dec 14, 2018 · N405YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION INNER DOUBLER ON PANEL 192BL. REMOVED AND REPLACED INNER DOUBLER PN: 170-13414-003 REF SRM 51-40-08. SEE W/O H6577 SN 416 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
- [SDR R61A201901020002](https://openairdocs.org/sdr/R61A201901020002.md): Doubler · corroded · Dec 14, 2018 · N405YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION INNER DOUBLER ON PANEL 192CR. REMOVED AND REPLACED INNER DOUBLER PN: 170-13414-003 REF SRM 51-40-08. SEE W/O H6577 SN 413 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
- [SDR R61A201901020001](https://openairdocs.org/sdr/R61A201901020001.md): Seat Track · corroded · Dec 13, 2018 · N405YX · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION_FWD WET AREA R.HAND SEAT TRACK AT FR.17 HAS SURFACE CORROSION AS MARKED. REMOVED CORROSION BY BLENDING. 100% PERCENT THROUGH DAMAGE, FOUND TO BE OUT OF LIMITS PER SRM 53-10-10/AD01. REMOVED AND INSTALLED NEW FWD RT INBD SEAT TRACK FR13 - FR20. APPLIE
- [SDR R61A201901020006](https://openairdocs.org/sdr/R61A201901020006.md): Finger Doubler · corroded · Dec 12, 2018 · N405YX · Emb ERJ170200LR · Fuselage Main, Structure
  > MAJOR REPAIR: AFT CARGO DOOR HORIZONTAL BEAM STOP FITTING LOCATED AT FR 76-77 HAS SURFACE OXIDATION ON FASTENER AS MARKED WITH RED GREASE PENCIL. BLENDED OUT DAMAGE ON AFT CARGO DOOR FWD FINGER DOUBLER, BLEND AREA: 2.2"L X 0.900"W X -0.025"H, NOMINAL THICKNES
- [SDR R61A2018051870597](https://openairdocs.org/sdr/R61A2018051870597.md): Power Supply · inoperative · May 17, 2018 · N405YX · Emb ERJ170200LR · Emergency Lighting
  > EMERGENCY LIGHT INOPERATIVE AT ROW 12. R & R THE POWER SUPPLY IAW AMM 33-50-01.
- [SDR R61A201704170277](https://openairdocs.org/sdr/R61A201704170277.md): Floor Support · corroded · Apr 10, 2017 · N405YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > FWD CABIN RT FLOOR SUPPORT BETWEEN FRAMES 12 - 14 CORRODED. REMOVED AND REPLACED THE FLOOR SUPORT IAW SRM 51-21-01, 51-41-02, 51-43-04, 51-23-04, 51-23-05, AND 51-23-06.
- [SDR R61A201704170276](https://openairdocs.org/sdr/R61A201704170276.md): Gusset · corroded · Apr 10, 2017 · N405YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > AFT CABIN GUSSET PLATE AT FRAME 90 CORRODED. REMOVED AND REPLACED THE GUSSET, ALODINED AND TOP COATED IAW SRM 51-41-02, 51-23-04, 51-23-06, 51-42-01, AND 51-40-02.
- [SDR R61A201704170275](https://openairdocs.org/sdr/R61A201704170275.md): Shear Panel · corroded · Apr 10, 2017 · N405YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > AFT CABIN RT SHEAR PANEL BETWEEN FRAMES 87- 88. REMOVED AND REPLACED THE SHEAR PANEL, ALODINED AND TOP COATED IAW SRM 51-40-02, 51-23-04, 51-23-05, AND 51-42-01.
- [SDR R61A201701060029](https://openairdocs.org/sdr/R61A201701060029.md): Controller · malfunctioned · Jan 6, 2017 · N405YX · Emb ERJ170200LR · Cabin Pressure Control System
  > CREW RECEIVED A BLEED 2 OVERPRESSURE MESSAGE. NOTED THAT THE CABIN PRESSURE WAS CLIMBING FOLLOWED BY A CABIN ALTITUDE HIGH WARNING MESSAGE. DONNED OXYGEN MASKS AND BEGAN DECENT TO 10000 FEET WHERE CABIN ALTITUDE STABILIZED, BUT THEN BEGAN GOING UP AGAIN. DEC
- [SDR R61A201605230365](https://openairdocs.org/sdr/R61A201605230365.md): Battery Pack · inoperative · May 23, 2016 · N405YX · Emb ERJ170200LR · Emergency Lighting
  > CREW REPORTED THAT THE OVERHEAD CABIN EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE R & R EMERGENCY BATTERY IAW AMM AND OPS CHECKED GOOD.
- [SDR R61A201605210363](https://openairdocs.org/sdr/R61A201605210363.md): Connector · disconnected · May 21, 2016 · N405YX · Emb ERJ170200LR · Emergency Lighting
  > CREW REPORTED THAT THE RAINBOW LIGHTS WERE NOT ALL COMING ON DURING TEST. MAINTENANCE PLACED ON MEL AND LATER FOUND AFT LAV PCB CONNECTOR DISCONNECTED. MAINTENANCE RECONNECTED IAW AMM AND OPS CHECKED GOOD.
- [SDR R61A201605170355](https://openairdocs.org/sdr/R61A201605170355.md): Battery Pack · inoperative · May 17, 2016 · N405YX · Emb ERJ170200LR · Emergency Lighting
  > CREW REPORTED THAT THE EMERGENCY LIGHT OVER ROW 4 WAS INOPERATIVE. MAINTENANCE R & R EMERGENCY BATTERY IAW AMM AND OPS CHECKED GOOD.
- [SDR R61A201506050347](https://openairdocs.org/sdr/R61A201506050347.md): Light · damaged · Jun 5, 2015 · N405YX · Emb ERJ170200LR · Emergency Lighting
  > MAINTENANCE REPORTED THAT THE PHOTOLUMINESCENT STRIP AT ROW 1D WAS DAMAGED. MAINTENANCE R & R PHOTOLUMINESCENT STRIP AT ROW 1D IAW AMM AND OPS CHECKED GOOD.
- [SDR R61A201411241206](https://openairdocs.org/sdr/R61A201411241206.md): Unknown · unknown · Nov 24, 2014 · N405YX · Emb ERJ170200LR · Passenger/Crew Doors
  > CREW REPORTED THAT THE L2 DOOR WAS DIFFICULT TO ARM. MAINTENANCE INSPECTED AND FOUND THE FLEX BALL CABLE IN GOOD SHAPE. MAINTENANCE REPORTS THAT THE ESCAPE SLIDE ARM/DISARM INDICATOR IS NOT COMING INTO VIEW.

## 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 = 'N405YX' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N405YX/reports

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