# Service difficulty reports: N921XJ

A list on [N921XJ](https://openairdocs.org/aircraft/N921XJ.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 · 153 reports

- [SDR REXA2026073001337](https://openairdocs.org/sdr/REXA2026073001337.md): Lamp · inoperative · Jul 28, 2026 · N921XJ · Cndair CL6002D24 · Emergency Lighting
  > LH FWD MOST EMERGENCY LIGHT INOP R/R LH FWD MOST EMERGENCY LIGHT BULB REF AMM 33-51-15 PN OFF/ON 8GH002473-08 OPS CHECK GOOD
- [SDR REXA2026052700780](https://openairdocs.org/sdr/REXA2026052700780.md): Attach Angle · cracked · Dec 15, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > CRACKED ATTACHEMENT ANGLE BTW FRAME TO INTERCOSTAL, FRAME FS 310,STRINGER 21L. ATTACHEMENT ANGLE BTW FRAME TO INTERCOSTAL, FRAME FS 310, STRINGER 21L WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-40-11-001-001-A01
- [SDR REXA2026052700763](https://openairdocs.org/sdr/REXA2026052700763.md): Frame · damaged · Dec 15, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Main, Frame
  > ELONGATED HOLE 2 EA AT LOWER SECTION OF FRAME FS 310,STRINGER 21L. ELONGATED HOLE 2 EA AT LOWER SECTION OF FRAME FS 310,STRINGER 21L WAS REPAIRED PER REO 690-53-21-2086 REV -B STEP 11
- [SDR REXA2026052700738](https://openairdocs.org/sdr/REXA2026052700738.md): Strut · corroded · Dec 13, 2025 · N921XJ · Cndair CL6002D24 · Main Landing Gear Strut/Axle/Truck
  > PITTING WAS FOUND ON MLG SHOCK STRUT LH SIDE BELOW IDENTIFICATION PLACARD. MLG SHOCK STRUT WILL BE REPLACED BY CARD 900-32-730-705
- [SDR REXA2026052700762](https://openairdocs.org/sdr/REXA2026052700762.md): Diaphragm · chafed · Dec 12, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SECONDARY NRC FROM NRC 00111: AFTER FASTENERS REMOVAL, HIDDEN DAMAGE (WEAR) AROUND HOLES WAS FOUND ON DIAPHRAMG STRINGER 14 ABOVE CATCH PIN SUPPORT BRACKET AT INTERNAL STRUCTURE OF GALLEY SERVICE DOOR. DIAPHRAMG STRINGER 14 ABOVE CATCH PIN SUPPORT BRACKET AT I
- [SDR REXA2026052700761](https://openairdocs.org/sdr/REXA2026052700761.md): Plate · corroded · Dec 9, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION WAS FOUND ON UPPER AND LATERAL PLATES (3 EAS) CORROSION ON UPPER PLATE (1 EA) WAS EVALUATED OUT OFF LIMITS PER CRJ/900 SRM 51-10-06-001-001-A01 AND NEW PLATE WAS DRILLED PER CRJ/900 SRM 51-40-11-001-001-A01. PAINT ON LATERAL PLATES (2 EAS) AT FWD BAG
- [SDR REXA2026052700759](https://openairdocs.org/sdr/REXA2026052700759.md): Hinge · chafed · Dec 8, 2025 · N921XJ · Cndair CL6002D24 · Fuselage, Door Hinge
  > WEAR ON PIANO HINGE FUSELAGE SIDE AT PASSENGER DOOR. WEAR ON PIANO HINGE FUSELAGE SIDE AT PASSENGER DOOR WAS BLEND OUT CRJ-900 SRM 51-12-00-001-001-A01 AND EVALUTED OU OFF LIMITS PER CRJ-900 SRM 53-21-23-201-010-A01 AND PIANO HINGE WAS REPLACED PER CRJ900 SRM
- [SDR REXA2026052700778](https://openairdocs.org/sdr/REXA2026052700778.md): Bracket · corroded · Dec 5, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON BRACKET MACHINED (10 E/AS) AT FWD CARGO COMPARTMENT BRACKETS MACHINED ON FS.517.00 (2 EAS), FS560.00 (1 EA), FS660.00(1 EA),FS661.00+1 6.00 (2 EAS) WERE CLEANED PER CRJ900 SRM 51-26-00-001-001-A01 AND CORROSION NOT WAS FOUND. ALSO CORROSION ON BR
- [SDR REXA2026052700776](https://openairdocs.org/sdr/REXA2026052700776.md): Seat Track · corroded · Dec 5, 2025 · N921XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL RBL=9 BTW FS477 TO 669 AT CPAX. CORROSION ON SEAT RAIL RBL=9 BTW FS661+46 TO 669 AT CPAX WAS EVALUATED OUT OFF LIMITS PER CRJ/900 SRM 53-31-49-101-001-A02 AND IT WAS REPLACED PER CRJ900 SRM 51-40-11-001-001-A01 AND CRJ900 AMM 53-00-49 AN
- [SDR REXA2026052700775](https://openairdocs.org/sdr/REXA2026052700775.md): Seat Track · corroded · Dec 5, 2025 · N921XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAILS BTW FS 472.00, 566.00, 661+100, 698.00, 712.00, 744.00, 785.00 TO 811.00 AND OVER FS 962.00 AT RH SIDE PASSENGER CABIN CORROSION ON SIDE SEAT RAILS BTW FS 472.00, 566.00, 661+100, 698.00, 712.00, 744.00, 785.00 TO 811.00 AND OVER F
- [SDR REXA2026052700767](https://openairdocs.org/sdr/REXA2026052700767.md): Seat Track · cracked · Dec 5, 2025 · N921XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS ON LBL 9 BTW FS 379.00, 613.00 TO 661+16, 661+46 TO 661+62, ON RBL BTW FS 349.00, 421.00, 453.00 TO 469.00, 495.00 TO 661+26, ON LBL27 BTW FS 465.00, 495.00 TO 581.00. SEAT RAILS ON LBL 9 BTW FS 379.00, 613.00 TO 661+16, 661+46 TO 661+6
- [SDR REXA2026052700766](https://openairdocs.org/sdr/REXA2026052700766.md): Seat Track · corroded · Dec 5, 2025 · N921XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL LBL=27 BTW FS477 TO 570 AT CPAX. SEAT RAIL (1EA) LBL=27 BTW FS477 TO 501 AT CPAX WERE CLEANED AND NOT CORROSION WAS FOUND PER CRJ/900 SRM 51-26-00 001-001-A01 AND SEAT RAIL (1EA) LBL=27 BTW FS501 TO 588 AT CPAX WAS EVALUATED OUT OF LIM
- [SDR REXA2026052700765](https://openairdocs.org/sdr/REXA2026052700765.md): Seat Track · corroded · Dec 5, 2025 · N921XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAILS BTW FS 409.00, 473.00, 485.00 TO 545.00, 661.00, 661+32 TO 661+46, 700.00, 744.00, 785.00 TO 840.00, AND OVER FS 847+32 AT LH SIDE PASSENGER CABIN. CORROSION ON SIDE SEAT RAILS BTW FS 409.00, 473.00, 485.00 TO 545.00, 661.00, 661+3
- [SDR REXA2026052700758](https://openairdocs.org/sdr/REXA2026052700758.md): Intercostal · corroded · Dec 5, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL OVER S26L BTW BS 865 - 913 AT INTERNAL FUSELAGE STRUCTURE. CORROSION ON INTERCOSTAL OVER S26L BTW BS 865 - 881 AT INTERNAL FUSELAGE STRUCTURE WAS REMOVED PER SRM 51-21-06-001-001-A01 AND EVALUATED ORIGINAL THICKNESS: 0.063 IN AND MINIM
- [SDR REXA2026052700757](https://openairdocs.org/sdr/REXA2026052700757.md): Floor Support · corroded · Dec 5, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON LONGITUDINAL BEAM UPPER FACE AT LBL 9.00. AND BTW FS=977.00 TO FS=1098.00 AT PAX CABIN AREA FS 977 BTW FS 1000 AND FS 1076 BTW FS 1098 WAS CLEANED PER CRJ900 SRM 51-26-00-001-001-A01 AND NOT COROSION WAS FOUND ALSO DUE TO EXCESSIVE CORROSION ON SE
- [SDR REXA2026052700756](https://openairdocs.org/sdr/REXA2026052700756.md): Stringer · corroded · Dec 5, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON SGTR 20L BTW FS=847.00+16 AND 847.00 +32 BELOW FLOOR STRUCTURE. CORROSION ON SGTR 20L BTW FS=847.00+16 AND 847.00 +32 BELOW FLOOR STRUCTURE WAS REPAIRED PER EA. NO. CRJ953-21177 REV. A
- [SDR REXA2026052700755](https://openairdocs.org/sdr/REXA2026052700755.md): Frame · corroded · Dec 5, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION ON FRAME BELOW FLOOR STRUCTURE OVER FS 969.00 AND STGR 25L TO 25R. CORROSION ON FRAME BELOW FLOOR STRUCTURE OVER FS 969.00 AND STGR 25L TO 25R WAS REPAIRED PER EA NO. CRJ953-21134 REV IR.
- [SDR REXA2026052700733](https://openairdocs.org/sdr/REXA2026052700733.md): Stringer Splice · corroded · Dec 5, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON SPLICES (4 E/AS) AS FOLOW FS 517, FS 565, FS 661+15 APROX AND FS 629 ALL ON STGR 24LH/25LH OVER WEBS OF LOWER JAMB AT FWD CARGO COMPARTMENT SPLICES (2 E/AS) AS FOLOW FS 517 AND FS 629) WAS REPAIRED PER EA NO: CRJ953-21101 REV IR AND EA NO: CRJ953
- [SDR REXA2026052700732](https://openairdocs.org/sdr/REXA2026052700732.md): Floor Support · corroded · Dec 5, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON LONGITUDINAL BEAM UPPER FACE AT LBL 27.00. AND BTW FS=977.00 TO FS=1098.00 AT PAX CABIN FLOOR STRUCTURE. AREA FLOOR BEAM BTW FS 977 AND FS 1059 WAS CLEANED PER CRJ900 SRM 51-26-00-001-001-A01 AND NOT CORROSIÏ¿½N WAS FOUND AND REPAIR PREVIOUS 27LBL
- [SDR REXA2026052700731](https://openairdocs.org/sdr/REXA2026052700731.md): Seat Track · corroded · Dec 5, 2025 · N921XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEVERAL AREAS OF SEAT TRACKS RAILS BTW FS 847.00 TO 1000.00 RBL 9 AND LBL9 AND OVER RBL AND LBL 27 BTW FS 927.00 TO 1000.00. CORROSION ON SEVERAL AREAS OF SEAT TRACKS RAILS BTW FS 847.00 TO 1000.00 RBL 9 AND LBL9 AND OVER RBL AND LBL 27 BTW FS 92
- [SDR REXA2026052700754](https://openairdocs.org/sdr/REXA2026052700754.md): Access Panel · corroded · Dec 4, 2025 · N921XJ · Cndair CL6002D24 · Wing, Plate/Skin
  > RUSTED COUNTERSINK HOLES ON RIGHT WING ACCESS PANEL 542AT. SUMMARY: PART NUMBER OF ACCESS PANEL 542AT WAS VERIFIED PER CRJ900 AIPC 57-20-32 ON ITEM 10 AND WAS REPLACED/INSTALLED PANEL UNDER JOBCARD CRJ900-500-OPEN/CLOSE.
- [SDR REXA2026052700753](https://openairdocs.org/sdr/REXA2026052700753.md): Angle · corroded · Dec 4, 2025 · N921XJ · Cndair CL6002D24 · Fluid Service Doors
  > CORROSION AT FWD WASTE SERVICE DOOR INTERNAL STRUCTURE, INCLUDING IMPACT ANGLE, FWD FRAME, AFT FRAME, UPPER & LOWER MEMBRANE.RMENT DOOR. CORROSION AT FWD WASTE SERVICE DOOR INTERNAL STRUCTURE, INCLUDING IMPACT ANGLE, FWD FRAME, AFT FRAME, UPPER & LOWER MEMBRAN
- [SDR REXA2026052700751](https://openairdocs.org/sdr/REXA2026052700751.md): Packer · corroded · Dec 4, 2025 · N921XJ · Cndair CL6002D24 · Electrical/Electronic Compartment Doors
  > CORROSION AROUND ON PRESSURE SEAL RETAINER AT E/E COMPARMENT DOOR. CORROSION IN SERVICE DOOR 142BR WAS REPAIRED PER EA NO. CRJ952-21062 REV IR AND DUE TO EXECESSIVE CORROSION ON PACKERS WERE REPLACED PER EA CRJ952-21063 REV: IR AND CRJ 900 SRM 51-42-02-001-001
- [SDR REXA2026052700741](https://openairdocs.org/sdr/REXA2026052700741.md): Intercostal · corroded · Dec 4, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTALS (2 E/AS) LOWER FACE BTW FS 310 TO 349 & STRINGER 21L ALSO BENT CONNECTOR J393 SUPPORT. CORROSION ON INTERCOSTALS (2 E/AS) LOWER FACE BTW FS 310 TO 349 & STRINGER 21L WAS REMOVED PER CRJ 900 SRM 51-21-06-001-001-A01, WERE EVALUATED OUT
- [SDR REXA2026052700740](https://openairdocs.org/sdr/REXA2026052700740.md): Intercostal · corroded · Dec 4, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTALS (2 E/AS) LOWER FACE BTW FS 310 TO 349 & STRINGER 21L ALSO BENT CONNECTOR J393 SUPPORT. CORROSION ON INTERCOSTALS (2 E/AS) LOWER FACE BTW FS 310 TO 349 & STRINGER 21L WAS REMOVED PER CRJ 900 SRM 51-21-06-001-001-A01, WERE EVALUATED OUT
- [SDR REXA2026052700774](https://openairdocs.org/sdr/REXA2026052700774.md): Floor Support · cracked · Dec 3, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACKED ANGLES AT FLOOR SUPPORT STRUCTURE BTW FS 260.00 TO 280.00 AND RBL 12.00 AND LBL12.00. ANGLES AT FLOOR SUPPORT STRUCTURE BTW FS 260.00 TO 280.00 AND RBL 12.00 AND LBL12.00 WERE REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND
- [SDR REXA2026052700752](https://openairdocs.org/sdr/REXA2026052700752.md): Floor Support · corroded · Dec 3, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR SUPPORT BTW FS 315 TO FS 345 ON THRESSHOLD AT PASSENGER CABIN CORROSION FLOOR SUPPORT BTW FS 315 TO FS 345 ON THRESSHOLD AT PASSENGER CABIN WAS EVALUATE OUT OFF LIMITS PER CRJ-900 SRM 51-10-06-001-001-A01 AND FLOOR SUPPORT WAS REPLACED PER CRJ-
- [SDR REXA2026052700739](https://openairdocs.org/sdr/REXA2026052700739.md): Fitting · corroded · Dec 3, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON CLOSING FITTINGS AT PASSENGER FLOOR STRUCTURE OVER FS 314.00 - LBL 40.00 AND FS 342.00 - LBL 40.00. CORROSION ON CLOSING FITTINGS AT PASSENGER FLOOR STRUCTURE OVER FS 314.00 - LBL 40.00 AND FS 342.00 - LBL 40.00. WAS REMOVED PER CRJ-900 SRM 51-21-
- [SDR REXA2026052700783](https://openairdocs.org/sdr/REXA2026052700783.md): Fitting · corroded · Dec 2, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION IN FITTING UNDER LAMP (1EA) ON GALLEY 2 FITTING UNDER LAMP (A391251-3 1EA) ON GALLEY 2 WAS REPLACED PER CMM SAFRAN 25-32-84
- [SDR REXA2026052700730](https://openairdocs.org/sdr/REXA2026052700730.md): Fitting · corroded · Dec 2, 2025 · N921XJ · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION FLOOR FITTING BEHIND ACCESS 108 (1EA) AND IN FRONT ACCESS 107 (1EA) ON GALLEY 1. FLOOR FITTING IN FRONT ACCESS 107 (1 EA) WAS REPLACED PER SAFRAN CMM 25-33-67 AND FLOOR FITTING BEHIND ACCESS 108 (1EA) WAS FABRICATED PER EA CRJ953-21146. REV IR AND I
- [SDR REXA2026052700773](https://openairdocs.org/sdr/REXA2026052700773.md): Frame · cracked · Nov 30, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Main, Frame
  > CRACK ON FRAME AT INTERNAL FUSELAGE STRUCTURE OVER FS 333.00 AND BTW STGR 2L-2R. CRACK ON FRAME AT INTERNAL FUSELAGE STRUCTURE OVER FS 333.00 AND BTW STGR 2L-2R WAS REPAIRED PER EA NO.: CRJ953-20900 REV IR
- [SDR REXA2026052700772](https://openairdocs.org/sdr/REXA2026052700772.md): Frame · cracked · Nov 30, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Main, Frame
  > CRACK ON FRAME AT INTERNAL FUSELAGE STRUCTURE OVER FS 333.00 AND BTW STGR 2L-2R CRACK ON FRAME AT INTERNAL FUSELAGE STRUCTURE OVER FS 333.00 AND BTW STGR 2L-2R WAS REPAIRED PER EA NO.: CRJ953-20900 REV IR
- [SDR REXA2026052700750](https://openairdocs.org/sdr/REXA2026052700750.md): Rib · cracked · Nov 30, 2025 · N921XJ · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACK ON MACHINED RIB LEADING EDGE SS57.16 AT LEFT WING. CRACKED MACHINED RIB LEADING EDGE SS57.16 AT LEFT WING WAS REPLACED PER SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01
- [SDR REXA2026052700749](https://openairdocs.org/sdr/REXA2026052700749.md): Rib · cracked · Nov 30, 2025 · N921XJ · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACK ON WING RIB LEADING EDGE SS27.16 AT LEFT WING. CRACKED RIB LEADING EDGE SS27.16 AT LEFT WING WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ-900 SRM 51-42-10-001-001-A01 AND ELONGATE HOLES WERE REPAIRED PER EA NO. CRJ957-21136 REV A.
- [SDR REXA2026052700743](https://openairdocs.org/sdr/REXA2026052700743.md): Retainer · corroded · Nov 30, 2025 · N921XJ · Cndair CL6002D24 · Electrical/Electronic Compartment Doors
  > CORROSION AROUND ON PRESSURE SEAL RETAINER AT E/E COMPARMENT DOOR. PRESSURE SEAL RETAINER AT E/E COMPARMENT DOOR WERE EVALUATED DUE TO EXCESSIVE DAMAGE PER CRJ 900 SRM 53-61-43-101-001-A02 AND WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
- [SDR REXA2026052700742](https://openairdocs.org/sdr/REXA2026052700742.md): Retainer · corroded · Nov 30, 2025 · N921XJ · Cndair CL6002D24 · Electrical/Electronic Compartment Doors
  > CORROSION AROUND ON PRESSURE SEAL RETAINER AT E/E COMPARMENT DOOR. PRESSURE SEAL RETAINER AT E/E COMPARMENT DOOR WERE EVALUATED DUE TO EXCESSIVE DAMAGE PER CRJ 900 SRM 53-61-43-101-001-A02 AND WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
- [SDR REXA2026052700748](https://openairdocs.org/sdr/REXA2026052700748.md): Support Angle · corroded · Nov 29, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION & CHAFE DAMAGE ON WHEEL BIN SUPPORT ANGLES( 2 EAS), AT RH / LH WHEEL WELL AREA. CORROSION & CHAFE DAMAGE ON WHEEL BIN SUPPORT ANGLES( 2 EAS), AT LH WHEEL WELL AREA WAS REPAIRED PER CRJ953-20960 REV IR AND DUE TO EXCESIVE DAMAGE MACHINED WEB ANGLE O
- [SDR REXA2026052700747](https://openairdocs.org/sdr/REXA2026052700747.md): Bracket · corroded · Nov 28, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) ON LH/RH MAIN WHEEL WELL CORROSION ON CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) ON LH/RH MAIN WHEEL WELL WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND EVALUATED OUT OFF
- [SDR REXA2026052700746](https://openairdocs.org/sdr/REXA2026052700746.md): Diaphragm · cracked · Nov 28, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON LH/RH DIAPHRAGM AT_ FWD AREA OF MLG W/W BTW FS= 797 TO FS= 807 LBL 35 AND RBL35. LH/RH DIAPHRAGMS AT_ FWD AREA OF MLG W/W BTW FS= 797 TO FS= 807 LBL 35 AND RBL35 WERE REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01 AND PER CRJ-900 AMM 20-21-00-910-801-A
- [SDR REXA2026052700768](https://openairdocs.org/sdr/REXA2026052700768.md): Door Sill · cracked · Nov 27, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Main, Structure
  > CRACK ON AFT RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR). RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR WAS REPLACED PER EA NO. CRJ953-21058 REV. IR, CRJ 900 SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01
- [SDR REXA2026052700745](https://openairdocs.org/sdr/REXA2026052700745.md): Bracket · cracked · Nov 27, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION AT LIGHT, CLIP & SUPPORT STRUCTURE OF PRESS-TO-TEST INDICATOR LIGHT OF AFT WASTE TANK (BTW STGR 24RH AND STGR 23RH, FS 959.00). CORROSION AT LIGHT, CLIP & SUPPORT STRUCTURE OF PRESS-TO-TEST INDICATOR LIGHT OF AFT WASTE TANK (BTW STGR 24RH AND STGR 23
- [SDR REXA2026052700744](https://openairdocs.org/sdr/REXA2026052700744.md): Angle · cracked · Nov 27, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACKED INTERNAL ANGLE OF EXTERNAL POWER RECEPTACLE SUPPORT STRUCTURE. CRACKED ANGLE OF EXTERNAL POWER RECEPTACLE SUPPORT STRUCTURE WAS REPLACED PER CRJ900 SRM SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-00
- [SDR REXA2026052700737](https://openairdocs.org/sdr/REXA2026052700737.md): Hinge · corroded · Nov 27, 2025 · N921XJ · Cndair CL6002D24 · Aerodynamic Fairings
  > CORROSION ON HINGES (2EA) AND HINGE FITTINGS (2EA) AT ACCESS FAIRING PANEL 196DR CORROSION ON HINGES (2EA) AND HINGE FITTINGS (2EA) AT ACCESS FAIRING PANEL 196DR WAS EVALUATED OUT OFF LIMITS PER CRJ900 SRM 51-10-06-001-001-A01 AND HINGES AND FITTINGS WERE REP
- [SDR REXA2026052700736](https://openairdocs.org/sdr/REXA2026052700736.md): Hinge · corroded · Nov 27, 2025 · N921XJ · Cndair CL6002D24 · Aerodynamic Fairings
  > CORROSION ON HINGES (2EA) AND HINGE FITTINGS (2EA) AT ACCESS FAIRING PANEL 196DR CORROSION ON HINGES (2EA) AND HINGE FITTINGS (2EA) AT ACCESS FAIRING PANEL 196DR WAS EVALUATED OUT OFF LIMITS PER CRJ900 SRM 51-10-06-001-001-A01 AND HINGES AND FITTINGS WERE REP
- [SDR REXA2026052700735](https://openairdocs.org/sdr/REXA2026052700735.md): Hinge · corroded · Nov 27, 2025 · N921XJ · Cndair CL6002D24 · Aerodynamic Fairings
  > CORROSION ON HINGES (2EA) AND HINGE FITTINGS (2EA) AT ACCESS FAIRING PANEL 196DR CORROSION ON HINGES (2EA) AND HINGE FITTINGS (2EA) AT ACCESS FAIRING PANEL 196DR WAS EVALUATED OUT OFF LIMITS PER SRM 51-10-06-001-001-A01 AND HINGES AND FITTINGS WERE REPLACED P
- [SDR REXA2026052700779](https://openairdocs.org/sdr/REXA2026052700779.md): Channel · cracked · Nov 26, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON CHANNEL AT AFT BAGGAGE BAY STRUCTURE CRACK ON CHANNEL AT AFT BAGGAGE BAY STRUCTURE WAS REPAIRED PER EA CRJ953-20952 REV IR
- [SDR REXA2024111101466](https://openairdocs.org/sdr/REXA2024111101466.md): Lamp · inoperative · Nov 3, 2024 · N921XJ · Cndair CL6002D24 · Emergency Lighting
  > RH FARTHEST AFT EMERGENCY LIGHT OUT AND LENS CRACKED. RE-LAMPED RH AFT EMERGENCY LIGHT IAW CMM 33-52-07. REMOVED AND REPLACED LENS IAW CMM 33-52-07. OPS CHECK GOOD. PN OFF/ON: 8GH002473-08 PN OFF/ON: 9EL400042-11
- [SDR REXA2024110101413](https://openairdocs.org/sdr/REXA2024110101413.md): Door · cracked · May 17, 2024 · N921XJ · Cndair CL6002D24 · Emergency Exits
  > FOUND THE RH FWD OVERWING EMERGENCY EXIT TO HAVE A CRACK JUST BELOW THE UPPER AFT LUG. DOOR PN# SH670-36600, SN# SB0707. REPAIRED IAW ENDEAVOR EA CRJ952-16678 REV. P2 DATED 5-28-2024
- [SDR REXA2024110101412](https://openairdocs.org/sdr/REXA2024110101412.md): Door · cracked · May 17, 2024 · N921XJ · Cndair CL6002D24 · Emergency Exits
  > FOUND THE LH AFT OVERWING EMERGENCY EXIT TO HAVE A CRACK JUST BELOW THE UPPER FWD LUG. DOOR PN# SH670-36600, SN# SB0704. REPAIRED IAW ENDEAVOR EA CRJ952-16680 REV. DATED 5-28-2024
- [SDR REXA2024110101411](https://openairdocs.org/sdr/REXA2024110101411.md): Door · cracked · May 17, 2024 · N921XJ · Cndair CL6002D24 · Emergency Exits
  > FOUND THE LH FWD OVERWING EMERGENCY EXIT TO HAVE A CRACK JUST BELOW THE UPPER AFT LUG. DOOR PN# SH670-36600, SN# SB0706. REPAIRED IAW ENDEAVOR EA CRJ952-16679 REV. P2 DATED 5-28-2024

Next page: https://openairdocs.org/aircraft/N921XJ/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 = 'N921XJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N921XJ/reports

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