# Service difficulty reports: N422YX

A list on [N422YX](https://openairdocs.org/aircraft/N422YX.md).

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

- [SDR R61A2025013100006](https://openairdocs.org/sdr/R61A2025013100006.md): Elec Connector · inoperative · Jan 31, 2025 · N422YX · Emb ERJ170200LR · Light System Wiring
  > EMERGENCY LIGHT AT ROW 9 INOP. REINSTALLED CANNON PLUG ON EMERGENCY PANEL LIGHT.
- [SDR R61A2023051700290](https://openairdocs.org/sdr/R61A2023051700290.md): Spar · damaged · Apr 24, 2023 · N422YX · Emb ERJ170200LR · Fuselage Main, Structure
  > REMOVE AND REPLACE LH NLG SPAR 170-04033-005 FRDUE TO DAMAGED HOLES. REMOVED AND REPLACED LH NLG LOWER SPAR PER SM 51-40-08.
- [SDR R61A2023051700288](https://openairdocs.org/sdr/R61A2023051700288.md): Stringer · damaged · Apr 24, 2023 · N422YX · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > REPAIR ELONGAED HLE IN STRINGER 24R 170-03909-001 AT FR 15 PER ETD 2023-170-009823. REPAIRED ELONGAED HOLE IN STRINGER 24R 170-03909-001 AT FR 15 PER ETD 2023-170-009823 REV B
- [SDR R61A2023051600287](https://openairdocs.org/sdr/R61A2023051600287.md): Stringer · damaged · Apr 24, 2023 · N422YX · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > "REMOVE AND REPLACE STRINGER 20R FR 12-20 DUE TO DAMAGED HOLES.: REMOVED AND REPLACED STRINGER 20R FR 12-20 DUE TO DAMAGED HOLES PER SRM 51-40-08.
- [SDR R61A2023051600286](https://openairdocs.org/sdr/R61A2023051600286.md): Skin Splice · damaged · Apr 24, 2023 · N422YX · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > REPAIR RH SKIN SPLICE 170-03589-001 FR 12-17 ABOVE STR 20R. REPAIRED THE SKIN SPLICE AS PER THE PROCEDURE. REF ETD2023-170-009823 REV B.
- [SDR R61A2023051600282](https://openairdocs.org/sdr/R61A2023051600282.md): Shear Tie · damaged · Apr 24, 2023 · N422YX · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > "SHEAR CLIP CRACKED ON FR 12 BETWEEN STGR 17L AND STGR 18L.: REMOVED AND REPLACED SHEAR FOOT ON FRAME 12 BETWEEN STR 17L AND 18L REF SRM 51-40-08.
- [SDR R61A2023051700292](https://openairdocs.org/sdr/R61A2023051700292.md): Spar · damaged · Apr 23, 2023 · N422YX · Emb ERJ170200LR · Wing Spar
  > 170EO-57-20-0050MA_1 RIGHT-OUTBOARD-MAIN WING SPAR 1 INSPECTION AND REWORK SB57-73G1P2. ROUTINE TASK CARD COMPLIED WITH.
- [SDR R61A2023051600285](https://openairdocs.org/sdr/R61A2023051600285.md): Shear Tie · damaged · Apr 14, 2023 · N422YX · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > "THREE MIS-DRILLED HOLES ON SHEAR CLIP AT FR 17 BETWEEN STRINGERS 21L AND 22L AS MARKED.: REMOVED AND REPLACED SHEAR CLIP AT FR 17 STGR 21L/22L. REF EMB SRM 51-40-08.
- [SDR R61A2023051500275](https://openairdocs.org/sdr/R61A2023051500275.md): Stringer · damaged · Apr 12, 2023 · N422YX · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > "ELONGTED HOLE ON STGR 23R BETWEEN FR 16 AND 17. REPAIRED ELONGATED HOLE ON STGR 23R BETWEEN FR 16 AND 17 BY INSTALLING A FREEZE PLUG PER ETD2023-170-009821"
- [SDR R61A2023051500281](https://openairdocs.org/sdr/R61A2023051500281.md): Shear Tie · damaged · Apr 11, 2023 · N422YX · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > INTERNAL RADIUS DAMAGE ON SHEAR CLIP AT FR 17 STGR 20R/21R.: REMOVED AND REPLACED SHEAR CLIP AT FR 17 STGR 20R/21R. REF EMB SRM 51-40-08.
- [SDR R61A2023051500279](https://openairdocs.org/sdr/R61A2023051500279.md): Shear Tie · damaged · Apr 11, 2023 · N422YX · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > INTERNAL RADIUS DAMAGE ON SHEAR CLIP AT FR 17 STGR 24R/25R. REMOVED AND REPLACE SHEAR CLIP AT FR 17 STGR 24R/25R PER SRM 51-40--08
- [SDR R61A2023051600284](https://openairdocs.org/sdr/R61A2023051600284.md): Shear Tie · damaged · Mar 28, 2023 · N422YX · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > "INTERNAL RADIUS DAMAGE ON SHEAR CLIP AT FR 17 STGR 26R/27R. REMOVED AND REPLACED SHEAR CLIP AT FR 17 STGR 26R/27R. PER SRM 51-40-08.
- [SDR R61A2023051600283](https://openairdocs.org/sdr/R61A2023051600283.md): Stringer · damaged · Mar 27, 2023 · N422YX · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > STRINGER 18L IS DENTED FROM FR 10 - FR 12 APPROX 0.033" REF NDT INTRODUCTION AND SRM 51-10-02 EVALUATION. REMOVED AND REPLACED STRINGER 18L FROM FRAME 10-FRAME 12 REF SRM 51-40-08
- [SDR R61A2023051700291](https://openairdocs.org/sdr/R61A2023051700291.md): Spar · damaged · Mar 23, 2023 · N422YX · Emb ERJ170200LR · Wing Spar
  > 170EO-57-20-0049MA_1 LEFT-OUTBOARD-MAIN WING SPAR 1 INSPECTION AND REWORK SB57-73G1P1. ROUTINE TASK CARD COMPLIED WITH.
- [SDR R61A2023051500277](https://openairdocs.org/sdr/R61A2023051500277.md): Skin · dented · Mar 21, 2023 · N422YX · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > RH FUSELAGE SKIN P/N 170-05669-003 HAS ONE DENT BETWEEN FR 17 - X= 5164.0 AND ST 20R - ST 21R.: REMOVED AND REPLACED RH FUSELAGE SKIN P/N 170-05669-003 BETWEEN FR 17 - X=5164.0 AND ST 20R - ST 21R REF SRM 51-40-08
- [SDR R61A2023051500276](https://openairdocs.org/sdr/R61A2023051500276.md): Skin · dented · Mar 21, 2023 · N422YX · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > LH FUSELAGE SKIN P/N 170-03387-003 HAS SEVERAL DENTS FROM FR 10-FR 12 AND ST 17L - ST 19L. REMOVED AND REPLACED LH FUSELAGE SKIN P/N 170-03387-003 FR 10-FR 12 AND ST 17L - ST 19L PER SRM 51-40-08.
- [SDR R61A2022102800671](https://openairdocs.org/sdr/R61A2022102800671.md): Power Supply · inoperative · Oct 25, 2022 · N422YX · Emb ERJ170200LR · Emergency Lighting
  > L2 EMERGENCY EXIT IDENTIFIER SIGN INOP. REMOVED AND REPLACED AFT ELPU #5.
- [SDR R61A2021062500502](https://openairdocs.org/sdr/R61A2021062500502.md): Power Supply · inoperative · Jun 23, 2021 · N422YX · Emb ERJ170200LR · Emergency Lighting
  > AFT GALLEY CENTER AISLE EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. R&R AFT EMERGENCY LIGHT POWER UNIT REF AMM 33-50-01.
- [SDR R61A2021011900071](https://openairdocs.org/sdr/R61A2021011900071.md): Unknown · smoke · Jan 17, 2021 · N422YX · Emb ERJ170200LR · Air Distribution System
  > SMOKE IN COCKPIT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. RAN PACK 1, RECIRCULATION SYSTEM, AND ENGINE BLEED SYSTEMS WITH NO DEFECTS NOTED, IAW AMM 21-22-00 AND 36-00-00. COULD NOT DUPLICATE.
- [SDR R61A2020102600722](https://openairdocs.org/sdr/R61A2020102600722.md): Crossbeam · corroded · Oct 26, 2020 · N422YX · Emb ERJ170200LR · Fuselage Main, Structure
  > WHILE IN HEAVY CHECK MAJOR REPAIR. CORROSION CENTER FUSELAGE AREA 53-21 CROSSBEAM FR 17 BETWEEN SEAT TRACK Y+=10.748" AT EDGE OF SEAT TRACK AND UPPER FLANGE. INSTALLED L-ANGLE REPAIR, IAW SRM 53-00-10 REPAIR 03.
- [SDR R61A2020102600721](https://openairdocs.org/sdr/R61A2020102600721.md): Spar · cracked · Oct 26, 2020 · N422YX · Emb ERJ170200LR · Wing Spar
  > DURING HEAVY MX VISIT, LT WINGTIP SPAR NR 1 HAS CRACK, AS MARKED. REMOVED AND REPLACED LT WINGTIP SPAR NR 1, REF SRM 51-40-08.
- [SDR R61A2020071700568](https://openairdocs.org/sdr/R61A2020071700568.md): Glowstrip · worn · Jul 17, 2020 · N422YX · Emb ERJ170200LR · Emergency Equipment
  > PHOTOLUMINESCENT STRIPS WORN IN FIRST CLASS SECTION OF CABIN. R&R PHOTOLUMINESCENT STRIPS PER AMM 23-80-21.
- [SDR R61A2020011760031](https://openairdocs.org/sdr/R61A2020011760031.md): Light · damaged · Jan 16, 2020 · N422YX · Emb ERJ170200LR · Emergency Lighting
  > PHOTOLUMINESCENT STRIP NEAR GALLEY WARDROBE FADED. R&R PHOTOLUMINESCENT STRIP AT WARDROBE IAW 33-50-21.
- [SDR R61A201909180969](https://openairdocs.org/sdr/R61A201909180969.md): Glowstrip · damaged · Sep 18, 2019 · N422YX · Emb ERJ170200LR · Emergency Equipment
  > PHOTOLUMINESCENT STRIP RT SIDE ROW #1 DAMAGED. R&R PHOTOLUMINESCENT STRIP RT SIDE ROW #1 IAW AMM 33-50-21, OPS CHECK GOOD.
- [SDR R61A201909070937](https://openairdocs.org/sdr/R61A201909070937.md): Glowstrip · missing · Sep 7, 2019 · N422YX · Emb ERJ170200LR · Emergency Equipment
  > EMERGENCY PHOTOLUMINESCENT FLOOR STRIP MISSING ADJACENT TO SEAT 14C. R&R MISSING PHOTOLUMINESCENT STRIP AT SEAT 14C IAW AMM 33-50-21.
- [SDR R61A2018090420924](https://openairdocs.org/sdr/R61A2018090420924.md): Splice Plate · corroded · Aug 22, 2018 · N422YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, MAINTENANCE REPORTED LEVEL 2 CORROSION ON THE FLOOR STRUCTURE GUSSET SPLICE PLATE AT FR 89 FLOORBEAM RBL 10. MAINTENANCE REMOVED AND REPLACED GUSSET PLATE AT FR 89 FLOORBEAM RBL 10 IAW SRM 51-40-08 AND 53-30-10. AIRCRAFT
- [SDR R61A2018090410923](https://openairdocs.org/sdr/R61A2018090410923.md): Seat Track · corroded · Aug 21, 2018 · N422YX · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, MAINTENANCE REPORTED LEVEL 2 CORROSION ON THE RT INBOARD SEAT TRACK AT FR 82. MAINTENANCE REMOVED AND SPLICED IN NEW SEAT TRACK SECTION AT THE RT INBOARD SEAT TRACK AT FR 82 IAW SRM 53-00-10 & 51-40-08. AIRCRAFT IS CURREN
- [SDR R61A2018090210921](https://openairdocs.org/sdr/R61A2018090210921.md): Web · corroded · Aug 21, 2018 · N422YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE AC WAS IN FOR HEAVY CHECK FOUND PAX CABIN FLOOR FR 14 FLOOR WEB CORRODED 0-14" INBD OF R1 DOORWAY 2 EACH LOCATIONS. MX REMOVED AND REPLACED WEB PN 170-05663-005 IAW SRM 53-10-10, 51-40-08, ETD2011-190/01333 REVC. AC REMAINS IN IND FOR COMPLETION.
- [SDR R61A201808200922](https://openairdocs.org/sdr/R61A201808200922.md): Shear Panel · corroded · Aug 20, 2018 · N422YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, MAINTENANCE REPORTED LEVEL 2 CORROSION AT THE (MAIN CABIN) RT AFT WET AREA, FLOOR WEB ASSY AT RBL 10 FR 87 TO FR 88 TO RBL 40. MAINTENANCE REMOVED AND REPLACED THE SHEAR PANEL WEB ASSY AT RBL 10 FR 87 TO FR 88 TO RBL 40 I
- [SDR R61A2018090200920](https://openairdocs.org/sdr/R61A2018090200920.md): Web · corroded · Aug 20, 2018 · N422YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE AC WAS IN FOR HEAVY CHECK FOUND MAIN CABIN LT AFT WET AREA FLOOR WEB ASSY LBL 8.5 FR 87 TO FR 88 HAS LARGE AREA OF CORROSION. MX REMOVED AND REPLACED WEB PN 170-65928-001 IAW SRM 53-23-10, ETD2011-190/01333 REV C. AC REMAINS IN IND FOR COMPLETION.
- [SDR R61A2018090200919](https://openairdocs.org/sdr/R61A2018090200919.md): Upper Sheet · corroded · Aug 20, 2018 · N422YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE AC WAS IN FOR HVY CHECK FOUND MAIN CABIN RT AFT WET AREA FLOORBEAM AT RBL 10 FR86 HAS SPOT OF CORROSION. MX REMOVED AND REPLACED UPPER SHEET PN 170-86101-001 IAW SRM 51-75-16, 51-40-08, ETD2011-190/01333 REV C. AC REMAINS IN IND FOR COMPLETION.
- [SDR R61A201608190496](https://openairdocs.org/sdr/R61A201608190496.md): Hook · defective · Aug 19, 2016 · N422YX · Emb ERJ170200LR · Passenger/Crew Doors
  > CREW REPORTED THAT THE L1 DOOR GUST LOCK WAS INOPERATIVE. ACFT WAS FLOWN VIA MAINTENANCE FERRY, WHERE MAINTENANCE R & R PASSENGER DOOR HOOK AND SHAFT ASSY IAW AMM AND OPS CHECKED GOOD.
- [SDR R61A201608190495](https://openairdocs.org/sdr/R61A201608190495.md): Gust Lock · out of adjust · Aug 19, 2016 · N422YX · Emb ERJ170200LR · Passenger/Crew Doors
  > CREW REPORTED THAT THE L1 DOOR GUST LOCK WAS INOPERATIVE. MAINTENANCE ADJUSTED DOOR LOCK IAW AMM AND OPS CHECKED GOOD.
- [SDR R61A201608040453](https://openairdocs.org/sdr/R61A201608040453.md): Diaphragm · defective · Aug 4, 2016 · N422YX · Emb ERJ170200LR · Passenger/Crew Doors
  > CREW REPORTED THAT THE F/A COULD NOT GET THE L1 DOOR CLOSED. DOOR WAS DISARMED AND WHEN THE DOOR WAS OPENED F/A COULD HEAR THE ASSIST BOTTLE LOSE PRESSURE. MAINTENANCE R & R L1 DOOR DIAPHRAGM AND SERVICED IAW AMM AND OPS CHECKED GOOD.
- [SDR R61A201605080336](https://openairdocs.org/sdr/R61A201605080336.md): Light · inoperative · May 8, 2016 · N422YX · Emb ERJ170200LR · Emergency Lighting
  > CREW REPORTED THAT THE EMERGENCY LIGHT STRIP NEAR THE FORWARD CLOSET WAS INOPERATIVE. MAINTENANCE R & R FORWARD EMERGENCY LIGHT STRIP IAW AMM AND OPS CHECKED GOOD.
- [SDR R61A201601150066](https://openairdocs.org/sdr/R61A201601150066.md): Light · inoperative · Jan 15, 2016 · N422YX · Emb ERJ170200LR · Emergency Lighting
  > MAINTENANCE REPORTED THAT THE EMERGENCY LIGHT STRIP AT SEAT 1D & F WERE INOPERATIVE. MAINTENANCE R & R EMERGENCY LIGHT STRIP AT SEAT 1D & F IAW AMM AND OPS CHECKED GOOD.
- [SDR R61A201506040344](https://openairdocs.org/sdr/R61A201506040344.md): Unknown · odor · Jun 4, 2015 · N422YX · Emb ERJ170200LR · Air Distribution System
  > THE CREW REPORTED A SMOKE ODOR COMING FROM THE GUIDANCE PANEL AREA IN FLIGHT. THE CREW CYCLED THE PACKS AND RECIRCULATION FANS AND THE ODOR DISSIPATED. THE CREW LANDED AT ITS INTENDED DESTINATION WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED OPS CHECKS O
- [SDR R61A201504290276](https://openairdocs.org/sdr/R61A201504290276.md): Control Module · inoperative · Apr 29, 2015 · N422YX · Emb ERJ170200LR · Landing Gear Brake System
  > CREW REPORTED RT AND LT BRAKE FAULT WITH LOSS OF BRAKING ACTION ON ROLLOUT. MAINTENANCE TROUBLESHOT TO A BAD BRAKE CONTROL MODULE. MAINTENANCE R & R BRAKE CONTROL MODULE NR 2 IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.
- [SDR R61A201502240117](https://openairdocs.org/sdr/R61A201502240117.md): Microphone · stuck · Feb 24, 2015 · N422YX · Emb ERJ170200LR · Audio Integrating System
  > CREW WAS ADVISED BY THE F/A`S THAT THEY HEARD THE EMERGENCY TRIPLE CHIME AND WHEN THEY PICKED UP THE PHONE NO ONE WAS THERE. CAPTAIN THEN NOTICED 'STKMIC' MESSAGE. TRIED TO CONTACT ATC, BUT DID NOT GET A RESPONSE. CREW SQUAWKED 7600 AND CONTINUED ONTO DESTINAT

## 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 = 'N422YX' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N422YX/reports

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