# Service difficulty reports: N168SY

A list on [N168SY](https://openairdocs.org/aircraft/N168SY.md).

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

- [SDR SWIA2026100277475](https://openairdocs.org/sdr/SWIA2026100277475.md): Pin · installed · Oct 2, 2026 · N168SY · Emb ERJ170200LR · Nose/Tail Landing Gear
  > MLG LEVEL DISAGREE ON GEAR RETRACTION, NOSE GEAR DID NOT RETRACT. RETURNED TO FIELD AND DISCOVERED GEAR PIN WITHOUT A FLAG IN THE NOSE GEAR. INSTALLED NEW FLAG ON PIN IAW 32-00-05-000-801A, VERIFIED ALL THREE PINS ARE IN FLIGHT DECK AND HAVE FLAGS INSTALLED A
- [SDR SWIA2025092900026](https://openairdocs.org/sdr/SWIA2025092900026.md): Pitot Tube · damaged · Sep 26, 2025 · N168SY · Emb ERJ170200LR · Pitot/Static System
  > HIT BIRD ON TAKE OFF (FLIGHT 5761 - FILED CLOSED)CLEANED BIRD REMAINS AND PERFORMED BIRD STRIKE INSPECTION PER ERJ175 AMM 05-50-02.FOUND DAMAGE TO INTEGRATED PITOT/STATIC SENSOR 4. PLEASE REFERENCE EAML 1713879 FOR WORK PERFORMED ON PITOT/STATIC SENSOR 4.NO F
- [SDR SWIA202507030623](https://openairdocs.org/sdr/SWIA202507030623.md): Valve · faulted · Jun 23, 2025 · N168SY · Emb ERJ170200LR · Compressor Bleed Valve
  > AIRCRAFT SUFFERED LOSS OF PRESSURIZATION TWICE. BLEED 2 FAIL CAUTION IN FLIGHT OCCURRED TWICE. BOTH AT FL220. RAN QRH FOR BOTH OCCURRENCES. CAUTIONS AND ADVISORIES PRESENT USING EVENT WERE: ICE CONDITION, PACK 1 OFF, BLEED 2 FAIL. (FLIGHT 5746 - FILED CLOSED)
- [SDR SWIA202506240023](https://openairdocs.org/sdr/SWIA202506240023.md): Cabin Pressure · malfunctioned · Jun 23, 2025 · N168SY · Emb ERJ170200LR · Cabin Pressure Control System
  > AIRCRAFT SUFFERED LOSS OF PRESSURIZATION TWICE. BLEED 2 FAIL CAUTION IN FLIGHT OCCURRED TWICE. BOTH AT FL220. RAN QRH FOR BOTH OCCURRENCES. CAUTIONS AND ADVISORIES PRESENT USING EVENT WERE: ICE CONDITION, PACK 1 OFF, BLEED 2 FAIL. (FLIGHT 5746 - FILED OPEN)TH
- [SDR SWIA20250616529](https://openairdocs.org/sdr/SWIA20250616529.md): Shear Tie · corroded · May 29, 2025 · N168SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORRODED SHEAR CLIP FR85 STR 28R. (FILED CLOSED) (C-CHECK RO 06/14/2025)REMOVED AND REPLACED SHEAR CLIP AT FR 85 STGR 27R-28R WITH NEW REF. ERJ175 SRM 51-40-08. REPLACED WITH OEM PART, NO CHANGE TO WEIGHT AND BALANCE. SEE CONTINUATION CARD FOR FURTHER WORK PER
- [SDR SWI2025F00695](https://openairdocs.org/sdr/SWI2025F00695.md): Shear Tie · corroded · May 29, 2025 · N168SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORRODED SHEAR CLIP FR85 STR 28R. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWI2025F00734](https://openairdocs.org/sdr/SWI2025F00734.md): Seat Track · corroded · May 27, 2025 · N168SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > LH SEAT TRACK CORRODED IN 11 SPOTS AS MARKED FR 73-85 (C-CHECK RO 06/14/2025)PERFORMED LH SEAT TRACK SPLICE REPAIR BETWEEN FR 83 - FR 84 REF. ETD2022-170-022163 REV. C. SEE CONTINUATION CARD FOR WORK PERFORMED. THIS REPAIR DOES NOT CHANGE WEIGHT AND BALANCE.
- [SDR SWI2025F00733](https://openairdocs.org/sdr/SWI2025F00733.md): Rib · cracked · May 27, 2025 · N168SY · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > LH HORIZONTAL STAB RIB 11 HAS SUSPECTED CRACK ON UPPER SIDE AT 5TH FROM FWD FASTENER BETWEEN FRONT SPAR AND STRINGER2. (C-CHECK RO 06/14/2025)REMOVED AND REPLACED LH HORIZONTAL STAB RIB 11 REF SRM 51-40-08 AND ETD2025-170-922014 REV. A. SEE CONTINUATION CARD
- [SDR SWIA20250616527](https://openairdocs.org/sdr/SWIA20250616527.md): Rib · cracked · May 27, 2025 · N168SY · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > LH HORIZONTAL STAB RIB 12 HAS SUSPECTED CRACK ON UPPER SIDE AT 4TH FROM FWD FASTENER BETWEEN FRONT SPAR AND STRINGER2. (C-CHECK RO 06/14/2025)REMOVED AND REPLACED LH HORIZONTAL STAB RIB 12 REF SRM 51-40-08 AND ETD2025-170-922014 REV. A. SEE CONTINUATION CARD
- [SDR SWI2025F00732](https://openairdocs.org/sdr/SWI2025F00732.md): Seat Track · gouged · May 24, 2025 · N168SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > LH OB SEAT TRACK GOUGED FROM FR 23 TO FR 34 (C-CHECK RO 06/14/2025)REMOVED AND REPLACED LH OB SEAT TRACK FROM FR 23 TO FR 34 REF. SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED. OEM PARTS CHANGE - NO CHANGE TO WEIGHT AND BALANCE NOTED.
- [SDR SWIA20250616524](https://openairdocs.org/sdr/SWIA20250616524.md): Seat Track · gouged · May 24, 2025 · N168SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > RH OB SEAT TRACK GOUGED FROM FR 22 TO FR 34 (C-CHECK RO 06/14/2025)REMOVED AND REPLACED RH OB SEAT TRACK BETWEEN FR 22 TO FR 34 REF SRM 51-40-08. FABRICATED NEW RH OB SEAT TRACK. REF: ETD2025-170922624 AND SPLICED IN REPLACED SEAT TRACK SEGMENTS, REF ETD20
- [SDR SWIA20250616523](https://openairdocs.org/sdr/SWIA20250616523.md): Skin · cracked · May 23, 2025 · N168SY · Emb ERJ170200LR · Wing, Plate/Skin
  > LH WING LOWER SKIN PANEL HAS EVIDENCE OF CRACK AS MARKED BETWEEN RIB 2 AND 3 FORWARD OF MLG CUTOUT AFT OF SPAR II. (C-CHECK RO 06/14/2025)CUT OUT DAMAGED SECTION OF L/H LOWER WING SKIN. FABRICATED AND INSTALLED FILLER/DOUBLER TRIPLER REPAIR ON L/H WING LOWER
- [SDR SWI2025F00731](https://openairdocs.org/sdr/SWI2025F00731.md): Skin · corroded · May 23, 2025 · N168SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > WASTER SERVICE DOOR CUTOUT CORRODED ON INSIDE EDGE (C-CHECK RO 06/14/2025)REMOVED AND REPLACED WASTE BOX DOUBLER WITH NEW REF. ERJ175 SRM 51-40-08. REPLACED WITH OEM PART, NO CHANGE TO WEIGHT AND BALANCE. SEE CONTINUATION CARD FOR FURTHER WORK PERFORMED.
- [SDR SWIA20250616505](https://openairdocs.org/sdr/SWIA20250616505.md): Skin · dented · May 5, 2025 · N168SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA79960-ETD2022-170-026072 MXCODEID63557-PR - DENT FOUND ON THE LH NOSE OF AIRCRAFT FWD OF #3 PROBE IN THE FWD UPPER CORNER OF RVSM AREA MEASURING WIDTH 4.0'' X LENGTH 3.375'' X DEPTH 0.125'' LOCATED BETWEEN STRG-12L TO
- [SDR SWIA20230916](https://openairdocs.org/sdr/SWIA20230916.md): Seat Track · damaged · Sep 16, 2023 · N168SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > THE SEAT TRACK AT SEATS 20C & 22C ARE DAMAGED. (FILED CLOSED) REMOVED AND REPLACED THE SEAT TRACK AT SEATS 20C & 22C IN REF TO AMM 25-21-11
- [SDR SWIA202265535](https://openairdocs.org/sdr/SWIA202265535.md): None · corroded · Apr 12, 2022 · N168SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > L/H FLOOR BEAM HAS AREAS OF CORROSION BETWEEN FRAMES 86/89. (C-CHECK RO 4/27/2022) REMOVED AND REPLACED LH FLOOR BEAM BETWEEN FRAMES 86/89. WEIGHT AND BALANCE NOT EFFECTIVE. REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06 AND CIC PROTECTI
- [SDR SWIA202265534](https://openairdocs.org/sdr/SWIA202265534.md): None · corroded · Apr 12, 2022 · N168SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > R/H FLOOR BEAM HAS AREAS OF CORROSION BETWEEN FRAMES 86/89. (C-CHECK RO 4/27/2022) REMOVED AND REPLACED R/H FLOOR BEAM BETWEEN FRAMES 86-89. SEE CONTINUATION CARD FOR WORK PERFORMED. / REF SRM 51-40-08 SRM 51-40-02
- [SDR SWIA202265537](https://openairdocs.org/sdr/SWIA202265537.md): None · corroded · Apr 11, 2022 · N168SY · Emb ERJ170200LR · Fuselage Structure (General)
  > L/H FLOOR DOUBLER HAS CORROSION ON AFT INBOARD SURFACE LOCATED AT FRAME 15. (C-CHECK RO 4/27/2022) REMOVED AND REPLACED CORRODED L/H FLOOR DOUBLE AT FRAME 15 REF SRM 51-40-08 SEE CONTINUE CARD FOR WORK ACCOMPLISHED
- [SDR SWIA202265536](https://openairdocs.org/sdr/SWIA202265536.md): None · corroded · Apr 11, 2022 · N168SY · Emb ERJ170200LR · Fuselage Main, Frame
  > R/H SPLICE PLATE HAS AREAS OF CORROSION ON UPPER SURFACE LOCATED AT FRAME 89. (C-CHECK RO 4/27/2022) REMOVED AND REPLACED R/H SPLICE PLATE AT FR 89, REF SRM 51-40-08.
- [SDR SWIA202265533](https://openairdocs.org/sdr/SWIA202265533.md): None · corroded · Apr 11, 2022 · N168SY · Emb ERJ170200LR · Fuselage, Powerplant Attach Fittings
  > CORROSION ON FWD WET AREA R/H SEAT TRACK BETWEEN FR13 AND FR21 IN 4 LOCATIONS AS MARKED. (C-CHECK RO 4/27/2022) REMOVED AND REPLACED R/H SEAT TRACK BETWEEN FR 13-21. REF EMB SRM 51-40-08. SEE CONTINUATION FOR WORK PERFORMED.
- [SDR SWIA202265532](https://openairdocs.org/sdr/SWIA202265532.md): None · corroded · Apr 11, 2022 · N168SY · Emb ERJ170200LR · Fuselage, Powerplant Attach Fittings
  > L/H TRACK HAS CORROSION LOCATED AT FRAME 17. (C-CHECK RO 4/27/2022) REPAIRED L/H TRACK AT FR 17 REF SRM 53-10-10/REPAIR01P SEE CONTINUATION CARD ITEMS 1-10 FOR WORK ACCOMPLISHED
- [SDR SWIA202265538](https://openairdocs.org/sdr/SWIA202265538.md): Windshield · scratched · Apr 9, 2022 · N168SY · Emb ERJ170200LR · Window/Windshield System
  > D: RIGHT WINDSHIELD WIPER APPEARS TO BE SCRATCHING THE WINDSHIELD. / C: MCI / PERFORMED INSPECTION OF FO WINDSHIELD AND FOUND SCRATCH TO BE WITHIN LIMITS AT THIS TIME IN REF TO SRM 56-11-00, NO ACTION NEEDED (C-CHECK RO 4/27/2022) REPLACED RH WINDSHIELD

## 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 = 'N168SY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N168SY/reports

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