# Service difficulty reports: N929XJ A list on [N929XJ](https://openairdocs.org/aircraft/N929XJ.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 · 174 reports - [SDR REXA2026072801199](https://openairdocs.org/sdr/REXA2026072801199.md): Striker · cracked · Jul 7, 2026 · N929XJ · Cndair CL6002D24 · Fuselage Main, Structure > WEAR ON FWD FRAME OVER FS629.00 AND STGR24L / STGR23L AT CENTER BAGGAGE BAY DOOR FOR EXCESSIVE DAMAGE ON FRAME OVER FS629.00 AND STGR24L / STGR23L AT CENTER BAGGAGE BAY DOOR WAS REPLACED PER CRJ-900 SRM 53-31-23-101-001-A02, SRM 51-41-02-001-001-A01 AND SRM 5 - [SDR REXA2026072801198](https://openairdocs.org/sdr/REXA2026072801198.md): Floorbeam · cracked · Jul 7, 2026 · N929XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam > CRACKED CENTER COCKPIT FLOOR BEAM LBL 12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. FLOOR BEAM LBL 12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-2217 REV -- - [SDR REXA2026072801195](https://openairdocs.org/sdr/REXA2026072801195.md): Stiffener · cracked · Jul 7, 2026 · N929XJ · Cndair CL6002D24 · Passenger/Crew Doors > CRACK ON UPPPER STIFFENER ATTACHED TO POWER-ASSIST MOTOR BTW DATUM 4 AND DATUM 5 (AFT SIDE PANEL) OF PASSENGER DOOR INTERNAL STRUCTURE. STIFFENER ATTACHED TO POWER-ASSIST MOTOR BTW DATUM 4 AND DATUM 5 (AFT SIDE PANEL) OF PASSENGER DOOR INTERNAL STRUCTURE WAS R - [SDR REXA2026072801194](https://openairdocs.org/sdr/REXA2026072801194.md): Web · cracked · Jul 7, 2026 · N929XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACK ON LT FLOOR WEB AT ELECTRICAL BAY (BELOW BRAKE ACCUMULATOR INDICATION SUPPORT DOUBLER) BS 193 LT FLOOR WEB AT ELECTRICAL BAY (BELOW BRAKE ACCUMULATOR INDICATION SUPPORT DOUBLER) FS193.00 WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01 - [SDR REXA2026072801201](https://openairdocs.org/sdr/REXA2026072801201.md): Seat Track · cracked · Jun 17, 2026 · N929XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON SIDE SEAT RAILS IN SECTIONS FS= 437.00 TO FS= 469.00 AND FROM FS 629.00 TO FS 785.00, STGR 15LH. AND FS 613.00 TO FS 797.00 STGR 15RH AT PAX CABIN SIDE SEAT RAILS IN SECTIONS FS= 437.00 TO FS= 469.00 AND FROM FS 629.00 TO FS 785.00, STGR 15LH. AND - [SDR REXA2026072801200](https://openairdocs.org/sdr/REXA2026072801200.md): Seat Track · cracked · Jun 17, 2026 · N929XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON FLOOR SEAT RAILS IN SECTIONS FS= 364.00 TO FS= 485.00, LBL 27 AT PAX CABIN. FLOOR SEAT RAILS IN SECTIONS FS= 364.00 TO FS= 485.00, LBL 27 AT PAX CABIN WAS REPLACED PER CRJ900 AMM 53-00-49 - [SDR REXA2026072801192](https://openairdocs.org/sdr/REXA2026072801192.md): Seat Track · cracked · Jun 17, 2026 · N929XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON FLOOR SEAT RAILS IN SECTIONS FS= 379.00 TO FS= 485.00, LBL9 AT PAX CABIN. FLOOR SEAT RAILS IN SECTIONS FS= 379.00 TO FS= 485.00, LBL9 AT PAX CABIN WAS REPLACED PER CRJ900 AMM 53-00-49 - [SDR REXA2026072801196](https://openairdocs.org/sdr/REXA2026072801196.md): Rib · cracked · Jun 14, 2026 · N929XJ · Cndair CL6002D24 · Wing, Rib/Bulkhead > CRACK ON LEADING EDGE RIB SS57.16 AT RH WING LEADING EDGE RIB SS57.16 AT RT WING WAS REPAIRED PER REO 690-57-41-604 REV - - - [SDR REXA2026072801197](https://openairdocs.org/sdr/REXA2026072801197.md): Support Bracket · cracked · Jun 13, 2026 · N929XJ · Cndair CL6002D24 · Engine Thrust Reverser > CRACK ON SUPPORT BRACKET TO TIE BAR AT LEFT PYLON SUPPORT BRACKET TO TIE BAR AT LEFT PYLON WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 - [SDR REXA2026072801193](https://openairdocs.org/sdr/REXA2026072801193.md): Support · cracked · Jun 10, 2026 · N929XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACK AT CORNERS OF SUPPORT AT THE JB 6 MODULE AT FWD EQUIPMENT COMPARTMENT. SUPPORT AT THE JB 6 MODULE AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER SRM 51-42-06-001-001-A01 - [SDR REXA2026072801191](https://openairdocs.org/sdr/REXA2026072801191.md): Drag Angle · cracked · Jun 10, 2026 · N929XJ · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings > CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ900 SRM - [SDR REXA2026072801190](https://openairdocs.org/sdr/REXA2026072801190.md): Door Sill · cracked · Jun 10, 2026 · N929XJ · Cndair CL6002D24 · Fuselage Main, Structure > CRACK ON AFT RT DOOR LANDING AT FS 188.00 (AFT LATCH CUT OUT OF ACCESS DOOR 212AR) AFT RT DOOR LANDING AT FS 188.00 (AFT LATCH CUT OUT OF ACCESS DOOR 212AR) WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 & SRM 51-42-13-001-001-A01 - [SDR REXA2024042900365](https://openairdocs.org/sdr/REXA2024042900365.md): Latch · inoperative · Apr 19, 2024 · N929XJ · Cndair CL6002D24 · Passenger Oxygen System > PAX O2 DEPLOYMENT SYSTEM FAILS OPS CHECK. THE MASKS AT THE FOLLOWING SEAT LOCATIONS FAILED TO DROP: 10DC, 14DC, 17BA, AND 20BA. TROUBLESHOT AND FOUND LATCHES TO BE BAD. REMOVED AND REPLACED PAX O2 MASK BOX LATCHES FOR SEATS 10DC, 14DC, 17BA, AND 20BA IAW CRJ-9 - [SDR REXA2024042400362](https://openairdocs.org/sdr/REXA2024042400362.md): Door Frame · cracked · Apr 1, 2024 · N929XJ · Cndair CL6002D24 · Fuselage Main, Structure > RH AFT EMERGENCY EXIT FWD LUG IS CRACKED. REPAIRED IAW ENDEAVOR EA CRJ952-16335 REV IR DATED 4-9-2024. - [SDR REXA2024042400361](https://openairdocs.org/sdr/REXA2024042400361.md): Door Frame · cracked · Apr 1, 2024 · N929XJ · Cndair CL6002D24 · Fuselage Main, Structure > RH FWD EMERGENCY EXIT AFT LUG IS CRACKED. REPAIRED IAW ENDEAVOR EA CRJ952-16334 REV IR DATED 4-9-2024. - [SDR REXA2019120621718](https://openairdocs.org/sdr/REXA2019120621718.md): Battery · discharged · Dec 2, 2019 · N929XJ · Cndair CL6002D24 · Battery/Charger System > ON WAKE UP FOUND MASTER BATTERY SWITCH ON. EMER. LIGHTS WERE NOT COMING ON DUE TO LOW BATTERY CHARGE R/R MAIN BATTERY IAW CRJ900 JC 24-210-901. OPS TEST GOOD AT THIS TIME - [SDR REXA2019102481504](https://openairdocs.org/sdr/REXA2019102481504.md): Intercostal · corroded · Oct 18, 2019 · N929XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > INITIAL INSPECTION: CORROSION ON INTERCOSTAL 27(RH SIDE) AND 26R BTW. FS349 AND FS364 (FWD TO E/E DOOR) [IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E)(TCI 100-09) SUMMARY:INTERCOSTAL 27RH AND 26RH BTW. FS349 AND - [SDR REXA2019102411479](https://openairdocs.org/sdr/REXA2019102411479.md): Hinge · damaged · Oct 18, 2019 · N929XJ · Cndair CL6002D24 · Fuselage, Door Hinge > INITIAL INSPECTION: SPRING DAMAGED AT GROUND POWER ACCESS DOOR(122DR). (SM)(FUS). SUMMARY: HINGE AT GROUND POWER ACCESS DOOR WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01. - [SDR REXA2019102471520](https://openairdocs.org/sdr/REXA2019102471520.md): Hinge Fitting · corroded · Oct 17, 2019 · N929XJ · Cndair CL6002D24 · Landing Gear Doors > AWR HIDDEN DISCREPANCY: AFTER BUSHINGS REMOVAL CORROSION WAS FOUND ON LH/RH HINGE FITTING IN REF JC 900-32-710-902 STEP 5. (FYT) SUMMARY: ON NRC 00369 LH/RH FITTINGS OF NLG AFT DOOR WERE REPLACED FOR NEW ONES PER CRJ-900 SRM 51-42-21-001-001 A01. - [SDR REXA2019102471515](https://openairdocs.org/sdr/REXA2019102471515.md): Frame · corroded · Oct 17, 2019 · N929XJ · Cndair CL6002D24 · Fuselage Main, Frame > INITIAL INSPECTION: CORROSION ON FRAME FS=265 BTW STGR 26R / 26L AT INTERNAL STRUCTURE OF FWD FUSELAGE (SM) (TCI 100-06) SUMMARY: CORROSION ON FRAME FS=265 BTW STGR 26R / 26L AT INTERNAL STRUCTURE OF FWD FUSELAGE WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A - [SDR REXA2019102471514](https://openairdocs.org/sdr/REXA2019102471514.md): Support · corroded · Oct 17, 2019 · N929XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > INITIAL INSPECTION: CORROSION ON JACK FITTING SUPPORT (2EAS) BTW FS=280 / FS=265 AND STGR 26R / 26L AT INTERNAL STRUCTURE OF FWD FUSELAGE (SM) (TCI 53-10-305). SUMMARY OF NRC: 00267 CORROSION ON JACK FITTING SUPPORT (2EAS) BTW FS=280 / FS=265 AND STGR 26R / - [SDR REXA2019102471503](https://openairdocs.org/sdr/REXA2019102471503.md): Intercostal · corroded · Oct 17, 2019 · N929XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > INITIAL INSPECTION: CORROSION ON [INTERCOSTAL] 26L AND 27(LH SIDE) BTW. FS349 AND FS364 (FWD TO E/E DOOR) AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIX A]. (E/E)(TCI 100-09) SUMMARY: CORROSION LEVEL 2.INTERCOSTAL 27(LH SIDE) AND 2 - [SDR REXA2019101701497](https://openairdocs.org/sdr/REXA2019101701497.md): Stringer · corroded · Oct 17, 2019 · N929XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > INITIAL INSPECTION: CORROSION ON STRINGER 25R BTW. FS319.70 AND FS349 AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E)(TCI 100-09). SUMMARY OF NRC; 00170: CORROSION LEVEL #2 ON STRINGER 25R BTW. FS319.70 AND FS349 AT MAIN AVION - [SDR REXA2019102471495](https://openairdocs.org/sdr/REXA2019102471495.md): Stringer · corroded · Oct 17, 2019 · N929XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > INITIAL INSPECTION: CORROSION ON STRINGER 25R BTW. FS280 AND FS333 ALSO HYDRAULIC LINES STANDOFF (2E/A) AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIX A] SUMMARY: ON NRC. 00167 CORROSION LEVEL 2, STRINGER 25R BTW. FS280 AND FS333 AND - [SDR REXA2019102471480](https://openairdocs.org/sdr/REXA2019102471480.md): Coaming · cracked · Oct 17, 2019 · N929XJ · Cndair CL6002D24 · Nacelle/Pylon, Main Frame > INITIAL INSPECTION: CRACKED COAMING LATCH DOOR AND AFT CHANNEL ON LOWER HALF TRANSCOWL RH ENGINE ( MOT 2). SUMMARY: ON NRC. 00041, COAMING LATCH DOOR AND AFT CHANNEL ON LOWER HALF TRANSCOWL RH ENGINE WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SR - [SDR REXA2019102451516](https://openairdocs.org/sdr/REXA2019102451516.md): Floor Support · corroded · Oct 15, 2019 · N929XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > INITIAL INSPECTION: CORROSION ON FLOOR BEAM 27LBL FROM FS1000 TO FS1047 AT AFT BAGGAGE BAY. (CCT) (TCI: 53-30-306). SUMMARY: DUE CORROSION LEVEL 2 ON FLOOR BEAM LBL27 STA FS 1000 TO FS 1047 AT AFT CARGO COMPARTMENT WAS REPAIRED PER CRJ/900 SRM 53-00-41-201 - [SDR REXA2019102451509](https://openairdocs.org/sdr/REXA2019102451509.md): Doubler · corroded · Oct 15, 2019 · N929XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin > HIDDEN DAMAGE IN REF. JOBCARD 900-34-900-702. CORROSION ON DOUBLE IN SETTLEMENT AREA OF TRANSMIT ANTENNA 2 E19. (SM) (FUS). SUMMARY: DOUBLES (SPACER) WAS FABRICATED PER E/A CRJ 953-09832 REV IR. AND WAS INSTALLED PER CRJ 900 SRM 51-42-06-001-001-A01. - [SDR REXA2019102451501](https://openairdocs.org/sdr/REXA2019102451501.md): Stringer · corroded · Oct 15, 2019 · N929XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > INITIAL INSPECTION: CORROSION ON STRINGER 26L BTW FS333 AND FS349 AT MAIN AVIONICS COMPARTMENT [ IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E)(TCI). SUMMARY: STRINGER 26LH FROM FS 333-364 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-0 - [SDR REXA2019102451494](https://openairdocs.org/sdr/REXA2019102451494.md): Frame · corroded · Oct 15, 2019 · N929XJ · Cndair CL6002D24 · Fuselage Main, Frame > INITIAL INSPECTION: CORROSION ON FRAME FS295 BTW. STGR.26L AND 26R AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E)(TCI 100-09). SUMMARY:ON NRC. 00163 CORROSION LEVEL 1 ON FRAME FS295 BTW. STGR.26L AND 26R AT MAIN AVIONICS CO - [SDR REXA2019102451493](https://openairdocs.org/sdr/REXA2019102451493.md): Stringer · corroded · Oct 15, 2019 · N929XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > INITIAL INSPECTION: CORROSION ON STRINGER 26R BTW FS280 AND FS364 AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E)(TCI 100-09). SUMMARY: STRINGER 26R BTW FS280 AND FS364 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM - [SDR REXA2019102451492](https://openairdocs.org/sdr/REXA2019102451492.md): Stringer · corroded · Oct 15, 2019 · N929XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > INITIAL INSPECTION: CORROSION ON STRINGER 27 BTW.FS280 AND FS310 AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E) (TCI 100-09). SUMMARY: ON NRC. 00160 CORROSION LEVEL 2, STRINGER 27 BTW.FS280 AND FS310 AT MAIN AVIONICS COMPARTM - [SDR REXA2019102451483](https://openairdocs.org/sdr/REXA2019102451483.md): Striker · worn · Oct 15, 2019 · N929XJ · Cndair CL6002D24 · Cargo/Baggage Doors > INITIAL INSPECTION: WEAR FWD STRIKER SEAL AT CENTER BAGGAGE BAY DOOR SURROUND STRUCTURE (C1) (SM). SUMMARY: FWD STRIKER SEAL AT CENTER BAGGAGE BAY DOOR SURROUND STRUCTURE NO DAMAGE ALLOWED PER CRJ-900 SRM 53-31-23-101-001-A02. DAMAGED FWD STRIKER SEAL AT CENT - [SDR REXA201910241508](https://openairdocs.org/sdr/REXA201910241508.md): Floor Support · corroded · Oct 14, 2019 · N929XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > AWR: CORROSION ON FLOOR SUPPORTS BTW FS310 TO FS349 AT PAX CABIN FLOOR STRUCTURE, PASSENGER DOOR LOWER SILL. (CPAX). SUMMARY OF NRC 00233: FLOOR SUPPORTS BTW FS310 TO FS349 AT PAX CABIN FLOOR STRUCTURE, PASSENGER DOOR LOWER SILL WERE REPLACED PER CRJ-900 SRM - [SDR REXA2019102401500](https://openairdocs.org/sdr/REXA2019102401500.md): Stringer Splice · corroded · Oct 14, 2019 · N929XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > INITIAL INSPECTION: CORROSION ON SPLICE STA FS333 OF STRINGERS (3 E/A) STGR. 26L, 26R, AND 25R AT MAIN AVIONICS COMPARTMENT[IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E)(TCI 100-09). SUMMARY: SPLICE STA FS333 OF STRINGERS (3 E/A) STGR. 26L, 26R, AND 25R - [SDR REXA2019102431499](https://openairdocs.org/sdr/REXA2019102431499.md): Frame · corroded · Oct 13, 2019 · N929XJ · Cndair CL6002D24 · Fuselage Main, Frame > INITIAL INSPECTION: CORROSION ON FRAME FS319.70 BTW STGR 26L AND 26R AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E)(TCI 100-09). SUMMARY OF NRC 00172: CORROSION LEVEL-1 ON FRAME FS319.70 BTW STGR 26L AND 26R AT MAIN AVIONI - [SDR REXA2019101301498](https://openairdocs.org/sdr/REXA2019101301498.md): Frame · corroded · Oct 13, 2019 · N929XJ · Cndair CL6002D24 · Fuselage Main, Frame > INITIAL INSPECTION: CORROSION ON FRAME FS333 BTW. STGR 26L AND 25R AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIXA]. (E/E)(TCI 100-09). SUMMARY: CORROSION LEVEL 1 ON FRAME FS333 BTW. STGR 26L AND 25R AT MAIN AVIONICS COMPARTMENT WAS R - [SDR REXA2019102431496](https://openairdocs.org/sdr/REXA2019102431496.md): Frame · corroded · Oct 13, 2019 · N929XJ · Cndair CL6002D24 · Fuselage Main, Frame > INITIAL INSPECTION: CORROSION ON FRAME FS310 BTW. STGR.26L AND 25R AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIXA].(E/E)(TCI 100-09). CORROSION LEVEL 1 ON FRAME FS310 BTW. STGR.26L AND 25R AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER - [SDR REXA2019102431488](https://openairdocs.org/sdr/REXA2019102431488.md): Support Angle · corroded · Oct 13, 2019 · N929XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > INITIAL INSPECTION: CORROSION ON FLOOR SETTLEMENT (141ALF) AT MAIN AVIONICS COMPARTMENT FS280 BTW. STGR 25L AND 25R.(E/E)(100-09). SUMMARY: DAMAGED ANGLE SUPPORT, CRAWLWAY FLOOR ON FS=280.00 BTW STGR 25L AND 25R AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTM - [SDR REXA2019102411506](https://openairdocs.org/sdr/REXA2019102411506.md): Door Frame · corroded · Oct 11, 2019 · N929XJ · Cndair CL6002D24 · Fuselage Main, Structure > INITIAL INSPECTION: CORROSION ON MOUNTING ANGLE OF SERVICE DOOR SURROUND STRUCTURE LOWER SILL.(PTAS)(TCI 53-20-219). SUMMARY: ON NRC: 00218 CORROSION LEVEL 2, MOUNTING ANGLE OF SERVICE DOOR SURROUND STRUCTURE LOWER SILL WAS REPLACED PER CRJ-900 SRM 51-42-06-0 - [SDR REXA2019102411505](https://openairdocs.org/sdr/REXA2019102411505.md): Scuff Plate · corroded · Oct 11, 2019 · N929XJ · Cndair CL6002D24 · Service Doors > INITIAL INSPECTION: CORROSION ON SCUFF PLATE SUPPORTS AND ANGLES AT GALLEY SERVICE DOOR LOWER SURROUND STRUCTURE. (PTAS)(TCI:53-20-219). SUMMARY: ON NRC. 00215 CORROSION LEVEL 2 SCUFF PLATE SUPPORTS AND ANGLES AT GALLEY SERVICE DOOR LOWER SURROUND STRUCTURE W - [SDR REXA2019102411502](https://openairdocs.org/sdr/REXA2019102411502.md): Frame · corroded · Oct 11, 2019 · N929XJ · Cndair CL6002D24 · Fuselage Main, Frame > INITIAL INSPECTION: CORROSION ON FRAME FS349 BTW. STGR. 26L AND 25R AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E)(TCI 100-09). SUMMARY: ON NRC. 00175, CORROSION LEVEL 1, FRAME FS349 BTW. STGR. 26L AND 25R AT MAIN AVIONICS CO - [SDR REXA2019102411510](https://openairdocs.org/sdr/REXA2019102411510.md): Floor Support · corroded · Oct 10, 2019 · N929XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > INITIAL INSPECTION: CORROSION ON FLOOR SUPPORT AT FUSELAGE STRUCTURE BTW FS 565 / FS 581 AND STGR 22L/23L (C1). SUMMARY OF NRC 00257 CORROSION LEVEL 2: FLOOR SUPPORT AT FUSELAGE STRUCTURE BTW FS 565 / FS 581 AND STGR 22L/23L WAS REPLACED PER CRJ 900 SRM 51-4 - [SDR REXA2019102491522](https://openairdocs.org/sdr/REXA2019102491522.md): Floorbeam · cracked · Oct 9, 2019 · N929XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam > AWR HIDDEN DAMAGE: DURING REMOVAL FLOOR BEAM FS=280, ANGLE WAS FOUND CRACKED AT STA FS280 LBL26 PAX CABIN (CPAX) (IN REF. NRC 00264) SUMMARY: ON NRC. 00393, ANGLE AT STA FS280 LBL26 PAX CABIN WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-13 - [SDR REXA2019102491521](https://openairdocs.org/sdr/REXA2019102491521.md): Floorbeam · cracked · Oct 9, 2019 · N929XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam > AWR HIDDEN DAMAGE: DURING REMOVAL FLOOR BEAM 280, ANGLE WAS FOUND CRACKED AT STA FS280 RBL26 PAX CABIN (CPAX) (IN REF. NRC 00263) SUMMARY: ON NRC. 00392, ANGLE AT STA FS280 RBL26 PAX CABIN WAS REPLACED PER CRJ-900 SRM 51-42-06-001 AND SRM 51-42-13-001-001-A01 - [SDR REXA2019102491513](https://openairdocs.org/sdr/REXA2019102491513.md): Floorbeam · corroded · Oct 9, 2019 · N929XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam > AWR HIDDEN DISCREPANCY: AFTER FLOOR PANEL SUPPORT ANGLE REMOVAL CORROSION WAS FOUND ON FLOOR BEAM STA 280 BTW BL0.00 AND LBL 11 AT PAX CABIN (W1) IN REF NRC S/N 00159. SUMMARY: ON NRC. 00264 CORROSION LEVEL 2, CROSSBEAM AT FS 280.00 BTW BL 0 TO LBL 42 WAS REP - [SDR REXA2019102491512](https://openairdocs.org/sdr/REXA2019102491512.md): Floorbeam · corroded · Oct 9, 2019 · N929XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam > AWR HIDDEN DISCREPANCY: AFTER FLOOR PANEL SUPPORT ANGLE REMOVAL CORROSION WAS FOUND ON FLOOR BEAM STA 280 BTW BL0.00 AND RBL 11 AT PAX CABIN (W1) IN REF NRC S/N 00159. SUMMARY: ON NRC. 00263, CORROSION LEVEL 2, CROSSBEAM AT FS 280.00 BTW BL 0 TO RBL 42 WAS RE - [SDR REXA2019102491484](https://openairdocs.org/sdr/REXA2019102491484.md): Intercostal · corroded · Oct 9, 2019 · N929XJ · Cndair CL6002D24 · Passenger/Crew Doors > INITIAL INSPECTION: CORROSION ON INTERCOSTAL DD6 BTW FORMER FS 338.9 AND FRAME FS 327.7 INSIDE STRUCTURE AT PASSENGER DOOR. (PTAS)(TSI: 52-10-301). SUMMARY: INTERCOSTAL DD6 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 PAR. 6. (C) AND SRM 51-42-21-001-001 - [SDR REXA2019102491481](https://openairdocs.org/sdr/REXA2019102491481.md): Strap · corroded · Oct 9, 2019 · N929XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > INITIAL INSPECTION: CORROSION ON SETTLEMENT AREA AT PANEL ACCESS 193AB AND 195AB (SM). SUMMARY: ON NRC. 00110, ON SETTLEMENT AREA AT PANEL ACCESS 193AB AND 195AB, STRAPS WERE REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01 PAR. 8 - [SDR REXA2019102481519](https://openairdocs.org/sdr/REXA2019102481519.md): Canister · cracked · Oct 8, 2019 · N929XJ · Cndair CL6002D24 · Fuel Storage > INITIAL INSPECTION: CRACK IN CANISTER, WELDED NO.3 IN STA. WS148 AT LH MAIN FUEL TANK. (AI) SUMMARY: ON NRC. 00303 CANISTER, WELDED NO.3 IN STA. WS148 AT LH MAIN FUEL TANK WAS REPAIRED PER CRJ-900 REO 670-57-42-577 REV. - [SDR REXA2019102481518](https://openairdocs.org/sdr/REXA2019102481518.md): Stringer Splice · corroded · Oct 8, 2019 · N929XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > INITIAL INSPECTION: CORROSION ON STGR SPLICE 22 RH AND FS=333 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (SM) (TCI 53-20-319). SUMMARY: ON NRC. 00289 CORROSION LEVEL 2, STGR SPLICE 22 RH AND FS=333 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT Next page: https://openairdocs.org/aircraft/N929XJ/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 = 'N929XJ' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N929XJ/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.