# Service difficulty reports: N138SY

A list on [N138SY](https://openairdocs.org/aircraft/N138SY.md).

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

- [SDR SWIA2026020575238](https://openairdocs.org/sdr/SWIA2026020575238.md): Rib · cracked · Feb 5, 2026 · N138SY · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > RIGHT HORIZONTAL RIB 12A CRACKED. REPAIRED RT HORIZONTAL RIB 12A AT INDICATED AREA. PERFORMED ETD 2026-170-002239.
- [SDR SWIA2026012075243](https://openairdocs.org/sdr/SWIA2026012075243.md): Seat Track · gouged · Jan 20, 2026 · N138SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > FORWARD WET AREA RT SEAT TRACK SEGMENT AT FR 17 - 22 GOUGED. REMOVED AND REPLACED FWD WET AREA RT INBD SEAT TRACK IAW SRM 51-40-08.
- [SDR SWIA2026021375241](https://openairdocs.org/sdr/SWIA2026021375241.md): Seat Track · gouged · Jan 20, 2026 · N138SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > FORWARD WET AREA, LT SEAT TRACK SEGMENT AT FR 19/22 GOUGED. REPAIRED FWD LT SEAT TRACK AT FR 19/22 BY CUT OUT AND INSTALLATION OF REPAIR FILLER AND DOUBLER. IAW SRM 53-10-10/AD01.
- [SDR SWIA2026021375242](https://openairdocs.org/sdr/SWIA2026021375242.md): Floorbeam · corroded · Jan 19, 2026 · N138SY · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > CORROSION, AFT WET AREA AROUND RIVET HEAD ON LH LONGITUDINAL FLOORBEAM AT FRAME 87 WHERE THE BEAM PASSES BETWEEN THE LT AND CENTER SHEAR PANELS REMOVED AND REPLACED LT LONGITUDINAL FLOORBEAM AT FRAME 87. IAW SRM 51-40-08.
- [SDR SWIA2026021375236](https://openairdocs.org/sdr/SWIA2026021375236.md): Angle · corroded · Jan 19, 2026 · N138SY · Emb ERJ170200LR · Fuselage Main, Structure
  > CORROSION IN FORWARD CLIP AT AFT DRAIN MAST BETWEEN FR.86-87. REMOVED AND REPLACED FORWARD CLIP AT AFT DRAIN MAST BETWEEN FR.86-87 IAW SRM 51-40-08.
- [SDR SWIA2026011875244](https://openairdocs.org/sdr/SWIA2026011875244.md): Backboard · cracked · Jan 18, 2026 · N138SY · Emb ERJ170200LR · Escape Slide
  > AFT SERVICE DOOR EVACUATION SLIDE COMPOSITE BACK HAS A HAIRLINE CRACK. REMOVED AND REPLACED THE AFT SERVICE DOOR EVACUATION SLIDE IAW AMM 25-65-01. SEE CP 31491850 FOR GIRTBAR ADJUSTMENT VERIFICATION.
- [SDR SWIA2026011875237](https://openairdocs.org/sdr/SWIA2026011875237.md): Doubler · corroded · Jan 18, 2026 · N138SY · Emb ERJ170200LR · Fuselage Main, Structure
  > CENTER FUSELAGE III WASTE SERVICE DOOR CUTOUT INTERNAL DOUBLER CORRODED INBD CORNER. REMOVED AND REPLACED CENTER FUSELAGE III WASTE SERVICE DOOR CUTOUT INTERNAL DOUBLER IAW SRM 51-40-08, RESTORED SURFACE PROTECTION IAW SRM 51-23-04, SRM 51-23-05, SRM 51-23-0
- [SDR SWIA2026021375240](https://openairdocs.org/sdr/SWIA2026021375240.md): Rib · cracked · Jan 17, 2026 · N138SY · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > SUSPECTED CRACK RT HORIZONTAL RIB 11A FORWARD UPPER FLANGE AT AFT RIVET HOLE. REMOVED AND RELACED THE RT HORIZONTAL RIB 11A ON THE RT HORIZONTAL. IAW SRM 51-40-08. PERFORMED.TASK CARD 27-31-05-001-SKY-U,
- [SDR SWIA2026021375239](https://openairdocs.org/sdr/SWIA2026021375239.md): Skin · cracked · Jan 17, 2026 · N138SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > HFEC CONFIRMED CRACK RT LOWER SKIN JUST FORWARD OF RT LANDING GEAR WHEEL WELL CUT OUT AT RIB 3. PERFORMED CRACK REPAIR AT RIB 3 JUST FORWARD OF LANDING GEAR CUTOUT ON RIGHT WING LOWER SKIN IAW ETD2026-170-001158. REPAIR PARTS WEIGHED LESS THAN 2.5 LBS, NO WEI
- [SDR SWIA202310100008](https://openairdocs.org/sdr/SWIA202310100008.md): Unknown · pressure loss · Oct 8, 2023 · N138SY · Emb ERJ170200LR · Air Conditioning System
  > CLIMBING OUT OF ONTARIO ON THE SUNSHINE DEPARTURE, AT APPROX 4000 FEET, THE AUTO THROTTLES KICKED OFF. ATTEMPTED TO RE-ARM BUT DID NOT COME BACK ON. WE DECIDED TO HAND FLY THE REST OF THE WAY TO SFO. AT APPROXIMATELY 12,000 FEET, NOTICED MY EARS POPPING AND
- [SDR SWIA202302023](https://openairdocs.org/sdr/SWIA202302023.md): None · gouged · Feb 2, 2023 · N138SY · Emb ERJ170200LR · Fuselage Structure (General)
  > RH SIDEWALL SEAT TRACK 74/84 IS GOUGED AFT OF FRAME 78, 82 AND 83. (C-CHECK RO 2/20/2023) REMOVED AND REPLACE DAMAGED RG SIDEWALL SEAT TRACK AFT OF FR80 IAW ETD2023-170-003067. RESTORED SURFACE PROTECTION IAW SRM 51-23-05. APPLIED CIC IAW CPM 51-25-00-9
- [SDR SWIA202302022](https://openairdocs.org/sdr/SWIA202302022.md): None · gouged · Feb 2, 2023 · N138SY · Emb ERJ170200LR · Fuselage Structure (General)
  > LH FLOOR SEAT TRACK 74/84 IS GOUGED AFT OF FLOOR BEAMS 75, 76(2), 77, 78, 81, 82 AND 83. (C-CHECK RO 2/20/2023) REMOVED AND REPLACED LH FLOOR SEAT TRACK BETWEEN FR 74-84 WITH NEW. REF SRM 51-40-08. WEIGHT AND BALANCE NOT AFFECTED, SEE CONTINUATION CARD
- [SDR SWIA202302021](https://openairdocs.org/sdr/SWIA202302021.md): None · gouged · Feb 2, 2023 · N138SY · Emb ERJ170200LR · Fuselage Structure (General)
  > RH FLOOR SEAT TRACK 74/84 IS GOUGED AFT OF FLOOR BEAMS 73, 74, 75, 76(2), 77(2), 78, 79, 80, 81, 82, 83 AND AT THE END OF OF SEAT TRACK AFT OF 84. (C-CHECK RO 2/20/2023) REMOVED AND REPLACED RH FLOOR SEAT TRACK BETWEEN FR 74-84 REF SRM 51-40-08. WEIGHT
- [SDR SWIA202302012](https://openairdocs.org/sdr/SWIA202302012.md): None · dented · Feb 1, 2023 · N138SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > PROTRUDING DENT FOUND ON REAR FUSELAGE SIDE SKIN PANEL BETWEEN FR93 AND FR94, AND BETWEEN STGR 19RH AND STGR 21RH. (C-CHECK RO 2/20/2023) PERFORMED PERMANENT REPAIR TO PROTRUDING DENT FOUND ON REAR FUSELAGE SIDE SKIN PANEL BETWEEN FR93 AND FR94, AND BET
- [SDR SWIA202301311](https://openairdocs.org/sdr/SWIA202301311.md): None · gouged · Jan 31, 2023 · N138SY · Emb ERJ170200LR · Fuselage Structure (General)
  > GOUGES ON R/H SIDEWALL SEAT TRACK BETWEEN FR43-60 IN 14 LOCATIONS AS MARKED. (C-CHECK RO 2/20/2023) REMOVED GOUGES BY BLENDING. FOUND ALL WITHIN LIMITS EXCLUDING FR 57 COMPLIED WITH SPLICE DEVICE REPAIR ON FR 57. REF SRM 53-00-10 AND ETD 2022-170-022-16
- [SDR SWIA202301302](https://openairdocs.org/sdr/SWIA202301302.md): None · corroded · Jan 30, 2023 · N138SY · Emb ERJ170200LR · Fuselage Structure (General)
  > L/H TRACK BEAM HAS CORROSION AT FRAME 16. (C-CHECK RO 2/20/2023) PERFORMED CUTOUT REPAIR OF THE L/H TRACK BEAM AT FRAME 16, REF EMB175 SRM 53-10-10/REPAIR 01P. NO WEIGHT AND BALANCE CHANGE REQUIRED DUE TO REPAIR PARTS WEIGHING LESS THAN 2.5 LBS.
- [SDR SWIA20230127](https://openairdocs.org/sdr/SWIA20230127.md): None · damaged · Jan 27, 2023 · N138SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > INBOUND EVALUATION OF HAIL DAMAGE TO THE FWD FUSELAGE LEFT HAND SKIN (P/N 170-03385-003) FOUND TO BE BEYOND ECONOMICAL REPAIR. (C-CHECK RO 2/20/2023) REMOVED AND REPLACED FWD FUSELAGE L/H SKIN (P/N 170-03385-003) REF EMB 175 SRM 51-40-08. THIS ACTION DO
- [SDR SWIA202002048217](https://openairdocs.org/sdr/SWIA202002048217.md): Threshold · corroded · Jan 21, 2020 · N138SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > FWD PAX THRESHOLD LOWER BEAM CORRODED (C-CHECK) RO 2/02/2020 REMOVED AND REPLACED FWD PAX THRESHOLD LOWER BEAM REF EMB SRM.
- [SDR SWIA202002048216](https://openairdocs.org/sdr/SWIA202002048216.md): Plate · corroded · Jan 16, 2020 · N138SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION LOCATED AT LH SPLICE PLATE FR 85 (C-CHECK) RO 2/02/2020 REMOVED AND REPLACED AND REPLACED LH SPLICE PLATE FR 85 REF SRM.
- [SDR SWIA202002048215](https://openairdocs.org/sdr/SWIA202002048215.md): Seat Track · corroded · Jan 16, 2020 · N138SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION LOCATED ON RH SEAT TRACK AT FR 85 (C-CHECK) RO 2/02/2020 BLENDED DAMAGED AREA ON RH SEAT TRACK AT FR 85 REF SRM. REPAIRED DAMAGED AREA REF ETD. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA202002048214](https://openairdocs.org/sdr/SWIA202002048214.md): Seat Track · corroded · Jan 16, 2020 · N138SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION LOCATED ON LH SEAT TRACK AT FR 85 (C-CHECK) RO 2/02/2020 BLENDED DAMAGED AREA ON LH SEAT TRACK AT FR 85 REF SRM. REPAIRED DAMAGED AREA REF ETD. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA202002048213](https://openairdocs.org/sdr/SWIA202002048213.md): Beam · corroded · Jan 16, 2020 · N138SY · Emb ERJ170200LR · Fuselage Main, Structure
  > CORROSION ON INTERCOSTAL BEAM BEHIND FR 90 Y=+10.748" (C-CHECK) RO 2/02/2020 REMOVED AND REPLACED INTERCOASTAL BEAM BEHIND FR 90 Y=+10.748". REF SRM.
- [SDR SWIA202002048212](https://openairdocs.org/sdr/SWIA202002048212.md): Plate · corroded · Jan 16, 2020 · N138SY · Emb ERJ170200LR · Fuselage Main, Frame
  > CORROSION AT LH SPLICE PLATE BETWEEN FR 87-88 (C-CHECK) RO 2/02/2020 REMOVED AND REPLACED LH SPLICE PLATE BETWEEN FR 87-88 DUE TO100 PERCENT MATERIAL LOSS REF SRM.
- [SDR SWIA202002048211](https://openairdocs.org/sdr/SWIA202002048211.md): Plate · corroded · Jan 16, 2020 · N138SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > RH SPLICE PLATE BETWEEN FR 87-88 HAS CORROSION (C-CHECK) RO 2/02/2020 REMOVE AND REPLACED RH SPLICE PLATE BETWEEN FR 87-88 REF SRM.
- [SDR SWIA202002048209](https://openairdocs.org/sdr/SWIA202002048209.md): Rib · cracked · Jan 16, 2020 · N138SY · Emb ERJ170200LR · Fuselage Main, Structure
  > FR 52 SUPPORT RIB UPPER ATTACHMENT ANGLE IS CRACKED AT LH MLG WHEEL WELL AREA. (C-CHECK) RO 2/02/2020 REMOVED AND REPLACED FR52 SUPPORT RIB UPPER ATTACHMENT ANGLE AT FR52 LH MLG WHEEL WELL, REF. SRM.
- [SDR SWIA202002048210](https://openairdocs.org/sdr/SWIA202002048210.md): Door · corroded · Jan 14, 2020 · N138SY · Emb ERJ170200LR · Fluid Service Doors
  > CORROSION IN LAV. SERVICE DOOR INTERNAL/EXTERNAL SIDES. (C-CHECK) RO 2/02/2020 REMOVED AND REPLACED LAV. SERVICE DOOR REF AMM. ASSET # EAMS 7400 CAL DUE 4-10-20.
- [SDR SWIA201902048208](https://openairdocs.org/sdr/SWIA201902048208.md): Skin · dented · Dec 2, 2019 · N138SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: DENT ABOVE RADOME CENTERED BETWEEN THE WINDSHIELD 9' ABOVE RADOME DENT MEASURES 6"X 4.9" AND IS 0.1 INCHES IN DEPTH. COMPLIED WITH TEMPORARY REPAIR PER EMBRAER ETD PERMANENT REPAIR FOR 7500 CYCLES DUE BY TAC 9658, PART N

## 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 = 'N138SY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N138SY/reports

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