# Service difficulty reports: N244SY

A list on [N244SY](https://openairdocs.org/aircraft/N244SY.md).

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

- [SDR SWIA2026060676200](https://openairdocs.org/sdr/SWIA2026060676200.md): Engine · failed · Jun 6, 2026 · N244SY · Emb ERJ170200LR · Engine (Turbine/Turboprop)
  > RT ENGINE FAILURE. LOUD BANG AT APPROX 7000 FT ON DEPARTURE. RAN QRC, QRH, TEAM. BLEW R FIRE BOTTLE PER QRH. RETURN TO MSP. (FLIGHT 4122) R & R THE RT ENGINE IN REFERENCE TO AMM 71-00-01. COMPLIED WITH TASK CARD 71-00-001-SKY-U.ON TASK CARD 71-00-01-001-SK
- [SDR SWIA20250211121](https://openairdocs.org/sdr/SWIA20250211121.md): Doubler · corroded · Jan 21, 2025 · N244SY · Emb ERJ170200LR · Fuselage Main, Structure
  > RH COCKPIT FLOOR DOUBLER HAS CORROSION ON UPPER SURFACE AROUND THE AFT END OF INBOARD CO-PILOT SEAT TRACK, BETWEEN FRAMES 11 AND 12. (C-CHECK RO 2/10/2025) CUT OUT DAMAGED PORTION OF THE RH COCKPIT FLOOR DOUBLER AND INSTALLED NEW FILLER PIECE AND FABRIC
- [SDR SWIA20250211120](https://openairdocs.org/sdr/SWIA20250211120.md): Seat Track · corroded · Jan 20, 2025 · N244SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION, FWD WET AREA, ON RH INBOARD FLOOR SEAT TRACK BETWEEN FRAMES 17-18, ON TOP OF SEAT TRACK TEETH AT FORWARD END AND ON FLANGE FORWARD OF SEAT TRACK TEETH. (C-CHECK RO 2/10/2025) REMOVED AND REPLACED RIGHT HAND INBOARD FORWARD WET AREA SEAT TRACK
- [SDR SWIA2023071809](https://openairdocs.org/sdr/SWIA2023071809.md): Unknown · dented · Jul 9, 2023 · N244SY · Emb ERJ170200LR · Fuselage Main, Frame
  > DENT BETWEEN LEFT FUSELAGE STATION FR 10 AND FR 11, STGL 14L AND 15L. NEXT TO SKYWEST LOGO. (FILED CLOSED)COMPLIED WITH PERMANENT REPAIR OF DENT DAMAGE ON FWD FUSELAGE SKIN AT FR10 AND FR11, STGR14L AND STGR15L, IN ACCORDANCE WITH ERJ175 SRM 53-10-01/REPAIR 1
- [SDR SWIA2023071009](https://openairdocs.org/sdr/SWIA2023071009.md): Unknown · dented · Jul 9, 2023 · N244SY · Emb ERJ170200LR · Fuselage Main, Frame
  > DENT BETWEEN LEFT FUSELAGE STATION FR 10 AND FR 11, STGL 14L AND 15L. NEXT TO SKYWEST LOGO. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA202265128](https://openairdocs.org/sdr/SWIA202265128.md): None · corroded · Mar 7, 2022 · N244SY · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > RH OTBD DBLR FR 87/88 AT SHEAR PNL CORRODED (C-CHECK RO 03-19-2022) REMOVED AND REPLACED RH OTBD DBLR FR 87/88 AT SHEAR PNL REF EMB SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06.
- [SDR SWIA202265127](https://openairdocs.org/sdr/SWIA202265127.md): None · corroded · Mar 5, 2022 · N244SY · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > CORROSION AT MOUNT HOLES ON R/H SHEAR PANEL LOCATED AT FRAME 87/88. (C-CHECK RO 03-19-2022) REMOVED AND REPLACED R/H SHEAR PANEL LOCATED AT FRAME 87/88 REF EMB SRM 51-40-08 AND RESTORED SURFACE PROTECTION REF SRM 51-23-06
- [SDR SWIA202265131](https://openairdocs.org/sdr/SWIA202265131.md): None · seized · Mar 3, 2022 · N244SY · Emb ERJ170200LR · Elevator Tab, Attach Fittings
  > RH ELEVATOR HINGE #3 HARDWARE IS OXIDIZED, AND SEIZED. (C-CHECK RO 03-19-2022) REMOVED AND REPLACED RH ELEVATOR HINGE #3 HARDWARE REF EMB 175 AMM 27-31-05. SEE CAMP# 24304069 FOR FINAL INSTALLATION.
- [SDR SWIA202265130](https://openairdocs.org/sdr/SWIA202265130.md): None · seized · Mar 3, 2022 · N244SY · Emb ERJ170200LR · Elevator Tab, Attach Fittings
  > LH ELEVATOR BOTH INBD, AND OTBD PCU TOGGLE LINK HARDWARE (ON ELEVATOR) IS OXIDIZED, AND SEIZED. (C-CHECK RO 03-19-2022) REMOVED AND REPLACED LH ELEVATOR BOTH INBD, AND OTBD PCU TOGGLE LINK HARDWARE (ON ELEVATOR) REF EMB 175 AMM 27-32-02. SEE CAMP# 24304068
- [SDR SWIA202265129](https://openairdocs.org/sdr/SWIA202265129.md): None · seized · Mar 3, 2022 · N244SY · Emb ERJ170200LR · Elevator Tab, Attach Fittings
  > LH ELEVATOR HINGES #2, AND #3 HARDWARE IS OXIDIZED, AND SEIZED. (C-CHECK RO 03-19-2022) REMOVED AND REPLACED LH ELEVATOR HINGES #2, AND #3 HARDWARE ON RACK REF EMB 175 AMM 27-31-05. SEE CAMP# 24304068 FOR FINAL INSTALLATION.
- [SDR SWIA202265136](https://openairdocs.org/sdr/SWIA202265136.md): None · worn · Mar 2, 2022 · N244SY · Emb ERJ170200LR · Elevator Tab, Attach Fittings
  > LH ELEVATOR #3 FIXED HINGE BEARING HAS EXCESSIVE AXIAL PLAY. (C-CHECK RO 03-19-2022) / REMOVED AND REPLACED L/H ELEVATOR #3 HINGE BEARING WITH NEW REF E 175 AMM 20-10-08
- [SDR SWIA202265135](https://openairdocs.org/sdr/SWIA202265135.md): None · broken · Mar 1, 2022 · N244SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > RH AFT WET AREA PNL SUPPORT BROKEN OFF (ACCOUNTED FOR) AT FR 86 (C-CHECK RO 03-19-2022) REMOVED EXISTING AND INSTALLED NEW RH AFT WET AREA PANEL SUPPORT AT FRAME 86 REF EMB SRM 51-40-08
- [SDR SWIA202265134](https://openairdocs.org/sdr/SWIA202265134.md): None · broken · Mar 1, 2022 · N244SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > LH AFT WET AREA PNL SUPPORT BROKEN OFF (ACCOUNTED FOR) AT FR 86 (C-CHECK RO 03-19-2022) REMOVED EXISTING AND INSTALLED NEW, LH AFT WET AREA PNL SUPPORT FR 86. REF EMB SRM 51-40-08
- [SDR SWIA202265126](https://openairdocs.org/sdr/SWIA202265126.md): None · cracked · Mar 1, 2022 · N244SY · Emb ERJ170200LR · Fuselage Structure (General)
  > L/H FRAME 52 ANGLE IN WHEEL WELL CRACKED (C-CHECK RO 03-19-2022) REMOVED AND REPLACED L/H FRAME 52 ANGLE IN WHEEL WELL. / REF SRM 51-40-08
- [SDR SWIA202265125](https://openairdocs.org/sdr/SWIA202265125.md): None · corroded · Mar 1, 2022 · N244SY · Emb ERJ170200LR · Fuselage Internal Stairs
  > FWD WET AREA RIGHT STILL AT FR 14 HAS CORROSION ON AFT LH CORNER (C-CHECK RO 03-19-2022) REMOVED AND REPLACED FWD WET AREA RIGHT SILL AT FR 14 REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06 AND CPM 51-25-00910-001-A
- [SDR SWIA202265124](https://openairdocs.org/sdr/SWIA202265124.md): None · chafed · Mar 1, 2022 · N244SY · Emb ERJ170200LR · Doors
  > FWD CARGO DOOR 2 EACH INTERNAL STUD RECEPTACLES BRACKETS CHAFED (C-CHECK RO 03-19-2022) REMOVED AND REPLACED FWD CARGO DOOR 2 EACH INTERNAL STUD RECEPTACLES REF EMB SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06. APPLIED CIC REF CPM 51-25-00-91
- [SDR SWIA202265121](https://openairdocs.org/sdr/SWIA202265121.md): None · corroded · Mar 1, 2022 · N244SY · Emb ERJ170200LR · Fuselage Main, Bulkhead
  > AFT WET AREA SHEAR CLIP CORRODED AT FR 85 AND 28R (C-CHECK RO 03-19-2022) REMOVED AND REPLACED SHEAR CLIP AT FRAME 85, BETWEEN STRINGER 27R - 28R, REF EMB175 SRM 51-40-08, SEE CONTINUATION CARD FOR WORK PERFORMED. PART REPLACED WITH OEM PART NO CHANGE TO W
- [SDR SWIA202265120](https://openairdocs.org/sdr/SWIA202265120.md): None · corroded · Mar 1, 2022 · N244SY · Emb ERJ170200LR · Fuselage Main, Bulkhead
  > CORROSION ON SHEAR CLIP AT FR88 BETWEEN STGR 27R-28R. (C-CHECK RO 03-19-2022) REMOVED AND REPLACED SHEAR CLIP AT FRAME 88 BETWEEN STRINGERS 27R AND 28R REF EMB175 SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED.PART CHANGE WITH OEM PART NO CHANGE TO
- [SDR SWIA202265119](https://openairdocs.org/sdr/SWIA202265119.md): None · corroded · Mar 1, 2022 · N244SY · Emb ERJ170200LR · Fuselage Main, Bulkhead
  > CORROSION ON SHEAR CLIP AT FR87 BETWEEN STGR 27R-28R. (C-CHECK RO 03-19-2022) REMOVED AND REPLACED SHEAR CLIP AT FRAME 87 BETWEEN STRINGERS 27R AND 28R REF EMB175 SRM 51-40-08. SEE CONTIUATION CARD FOR WORK PERFORMED. PART REPLACED WITH OEM PART NO CHANGE
- [SDR SWIA202265132](https://openairdocs.org/sdr/SWIA202265132.md): None · failed · Feb 28, 2022 · N244SY · Emb ERJ170200LR · Elevator Tab, Attach Fittings
  > RH ELEVATOR OUTBOARD PCU FAILS BACKLASH FUNCTIONAL TEST. (C-CHECK RO 03-19-2022) REPLACED HARDWARE TO THE R/H ELEVATOR O/B PCU TO ELEVATOR ATTACH POINT ON RACK. REF. E175 AMM 27-32-01. REACOMPLISHED RH ELEVATOR BACKLASH FUNCTIONAL TEST FOR RH ELEVATOR OUTB
- [SDR SWIA202265133](https://openairdocs.org/sdr/SWIA202265133.md): None · failed · Feb 27, 2022 · N244SY · Emb ERJ170200LR · Elevator Tab, Attach Fittings
  > RH ELEVATOR INBOARD PCU FAILS BACKLASH FUNCTIONAL TEST. (C-CHECK RO 03-19-2022) / REPLACED HARDWARE TO THE R/H ELEVATOR I/B PCU TO ELEVATOR ATTACH POINT ON RACK. REF. E175 AMM 27-32-01. REACOMPLISHED RH ELEVATOR BACKLASH FUNCTIONAL TEST FOR RH ELEVATOR IN
- [SDR SWIA202265123](https://openairdocs.org/sdr/SWIA202265123.md): None · gouged · Feb 27, 2022 · N244SY · Emb ERJ170200LR · Fuselage Structure (General)
  > FWD AVIONICS DOOR FRAME IS GOUGED AT 3EA STOPS. (C-CHECK RO 03-19-2022) / REMOVED AND REPLACED RWD AVIONICS DOOR FRAME REF SRM 51-40-08. RESTORED SURFACE PROTECION REF SRM 51-23-04. 51-23-05, 51-23-06.
- [SDR SWIA202265122](https://openairdocs.org/sdr/SWIA202265122.md): None · chafed · Feb 27, 2022 · N244SY · Emb ERJ170200LR · Nacelle/Pylon, Frame/Spar/Rib
  > L/H AFT PYLON FWD FRAME CHAFED INBD AND OTBD SIDES (C-CHECK RO 03-19-2022) / REMOVED AND REPLACED L/H AFT PYLON FWD FRAME 1 REF EMB SRM 51-40-08
- [SDR SWIA202265118](https://openairdocs.org/sdr/SWIA202265118.md): None · dented · Feb 26, 2022 · N244SY · Emb ERJ170200LR · Fuselage Structure (General)
  > DENT FORWARD FUSELAGE LOWER SKIN BETWEEN FR18 - FR19 AND BETWEEN STRG 27R - STRG 28R. (C-CHECK RO 3-19-2022) REPAIRED FORWARD FUSELAGE LOWER SKIN BETWEEN FR18-19 AND BETWEEN STRG 27R-28R REF SRM 53-10-01/ REPAIR 08P.

## 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 = 'N244SY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N244SY/reports

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