# Service difficulty reports: N742YX

A list on [N742YX](https://openairdocs.org/aircraft/N742YX.md).

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

- [SDR R61A2024111800551](https://openairdocs.org/sdr/R61A2024111800551.md): Profile · cracked · Nov 1, 2024 · N742YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CFII MLG BAY FR-52, BL0 FOUND TO HAVE CRACKED ANGLE SUPPORT. CFII MLG BAY FR-52, BL0, THE ANGLE SUPPORT WAS REPLACED IAW ERJ 175 SRM 51-41-01 AND ERJ 175 SRM 51-42-01.
- [SDR R61A2024111800550](https://openairdocs.org/sdr/R61A2024111800550.md): Support Angle · cracked · Nov 1, 2024 · N742YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CFII MLG BAY FR-52 LH SIDE FOUND TO HAVE CRACK LOWER ANGLE SUPPORT ON LOWER SKIN. CFII MLG BAY FR-52 LH SIDE ON LOWER SKIN, LOWER ANGLE SUPPORT WAS REPLACED IAW ERJ 175 SRM 51-43-03 AND ERJ 175 SRM 51-21-05
- [SDR R61A2024111800549](https://openairdocs.org/sdr/R61A2024111800549.md): Doubler · corroded · Oct 31, 2024 · N742YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CFIII FR-84, RBL10 FOUND CORRODED FLOOR SUPPORT DOUBLER. CFIII FR-84, RBL10 CORRODED FLOOR SUPPORT DOUBLER REMOVED AND REPLACED IAW EMBRAER 175 SRM 51-43-04.
- [SDR R61A2024111800548](https://openairdocs.org/sdr/R61A2024111800548.md): Support Angle · cracked · Oct 31, 2024 · N742YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CFIII FR-86, RBL25 FOUND ANGLE BRACKET CRACKED. ANGLE BRACKET AT CFIII FR-86, RBL25 REMOVED AND REPLACED /INSTALLED IAW SRM 51-41-01.
- [SDR R61A2024111800547](https://openairdocs.org/sdr/R61A2024111800547.md): Seat Track · corroded · Oct 31, 2024 · N742YX · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CFIII INBD RH SEAT TRACK CORRODED. CFIII CORRODED INBD RH SEAT TRACK REMOVED AND REPLACED IAW EMBRAER 175 SRM 51-41-01, 51-43-03 AND 51-43-04.
- [SDR R61A2024111800546](https://openairdocs.org/sdr/R61A2024111800546.md): Frame · cracked · Oct 28, 2024 · N742YX · Emb ERJ170200LR · Fuselage Main, Frame
  > REF DEFECT: DMI R1008580/1: LH WHEEL WELL FR-52 CRACKED. LH WHEEL WELL FR-52 HAS BEEN REPLACED IAW SRM 51-41-01 AND SRM 51-43-03. THIS CLEARS DMI R1008580/1.
- [SDR R61A2024100300458](https://openairdocs.org/sdr/R61A2024100300458.md): Acm · smoke · Oct 3, 2024 · N742YX · Emb ERJ170200LR · Cabin Cooling System
  > PACK 2 FAIL AND SMOKE IN CABIN. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R ACM 2.
- [SDR R61A2024032500130](https://openairdocs.org/sdr/R61A2024032500130.md): Skin · gouged · Mar 22, 2024 · N742YX · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > AIRCRAFT DAMAGED,HAS GOUGE ON CARGO DOOR AND FUSELAGE SKIN AT FRA 77 AND UNDER STR 22R.REPAIRED DAMAGE ON DOOR AND SKIN IAW ETD2024-170-008290, ALSO REF VP-011976-2024 N/R # 1 FOR WORK ACCOMPLISHED.
- [SDR R61A2024011900016](https://openairdocs.org/sdr/R61A2024011900016.md): Power Supply · inoperative · Jan 17, 2024 · N742YX · Emb ERJ170200LR · Emergency Lighting
  > EMERGENCY LIGHT BATTERY #2 FAILED FUNCTIONAL CHECK, DID NOT STAY ON FOR 15 MINUTES. R&R #2 EMERGENCY LIGHT POWER SUPPLY.
- [SDR R61A2022090900549](https://openairdocs.org/sdr/R61A2022090900549.md): Actuator · failed · Sep 5, 2022 · N742YX · Emb ERJ170200LR · Trailing Edge Flap Control System
  > FLAP FAIL AFTER RETRACTION 1 TO 0 POSITION. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R 4R FLAP ACTUATOR.
- [SDR R61A2022090900548](https://openairdocs.org/sdr/R61A2022090900548.md): None · none · Sep 5, 2022 · N742YX · Emb ERJ170200LR · Trailing Edge Flap Control System
  > FLAP FAIL ON TAKE OFF RETRACTION FROM POS 1 TO 0. AUTO THROTTLE FAIL ON DEPARTURE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOLLOW FIM TASK 27-51-00, PERFORM INSPECTION OF TORQUE LIMIT TRIPS, NO TRIPS FOUND. PERFORM OPS CHECK OF FLAP/SLAT IAW AMM 27-50-00
- [SDR R61A2022010300013](https://openairdocs.org/sdr/R61A2022010300013.md): Shear Panel · corroded · Dec 17, 2021 · N742YX · Emb ERJ170200LR · Fuselage Structure (General)
  > CORROSION FOUND ON AFT WET AREA FLOOR STRUCTURE, RH SHEAR WEB BETWEEN FR87 AND FR88. REPLACED IAW SRM 51-43-01 AND 51-42-01
- [SDR R61A2022010200011](https://openairdocs.org/sdr/R61A2022010200011.md): Gusset · corroded · Dec 17, 2021 · N742YX · Emb ERJ170200LR · Fuselage Structure (General)
  > CORROSION FOUND ON AFT WET AREA FLOOR STRUCTURE GUSSET ON RH OUTBOARD SIDE AT FR90, REPLACED IAW SRM 51-41-02
- [SDR R61A2022010200010](https://openairdocs.org/sdr/R61A2022010200010.md): Splice · corroded · Dec 17, 2021 · N742YX · Emb ERJ170200LR · Fuselage Structure (General)
  > CORROSION FOUND ON AFT WET AREA FLOOD STRUCTURE GUSSET ON RH INBD SIDE AT FR89, REPLACED IAW SRM 51-43-01
- [SDR R61A2022010200009](https://openairdocs.org/sdr/R61A2022010200009.md): Splice · corroded · Dec 17, 2021 · N742YX · Emb ERJ170200LR · Fuselage Structure (General)
  > CORROSION FOUND ON AFT WET AREA FLOOR STRUCTURE GUSSET ON RH OUTBD SIDE AT FR89, REPLACED IAW SRM 51-43-03
- [SDR R61A2022010200008](https://openairdocs.org/sdr/R61A2022010200008.md): Panel Support · corroded · Dec 17, 2021 · N742YX · Emb ERJ170200LR · Fuselage Structure (General)
  > CORROSION FOUND ON AFT WET AREA FLOOR PANEL SUPPORT ON RH OUTBD SIDE, BETWEEN FR88 AND FR90. REPLACED IAW SRM 51-43-03
- [SDR R61A2022010200007](https://openairdocs.org/sdr/R61A2022010200007.md): Shear Panel · corroded · Dec 17, 2021 · N742YX · Emb ERJ170200LR · Fuselage Structure (General)
  > CORROSION FOUND ON AFT WET AREA FLOOR STRUCTURE, CENTER SHEAR WEB BETWEEN FR87 AND FR88. REPLACED IAW SRM 51-42-01
- [SDR R61A2022010200006](https://openairdocs.org/sdr/R61A2022010200006.md): Shear Panel · corroded · Dec 17, 2021 · N742YX · Emb ERJ170200LR · Fuselage Structure (General)
  > CORROSION FOUND ON AFT WET AREA FLOOR STRUCTURE, LH SHEAR WEB BETWEEN FR87 AND FR88. REPLACED IAW SRM 51-41-01
- [SDR R61A2022010200005](https://openairdocs.org/sdr/R61A2022010200005.md): Seat Track · corroded · Dec 17, 2021 · N742YX · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON FWD FUSELAGE RH INBD CABIN SEAT TRACK BETWEEN FR12 AND FR20. REPLACED SEAT TRACK IAW SRM 51-41-01, 51-41-02, 51-43-03 & 51-43-04
- [SDR R61A2022010200004](https://openairdocs.org/sdr/R61A2022010200004.md): Seat Track · corroded · Dec 17, 2021 · N742YX · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON FWD FUSELAGE LH INBD CABIN SEAT TRACK BETWEEN FR12 AND FR20. REPLACED SEAT TRACK IAW SRM 51-41-01, 51-41-02, 51-43-03 & 51-43-04
- [SDR R61A2022010500027](https://openairdocs.org/sdr/R61A2022010500027.md): Latch · corroded · Dec 15, 2021 · N742YX · Emb ERJ170200LR · Fuselage Structure (General)
  > LIGHT CORROSION FOUND ON RH INBD CABIN SEAT TRACK BETWEEN FR82 & FR83 REPAIRED IAW SRM 53-00-10 REPAIR 02
- [SDR R61A2022010300012](https://openairdocs.org/sdr/R61A2022010300012.md): Door · corroded · Dec 13, 2021 · N742YX · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON CENTER FUSELAGE III WASTE ACCESS DOOR INNER SKIN. REPLACED IAW AMM 53-03-00-440-801-A
- [SDR R61A2020061100525](https://openairdocs.org/sdr/R61A2020061100525.md): Glowstrip · missing · Jun 9, 2020 · N742YX · Emb ERJ170200LR · Emergency Equipment
  > 1C PHOTOLUMINESCENT STRIP MISSING. INSTALLED PHOTOLUMINESCENT STRIP AT SEAT 1C PER AMM 33-50-21.
- [SDR R61A2020041480486](https://openairdocs.org/sdr/R61A2020041480486.md): Structure · dented · Apr 10, 2020 · N742YX · Emb ERJ170200LR · Wing Miscellaneous Structure
  > LH WINF HAS A DENT BETWEEN RIBS 25/26 FWD SPAR 1 MEASURING 1.375"L X 4.06"W X.057"D. DAMAGE BETWEEN RIBS 25/26 FWD OF SPAR 1 IS PERMANENT ALLOWABLE DAMAGE PER ETD2020-170-014204.
- [SDR R61A2020041480485](https://openairdocs.org/sdr/R61A2020041480485.md): Slat · scratched · Apr 10, 2020 · N742YX · Emb ERJ170200LR · Leading Edge Devices
  > LH SLAT #4 HAS A SCRATCH MEASURING 12.5"L X.375"W X.019"D. PERFORMED TEMPORARY REPAIR OF LH SLAT #4 DAMAGE PER ETD2020-170-014195. SEE DMI R674599/3 FOR PERMANENT REPAIR.
- [SDR R61A2019113051342](https://openairdocs.org/sdr/R61A2019113051342.md): Flange · corroded · Nov 25, 2019 · N742YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON INTERNAL FLANGE ON PANEL 192CR. REMOVED AND REPLACED INTERNAL FLANGEON PANEL 192CR PER REF 175-SRM 51-40-08. RESTORED TOPCOAT SURFACE PROTECTION TO FLANGE ON PANEL 192CR. REF SRM 51-23-06. A/C REMAINS IN CHECK
- [SDR R61A2019113051341](https://openairdocs.org/sdr/R61A2019113051341.md): Angle · corroded · Nov 25, 2019 · N742YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON LOWER 2 EA ANGLES ON PANEL 1431DL. REMOVED AND REPLACED LOWER 2 EA ANGLES ON PANEL 1431DL.PER SRM 51-40-08. A/C REMAINS IN CHECK.

## 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 = 'N742YX' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N742YX/reports

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