# Service difficulty reports: N232JQ

A list on [N232JQ](https://openairdocs.org/aircraft/N232JQ.md).

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

- [SDR R61A2025092700416](https://openairdocs.org/sdr/R61A2025092700416.md): Seal Rest · corroded · Sep 24, 2025 · N232JQ · Emb ERJ170200LR · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE VISIT UPON REMOVAL OF FWD CARGO FWD CORNER SEAL REST AND LATCH FITTING NOTED CORROSION ON DOOR BEAM. REMOVED AND REPLACED LOWER FWD CARGO DOOR BEAM. REF: EMB SRM 51-40-08.
- [SDR R61A2025092700415](https://openairdocs.org/sdr/R61A2025092700415.md): Rib · corroded · Sep 18, 2025 · N232JQ · Emb ERJ170200LR · Wing, Rib/Bulkhead
  > DURING HEAVY MAINTENANCE VISIT CORROSION FOUND AT RIB 4A DURING REMOVAL OF FASTNER RH WING AS SEEN THROUGH PANEL 622DB. REMOVED CORROSION FROM HOLE AT RIB 4A BY REAMING AND INSTALLED PERMANENT BUSHING REPAIR REF. ETD2025-170-928020.
- [SDR R61A2025092700414](https://openairdocs.org/sdr/R61A2025092700414.md): Skin · corroded · Sep 16, 2025 · N232JQ · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE VISIT CORROSION ON LOWER FUSELAGE SKIN AT FR 97-98, STGR 28R-29L. REPAIRED LOWER FUSELAGE SKIN AROUND IDENTIFICATION PLACARD AT FR 97-98, STGR 28R-29L PER ETD2025-170-927947 REV. A.
- [SDR R61A2023070800386](https://openairdocs.org/sdr/R61A2023070800386.md): Bushing · elongated · Jun 19, 2023 · N232JQ · Emb ERJ170200LR · Wing Main, Frame Structure
  > WHILE ACFT IN HEAVY CHECK AND PERFORMING 170EO-57-10-0017 F52 REINF & RR AILERON TORQUE TUBE SUPPORTS. FOUND 2EA. STUCK FASTENERS FOR REMOVAL THROUGH AILERON TORQUE TUBE SUPPORT FITTINGS. PERFORMED PERMANENT REPAIR BY REAMING HOLE AND FABRICATING AND INSTALLIN
- [SDR R61A2023070800387](https://openairdocs.org/sdr/R61A2023070800387.md): Beam · corroded · Jun 14, 2023 · N232JQ · Emb ERJ170200LR · Fuselage Structure (General)
  > AFT PAX DOOR CUTOUT LOWER BEAM IS CORRODED AS MARKED FR 85- FR 87. REMOVED AND REPLACED AFT PAX DOOR CUTOUT LOWER BEAM. REF EMB SRM 51-40-08
- [SDR R61A2023070800385](https://openairdocs.org/sdr/R61A2023070800385.md): Skin · dented · Jun 11, 2023 · N232JQ · Emb ERJ170200LR · Fuselage Structure (General)
  > R791276/1 TRANSFER FROM VP- 014782-2021 C1 & C2. DENT ON LH FWD FUSELAGE BETWEEN FRAME 6-7 STR 17L & 18L. DENT IS W=1.4", H=0.015", W/H= 93.- 333".GOUGE A DEPT. PERFORMED PERMANENT REPAIR BY CUTOUT AND DOUBLER REPAIR AT LH FWD FUSELAGE BETWEEN FRAME 6-7 STR 17
- [SDR R61A2023070800384](https://openairdocs.org/sdr/R61A2023070800384.md): Skin · cracked · Jun 11, 2023 · N232JQ · Emb ERJ170200LR · Wing Structure
  > CRACK RH WING BOTTOM SIDE AREA OF RIB 4A. PERFORMED TEMPORARY REPAIR ON RH WING LOWER SKIN AREA OF RIB 4A BY CUTTING OUT DAMAGE AND INSTALLING REPAIR FILLER AND DOUBLER. REF EMB ETD2023-170-014723.
- [SDR R61A2022112400741](https://openairdocs.org/sdr/R61A2022112400741.md): Doubler · corroded · Nov 18, 2022 · N232JQ · Emb ERJ170200LR · Fuselage Main, Structure
  > SKIN DOUBLER FOR WASTE BOX INBD FWD CORNER CORRODED. REMOVED AND REPLACED DOUBLER AND WASTE BOX IAW EMB SRM 51-42-02 AND 51-43-04. ALSO REF VP-050847-2022 N/R 1,9,12,13,14,15,16,17 FOR WORK ACCOMPLISHED.
- [SDR R61A2022061700395](https://openairdocs.org/sdr/R61A2022061700395.md): Processing Unit · failed · Jun 14, 2022 · N232JQ · Emb ERJ170200LR · Central Computers
  > AVNX MAU 2B FAIL IN FLIGHT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R NIC PROC MOD 4 LOCATED IN MAU 2 NIC 2.
- [SDR R61A202002220241](https://openairdocs.org/sdr/R61A202002220241.md): Seal Rest · corroded · Feb 9, 2020 · N232JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND FWD CARGO LOWER SEAL REST CORRODED BETWEEN FRAMES 25-26 AS MARKED. BLENDED OUT CORROSION ON FWD CARGO DOOR LOWER (CENTER) SEAL REST, IN ACCORDANCE WITH SRM 51-10-03. ORIGINAL THICKNESS 0.090", MATERIAL REMOVED 0.050", REMAI
- [SDR R61A202002220240](https://openairdocs.org/sdr/R61A202002220240.md): Doubler · corroded · Feb 9, 2020 · N232JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND RH COCKPIT FLOOR DOUBLER CORRODED AS MARKED FR 8-12. REMOVED DAMAGED PORTION OF RH COCKPIT FLOOR DOUBLER, AT FR 8-12. FABRICATED, LOCATED, DRILLED AND INSTALLED REPAIR SPLICE PIECES AND NEW PORTION OF RH COCKPIT DOUBLER, A
- [SDR R61A202002220239](https://openairdocs.org/sdr/R61A202002220239.md): Intercostal · corroded · Feb 8, 2020 · N232JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND FWD INTERCOSTAL FOR AFT DRAIN CORRODED FR 86/87 STR 27R/28R. REMOVED AND REPLACED FWD INTERCOSTAL FOR AFT DRAIN AT FR 86/87 BETWEEN STR 27R/28R PER SRM 51-40-08. RESTORED SURFACE PROTECTION PER SRM 51-23-26 CPM 51-25-00. A
- [SDR R61A202002220238](https://openairdocs.org/sdr/R61A202002220238.md): Shear Tie · corroded · Feb 8, 2020 · N232JQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND SHEAR CLIP FR88 STR 27R/28R CORRODED. REMOVED AND REPLACED SHEAR CLIP AT FR-88 BETWEEN STR 27R/28R PER SRM 51-40-08. RESTORED SURFACE PROTECTION TO FASTENERS PER SRM 51-23-06 AND CPM 51-25-00. A/C REMAINS IN CHECK.
- [SDR R61A202002220237](https://openairdocs.org/sdr/R61A202002220237.md): Shear Tie · corroded · Feb 8, 2020 · N232JQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND SHEAR CLIP FR 87 STR 27R/28R CORRODED. REMOVED AND REPLACED SHEAR CLIP AT FR87 BETWEEN STR 27R/28R PER SRM 51-40-08. TREATED, PRIMED AND TOP COATED FASTENERS PER SRM 51-23-06. A/C REMAINS IN CHECK.
- [SDR R61A202002220236](https://openairdocs.org/sdr/R61A202002220236.md): Finger Doubler · corroded · Feb 4, 2020 · N232JQ · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > DURING HEAVY CHECK MAINTENANCE FOUND FWD CARGO DOOR AFT FINGER DOUBLER CORRODED AS MARKED. BLENDED OUT CORROSION AT FWD CARGO DOOR AFT FINGER DOUBLER REF SRM 51-10-03. AREA OF REMOVAL LIS 4" X 1" WITH 0.004" REMOVED USING CAL. TOOL 61468 WITH CAL DUE DATE OF
- [SDR R61A202002220235](https://openairdocs.org/sdr/R61A202002220235.md): Finger Doubler · corroded · Feb 4, 2020 · N232JQ · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > DURING HEAVY CHECK MAINTENANCE FOUND FWD CARGO DOOR FWD FINGER DOUBLER CORRODED AS MARKED. REMOVED CORROSION BY BLENDING AT FWD CARGO DOOR FWD FINGER DOUBLER PER SRM 51-10-03. FOUND IN LIMITS PER ETD2020-170-005062. NOMINAL MAT 0.098'' MATERIAL REMOVED 0.030'
- [SDR R61A202002220234](https://openairdocs.org/sdr/R61A202002220234.md): Seat Track · corroded · Feb 3, 2020 · N232JQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY CHECK MAINTENANCE FOUND RH LATERAL SEAT TRACK FR 23-43 HAS CORROSION AT OR NEAR FRAME 30 AS MARKED. REMOVED CORROSION FROM RH LATERAL SEAT TRACK NEAR FR. 30 REF SRM 51-12-01. MATERIAL LOSS IS 0.012" WHICH HAS BEEN ACCEPTED AS ALLOWABLE DAMAGE REF
- [SDR R61A202002220233](https://openairdocs.org/sdr/R61A202002220233.md): Angle · corroded · Feb 3, 2020 · N232JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND CORRODED ANGLE 3 EA AND 3 EA CRACK RECEPTACLE ON PANEL 1441FR. REMOVED THE CORROSION ON THE ANGLE 3 ON THE 1441FR PANEL. THE BLENDED AREA IS 18.0" X 2.0" X.008". NOMINAL THICKNESS OF THE ANGLE IS 0.050". REMOVED AND REPLA
- [SDR R61A202002220231](https://openairdocs.org/sdr/R61A202002220231.md): Crossbeam · corroded · Feb 2, 2020 · N232JQ · Emb ERJ170200LR · Fuselage Main, Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON AFT WET AREA CROSSBEAM AT FR84 LBL 30" IN 2 LOCATIONS AS MARKED. PERFORMED CUTOUT AND INSTALLED REPAIR INNER DOUBLER, FILLER 2EA, AND SHIM AT CROSSBEAM FR 84 LBL 30'' REF ETD2020-170-003716 AND SRM 53-00-10 TA
- [SDR R61A202002220230](https://openairdocs.org/sdr/R61A202002220230.md): Splice Plate · corroded · Feb 2, 2020 · N232JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON AFT WET AREA SPLICE PLATE AT FR84 RBL 24" AS MARKED. REMOVED CORROSION ON AFT WET AREA SPLICE PLATE AT FR84 RBL 24" REF SRM 51-12-01 WITH A MAX MATERIAL LOSS OF.020" AND FOUND TO BE OUT OF LIMITS REF SRM 51-7
- [SDR R61A202002220229](https://openairdocs.org/sdr/R61A202002220229.md): Shear Panel · corroded · Feb 2, 2020 · N232JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON AFT WET AREA R/H SHEAR PANEL BETWEEN FR87 AND FR88 IN 3 LOCATIONS AS MARKED. REMOVED CORROSION ON AFT WET AREA R/H SHEAR PANEL BETWEEN FR87 AND FR88 REF SRM 51-12-01. MAX MATERIAL LOSS OF.030" AND FOUND TO BE
- [SDR R61A202002220228](https://openairdocs.org/sdr/R61A202002220228.md): Shear Panel · corroded · Feb 2, 2020 · N232JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON AFT WET AREA R/H SHEAR PANEL SPLICE PLATE BETWEEN FR87 AND FR88 IN 3 LOCATIONS AS MARKED. REMOVED CORROSION ON AFT WET AREA R/H SHEAR PANEL SPLICE PLATE BETWEEN FR87 AND FR-88 IN 3 LOCATIONS AS MARKED. MAX MATE
- [SDR R61A202002220227](https://openairdocs.org/sdr/R61A202002220227.md): Gusset · corroded · Feb 2, 2020 · N232JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND CORROSION AFT WET AREA GUSSET AT FR90 RBL 24" AS MARKED. REMOVED, REPLACED AFT WET AREAS GUSSET AT FR90 RBL 24'' AND APPLIED SURFACE PROTECTION TO AFT WET AREA GUSSET AT FR90 RBL 24" REF SRM 51-40-08, 51-23-04, 51-23-05, 5
- [SDR R61A202002220226](https://openairdocs.org/sdr/R61A202002220226.md): Splice Plate · corroded · Feb 2, 2020 · N232JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND CORROSION AFT WET AREA CENTER FLOOR SPLICE PLATE AT FR90 AS MARKED.REMOVED CORROSION ON PART# 170-86119-006, ON CENTER SPLICE PLATE IN AFT WET AREA FR90. NOMINAL THICKNESS OF.050" WITH MAX MATERIAL LOSS OF.008", AND FOUND
- [SDR R61A202002220225](https://openairdocs.org/sdr/R61A202002220225.md): Floor Splice · corroded · Feb 2, 2020 · N232JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND CORROSION AFT WET AREA FLOOR SPLICE AT FR90 LBL 11". REMOVED CORROSION IN AFT WET AREA FLOOR SPLICE AT FR90 LBL 11". PART#170-60257-001. NOMINAL THICKNESS OF.040" WITH MAX MATERIAL LOSS OF.020", AND FOUND TO BE OUT OF LI
- [SDR R61A202002220224](https://openairdocs.org/sdr/R61A202002220224.md): Support · corroded · Feb 2, 2020 · N232JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND CORROSION AFT WET AREA R/H AFT PANEL SUPPORT BETWEEN FR88 AND FR91 IN 4 LOCATIONS AS MARKED. REMOVED AND REPLACED AFT WET AREA R/ H AFT PANEL SUPPORT BETWEEN FR88 AND FR91 PER SRM 51-40-08. TREATED, PRIMED AND TOP COATED A
- [SDR R61A202002220223](https://openairdocs.org/sdr/R61A202002220223.md): Support · corroded · Feb 2, 2020 · N232JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND CORROSION AFT WET AREA L/H AFT PANEL SUPPORT BETWEEN FR88 AND FR90 IN 6 LOCATIONS AS MARKED. REMOVED AND REPLACED AFT WET AREA L/H AFT PANEL SUPPORT BETWEEN FR88 AND FR90 PER SRM 51-40-08. RESTORED SURFACE PROTECTION PER S
- [SDR R61A202002220220](https://openairdocs.org/sdr/R61A202002220220.md): Seat Track · corroded · Feb 2, 2020 · N232JQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY CHECK MAINTENANCE FOUND FWD WET AREA LH SEAT TRACK IS CORRODED BETWEEN FRAMES 17-20 AS MARKED. REMOVED CORROSION BY BLENDING AT FWD WET AREA LH SEAT TRACK BETWEEN FRAMES 17-20 PER SRM 51-10-03. FOUND TO BE IN LIMITS PER SRM 53-10-10/AD01AND ETD20
- [SDR R61A202002220222](https://openairdocs.org/sdr/R61A202002220222.md): Doubler · corroded · Feb 2, 2020 · N232JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND FWD WET CORROSION ON 9 HOLE DOUBLER FR13-16 AS MARKED. REMOVED CORROSION BY BLENDING AT 9 HOLE DOUBLER BETWEEN FRAMES 13-16 (FWD WET AREA). MATERIAL REMOVED:H-100% NOMINAL.050" REMAINING.000" OUT OF LIMITS. REF EMB SRM 5
- [SDR R61A202002160192](https://openairdocs.org/sdr/R61A202002160192.md): Seat Track · corroded · Feb 2, 2020 · N232JQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > WHILE IN HEAVY CHECK FOUND "FWD WET CORROSION ON RH SEAT TRACK FR12-17 (SEVERAL PLACES) AS MARKED. FABRICATED AND INSTALLED REPAIR DOUBLER AT FWD WET RH SEAT TRACK FR12-17 PER SRM 51--40-08 AND 53-10-10. RESTORED SURFACE PROTECTION PER SRM 51-23-06 PO# 259007
- [SDR R61A202002160191](https://openairdocs.org/sdr/R61A202002160191.md): Angle · corroded · Feb 2, 2020 · N232JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND "FWD WET AREA FFR14 RH CORRODED BETWEEN SEAT TRACK AND FWD SILL. PERFORMED CROSSBEAM 14 ''L'' ANGLE REPAIR PER SRM 53-00-10/REPAIR 03P AND 51-40-08.RESTORED SURFACE PROTECTION PER SRM 51-23-06 AND CPM 51-25-00"
- [SDR R61A202002150190](https://openairdocs.org/sdr/R61A202002150190.md): Floor Support · corroded · Feb 2, 2020 · N232JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND FWD WET AREA FWD RH SILL FR 12-14 CORRODED. REMOVED CORROSION ON RH SILL FR12-14 IN FWD WET AREA REF SRM 51-10-03. 100% MATERIAL LOSS, OUT OF LIMITS REF SRM 53-10-10/AD06. REMOVED AND REPLACED RH SILL REF SRM 51-40-08. PAINTED TOP C
- [SDR C77A2019121600003](https://openairdocs.org/sdr/C77A2019121600003.md): Battery · failed · Dec 14, 2019 · N232JQ · Emb ERJ170200LR · Emergency Equipment
  > R2 DOOR FLASHLIGHT RED LIGHT DOES NOT FLASH. R & R FLASHLIGHT BATTERY IAW AMM 33-51-00. NO FURTHER DEFECTS NOTED AT THIS TIME. OPS CHECK GOOD. OK FOR SVC.

## 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 = 'N232JQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N232JQ/reports

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