# Service difficulty reports: N937XJ

A list on [N937XJ](https://openairdocs.org/aircraft/N937XJ.md).

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

Page 1 of 4 · 187 reports

- [SDR REXA2026050600496](https://openairdocs.org/sdr/REXA2026050600496.md): Light · inoperative · May 4, 2026 · N937XJ · Cndair CL6002D24 · Emergency Lighting
  > RH OVERWING EMERGENCY LIGHT INOP REMOVED AND REPLACED RH OVERWING EMERGENCY LIGHT IAW AMM 33-51-15. OPS CHECK GOOD. P/N ON/OFF 2LA006954-00
- [SDR REXA2026041500286](https://openairdocs.org/sdr/REXA2026041500286.md): Door Sill · corroded · Mar 21, 2026 · N937XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > PASSENGER DOOR SILL MID CAP ANGLE IS CORRODED BETWEEN F.S.310 TO F.S.349 REMOVED THE PAX DOOR MID CAP ANGLE BY REMOVING 4 EA SCREWS IAW CRJ-900 SRM 51-41-04-001-001-A01 LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR MID CAP ANGLE PN SH670-31825-9S IAW CRJ-900 SR
- [SDR REXA2026041700292](https://openairdocs.org/sdr/REXA2026041700292.md): Floorbeam · corroded · Mar 15, 2026 · N937XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > THE RH FS 280 FLOOR BEAM IS CORRODED. BEGAN REMOVING CORROSION FROM RH FS 280.00 CROSSBEAM IAW CRJ900 SRM 51-21-06-001-001-A01. PART IS HEAVILY CORRODED FROM BL0 TO RBL9 WITH MORE THAN 50% MATERIAL LOST AND DAMAGE STILL PRESENT. CROSSBEAM REQUIRES REPLACEMENT
- [SDR REXA2026041600289](https://openairdocs.org/sdr/REXA2026041600289.md): Floorbeam · corroded · Mar 15, 2026 · N937XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > THE LT FS 280 FLOORBEAM CORRODED REMOVED CORROSION FROM LT FLOORBEAM IAW SRM 51-21-06-001-001-A01. PART IS HEAVILY CORRODED FROM BL0 TO LBL9 WITH MORE THAN 50% MATERIAL LOST & DAMAGE STILL PRESENT. LOCATED & DRILLED A NEW FLOORBEAM IAW SRM 51-40-11-001-001-A0
- [SDR REXA2026033000277](https://openairdocs.org/sdr/REXA2026033000277.md): Skin · chafed · Mar 13, 2026 · N937XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > "FUSELAGE OUT SKIN IS CHAFED AT FS 913.00 STGR 27 STRIPPED PAINT AT AREA OF DAMAGE FS 913.00 STGR 27 OUTER SKIN IAW CRJ 900 SRM 51-26-01-001-001-A01. REMOVED 2 RIVETS AND BLENDED OUT DAMAGE IN SKIN AT FS 913.00 STGR 27 IAW STEP A. OF BOMBARDIER REO 670-53-00-2
- [SDR REXA2026032700266](https://openairdocs.org/sdr/REXA2026032700266.md): Angle · corroded · Mar 13, 2026 · N937XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > BS 280 J-ANGLE IS HEAVILY CORRODED AND REQUIRES REPLACEMENT LOCATED AND DRILLED NEW J ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED NEW J ANGLE IAW SRM 51-42-06-001-001-A01. AND SRM 51-42-21-001-001-A01. INSTALLED SAME SERVICEABLE LIGHT BRACKET COMMON TO J A
- [SDR REXA2025051200580](https://openairdocs.org/sdr/REXA2025051200580.md): Door · cracked · Apr 25, 2025 · N937XJ · Cndair CL6002D24 · Emergency Exits
  > RH AFT EMERGENCY EXIT LUG CRACKED REPAIRED R/H AFT EMERGENCY EXIT DOOR IAW MHIRJ GREO 670-52-21-103 RV-- DATED 11/06/2024. REPAIR ACCOMPLISHED UNDER MWC HN 00237991.
- [SDR REXA2025051200579](https://openairdocs.org/sdr/REXA2025051200579.md): Door · cracked · Apr 25, 2025 · N937XJ · Cndair CL6002D24 · Emergency Exits
  > RH FWD EMERGENCY EXIT LUG CRACKED REPAIRED R/H FWD EMERGENCY EXIT DOOR IAW MHIRJ GREO 670-52-21-103 REV-- DATED 11/06/2024. REPAIR ACCOMPLISHED UNDER MWC HN 00237990.
- [SDR REXA2025051200578](https://openairdocs.org/sdr/REXA2025051200578.md): Door · cracked · Apr 25, 2025 · N937XJ · Cndair CL6002D24 · Emergency Exits
  > LH AFT EMERGENCY EXIT LUG CRACKED REPAIRED L/H AFT EMERGENCY EXIT DOOR IAW MHIRJ GREO 670-52-21-103 RV-- DATED 11/06/2024. REPAIR ACCOMPLISHED UNDER MWC HN 00237989.
- [SDR REXA2025051200577](https://openairdocs.org/sdr/REXA2025051200577.md): Door · cracked · Apr 25, 2025 · N937XJ · Cndair CL6002D24 · Emergency Exits
  > LH FWD EMERGENCY EXIT LUG CRACKED REPAIRED L/H FWD EMERGENCY EXIT DOOR IAW MHIRJ GREO 670-52-21-103 REV-- DATED 11/06/2024. REPAIR ACCOMPLISHED UNDER MWC HN 00237988.
- [SDR REXA2022010900100](https://openairdocs.org/sdr/REXA2022010900100.md): Lamp · inoperative · Jan 7, 2023 · N937XJ · Cndair CL6002D24 · Emergency Lighting
  > LH AFT OVERWING EMERGENCY EXIT LIGHT BULB NOT WORKING REMOVED & REPLACED BULB FOR LH AFT OVERWING EMERGENCY EXIT LIGHT PN# 8GH002473-08 IAW CRJ 900 AMM 33-51-15 OPS CHECK GOOD
- [SDR REXA2022121302701](https://openairdocs.org/sdr/REXA2022121302701.md): Ground Wire · loose · Dec 7, 2022 · N937XJ · Cndair CL6002D24 · Light System Wiring
  > RIGHT WING SIDE AFT EMERGENCY LIGHT OUT. RE-SECURED GROUND WIRE ON RIGHT WING AFT EMERGENCY LIGHT IAW AMM 33-51-15. OPS CHECKS GOOD.
- [SDR REXA2022083001990](https://openairdocs.org/sdr/REXA2022083001990.md): Stop Fitting · cracked · Aug 25, 2022 · N937XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX DOOR SURROUND STRUCTURE FWD UPPER STOP FITTING HAS 1.0" CRACK REPLACED STOP FITTING
- [SDR REXA2022081801904](https://openairdocs.org/sdr/REXA2022081801904.md): Hinge · corroded · Aug 11, 2022 · N937XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR KICKPLATE HINGE HAS AREAS OF CORROSION WITH 100% MATERIAL LOSS REPLACED HINGE
- [SDR REXA2022081201866](https://openairdocs.org/sdr/REXA2022081201866.md): Skin · cracked · Aug 2, 2022 · N937XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > LH LOWER TRANSCOWL HAS.90" CRACK ON INNER SKIN THAT RUNS THROUGH FASTENER HOLE UNDER Z STIFFENER. REPAIRED LH LOWER TRANSCOWL INNER SKIN IAW EA CRJ954-14302
- [SDR REXA2022081201865](https://openairdocs.org/sdr/REXA2022081201865.md): Fairing · cracked · Jul 29, 2022 · N937XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > RH LOWER TRANSCOWL HINGE LINE FAIRING SKIN CRACKED IN HALF. REPLACED HINGE LING FAIRING
- [SDR REXA2022081201864](https://openairdocs.org/sdr/REXA2022081201864.md): Panel · chafed · Jul 28, 2022 · N937XJ · Cndair CL6002D24 · Wing, Control Surfaces
  > LHIB FLAP PANEL 584GB CHAFED. BLENDED CHAFE, DIMENSIONS AS FOLLOWS. 2.0" X 1.0" X.027" DEEP REMOVED AND REPLACED ACCESS PANEL 584GB.
- [SDR REXA2022081201863](https://openairdocs.org/sdr/REXA2022081201863.md): Latch · worn · Jul 27, 2022 · N937XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > LH LOWER TRANSCOWL LOWER LATCH GUIDE PINS HAVE WEAR HOLES IN THEM. REMOVED AND REPLACED LATCH
- [SDR REXA2022081201862](https://openairdocs.org/sdr/REXA2022081201862.md): Coaming · chafed · Jul 27, 2022 · N937XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > LH LOWER TRANSCOWL LOWER LATCH COAMING IS CHAFED ON LOWER EDGE WITH 100% MATERIAL LOSS. REMOVED AND REPLACED COAMING
- [SDR REXA2022081201861](https://openairdocs.org/sdr/REXA2022081201861.md): Striker · chafed · Jul 27, 2022 · N937XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > LH UPPER TRANSCOWL LATCH DOOR CUT OUT STRIKER PLATES CHAFED WITH 100% MATERIAL LOSS REMOVED AND REPLACED PLATES
- [SDR REXA2022081201860](https://openairdocs.org/sdr/REXA2022081201860.md): Doubler · chafed · Jul 27, 2022 · N937XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > LH UPPER TRANSCOWL LATCH DOOR CUT OUT INNER DOUBLER CHAFED WITH 100% MATERIAL LOSS REMOVED AND REPLACED DOUBLER
- [SDR REXA2022081201859](https://openairdocs.org/sdr/REXA2022081201859.md): Coaming · chafed · Jul 27, 2022 · N937XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > LH UPPER TRANSCOWL LATCH DOOR COAMING CHAFED WITH 100% MATERIAL LOSS. REMOVED AND REPLACED COAMING
- [SDR REXA2022081201858](https://openairdocs.org/sdr/REXA2022081201858.md): Skin · cracked · Jul 27, 2022 · N937XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > LH UPPER TRANSCOWL INNER SKIN HAS.85" CRACK THAT RUNS THROUGH FASTENER HOLE UNDER Z STIFFENER. REPAIRED LH UPPER TRANSCOWL IAW EA# CRJ954-14261.
- [SDR REXA2022081201857](https://openairdocs.org/sdr/REXA2022081201857.md): Hinge · corroded · Jul 27, 2022 · N937XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR TOP STEP PANEL HINGE HAS AREAD OF CORROSION WITH 100% MATERIAL LOSS. REMOVED AND REPLACED HINGE.
- [SDR REXA2022081801903](https://openairdocs.org/sdr/REXA2022081801903.md): Stringer · corroded · Jul 17, 2022 · N937XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STR 22R HAS MULTIPLE SPOTS OF CORROSION WITH 100% MATERIAL LOSS BETWEEN FS280-333 REPLACED STR 22R IAW EA# CRJ953-14243
- [SDR REXA2022081201856](https://openairdocs.org/sdr/REXA2022081201856.md): Panel · chafed · Jul 17, 2022 · N937XJ · Cndair CL6002D24 · Wing, Control Surfaces
  > LHIB FLAP PANEL 584EB CHAFED. BLENDED CHAFE, DIMENSIONS AS FOLLOWS. 3.0" X 1.5" X.042" DEEP REMOVED AND REPLACED ACCESS PANEL 584EB.
- [SDR REXA2022081201855](https://openairdocs.org/sdr/REXA2022081201855.md): Stringer · corroded · Jul 17, 2022 · N937XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STR 23R HAS MULTIPLE SPOTS OF CORROSION WITH 100% MATERIAL LOSS BETWEEN FS 364-379 REPLACED STRINGER
- [SDR REXA2022081101850](https://openairdocs.org/sdr/REXA2022081101850.md): Stringer · corroded · Jul 17, 2022 · N937XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STR 21R HAS MULTIPLE SPOTS OF CORROSION WITH 100% MATERIAL LOSS BETWEEN FS 333-349 REPLACED STRINGER
- [SDR REXA2022072801687](https://openairdocs.org/sdr/REXA2022072801687.md): Stringer · corroded · Jul 17, 2022 · N937XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STR 24R HAS AREAS OF CORROSION BETWEEN FS 280-333 WITH 100% MATERIAL LOSS REMOVED AND REPLACED STRINGER
- [SDR REXA2022081101849](https://openairdocs.org/sdr/REXA2022081101849.md): Former · corroded · Jul 16, 2022 · N937XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR LOWER CENTER FORMER HAS AREA OF CORROSION WITH 100% MATERIAL LOSS. REMOVED AND REPLACED FORMER
- [SDR REXA2022081101848](https://openairdocs.org/sdr/REXA2022081101848.md): Intercostal · corroded · Jul 16, 2022 · N937XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT LWR INTERCOSTAL HAS AREA OF CORROSION WITH 100% MATERIAL LOSS REMOVED AND REPLACED INTERCOSTAL
- [SDR REXA2022081101847](https://openairdocs.org/sdr/REXA2022081101847.md): Beam · corroded · Jul 15, 2022 · N937XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT BEAM AT FS280 HAS MULTIPLE SPOTS OF CORROSION WITH 100% MATERIAL LOSS. REMOVED AND REPLACED BEAM
- [SDR REXA2022083001989](https://openairdocs.org/sdr/REXA2022083001989.md): Seat Track · corroded · Jul 14, 2022 · N937XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH SEAT TRACK HAS AREA OF CORROSION BETWEEN FS349-364. 1.0" X 1.0" X.030" DEEP REPLACED SEAT TRACK
- [SDR REXA2022083001988](https://openairdocs.org/sdr/REXA2022083001988.md): Seat Track · corroded · Jul 14, 2022 · N937XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LH SEAT TRACK HAS AREAS OF CORROSION BETWEEN FS664+46-677 WITH.010" LOSS AROUND FASTENER HOLES. REPLACED SEAT TRACK
- [SDR REXA2022083001987](https://openairdocs.org/sdr/REXA2022083001987.md): Seat Track · corroded · Jul 14, 2022 · N937XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LH SEAT TRACK HAS AREAS OF CORROSION BETWEEN FS485-565, 6.0" X 1.0" WITH.010" LOSS AROUND FASTENER HOLES. REPLACED SEAT TRACK
- [SDR REXA2022083001986](https://openairdocs.org/sdr/REXA2022083001986.md): Seat Track · corroded · Jul 14, 2022 · N937XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LH SEAT TRACK HAS AREA OF CORROSION AT FS 382. 1.0" X 1.0" X.030" DEEP REPLACED SEAT TRACK
- [SDR REXA2022082601970](https://openairdocs.org/sdr/REXA2022082601970.md): Seat Track · corroded · Jul 14, 2022 · N937XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH SEAT TRACK HAS AREAS OF CORROSION AT FS 830. 4.0" X.40" X.010" DEEP REPLACED SEAT TRACK
- [SDR REXA2022082601969](https://openairdocs.org/sdr/REXA2022082601969.md): Seat Track · corroded · Jul 14, 2022 · N937XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH SEAT TRACK HAS AREAS OF CORROSION BETWEEN FS847-847+ 48. 4.0" X.40" X.010" DEEP REPLACED SEAT TRACK
- [SDR REXA2022082601968](https://openairdocs.org/sdr/REXA2022082601968.md): Seat Track · corroded · Jul 14, 2022 · N937XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH SEAT TRACK HAS AREAS OF CORROSION BETWEEN FS881-954. 4.0" X.40" X.010" DEEP REPLACED SEAT TRACK
- [SDR REXA2022082601967](https://openairdocs.org/sdr/REXA2022082601967.md): Seat Track · corroded · Jul 14, 2022 · N937XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LH SEAT TRACK HAS AREAS OF CORROSION BETWEEN FS 830-847. 4.0" X.40" X.010" DEEP REPLACED SEAT TRACK
- [SDR REXA2022081101846](https://openairdocs.org/sdr/REXA2022081101846.md): Intercostal · corroded · Jul 13, 2022 · N937XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT CENTER INTERCOSTAL HAS AREA OF CORROSION WITH 100% MATERIAL LOSS REMOVED AND REPLACED INTERCOSTAL
- [SDR REXA2022081101845](https://openairdocs.org/sdr/REXA2022081101845.md): Tie Clip · corroded · Jul 13, 2022 · N937XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD LOWER INTERCOSTAL CLIP HAS AREA OF CORROSION WITH 100% MATERIAL LOSS. REPLACED CLIP.
- [SDR REXA2022081101844](https://openairdocs.org/sdr/REXA2022081101844.md): Cleat · corroded · Jul 13, 2022 · N937XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD CENTER CLEAT HAS AREA OF CORROSION WITH 100% MATERIAL LOSS. REMOVED AND REPLACED CLEAT
- [SDR REXA2022081101843](https://openairdocs.org/sdr/REXA2022081101843.md): Intercostal · corroded · Jul 13, 2022 · N937XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR LWR CENTER INTERCOSTAL HAS AREA OF CORROSION WITH 100% MATERIAL LOSS REMOVED AND REPLACED INTERCOSTAL
- [SDR REXA2022072801704](https://openairdocs.org/sdr/REXA2022072801704.md): Riser · corroded · Jul 13, 2022 · N937XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD RISER HAS AREAS OF CORROSION WITH 100% MATERIAL LOSS REMOVED AND REPLACED FWD RISER
- [SDR REXA2022081101842](https://openairdocs.org/sdr/REXA2022081101842.md): Cleat · corroded · Jul 12, 2022 · N937XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STR22R CLEAT AT FS310 CORRODED. 1.5" X.50" X.040" DEEP REMOVED AND REPLACED CLEAT
- [SDR REXA2022081101841](https://openairdocs.org/sdr/REXA2022081101841.md): Splice · corroded · Jul 12, 2022 · N937XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STR 23R SPLICE AT FS 333.00 HAS AREA OF CORROSION WITH 100% MATERIAL LOSS REMOVED AND REPLACED SPLICE.
- [SDR REXA2022081101840](https://openairdocs.org/sdr/REXA2022081101840.md): Panel · corroded · Jul 12, 2022 · N937XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR LOWER STEP PANEL HAS MULTIPLE AREAS OF CORROSION WITH A MAX DEPTH OF.012" REMOVED AND REPLACED LOWER STEP PANEL.
- [SDR REXA2022081101839](https://openairdocs.org/sdr/REXA2022081101839.md): Riser · corroded · Jul 12, 2022 · N937XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT RISER HAS AREA OF CORROSION WITH 100% MATERIAL LOSS REMOVED AND REPLACED AFT RISER
- [SDR REXA2022081101838](https://openairdocs.org/sdr/REXA2022081101838.md): Angle · corroded · Jul 11, 2022 · N937XJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR SURROUND STRUCTURE LOWER SILL ANGLE CORRODED. 17.5" X 1.0" X.033" DEEP REPLACED PAX DOOR LOWER SILL ANGLE.

Next page: https://openairdocs.org/aircraft/N937XJ/reports.md?page=2

## 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 = 'N937XJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N937XJ/reports

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