# Service difficulty reports: N233JQ

A list on [N233JQ](https://openairdocs.org/aircraft/N233JQ.md).

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

- [SDR R61A2026102100309](https://openairdocs.org/sdr/R61A2026102100309.md): Slide · deployed · Oct 18, 2026 · N233JQ · Emb ERJ170200LR · Escape Slide
  > L1 DOOR SLIDE DEPLOYED. MECHANIC REMOVED THE DEPLOYED L1 DOOR EMERGENCY EVACUATION SLIDE IAW AMM AND REPLACED L1 DOOR SLIDE IAW SRIIM INSPECTOR PERFORMED RII INSPECTION OF L1 EMERGENCY EVACUATION SLIDE REPLACEMENT IAW SRIIM
- [SDR R61A2026071200190](https://openairdocs.org/sdr/R61A2026071200190.md): Warning Message · false activation · Jul 12, 2026 · N233JQ · Emb ERJ170200LR · Central Warning
  > BLEED 2 OVERPRESSURE RIGHT AFTER TAKE OFF. MAX OBSERVED PSI 110. FOLLOWED QRH PROCEDURE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED EMB FIM TASK 36-11-00-810-812-A AND 36-14-00-810-818-A. NO DEFECTS NOTED. PERFORMED ENGINE PNEUMATIC BLEED SYSTEM O
- [SDR R61A2025080100327](https://openairdocs.org/sdr/R61A2025080100327.md): Rib · cracked · Jul 21, 2025 · N233JQ · Emb ERJ170200LR · Wing, Rib/Bulkhead
  > LEFT WING RIB 4A UPPER AND LOWER FASTENER HOLES FOUND TO HAVE CRACKS PRESENT INSIDE OF HOLES AT 12 O'CLOCK POSITIONS. REPAIRED LT WING RIB 4A UPPER AND LOWER FASTENER HOLES REF. ETD2025-170-925529
- [SDR R61A2025073100325](https://openairdocs.org/sdr/R61A2025073100325.md): Beam · mislocated · Jul 16, 2025 · N233JQ · Emb ERJ170200LR · Fuselage Main, Structure
  > AFT SERVICE DOOR LOWER BEAM HAD 2 HOLES MIS-DRILLED, INSTALLED HAT BUSHINGS.
- [SDR R61A2025073100326](https://openairdocs.org/sdr/R61A2025073100326.md): Skin · cracked · Jul 10, 2025 · N233JQ · Emb ERJ170200LR · Wing, Plate/Skin
  > LEFT WING LOWER SKIN IS CRACKED AT RIB 4A AND SPAR 2. REPAIRED LH WING LOWER SKIN AT RIB 4A AND SPAR 2 ETD2025-170-924781 REV.: B
- [SDR R61A2025050900232](https://openairdocs.org/sdr/R61A2025050900232.md): Battery · no test · May 7, 2025 · N233JQ · Emb ERJ170200LR · Emergency Lighting
  > L2 DOOR EMERGENCY LIGHTS DO NOT ILLUMINATE. R&R EMERGENCY BATTERY 3.
- [SDR R61A202040400173](https://openairdocs.org/sdr/R61A202040400173.md): Engine · stalled · Apr 4, 2025 · N233JQ · Emb ERJ170200LR · Engine (Turbine/Turboprop)
  > COMPRESSOR STALL IN AIR. NUMBER 2 ENGINE, TWO SETS OF LOUD BANGS FOLLOWED BY HIGH ITT INDICATION. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R E2.
- [SDR R61A2023050700265](https://openairdocs.org/sdr/R61A2023050700265.md): Unknown · unknown · May 4, 2023 · N233JQ · Emb ERJ170200LR · Fuselage Main, Structure
  > LIGHTING STRIKE DAMAGE AT FRA 24 TO FRA 25 BELOW STR 25L. FABRICATED AND INSTALLED REPAIR IAW EMB 170/175 SRM 53-21-01 REPAIR 13. ALSO REF VP-018676-2023 N/R 14 C1 THRU C3 FOR WORK PERFORMED.
- [SDR R61A2023050700264](https://openairdocs.org/sdr/R61A2023050700264.md): Unknown · unknown · May 4, 2023 · N233JQ · Emb ERJ170200LR · Fuselage Main, Structure
  > LIGHTING STRIKE DAMAGE AT FRA 21 ABOVE STR 26L.FABRICATED AND INSTALLED REPAIR IAW ETD2023-170-011274 REV B. ALSO REF VP-018676-2023 N/R 11 C1-C3 FOR WORK PERFORMED.
- [SDR R61A2022092700575](https://openairdocs.org/sdr/R61A2022092700575.md): Shear Angle · corroded · Sep 10, 2022 · N233JQ · Emb ERJ170200LR · Fuselage Structure (General)
  > SHEAR CLIP IS CORRODED AT FRAME 74 BETWEEN STRINGERS 29R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.
- [SDR R61A2022092700574](https://openairdocs.org/sdr/R61A2022092700574.md): Shear Angle · corroded · Sep 10, 2022 · N233JQ · Emb ERJ170200LR · Fuselage Structure (General)
  > SHEAR CLIP IS CORRODED AT FRAME 74 BETWEEN STRINGERS 28R AND 27R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.
- [SDR R61A2022092700573](https://openairdocs.org/sdr/R61A2022092700573.md): Shear Angle · corroded · Sep 10, 2022 · N233JQ · Emb ERJ170200LR · Fuselage Structure (General)
  > SHEAR CLIP IS CORRODED AT FRAME 75 BETWEEN STRINGERS 28R AND 27R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.
- [SDR R61A2022092700572](https://openairdocs.org/sdr/R61A2022092700572.md): Shear Angle · corroded · Sep 10, 2022 · N233JQ · Emb ERJ170200LR · Fuselage Structure (General)
  > SHEAR CLIP IS CORRODED AT FRAME 76 BETWEEN STRINGERS 28R AND 27R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.
- [SDR R61A2022092700571](https://openairdocs.org/sdr/R61A2022092700571.md): Shear Angle · corroded · Sep 10, 2022 · N233JQ · Emb ERJ170200LR · Fuselage Structure (General)
  > SHEAR CLIP IS CORRODED AT FRAME 84 BETWEEN STRINGERS 28R AND 27R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.
- [SDR R61A2022092700570](https://openairdocs.org/sdr/R61A2022092700570.md): Shear Angle · corroded · Sep 10, 2022 · N233JQ · Emb ERJ170200LR · Fuselage Structure (General)
  > SHEAR CLIP IS CORRODED AT FRAME 82 BETWEEN STRINGERS 27R AND 26R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.
- [SDR R61A2022092700569](https://openairdocs.org/sdr/R61A2022092700569.md): Shear Angle · corroded · Sep 10, 2022 · N233JQ · Emb ERJ170200LR · Fuselage Structure (General)
  > SHEAR CLIP IS CORRODED AT FRAME 82 BETWEEN STRINGERS 28R AND 27R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.
- [SDR R61A2022092700568](https://openairdocs.org/sdr/R61A2022092700568.md): Shear Angle · corroded · Sep 10, 2022 · N233JQ · Emb ERJ170200LR · Fuselage Structure (General)
  > SHEAR CLIP IS CORRODED AT FRAME 83 BETWEEN STRINGERS 28R AND 27R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.
- [SDR R61A2022092700567](https://openairdocs.org/sdr/R61A2022092700567.md): Shear Angle · corroded · Sep 10, 2022 · N233JQ · Emb ERJ170200LR · Fuselage Structure (General)
  > SHEAR CLIP IS CORRODED AT FRAME 81 BETWEEN STRINGERS 27R AND 28R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.
- [SDR R61A2022092700566](https://openairdocs.org/sdr/R61A2022092700566.md): Stringer Splice · corroded · Sep 10, 2022 · N233JQ · Emb ERJ170200LR · Fuselage Structure (General)
  > CORROSION ON STRINGER AT RIVET ON STRINGER 19R AFT OF FRAME 88. REPAIRED STRINGER 19R PER ETD2022-170-028727.
- [SDR R61A2021111800912](https://openairdocs.org/sdr/R61A2021111800912.md): Light · dirty · Nov 15, 2021 · N233JQ · Emb ERJ170200LR · Emergency Lighting
  > PHOTOLUMINESCENT FLOOR LIGHTING WORN AND WILL NOT ILLUMINATE. CLEANED ALL AIRCRAFT PHOTOLUMINESCENT INDICATOR LIGHT STRIPS ON FLOOR.
- [SDR R61A2021052000440](https://openairdocs.org/sdr/R61A2021052000440.md): Slide · partial deploy · May 16, 2021 · N233JQ · Emb ERJ170200LR · Escape Slide
  > L1 DOOR SLIDE IS PARTIALLY DEPLOYED. R&R L1 SLIDE ASSEMBLY.
- [SDR R61A2020092300641](https://openairdocs.org/sdr/R61A2020092300641.md): Power Supply · inoperative · Sep 21, 2020 · N233JQ · Emb ERJ170200LR · Emergency Lighting
  > EMERGENCY BATTERY LIGHT FAULT ON EICAS DURING ELPU FUNCTIONAL TEST. R & R ELPU 2, REF AMM 33-50-01.
- [SDR R61A2020032430446](https://openairdocs.org/sdr/R61A2020032430446.md): Rib · cracked · Mar 4, 2020 · N233JQ · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > "SUSPECTED CRACK ON RIB 11 RH HORIZONTAL STABILIZER. COMPLIED WITH EO 170EO-55-10-0004_1. LEFT AND RIGHT HSTAB RIB 10A, 11A & 12A REPLACEMENTS."
- [SDR R61A202003210440](https://openairdocs.org/sdr/R61A202003210440.md): Stringer · corroded · Mar 4, 2020 · N233JQ · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > DURING HEAVY CHECK MAINTENANCE FOUND CORROSION, AFT FUSELAGE AT WASTE BOX ON STRINGER 28R AT FRAME 88. REMOVED DAMAGE STRINGER BY CUTTING, DRILLED AND INSTALLED SPLICE REPAIR PARTS ON STRINGER 28R BETWEEN FRAMES 86-90 REF EDT2020-170-008593. RESTORED SURFACE
- [SDR R61A202003140401](https://openairdocs.org/sdr/R61A202003140401.md): Crossbeam · corroded · Mar 3, 2020 · N233JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND CORROSION - RH SIDE OF CROSSBEAM AT FRAME 14. REMOVED CORROSION BY BLENDING ON RH SIDE OF CROSSBEAM AT FRAME 14 PREVIOUS REPAIR PER SRM 51-10-03, FOUND OUT OF LIMITS PER SRM 53-10-10/AD02. INSTALLED NEW RH FR 14 REPAIR AS REQUIRED RE
- [SDR R61A202003210439](https://openairdocs.org/sdr/R61A202003210439.md): Floorbeam · corroded · Mar 1, 2020 · N233JQ · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > DURING HEAVY CHECK MAINTENANCE FOUND RH FLOOR BEAM CORRODED AS MARKED @ FRAME 87. PERFORMED CUT-OUT OF DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER ON RH AFT FLOOR BEAM @ FR87 REF EMB SRM 53-23-10 R01P. APPLIED SURFACE PROTECTION PER SRM 51-23-05, 51
- [SDR R61A202003200437](https://openairdocs.org/sdr/R61A202003200437.md): Panel Support · corroded · Mar 1, 2020 · N233JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND RH FLOOR PANEL SUPPORT CORRODED FRAME 86 CROSSBEAM. REMOVED AND REPLACED RH FLOOR PANEL SUPPORT AT FRAME 86 REF EMB SRM 51-40-08, RESTORED SURFACE PROTECTION PER SRM 51-23-06. A/C REMAINS IN CHECK.
- [SDR R61A202003140413](https://openairdocs.org/sdr/R61A202003140413.md): Door Sill · corroded · Mar 1, 2020 · N233JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND LH FLOOR SILL CORRODED AS MARKED @ FRAME 90. REMOVED CORRODED LH FLOOR SILL @ FR90 REF EMB SRM 51-40-08 INSTALLED NEW LH SILL @FR90 REF EMB SRM 51-40-08
- [SDR R61A202003140412](https://openairdocs.org/sdr/R61A202003140412.md): Splice · corroded · Mar 1, 2020 · N233JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND SPLICE CORRODED AS MARKED @ CENTER OF FRAME 90. REMOVED CORROSION BY BLENDING AT CENTER SPLICE. FRAME 90. MATERIAL REMOVED: H-.010" NOMINAL.050" OUT OF LIMITS. REF EMB SRM 51-75-16 SRM 51-10-03 TOOLING TC1-66878-2 08-07-20 TC2-7449
- [SDR R61A202003140410](https://openairdocs.org/sdr/R61A202003140410.md): Panel Support · corroded · Mar 1, 2020 · N233JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND RH FLOOR PANEL SUPPORT CORRODED AS MARKED FRAME 87 @ RH SHEAR PANEL. REMOVED RH FLOOR PANEL SUPPORT. FRAME 87 @ RH SHEAR PANEL. LOCATED, DRILLED, AND APPLIED ALODINE TO NEW RH FLOOR PANEL SUPPORT. FRAME 87 @ RH SHEAR PANEL PER REF E
- [SDR R61A202003140408](https://openairdocs.org/sdr/R61A202003140408.md): Gusset · corroded · Mar 1, 2020 · N233JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND GUSSET CORRODED AS MARKED FRAME 84 @ RH INBD. SEAT TRACK. REMOVED AND REPLACED FLOOR GUSSET AT RH INBD SIDE OF FRAME 84 PER SRM 51-40-08. RESTORED SURFACE PROTECTION AND REMOVED EWIS PROTECTION PER SRM 51-23-06 PO# 258790, SWPM 20-67
- [SDR R61A202003140407](https://openairdocs.org/sdr/R61A202003140407.md): Door Sill · corroded · Mar 1, 2020 · N233JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND CORROSION RH FLOOR SILL AS MARKED FRAME 84. REMOVED AND REPLACED RH FLOOR SILL FRAME 84 REF EMB SRM 51-40-08
- [SDR R61A202003140403](https://openairdocs.org/sdr/R61A202003140403.md): Crossbeam · corroded · Mar 1, 2020 · N233JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND CORROSION - RH SIDE OF CROSSBEAM AT FRAME 16. REMOVED CROSSBEAM SUPPORT AT FRAME 16 (RH SIDE). REF EMB SRM 51-40-08 INSTALLED NEW FLOOR SUPPORT AT CROSSBEAM FRAME 16 (RH SIDE). REF EMB SRM 51-40-08
- [SDR R61A202003140402](https://openairdocs.org/sdr/R61A202003140402.md): Crossbeam · corroded · Mar 1, 2020 · N233JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND CORROSION - RH SIDE OF CROSSBEAM AT FRAME 15. REMOVED CROSSBEAM SUPPORT AT FRAME 15 (RH SIDE). REF EMB SRM 51-40-08 INSTALLED NEW FLOOR SUPPORT AT CROSSBEAM FRAME 15 (RH SIDE). REF EMB SRM 51-40-08
- [SDR R61A202003140400](https://openairdocs.org/sdr/R61A202003140400.md): Seat Track · corroded · Mar 1, 2020 · N233JQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > WHILE IN HEAVY CHECK FOUND CORROSION - LH SEAT TRACK BETWEEN FRAMES 12 AND 16. REMOVED CORROSION BY BLENDING ON LH SEAT TRACK BETWEEN FRAMES 12-16 PER SRM 51-10-03, FOUND OUT OF LIMITS PER SRM 53-10-10/AD01. FABRICATED NEW DOUBLER AND FILLER. REF EMB SRM 53-10
- [SDR R61A2020032100438](https://openairdocs.org/sdr/R61A2020032100438.md): Doubler · corroded · Feb 29, 2020 · N233JQ · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > DURING HEAVY CHECK MAINTENANCE FOUND CORROSION, AFT FUSELAGE INTERNAL SKIN AT WASTE BOX FRAME 88-89 STRINGER 28R. REMOVED AND REPLACE AFT FUSELAGE INTERNAL SKIN DOUBLER AT WASTE BOX BETWEEN FRAME 88-89 STRINGER 28R PER SRM 51-40-08, RESTORED SURFACE PROTECTI
- [SDR R61A202003200436](https://openairdocs.org/sdr/R61A202003200436.md): Intercostal · corroded · Feb 29, 2020 · N233JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND CORROSION, AFT FUSELAGE INTERNAL AFT INTERCOSTAL AT WATER DRAIN FRAME 86-87 STRINGER 28R. REMVED AND REPLACED AFT INTERCOSTAL AT WATER DRAIN FRAME 86-87 STRINGER 28R PER SRM 51-40-08, RESTORED SURFASCE PROTECTION TO FASTEN
- [SDR R61A202003200435](https://openairdocs.org/sdr/R61A202003200435.md): Shear Tie · corroded · Feb 29, 2020 · N233JQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND CORROSION, AFT FUSELAGE INTERNAL SHEAR CLIP AT FRAME 84 STRINGER 28R. REMOVED AND REPLACED AFT FUSELAGE INTERNAL SHEAR CLIP AT FRAME 84 STRINGER 28R PER SRM 51-40-08. APPLIED SURFACE PROTECTIOIN TO RIVETS PER SRM 51-23-05,
- [SDR R61A202003200434](https://openairdocs.org/sdr/R61A202003200434.md): Shear Tie · corroded · Feb 29, 2020 · N233JQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND CORROSION, AFT FUSELAGE INTERNAL SHEAR CLIP AT FRAME 85 STRINGER 28R. REMOVED AND REPLACED AFT FUSELAGE INTERNAL SHEAR CLIP AT FRAME 85 STRINGER 28R PER SRM 51-40-08, RESTORED SURFACE PROTECTIOM TO FASTENERS PER SRM 51-23
- [SDR R61A202003200433](https://openairdocs.org/sdr/R61A202003200433.md): Shear Tie · corroded · Feb 29, 2020 · N233JQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND CORROSION, AFT FUSELAGE INTERNAL SHEAR CLIP AT FRAME 87 STRINGER 28R. REMOVED DAMAGED SHEAR CLIP, IN AFT CARGO, AT FRAME 87 STRINGER 28R. LOCATED, DRILLED AND INSTALLED NEW SHEAR CLIP, IN AFT CARGO, AT FRAME 87 STRINGER 2
- [SDR R61A202003200432](https://openairdocs.org/sdr/R61A202003200432.md): Shear Tie · corroded · Feb 29, 2020 · N233JQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND CORROSION, AFT FUSELAGE INTERNAL SHEAR CLIP AT FRAME 88 STRINGER 28R. REMOVED THE AFT FUSELAGE INTERNAL SHEAR CLIP AT FRAME 88 STRINGER 28R T EVALUATE THE CORROSION. THE SHEAR CLIP IS 100% CORRODED. THIS IS OUT OF LIMITS.
- [SDR R61A202003200429](https://openairdocs.org/sdr/R61A202003200429.md): Door Sill · corroded · Feb 29, 2020 · N233JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK MAINTENANCE FOUND CORROSION - LH SILL AT FRAMES 13, 14, 15 AND 16. REMOVED DAMAGED LH SILL AT FRAMES 13-16. LOCATED, DRILLED, AND INSTALLED NEW LH SILL, AT FRAMES 13-16. SURFACE PROTECTION APPLIED. REF. SRM 51-40-08, 51-23-00. A/C REMAINS
- [SDR R61A202003140406](https://openairdocs.org/sdr/R61A202003140406.md): Stand Off · corroded · Feb 29, 2020 · N233JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND CORROSION - LH STAND OFF AT FRAME 17. REMOVED, REPLACED, AND APPLIED SURFACE PROTECTION ON LH STAND OFF AT FRAME 17. REF SRM 51-40-08, 51-23-04, 51-23-05, 51-23-06
- [SDR R61A202003140405](https://openairdocs.org/sdr/R61A202003140405.md): Door Sill · corroded · Feb 29, 2020 · N233JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND CORROSION - LH SILL AT FRAME 19. REMOVED, LOCATED, DRILLED, AND ALODINE LH SILL AT FRAME 19. REF SRM 51-40-02, 51-40-08, 51-23-04 INSTALLED AND APPLIED SURFACE PROTECTION TO LH SILL AT FRAME 19. REF SRM 51-23-06, 51-40-08
- [SDR R61A202003140404](https://openairdocs.org/sdr/R61A202003140404.md): Door Sill · corroded · Feb 29, 2020 · N233JQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND CORROSION - RH SILL AT FRAMES 12, 13 AND 14. REMOVED RH SILL AT FRAMES 12, 13 AND 14.PER REF SRM 51-40-02 51-40-08 INSTALLED NEW RH SILL AT FRAMES 12, 13 AND 14.PER REF SRM 51-40-02 51-40-08 APPLIED TOP COAT SRM 51-23-06 PO#258790
- [SDR R61A202003200428](https://openairdocs.org/sdr/R61A202003200428.md): Skin Panel · corroded · Feb 27, 2020 · N233JQ · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > DURING HEAVY CHECK MAINTENANCE FOUND SURFACE CORROSION ON SKIN AT LAV SERVICE PANEL AS MARKED. REMOVED AND REPLACED WASTE DOOR SERVICE PANEL PER SRM AMM 53-03-62-440-801-A TW# TC2-7398 DUE 6-10-20. RESTORED SURFACE PROTECTION TO SERVICE DOOR SKIN PANEL PER SR

## 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 = 'N233JQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N233JQ/reports

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