# Service difficulty reports: N375JB, cancelled Mar 25, 2026

A list on [N375JB, cancelled Mar 25, 2026](https://openairdocs.org/deregistered/N375JB-2026-03-25.md).

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

- [SDR YENA2024051400726](https://openairdocs.org/sdr/YENA2024051400726.md): Pressure Switch · failed · May 9, 2024 · N375JB · Emb ERJ190100IGW · Engine Bleed Air System
  > FLT#1487, BOS-CHS. (AIRCRAFT PERFORMED AN AIR TURN BACK TO BOS) ' BLEED 2 OVERPRESS EICAS MSG AFTER TAKEOFF, WOULD NOT RESET PER QRH ( ENGINE BLEED SYSTEMS CROSSBLEED OPERATIVE); FIM 36-14-00-810-80-A00 REPLACED BLEED OVERPRESSURE SWITCH RH BLEED REF AMM 36-
- [SDR YENA2023060600585](https://openairdocs.org/sdr/YENA2023060600585.md): Unknown · unknown · Jun 1, 2023 · N375JB · Emb ERJ190100IGW · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION WAS FOUND ON SHEAR CLIP BTW FRAME 81 AND STR 28R/27L; REF TOMX WO 2196 NR 00105 SHEAR CLIP BTW FR 81 AND STGR 28R/27R WAS EVALUATED AND FOR DUE EXCESSIVE DAMAGE WAS REPLACED PER EMB-190 SRM 51-10-02, SRM 51-41-01 AND SRM 51-
- [SDR YENA2023060600584](https://openairdocs.org/sdr/YENA2023060600584.md): Unknown · unknown · Jun 1, 2023 · N375JB · Emb ERJ190100IGW · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CPCP FINDING, CORROSION ON FRAME 80- BTW STGR 28R/27R AT AFT CARGO DOOR CUTOUT STRUCTURE; (RESOLVED ON W/O: 1219624 TASKCARD: NR-00009) REF TOMEX NR 00102, CORROSION ON FRAME 80 BTW STGR 28R/27R AT AFT CARGO DOOR CUTOUT STRUCTURE WAS
- [SDR YENA2023060600583](https://openairdocs.org/sdr/YENA2023060600583.md): Unknown · unknown · Jun 1, 2023 · N375JB · Emb ERJ190100IGW · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE: CPCP FOUND, CORROSION ON SEAT TRACK BEAM BTW FR 84 AND Y:340 LH AT CABIN FLOOR STRUCTURE. (W2); (RESOLVED ON W/O: 1242241 TASKCARD: NR-00004) REF TOMEX WO 2196, NR 00084, CORROSION ON SEAT TRACK BEAM BTW FR 84 AND Y: 340 LH AT CABIN
- [SDR YENA2023060600582](https://openairdocs.org/sdr/YENA2023060600582.md): Unknown · unknown · Jun 1, 2023 · N375JB · Emb ERJ190100IGW · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CPCP FINDING, CORROSION ON RH SEAT TRACK BEAM BTW FR 12/18 AND Y:300 RH AT CABIN FLOOR STRUCTURE (W1); (RESOLVED ON W/O: 1242241 TASKCARD: NR-00005) REF TOMEX WO 2196, NRC 00091, CORROSION ON RH SEAT TRACK BEAM BTW FR 12/18 AND Y:300
- [SDR YENA2023060600581](https://openairdocs.org/sdr/YENA2023060600581.md): Unknown · unknown · Jun 1, 2023 · N375JB · Emb ERJ190100IGW · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CPCP FINDING, CORROSION ON RH SEAT TRACK BEAM BTW FR 12/18 AND Y:300 RH AT CABIN FLOOR STRUCTURE (W1); REF TOMEX WO 2196, NRC 00091, CORROSION ON RH SEAT TRACK BEAM BTW FR 12/18 AND Y:300 AT CABIN FLOOR STRUCTURE (W1) WAS REMOVED AND
- [SDR YENA2023060600580](https://openairdocs.org/sdr/YENA2023060600580.md): Unknown · unknown · Jun 1, 2023 · N375JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: CPCP FOUND, CORROSION ON SEAT TRACK BEAM BTW FR 84 AND Y:340 LH AT CABIN FLOOR STRUCTURE. (W2); REF TOMEX WO 2196, NR 00084, CORROSION ON SEAT TRACK BEAM BTW FR 84 AND Y: 340 LH AT CABIN FLOOR STRUCTURE WSS REMOVED AND EVALUATED OUT O
- [SDR YENA2023060600579](https://openairdocs.org/sdr/YENA2023060600579.md): Unknown · unknown · Jun 1, 2023 · N375JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: CPCP FINDING, CORROSION ON FRAME 80- BTW STGR 28R/27R AT AFT CARGO DOOR CUTOUT STRUCTURE; REF TOMEX NR 00102, CORROSION ON FRAME 80 BTW STGR 28R/27R AT AFT CARGO DOOR CUTOUT STRUCTURE WAS REMOVED AND EVALUATED OUT OF LIMITS OT=0.118
- [SDR YENA2023060600578](https://openairdocs.org/sdr/YENA2023060600578.md): Unknown · unknown · Jun 1, 2023 · N375JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / FLOOR STRUCTURE / FWD RH FLOOR TRACK / BTWN FR 13-14 AND 17-18 / CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2022030400122](https://openairdocs.org/sdr/YENA2022030400122.md): Feedback Unit · failed · Feb 26, 2022 · N375JB · Emb ERJ190100IGW · Landing Gear Steering System
  > FLT # 1486, PIT-BOS. ON LANDING " STEER FAIL" EICAS. QRH PROCEDURE DID NO CLEAR MESSAGE, DIFF BRAKING USED;BOTH FEEDBACK SENSORS AND FEEDBACK ASSY WERE REPLACED REF DEFECT 3248112-1, 3248112-2 AND 3248111-1, 3248111-2. ADJUSTMENT OF FEEDBACK SENSORS AND OPS C
- [SDR YENA2022030400121](https://openairdocs.org/sdr/YENA2022030400121.md): Feedback Unit · failed · Feb 26, 2022 · N375JB · Emb ERJ190100IGW · Landing Gear Steering System
  > FLT # 1486, PIT-BOS. ON LANDING " STEER FAIL" EICAS. QRH PROCEDURE DID NO CLEAR MESSAGE, DIFF BRAKING USED;BOTH FEEDBACK SENSORS AND FEEDBACK ASSY WERE REPLACED REF DEFECT 3248112-1, 3248112-2 AND 3248111-1, 3248111-2. ADJUSTMENT OF FEEDBACK SENSORS AND OPS C
- [SDR YENA2022030400120](https://openairdocs.org/sdr/YENA2022030400120.md): Feedback Unit · failed · Feb 26, 2022 · N375JB · Emb ERJ190100IGW · Landing Gear Steering System
  > FLT # 1486, PIT-BOS. ON LANDING " STEER FAIL" EICAS. QRH PROCEDURE DID NO CLEAR MESSAGE, DIFF BRAKING USED;BOTH FEEDBACK SENSORS AND FEEDBACK ASSY WERE REPLACED REF DEFECT 3248112-1, 3248112-2 AND 3248111-1, 3248111-2. ADJUSTMENT OF FEEDBACK SENSORS AND OPS C
- [SDR YENA2022030400119](https://openairdocs.org/sdr/YENA2022030400119.md): Feedback Unit · failed · Feb 26, 2022 · N375JB · Emb ERJ190100IGW · Landing Gear Steering System
  > FLT # 1486, PIT-BOS. ON LANDING " STEER FAIL" EICAS. QRH PROCEDURE DID NO CLEAR MESSAGE, DIFF BRAKING USED;BOTH FEEDBACK SENSORS AND FEEDBACK ASSY WERE REPLACED REF DEFECT 3248112-1, 3248112-2 AND 3248111-1, 3248111-2. ADJUSTMENT OF FEEDBACK SENSORS AND OPS C
- [SDR YENA2021042900296](https://openairdocs.org/sdr/YENA2021042900296.md): Seal Rest · corroded · Apr 24, 2021 · N375JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION LOWER SEAL REST AFT CARGO COMPARTMENT FR77-80; (REF TOMX NR 00277) R & R SEAL REST AT AFT CARGO COMPARTMENT IAW SRM 51-40-01 PAR 6 () TO (I), SRM 51-23-05 PAR 7, 51-40-08 PAR 6, AND 51-23-04 PAR 5B.
- [SDR YENA2021042900295](https://openairdocs.org/sdr/YENA2021042900295.md): Light · no test · Apr 24, 2021 · N375JB · Emb ERJ190100IGW · Emergency Lighting
  > DURING HEAVY MAINTENANCE, MID LH & FWD RH EXTERNAL EMERGENCY LIGHT FAILED OPS CHECK; (REF TOMX NR 00407) R & R MID LH EMERGENCY LIGHT AND FWD RH EMERGENCY LIGHT IAW AMM 33-50-25-000-802-A AND 33-50-25-400-802-A. OPS CHECKS SATIS.
- [SDR YENA2021042900294](https://openairdocs.org/sdr/YENA2021042900294.md): Skin · cracked · Apr 24, 2021 · N375JB · Emb ERJ190100IGW · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, CRACK LOWER SKIN LH WING AT RIB 10. L=0.812"; (REF TOMX NR 00021) ACCOMPLISHED REPAIR EMBRAER SRM 57-10-01 REPAIR 54.
- [SDR YENA2021031500175](https://openairdocs.org/sdr/YENA2021031500175.md): Girt Bar · dislodged · Mar 9, 2021 · N375JB · Emb ERJ190100IGW · Emergency Equipment
  > FLT 490, DCA-BOS. DOOR 1L (BOARDING DOOR) IS DIFFICULT TO ARM. REQUIRES TWO PEOPLE TO ARM/DISARM; FOUND GIRT BAR DISLODGED FROM THE AFT BELLCRANK OF THE L1 DOOR. INSERTED GIRT BAR INTO BELLCRANK IAW APPLICABLE STEPS OF AMM 52-11-41. OPS CHECK GOOD.
- [SDR YENA2021030500154](https://openairdocs.org/sdr/YENA2021030500154.md): Slide · defective · Mar 2, 2021 · N375JB · Emb ERJ190100IGW · Emergency Equipment
  > FLT # 6220, MZJ-BOS. R-1 DOOR SLIDE S/N EF0131 FAILED FIRING CABLE TRAVEL LIMITS CHECK AS REQUIRED PER T/C # C2514012-01; R&R R1 DOOR SLIDE IAW AMM 25-65-01
- [SDR YENA201803020118](https://openairdocs.org/sdr/YENA201803020118.md): Power Supply · inoperative · Mar 2, 2018 · N375JB · Emb ERJ190100IGW · Emergency Lighting
  > INOPERATIVE CEILING EMERGENCY LIGHT IN PASSENGER CABIN. REPLACED THE EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-50-01-400-801-A, PERFORMED AN OPS TEST IAW 35-50-01-710-801-A.
- [SDR YENA201711010883](https://openairdocs.org/sdr/YENA201711010883.md): Strut · discharged · Nov 1, 2017 · N375JB · Emb ERJ190100IGW · Nose/Tail Landing Gear Strut/Axle
  > RETURNED TO FIELD DUE TO A LG WOW SYS FAIL UPON ATTEMPTED GEAR RETRACTION AFTER TAKEOFF. EXECUTED QRH PROCEDURE'S LG WOW SYS FAIL AND OVERWEIGHT LANDING. PERFORMED NLG FULL HYD & NITRO SERVICING IAW AMM 12-12-09. ALL CHECKED GOOD AND NO LEAKS NOTED. PERF
- [SDR YENA201701160038](https://openairdocs.org/sdr/YENA201701160038.md): Acm · failed · Jan 16, 2017 · N375JB · Emb ERJ190100IGW · Cabin Cooling System
  > FLT 207, PWM-JFK. UPON LANDING AND DEPLOYING THRUST REVERSERS NR 1 REVERSER DID NOT DEPLOY. STOWED AND DEPLOYED. TR 1 STILL DID NOT DEPLOY. FIVE SECONDS LATER, TR1 FAIL EICAS FOLLOWED BY STRONG BURNING ODOR THROUGHOUT THE ENTIRE CABIN. SMELL WAS EVIDENT UP T
- [SDR YENA201701160037](https://openairdocs.org/sdr/YENA201701160037.md): Control Quadrant · failed · Jan 16, 2017 · N375JB · Emb ERJ190100IGW · Engine Thrust Reverser
  > FLT 207, PWM-JFK. UPON LANDING AND DEPLOYING THRUST REVERSERS, NR 1 REVERSER DID NOT DEPLOY. STOWED AND DEPLOYED. TR 1 STILL DID NOT DEPLOY. FIVE SECONDS LATER, TR1 FAIL EICAS FOLLOWED BY STRONG BURNING ODOR THROUGHOUT THE ENTIRE CABIN. SMELL WAS EVIDENT UP
- [SDR YENA20160930900](https://openairdocs.org/sdr/YENA20160930900.md): Battery · failed · Sep 30, 2016 · N375JB · Emb ERJ190100IGW · Emergency Lighting
  > DURING A ROUTINE MAINTENANCE INSPECTION, THE RT AFT EXIT EMERGENCY LIGHT AND EMERGENCY CEILING LIGHT AT ROW 21, WERE FOUND TO BE INOPERATIVE.; REMOVED & REPLACED EMERGENCY BATTERY IAW AMM 33-50-01. PERFORMED OPS CHECK. OPS CHECK PASSED.
- [SDR YENA20160922850](https://openairdocs.org/sdr/YENA20160922850.md): Apu · failed · Sep 22, 2016 · N375JB · Emb ERJ190100IGW · APU Core Engine
  > PRIOR TO OPERATING THE FLIGHT, THE APU AUTO-SHUTDOWN. THE PILOT REPORTED: APU FAILED AT GATE, HEAVY SMOKE IN CABIN AND OUTSIDE. EVACUATION CHECKLIST RUN. APU FIRE BOTTLE PRESSED. ACFT WAS CLEARED OF PASSENGERS WITHOUT INCIDENT. THE ACFT WAS THEN MOVED OFF
- [SDR YENA20131224249](https://openairdocs.org/sdr/YENA20131224249.md): Wire Harness · failed · Dec 24, 2013 · N375JB · Emb ERJ190100IGW · Landing Gear System Wiring
  > LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF, AIR RETURN. HANDLE WOULD NOT MOVE, NO MESSAGES. R & R LT WEIGHT OFF WHEELS HARNESS NR 1. NO EICAS MSGS PRESENT ON ECAM. ALL WORK DONE IAW AMM 32-00-01. ACCOMPLISHED LANDING GEAR EXTENSION, RETRACTION TEST IAW

## 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 = 'N375JB' AND deregistration_id = 'N375JB-2026-03-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N375JB-2026-03-25/reports

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