N921XJ

Service difficulty reports · 153

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR REXA2026073001337Lamp · inoperativeLH 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 GOODJul 28, 2026 · N921XJ · Cndair CL6002D24 · Emergency LightingSDR REXA2026052700780Attach Angle · crackedCRACKED 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-A01Dec 15, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Main, Attach FittingsSDR REXA2026052700763Frame · damagedELONGATED 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 11Dec 15, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2026052700738Strut · corrodedPITTING WAS FOUND ON MLG SHOCK STRUT LH SIDE BELOW IDENTIFICATION PLACARD. MLG SHOCK STRUT WILL BE REPLACED BY CARD 900-32-730-705Dec 13, 2025 · N921XJ · Cndair CL6002D24 · Main Landing Gear Strut/Axle/TruckSDR REXA2026052700762Diaphragm · chafedSECONDARY 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 IDec 12, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052700761Plate · corrodedCORROSION 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 BAGDec 9, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026052700759Hinge · chafedWEAR 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 Dec 8, 2025 · N921XJ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026052700778Bracket · corrodedCORROSION 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 BRDec 5, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052700776Seat Track · corrodedCORROSION 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 ANDec 5, 2025 · N921XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026052700775Seat Track · corrodedCORROSION 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 FDec 5, 2025 · N921XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026052700767Seat Track · crackedCORROSION 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+6Dec 5, 2025 · N921XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026052700766Seat Track · corrodedCORROSION 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 LIMDec 5, 2025 · N921XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026052700765Seat Track · corrodedCORROSION 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+3Dec 5, 2025 · N921XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026052700758Intercostal · corrodedCORROSION 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 MINIMDec 5, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052700757Floor Support · corrodedCORROSION 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 SEDec 5, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052700756Stringer · corrodedCORROSION 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. ADec 5, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026052700755Frame · corrodedCORROSION 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.Dec 5, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2026052700733Stringer Splice · corrodedCORROSION 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: CRJ953Dec 5, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026052700732Floor Support · corrodedCORROSION 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 27LBLDec 5, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052700731Seat Track · corrodedCORROSION 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 92Dec 5, 2025 · N921XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026052700754Access Panel · corrodedRUSTED 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.Dec 4, 2025 · N921XJ · Cndair CL6002D24 · Wing, Plate/SkinSDR REXA2026052700753Angle · corrodedCORROSION 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 MEMBRANDec 4, 2025 · N921XJ · Cndair CL6002D24 · Fluid Service DoorsSDR REXA2026052700751Packer · corrodedCORROSION 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 51-42-02-001-001Dec 4, 2025 · N921XJ · Cndair CL6002D24 · Electrical/Electronic Compartment DoorsSDR REXA2026052700741Intercostal · corrodedCORROSION 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 OUTDec 4, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052700740Intercostal · corrodedCORROSION 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 OUTDec 4, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052700774Floor Support · crackedCRACKED 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 Dec 3, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052700752Floor Support · corrodedCORROSION 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-Dec 3, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052700739Fitting · corrodedCORROSION 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-Dec 3, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052700783Fitting · corrodedCORROSION IN FITTING UNDER LAMP (1EA) ON GALLEY 2 FITTING UNDER LAMP (A391251-3 1EA) ON GALLEY 2 WAS REPLACED PER CMM SAFRAN 25-32-84Dec 2, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052700730Fitting · corrodedCORROSION 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 IDec 2, 2025 · N921XJ · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026052700773Frame · crackedCRACK 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 IRNov 30, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2026052700772Frame · crackedCRACK 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 IRNov 30, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2026052700750Rib · crackedCRACK 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-A01Nov 30, 2025 · N921XJ · Cndair CL6002D24 · Wing, Rib/BulkheadSDR REXA2026052700749Rib · crackedCRACK 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.Nov 30, 2025 · N921XJ · Cndair CL6002D24 · Wing, Rib/BulkheadSDR REXA2026052700743Retainer · corrodedCORROSION 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-A01Nov 30, 2025 · N921XJ · Cndair CL6002D24 · Electrical/Electronic Compartment DoorsSDR REXA2026052700742Retainer · corrodedCORROSION 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-A01Nov 30, 2025 · N921XJ · Cndair CL6002D24 · Electrical/Electronic Compartment DoorsSDR REXA2026052700748Support Angle · corrodedCORROSION & 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 ONov 29, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052700747Bracket · corrodedCORROSION 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 OFFNov 28, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052700746Diaphragm · crackedCRACK 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-ANov 28, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052700768Door Sill · crackedCRACK 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-A01Nov 27, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026052700745Bracket · crackedCORROSION 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 23Nov 27, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052700744Angle · crackedCRACKED 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 51-42-21-001-00Nov 27, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052700737Hinge · corrodedCORROSION 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 REPNov 27, 2025 · N921XJ · Cndair CL6002D24 · Aerodynamic FairingsSDR REXA2026052700736Hinge · corrodedCORROSION 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 REPNov 27, 2025 · N921XJ · Cndair CL6002D24 · Aerodynamic FairingsSDR REXA2026052700735Hinge · corrodedCORROSION 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 PNov 27, 2025 · N921XJ · Cndair CL6002D24 · Aerodynamic FairingsSDR REXA2026052700779Channel · crackedCRACK ON CHANNEL AT AFT BAGGAGE BAY STRUCTURE CRACK ON CHANNEL AT AFT BAGGAGE BAY STRUCTURE WAS REPAIRED PER EA CRJ953-20952 REV IRNov 26, 2025 · N921XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2024111101466Lamp · inoperativeRH 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: 9EL400042-11Nov 3, 2024 · N921XJ · Cndair CL6002D24 · Emergency LightingSDR REXA2024110101413Door · crackedFOUND 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 5-28-2024May 17, 2024 · N921XJ · Cndair CL6002D24 · Emergency ExitsSDR REXA2024110101412Door · crackedFOUND 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 5-28-2024May 17, 2024 · N921XJ · Cndair CL6002D24 · Emergency ExitsSDR REXA2024110101411Door · crackedFOUND 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 5-28-2024May 17, 2024 · N921XJ · Cndair CL6002D24 · Emergency Exits
Back to N921XJ