N928XJ

Service difficulty reports · 233

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 = 'N928XJ' 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 REXA2026082401626Stringer · corrodedCORROSION WAS FOUND ON STGR 26R BTW FS 1015.00 TO 1031.00 AT INTERNAL FUSELAGE STRUCTURE. CORROSION ON STGR 26R BTW FS 1015.00 TO 1031.00 AT INTERNAL FUSELAGE STRUCTURE WAS REPAIRED PER EA NO. CRJ953-22756 REV. IRAug 4, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026082401609Stringer · corrodedAFTER SPLICE REMOVAL, CORROSION WAS FOUND ON STGR 23R BTW FS 333. STRINGER SECTION 23RH BTW FS 333.00 TO 379.00 WAS REMPLACED PER CRJ 900 SRM 51-42-21-001-001-A01 6. C. AND SRM 51-42-13-001-001-A01 PAR 6Aug 4, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026082401569Hinge · crackedDURING L1 DOOR ACCESS PANEL 832ET REMOVAL, CRACK WAS FOUND ON HINGE. HINGE ON ACCESS PANEL 832ET WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01.Jul 21, 2026 · N928XJ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026082401556Stiffener · corrodedAFTER TOP PANEL REMOVAL, CORROSION ON STIFFERNERS OF THE TOP PANEL WAS FOUND ON FWD PASSENGER DOOR. STIFFENERS (3 EAS) WERE REPLACED AND STIFFERNERS (2 EAS) WERE REMOVED AND CLEANED AND AFTER STIFFENER WERE CLEANED AND DVI WAS PERFORMED AND NOT CORROSION WAS FJul 14, 2026 · N928XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2026082401629Skin · corrodedCORROSION AND SCRATCHES AROUND OF SETTLEMENT AREA WERE FOUND. CORROSION AND SCRATCHES AROUND OF SETTLEMENT AREA WERE REPAIRED PER EA NO. CRJ953-22761 REV. IRJul 12, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR REXA2026082401608Floor Support · corrodedAFTER ANGLE REMOVAL, CRACKED ANGLE WAS FOUND OVER RBL12 BTW FS 250.00 TO 280.00 AT FLOOR STRUCTURE. NEW ANGLE OVER RBL12 BTW FS 250.00 TO 280.00 AT FLOOR STRUCTURE WAS DRILLED, TREATED & PAINTED PER CRJ 900 SRM 51-40-11-001-001-A01, SRM 51-21-11-001-001-A01 & Jul 10, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082401607Stringer · corrodedCORROSION WAS FOUND ON STRINGER 22R BTW FS 333.00 TO 349.00. DUE TO EXCESSIVE CORROSION ON STRINGER 22R BTW FS 333.00 TO 349.00, STRINGER WAS REPLACED PER CRJ 900 SRM 51-10-06-001-001-A01, SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01Jul 10, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082401627Floor Support · crackedAFTER ANGLE FLOOR SUPPORT REMOVAL AT LBL 12 IN REF NRC 00250,CRACK WAS FOUND. ANGLE FLOOR SUPPORT AT LBL 12 BTW 265 TO 280 WAS DRILLED AND TREATED PER CRJ 900 SRM 51-40-11-001-001-A01, CRJ 900 SRM 51-21-11-001-001-A01 AND SRM 51-25-06-001-001-A01 WILL BE INSTAJul 9, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082401606Fitting · corrodedCORROSION WAS FOUND ON FITTING HANDRAIL (2EAS). FITTING HANDRAIL (2EAS) WERE REPLACED PER CRJ-900 SRM 51-42-20-001-001-A01Jul 9, 2026 · N928XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2026082401605Fitting · corrodedCORROSION WAS FOUND ON FITTING HANDRAIL (2EAS). FITTING HANDRAIL (2EAS) WERE REPLACED PER CRJ-900 SRM 51-42-20-001-001-A01Jul 9, 2026 · N928XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2026082401560Angle · corrodedCORROSION WAS FOUND ON KICKPLATE ANGLE. THE KICKPLATE ANGLE WAS REPLACED IAW SRM 51-42-06-001-001-A01.Jul 8, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082401625Striker · crackedCORROSION ON SEAL STRIKER WAS FOUND BTW FS 310.00 TO 349.00 AT GALLEY SERVICE DOOR SURROUND STRUCTURE. DUE TO EXCESSIVE CORROSION ON SEAL STRIKER ON BTW FS 310.00 TO 349.00 AT GALLEY SERVICE DOOR SURROUND STRUCTURE WAS EVALUATED OUT LIMITS PER CRJ 900 SRM 51-1Jul 6, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026082401603Hinge Fitting · corrodedCORROSION WAS FOUND ON LH/RH NLG AFT DOOR HINGE FITTING (2 EAS) AND CORROSION ON RH/LH AIRFRAME HINGE FITTING (2 EAS) AT NLG DUE TO EXCESSIVE CORROSION ON LH/RH NLG AFT DOOR HINGE FITTING (2 EAS) AND RH/LH AIRFRAME HINGE FITTING (2 EAS) AT NLG WERE REPLACED PEJul 3, 2026 · N928XJ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026082401602Hinge Fitting · corrodedCORROSION WAS FOUND ON LH/RH NLG AFT DOOR HINGE FITTING (2 EAS) AND CORROSION ON RH/LH AIRFRAME HINGE FITTING (2 EAS) AT NLG DUE TO EXCESSIVE CORROSION ON LH/RH NLG AFT DOOR HINGE FITTING (2 EAS) AND RH/LH AIRFRAME HINGE FITTING (2 EAS) AT NLG WERE REPLACED PEJul 3, 2026 · N928XJ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026082401601Hinge Fitting · corrodedCORROSION WAS FOUND ON LT/RT NLG AFT DOOR HINGE FITTING (2 EAS) AND CORROSION ON RH/LH AIRFRAME HINGE FITTING (2 EAS) AT NLG DUE TO EXCESSIVE CORROSION ON LH/RH NLG AFT DOOR HINGE FITTING (2 EAS) AND RH/LH AIRFRAME HINGE FITTING (2 EAS) AT NLG WERE REPLACED PEJul 3, 2026 · N928XJ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026082401637Fitting · corrodedCORROSION FLOOR FITTING IN FWD ACCESS 305 (1EA) ON GALLEY 3. SUMMARY OF NRC 00296:FLOOR FITTING IN FWD ACCESS 305 (1 EA) ON GALLEY 3 WAS REPLACED PER ZODIAC AEROSPACE CMM 25-33-18 REV 5 DATE MAY 15/15Jul 1, 2026 · N928XJ · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026082401636Fitting · corrodedCORROSION FLOOR FITTING IN FWD ACCESS 306 (1EA) ON GALLEY 3. SUMMARY OF NRC 00295: FLOOR FITTING IN FWD ACCESS 306 (1EA) ON GALLEY 3 WAS INSTALLED PER ZODIAC AEROSPACE CMM 25-33-18 REV 5 DATE MAY 15/15.Jul 1, 2026 · N928XJ · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026082401633Hinge Fitting · corrodedAFTER BUSHINGS REMOVAL, CORROSION WAS FOUND ON AILERON CENTER FITTING LUGS L1, L2, L5 AND L6 ALSO CORROSION ON LOWER AND UPPER LUGS OF OUT FITTING AT LH AILERON. LUGS BORES ON CENTER FITTING L1, L2 AND L6 AND UPPER LUG OF OUT FITTING FROM LH AILERON WERE CLEANJul 1, 2026 · N928XJ · Cndair CL6002D24 · AileronsSDR REXA2026082401568Access Panel · corrodedCORROSION ON ACCESS PANEL 832AT, 832BT, 832CT, 832ET AND 832FT ALSO ENLOGANTED SUPPORT ANGLE AND BROKEN ACCESS PANEL 832FT. CORROSION WAS REMOVED ON ACCESS PANEL 832AT, 832BT, 832CT, 832ET PER SRM 51-21-06-001-001-A01 AND WERE FOUND WITHIN LIMITS PER SRM 52-11Jul 1, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Structure (General)SDR REXA2026082401555Fitting · corrodedSECONDARY NRC FROM RC 900-27-900-912': AFTER BUSHINGS REMOVAL, CORROSION WAS FOUND ON AILERON CENTER FITTING LUGS R1, R2, R3, R4, R5 AND R6 AT RH AILERON. LUGS BORES ON FITTING CENTER R1, R2, R3, R4 AND R6 FROM RH AILERON WERE CLEANED PER SRM 51-26-00-001-001-Jul 1, 2026 · N928XJ · Cndair CL6002D24 · AileronsSDR REXA2026082401628Support · crackedAFTER SEAL RETAINERS SUPPORTS REMOVAL, CRACKED FORWARD LOWER SKIN ANGLE (SUPPORT OF SEAL RETAINERS) WAS FOUND AT RH WING. FORWARD LOWER SKIN ANGLE WAS REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01 PAR. 8 C AND SRM CRJ 900 SRM 51-42-21-001-001-A01 PAR 6. C.Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082401624Frame · corrodedCORROSION ON ANGLE OF FRAME FS 1015 STGR 20L CORROSION ON ANGLE OF FRAME FS 1015 STGR 20L WAS REOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND EVALUATED OUT LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 AND IT WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2026082401623Frame · corrodedCORROSION ON FRAME FS 1015 STGR 26R TO STGR 23L REPAIR PER EA NO. CRJ953-22686 REV. IRJun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2026082401622Window Frame · crackedCRACK ON BOTTOM ANGLE POST (2 EAS) LH/RH ON INTERNAL STRUCTURE BTWN WINDSHIELD AND SIDE WINDOWS. ANGLE POST (2 EAS) LH/RH ON INTERNAL STRUCTURE BTWN WINDSHIELD AND SIDE WINDOWS WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026082401621Window Frame · crackedCRACK ON BOTTOM ANGLE POST (2 EAS) LH/RH ON INTERNAL STRUCTURE BTWN WINDSHIELD AND SIDE WINDOWS. ANGLE POST (2 EAS) LH/RH ON INTERNAL STRUCTURE BTWN WINDSHIELD AND SIDE WINDOWS WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026082401620Floorbeam · crackedCRACK ON FLOOR BEAM RBL12 ON FS280 AT FLIGHT COMPARTMENT FLOOR STRUCTURE. FLOOR BEAM RBL12 ON FS280 AT FLIGHT COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER REO 690-53-11-2225 REV - -Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2026082401619Intercostal · corrodedCORROSION ON INTERCOSTAL BTW FS=866 TO 861/ STGR 21R AT INTERNAL FUSELAGE STRUCTURE DUE TO EXCESSIVE CORROSION ON INTERCOSTAL BTW FS=866 TO 861/ STGR 21R AT INTERNAL FUSELAGE STRUCTURE WAS REPLACED PER CRJ-900 SRM 51-10-06-001-001-A01, SRM 51-42-06-001-001-A01Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082401618Support Angle · crackedCRACK ANGLE SUPPORT INSIDE OF ACCESS PANEL 122CR ANGLE SUPPORT INSIDE OF ACCESS PANEL 122CR WAS FABRICATED AND REPLACED PER EA NO CRJ953-22677 REV. IR AND CRJ-900 SRM 51-42-21-001-001-A01Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082401617Frame · crackedCORROSION ON FRAME FS 661+46 BTW STGR25R TO STGR 23R, FRAME 661+32 BTW STGR 27 TO STGR 25R, FRAME FS 661 BTW STGR 27R TO STGR 26R, FRAME FS 597 BTW STGR 27 TO STGR 26R. FRAME FS 661 BTW STGR 27R TO STGR 26R WAS REPAIRED PER CRJ 900 SRM 53-00-06-201-001-A03Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2026082401614Web · corrodedCORROSION ON WEB BTW 1LBL TO 27LBL BTW FS 1088 TO FS 1098 CORROSION ON WEB BTW 1LBL TO 27LBL BTW FS 1088 TO FS 1098 WAS EA NO. REPAIRED PER CRJ953-22801 REV. BJun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082401600Hinge Fitting · corrodedCORROSION WAS FOUND ON BORE LUGS OF AILERON HINGES 2, 3 AND 4, ALSO CORROSION ON INB LUG FACE OF HINGE 4 AT RH WING REAR SPAR. BORE LUGS OF AILERON HINGES 2, 3 AND 4, ALSO INB LUG FACE OF HINGE 4 AT RH WING REAR SPAR WERE REPAIRED PER REO 690-57-51-552 REV. - Jun 30, 2026 · N928XJ · Cndair CL6002D24 · AileronsSDR REXA2026082401599Hinge Fitting · corrodedCORROSION WAS FOUND ON BORE LUGS OF AILERON HINGES 2, 3 AND 4, ALSO CORROSION ON INB LUG FACE OF HINGE 4 AT RH WING REAR SPAR. BORE LUGS OF AILERON HINGES 2, 3 AND 4, ALSO INB LUG FACE OF HINGE 4 AT RH WING REAR SPAR WERE REPAIRED PER REO 690-57-51-552 REV. - Jun 30, 2026 · N928XJ · Cndair CL6002D24 · AileronsSDR REXA2026082401598Hinge Fitting · corrodedCORROSION WAS FOUND ON BORE LUGS OF AILERON HINGES 2, 3 AND 4, ALSO CORROSION ON INB LUG FACE OF HINGE 4 AT RH WING REAR SPAR. BORE LUGS OF AILERON HINGES 2, 3 AND 4, ALSO INB LUG FACE OF HINGE 4 AT RH WING REAR SPAR WERE REPAIRED PER REO 690-57-51-552 REV. - Jun 30, 2026 · N928XJ · Cndair CL6002D24 · AileronsSDR REXA2026082401597Support Beam · chafedWEAR ON BEAM SUPPORT OF BUNGE MECHANISM NEXT TO AFT PULLEY AT AFT BAGGAGE COMPARTMENT. WEAR ON BEAM SUPPORT OF BUNGE MECHANISM NEXT TO AFT PULLEY AT AFT BAGGAGE COMPARTMENT WAS REPAIRED PER EA NO. CRJ953-22738 REV. IRJun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026082401596Stringer · corrodedCORROSION ON STRINGER 21R FROM FS319 TO FS333 AND FROM FS394 TO FS453 AT E/E COMPARTMENT DUE TO EXCESSIVE CORROSION ON STRINGER 21R FROM FS394 TO FS477 AT E/E COMPARTMENT WAS REPLACED PER CRJ 900 SRM 51-10-06-001-001-A01, SRM 53-21-03-101-002-A04, SRM 51-42-06Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026082401595Stringer · corrodedCORROSION ON STRINGER 21R FROM FS319 TO FS333 AND FROM FS394 TO FS453 AT E/E COMPARTMENT DUE TO EXCESSIVE CORROSION ON STRINGER 21R FROM FS280 TO FS333 AT E/E COMPARTMENT WAS REPLACED PER CRJ 900 SRM 51-10-06-001-001-A01, SRM 53-21-03-101-002-A04, SRM 51-42-06Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026082401594Stringer · corrodedCORROSION ON STRINGER 19R FROM FS310 TO FS319 AND FROM FS437 TO FS477 AT E/E COMPARTMENT. DUE TO EXCESSIVE CORROSION ON STRINGER FS437 TO FS477 AT E/E COMPARTMENT WAS REPAIRED PER CRJ-900 SRM 53-00-03-201-001-A02Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026082401593Doubler · corrodedCORROSION ON INTERNAL ANTENNA DOUBLER BTW FS295 AND FS310 BTW STGR26L AND STGR26R AT E/E COMPARTMENT. INTERNAL ANTENNA DOUBLER BTW FS295 AND FS310 BTW STGR26L AND STGR26R AT E/E COMPARTMENT WAS REPAIRED PER EA NO. CRJ953-22769 REV. IRJun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR REXA2026082401592Stringer Splice · corrodedDUE TO EXCESSIVE CORROSION ON STRINGER SPLICES (3E/A) ON FS333 ON STGR21R, STGR22R AND STGR23R AT E/E COMPARTMENT WERE REPLACED PER CRJ 900 SRM 51-10-06-001-001-A01, SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01 DUE TO EXCESSIVE CORROSION ON STRINGER SJun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026082401591Stringer Splice · corrodedDUE TO EXCESSIVE CORROSION ON STRINGER SPLICES (3E/A) ON FS333 ON STGR21R, STGR22R AND STGR23R AT E/E COMPARTMENT WERE REPLACED PER CRJ 900 SRM 51-10-06-001-001-A01, SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01 DUE TO EXCESSIVE CORROSION ON STRINGER SJun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026082401590Stringer Splice · corrodedDUE TO EXCESSIVE CORROSION ON STRINGER SPLICES (3E/A) ON FS333 ON STGR21R, STGR22R AND STGR23R AT E/E COMPARTMENT WERE REPLACED PER CRJ 900 SRM 51-10-06-001-001-A01, SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01 DUE TO EXCESSIVE CORROSION ON STRINGER SJun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026082401589Frame · corrodedCORROSION ON FRAMES BTW FS=847+16/STGR26L TO 26R, FS=847+32/STGR26L TO 26R AT INTERNAL FUSELAGE STRUCTURE CORROSION ON FRAMES BTW FS=847+16/STGR26L TO 26R WAS REPAIRED PER EA NO. CRJ953-22764 REV. IRJun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2026082401559Structure · crackedCRACK EXTERNAL POWER BOX INSIDE OF ACCESS PANEL 122DR. EXTERNAL POWER BOX INSIDE OF ACCESS PANEL 122DR WAS REPLACED IAW SRM 51-42-06-001-001-A01, & SRM 51-42-21-001-001-A01.Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026082401558Seat Track · corrodedCORROSION ON SIDE SEAT TRACKS BTW BS 744 - 768 RT SIDE AND BTW BS 785 - 847+16 LT SIDE IN PAX CABIN. CORROSION ON SIDE SEAT TRACKS WAS EVALUATED OUT LIMITS IAW SRM 53-41-49-101-001-A02. REPLACED IAW AMM 53-00-49.Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026082401557Seat Track · corrodedCORROSION ON SIDE SEAT TRACK BTW BS 744 - 768 RT SIDE & BTW BS 785 - 847+16 LT SIDE AT PAX CABIN CORROSION ON SIDE SEAT TRACK LT SIDE EVALUATED OUT LIMITS IAW SRM 53-41-49-101-001-A02. REPLACED IAW AMM 53-00-49.Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026082401552Frame · corrodedCORRODED FRAME, FS 1000, STR 25R - 23L. THE FRAME WAS REPAIRED IAW EA CRJ953-22813, REV IR.Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2026082401549Rib · corrodedCRACK ON RIB WS=14.50 AT RH MLG WHEEL WELL AREA. THE RIB WAS REPLACED IAW SRM 51-42-21-001-001-A01, PAR 6.C, SRM 51-42-22-001-001-A01, PAR. 6.& AMM 32-32-06.Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082401616Angle · crackedCRACK ANGLE CLIPS (2EAS) BTW FS=1088.20 /STGR10R AND STGR10L AT AFT BAGGAGE BAY CRACK ANGLE CLIPS (2EAS) BTW FS=1088.20 /STGR10R AND STGR10L AT AFT BAGGAGE BAY WERE FABRICATED AND REPLACED PER EA CRJ953-22713 REV IR AND EA CRJ953-22714 REV IR AND CRJ-900 SRM Jun 29, 2026 · N928XJ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2026082401615Angle · crackedCRACK ANGLE CLIPS (2EAS) BTW FS=1088.20 /STGR10R AND STGR10L AT AFT BAGGAGE BAY CRACK ANGLE CLIPS (2EAS) BTW FS=1088.20 /STGR10R AND STGR10L AT AFT BAGGAGE BAY WERE FABRICATED AND REPLACED PER EA CRJ953-22713 REV IR AND EA CRJ953-22714 REV IR AND CRJ-900 SRM Jun 29, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082401566Angle · corrodedCORROSION ON MID CAP ANGLE (PASSENGER FLOOR SILL AREA) AT PAX CABIN FLOOR STRUCTURE MID CAP ANGLE (PASSENGER FLOOR SILL AREA) AT PAX CABIN FLOOR STRUCTURE WAS REPLACED PER CRJ900 SRM 51-40-11-001-001-A01 AND CRJ-900 SRM 51-41-02-001-001-A01Jun 29, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
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