# Service difficulty reports: N106SY

A list on [N106SY](https://openairdocs.org/aircraft/N106SY.md).

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

- [SDR SWIA2026020275107](https://openairdocs.org/sdr/SWIA2026020275107.md): Check Valve · faulted · Jan 30, 2026 · N106SY · Emb ERJ170200LR · Landing Gear Retraction/Extension System
  > ON TAKEOFF FROM PSC, RT MAIN GEAR DID NOT COME UP ALL THE WAY. RECEIVED RED MLG LEVER DISAGREE MESSAGE. RT MLG STILL SHOWED RED. RAN QRH WITH GEAR LEVER DOWN, RECEIVED 3 GREEN. CYCLED GEAR AGAIN, RT MLG HUNG UP, NOT RETRACTING. (FLIGHT 4744) TROUBLESHOT ISSU
- [SDR SWI2025F01078](https://openairdocs.org/sdr/SWI2025F01078.md): Seat Track · corroded · Jul 21, 2025 · N106SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > FWD WET AREA L/H SEAT TRACK BETWEEN FR 12 - FR 18 CORRODED. (C-CHECK RO 08/10/2025)REMOVED AND REPLACED FWD WET AREA L/H SEAT TRACK BETWEEN FR 12 - FR 20 REF SRM 51-40-08. REPLACED WITH OEM PART AND DOES NOT EFFECT WEIGHT AND BALANCE.
- [SDR SWI2025F01077](https://openairdocs.org/sdr/SWI2025F01077.md): Beam · corroded · Jul 21, 2025 · N106SY · Emb ERJ170200LR · Fuselage Main, Structure
  > AFT WET AREA L/H BEAM BETWEEN FR 86 - FR 89 CORRODED. (C-CHECK RO 08/10/2025)REMOVED AND REPLACED AFT WET AREA L/H BEAM BETWEEN FR 86 - FR 89. REF EMB SRM 51-40-08.REPLACED WIRH OEM PART AND DOES NOT EFFECT WEIGHT AND BALANCE.
- [SDR SWI2025F01076](https://openairdocs.org/sdr/SWI2025F01076.md): Seat Track · corroded · Jul 21, 2025 · N106SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > FWD WET AREA R/H SEAT TRACK BETWEEN FR 12 - FR 18 CORRODED. (C-CHECK RO 08/10/2025)PERFORMED A SEAT TRACK UPPER CAP REPAIR AT FRAME 17 REF SRM 53-10-10/REPAIR 01P. SEE CONTINUATION CARD FOR WORKED PERFORMED.
- [SDR SWI2025F00735](https://openairdocs.org/sdr/SWI2025F00735.md): Unknown · odor · Jun 16, 2025 · N106SY · Emb ERJ170200LR · Air Distribution System
  > LAV SMOKE IN FLIGHT. ELECTRICAL SMELL. PAX DENIED SMOKING (FLIGHT 5433 - FILED CLOSED)UPON ARRIVAL TO AIRCRAFT COULD NOT VERIFY ANY ELECTRICAL SMELL IN FWD OR AFT LAVS. TROUBLESHOT PER ERJ-175 FIM 21-20-00 AND 26-14-00. NO DISCREPANCIES DURING INSPECTIONS. PER
- [SDR SWIA202265626](https://openairdocs.org/sdr/SWIA202265626.md): None · damaged · Apr 28, 2022 · N106SY · Emb EMB110* · Fuselage Structure (General)
  > WARRANTY: P/N 170-2365-02-401-111 STIFFENER, AFT ATG ANTENNA WAS MISS TRIMMED DURING ACCOMPLISHMENT OF TASK 1086:ERJ3095B-23-ERJ3095B-23. (C CHECK RO 5/20/22) AQUIRED NEW P/N 170-2365-02-401-111 STIFFENER TO REPLACE MISS TRIMMED ONE. REF CP # 24612025 FOR
- [SDR SWIA202265631](https://openairdocs.org/sdr/SWIA202265631.md): None · corroded · Apr 25, 2022 · N106SY · Emb EMB110* · Fuselage Internal Mounting Structure
  > RH FLOOR SILL PANEL SUPPORT CORRODED FR 88-90 (C CHECK RO 5/20/22) REMOVED AND REPLACED RH FLOOR SILL PANEL SUPPORTFR 88-90, REF SRM 51-40-08
- [SDR SWIA202265630](https://openairdocs.org/sdr/SWIA202265630.md): None · corroded · Apr 20, 2022 · N106SY · Emb EMB110* · Fuselage Main, Frame
  > SMALL AREAS OF CORROSION AROUND FASTENERS INSIDE FWD PAX DOOR FWD AND AFT GIRT BAR FITTING CUTOUTS (C CHECK RO 5/20/22) REMOVED AND REPLACED FWD PAX DOOR LOWER SILL BEAM WITH NEW REF. SRM 51-40-08. NO WEIGHT & BALANCE CHANGE DUE TO OEM REPLACEMENT PART.
- [SDR SWIA202265629](https://openairdocs.org/sdr/SWIA202265629.md): None · damaged · Apr 20, 2022 · N106SY · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > CORROSION ON SHEAR CLIP AS MARKED AT FR 86 STGR 29R-28R. (C CHECK RO 5/20/22) REMOVED AND REPLACED SHEAR CLIP AT FR 86 STGR 29R-28R REF EMB 170/175 SRM 51-40-08. REF CONTINUATION CARD FOR CORRECTIVE ACTION DETAILS.
- [SDR SWIA202265628](https://openairdocs.org/sdr/SWIA202265628.md): None · seized · Apr 20, 2022 · N106SY · Emb EMB110* · Doors
  > LH ELEVATOR #1, 2, AND 3 HINGE BOLTS AND FLOATING BUSHINGS ARE RUSTED/SEIZED. (C CHECK RO 5/20/22) REMOVED AND REPLACED LH ELEVATOR #1, 2, AND 3 HINGE BOLTS AND FLOATING BUSHINGS ON RACK. REF E175 AMM 27-31-05. FOR FINAL INSTALL, SEE CP# 24643379.
- [SDR SWIA202265627](https://openairdocs.org/sdr/SWIA202265627.md): None · seized · Apr 20, 2022 · N106SY · Emb EMB110* · Elevator Tab, Attach Fittings
  > RH ELEVATOR #1, 2, AND 3 HINGE BOLTS AND FLOATING BUSHINGS ARE RUSTED/SEIZED. (C CHECK RO 5/20/22) REMOVED AND REPLACED RH ELEVATOR #1, 2, AND 3 HINGE BOLTS AND FLOATING BUSHINGS ON RACK. REF E175 AMM 27-31-05. FOR FINAL INSTALL, SEE CP# 24643380
- [SDR SWIA202160111](https://openairdocs.org/sdr/SWIA202160111.md): Windshield · cracked · Aug 6, 2021 · N106SY · Emb ERJ170200LR · Flight Compartment Windows
  > CAPTAINS WINDSHIELD IS CRACKED. (FLIGHT 4732 - FILED CLOSED) REPLACED CAPT'S SIDE WINDSHIELD PER ERJ 175 AMM 56-11-00, PRESSURIZATION CHECK AND WINDSHIELD HEAT SYSTEMS OPERATE NORMALLY, NO LEAKS.
- [SDR SWIA202054141](https://openairdocs.org/sdr/SWIA202054141.md): Seat Track · cracked · Nov 20, 2020 · N106SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > THE INBOARD SEAT TRACK AT SEAT 17C IS CRACKED/BROKEN. FILED CLOSED. REMOVED AND REPLACED THE INBOARD SEAT TRACK AT SEAT 17C, IN REF TO ERJ175 AMM.
- [SDR SWIA2020072951491](https://openairdocs.org/sdr/SWIA2020072951491.md): Actuator · tripped · Jul 26, 2020 · N106SY · Emb ERJ170200LR · Trailing Edge Flap Actuator
  > FLAP FAIL CAUTION MESSAGE AFTER CLIMB OUT DURING FLAP RETRACTION. PERFORMED 0 FLAP LANDING. FLIGHT 5261 AFTER INSPECTION FOUND RH WING OUTBOARD FLAP ACTUATOR TORQUE INDICATOR TO BE TRIPPED.
- [SDR SWIA2020072751491](https://openairdocs.org/sdr/SWIA2020072751491.md): Actuator · malfunctioned · Jul 26, 2020 · N106SY · Emb ERJ170200LR · Trailing Edge Flap Actuator
  > FLAP FAIL CAUTION MESSAGE AFTER CLIMB OUT DURING FLAP RETRACTION. PERFORMED 0 FLAP LANDING. FLIGHT 5261. AFTER INSPECTION FOUND RT WING OUTBOARD FLAP ACTUATOR TORQUE INDICATOR TO BE TRIPPED. PLEASE REFERENCE AML 461476 FOR FAIRING REMOVAL. PLEASE REFERENC
- [SDR SWIA2019080746148](https://openairdocs.org/sdr/SWIA2019080746148.md): Shear Panel · corroded · Jul 16, 2019 · N106SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION - CENTER SHEAR PANEL. (C-CHECK) RO: 08/02/2019 REMOVED AND INSTALLED NEW CENTER SHEAR PANEL IAW SRM.
- [SDR SWIA2019080746147](https://openairdocs.org/sdr/SWIA2019080746147.md): Shear Panel · corroded · Jul 16, 2019 · N106SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION - LH SHEAR PANEL. (C-CHECK) RO: 08/02/2019 REMOVED AND INSTALLED NEW LH CENTER SHEAR PANEL IAW SRM.
- [SDR SWIA2019080746146](https://openairdocs.org/sdr/SWIA2019080746146.md): Support · corroded · Jul 16, 2019 · N106SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION - PANEL SUPPORT FR85 RH. (C-CHECK) RO: 08/02/2019 REMOVED AND INSTALLED NEW PANEL SUPPORT AT FR 85 IAW SRM.
- [SDR SWIA2019080746145](https://openairdocs.org/sdr/SWIA2019080746145.md): Shear Panel · corroded · Jul 16, 2019 · N106SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION - RH SHEAR PANEL. REMOVED AND INSTALLED NEW RH SHEAR PANEL IAW SRM.
- [SDR SWIA2019080746144](https://openairdocs.org/sdr/SWIA2019080746144.md): Support · corroded · Jul 16, 2019 · N106SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION - FR84 AT RH SILL. REMOVED AND REPLACED RH SILL AT FR 84 IAW SRM.
- [SDR SWIA2019080746143](https://openairdocs.org/sdr/SWIA2019080746143.md): Beam · corroded · Jul 16, 2019 · N106SY · Emb ERJ170200LR · Fuselage Main, Structure
  > CORROSION - RH BEAM AT FR87. REMOVED AND REPLACED WITH NEW RH BEAM AT FR87. IAW SRM.
- [SDR SWIA2019080746142](https://openairdocs.org/sdr/SWIA2019080746142.md): Support · corroded · Jul 16, 2019 · N106SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION - FR88 LH PANEL SUPPORT. REMOVED AND REPLACED WITH NEW LT SILL AT FR 88.IAW SRM.
- [SDR SWIA2019080746141](https://openairdocs.org/sdr/SWIA2019080746141.md): Upper Sheet · corroded · Jul 16, 2019 · N106SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION - RH UPPER SHEET. REMOVED AND REPLACED WITH NEW RH UPPER SHEET IAW SRM.
- [SDR SWIA2019080746140](https://openairdocs.org/sdr/SWIA2019080746140.md): Beam · corroded · Jul 16, 2019 · N106SY · Emb ERJ170200LR · Fuselage Main, Structure
  > CORROSION - LH BEAM AT FR87. REMOVED CORROSION AND INSTALLED A NEW LH BEAM AT FR 87. IAW SRM.
- [SDR SWIA2019080746139](https://openairdocs.org/sdr/SWIA2019080746139.md): Floor Support · corroded · Jul 16, 2019 · N106SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION - LH FLOOR SPLICE FRAMES 87/88. REMOVED AND INSTALLED A NEW LH FLOOR SPLICE AT FR 87/88. IAW SRM.
- [SDR SWIA201743889](https://openairdocs.org/sdr/SWIA201743889.md): Switch · failed · Oct 23, 2017 · N106SY · Emb ERJ170200LR · Landing Gear Brake System
  > DURING FLIGHT, THE PARK BRAKE ON LIGHT ILLUMINATED INTERMITTENTLY AND THEN RECEIVED A PARKING BRAKE NOT RELEASED CAUTION MESSAGE.. DECLARED EMERGENCY. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE PARKING BRAKE SWITCH NR 2 IAW AMM. OPS AND LEAK CHEC
- [SDR SWIA2017091943777](https://openairdocs.org/sdr/SWIA2017091943777.md): Actuator · failed · Sep 15, 2017 · N106SY · Emb ERJ170200LR · Autopilot System
  > ON INITIAL DESCENT, CREW RECEIVED A PITCH TRIM FAIL CAUTION MESSAGE. RAN QRH AND MESSAGE WOULD NOT RESET. DECLARED AN EMERGENCY. REMOVED AND REPLACED HS ACE IAW AMM. OPS CHECKED GOOD.
- [SDR SWIA201641940](https://openairdocs.org/sdr/SWIA201641940.md): Warning Message · false activation · Mar 11, 2016 · N106SY · Emb ERJ170200LR · Trailing Edge Flap Control System
  > FLAP FAIL CAUTION MESSAGE. C/W FIM. MESSAGE CLEARED, NO FURTHER FAULTS NOTED.
- [SDR SWIA201541606](https://openairdocs.org/sdr/SWIA201541606.md): A/C Pack · failed · Nov 19, 2015 · N106SY · Emb ERJ170200LR · Cabin Cooling System
  > CREW RECEIVED A BLEED 1 OVERPRESSURE CAUTION MESSAGE AFTER TAKEOFF THAT WOULD NOT CLEAR. DECLARED EMERGENCY, RETURNED TO FIELD. C/W FIM PROCEDURES. FOUND THAT PACK 1 WAS PREVIOUSLY DEFERRED IAW THE FIM, ALL FAULTS CLEARED AND OPS NORMAL.
- [SDR SWIA201437936](https://openairdocs.org/sdr/SWIA201437936.md): Fms · malfunctioned · May 22, 2014 · N106SY · Emb ERJ170200LR · Auto Flight System
  > ON MISSED APPROACH, THE FMS PITCHED FOR AN UN COMMANDED SPEED OF 140-150 KIAS. WOULD NOT RESPOND TO MANUAL OR FMS SELECTED SPEEDS. ONCE A VERTICAL MODE WAS SELECTED (FPA) THE FWD PITCHED FOR COMMANDED PITCH. THEN ON DESCENT THE FMS SPEED SWITCHED FROM THE 2

## 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 = 'N106SY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N106SY/reports

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