# Service difficulty reports: N230JQ

A list on [N230JQ](https://openairdocs.org/aircraft/N230JQ.md).

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

- [SDR R61A2025081800345](https://openairdocs.org/sdr/R61A2025081800345.md): Skin · cracked · Aug 15, 2025 · N230JQ · Emb ERJ170200LR · Wing, Plate/Skin
  > DURING A PHASE 2 HARD LANDING INSPECTION FOUND LH WING UPPER SKIN CRACKED AT # 3 MULTI-FUNCTION SPOILER ACTUATOR UPPER HINGE POINT APROX 1 INCH IN LENGTH. REPAIRED IAW ETD2025-170-926670 ALSO REF VP-035109-2025 N/R #2 FOR WORK PERFORMED.
- [SDR R61A2024072600329](https://openairdocs.org/sdr/R61A2024072600329.md): Hydraulic Line · failed · Jul 25, 2024 · N230JQ · Emb ERJ170200LR · Hydraulic System, Main
  > HYD 1 LOW QUANTITY. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. DETERMINED SUCTION LINE ON #1 ENGINE LEAKING. R&R E1 HYDRAULIC SUCTION LINE.
- [SDR R61A2022100700623](https://openairdocs.org/sdr/R61A2022100700623.md): Power Unit · failed insp · Oct 7, 2022 · N230JQ · Emb ERJ170200LR · Emergency Lighting
  > EMERGENCY LIGHT BATTERY FAULT WHEN TESTING EMERGENCY LIGHTS. R&R AFT RH INBOARD EMERGENCY LIGHT POWER UNIT.
- [SDR R61A2022030800177](https://openairdocs.org/sdr/R61A2022030800177.md): Doubler · corroded · Feb 17, 2022 · N230JQ · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > CORROSION CO-PILOT INBD BEAM FRAME11-12 AS MARKED. REMOVED AND REPLACED DAMAGED PORTION OF CO-PILOT FLOOR DOUBLER, FROM FR 10 - FR 12. SURFACE PROTECTION RESTORED. REF ETD2022-170-006480.
- [SDR R61A2022030800175](https://openairdocs.org/sdr/R61A2022030800175.md): Shear Tie · corroded · Feb 15, 2022 · N230JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION ON SHEAR CLIP ON FR 85 STGR 27L-28L. REMOVED AND REPLACED SHEAR CLIP AT FR 85 BETWEEN STGR 27L-28L. REF EMB SRM 51-40-08
- [SDR R61A2022030800174](https://openairdocs.org/sdr/R61A2022030800174.md): Shear Angle · corroded · Feb 15, 2022 · N230JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION ON SHEAR CLIP FR 85 STGR 27R-28R. REMOVED AND REPLACED SHEAR CLIP AT FR 85 BETWEEN STGR 27R-28R. REF EMB SRM 51-40-08.
- [SDR R61A2022030800176](https://openairdocs.org/sdr/R61A2022030800176.md): Doubler · cracked · Feb 12, 2022 · N230JQ · Emb ERJ170200LR · Wing Miscellaneous Structure
  > CRACK AT LOWER RH WING RIB 4A FASTENER TO FASTENER. PERFORMED LOWER RH WING DOUBLER REPAIR AT RIB 4A REF ETD2022-170-006182
- [SDR R61A2021112900935](https://openairdocs.org/sdr/R61A2021112900935.md): Seal Rest · cracked · Nov 18, 2021 · N230JQ · Emb ERJ170200LR · Fuselage, Door Hinge
  > FWD CARGO DOOR CUT OUT, LOWER CENTER SEAL REST CRACKED. REMOVED AND REPLACED CENTER SEAL REST IAW EMB 175 SRM 51-41-01 AND 53-21-29. SEE VP-038874-2021 N/R #5 FOR WORKED PERFORMED.
- [SDR R61A2020121800906](https://openairdocs.org/sdr/R61A2020121800906.md): Door · unknown · Dec 15, 2020 · N230JQ · Emb ERJ170200LR · Service Doors
  > FLIGHT CREW REPORTED THAT THE REAR SERVICE DOOR WAS DIFFICULT TO ARM AND DISARM. MAINTENANCE PERFORMED A GVI OF THE DOOR AND TROUBLESHOT, PER FIM 52-42-00, WITH NO DEFECTS NOTED.
- [SDR R61A2020100100676](https://openairdocs.org/sdr/R61A2020100100676.md): Power Supply · inoperative · Oct 1, 2020 · N230JQ · Emb ERJ170200LR · Emergency Lighting
  > AFT LT PASSENGER DOOR LOWER EMERGENCY EXIT SIGN INOPERABLE AND AFT LT PASSENGER DOOR UPPER EMERGENCY EXIT SIGN INOPERABLE. R & R EMERGENCY LIGHT POWER UNIT, REF AMM 33-50-01.
- [SDR R61A2020062300536](https://openairdocs.org/sdr/R61A2020062300536.md): Power Supply · inoperative · Jun 20, 2020 · N230JQ · Emb ERJ170200LR · Emergency Lighting
  > L1 DOOR EMERGENCY LIGHTS DON'T COME ON WHEN MOVING SWITCH IN COCKPIT TO ON POSITION. R&R NR 2 EMERGENCY LIGHT POWER UNIT.
- [SDR R61A202002190193](https://openairdocs.org/sdr/R61A202002190193.md): Doubler · corroded · Feb 15, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > WHILE IN HEAVY CHECK FOUND FORWARD CARGO, CORRODED FASTENERS BETWEEN FR21-FR22, STGR28R- 27R. REMOVED CORROSION ON THE DOUBLER BY BLENDING. MAX. MATERIAL REMOVED WAS 0.003" FROM AN ORIGINAL OF 0.050". THERE ARE NO LIMITS AVAILABLE ON THE DOUBLER. REF SRM 51-10
- [SDR R61A202002190194](https://openairdocs.org/sdr/R61A202002190194.md): Stringer · corroded · Feb 12, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > WHILE IN HEAVY CHECK FOUND AFT CARGO COMPARTMENT CORROSION ON STGR29R FROM FR76 - FR81 BLENDED OUT CORROSION FROM FR 76 THROUGH FR 81, STRINGER 29R/OUTBOARD. REF SRM 51-10-03. FR 76-77, 11 HOLES BLENDED, MAX MATERIAL LOSS 0.034". FR 77-78, 6 HOLES BLENDED, MA
- [SDR R61A202002190195](https://openairdocs.org/sdr/R61A202002190195.md): Shear Panel · corroded · Feb 11, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND CTR FUSE 3 BELOW FLOOR. CORROSION AT FR 90 STGR 19AL (SHEARCLIP, STGR, STANDOFF, ETC) THE BLENDED AREA ON THE SHEAR CLIP AT FRAME 90 STR 19L IS 2.0" X 2.0" X.007". THIS IS OUT OF LIMITS. REF SRM 51-75-16. THE BLENDED AREA WAS ACCEPT
- [SDR R61A202002140185](https://openairdocs.org/sdr/R61A202002140185.md): Drain Mast · corroded · Feb 11, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND CTR FUSE 3 BELOW FLOOR. HOT WATER DRAIN MAST STRUCTURE HAS CORROSION FR 86-87 STGR 27R-28R BLENDED AND EVALUATED CORROSION ON FWD INTERCOSTAL ON HOT WATER DRAIN MAST STRUCTURE FR 86-87 STGR 27R-28R, REF. SRM 51-10-03. DAMAGE MEASURED
- [SDR R61A202002140184](https://openairdocs.org/sdr/R61A202002140184.md): Shear Tie · corroded · Feb 11, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > WHILE IN HEAVY CHECK FOUND CTR FUSE 3 BELOW FLOOR. CORRODED SHEAR CLIP FR 87R STGR 27R-28R BLENDED AND EVALUATED CORRODED SHEAR CLIP FR 87R STGR 27R-28R, REF. SRM 51-10-03. DAMAGE MEASURED 2.223"X1.953"X0.023", NO PUBLISHED LIMITS ON PART, OUT OF LIMITS. REMOV
- [SDR R61A202002140183](https://openairdocs.org/sdr/R61A202002140183.md): Shear Tie · corroded · Feb 11, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > WHILE IN HEAVY CHECK FOUND CTR FUSE 3 BELOW FLOOR. CORRODED SHEAR CLIP FR 87R STGR 29R-28R BLENDED AND EVALUATED CORRODED SHEAR CLIP FR 87R STGR 29R-28R, REF. SRM 51-10-03. DAMAGE MEASURED 1.732"X0.712"X0.014", NO PUBLISHED LIMITS ON PART, OUT OF LIMITS. REMOV
- [SDR R61A202002140176](https://openairdocs.org/sdr/R61A202002140176.md): Seal Rest · corroded · Feb 9, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Main, Structure
  > WHILE HEAVY CHECK FOUND FWD CARGO DOOR LOWER CORNER SEAL REST HAS CORROSION AS MARKED REMOVED CORROSION BY BLENDING ON THE FWD CARGO DOOR LOWER CORNER SEAL REST. NOMINAL THICKNESS OF THE SEAL REST IS.080". BLENDED AREA IS 2.0" X 2.0" X.031". REF SRM 53-21-1
- [SDR R61A202002200207](https://openairdocs.org/sdr/R61A202002200207.md): Stringer · corroded · Jan 31, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > DURING HEAVY CHECK MAINTENANCE FOUND CTR FUSE 3 BELOW FLOOR. STGR 19AL HAS CORROSION AT FASTENERS FR 88 -89. REMOVED DAMAGED PORTION OF STR 21L FROM FR88 TO FR 90. FABRICATED, LOCATED, DRILLED AND INSTALLED REPAIR FILLER AND REPAIR ANGLE, AT STR 21L FROM FR88
- [SDR R61A202002190196](https://openairdocs.org/sdr/R61A202002190196.md): Bracket · corroded · Jan 31, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Main, Attach Fittings
  > WHILE IN HEAVY CHECK FOUND CTR FUSE 3 SIGNS OF CORROSION ON ALL HARDWARE AND OR BRACKETS/STANDOFFS FR88-91 STGR 15AL-15AR TWO BRACKETS FOUND CORRODED. BRACKET (A) IS A ADELE CLIP BRACKET BETWEEN FRAMES 90-91AT STR 28L. BLENDED AREA IS 1.0" X 1.0" X.010". BRAC
- [SDR R61A202002140178](https://openairdocs.org/sdr/R61A202002140178.md): Support · corroded · Jan 31, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND CORROSION - RH OUTBD PANEL SUPPORT CORRODED AS MARKED FR 84 REMOVED CORROSION BY BLENDING ON THE R/H O/B PANEL SUPPORT AT FRAME 84, BLENDED AREAS IS 6.0" X 2.0" X.012" OUT OF LIMITS REF. SRM 51-75-16. REMOVED AND REPLACED R/H O/B P
- [SDR R61A202002200215](https://openairdocs.org/sdr/R61A202002200215.md): Shear Tie · corroded · Jan 30, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND AFT CARGO COMPARTMENT CORRODED SHEAR CLIP AT FR84 STGR 28R-29R. SHEAR CLIP AT FR. 84 STRG. 28R-29R WAS BLENDED TO REMOVE CORROSION REF SRM 51-12-01. BLEND OUT AT SHEAR CLIP MEASURES (L) 3" X (W) 2" WITH A MAX DEPTH OF (D)
- [SDR R61A202002200214](https://openairdocs.org/sdr/R61A202002200214.md): Shear Tie · odor · Jan 30, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND AFT CARGO COMPARTMENT CORRODED SHEAR CLIP AT FR83 STGR 28R-29R. AFTER REMOVING SHEAR CLIP AT FR 83 STGR 28R - 29R, FOUND NO EVIDENCE OF CORROSION AFTER CLEANING OF SHEAR CLIP AND AREA AROUND AND UNDER SHEAR CLIP. TOPCOAT A
- [SDR R61A202002200213](https://openairdocs.org/sdr/R61A202002200213.md): Shear Tie · corroded · Jan 30, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND AFT CARGO COMPARTMENT CORRODED SHEAR CLIP AT FR82 STGR 28R-29R. SHEAR CLIP WAS BLENDED TO REMOVE CORROSION REF SRM 51-12-01. BLEND OUT AT SHEAR CLIP MEASURES (L) 1.0" X (W) 0.7" WITH A MAX DEPTH OF (D)0.021". REMOVED AND R
- [SDR R61A202002200212](https://openairdocs.org/sdr/R61A202002200212.md): Shear Tie · corroded · Jan 30, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND AFT CARGO COMPARTMENT CORRODED SHEAR CLIP AT FR82 STGR 28R-27R. SHEAR CLIP WAS BLENDED TO REMOVE CORROSION REF SRM 51-12-01. BLEND OUT AT SHEAR CLIP MEASURES (L) 1.55" X (W) 0.7" WITH A MAX DEPTH OF (D)0.019". REMOVED AND
- [SDR R61A202002200211](https://openairdocs.org/sdr/R61A202002200211.md): Shear Tie · corroded · Jan 30, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND AFT CARGO COMPARTMENT CORRODED SHEAR CLIP AT FR75 STGR 29R-28R. SHEAR CLIP WAS BLENDED TO REMOVE CORROSION REF SRM 51-12-01. BLEND OUT AT SHEAR CLIP MEASURES (L) 1.35" X (W) 0.7" WITH A MAX DEPTH OF (D)0.015". REMOVED AND
- [SDR R61A202002200210](https://openairdocs.org/sdr/R61A202002200210.md): Shear Tie · corroded · Jan 30, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND AFT CARGO COMPARTMENT CORRODED SHEAR CLIPS AT FR75 STGR 29R-29L (2EA). REMOVED 2EA AFT CARGO COMPARTMENT CORRODED SHEAR CLIPS AT FR75 STGR 29R-29L. LOCATED, DRILLED AND INSTALLED 2EA NEW AFT CARGO COMPARTMENT CORRODED SHEA
- [SDR R61A202002200209](https://openairdocs.org/sdr/R61A202002200209.md): Shear Tie · corroded · Jan 30, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND AFT CARGO COMPARTMENT CORRODED SHEAR CLIPS AT FR76 STGR 29R-29L (2EA). SHEAR CLIPS (2 EACH) WERE BLENDED TO REMOVE CORROSION REF SRM 51-12-01. BLEND OUT AT RH SHEAR CLIP MEASURES (L) 2.0" X (W) 2.0" WITH A MAX DEPTH OF (D)
- [SDR R61A202002200208](https://openairdocs.org/sdr/R61A202002200208.md): Shear Tie · corroded · Jan 30, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND AFT CARGO COMPARTMENT CORRODED SHEAR CLIPS AT FR77 STGR 29R-29L (2EA). REMOVED AFT CARGO SHEAR CLIPS AT FR 77 STGR 29R-29L REF SRM 51-40-08. EVALUATED AND BLENDED 2 EACH SHEAR CLIPS REF. EMB SRM 51-10-02. BLEND OUT AT RH S
- [SDR R61A202002200205](https://openairdocs.org/sdr/R61A202002200205.md): Shear Tie · corroded · Jan 30, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND AFT CARGO COMPARTMENT CORRODED SHEAR CLIP AT FR84 STGR 28R-27R. REMOVED DAMAGED SHEAR CLIP AT FR84 STGR 28R-27R. LOCATED, DRILLED AND INSTALLED NEW SHEAR CLIP AT FR84 STGR 28R-27R. REF EMB SRM 51-40-08.
- [SDR R61A202002140182](https://openairdocs.org/sdr/R61A202002140182.md): Gusset · corroded · Jan 28, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND CORROSION - LH INBD GUSSET CORRODED AS MARKED FR 90 REMOVED CORROSION BY BLENDING ON THE L/H I/B GUSSET AT FRAME 90. BLENDED AREA IS 3.0" X 3.0" X.020". NOMINAL THICKNESS IS.040" THIS IS OUT OF LIMITS. REF SRM 51-75-16. REMOVED LH
- [SDR R61A202002140181](https://openairdocs.org/sdr/R61A202002140181.md): Gusset · corroded · Jan 28, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND CORROSION - CENTER GUSSET CORRODED AS MARKED FR 90 REMOVED CORROSION BY BLENDING ON THE CENTER GUSSET AT FRAME 90. BLENDED AREA IS 2.0" X 2.0" X.015". NOMINAL THICKNESS IS.063". THIS IS OUT OF LIMITS. REF SRM 51-75-16. REMOVED CENT
- [SDR R61A202002140180](https://openairdocs.org/sdr/R61A202002140180.md): Gusset · corroded · Jan 28, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND CORROSION - RH MIDDLE GUSSET CORRODED AS MARKED FR 90 REMOVED CORROSION BY BLENDING ON THE R/H MIDDLE GUSSET AT FRAME 90. BLENDED AREA IS 1.0" X 2.0" X.025". NOMINAL THICKNESS IS.040". THIS IS OUT OF LIMITS. REF SRM 51-75-16. REMOV
- [SDR R61A202002140179](https://openairdocs.org/sdr/R61A202002140179.md): Gusset · corroded · Jan 28, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND CORROSION - RH OUTBD GUSSET CORRODED AS MARKED FR 90 REMOVED CORROSION BY BLENDING ON THE R/H O/B GUSSET AT FRAME 90. BLENDED AREA IS 4.0" X 6.0" X.025" NOMINAL THICKNESS IS.040". THIS IS OUT OF LIMITS. REF SRM 51-75-16. REMOVED RH
- [SDR R61A202002140177](https://openairdocs.org/sdr/R61A202002140177.md): Floor Support · corroded · Jan 28, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND CORROSION- LH OUTBD PANEL SUPPORT CORRODED AS MARKED FR 88-90 REMOVED CORROSION BY BLENDING ON THE L/H O/B PANEL SUPPORT AT FRAME 88-90. BLENDED AREA IS 1.0"X5.0" X.009"- OUT OF LIMITS REF SRM 51-75-16. REMOVED AND REPLACED LH OTBD
- [SDR R61A202002190203](https://openairdocs.org/sdr/R61A202002190203.md): Splice · corroded · Jan 27, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND CORROSION ON FWD WET AREA LAV FLOOR SPLICE BETWEEN FR12 AND FR13 AS MARKED. BLENDED CORROSION OUT ON FWD WET AREA LAV FLOOR SPLICE PN170-07298-003 BETWEEN FR12 AND FR13 AS MARKED. H=0.010" X L=1" X W=1". THIS HAS BEEN ACCEPTED AS A
- [SDR R61A202002190202](https://openairdocs.org/sdr/R61A202002190202.md): Shear Panel · corroded · Jan 27, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND CORROSION - RH SHEAR PANEL CORRODED AS MARKED FR 87-88 REMOVED CORROSION ALONG THE FWD EDGE OF PANEL REF SRM 51-12-01. AREA OF REMOVAL IS 16" X 1" WITH 0.026" MAX. MATERIAL REMOVED. REMOVED AND REPLACED THE RH SHEAR PANEL REF SRM
- [SDR R61A202002190201](https://openairdocs.org/sdr/R61A202002190201.md): Floor Support · corroded · Jan 27, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND CORROSION ON FWD WET AREA R/H SILL BETWEEN FR12 AND FR14 IN 4 LOCATIONS AS MARKED. REMOVED DAMAGE BY BLENDING ON FWD WET AREA R/H SILL BETWEEN FR12 AND FR14 WITH THE DEEPEST DIMENSIONS L=3.5XW=1.25XH=.022. OUT OF LIMITS REF SRM 53-1
- [SDR R61A202002190200](https://openairdocs.org/sdr/R61A202002190200.md): Beam · corroded · Jan 27, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Main, Structure
  > WHILE IN HEAVY CHECK FOUND CORROSION ON FWD WET AREA L/H BEAM BETWEEN FR16 AND FR19 IN 4 LOCATIONS AS MARKED. BLENDED CORROSION OUT IN 3 PLACES ON THE L/H BEAM PN170-03264-001 BETWEEN FR16 AND FR19 AS MARKED. FR 16-17 H=0.019", L=1", W=2". FR 17-18 H=0.023", L
- [SDR R61A202002190199](https://openairdocs.org/sdr/R61A202002190199.md): Doubler · corroded · Jan 27, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND CORROSION ON FWD WET AREA FWD LAV FLOOR DOUBLER AT FR16 IN 2 LOCATIONS AS MARKED 100 PERCENT MATERIAL LOSS ON THE FWD WET AREA FWD LAV DOUBLER AT FR16 IN TWO LOCATIONS AS MARKED REF SRM 53-10-10/AD06. REMOVED AND REPLACED FWD LAV FLO
- [SDR R61A202002190198](https://openairdocs.org/sdr/R61A202002190198.md): Floor Support · corroded · Jan 27, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND CORROSION ON FWD WET AREA FWD LAV FLOOR MOUNT BRACKET AT FR16 AS MARKED 100 PERCENT MATERIAL LOSS ON THE FWD WET AREA FWD LAV FLOOR MOUNT BRACKET AT FR16 AS MARKED REF SRM 51-75-16. REMOVED AND REPLACED FWD LAV MOUNT BRACKET REF SRM
- [SDR R61A202002190197](https://openairdocs.org/sdr/R61A202002190197.md): Floor Support · corroded · Jan 27, 2020 · N230JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND CORROSION ON FWD WET AREA FWD L/H SILL AT FR16 AS MARKED 100 PERCENT MATERIAL LOSS ON THE FWD WET AREA FWD L/H SILL AT FR 16 REF SRM 53-10-10/AD06. REMOVED AND REPLACED L/H SILL REF SRM 51-40-02, 51-40-04, 51-23-04, AND 51-40-08. A

## 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 = 'N230JQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N230JQ/reports

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