# Service difficulty reports: N933XJ

A list on [N933XJ](https://openairdocs.org/aircraft/N933XJ.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 · 158 reports

- [SDR REXA2026052900879](https://openairdocs.org/sdr/REXA2026052900879.md): Hinge · damaged · Apr 29, 2026 · N933XJ · Cndair CL6002D24 · Fuselage, Door Hinge
  > UPPER HINGE OF TOILET SERVICE DOOR DOES NOT LATCH ON OPEN POSITION AT FWD LOWER FUSELAGE. UPPER HINGE OF TOILET SERVICE DOOR AT FWD LOWER FUSELAGE.WAS REPLACED PER SRM 51-41-02-001-001-A01.
- [SDR REXA2026052900878](https://openairdocs.org/sdr/REXA2026052900878.md): Attach Angle · corroded · Apr 29, 2026 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON ATTACHMENT ANGLE OF BONDING JUMPER ON TOILET SERVICE DOOR AT FWD LOWER FUSELAGE CORROSION ON ATTACHMENT ANGLE OF BONDING JUMPER ON TOILET SERVICE DOOR AT FWD LOWER FUSELAGE. WAS REMOVED AND EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-21-06-001-001-
- [SDR REXA2026052900876](https://openairdocs.org/sdr/REXA2026052900876.md): Gusset · cracked · Apr 29, 2026 · N933XJ · Cndair CL6002D24 · Electrical/Electronic Compartment Doors
  > CRACK ON GUSET ON AFT EQUIPMENT COMPARTMENT DOOR STRUCTURE. GUSSET ON AFT EQUIPMENT COMPARTMENT DOOR STRUCTURE WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
- [SDR REXA2026052900875](https://openairdocs.org/sdr/REXA2026052900875.md): Plate · cracked · Apr 29, 2026 · N933XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > CRACK ON PLATE BTW FS 1144.00 AND LBL 3 AT AFT EQUIMPMENT COMPARTMENT. CRACK ON PLATE BTW FS 1144.00 AND LBL 3 AT AFT EQUIMPMENT COMPARTMENT.WAS REMOVED AND EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-00-00-101-001-A01
- [SDR REXA2026052900873](https://openairdocs.org/sdr/REXA2026052900873.md): Door Sill · cracked · Apr 29, 2026 · N933XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > CRACK ON FWD RT DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) FWD RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) WAS REPLACED PER SRM 51-42-10-001-001-A01 AND SRM 51-42-06-001-001-A01
- [SDR REXA2026052900889](https://openairdocs.org/sdr/REXA2026052900889.md): Hinge · corroded · Apr 25, 2026 · N933XJ · Cndair CL6002D24 · Aerodynamic Fairings
  > CORROSION ON HINGE ARMS (2E/A) OF ACCESS DOOR ON BODY FAIRING ACCESS PANEL 196DR HINGES ARMS (2EAS) OF ACCESS DOOR ON BODY FAIRING ACCESS PANEL 196DR WERE REPLACED PER SRM 51-41-02-001-001-A01 AND AMM 20-21-00.
- [SDR REXA2026052900888](https://openairdocs.org/sdr/REXA2026052900888.md): Hinge · corroded · Apr 25, 2026 · N933XJ · Cndair CL6002D24 · Aerodynamic Fairings
  > CORROSION ON HINGE ARMS (2E/A) OF ACCESS DOOR ON BODY FAIRING ACCESS PANEL 196DR HINGES ARMS (2EAS) OF ACCESS DOOR ON BODY FAIRING ACCESS PANEL 196DR WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND CRJ900 AMM 20-21-00
- [SDR REXA2026052900893](https://openairdocs.org/sdr/REXA2026052900893.md): Web · cracked · Apr 24, 2026 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK FLOOR WEB LEFT SIDE WL=79.5 AND FS193.00 (NEAR TO BRAKE ACCUMULATOR INDICATION SUPPORT) ON FWD EQUIPMENT COMPARTMENT. FLOOR WEB LEFT SIDE WL=79.5 AND FS193.00 (NEAR TO BRAKE ACCUMULATOR INDICATION SUPPORT) ON FWD EQUIPMENT COMPARTMENT. WAS REPAIRED PER
- [SDR REXA2026052900891](https://openairdocs.org/sdr/REXA2026052900891.md): Angle · corroded · Apr 24, 2026 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFTER REMOVAL MID CAP ANGLE, WAS FOUND CORRSION ON KICKPLATE ANGLE AT DOOR SURROUND STRUCTURE OF THE PASSENGER DOOR KICKPLATE ANGLE AT DOOR SURROUND STRUCTURE OF THE PASSENGER DOOR WAS EVALUATED OUT OF LIMITS PER SRM SRM 53-21-23-101-001-A02 AND WAS REPLACED
- [SDR REXA2026052900887](https://openairdocs.org/sdr/REXA2026052900887.md): Angle · corroded · Apr 24, 2026 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON MID CAP ANGLE ON LOWER SIDE OF PASSENGER SURROUND STRUCTURE. CORROSION ON MID CAP ANGLE ON LOWER SIDE OF PASSENGER SURROUND STRUCTURE. WAS EVALUATED OUT OF LIMITS PER SRM 51-10-06-001-001-A01 AND WAS REPLACED PER SRM 51-41-02-001-001-A01
- [SDR REXA2026052900886](https://openairdocs.org/sdr/REXA2026052900886.md): Floorbeam · corroded · Apr 24, 2026 · N933XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM FS333 BTW LBL9 AND LBL27 AT PASSENGER FLOOR STRUCTURE. CORROSION ON FLOOR BEAM FS333 BTW LBL9 AND LBL27 AT PASSENGER FLOOR STRUCTURE WAS REPAIRED PER EA NO: CRJ953-22088 REV IR
- [SDR REXA2026052900885](https://openairdocs.org/sdr/REXA2026052900885.md): Support · corroded · Apr 24, 2026 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON RT/LT MLG HYDRAULIC LINES SUPPORT PLATE (UPPER AND LOWER) (IN BK, LG EXT, LG RET) (4 EAS) RBL 45/LBL 45 ON WHEEL WELL AREA CORROSION ON RT MLG HYDRAULIC LINES SUPPORT PLATE (UPPER AND LOWER) (IN BK, LG EXT, LG RET) (2 EAS) RBL 45 ON WHEEL WELL ARE
- [SDR REXA2026052900884](https://openairdocs.org/sdr/REXA2026052900884.md): Support Plate · corroded · Apr 24, 2026 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON RH/LH MLG HYDRAULIC LINES SUPPORT PLATE (UPPER AND LOWER) (IN BK, LG EXT, LG RET) (4 EAS) RBL 45/LBL 45 ON WHEEL WELL AREA CORROSION ON RHMLG HYDRAULIC LINES SUPPORT PLATE (UPPER AND LOWER) (IN BK, LG EXT, LG RET) (2 EAS) RBL 45 ON WHEEL WELL AREA
- [SDR REXA2026052900883](https://openairdocs.org/sdr/REXA2026052900883.md): Support Plate · corroded · Apr 24, 2026 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON CONNECTORS SUPPORT PLATES (PX33, PX17, PX34, PX19) AT LH/RH MAIN WHEEL WELL CORROSION ON CONNECTORS SUPPORT PLATES (PX33, PX17, PX34, PX19) AT LH/RH MAIN WHEEL WELL WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-10-06-001-001-A01 AND WERE REPLACE
- [SDR REXA2026052900882](https://openairdocs.org/sdr/REXA2026052900882.md): Support Plate · corroded · Apr 24, 2026 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON CONNECTORS SUPPORT PLATES (PX33, PX17, PX34, PX19) AT LT/RT MAIN WHEEL WELL CORROSION ON CONNECTORS SUPPORT PLATES (PX33, PX17, PX34, PX19) AT LH/RH MAIN WHEEL WELL WERE EVALUATED OUT OF LIMITS PER SRM 51-10-06-001-001-A01 AND WERE REPLACED PER S
- [SDR REXA2026052900881](https://openairdocs.org/sdr/REXA2026052900881.md): Web · cracked · Apr 24, 2026 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON RT MLG BINS SUPPORT STRUCTURE RETAINER ANGLE BS 797.00 AND RBL 34 AT RH WHEEL WELL AREA RT MLG BINS SUPPORT STRUCTURE RETAINER ANGLE BS 797 AND RBL 34 AT RH WHEEL WELL AREA WAS REPLACED PER SRM 51-41-02-001-001-A01 AND SRM 51-42-10-001-001-A01.
- [SDR REXA2026052900880](https://openairdocs.org/sdr/REXA2026052900880.md): Bracket · corroded · Apr 24, 2026 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON PRESS-TO-TEST INDICATOR LIGHT BRAKET BTW FS881 TO FS897.70 AND STGR 23R TO 24R AT AFT WASTE SERVICE PANEL CORROSION ON PRESS-TO-TEST INDICATOR LIGHT BRAKET BTW FS881 TO FS897.70 AND STGR 23R TO 24R AT AFT WASTE SERVICE PANEL WAS REMOVED AND EVALU
- [SDR REXA2026052900877](https://openairdocs.org/sdr/REXA2026052900877.md): Support Angle · cracked · Apr 24, 2026 · N933XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > CRACKED SUPPORT ANGLE OF ACCESS PANEL 433BT AT LH INTERNAL PYLON STRUCTURE. SUPPORT ANGLE OF ACCESS PANEL 433BT AT LH INTERNAL PYLON STRUCTURE WAS REPLACED PER SRM 51-42-06-001-001-A01.
- [SDR REXA2026052900874](https://openairdocs.org/sdr/REXA2026052900874.md): Angle · cracked · Apr 24, 2026 · N933XJ · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > CRACK ON LT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD - AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD / AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SP
- [SDR REXA2025063000703](https://openairdocs.org/sdr/REXA2025063000703.md): Battery Pack · no test · Jun 27, 2025 · N933XJ · Cndair CL6002D24 · Emergency Lighting
  > LH EXTERNAL EMERGENCY LIGHT AFT OFLEADING EDGE OF THE WING IS INOP. (DS93) REMOVED AND REPLACED LIGHT EMERG.EXTERNAL & LAMP PER AMM 33-51-15. REMOVED AND REPLACED CHARGER ASSY,BATTERY AND BATTERY PACK AT PS37 PER AMM31-51-17.NO FIX. PERFORMED WIRE CHECKS PER
- [SDR REXA2024083000674](https://openairdocs.org/sdr/REXA2024083000674.md): Light · inoperative · Aug 25, 2024 · N933XJ · Cndair CL6002D24 · Emergency Lighting
  > LEFT OVERWING EXTERIOR EMERGENCY LIGHT INOP RELAMPED LEFT HAND EXTERIOR EMERGENCY LIGHT (DS93), LOCATED ON THE LEFT OVERWING FAIRING. NO FIX. R/R EXTERIOR EMERGENCY LIGHT DS93 & REPINNED WIRES FOR DS93, YAH8493 & YAH8501N IAW CRJ 900 AMM 33-51-15 & ESPM 2
- [SDR REXA2022082800706](https://openairdocs.org/sdr/REXA2022082800706.md): Lamp · inoperative · Aug 24, 2023 · N933XJ · Cndair CL6002D24 · Emergency Lighting
  > FOUND EXTERIOR EMERGENCY LIGHT INOP REMOVED AND REPLACED EXTERIOR EMERGENCY LIGHT BULB IAW CRJ900 AMM 33-51-15. OPS CHECK GOOD IAW JC LINE 900. OK FOR SERVICE. PN ON/OFF: 8GH005123-06, NSN.
- [SDR REXA2022101302259](https://openairdocs.org/sdr/REXA2022101302259.md): Skin · damaged · Oct 4, 2022 · N933XJ · Cndair CL6002D24 · Wing, Plate/Skin
  > RH UPPER WING PLANK HAS ELONGATED HOLE ON FWD EDGE UNDER PANEL 621AT AT APPROX. WS 29.00. HOLE IS ELONGATED TO.299". REPAIRED ELONGATED HOLE IAW EA CRJ957-14691.
- [SDR REXA2022101702272](https://openairdocs.org/sdr/REXA2022101702272.md): None · corroded · Sep 26, 2022 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > GALLEY SERVICE DOOR SURROUND STRUCTURE LOWER AFT FLOOR WEB PROTECTOR CORRODED. 2.5" X 1.0" X.030" DEEP REPLACED FLOOR WEB PROTECTOR
- [SDR REXA2022101702271](https://openairdocs.org/sdr/REXA2022101702271.md): None · worn · Sep 22, 2022 · N933XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > RH UPPER TRANSCOWL LATCH DOOR CHAFED..90" X.42" X.028" DEEP REPLACED DOOR
- [SDR REXA2022101702270](https://openairdocs.org/sdr/REXA2022101702270.md): None · worn · Sep 22, 2022 · N933XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > LH LOWER TRANSCOWL LATCH DOOR CHAFED. 3.0" X.511" X.009" DEEP REPLACED LATCH DOOR
- [SDR REXA2022103102325](https://openairdocs.org/sdr/REXA2022103102325.md): Access Panel · chafed · Sep 20, 2022 · N933XJ · Cndair CL6002D24 · Ailerons
  > RH AILERON ACCESS PANEL 699BB CHAFED. BLENDED CHAFE DIMENSIONS AS FOLLOWS 4.0" X 1.5" X.025" DEEP REMOVED AND REPLACED PANEL
- [SDR REXA2022100602224](https://openairdocs.org/sdr/REXA2022100602224.md): Lintel · cracked · Sep 19, 2022 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STR 3L LINTEL HAS 2.0" CRACK AT FS 280.00 REPAIRED STR 3 LINTEL IAW ENDEAVOR AIR EO# R53568.
- [SDR REXA2022101702269](https://openairdocs.org/sdr/REXA2022101702269.md): Hinge Fitting · worn · Sep 15, 2022 · N933XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > RH UPPER TRANSCOWL LATCH DOOR HINGE FITTINGS CHAFED..20" X.20" X.015" DEEP REPLACED HINGE FITTINGS, FWD FITTING P/N CN624-2024-203, AFT FITTING P/N CN624-2030-205
- [SDR REXA2022101702268](https://openairdocs.org/sdr/REXA2022101702268.md): Doubler · worn · Sep 15, 2022 · N933XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > LH UPPER TRANSCOWL LATCH DOOR GUIDE PIN HOLE DOUBLER CHAFED. 2.0" X 2.0" X.041" DEEP REPLACED DOUBLER
- [SDR REXA2022101502267](https://openairdocs.org/sdr/REXA2022101502267.md): Hinge Fitting · worn · Sep 15, 2022 · N933XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > LH LOWER TRANSCOWL LATCH DOOR HINGE FITTING CHAFED..80" X.19" X.020" DEEP REPLACED HINGE FITTING
- [SDR REXA2022101402266](https://openairdocs.org/sdr/REXA2022101402266.md): Spigot · worn · Sep 15, 2022 · N933XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > RH UPPER TRANSCOWL LATCH DOOR SPIGOT CHAFED..60" X.20" X.020" DEEP REPLACE SPIGOT
- [SDR REXA2022101402265](https://openairdocs.org/sdr/REXA2022101402265.md): Spigot · worn · Sep 15, 2022 · N933XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > LH LOWER TRANSCOWL LATCH DOOR SPIGOT CHAFED..50" X.20" X.050" DEEP REPLACE SPIGOT
- [SDR REXA2022092702151](https://openairdocs.org/sdr/REXA2022092702151.md): Splice · corroded · Sep 15, 2022 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STR 25R SPLICE AT FS 333 HAS MULTIPLE SPOTS OF CORROSION WITH UP TO 100% MATERIAL LOSS REPLACED STRINGER SPLICE
- [SDR REXA2022103102323](https://openairdocs.org/sdr/REXA2022103102323.md): Stiffener · cracked · Sep 14, 2022 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SURROUND UPPER FRAME STIFFENER ON AFT FRAME HAS 2.0" CRACK. REPLACED STIFFENER
- [SDR REXA2022103102322](https://openairdocs.org/sdr/REXA2022103102322.md): Floor Support · corroded · Sep 14, 2022 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH FLOOR SILL AT FS 319.70 HAS MULTIPLE AREAS OF CORROSION WITH A MAX DEPTH OF.030". REMOVED AND REPLACED FLOOR SILL
- [SDR REXA2022092702150](https://openairdocs.org/sdr/REXA2022092702150.md): Cleat · corroded · Sep 14, 2022 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STR 22R CLEAT AT FS310.00 HAS AREA OF CORROSION WITH 100% MATERIAL LOSS REPLACED STR 22R CLEAT
- [SDR REXA2022092702149](https://openairdocs.org/sdr/REXA2022092702149.md): Stringer · corroded · Sep 14, 2022 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STR 25R HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS319-333 WITH UP TO 100% MATERIAL LOSS. REPLACED STRINGER
- [SDR REXA2022111002425](https://openairdocs.org/sdr/REXA2022111002425.md): Seat Track · corroded · Sep 13, 2022 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LH SIDE SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS 785.15-847+32 WITH A MAX DEPTH OF.055" REMOVED AND REPLACED SEAT TRACK
- [SDR REXA2022111002424](https://openairdocs.org/sdr/REXA2022111002424.md): Seat Track · corroded · Sep 13, 2022 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH FLOOR SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS847+62-975 WITH A MAX DEPTH OF.010" AROUND FASTENER HOLES REMOVED AND REPLACED SEAT TRACK
- [SDR REXA2022111002423](https://openairdocs.org/sdr/REXA2022111002423.md): Seat Track · corroded · Sep 13, 2022 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LH FLOOR SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS847+62-988 WITH A MAX DEPTH OF.010" DEEP AROUND FASTENER HOLES REMOVED AND REPLACED SEAT TRACK
- [SDR REXA2022111002422](https://openairdocs.org/sdr/REXA2022111002422.md): Seat Track · corroded · Sep 13, 2022 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH FLOOR SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS830-847+62 WITH A MAX DEPTH OF.010" AROUND FASTENER HOLES REMOVED AND REPLACED SEAT TRACK
- [SDR REXA2022111002421](https://openairdocs.org/sdr/REXA2022111002421.md): Seat Track · corroded · Sep 13, 2022 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LH FLOOR SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS830-847 WITH A MAX DEPTH OF.075" REMOVED AND REPLACED SEAT TRACK
- [SDR REXA2022111002420](https://openairdocs.org/sdr/REXA2022111002420.md): Seat Track · corroded · Sep 13, 2022 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH FLOOR SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS693-830 WITH A MAX DEPTH OF.010" AROUND FASTENER HOLES REMOVED AND REPLACED SEAT TRACK
- [SDR REXA2022111002419](https://openairdocs.org/sdr/REXA2022111002419.md): Seat Track · corroded · Sep 13, 2022 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LH FLOOR SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS693-830 WITH A MAX DEPTH OF.075" REMOVED AND REPLACED SEAT TRACK
- [SDR REXA2022111002418](https://openairdocs.org/sdr/REXA2022111002418.md): Seat Track · corroded · Sep 13, 2022 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LH FLOOR SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS661+32-693 WITH A MAX DEPTH OF.075" REMOVED AND REPLACED SEAT TRACK
- [SDR REXA2022110402416](https://openairdocs.org/sdr/REXA2022110402416.md): Seat Track · corroded · Sep 13, 2022 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH FLOOR SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS661+32-693 WITH A MAX DEPTH OF.070" REMOVED AND REPLACED SEAT TRACK
- [SDR REXA2022110402415](https://openairdocs.org/sdr/REXA2022110402415.md): Seat Track · corroded · Sep 13, 2022 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RBL9 FLOOR SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS581-661+32 WITH A MAX DEPTH OF.070" REMOVED AND REPLACED SEAT TRACK
- [SDR REXA2022110402414](https://openairdocs.org/sdr/REXA2022110402414.md): Seat Track · corroded · Sep 13, 2022 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LBL9 FLOOR SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS581-661+32 WITH A MAX DEPTH OF.075" REMOVED AND REPLACED SEAT TRACK
- [SDR REXA2022110302405](https://openairdocs.org/sdr/REXA2022110302405.md): Panel · chafed · Sep 13, 2022 · N933XJ · Cndair CL6002D24 · Wing, Control Surfaces
  > LHIB FLAP ACCESS PANEL 584BB CHAFED 10.0" X 1.5" X.033" DEEP REMOVED AND REPLACED PANEL

Next page: https://openairdocs.org/aircraft/N933XJ/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 = 'N933XJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N933XJ/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.