# Service difficulty reports: N240SY

A list on [N240SY](https://openairdocs.org/aircraft/N240SY.md).

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

- [SDR SWIA2025031106](https://openairdocs.org/sdr/SWIA2025031106.md): Shutoff Valve · faulted · Mar 6, 2025 · N240SY · Emb ERJ170200LR · Cabin Pressure Control System
  > GOT CABIN ALTITUDE HI WARNING MESSAGE WHEN DESCENDING THROUGH FL210 CABIN ALTITUDE INCREASED TO 12000. WENT THROUGH THE QRC AND QRH PERFORMED EMERGENCY DESCENT, MESSAGE EXTINGUISHED UPON REACHING 10,000. (FLIGHT 3863) REMOVED AND REPLACED LH NAPRSOV AND
- [SDR SWIA20250307006](https://openairdocs.org/sdr/SWIA20250307006.md): Warning Message · illuminated · Mar 6, 2025 · N240SY · Emb ERJ170200LR · Cabin Pressure Control System
  > GOT CABIN ALTITUDE HI WARNING MESSAGE WHEN DESCENDING THROUGH FL210 CABIN ALTITUDE INCREASED TO 12000. WENT THROUGH THE QRC AND QRH PERFORMED EMERGENCY DESCENT, MESSAGE EXTINGUISHED UPON REACHING 10,000. (FLIGHT 3863 - FILED OPEN) THIS IS CURRENTLY A WOR
- [SDR SWIA2024112210301](https://openairdocs.org/sdr/SWIA2024112210301.md): Floor Support · gouged · Oct 30, 2024 · N240SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CENTER FUSELAGE III, RH FLOOR BEAM Y=+273MM FROM FR74 TO FR79 HAS GOUGES IN CENTER OF SEAT TRACK IN SEVERAL PLACES (C-CHECK RO 11/21/2024) REMOVED AND REPLACED CENTER FUSELAGE III, RH FLOOR BEAM Y=+273MM FROM FR74 TO FR79 REF EMB 175 SRM 51-40-08.
- [SDR SWIA202411221029](https://openairdocs.org/sdr/SWIA202411221029.md): Seat Track · gouged · Oct 29, 2024 · N240SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > RH LATERAL SEAT TRACK HAS GOUGES IN SEVERAL AREAS FROM FR74 TO FR83 (C-CHECK RO 11/21/2024) REMOVED AND REPLACED RH LATERAL SEAT TRACK FROM FR74 TO FR83 REF EMB 175 SRM 51-40-08
- [SDR SWIA202163811](https://openairdocs.org/sdr/SWIA202163811.md): None · cracked · Dec 28, 2021 · N240SY · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > FRAME CLIP CRACKED ON COCKPIT FLOOR AT FR12 AND LEFT BUTT LINE 36". (C CHECK RO 1/14/2022) REMOVED AND REPLACED FRAME CLIP AT FR 12 AND LEFT BUTT LIN 36". REF EMB SRM 51-40-08. SEE CONTINUATION FOR WORK PERFORMED.
- [SDR SWIA202163810](https://openairdocs.org/sdr/SWIA202163810.md): None · cracked · Dec 28, 2021 · N240SY · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > FRAME CLIP CRACKED ON COCKPIT FLOOR AT FR12 AND CENTER BUTT LINE. (C CHECK RO 1/14/2022) REMOVED AND REPLACED FRAME CLIP AT FR 12 CENTER BUTT LINE. REF 51-40-08. SEE CONTINUATION FOR WORK PERFORMED.
- [SDR SWIA202163802](https://openairdocs.org/sdr/SWIA202163802.md): None · damaged · Dec 28, 2021 · N240SY · Emb ERJ170200LR · Ailerons
  > L/H WING FLAP TRACK 1A HAS DEPTH REDUCTION DAMAGE OF.039" WITH MAX ALLOWABLE DEPTH OF.068". DAMAGE IS IN ALLOWABLE LIMITS, BUT WILL REQUIRE AN INSPECTION INTERVAL EVERY 200FC PER SRM 57-52-03/AD01. ASSET# TC2-7153 CAL DUE 11-18-22. (C CHECK RO 1/14/2022)
- [SDR SWIA202163809](https://openairdocs.org/sdr/SWIA202163809.md): None · cracked · Dec 27, 2021 · N240SY · Emb ERJ170200LR · Fuselage Structure (General)
  > L/H WHEEL WELL FR 52 ANGLE CRACKED. (C CHECK RO 1/14/2022) REMOVED AND REPLACED L/H WHEEL WELL FR 52 ANGLE REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR DETAILS
- [SDR SWIA202163808](https://openairdocs.org/sdr/SWIA202163808.md): None · corroded · Dec 26, 2021 · N240SY · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > CORROSION, AFT WET AREA INTERNAL SIDE OF FUSELAGE BELOW FLOOR, ON SHEAR CLIP ATTACHED TO FRAME 86 BETWEEN STRINGERS 28R AND 27R. (C CHECK RO 1/14/2022) / REMOVED AND REPLACED AFT WET AREA INTERNAL SIDE OF FUSELAGE BELOW FLOOR, ON SHEAR CLIP ATTACHED TO F
- [SDR SWIA202163807](https://openairdocs.org/sdr/SWIA202163807.md): None · cracked · Dec 26, 2021 · N240SY · Emb ERJ170200LR · Fuselage Internal Stairs
  > AFT WET AREA, LH AND RH PANEL SUPPORTS ARE CRACKED/BROKEN OFF ON FRAME 86 FLOOR CROSS BEAM. (C CHECK RO 1/14/2022) / REMOVED AND REPLACED LH AND RH FLOOR PANEL SUPPORTS ON AFT WET AREA, FRAME 86. / SEE CONTINUATION CARD FOR WORK PERFORMED. REF SRM 51-40-
- [SDR SWIA202163806](https://openairdocs.org/sdr/SWIA202163806.md): None · corroded · Dec 26, 2021 · N240SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORROSION - LH SILL AT FR19 (C CHECK RO 1/14/2022) / REMOVED AND REPLACED LH SILL AT FR19 REF EMB SRM 51-40-08
- [SDR SWIA202163805](https://openairdocs.org/sdr/SWIA202163805.md): None · none · Dec 26, 2021 · N240SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORROSION, AFT WET AREA, ON LH SPLICE PLATE AT FRAME 89. (C CHECK RO 1/14/2022) / REMOVED AND REPLACED LH SPLICE PLATE AT FRAME 89 REF EMB SRM 51-40-08 AND RESTORED SURFACE PROTECTION REF EMB SRM 51-23-06
- [SDR SWIA202163804](https://openairdocs.org/sdr/SWIA202163804.md): None · corroded · Dec 26, 2021 · N240SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORROSION, AFT WET AREA, ON RH SHEAR PANEL BETWEEN FRAMES 86 AND 87 AROUND GALLEY MOUNT POINTS AND ALONG FORWARD EDGE (C CHECK RO 1/14/2022) / REMOVED AND REPLACED RH SHEAR PANEL BETWEEN FRAMES 86 AND 87 REF EMB SRM 51-40-08 SEE CONTINUATION CARD FOR WOR
- [SDR SWIA202163803](https://openairdocs.org/sdr/SWIA202163803.md): None · corroded · Dec 26, 2021 · N240SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORROSION, AFT WET AREA, ON CENTER SHEAR PANEL BETWEEN FRAMES 86 AND 87 AROUND GALLEY MOUNT POINT AND FORWARD EDGE. (C CHECK RO 1/14/2022) / REMOVED AND REPLACED CENTER SHEAR PANEL BETWEEN FRAMES 86 AND 87 REF EMB SRM 51-40-08 SEE CONTINUATION CARD FOR WO
- [SDR SWIA202163800](https://openairdocs.org/sdr/SWIA202163800.md): None · corroded · Dec 26, 2021 · N240SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORROSION, AFT WET AREA INTERNAL SIDE OF FUSELAGE BELOW FLOOR, ON SHEAR CLIP ATTACHED TO FRAME 88 BETWEEN STRINGERS 28R AND 27R. (C CHECK RO 1/14/2022) / REMOVED AND REPLACED AFT WET AREA INTERNAL SIDE OF FUSELAGE BELOW FLOOR, ON SHEAR CLIP ATTACHED TO F
- [SDR SWIA202163799](https://openairdocs.org/sdr/SWIA202163799.md): None · corroded · Dec 26, 2021 · N240SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORROSION, AFT WET AREA INTERNAL SIDE OF FUSELAGE BELOW FLOOR, ON SHEAR CLIP ATTACHED TO FRAME 85 BETWEEN STRINGERS 28R AND 27R. (C CHECK RO 1/14/2022) / REMOVD AND REPLACED AFT WET AREA INTERNAL SIDE OF FUSELAGE BELOW FLOOR, ON SHEAR CLIP ATTACHED TO FRA
- [SDR SWIA202163798](https://openairdocs.org/sdr/SWIA202163798.md): None · corroded · Dec 26, 2021 · N240SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORROSION, AFT WET AREA, ON RH LONGITUDINAL FLOOR BEAM FORWARD OF FRAME 87 IN AN ELONGATED SCREW HOLE. (C CHECK RO 1/14/2022) / REMOVED AND REPLACED RH LONGITUDINAL FLOOR BEAM FORWARD OF FRAME 87. BEAM WAS REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BA
- [SDR SWIA202163797](https://openairdocs.org/sdr/SWIA202163797.md): None · corroded · Dec 26, 2021 · N240SY · Emb ERJ170200LR · Fuselage, Powerplant Attach Fittings
  > CORROSION - LH I/B SEAT TRACK BETWEEN FR19/20 (C CHECK RO 1/14/2022) / REMOVED AND REPLACED LH I/B SEAT TRACK BETWEEN FR19/20 REF EMB SRM 51-40-08. PART WAS REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE
- [SDR SWIA202163796](https://openairdocs.org/sdr/SWIA202163796.md): None · corroded · Dec 26, 2021 · N240SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORROSION, AFT WET AREA, ON LH LONGITUDINAL FLOOR BEAM AT FRAME 87 WHERE THE BEAM PASSES BETWEEN THE LH AND CENTER SHEAR PANELS. (C CHECK RO 1/14/2022) / REMOVED AND REPLACED LH LONGITUDINAL FLOOR BEAM AT FRAME 87 REF EMB SRM 51-40-08 SEE CONTINUATION CAR
- [SDR SWIA202163801](https://openairdocs.org/sdr/SWIA202163801.md): None · gouged · Dec 23, 2021 · N240SY · Emb ERJ170200LR · Fuselage, Powerplant Attach Fittings
  > PILOT SEAT, I/B SEAT TRACK HAS GOUGE ON THE FWD STOP/ RAMP AS MARKED (C CHECK RO 1/14/2022) REMOVED AND REPLACED PILOT SEAT IB SEAT TRACK. REF AMM 53-06-01
- [SDR SWIA202158375](https://openairdocs.org/sdr/SWIA202158375.md): A/C Pack · seized · May 23, 2021 · N240SY · Emb ERJ170200LR · Cabin Cooling System
  > FA HEARD A POP AND NOTICED HAZE IN THE CABIN APPROX 3 MINS AFTER TAKEOFF. OFF SMELL WAS NOTED, NOT SMOKE. SMELL AND HAZE DISSIPATED WITHIN A MINUTE. SMELL AND HAZE WAS NOTED AGAIN AFTER LANDING. (FLIGHT 3732 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFER

## 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 = 'N240SY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N240SY/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.