# Service difficulty reports: N928XJ A list on [N928XJ](https://openairdocs.org/aircraft/N928XJ.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 5 · 233 reports - [SDR REXA2026082401626](https://openairdocs.org/sdr/REXA2026082401626.md): Stringer · corroded · Aug 4, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION 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. IR - [SDR REXA2026082401609](https://openairdocs.org/sdr/REXA2026082401609.md): Stringer · corroded · Aug 4, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > AFTER 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 6 - [SDR REXA2026082401569](https://openairdocs.org/sdr/REXA2026082401569.md): Hinge · cracked · Jul 21, 2026 · N928XJ · Cndair CL6002D24 · Fuselage, Door Hinge > DURING 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. - [SDR REXA2026082401556](https://openairdocs.org/sdr/REXA2026082401556.md): Stiffener · corroded · Jul 14, 2026 · N928XJ · Cndair CL6002D24 · Passenger/Crew Doors > AFTER 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 F - [SDR REXA2026082401629](https://openairdocs.org/sdr/REXA2026082401629.md): Skin · corroded · Jul 12, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin > CORROSION AND SCRATCHES AROUND OF SETTLEMENT AREA WERE FOUND. CORROSION AND SCRATCHES AROUND OF SETTLEMENT AREA WERE REPAIRED PER EA NO. CRJ953-22761 REV. IR - [SDR REXA2026082401608](https://openairdocs.org/sdr/REXA2026082401608.md): Floor Support · corroded · Jul 10, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > AFTER 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 & - [SDR REXA2026082401607](https://openairdocs.org/sdr/REXA2026082401607.md): Stringer · corroded · Jul 10, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION 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-A01 - [SDR REXA2026082401627](https://openairdocs.org/sdr/REXA2026082401627.md): Floor Support · cracked · Jul 9, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > AFTER 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 INSTA - [SDR REXA2026082401606](https://openairdocs.org/sdr/REXA2026082401606.md): Fitting · corroded · Jul 9, 2026 · N928XJ · Cndair CL6002D24 · Passenger/Crew Doors > CORROSION WAS FOUND ON FITTING HANDRAIL (2EAS). FITTING HANDRAIL (2EAS) WERE REPLACED PER CRJ-900 SRM 51-42-20-001-001-A01 - [SDR REXA2026082401605](https://openairdocs.org/sdr/REXA2026082401605.md): Fitting · corroded · Jul 9, 2026 · N928XJ · Cndair CL6002D24 · Passenger/Crew Doors > CORROSION WAS FOUND ON FITTING HANDRAIL (2EAS). FITTING HANDRAIL (2EAS) WERE REPLACED PER CRJ-900 SRM 51-42-20-001-001-A01 - [SDR REXA2026082401560](https://openairdocs.org/sdr/REXA2026082401560.md): Angle · corroded · Jul 8, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION WAS FOUND ON KICKPLATE ANGLE. THE KICKPLATE ANGLE WAS REPLACED IAW SRM 51-42-06-001-001-A01. - [SDR REXA2026082401625](https://openairdocs.org/sdr/REXA2026082401625.md): Striker · cracked · Jul 6, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Structure > CORROSION 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 51-1 - [SDR REXA2026082401603](https://openairdocs.org/sdr/REXA2026082401603.md): Hinge Fitting · corroded · Jul 3, 2026 · N928XJ · Cndair CL6002D24 · Fuselage, Door Hinge > CORROSION 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 PE - [SDR REXA2026082401602](https://openairdocs.org/sdr/REXA2026082401602.md): Hinge Fitting · corroded · Jul 3, 2026 · N928XJ · Cndair CL6002D24 · Fuselage, Door Hinge > CORROSION 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 PE - [SDR REXA2026082401601](https://openairdocs.org/sdr/REXA2026082401601.md): Hinge Fitting · corroded · Jul 3, 2026 · N928XJ · Cndair CL6002D24 · Fuselage, Door Hinge > CORROSION 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 PE - [SDR REXA2026082401637](https://openairdocs.org/sdr/REXA2026082401637.md): Fitting · corroded · Jul 1, 2026 · N928XJ · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings > CORROSION 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 15/15 - [SDR REXA2026082401636](https://openairdocs.org/sdr/REXA2026082401636.md): Fitting · corroded · Jul 1, 2026 · N928XJ · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings > CORROSION 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. - [SDR REXA2026082401633](https://openairdocs.org/sdr/REXA2026082401633.md): Hinge Fitting · corroded · Jul 1, 2026 · N928XJ · Cndair CL6002D24 · Ailerons > AFTER 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 CLEAN - [SDR REXA2026082401568](https://openairdocs.org/sdr/REXA2026082401568.md): Access Panel · corroded · Jul 1, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Structure (General) > CORROSION 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 52-11 - [SDR REXA2026082401555](https://openairdocs.org/sdr/REXA2026082401555.md): Fitting · corroded · Jul 1, 2026 · N928XJ · Cndair CL6002D24 · Ailerons > SECONDARY 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- - [SDR REXA2026082401628](https://openairdocs.org/sdr/REXA2026082401628.md): Support · cracked · Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > AFTER 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. - [SDR REXA2026082401624](https://openairdocs.org/sdr/REXA2026082401624.md): Frame · corroded · Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Frame > CORROSION 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-A01 - [SDR REXA2026082401623](https://openairdocs.org/sdr/REXA2026082401623.md): Frame · corroded · Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Frame > CORROSION ON FRAME FS 1015 STGR 26R TO STGR 23L REPAIR PER EA NO. CRJ953-22686 REV. IR - [SDR REXA2026082401622](https://openairdocs.org/sdr/REXA2026082401622.md): Window Frame · cracked · Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Structure > CRACK 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-A01 - [SDR REXA2026082401621](https://openairdocs.org/sdr/REXA2026082401621.md): Window Frame · cracked · Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Structure > CRACK 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-A01 - [SDR REXA2026082401620](https://openairdocs.org/sdr/REXA2026082401620.md): Floorbeam · cracked · Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam > CRACK 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 - - - [SDR REXA2026082401619](https://openairdocs.org/sdr/REXA2026082401619.md): Intercostal · corroded · Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION 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-A01 - [SDR REXA2026082401618](https://openairdocs.org/sdr/REXA2026082401618.md): Support Angle · cracked · Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACK 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-A01 - [SDR REXA2026082401617](https://openairdocs.org/sdr/REXA2026082401617.md): Frame · cracked · Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Frame > CORROSION 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-A03 - [SDR REXA2026082401614](https://openairdocs.org/sdr/REXA2026082401614.md): Web · corroded · Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION 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. B - [SDR REXA2026082401600](https://openairdocs.org/sdr/REXA2026082401600.md): Hinge Fitting · corroded · Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Ailerons > CORROSION 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. - - [SDR REXA2026082401599](https://openairdocs.org/sdr/REXA2026082401599.md): Hinge Fitting · corroded · Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Ailerons > CORROSION 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. - - [SDR REXA2026082401598](https://openairdocs.org/sdr/REXA2026082401598.md): Hinge Fitting · corroded · Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Ailerons > CORROSION 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. - - [SDR REXA2026082401597](https://openairdocs.org/sdr/REXA2026082401597.md): Support Beam · chafed · Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Structure > WEAR 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. IR - [SDR REXA2026082401596](https://openairdocs.org/sdr/REXA2026082401596.md): Stringer · corroded · Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION 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 51-42-06 - [SDR REXA2026082401595](https://openairdocs.org/sdr/REXA2026082401595.md): Stringer · corroded · Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION 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 51-42-06 - [SDR REXA2026082401594](https://openairdocs.org/sdr/REXA2026082401594.md): Stringer · corroded · Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION 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-A02 - [SDR REXA2026082401593](https://openairdocs.org/sdr/REXA2026082401593.md): Doubler · corroded · Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin > CORROSION 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. IR - [SDR REXA2026082401592](https://openairdocs.org/sdr/REXA2026082401592.md): Stringer Splice · corroded · Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > DUE 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 S - [SDR REXA2026082401591](https://openairdocs.org/sdr/REXA2026082401591.md): Stringer Splice · corroded · Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > DUE 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 S - [SDR REXA2026082401590](https://openairdocs.org/sdr/REXA2026082401590.md): Stringer Splice · corroded · Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > DUE 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 S - [SDR REXA2026082401589](https://openairdocs.org/sdr/REXA2026082401589.md): Frame · corroded · Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Frame > CORROSION 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. IR - [SDR REXA2026082401559](https://openairdocs.org/sdr/REXA2026082401559.md): Structure · cracked · Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Structure > CRACK 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. - [SDR REXA2026082401558](https://openairdocs.org/sdr/REXA2026082401558.md): Seat Track · corroded · Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION 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. - [SDR REXA2026082401557](https://openairdocs.org/sdr/REXA2026082401557.md): Seat Track · corroded · Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION 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. - [SDR REXA2026082401552](https://openairdocs.org/sdr/REXA2026082401552.md): Frame · corroded · Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Frame > CORRODED FRAME, FS 1000, STR 25R - 23L. THE FRAME WAS REPAIRED IAW EA CRJ953-22813, REV IR. - [SDR REXA2026082401549](https://openairdocs.org/sdr/REXA2026082401549.md): Rib · corroded · Jun 30, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACK 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. - [SDR REXA2026082401616](https://openairdocs.org/sdr/REXA2026082401616.md): Angle · cracked · Jun 29, 2026 · N928XJ · Cndair CL6002D24 · Cargo/Baggage Doors > CRACK 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 - [SDR REXA2026082401615](https://openairdocs.org/sdr/REXA2026082401615.md): Angle · cracked · Jun 29, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACK 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 - [SDR REXA2026082401566](https://openairdocs.org/sdr/REXA2026082401566.md): Angle · corroded · Jun 29, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION 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-A01 Next page: https://openairdocs.org/aircraft/N928XJ/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 = 'N928XJ' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N928XJ/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.